ANALYSIS OF UNSTEADY TRANSONIC CHANNEL FLOW WITH SHOCK-WAVES

被引：13
|
作者：
RICHEY, GK
ADAMSON, TC
机构：
[1] USAF,FLIGHT DYNAM LAB,WRIGHT PATTERSON AFB,OH 45433
[2] UNIV MICHIGAN,ANN ARBOR,MI 48104
来源：
AIAA JOURNAL | 1976年 / 14卷 / 08期
关键词：
D O I：
10.2514/3.61441
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：1054 / 1061
页数：8
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