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Harijono Djojodihardjo | Institut Teknologi Bandung - Academia.edu

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ds-divider-16" style="margin: 0px;"></div><div class="documents-container backbone-social-profile-documents" style="width: 100%;"><div class="u-taCenter"></div><div class="profile--tab_content_container js-tab-pane tab-pane active" id="all"><div class="profile--tab_heading_container js-section-heading" data-section="Papers" id="Papers"><h3 class="profile--tab_heading_container">Papers by Harijono Djojodihardjo</h3></div><div class="js-work-strip profile--work_container" data-work-id="122305159"><div class="profile--work_thumbnail hidden-xs"><a class="js-work-strip-work-link" data-click-track="profile-work-strip-thumbnail" href="https://www.academia.edu/122305159/Indonesian_Remote_Sensing_for_Forestry_Management_Challenges_and_Approaches"><img alt="Research paper thumbnail of Indonesian Remote Sensing for Forestry Management: Challenges and Approaches" class="work-thumbnail" src="https://a.academia-assets.com/images/blank-paper.jpg" /></a></div><div class="wp-workCard wp-workCard_itemContainer"><div class="wp-workCard_item wp-workCard--title"><a class="js-work-strip-work-link text-gray-darker" data-click-track="profile-work-strip-title" href="https://www.academia.edu/122305159/Indonesian_Remote_Sensing_for_Forestry_Management_Challenges_and_Approaches">Indonesian Remote Sensing for Forestry Management: Challenges and Approaches</a></div><div class="wp-workCard_item"><span>United Nations Programme on Space Applications</span><span>, 2000</span></div><div class="wp-workCard_item wp-workCard--actions"><span class="work-strip-bookmark-button-container"></span><span class="wp-workCard--action visible-if-viewed-by-owner inline-block" style="display: none;"><span class="js-profile-work-strip-edit-button-wrapper profile-work-strip-edit-button-wrapper" data-work-id="122305159"><a class="js-profile-work-strip-edit-button" tabindex="0"><span><i class="fa fa-pencil"></i></span><span>Edit</span></a></span></span><span 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alt="Research paper thumbnail of Vibro-acoustic analysis of the acoustic-structure interaction of flexible structure due to acoustic excitation" class="work-thumbnail" src="https://attachments.academia-assets.com/116998333/thumbnails/1.jpg" /></a></div><div class="wp-workCard wp-workCard_itemContainer"><div class="wp-workCard_item wp-workCard--title"><a class="js-work-strip-work-link text-gray-darker" data-click-track="profile-work-strip-title" href="https://www.academia.edu/122305158/Vibro_acoustic_analysis_of_the_acoustic_structure_interaction_of_flexible_structure_due_to_acoustic_excitation">Vibro-acoustic analysis of the acoustic-structure interaction of flexible structure due to acoustic excitation</a></div><div class="wp-workCard_item"><span>Acta Astronautica</span><span>, Mar 1, 2015</span></div><div class="wp-workCard_item wp-workCard--actions"><span class="work-strip-bookmark-button-container"></span><a id="42e5b8600091835479b39c99511952c6" class="wp-workCard--action" 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$(this).data('initialized', true); } }); $a.trackClickSource(".js-work-strip-work-link", "profile_work_strip") }); </script> <div class="js-work-strip profile--work_container" data-work-id="122305157"><div class="profile--work_thumbnail hidden-xs"><a class="js-work-strip-work-link" data-click-track="profile-work-strip-thumbnail" href="https://www.academia.edu/122305157/Numerical_boundary_element_computation_of_submerged_body_surface_wave_interaction"><img alt="Research paper thumbnail of Numerical boundary element computation of submerged body-surface wave interaction" class="work-thumbnail" src="https://a.academia-assets.com/images/blank-paper.jpg" /></a></div><div class="wp-workCard wp-workCard_itemContainer"><div class="wp-workCard_item wp-workCard--title"><a class="js-work-strip-work-link text-gray-darker" data-click-track="profile-work-strip-title" href="https://www.academia.edu/122305157/Numerical_boundary_element_computation_of_submerged_body_surface_wave_interaction">Numerical boundary element computation of submerged body-surface wave interaction</a></div><div class="wp-workCard_item"><span>The Proceedings of the ... International Offshore and Polar Engineering Conference</span><span>, 1993</span></div><div class="wp-workCard_item"><span class="js-work-more-abstract-truncated">A simple method to solve potential flow problems of submerged body-surface wave interaction is pr...</span><a class="js-work-more-abstract" data-broccoli-component="work_strip.more_abstract" data-click-track="profile-work-strip-more-abstract" href="javascript:;"><span> more </span><span><i class="fa fa-caret-down"></i></span></a><span class="js-work-more-abstract-untruncated hidden">A simple method to solve potential flow problems of submerged body-surface wave interaction is presented. The Laplace equation governs flow below the surface. The boundary condition on the body is of Neumann type, while on the free surface the nonlinear dynamic free surface condition has to be satisfied. In addition, the farfield and radiation condition, which determine the behaviour of waves going to infinity, have to be satisfied. Taking advantage of the potential flow model, Green Identity is then used to transform the problem of the Laplace equation with nonlinear boundary conation into a nonlinear problem in its boundary. To satisfy the nonlinear dynamic free surface condition, Newton iteration is employed. The scheme for relaxation is obtained by expanding the nonlinear dynamic free surface condition to obtain correction terms to the velocity potential. Truncation up to linear terms results in a simple scheme. Since the dynamic condition is valid on the unknown location of the free surface, in each iteration step the position of the free surface where the equation is applied, is corrected using the Bernoulli equation. In this manner, dynamic free surface condition is satisfied exactly at the collocation points. Results from two and three dimensional nonlifting problem are presented as examples.</span></div><div class="wp-workCard_item wp-workCard--actions"><span class="work-strip-bookmark-button-container"></span><span class="wp-workCard--action visible-if-viewed-by-owner inline-block" style="display: none;"><span class="js-profile-work-strip-edit-button-wrapper profile-work-strip-edit-button-wrapper" data-work-id="122305157"><a class="js-profile-work-strip-edit-button" tabindex="0"><span><i class="fa fa-pencil"></i></span><span>Edit</span></a></span></span><span id="work-strip-rankings-button-container"></span></div><div class="wp-workCard_item wp-workCard--stats"><span><span><span class="js-view-count view-count u-mr2x" data-work-id="122305157"><i class="fa fa-spinner fa-spin"></i></span><script>$(function () { var workId = 122305157; window.Academia.workViewCountsFetcher.queue(workId, function (count) { var description = window.$h.commaizeInt(count) + " " + window.$h.pluralize(count, 'View'); $(".js-view-count[data-work-id=122305157]").text(description); $(".js-view-count[data-work-id=122305157]").attr('title', description).tooltip(); }); });</script></span></span><span><span class="percentile-widget hidden"><span class="u-mr2x work-percentile"></span></span><script>$(function () { var workId = 122305157; window.Academia.workPercentilesFetcher.queue(workId, function (percentileText) { var container = $(".js-work-strip[data-work-id='122305157']"); container.find('.work-percentile').text(percentileText.charAt(0).toUpperCase() + percentileText.slice(1)); container.find('.percentile-widget').show(); container.find('.percentile-widget').removeClass('hidden'); }); });</script></span><span><script>$(function() { new Works.PaperRankView({ workId: 122305157, container: "", }); });</script></span></div><div id="work-strip-premium-row-container"></div></div></div><script> require.config({ waitSeconds: 90 })(["https://a.academia-assets.com/assets/wow_profile-f77ea15d77ce96025a6048a514272ad8becbad23c641fc2b3bd6e24ca6ff1932.js","https://a.academia-assets.com/assets/work_edit-ad038b8c047c1a8d4fa01b402d530ff93c45fee2137a149a4a5398bc8ad67560.js"], function() { // from javascript_helper.rb var dispatcherData = {} if (false){ window.WowProfile.dispatcher = window.WowProfile.dispatcher || _.clone(Backbone.Events); dispatcherData = { dispatcher: window.WowProfile.dispatcher, downloadLinkId: "-1" } } $('.js-work-strip[data-work-id=122305157]').each(function() { if (!$(this).data('initialized')) { new WowProfile.WorkStripView({ el: this, workJSON: {"id":122305157,"title":"Numerical boundary element computation of submerged body-surface wave interaction","translated_title":"","metadata":{"abstract":"A simple method to solve potential flow problems of submerged body-surface wave interaction is presented. 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Since the dynamic condition is valid on the unknown location of the free surface, in each iteration step the position of the free surface where the equation is applied, is corrected using the Bernoulli equation. In this manner, dynamic free surface condition is satisfied exactly at the collocation points. Results from two and three dimensional nonlifting problem are presented as examples.","publication_date":{"day":null,"month":null,"year":1993,"errors":{}},"publication_name":"The Proceedings of the ... International Offshore and Polar Engineering Conference"},"translated_abstract":"A simple method to solve potential flow problems of submerged body-surface wave interaction is presented. The Laplace equation governs flow below the surface. The boundary condition on the body is of Neumann type, while on the free surface the nonlinear dynamic free surface condition has to be satisfied. 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$(this).data('initialized', true); } }); $a.trackClickSource(".js-work-strip-work-link", "profile_work_strip") }); </script> <div class="js-work-strip profile--work_container" data-work-id="122305152"><div class="profile--work_thumbnail hidden-xs"><a class="js-work-strip-work-link" data-click-track="profile-work-strip-thumbnail" href="https://www.academia.edu/122305152/Buffeting_Problems_Modelling_by_Use_of_Lifting_Surface_Methods_in_Unsteady_Aerodynamics_with_Separation"><img alt="Research paper thumbnail of Buffeting Problems Modelling by Use of Lifting Surface Methods in Unsteady Aerodynamics with Separation" class="work-thumbnail" src="https://a.academia-assets.com/images/blank-paper.jpg" /></a></div><div class="wp-workCard wp-workCard_itemContainer"><div class="wp-workCard_item wp-workCard--title"><a class="js-work-strip-work-link text-gray-darker" data-click-track="profile-work-strip-title" href="https://www.academia.edu/122305152/Buffeting_Problems_Modelling_by_Use_of_Lifting_Surface_Methods_in_Unsteady_Aerodynamics_with_Separation">Buffeting Problems Modelling by Use of Lifting Surface Methods in Unsteady Aerodynamics with Separation</a></div><div class="wp-workCard_item"><span class="js-work-more-abstract-truncated">The analytical approach to buffeting problem in subsonic flow is a challenging one and has been g...</span><a class="js-work-more-abstract" data-broccoli-component="work_strip.more_abstract" data-click-track="profile-work-strip-more-abstract" href="javascript:;"><span> more </span><span><i class="fa fa-caret-down"></i></span></a><span class="js-work-more-abstract-untruncated hidden">The analytical approach to buffeting problem in subsonic flow is a challenging one and has been given attention by many researchers; no purely analytical approach has been satisfactorily capable of simulating the phenomenon. An attempt to develop a computational method for the calculation of the aerodynamic load for separated subsonic flow using kernel function technique in linearized aerodynamics has been made by the author and his associates, as an alternative to the more accurate but elaborate technique of direct numerical attack to the viscous flow problem. Two approaches were then made. First, to treat the buffeting problem as a stability one by solving the flutter equation. Second, treating buffeting problem using dynamic response approach. Comparison of the unsteady load calculation method with other existing results for non-separated flow cases indicated good agreements. For separated flow case, no other methods are available for comparison. However, flutter solution approach made by the present study indicated that the presence of the separation bubble tends to destabilize the system compared to the attached flow case. The analytical approach to the buffeting problem using dynamic response technique was made by assuming that there is no coupling between the motion induced unsteady loads and the independent-motion unsteady loads. The motion induced unsteady airloads is calculated using the present method while the buffeting excitation load was based on experimental data. Computational results for the bending moment of a wing experiencing buffeting with experimental results indicated good agreement but lower values for the onset of buffeting.</span></div><div class="wp-workCard_item wp-workCard--actions"><span class="work-strip-bookmark-button-container"></span><span class="wp-workCard--action visible-if-viewed-by-owner inline-block" style="display: none;"><span class="js-profile-work-strip-edit-button-wrapper profile-work-strip-edit-button-wrapper" data-work-id="122305152"><a class="js-profile-work-strip-edit-button" tabindex="0"><span><i class="fa fa-pencil"></i></span><span>Edit</span></a></span></span><span id="work-strip-rankings-button-container"></span></div><div class="wp-workCard_item wp-workCard--stats"><span><span><span class="js-view-count view-count u-mr2x" data-work-id="122305152"><i class="fa fa-spinner fa-spin"></i></span><script>$(function () { var workId = 122305152; window.Academia.workViewCountsFetcher.queue(workId, function (count) { var description = window.$h.commaizeInt(count) + " " + window.$h.pluralize(count, 'View'); $(".js-view-count[data-work-id=122305152]").text(description); $(".js-view-count[data-work-id=122305152]").attr('title', description).tooltip(); }); });</script></span></span><span><span class="percentile-widget hidden"><span class="u-mr2x work-percentile"></span></span><script>$(function () { var workId = 122305152; window.Academia.workPercentilesFetcher.queue(workId, function (percentileText) { var container = $(".js-work-strip[data-work-id='122305152']"); container.find('.work-percentile').text(percentileText.charAt(0).toUpperCase() + percentileText.slice(1)); container.find('.percentile-widget').show(); container.find('.percentile-widget').removeClass('hidden'); }); });</script></span><span><script>$(function() { new Works.PaperRankView({ workId: 122305152, container: "", }); });</script></span></div><div id="work-strip-premium-row-container"></div></div></div><script> require.config({ waitSeconds: 90 })(["https://a.academia-assets.com/assets/wow_profile-f77ea15d77ce96025a6048a514272ad8becbad23c641fc2b3bd6e24ca6ff1932.js","https://a.academia-assets.com/assets/work_edit-ad038b8c047c1a8d4fa01b402d530ff93c45fee2137a149a4a5398bc8ad67560.js"], function() { // from javascript_helper.rb var dispatcherData = {} if (false){ window.WowProfile.dispatcher = window.WowProfile.dispatcher || _.clone(Backbone.Events); dispatcherData = { dispatcher: window.WowProfile.dispatcher, downloadLinkId: "-1" } } $('.js-work-strip[data-work-id=122305152]').each(function() { if (!$(this).data('initialized')) { new WowProfile.WorkStripView({ el: this, workJSON: {"id":122305152,"title":"Buffeting Problems Modelling by Use of Lifting Surface Methods in Unsteady Aerodynamics with Separation","translated_title":"","metadata":{"abstract":"The analytical approach to buffeting problem in subsonic flow is a challenging one and has been given attention by many researchers; no purely analytical approach has been satisfactorily capable of simulating the phenomenon. 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An attempt to develop a computational method for the calculation of the aerodynamic load for separated subsonic flow using kernel function technique in linearized aerodynamics has been made by the author and his associates, as an alternative to the more accurate but elaborate technique of direct numerical attack to the viscous flow problem. Two approaches were then made. First, to treat the buffeting problem as a stability one by solving the flutter equation. Second, treating buffeting problem using dynamic response approach. Comparison of the unsteady load calculation method with other existing results for non-separated flow cases indicated good agreements. For separated flow case, no other methods are available for comparison. However, flutter solution approach made by the present study indicated that the presence of the separation bubble tends to destabilize the system compared to the attached flow case. The analytical approach to the buffeting problem using dynamic response technique was made by assuming that there is no coupling between the motion induced unsteady loads and the independent-motion unsteady loads. The motion induced unsteady airloads is calculated using the present method while the buffeting excitation load was based on experimental data. Computational results for the bending moment of a wing experiencing buffeting with experimental results indicated good agreement but lower values for the onset of buffeting.","internal_url":"https://www.academia.edu/122305152/Buffeting_Problems_Modelling_by_Use_of_Lifting_Surface_Methods_in_Unsteady_Aerodynamics_with_Separation","translated_internal_url":"","created_at":"2024-07-23T22:14:44.994-07:00","preview_url":null,"current_user_can_edit":null,"current_user_is_owner":null,"owner_id":4040157,"coauthors_can_edit":true,"document_type":"paper","co_author_tags":[],"downloadable_attachments":[],"slug":"Buffeting_Problems_Modelling_by_Use_of_Lifting_Surface_Methods_in_Unsteady_Aerodynamics_with_Separation","translated_slug":"","page_count":null,"language":"en","content_type":"Work","owner":{"id":4040157,"first_name":"Harijono","middle_initials":"","last_name":"Djojodihardjo","page_name":"HarijonoDjojodihardjo","domain_name":"itb","created_at":"2013-05-03T11:27:42.148-07:00","display_name":"Harijono Djojodihardjo","url":"https://itb.academia.edu/HarijonoDjojodihardjo"},"attachments":[],"research_interests":[{"id":422,"name":"Computer Science","url":"https://www.academia.edu/Documents/in/Computer_Science"},{"id":10875,"name":"Aerodynamics","url":"https://www.academia.edu/Documents/in/Aerodynamics"},{"id":36296,"name":"Aeroelasticity","url":"https://www.academia.edu/Documents/in/Aeroelasticity"},{"id":309117,"name":"Flutter","url":"https://www.academia.edu/Documents/in/Flutter"}],"urls":[{"id":43662299,"url":"https://doi.org/10.1007/978-94-011-5157-3_3"}]}, dispatcherData: dispatcherData }); 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Of particular importance is the utilization and development of earth observation capabilities for environmental natural resources imperatives to this end is quite significant. On one hand there may appear challenges to achieve unique and high quality requirements on many of the elements of social and economic progress, i.e.</span></div><div class="wp-workCard_item wp-workCard--actions"><span class="work-strip-bookmark-button-container"></span><span class="wp-workCard--action visible-if-viewed-by-owner inline-block" style="display: none;"><span class="js-profile-work-strip-edit-button-wrapper profile-work-strip-edit-button-wrapper" data-work-id="122305150"><a class="js-profile-work-strip-edit-button" tabindex="0"><span><i class="fa fa-pencil"></i></span><span>Edit</span></a></span></span><span id="work-strip-rankings-button-container"></span></div><div class="wp-workCard_item wp-workCard--stats"><span><span><span class="js-view-count view-count u-mr2x" data-work-id="122305150"><i class="fa fa-spinner fa-spin"></i></span><script>$(function () { var workId = 122305150; window.Academia.workViewCountsFetcher.queue(workId, function (count) { var description = window.$h.commaizeInt(count) + " " + window.$h.pluralize(count, 'View'); $(".js-view-count[data-work-id=122305150]").text(description); $(".js-view-count[data-work-id=122305150]").attr('title', description).tooltip(); }); });</script></span></span><span><span class="percentile-widget hidden"><span class="u-mr2x work-percentile"></span></span><script>$(function () { var workId = 122305150; window.Academia.workPercentilesFetcher.queue(workId, function (percentileText) { var container = $(".js-work-strip[data-work-id='122305150']"); container.find('.work-percentile').text(percentileText.charAt(0).toUpperCase() + percentileText.slice(1)); container.find('.percentile-widget').show(); container.find('.percentile-widget').removeClass('hidden'); }); });</script></span><span><script>$(function() { new Works.PaperRankView({ workId: 122305150, container: "", }); });</script></span></div><div id="work-strip-premium-row-container"></div></div></div><script> require.config({ waitSeconds: 90 })(["https://a.academia-assets.com/assets/wow_profile-f77ea15d77ce96025a6048a514272ad8becbad23c641fc2b3bd6e24ca6ff1932.js","https://a.academia-assets.com/assets/work_edit-ad038b8c047c1a8d4fa01b402d530ff93c45fee2137a149a4a5398bc8ad67560.js"], function() { // from javascript_helper.rb var dispatcherData = {} if (false){ window.WowProfile.dispatcher = window.WowProfile.dispatcher || _.clone(Backbone.Events); dispatcherData = { dispatcher: window.WowProfile.dispatcher, downloadLinkId: "-1" } } $('.js-work-strip[data-work-id=122305150]').each(function() { if (!$(this).data('initialized')) { new WowProfile.WorkStripView({ el: this, workJSON: {"id":122305150,"title":"Comprehensive Study on Small and Low Cost Satellite Technology for Earth Observation with Case Study for Indonesia: Projection for 2002-2022","translated_title":"","metadata":{"abstract":"and economic progress, while facing global competitiveness locally as opportunities and challenges. 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$(this).data('initialized', true); } }); $a.trackClickSource(".js-work-strip-work-link", "profile_work_strip") }); </script> <div class="js-work-strip profile--work_container" data-work-id="122305147"><div class="profile--work_thumbnail hidden-xs"><a class="js-work-strip-work-link" data-click-track="profile-work-strip-thumbnail" href="https://www.academia.edu/122305147/Locally_Linearized_Solution_of_Lifting_Transonic_Flow_by_Method_of_Parametric_Differentiation"><img alt="Research paper thumbnail of Locally Linearized Solution of Lifting Transonic Flow by Method of Parametric Differentiation" class="work-thumbnail" src="https://a.academia-assets.com/images/blank-paper.jpg" /></a></div><div class="wp-workCard wp-workCard_itemContainer"><div class="wp-workCard_item wp-workCard--title"><a class="js-work-strip-work-link text-gray-darker" data-click-track="profile-work-strip-title" href="https://www.academia.edu/122305147/Locally_Linearized_Solution_of_Lifting_Transonic_Flow_by_Method_of_Parametric_Differentiation">Locally Linearized Solution of Lifting Transonic Flow by Method of Parametric Differentiation</a></div><div class="wp-workCard_item"><span>DOAJ (DOAJ: Directory of Open Access Journals)</span><span>, Feb 1, 2019</span></div><div class="wp-workCard_item"><span class="js-work-more-abstract-truncated">The governing equation of transonic small disturbance flow present a non-linear partial different...</span><a class="js-work-more-abstract" data-broccoli-component="work_strip.more_abstract" data-click-track="profile-work-strip-more-abstract" href="javascript:;"><span> more </span><span><i class="fa fa-caret-down"></i></span></a><span class="js-work-more-abstract-untruncated hidden">The governing equation of transonic small disturbance flow present a non-linear partial differential equation which is difficult to solve. The method of parametric differentiation reduces the non-linear partial differential equation of transonic flow into an ordinary differential equation with variable coefficient, which is generally much simple to solve. Further simplification is introduced, as also done in the method of local linearization, by assuming (1-M 1 2 ) to vary sufficiently slowly, so that in some part of the analysis its derivatives with respect to x can be disregarded. Based upon these methods, the lifting transonic flow was analyzed. For the subsonic and supersonic parts, closed form solutions were obtained. For the case M 1  ≈ 1, the method yields an integral equation, which can be solved by an iterative scheme starting from the non-lifting solution.</span></div><div class="wp-workCard_item wp-workCard--actions"><span class="work-strip-bookmark-button-container"></span><span class="wp-workCard--action visible-if-viewed-by-owner inline-block" style="display: none;"><span class="js-profile-work-strip-edit-button-wrapper profile-work-strip-edit-button-wrapper" data-work-id="122305147"><a class="js-profile-work-strip-edit-button" tabindex="0"><span><i class="fa fa-pencil"></i></span><span>Edit</span></a></span></span><span id="work-strip-rankings-button-container"></span></div><div class="wp-workCard_item wp-workCard--stats"><span><span><span class="js-view-count view-count u-mr2x" data-work-id="122305147"><i class="fa fa-spinner fa-spin"></i></span><script>$(function () { var workId = 122305147; window.Academia.workViewCountsFetcher.queue(workId, function (count) { var description = window.$h.commaizeInt(count) + " " + window.$h.pluralize(count, 'View'); $(".js-view-count[data-work-id=122305147]").text(description); $(".js-view-count[data-work-id=122305147]").attr('title', description).tooltip(); }); });</script></span></span><span><span class="percentile-widget hidden"><span class="u-mr2x work-percentile"></span></span><script>$(function () { var workId = 122305147; window.Academia.workPercentilesFetcher.queue(workId, function (percentileText) { var container = $(".js-work-strip[data-work-id='122305147']"); container.find('.work-percentile').text(percentileText.charAt(0).toUpperCase() + percentileText.slice(1)); container.find('.percentile-widget').show(); container.find('.percentile-widget').removeClass('hidden'); }); });</script></span><span><script>$(function() { new Works.PaperRankView({ workId: 122305147, container: "", }); });</script></span></div><div id="work-strip-premium-row-container"></div></div></div><script> require.config({ waitSeconds: 90 })(["https://a.academia-assets.com/assets/wow_profile-f77ea15d77ce96025a6048a514272ad8becbad23c641fc2b3bd6e24ca6ff1932.js","https://a.academia-assets.com/assets/work_edit-ad038b8c047c1a8d4fa01b402d530ff93c45fee2137a149a4a5398bc8ad67560.js"], function() { // from javascript_helper.rb var dispatcherData = {} if (false){ window.WowProfile.dispatcher = window.WowProfile.dispatcher || _.clone(Backbone.Events); dispatcherData = { dispatcher: window.WowProfile.dispatcher, downloadLinkId: "-1" } } $('.js-work-strip[data-work-id=122305147]').each(function() { if (!$(this).data('initialized')) { new WowProfile.WorkStripView({ el: this, workJSON: {"id":122305147,"title":"Locally Linearized Solution of Lifting Transonic Flow by Method of Parametric Differentiation","translated_title":"","metadata":{"abstract":"The governing equation of transonic small disturbance flow present a non-linear partial differential equation which is difficult to solve. The method of parametric differentiation reduces the non-linear partial differential equation of transonic flow into an ordinary differential equation with variable coefficient, which is generally much simple to solve. Further simplification is introduced, as also done in the method of local linearization, by assuming (1-M 1 2 ) to vary sufficiently slowly, so that in some part of the analysis its derivatives with respect to x can be disregarded. Based upon these methods, the lifting transonic flow was analyzed. For the subsonic and supersonic parts, closed form solutions were obtained. For the case M 1  ≈ 1, the method yields an integral equation, which can be solved by an iterative scheme starting from the non-lifting solution.","publisher":"DOAJ: Directory of Open Access Journals","publication_date":{"day":1,"month":2,"year":2019,"errors":{}},"publication_name":"DOAJ (DOAJ: Directory of Open Access Journals)"},"translated_abstract":"The governing equation of transonic small disturbance flow present a non-linear partial differential equation which is difficult to solve. The method of parametric differentiation reduces the non-linear partial differential equation of transonic flow into an ordinary differential equation with variable coefficient, which is generally much simple to solve. Further simplification is introduced, as also done in the method of local linearization, by assuming (1-M 1 2 ) to vary sufficiently slowly, so that in some part of the analysis its derivatives with respect to x can be disregarded. Based upon these methods, the lifting transonic flow was analyzed. For the subsonic and supersonic parts, closed form solutions were obtained. For the case M 1  ≈ 1, the method yields an integral equation, which can be solved by an iterative scheme starting from the non-lifting solution.","internal_url":"https://www.academia.edu/122305147/Locally_Linearized_Solution_of_Lifting_Transonic_Flow_by_Method_of_Parametric_Differentiation","translated_internal_url":"","created_at":"2024-07-23T22:14:42.931-07:00","preview_url":null,"current_user_can_edit":null,"current_user_is_owner":null,"owner_id":4040157,"coauthors_can_edit":true,"document_type":"paper","co_author_tags":[],"downloadable_attachments":[],"slug":"Locally_Linearized_Solution_of_Lifting_Transonic_Flow_by_Method_of_Parametric_Differentiation","translated_slug":"","page_count":null,"language":"en","content_type":"Work","owner":{"id":4040157,"first_name":"Harijono","middle_initials":"","last_name":"Djojodihardjo","page_name":"HarijonoDjojodihardjo","domain_name":"itb","created_at":"2013-05-03T11:27:42.148-07:00","display_name":"Harijono Djojodihardjo","url":"https://itb.academia.edu/HarijonoDjojodihardjo"},"attachments":[],"research_interests":[{"id":300,"name":"Mathematics","url":"https://www.academia.edu/Documents/in/Mathematics"},{"id":86034,"name":"Mathematical Analysis","url":"https://www.academia.edu/Documents/in/Mathematical_Analysis"},{"id":194130,"name":"PARTIAL DIFFERENTIAL EQUATION","url":"https://www.academia.edu/Documents/in/PARTIAL_DIFFERENTIAL_EQUATION"},{"id":349904,"name":"Linearization","url":"https://www.academia.edu/Documents/in/Linearization"},{"id":830168,"name":"Method of Characteristics","url":"https://www.academia.edu/Documents/in/Method_of_Characteristics"},{"id":1770555,"name":"Ordinary Differential Equation","url":"https://www.academia.edu/Documents/in/Ordinary_Differential_Equation"},{"id":2778229,"name":"Supersonic speed","url":"https://www.academia.edu/Documents/in/Supersonic_speed"}],"urls":[{"id":43662294,"url":"https://doaj.org/article/c4fa46d1665e4957a4ce242df4b8e88b"}]}, dispatcherData: dispatcherData }); $(this).data('initialized', true); } }); $a.trackClickSource(".js-work-strip-work-link", "profile_work_strip") }); </script> <div class="js-work-strip profile--work_container" data-work-id="122305146"><div class="profile--work_thumbnail hidden-xs"><a class="js-work-strip-work-link" data-click-track="profile-work-strip-thumbnail" href="https://www.academia.edu/122305146/Acoustic_Method_for_the_Suppression_of_Acoustic_and_Aerodynamically_Induced_Vibration_on_Structures"><img alt="Research paper thumbnail of Acoustic Method for the Suppression of Acoustic and Aerodynamically Induced Vibration on Structures" class="work-thumbnail" src="https://attachments.academia-assets.com/116998312/thumbnails/1.jpg" /></a></div><div class="wp-workCard wp-workCard_itemContainer"><div class="wp-workCard_item wp-workCard--title"><a class="js-work-strip-work-link text-gray-darker" data-click-track="profile-work-strip-title" href="https://www.academia.edu/122305146/Acoustic_Method_for_the_Suppression_of_Acoustic_and_Aerodynamically_Induced_Vibration_on_Structures">Acoustic Method for the Suppression of Acoustic and Aerodynamically Induced Vibration on Structures</a></div><div class="wp-workCard_item"><span>Advances in civil and industrial engineering book series</span><span>, 2017</span></div><div class="wp-workCard_item wp-workCard--actions"><span class="work-strip-bookmark-button-container"></span><a id="5ae2cb772427d9062f0de44d94280e1c" class="wp-workCard--action" rel="nofollow" data-click-track="profile-work-strip-download" data-download="{&quot;attachment_id&quot;:116998312,&quot;asset_id&quot;:122305146,&quot;asset_type&quot;:&quot;Work&quot;,&quot;button_location&quot;:&quot;profile&quot;}" href="https://www.academia.edu/attachments/116998312/download_file?st=MTczMzAzMTQwNiw4LjIyMi4yMDguMTQ2&s=profile"><span><i class="fa fa-arrow-down"></i></span><span>Download</span></a><span class="wp-workCard--action visible-if-viewed-by-owner inline-block" style="display: none;"><span class="js-profile-work-strip-edit-button-wrapper profile-work-strip-edit-button-wrapper" data-work-id="122305146"><a class="js-profile-work-strip-edit-button" tabindex="0"><span><i class="fa fa-pencil"></i></span><span>Edit</span></a></span></span><span id="work-strip-rankings-button-container"></span></div><div class="wp-workCard_item wp-workCard--stats"><span><span><span class="js-view-count view-count u-mr2x" data-work-id="122305146"><i class="fa fa-spinner fa-spin"></i></span><script>$(function () { var workId = 122305146; 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$(this).data('initialized', true); } }); $a.trackClickSource(".js-work-strip-work-link", "profile_work_strip") }); </script> <div class="js-work-strip profile--work_container" data-work-id="122305145"><div class="profile--work_thumbnail hidden-xs"><a class="js-work-strip-work-link" data-click-track="profile-work-strip-thumbnail" href="https://www.academia.edu/122305145/An_Expansion_Series_for_Solving_Improper_Cylindrical_Functions_Occurring_in_Subsonic_Supersonic_and_Transonic_Kernel_Formulations"><img alt="Research paper thumbnail of An Expansion Series for Solving Improper Cylindrical Functions Occurring in Subsonic, Supersonic and Transonic Kernel Formulations" class="work-thumbnail" src="https://a.academia-assets.com/images/blank-paper.jpg" /></a></div><div class="wp-workCard wp-workCard_itemContainer"><div class="wp-workCard_item wp-workCard--title"><a class="js-work-strip-work-link text-gray-darker" data-click-track="profile-work-strip-title" href="https://www.academia.edu/122305145/An_Expansion_Series_for_Solving_Improper_Cylindrical_Functions_Occurring_in_Subsonic_Supersonic_and_Transonic_Kernel_Formulations">An Expansion Series for Solving Improper Cylindrical Functions Occurring in Subsonic, Supersonic and Transonic Kernel Formulations</a></div><div class="wp-workCard_item"><span>Springer eBooks</span><span>, 1995</span></div><div class="wp-workCard_item"><span class="js-work-more-abstract-truncated">A brief survey of the kernel functions occurring in unsteady subsonic or supersonic lifting surfa...