Numerical Study of the Scramjet Inlet with Shape Transition
碩士 === 國防大學理工學院 === 航空太空工程碩士班 === 105 === The inlet of supersonic combustion ramjets (Scramjets) can provide an appropriate supersonic flow for the combustor to achieve hypersonic flight. Therefore the inlet design is the key technology for a Scramjet. CFD predictions have been used to investigate t...
| Main Authors: | , |
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| Other Authors: | |
| Format: | Others |
| Language: | zh-TW |
| Published: |
2017
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| Online Access: | http://ndltd.ncl.edu.tw/handle/6nduc7 |