Single Lap Joint | Scientific.Net

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class="pagination-container"><ul class="pagination"><li class="active"><span>1</span></li><li><a href="/paper-keyword/single-lap-joint-1/2">2</a></li><li class="PagedList-skipToNext"><a href="/paper-keyword/single-lap-joint-1/2" rel="next">></a></li></ul></div> </div> <div class="block-volume-title normal-text-gray"> <p> Paper Title<span>Page</span> </p> </div> <div class="item-block"> <div class="item-link"> <a href="/AMR.1181.19">Experimental Analysis of the Behavior of Multiple Adhesive on the Single Lap Joint Strength</a> </div> <div class="item-link volume-authors"> <div class="semibold-middle-text"> Authors: Chirag R. Desai, Dilip C. Patel, Chaitanya Desai, Mohd Asif Hasan </div> </div> <div id="abstractTextBlock610026" class="volume-info volume-info-text volume-info-description"> Abstract: The usage of adhesively bonded lap joints in industrial applications has been growing in recent years because of the numerous advantages compared to other joining processes such as fastening, welding, and riveting. For effective design of the adhesively bonded engineering lap joints, it is essential to govern the failure potential of a particular adhesive joint under a certain load causing some stress and strain. In this work, study has been carried out by the application of multiple adhesives along the bondline region of lap joint. The objective of this paper is to experimentally examine the results of applications of single and multi-adhesives material with very different mechanical behavior along the bondline region in the single lap adhesive joint. Experimental investigations have been carried out for extracting load displacement data using tensile testing machine, Tensometer, having a capacity of 2 tonne. Multi Adhesive joint can minimize the stress concentration and improve joint strength by using different adhesive stiffness along the bondline region of lap joint and the outcome shows computable increase in the strength of the multiple adhesive bonded lap joints associated with those in which single adhesives were used over the full length of the bondline region. </div> <div> <a data-readmore="{ block: '#abstractTextBlock610026', lines: 2, expandText: '...more', collapseText: '...less' }"></a> </div> <div class="page-number semibold-large-text"> 19 </div> </div> <div class="item-block"> <div class="item-link"> <a href="/KEM.858.20">Effect of Interface Geometry on Strength of Single Lap Adhesive Joint of Sisal-Glass/Epoxy Laminates</a> </div> <div class="item-link volume-authors"> <div class="semibold-middle-text"> Authors: Asad A. Khalid </div> </div> <div id="abstractTextBlock553436" class="volume-info volume-info-text volume-info-description"> Abstract: In this project, experimental work on tensile behaviour of single lap adhesive joints of sisal, glass and hybrid sisal-glass/epoxy composite laminates has been carried out. Composite laminates were fabricated by hand lay-up method using chopped strand mat sisal and glass fibers with epoxy resin matrix. Lab joints of four interface geometries; straight flat, triangular, rectangular and sinusoidal were fabricated. Tensile load-displacement relations were drawn and discussed. Effect of interface geometry and material type on maximum load and strength of the single lap joint was investigated. Failure mechanism of the fractured specimens was discussed. Results show that the glass/epoxy lap joints with semi-circular adhesive interface geometry supported load higher respectively 14.26%, 26.13%, and 30.79% than rectangular, triangular and straight flat interface geometries. Glass/epoxy lap joint with semi-circular interface geometry supported tensile load higher 5.61% and 21.83% than that obtained from hybrid sisal-glass and sisal/ epoxy adhesive joints. While the shear strength was found higher respectively 6.19% and 18.69%. Adhesive failure mode was observed for most of the single lap joints investigated. Mixed failure mode of adhesive and adherend materials was observed on the sisal/epoxy lap joints. </div> <div> <a data-readmore="{ block: '#abstractTextBlock553436', lines: 2, expandText: '...more', collapseText: '...less' }"></a> </div> <div class="page-number semibold-large-text"> 20 </div> </div> <div class="item-block"> <div class="item-link"> <a href="/KEM.754.256">The Effect of Interface Geometry