</span><a class="js-work-more-abstract" data-broccoli-component="work_strip.more_abstract" data-click-track="profile-work-strip-more-abstract" href="javascript:;"><span> more </span><span><i class="fa fa-caret-down"></i></span></a><span class="js-work-more-abstract-untruncated hidden">A brief survey of the kernel functions occurring in unsteady subsonic or supersonic lifting surface formulations is presented. The discussion will be focused on the solutions of the improper cylindrical function as a main part of the kernel function. A new expansion series is proposed as an exact solution to the improper integral and may be regarded as an extension of the Ueda series. The new solution offers a very simple and convenient form since the singular and regular parts are explicitly separated. The simple form of the singular functions is a key point which is particularly significant in simplifying the Mangler integration; hence this approach is shown to be useful in improving the accuracy of many planar and nonplanar lifting surface methods. Results are discussed and their accuracy is presented.</span></div><div class="wp-workCard_item wp-workCard--actions"><span class="work-strip-bookmark-button-container"></span><span class="wp-workCard--action visible-if-viewed-by-owner inline-block" style="display: none;"><span class="js-profile-work-strip-edit-button-wrapper profile-work-strip-edit-button-wrapper" data-work-id="122305145"><a class="js-profile-work-strip-edit-button" tabindex="0"><span><i class="fa fa-pencil"></i></span><span>Edit</span></a></span></span><span id="work-strip-rankings-button-container"></span></div><div class="wp-workCard_item wp-workCard--stats"><span><span><span class="js-view-count view-count u-mr2x" data-work-id="122305145"><i class="fa fa-spinner fa-spin"></i></span><script>$(function () { var workId = 122305145; window.Academia.workViewCountsFetcher.queue(workId, function (count) { var description = window.$h.commaizeInt(count) + " " + window.$h.pluralize(count, 'View'); $(".js-view-count[data-work-id=122305145]").text(description); $(".js-view-count[data-work-id=122305145]").attr('title', description).tooltip(); }); });</script></span></span><span><span class="percentile-widget hidden"><span class="u-mr2x work-percentile"></span></span><script>$(function () { var workId = 122305145; window.Academia.workPercentilesFetcher.queue(workId, function (percentileText) { var container = $(".js-work-strip[data-work-id='122305145']"); container.find('.work-percentile').text(percentileText.charAt(0).toUpperCase() + percentileText.slice(1)); container.find('.percentile-widget').show(); container.find('.percentile-widget').removeClass('hidden'); }); });</script></span><span><script>$(function() { new Works.PaperRankView({ workId: 122305145, container: "", }); });</script></span></div><div id="work-strip-premium-row-container"></div></div></div><script> require.config({ waitSeconds: 90 })(["https://a.academia-assets.com/assets/wow_profile-f77ea15d77ce96025a6048a514272ad8becbad23c641fc2b3bd6e24ca6ff1932.js","https://a.academia-assets.com/assets/work_edit-ad038b8c047c1a8d4fa01b402d530ff93c45fee2137a149a4a5398bc8ad67560.js"], function() { // from javascript_helper.rb var dispatcherData = {} if (false){ window.WowProfile.dispatcher = window.WowProfile.dispatcher || _.clone(Backbone.Events); dispatcherData = { dispatcher: window.WowProfile.dispatcher, downloadLinkId: "-1" } } $('.js-work-strip[data-work-id=122305145]').each(function() { if (!$(this).data('initialized')) { new WowProfile.WorkStripView({ el: this, workJSON: {"id":122305145,"title":"An Expansion Series for Solving Improper Cylindrical Functions Occurring in Subsonic, Supersonic and Transonic Kernel Formulations","translated_title":"","metadata":{"abstract":"A brief survey of the kernel functions occurring in unsteady subsonic or supersonic lifting surface formulations is presented. The discussion will be focused on the solutions of the improper cylindrical function as a main part of the kernel function. A new expansion series is proposed as an exact solution to the improper integral and may be regarded as an extension of the Ueda series. The new solution offers a very simple and convenient form since the singular and regular parts are explicitly separated. The simple form of the singular functions is a key point which is particularly significant in simplifying the Mangler integration; hence this approach is shown to be useful in improving the accuracy of many planar and nonplanar lifting surface methods. Results are discussed and their accuracy is presented.","publisher":"Springer Nature","publication_date":{"day":null,"month":null,"year":1995,"errors":{}},"publication_name":"Springer eBooks"},"translated_abstract":"A brief survey of the kernel functions occurring in unsteady subsonic or supersonic lifting surface formulations is presented. The discussion will be focused on the solutions of the improper cylindrical function as a main part of the kernel function. A new expansion series is proposed as an exact solution to the improper integral and may be regarded as an extension of the Ueda series. The new solution offers a very simple and convenient form since the singular and regular parts are explicitly separated. The simple form of the singular functions is a key point which is particularly significant in simplifying the Mangler integration; hence this approach is shown to be useful in improving the accuracy of many planar and nonplanar lifting surface methods. Results are discussed and their accuracy is presented.","internal_url":"https://www.academia.edu/122305145/An_Expansion_Series_for_Solving_Improper_Cylindrical_Functions_Occurring_in_Subsonic_Supersonic_and_Transonic_Kernel_Formulations","translated_internal_url":"","created_at":"2024-07-23T22:14:42.548-07:00","preview_url":null,"current_user_can_edit":null,"current_user_is_owner":null,"owner_id":4040157,"coauthors_can_edit":true,"document_type":"paper","co_author_tags":[],"downloadable_attachments":[],"slug":"An_Expansion_Series_for_Solving_Improper_Cylindrical_Functions_Occurring_in_Subsonic_Supersonic_and_Transonic_Kernel_Formulations","translated_slug":"","page_count":null,"language":"en","content_type":"Work","owner":{"id":4040157,"first_name":"Harijono","middle_initials":"","last_name":"Djojodihardjo","page_name":"HarijonoDjojodihardjo","domain_name":"itb","created_at":"2013-05-03T11:27:42.148-07:00","display_name":"Harijono Djojodihardjo","url":"https://itb.academia.edu/HarijonoDjojodihardjo"},"attachments":[],"research_interests":[{"id":48,"name":"Engineering","url":"https://www.academia.edu/Documents/in/Engineering"},{"id":60,"name":"Mechanical Engineering","url":"https://www.academia.edu/Documents/in/Mechanical_Engineering"},{"id":88,"name":"Aerospace Engineering","url":"https://www.academia.edu/Documents/in/Aerospace_Engineering"},{"id":300,"name":"Mathematics","url":"https://www.academia.edu/Documents/in/Mathematics"},{"id":305,"name":"Applied Mathematics","url":"https://www.academia.edu/Documents/in/Applied_Mathematics"},{"id":422,"name":"Computer Science","url":"https://www.academia.edu/Documents/in/Computer_Science"},{"id":3641,"name":"Aeronautical Engineering","url":"https://www.academia.edu/Documents/in/Aeronautical_Engineering"},{"id":2657384,"name":"Taylor expansion series","url":"https://www.academia.edu/Documents/in/Taylor_expansion_series"},{"id":2778229,"name":"Supersonic speed","url":"https://www.academia.edu/Documents/in/Supersonic_speed"},{"id":3647879,"name":"Springer Ebooks","url":"https://www.academia.edu/Documents/in/Springer_Ebooks"}],"urls":[{"id":43662292,"url":"https://doi.org/10.1007/978-3-642-80001-6_38"}]}, dispatcherData: dispatcherData }); $(this).data('initialized', true); } }); $a.trackClickSource(".js-work-strip-work-link", "profile_work_strip") }); </script> <div class="js-work-strip profile--work_container" data-work-id="122305144"><div class="profile--work_thumbnail hidden-xs"><a class="js-work-strip-work-link" data-click-track="profile-work-strip-thumbnail" href="https://www.academia.edu/122305144/Aerospace_Technology_Green_Energy_System_Perspectives"><img alt="Research paper thumbnail of Aerospace Technology Green Energy System Perspectives" class="work-thumbnail" src="https://attachments.academia-assets.com/116998313/thumbnails/1.jpg" /></a></div><div class="wp-workCard wp-workCard_itemContainer"><div class="wp-workCard_item wp-workCard--title"><a class="js-work-strip-work-link text-gray-darker" data-click-track="profile-work-strip-title" href="https://www.academia.edu/122305144/Aerospace_Technology_Green_Energy_System_Perspectives">Aerospace Technology Green Energy System Perspectives</a></div><div class="wp-workCard_item"><span>DEStech Transactions on Environment, Energy and Earth Science</span><span>, Jan 10, 2017</span></div><div class="wp-workCard_item wp-workCard--actions"><span class="work-strip-bookmark-button-container"></span><a id="2e48c6cdf2de3a6a4d45e07cce09bd23" class="wp-workCard--action" rel="nofollow" data-click-track="profile-work-strip-download" data-download="{&quot;attachment_id&quot;:116998313,&quot;asset_id&quot;:122305144,&quot;asset_type&quot;:&quot;Work&quot;,&quot;button_location&quot;:&quot;profile&quot;}" href="https://www.academia.edu/attachments/116998313/download_file?st=MTczMzAzMTQwNiw4LjIyMi4yMDguMTQ2&s=profile"><span><i class="fa fa-arrow-down"></i></span><span>Download</span></a><span class="wp-workCard--action visible-if-viewed-by-owner inline-block" style="display: none;"><span class="js-profile-work-strip-edit-button-wrapper profile-work-strip-edit-button-wrapper" data-work-id="122305144"><a class="js-profile-work-strip-edit-button" tabindex="0"><span><i class="fa fa-pencil"></i></span><span>Edit</span></a></span></span><span id="work-strip-rankings-button-container"></span></div><div class="wp-workCard_item wp-workCard--stats"><span><span><span class="js-view-count view-count u-mr2x" data-work-id="122305144"><i class="fa fa-spinner fa-spin"></i></span><script>$(function () { var workId = 122305144; 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$(this).data('initialized', true); } }); $a.trackClickSource(".js-work-strip-work-link", "profile_work_strip") }); </script> <div class="js-work-strip profile--work_container" data-work-id="122305142"><div class="profile--work_thumbnail hidden-xs"><a class="js-work-strip-work-link" data-click-track="profile-work-strip-thumbnail" href="https://www.academia.edu/122305142/CFD_Simulation_of_Coand%C4%83_Effect_on_the_Upper_Respiratory_System"><img alt="Research paper thumbnail of CFD Simulation of Coandă Effect on the Upper Respiratory System" class="work-thumbnail" src="https://a.academia-assets.com/images/blank-paper.jpg" /></a></div><div class="wp-workCard wp-workCard_itemContainer"><div class="wp-workCard_item wp-workCard--title"><a class="js-work-strip-work-link text-gray-darker" data-click-track="profile-work-strip-title" href="https://www.academia.edu/122305142/CFD_Simulation_of_Coand%C4%83_Effect_on_the_Upper_Respiratory_System">CFD Simulation of Coandă Effect on the Upper Respiratory System</a></div><div class="wp-workCard_item"><span>Journal of Medical Imaging and Health Informatics</span><span>, Oct 1, 2016</span></div><div class="wp-workCard_item"><span class="js-work-more-abstract-truncated">Based on the authors’ various studies on Coandă effect, the present study is devoted to focus on ...</span><a class="js-work-more-abstract" data-broccoli-component="work_strip.more_abstract" data-click-track="profile-work-strip-more-abstract" href="javascript:;"><span> more </span><span><i class="fa fa-caret-down"></i></span></a><span class="js-work-more-abstract-untruncated hidden">Based on the authors’ various studies on Coandă effect, the present study is devoted to focus on the development and influence of Coandă effect on the flow along a conduit with constriction representing the upper respiratory system of the human body, including the constriction dynamics and aerodynamics that may prevail there. For this purpose, theoretical analyses as well as CFD simulation are being carried out. Comparison of the results obtained with other medical based studies has exhibited striking similarities and are assessed for their physical significance.</span></div><div class="wp-workCard_item wp-workCard--actions"><span class="work-strip-bookmark-button-container"></span><span class="wp-workCard--action visible-if-viewed-by-owner inline-block" style="display: none;"><span class="js-profile-work-strip-edit-button-wrapper profile-work-strip-edit-button-wrapper" data-work-id="122305142"><a class="js-profile-work-strip-edit-button" tabindex="0"><span><i class="fa fa-pencil"></i></span><span>Edit</span></a></span></span><span id="work-strip-rankings-button-container"></span></div><div class="wp-workCard_item wp-workCard--stats"><span><span><span class="js-view-count view-count u-mr2x" data-work-id="122305142"><i class="fa fa-spinner fa-spin"></i></span><script>$(function () { var workId = 122305142; window.Academia.workViewCountsFetcher.queue(workId, function (count) { var description = window.$h.commaizeInt(count) + " " + window.$h.pluralize(count, 'View'); $(".js-view-count[data-work-id=122305142]").text(description); $(".js-view-count[data-work-id=122305142]").attr('title', description).tooltip(); }); });</script></span></span><span><span class="percentile-widget hidden"><span class="u-mr2x work-percentile"></span></span><script>$(function () { var workId = 122305142; window.Academia.workPercentilesFetcher.queue(workId, function (percentileText) { var container = $(".js-work-strip[data-work-id='122305142']"); container.find('.work-percentile').text(percentileText.charAt(0).toUpperCase() + percentileText.slice(1)); container.find('.percentile-widget').show(); container.find('.percentile-widget').removeClass('hidden'); }); });</script></span><span><script>$(function() { new Works.PaperRankView({ workId: 122305142, container: "", }); });</script></span></div><div id="work-strip-premium-row-container"></div></div></div><script> require.config({ waitSeconds: 90 })(["https://a.academia-assets.com/assets/wow_profile-f77ea15d77ce96025a6048a514272ad8becbad23c641fc2b3bd6e24ca6ff1932.js","https://a.academia-assets.com/assets/work_edit-ad038b8c047c1a8d4fa01b402d530ff93c45fee2137a149a4a5398bc8ad67560.js"], function() { // from javascript_helper.rb var dispatcherData = {} if (false){ window.WowProfile.dispatcher = window.WowProfile.dispatcher || _.clone(Backbone.Events); dispatcherData = { dispatcher: window.WowProfile.dispatcher, downloadLinkId: "-1" } } $('.js-work-strip[data-work-id=122305142]').each(function() { if (!$(this).data('initialized')) { new WowProfile.WorkStripView({ el: this, workJSON: {"id":122305142,"title":"CFD Simulation of Coandă Effect on the Upper Respiratory System","translated_title":"","metadata":{"abstract":"Based on the authors’ various studies on Coandă effect, the present study is devoted to focus on the development and influence of Coandă effect on the flow along a conduit with constriction representing the upper respiratory system of the human body, including the constriction dynamics and aerodynamics that may prevail there. 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Mobility: The Technical Challenge; Proceedings of the Fourth International Pacific Conference on Automotive Engineering, Melbourne, Australia, November 8-14, 1987. Volumes 1 to 3" class="work-thumbnail" src="https://a.academia-assets.com/images/blank-paper.jpg" /></a></div><div class="wp-workCard wp-workCard_itemContainer"><div class="wp-workCard_item wp-workCard--title"><a class="js-work-strip-work-link text-gray-darker" data-click-track="profile-work-strip-title" href="https://www.academia.edu/122305141/An_Analytical_Study_of_Small_Commercial_Vehicle_Stability_Mobility_The_Technical_Challenge_Proceedings_of_the_Fourth_International_Pacific_Conference_on_Automotive_Engineering_Melbourne_Australia_November_8_14_1987_Volumes_1_to_3">An Analytical Study of Small Commercial Vehicle Stability. Mobility: The Technical Challenge; Proceedings of the Fourth International Pacific Conference on Automotive Engineering, Melbourne, Australia, November 8-14, 1987. Volumes 1 to 3</a></div><div class="wp-workCard_item"><span>Publication of: Society of Automotive Engineers</span><span>, 1987</span></div><div class="wp-workCard_item"><span class="js-work-more-abstract-truncated">An analysis of lateral and directional steady state stability of a typical small commercial vehic...</span><a class="js-work-more-abstract" data-broccoli-component="work_strip.more_abstract" data-click-track="profile-work-strip-more-abstract" href="javascript:;"><span> more </span><span><i class="fa fa-caret-down"></i></span></a><span class="js-work-more-abstract-untruncated hidden">An analysis of lateral and directional steady state stability of a typical small commercial vehicle configuration is performed limiting the movement to three degrees of freedom: side slipping, yawing and rolling. Based on the analysis, a parametric study is performed to investigate the influence of some design and operational parameters, in order to arrive at some design guidelines. SAE paper no 871182. (Author/TRRL)</span></div><div class="wp-workCard_item wp-workCard--actions"><span class="work-strip-bookmark-button-container"></span><span class="wp-workCard--action visible-if-viewed-by-owner inline-block" style="display: none;"><span class="js-profile-work-strip-edit-button-wrapper profile-work-strip-edit-button-wrapper" data-work-id="122305141"><a class="js-profile-work-strip-edit-button" tabindex="0"><span><i class="fa fa-pencil"></i></span><span>Edit</span></a></span></span><span id="work-strip-rankings-button-container"></span></div><div class="wp-workCard_item wp-workCard--stats"><span><span><span class="js-view-count view-count u-mr2x" data-work-id="122305141"><i class="fa fa-spinner fa-spin"></i></span><script>$(function () { var workId = 122305141; window.Academia.workViewCountsFetcher.queue(workId, function (count) { var description = window.$h.commaizeInt(count) + " " + window.$h.pluralize(count, 'View'); $(".js-view-count[data-work-id=122305141]").text(description); $(".js-view-count[data-work-id=122305141]").attr('title', description).tooltip(); }); });</script></span></span><span><span class="percentile-widget hidden"><span class="u-mr2x work-percentile"></span></span><script>$(function () { var workId = 122305141; window.Academia.workPercentilesFetcher.queue(workId, function (percentileText) { var container = $(".js-work-strip[data-work-id='122305141']"); container.find('.work-percentile').text(percentileText.charAt(0).toUpperCase() + percentileText.slice(1)); container.find('.percentile-widget').show(); container.find('.percentile-widget').removeClass('hidden'); }); });</script></span><span><script>$(function() { new Works.PaperRankView({ workId: 122305141, container: "", }); });</script></span></div><div id="work-strip-premium-row-container"></div></div></div><script> require.config({ waitSeconds: 90 })(["https://a.academia-assets.com/assets/wow_profile-f77ea15d77ce96025a6048a514272ad8becbad23c641fc2b3bd6e24ca6ff1932.js","https://a.academia-assets.com/assets/work_edit-ad038b8c047c1a8d4fa01b402d530ff93c45fee2137a149a4a5398bc8ad67560.js"], function() { // from javascript_helper.rb var dispatcherData = {} if (false){ window.WowProfile.dispatcher = window.WowProfile.dispatcher || _.clone(Backbone.Events); dispatcherData = { dispatcher: window.WowProfile.dispatcher, downloadLinkId: "-1" } } $('.js-work-strip[data-work-id=122305141]').each(function() { if (!$(this).data('initialized')) { new WowProfile.WorkStripView({ el: this, workJSON: {"id":122305141,"title":"An Analytical Study of Small Commercial Vehicle Stability. 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$(this).data('initialized', true); } }); $a.trackClickSource(".js-work-strip-work-link", "profile_work_strip") }); </script> <div class="js-work-strip profile--work_container" data-work-id="122305157"><div class="profile--work_thumbnail hidden-xs"><a class="js-work-strip-work-link" data-click-track="profile-work-strip-thumbnail" href="https://www.academia.edu/122305157/Numerical_boundary_element_computation_of_submerged_body_surface_wave_interaction"><img alt="Research paper thumbnail of Numerical boundary element computation of submerged body-surface wave interaction" class="work-thumbnail" src="https://a.academia-assets.com/images/blank-paper.jpg" /></a></div><div class="wp-workCard wp-workCard_itemContainer"><div class="wp-workCard_item wp-workCard--title"><a class="js-work-strip-work-link text-gray-darker" data-click-track="profile-work-strip-title" href="https://www.academia.edu/122305157/Numerical_boundary_element_computation_of_submerged_body_surface_wave_interaction">Numerical boundary element computation of submerged body-surface wave interaction</a></div><div class="wp-workCard_item"><span>The Proceedings of the ... International Offshore and Polar Engineering Conference</span><span>, 1993</span></div><div class="wp-workCard_item"><span class="js-work-more-abstract-truncated">A simple method to solve potential flow problems of submerged body-surface wave interaction is pr...</span><a class="js-work-more-abstract" data-broccoli-component="work_strip.more_abstract" data-click-track="profile-work-strip-more-abstract" href="javascript:;"><span> more </span><span><i class="fa fa-caret-down"></i></span></a><span class="js-work-more-abstract-untruncated hidden">A simple method to solve potential flow problems of submerged body-surface wave interaction is presented. The Laplace equation governs flow below the surface. The boundary condition on the body is of Neumann type, while on the free surface the nonlinear dynamic free surface condition has to be satisfied. In addition, the farfield and radiation condition, which determine the behaviour of waves going to infinity, have to be satisfied. Taking advantage of the potential flow model, Green Identity is then used to transform the problem of the Laplace equation with nonlinear boundary conation into a nonlinear problem in its boundary. To satisfy the nonlinear dynamic free surface condition, Newton iteration is employed. The scheme for relaxation is obtained by expanding the nonlinear dynamic free surface condition to obtain correction terms to the velocity potential. Truncation up to linear terms results in a simple scheme. Since the dynamic condition is valid on the unknown location of the free surface, in each iteration step the position of the free surface where the equation is applied, is corrected using the Bernoulli equation. In this manner, dynamic free surface condition is satisfied exactly at the collocation points. 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$(this).data('initialized', true); } }); $a.trackClickSource(".js-work-strip-work-link", "profile_work_strip") }); </script> <div class="js-work-strip profile--work_container" data-work-id="122305152"><div class="profile--work_thumbnail hidden-xs"><a class="js-work-strip-work-link" data-click-track="profile-work-strip-thumbnail" href="https://www.academia.edu/122305152/Buffeting_Problems_Modelling_by_Use_of_Lifting_Surface_Methods_in_Unsteady_Aerodynamics_with_Separation"><img alt="Research paper thumbnail of Buffeting Problems Modelling by Use of Lifting Surface Methods in Unsteady Aerodynamics with Separation" class="work-thumbnail" src="https://a.academia-assets.com/images/blank-paper.jpg" /></a></div><div class="wp-workCard wp-workCard_itemContainer"><div class="wp-workCard_item wp-workCard--title"><a class="js-work-strip-work-link text-gray-darker" data-click-track="profile-work-strip-title" href="https://www.academia.edu/122305152/Buffeting_Problems_Modelling_by_Use_of_Lifting_Surface_Methods_in_Unsteady_Aerodynamics_with_Separation">Buffeting Problems Modelling by Use of Lifting Surface Methods in Unsteady Aerodynamics with Separation</a></div><div class="wp-workCard_item"><span class="js-work-more-abstract-truncated">The analytical approach to buffeting problem in subsonic flow is a challenging one and has been g...</span><a class="js-work-more-abstract" data-broccoli-component="work_strip.more_abstract" data-click-track="profile-work-strip-more-abstract" href="javascript:;"><span> more </span><span><i class="fa fa-caret-down"></i></span></a><span class="js-work-more-abstract-untruncated hidden">The analytical approach to buffeting problem in subsonic flow is a challenging one and has been given attention by many researchers; no purely analytical approach has been satisfactorily capable of simulating the phenomenon. An attempt to develop a computational method for the calculation of the aerodynamic load for separated subsonic flow using kernel function technique in linearized aerodynamics has been made by the author and his associates, as an alternative to the more accurate but elaborate technique of direct numerical attack to the viscous flow problem. Two approaches were then made. First, to treat the buffeting problem as a stability one by solving the flutter equation. Second, treating buffeting problem using dynamic response approach. Comparison of the unsteady load calculation method with other existing results for non-separated flow cases indicated good agreements. For separated flow case, no other methods are available for comparison. However, flutter solution approach made by the present study indicated that the presence of the separation bubble tends to destabilize the system compared to the attached flow case. The analytical approach to the buffeting problem using dynamic response technique was made by assuming that there is no coupling between the motion induced unsteady loads and the independent-motion unsteady loads. The motion induced unsteady airloads is calculated using the present method while the buffeting excitation load was based on experimental data. Computational results for the bending moment of a wing experiencing buffeting with experimental results indicated good agreement but lower values for the onset of buffeting.</span></div><div class="wp-workCard_item wp-workCard--actions"><span class="work-strip-bookmark-button-container"></span><span class="wp-workCard--action visible-if-viewed-by-owner inline-block" style="display: none;"><span class="js-profile-work-strip-edit-button-wrapper profile-work-strip-edit-button-wrapper" data-work-id="122305152"><a class="js-profile-work-strip-edit-button" tabindex="0"><span><i class="fa fa-pencil"></i></span><span>Edit</span></a></span></span><span id="work-strip-rankings-button-container"></span></div><div class="wp-workCard_item wp-workCard--stats"><span><span><span class="js-view-count view-count u-mr2x" data-work-id="122305152"><i class="fa fa-spinner fa-spin"></i></span><script>$(function () { var workId = 122305152; window.Academia.workViewCountsFetcher.queue(workId, function (count) { var description = window.$h.commaizeInt(count) + " " + window.$h.pluralize(count, 'View'); $(".js-view-count[data-work-id=122305152]").text(description); $(".js-view-count[data-work-id=122305152]").attr('title', description).tooltip(); }); });</script></span></span><span><span class="percentile-widget hidden"><span class="u-mr2x work-percentile"></span></span><script>$(function () { var workId = 122305152; window.Academia.workPercentilesFetcher.queue(workId, function (percentileText) { var container = $(".js-work-strip[data-work-id='122305152']"); container.find('.work-percentile').text(percentileText.charAt(0).toUpperCase() + percentileText.slice(1)); container.find('.percentile-widget').show(); container.find('.percentile-widget').removeClass('hidden'); }); });</script></span><span><script>$(function() { new Works.PaperRankView({ workId: 122305152, container: "", }); });</script></span></div><div id="work-strip-premium-row-container"></div></div></div><script> require.config({ waitSeconds: 90 })(["https://a.academia-assets.com/assets/wow_profile-f77ea15d77ce96025a6048a514272ad8becbad23c641fc2b3bd6e24ca6ff1932.js","https://a.academia-assets.com/assets/work_edit-ad038b8c047c1a8d4fa01b402d530ff93c45fee2137a149a4a5398bc8ad67560.js"], function() { // from javascript_helper.rb var dispatcherData = {} if (false){ window.WowProfile.dispatcher = window.WowProfile.dispatcher || _.clone(Backbone.Events); dispatcherData = { dispatcher: window.WowProfile.dispatcher, downloadLinkId: "-1" } } $('.js-work-strip[data-work-id=122305152]').each(function() { if (!$(this).data('initialized')) { new WowProfile.WorkStripView({ el: this, workJSON: {"id":122305152,"title":"Buffeting Problems Modelling by Use of Lifting Surface Methods in Unsteady Aerodynamics with Separation","translated_title":"","metadata":{"abstract":"The analytical approach to buffeting problem in subsonic flow is a challenging one and has been given attention by many researchers; no purely analytical approach has been satisfactorily capable of simulating the phenomenon. 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An attempt to develop a computational method for the calculation of the aerodynamic load for separated subsonic flow using kernel function technique in linearized aerodynamics has been made by the author and his associates, as an alternative to the more accurate but elaborate technique of direct numerical attack to the viscous flow problem. Two approaches were then made. First, to treat the buffeting problem as a stability one by solving the flutter equation. Second, treating buffeting problem using dynamic response approach. Comparison of the unsteady load calculation method with other existing results for non-separated flow cases indicated good agreements. For separated flow case, no other methods are available for comparison. However, flutter solution approach made by the present study indicated that the presence of the separation bubble tends to destabilize the system compared to the attached flow case. The analytical approach to the buffeting problem using dynamic response technique was made by assuming that there is no coupling between the motion induced unsteady loads and the independent-motion unsteady loads. The motion induced unsteady airloads is calculated using the present method while the buffeting excitation load was based on experimental data. Computational results for the bending moment of a wing experiencing buffeting with experimental results indicated good agreement but lower values for the onset of buffeting.","internal_url":"https://www.academia.edu/122305152/Buffeting_Problems_Modelling_by_Use_of_Lifting_Surface_Methods_in_Unsteady_Aerodynamics_with_Separation","translated_internal_url":"","created_at":"2024-07-23T22:14:44.994-07:00","preview_url":null,"current_user_can_edit":null,"current_user_is_owner":null,"owner_id":4040157,"coauthors_can_edit":true,"document_type":"paper","co_author_tags":[],"downloadable_attachments":[],"slug":"Buffeting_Problems_Modelling_by_Use_of_Lifting_Surface_Methods_in_Unsteady_Aerodynamics_with_Separation","translated_slug":"","page_count":null,"language":"en","content_type":"Work","owner":{"id":4040157,"first_name":"Harijono","middle_initials":"","last_name":"Djojodihardjo","page_name":"HarijonoDjojodihardjo","domain_name":"itb","created_at":"2013-05-03T11:27:42.148-07:00","display_name":"Harijono Djojodihardjo","url":"https://itb.academia.edu/HarijonoDjojodihardjo"},"attachments":[],"research_interests":[{"id":422,"name":"Computer Science","url":"https://www.academia.edu/Documents/in/Computer_Science"},{"id":10875,"name":"Aerodynamics","url":"https://www.academia.edu/Documents/in/Aerodynamics"},{"id":36296,"name":"Aeroelasticity","url":"https://www.academia.edu/Documents/in/Aeroelasticity"},{"id":309117,"name":"Flutter","url":"https://www.academia.edu/Documents/in/Flutter"}],"urls":[{"id":43662299,"url":"https://doi.org/10.1007/978-94-011-5157-3_3"}]}, dispatcherData: dispatcherData }); 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Of particular importance is the utilization and development of earth observation capabilities for environmental natural resources imperatives to this end is quite significant. On one hand there may appear challenges to achieve unique and high quality requirements on many of the elements of social and economic progress, i.e.</span></div><div class="wp-workCard_item wp-workCard--actions"><span class="work-strip-bookmark-button-container"></span><span class="wp-workCard--action visible-if-viewed-by-owner inline-block" style="display: none;"><span class="js-profile-work-strip-edit-button-wrapper profile-work-strip-edit-button-wrapper" data-work-id="122305150"><a class="js-profile-work-strip-edit-button" tabindex="0"><span><i class="fa fa-pencil"></i></span><span>Edit</span></a></span></span><span id="work-strip-rankings-button-container"></span></div><div class="wp-workCard_item wp-workCard--stats"><span><span><span class="js-view-count view-count u-mr2x" data-work-id="122305150"><i class="fa fa-spinner fa-spin"></i></span><script>$(function () { var workId = 122305150; window.Academia.workViewCountsFetcher.queue(workId, function (count) { var description = window.$h.commaizeInt(count) + " " + window.