Numerical Aerodynamic Performance Evaluation of Airfoil with Protuberances on Leading Edge
碩士 === 國立臺灣大學 === 工程科學及海洋工程學研究所 === 99 === This study employs computational fluid dynamics (CFD) to investigate the effects of protuberances of varying geometric parameters on the performance of an airfoil with leading edge protuberances. The NACA 0012 airfoil is adopted as the baseline airfoil, and...
| Main Authors: | , |
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| Other Authors: | |
| Format: | Others |
| Language: | zh-TW |
| Published: |
2011
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| Online Access: | http://ndltd.ncl.edu.tw/handle/61706441052363154703 |