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1
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0005966635
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Heat Transfer Measurements in Square Ducts With Transverse Ribs
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presented at the, Aug
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Baughn, J. W., and Yan, X., 1992, “Heat Transfer Measurements in Square Ducts With Transverse Ribs,” presented at the National Heat Transfer Conference, Aug.
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(1992)
National Heat Transfer Conference
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Baughn, J.W.1
Yan, X.2
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2
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84877447116
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An Investigation of Aircraft Heaters XXVII: The Distribution of Heat Transfer Rate in the Entrance Region of a Circular Tube
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Washington, DC
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Boelter, L. M. K., Young, G., and Iversen, H. W., 1948, “An Investigation of Aircraft Heaters XXVII: The Distribution of Heat Transfer Rate in the Entrance Region of a Circular Tube,” NACA TN1451, Washington, DC.
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NACA TN1451
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Boelter, L.M.K.1
Young, G.2
Iversen, H.W.3
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3
-
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4043059628
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ASME Paper No. 88-GT-155
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Byerley, A. R., Ireland, P. T., Jones, T. V., and Ashton, S. A., 1988, “Detailed Heat Transfer Measurements Near and Within the Entrance of a Film Cooling Hole,” ASME Paper No. 88-GT-155.
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(1988)
Detailed Heat Transfer Measurements near and within the Entrance of a Film Cooling Hole
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Byerley, A.R.1
Ireland, P.T.2
Jones, T.V.3
Ashton, S.A.4
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4
-
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2942660606
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ASME Paper No. 92-GT-241
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Byerley, A. R., Jones, T. V., and Ireland, P. T., 1992, “Internal Cooling Passage Heat Transfer Near the Entrance to a Film Cooling Hole: Experimental and Computational Results,” ASME Paper No. 92-GT-241.
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(1992)
Internal Cooling Passage Heat Transfer near the Entrance to a Film Cooling Hole: Experimental and Computational Results
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Byerley, A.R.1
Jones, T.V.2
Ireland, P.T.3
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5
-
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0004181379
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Heat Transfer Near the Entrance to a Film Cooling Hole in a Gas Turbine Blade
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University of Oxford, United Kingdom
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Byerley, A. R., 1989, “Heat Transfer Near the Entrance to a Film Cooling Hole in a Gas Turbine Blade,” D. Phil Thesis, Department of Engineering Science, University of Oxford, United Kingdom.
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(1989)
D. Phil Thesis, Department of Engineering Science
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Byerley, A.R.1
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6
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0342911115
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A Study of Flow and Heat Transfer in Gas Turbine Blade Cooling Passages
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University of Oxford, United Kingdom
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Dunne, S. T., 1982, “A Study of Flow and Heat Transfer in Gas Turbine Blade Cooling Passages,” D. Phil Thesis, Department of Engineering Science, University of Oxford, United Kingdom.
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(1982)
D. Phil Thesis, Department of Engineering Science
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Dunne, S.T.1
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7
-
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0024173746
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Compressible Flow Losses in Branched Ducts
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Haidar, N. I. A., and Dixon, S. L., 1988, “Compressible Flow Losses in Branched Ducts,” ASME HTD-Vol. 104, No. 2, pp. 17-23.
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(1988)
ASME HTD
, vol.104
, Issue.2
, pp. 17-23
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Haidar, N.I.A.1
Dixon, S.L.2
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8
-
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0345608196
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The Measurement of Local Heat Transfer Coefficients in Blade Cooling Geometries
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presented at the
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Ireland, P. T., and Jones, T. V., 1985, “The Measurement of Local Heat Transfer Coefficients in Blade Cooling Geometries,” presented at the AGARD Conference on Heat Transfer and Cooling in Gas Turbines, CP 390, Paper 28.
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(1985)
AGARD Conference on Heat Transfer and Cooling in Gas Turbines, CP 390
, pp. 28
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Ireland, P.T.1
Jones, T.V.2
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9
-
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0003690710
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Internal Cooling of Turbine Blades
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University of Oxford, United Kingdom
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Ireland, P. T., 1987, “Internal Cooling of Turbine Blades,” D. Phil Thesis, Department of Engineering Science, University of Oxford, United Kingdom.
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(1987)
D. Phil Thesis, Department of Engineering Science
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Ireland, P.T.1
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11
-
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0043061622
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Mathematical Models for a Fluid Flow Arising in Turbine Blade Cooling Passages
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University of Oxford, United Kingdom
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Morland, L. C., 1989, “Mathematical Models for a Fluid Flow Arising in Turbine Blade Cooling Passages,” D. Phil Thesis, University of Oxford, United Kingdom.
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(1989)
D. Phil Thesis
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Morland, L.C.1
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12
-
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4243193492
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Heat Transfer Coefficient Enhancement in a Gas Turbine Blade Cooling Passage Due to Film Cooling Holes
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London
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Shen, J.-R., Ireland, P. T., Wang, Z., and Jones, T. V., 1991, “Heat Transfer Coefficient Enhancement in a Gas Turbine Blade Cooling Passage Due to Film Cooling Holes,” Proceedings of the Institution of Mechanical Engineers, Turbomachinery, London, pp. 219-226.
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(1991)
Proceedings of the Institution of Mechanical Engineers, Turbomachinery
, pp. 219-226
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Shen, J.-R.1
Ireland, P.T.2
Wang, Z.3
Jones, T.V.4
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13
-
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84924352092
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Heat Transfer Enhancement Within a Turbine Blade Cooling Passage Using Ribs and Combinations of Ribs With Film Cooling Holes
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ASME Paper No. 94-GT-232; accepted for publication in the
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Shen, J.-R., Ireland, P. T., Wang, Z., and Jones, T. V., 1994, “Heat Transfer Enhancement Within a Turbine Blade Cooling Passage Using Ribs and Combinations of Ribs With Film Cooling Holes,” ASME Paper No. 94-GT-232; accepted for publication in the ASME Journal of Turbomachinery.
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(1994)
ASME Journal of Turbomachinery
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Shen, J.-R.1
Ireland, P.T.2
Wang, Z.3
Jones, T.V.4
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15
-
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0003769182
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The Application of Thermochromatic Liquid Crystals to Detailed Turbine Cooling Measurements
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University of Oxford, United Kingdom
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Wang, Z., 1991, “The Application of Thermochromatic Liquid Crystals to Detailed Turbine Cooling Measurements,” D. Phil Thesis, Department of Engineering Science, University of Oxford, United Kingdom.
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(1991)
D. Phil Thesis, Department of Engineering Science
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Wang, Z.1
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16
-
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0029106034
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An Advanced Method of Processing Liquid Crystal Video Signals From Transient Heat Transfer Experiments
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Wang, Z., Ireland, P. T., and Jones, T. V., 1995, “An Advanced Method of Processing Liquid Crystal Video Signals From Transient Heat Transfer Experiments,” ASME Journal of Turbomachinery, Vol. 117, pp. 184-189.
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(1995)
ASME Journal of Turbomachinery
, vol.117
, pp. 184-189
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Wang, Z.1
Ireland, P.T.2
Jones, T.V.3
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17
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0026980724
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The Effect of Reynolds Number on the Heat Transfer Distribution From a Flat Plate to an Impinging Jet
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Yan, X., Baughan, J. W., and Mesbah, M., 1992, “The Effect of Reynolds Number on the Heat Transfer Distribution From a Flat Plate to an Impinging Jet,” ASME HTD-Vol. 226, pp. 1-8.
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(1992)
ASME HTD
, vol.226
, pp. 1-8
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Yan, X.1
Baughan, J.W.2
Mesbah, M.3
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