Numerical Simulations and Analyses of the Supersonic Combustion Flow
碩士 === 國立成功大學 === 航空太空工程學系碩博士班 === 98 === General supersonic flow field is complex, due to the mixing and combustion of the injected fuel in the high-speed flow and the interaction between the shock wave and the boundary layer. Therefore, the numerical model for the supersonic flow has been establis...
| Main Authors: | , |
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| Other Authors: | |
| Format: | Others |
| Language: | zh-TW |
| Published: |
2010
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| Online Access: | http://ndltd.ncl.edu.tw/handle/47766915122849003795 |