LAMINARIZATION OF A TURBULENT BOUNDARY LAYER IN NOZZLE FLOW - BOUNDARY LAYER AND HEAT TRANSFER MEASUREMENTS WITH WALL COOLING

被引：21

作者：

BACK, LH

CUFFEL, RF

MASSIER, PF

机构：

来源：

JOURNAL OF HEAT TRANSFER | 1970年 / 92卷 / 03期

关键词：

D O I：

10.1115/1.3449668

中图分类号：

O414.1 [热力学];

学科分类号：

摘要：

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页码：333 / &

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[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] HEAT-TRANSFER MEASUREMENTS IN SHOCK-INDUCED FLOW SPEARATION REGION IN A SUPERSONIC NOZZLE
BACK, LH
MASSIER, PF
CUFFEL, RF
[J]. AIAA JOURNAL, 1968, 6 (05) : 923 - &
[3] ACCELERATION AND COOLING EFFECTS IN LAMINAR BOUNDARY LAYERS - SUBSONIC, TRANSONIC, AND SUPERSONIC SPEEDS
BACK, LH
[J]. AIAA JOURNAL, 1970, 8 (04) : 794 - &
[4] SOME OBSERVATIONS ON REDUCTION OF TURBULENT BOUNDARY-LAYER HEAT TRANSFER IN NOZZLES
BACK, LH
MASSIER, PF
CUFFEL, RF
[J]. AIAA JOURNAL, 1966, 4 (12) : 2226 - &
[5] COMPARISON OF MEASURED AND PREDICTED FLOWS THROUGH CONICAL SUPERSONIC NOZZLES WITH EMPHASIS ON TRANSONIC REGION
BACK, LH
MASSIER, PF
GIER, HL
[J]. AIAA JOURNAL, 1965, 3 (09) : 1606 - &
[6] 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 - &
[7] BACK LH, 1967, P HEAT TRANSFER FLUI, P410
[8] BACK LH, 1962, THESIS U CALIFORNIA
[9] BACK LH, TO BE PUBLISHED
[10] BACK LH, 1966, T ASME C, V88, P249

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