HEAT-TRANSFER MEASUREMENTS IN SHOCK-INDUCED FLOW SPEARATION REGION IN A SUPERSONIC NOZZLE

被引：4

作者：

BACK, LH

MASSIER, PF

CUFFEL, RF

机构：

来源：

关键词：

D O I：

10.2514/3.4626

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

引用

页码：923 / &

共 4 条

[1] Back L.H., 1964, INT J HEAT MASS TRAN, V7, P549, DOI [10.1016/0017-9310(64)90052-3, DOI 10.1016/0017-9310(64)90052-3]
[2] DETECTION OF OBLIQUE SHOCKS IN A CONICAL NOZZLE WITH A CIRCULAR-ARC THROAT
BACK, LH
CUFFEL, RF
[J]. AIAA JOURNAL, 1966, 4 (12) : 2219 - &
[3] FLOW PHENOMENA AND CONVECTIVE HEAT TRANSFER IN A CONICAL SUPERSONIC NOZZLE
BACK, LH
MASSIER, PF
CUFFEL, RF
[J]. JOURNAL OF SPACECRAFT AND ROCKETS, 1967, 4 (08) : 1040 - &
[4] CROCCO L, 1958, FUNDAMENTALS GAS DYN, V3, P167