ACCELERATION AND COOLING EFFECTS IN LAMINAR BOUNDARY LAYERS - SUBSONIC, TRANSONIC, AND SUPERSONIC SPEEDS

被引：22

作者：

BACK, LH

机构：

来源：

关键词：

D O I：

10.2514/3.5758

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

引用

页码：794 / &

共 29 条

[1] 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 - &
[2] FLOW AND HEAT TRANSFER IN LAMINAR BOUNDARY LAYERS WITH SWIRL
BACK, LH
[J]. AIAA JOURNAL, 1969, 7 (09) : 1781 - &
[3] BACK LH, 1968, TR321301 JET PROP LA
[4] BACK LH, 1967, P HEAT TRANSFER FLUI, P410
[5] BACK LH, TO BE PUBLISHED
[6] BACK LH, 1966, T ASME C, V88, P249
[7] STAGNATION-POINT HEAT TRANSFER IN A HIGH-TEMPERATURE INERT GAS
BADE, WL
[J]. PHYSICS OF FLUIDS, 1962, 5 (02) : 150 - 154
[8] BECKWITH IE, 1961, TND625 NASA
[9] COHEN CB, 1956, R1293 NACA
[10] COLES D, 1957, P HEAT TRANSFER FLUI, P119