Experimental Study Of Aerodynamic Characteristic For Airfoil At Low Reynolds Number
碩士 === 國防大學理工學院 === 航空太空工程碩士班 === 100 === The effects of surface roughness on flowfield and aerodynamic characteristics of a sweptback low Reynolds number airfoil for MAVs have been studied in this thesis using wind tunnel experiments. The test model selected in this study was a better lift-to-drag...
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| Other Authors: | |
| Format: | Others |
| Language: | zh-TW |
| Published: |
2012
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| Online Access: | http://ndltd.ncl.edu.tw/handle/nqahsa |