SHOCK-WAVE BOUNDARY-LAYER INTERACTIONS IN LAMINAR TRANSONIC FLOW

被引:12
|
作者
BRILLIANT, HM [1 ]
ADAMSON, TC [1 ]
机构
[1] UNIV MICHIGAN, ANN ARBOR, MI USA
关键词
D O I
10.2514/3.49228
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:323 / 329
页数:7
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