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Search results for: S. Maheshwaran
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Maheshwaran</title> <meta name="description" content="Search results for: S. Maheshwaran"> <meta name="keywords" content="S. Maheshwaran"> <meta name="viewport" content="width=device-width, initial-scale=1, minimum-scale=1, maximum-scale=1, user-scalable=no"> <meta charset="utf-8"> <link href="https://cdn.waset.org/favicon.ico" type="image/x-icon" rel="shortcut icon"> <link href="https://cdn.waset.org/static/plugins/bootstrap-4.2.1/css/bootstrap.min.css" rel="stylesheet"> <link href="https://cdn.waset.org/static/plugins/fontawesome/css/all.min.css" rel="stylesheet"> <link href="https://cdn.waset.org/static/css/site.css?v=150220211555" rel="stylesheet"> </head> <body> <header> <div class="container"> <nav class="navbar navbar-expand-lg navbar-light"> <a class="navbar-brand" href="https://waset.org"> <img src="https://cdn.waset.org/static/images/wasetc.png" alt="Open Science Research Excellence" title="Open Science Research Excellence" /> </a> <button class="d-block d-lg-none navbar-toggler ml-auto" type="button" data-toggle="collapse" data-target="#navbarMenu" aria-controls="navbarMenu" aria-expanded="false" aria-label="Toggle navigation"> <span class="navbar-toggler-icon"></span> </button> <div class="w-100"> <div class="d-none d-lg-flex flex-row-reverse"> <form method="get" action="https://waset.org/search" class="form-inline my-2 my-lg-0"> <input class="form-control mr-sm-2" type="search" placeholder="Search Conferences" value="S. 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Maheshwaran"> <input type="submit" class="btn_search" value="Search"> </div> </div> </form> </div> </div> <div class="row mt-3"> <div class="col-sm-3"> <div class="card"> <div class="card-body"><strong>Commenced</strong> in January 2007</div> </div> </div> <div class="col-sm-3"> <div class="card"> <div class="card-body"><strong>Frequency:</strong> Monthly</div> </div> </div> <div class="col-sm-3"> <div class="card"> <div class="card-body"><strong>Edition:</strong> International</div> </div> </div> <div class="col-sm-3"> <div class="card"> <div class="card-body"><strong>Paper Count:</strong> 2</div> </div> </div> </div> <h1 class="mt-3 mb-3 text-center" style="font-size:1.6rem;">Search results for: S. Maheshwaran</h1> <div class="card paper-listing mb-3 mt-3"> <h5 class="card-header" style="font-size:.9rem"><span class="badge badge-info">2</span> Design, Prototyping, Integration, Flight Testing of a 20 cm Span Fully Autonomous Fixed Wing Micro Air Vehicle</h5> <div class="card-body"> <p class="card-text"><strong>Authors:</strong> <a href="https://publications.waset.org/abstracts/search?q=Vivek%20Paul">Vivek Paul</a>, <a href="https://publications.waset.org/abstracts/search?q=Abel%20Nelly"> Abel Nelly</a>, <a href="https://publications.waset.org/abstracts/search?q=Shoeb%20A%20Adeel"> Shoeb A Adeel</a>, <a href="https://publications.waset.org/abstracts/search?q=R.%20Tilak"> R. Tilak</a>, <a href="https://publications.waset.org/abstracts/search?q=S.%20Maheshwaran"> S. Maheshwaran</a>, <a href="https://publications.waset.org/abstracts/search?q=S.%20Pulikeshi"> S. Pulikeshi</a>, <a href="https://publications.waset.org/abstracts/search?q=Roshan%20Antony"> Roshan Antony</a>, <a href="https://publications.waset.org/abstracts/search?q=C.%20S.%20Suraj"> C. S. Suraj</a> </p> <p class="card-text"><strong>Abstract:</strong></p> This paper presents the complete design and development cycle of a 20 cm span fixed wing micro air vehicle that was developed at CSIR-NAL, under the micro air vehicle development program. The design is a cropped delta flying wing MAV with a modified N22 airfoil of 12.3% thickness. The design was fabricated using the fused deposition method- RPT technique. COTS components were procured and integrated into this RPT prototype. A commercial autopilot that was proven in the earlier MAV designs was used for this MAV. The MAV was flown fully autonomous for 14mins at an open field. The flight data showed good performance as expected from the MAV design. The paper also describes about the process involved in the design of MAVs. <p class="card-text"><strong>Keywords:</strong> <a href="https://publications.waset.org/abstracts/search?q=autopilot" title="autopilot">autopilot</a>, <a href="https://publications.waset.org/abstracts/search?q=autonomous%20mode" title=" autonomous mode"> autonomous mode</a>, <a