INFLUENCE OF THE LEADING-EDGE SHOCK WAVE ON THE LAMINAR BOUNDARY LAYER AT HYPERSONIC SPEEDS

被引：7
|
作者：
LEES, L
机构：
来源：
JOURNAL OF THE AERONAUTICAL SCIENCES | 1956年 / 23卷 / 06期
关键词：
D O I：
10.2514/8.3614
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
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页码：594 / &
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