Experimental Study of Leading-edge Flap Excitation on Stalled Airfoil
博士 === 國立成功大學 === 航空太空工程學系 === 87 === The phenomenon of flow separation on airfoils and its control have been investigated for decades. The leading-edge flap excitation, which is one of the active control concepts, has been proved to be an effective approach to improve the aerodynamic performance of...
Main Authors: | , |
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Other Authors: | |
Format: | Others |
Language: | en_US |
Published: |
1999
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Online Access: | http://ndltd.ncl.edu.tw/handle/93928031450459435262 |