href="https://publications.waset.org/abstracts/search?q=flight%20testing" title=" flight testing"> flight testing</a>, <a href="https://publications.waset.org/abstracts/search?q=MAV" title=" MAV"> MAV</a>, <a href="https://publications.waset.org/abstracts/search?q=RPT" title=" RPT"> RPT</a> </p> <a href="https://publications.waset.org/abstracts/35288/design-prototyping-integration-flight-testing-of-a-20-cm-span-fully-autonomous-fixed-wing-micro-air-vehicle" class="btn btn-primary btn-sm">Procedia</a> <a href="https://publications.waset.org/abstracts/35288.pdf" target="_blank" class="btn btn-primary btn-sm">PDF</a> <span class="bg-info text-light px-1 py-1 float-right rounded"> Downloads <span class="badge badge-light">519</span> </span> </div> </div> <div class="card paper-listing mb-3 mt-3"> <h5 class="card-header" style="font-size:.9rem"><span class="badge badge-info">1</span> A Review Of Blended Wing Body And Slender Delta Wing Performance Utilizing Experimental Techniques And Computational Fluid Dynamics</h5> <div class="card-body"> <p class="card-text"><strong>Authors:</strong> <a href="https://publications.waset.org/abstracts/search?q=Abhiyan%20Paudel">Abhiyan Paudel</a>, <a href="https://publications.waset.org/abstracts/search?q=Maheshwaran%20M%20Pillai"> Maheshwaran M Pillai</a> </p> <p class="card-text"><strong>Abstract:</strong></p> This paper deals with the optimization and comparison of slender delta wing and blended wing body. The objective is to study the difference between the two wing types and analyze the various aerodynamic characteristics of both of these types.The blended-wing body is an aircraft configuration that has the potential to be more efficient than conventional large transport aircraft configurations with the same capability. The purported advantages of the BWB approach are efficient high-lift wings and a wide airfoil-shaped body. Similarly, symmetric separation vortices over slender delta wing may become asymmetric as the angle of attack is increased beyond a certain value, causing asymmetric forces even at symmetric flight conditions. The transition of the vortex pattern from being symmetric to asymmetric over symmetric bodies under symmetric flow conditions is a fascinating fluid dynamics problem and of major importance for the performance and control of high-maneuverability flight vehicles that favor the use of slender bodies. With the use of Star CCM, we analyze both the fluid properties. The CL, CD and CM were investigated in steady state CFD of BWB at Mach 0.3 and through wind tunnel experiments on 1/6th model of BWB at Mach 0.1. From CFD analysis pressure variation, Mach number contours and turbulence area was observed. <p class="card-text"><strong>Keywords:</strong> <a href="https://publications.waset.org/abstracts/search?q=Coefficient%20%20of%20%20Lift" title="Coefficient of Lift">Coefficient of Lift</a>, <a href="https://publications.waset.org/abstracts/search?q=Coefficient%20%20of%20%20Drag" title=" Coefficient of Drag"> Coefficient of Drag</a>, <a href="https://publications.waset.org/abstracts/search?q=CFD%3DComputational%20%20Fluid%20%20Dynamics" title=" CFD=Computational Fluid Dynamics"> CFD=Computational Fluid Dynamics</a>, <a href="https://publications.waset.org/abstracts/search?q=BWB%3DBlended%20Wing%20Body" title=" BWB=Blended Wing Body"> BWB=Blended Wing Body</a>, <a href="https://publications.waset.org/abstracts/search?q=slender%20delta%20wing" title=" slender delta wing"> slender delta wing</a> </p> <a href="https://publications.waset.org/abstracts/17417/a-review-of-blended-wing-body-and-slender-delta-wing-performance-utilizing-experimental-techniques-and-computational-fluid-dynamics" class="btn btn-primary btn-sm">Procedia</a> <a href="https://publications.waset.org/abstracts/17417.pdf" target="_blank" class="btn btn-primary btn-sm">PDF</a> <span class="bg-info text-light px-1 py-1 float-right rounded"> Downloads <span class="badge badge-light">531</span> </span> </div> </div> </div> </main> <footer> <div id="infolinks" class="pt-3 pb-2"> <div class="container"> <div style="background-color:#f5f5f5;" class="p-3"> <div class="row"> <div class="col-md-2"> <ul class="list-unstyled"> About <li><a href="https://waset.org/page/support">About Us</a></li> <li><a href="https://waset.org/page/support#legal-information">Legal</a></li> <li><a target="_blank" rel="nofollow" href="https://publications.waset.org/static/files/WASET-16th-foundational-anniversary.pdf">WASET celebrates its 16th 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