DELTA WING SHOCK SHAPE AT HYPERSONIC SPEED

被引：2
|
作者：
RAO, DM
机构：
来源：
AIAA JOURNAL | 1971年 / 9卷 / 10期
关键词：
D O I：
10.2514/3.6479
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：2093 / &
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