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Descripción
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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 | |
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Internacional
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Si |
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Nombre congreso
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5th EUCASS CONFERENCE (EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES) |
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Tipo de participación
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960 |
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Lugar del congreso
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Munich (Germany) |
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Revisores
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Si |
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ISBN o ISSN
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978-84-941531-0-5 |
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DOI
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Fecha inicio congreso
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01/07/2013 |
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Fecha fin congreso
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05/07/2013 |
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Título de las actas
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5th EUCASS CONFERENCE |