$h.pluralize(count, 'View'); $(".js-view-count[data-work-id=122305150]").text(description); $(".js-view-count[data-work-id=122305150]").attr('title', description).tooltip(); }); });</script></span></span><span><span class="percentile-widget hidden"><span class="u-mr2x work-percentile"></span></span><script>$(function () { var workId = 122305150; window.Academia.workPercentilesFetcher.queue(workId, function (percentileText) { var container = $(".js-work-strip[data-work-id='122305150']"); container.find('.work-percentile').text(percentileText.charAt(0).toUpperCase() + percentileText.slice(1)); container.find('.percentile-widget').show(); container.find('.percentile-widget').removeClass('hidden'); }); });</script></span><span><script>$(function() { new Works.PaperRankView({ workId: 122305150, container: "", }); });</script></span></div><div id="work-strip-premium-row-container"></div></div></div><script> require.config({ waitSeconds: 90 })(["https://a.academia-assets.com/assets/wow_profile-f77ea15d77ce96025a6048a514272ad8becbad23c641fc2b3bd6e24ca6ff1932.js","https://a.academia-assets.com/assets/work_edit-ad038b8c047c1a8d4fa01b402d530ff93c45fee2137a149a4a5398bc8ad67560.js"], function() { // from javascript_helper.rb var dispatcherData = {} if (false){ window.WowProfile.dispatcher = window.WowProfile.dispatcher || _.clone(Backbone.Events); dispatcherData = { dispatcher: window.WowProfile.dispatcher, downloadLinkId: "-1" } } $('.js-work-strip[data-work-id=122305150]').each(function() { if (!$(this).data('initialized')) { new WowProfile.WorkStripView({ el: this, workJSON: {"id":122305150,"title":"Comprehensive Study on Small and Low Cost Satellite Technology for Earth Observation with Case Study for Indonesia: Projection for 2002-2022","translated_title":"","metadata":{"abstract":"and economic progress, while facing global competitiveness locally as opportunities and challenges. 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$(this).data('initialized', true); } }); $a.trackClickSource(".js-work-strip-work-link", "profile_work_strip") }); </script> <div class="js-work-strip profile--work_container" data-work-id="122305147"><div class="profile--work_thumbnail hidden-xs"><a class="js-work-strip-work-link" data-click-track="profile-work-strip-thumbnail" href="https://www.academia.edu/122305147/Locally_Linearized_Solution_of_Lifting_Transonic_Flow_by_Method_of_Parametric_Differentiation"><img alt="Research paper thumbnail of Locally Linearized Solution of Lifting Transonic Flow by Method of Parametric Differentiation" class="work-thumbnail" src="https://a.academia-assets.com/images/blank-paper.jpg" /></a></div><div class="wp-workCard wp-workCard_itemContainer"><div class="wp-workCard_item wp-workCard--title"><a class="js-work-strip-work-link text-gray-darker" data-click-track="profile-work-strip-title" href="https://www.academia.edu/122305147/Locally_Linearized_Solution_of_Lifting_Transonic_Flow_by_Method_of_Parametric_Differentiation">Locally Linearized Solution of Lifting Transonic Flow by Method of Parametric Differentiation</a></div><div class="wp-workCard_item"><span>DOAJ (DOAJ: Directory of Open Access Journals)</span><span>, Feb 1, 2019</span></div><div class="wp-workCard_item"><span class="js-work-more-abstract-truncated">The governing equation of transonic small disturbance flow present a non-linear partial different...</span><a class="js-work-more-abstract" data-broccoli-component="work_strip.more_abstract" data-click-track="profile-work-strip-more-abstract" href="javascript:;"><span> more </span><span><i class="fa fa-caret-down"></i></span></a><span class="js-work-more-abstract-untruncated hidden">The governing equation of transonic small disturbance flow present a non-linear partial differential equation which is difficult to solve. The method of parametric differentiation reduces the non-linear partial differential equation of transonic flow into an ordinary differential equation with variable coefficient, which is generally much simple to solve. Further simplification is introduced, as also done in the method of local linearization, by assuming (1-M 1 2 ) to vary sufficiently slowly, so that in some part of the analysis its derivatives with respect to x can be disregarded. Based upon these methods, the lifting transonic flow was analyzed. For the subsonic and supersonic parts, closed form solutions were obtained. For the case M 1  ≈ 1, the method yields an integral equation, which can be solved by an iterative scheme starting from the non-lifting solution.</span></div><div class="wp-workCard_item wp-workCard--actions"><span class="work-strip-bookmark-button-container"></span><span class="wp-workCard--action visible-if-viewed-by-owner inline-block" style="display: none;"><span class="js-profile-work-strip-edit-button-wrapper profile-work-strip-edit-button-wrapper" data-work-id="122305147"><a class="js-profile-work-strip-edit-button" tabindex="0"><span><i class="fa fa-pencil"></i></span><span>Edit</span></a></span></span><span id="work-strip-rankings-button-container"></span></div><div class="wp-workCard_item wp-workCard--stats"><span><span><span class="js-view-count view-count u-mr2x" data-work-id="122305147"><i class="fa fa-spinner fa-spin"></i></span><script>$(function () { var workId = 122305147; window.Academia.workViewCountsFetcher.queue(workId, function (count) { var description = window.$h.commaizeInt(count) + " " + window.$h.pluralize(count, 'View'); $(".js-view-count[data-work-id=122305147]").text(description); $(".js-view-count[data-work-id=122305147]").attr('title', description).tooltip(); }); });</script></span></span><span><span class="percentile-widget hidden"><span class="u-mr2x work-percentile"></span></span><script>$(function () { var workId = 122305147; window.Academia.workPercentilesFetcher.queue(workId, function (percentileText) { var container = $(".js-work-strip[data-work-id='122305147']"); container.find('.work-percentile').text(percentileText.charAt(0).toUpperCase() + percentileText.slice(1)); container.find('.percentile-widget').show(); container.find('.percentile-widget').removeClass('hidden'); }); });</script></span><span><script>$(function() { new Works.PaperRankView({ workId: 122305147, container: "", }); });</script></span></div><div id="work-strip-premium-row-container"></div></div></div><script> require.config({ waitSeconds: 90 })(["https://a.academia-assets.com/assets/wow_profile-f77ea15d77ce96025a6048a514272ad8becbad23c641fc2b3bd6e24ca6ff1932.js","https://a.academia-assets.com/assets/work_edit-ad038b8c047c1a8d4fa01b402d530ff93c45fee2137a149a4a5398bc8ad67560.js"], function() { // from javascript_helper.rb var dispatcherData = {} if (false){ window.WowProfile.dispatcher = window.WowProfile.dispatcher || _.clone(Backbone.Events); dispatcherData = { dispatcher: window.WowProfile.dispatcher, downloadLinkId: "-1" } } $('.js-work-strip[data-work-id=122305147]').each(function() { if (!$(this).data('initialized')) { new WowProfile.WorkStripView({ el: this, workJSON: {"id":122305147,"title":"Locally Linearized Solution of Lifting Transonic Flow by Method of Parametric Differentiation","translated_title":"","metadata":{"abstract":"The governing equation of transonic small disturbance flow present a non-linear partial differential equation which is difficult to solve. The method of parametric differentiation reduces the non-linear partial differential equation of transonic flow into an ordinary differential equation with variable coefficient, which is generally much simple to solve. Further simplification is introduced, as also done in the method of local linearization, by assuming (1-M 1 2 ) to vary sufficiently slowly, so that in some part of the analysis its derivatives with respect to x can be disregarded. Based upon these methods, the lifting transonic flow was analyzed. For the subsonic and supersonic parts, closed form solutions were obtained. For the case M 1  ≈ 1, the method yields an integral equation, which can be solved by an iterative scheme starting from the non-lifting solution.","publisher":"DOAJ: Directory of Open Access Journals","publication_date":{"day":1,"month":2,"year":2019,"errors":{}},"publication_name":"DOAJ (DOAJ: Directory of Open Access Journals)"},"translated_abstract":"The governing equation of transonic small disturbance flow present a non-linear partial differential equation which is difficult to solve. The method of parametric differentiation reduces the non-linear partial differential equation of transonic flow into an ordinary differential equation with variable coefficient, which is generally much simple to solve. Further simplification is introduced, as also done in the method of local linearization, by assuming (1-M 1 2 ) to vary sufficiently slowly, so that in some part of the analysis its derivatives with respect to x can be disregarded. Based upon these methods, the lifting transonic flow was analyzed. For the subsonic and supersonic parts, closed form solutions were obtained. For the case M 1  ≈ 1, the method yields an integral equation, which can be solved by an iterative scheme starting from the non-lifting solution.","internal_url":"https://www.academia.edu/122305147/Locally_Linearized_Solution_of_Lifting_Transonic_Flow_by_Method_of_Parametric_Differentiation","translated_internal_url":"","created_at":"2024-07-23T22:14:42.931-07:00","preview_url":null,"current_user_can_edit":null,"current_user_is_owner":null,"owner_id":4040157,"coauthors_can_edit":true,"document_type":"paper","co_author_tags":[],"downloadable_attachments":[],"slug":"Locally_Linearized_Solution_of_Lifting_Transonic_Flow_by_Method_of_Parametric_Differentiation","translated_slug":"","page_count":null,"language":"en","content_type":"Work","owner":{"id":4040157,"first_name":"Harijono","middle_initials":"","last_name":"Djojodihardjo","page_name":"HarijonoDjojodihardjo","domain_name":"itb","created_at":"2013-05-03T11:27:42.148-07:00","display_name":"Harijono Djojodihardjo","url":"https://itb.academia.edu/HarijonoDjojodihardjo"},"attachments":[],"research_interests":[{"id":300,"name":"Mathematics","url":"https://www.academia.edu/Documents/in/Mathematics"},{"id":86034,"name":"Mathematical Analysis","url":"https://www.academia.edu/Documents/in/Mathematical_Analysis"},{"id":194130,"name":"PARTIAL DIFFERENTIAL EQUATION","url":"https://www.academia.edu/Documents/in/PARTIAL_DIFFERENTIAL_EQUATION"},{"id":349904,"name":"Linearization","url":"https://www.academia.edu/Documents/in/Linearization"},{"id":830168,"name":"Method of Characteristics","url":"https://www.academia.edu/Documents/in/Method_of_Characteristics"},{"id":1770555,"name":"Ordinary Differential Equation","url":"https://www.academia.edu/Documents/in/Ordinary_Differential_Equation"},{"id":2778229,"name":"Supersonic speed","url":"https://www.academia.edu/Documents/in/Supersonic_speed"}],"urls":[{"id":43662294,"url":"https://doaj.org/article/c4fa46d1665e4957a4ce242df4b8e88b"}]}, dispatcherData: dispatcherData }); $(this).data('initialized', true); } }); $a.trackClickSource(".js-work-strip-work-link", "profile_work_strip") }); </script> <div class="js-work-strip profile--work_container" data-work-id="122305146"><div class="profile--work_thumbnail hidden-xs"><a class="js-work-strip-work-link" data-click-track="profile-work-strip-thumbnail" href="https://www.academia.edu/122305146/Acoustic_Method_for_the_Suppression_of_Acoustic_and_Aerodynamically_Induced_Vibration_on_Structures"><img alt="Research paper thumbnail of Acoustic Method for the Suppression of Acoustic and Aerodynamically Induced Vibration on Structures" class="work-thumbnail" src="https://attachments.academia-assets.com/116998312/thumbnails/1.jpg" /></a></div><div class="wp-workCard wp-workCard_itemContainer"><div class="wp-workCard_item wp-workCard--title"><a class="js-work-strip-work-link text-gray-darker" data-click-track="profile-work-strip-title" href="https://www.academia.edu/122305146/Acoustic_Method_for_the_Suppression_of_Acoustic_and_Aerodynamically_Induced_Vibration_on_Structures">Acoustic Method for the Suppression of Acoustic and Aerodynamically Induced Vibration on Structures</a></div><div class="wp-workCard_item"><span>Advances in civil and industrial engineering book series</span><span>, 2017</span></div><div class="wp-workCard_item wp-workCard--actions"><span class="work-strip-bookmark-button-container"></span><a id="5ae2cb772427d9062f0de44d94280e1c" class="wp-workCard--action" rel="nofollow" data-click-track="profile-work-strip-download" data-download="{&quot;attachment_id&quot;:116998312,&quot;asset_id&quot;:122305146,&quot;asset_type&quot;:&quot;Work&quot;,&quot;button_location&quot;:&quot;profile&quot;}" href="https://www.academia.edu/attachments/116998312/download_file?st=MTczMzAzMTQwNiw4LjIyMi4yMDguMTQ2&s=profile"><span><i class="fa fa-arrow-down"></i></span><span>Download</span></a><span class="wp-workCard--action visible-if-viewed-by-owner inline-block" style="display: none;"><span class="js-profile-work-strip-edit-button-wrapper profile-work-strip-edit-button-wrapper" data-work-id="122305146"><a class="js-profile-work-strip-edit-button" tabindex="0"><span><i class="fa fa-pencil"></i></span><span>Edit</span></a></span></span><span id="work-strip-rankings-button-container"></span></div><div class="wp-workCard_item wp-workCard--stats"><span><span><span class="js-view-count view-count u-mr2x" data-work-id="122305146"><i class="fa fa-spinner fa-spin"></i></span><script>$(function () { var workId = 122305146; 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$(this).data('initialized', true); } }); $a.trackClickSource(".js-work-strip-work-link", "profile_work_strip") }); </script> <div class="js-work-strip profile--work_container" data-work-id="122305145"><div class="profile--work_thumbnail hidden-xs"><a class="js-work-strip-work-link" data-click-track="profile-work-strip-thumbnail" href="https://www.academia.edu/122305145/An_Expansion_Series_for_Solving_Improper_Cylindrical_Functions_Occurring_in_Subsonic_Supersonic_and_Transonic_Kernel_Formulations"><img alt="Research paper thumbnail of An Expansion Series for Solving Improper Cylindrical Functions Occurring in Subsonic, Supersonic and Transonic Kernel Formulations" class="work-thumbnail" src="https://a.academia-assets.com/images/blank-paper.jpg" /></a></div><div class="wp-workCard wp-workCard_itemContainer"><div class="wp-workCard_item wp-workCard--title"><a class="js-work-strip-work-link text-gray-darker" data-click-track="profile-work-strip-title" href="https://www.academia.edu/122305145/An_Expansion_Series_for_Solving_Improper_Cylindrical_Functions_Occurring_in_Subsonic_Supersonic_and_Transonic_Kernel_Formulations">An Expansion Series for Solving Improper Cylindrical Functions Occurring in Subsonic, Supersonic and Transonic Kernel Formulations</a></div><div class="wp-workCard_item"><span>Springer eBooks</span><span>, 1995</span></div><div class="wp-workCard_item"><span class="js-work-more-abstract-truncated">A brief survey of the kernel functions occurring in unsteady subsonic or supersonic lifting surfa...</span><a class="js-work-more-abstract" data-broccoli-component="work_strip.more_abstract" data-click-track="profile-work-strip-more-abstract" href="javascript:;"><span> more </span><span><i class="fa fa-caret-down"></i></span></a><span class="js-work-more-abstract-untruncated hidden">A brief survey of the kernel functions occurring in unsteady subsonic or supersonic lifting surface formulations is presented. The discussion will be focused on the solutions of the improper cylindrical function as a main part of the kernel function. A new expansion series is proposed as an exact solution to the improper integral and may be regarded as an extension of the Ueda series. The new solution offers a very simple and convenient form since the singular and regular parts are explicitly separated. The simple form of the singular functions is a key point which is particularly significant in simplifying the Mangler integration; hence this approach is shown to be useful in improving the accuracy of many planar and nonplanar lifting surface methods. Results are discussed and their accuracy is presented.</span></div><div class="wp-workCard_item wp-workCard--actions"><span class="work-strip-bookmark-button-container"></span><span class="wp-workCard--action visible-if-viewed-by-owner inline-block" style="display: none;"><span class="js-profile-work-strip-edit-button-wrapper profile-work-strip-edit-button-wrapper" data-work-id="122305145"><a class="js-profile-work-strip-edit-button" tabindex="0"><span><i class="fa fa-pencil"></i></span><span>Edit</span></a></span></span><span id="work-strip-rankings-button-container"></span></div><div class="wp-workCard_item wp-workCard--stats"><span><span><span class="js-view-count view-count u-mr2x" data-work-id="122305145"><i class="fa fa-spinner fa-spin"></i></span><script>$(function () { var workId = 122305145; window.Academia.workViewCountsFetcher.queue(workId, function (count) { var description = window.$h.commaizeInt(count) + " " + window.$h.pluralize(count, 'View'); $(".js-view-count[data-work-id=122305145]").text(description); $(".js-view-count[data-work-id=122305145]").attr('title', description).tooltip(); }); });</script></span></span><span><span class="percentile-widget hidden"><span class="u-mr2x work-percentile"></span></span><script>$(function () { var workId = 122305145; window.Academia.workPercentilesFetcher.queue(workId, function (percentileText) { var container = $(".js-work-strip[data-work-id='122305145']"); container.find('.work-percentile').text(percentileText.charAt(0).toUpperCase() + percentileText.slice(1)); container.find('.percentile-widget').show(); container.find('.percentile-widget').removeClass('hidden'); }); });</script></span><span><script>$(function() { new Works.PaperRankView({ workId: 122305145, container: "", }); });</script></span></div><div id="work-strip-premium-row-container"></div></div></div><script> require.config({ waitSeconds: 90 })(["https://a.academia-assets.com/assets/wow_profile-f77ea15d77ce96025a6048a514272ad8becbad23c641fc2b3bd6e24ca6ff1932.js","https://a.academia-assets.com/assets/work_edit-ad038b8c047c1a8d4fa01b402d530ff93c45fee2137a149a4a5398bc8ad67560.js"], function() { // from javascript_helper.rb var dispatcherData = {} if (false){ window.WowProfile.dispatcher = window.WowProfile.dispatcher || _.clone(Backbone.Events); dispatcherData = { dispatcher: window.WowProfile.dispatcher, downloadLinkId: "-1" } } $('.js-work-strip[data-work-id=122305145]').each(function() { if (!$(this).data('initialized')) { new WowProfile.WorkStripView({ el: this, workJSON: {"id":122305145,"title":"An Expansion Series for Solving Improper Cylindrical Functions Occurring in Subsonic, Supersonic and Transonic Kernel Formulations","translated_title":"","metadata":{"abstract":"A brief survey of the kernel functions occurring in unsteady subsonic or supersonic lifting surface formulations is presented. The discussion will be focused on the solutions of the improper cylindrical function as a main part of the kernel function. A new expansion series is proposed as an exact solution to the improper integral and may be regarded as an extension of the Ueda series. The new solution offers a very simple and convenient form since the singular and regular parts are explicitly separated. The simple form of the singular functions is a key point which is particularly significant in simplifying the Mangler integration; hence this approach is shown to be useful in improving the accuracy of many planar and nonplanar lifting surface methods. Results are discussed and their accuracy is presented.","publisher":"Springer Nature","publication_date":{"day":null,"month":null,"year":1995,"errors":{}},"publication_name":"Springer eBooks"},"translated_abstract":"A brief survey of the kernel functions occurring in unsteady subsonic or supersonic lifting surface formulations is presented. The discussion will be focused on the solutions of the improper cylindrical function as a main part of the kernel function. A new expansion series is proposed as an exact solution to the improper integral and may be regarded as an extension of the Ueda series. The new solution offers a very simple and convenient form since the singular and regular parts are explicitly separated. The simple form of the singular functions is a key point which is particularly significant in simplifying the Mangler integration; hence this approach is shown to be useful in improving the accuracy of many planar and nonplanar lifting surface methods. Results are discussed and their accuracy is presented.","internal_url":"https://www.academia.edu/122305145/An_Expansion_Series_for_Solving_Improper_Cylindrical_Functions_Occurring_in_Subsonic_Supersonic_and_Transonic_Kernel_Formulations","translated_internal_url":"","created_at":"2024-07-23T22:14:42.548-07:00","preview_url":null,"current_user_can_edit":null,"current_user_is_owner":null,"owner_id":4040157,"coauthors_can_edit":true,"document_type":"paper","co_author_tags":[],"downloadable_attachments":[],"slug":"An_Expansion_Series_for_Solving_Improper_Cylindrical_Functions_Occurring_in_Subsonic_Supersonic_and_Transonic_Kernel_Formulations","translated_slug":"","page_count":null,"language":"en","content_type":"Work","owner":{"id":4040157,"first_name":"Harijono","middle_initials":"","last_name":"Djojodihardjo","page_name":"HarijonoDjojodihardjo","domain_name":"itb","created_at":"2013-05-03T11:27:42.148-07:00","display_name":"Harijono Djojodihardjo","url":"https://itb.academia.edu/HarijonoDjojodihardjo"},"attachments":[],"research_interests":[{"id":48,"name":"Engineering","url":"https://www.academia.edu/Documents/in/Engineering"},{"id":60,"name":"Mechanical Engineering","url":"https://www.academia.edu/Documents/in/Mechanical_Engineering"},{"id":88,"name":"Aerospace Engineering","url":"https://www.academia.edu/Documents/in/Aerospace_Engineering"},{"id":300,"name":"Mathematics","url":"https://www.academia.edu/Documents/in/Mathematics"},{"id":305,"name":"Applied Mathematics","url":"https://www.academia.edu/Documents/in/Applied_Mathematics"},{"id":422,"name":"Computer Science","url":"https://www.academia.edu/Documents/in/Computer_Science"},{"id":3641,"name":"Aeronautical Engineering","url":"https://www.academia.edu/Documents/in/Aeronautical_Engineering"},{"id":2657384,"name":"Taylor expansion series","url":"https://www.academia.edu/Documents/in/Taylor_expansion_series"},{"id":2778229,"name":"Supersonic speed","url":"https://www.academia.edu/Documents/in/Supersonic_speed"},{"id":3647879,"name":"Springer Ebooks","url":"https://www.academia.edu/Documents/in/Springer_Ebooks"}],"urls":[{"id":43662292,"url":"https://doi.org/10.1007/978-3-642-80001-6_38"}]}, dispatcherData: dispatcherData }); $(this).data('initialized', true); } }); $a.trackClickSource(".js-work-strip-work-link", "profile_work_strip") }); </script> <div class="js-work-strip profile--work_container" data-work-id="122305144"><div class="profile--work_thumbnail hidden-xs"><a class="js-work-strip-work-link" data-click-track="profile-work-strip-thumbnail" href="https://www.academia.edu/122305144/Aerospace_Technology_Green_Energy_System_Perspectives"><img alt="Research paper thumbnail of Aerospace Technology Green Energy System Perspectives" class="work-thumbnail" src="https://attachments.academia-assets.com/116998313/thumbnails/1.jpg" /></a></div><div class="wp-workCard wp-workCard_itemContainer"><div class="wp-workCard_item wp-workCard--title"><a class="js-work-strip-work-link text-gray-darker" data-click-track="profile-work-strip-title" href="https://www.academia.edu/122305144/Aerospace_Technology_Green_Energy_System_Perspectives">Aerospace Technology Green Energy System Perspectives</a></div><div class="wp-workCard_item"><span>DEStech Transactions on Environment, Energy and Earth Science</span><span>, Jan 10, 2017</span></div><div class="wp-workCard_item wp-workCard--actions"><span class="work-strip-bookmark-button-container"></span><a id="2e48c6cdf2de3a6a4d45e07cce09bd23" class="wp-workCard--action" rel="nofollow" data-click-track="profile-work-strip-download" data-download="{&quot;attachment_id&quot;:116998313,&quot;asset_id&quot;:122305144,&quot;asset_type&quot;:&quot;Work&quot;,&quot;button_location&quot;:&quot;profile&quot;}" href="https://www.academia.edu/attachments/116998313/download_file?st=MTczMzAzMTQwNiw4LjIyMi4yMDguMTQ2&s=profile"><span><i class="fa fa-arrow-down"></i></span><span>Download</span></a><span class="wp-workCard--action visible-if-viewed-by-owner inline-block" style="display: none;"><span class="js-profile-work-strip-edit-button-wrapper profile-work-strip-edit-button-wrapper" data-work-id="122305144"><a class="js-profile-work-strip-edit-button" tabindex="0"><span><i class="fa fa-pencil"></i></span><span>Edit</span></a></span></span><span id="work-strip-rankings-button-container"></span></div><div class="wp-workCard_item wp-workCard--stats"><span><span><span class="js-view-count view-count u-mr2x" data-work-id="122305144"><i class="fa fa-spinner fa-spin"></i></span><script>$(function () { var workId = 122305144; 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$(this).data('initialized', true); } }); $a.trackClickSource(".js-work-strip-work-link", "profile_work_strip") }); </script> <div class="js-work-strip profile--work_container" data-work-id="122305142"><div class="profile--work_thumbnail hidden-xs"><a class="js-work-strip-work-link" data-click-track="profile-work-strip-thumbnail" href="https://www.academia.edu/122305142/CFD_Simulation_of_Coand%C4%83_Effect_on_the_Upper_Respiratory_System"><img alt="Research paper thumbnail of CFD Simulation of Coandă Effect on the Upper Respiratory System" class="work-thumbnail" src="https://a.academia-assets.com/images/blank-paper.jpg" /></a></div><div class="wp-workCard wp-workCard_itemContainer"><div class="wp-workCard_item wp-workCard--title"><a class="js-work-strip-work-link text-gray-darker" data-click-track="profile-work-strip-title" href="https://www.academia.edu/122305142/CFD_Simulation_of_Coand%C4%83_Effect_on_the_Upper_Respiratory_System">CFD Simulation of Coandă Effect on the Upper Respiratory System</a></div><div class="wp-workCard_item"><span>Journal of Medical Imaging and Health Informatics</span><span>, Oct 1, 2016</span></div><div class="wp-workCard_item"><span class="js-work-more-abstract-truncated">Based on the authors’ various studies on Coandă effect, the present study is devoted to focus on ...</span><a class="js-work-more-abstract" data-broccoli-component="work_strip.more_abstract" data-click-track="profile-work-strip-more-abstract" href="javascript:;"><span> more </span><span><i class="fa fa-caret-down"></i></span></a><span class="js-work-more-abstract-untruncated hidden">Based on the authors’ various studies on Coandă effect, the present study is devoted to focus on the development and influence of Coandă effect on the flow along a conduit with constriction representing the upper respiratory system of the human body, including the constriction dynamics and aerodynamics that may prevail there. For this purpose, theoretical analyses as well as CFD simulation are being carried out. Comparison of the results obtained with other medical based studies has exhibited striking similarities and are assessed for their physical significance.</span></div><div class="wp-workCard_item wp-workCard--actions"><span class="work-strip-bookmark-button-container"></span><span class="wp-workCard--action visible-if-viewed-by-owner inline-block" style="display: none;"><span class="js-profile-work-strip-edit-button-wrapper profile-work-strip-edit-button-wrapper" data-work-id="122305142"><a class="js-profile-work-strip-edit-button" tabindex="0"><span><i class="fa fa-pencil"></i></span><span>Edit</span></a></span></span><span id="work-strip-rankings-button-container"></span></div><div class="wp-workCard_item wp-workCard--stats"><span><span><span class="js-view-count view-count u-mr2x" data-work-id="122305142"><i class="fa fa-spinner fa-spin"></i></span><script>$(function () { var workId = 122305142; window.Academia.workViewCountsFetcher.queue(workId, function (count) { var description = window.$h.commaizeInt(count) + " " + window.$h.pluralize(count, 'View'); $(".js-view-count[data-work-id=122305142]").text(description); $(".js-view-count[data-work-id=122305142]").attr('title', description).tooltip(); }); });</script></span></span><span><span class="percentile-widget hidden"><span class="u-mr2x work-percentile"></span></span><script>$(function () { var workId = 122305142; window.Academia.workPercentilesFetcher.queue(workId, function (percentileText) { var container = $(".js-work-strip[data-work-id='122305142']"); container.find('.work-percentile').text(percentileText.charAt(0).toUpperCase() + percentileText.slice(1)); container.find('.percentile-widget').show(); container.find('.percentile-widget').removeClass('hidden'); }); });</script></span><span><script>$(function() { new Works.PaperRankView({ workId: 122305142, container: "", }); });</script></span></div><div id="work-strip-premium-row-container"></div></div></div><script> require.config({ waitSeconds: 90 })(["https://a.academia-assets.com/assets/wow_profile-f77ea15d77ce96025a6048a514272ad8becbad23c641fc2b3bd6e24ca6ff1932.js","https://a.academia-assets.com/assets/work_edit-ad038b8c047c1a8d4fa01b402d530ff93c45fee2137a149a4a5398bc8ad67560.js"], function() { // from javascript_helper.rb var dispatcherData = {} if (false){ window.WowProfile.dispatcher = window.WowProfile.dispatcher || _.clone(Backbone.Events); dispatcherData = { dispatcher: window.WowProfile.dispatcher, downloadLinkId: "-1" } } $('.js-work-strip[data-work-id=122305142]').each(function() { if (!$(this).data('initialized')) { new WowProfile.WorkStripView({ el: this, workJSON: {"id":122305142,"title":"CFD Simulation of Coandă Effect on the Upper Respiratory System","translated_title":"","metadata":{"abstract":"Based on the authors’ various studies on Coandă effect, the present study is devoted to focus on the development and influence of Coandă effect on the flow along a conduit with constriction representing the upper respiratory system of the human body, including the constriction dynamics and aerodynamics that may prevail there. 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Mobility: The Technical Challenge; Proceedings of the Fourth International Pacific Conference on Automotive Engineering, Melbourne, Australia, November 8-14, 1987. Volumes 1 to 3" class="work-thumbnail" src="https://a.academia-assets.com/images/blank-paper.jpg" /></a></div><div class="wp-workCard wp-workCard_itemContainer"><div class="wp-workCard_item wp-workCard--title"><a class="js-work-strip-work-link text-gray-darker" data-click-track="profile-work-strip-title" href="https://www.academia.edu/122305141/An_Analytical_Study_of_Small_Commercial_Vehicle_Stability_Mobility_The_Technical_Challenge_Proceedings_of_the_Fourth_International_Pacific_Conference_on_Automotive_Engineering_Melbourne_Australia_November_8_14_1987_Volumes_1_to_3">An Analytical Study of Small Commercial Vehicle Stability. Mobility: The Technical Challenge; Proceedings of the Fourth International Pacific Conference on Automotive Engineering, Melbourne, Australia, November 8-14, 1987. Volumes 1 to 3</a></div><div class="wp-workCard_item"><span>Publication of: Society of Automotive Engineers</span><span>, 1987</span></div><div class="wp-workCard_item"><span class="js-work-more-abstract-truncated">An analysis of lateral and directional steady state stability of a typical small commercial vehic...</span><a class="js-work-more-abstract" data-broccoli-component="work_strip.more_abstract" data-click-track="profile-work-strip-more-abstract" href="javascript:;"><span> more </span><span><i class="fa fa-caret-down"></i></span></a><span class="js-work-more-abstract-untruncated hidden">An analysis of lateral and directional steady state stability of a typical small commercial vehicle configuration is performed limiting the movement to three degrees of freedom: side slipping, yawing and rolling. Based on the analysis, a parametric study is performed to investigate the influence of some design and operational parameters, in order to arrive at some design guidelines. SAE paper no 871182. (Author/TRRL)</span></div><div class="wp-workCard_item wp-workCard--actions"><span class="work-strip-bookmark-button-container"></span><span class="wp-workCard--action visible-if-viewed-by-owner inline-block" style="display: none;"><span class="js-profile-work-strip-edit-button-wrapper profile-work-strip-edit-button-wrapper" data-work-id="122305141"><a class="js-profile-work-strip-edit-button" tabindex="0"><span><i class="fa fa-pencil"></i></span><span>Edit</span></a></span></span><span id="work-strip-rankings-button-container"></span></div><div class="wp-workCard_item wp-workCard--stats"><span><span><span class="js-view-count view-count u-mr2x" data-work-id="122305141"><i class="fa fa-spinner fa-spin"></i></span><script>$(function () { var workId = 122305141; window.Academia.workViewCountsFetcher.queue(workId, function (count) { var description = window.$h.commaizeInt(count) + " " + window.$h.pluralize(count, 'View'); $(".js-view-count[data-work-id=122305141]").text(description); $(".js-view-count[data-work-id=122305141]").attr('title', description).tooltip(); }); });</script></span></span><span><span class="percentile-widget hidden"><span class="u-mr2x work-percentile"></span></span><script>$(function () { var workId = 122305141; window.Academia.workPercentilesFetcher.queue(workId, function (percentileText) { var container = $(".js-work-strip[data-work-id='122305141']"); container.find('.work-percentile').text(percentileText.charAt(0).toUpperCase() + percentileText.slice(1)); container.find('.percentile-widget').show(); container.find('.percentile-widget').removeClass('hidden'); }); });</script></span><span><script>$(function() { new Works.PaperRankView({ workId: 122305141, container: "", }); });</script></span></div><div id="work-strip-premium-row-container"></div></div></div><script> require.config({ waitSeconds: 90 })(["https://a.academia-assets.com/assets/wow_profile-f77ea15d77ce96025a6048a514272ad8becbad23c641fc2b3bd6e24ca6ff1932.js","https://a.academia-assets.com/assets/work_edit-ad038b8c047c1a8d4fa01b402d530ff93c45fee2137a149a4a5398bc8ad67560.js"], function() { // from javascript_helper.rb var dispatcherData = {} if (false){ window.WowProfile.dispatcher = window.WowProfile.dispatcher || _.clone(Backbone.Events); dispatcherData = { dispatcher: window.WowProfile.dispatcher, downloadLinkId: "-1" } } $('.js-work-strip[data-work-id=122305141]').each(function() { if (!