Experimental and Numerical Analysis of Finite Wing inGround Effect at Low Reynolds Numbers
碩士 === 國立臺灣大學 === 應用力學研究所 === 106 === This study is aimed to investigate the influence of ground effect during the landing process of the airfoil NACA 4412 under static and dynamic experimental force measurements in a water tunnel that has moving ground simulation with numerical validations. Airfoil...
| Main Authors: | , |
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| Format: | Others |
| Language: | zh-TW |
| Published: |
2017
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| Online Access: | http://ndltd.ncl.edu.tw/handle/tfj99w |