Numerical Analysis for Flow Over Airfoils with Different Shape of Trailing-Edge
碩士 === 國立中興大學 === 機械工程研究所 === 81 === The flow field of airfoil with different Trailing- Edge geometry have studied. For this research, the two -zone grid, created by solving elliptic partial diffe- rential equations and algebraic equs, was...
| Main Authors: | , |
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| Other Authors: | |
| Format: | Others |
| Language: | zh-TW |
| Published: |
1993
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| Online Access: | http://ndltd.ncl.edu.tw/handle/71552270455461171670 |