Descripción
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The interest of this study is based on the observation that some manufacturing processes of various vehicles wings, such as unmanned aerial vehicle (UAV), or blades, such as wind turbine blades, or other devices that use aerodynamic profiles, produce imperfections in the leading edge or open trailing edge with bigger thickness than original airfoil, because, for example, they are manufactured in two parts, top surface and bottom surface and subsequently joined. In this last step might appear a sliding between the top surface and the bottom surface having a small step on the leading edge or a small thickness gain can occur on the trailing edge. Normally these imperfections are corrected through a refill and/or sanding processes using many hours of manual labor. Therefore the initial objective of this research is to determine the level of influence in the aerodynamic characteristics at low Reynolds numbers (Lissaman, 1981, Carmichael, 1981, Nagamatsu and Cuche, 1981, Schmitz, 1957, Cebeci, 1989, Mueller and Batill, 1982) of these imperfections in the manufacture, and determine whether there may be a value for which it would not be necessary to correct them. | |
Internacional
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Si |
Nombre congreso
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ICWE13 - 13th International Conference on Wind Engineering |
Tipo de participación
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960 |
Lugar del congreso
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Amsterdam, Holanda |
Revisores
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Si |
ISBN o ISSN
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978-1-907132-33-9 |
DOI
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Fecha inicio congreso
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10/09/2011 |
Fecha fin congreso
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15/09/2011 |
Desde la página
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1 |
Hasta la página
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10 |
Título de las actas
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ICW13 Proceedings |