渦輪引擎穿音速壓縮氣流場模擬
碩士 === 國防大學中正理工學院 === 兵器系統工程研究所 === 93 === The main objective of this research project is to develop the capability of numerical simulation on the internal flow field in the compressor for gas turbine engine. The flow characteristics of transonic multi-stage compressors will be investigated numerica...
| Main Authors: | , |
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| Format: | Others |
| Language: | zh-TW |
| Published: |
2005
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| Online Access: | http://ndltd.ncl.edu.tw/handle/90142836622215039862 |