$(this).data('initialized')) { new WowProfile.WorkStripView({ el: this, workJSON: {"id":122305141,"title":"An Analytical Study of Small Commercial Vehicle Stability. Mobility: The Technical Challenge; Proceedings of the Fourth International Pacific Conference on Automotive Engineering, Melbourne, Australia, November 8-14, 1987. Volumes 1 to 3","translated_title":"","metadata":{"abstract":"An analysis of lateral and directional steady state stability of a typical small commercial vehicle configuration is performed limiting the movement to three degrees of freedom: side slipping, yawing and rolling. Based on the analysis, a parametric study is performed to investigate the influence of some design and operational parameters, in order to arrive at some design guidelines. SAE paper no 871182. (Author/TRRL)","publication_date":{"day":null,"month":null,"year":1987,"errors":{}},"publication_name":"Publication of: Society of Automotive Engineers"},"translated_abstract":"An analysis of lateral and directional steady state stability of a typical small commercial vehicle configuration is performed limiting the movement to three degrees of freedom: side slipping, yawing and rolling. Based on the analysis, a parametric study is performed to investigate the influence of some design and operational parameters, in order to arrive at some design guidelines. SAE paper no 871182. (Author/TRRL)","internal_url":"https://www.academia.edu/122305141/An_Analytical_Study_of_Small_Commercial_Vehicle_Stability_Mobility_The_Technical_Challenge_Proceedings_of_the_Fourth_International_Pacific_Conference_on_Automotive_Engineering_Melbourne_Australia_November_8_14_1987_Volumes_1_to_3","translated_internal_url":"","created_at":"2024-07-23T22:14:41.688-07:00","preview_url":null,"current_user_can_edit":null,"current_user_is_owner":null,"owner_id":4040157,"coauthors_can_edit":true,"document_type":"paper","co_author_tags":[],"downloadable_attachments":[],"slug":"An_Analytical_Study_of_Small_Commercial_Vehicle_Stability_Mobility_The_Technical_Challenge_Proceedings_of_the_Fourth_International_Pacific_Conference_on_Automotive_Engineering_Melbourne_Australia_November_8_14_1987_Volumes_1_to_3","translated_slug":"","page_count":null,"language":"en","content_type":"Work","owner":{"id":4040157,"first_name":"Harijono","middle_initials":"","last_name":"Djojodihardjo","page_name":"HarijonoDjojodihardjo","domain_name":"itb","created_at":"2013-05-03T11:27:42.148-07:00","display_name":"Harijono Djojodihardjo","url":"https://itb.academia.edu/HarijonoDjojodihardjo"},"attachments":[],"research_interests":[{"id":48,"name":"Engineering","url":"https://www.academia.edu/Documents/in/Engineering"},{"id":18873,"name":"Automotive Industry","url":"https://www.academia.edu/Documents/in/Automotive_Industry"},{"id":3834490,"name":"Limiting","url":"https://www.academia.edu/Documents/in/Limiting"},{"id":4080683,"name":"slipping","url":"https://www.academia.edu/Documents/in/slipping"}],"urls":[{"id":43662288,"url":"https://trid.trb.org/view/284967"}]}, dispatcherData: dispatcherData }); $(this).data('initialized', true); } }); $a.trackClickSource(".js-work-strip-work-link", "profile_work_strip") }); </script> <div class="js-work-strip profile--work_container" data-work-id="122305140"><div class="profile--work_thumbnail hidden-xs"><a class="js-work-strip-work-link" data-click-track="profile-work-strip-thumbnail" href="https://www.academia.edu/122305140/Unified_Aerodynamic_Acoustic_Formulation_for_Aero_Acoustic_Structure_Coupling"><img alt="Research paper thumbnail of Unified Aerodynamic-Acoustic Formulation for Aero-Acoustic Structure Coupling" class="work-thumbnail" src="https://a.academia-assets.com/images/blank-paper.jpg" /></a></div><div class="wp-workCard wp-workCard_itemContainer"><div class="wp-workCard_item wp-workCard--title"><a class="js-work-strip-work-link text-gray-darker" data-click-track="profile-work-strip-title" href="https://www.academia.edu/122305140/Unified_Aerodynamic_Acoustic_Formulation_for_Aero_Acoustic_Structure_Coupling">Unified Aerodynamic-Acoustic Formulation for Aero-Acoustic Structure Coupling</a></div><div class="wp-workCard_item"><span>Journal of mechanics engineering and automation</span><span>, Apr 28, 2013</span></div><div class="wp-workCard_item wp-workCard--actions"><span class="work-strip-bookmark-button-container"></span><span class="wp-workCard--action visible-if-viewed-by-owner inline-block" style="display: none;"><span class="js-profile-work-strip-edit-button-wrapper profile-work-strip-edit-button-wrapper" data-work-id="122305140"><a class="js-profile-work-strip-edit-button" tabindex="0"><span><i class="fa fa-pencil"></i></span><span>Edit</span></a></span></span><span id="work-strip-rankings-button-container"></span></div><div class="wp-workCard_item wp-workCard--stats"><span><span><span class="js-view-count view-count u-mr2x" data-work-id="122305140"><i class="fa fa-spinner fa-spin"></i></span><script>$(function () { var workId = 122305140; window.Academia.workViewCountsFetcher.queue(workId, function (count) { var description = window.$h.commaizeInt(count) + " " + window.$h.pluralize(count, 'View'); $(".js-view-count[data-work-id=122305140]").text(description); $(".js-view-count[data-work-id=122305140]").attr('title', description).tooltip(); }); });</script></span></span><span><span class="percentile-widget hidden"><span class="u-mr2x work-percentile"></span></span><script>$(function () { var workId = 122305140; window.Academia.workPercentilesFetcher.queue(workId, function (percentileText) { var container = $(".js-work-strip[data-work-id='122305140']"); container.find('.work-percentile').text(percentileText.charAt(0).toUpperCase() + percentileText.slice(1)); container.find('.percentile-widget').show(); container.find('.percentile-widget').removeClass('hidden'); }); });</script></span><span><script>$(function() { new Works.PaperRankView({ workId: 122305140, container: "", }); });</script></span></div><div id="work-strip-premium-row-container"></div></div></div><script> require.config({ waitSeconds: 90 })(["https://a.academia-assets.com/assets/wow_profile-f77ea15d77ce96025a6048a514272ad8becbad23c641fc2b3bd6e24ca6ff1932.js","https://a.academia-assets.com/assets/work_edit-ad038b8c047c1a8d4fa01b402d530ff93c45fee2137a149a4a5398bc8ad67560.js"], function() { // from javascript_helper.rb var dispatcherData = {} if (false){ window.WowProfile.dispatcher = window.WowProfile.dispatcher || _.clone(Backbone.Events); 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$(this).data('initialized', true); } }); $a.trackClickSource(".js-work-strip-work-link", "profile_work_strip") }); </script> </div><div class="profile--tab_content_container js-tab-pane tab-pane" data-section-id="5360162" id="conferencepresentations"><div class="js-work-strip profile--work_container" data-work-id="100151022"><div class="profile--work_thumbnail hidden-xs"><a class="js-work-strip-work-link" data-click-track="profile-work-strip-thumbnail" href="https://www.academia.edu/100151022/SUMBER_DAYA_NUKLIR_PADA_WAHANA_ANTARIKSA"><img alt="Research paper thumbnail of SUMBER DAYA NUKLIR PADA WAHANA ANTARIKSA" class="work-thumbnail" src="https://attachments.academia-assets.com/101053274/thumbnails/1.jpg" /></a></div><div class="wp-workCard wp-workCard_itemContainer"><div class="wp-workCard_item wp-workCard--title"><a class="js-work-strip-work-link text-gray-darker" data-click-track="profile-work-strip-title" href="https://www.academia.edu/100151022/SUMBER_DAYA_NUKLIR_PADA_WAHANA_ANTARIKSA">SUMBER DAYA NUKLIR PADA WAHANA ANTARIKSA</a></div><div class="wp-workCard_item"><span>Internal Reports of LAPAN (Indonesian Space Agency) and Aerospace Engineering Department at Institut Teknologi Bandung</span><span>, 2017</span></div><div class="wp-workCard_item"><span class="js-work-more-abstract-truncated">Ringkasan Masalah penggunaan sumber daya nuklir pada wahana antariksa telah menark perhatian bany...</span><a class="js-work-more-abstract" data-broccoli-component="work_strip.more_abstract" data-click-track="profile-work-strip-more-abstract" href="javascript:;"><span> more </span><span><i class="fa fa-caret-down"></i></span></a><span class="js-work-more-abstract-untruncated hidden">Ringkasan<br />Masalah penggunaan sumber daya nuklir pada wahana antariksa telah menark perhatian banyak negara di dunia, berkaitan dengan keprihatinan terhadap kejatuhan pecahan satelit yang bersifat radio aktif. Untuk memahami lingkup bahaya yang mungkin timbul, akan dibahas aspek penggunaan sumber daya nuklir pada wahana antariksa.<br /><br />Abstract<br />The issue of nuclear power source in space vehile has drawn concern of many countries for the possibility of their space debris during failure or decommissionimng and other related nuclear contamination that may affect the earth environment. To this end and to gain further knowledge on this issue, various aspects on the use of nuclear power in spacecrafts to date are elaborated.</span></div><div class="wp-workCard_item wp-workCard--actions"><span class="work-strip-bookmark-button-container"></span><a id="f4143502d7bf5b16d1658b4df410ab9f" class="wp-workCard--action" rel="nofollow" data-click-track="profile-work-strip-download" data-download="{&quot;attachment_id&quot;:101053274,&quot;asset_id&quot;:100151022,&quot;asset_type&quot;:&quot;Work&quot;,&quot;button_location&quot;:&quot;profile&quot;}" href="https://www.academia.edu/attachments/101053274/download_file?st=MTczMzAzMTQwNiw4LjIyMi4yMDguMTQ2&s=profile"><span><i class="fa fa-arrow-down"></i></span><span>Download</span></a><span class="wp-workCard--action visible-if-viewed-by-owner inline-block" style="display: none;"><span class="js-profile-work-strip-edit-button-wrapper profile-work-strip-edit-button-wrapper" data-work-id="100151022"><a class="js-profile-work-strip-edit-button" tabindex="0"><span><i class="fa fa-pencil"></i></span><span>Edit</span></a></span></span><span id="work-strip-rankings-button-container"></span></div><div class="wp-workCard_item wp-workCard--stats"><span><span><span class="js-view-count view-count u-mr2x" data-work-id="100151022"><i class="fa fa-spinner fa-spin"></i></span><script>$(function () { var workId = 100151022; window.Academia.workViewCountsFetcher.queue(workId, function (count) { var description = window.$h.commaizeInt(count) + " " + window.$h.pluralize(count, 'View'); $(".js-view-count[data-work-id=100151022]").text(description); $(".js-view-count[data-work-id=100151022]").attr('title', description).tooltip(); }); });</script></span></span><span><span class="percentile-widget hidden"><span class="u-mr2x work-percentile"></span></span><script>$(function () { var workId = 100151022; window.Academia.workPercentilesFetcher.queue(workId, function (percentileText) { var container = $(".js-work-strip[data-work-id='100151022']"); container.find('.work-percentile').text(percentileText.charAt(0).toUpperCase() + percentileText.slice(1)); container.find('.percentile-widget').show(); container.find('.percentile-widget').removeClass('hidden'); }); });</script></span><span><script>$(function() { new Works.PaperRankView({ workId: 100151022, container: "", }); });</script></span></div><div id="work-strip-premium-row-container"></div></div></div><script> require.config({ waitSeconds: 90 })(["https://a.academia-assets.com/assets/wow_profile-f77ea15d77ce96025a6048a514272ad8becbad23c641fc2b3bd6e24ca6ff1932.js","https://a.academia-assets.com/assets/work_edit-ad038b8c047c1a8d4fa01b402d530ff93c45fee2137a149a4a5398bc8ad67560.js"], function() { // from javascript_helper.rb var dispatcherData = {} if (true){ window.WowProfile.dispatcher = window.WowProfile.dispatcher || _.clone(Backbone.Events); dispatcherData = { dispatcher: window.WowProfile.dispatcher, downloadLinkId: "f4143502d7bf5b16d1658b4df410ab9f" } } $('.js-work-strip[data-work-id=100151022]').each(function() { if (!$(this).data('initialized')) { new WowProfile.WorkStripView({ el: this, workJSON: {"id":100151022,"title":"SUMBER DAYA NUKLIR PADA WAHANA ANTARIKSA","translated_title":"","metadata":{"abstract":"Ringkasan\nMasalah penggunaan sumber daya nuklir pada wahana antariksa telah menark perhatian banyak negara di dunia, berkaitan dengan keprihatinan terhadap kejatuhan pecahan satelit yang bersifat radio aktif. Untuk memahami lingkup bahaya yang mungkin timbul, akan dibahas aspek penggunaan sumber daya nuklir pada wahana antariksa.\n\nAbstract\nThe issue of nuclear power source in space vehile has drawn concern of many countries for the possibility of their space debris during failure or decommissionimng and other related nuclear contamination that may affect the earth environment. To this end and to gain further knowledge on this issue, various aspects on the use of nuclear power in spacecrafts to date are elaborated.","publication_date":{"day":null,"month":null,"year":2017,"errors":{}},"publication_name":"Internal Reports of LAPAN (Indonesian Space Agency) and Aerospace Engineering Department at Institut Teknologi Bandung"},"translated_abstract":"Ringkasan\nMasalah penggunaan sumber daya nuklir pada wahana antariksa telah menark perhatian banyak negara di dunia, berkaitan dengan keprihatinan terhadap kejatuhan pecahan satelit yang bersifat radio aktif. Untuk memahami lingkup bahaya yang mungkin timbul, akan dibahas aspek penggunaan sumber daya nuklir pada wahana antariksa.\n\nAbstract\nThe issue of nuclear power source in space vehile has drawn concern of many countries for the possibility of their space debris during failure or decommissionimng and other related nuclear contamination that may affect the earth environment. To this end and to gain further knowledge on this issue, various aspects on the use of nuclear power in spacecrafts to date are elaborated.","internal_url":"https://www.academia.edu/100151022/SUMBER_DAYA_NUKLIR_PADA_WAHANA_ANTARIKSA","translated_internal_url":"","created_at":"2023-04-13T09:45:31.219-07:00","preview_url":null,"current_user_can_edit":null,"current_user_is_owner":null,"owner_id":4040157,"coauthors_can_edit":true,"document_type":"draft","co_author_tags":[{"id":39746787,"work_id":100151022,"tagging_user_id":4040157,"tagged_user_id":null,"co_author_invite_id":3223809,"email":"h***o@yahoo.co.id","display_order":1,"name":"Harijono Djojodihardjo","title":"SUMBER DAYA NUKLIR PADA WAHANA ANTARIKSA"}],"downloadable_attachments":[{"id":101053274,"title":"","file_type":"pdf","scribd_thumbnail_url":"https://attachments.academia-assets.com/101053274/thumbnails/1.jpg","file_name":"Harijono_Djojodihardjo_SUMBER_DAYA_NUKLIR_PADA_WAHANA_ANTARIKSA_2017_unpublished.pdf","download_url":"https://www.academia.edu/attachments/101053274/download_file?st=MTczMzAzMTQwNiw4LjIyMi4yMDguMTQ2&","bulk_download_file_name":"SUMBER_DAYA_NUKLIR_PADA_WAHANA_ANTARIKSA.pdf","bulk_download_url":"https://d1wqtxts1xzle7.cloudfront.net/101053274/Harijono_Djojodihardjo_SUMBER_DAYA_NUKLIR_PADA_WAHANA_ANTARIKSA_2017_unpublished-libre.pdf?1681406193=\u0026response-content-disposition=attachment%3B+filename%3DSUMBER_DAYA_NUKLIR_PADA_WAHANA_ANTARIKSA.pdf\u0026Expires=1732987661\u0026Signature=QEopoV0i5Tgvb807uCS0L6KatcorO8qz6beLpCWrriHHd8fY~JipYqWYJ2k5IL5lpzvkyIhR4-WAWzalO81syPwoygA9~A6MrN9DU-6UdLznbrIX82i03Z-u02Iz8WxJ0VhxIM7uE3w5Lsd~VS4AGzl7Q1yFOUHB3NnwtR4bB~-LCMpG3MAdYiTarDqdkjycfMg9EIWEpmFWD4MKp6Gul3Fr1EwAGu0IF9H2JTsDGjJ4qrcOYl2dprBkRWmeggrrpd5RhQu0~dZ~tqvfvkQ1QceR8tnUxUT7B4iJTR6Q2wIcIabgcjss5byDxw8YnozEr5cpimBaO9QPOJ5PW19V6w__\u0026Key-Pair-Id=APKAJLOHF5GGSLRBV4ZA"}],"slug":"SUMBER_DAYA_NUKLIR_PADA_WAHANA_ANTARIKSA","translated_slug":"","page_count":8,"language":"en","content_type":"Work","owner":{"id":4040157,"first_name":"Harijono","middle_initials":"","last_name":"Djojodihardjo","page_name":"HarijonoDjojodihardjo","domain_name":"itb","created_at":"2013-05-03T11:27:42.148-07:00","display_name":"Harijono Djojodihardjo","url":"https://itb.academia.edu/HarijonoDjojodihardjo"},"attachments":[{"id":101053274,"title":"","file_type":"pdf","scribd_thumbnail_url":"https://attachments.academia-assets.com/101053274/thumbnails/1.jpg","file_name":"Harijono_Djojodihardjo_SUMBER_DAYA_NUKLIR_PADA_WAHANA_ANTARIKSA_2017_unpublished.pdf","download_url":"https://www.academia.edu/attachments/101053274/download_file?st=MTczMzAzMTQwNiw4LjIyMi4yMDguMTQ2&","bulk_download_file_name":"SUMBER_DAYA_NUKLIR_PADA_WAHANA_ANTARIKSA.pdf","bulk_download_url":"https://d1wqtxts1xzle7.cloudfront.net/101053274/Harijono_Djojodihardjo_SUMBER_DAYA_NUKLIR_PADA_WAHANA_ANTARIKSA_2017_unpublished-libre.pdf?1681406193=\u0026response-content-disposition=attachment%3B+filename%3DSUMBER_DAYA_NUKLIR_PADA_WAHANA_ANTARIKSA.pdf\u0026Expires=1732987661\u0026Signature=QEopoV0i5Tgvb807uCS0L6KatcorO8qz6beLpCWrriHHd8fY~JipYqWYJ2k5IL5lpzvkyIhR4-WAWzalO81syPwoygA9~A6MrN9DU-6UdLznbrIX82i03Z-u02Iz8WxJ0VhxIM7uE3w5Lsd~VS4AGzl7Q1yFOUHB3NnwtR4bB~-LCMpG3MAdYiTarDqdkjycfMg9EIWEpmFWD4MKp6Gul3Fr1EwAGu0IF9H2JTsDGjJ4qrcOYl2dprBkRWmeggrrpd5RhQu0~dZ~tqvfvkQ1QceR8tnUxUT7B4iJTR6Q2wIcIabgcjss5byDxw8YnozEr5cpimBaO9QPOJ5PW19V6w__\u0026Key-Pair-Id=APKAJLOHF5GGSLRBV4ZA"}],"research_interests":[{"id":88,"name":"Aerospace Engineering","url":"https://www.academia.edu/Documents/in/Aerospace_Engineering"},{"id":305,"name":"Applied Mathematics","url":"https://www.academia.edu/Documents/in/Applied_Mathematics"},{"id":10875,"name":"Aerodynamics","url":"https://www.academia.edu/Documents/in/Aerodynamics"},{"id":54256,"name":"System Analysis and Design","url":"https://www.academia.edu/Documents/in/System_Analysis_and_Design"},{"id":1003114,"name":"Applied and Computational Mechanics","url":"https://www.academia.edu/Documents/in/Applied_and_Computational_Mechanics"}],"urls":[]}, dispatcherData: dispatcherData }); $(this).data('initialized', true); } }); $a.trackClickSource(".js-work-strip-work-link", "profile_work_strip") }); </script> <div class="js-work-strip profile--work_container" data-work-id="98036038"><div class="profile--work_thumbnail hidden-xs"><a class="js-work-strip-work-link" data-click-track="profile-work-strip-thumbnail" href="https://www.academia.edu/98036038/Development_and_application_of_semi_analytically_modified_transfer_matrix_method_for_structural_dynamic_analysis_of_arbitrary_structure_Conference_Paper"><img alt="Research paper thumbnail of Development and application of semi-analytically modified transfer matrix method for structural dynamic analysis of arbitrary structure (Conference Paper" class="work-thumbnail" src="https://attachments.academia-assets.com/99497077/thumbnails/1.jpg" /></a></div><div class="wp-workCard wp-workCard_itemContainer"><div class="wp-workCard_item wp-workCard--title"><a class="js-work-strip-work-link text-gray-darker" data-click-track="profile-work-strip-title" href="https://www.academia.edu/98036038/Development_and_application_of_semi_analytically_modified_transfer_matrix_method_for_structural_dynamic_analysis_of_arbitrary_structure_Conference_Paper">Development and application of semi-analytically modified transfer matrix method for structural dynamic analysis of arbitrary structure (Conference Paper</a></div><div class="wp-workCard_item"><span>Proceedings of the 6th International Pacific Conference on Automotive Engingeering 1991, Pages 1141-1153 Proceedings of the 6th International Pacific Conference on Automotive Engingeering; Seoul, South Korea; ; 28 October 1991 through 1 November 1991; Code 16333</span><span>, 1991</span></div><div class="wp-workCard_item"><span class="js-work-more-abstract-truncated">Structural dynamic analysis of an arbitrary structure such as vehicle structure can be carried ou...</span><a class="js-work-more-abstract" data-broccoli-component="work_strip.more_abstract" data-click-track="profile-work-strip-more-abstract" href="javascript:;"><span> more </span><span><i class="fa fa-caret-down"></i></span></a><span class="js-work-more-abstract-untruncated hidden">Structural dynamic analysis of an arbitrary structure such as vehicle structure can be carried out using finite element method or other numerically oriented approaches. Analytical approach is usually preferred due to its convenience for parametric studies, however such an approach can usually be followed for limited class of geometries only. In the present work, a method which was proposed by Barboni, Gaudenzi, Mannini and Santini, which modified the well known transfer matrix method by expanding the governing differential equations for the structural state vector into a power series, with the power related to the eigenvalues of the dynamic eigenvalue problem, is followed and rederived. The procedure is first applied to basic bending and torsional oscillation of beams, and the results are compared to analytical solution. Next the problem of structure with arbitrary geometry is analysed. For this purpose, the bending oscillation of non-prismatic beam is considered. Previous formulation can readily be applied for piecewise continuous approximation to the structure.</span></div><div class="wp-workCard_item wp-workCard--actions"><span class="work-strip-bookmark-button-container"></span><a id="77033d4b76bec0c5853e85a2fe00feb1" class="wp-workCard--action" rel="nofollow" data-click-track="profile-work-strip-download" data-download="{&quot;attachment_id&quot;:99497077,&quot;asset_id&quot;:98036038,&quot;asset_type&quot;:&quot;Work&quot;,&quot;button_location&quot;:&quot;profile&quot;}" href="https://www.academia.edu/attachments/99497077/download_file?st=MTczMzAzMTQwNiw4LjIyMi4yMDguMTQ2&s=profile"><span><i class="fa fa-arrow-down"></i></span><span>Download</span></a><span class="wp-workCard--action visible-if-viewed-by-owner inline-block" style="display: none;"><span class="js-profile-work-strip-edit-button-wrapper profile-work-strip-edit-button-wrapper" data-work-id="98036038"><a class="js-profile-work-strip-edit-button" tabindex="0"><span><i class="fa fa-pencil"></i></span><span>Edit</span></a></span></span><span id="work-strip-rankings-button-container"></span></div><div class="wp-workCard_item wp-workCard--stats"><span><span><span class="js-view-count view-count u-mr2x" data-work-id="98036038"><i class="fa fa-spinner fa-spin"></i></span><script>$(function () { var workId = 98036038; window.Academia.workViewCountsFetcher.queue(workId, function (count) { var description = window.$h.commaizeInt(count) + " " + window.$h.pluralize(count, 'View'); $(".js-view-count[data-work-id=98036038]").text(description); $(".js-view-count[data-work-id=98036038]").attr('title', description).tooltip(); }); });</script></span></span><span><span class="percentile-widget hidden"><span class="u-mr2x work-percentile"></span></span><script>$(function () { var workId = 98036038; window.Academia.workPercentilesFetcher.queue(workId, function (percentileText) { var container = $(".js-work-strip[data-work-id='98036038']"); container.find('.work-percentile').text(percentileText.charAt(0).toUpperCase() + percentileText.slice(1)); container.find('.percentile-widget').show(); container.find('.percentile-widget').removeClass('hidden'); }); });</script></span><span><script>$(function() { new Works.PaperRankView({ workId: 98036038, container: "", }); });</script></span></div><div id="work-strip-premium-row-container"></div></div></div><script> require.config({ waitSeconds: 90 })(["https://a.academia-assets.com/assets/wow_profile-f77ea15d77ce96025a6048a514272ad8becbad23c641fc2b3bd6e24ca6ff1932.js","https://a.academia-assets.com/assets/work_edit-ad038b8c047c1a8d4fa01b402d530ff93c45fee2137a149a4a5398bc8ad67560.js"], function() { // from javascript_helper.rb var dispatcherData = {} if (true){ window.WowProfile.dispatcher = window.WowProfile.dispatcher || _.clone(Backbone.Events); dispatcherData = { dispatcher: window.WowProfile.dispatcher, downloadLinkId: "77033d4b76bec0c5853e85a2fe00feb1" } } $('.js-work-strip[data-work-id=98036038]').each(function() { if (!$(this).data('initialized')) { new WowProfile.WorkStripView({ el: this, workJSON: {"id":98036038,"title":"Development and application of semi-analytically modified transfer matrix method for structural dynamic analysis of arbitrary structure (Conference Paper","translated_title":"","metadata":{"abstract":"Structural dynamic analysis of an arbitrary structure such as vehicle structure can be carried out using finite element method or other numerically oriented approaches. Analytical approach is usually preferred due to its convenience for parametric studies, however such an approach can usually be followed for limited class of geometries only. In the present work, a method which was proposed by Barboni, Gaudenzi, Mannini and Santini, which modified the well known transfer matrix method by expanding the governing differential equations for the structural state vector into a power series, with the power related to the eigenvalues of the dynamic eigenvalue problem, is followed and rederived. The procedure is first applied to basic bending and torsional oscillation of beams, and the results are compared to analytical solution. Next the problem of structure with arbitrary geometry is analysed. For this purpose, the bending oscillation of non-prismatic beam is considered. 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$(this).data('initialized', true); } }); $a.trackClickSource(".js-work-strip-work-link", "profile_work_strip") }); </script> <div class="js-work-strip profile--work_container" data-work-id="34985925"><div class="profile--work_thumbnail hidden-xs"><a class="js-work-strip-work-link" data-click-track="profile-work-strip-thumbnail" href="https://www.academia.edu/34985925/Vibration_Analysis_and_Control_of_a_Piezoelectric_Elements_Bonded_Flexural_Torsional_Beam"><img alt="Research paper thumbnail of Vibration Analysis and Control of a Piezoelectric Elements Bonded Flexural-Torsional Beam" class="work-thumbnail" src="https://attachments.academia-assets.com/54849948/thumbnails/1.jpg" /></a></div><div class="wp-workCard wp-workCard_itemContainer"><div class="wp-workCard_item wp-workCard--title"><a class="js-work-strip-work-link text-gray-darker" data-click-track="profile-work-strip-title" href="https://www.academia.edu/34985925/Vibration_Analysis_and_Control_of_a_Piezoelectric_Elements_Bonded_Flexural_Torsional_Beam">Vibration Analysis and Control of a Piezoelectric Elements Bonded Flexural-Torsional Beam</a></div><div class="wp-workCard_item"><span class="js-work-more-abstract-truncated">An analytical method for flexural and torsional vibration analysis of a Euler-Bernoulli beam has ...</span><a class="js-work-more-abstract" data-broccoli-component="work_strip.more_abstract" data-click-track="profile-work-strip-more-abstract" href="javascript:;"><span> more </span><span><i class="fa fa-caret-down"></i></span></a><span class="js-work-more-abstract-untruncated hidden">An analytical method for flexural and torsional vibration analysis of a Euler-Bernoulli beam has been developed as a baseline for treating flexible beam attached to central-body space structure. Extension of this work is carried out for the generic problem of Active Vibration Suppressionof a cantilevered Euler-Bernoulli beam with piezoelectric sensor and actuator attached as appropriate along the beam. Such generic example can be further extended for tackling lightweight structures in space applications, such as antennas, robot&#39;s arms and solar panels. For comparative study, three generic configurations of the combined beam and piezoelectric elements are solved. The equation of motion of the beam is expressed using Hamilton&#39;s principle, and the baseline problem is solved using Galerkin based finite element method. Nomenclature a,b,c,d = coefficients in the frequency equation C = origin of coordinate system D = shear center e ,s = curvilinear coordinates F = area of cross section f = frequency G = shear modulus K = Saint Venant torsion constant L = length of element M, Mx, My = bending moments Mω = bimoment mx, my, mD, mω= external bending moments, torsional moment and bimoment per unit length of the beam N = axial force O = starting point (point from which s is measured) P = external force px, py, pz = externally loads per unit length of the beam x y z p , p , p = externally applied loads per unit area of midplane of the beam TD = total torsional moment T = torsional momet on the beam Tk = kinetic Energy t = thickness of wall U, V,F = amplitudes of the transverse displacements and torsional rotation U = work of actual stresses u = vector of displacements u, v, w = displacements of shear center</span></div><div class="wp-workCard_item wp-workCard--actions"><span class="work-strip-bookmark-button-container"></span><a id="2dd0a2e35d63c6717cf3fa8d454c57fb" class="wp-workCard--action" rel="nofollow" data-click-track="profile-work-strip-download" data-download="{&quot;attachment_id&quot;:54849948,&quot;asset_id&quot;:34985925,&quot;asset_type&quot;:&quot;Work&quot;,&quot;button_location&quot;:&quot;profile&quot;}" href="https://www.academia.edu/attachments/54849948/download_file?st=MTczMzAzMTQwNiw4LjIyMi4yMDguMTQ2&s=profile"><span><i class="fa fa-arrow-down"></i></span><span>Download</span></a><span class="wp-workCard--action visible-if-viewed-by-owner inline-block" style="display: none;"><span class="js-profile-work-strip-edit-button-wrapper profile-work-strip-edit-button-wrapper" data-work-id="34985925"><a class="js-profile-work-strip-edit-button" tabindex="0"><span><i class="fa fa-pencil"></i></span><span>Edit</span></a></span></span><span id="work-strip-rankings-button-container"></span></div><div class="wp-workCard_item wp-workCard--stats"><span><span><span class="js-view-count view-count u-mr2x" data-work-id="34985925"><i class="fa fa-spinner fa-spin"></i></span><script>$(function () { var workId = 34985925; window.Academia.workViewCountsFetcher.queue(workId, function (count) { var description = window.$h.commaizeInt(count) + " " + window.$h.pluralize(count, 'View'); $(".js-view-count[data-work-id=34985925]").text(description); $(".js-view-count[data-work-id=34985925]").attr('title', description).tooltip(); }); });</script></span></span><span><span class="percentile-widget hidden"><span class="u-mr2x work-percentile"></span></span><script>$(function () { var workId = 34985925; window.Academia.workPercentilesFetcher.queue(workId, function (percentileText) { var container = $(".js-work-strip[data-work-id='34985925']"); container.find('.work-percentile').text(percentileText.charAt(0).toUpperCase() + percentileText.slice(1)); container.find('.percentile-widget').show(); container.find('.percentile-widget').removeClass('hidden'); }); });</script></span><span><script>$(function() { new Works.PaperRankView({ workId: 34985925, container: "", }); });</script></span></div><div id="work-strip-premium-row-container"></div></div></div><script> require.config({ waitSeconds: 90 })(["https://a.academia-assets.com/assets/wow_profile-f77ea15d77ce96025a6048a514272ad8becbad23c641fc2b3bd6e24ca6ff1932.js","https://a.academia-assets.com/assets/work_edit-ad038b8c047c1a8d4fa01b402d530ff93c45fee2137a149a4a5398bc8ad67560.js"], function() { // from javascript_helper.rb var dispatcherData = {} if (true){ window.WowProfile.dispatcher = window.WowProfile.dispatcher || _.clone(Backbone.Events); dispatcherData = { dispatcher: window.WowProfile.dispatcher, downloadLinkId: "2dd0a2e35d63c6717cf3fa8d454c57fb" } } $('.js-work-strip[data-work-id=34985925]').each(function() { if (!