液態推進劑系統噴霧燃室流場渦漩交互現象之解析模擬研究
碩士 === 國防大學中正理工學院 === 兵器系統工程研究所 === 92 === Inspired by the fact that turbulent combustion is a popular phenomenon existing in the burner of most ramjet and liquid rocket propulsion systems and playing a role in determining the system performance, the present thesis proposes a fundamental study of th...
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| Format: | Others |
| Language: | zh-TW |
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2004
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| Online Access: | http://ndltd.ncl.edu.tw/handle/54701477506535239123 |