EFFECT OF INLET BOUNDARY-LAYER THICKNESS AND STRUCTURE ON HEAT TRANSFER IN A SUPERSONIC NOZZLE

被引：5
|
作者：
BACK, LH
MASSIER, PF
CUFFEL, RF
机构：
来源：
JOURNAL OF SPACECRAFT AND ROCKETS | 1968年 / 5卷 / 01期
关键词：
D O I：
10.2514/3.29200
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
引用
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页码：121 / &
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