TRANSONIC LAMINAR BOUNDARY-LAYERS WITH SURFACE CURVATURE

被引：3

作者：

BACK, LH ^{[1
]}

机构：

[1] CALTECH,PROP RES & ADV CONCEPTS SECT,JET PROP LAB,PASADENA,CA 91109

来源：

INTERNATIONAL JOURNAL OF HEAT AND MASS TRANSFER | 1973年 / 16卷 / 09期

关键词：

D O I：

10.1016/0017-9310(73)90165-8

中图分类号：

O414.1 [热力学];

学科分类号：

摘要：

引用

页码：1745 / 1761

页数：17

共 36 条

[1]

ADAMS JC, 1968, AEDCTR6857 ARN ENG D

[2]

ADAMS JC, 1967, SEP AGARD SEM NUM ME

[3] VISCOUS NON-ADIABATIC LAMINAR-FLOW THROUGH A SUPERSONIC NOZZLE - EXPERIMENTAL RESULTS AND NUMERICAL CALCULATIONS [J].

BACK, LH ;

MASSIER, PF .

JOURNAL OF HEAT TRANSFER, 1972, 94 (04) :437-&

[4] EFFECT OF INLET BOUNDARY-LAYER THICKNESS AND STRUCTURE ON HEAT TRANSFER IN A SUPERSONIC NOZZLE [J].

BACK, LH ;

MASSIER, PF ;

CUFFEL, RF .

JOURNAL OF SPACECRAFT AND ROCKETS, 1968, 5 (01) :121-&

[5] PREDICTION OF HEAT TRANSFER FROM LAMINAR BOUNDARY LAYERS WITH EMPHASIS ON LARGE FREE-STREAM VELOCITY GRADIENTS AND HIGHLY COOLED WALLS [J].

BACK, LH ;

WITTE, AB .

JOURNAL OF HEAT TRANSFER, 1966, 88 (03) :249-&

[6] ACCELERATION AND COOLING EFFECTS IN LAMINAR BOUNDARY LAYERS - SUBSONIC, TRANSONIC, AND SUPERSONIC SPEEDS [J].

BACK, LH .

AIAA JOURNAL, 1970, 8 (04) :794-&

[7] 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-&

[8] 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-&

[9] 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-&

[10] FLOW AND HEAT TRANSFER IN LAMINAR BOUNDARY LAYERS WITH SWIRL [J].

BACK, LH .

AIAA JOURNAL, 1969, 7 (09) :1781-&

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