Modified axisymmetric basic flowfield for hypersonic inward turning inlet

被引：0
|
作者：
Li, Yong-Zhou [1 ]
Zhang, Kun-Yuan [1 ]
Luo, Lei [1 ]
Wang, Lei [1 ]
机构：
[1] College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China
来源：
Hangkong Dongli Xuebao/Journal of Aerospace Power | 2013年 / 28卷 / 11期
关键词：
Compression ratio (machinery) - Mass transfer - Design - Shock waves - Hypersonic inlets - Numerical methods - Aerodynamics - Flow fields;
D O I：
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中图分类号：
学科分类号：
摘要：
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页码：2543 / 2552
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