-
1
-
-
0025460683
-
The effect of density ratio on the heat transfer coefficient from a film-cooled flat plate
-
Ammari H.D., Hay N., Lampard D. The effect of density ratio on the heat transfer coefficient from a film-cooled flat plate. ASME Journal of Turbomachinery. 112:1990;444-450.
-
(1990)
ASME Journal of Turbomachinery
, vol.112
, pp. 444-450
-
-
Ammari, H.D.1
Hay, N.2
Lampard, D.3
-
2
-
-
0031360624
-
The Influence of coolant supply geometry on film coolant exit flow and surface adiabatic effectiveness
-
Burd, S.W., Simon, T.W., 1997. The Influence of coolant supply geometry on film coolant exit flow and surface adiabatic effectiveness. ASME Paper 97-GT-25.
-
(1997)
ASME Paper 97-GT-25
-
-
Burd, S.W.1
Simon, T.W.2
-
3
-
-
0029155060
-
Heat (mass) transfer and film cooling effectiveness with injection through discrete holes: Part II - On the exposed surface
-
Cho H.H., Goldstein R.J. Heat (mass) transfer and film cooling effectiveness with injection through discrete holes: Part II - On the exposed surface. ASME Journal of Turbomachinery. 117:1995;451-460.
-
(1995)
ASME Journal of Turbomachinery
, vol.117
, pp. 451-460
-
-
Cho, H.H.1
Goldstein, R.J.2
-
5
-
-
0021190898
-
Analysis of film cooling and full-coverage film cooling of gas turbine blades
-
Eckert E.R.G. Analysis of film cooling and full-coverage film cooling of gas turbine blades. ASME Journal of Engineering for Gas Turbines and Power. 106:1984;206-213.
-
(1984)
ASME Journal of Engineering for Gas Turbines and Power
, vol.106
, pp. 206-213
-
-
Eckert, E.R.G.1
-
6
-
-
0031191260
-
2 injection through compound angle holes using a transient liquid crystal image method
-
2 injection through compound angle holes using a transient liquid crystal image method ASME Journal of Turbomachinery. 119:1997a;587-593.
-
(1997)
ASME Journal of Turbomachinery
, vol.119
, pp. 587-593
-
-
Ekkad, S.V.1
Zapata, D.2
Han, J.C.3
-
7
-
-
0031190345
-
2 injection through compound angle holes using a transient liquid crystal image method
-
2 injection through compound angle holes using a transient liquid crystal image method ASME Journal of Turbomachinery. 119:1997b;580-586.
-
(1997)
ASME Journal of Turbomachinery
, vol.119
, pp. 580-586
-
-
Ekkad, S.V.1
Zapata, D.2
Han, J.C.3
-
8
-
-
0016058529
-
Heat transfer and film cooling following injection through inclined circular tubes
-
Eriksen V.L., Goldstein R.J. Heat transfer and film cooling following injection through inclined circular tubes. ASME Journal of Heat Transfer. 96:1974;239-245.
-
(1974)
ASME Journal of Heat Transfer
, vol.96
, pp. 239-245
-
-
Eriksen, V.L.1
Goldstein, R.J.2
-
10
-
-
0031354242
-
Film-cooling from holes with expanded exits: comparison of computational results with experiment
-
Giebert, D., Gritsch, M., Schulz, A., Wittig, S., 1997. Film-cooling from holes with expanded exits: comparison of computational results with experiment. ASME Paper 97-GT-163.
-
(1997)
ASME Paper 97-GT-163
-
-
Giebert, D.1
Gritsch, M.2
Schulz, A.3
Wittig, S.4
-
13
-
-
0020206771
-
Mass transfer in the neighborhood of jets entering a crossflow
-
Goldstein R.J., Taylor J.R. Mass transfer in the neighborhood of jets entering a crossflow. ASME Journal of Heat Transfer. 104:1982;715-721.
-
(1982)
ASME Journal of Heat Transfer
, vol.104
, pp. 715-721
-
-
Goldstein, R.J.1
Taylor, J.R.2
-
14
-
-
84928494157
-
The superposition approach to local heat transfer coefficients in high density ratio film-cooling flows
-
Gritsch, M., Baldauf, S., Martiny, M., Schulz, A., Wittig, S., 1999. The superposition approach to local heat transfer coefficients in high density ratio film-cooling flows, ASME Paper 99-GT-168.
