紊流模式應用於彈底噴流效應之數值研究
碩士 === 中正理工學院 === 兵器系統工程研究所 === 88 === The aim of present study is to simulate the transonic flow field and aerodynamic coefficients of a 20mm projectile with and without base bleed. A computer code based on the control volume method was developed to solve the Reynolds-averaged Navier-Stokes equati...
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| Format: | Others |
| Language: | zh-TW |
| Published: |
2000
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| Online Access: | http://ndltd.ncl.edu.tw/handle/14728441607442667528 |