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1
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0028428047
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Film-cooling from holes with compound angle orientations: Part 1- results downstream of two staggered rows of holes with 3d spanwise spacing
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Ligrani, P.M., Wigle, J.M., Ciriello, S., and Jackson, S.W., 1994a, "Film-Cooling From Holes with Compound Angle Orientations: Part 1- Results Downstream of Two Staggered Rows of Holes with 3d Spanwise Spacing," ASME Journal of Heat Transfer, 116, pp. 341-352.
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(1994)
ASME Journal of Heat Transfer
, vol.116
, pp. 341-352
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Ligrani, P.M.1
Wigle, J.M.2
Ciriello, S.3
Jackson, S.W.4
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2
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0028424911
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Film- cooling from holes with compound angle orientations: Part 2- results downstream of a single row of holes with 6d spanwise spacing
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Ligrani, P.M., Wigle, J.M., and Jackson, S.W., 1994b, "Film- Cooling From Holes with Compound Angle Orientations: Part 2- Results Downstream of a Single Row of Holes with 6d Spanwise Spacing," ASME Journal of Heat Transfer, 116, pp. 353-362.
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(1994)
ASME Journal of Heat Transfer
, vol.116
, pp. 353-362
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Ligrani, P.M.1
Wigle, J.M.2
Jackson, S.W.3
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3
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-
0030446933
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Film cooling with compound angle holes: Heat transfer
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Sen, B., Schmidt, D.L., and Bogard, D.G., 1996, "Film Cooling with Compound Angle Holes: Heat Transfer," ASME Journal of Turbomachinery, 118, pp. 801-807.
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(1996)
ASME Journal of Turbomachinery
, vol.118
, pp. 801-807
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-
Sen, B.1
Schmidt, D.L.2
Bogard, D.G.3
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4
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4243193913
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Film cooling with compound angle holes: Adiabatic effectiveness
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Schmidt, D.L., Sen, B., and Bogard, D.G., 1996, "Film Cooling with Compound Angle Holes: Adiabatic Effectiveness," ASME Journal of Turbomachinery, 118, pp. 807-813.
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(1996)
ASME Journal of Turbomachinery
, vol.118
, pp. 807-813
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Schmidt, D.L.1
Sen, B.2
Bogard, D.G.3
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5
-
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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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Ekkad, S. V., Zapata, D., and Han, J. C., 1997a, "Heat Transfer Coefficients Over a Flat Surface with Air and CO2 Injection Through Compound Angle Holes Using a Transient Liquid Crystal Image Method," ASME Journal of Turbomachinery, 119, pp. 580-586.
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(1997)
ASME Journal of Turbomachinery
, vol.119
, pp. 580-586
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Ekkad, S.V.1
Zapata, D.2
Han, J.C.3
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6
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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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Ekkad, S. V., Zapata, D., and Han, J.C., 1997b, "Film Effectiveness Over a Flat Surface with Air and CO2 Injection Through Compound Angle Holes Using a Transient Liquid Crystal Image Method," ASME Journal of Turbomachinery, 119, pp. 587-593.
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(1997)
ASME Journal of Turbomachinery
, vol.119
, pp. 587-593
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-
Ekkad, S.V.1
Zapata, D.2
Han, J.C.3
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7
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0031340610
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Heat transfer coefficient measurements of film cooling holes with expanded slots
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Gritsch, M., Schulz, A., and Wittig, S., 1998a, "Heat Transfer Coefficient Measurements of Film Cooling Holes with Expanded Slots," ASME Paper 98-GT-28.
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(1998)
ASME Paper 98-GT-28
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Gritsch, M.1
Schulz, A.2
Wittig, S.3
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8
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0032124987
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Adiabatic wall effectiveness measurements of film cooling holes with expanded exits
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Gritsch, M., Schulz, A., and Wittig, S., 1998b, "Adiabatic Wall Effectiveness Measurements of Film Cooling Holes with Expanded Exits," ASME Journal of Turbomachinery, 120, pp. 549-556.
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(1998)
ASME Journal of Turbomachinery
, vol.120
, pp. 549-556
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Gritsch, M.1
Schulz, A.2
Wittig, S.3
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9
-
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0016543556
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The distortion of a jet by tabs
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Bradbury, L. J. S., and Khadem, A. H., 1975, "The Distortion of a Jet by Tabs," Journal of Fluid Mechanics, 70, pp. 801-813.
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(1975)
Journal of Fluid Mechanics
, vol.70
, pp. 801-813
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Bradbury, L.J.S.1
Khadem, A.H.2
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10
-
-
0030927052
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The effect of vortex generators on a jet in a cross-flow
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Zaman, K. B. M. Q., and Foss, J. K., 1997, "The Effect of Vortex Generators on a Jet in a Cross-Flow," Physics of Fluids, 9, pp. 106-114.
