Aerodynamic Analysis of a Flapping-Wing Micro Aerial Vehicle
碩士 === 中華大學 === 機械與航太工程研究所 === 95 === The investigation of aerodynamic performance and design/fabrication a planar membrane wing shape airfoil are goals in the study. And take the simulation result the average lifting force value does weight of basis as the flapping wing MAV (weight must be lower th...
| Main Authors: | , |
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| Other Authors: | |
| Format: | Others |
| Language: | zh-TW |
| Published: |
2007
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| Online Access: | http://ndltd.ncl.edu.tw/handle/05283733707152680877 |