on the Mechanical Behavior of Adhesive Joints</a> </div> <div class="item-link volume-authors"> <div class="semibold-middle-text"> Authors: Nima Razavi, M. Peron, J. Torgersen, F. Berto </div> </div> <div id="abstractTextBlock525702" class="volume-info volume-info-text volume-info-description"> Abstract: The role of sinusoid interface shape on the load bearing capacity of the adhesively bonded single lap joints has been investigated experimentally. The experimental results showed that the interface non-flatness can considerably influence the adhesive joint strength. The main parameters that can affect the load bearing of the non-flat joints are wave heights, wave lengths and also mechanical properties of adhesives and adherends. In this paper, the effect of wave length was evaluated as the key variable parameter. According to the experimental results for the best studied case, non-flat sinusoid single lap joints had about 51% higher load bearing compared to the conventional flat single lap joints. </div> <div> <a data-readmore="{ block: '#abstractTextBlock525702', lines: 2, expandText: '...more', collapseText: '...less' }"></a> </div> <div class="page-number semibold-large-text"> 256 </div> </div> <div class="item-block"> <div class="item-link"> <a href="/MSF.859.45">Comparison of Bonding Performance for CFRP-SPCC Single Lap Joint Using Adhesives and Rivets</a> </div> <div class="item-link volume-authors"> <div class="semibold-middle-text"> Authors: Ok Hyoung Lee, Il Teak Lee, Hee Yong Kang, Sung Mo Yang, Jun Young Yim, Dae Su Kim, Hyo Jun Ahn </div> </div> <div id="abstractTextBlock499224" class="volume-info volume-info-text volume-info-description"> Abstract: The recent trend in automotive industry is characterized by the replacement of existing metal materials with composite ones or the combination of both for lightweight parts. This study 1) created single lap joint specimens of SPCC used for automobile frame and four adhesives; epoxy, urethane, acrylic, mixed (urethane and acrylic) and rivets to bind dissimilar materials of CFRP necessary for weight lightening, and 2) performed a tensile shear test on adhesive bonding versus adhesive bonding with rivets. In summary, this study investigated on the bonding performance of different specimens: bonding strength, shapes of the failure surface, and the effect of rivets on bond strength. </div> <div> <a data-readmore="{ block: '#abstractTextBlock499224', lines: 2, expandText: '...more', collapseText: '...less' }"></a> </div> <div class="page-number semibold-large-text"> 45 </div> </div> <div class="item-block"> <div class="item-link"> <a href="/MSF.813.28">Study on the Factors of Residual Thermal Stress on Single Lap Joint</a> </div> <div class="item-link volume-authors"> <div class="semibold-middle-text"> Authors: Cheng Kun Ma, Ji Feng Zhang, Bin Yang, Lu Zhang, Qi Chen </div> </div> <div id="abstractTextBlock464955" class="volume-info volume-info-text volume-info-description"> Abstract: This paper discussed the residual thermal stress on single lap joint of various materials. Finite element method (FEM) was adopted to simulate the experimental phenomena. The adherend and adhesive were the main research objects. Mismatch of adherend, adhesive thickness, temperature variation which were the three key factors on the residual thermal stress were analyzed. While, four kinds of materials that include C/SiC, SiC, high temperature nickel based alloy GH1035 (GH1035) and high temperature boron fiber reinforced epoxy composite (composite) formed seven approaches for numerical analysis. The results showed that the adhesive with the C/SiC has the best performance and the best thickness of every approach was determined. Moreover, the ladder temperature is better than other temperature styles. </div> <div> <a data-readmore="{ block: '#abstractTextBlock464955', lines: 2, expandText: '...more', collapseText: '...less' }"></a> </div> <div class="page-number semibold-large-text"> 28 </div> </div> <div class="item-block"> <div class="item-link"> <a href="/AMR.1061-1062.471">Numerical Analysis of Multi-Layer on the Stress Distribution in Adhesively Bonded Single Lap Aluminum Joint</a> </div> <div class="item-link volume-authors"> <div class="semibold-middle-text"> Authors: Min You, Ya Lan Zhao, Jian Li Li, Ying Ying Li </div> </div> <div id="abstractTextBlock445770" class="volume-info volume-info-text