-
2
-
-
0017479546
-
Near-field character of a jet discharged through a wall at 30° to a mainstream
-
Bergeles G; Gosman AD; Launder BE (1977) Near-field character of a jet discharged through a wall at 30° to a mainstream. AIAA J 15: 499-504
-
(1977)
AIAA J
, vol.15
, pp. 499-504
-
-
Bergeles, G.1
Gosman, A.D.2
Launder, B.E.3
-
3
-
-
0016058529
-
Heat transfer and film cooling following injection through inclined circular holes
-
Eriksen VL; Goldstein RJ (1974) Heat transfer and film cooling following injection through inclined circular holes. ASME J Heat Transfer 96: 239-245
-
(1974)
ASME J Heat Transfer
, vol.96
, pp. 239-245
-
-
Eriksen, V.L.1
Goldstein, R.J.2
-
4
-
-
0016462499
-
-
McGraw-Hill, New York
-
Hinze JO; (1975) Turbulence. McGraw-Hill, New York
-
(1975)
Turbulence
-
-
Hinze, J.O.1
-
5
-
-
0025461031
-
Surface injection effect on mass transfer from a cylinder in crossflow: A simulation of film cooling in the leading edge region of a turbine blade
-
Karni J; Goldstein RJ (1990) Surface injection effect on mass transfer from a cylinder in crossflow: A simulation of film cooling in the leading edge region of a turbine blade. ASME J Turbomach 112: 418-427
-
(1990)
ASME J Turbomach
, vol.112
, pp. 418-427
-
-
Karni, J.1
Goldstein, R.J.2
-
6
-
-
0028179322
-
Effects of embedded vortices on injectant from film cooling holes with large spanwise spacing and compound angle orientations in a turbulent boundary layer
-
Ligrani PM; Mitchell SW (1994) Effects of embedded vortices on injectant from film cooling holes with large spanwise spacing and compound angle orientations in a turbulent boundary layer. ASME J Turbomach 116: 709-720
-
(1994)
ASME J Turbomach
, vol.116
, pp. 709-720
-
-
Ligrani, P.M.1
Mitchell, S.W.2
-
7
-
-
0028424911
-
Film-cooling from holes with compound angle orientations: Part 2 - Results downstream of a single row of holes with 6d spanwise spacing
-
Ligrani PM; Wigle JM; Jackson SW (1994) Film-cooling from holes with compound angle orientations: Part 2 - Results downstream of a single row of holes with 6d spanwise spacing. ASME J Heat Transfer 116: 353-362
-
(1994)
ASME J Heat Transfer
, vol.116
, pp. 353-362
-
-
Ligrani, P.M.1
Wigle, J.M.2
Jackson, S.W.3
-
8
-
-
0017490856
-
Stagnation region gas film cooling for turbine blade leading-edge applications
-
Luckey DW; Winstanley DK; Hanus GJ; L'Ecuyer MR (1977) Stagnation region gas film cooling for turbine blade leading-edge applications. J Aircraft 14: 494-501
-
(1977)
J Aircraft
, vol.14
, pp. 494-501
-
-
Luckey, D.W.1
Winstanley, D.K.2
Hanus, G.J.3
L'Ecuyer, M.R.4
-
9
-
-
0023828989
-
Stagnation film cooling and heat transfer, including its effect within the hole pattern
-
Mick WJ; Mayle RE (1988) Stagnation film cooling and heat transfer, including its effect within the hole pattern. ASME J Turbomach 110: 66-72.
-
(1988)
ASME J Turbomach
, vol.110
, pp. 66-72
-
-
Mick, W.J.1
Mayle, R.E.2
-
10
-
-
0028051174
-
Leading edge film cooling heat transfer through one row of inclined film slots and holes including mainstream turbulence effects
-
Ou S; Han JC (1994) Leading edge film cooling heat transfer through one row of inclined film slots and holes including mainstream turbulence effects. ASME J Heat Transfer 116: 561-569
-
(1994)
ASME J Heat Transfer
, vol.116
, pp. 561-569
-
-
Ou, S.1
Han, J.C.2
-
11
-
-
11644275941
-
An experimental investigation of the velocity and temperature fields of cold jets injected into a hot crossflow
-
Rydholm HA (1998) An experimental investigation of the velocity and temperature fields of cold jets injected into a hot crossflow. ASME J Turbomach 120: 320-326
-
(1998)
ASME J Turbomach
, vol.120
, pp. 320-326
-
-
Rydholm, H.A.1
-
12
-
-
4243193913
-
Film cooling with compound angle holes: Adiabatic effectiveness
-
Schmidt DL; Sen B; Bogard DG (1996) Film cooling with compound angle holes: adiabatic effectiveness. ASME J Turbomach 118: 807-813
-
(1996)
ASME J Turbomach
, vol.118
, pp. 807-813
-
-
Schmidt, D.L.1
Sen, B.2
Bogard, D.G.3
-
13
-
-
0030446933
-
Film cooling with compound angle holes: Heat transfer
-
Sen B; Schmidt DL; Bogard DG (1996) Film cooling with compound angle holes: heat transfer. ASME J Turbomach 118: 800-806
-
(1996)
ASME J Turbomach
, vol.118
, pp. 800-806
-
-
Sen, B.1
Schmidt, D.L.2
Bogard, D.G.3
-
14
-
-
0026188801
-
Film-cooling effectiveness downstream of a single row of holes with variable density ratio
-
Sinha AK; Bogard DG; Crawford ME (1991) Film-cooling effectiveness downstream of a single row of holes with variable density ratio. ASME J Turbomach 113: 442-449
-
(1991)
ASME J Turbomach
, vol.113
, pp. 442-449
-
-
Sinha, A.K.1
Bogard, D.G.2
Crawford, M.E.3
-
15
-
-
0032000903
-
Mixing, structure and scaling of the jet in crossflow
-
Smith SH; Mungal MG (1998) Mixing, structure and scaling of the jet in crossflow. J Fluid Mech 357: 83-122
-
(1998)
J Fluid Mech
, vol.357
, pp. 83-122
-
-
Smith, S.H.1
Mungal, M.G.2
-
16
-
-
0024302148
-
The use of foreign gas to simulate the effects of density ratios in film cooling
-
Teekaram AJH; Forth CJP; Jones TV (1989) The use of foreign gas to simulate the effects of density ratios in film cooling. ASME J Turbomach 111: 57-62
-
(1989)
ASME J Turbomach
, vol.111
, pp. 57-62
-
-
Teekaram, A.J.H.1
Forth, C.J.P.2
Jones, T.V.3
-
17
-
-
11644284181
-
Flowfield measurements for film-cooling holes with expanded exits
-
Thole K; Gritsch M; Schulz A; Wittig S (1998) Flowfield measurements for film-cooling holes with expanded exits. ASME J Turbomach 120: 327-336
-
(1998)
ASME J Turbomach
, vol.120
, pp. 327-336
-
-
Thole, K.1
Gritsch, M.2
Schulz, A.3
Wittig, S.4
|