FLOW PHENOMENA AND CONVECTIVE HEAT TRANSFER IN A CONICAL SUPERSONIC NOZZLE

被引:33
作者
BACK, LH
MASSIER, PF
CUFFEL, RF
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关键词
D O I
10.2514/3.29015
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
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页码:1040 / &
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共 32 条
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[3]   DETECTION OF OBLIQUE SHOCKS IN A CONICAL NOZZLE WITH A CIRCULAR-ARC THROAT [J].
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[4]   SOME OBSERVATIONS ON REDUCTION OF TURBULENT BOUNDARY-LAYER HEAT TRANSFER IN NOZZLES [J].
BACK, LH ;
MASSIER, PF ;
CUFFEL, RF .
AIAA JOURNAL, 1966, 4 (12) :2226-&
[5]   COMPARISON OF MEASURED AND PREDICTED FLOWS THROUGH CONICAL SUPERSONIC NOZZLES WITH EMPHASIS ON TRANSONIC REGION [J].
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MASSIER, PF ;
GIER, HL .
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