-
(1999)
ASME Paper 99-GT-168
-
-
Gritsch, M.1
Baldauf, S.2
Martiny, M.3
Schulz, A.4
Wittig, S.5
-
15
-
-
0032124987
-
Adiabatic wall effectiveness measurements of film-cooling holes with expanded exits
-
Gritsch M., Schulz A., Wittig S. Adiabatic wall effectiveness measurements of film-cooling holes with expanded exits. ASME Journal of Turbomachinery. 120:1998;549-556.
-
(1998)
ASME Journal of Turbomachinery
, vol.120
, pp. 549-556
-
-
Gritsch, M.1
Schulz, A.2
Wittig, S.3
-
16
-
-
0020926764
-
Aerodynamic loss penalty produced by film cooling transonic turbine blades
-
Haller, B.R., Camus, J.J., 1983. Aerodynamic loss penalty produced by film cooling transonic turbine blades. ASME Paper 83-GT-77.
-
(1983)
ASME Paper 83-GT-77
-
-
Haller, B.R.1
Camus, J.J.2
-
17
-
-
0029107256
-
Heat transfer measurements on turbine airfoils using the naphtalene sublimation technique
-
Häring M., Bölcs A., Harasgama S.P., Richter J. Heat transfer measurements on turbine airfoils using the naphtalene sublimation technique. ASME Journal of Turbomachinery. 117:1995;432-439.
-
(1995)
ASME Journal of Turbomachinery
, vol.117
, pp. 432-439
-
-
Häring, M.1
Bölcs, A.2
Harasgama, S.P.3
Richter, J.4
-
18
-
-
18744432219
-
The discharge coefficient of flared film cooling holes
-
Hay, N., Lampard, D., 1995. The discharge coefficient of flared film cooling holes. ASME Paper 95-GT-15.
-
(1995)
ASME Paper 95-GT-15
-
-
Hay, N.1
Lampard, D.2
-
20
-
-
84973150076
-
The swollen polymer technique and its use for heat transfer investigations on film cooled surfaces
-
AGARD-CP-527 Paper 19
-
Hay, N., Lampard, D., Macleod, N., 1993. The swollen polymer technique and its use for heat transfer investigations on film cooled surfaces. Heat Transfer and Cooling in Gas Turbines, AGARD-CP-527 Paper 19.
-
(1993)
Heat Transfer and Cooling in Gas Turbines
-
-
Hay, N.1
Lampard, D.2
Macleod, N.3
-
21
-
-
0021898059
-
Effects of cooling films on the heat transfer coefficient on a flat plate with zero mainstream pressure gradient
-
Hay N., Lampard D., Saluja C.L. Effects of cooling films on the heat transfer coefficient on a flat plate with zero mainstream pressure gradient. Journal of Engineering for Gas Turbines and Power. 107:1985;104-110.
-
(1985)
Journal of Engineering for Gas Turbines and Power
, vol.107
, pp. 104-110
-
-
Hay, N.1
Lampard, D.2
Saluja, C.L.3
-
22
-
-
0031382999
-
A detailed analysis of film cooling physics Part III: Streamwise injection with shaped holes
-
Hyams, D.G., Leylek, J.H., 1997. A detailed analysis of film cooling physics Part III: Streamwise injection with shaped holes. ASME Paper 97-GT-271.
-
(1997)
ASME Paper 97-GT-271
-
-
Hyams, D.G.1
Leylek, J.H.2
-
24
-
-
0002477246
-
Describing uncertainties in single-sample experiments
-
Kline S.J., McClintock F.A. Describing uncertainties in single-sample experiments. Mechanical Engineering. 75:1953;3-8.
-
(1953)
Mechanical Engineering
, vol.75
, pp. 3-8
-
-
Kline, S.J.1
McClintock, F.A.2
-
25
-
-
0000212924
-
A CFD investigation on the effects of entrance crossflow directions to film-cooling holes
-
Baltimore, MD, 10-12 August 1997
-
Kohli, A., Thole, K.A., 1997. A CFD investigation on the effects of entrance crossflow directions to film-cooling holes. In: Proceedings of the 32nd National Heat Transfer Conference. Baltimore, MD, 10-12 August 1997.
-
(1997)
In: Proceedings of the 32nd National Heat Transfer Conference
-
-
Kohli, A.1
Thole, K.A.2
-
26
-
-
0016432272
-
Experimental investigation of film cooling with ejection from a row of holes for the application to gas turbine blades
-
Liess C. Experimental investigation of film cooling with ejection from a row of holes for the application to gas turbine blades. ASME Journal of Engineering for Power. 97:1975;21-27.
