A Study of the Exact Solution of Supersonic Flow Past a Corner and Parabolic-Shaped Airfoil
碩士 === 淡江大學 === 航空太空工程學系碩士班 === 94 === Due to the singularity at the corner,the supersonic linearized theory is invalid for calculating the flow field of the corner flow.By using the method of strained coordinate,the nonlinear theory of supersonic flow in whole field of the corner flow is built. By...
| Main Authors: | , |
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| Other Authors: | |
| Format: | Others |
| Language: | zh-TW |
| Published: |
2004
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| Online Access: | http://ndltd.ncl.edu.tw/handle/88274778296018793098 |