$(this).data('initialized')) { new WowProfile.WorkStripView({ el: this, workJSON: {"id":34985925,"title":"Vibration Analysis and Control of a Piezoelectric Elements Bonded Flexural-Torsional Beam","translated_title":"","metadata":{"abstract":"An analytical method for flexural and torsional vibration analysis of a Euler-Bernoulli beam has been developed as a baseline for treating flexible beam attached to central-body space structure. Extension of this work is carried out for the generic problem of Active Vibration Suppressionof a cantilevered Euler-Bernoulli beam with piezoelectric sensor and actuator attached as appropriate along the beam. Such generic example can be further extended for tackling lightweight structures in space applications, such as antennas, robot's arms and solar panels. For comparative study, three generic configurations of the combined beam and piezoelectric elements are solved. The equation of motion of the beam is expressed using Hamilton's principle, and the baseline problem is solved using Galerkin based finite element method. Nomenclature a,b,c,d = coefficients in the frequency equation C = origin of coordinate system D = shear center e ,s = curvilinear coordinates F = area of cross section f = frequency G = shear modulus K = Saint Venant torsion constant L = length of element M, Mx, My = bending moments Mω = bimoment mx, my, mD, mω= external bending moments, torsional moment and bimoment per unit length of the beam N = axial force O = starting point (point from which s is measured) P = external force px, py, pz = externally loads per unit length of the beam x y z p , p , p = externally applied loads per unit area of midplane of the beam TD = total torsional moment T = torsional momet on the beam Tk = kinetic Energy t = thickness of wall U, V,F = amplitudes of the transverse displacements and torsional rotation U = work of actual stresses u = vector of displacements u, v, w = displacements of shear center"},"translated_abstract":"An analytical method for flexural and torsional vibration analysis of a Euler-Bernoulli beam has been developed as a baseline for treating flexible beam attached to central-body space structure. Extension of this work is carried out for the generic problem of Active Vibration Suppressionof a cantilevered Euler-Bernoulli beam with piezoelectric sensor and actuator attached as appropriate along the beam. Such generic example can be further extended for tackling lightweight structures in space applications, such as antennas, robot's arms and solar panels. For comparative study, three generic configurations of the combined beam and piezoelectric elements are solved. The equation of motion of the beam is expressed using Hamilton's principle, and the baseline problem is solved using Galerkin based finite element method. Nomenclature a,b,c,d = coefficients in the frequency equation C = origin of coordinate system D = shear center e ,s = curvilinear coordinates F = area of cross section f = frequency G = shear modulus K = Saint Venant torsion constant L = length of element M, Mx, My = bending moments Mω = bimoment mx, my, mD, mω= external bending moments, torsional moment and bimoment per unit length of the beam N = axial force O = starting point (point from which s is measured) P = external force px, py, pz = externally loads per unit length of the beam x y z p , p , p = externally applied loads per unit area of midplane of the beam TD = total torsional moment T = torsional momet on the beam Tk = kinetic Energy t = thickness of wall U, V,F = amplitudes of the transverse displacements and torsional rotation U = work of actual stresses u = vector of displacements u, v, w = displacements of shear center","internal_url":"https://www.academia.edu/34985925/Vibration_Analysis_and_Control_of_a_Piezoelectric_Elements_Bonded_Flexural_Torsional_Beam","translated_internal_url":"","created_at":"2017-10-28T20:41:44.656-07:00","preview_url":null,"current_user_can_edit":null,"current_user_is_owner":null,"owner_id":4040157,"coauthors_can_edit":true,"document_type":"conference_presentation","co_author_tags":[],"downloadable_attachments":[{"id":54849948,"title":"","file_type":"pdf","scribd_thumbnail_url":"https://attachments.academia-assets.com/54849948/thumbnails/1.jpg","file_name":"HD-IAC17.C2.3.6-VIBRATION_ANALYSIS__CONTROL_AND_OPTIMIZATION_OF_FLEXURAL_-_TORSIONAL_BEAM.pdf","download_url":"https://www.academia.edu/attachments/54849948/download_file?st=MTczMzAzMTQwNiw4LjIyMi4yMDguMTQ2&","bulk_download_file_name":"Vibration_Analysis_and_Control_of_a_Piez.pdf","bulk_download_url":"https://d1wqtxts1xzle7.cloudfront.net/54849948/HD-IAC17.C2.3.6-VIBRATION_ANALYSIS__CONTROL_AND_OPTIMIZATION_OF_FLEXURAL_-_TORSIONAL_BEAM-libre.pdf?1509248748=\u0026response-content-disposition=attachment%3B+filename%3DVibration_Analysis_and_Control_of_a_Piez.pdf\u0026Expires=1732987661\u0026Signature=SQNFzhZlRRuH7j4eRIVtx9HxKDc73sSmZeTYdoDZt2j6tTd2ERy7mPg9-Wc1wQiHTUw14Fdq94vQOSv4tNSiJyaXwfcNrTYJiCVIi7F~2Q1yx2xegYRm7bgt5qCtsMII7V~7Ktj5Otycj2uxeUsMvIMYU8UcrxxZ7EgLxRjvUCM7zGp8qx7HljrL3Ez2LBgcLuizYgEF0DlfS97CERd9BBea9rNdVwKONmAA0M8GD0jtWoxb-1q~s2Tic8gEeZ7A2uICjDS9VvFAc1vIK6ko575VQOHs4CCLXDE8vhrbgXBpek7na-ArZRrtrTL4V2nAGezUQCkAs1aEqpgZCxrp~A__\u0026Key-Pair-Id=APKAJLOHF5GGSLRBV4ZA"}],"slug":"Vibration_Analysis_and_Control_of_a_Piezoelectric_Elements_Bonded_Flexural_Torsional_Beam","translated_slug":"","page_count":20,"language":"en","content_type":"Work","owner":{"id":4040157,"first_name":"Harijono","middle_initials":"","last_name":"Djojodihardjo","page_name":"HarijonoDjojodihardjo","domain_name":"itb","created_at":"2013-05-03T11:27:42.148-07:00","display_name":"Harijono Djojodihardjo","url":"https://itb.academia.edu/HarijonoDjojodihardjo"},"attachments":[{"id":54849948,"title":"","file_type":"pdf","scribd_thumbnail_url":"https://attachments.academia-assets.com/54849948/thumbnails/1.jpg","file_name":"HD-IAC17.C2.3.6-VIBRATION_ANALYSIS__CONTROL_AND_OPTIMIZATION_OF_FLEXURAL_-_TORSIONAL_BEAM.pdf","download_url":"https://www.academia.edu/attachments/54849948/download_file?st=MTczMzAzMTQwNiw4LjIyMi4yMDguMTQ2&","bulk_download_file_name":"Vibration_Analysis_and_Control_of_a_Piez.pdf","bulk_download_url":"https://d1wqtxts1xzle7.cloudfront.net/54849948/HD-IAC17.C2.3.6-VIBRATION_ANALYSIS__CONTROL_AND_OPTIMIZATION_OF_FLEXURAL_-_TORSIONAL_BEAM-libre.pdf?1509248748=\u0026response-content-disposition=attachment%3B+filename%3DVibration_Analysis_and_Control_of_a_Piez.pdf\u0026Expires=1732987661\u0026Signature=SQNFzhZlRRuH7j4eRIVtx9HxKDc73sSmZeTYdoDZt2j6tTd2ERy7mPg9-Wc1wQiHTUw14Fdq94vQOSv4tNSiJyaXwfcNrTYJiCVIi7F~2Q1yx2xegYRm7bgt5qCtsMII7V~7Ktj5Otycj2uxeUsMvIMYU8UcrxxZ7EgLxRjvUCM7zGp8qx7HljrL3Ez2LBgcLuizYgEF0DlfS97CERd9BBea9rNdVwKONmAA0M8GD0jtWoxb-1q~s2Tic8gEeZ7A2uICjDS9VvFAc1vIK6ko575VQOHs4CCLXDE8vhrbgXBpek7na-ArZRrtrTL4V2nAGezUQCkAs1aEqpgZCxrp~A__\u0026Key-Pair-Id=APKAJLOHF5GGSLRBV4ZA"}],"research_interests":[{"id":48,"name":"Engineering","url":"https://www.academia.edu/Documents/in/Engineering"},{"id":60,"name":"Mechanical Engineering","url":"https://www.academia.edu/Documents/in/Mechanical_Engineering"},{"id":78,"name":"Control Systems Engineering","url":"https://www.academia.edu/Documents/in/Control_Systems_Engineering"},{"id":88,"name":"Aerospace Engineering","url":"https://www.academia.edu/Documents/in/Aerospace_Engineering"},{"id":300,"name":"Mathematics","url":"https://www.academia.edu/Documents/in/Mathematics"},{"id":512,"name":"Mechanics","url":"https://www.academia.edu/Documents/in/Mechanics"}],"urls":[]}, dispatcherData: dispatcherData }); $(this).data('initialized', true); } }); $a.trackClickSource(".js-work-strip-work-link", "profile_work_strip") }); </script> <div class="js-work-strip profile--work_container" data-work-id="34364696"><div class="profile--work_thumbnail hidden-xs"><a class="js-work-strip-work-link" data-click-track="profile-work-strip-thumbnail" href="https://www.academia.edu/34364696/ANALYSIS_OF_CONCEPTUAL_MAGNETOSPHERIC_PLASMA_PROPULSION_FOR_SMALL_EARTH_OBSERVATION_SATELLITE"><img alt="Research paper thumbnail of ANALYSIS OF CONCEPTUAL MAGNETOSPHERIC PLASMA PROPULSION FOR SMALL EARTH OBSERVATION SATELLITE" class="work-thumbnail" src="https://attachments.academia-assets.com/54254245/thumbnails/1.jpg" /></a></div><div class="wp-workCard wp-workCard_itemContainer"><div class="wp-workCard_item wp-workCard--title"><a class="js-work-strip-work-link text-gray-darker" data-click-track="profile-work-strip-title" href="https://www.academia.edu/34364696/ANALYSIS_OF_CONCEPTUAL_MAGNETOSPHERIC_PLASMA_PROPULSION_FOR_SMALL_EARTH_OBSERVATION_SATELLITE">ANALYSIS OF CONCEPTUAL MAGNETOSPHERIC PLASMA PROPULSION FOR SMALL EARTH OBSERVATION SATELLITE</a></div><div class="wp-workCard_item"><span class="js-work-more-abstract-truncated">Small satellites with a mass less than 500 kg have become a competitor to large satellites. The i...</span><a class="js-work-more-abstract" data-broccoli-component="work_strip.more_abstract" data-click-track="profile-work-strip-more-abstract" href="javascript:;"><span> more </span><span><i class="fa fa-caret-down"></i></span></a><span class="js-work-more-abstract-untruncated hidden">Small satellites with a mass less than 500 kg have become a competitor to large satellites. The important advantages of Magnetospeheric Plasma Propulsion such as low propellant consumption, cheaper launchers, longer mission and controllable thrust are assessed in view of earth observation mission and leads to the efforts of exploring and utilizing new types of sustainable power source to be derived directly from space, without utilizing Earth based propulsion system and propellant. The original idea of magnetic sailing spacecraft (MagSail), as proposed by Zubrin. Winglee and Funaki utilizes the interaction between solar wind and an artificial magnetic field that is generated by a loop of superconducting wire attached onboard of the spacecraft to reflect the solar wind particles approaching the coil. Further development was proposed by Funaki as a Magneto Plasma Sail (MPS), as an alternative to Winglee et al MiniMagnetospheric Plasma Propulsion (M2P2) proposed system (2000) can dramatically produce large acceleration of M2P2 spacecraft without requiring large structure is required by inflating the magnetosphere by a plasma jet instead of employing a huge coil. Then the present study will review and assess these Magnetospheric Plasma Propulsion and synthesize an appropriate configuration for earth observation mission. Subject to the prevailing solar wind field, a baseline study is carried out to conceptually design a Magnetospheric Plasma propelled satellite.</span></div><div class="wp-workCard_item wp-workCard--actions"><span class="work-strip-bookmark-button-container"></span><a id="778a717f478efa430c796e2ed66e6b00" class="wp-workCard--action" rel="nofollow" data-click-track="profile-work-strip-download" data-download="{&quot;attachment_id&quot;:54254245,&quot;asset_id&quot;:34364696,&quot;asset_type&quot;:&quot;Work&quot;,&quot;button_location&quot;:&quot;profile&quot;}" href="https://www.academia.edu/attachments/54254245/download_file?st=MTczMzAzMTQwNiw4LjIyMi4yMDguMTQ2&s=profile"><span><i class="fa fa-arrow-down"></i></span><span>Download</span></a><span class="wp-workCard--action visible-if-viewed-by-owner inline-block" style="display: none;"><span class="js-profile-work-strip-edit-button-wrapper profile-work-strip-edit-button-wrapper" data-work-id="34364696"><a class="js-profile-work-strip-edit-button" tabindex="0"><span><i class="fa fa-pencil"></i></span><span>Edit</span></a></span></span><span id="work-strip-rankings-button-container"></span></div><div class="wp-workCard_item wp-workCard--stats"><span><span><span class="js-view-count view-count u-mr2x" data-work-id="34364696"><i class="fa fa-spinner fa-spin"></i></span><script>$(function () { var workId = 34364696; window.Academia.workViewCountsFetcher.queue(workId, function (count) { var description = window.$h.commaizeInt(count) + " " + window.$h.pluralize(count, 'View'); $(".js-view-count[data-work-id=34364696]").text(description); $(".js-view-count[data-work-id=34364696]").attr('title', description).tooltip(); }); });</script></span></span><span><span class="percentile-widget hidden"><span class="u-mr2x work-percentile"></span></span><script>$(function () { var workId = 34364696; window.Academia.workPercentilesFetcher.queue(workId, function (percentileText) { var container = $(".js-work-strip[data-work-id='34364696']"); container.find('.work-percentile').text(percentileText.charAt(0).toUpperCase() + percentileText.slice(1)); container.find('.percentile-widget').show(); container.find('.percentile-widget').removeClass('hidden'); }); });</script></span><span><script>$(function() { new Works.PaperRankView({ workId: 34364696, container: "", }); });</script></span></div><div id="work-strip-premium-row-container"></div></div></div><script> require.config({ waitSeconds: 90 })(["https://a.academia-assets.com/assets/wow_profile-f77ea15d77ce96025a6048a514272ad8becbad23c641fc2b3bd6e24ca6ff1932.js","https://a.academia-assets.com/assets/work_edit-ad038b8c047c1a8d4fa01b402d530ff93c45fee2137a149a4a5398bc8ad67560.js"], function() { // from javascript_helper.rb var dispatcherData = {} if (true){ window.WowProfile.dispatcher = window.WowProfile.dispatcher || _.clone(Backbone.Events); dispatcherData = { dispatcher: window.WowProfile.dispatcher, downloadLinkId: "778a717f478efa430c796e2ed66e6b00" } } $('.js-work-strip[data-work-id=34364696]').each(function() { if (!$(this).data('initialized')) { new WowProfile.WorkStripView({ el: this, workJSON: {"id":34364696,"title":"ANALYSIS OF CONCEPTUAL MAGNETOSPHERIC PLASMA PROPULSION FOR SMALL EARTH OBSERVATION SATELLITE","translated_title":"","metadata":{"abstract":"Small satellites with a mass less than 500 kg have become a competitor to large satellites. The important advantages of Magnetospeheric Plasma Propulsion such as low propellant consumption, cheaper launchers, longer mission and controllable thrust are assessed in view of earth observation mission and leads to the efforts of exploring and utilizing new types of sustainable power source to be derived directly from space, without utilizing Earth based propulsion system and propellant. The original idea of magnetic sailing spacecraft (MagSail), as proposed by Zubrin. Winglee and Funaki utilizes the interaction between solar wind and an artificial magnetic field that is generated by a loop of superconducting wire attached onboard of the spacecraft to reflect the solar wind particles approaching the coil. Further development was proposed by Funaki as a Magneto Plasma Sail (MPS), as an alternative to Winglee et al MiniMagnetospheric Plasma Propulsion (M2P2) proposed system (2000) can dramatically produce large acceleration of M2P2 spacecraft without requiring large structure is required by inflating the magnetosphere by a plasma jet instead of employing a huge coil. Then the present study will review and assess these Magnetospheric Plasma Propulsion and synthesize an appropriate configuration for earth observation mission. Subject to the prevailing solar wind field, a baseline study is carried out to conceptually design a Magnetospheric Plasma propelled satellite.","ai_title_tag":"Conceptual Magnetospheric Plasma Propulsion for Small Satellites"},"translated_abstract":"Small satellites with a mass less than 500 kg have become a competitor to large satellites. The important advantages of Magnetospeheric Plasma Propulsion such as low propellant consumption, cheaper launchers, longer mission and controllable thrust are assessed in view of earth observation mission and leads to the efforts of exploring and utilizing new types of sustainable power source to be derived directly from space, without utilizing Earth based propulsion system and propellant. The original idea of magnetic sailing spacecraft (MagSail), as proposed by Zubrin. Winglee and Funaki utilizes the interaction between solar wind and an artificial magnetic field that is generated by a loop of superconducting wire attached onboard of the spacecraft to reflect the solar wind particles approaching the coil. Further development was proposed by Funaki as a Magneto Plasma Sail (MPS), as an alternative to Winglee et al MiniMagnetospheric Plasma Propulsion (M2P2) proposed system (2000) can dramatically produce large acceleration of M2P2 spacecraft without requiring large structure is required by inflating the magnetosphere by a plasma jet instead of employing a huge coil. Then the present study will review and assess these Magnetospheric Plasma Propulsion and synthesize an appropriate configuration for earth observation mission. Subject to the prevailing solar wind field, a baseline study is carried out to conceptually design a Magnetospheric Plasma propelled satellite.","internal_url":"https://www.academia.edu/34364696/ANALYSIS_OF_CONCEPTUAL_MAGNETOSPHERIC_PLASMA_PROPULSION_FOR_SMALL_EARTH_OBSERVATION_SATELLITE","translated_internal_url":"","created_at":"2017-08-26T16:18:20.519-07:00","preview_url":null,"current_user_can_edit":null,"current_user_is_owner":null,"owner_id":4040157,"coauthors_can_edit":true,"document_type":"conference_presentation","co_author_tags":[{"id":30122329,"work_id":34364696,"tagging_user_id":4040157,"tagged_user_id":null,"co_author_invite_id":3223809,"email":"h***o@yahoo.co.id","display_order":1,"name":"Harijono Djojodihardjo","title":"ANALYSIS OF CONCEPTUAL MAGNETOSPHERIC PLASMA PROPULSION FOR SMALL EARTH OBSERVATION SATELLITE"}],"downloadable_attachments":[{"id":54254245,"title":"","file_type":"pdf","scribd_thumbnail_url":"https://attachments.academia-assets.com/54254245/thumbnails/1.jpg","file_name":"IAA-NEA-0104-MINI-MAGNETOSPHERIC_PLASMA_PROPULSION_FOR_SMALL_EO_SATELLITE.pdf","download_url":"https://www.academia.edu/attachments/54254245/download_file?st=MTczMzAzMTQwNiw4LjIyMi4yMDguMTQ2&","bulk_download_file_name":"ANALYSIS_OF_CONCEPTUAL_MAGNETOSPHERIC_PL.pdf","bulk_download_url":"https://d1wqtxts1xzle7.cloudfront.net/54254245/IAA-NEA-0104-MINI-MAGNETOSPHERIC_PLASMA_PROPULSION_FOR_SMALL_EO_SATELLITE-libre.pdf?1503789512=\u0026response-content-disposition=attachment%3B+filename%3DANALYSIS_OF_CONCEPTUAL_MAGNETOSPHERIC_PL.pdf\u0026Expires=1732987661\u0026Signature=Wi7dgrZstuRaA3Eo7d49BGg4s31OiMFn9m5EIGSkMgwSbZXW3V68XQeipHQIecWm9srGVuja~Ml-AjTmhyEDl6oEpkwdmf6XDymQSbUETWJrlJ48XpwvwF2hqVLb9PEThUQVV9wL5v-NOgTCWIjiDdSO6OT6lWmBfIau0RkzyJaRd-FLCrltmf2KoU8cN14w0SyCpbStvvxSXGPXLeDtqbHRy9JA~r9GrEYt0E-HeuM7-weHWqZAM5jCr8imIhF3QvoupeOMBW0Ft3dGORr-26NyQ7kFx0Rw1HZW11KxevWJr4eI~2S-IeslOne6YgS-WzFu~HjXDagmJ9-TVOTRXw__\u0026Key-Pair-Id=APKAJLOHF5GGSLRBV4ZA"}],"slug":"ANALYSIS_OF_CONCEPTUAL_MAGNETOSPHERIC_PLASMA_PROPULSION_FOR_SMALL_EARTH_OBSERVATION_SATELLITE","translated_slug":"","page_count":24,"language":"en","content_type":"Work","owner":{"id":4040157,"first_name":"Harijono","middle_initials":"","last_name":"Djojodihardjo","page_name":"HarijonoDjojodihardjo","domain_name":"itb","created_at":"2013-05-03T11:27:42.148-07:00","display_name":"Harijono Djojodihardjo","url":"https://itb.academia.edu/HarijonoDjojodihardjo"},"attachments":[{"id":54254245,"title":"","file_type":"pdf","scribd_thumbnail_url":"https://attachments.academia-assets.com/54254245/thumbnails/1.jpg","file_name":"IAA-NEA-0104-MINI-MAGNETOSPHERIC_PLASMA_PROPULSION_FOR_SMALL_EO_SATELLITE.pdf","download_url":"https://www.academia.edu/attachments/54254245/download_file?st=MTczMzAzMTQwNiw4LjIyMi4yMDguMTQ2&","bulk_download_file_name":"ANALYSIS_OF_CONCEPTUAL_MAGNETOSPHERIC_PL.pdf","bulk_download_url":"https://d1wqtxts1xzle7.cloudfront.net/54254245/IAA-NEA-0104-MINI-MAGNETOSPHERIC_PLASMA_PROPULSION_FOR_SMALL_EO_SATELLITE-libre.pdf?1503789512=\u0026response-content-disposition=attachment%3B+filename%3DANALYSIS_OF_CONCEPTUAL_MAGNETOSPHERIC_PL.pdf\u0026Expires=1732987661\u0026Signature=Wi7dgrZstuRaA3Eo7d49BGg4s31OiMFn9m5EIGSkMgwSbZXW3V68XQeipHQIecWm9srGVuja~Ml-AjTmhyEDl6oEpkwdmf6XDymQSbUETWJrlJ48XpwvwF2hqVLb9PEThUQVV9wL5v-NOgTCWIjiDdSO6OT6lWmBfIau0RkzyJaRd-FLCrltmf2KoU8cN14w0SyCpbStvvxSXGPXLeDtqbHRy9JA~r9GrEYt0E-HeuM7-weHWqZAM5jCr8imIhF3QvoupeOMBW0Ft3dGORr-26NyQ7kFx0Rw1HZW11KxevWJr4eI~2S-IeslOne6YgS-WzFu~HjXDagmJ9-TVOTRXw__\u0026Key-Pair-Id=APKAJLOHF5GGSLRBV4ZA"}],"research_interests":[{"id":88,"name":"Aerospace Engineering","url":"https://www.academia.edu/Documents/in/Aerospace_Engineering"},{"id":14668,"name":"Aerospace","url":"https://www.academia.edu/Documents/in/Aerospace"},{"id":15525,"name":"Spacecraft Dynamics \u0026 Control","url":"https://www.academia.edu/Documents/in/Spacecraft_Dynamics_and_Control"},{"id":18845,"name":"Environmental Sustainability","url":"https://www.academia.edu/Documents/in/Environmental_Sustainability"},{"id":24557,"name":"Propulsion","url":"https://www.academia.edu/Documents/in/Propulsion"}],"urls":[]}, dispatcherData: dispatcherData }); $(this).data('initialized', true); } }); $a.trackClickSource(".js-work-strip-work-link", "profile_work_strip") }); </script> <div class="js-work-strip profile--work_container" data-work-id="30323737"><div class="profile--work_thumbnail hidden-xs"><a class="js-work-strip-work-link" data-click-track="profile-work-strip-thumbnail" href="https://www.academia.edu/30323737/Numerical_Boundary_Element_Computation_of_Submerged_Body_Surface_Wave_Interaction"><img alt="Research paper thumbnail of Numerical Boundary Element Computation of Submerged Body-Surface Wave Interaction" class="work-thumbnail" src="https://attachments.academia-assets.com/50779720/thumbnails/1.jpg" /></a></div><div class="wp-workCard wp-workCard_itemContainer"><div class="wp-workCard_item wp-workCard--title"><a class="js-work-strip-work-link text-gray-darker" data-click-track="profile-work-strip-title" href="https://www.academia.edu/30323737/Numerical_Boundary_Element_Computation_of_Submerged_Body_Surface_Wave_Interaction">Numerical Boundary Element Computation of Submerged Body-Surface Wave Interaction</a></div><div class="wp-workCard_item"><span class="js-work-more-abstract-truncated">A simple method to solve potential flow problem of submerged body-surface wave interaction is pre...</span><a class="js-work-more-abstract" data-broccoli-component="work_strip.more_abstract" data-click-track="profile-work-strip-more-abstract" href="javascript:;"><span> more </span><span><i class="fa fa-caret-down"></i></span></a><span class="js-work-more-abstract-untruncated hidden">A simple method to solve potential flow problem of submerged body-surface wave interaction is presented. The equation governing flow below the surface is Laplace equation. The boundary condition on the body is of Neumann type, while on the free surface the nonlinear dynamic free surface condition has to be satisfied. In addition, farfield and radiation condition, which determine the behavior of wave going to infinity, have to be satisfied. Taking advantage of potential flow model, then Green Identity is used to transform the problem of Laplace equation with nonlinear boundary condition into &#39;a nonlinear problem in its boundary. To satisfy the nonlinear dynamic free surface condition, Newton iteration is employed. The scheme for relaxation is obtained by expanding the nonlinear dynamic free surface condition obtain correction terms to the velocity potential. Truncation up to linear terms results in a simple scheme. Since the dynamic condition is valid on the unknown location of the free surface, in each iteration step the position of the free surface where the equation is applied, is corrected using Bernoulli equation. In this manner, dynamic free surface condition is satisfied exactly at the collocation points. Results for two and three dimensional nonlifting problem are presented as examples.</span></div><div class="wp-workCard_item wp-workCard--actions"><span class="work-strip-bookmark-button-container"></span><a id="8d6c30e5e86e9e2f055576e243a1f766" class="wp-workCard--action" rel="nofollow" data-click-track="profile-work-strip-download" data-download="{&quot;attachment_id&quot;:50779720,&quot;asset_id&quot;:30323737,&quot;asset_type&quot;:&quot;Work&quot;,&quot;button_location&quot;:&quot;profile&quot;}" href="https://www.academia.edu/attachments/50779720/download_file?st=MTczMzAzMTQwNiw4LjIyMi4yMDguMTQ2&s=profile"><span><i class="fa fa-arrow-down"></i></span><span>Download</span></a><span class="wp-workCard--action visible-if-viewed-by-owner inline-block" style="display: none;"><span class="js-profile-work-strip-edit-button-wrapper profile-work-strip-edit-button-wrapper" data-work-id="30323737"><a class="js-profile-work-strip-edit-button" tabindex="0"><span><i class="fa fa-pencil"></i></span><span>Edit</span></a></span></span><span id="work-strip-rankings-button-container"></span></div><div class="wp-workCard_item wp-workCard--stats"><span><span><span class="js-view-count view-count u-mr2x" data-work-id="30323737"><i class="fa fa-spinner fa-spin"></i></span><script>$(function () { var workId = 30323737; window.Academia.workViewCountsFetcher.queue(workId, function (count) { var description = window.$h.commaizeInt(count) + " " + window.$h.pluralize(count, 'View'); $(".js-view-count[data-work-id=30323737]").text(description); $(".js-view-count[data-work-id=30323737]").attr('title', description).tooltip(); }); });</script></span></span><span><span class="percentile-widget hidden"><span class="u-mr2x work-percentile"></span></span><script>$(function () { var workId = 30323737; window.Academia.workPercentilesFetcher.queue(workId, function (percentileText) { var container = $(".js-work-strip[data-work-id='30323737']"); container.find('.work-percentile').text(percentileText.charAt(0).toUpperCase() + percentileText.slice(1)); container.find('.percentile-widget').show(); container.find('.percentile-widget').removeClass('hidden'); }); });</script></span><span><script>$(function() { new Works.PaperRankView({ workId: 30323737, container: "", }); });</script></span></div><div id="work-strip-premium-row-container"></div></div></div><script> require.config({ waitSeconds: 90 })(["https://a.academia-assets.com/assets/wow_profile-f77ea15d77ce96025a6048a514272ad8becbad23c641fc2b3bd6e24ca6ff1932.js","https://a.academia-assets.com/assets/work_edit-ad038b8c047c1a8d4fa01b402d530ff93c45fee2137a149a4a5398bc8ad67560.js"], function() { // from javascript_helper.rb var dispatcherData = {} if (true){ window.WowProfile.dispatcher = window.WowProfile.dispatcher || _.clone(Backbone.Events); dispatcherData = { dispatcher: window.WowProfile.dispatcher, downloadLinkId: "8d6c30e5e86e9e2f055576e243a1f766" } } $('.js-work-strip[data-work-id=30323737]').each(function() { if (!$(this).data('initialized')) { new WowProfile.WorkStripView({ el: this, workJSON: {"id":30323737,"title":"Numerical Boundary Element Computation of Submerged Body-Surface Wave Interaction","translated_title":"","metadata":{"abstract":"A simple method to solve potential flow problem of submerged body-surface wave interaction is presented. The equation governing flow below the surface is Laplace equation. The boundary condition on the body is of Neumann type, while on the free surface the nonlinear dynamic free surface condition has to be satisfied. In addition, farfield and radiation condition, which determine the behavior of wave going to infinity, have to be satisfied. Taking advantage of potential flow model, then Green Identity is used to transform the problem of Laplace equation with nonlinear boundary condition into 'a nonlinear problem in its boundary. To satisfy the nonlinear dynamic free surface condition, Newton iteration is employed. The scheme for relaxation is obtained by expanding the nonlinear dynamic free surface condition obtain correction terms to the velocity potential. Truncation up to linear terms results in a simple scheme. Since the dynamic condition is valid on the unknown location of the free surface, in each iteration step the position of the free surface where the equation is applied, is corrected using Bernoulli equation. In this manner, dynamic free surface condition is satisfied exactly at the collocation points. Results for two and three dimensional nonlifting problem are presented as examples."},"translated_abstract":"A simple method to solve potential flow problem of submerged body-surface wave interaction is presented. The equation governing flow below the surface is Laplace equation. The boundary condition on the body is of Neumann type, while on the free surface the nonlinear dynamic free surface condition has to be satisfied. In addition, farfield and radiation condition, which determine the behavior of wave going to infinity, have to be satisfied. Taking advantage of potential flow model, then Green Identity is used to transform the problem of Laplace equation with nonlinear boundary condition into 'a nonlinear problem in its boundary. To satisfy the nonlinear dynamic free surface condition, Newton iteration is employed. The scheme for relaxation is obtained by expanding the nonlinear dynamic free surface condition obtain correction terms to the velocity potential. Truncation up to linear terms results in a simple scheme. Since the dynamic condition is valid on the unknown location of the free surface, in each iteration step the position of the free surface where the equation is applied, is corrected using Bernoulli equation. In this manner, dynamic free surface condition is satisfied exactly at the collocation points. Results for two and three dimensional nonlifting problem are presented as examples.","internal_url":"https://www.academia.edu/30323737/Numerical_Boundary_Element_Computation_of_Submerged_Body_Surface_Wave_Interaction","translated_internal_url":"","created_at":"2016-12-08T00:24:12.587-08:00","preview_url":null,"current_user_can_edit":null,"current_user_is_owner":null,"owner_id":4040157,"coauthors_can_edit":true,"document_type":"conference_presentation","co_author_tags":[{"id":26453772,"work_id":30323737,"tagging_user_id":4040157,"tagged_user_id":null,"co_author_invite_id":5831517,"email":"b***a@gmail.com","display_order":1,"name":"B.Bimo Prananta","title":"Numerical Boundary Element Computation of Submerged Body-Surface Wave Interaction"}],"downloadable_attachments":[{"id":50779720,"title":"","file_type":"pdf","scribd_thumbnail_url":"https://attachments.academia-assets.com/50779720/thumbnails/1.jpg","file_name":"Djojodihardjo_Numerical_Boundary_Element_Computation_of_Submerged_Body-Surface_Wave_Interaction_-_ISOPE-I-93-259.pdf","download_url":"https://www.academia.edu/attachments/50779720/download_file?st=MTczMzAzMTQwNiw4LjIyMi4yMDguMTQ2&","bulk_download_file_name":"Numerical_Boundary_Element_Computation_o.pdf","bulk_download_url":"https://d1wqtxts1xzle7.cloudfront.net/50779720/Djojodihardjo_Numerical_Boundary_Element_Computation_of_Submerged_Body-Surface_Wave_Interaction_-_ISOPE-I-93-259-libre.pdf?1481185920=\u0026response-content-disposition=attachment%3B+filename%3DNumerical_Boundary_Element_Computation_o.pdf\u0026Expires=1732987662\u0026Signature=PmHuUkDjqCMab8YK6MYGRSSz3LYUWCcoSforcTE5gIUkiG9p1X95JbBWXtZmQ5auEcbuwii55o8ZJaK363TNLqGhq~uEKqWg09BSd7tUW0X3uyUWsdovPrKbYo92oOBBc6-g~tzaYV1kDLzrVDVUJC9NceTRmk7qPld62C9scD2EbBJJD4vbsU2rlgGgLiUkbL~pskIKIZN7bcgbESIuxhG9qxvZ2ZvfKTrlIpaZjrIm6mMvFWMlBKmkMQEwU6GfjhZxTwqTN3D1I0EBL6P9JGd7AQhjwDgMolSCme-0Q5nqNNwejI8spkIwsRy3Hu1BzyBMmjFgQJWoDxSIZTm5VQ__\u0026Key-Pair-Id=APKAJLOHF5GGSLRBV4ZA"}],"slug":"Numerical_Boundary_Element_Computation_of_Submerged_Body_Surface_Wave_Interaction","translated_slug":"","page_count":8,"language":"en","content_type":"Work","owner":{"id":4040157,"first_name":"Harijono","middle_initials":"","last_name":"Djojodihardjo","page_name":"HarijonoDjojodihardjo","domain_name":"itb","created_at":"2013-05-03T11:27:42.148-07:00","display_name":"Harijono Djojodihardjo","url":"https://itb.academia.edu/HarijonoDjojodihardjo"},"attachments":[{"id":50779720,"title":"","file_type":"pdf","scribd_thumbnail_url":"https://attachments.academia-assets.com/50779720/thumbnails/1.jpg","file_name":"Djojodihardjo_Numerical_Boundary_Element_Computation_of_Submerged_Body-Surface_Wave_Interaction_-_ISOPE-I-93-259.pdf","download_url":"https://www.academia.edu/attachments/50779720/download_file?st=MTczMzAzMTQwNiw4LjIyMi4yMDguMTQ2&","bulk_download_file_name":"Numerical_Boundary_Element_Computation_o.pdf","bulk_download_url":"https://d1wqtxts1xzle7.cloudfront.net/50779720/Djojodihardjo_Numerical_Boundary_Element_Computation_of_Submerged_Body-Surface_Wave_Interaction_-_ISOPE-I-93-259-libre.pdf?1481185920=\u0026response-content-disposition=attachment%3B+filename%3DNumerical_Boundary_Element_Computation_o.pdf\u0026Expires=1732987662\u0026Signature=PmHuUkDjqCMab8YK6MYGRSSz3LYUWCcoSforcTE5gIUkiG9p1X95JbBWXtZmQ5auEcbuwii55o8ZJaK363TNLqGhq~uEKqWg09BSd7tUW0X3uyUWsdovPrKbYo92oOBBc6-g~tzaYV1kDLzrVDVUJC9NceTRmk7qPld62C9scD2EbBJJD4vbsU2rlgGgLiUkbL~pskIKIZN7bcgbESIuxhG9qxvZ2ZvfKTrlIpaZjrIm6mMvFWMlBKmkMQEwU6GfjhZxTwqTN3D1I0EBL6P9JGd7AQhjwDgMolSCme-0Q5nqNNwejI8spkIwsRy3Hu1BzyBMmjFgQJWoDxSIZTm5VQ__\u0026Key-Pair-Id=APKAJLOHF5GGSLRBV4ZA"}],"research_interests":[{"id":48,"name":"Engineering","url":"https://www.academia.edu/Documents/in/Engineering"},{"id":81,"name":"Ocean Engineering","url":"https://www.academia.edu/Documents/in/Ocean_Engineering"},{"id":88,"name":"Aerospace Engineering","url":"https://www.academia.edu/Documents/in/Aerospace_Engineering"},{"id":2298,"name":"Computational Fluid Dynamics","url":"https://www.academia.edu/Documents/in/Computational_Fluid_Dynamics"},{"id":2435,"name":"Fluid Mechanics","url":"https://www.academia.edu/Documents/in/Fluid_Mechanics"},{"id":4955,"name":"Computational Modelling","url":"https://www.academia.edu/Documents/in/Computational_Modelling"},{"id":15532,"name":"Marine Engineering","url":"https://www.academia.edu/Documents/in/Marine_Engineering"}],"urls":[]}, dispatcherData: dispatcherData }); $(this).data('initialized', true); } }); $a.trackClickSource(".js-work-strip-work-link", "profile_work_strip") }); </script> <div class="js-work-strip profile--work_container" data-work-id="29509439"><div class="profile--work_thumbnail hidden-xs"><a class="js-work-strip-work-link" data-click-track="profile-work-strip-thumbnail" href="https://www.academia.edu/29509439/PROGRESS_AND_DEVELOPMENT_OF_COAND%C4%82_JET_FOR_AERODYNAMIC_SURFACE_CIRCULATION_CONTROL_AND_MICRO_AIR_VEHICLE_AN_OVERVIEW"><img alt="Research paper thumbnail of PROGRESS AND DEVELOPMENT OF COANDĂ JET FOR AERODYNAMIC SURFACE CIRCULATION CONTROL AND MICRO-AIR-VEHICLE: AN OVERVIEW" class="work-thumbnail" src="https://attachments.academia-assets.com/49946811/thumbnails/1.jpg" /></a></div><div class="wp-workCard wp-workCard_itemContainer"><div class="wp-workCard_item wp-workCard--title"><a class="js-work-strip-work-link text-gray-darker" data-click-track="profile-work-strip-title" href="https://www.academia.edu/29509439/PROGRESS_AND_DEVELOPMENT_OF_COAND%C4%82_JET_FOR_AERODYNAMIC_SURFACE_CIRCULATION_CONTROL_AND_MICRO_AIR_VEHICLE_AN_OVERVIEW">PROGRESS AND DEVELOPMENT OF COANDĂ JET FOR AERODYNAMIC SURFACE CIRCULATION CONTROL AND MICRO-AIR-VEHICLE: AN OVERVIEW</a></div><div class="wp-workCard_item"><span class="js-work-more-abstract-truncated">Coandă jet has always been referred to in the consideration of various flow control methods to en...</span><a class="js-work-more-abstract" data-broccoli-component="work_strip.more_abstract" data-click-track="profile-work-strip-more-abstract" href="javascript:;"><span> more </span><span><i class="fa fa-caret-down"></i></span></a><span class="js-work-more-abstract-untruncated hidden">Coandă jet has always been referred to in the consideration of various flow control methods to enhance aerodynamic performance, i.e. to enhance lift, reduce drag and delay stall at higher angle of attack, along with continuous, synthetic and pulsed jets, compliant surface, vortex-cell, and the like. Coandă jet has also been applied in the development of novel aircrafts for short take off and landing. In addition, with the increasing need and the progress and sophistication of enabling technologies for disaster mitigation, security, and climate changes, there are new challenges for the application of Coandă jet for Micro-Air Vehicle for such applications. Then it becomes crucial and urgent to revolutionize the integration of Coandă jet technologies and other novel technologies for the development of agile o Micro-Air Vehicle.<br />It is with such motivation that within the aerodynamics surface blowing techniques, and Coandă jet will be reviewed, to assess their characteristics in dramatically alter the behavior of aerodynamic components such as airfoils, wings, and bodies. Capitalizing on a host of research and technology development efforts on Coandă and surface blowing circulation enhancement, the present work reviews the influence, effectiveness and configuration of airfoil surface blowing of Coandă-jet in circulation enhancement and control of aerodynamic surfaces&nbsp; and their applications to MAV’s dynamics and related technologies. The crux of the Coandă jet active research is their stabilization and contol, which will be relevant in its application to Coanada MAV’s.</span></div><div class="wp-workCard_item wp-workCard--actions"><span class="work-strip-bookmark-button-container"></span><a id="d14086bf7f5f73bcec29f131443083a6" class="wp-workCard--action" rel="nofollow" data-click-track="profile-work-strip-download" data-download="{&quot;attachment_id&quot;:49946811,&quot;asset_id&quot;:29509439,&quot;asset_type&quot;:&quot;Work&quot;,&quot;button_location&quot;:&quot;profile&quot;}" href="https://www.academia.edu/attachments/49946811/download_file?st=MTczMzAzMTQwNiw4LjIyMi4yMDguMTQ2&s=profile"><span><i class="fa fa-arrow-down"></i></span><span>Download</span></a><span class="wp-workCard--action visible-if-viewed-by-owner inline-block" style="display: none;"><span class="js-profile-work-strip-edit-button-wrapper profile-work-strip-edit-button-wrapper" data-work-id="29509439"><a class="js-profile-work-strip-edit-button" tabindex="0"><span><i class="fa fa-pencil"></i></span><span>Edit</span></a></span></span><span id="work-strip-rankings-button-container"></span></div><div class="wp-workCard_item wp-workCard--stats"><span><span><span class="js-view-count view-count u-mr2x" data-work-id="29509439"><i class="fa fa-spinner fa-spin"></i></span><script>$(function () { var workId = 29509439; window.Academia.workViewCountsFetcher.queue(workId, function (count) { var description = window.$h.commaizeInt(count) + " " + window.