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Volumn 118, Issue 1, 1996, Pages 109-120

Computation and simulation of wake-generated unsteady pressure and boundary layers in cascades: Part 2-simulation of unsteady boundary layer flow physics

Author keywords

[No Author keywords available]

Indexed keywords

BOUNDARY LAYER MODELS; CASCADES; WAKES;

EID: 0029671712     PISSN: 0889504X     EISSN: 15288900     Source Type: Journal    
DOI: 10.1115/1.2836589     Document Type: Article
Times cited : (7)

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


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.