Study of Shock Waves/Boundary Layer Interactions on Hypersonic Intake Flows
碩士 === 逢甲大學 === 航太與系統工程所 === 100 === This paper describes using finite volume method to solve Reynold average Navier-Stokes Equations, simulated a hypersonic intake has a double-ramp compress section. Considering varied geometry to carry out 2-D and 3-D computing simulation of flow field. Computing...
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| Format: | Others |
| Language: | zh-TW |
| Published: |
2012
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| Online Access: | http://ndltd.ncl.edu.tw/handle/04293377258246163738 |