$h.pluralize(count, 'View'); $(".js-view-count[data-work-id=29509439]").text(description); $(".js-view-count[data-work-id=29509439]").attr('title', description).tooltip(); }); });</script></span></span><span><span class="percentile-widget hidden"><span class="u-mr2x work-percentile"></span></span><script>$(function () { var workId = 29509439; window.Academia.workPercentilesFetcher.queue(workId, function (percentileText) { var container = $(".js-work-strip[data-work-id='29509439']"); container.find('.work-percentile').text(percentileText.charAt(0).toUpperCase() + percentileText.slice(1)); container.find('.percentile-widget').show(); container.find('.percentile-widget').removeClass('hidden'); }); });</script></span><span><script>$(function() { new Works.PaperRankView({ workId: 29509439, container: "", }); });</script></span></div><div id="work-strip-premium-row-container"></div></div></div><script> require.config({ waitSeconds: 90 })(["https://a.academia-assets.com/assets/wow_profile-f77ea15d77ce96025a6048a514272ad8becbad23c641fc2b3bd6e24ca6ff1932.js","https://a.academia-assets.com/assets/work_edit-ad038b8c047c1a8d4fa01b402d530ff93c45fee2137a149a4a5398bc8ad67560.js"], function() { // from javascript_helper.rb var dispatcherData = {} if (true){ window.WowProfile.dispatcher = window.WowProfile.dispatcher || _.clone(Backbone.Events); dispatcherData = { dispatcher: window.WowProfile.dispatcher, downloadLinkId: "d14086bf7f5f73bcec29f131443083a6" } } $('.js-work-strip[data-work-id=29509439]').each(function() { if (!$(this).data('initialized')) { new WowProfile.WorkStripView({ el: this, workJSON: {"id":29509439,"title":"PROGRESS AND DEVELOPMENT OF COANDĂ JET FOR AERODYNAMIC SURFACE CIRCULATION CONTROL AND MICRO-AIR-VEHICLE: AN OVERVIEW","translated_title":"","metadata":{"abstract":"Coandă jet has always been referred to in the consideration of various flow control methods to enhance aerodynamic performance, i.e. to enhance lift, reduce drag and delay stall at higher angle of attack, along with continuous, synthetic and pulsed jets, compliant surface, vortex-cell, and the like. Coandă jet has also been applied in the development of novel aircrafts for short take off and landing. In addition, with the increasing need and the progress and sophistication of enabling technologies for disaster mitigation, security, and climate changes, there are new challenges for the application of Coandă jet for Micro-Air Vehicle for such applications. Then it becomes crucial and urgent to revolutionize the integration of Coandă jet technologies and other novel technologies for the development of agile o Micro-Air Vehicle.\nIt is with such motivation that within the aerodynamics surface blowing techniques, and Coandă jet will be reviewed, to assess their characteristics in dramatically alter the behavior of aerodynamic components such as airfoils, wings, and bodies. Capitalizing on a host of research and technology development efforts on Coandă and surface blowing circulation enhancement, the present work reviews the influence, effectiveness and configuration of airfoil surface blowing of Coandă-jet in circulation enhancement and control of aerodynamic surfaces and their applications to MAV’s dynamics and related technologies. The crux of the Coandă jet active research is their stabilization and contol, which will be relevant in its application to Coanada MAV’s.\n"},"translated_abstract":"Coandă jet has always been referred to in the consideration of various flow control methods to enhance aerodynamic performance, i.e. to enhance lift, reduce drag and delay stall at higher angle of attack, along with continuous, synthetic and pulsed jets, compliant surface, vortex-cell, and the like. Coandă jet has also been applied in the development of novel aircrafts for short take off and landing. In addition, with the increasing need and the progress and sophistication of enabling technologies for disaster mitigation, security, and climate changes, there are new challenges for the application of Coandă jet for Micro-Air Vehicle for such applications. Then it becomes crucial and urgent to revolutionize the integration of Coandă jet technologies and other novel technologies for the development of agile o Micro-Air Vehicle.\nIt is with such motivation that within the aerodynamics surface blowing techniques, and Coandă jet will be reviewed, to assess their characteristics in dramatically alter the behavior of aerodynamic components such as airfoils, wings, and bodies. Capitalizing on a host of research and technology development efforts on Coandă and surface blowing circulation enhancement, the present work reviews the influence, effectiveness and configuration of airfoil surface blowing of Coandă-jet in circulation enhancement and control of aerodynamic surfaces and their applications to MAV’s dynamics and related technologies. The crux of the Coandă jet active research is their stabilization and contol, which will be relevant in its application to Coanada MAV’s.\n","internal_url":"https://www.academia.edu/29509439/PROGRESS_AND_DEVELOPMENT_OF_COAND%C4%82_JET_FOR_AERODYNAMIC_SURFACE_CIRCULATION_CONTROL_AND_MICRO_AIR_VEHICLE_AN_OVERVIEW","translated_internal_url":"","created_at":"2016-10-28T14:32:19.204-07:00","preview_url":null,"current_user_can_edit":null,"current_user_is_owner":null,"owner_id":4040157,"coauthors_can_edit":true,"document_type":"conference_presentation","co_author_tags":[],"downloadable_attachments":[{"id":49946811,"title":"","file_type":"pdf","scribd_thumbnail_url":"https://attachments.academia-assets.com/49946811/thumbnails/1.jpg","file_name":"Progress_and_Development_of_Coanda_Jet_for_Aerodynamic_Surface_Circulation_Control_and_Micro-Air-Vehicle.pdf","download_url":"https://www.academia.edu/attachments/49946811/download_file?st=MTczMzAzMTQwNiw4LjIyMi4yMDguMTQ2&","bulk_download_file_name":"PROGRESS_AND_DEVELOPMENT_OF_COANDA_JET_F.pdf","bulk_download_url":"https://d1wqtxts1xzle7.cloudfront.net/49946811/Progress_and_Development_of_Coanda_Jet_for_Aerodynamic_Surface_Circulation_Control_and_Micro-Air-Vehicle-libre.pdf?1477691678=\u0026response-content-disposition=attachment%3B+filename%3DPROGRESS_AND_DEVELOPMENT_OF_COANDA_JET_F.pdf\u0026Expires=1732987662\u0026Signature=bET~14o1-51vStPc1p7Mg1FQRSQWnt9PrygBlo5GFEkAM-9CfPQu9bk3Pmuinzw~YLqPKK0D4Tfure3zCn3mMjLW7Zev0BIyB6vtFRLsQx2F7PaPsqGcFvET8mZSxN130tl5Px4SDZ-n4A83EJyvSfOtCF4ly7lnfI8c8J0n0pjqvzO3KT0Lu4H9xASF9PW1bBC5cVTqSqFobBh16rtPYELcX5bBU-V47MvRUDdezX1uObg7kO13uhJ8-KbNHFfqfn8kYfAgk4bfmae9G1itdZNCjGCfaQkifComgqyk7hPGzbxtJAodfni7IhT1Su1bh2k0q-pSCLvxJKm7IH~ofA__\u0026Key-Pair-Id=APKAJLOHF5GGSLRBV4ZA"}],"slug":"PROGRESS_AND_DEVELOPMENT_OF_COANDĂ_JET_FOR_AERODYNAMIC_SURFACE_CIRCULATION_CONTROL_AND_MICRO_AIR_VEHICLE_AN_OVERVIEW","translated_slug":"","page_count":46,"language":"en","content_type":"Work","owner":{"id":4040157,"first_name":"Harijono","middle_initials":"","last_name":"Djojodihardjo","page_name":"HarijonoDjojodihardjo","domain_name":"itb","created_at":"2013-05-03T11:27:42.148-07:00","display_name":"Harijono Djojodihardjo","url":"https://itb.academia.edu/HarijonoDjojodihardjo"},"attachments":[{"id":49946811,"title":"","file_type":"pdf","scribd_thumbnail_url":"https://attachments.academia-assets.com/49946811/thumbnails/1.jpg","file_name":"Progress_and_Development_of_Coanda_Jet_for_Aerodynamic_Surface_Circulation_Control_and_Micro-Air-Vehicle.pdf","download_url":"https://www.academia.edu/attachments/49946811/download_file?st=MTczMzAzMTQwNiw4LjIyMi4yMDguMTQ2&","bulk_download_file_name":"PROGRESS_AND_DEVELOPMENT_OF_COANDA_JET_F.pdf","bulk_download_url":"https://d1wqtxts1xzle7.cloudfront.net/49946811/Progress_and_Development_of_Coanda_Jet_for_Aerodynamic_Surface_Circulation_Control_and_Micro-Air-Vehicle-libre.pdf?1477691678=\u0026response-content-disposition=attachment%3B+filename%3DPROGRESS_AND_DEVELOPMENT_OF_COANDA_JET_F.pdf\u0026Expires=1732987662\u0026Signature=bET~14o1-51vStPc1p7Mg1FQRSQWnt9PrygBlo5GFEkAM-9CfPQu9bk3Pmuinzw~YLqPKK0D4Tfure3zCn3mMjLW7Zev0BIyB6vtFRLsQx2F7PaPsqGcFvET8mZSxN130tl5Px4SDZ-n4A83EJyvSfOtCF4ly7lnfI8c8J0n0pjqvzO3KT0Lu4H9xASF9PW1bBC5cVTqSqFobBh16rtPYELcX5bBU-V47MvRUDdezX1uObg7kO13uhJ8-KbNHFfqfn8kYfAgk4bfmae9G1itdZNCjGCfaQkifComgqyk7hPGzbxtJAodfni7IhT1Su1bh2k0q-pSCLvxJKm7IH~ofA__\u0026Key-Pair-Id=APKAJLOHF5GGSLRBV4ZA"}],"research_interests":[{"id":48,"name":"Engineering","url":"https://www.academia.edu/Documents/in/Engineering"},{"id":60,"name":"Mechanical Engineering","url":"https://www.academia.edu/Documents/in/Mechanical_Engineering"},{"id":77,"name":"Robotics","url":"https://www.academia.edu/Documents/in/Robotics"},{"id":88,"name":"Aerospace Engineering","url":"https://www.academia.edu/Documents/in/Aerospace_Engineering"},{"id":11820,"name":"Modeling and Simulation","url":"https://www.academia.edu/Documents/in/Modeling_and_Simulation"}],"urls":[]}, dispatcherData: dispatcherData }); $(this).data('initialized', true); } }); $a.trackClickSource(".js-work-strip-work-link", "profile_work_strip") }); </script> <div class="js-work-strip profile--work_container" data-work-id="29509349"><div class="profile--work_thumbnail hidden-xs"><a class="js-work-strip-work-link" data-click-track="profile-work-strip-thumbnail" href="https://www.academia.edu/29509349/OVERVIEW_OF_GREEN_AND_N_2_BUSINESS_JET_AIRCRAFT_WITH_AN_EXAMPLE_OF_QJBJ_CONCEPTUAL_DESIGN_pdf"><img alt="Research paper thumbnail of OVERVIEW OF GREEN AND N+2 BUSINESS JET AIRCRAFT WITH AN EXAMPLE OF QJBJ CONCEPTUAL DESIGN.pdf" class="work-thumbnail" src="https://attachments.academia-assets.com/49946710/thumbnails/1.jpg" /></a></div><div class="wp-workCard wp-workCard_itemContainer"><div class="wp-workCard_item wp-workCard--title"><a class="js-work-strip-work-link text-gray-darker" data-click-track="profile-work-strip-title" href="https://www.academia.edu/29509349/OVERVIEW_OF_GREEN_AND_N_2_BUSINESS_JET_AIRCRAFT_WITH_AN_EXAMPLE_OF_QJBJ_CONCEPTUAL_DESIGN_pdf">OVERVIEW OF GREEN AND N+2 BUSINESS JET AIRCRAFT WITH AN EXAMPLE OF QJBJ CONCEPTUAL DESIGN.pdf</a></div><div class="wp-workCard_item"><span class="js-work-more-abstract-truncated">Aircraft Industries, International and Government Aviation Related Institution and Universities h...</span><a class="js-work-more-abstract" data-broccoli-component="work_strip.more_abstract" data-click-track="profile-work-strip-more-abstract" href="javascript:;"><span> more </span><span><i class="fa fa-caret-down"></i></span></a><span class="js-work-more-abstract-untruncated hidden">Aircraft Industries, International and Government Aviation Related Institution and Universities have been devoting efforts to identify future aircrafts that will meet air transportation demand, economic growth and environmental conservation. To this end, anticipating potential air transportation markets in the business jet type, the present work is devoted for exploring the possibilities of introducing some of a number of visionary and pioneering ideas and upcoming enabling technologies within Green and N+2 Aircraft framework in the Aerodynamic and Conceptual Design Study of Quad-Bubble Business Jet (QB-BJ). In view of and driven by the vision for a fuel efficient, environmentally friendly and technology driven aircraft to meet global need within the next 15 years, the characteristics of the conceptually designed aircraft will be assessed in comparison to an appropriately chosen business jet as a reference, as well as recent novel concepts, within the subsonic flight regimes. Major ideas derived from D8 and other novel concepts are appropriately applied in the work, which starts with fuel efficient motivation, and followed by wing Aerodynamics and other critical factors related to the Design Requirements and Objectives. These preliminary results are assessed within recent aircraft technology development.</span></div><div class="wp-workCard_item wp-workCard--actions"><span class="work-strip-bookmark-button-container"></span><a id="cc65f57f199dda7ec9cf6ea163272b95" class="wp-workCard--action" rel="nofollow" data-click-track="profile-work-strip-download" data-download="{&quot;attachment_id&quot;:49946710,&quot;asset_id&quot;:29509349,&quot;asset_type&quot;:&quot;Work&quot;,&quot;button_location&quot;:&quot;profile&quot;}" href="https://www.academia.edu/attachments/49946710/download_file?st=MTczMzAzMTQwNiw4LjIyMi4yMDguMTQ2&s=profile"><span><i class="fa fa-arrow-down"></i></span><span>Download</span></a><span class="wp-workCard--action visible-if-viewed-by-owner inline-block" style="display: none;"><span class="js-profile-work-strip-edit-button-wrapper profile-work-strip-edit-button-wrapper" data-work-id="29509349"><a class="js-profile-work-strip-edit-button" tabindex="0"><span><i class="fa fa-pencil"></i></span><span>Edit</span></a></span></span><span id="work-strip-rankings-button-container"></span></div><div class="wp-workCard_item wp-workCard--stats"><span><span><span class="js-view-count view-count u-mr2x" data-work-id="29509349"><i class="fa fa-spinner fa-spin"></i></span><script>$(function () { var workId = 29509349; window.Academia.workViewCountsFetcher.queue(workId, function (count) { var description = window.$h.commaizeInt(count) + " " + window.$h.pluralize(count, 'View'); $(".js-view-count[data-work-id=29509349]").text(description); $(".js-view-count[data-work-id=29509349]").attr('title', description).tooltip(); }); });</script></span></span><span><span class="percentile-widget hidden"><span class="u-mr2x work-percentile"></span></span><script>$(function () { var workId = 29509349; window.Academia.workPercentilesFetcher.queue(workId, function (percentileText) { var container = $(".js-work-strip[data-work-id='29509349']"); container.find('.work-percentile').text(percentileText.charAt(0).toUpperCase() + percentileText.slice(1)); container.find('.percentile-widget').show(); container.find('.percentile-widget').removeClass('hidden'); }); });</script></span><span><script>$(function() { new Works.PaperRankView({ workId: 29509349, container: "", }); });</script></span></div><div id="work-strip-premium-row-container"></div></div></div><script> require.config({ waitSeconds: 90 })(["https://a.academia-assets.com/assets/wow_profile-f77ea15d77ce96025a6048a514272ad8becbad23c641fc2b3bd6e24ca6ff1932.js","https://a.academia-assets.com/assets/work_edit-ad038b8c047c1a8d4fa01b402d530ff93c45fee2137a149a4a5398bc8ad67560.js"], function() { // from javascript_helper.rb var dispatcherData = {} if (true){ window.WowProfile.dispatcher = window.WowProfile.dispatcher || _.clone(Backbone.Events); dispatcherData = { dispatcher: window.WowProfile.dispatcher, downloadLinkId: "cc65f57f199dda7ec9cf6ea163272b95" } } $('.js-work-strip[data-work-id=29509349]').each(function() { if (!$(this).data('initialized')) { new WowProfile.WorkStripView({ el: this, workJSON: {"id":29509349,"title":"OVERVIEW OF GREEN AND N+2 BUSINESS JET AIRCRAFT WITH AN EXAMPLE OF QJBJ CONCEPTUAL DESIGN.pdf","translated_title":"","metadata":{"abstract":"Aircraft Industries, International and Government Aviation Related Institution and Universities have been devoting efforts to identify future aircrafts that will meet air transportation demand, economic growth and environmental conservation. To this end, anticipating potential air transportation markets in the business jet type, the present work is devoted for exploring the possibilities of introducing some of a number of visionary and pioneering ideas and upcoming enabling technologies within Green and N+2 Aircraft framework in the Aerodynamic and Conceptual Design Study of Quad-Bubble Business Jet (QB-BJ). In view of and driven by the vision for a fuel efficient, environmentally friendly and technology driven aircraft to meet global need within the next 15 years, the characteristics of the conceptually designed aircraft will be assessed in comparison to an appropriately chosen business jet as a reference, as well as recent novel concepts, within the subsonic flight regimes. Major ideas derived from D8 and other novel concepts are appropriately applied in the work, which starts with fuel efficient motivation, and followed by wing Aerodynamics and other critical factors related to the Design Requirements and Objectives. These preliminary results are assessed within recent aircraft technology development.","ai_title_tag":"Green and N+2 Business Jets: QB-BJ Conceptual Design Overview"},"translated_abstract":"Aircraft Industries, International and Government Aviation Related Institution and Universities have been devoting efforts to identify future aircrafts that will meet air transportation demand, economic growth and environmental conservation. To this end, anticipating potential air transportation markets in the business jet type, the present work is devoted for exploring the possibilities of introducing some of a number of visionary and pioneering ideas and upcoming enabling technologies within Green and N+2 Aircraft framework in the Aerodynamic and Conceptual Design Study of Quad-Bubble Business Jet (QB-BJ). 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These preliminary results are assessed within recent aircraft technology development.","internal_url":"https://www.academia.edu/29509349/OVERVIEW_OF_GREEN_AND_N_2_BUSINESS_JET_AIRCRAFT_WITH_AN_EXAMPLE_OF_QJBJ_CONCEPTUAL_DESIGN_pdf","translated_internal_url":"","created_at":"2016-10-28T14:16:56.632-07:00","preview_url":null,"current_user_can_edit":null,"current_user_is_owner":null,"owner_id":4040157,"coauthors_can_edit":true,"document_type":"conference_presentation","co_author_tags":[],"downloadable_attachments":[{"id":49946710,"title":"","file_type":"pdf","scribd_thumbnail_url":"https://attachments.academia-assets.com/49946710/thumbnails/1.jpg","file_name":"OVERVIEW_OF_GREEN_AND_N_2_BUSINESS_JET_AIRCRAFT_WITH_AN_EXAMPLE_OF_QJBJ_CONCEPTUAL_DESIGN.pdf","download_url":"https://www.academia.edu/attachments/49946710/download_file?st=MTczMzAzMTQwNiw4LjIyMi4yMDguMTQ2&","bulk_download_file_name":"OVERVIEW_OF_GREEN_AND_N_2_BUSINESS_JET_A.pdf","bulk_download_url":"https://d1wqtxts1xzle7.cloudfront.net/49946710/OVERVIEW_OF_GREEN_AND_N_2_BUSINESS_JET_AIRCRAFT_WITH_AN_EXAMPLE_OF_QJBJ_CONCEPTUAL_DESIGN-libre.pdf?1477689718=\u0026response-content-disposition=attachment%3B+filename%3DOVERVIEW_OF_GREEN_AND_N_2_BUSINESS_JET_A.pdf\u0026Expires=1732987662\u0026Signature=EhC~hOwGctWUzAK0iakyJApqsxQgKZDzgNVlGkyrkBJZMASx-~Mu7jd1G6UStaUHX3Dky7RAv7ZnScLShEqDtoNrm9bnGX8U~9nfsdDATnzki~Uh0GxkNHq974nhQ-OuxYtevtTuJH~sY-SMFspB7PsUrvZdIheOFxaNCxdsKJKxUJxcl-o~5DW4motkIq0eaOaFOiUI8U9iNmAXqVMUZ~JmtJhMz5Iy23yR2roN-t~7CZjyogeBTPJ77WeFs67LgJJE10V763ssaZcAHdOpwgHb4c4Q2p9QYbwSCljDtnc7dFM0xdXGFIQN9MRpDGw~CykZOjZPK088awgI8YgtYQ__\u0026Key-Pair-Id=APKAJLOHF5GGSLRBV4ZA"}],"slug":"OVERVIEW_OF_GREEN_AND_N_2_BUSINESS_JET_AIRCRAFT_WITH_AN_EXAMPLE_OF_QJBJ_CONCEPTUAL_DESIGN_pdf","translated_slug":"","page_count":44,"language":"en","content_type":"Work","owner":{"id":4040157,"first_name":"Harijono","middle_initials":"","last_name":"Djojodihardjo","page_name":"HarijonoDjojodihardjo","domain_name":"itb","created_at":"2013-05-03T11:27:42.148-07:00","display_name":"Harijono Djojodihardjo","url":"https://itb.academia.edu/HarijonoDjojodihardjo"},"attachments":[{"id":49946710,"title":"","file_type":"pdf","scribd_thumbnail_url":"https://attachments.academia-assets.com/49946710/thumbnails/1.jpg","file_name":"OVERVIEW_OF_GREEN_AND_N_2_BUSINESS_JET_AIRCRAFT_WITH_AN_EXAMPLE_OF_QJBJ_CONCEPTUAL_DESIGN.pdf","download_url":"https://www.academia.edu/attachments/49946710/download_file?st=MTczMzAzMTQwNiw4LjIyMi4yMDguMTQ2&","bulk_download_file_name":"OVERVIEW_OF_GREEN_AND_N_2_BUSINESS_JET_A.pdf","bulk_download_url":"https://d1wqtxts1xzle7.cloudfront.net/49946710/OVERVIEW_OF_GREEN_AND_N_2_BUSINESS_JET_AIRCRAFT_WITH_AN_EXAMPLE_OF_QJBJ_CONCEPTUAL_DESIGN-libre.pdf?1477689718=\u0026response-content-disposition=attachment%3B+filename%3DOVERVIEW_OF_GREEN_AND_N_2_BUSINESS_JET_A.pdf\u0026Expires=1732987662\u0026Signature=EhC~hOwGctWUzAK0iakyJApqsxQgKZDzgNVlGkyrkBJZMASx-~Mu7jd1G6UStaUHX3Dky7RAv7ZnScLShEqDtoNrm9bnGX8U~9nfsdDATnzki~Uh0GxkNHq974nhQ-OuxYtevtTuJH~sY-SMFspB7PsUrvZdIheOFxaNCxdsKJKxUJxcl-o~5DW4motkIq0eaOaFOiUI8U9iNmAXqVMUZ~JmtJhMz5Iy23yR2roN-t~7CZjyogeBTPJ77WeFs67LgJJE10V763ssaZcAHdOpwgHb4c4Q2p9QYbwSCljDtnc7dFM0xdXGFIQN9MRpDGw~CykZOjZPK088awgI8YgtYQ__\u0026Key-Pair-Id=APKAJLOHF5GGSLRBV4ZA"}],"research_interests":[{"id":48,"name":"Engineering","url":"https://www.academia.edu/Documents/in/Engineering"},{"id":88,"name":"Aerospace Engineering","url":"https://www.academia.edu/Documents/in/Aerospace_Engineering"},{"id":988,"name":"Design","url":"https://www.academia.edu/Documents/in/Design"},{"id":13309,"name":"New Product Development","url":"https://www.academia.edu/Documents/in/New_Product_Development"},{"id":52421,"name":"Green Technology","url":"https://www.academia.edu/Documents/in/Green_Technology"}],"urls":[]}, dispatcherData: dispatcherData }); $(this).data('initialized', true); } }); $a.trackClickSource(".js-work-strip-work-link", "profile_work_strip") }); </script> <div class="js-work-strip profile--work_container" data-work-id="26059284"><div class="profile--work_thumbnail hidden-xs"><a class="js-work-strip-work-link" data-click-track="profile-work-strip-thumbnail" href="https://www.academia.edu/26059284/Potential_and_Prospects_of_Offshore_Wind_and_Photovoltaic_Energy"><img alt="Research paper thumbnail of Potential and Prospects of Offshore Wind and Photovoltaic Energy" class="work-thumbnail" src="https://attachments.academia-assets.com/46400782/thumbnails/1.jpg" /></a></div><div class="wp-workCard wp-workCard_itemContainer"><div class="wp-workCard_item wp-workCard--title"><a class="js-work-strip-work-link text-gray-darker" data-click-track="profile-work-strip-title" href="https://www.academia.edu/26059284/Potential_and_Prospects_of_Offshore_Wind_and_Photovoltaic_Energy">Potential and Prospects of Offshore Wind and Photovoltaic Energy</a></div><div class="wp-workCard_item"><span class="js-work-more-abstract-truncated">The Ocean Energy sector has the potential to contribute to the supply of energy to countries and ...</span><a class="js-work-more-abstract" data-broccoli-component="work_strip.more_abstract" data-click-track="profile-work-strip-more-abstract" href="javascript:;"><span> more </span><span><i class="fa fa-caret-down"></i></span></a><span class="js-work-more-abstract-untruncated hidden">The Ocean Energy sector has the potential to contribute to the supply of energy to countries and communities located close to the sea, although presently this considerable source of renewable energy have not been much utilized.&nbsp; The present paper focuses on current developments in offshore wind and photovoltaic energy, highlighting current efforts in many countries, particularly in the Asian-Pacific countries. The potential of these energy sources and technology will be assessed, referring to the trends in the offshore wind industry to project future growth potentials. <br />Based on an exhaustive review on Offshore Wind Energy and Photo Voltaic Power System technology and Applications in various parts of the world, and particular applications in Malaysia and Indonesia, a comprehensive insight on the potential and prospects of wind and photovoltaic energy, two promising renewable energies, are elaborated.&nbsp; An example of a&nbsp; conceptual design and preliminary configuration of a Co-Located Photovoltaic Agriculture system is proposed, including the probable investment and rate of return.</span></div><div class="wp-workCard_item wp-workCard--actions"><span class="work-strip-bookmark-button-container"></span><a id="0922a52098f6ab1eb75b80f3c3865913" class="wp-workCard--action" rel="nofollow" data-click-track="profile-work-strip-download" data-download="{&quot;attachment_id&quot;:46400782,&quot;asset_id&quot;:26059284,&quot;asset_type&quot;:&quot;Work&quot;,&quot;button_location&quot;:&quot;profile&quot;}" href="https://www.academia.edu/attachments/46400782/download_file?st=MTczMzAzMTQwNiw4LjIyMi4yMDguMTQ2&s=profile"><span><i class="fa fa-arrow-down"></i></span><span>Download</span></a><span class="wp-workCard--action visible-if-viewed-by-owner inline-block" style="display: none;"><span class="js-profile-work-strip-edit-button-wrapper profile-work-strip-edit-button-wrapper" data-work-id="26059284"><a class="js-profile-work-strip-edit-button" tabindex="0"><span><i class="fa fa-pencil"></i></span><span>Edit</span></a></span></span><span id="work-strip-rankings-button-container"></span></div><div class="wp-workCard_item wp-workCard--stats"><span><span><span class="js-view-count view-count u-mr2x" data-work-id="26059284"><i class="fa fa-spinner fa-spin"></i></span><script>$(function () { var workId = 26059284; window.Academia.workViewCountsFetcher.queue(workId, function (count) { var description = window.$h.commaizeInt(count) + " " + window.$h.pluralize(count, 'View'); $(".js-view-count[data-work-id=26059284]").text(description); $(".js-view-count[data-work-id=26059284]").attr('title', description).tooltip(); }); });</script></span></span><span><span class="percentile-widget hidden"><span class="u-mr2x work-percentile"></span></span><script>$(function () { var workId = 26059284; window.Academia.workPercentilesFetcher.queue(workId, function (percentileText) { var container = $(".js-work-strip[data-work-id='26059284']"); container.find('.work-percentile').text(percentileText.charAt(0).toUpperCase() + percentileText.slice(1)); container.find('.percentile-widget').show(); container.find('.percentile-widget').removeClass('hidden'); }); });</script></span><span><script>$(function() { new Works.PaperRankView({ workId: 26059284, container: "", }); });</script></span></div><div id="work-strip-premium-row-container"></div></div></div><script> require.config({ waitSeconds: 90 })(["https://a.academia-assets.com/assets/wow_profile-f77ea15d77ce96025a6048a514272ad8becbad23c641fc2b3bd6e24ca6ff1932.js","https://a.academia-assets.com/assets/work_edit-ad038b8c047c1a8d4fa01b402d530ff93c45fee2137a149a4a5398bc8ad67560.js"], function() { // from javascript_helper.rb var dispatcherData = {} if (true){ window.WowProfile.dispatcher = window.WowProfile.dispatcher || _.clone(Backbone.Events); dispatcherData = { dispatcher: window.WowProfile.dispatcher, downloadLinkId: "0922a52098f6ab1eb75b80f3c3865913" } } $('.js-work-strip[data-work-id=26059284]').each(function() { if (!$(this).data('initialized')) { new WowProfile.WorkStripView({ el: this, workJSON: {"id":26059284,"title":"Potential and Prospects of Offshore Wind and Photovoltaic Energy","translated_title":"","metadata":{"abstract":"The Ocean Energy sector has the potential to contribute to the supply of energy to countries and communities located close to the sea, although presently this considerable source of renewable energy have not been much utilized. The present paper focuses on current developments in offshore wind and photovoltaic energy, highlighting current efforts in many countries, particularly in the Asian-Pacific countries. The potential of these energy sources and technology will be assessed, referring to the trends in the offshore wind industry to project future growth potentials. \nBased on an exhaustive review on Offshore Wind Energy and Photo Voltaic Power System technology and Applications in various parts of the world, and particular applications in Malaysia and Indonesia, a comprehensive insight on the potential and prospects of wind and photovoltaic energy, two promising renewable energies, are elaborated. An example of a conceptual design and preliminary configuration of a Co-Located Photovoltaic Agriculture system is proposed, including the probable investment and rate of return."},"translated_abstract":"The Ocean Energy sector has the potential to contribute to the supply of energy to countries and communities located close to the sea, although presently this considerable source of renewable energy have not been much utilized. The present paper focuses on current developments in offshore wind and photovoltaic energy, highlighting current efforts in many countries, particularly in the Asian-Pacific countries. The potential of these energy sources and technology will be assessed, referring to the trends in the offshore wind industry to project future growth potentials. \nBased on an exhaustive review on Offshore Wind Energy and Photo Voltaic Power System technology and Applications in various parts of the world, and particular applications in Malaysia and Indonesia, a comprehensive insight on the potential and prospects of wind and photovoltaic energy, two promising renewable energies, are elaborated. An example of a conceptual design and preliminary configuration of a Co-Located Photovoltaic Agriculture system is proposed, including the probable investment and rate of return.","internal_url":"https://www.academia.edu/26059284/Potential_and_Prospects_of_Offshore_Wind_and_Photovoltaic_Energy","translated_internal_url":"","created_at":"2016-06-11T09:55:03.679-07:00","preview_url":null,"current_user_can_edit":null,"current_user_is_owner":null,"owner_id":4040157,"coauthors_can_edit":true,"document_type":"conference_presentation","co_author_tags":[{"id":21199865,"work_id":26059284,"tagging_user_id":4040157,"tagged_user_id":null,"co_author_invite_id":3223809,"email":"h***o@yahoo.co.id","display_order":0,"name":"H. 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href="https://www.academia.edu/122059825/HD_CV"><img alt="Research paper thumbnail of HD CV" class="work-thumbnail" src="https://attachments.academia-assets.com/116797755/thumbnails/1.jpg" /></a></div><div class="wp-workCard wp-workCard_itemContainer"><div class="wp-workCard_item wp-workCard--title"><a class="js-work-strip-work-link text-gray-darker" data-click-track="profile-work-strip-title" href="https://www.academia.edu/122059825/HD_CV">HD CV</a></div><div class="wp-workCard_item"><span>Personal and Academic Curriculum Vitae</span></div><div class="wp-workCard_item"><span class="js-work-more-abstract-truncated">Prof.HARIJONO DJOJODIHARDJO, Sc.D., IPU, ACPE Insinyur Professional Utama (IPU, Perhimpunan Insin...</span><a class="js-work-more-abstract" data-broccoli-component="work_strip.more_abstract" data-click-track="profile-work-strip-more-abstract" href="javascript:;"><span> more </span><span><i class="fa fa-caret-down"></i></span></a><span class="js-work-more-abstract-untruncated hidden">Prof.HARIJONO DJOJODIHARDJO, Sc.D., IPU, ACPE<br />Insinyur Professional Utama (IPU, Perhimpunan Insinyur Indonesia),<br />ASEAN Chartered Professional Engineer (ACPE, ASEAN Chartered Professional Engineer Coordinating Committee)<br />Academician, International Academy of Astronautics,<br />Senior Life Member, American Institute of Aeronautics and Astronautics<br />Chairman of the Board<br />Yayasan Persada Kriyareka Dirgantara (The Institute for the Advancement of Aerospace Science and Technology)<br />Jakarta 15419, Indonesia<br />Founding Member and Advisor, Pusat Kajian Teknologi dan Inovasi – Center for Technology and Innovation Studies<br />E-mail: <a href="mailto:harijono@djojodihardjo.com" rel="nofollow">harijono@djojodihardjo.com</a>;<a href="mailto:harijono.djojodihardjo@gmail.com" rel="nofollow">harijono.djojodihardjo@gmail.com</a>; <a href="mailto:harijono.djojodihardjo@yahoo.com" rel="nofollow">harijono.djojodihardjo@yahoo.com</a>; <a href="mailto:harijono@president.ac.id" rel="nofollow">harijono@president.ac.id</a>; <a href="mailto:h.djojodihardjo@alumn.mit.ed" rel="nofollow">h.djojodihardjo@alumn.mit.ed</a></span></div><div class="wp-workCard_item wp-workCard--actions"><span class="work-strip-bookmark-button-container"></span><a id="f235e297425a094427c4ac8dec2b511e" class="wp-workCard--action" rel="nofollow" data-click-track="profile-work-strip-download" data-download="{&quot;attachment_id&quot;:116797755,&quot;asset_id&quot;:122059825,&quot;asset_type&quot;:&quot;Work&quot;,&quot;button_location&quot;:&quot;profile&quot;}" href="https://www.academia.edu/attachments/116797755/download_file?st=MTczMzAzMTQwNiw4LjIyMi4yMDguMTQ2&s=profile"><span><i class="fa fa-arrow-down"></i></span><span>Download</span></a><span class="wp-workCard--action visible-if-viewed-by-owner inline-block" style="display: none;"><span class="js-profile-work-strip-edit-button-wrapper profile-work-strip-edit-button-wrapper" 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harijono.djojodihardjo@yahoo.com; harijono@president.ac.id; h.djojodihardjo@alumn.mit.ed","publication_name":"Personal and Academic Curriculum Vitae"},"translated_abstract":"Prof.HARIJONO DJOJODIHARDJO, Sc.D., IPU, ACPE\nInsinyur Professional Utama (IPU, Perhimpunan Insinyur Indonesia),\nASEAN Chartered Professional Engineer (ACPE, ASEAN Chartered Professional Engineer Coordinating Committee)\nAcademician, International Academy of Astronautics,\nSenior Life Member, American Institute of Aeronautics and Astronautics\nChairman of the Board\nYayasan Persada Kriyareka Dirgantara (The Institute for the Advancement of Aerospace Science and Technology)\nJakarta 15419, Indonesia\nFounding Member and Advisor, Pusat Kajian Teknologi dan Inovasi – Center for Technology and Innovation Studies\nE-mail: harijono@djojodihardjo.com;harijono.djojodihardjo@gmail.com; harijono.djojodihardjo@yahoo.com; harijono@president.ac.id; h.djojodihardjo@alumn.mit.ed","internal_url":"https://www.academia.edu/122059825/HD_CV","translated_internal_url":"","created_at":"2024-07-15T01:46:38.791-07:00","preview_url":null,"current_user_can_edit":null,"current_user_is_owner":null,"owner_id":4040157,"coauthors_can_edit":true,"document_type":"book","co_author_tags":[],"downloadable_attachments":[{"id":116797755,"title":"","file_type":"pdf","scribd_thumbnail_url":"https://attachments.academia-assets.com/116797755/thumbnails/1.jpg","file_name":"HD_CV_2024.pdf","download_url":"https://www.academia.edu/attachments/116797755/download_file?st=MTczMzAzMTQwNiw4LjIyMi4yMDguMTQ2&","bulk_download_file_name":"HD_CV.pdf","bulk_download_url":"https://d1wqtxts1xzle7.cloudfront.net/116797755/HD_CV_2024-libre.pdf?1721037472=\u0026response-content-disposition=attachment%3B+filename%3DHD_CV.pdf\u0026Expires=1732987662\u0026Signature=hAqp~JrV5pHeqBq4uqDPIqFMXWb5r~y-ZjNogmSz9Iyeji73ALeWvDdxGp56caAlkeF471PIf2NaDVrtGy0SOuutmVq6oXXFtGMj2Q1Q0rdh9hHkWAAIEgk2hLSJyR3pbvdvkqNzL2KrCfKzL~Xc4RIbZNI77O5dmK5SgH~I6tCs2nTAIFkPvbOKGQrDCoSg~5GaL44w1U8I4LaiQpsMlSACYuZe~KSmOfhxM3ZGmvUHtCXwoHtwkClzAINev4zt8sSMrip6FReHiE8CZvcFQXW~vdC6c~83BiyMKR53dkhwbMCOOvTkxdSAwoHVtepWD8z~jBjfpg9gyUEyNw8AWA__\u0026Key-Pair-Id=APKAJLOHF5GGSLRBV4ZA"}],"slug":"HD_CV","translated_slug":"","page_count":51,"language":"en","content_type":"Work","owner":{"id":4040157,"first_name":"Harijono","middle_initials":"","last_name":"Djojodihardjo","page_name":"HarijonoDjojodihardjo","domain_name":"itb","created_at":"2013-05-03T11:27:42.148-07:00","display_name":"Harijono 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data-click-track="profile-work-strip-thumbnail" href="https://www.academia.edu/104266047/HDS_MAKANAN_KESUKAANKU_HD_MS_AH"><img alt="Research paper thumbnail of HDS MAKANAN KESUKAANKU HD MS AH" class="work-thumbnail" src="https://attachments.academia-assets.com/104042022/thumbnails/1.jpg" /></a></div><div class="wp-workCard wp-workCard_itemContainer"><div class="wp-workCard_item wp-workCard--title"><a class="js-work-strip-work-link text-gray-darker" data-click-track="profile-work-strip-title" href="https://www.academia.edu/104266047/HDS_MAKANAN_KESUKAANKU_HD_MS_AH">HDS MAKANAN KESUKAANKU HD MS AH</a></div><div class="wp-workCard_item"><span>Makanan - Masakan Kesukaanku (My Favourite Food and Cooking)</span><span>, 2022</span></div><div class="wp-workCard_item"><span class="js-work-more-abstract-truncated">The book summarizes many different food, International and Indonesian, that are the favorite of t...