FLOW NEAR A WEAK SHOCK-WAVE DOWNSTREAM OF A NOZZLE THROAT

被引:15
|
作者
MESSITER, AF [1 ]
ADAMSON, TC [1 ]
机构
[1] UNIV MICHIGAN,DEPT AEROSP ENGN,ANN ARBOR,MI 48104
关键词
D O I
10.1017/S0022112075001334
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
引用
收藏
页码:97 / 108
页数:12
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