UNSTEADY HYPERSONIC FLOW OVER DELTA WINGS WITH DETACHED SHOCK-WAVES

被引：13
作者：
HUI, WH [1 ]
HEMDAN, HT [1 ]
机构：
[1] UNIV WATERLOO,DEPT APPL MATH,WATERLOO,ONTARIO,CANADA
来源：
AIAA JOURNAL | 1976年 / 14卷 / 04期
关键词：
D O I：
10.2514/3.7120
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
引用
收藏
页码：505 / 511
页数：7
相关论文
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[8]   METHODS FOR CALCULATING NONLINEAR FLOWS WITH ATTACHED SHOCK-WAVES OVER CONICAL WINGS [J].
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[9]  
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LIU DL, TO BE PUBLISHED
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