</span><a class="js-work-more-abstract" data-broccoli-component="work_strip.more_abstract" data-click-track="profile-work-strip-more-abstract" href="javascript:;"><span> more </span><span><i class="fa fa-caret-down"></i></span></a><span class="js-work-more-abstract-untruncated hidden">The book summarizes many different food, International and Indonesian, that are the favorite of the authors and considered to be healthy. In addition the authors are very fond of preparing these themselves. Some food are accompanied by brief recipes. There are stories attached to almost each choice of food. At the end of&nbsp; the book, some notes on the ingredients are attached, collected from well published resources, selectively. The philosophy of enjoying the food is mentioned briefly at the end of the book. Each food is accompanied by a picture, and is written in Latin (Roman) characters, so that although the book is written in Indonesian, it may be comprehensible for many other readers.</span></div><div class="wp-workCard_item wp-workCard--actions"><span class="work-strip-bookmark-button-container"></span><a id="8d089e374a286bea92f69864455d23bc" class="wp-workCard--action" rel="nofollow" data-click-track="profile-work-strip-download" data-download="{&quot;attachment_id&quot;:104042022,&quot;asset_id&quot;:104266047,&quot;asset_type&quot;:&quot;Work&quot;,&quot;button_location&quot;:&quot;profile&quot;}" href="https://www.academia.edu/attachments/104042022/download_file?st=MTczMzAzMTQwNiw4LjIyMi4yMDguMTQ2&s=profile"><span><i class="fa fa-arrow-down"></i></span><span>Download</span></a><span class="wp-workCard--action visible-if-viewed-by-owner inline-block" style="display: none;"><span class="js-profile-work-strip-edit-button-wrapper profile-work-strip-edit-button-wrapper" data-work-id="104266047"><a class="js-profile-work-strip-edit-button" tabindex="0"><span><i class="fa fa-pencil"></i></span><span>Edit</span></a></span></span><span id="work-strip-rankings-button-container"></span></div><div class="wp-workCard_item wp-workCard--stats"><span><span><span class="js-view-count view-count u-mr2x" data-work-id="104266047"><i class="fa fa-spinner fa-spin"></i></span><script>$(function () { var workId = 104266047; window.Academia.workViewCountsFetcher.queue(workId, function (count) { var description = window.$h.commaizeInt(count) + " " + window.$h.pluralize(count, 'View'); $(".js-view-count[data-work-id=104266047]").text(description); $(".js-view-count[data-work-id=104266047]").attr('title', description).tooltip(); }); });</script></span></span><span><span class="percentile-widget hidden"><span class="u-mr2x work-percentile"></span></span><script>$(function () { var workId = 104266047; window.Academia.workPercentilesFetcher.queue(workId, function (percentileText) { var container = $(".js-work-strip[data-work-id='104266047']"); container.find('.work-percentile').text(percentileText.charAt(0).toUpperCase() + percentileText.slice(1)); container.find('.percentile-widget').show(); container.find('.percentile-widget').removeClass('hidden'); }); });</script></span><span><script>$(function() { new Works.PaperRankView({ workId: 104266047, container: "", }); });</script></span></div><div id="work-strip-premium-row-container"></div></div></div><script> require.config({ waitSeconds: 90 })(["https://a.academia-assets.com/assets/wow_profile-f77ea15d77ce96025a6048a514272ad8becbad23c641fc2b3bd6e24ca6ff1932.js","https://a.academia-assets.com/assets/work_edit-ad038b8c047c1a8d4fa01b402d530ff93c45fee2137a149a4a5398bc8ad67560.js"], function() { // from javascript_helper.rb var dispatcherData = {} if (true){ window.WowProfile.dispatcher = window.WowProfile.dispatcher || _.clone(Backbone.Events); dispatcherData = { dispatcher: window.WowProfile.dispatcher, downloadLinkId: "8d089e374a286bea92f69864455d23bc" } } $('.js-work-strip[data-work-id=104266047]').each(function() { if (!$(this).data('initialized')) { new WowProfile.WorkStripView({ el: this, workJSON: {"id":104266047,"title":"HDS MAKANAN KESUKAANKU HD MS AH","translated_title":"","metadata":{"abstract":"The book summarizes many different food, International and Indonesian, that are the favorite of the authors and considered to be healthy. 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$(this).data('initialized', true); } }); $a.trackClickSource(".js-work-strip-work-link", "profile_work_strip") }); </script> <div class="js-work-strip profile--work_container" data-work-id="44122144"><div class="profile--work_thumbnail hidden-xs"><a class="js-work-strip-work-link" data-click-track="profile-work-strip-thumbnail" href="https://www.academia.edu/44122144/INGENUITY_FOR_NATIONAL_CULTURE"><img alt="Research paper thumbnail of INGENUITY FOR NATIONAL CULTURE" class="work-thumbnail" src="https://attachments.academia-assets.com/64472518/thumbnails/1.jpg" /></a></div><div class="wp-workCard wp-workCard_itemContainer"><div class="wp-workCard_item wp-workCard--title"><a class="js-work-strip-work-link text-gray-darker" data-click-track="profile-work-strip-title" href="https://www.academia.edu/44122144/INGENUITY_FOR_NATIONAL_CULTURE">INGENUITY FOR NATIONAL CULTURE</a></div><div class="wp-workCard_item"><span>Kosa Kata Kita &amp; Persada Kriyareka Dirgantara</span><span>, 2020</span></div><div class="wp-workCard_item"><span class="js-work-more-abstract-truncated">The present book has evolved from the intention of the author to have an introspection and retros...</span><a class="js-work-more-abstract" data-broccoli-component="work_strip.more_abstract" data-click-track="profile-work-strip-more-abstract" href="javascript:;"><span> more </span><span><i class="fa fa-caret-down"></i></span></a><span class="js-work-more-abstract-untruncated hidden">The present book has evolved from the intention of the<br />author to have an introspection and retrospection of what the<br />author has experienced during his life, that is when his 80th<br />birthday forthcoming. It is also intended to be an expression to<br />God Almighty that has endowed upon him a life that the<br />author has been extremely gratified. Then, what should be<br />written should be something that the author has learned and<br />like to share with his children, grandchildren, relatives,<br />students and former students alike, and more importantly to<br />the interested readers and mankind. It is by no means an<br />autobiography or memoir, but something like a part of a “flashback”, that may represent<br />my “accountability” in life. Having spent a large part of my life in academia, as a civil<br />servant in government institutions dealing with science and technology, and partly in<br />industry, but realizing that no extraordinary achievement have been delivered to the<br />public, it seems appropriate that I would start from how and why what I have been doing<br />began. It appears to me that all of these started from “my dream”, and from what I have<br />been thankful, my capability to use my “reasoning capability”. This is something that<br />need more thoughtful elaboration, and this is all about the book. My dream and why I<br />have dreamed. I just want to share this dream and how I have been attempting to<br />realize this dream through a life paradigm that I dubbed “Being Together” reflecting the<br />high-values of mankind reflected by many, if not all religions, that is Love, Care, Share,<br />Give and Serve. In my mother’s tongue Javanese, this is expressed as “Guyub: Tresno,<br />Gumati, Asih-Asih-Asuh, Caos, Laden”. I cannot claim I have delivered many downstream<br />products to mankind and universe, but I have a dream and started to interact<br />with mankind and nature from upstream and from within my deep-self, by using the<br />most sacred gift from God-All-Mighty, my “reasoning capability”, with the objective to<br />contribute to the development of the culture of the society that should be so based,<br />though my expertise. The latter goes on the scientific attitude and scientific culture, to<br />expansion and sharing with associates the dream to generate the following dreams. As<br />cases in point, writings and presentations, are ways of expressing your dream to a certain<br />extent, disseminating ideas, and interact with co-workers, mostly young and inspiring<br />young colleagues. These I found gratifying.<br />With such background, the book is intended by the author to contribute in the<br />long run to the cultural development and transformation of the nation, along the line of<br />the historical progress of mankind, for the development of the nation to acquire smart<br />and competitive culture. And that dictates the title of the book INGENUITY FOR<br />NATIONAL CULTURE. Starting from basic philosophical point of views, motivation and<br />ideas are elaborated. The product of the dream and reasoning capabilities that have<br />been enjoyed by the author are exemplified in other dreams: presentations and<br />scientific work in partnership with co-workers that represent development efforts, which<br />could still comprise further scientifically elaborated dreams. For the author, the choice of<br />the title of the book is natural and intuitional.<br />At the beginning of the writing, the book contains chapters in Indonesia and<br />English, following the relevant event presented. Constructive suggestions by reviewers<br />lead to the split up of the book into two versions. One, a shorter version in Indonesian,<br />and another one, a most complete delivery of the ideas in English. The present one is<br />the latter. In elaborating the ideas following the dream and motivation, the chapters are<br />divided into two groups, Macro-Aspects and Micro-Aspects.<br />As a closing remark, the author would like to thank many individuals that have<br />given constructive suggestions to the preliminary edition of the book. Likewise, the<br />author would welcome further suggestions and criticism from the readers for mutual<br />interest.</span></div><div class="wp-workCard_item wp-workCard--actions"><span class="work-strip-bookmark-button-container"></span><a id="538f3e6c40a14a092bdd57f7a3bde62e" class="wp-workCard--action" rel="nofollow" data-click-track="profile-work-strip-download" data-download="{&quot;attachment_id&quot;:64472518,&quot;asset_id&quot;:44122144,&quot;asset_type&quot;:&quot;Work&quot;,&quot;button_location&quot;:&quot;profile&quot;}" href="https://www.academia.edu/attachments/64472518/download_file?st=MTczMzAzMTQwNiw4LjIyMi4yMDguMTQ2&s=profile"><span><i class="fa fa-arrow-down"></i></span><span>Download</span></a><span class="wp-workCard--action visible-if-viewed-by-owner inline-block" style="display: none;"><span class="js-profile-work-strip-edit-button-wrapper profile-work-strip-edit-button-wrapper" data-work-id="44122144"><a class="js-profile-work-strip-edit-button" tabindex="0"><span><i class="fa fa-pencil"></i></span><span>Edit</span></a></span></span><span id="work-strip-rankings-button-container"></span></div><div class="wp-workCard_item wp-workCard--stats"><span><span><span class="js-view-count view-count u-mr2x" data-work-id="44122144"><i class="fa fa-spinner fa-spin"></i></span><script>$(function () { var workId = 44122144; window.Academia.workViewCountsFetcher.queue(workId, function (count) { var description = window.$h.commaizeInt(count) + " " + window.$h.pluralize(count, 'View'); $(".js-view-count[data-work-id=44122144]").text(description); $(".js-view-count[data-work-id=44122144]").attr('title', description).tooltip(); }); });</script></span></span><span><span class="percentile-widget hidden"><span class="u-mr2x work-percentile"></span></span><script>$(function () { var workId = 44122144; window.Academia.workPercentilesFetcher.queue(workId, function (percentileText) { var container = $(".js-work-strip[data-work-id='44122144']"); container.find('.work-percentile').text(percentileText.charAt(0).toUpperCase() + percentileText.slice(1)); container.find('.percentile-widget').show(); container.find('.percentile-widget').removeClass('hidden'); }); });</script></span><span><script>$(function() { new Works.PaperRankView({ workId: 44122144, container: "", }); });</script></span></div><div id="work-strip-premium-row-container"></div></div></div><script> require.config({ waitSeconds: 90 })(["https://a.academia-assets.com/assets/wow_profile-f77ea15d77ce96025a6048a514272ad8becbad23c641fc2b3bd6e24ca6ff1932.js","https://a.academia-assets.com/assets/work_edit-ad038b8c047c1a8d4fa01b402d530ff93c45fee2137a149a4a5398bc8ad67560.js"], function() { // from javascript_helper.rb var dispatcherData = {} if (true){ window.WowProfile.dispatcher = window.WowProfile.dispatcher || _.clone(Backbone.Events); dispatcherData = { dispatcher: window.WowProfile.dispatcher, downloadLinkId: "538f3e6c40a14a092bdd57f7a3bde62e" } } $('.js-work-strip[data-work-id=44122144]').each(function() { if (!$(this).data('initialized')) { new WowProfile.WorkStripView({ el: this, workJSON: {"id":44122144,"title":"INGENUITY FOR NATIONAL CULTURE","translated_title":"","metadata":{"abstract":"The present book has evolved from the intention of the\nauthor to have an introspection and retrospection of what the\nauthor has experienced during his life, that is when his 80th\nbirthday forthcoming. It is also intended to be an expression to\nGod Almighty that has endowed upon him a life that the\nauthor has been extremely gratified. Then, what should be\nwritten should be something that the author has learned and\nlike to share with his children, grandchildren, relatives,\nstudents and former students alike, and more importantly to\nthe interested readers and mankind. It is by no means an\nautobiography or memoir, but something like a part of a “flashback”, that may represent\nmy “accountability” in life. Having spent a large part of my life in academia, as a civil\nservant in government institutions dealing with science and technology, and partly in\nindustry, but realizing that no extraordinary achievement have been delivered to the\npublic, it seems appropriate that I would start from how and why what I have been doing\nbegan. It appears to me that all of these started from “my dream”, and from what I have\nbeen thankful, my capability to use my “reasoning capability”. This is something that\nneed more thoughtful elaboration, and this is all about the book. My dream and why I\nhave dreamed. I just want to share this dream and how I have been attempting to\nrealize this dream through a life paradigm that I dubbed “Being Together” reflecting the\nhigh-values of mankind reflected by many, if not all religions, that is Love, Care, Share,\nGive and Serve. In my mother’s tongue Javanese, this is expressed as “Guyub: Tresno,\nGumati, Asih-Asih-Asuh, Caos, Laden”. I cannot claim I have delivered many downstream\nproducts to mankind and universe, but I have a dream and started to interact\nwith mankind and nature from upstream and from within my deep-self, by using the\nmost sacred gift from God-All-Mighty, my “reasoning capability”, with the objective to\ncontribute to the development of the culture of the society that should be so based,\nthough my expertise. The latter goes on the scientific attitude and scientific culture, to\nexpansion and sharing with associates the dream to generate the following dreams. As\ncases in point, writings and presentations, are ways of expressing your dream to a certain\nextent, disseminating ideas, and interact with co-workers, mostly young and inspiring\nyoung colleagues. These I found gratifying.\nWith such background, the book is intended by the author to contribute in the\nlong run to the cultural development and transformation of the nation, along the line of\nthe historical progress of mankind, for the development of the nation to acquire smart\nand competitive culture. And that dictates the title of the book INGENUITY FOR\nNATIONAL CULTURE. Starting from basic philosophical point of views, motivation and\nideas are elaborated. The product of the dream and reasoning capabilities that have\nbeen enjoyed by the author are exemplified in other dreams: presentations and\nscientific work in partnership with co-workers that represent development efforts, which\ncould still comprise further scientifically elaborated dreams. For the author, the choice of\nthe title of the book is natural and intuitional.\nAt the beginning of the writing, the book contains chapters in Indonesia and\nEnglish, following the relevant event presented. Constructive suggestions by reviewers\nlead to the split up of the book into two versions. One, a shorter version in Indonesian,\nand another one, a most complete delivery of the ideas in English. The present one is\nthe latter. In elaborating the ideas following the dream and motivation, the chapters are\ndivided into two groups, Macro-Aspects and Micro-Aspects.\nAs a closing remark, the author would like to thank many individuals that have\ngiven constructive suggestions to the preliminary edition of the book. Likewise, the\nauthor would welcome further suggestions and criticism from the readers for mutual\ninterest.\n","publication_date":{"day":null,"month":null,"year":2020,"errors":{}},"publication_name":"Kosa Kata Kita \u0026 Persada Kriyareka Dirgantara"},"translated_abstract":"The present book has evolved from the intention of the\nauthor to have an introspection and retrospection of what the\nauthor has experienced during his life, that is when his 80th\nbirthday forthcoming. It is also intended to be an expression to\nGod Almighty that has endowed upon him a life that the\nauthor has been extremely gratified. Then, what should be\nwritten should be something that the author has learned and\nlike to share with his children, grandchildren, relatives,\nstudents and former students alike, and more importantly to\nthe interested readers and mankind. It is by no means an\nautobiography or memoir, but something like a part of a “flashback”, that may represent\nmy “accountability” in life. Having spent a large part of my life in academia, as a civil\nservant in government institutions dealing with science and technology, and partly in\nindustry, but realizing that no extraordinary achievement have been delivered to the\npublic, it seems appropriate that I would start from how and why what I have been doing\nbegan. It appears to me that all of these started from “my dream”, and from what I have\nbeen thankful, my capability to use my “reasoning capability”. This is something that\nneed more thoughtful elaboration, and this is all about the book. My dream and why I\nhave dreamed. I just want to share this dream and how I have been attempting to\nrealize this dream through a life paradigm that I dubbed “Being Together” reflecting the\nhigh-values of mankind reflected by many, if not all religions, that is Love, Care, Share,\nGive and Serve. In my mother’s tongue Javanese, this is expressed as “Guyub: Tresno,\nGumati, Asih-Asih-Asuh, Caos, Laden”. I cannot claim I have delivered many downstream\nproducts to mankind and universe, but I have a dream and started to interact\nwith mankind and nature from upstream and from within my deep-self, by using the\nmost sacred gift from God-All-Mighty, my “reasoning capability”, with the objective to\ncontribute to the development of the culture of the society that should be so based,\nthough my expertise. The latter goes on the scientific attitude and scientific culture, to\nexpansion and sharing with associates the dream to generate the following dreams. As\ncases in point, writings and presentations, are ways of expressing your dream to a certain\nextent, disseminating ideas, and interact with co-workers, mostly young and inspiring\nyoung colleagues. These I found gratifying.\nWith such background, the book is intended by the author to contribute in the\nlong run to the cultural development and transformation of the nation, along the line of\nthe historical progress of mankind, for the development of the nation to acquire smart\nand competitive culture. And that dictates the title of the book INGENUITY FOR\nNATIONAL CULTURE. Starting from basic philosophical point of views, motivation and\nideas are elaborated. The product of the dream and reasoning capabilities that have\nbeen enjoyed by the author are exemplified in other dreams: presentations and\nscientific work in partnership with co-workers that represent development efforts, which\ncould still comprise further scientifically elaborated dreams. 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The approach can be further modified with certain relationships to account for the difference with physically observed phenomena using either approximation or analytically derived relationships obtained by leading researchers,<br />or by heuristically derived approximations based on analytical work, physical reasoning and experiments, and Computational Fluid Dynamic simulations.</span></div><div class="wp-workCard_item wp-workCard--actions"><span class="work-strip-bookmark-button-container"></span><a id="60d32c77c4c0c159a9984eca67d77731" class="wp-workCard--action" rel="nofollow" data-click-track="profile-work-strip-download" data-download="{&quot;attachment_id&quot;:64468682,&quot;asset_id&quot;:44118885,&quot;asset_type&quot;:&quot;Work&quot;,&quot;button_location&quot;:&quot;profile&quot;}" href="https://www.academia.edu/attachments/64468682/download_file?st=MTczMzAzMTQwNiw4LjIyMi4yMDguMTQ2&s=profile"><span><i class="fa fa-arrow-down"></i></span><span>Download</span></a><span class="wp-workCard--action visible-if-viewed-by-owner inline-block" style="display: none;"><span class="js-profile-work-strip-edit-button-wrapper profile-work-strip-edit-button-wrapper" data-work-id="44118885"><a class="js-profile-work-strip-edit-button" tabindex="0"><span><i class="fa fa-pencil"></i></span><span>Edit</span></a></span></span><span id="work-strip-rankings-button-container"></span></div><div class="wp-workCard_item wp-workCard--stats"><span><span><span class="js-view-count view-count u-mr2x" data-work-id="44118885"><i class="fa fa-spinner fa-spin"></i></span><script>$(function () { var workId = 44118885; window.Academia.workViewCountsFetcher.queue(workId, function (count) { var description = window.$h.commaizeInt(count) + " " + window.$h.pluralize(count, 'View'); $(".js-view-count[data-work-id=44118885]").text(description); $(".js-view-count[data-work-id=44118885]").attr('title', description).tooltip(); }); });</script></span></span><span><span class="percentile-widget hidden"><span class="u-mr2x work-percentile"></span></span><script>$(function () { var workId = 44118885; window.Academia.workPercentilesFetcher.queue(workId, function (percentileText) { var container = $(".js-work-strip[data-work-id='44118885']"); container.find('.work-percentile').text(percentileText.charAt(0).toUpperCase() + percentileText.slice(1)); container.find('.percentile-widget').show(); container.find('.percentile-widget').removeClass('hidden'); }); });</script></span><span><script>$(function() { new Works.PaperRankView({ workId: 44118885, container: "", }); });</script></span></div><div id="work-strip-premium-row-container"></div></div></div><script> require.config({ waitSeconds: 90 })(["https://a.academia-assets.com/assets/wow_profile-f77ea15d77ce96025a6048a514272ad8becbad23c641fc2b3bd6e24ca6ff1932.js","https://a.academia-assets.com/assets/work_edit-ad038b8c047c1a8d4fa01b402d530ff93c45fee2137a149a4a5398bc8ad67560.js"], function() { // from javascript_helper.rb var dispatcherData = {} if (true){ window.WowProfile.dispatcher = window.WowProfile.dispatcher || _.clone(Backbone.Events); dispatcherData = { dispatcher: window.WowProfile.dispatcher, downloadLinkId: "60d32c77c4c0c159a9984eca67d77731" } } $('.js-work-strip[data-work-id=44118885]').each(function() { if (!$(this).data('initialized')) { new WowProfile.WorkStripView({ el: this, workJSON: {"id":44118885,"title":"Aerodynamics and Flight Mechanics of Coandă Effect Micro Air Vehicle","translated_title":"","metadata":{"abstract":"The present especially dedicated book on the niche topic “Aerodynamic and Flight Mechanic Analysis of Coandă Effect Lift Based Micro Air Vehicle” has been a manifestation on one of my rising interests since I was asked by Bentham Recent Patents in Mechanical Engineering to write a critical review on Research, Development and Recent Patents on Aerodynamic Surface Circulation Control.\nThe main objective of the work, based on resorting to a simple approach but the capability to provide a quick impression on the physical phenomena being studied, and limitation in time and hardware resources that prevail in an educational environment,\nsubject to instructional objectives for participating students, is to devise an approach for gaining insight and carry out numerical computation and simulation approach based on first principles, aerodynamic and flight mechanic modeling, and on linearized approach. 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$(this).data('initialized', true); } }); $a.trackClickSource(".js-work-strip-work-link", "profile_work_strip") }); </script> <div class="js-work-strip profile--work_container" data-work-id="44118767"><div class="profile--work_thumbnail hidden-xs"><a class="js-work-strip-work-link" data-click-track="profile-work-strip-thumbnail" href="https://www.academia.edu/44118767/AKAL_BUDI_UNTUK_BUDAYA_BANGSA"><img alt="Research paper thumbnail of AKAL BUDI UNTUK BUDAYA BANGSA" class="work-thumbnail" src="https://attachments.academia-assets.com/64468430/thumbnails/1.jpg" /></a></div><div class="wp-workCard wp-workCard_itemContainer"><div class="wp-workCard_item wp-workCard--title"><a class="js-work-strip-work-link text-gray-darker" data-click-track="profile-work-strip-title" href="https://www.academia.edu/44118767/AKAL_BUDI_UNTUK_BUDAYA_BANGSA">AKAL BUDI UNTUK BUDAYA BANGSA</a></div><div class="wp-workCard_item"><span>AKAL BUDI UNTUK BUDAYA BANGSA</span><span>, 2020</span></div><div class="wp-workCard_item"><span class="js-work-more-abstract-truncated">The present book has evolved from the intention of the author to have an introspection and retros...</span><a class="js-work-more-abstract" data-broccoli-component="work_strip.more_abstract" data-click-track="profile-work-strip-more-abstract" href="javascript:;"><span> more </span><span><i class="fa fa-caret-down"></i></span></a><span class="js-work-more-abstract-untruncated hidden">The present book has evolved from the intention of the author to have an introspection and retrospection of what the author has experienced during his life, that is when his 80th birthday forthcoming. It is also intended to be an expression to God Almighty that has endowed upon him a life that the author has been extremely gratified. Then, what should be written should be something that the author has learned and like to share with his children, grandchildren, relatives, students and former students alike, and more importantly to the interested readers and mankind. It is by no means an autobiography or memoir, but something like a part of a “flashback”, that may represent my “accountability” in life. Having spent a large part of my life in academia, as a civil servant in government institutions dealing with science and technology, and partly in industry, but realizing that no extraordinary achievement have been delivered to the public, it seems appropriate that I would start from how and why what I have been doing began. It appears to me that all of these started from “my dream”, and from what I have been thankful, my capability to use my “reasoning capability”. This is something that need more thoughtful elaboration, and this is all about the book. My dream and why I have dreamed. I just want to share this dream and how I have been attempting to realize this dream through&nbsp; a life paradigm that I dubbed “Being Together” reflecting the high-values of mankind reflected by many, if not all religions, that is Love, Care, Share, Give and Serve. In my mother’s tongue Javanese, this is expressed as “Guyub: Tresno, Gumati, Asih-Asih-Asuh, Caos, Laden”. I cannot claim I have delivered many down-stream products to mankind and universe, but I have a dream and started to interact with mankind and nature from upstream and from within my deep-self, by using the most sacred gift from God-All-Mighty, my “reasoning capability”, with the objective to contribute to the development of the culture of the society that should be so based, though my expertise. The latter goes on the scientific attitude and scientific culture, to expansion and sharing with associates the dream to generate the following dreams. As cases in point, writings and presentations, are ways of expressing your dream to certain extent, disseminating ideas and interact with co-workers, mostly young and inspiring young colleagues. These I found gratifying.&nbsp; <br />With such background, the book is intended by the author to contribute in the long run to the cultural development and transformation of the nation, along the line of the historical progress of mankind, for the development of the nation to acquire smart and competitive culture. And that dictates the title of the book INGENUITY FOR NATIONAL CULTURE. Starting from basic philosophical point of views, motivation and ideas are elaborated. The product of the dream and reasoning capabilities that have been enjoyed by the author are exemplified in other dreams: presentations and scientific work in partnership with co-workers that represent development efforts, which could still comprise further scientifically elaborated dreams. For the author, the choice of the title of the book is natural and intuitional. <br />To complement the ideas elaborated in the chapters, the author provides a detailed biography. Having completed his engineering education at the Institute of Technology of Bandung (ITB), University of Kentucky and Massachusetts Institute of Technology (MIT) , he has served as academic faculty member at ITB and other universities, at the Government Science and Technology Offices such as The Indonesian Space Agency (LAPAN), the Agency for the Assessment and Application of Technology (BPPT), The Indonesia Aircraft Industry (PT IPTN, now PT DI) and the Office of the President, among others. These experiences have strengthened his motivation and dedication to contribute pro-actively for the cultural development of his Nation, at his capacity as a member of the silent moral force.<br />At the beginning of the writing, the book contains chapters in Indonesia and English, following the relevant event presented. Constructive suggestions by reviewers&nbsp; lead to the split up of the book into two versions. One, a shorter version in Indonesian, and another one, a most complete delivery of the ideas in English. The present one is the latter. In elaborating the ideas following the dream and motivation, the chapters are divided into two groups, Macro-Aspects and Micro-Aspects. <br />The biography of the author is elaborated in some detail en-lieu of elaborating it in the main text to provide further background for the essays contained in the main body of the book.<br />As a closing remark, the author would like to thank many individuals that have given constructive suggestions to the preliminary edition of the book. Likewise, the author would welcome further suggestions and criticism from the readers for mutual interest.</span></div><div class="wp-workCard_item wp-workCard--actions"><span class="work-strip-bookmark-button-container"></span><a id="77a7a83c93131e35dd96c948d571acf2" class="wp-workCard--action" rel="nofollow" data-click-track="profile-work-strip-download" data-download="{&quot;attachment_id&quot;:64468430,&quot;asset_id&quot;:44118767,&quot;asset_type&quot;:&quot;Work&quot;,&quot;button_location&quot;:&quot;profile&quot;}" href="https://www.academia.edu/attachments/64468430/download_file?st=MTczMzAzMTQwNiw4LjIyMi4yMDguMTQ2&s=profile"><span><i class="fa fa-arrow-down"></i></span><span>Download</span></a><span class="wp-workCard--action visible-if-viewed-by-owner inline-block" style="display: none;"><span class="js-profile-work-strip-edit-button-wrapper profile-work-strip-edit-button-wrapper" data-work-id="44118767"><a class="js-profile-work-strip-edit-button" tabindex="0"><span><i class="fa fa-pencil"></i></span><span>Edit</span></a></span></span><span id="work-strip-rankings-button-container"></span></div><div class="wp-workCard_item wp-workCard--stats"><span><span><span class="js-view-count view-count u-mr2x" data-work-id="44118767"><i class="fa fa-spinner fa-spin"></i></span><script>$(function () { var workId = 44118767; window.Academia.workViewCountsFetcher.queue(workId, function (count) { var description = window.$h.commaizeInt(count) + " " + window.$h.pluralize(count, 'View'); $(".js-view-count[data-work-id=44118767]").text(description); $(".js-view-count[data-work-id=44118767]").attr('title', description).tooltip(); }); });</script></span></span><span><span class="percentile-widget hidden"><span class="u-mr2x work-percentile"></span></span><script>$(function () { var workId = 44118767; window.Academia.workPercentilesFetcher.queue(workId, function (percentileText) { var container = $(".js-work-strip[data-work-id='44118767']"); container.find('.work-percentile').text(percentileText.charAt(0).toUpperCase() + percentileText.slice(1)); container.find('.percentile-widget').show(); container.find('.percentile-widget').removeClass('hidden'); }); });</script></span><span><script>$(function() { new Works.PaperRankView({ workId: 44118767, container: "", }); });</script></span></div><div id="work-strip-premium-row-container"></div></div></div><script> require.config({ waitSeconds: 90 })(["https://a.academia-assets.com/assets/wow_profile-f77ea15d77ce96025a6048a514272ad8becbad23c641fc2b3bd6e24ca6ff1932.js","https://a.academia-assets.com/assets/work_edit-ad038b8c047c1a8d4fa01b402d530ff93c45fee2137a149a4a5398bc8ad67560.js"], function() { // from javascript_helper.rb var dispatcherData = {} if (true){ window.WowProfile.dispatcher = window.WowProfile.dispatcher || _.clone(Backbone.Events); dispatcherData = { dispatcher: window.WowProfile.dispatcher, downloadLinkId: "77a7a83c93131e35dd96c948d571acf2" } } $('.js-work-strip[data-work-id=44118767]').each(function() { if (!