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1
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0025414343
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Unsteady Transition in an Axial-Flow Turbine: Part 1-Measurements on the Turbine Rotor; Part 2-Cascade Measurements and Modeling
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Addison, J. S., and Hodson, H. P., 1990, “Unsteady Transition in an Axial-Flow Turbine: Part 1-Measurements on the Turbine Rotor; Part 2-Cascade Measurements and Modeling,” ASME Journal of Turbomachinery, Vol. 112, pp. 206-221.
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(1990)
ASME Journal of Turbomachinery
, vol.112
, pp. 206-221
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Addison, J.S.1
Hodson, H.P.2
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2
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0024641116
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Unsteady Interaction Effects on a Transitional Turbine Blade Boundary Layer
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Ashworth, D. A., Lagraff, J. E., and Schultz, D. L„ 1989, “Unsteady Interaction Effects on a Transitional Turbine Blade Boundary Layer,” ASME Journal of Turbomachinery, Vol. Ill, pp. 162-168.
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(1989)
ASME Journal of Turbomachinery
, vol.3
, pp. 162-168
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Ashworth, D.A.1
Lagraff, J.E.2
Schultz, D.L.3
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3
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0025009655
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Compressor Blade Boundary Layers, Part 1: Test Facility and Measurements With No Incident Wakes; Part 2: Measurements With Incident Wakes
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Dong, Y., and Cumpsty, N. A., 1990, “Compressor Blade Boundary Layers, Part 1: Test Facility and Measurements With No Incident Wakes; Part 2: Measurements With Incident Wakes,” ASME Journal of Turbomachinery, Vol. 112, pp. 222-240.
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(1990)
ASME Journal of Turbomachinery
, vol.112
, pp. 222-240
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Dong, Y.1
Cumpsty, N.A.2
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4
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0026190225
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The Effect of Incident Wake Conditions on the Mean Heat Transfer of an Airfoil
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Dullenkopf, K., Schulz, A., and Wittig, S., 1991, “The Effect of Incident Wake Conditions on the Mean Heat Transfer of an Airfoil,” ASME Journal of Turbomachinery, Vol. 113, pp. 412-418.
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(1991)
ASME Journal of Turbomachinery
, vol.113
, pp. 412-418
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Dullenkopf, K.1
Schulz, A.2
Wittig, S.3
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5
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0029671701
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Computation and Simulation of Wake-Generated Unsteady Pressure and Boundary Layers in Cascades: Part 1 - Description of Approach and Validation
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this issue
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Fan, S., and Lakshminarayana, B., 1996, “Computation and Simulation of Wake-Generated Unsteady Pressure and Boundary Layers in Cascades: Part 1 - Description of Approach and Validation,” ASME Journal of Turbomachinery, Vol. 118, this issue, pp. 96-108.
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(1996)
ASME Journal of Turbomachinery
, vol.118
, pp. 96-108
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Fan, S.1
Lakshminarayana, B.2
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6
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0021974080
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Boundary-Layer Transition and Separation Near the Leading Edge of a High-Speed Turbine Blade
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Hodson, H. P., 1985, “Boundary-Layer Transition and Separation Near the Leading Edge of a High-Speed Turbine Blade,” ASME Journal of Engineering for Gas Turbines and Power, Vol. 107, pp. 127-134.
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(1985)
ASME Journal of Engineering for Gas Turbines and Power
, vol.107
, pp. 127-134
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-
Hodson, H.P.1
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7
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85007924016
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Modeling Unsteady Transition and Its Effects on Profile Loss
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Hodson, H. P., 1990, “Modeling Unsteady Transition and Its Effects on Profile Loss,” ASME Journal of Turbomachinery, Vol. 112, pp. 691-701.
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(1990)
ASME Journal of Turbomachinery
, vol.112
, pp. 691-701
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Hodson, H.P.1
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8
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0026762040
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On the Prediction of Unsteady Forces on Gas Turbine Blades. Part 1: Description of the Approach; Part 2: Analysis of the Results
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Korakianitis, T., 1992, “On the Prediction of Unsteady Forces on Gas Turbine Blades. Part 1: Description of the Approach; Part 2: Analysis of the Results,” ASME Journal of Turbomachinery, Vol. 114, pp. 114-131.
