INFLUENCE OF SHOCK-WAVE ATTENUATION BY BOUNDARY-LAYER GROWTH ON CONTACT-SURFACE MOTION IN A SHOCK TUBE

被引：5
|
作者：
ROSCISZEWSKI, J
机构：
来源：
JOURNAL OF THE AEROSPACE SCIENCES | 1959年 / 26卷 / 06期
关键词：
D O I：
10.2514/8.8098
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：388 / 389
页数：2
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