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1
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2
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3
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0016061470
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Goldstein, R. J, Eckert, E. R. G., and Burggraf, F., 1974, "Effects of Hole Geometry and Density on Three-Dimensional Film Cooling," Int. J. Heat Mass Transfer, 17, pp. 595-607.
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4
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84912121123
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Lopez-Pena, F.1
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5
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84923917377
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"Flowfield Measurements for Film Cooling Holes With Expanded Exits"
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Birmingham, UK, Paper 96-GT-174
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Thole, K., Gritsch, M., Schulz, A., and Wittig, S., 1996, "Flowfield Measurements for Film Cooling Holes With Expanded Exits," IGTI Turbo Expo, Birmingham, UK, Paper 96-GT-174.
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(1996)
IGTI Turbo Expo
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Thole, K.1
Gritsch, M.2
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6
-
-
84973636061
-
"Anti-Kidney Pair of Vortices in Shaped Holes and Their Influence on Film Cooling Effectiveness"
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Orlando, Paper 97-GT-45
-
Haven, B. A., Yamagata, D. K., Kurosaka, M., Yamawaki, S., and Maya, T., 1997, "Anti-Kidney Pair of Vortices in Shaped Holes and Their Influence on Film Cooling Effectiveness," IGTI Turbo Expo, Orlando, Paper 97-GT-45.
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(1997)
IGTI Turbo Expo
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Haven, B.A.1
Yamagata, D.K.2
Kurosaka, M.3
Yamawaki, S.4
Maya, T.5
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7
-
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0030449706
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"The Aerodynamic Mixing Effect of Discrete Cooling Jets With Mainstream Flow on a Highly Loaded Turbine Blade"
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Wilfert, G., and Fottner, L., 1996, "The Aerodynamic Mixing Effect of Discrete Cooling Jets With Mainstream Flow on a Highly Loaded Turbine Blade," ASME J. Turbomach., 118, pp. 468-478,
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, vol.118
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Wilfert, G.1
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8
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84955165179
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"Systematic Experimental and Numerical Investigations on the Aerothermodynamics of a Film Cooled Turbine Cascade With Variation of the Cooling Hole Shape, Part 1, Experimental Approach"
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Munich, Paper 2000-GT-295
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Ganzert, W., Hildebrandt, T., and Fottner, L., 2000, "Systematic Experimental and Numerical Investigations on the Aerothermodynamics of a Film Cooled Turbine Cascade With Variation of the Cooling Hole Shape, Part 1, Experimental Approach," IGTI Turbo Expo, Munich, Paper 2000-GT-295.
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(2000)
IGTI Turbo Expo
-
-
Ganzert, W.1
Hildebrandt, T.2
Fottner, L.3
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9
-
-
0008027743
-
"Prediction of Effects of Mass Transfer Cooling on the Blade Row Efficiency of Turbine Airfoils"
-
AIAA Aerospace Sciences Meeting, San Diego, Jan. 17-19, AIAA Paper 72-11
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Hartsel, J. E., 1972, "Prediction of Effects of Mass Transfer Cooling on the Blade Row Efficiency of Turbine Airfoils," AIAA Aerospace Sciences Meeting, San Diego, Jan. 17-19, AIAA Paper 72-11.
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(1972)
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Hartsel, J.E.1
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10
-
-
84973130491
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"Efficiency Measurements of an Annular Nozzle Guide Vane Cascade With Different Film Cooling Geometries"
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Stockholm, Paper 98-GT-538
-
Day, C. R. B., Oldfield, M. L. G., Lock, G. D., and Dancer, S. N., 1998, "Efficiency Measurements of an Annular Nozzle Guide Vane Cascade With Different Film Cooling Geometries," IGTI Turbo Expo, Stockholm, Paper 98-GT-538.
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(1998)
IGTI Turbo Expo
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-
Day, C.R.B.1
Oldfield, M.L.G.2
Lock, G.D.3
Dancer, S.N.4
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11
-
-
18844369368
-
"Adiabatic Wall Effectiveness Measurements of Film-Cooling Holes With Expanded Exits"
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Orlando, Paper 97-GT-164
-
Gritsch, M., Schulz, A., and Wittig, S., 1997, "Adiabatic Wall Effectiveness Measurements of Film-Cooling Holes With Expanded Exits," IGTI Conference, Orlando, Paper 97-GT-164.
