SHOCK-TUBE STUDIES OF TRANSONIC FLOW OVER WEDGE PROFILES

被引：12
作者：
GRIFFITH, W
机构：
来源：
JOURNAL OF THE AERONAUTICAL SCIENCES | 1952年 / 19卷 / 04期
关键词：
D O I：
10.2514/8.2242
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：249 / &
相关论文
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