EXPERIMENTAL STUDY OF HIGH-ENTHALPY SHOCK-TUNNEL FLOW .2. NOZZLE-FLOW CHARACTERISTICS

被引：6
|
作者：
DUNN, MG
机构：
来源：
AIAA JOURNAL | 1969年 / 7卷 / 09期
关键词：
D O I：
10.2514/3.5381
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：1717 / &
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