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(1997)
IGTI Conference
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Gritsch, M.1
Schulz, A.2
Wittig, S.3
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12
-
-
18844451571
-
"Film Cooling Effectiveness and Heat Transfer Coefficient Distributions Around Diffusion Shaped Holes"
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Indianapolis, Paper 99-GT-34
-
Yu, Y., Yen, C.-H., Shih, T. I.-P., Chyu, M. K., and Gogineni, S., 1999, "Film Cooling Effectiveness and Heat Transfer Coefficient Distributions Around Diffusion Shaped Holes," IGTI Conference, Indianapolis, Paper 99-GT-34.
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(1999)
IGTI Conference
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Yu, Y.1
Yen, C.-H.2
Shih, T.I.-P.3
Chyu, M.K.4
Gogineni, S.5
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13
-
-
18844451969
-
"Effect of Partial Coating Blockage on Film Cooling Effectiveness"
-
Munich, Paper 2000-GT-244
-
Bunker, R. S., 2000, "Effect of Partial Coating Blockage on Film Cooling Effectiveness," IGTI Conference, Munich, Paper 2000-GT-244.
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(2000)
IGTI Conference
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Bunker, R.S.1
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14
-
-
84905755890
-
"Film Cooling Effectiveness Downstream of Compound and Fan-Shaped Holes"
-
New Orleans, Paper 2001-GT-0131
-
Yuen, C. H. N., Martinez-Botas, R. F., and Whitelaw, J. H., 2001, "Film Cooling Effectiveness Downstream of Compound and Fan-Shaped Holes," IGTI Turbo Expo, New Orleans, Paper 2001-GT-0131.
-
(2001)
IGTI Turbo Expo
-
-
Yuen, C.H.N.1
Martinez-Botas, R.F.2
Whitelaw, J.H.3
-
15
-
-
0034952040
-
"The Variation of Heat Transfer Coefficient, Adiabatic Effectiveness, and Aerodynamic Loss With Film Cooling Hole Shape"
-
Sargison, J. E., Guo, S. M., Oldfield, M. L. G., and Rawlinson, A. J., 2001, "The Variation of Heat Transfer Coefficient, Adiabatic Effectiveness, and Aerodynamic Loss With Film Cooling Hole Shape," Ann. N.Y. Acad. Sci., 934, pp. 361-368.
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Sargison, J.E.1
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Rawlinson, A.J.4
-
16
-
-
84924389890
-
"Film Cooling With Compound Angle Holes: Adiabatic Effectiveness"
-
The Hague, Netherlands, Paper 94-GT-312
-
Schmidt, D. L., Sen, B., and Bogard, D. G., 1994, "Film Cooling With Compound Angle Holes: Adiabatic Effectiveness," IGTI Turbo Expo, The Hague, Netherlands, Paper 94-GT-312.
-
(1994)
IGTI Turbo Expo
-
-
Schmidt, D.L.1
Sen, B.2
Bogard, D.G.3
-
17
-
-
0034963737
-
"Film Cooling Performance on Curved Walls With Compound Angle Hole Configuration"
-
Chen, P. H., Hung, M. S., and Ding, P. P., 2001, "Film Cooling Performance on Curved Walls With Compound Angle Hole Configuration," Ann. N.Y. Acad. Sci., 934, pp. 353-360.
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Ann. N.Y. Acad. Sci.
, vol.934
, pp. 353-360
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-
Chen, P.H.1
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Ding, P.P.3
-
18
-
-
84928501123
-
"Experimental Study of Showerhead Cooling on a Cylinder Comparing Several Configurations Using Cylindrical and Shaped Holes"
-
Indianapolis, Paper 99-GT-123
-
Reiss, H., and Boeles, A., 1999, "Experimental Study of Showerhead Cooling on a Cylinder Comparing Several Configurations Using Cylindrical and Shaped Holes," IGTI Turbo Expo, Indianapolis, Paper 99-GT-123.
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(1999)
IGTI Turbo Expo
-
-
Reiss, H.1
Boeles, A.2
-
19
-
-
0037000690
-
"Assessment of Various Film Cooling Configurations Including Shaped and Compound Angle Holes Based on Large Scale Experiments"
-
Amsterdam, Paper GT2002-30176
-
Dittmar, J., Schulz, A., and Wittig, S., 2002, "Assessment of Various Film Cooling Configurations Including Shaped and Compound Angle Holes Based on Large Scale Experiments," IGTI Turbo Expo, Amsterdam, Paper GT2002-30176.