-
(1975)
ASME Journal of Engineering for Power
, vol.97
, pp. 21-27
-
-
Liess, C.1
-
27
-
-
0026108367
-
Effects of vortices with different circulations on heat transfer and injectant downstream of a single film-cooling hole in a turbulent boundary layer
-
Ligrani P.M., Subramanian C.S., Craig D.W., Kaisuwan P. Effects of vortices with different circulations on heat transfer and injectant downstream of a single film-cooling hole in a turbulent boundary layer. ASME Journal of Heat Transfer. 113:1991;79-90.
-
(1991)
ASME Journal of Heat Transfer
, vol.113
, pp. 79-90
-
-
Ligrani, P.M.1
Subramanian, C.S.2
Craig, D.W.3
Kaisuwan, P.4
-
28
-
-
85077335033
-
An experimental study of film cooling from diffused trapezoidal shaped holes
-
Makki, Y.H., Jakubowski, G., 1986. An experimental study of film cooling from diffused trapezoidal shaped holes. AIAA Paper 86-1326.
-
(1986)
AIAA Paper 86-1326
-
-
Makki, Y.H.1
Jakubowski, G.2
-
29
-
-
0141690516
-
In situ calibration for quantitative infrared thermography
-
Germany, 2-5 September 1996
-
Martiny, M., Schiele, R., Gritsch, M., Schulz, A., Wittig, S., 1996. In situ calibration for quantitative infrared thermography. QIRT'96 Eurotherm Seminar No. 50 Stuttgart, Germany, 2-5 September 1996.
-
(1996)
QIRT'96 Eurotherm Seminar No. 50 Stuttgart
-
-
Martiny, M.1
Schiele, R.2
Gritsch, M.3
Schulz, A.4
Wittig, S.5
-
30
-
-
0031375127
-
Influence of a mixing-jet on film cooling
-
Martiny, M., Schulz, A., Wittig, S., Dilzer, M., 1997. Influence of a mixing-jet on film cooling. ASME Paper 97-GT-247.
-
(1997)
ASME Paper 97-GT-247
-
-
Martiny, M.1
Schulz, A.2
Wittig, S.3
Dilzer, M.4
-
31
-
-
0014975054
-
Evaluation of heat transfer for film-cooled turbine components
-
Metzger D.E., Fletcher D.D. Evaluation of heat transfer for film-cooled turbine components. Journal of Aircraft. 8:1971;33-38.
-
(1971)
Journal of Aircraft
, vol.8
, pp. 33-38
-
-
Metzger, D.E.1
Fletcher, D.D.2
-
32
-
-
0025767375
-
Jets in a crossflow: Effects of hole spacing to diameter ratio on the spatial distribution of heat transfer
-
Scherer, V., Wittig, S., Morad, K., Mikhael, N., 1991. Jets in a crossflow: effects of hole spacing to diameter ratio on the spatial distribution of heat transfer. ASME Paper 91-GT-356.
-
(1991)
ASME Paper 91-GT-356
-
-
Scherer, V.1
Wittig, S.2
Morad, K.3
Mikhael, N.4
-
35
-
-
4243193492
-
Heat transfer coefficient enhancement in a gas turbine blade cooling passage due to film cooling holes
-
Paper C 423/040, Proceedings of the Institution of Mechanical Engineers
-
Shen, J.R., Ireland, P.T., Wang, Z., Jones, T.V., 1991. Heat transfer coefficient enhancement in a gas turbine blade cooling passage due to film cooling holes. In: Turbomachinery: Latest Developments in a Changing Scene, Paper C 423/040, Proceedings of the Institution of Mechanical Engineers.
-
(1991)
In: Turbomachinery: Latest Developments in a Changing Scene
-
-
Shen, J.R.1
Ireland, P.T.2
Wang, Z.3
Jones, T.V.4
-
36
-
-
0024302148
-
The use of foreign gas to simulate the effects of density ratios in film cooling
-
Teekaram A.J.H., Forth C.J.P., Jones T.V. The use of foreign gas to simulate the effects of density ratios in film cooling. ASME Journal of Turbomachinery. 111:1989;57-61.
-
(1989)
ASME Journal of Turbomachinery
, vol.111
, pp. 57-61
-
-
Teekaram, A.J.H.1
Forth, C.J.P.2
Jones, T.V.3
-
39
-
-
17344391578
-
Transonic film-cooling investigations: effects of hole shapes and orientations
-
Wittig, S., Schulz, A., Gritsch, M., Thole, K.A., 1996. Transonic film-cooling investigations: effects of hole shapes and orientations. ASME Paper 96-GT-222.
-
(1996)
ASME Paper 96-GT-222
-
-
Wittig, S.1
Schulz, A.2
Gritsch, M.3
Thole, K.A.4
|