Comparative analysis of computational methods of supersonic combustor flowfield

被引：0
|
作者：
Wang, Cheng-Peng [1 ]
Yang, Yong-Yang [1 ]
Liu, Chen [1 ]
Wang, Jiang-Feng [1 ]
Cheng, Ke-Ming [1 ]
Wu, Yi-Zhao [1 ]
机构：
[1] College of Aerospace Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China
来源：
Hangkong Dongli Xuebao/Journal of Aerospace Power | 2009年 / 24卷 / 05期
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页码：963 / 969
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