PARTIALLY IONIZED-GAS FLOW AND HEAT-TRANSFER IN SEPARATION, REATTACHMENT, AND REDEVELOPMENT REGIONS DOWNSTREAM OF AN ABRUPT CIRCULAR CHANNEL EXPANSION

被引:3
作者
BACK, LH
ROSCHKE, EJ
MASSIER, PF
机构
来源
JOURNAL OF HEAT TRANSFER | 1972年 / 94卷 / 01期
关键词
D O I
10.1115/1.3449859
中图分类号
O414.1 [热力学];
学科分类号
摘要
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页码:119 / +
页数:1
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[1]  
ABUROMIA MM, 1969, AIAA69601 PAP
[2]   MEASUREMENT OF VISCOSITY OF ATMOSPHERIC ARGON FROM 3500 TO 8500 DEGREES K [J].
AESCHLIMAN, DP ;
CAMBEL, AB .
PHYSICS OF FLUIDS, 1970, 13 (10) :2466-+
[3]   PROPERTIES OF GASES AT VERY HIGH TEMPERATURES [J].
AMDUR, I ;
MASON, EA .
PHYSICS OF FLUIDS, 1958, 1 (05) :370-383
[4]   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-&
[5]   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-&
[6]   LAMINAR BOUNDARY-LAYER HEAT TRANSFER FROM A PARTIALLY IONIZED MONATOMIC GAS [J].
BACK, LH .
PHYSICS OF FLUIDS, 1967, 10 (04) :807-&
[7]   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-&
[8]   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-&
[9]   FLOW AND HEAT TRANSFER IN LAMINAR BOUNDARY LAYERS WITH SWIRL [J].
BACK, LH .
AIAA JOURNAL, 1969, 7 (09) :1781-&
[10]  
BACK LH, 1968, 321301 JET PROP LAB