FURTHER EXPERIMENTS ON SHOCK-TUBE WALL BOUNDARY-LAYER-TRANSITION - REPLY

被引:0
作者
COOK, WJ [1 ]
CHANEY, MJ [1 ]
机构
[1] SVERDRUP TECHNOL INC, ARNOLD AFB, TN USA
关键词
D O I
10.2514/3.8198
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:1298 / 1299
页数:2
相关论文
共 3 条
[1]   FURTHER EXPERIMENTS ON SHOCK-TUBE WALL BOUNDARY-LAYER-TRANSITION [J].
CHANEY, MJ ;
COOK, WJ .
AIAA JOURNAL, 1983, 21 (07) :1046-1048
[2]  
CHANEY MJ, 1977, THESIS IOWA STATE U
[3]   TURBULENT SPOTS AND WALL ROUGHNESS EFFECTS IN SHOCK TUBE BOUNDARY LAYER TRANSITION [J].
THOMPSON, WP ;
EMRICH, RJ .
PHYSICS OF FLUIDS, 1967, 10 (01) :17-&