-
(2002)
IGTI Turbo Expo
-
-
Dittmar, J.1
Schulz, A.2
Wittig, S.3
-
20
-
-
0036991651
-
"Film Cooling on a Modern HP Turbine Blade Part IV: Compound Angle Shaped Holes"
-
Amsterdam, Paper GT2002-30521
-
McGrath, E. L., Leylek, J. H., and Buck, F. A., 2002, "Film Cooling on a Modern HP Turbine Blade Part IV: Compound Angle Shaped Holes," IGTI Turbo Expo, Amsterdam, Paper GT2002-30521.
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(2002)
IGTI Turbo Expo
-
-
McGrath, E.L.1
Leylek, J.H.2
Buck, F.A.3
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21
-
-
0036994399
-
"Film Cooling on a Modern HP Turbine Blade Part III: Axial Shaped Holes"
-
Amsterdam, Paper GT2002-30522
-
Ferguson, J. D., Leylek, J. H., and Buck, F. A., 2002, "Film Cooling on a Modern HP Turbine Blade Part III: Axial Shaped Holes," IGTI Turbo Expo, Amsterdam, Paper GT2002-30522.
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(2002)
IGTI Turbo Expo
-
-
Ferguson, J.D.1
Leylek, J.H.2
Buck, F.A.3
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22
-
-
85077335033
-
"An Experimental Study of Film Cooling From Diffused Trapezoidal Shaped Holes"
-
AIAA/ASME 4th Joint Thermophysics and Heat Transfer Conference, Boston
-
Makki, Y. H., and Jakubowski, G. S., 1986, "An Experimental Study of Film Cooling From Diffused Trapezoidal Shaped Holes," AIAA/ASME 4th Joint Thermophysics and Heat Transfer Conference, Boston.
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(1986)
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Makki, Y.H.1
Jakubowski, G.S.2
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23
-
-
18844377461
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"Heat Transfer Coefficients Measurements of Film-Cooling Holes With Expanded Exits"
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Stockholm, Paper 98-GT-28
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Gritsch, M., Schulz, A., and Wittig, S., 1998, "Heat Transfer Coefficients Measurements of Film-Cooling Holes With Expanded Exits," IGTI Conference, Stockholm, Paper 98-GT-28.
-
(1998)
IGTI Conference
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Gritsch, M.1
Schulz, A.2
Wittig, S.3
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24
-
-
84924348383
-
"Film Cooling With Compound Angle Holes: Heat Transfer"
-
The Hague, Netherlands, Paper 94-GT-311
-
Sen, B., Schmidt, D. L., and Bogard, D. G., 1994, "Film Cooling With Compound Angle Holes: Heat Transfer," IGTI Turbo Expo, The Hague, Netherlands, Paper 94-GT-311.
-
(1994)
IGTI Turbo Expo
-
-
Sen, B.1
Schmidt, D.L.2
Bogard, D.G.3
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25
-
-
0030835581
-
"Heat Transfer and Film Cooling Effectiveness in a Linear Airfoil Cascade"
-
Abuaf, N., Bunker, R., and Lee, C. P., 1997, "Heat Transfer and Film Cooling Effectiveness in a Linear Airfoil Cascade," ASME J. Turbomach., 119, pp. 302-309.
-
(1997)
ASME J. Turbomach.
, vol.119
, pp. 302-309
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-
Abuaf, N.1
Bunker, R.2
Lee, C.P.3
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26
-
-
0034069823
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"Effect of Internal Coolant Crossflow Orientation on the Discharge Coefficient of Shaped Film Cooling Holes"
-
Gritsch, M., Saumweber, C., Schulz, A., Wittig, S., and Sharp, E., 2000, "Effect of Internal Coolant Crossflow Orientation on the Discharge Coefficient of Shaped Film Cooling Holes," ASME J. Turbomach., 122 , pp. 146-152.
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(2000)
ASME J. Turbomach.
, vol.122
, pp. 146-152
-
-
Gritsch, M.1
Saumweber, C.2
Schulz, A.3
Wittig, S.4
Sharp, E.5
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27
-
-
0035483802
-
"Film Cooling Discharge Coefficient Measurements in a Turbulated Passage With Internal Cross Flow"
-
Bunker, R. S., and Bailey, J. C., 2001, "Film Cooling Discharge Coefficient Measurements in a Turbulated Passage With Internal Cross Flow," ASME J. Turbomach., 123, pp. 774-780.
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(2001)
ASME J. Turbomach.