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(1997)
Physics of Fluids
, vol.9
, pp. 106-114
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Zaman, K.B.M.Q.1
Foss, J.K.2
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11
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85088198414
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Reduction of jet penetration in a cross-flow by using tabs
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AIAA Paper 98-3276, Cleveland, July 1998
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Zaman, K. B. M. Q., 1998, "Reduction of Jet Penetration in a Cross-Flow by Using Tabs," AIAA Paper 98-3276, 34th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, Cleveland, July 1998.
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(1998)
th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit
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Zaman, K.B.M.Q.1
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12
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84994515010
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Film cooling on a flat surface with a single row of cylindrical angled holes: Effect of discrete tabs
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presented at the, Orlando, Florida, November 2000
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Ekkad, S. V., Nasir, H., and Acharya, S., 2000, "Film Cooling on a Flat Surface with a Single Row of Cylindrical Angled Holes: Effect of Discrete Tabs," presented at the 2000 IMECE conference, Orlando, Florida, November 2000.
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(2000)
2000 IMECE Conference
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Ekkad, S.V.1
Nasir, H.2
Acharya, S.3
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13
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0034123047
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A detailed analysis of film cooling physics: Part III - Streamwise injection with shaped holes
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Hyams, D. G., and Leylek, J. H., 2000, "A Detailed Analysis of Film Cooling Physics: Part III - Streamwise Injection with Shaped Holes," ASME Journal of Turbomachinery, 122, pp. 122-132.
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(2000)
ASME Journal of Turbomachinery
, vol.122
, pp. 122-132
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Hyams, D.G.1
Leylek, J.H.2
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14
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0002477246
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Describing uncertainties in single sample experiments
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Kline, S.J. and McClintock, F.A., 1953, "Describing Uncertainties in Single Sample Experiments," Mechanical Engineering, 75, pp. 3-8.
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(1953)
Mechanical Engineering
, vol.75
, pp. 3-8
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Kline, S.J.1
McClintock, F.A.2
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15
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0017552828
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Film cooling with large density differences between the mainstream and the secondary fluid measured by the heat-mass transfer analogy
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Pedersen, D. R., Eckert, E. R. G., and Goldstein, R. J., 1977, "Film Cooling with Large Density Differences Between the Mainstream and the Secondary Fluid Measured by the Heat-Mass Transfer Analogy," ASME Journal of Heat Transfer, 99, pp. 620-627.
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(1977)
ASME Journal of Heat Transfer
, vol.99
, pp. 620-627
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Pedersen, D.R.1
Eckert, E.R.G.2
Goldstein, R.J.3
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16
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0016058529
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Heat transfer and film cooling following injection through inclined circular holes
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Eriksen, V. L., and Goldstein, R. J., 1974, "Heat Transfer and Film Cooling Following Injection Through Inclined Circular Holes," ASME Journal of Heat Transfer, 96, pp. 239-245.
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(1974)
ASME Journal of Heat Transfer
, vol.96
, pp. 239-245
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Eriksen, V.L.1
Goldstein, R.J.2
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17
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0021898059
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Effect of cooling films on the heat transfer coefficient on a flat plate with zero mainstream pressure gradient
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Hay, N., Lampard, D., and Saluja, C. L., 1985, "Effect of Cooling Films on the Heat Transfer Coefficient on a Flat Plate with Zero Mainstream Pressure Gradient," ASME Journal of Engineering for Gas Turbines and Power, 107, pp. 105-110.
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(1985)
ASME Journal of Engineering for Gas Turbines and Power
, vol.107
, pp. 105-110
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Hay, N.1
Lampard, D.2
Saluja, C.L.3
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18
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0020206771
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Mass transfer in the neighborhood of jets entering a crossflow
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Goldstein, R. J., and Taylor, J. R., 1982, "Mass Transfer in the Neighborhood of Jets Entering a Crossflow," ASME Journal of Heat Transfer, 104, pp. 715-721.
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(1982)
ASME Journal of Heat Transfer
, vol.104
, pp. 715-721
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Goldstein, R.J.1
Taylor, J.R.2
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19
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0032125401
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Discharge coefficient measurements of film cooling holes with expanded exits
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Gritsch, M., Schulz, A., and Wittig, S., 1998c, "Discharge Coefficient Measurements of Film Cooling Holes with Expanded Exits," ASME Journal of Turbomachinery, 120, pp. 557-563.
-
(1998)
ASME Journal of Turbomachinery
, vol.120
, pp. 557-563
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Gritsch, M.1
Schulz, A.2
Wittig, S.3
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