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Computational Design Of Low Aspect Ratio Wing Winglets For Transonic Wind Tunnel Testing
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Book Synopsis Computational Design of Low Aspect Ratio Wing-winglets for Transonic Wind-tunnel Testing by : John M. Kuhlman
Download or read book Computational Design of Low Aspect Ratio Wing-winglets for Transonic Wind-tunnel Testing written by John M. Kuhlman and published by . This book was released on 1989 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :National Aeronautics and Space Administration (NASA) Publisher :Createspace Independent Publishing Platform ISBN 13 :9781722312329 Total Pages :64 pages Book Rating :4.3/5 (123 download)
Book Synopsis Computational Design of Low Aspect Ratio Wing-Winglet Configurations for Transonic Wind-Tunnel Tests by : National Aeronautics and Space Administration (NASA)
Download or read book Computational Design of Low Aspect Ratio Wing-Winglet Configurations for Transonic Wind-Tunnel Tests written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-07-06 with total page 64 pages. Available in PDF, EPUB and Kindle. Book excerpt: A computational design has been performed for three different low aspect ratio wing planforms fitted with nonplanar winglets; one of the three planforms has been selected to be constructed as a wind tunnel model for testing in the NASA LaRC 7 x 10 High Speed Wind Tunnel. A design point of M = 0.8, CL approx = 0.3 was selected, for wings of aspect ratio equal to 2.2, and leading edge sweep angles of 45 and 50 deg. Winglet length is 15 percent of the wing semispan, with a cant angle of 15 deg, and a leading edge sweep of 50 deg. Winglet total area equals 2.25 percent of the wing reference area. This report summarizes the design process and the predicted transonic performance for each configuration. Kuhlman, John M. and Brown, Christopher K. Unspecified Center...
Book Synopsis Computational Design of Low Aspect Ratio Wing-winglet Configurations for Transonic Wind-tunnel Tests by :
Download or read book Computational Design of Low Aspect Ratio Wing-winglet Configurations for Transonic Wind-tunnel Tests written by and published by . This book was released on 1989 with total page 118 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Scientific and Technical Aerospace Reports by :
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Book Synopsis Effects of Winglets on the Drag of a Low-Aspect-Ratio Configuration by : Leigh Ann Smith
Download or read book Effects of Winglets on the Drag of a Low-Aspect-Ratio Configuration written by Leigh Ann Smith and published by . This book was released on 1996 with total page 66 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis AIAA 27th Aerospace Sciences Meeting by :
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Book Synopsis Monthly Catalog of United States Government Publications by :
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Book Synopsis Aircraft Aerodynamic Design with Computational Software by : Arthur Rizzi
Download or read book Aircraft Aerodynamic Design with Computational Software written by Arthur Rizzi and published by Cambridge University Press. This book was released on 2021-05-20 with total page 467 pages. Available in PDF, EPUB and Kindle. Book excerpt: This modern text presents aerodynamic design of aircraft with realistic applications, using CFD software and guidance on its use. Tutorials, exercises, and mini-projects provided involve design of real aircraft, ranging from straight to swept to slender wings, from low speed to supersonic. Supported by online resources and supplements, this toolkit covers topics such as shape optimization to minimize drag and collaborative designing. Prepares seniors and first-year graduate students for design and analysis tasks in aerospace companies. In addition, it is a valuable resource for practicing engineers, aircraft designers, and entrepreneurial consultants.
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Book Synopsis Frontiers of Computational Fluid Dynamics 1998 by : David A. Caughey
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Book Synopsis Wind tunnel testing of low aspect ratio tapper wings at subsonic speeds by : Han Lee Loh
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