, vol.123
, pp. 774-780
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-
Bunker, R.S.1
Bailey, J.C.2
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28
-
-
0034964073
-
"Effects of Entrance Cross-Flow Directions to Film Cooling Holes"
-
Saumweber, C., Schulz, A., Wittig, S., and Gritsch, M., 2001, "Effects of Entrance Cross-Flow Directions to Film Cooling Holes," Ann. N.Y. Acad. Sci., 934, pp. 401-408.
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(2001)
Ann. N.Y. Acad. Sci.
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-
Saumweber, C.1
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Wittig, S.3
Gritsch, M.4
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29
-
-
84973160976
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"Entrance Effects on Diffused Film Cooling Holes"
-
Stockholm, Paper 98-GT-402
-
Kohli, A., and Thole, K. A., 1998, "Entrance Effects on Diffused Film Cooling Holes," IGTI Turbo Expo, Stockholm, Paper 98-GT-402.
-
(1998)
IGTI Turbo Expo
-
-
Kohli, A.1
Thole, K.A.2
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30
-
-
0036998221
-
"Free-Stream Turbulence Effects on Film Cooling With Shaped Holes"
-
Amsterdam, Paper GT2002-30170
-
Saumweber, C., Schulz, A., and Wittig, S., 2002, "Free-Stream Turbulence Effects on Film Cooling With Shaped Holes," IGTI Turbo Expo, Amsterdam, Paper GT2002-30170.
-
(2002)
IGTI Turbo Expo
-
-
Saumweber, C.1
Schulz, A.2
Wittig, S.3
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31
-
-
0034952581
-
"Contribution of Heat Transfer to Turbine Blades and Vanes for High Temperature Industrial Gas Turbines: Part 1, Film Cooling"
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Takeishi, K. I., and Aoki, S., 2001, "Contribution of Heat Transfer to Turbine Blades and Vanes for High Temperature Industrial Gas Turbines: Part 1, Film Cooling," Ann. N.Y. Acad. Sci., 934, pp. 305-312.
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-
Takeishi, K.I.1
Aoki, S.2
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32
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84955165858
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"Novel Blade Cooling Engineering Solution"
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Munich, Paper 2000-GT-242
-
Moser, S., Ivanisin, M., Woisetschlaeger, J., and Jericha, H., 2000' "Novel Blade Cooling Engineering Solution," IGTI Turbo Expo, Munich, Paper 2000-GT-242.
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(2000)
IGTI Turbo Expo
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-
Moser, S.1
Ivanisin, M.2
Woisetschlaeger, J.3
Jericha, H.4
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33
-
-
84905728361
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"A Converging Slot-Hole Film Cooling Geometry Part 1: Low-Speed Flat Plate Heat Transfer and Loss"
-
New Orleans, Paper 2001-GT-0126
-
Sargison, J. E., Guo, S. M., Oldfield, M. L. G., Lock, G. D., and Rawlinson, A. J., 2001, "A Converging Slot-Hole Film Cooling Geometry Part 1: Low-Speed Flat Plate Heat Transfer and Loss," IGTI Turbo Expo, New Orleans, Paper 2001-GT-0126.
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(2001)
IGTI Turbo Expo
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-
Sargison, J.E.1
Guo, S.M.2
Oldfield, M.L.G.3
Lock, G.D.4
Rawlinson, A.J.5
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34
-
-
84905728362
-
"A Converging Slot-Hole Film Cooling Geometry Part 2: Transonic Nozzle Guide Vane Heat Transfer and Loss"
-
New Orleans, Paper 2001-GT-0127
-
Sargison, J. F., Guo, S. M., Oldfield, M. L. G., Lock, G. D., and Rawlinson, A. J., 2001, "A Converging Slot-Hole Film Cooling Geometry Part 2: Transonic Nozzle Guide Vane Heat Transfer and Loss," IGTI Turbo Expo, New Orleans, Paper 2001-GT-0127.
-
(2001)
IGTI Turbo Expo
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-
Sargison, J.F.1
Guo, S.M.2
Oldfield, M.L.G.3
Lock, G.D.4
Rawlinson, A.J.5
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35
-
-
18844365695
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"Method for Improving the Cooling Effectiveness of a Gaseous Coolant Stream Which Flows Through a Substrate, and Related Articles of Manufacture"
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Fric, T. F., and Campbell, R. P, 2002, "Method for Improving the Cooling Effectiveness of a Gaseous Coolant Stream Which Flows Through a Substrate, and Related Articles of Manufacture," US Patent No. 6,383,602.