$(this).data('initialized')) { new WowProfile.WorkStripView({ el: this, workJSON: {"id":44118767,"title":"AKAL BUDI UNTUK BUDAYA BANGSA","translated_title":"","metadata":{"abstract":"The present book has evolved from the intention of the author to have an introspection and retrospection of what the author has experienced during his life, that is when his 80th birthday forthcoming. It is also intended to be an expression to God Almighty that has endowed upon him a life that the author has been extremely gratified. Then, what should be written should be something that the author has learned and like to share with his children, grandchildren, relatives, students and former students alike, and more importantly to the interested readers and mankind. It is by no means an autobiography or memoir, but something like a part of a “flashback”, that may represent my “accountability” in life. Having spent a large part of my life in academia, as a civil servant in government institutions dealing with science and technology, and partly in industry, but realizing that no extraordinary achievement have been delivered to the public, it seems appropriate that I would start from how and why what I have been doing began. It appears to me that all of these started from “my dream”, and from what I have been thankful, my capability to use my “reasoning capability”. This is something that need more thoughtful elaboration, and this is all about the book. My dream and why I have dreamed. I just want to share this dream and how I have been attempting to realize this dream through a life paradigm that I dubbed “Being Together” reflecting the high-values of mankind reflected by many, if not all religions, that is Love, Care, Share, Give and Serve. In my mother’s tongue Javanese, this is expressed as “Guyub: Tresno, Gumati, Asih-Asih-Asuh, Caos, Laden”. I cannot claim I have delivered many down-stream products to mankind and universe, but I have a dream and started to interact with mankind and nature from upstream and from within my deep-self, by using the most sacred gift from God-All-Mighty, my “reasoning capability”, with the objective to contribute to the development of the culture of the society that should be so based, though my expertise. The latter goes on the scientific attitude and scientific culture, to expansion and sharing with associates the dream to generate the following dreams. As cases in point, writings and presentations, are ways of expressing your dream to certain extent, disseminating ideas and interact with co-workers, mostly young and inspiring young colleagues. These I found gratifying. \nWith such background, the book is intended by the author to contribute in the long run to the cultural development and transformation of the nation, along the line of the historical progress of mankind, for the development of the nation to acquire smart and competitive culture. And that dictates the title of the book INGENUITY FOR NATIONAL CULTURE. Starting from basic philosophical point of views, motivation and ideas are elaborated. The product of the dream and reasoning capabilities that have been enjoyed by the author are exemplified in other dreams: presentations and scientific work in partnership with co-workers that represent development efforts, which could still comprise further scientifically elaborated dreams. For the author, the choice of the title of the book is natural and intuitional. \nTo complement the ideas elaborated in the chapters, the author provides a detailed biography. Having completed his engineering education at the Institute of Technology of Bandung (ITB), University of Kentucky and Massachusetts Institute of Technology (MIT) , he has served as academic faculty member at ITB and other universities, at the Government Science and Technology Offices such as The Indonesian Space Agency (LAPAN), the Agency for the Assessment and Application of Technology (BPPT), The Indonesia Aircraft Industry (PT IPTN, now PT DI) and the Office of the President, among others. These experiences have strengthened his motivation and dedication to contribute pro-actively for the cultural development of his Nation, at his capacity as a member of the silent moral force.\nAt the beginning of the writing, the book contains chapters in Indonesia and English, following the relevant event presented. Constructive suggestions by reviewers lead to the split up of the book into two versions. One, a shorter version in Indonesian, and another one, a most complete delivery of the ideas in English. The present one is the latter. In elaborating the ideas following the dream and motivation, the chapters are divided into two groups, Macro-Aspects and Micro-Aspects. \nThe biography of the author is elaborated in some detail en-lieu of elaborating it in the main text to provide further background for the essays contained in the main body of the book.\nAs a closing remark, the author would like to thank many individuals that have given constructive suggestions to the preliminary edition of the book. Likewise, the author would welcome further suggestions and criticism from the readers for mutual interest.\n\n","publication_date":{"day":null,"month":null,"year":2020,"errors":{}},"publication_name":"AKAL BUDI UNTUK BUDAYA BANGSA"},"translated_abstract":"The present book has evolved from the intention of the author to have an introspection and retrospection of what the author has experienced during his life, that is when his 80th birthday forthcoming. It is also intended to be an expression to God Almighty that has endowed upon him a life that the author has been extremely gratified. Then, what should be written should be something that the author has learned and like to share with his children, grandchildren, relatives, students and former students alike, and more importantly to the interested readers and mankind. It is by no means an autobiography or memoir, but something like a part of a “flashback”, that may represent my “accountability” in life. Having spent a large part of my life in academia, as a civil servant in government institutions dealing with science and technology, and partly in industry, but realizing that no extraordinary achievement have been delivered to the public, it seems appropriate that I would start from how and why what I have been doing began. It appears to me that all of these started from “my dream”, and from what I have been thankful, my capability to use my “reasoning capability”. This is something that need more thoughtful elaboration, and this is all about the book. My dream and why I have dreamed. I just want to share this dream and how I have been attempting to realize this dream through a life paradigm that I dubbed “Being Together” reflecting the high-values of mankind reflected by many, if not all religions, that is Love, Care, Share, Give and Serve. In my mother’s tongue Javanese, this is expressed as “Guyub: Tresno, Gumati, Asih-Asih-Asuh, Caos, Laden”. I cannot claim I have delivered many down-stream products to mankind and universe, but I have a dream and started to interact with mankind and nature from upstream and from within my deep-self, by using the most sacred gift from God-All-Mighty, my “reasoning capability”, with the objective to contribute to the development of the culture of the society that should be so based, though my expertise. The latter goes on the scientific attitude and scientific culture, to expansion and sharing with associates the dream to generate the following dreams. As cases in point, writings and presentations, are ways of expressing your dream to certain extent, disseminating ideas and interact with co-workers, mostly young and inspiring young colleagues. These I found gratifying. \nWith such background, the book is intended by the author to contribute in the long run to the cultural development and transformation of the nation, along the line of the historical progress of mankind, for the development of the nation to acquire smart and competitive culture. And that dictates the title of the book INGENUITY FOR NATIONAL CULTURE. Starting from basic philosophical point of views, motivation and ideas are elaborated. The product of the dream and reasoning capabilities that have been enjoyed by the author are exemplified in other dreams: presentations and scientific work in partnership with co-workers that represent development efforts, which could still comprise further scientifically elaborated dreams. For the author, the choice of the title of the book is natural and intuitional. \nTo complement the ideas elaborated in the chapters, the author provides a detailed biography. Having completed his engineering education at the Institute of Technology of Bandung (ITB), University of Kentucky and Massachusetts Institute of Technology (MIT) , he has served as academic faculty member at ITB and other universities, at the Government Science and Technology Offices such as The Indonesian Space Agency (LAPAN), the Agency for the Assessment and Application of Technology (BPPT), The Indonesia Aircraft Industry (PT IPTN, now PT DI) and the Office of the President, among others. These experiences have strengthened his motivation and dedication to contribute pro-actively for the cultural development of his Nation, at his capacity as a member of the silent moral force.\nAt the beginning of the writing, the book contains chapters in Indonesia and English, following the relevant event presented. Constructive suggestions by reviewers lead to the split up of the book into two versions. One, a shorter version in Indonesian, and another one, a most complete delivery of the ideas in English. The present one is the latter. In elaborating the ideas following the dream and motivation, the chapters are divided into two groups, Macro-Aspects and Micro-Aspects. \nThe biography of the author is elaborated in some detail en-lieu of elaborating it in the main text to provide further background for the essays contained in the main body of the book.\nAs a closing remark, the author would like to thank many individuals that have given constructive suggestions to the preliminary edition of the book. Likewise, the author would welcome further suggestions and criticism from the readers for mutual interest.\n\n","internal_url":"https://www.academia.edu/44118767/AKAL_BUDI_UNTUK_BUDAYA_BANGSA","translated_internal_url":"","created_at":"2020-09-18T23:27:53.601-07:00","preview_url":null,"current_user_can_edit":null,"current_user_is_owner":null,"owner_id":4040157,"coauthors_can_edit":true,"document_type":"book","co_author_tags":[],"downloadable_attachments":[{"id":64468430,"title":"","file_type":"pdf","scribd_thumbnail_url":"https://attachments.academia-assets.com/64468430/thumbnails/1.jpg","file_name":"HD-AKAL BUDI UNTUK BUDAYA BANGSA-Versi-13- Cover-Complete-f-16 July 2020-app-19 September 2020.pdf","download_url":"https://www.academia.edu/attachments/64468430/download_file?st=MTczMzAzMTQwNiw4LjIyMi4yMDguMTQ2&","bulk_download_file_name":"AKAL_BUDI_UNTUK_BUDAYA_BANGSA.pdf","bulk_download_url":"https://d1wqtxts1xzle7.cloudfront.net/64468430/HD-AKAL_BUDI_UNTUK_BUDAYA_BANGSA-Versi-13-_Cover-Complete-f-16_July_2020-app-19_September_2020-libre.pdf?1600497822=\u0026response-content-disposition=attachment%3B+filename%3DAKAL_BUDI_UNTUK_BUDAYA_BANGSA.pdf\u0026Expires=1732245646\u0026Signature=QGh~ccNqGhHpLB45keuf8g7guo7hefTBbIwj3uweIXyBuuXnkmcnN08u7WvUUdb5O6kEIlBMt4UWHM3TsoTEpgWY9J7DwUGnH82rTaKltD~GLQ~bbrDZ~ti-oN9tf7hGvaqnLM0ecnOdGYmLhPY7C63jdnroIkGYqTpFzStIvPPSMCLlzwb0evfNE2DnP6Kj6vi5FdvbYXFCbQXYPyuUH6asxV4Tx66jFvpdF40tnU~CAaV8FjtJtMyUhUCpXsF1F4R1dH-4-Sjc7XVWj2sN95QuaUT99K4ztoOm2CMRvG8k1-1L~MN-PfgVU5YxKea8H-nAoGQQ008umGNul9WlzA__\u0026Key-Pair-Id=APKAJLOHF5GGSLRBV4ZA"}],"slug":"AKAL_BUDI_UNTUK_BUDAYA_BANGSA","translated_slug":"","page_count":228,"language":"id","content_type":"Work","owner":{"id":4040157,"first_name":"Harijono","middle_initials":"","last_name":"Djojodihardjo","page_name":"HarijonoDjojodihardjo","domain_name":"itb","created_at":"2013-05-03T11:27:42.148-07:00","display_name":"Harijono Djojodihardjo","url":"https://itb.academia.edu/HarijonoDjojodihardjo"},"attachments":[{"id":64468430,"title":"","file_type":"pdf","scribd_thumbnail_url":"https://attachments.academia-assets.com/64468430/thumbnails/1.jpg","file_name":"HD-AKAL BUDI UNTUK BUDAYA BANGSA-Versi-13- Cover-Complete-f-16 July 2020-app-19 September 2020.pdf","download_url":"https://www.academia.edu/attachments/64468430/download_file?st=MTczMzAzMTQwNiw4LjIyMi4yMDguMTQ2&","bulk_download_file_name":"AKAL_BUDI_UNTUK_BUDAYA_BANGSA.pdf","bulk_download_url":"https://d1wqtxts1xzle7.cloudfront.net/64468430/HD-AKAL_BUDI_UNTUK_BUDAYA_BANGSA-Versi-13-_Cover-Complete-f-16_July_2020-app-19_September_2020-libre.pdf?1600497822=\u0026response-content-disposition=attachment%3B+filename%3DAKAL_BUDI_UNTUK_BUDAYA_BANGSA.pdf\u0026Expires=1732245646\u0026Signature=QGh~ccNqGhHpLB45keuf8g7guo7hefTBbIwj3uweIXyBuuXnkmcnN08u7WvUUdb5O6kEIlBMt4UWHM3TsoTEpgWY9J7DwUGnH82rTaKltD~GLQ~bbrDZ~ti-oN9tf7hGvaqnLM0ecnOdGYmLhPY7C63jdnroIkGYqTpFzStIvPPSMCLlzwb0evfNE2DnP6Kj6vi5FdvbYXFCbQXYPyuUH6asxV4Tx66jFvpdF40tnU~CAaV8FjtJtMyUhUCpXsF1F4R1dH-4-Sjc7XVWj2sN95QuaUT99K4ztoOm2CMRvG8k1-1L~MN-PfgVU5YxKea8H-nAoGQQ008umGNul9WlzA__\u0026Key-Pair-Id=APKAJLOHF5GGSLRBV4ZA"}],"research_interests":[{"id":88,"name":"Aerospace Engineering","url":"https://www.academia.edu/Documents/in/Aerospace_Engineering"},{"id":2298,"name":"Computational Fluid Dynamics","url":"https://www.academia.edu/Documents/in/Computational_Fluid_Dynamics"},{"id":4070,"name":"Structural Dynamics","url":"https://www.academia.edu/Documents/in/Structural_Dynamics"},{"id":10875,"name":"Aerodynamics","url":"https://www.academia.edu/Documents/in/Aerodynamics"},{"id":18845,"name":"Environmental Sustainability","url":"https://www.academia.edu/Documents/in/Environmental_Sustainability"},{"id":45039,"name":"Aerospace Engineering and Control System Engineering","url":"https://www.academia.edu/Documents/in/Aerospace_Engineering_and_Control_System_Engineering"},{"id":79152,"name":"Cultural Development","url":"https://www.academia.edu/Documents/in/Cultural_Development"},{"id":1445396,"name":"Applied Mathematics and Modelling Mechanical Engineering","url":"https://www.academia.edu/Documents/in/Applied_Mathematics_and_Modelling_Mechanical_Engineering"},{"id":1557164,"name":"Renewable Energy and Climate Change","url":"https://www.academia.edu/Documents/in/Renewable_Energy_and_Climate_Change"},{"id":1772635,"name":"Solar and Wind Energy","url":"https://www.academia.edu/Documents/in/Solar_and_Wind_Energy-1"}],"urls":[]}, dispatcherData: dispatcherData }); $(this).data('initialized', true); } }); $a.trackClickSource(".js-work-strip-work-link", "profile_work_strip") }); </script> <div class="js-work-strip profile--work_container" data-work-id="33516476"><div class="profile--work_thumbnail hidden-xs"><a class="js-work-strip-work-link" data-click-track="profile-work-strip-thumbnail" href="https://www.academia.edu/33516476/NUMERICAL_MODELLING_OF_FLAPPING_WING_KINEMATICS_AND_AERODYNAMICS_978_3_330_03529_wcover_pdf"><img alt="Research paper thumbnail of NUMERICAL MODELLING OF FLAPPING WING KINEMATICS AND AERODYNAMICS-978-3-330-03529-wcover.pdf" class="work-thumbnail" src="https://attachments.academia-assets.com/53552420/thumbnails/1.jpg" /></a></div><div class="wp-workCard wp-workCard_itemContainer"><div class="wp-workCard_item wp-workCard--title"><a class="js-work-strip-work-link text-gray-darker" data-click-track="profile-work-strip-title" href="https://www.academia.edu/33516476/NUMERICAL_MODELLING_OF_FLAPPING_WING_KINEMATICS_AND_AERODYNAMICS_978_3_330_03529_wcover_pdf">NUMERICAL MODELLING OF FLAPPING WING KINEMATICS AND AERODYNAMICS-978-3-330-03529-wcover.pdf</a></div><div class="wp-workCard_item"><span class="js-work-more-abstract-truncated">The present manuscript is a part of a series of work carried out by the author assisted by some c...</span><a class="js-work-more-abstract" data-broccoli-component="work_strip.more_abstract" data-click-track="profile-work-strip-more-abstract" href="javascript:;"><span> more </span><span><i class="fa fa-caret-down"></i></span></a><span class="js-work-more-abstract-untruncated hidden">The present manuscript is a part of a series of work carried out by the author assisted by some coworkers to address the exciting and inspiring field of birds’ and insects flight following a generic approach based on first principles to model the kinematics and aerodynamics of flapping wing ornithopter. The work is focused on flapping bi-wing and quad-wing ornithopter modeled and analyzed to mimic flapping wing biosystems to produce lift and thrust for forward flight. The emphasis of the work and the associated analysis, referring to a paradigm due to Weis-Fogh [1], has been placed on simplicity in the approach for quick estimate and understanding on the underlying principle, based on first principles of physics and applied mechanics.<br />Through a priori meticulous assumptions and sound application of first principles, the approach should be capable to reveal pertinent features of the physical phenomena to a logical and acceptable extent. A posteriori assessment of such approach would judge the extent of its applicability. Such approach involves approximations since the true flight system is so complicated which may not be tractable using first principles in their simple forms. However, when the analysis is confined to free flight and make use of the most reliable flight data available, the task will be more manageable, since it is possible to introduce simple corrections.<br />Then the objectives and contributions of this work are (i) To present and asses a simple approach which are based on first principles, translated into in house computational programs that should be capable of revealing particular characteristics, for conceptual design tool and establishing a simple and workable model. (ii) To review and establish a baseline of the state of the art based on the wealth of literature to date as check points. (iii) To summarize some critical and relevant characteristics, and identify which of these could be tackled with a simple approach, and which<br />cannot. (iv) To assess the usefulness and limitations of the approach, which will be useful for further elaborate approach.</span></div><div class="wp-workCard_item wp-workCard--actions"><span class="work-strip-bookmark-button-container"></span><a id="5999e25fbd8eb0162f336763efba8d6e" class="wp-workCard--action" rel="nofollow" data-click-track="profile-work-strip-download" data-download="{&quot;attachment_id&quot;:53552420,&quot;asset_id&quot;:33516476,&quot;asset_type&quot;:&quot;Work&quot;,&quot;button_location&quot;:&quot;profile&quot;}" href="https://www.academia.edu/attachments/53552420/download_file?st=MTczMzAzMTQwNiw4LjIyMi4yMDguMTQ2&s=profile"><span><i class="fa fa-arrow-down"></i></span><span>Download</span></a><span class="wp-workCard--action visible-if-viewed-by-owner inline-block" style="display: none;"><span class="js-profile-work-strip-edit-button-wrapper profile-work-strip-edit-button-wrapper" data-work-id="33516476"><a class="js-profile-work-strip-edit-button" tabindex="0"><span><i class="fa fa-pencil"></i></span><span>Edit</span></a></span></span><span id="work-strip-rankings-button-container"></span></div><div class="wp-workCard_item wp-workCard--stats"><span><span><span class="js-view-count view-count u-mr2x" data-work-id="33516476"><i class="fa fa-spinner fa-spin"></i></span><script>$(function () { var workId = 33516476; window.Academia.workViewCountsFetcher.queue(workId, function (count) { var description = window.$h.commaizeInt(count) + " " + window.$h.pluralize(count, 'View'); $(".js-view-count[data-work-id=33516476]").text(description); $(".js-view-count[data-work-id=33516476]").attr('title', description).tooltip(); }); });</script></span></span><span><span class="percentile-widget hidden"><span class="u-mr2x work-percentile"></span></span><script>$(function () { var workId = 33516476; window.Academia.workPercentilesFetcher.queue(workId, function (percentileText) { var container = $(".js-work-strip[data-work-id='33516476']"); container.find('.work-percentile').text(percentileText.charAt(0).toUpperCase() + percentileText.slice(1)); container.find('.percentile-widget').show(); container.find('.percentile-widget').removeClass('hidden'); }); });</script></span><span><script>$(function() { new Works.PaperRankView({ workId: 33516476, container: "", }); });</script></span></div><div id="work-strip-premium-row-container"></div></div></div><script> require.config({ waitSeconds: 90 })(["https://a.academia-assets.com/assets/wow_profile-f77ea15d77ce96025a6048a514272ad8becbad23c641fc2b3bd6e24ca6ff1932.js","https://a.academia-assets.com/assets/work_edit-ad038b8c047c1a8d4fa01b402d530ff93c45fee2137a149a4a5398bc8ad67560.js"], function() { // from javascript_helper.rb var dispatcherData = {} if (true){ window.WowProfile.dispatcher = window.WowProfile.dispatcher || _.clone(Backbone.Events); dispatcherData = { dispatcher: window.WowProfile.dispatcher, downloadLinkId: "5999e25fbd8eb0162f336763efba8d6e" } } $('.js-work-strip[data-work-id=33516476]').each(function() { if (!$(this).data('initialized')) { new WowProfile.WorkStripView({ el: this, workJSON: {"id":33516476,"title":"NUMERICAL MODELLING OF FLAPPING WING KINEMATICS AND AERODYNAMICS-978-3-330-03529-wcover.pdf","translated_title":"","metadata":{"abstract":"The present manuscript is a part of a series of work carried out by the author assisted by some coworkers to address the exciting and inspiring field of birds’ and insects flight following a generic approach based on first principles to model the kinematics and aerodynamics of flapping wing ornithopter. 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However, when the analysis is confined to free flight and make use of the most reliable flight data available, the task will be more manageable, since it is possible to introduce simple corrections.\nThen the objectives and contributions of this work are (i) To present and asses a simple approach which are based on first principles, translated into in house computational programs that should be capable of revealing particular characteristics, for conceptual design tool and establishing a simple and workable model. (ii) To review and establish a baseline of the state of the art based on the wealth of literature to date as check points. (iii) To summarize some critical and relevant characteristics, and identify which of these could be tackled with a simple approach, and which\ncannot. 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The emphasis of the work and the associated analysis, referring to a paradigm due to Weis-Fogh [1], has been placed on simplicity in the approach for quick estimate and understanding on the underlying principle, based on first principles of physics and applied mechanics.\nThrough a priori meticulous assumptions and sound application of first principles, the approach should be capable to reveal pertinent features of the physical phenomena to a logical and acceptable extent. A posteriori assessment of such approach would judge the extent of its applicability. Such approach involves approximations since the true flight system is so complicated which may not be tractable using first principles in their simple forms. However, when the analysis is confined to free flight and make use of the most reliable flight data available, the task will be more manageable, since it is possible to introduce simple corrections.\nThen the objectives and contributions of this work are (i) To present and asses a simple approach which are based on first principles, translated into in house computational programs that should be capable of revealing particular characteristics, for conceptual design tool and establishing a simple and workable model. (ii) To review and establish a baseline of the state of the art based on the wealth of literature to date as check points. (iii) To summarize some critical and relevant characteristics, and identify which of these could be tackled with a simple approach, and which\ncannot. 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$(this).data('initialized', true); } }); $a.trackClickSource(".js-work-strip-work-link", "profile_work_strip") }); </script> <div class="js-work-strip profile--work_container" data-work-id="27084459"><div class="profile--work_thumbnail hidden-xs"><a class="js-work-strip-work-link" data-click-track="profile-work-strip-thumbnail" href="https://www.academia.edu/27084459/Modeling_and_Simulation_Techniques_in_Structural_Engineering_ACOUSTIC_METHOD_FOR_THE_SUPPRESSION_OF_ACOUSTIC_AND_AERODYNAMICALLY_INDUCED_VIBRATION_ON_PLATES"><img alt="Research paper thumbnail of Modeling and Simulation Techniques in Structural Engineering ACOUSTIC METHOD FOR THE SUPPRESSION OF ACOUSTIC AND AERODYNAMICALLY INDUCED VIBRATION ON PLATES" class="work-thumbnail" src="https://attachments.academia-assets.com/47337760/thumbnails/1.jpg" /></a></div><div class="wp-workCard wp-workCard_itemContainer"><div class="wp-workCard_item wp-workCard--title"><a class="js-work-strip-work-link text-gray-darker" data-click-track="profile-work-strip-title" href="https://www.academia.edu/27084459/Modeling_and_Simulation_Techniques_in_Structural_Engineering_ACOUSTIC_METHOD_FOR_THE_SUPPRESSION_OF_ACOUSTIC_AND_AERODYNAMICALLY_INDUCED_VIBRATION_ON_PLATES">Modeling and Simulation Techniques in Structural Engineering ACOUSTIC METHOD FOR THE SUPPRESSION OF ACOUSTIC AND AERODYNAMICALLY INDUCED VIBRATION ON PLATES</a></div><div class="wp-workCard_item"><span class="js-work-more-abstract-truncated">The close relationship between noise and vibration is reviewed and analyzed for the interest of t...</span><a class="js-work-more-abstract" data-broccoli-component="work_strip.more_abstract" data-click-track="profile-work-strip-more-abstract" href="javascript:;"><span> more </span><span><i class="fa fa-caret-down"></i></span></a><span class="js-work-more-abstract-untruncated hidden">The close relationship between noise and vibration is reviewed and analyzed for the interest of the suppression of noise and vibration occurring in structures. Two suppression methods for noise and vibration, both by acoustic means, are addressed. For the first problem, an analysis is carried out on the representation of noise by monopoles and their higher harmonics, and to devise a straightforward method to counter their influence by selective secondary acoustic source. The second problem is analyzed using a methodology developed earlier for the computational scheme for the calculation of the acoustic disturbance to the aeroelasticity of structures. The generic approach of the latter consists of three parts. The first is the formulation of the acoustic wave propagation governed by the Helmholtz equation by using boundary element approach, to allow the calculation of the acoustic pressure on the acoustic-structure boundaries. The structural dynamic problem is formulated using finite elements. The third part involves the calculation of the unsteady aerodynamics loading on the structure using unsteady aerodynamics computational method.</span></div><div class="wp-workCard_item wp-workCard--actions"><span class="work-strip-bookmark-button-container"></span><a id="7a1bfef9138d28208f7c8e5cc2dae32c" class="wp-workCard--action" rel="nofollow" data-click-track="profile-work-strip-download" data-download="{&quot;attachment_id&quot;:47337760,&quot;asset_id&quot;:27084459,&quot;asset_type&quot;:&quot;Work&quot;,&quot;button_location&quot;:&quot;profile&quot;}" href="https://www.academia.edu/attachments/47337760/download_file?st=MTczMzAzMTQwNiw4LjIyMi4yMDguMTQ2&s=profile"><span><i class="fa fa-arrow-down"></i></span><span>Download</span></a><span class="wp-workCard--action visible-if-viewed-by-owner inline-block" style="display: none;"><span class="js-profile-work-strip-edit-button-wrapper profile-work-strip-edit-button-wrapper" data-work-id="27084459"><a class="js-profile-work-strip-edit-button" tabindex="0"><span><i class="fa fa-pencil"></i></span><span>Edit</span></a></span></span><span id="work-strip-rankings-button-container"></span></div><div class="wp-workCard_item wp-workCard--stats"><span><span><span class="js-view-count view-count u-mr2x" data-work-id="27084459"><i class="fa fa-spinner fa-spin"></i></span><script>$(function () { var workId = 27084459; window.Academia.workViewCountsFetcher.queue(workId, function (count) { var description = window.$h.commaizeInt(count) + " " + window.$h.pluralize(count, 'View'); $(".js-view-count[data-work-id=27084459]").text(description); $(".js-view-count[data-work-id=27084459]").attr('title', description).tooltip(); }); });</script></span></span><span><span class="percentile-widget hidden"><span class="u-mr2x work-percentile"></span></span><script>$(function () { var workId = 27084459; window.Academia.workPercentilesFetcher.queue(workId, function (percentileText) { var container = $(".js-work-strip[data-work-id='27084459']"); container.find('.work-percentile').text(percentileText.charAt(0).toUpperCase() + percentileText.slice(1)); container.find('.percentile-widget').show(); container.find('.percentile-widget').removeClass('hidden'); }); });</script></span><span><script>$(function() { new Works.PaperRankView({ workId: 27084459, container: "", }); });</script></span></div><div id="work-strip-premium-row-container"></div></div></div><script> require.config({ waitSeconds: 90 })(["https://a.academia-assets.com/assets/wow_profile-f77ea15d77ce96025a6048a514272ad8becbad23c641fc2b3bd6e24ca6ff1932.js","https://a.academia-assets.com/assets/work_edit-ad038b8c047c1a8d4fa01b402d530ff93c45fee2137a149a4a5398bc8ad67560.js"], function() { // from javascript_helper.rb var dispatcherData = {} if (true){ window.WowProfile.dispatcher = window.WowProfile.dispatcher || _.clone(Backbone.Events); dispatcherData = { dispatcher: window.WowProfile.dispatcher, downloadLinkId: "7a1bfef9138d28208f7c8e5cc2dae32c" } } $('.js-work-strip[data-work-id=27084459]').each(function() { if (!$(this).data('initialized')) { new WowProfile.WorkStripView({ el: this, workJSON: {"id":27084459,"title":"Modeling and Simulation Techniques in Structural Engineering ACOUSTIC METHOD FOR THE SUPPRESSION OF ACOUSTIC AND AERODYNAMICALLY INDUCED VIBRATION ON PLATES","translated_title":"","metadata":{"abstract":"The close relationship between noise and vibration is reviewed and analyzed for the interest of the suppression of noise and vibration occurring in structures. 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$(this).data('initialized', true); } }); $a.trackClickSource(".js-work-strip-work-link", "profile_work_strip") }); </script> </div><div class="profile--tab_content_container js-tab-pane tab-pane" data-section-id="10655008" id="teachingdocuments"><div class="js-work-strip profile--work_container" data-work-id="44122042"><div class="profile--work_thumbnail hidden-xs"><a class="js-work-strip-work-link" data-click-track="profile-work-strip-thumbnail" href="https://www.academia.edu/44122042/THE_PROSPECT_of_SOLAR_ENERGY_UTILIZATION"><img alt="Research paper thumbnail of THE PROSPECT of SOLAR ENERGY UTILIZATION" class="work-thumbnail" src="https://attachments.academia-assets.com/64472401/thumbnails/1.jpg" /></a></div><div class="wp-workCard wp-workCard_itemContainer"><div class="wp-workCard_item wp-workCard--title"><a class="js-work-strip-work-link text-gray-darker" data-click-track="profile-work-strip-title" href="https://www.academia.edu/44122042/THE_PROSPECT_of_SOLAR_ENERGY_UTILIZATION">THE PROSPECT of SOLAR ENERGY UTILIZATION</a></div><div class="wp-workCard_item"><span>Studium Generale President University 16 July 2020 F</span><span>, 2020</span></div><div class="wp-workCard_item"><span class="js-work-more-abstract-truncated">1. INTRODUCTION: 2. RENEWABE ENERGY POTENTIAL 3. WORLD ENERGY LANDSCAPE 4. PROGRESS AND RECENT TR...</span><a class="js-work-more-abstract" data-broccoli-component="work_strip.more_abstract" data-click-track="profile-work-strip-more-abstract" href="javascript:;"><span> more </span><span><i class="fa fa-caret-down"></i></span></a><span class="js-work-more-abstract-untruncated hidden">1.<br />INTRODUCTION:<br />2.<br />RENEWABE ENERGY POTENTIAL<br />3.<br />WORLD ENERGY LANDSCAPE<br />4.<br />PROGRESS AND RECENT TRENDS OF<br />RENEWABLE ENERGY TECHNOLOGY<br />5.<br />THE POTENTIAL AND IMPLEMENTATION OF<br />RENEWABLE ENERGY DEVELOPMENT IN<br />INDONESIA<br />6.<br />GLOBAL AND INDONESIAN SOLAR IRRADIATION<br />7.<br />GLOBAL WIND ENERGY POTENTIAL<br />8.<br />PHOTOVOLTAIC SOLAR ENERGY UTILIZATION IN<br />INDONESIA<br />9.<br />EXAMPLES OF SOLAR HOME SYSTEM<br />10.<br />WIND ENERGY TECHNOLOGY OVERVIEW<br />11.<br />STRATEGIC FEATURES OF WIND ENERGY<br />TECHNLOGY<br />12.<br />SOLAR PHOTOVOLTAIC Examples<br />13.<br />ECONOMICS OVERVIEW<br />14.<br />BRIEF ANALYSIS AND PROSPECTS<br />15.<br />CONCLUDING REMARKS<br />16.<br />THE WAY FORWARD</span></div><div class="wp-workCard_item wp-workCard--actions"><span class="work-strip-bookmark-button-container"></span><a id="37d52117e8e418f1ccdab7c8e6ef6d22" class="wp-workCard--action" rel="nofollow" data-click-track="profile-work-strip-download" data-download="{&quot;attachment_id&quot;:64472401,&quot;asset_id&quot;:44122042,&quot;asset_type&quot;:&quot;Work&quot;,&quot;button_location&quot;:&quot;profile&quot;}" href="https://www.academia.edu/attachments/64472401/download_file?st=MTczMzAzMTQwNiw4LjIyMi4yMDguMTQ2&s=profile"><span><i class="fa fa-arrow-down"></i></span><span>Download</span></a><span class="wp-workCard--action visible-if-viewed-by-owner inline-block" style="display: none;"><span class="js-profile-work-strip-edit-button-wrapper profile-work-strip-edit-button-wrapper" data-work-id="44122042"><a class="js-profile-work-strip-edit-button" tabindex="0"><span><i class="fa 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