Abstract
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This paper presents the visualization results obtained in a water channel. These results have shown the streamlines in several conventional and non-conventional wing planforms, in an incompressible and stationary flow over the range of low Reynolds number. The authors will present the results obtained in several configurations (delta wings, winglets, box-wing). These experimental results have been used in the preliminary design of non-conventional wing planforms. This tool for aerodynamic design has been applied to the process of developing and building of an UAV which the authors have carried out | |
International
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Si |
Congress
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5th EUCASS CONFERENCE (EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES) |
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960 |
Place
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Munich (Germany) |
Reviewers
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Si |
ISBN/ISSN
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978-84-941531-0-5 |
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Start Date
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01/07/2013 |
End Date
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05/07/2013 |
From page
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To page
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5th EUCASS CONFERENCE |