Hypersonic Viscous Flow Over Blunt Bodies
碩士 === 淡江大學 === 機械工程研究所 === 78 === In order to consider the strong viscous effects of the hypersonic flow over blunt bodies, unsteady thin layer Navier- Stokes equations are solved using the explicit upwind second order predictor-corrector scheme. The flux vector is splitted into forward and back...
| Main Authors: | , |
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| Other Authors: | |
| Format: | Others |
| Language: | zh-TW |
| Published: |
1990
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| Online Access: | http://ndltd.ncl.edu.tw/handle/82150891842985516031 |