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1
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0025464121
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An experimenlal study of turbine vane heat transfer with leading edge and downstream film cooling
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Nirmalan, V., and Hylton, L., 1990, &An Experimenlal Study of Turbine Vane Heat Transfer With Leading Edge and Downstream Film Cooling," ASME J. Turbomach., 112, pp. 477-487.
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(1990)
ASME J. Turbomach.
, vol.112
, pp. 477-487
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Nirmalan, V.1
Hylton, L.2
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2
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0343231820
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ASME Paper No. 95-GT-3
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Abuaf, N., Bunker, R., and Lee, C. P., 1995, "Heat Transfer and Film Cooling Effectiveness in a Linear Airfoil Cascade," ASME Paper No. 95-GT-3.
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(1995)
Heat Transfer and Film Cooling Effectiveness in a Linear Airfoil Cascade
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Abuaf, N.1
Bunker, R.2
Lee, C.P.3
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3
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0025462977
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An experimental convective heat transfer investigation around a film-cooled gas turbine blade
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Camci, C., and Arts, T., 1990, "An Experimental Convective Heat Transfer Investigation Around a Film-Cooled Gas Turbine Blade," ASME J. Turbomach., 112, pp. 497-503.
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(1990)
ASME J. Turbomach.
, vol.112
, pp. 497-503
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Camci, C.1
Arts, T.2
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4
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21144460887
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Film cooling on a gas turbine rotor blade
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Takeishi, K., Aoki, A., Sato, T., and Tsukagoshi, K., 1992, "Film Cooling on a Gas Turbine Rotor Blade," ASME J. Turbomach., 114, pp. 828-834.
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(1992)
ASME J. Turbomach.
, vol.114
, pp. 828-834
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Takeishi, K.1
Aoki, A.2
Sato, T.3
Tsukagoshi, K.4
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5
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0017995015
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Film cooling of a gas turbine blade
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Ito, S., Goldstein, R. J., and Eckert, E. R. G., 1978, "Film Cooling of a Gas Turbine Blade," ASME J. Eng. Power, 100, pp. 476-481.
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(1978)
ASME J. Eng. Power
, vol.100
, pp. 476-481
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Ito, S.1
Goldstein, R.J.2
Eckert, E.R.G.3
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6
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21144478004
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The influence of density difference between hot and coolant gas on film cooling by a row of holes: Predictions and experiments
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Haas, W., Rodi, W., and Schönung, B., 1992, "The Influence of Density Difference Between Hot and Coolant Gas on Film Cooling by a Row of Holes: Predictions and Experiments," ASME J. Turbomach., 114, pp. 747-755.
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(1992)
ASME J. Turbomach.
, vol.114
, pp. 747-755
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Haas, W.1
Rodi, W.2
Schönung, B.3
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7
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0032194649
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Aspects of vane film cooling with high turbulence: Part I - Heat transfer; part II - Adiabatic effectiveness
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Ames, F. E., 1998, "Aspects of Vane Film Cooling With High Turbulence: Part I - Heat Transfer; Part II - Adiabatic Effectiveness," ASME J. Turbomach., 120, pp. 768-784.
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(1998)
ASME J. Turbomach.
, vol.120
, pp. 768-784
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Ames, F.E.1
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8
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0028274429
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An experimental study of film cooling in a rotating transonic turbine
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Abhari, R. S., and Epstein, A. H., 1994, "An Experimental Study of Film Cooling in a Rotating Transonic Turbine," ASME J. Turbomach., 116, pp. 63-70.
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(1994)
ASME J. Turbomach.
, vol.116
, pp. 63-70
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Abhari, R.S.1
Epstein, A.H.2
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10
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0028038556
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2 film injection: Part II - Effect on film effectiveness and heat transfer distributions
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2 Film Injection: Part II - Effect on Film Effectiveness and Heat Transfer Distributions," ASME J. Turbomach., 116, pp. 730-737.
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(1994)
ASME J. Turbomach.
, vol.116
, pp. 730-737
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Mehendale, A.B.1
Han, J.C.2
Ou, S.3
Lee, C.P.4
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12
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0031190345
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2 injection through compound angle holes using a transient liquid crystal image method
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2 Injection Through Compound Angle Holes Using a Transient Liquid Crystal Image Method." ASME J. Turbomach., 119, No. 3, pp. 580-586.
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(1997)
ASME J. Turbomach.
, vol.119
, Issue.3
, pp. 580-586
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Ekkard, S.V.1
Zapata, D.2
Han, J.C.3
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13
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0031191260
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2 injection through compound angle holes using a transient liquid crystal image method
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2 Injection Through Compound Angle Holes Using a Transient Liquid Crystal Image Method." ASME J. Turbomach., 119, No. 3, pp. 587-593.
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(1997)
ASME J. Turbomach.
, vol.119
, Issue.3
, pp. 587-593
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Ekkard, S.V.1
Zapata, D.2
Han, J.C.3
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14
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0032194349
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Effect of unsteady wake on detailed heat transfer coefficient and film effectiveness distributions for a gas turbine blade
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Du, H., Han, J. C., and Ekkard, S. V., 1998, "Effect of Unsteady Wake on Detailed Heat Transfer Coefficient and Film Effectiveness Distributions for a Gas Turbine Blade," ASME J. Turbomach., 120, pp. 808-817.
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(1998)
ASME J. Turbomach.
, vol.120
, pp. 808-817
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Du, H.1
Han, J.C.2
Ekkard, S.V.3
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15
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0032704069
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Effect of unsteady wake with trailing edge coolant ejection on film cooling performance for a gas turbine blade
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Du, H., Ekkad, S. V., and Han, J., 1999, "Effect of Unsteady Wake With Trailing Edge Coolant Ejection on Film Cooling Performance for a Gas Turbine Blade," ASME J. Turbomach., 121, pp. 448-453.
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(1999)
ASME J. Turbomach.
, vol.121
, pp. 448-453
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Du, H.1
Ekkad, S.V.2
Han, J.3
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16
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0345425774
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Investigation of detailed film cooling effectiveness and heat transfer distributions on a gas turbine airfoil
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Drost, U., and Böles, A., 1999, "Investigation of Detailed Film Cooling Effectiveness and Heat Transfer Distributions on a Gas Turbine Airfoil," ASME J. Turbomach., 121, pp. 233-242.
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(1999)
ASME J. Turbomach.
, vol.121
, pp. 233-242
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Drost, U.1
Böles, A.2
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17
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0031945977
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Fluctuating thermal field in the near-hole region for film cooling flows
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Kohli, A., and Bogard, D. G., 1998, "Fluctuating Thermal Field in the Near-Hole Region for Film Cooling Flows," ASME J. Turbomach., 120, pp. 86-91.
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(1998)
ASME J. Turbomach.
, vol.120
, pp. 86-91
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Kohli, A.1
Bogard, D.G.2
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18
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84928480661
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Film temperature and effectiveness measurements on a cylindrical leading edge film cooling model
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Aug. 23-28, Kyongju, Korea
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Sohm, D. K., Teng, S., and Han, J. C., 1998, "Film Temperature and Effectiveness Measurements on a Cylindrical Leading Edge Film Cooling Model," Heat Transfer 1998, Proc. of 11th IHTC, 6, pp. 571-576, Aug. 23-28, Kyongju, Korea.
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(1998)
Heat Transfer 1998, Proc. of 11th IHTC
, vol.6
, pp. 571-576
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Sohm, D.K.1
Teng, S.2
Han, J.C.3
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