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(2002)
US Patent No. 6,383,602
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-
Fric, T.F.1
Campbell, R.P.2
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36
-
-
0036998196
-
"Film Cooling Effectiveness Due to Discrete Holes Within a Transverse Surface Slot"
-
Amsterdam, Paper GT2002-30178
-
Bunker, R. S., 2002, "Film Cooling Effectiveness Due to Discrete Holes Within a Transverse Surface Slot," IGTI Turbo Expo, Amsterdam, Paper GT2002-30178.
-
(2002)
IGTI Turbo Expo
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-
Bunker, R.S.1
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37
-
-
84905734720
-
"Film Cooling From a Single Row of Cylindrical Angled Holes With Triangular Tabs Having Different Orientations"
-
New Orleans, Paper 2001-GT-0124
-
Nasir, H., Acharya, S., and Ekkad, S., 2001, "Film Cooling From a Single Row of Cylindrical Angled Holes With Triangular Tabs Having Different Orientations," IGTI Turbo Expo, New Orleans, Paper 2001-GT-0124.
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(2001)
IGTI Turbo Expo
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-
Nasir, H.1
Acharya, S.2
Ekkad, S.3
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38
-
-
84928501087
-
"Effects of Hole Shape on Film Cooling With Large Angle Injection"
-
Indianapolis, Indiana, Paper 99-GT-165
-
Kohli, A., and Bogard, D. G., 1999, "Effects of Hole Shape on Film Cooling With Large Angle Injection," IGTI Turbo Expo, Indianapolis, Indiana, Paper 99-GT-165.
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(1999)
IGTI Turbo Expo
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-
Kohli, A.1
Bogard, D.G.2
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39
-
-
84928471491
-
"Transonic Aerodynamic Losses Due to Turbine Airfoil Suction Surface Film Cooling"
-
Indianapolis, Paper 99-GT-260
-
Jackson, D. J., Lee, K. L., Ligrani, P. M., Johnson, P. D., and Soechting, F. O., 1999, "Transonic Aerodynamic Losses Due to Turbine Airfoil Suction Surface Film Cooling," IGTI Turbo Expo, Indianapolis, Paper 99-GT-260.
-
(1999)
IGTI Turbo Expo
-
-
Jackson, D.J.1
Lee, K.L.2
Ligrani, P.M.3
Johnson, P.D.4
Soechting, F.O.5
-
40
-
-
84955073153
-
"Systematic Experimental and Numerical Investigations on the Aerothermodynamics of a Film Cooled Turbine Cascade With Variation of the Cooling Hole Shape, Part 2, Numerical Approach"
-
Munich, Paper 2000-GT-298
-
Hildebrandt, T., Ganzert, W., and Fottner, L., 2000, "Systematic Experimental and Numerical Investigations on the Aerothermodynamics of a Film Cooled Turbine Cascade With Variation of the Cooling Hole Shape, Part 2, Numerical Approach," IGTI Turbo Expo, Munich, Paper 2000-GT-298.
-
(2000)
IGTI Turbo Expo
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-
Hildebrandt, T.1
Ganzert, W.2
Fottner, L.3
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41
-
-
0034959350
-
"Experimental Investigation of Film Cooling Flow Induced by Shaped Holes"
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Barthet, S., and Bario, F., 2001, "Experimental Investigation of Film Cooling Flow Induced by Shaped Holes," Ann. N.Y. Acad. Sci., 34, pp. 313-320.
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(2001)
Ann. N.Y. Acad. Sci.
, vol.34
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Barthet, S.1
Bario, F.2
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42
-
-
0347596448
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"Interaction of Film Cooling Rows: Effects of Hole Geometry and Row Spacing on the Cooling Performance Downstream of the Second Row of Holes"
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Atlanta, Paper GT2003-38195
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Saumweber, C., and Schulz, A., 2003, "Interaction of Film Cooling Rows: Effects of Hole Geometry and Row Spacing on the Cooling Performance Downstream of the Second Row of Holes," IGTI Turbo Expo, Atlanta, Paper GT2003-38195.
-
(2003)
IGTI Turbo Expo
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-
Saumweber, C.1
Schulz, A.2
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43
-
-
0346327095
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"Conjugate Heat Transfer Analysis for Film Cooling Configurations With Different Hole Geometries"
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Atlanta, Paper GT2003-38369
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Bohn, D., Ren, J., and Kusterer, K., 2003, "Conjugate Heat Transfer Analysis for Film Cooling Configurations With Different Hole Geometries," IGTI Turbo Expo, Atlanta, Paper GT2003-38369.
-
(2003)
IGTI Turbo Expo
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-
Bohn, D.1
Ren, J.2
Kusterer, K.3
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