The Numerical Simulation and Analysis of Variable Forward-Swept Wing
碩士 === 國立成功大學 === 航空太空工程學系碩士在職專班 === 105 === This study uses the NASA M6 wing module as the wing main structure to investigate the airfoil performance. By changing the wing sweep angle from forward swept wing into Delta wing. In theory,one can combine the strength of these two airfoils to enhance th...
| Main Authors: | , |
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| Other Authors: | |
| Format: | Others |
| Language: | zh-TW |
| Published: |
2017
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| Online Access: | http://ndltd.ncl.edu.tw/handle/933949 |