INFLUENCE OF CONTRACTION SECTION SHAPE AND INLET FLOW DIRECTION ON SUPERSONIC NOZZLE FLOW AND PERFORMANCE

被引：8

作者：

BACK, LH

MASSIER, PF

CUFFEL, RF

机构：

来源：

JOURNAL OF SPACECRAFT AND ROCKETS | 1972年 / 9卷 / 06期

关键词：

D O I：

10.2514/3.61705

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

引用

页码：420 / +

页数：1

共 16 条

[1] DETECTION OF OBLIQUE SHOCKS IN A CONICAL NOZZLE WITH A CIRCULAR-ARC THROAT [J].

BACK, LH ;

CUFFEL, RF .

AIAA JOURNAL, 1966, 4 (12) :2219-&

[2] FLOW AND HEAT-TRANSFER MEASUREMENTS IN SUBSONIC AIR FLOW THROUGH A CONTRACTION SECTION [J].

BACK, LH ;

MASSIER, PF ;

CUFFEL, RF .

INTERNATIONAL JOURNAL OF HEAT AND MASS TRANSFER, 1969, 12 (01) :1-&

[3] FLOW COEFFICIENTS FOR SUPERSONIC NOZZLES WITH COMPARATIVELY SMALL RADIUS OF CURVATURE THROATS [J].

BACK, LH ;

CUFFEL, RF .

JOURNAL OF SPACECRAFT AND ROCKETS, 1971, 8 (02) :196-&

[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].

BACK, LH ;

MASSIER, PF ;

GIER, HL .

AIAA JOURNAL, 1965, 3 (09) :1606-&

[6] LAMINARIZATION OF A TURBULENT BOUNDARY LAYER IN NOZZLE FLOW - BOUNDARY LAYER AND HEAT TRANSFER MEASUREMENTS WITH WALL COOLING [J].

BACK, LH ;

CUFFEL, RF ;

MASSIER, PF .

JOURNAL OF HEAT TRANSFER, 1970, 92 (03) :333-&

[7] FLOW PHENOMENA AND CONVECTIVE HEAT TRANSFER IN A CONICAL SUPERSONIC NOZZLE [J].

BACK, LH ;

MASSIER, PF ;

CUFFEL, RF .

JOURNAL OF SPACECRAFT AND ROCKETS, 1967, 4 (08) :1040-&

[8] TRANSONIC FLOWFIELD IN A SUPERSONIC NOZZLE WITH SMALL THROAT RADIUS OF CURVATURE [J].

CUFFEL, RF ;

BACK, LH ;

MASSIER, PF .

AIAA JOURNAL, 1969, 7 (07) :1364-&

[9] THRUST CHARACTERISTICS OF UNDEREXPANDED NOZZLES [J].

DURHAM, FP .

JET PROPULSION, 1955, 25 (12) :696-700

[10]

DURHAM FP, 1953, N123S82337 CONTR

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