邢菲
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发表刊物:Hangkong Dongli Xuebao/Journal of Aerospace Power
合写作者:邢菲
论文类型:Journal article (JA)
卷号:28
期号:5
页面范围:1142-1149
是否译文:否
发表时间:2012-12-05
上一条:Performance analysis of three kinds of aero-engine with inter-stage turbine burner
下一条:Numerical study of the effect of surface topography on atomization performance in geometrically sensitive areas of centrifugal nozzles