INVERSE INTEGRAL COMPUTATIONAL METHOD FOR COMPRESSIBLE TURBULENT BOUNDARY LAYERS.

被引：0

|

作者：

Whitfield, D.L.

Swafford, T.W.

Donegan, T.L.

机构：

来源：

| 1982年

关键词：

Compendex;

D O I：

10.1007/978-3-642-81932-2_30

中图分类号：

学科分类号：

摘要：

MATHEMATICAL TECHNIQUES - Integral Equations

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页码：294 / 302

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[1] CALCULATION METHOD FOR THREE DIMENSIONAL TURBULENT BOUNDARY LAYERS.
Dubey, Neeraj
Wakhaloo, C.L.
Defence Science Journal, 1982, 32 (04) : 275 - 283
[2] HEAT TRANSFER OF DISC ROTATING IN A HOUSING WITH TRANSITIONAL AND TURBULENT BOUNDARY LAYERS.
Shchukin, V.K.
Olimpiev, V.V.
Soviet Aeronautics (English translation of Izvestiya VUZ, Aviatsionnaya Tekhnika), 1975, 18 (03): : 77 - 81
[3] NUMERICAL SIMULATION OF TURBULENT FLOWS IN THREE-DIMENSIONAL BOUNDARY LAYERS.
ALEKSIN, V.A.
SHEVELEV, YU.D.
1981, V 13 (N 4): : 130 - 135
[4] NUMERICAL SIMULATION OF TURBULENT FLOWS IN THREE-DIMENSIONAL BOUNDARY LAYERS.
Aleskin, V.A.
Shevelev, Yu.D.
Heat transfer. Soviet research, 1980, 13 (04): : 130 - 135
[5] EFFECT OF THE PROXIMITY OF THE WALL ON HOT-WIRE READINGS IN LAMINAR AND TURBULENT BOUNDARY LAYERS.
Zemskaya, A.S.
Levitskiy, V.N.
Repik, Ye.U.
Sosedko, Yu.P.
Fluid mechanics. Soviet research, 1979, 8 (01): : 133 - 141
[6] IMPROVED SOLUTION FOR LAMINAR THERMAL BOUNDARY LAYERS.
Macagno, Enzo O.
Macagno, Matilde
Miloh, Touvia
1600,
[7] HEAT TRANSFER TO NON-NEWTONIAN BOUNDARY LAYERS.
Shul'man, Z.P.
Heat transfer. Soviet research, 1980, 12 (01): : 17 - 30
[8] NUMERICAL STUDY OF SEPARATING SUPERSONIC LAMINAR BOUNDARY LAYERS.
Werle, M.J.
Senechal, G.D.
1600,
[9] METHODS FOR ESTIMATING PRESSURE AND THERMAL LOADS INDUCED BY ELEVON DEFLECTIONS ON HYPERSONIC-VEHICLE SURFACES WITH TURBULENT BOUNDARY LAYERS.
Kaufman II, Louis G.
Johnson, Charles B.
NASA Technical Memorandum, 1981,
[10] HEAT TRANSFER IN COMPRESSIBLE TURBULENT BOUNDARY LAYER.
Bauer, K.
Winkler, W.
Grigull, U.
1978,

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