Experimental Study of Optimal Staggered Configuration Aerodynamics of Flat-plate Cascade-wing Micro Aerial Vehicle
碩士 === 國立成功大學 === 航空太空工程學系專班 === 93 === This thesis is intended to investigate the aerodynamic characteristics of the flat-plate cascade-wing Micro Aerial Vehicle (MAV) at low Reynolds number by wind-tunnel testing and to determine the optimal staggered configuration of the wings for the MAV. Ther...
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| Format: | Others |
| Language: | zh-TW |
| Published: |
2005
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| Online Access: | http://ndltd.ncl.edu.tw/handle/65485171769617880537 |