渦輪引擎穿音速壓縮器轉子紊性流場之數值模擬
碩士 === 國防大學中正理工學院 === 兵器系統工程研究所 === 92 === The flow field within the blade rows of a multistage axial compressor is extremely complex. This includes transonic flows, turbulence, secondary flows, tip clearance flows, inter-blade row interference, etc. The blade shape in transonic axial compressor is...
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| Format: | Others |
| Language: | zh-TW |
| Published: |
2004
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| Online Access: | http://ndltd.ncl.edu.tw/handle/84289903510421706511 |