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(1992)
Asmejournal of Turbomachinery
, vol.114
, pp. 114-131
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Korakianitis, T.1
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10
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0026238106
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Experiments on Transitional Boundary Layers With Wake-Induced Unsteadiness
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Liu, X., and Rodi, W., 1991, “Experiments on Transitional Boundary Layers With Wake-Induced Unsteadiness,” Journal of Fluid Mechanics, Vol. 231, pp. 229-256.
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(1991)
Journal of Fluid Mechanics
, vol.231
, pp. 229-256
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-
Liu, X.1
Rodi, W.2
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11
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85024526673
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The Role of Laminar-Turbulent Transition in Gas Turbine Engines
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Mayle, R. E., 1991, “The Role of Laminar-Turbulent Transition in Gas Turbine Engines,” ASME Journal of Turbomachinery, Vol. 113, pp. 509-537.
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(1991)
ASME Journal of Turbomachinery
, vol.113
, pp. 509-537
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Mayle, R.E.1
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12
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0027681760
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Unsteady Boundary-Layer Transition in Flow Periodically Disturbed by Wakes
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Orth, U., 1993, “Unsteady Boundary-Layer Transition in Flow Periodically Disturbed by Wakes,” ASME Journal of Turbomachinery, Vol. 115, pp. 707-713.
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(1993)
ASME Journal of Turbomachinery
, vol.115
, pp. 707-713
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Orth, U.1
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13
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84997391827
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Investigation of the LaminarTurbulent Transition of Boundary Layers Disturbed by Wakes
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Pfeil, H., Herbst, R., and Schroder, T., 1983, “Investigation of the LaminarTurbulent Transition of Boundary Layers Disturbed by Wakes,” ASME Journal of Engineering for Power, Vol. 105, pp. 131-137.
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(1983)
ASME Journal of Engineering for Power
, vol.105
, pp. 131-137
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Pfeil, H.1
Herbst, R.2
Schroder, T.3
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14
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84976003277
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Characteristics of the Wake Behind a Cascade of Airfoils
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Raj, R., and Lakshminarayana, B., 1973, “Characteristics of the Wake Behind a Cascade of Airfoils,” Journal of Fluid Mechanics, Vol. 61, Part 4, pp. 707-730.
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(1973)
Journal of Fluid Mechanics
, vol.61
, pp. 707-730
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Raj, R.1
Lakshminarayana, B.2
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15
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84992485664
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Three-Dimensional Separated Flow Field in the End Wall Region of an Annular Compressor Cascade in the Presence of Rotor-Stator Interaction, Part 1: Quasi-Steady Flow Field and Comparison With Steady-State Data; Part 2: Unsteady Flow and Pressure Field
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Schulz, H. D., Gallus, H. E., and Lakshminarayana, B., 1990, “Three-Dimensional Separated Flow Field in the End Wall Region of an Annular Compressor Cascade in the Presence of Rotor-Stator Interaction, Part 1: Quasi-Steady Flow Field and Comparison With Steady-State Data; Part 2: Unsteady Flow and Pressure Field,” ASME Journal of Turbomachinery, Vol. 112, pp. 669-690.
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(1990)
Asmejournal of Turbomachinery
, vol.112
, pp. 669-690
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Schulz, H.D.1
Gallus, H.2
Lakshminarayana, E.B.3
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16
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4243701325
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NASA CR 4405
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Verdon, J. M., Barnett, M., Hall, K. C., and Ayer, T. C., 1991, “Development of Unsteady Aerodynamic Analyses for Turbomachinery Aeroelastic and Aeroa-coustic Applications,” NASA CR 4405.
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(1991)
Development of Unsteady Aerodynamic Analyses for Turbomachinery Aeroelastic and Aeroa-Coustic Applications
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Verdon, J.M.1
Barnett, M.2
Hall, K.3
Ayer, C.T.C.4
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17
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0023324603
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LaserDoppler Studies of the Wake-Effected Flow Field in a Turbine Cascade
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Wittig, S., Dullenkopf, K., Schulz, A., and Hestermann, R., 1987, “LaserDoppler Studies of the Wake-Effected Flow Field in a Turbine Cascade,” ASME Journal of Turbomachinery, Vol. 109, pp. 170-176.
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(1987)
ASME Journal of Turbomachinery
, vol.109
, pp. 170-176
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Wittig, S.1
Dullenkopf, K.2
Schulz, A.3
Hestermann, R.4
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