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
来源：
AIAA JOURNAL | 1974年 / 12卷 / 03期
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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