Effects of nozzle contour in convergent section and throat on mass flow rate

Lin Quan Chen, Yan Fang Li, Xiao Hou, Xin Gang Dong

科研成果: 期刊稿件文章同行评审

8 引用 (Scopus)
源语言英语
页(从-至)10
页数1
期刊Guti Huojian Jishu/Journal of Solid Rocket Technology
25
1
出版状态已出版 - 3月 2002

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