Descripción
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A study has been made on the influence of the open trailing edge in airfoils used in different devices relating their aerodynamic performances. Wind tunnel tests have been made at different Reynolds numbers and angles of attack in order to show this effect. Besides, a quantitative study of the aerodynamic properties has been made based on the different trailing edge thickness. | |
Internacional
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Si |
Nombre congreso
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49th AIAA Aerospace Sciences Meeting |
Tipo de participación
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960 |
Lugar del congreso
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Orlando, Florida, USA |
Revisores
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Si |
ISBN o ISSN
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9781617829482 |
DOI
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Fecha inicio congreso
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04/01/2011 |
Fecha fin congreso
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07/01/2011 |
Desde la página
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1 |
Hasta la página
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10 |
Título de las actas
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49th AIAA Aerospace Sciences Meeting proceedings |