MEASUREMENTS OF A SIMULATED ROCKET EXHAUST PLUME NEAR PRANDTL-MEYER LIMITING ANGLE

被引：5

作者：

CALIA, VS ^{[1
]}

BROOK, JW ^{[1
]}

机构：

[1] GRUMMAN AEROSP CORP,GAS DYNAM BRANCH,RES DEPT,BETHPAGE,NY 11714

来源：

关键词：

D O I：

10.2514/3.27831

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

引用

页码：205 / 208

页数：4

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[7] ANALYTICAL APPROXIMATION FOR FLOW FROM A NOZZLE INTO A VACUUM [J].

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DRAPER, JS .

[8]

LENG J, 1968, J SPACECRAFT ROCKETS, V5, P1148

[9]

OSONITSCH CW, 1967, LMO510668 LM ENG MEM

[10]

ROBERTS L, 1963, 31ST M I AER SCIENC