Simulation of Hypersonic Shock-Boundary Layer Interaction
碩士 === 逢甲大學 === 航太與系統工程所 === 99 === This paper describes using finite volume method to solve Navier-Stokes Equations about a hypersonic intake has a double-ramp compress section. Considering varied computing methods to process 2-D computing simulations of flow field. Computing simulations of the int...
| Main Authors: | , |
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| Other Authors: | |
| Format: | Others |
| Language: | zh-TW |
| Published: |
2011
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| Online Access: | http://ndltd.ncl.edu.tw/handle/65104448648249790865 |