volume-info-description"> Abstract: The effect of dual adhesives to form multi-layer on the stress distributed in adhesively bonded single lap aluminum joint was investigated using elasto-plastic finite element method (FEM). The results from the numerical simulation showed that the values of the peak stress along the bondline are influenced evidently when there is a multi-layer formed by a middle layer with higher elastic modulus adhesive and two layers with lower elastic modulus adhesive. </div> <div> <a data-readmore="{ block: '#abstractTextBlock445770', lines: 2, expandText: '...more', collapseText: '...less' }"></a> </div> <div class="page-number semibold-large-text"> 471 </div> </div> <div class="item-block"> <div class="item-link"> <a href="/AMR.644.189">Numerical Analysis of Bi-Adhesive Boded Single Lap Composite Joint with Mechanics Analysis</a> </div> <div class="item-link volume-authors"> <div class="semibold-middle-text"> Authors: Min You, Peng Wang, Hai Zhou Yu, Mei Li, Ya Lan Zhao </div> </div> <div id="abstractTextBlock255392" class="volume-info volume-info-text volume-info-description"> Abstract: The effect of dual adhesives with different length ratio on the stress distributed in adhesively bonded single lap steel joint was investigated using elasto-plastic finite element method (FEM). The results from the numerical simulation showed that the peak stress along the bondline moves from the ends of the overlap to the middle part of lap zone. Compared with the results from the mono-adhesive system, appropriate bond-length ratios is beneficial to optimize the stress distribution and it is 0.4 for bi-adhesive bonded single lap composite joint. </div> <div> <a data-readmore="{ block: '#abstractTextBlock255392', lines: 2, expandText: '...more', collapseText: '...less' }"></a> </div> <div class="page-number semibold-large-text"> 189 </div> </div> <div class="item-block"> <div class="item-link"> <a href="/AMR.644.243">Effect of the Metal Block on the Stress Distributed in the Adhesively Bonded Single Lap Steel Joint</a> </div> <div class="item-link volume-authors"> <div class="semibold-middle-text"> Authors: Min You, Lai Hu Song, Jiang Cheng Zhang, Mei Li </div> </div> <div id="abstractTextBlock250575" class="volume-info volume-info-text volume-info-description"> Abstract: The effect of 4 mm long metal block bonded to the end of the overlap zone on the stress distributed in adhesively bonded single lap steel joint was investigated using elasto-plastic finite element method (FEM). The results from the numerical simulation showed that the stress is varied a little when the joints with a couple of 4 mm long metal block adhered to both ends of the over lap or with a couple of adhesive fillet. Compared to the joint without the metal block, it is advantageous of reducing the peak stress in the adhesive layer near the ends of the lap zone in adhesively bonded single lap steel joints but its effect is less than that of the joint with a couple of adhesive fillet. There is no evidential difference in the effects between the steel and aluminum block. </div> <div> <a data-readmore="{ block: '#abstractTextBlock250575', lines: 2, expandText: '...more', collapseText: '...less' }"></a> </div> <div class="page-number semibold-large-text"> 243 </div> </div> <div class="item-block"> <div class="item-link"> <a href="/AMM.166-169.2896">Effect of Temperature on the Thermal Stress in the Single Lap Joint</a> </div> <div class="item-link volume-authors"> <div class="semibold-middle-text"> Authors: Min You, Cun Jun Chen, Hai Zhou Yu, Chun Zhi Mei, Mei Li </div> </div> <div id="abstractTextBlock190058" class="volume-info volume-info-text volume-info-description"> Abstract: The effect of the thermal shock temperature on the thermal stress distributed in the adhesively bonded steel single lap steel joint under a 10 s thermal shock was investigated using elasto-plastic finite element method (FEM). The results showed that both the highest temperature at the surface and the lowest one at the mid-bondline increases as the temperature of the thermal shock raised (80 C to 140 C) and all the peak values of the stresses at the mid-bondline and the zone of negative Sx in adherend increased as the temperature of the thermal shock elevated. </div> <div> <a data-readmore="{ block: '#abstractTextBlock190058', lines: 2, expandText: '...more', collapseText: '...less' }"></a> </div> <div class="page-number semibold-large-text"> 2896 </div> </div> <div class="item-block"> <div class="item-link"> <a href="/AMM.166-169.1904">Effect of Alkali on the Impact Toughness of Adhesively Bonded Joints</a> </div> <div class="item-link volume-authors"> <div class="semibold-middle-text"> Authors: Min You, Chun Zhi Mei, Wen Jun Liu, Jing Rong Hu, Ling Wu </div> </div> <div id="abstractTextBlock190053" class="volume-info volume-info-text volume-info-description"> Abstract: The effect of the temperature and immersed time of the alkali solution on the impact toughness of the adhesively bonded steel single lap joint under impact loading is studied using the experimental method. The results obtained show that the impact toughness of the specimen increased when the immersed time increased then it decreased as it beyond 3 days. When the immersed time is longer than 72 h, the higher the temperature is, the lower the impact toughness of the joint. The moisture absorption of the adhesive layer with the immersed time was also investigated and it was found that there is a relationship to the impact toughness of the adhesively bonded single lap joint. The epoxy adhesive layer was analyzed with FT-IR and it was found that the hydroxyl enhanced and bonding strength may increase after 72 h immersed in alkali solution. </div> <div> <a data-readmore="{ block: '#abstractTextBlock190053', lines: 2, expandText: '...more', collapseText: '...less' }"></a> </div> <div class="page-number semibold-large-text"> 1904 </div> </div> <div class="block-bottom-pagination"> <div class="pager-info"> Showing 1 to 10 of 19 Paper Titles </div> <div class="pagination-container"><ul class="pagination"><li class="active"><span>1</span></li><li><a href="/paper-keyword/single-lap-joint-1/2">2</a></li><li class="PagedList-skipToNext"><a href="/paper-keyword/single-lap-joint-1/2" rel="next">></a></li></ul></div> </div> </div> </div> </div> </div> </div> <div class="social-icon-popup"> <a href="https://www.facebook.com/Scientific.Net.Ltd/" target="_blank" rel="noopener" title="Scientific.Net"><i class="inline-icon facebook-popup-icon social-icon"></i></a> <a href="https://twitter.com/Scientific_Net/" target="_blank" rel="noopener" title="Scientific.Net"><i class="inline-icon twitter-popup-icon social-icon"></i></a> <a href="https://www.linkedin.com/company/scientificnet/" target="_blank" rel="noopener" title="Scientific.Net"><i class="inline-icon linkedin-popup-icon social-icon"></i></a> </div> </div> <div class="sc-footer"> <div class="footer-fluid"> <div class="container"> <div class="row"> <div class="footer-menu col-md-12 col-sm-12 col-xs-12"> <ul class="list-inline menu-font"> <li><a href="/ForLibraries">For Libraries</a></li> <li><a href="/ForPublication/Paper">For Publication</a></li> <li><a href="/insights" target="_blank">Insights</a></li> <li><a href="/DocuCenter">Downloads</a></li> <li><a href="/Home/AboutUs">About Us</a></li> <li><a href="/PolicyAndEthics/PublishingPolicies">Policy & Ethics</a></li> <li><a href="/Home/Contacts">Contact Us</a></li> <li><a href="/Home/Imprint">Imprint</a></li> <li><a href="/Home/PrivacyPolicy">Privacy Policy</a></li> <li><a href="/Home/Sitemap">Sitemap</a></li> <li><a href="/Conferences">All Conferences</a></li> <li><a href="/special-issues">All Special Issues</a></li> <li><a href="/news/all">All News</a></li> <li><a href="/read-and-publish-agreements">Read & Publish Agreements</a></li> </ul> </div> </div> </div> </div> <div class="line-footer"></div> <div class="footer-fluid"> <div class="container"> <div class="row"> <div class="col-xs-12"> <a href="https://www.facebook.com/Scientific.Net.Ltd/" target="_blank" rel="noopener" title="Scientific.Net"><i class="inline-icon facebook-footer-icon social-icon"></i></a> <a href="https://twitter.com/Scientific_Net/" target="_blank" rel="noopener" title="Scientific.Net"><i class="inline-icon twitter-footer-icon social-icon"></i></a> <a href="https://www.linkedin.com/company/scientificnet/" target="_blank" rel="noopener" title="Scientific.Net"><i class="inline-icon linkedin-footer-icon social-icon"></i></a> </div> </div> </div> </div> <div class="line-footer"></div> <div class="footer-fluid"> <div class="container"> <div class="row"> <div class="col-xs-12 footer-copyright"> <p> © 2024 Trans Tech Publications Ltd. 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