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Volumn 3 B, Issue , 2002, Pages 845-853

Pressure-side bleed film cooling: Part II - Unsteady framework for experimental and computational results

Author keywords

[No Author keywords available]

Indexed keywords

HIGH BLOWING RATIO; HOT COOLANT FLOW; LOW BLOWING RATIO; MACH NUMBER; PRESSURE-SIDE BLEED FILM COOLING;

EID: 0036991423     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1115/GT2002-30472     Document Type: Conference Paper
Times cited : (59)

References (6)
  • 1
    • 0002021897 scopus 로고
    • Calculation of steady and unsteady flows in a film-cooling arrangement using a two-layer algebraic stress model
    • Jansson, L. S., Davidson, L., and Olsson, E., 1994, "Calculation of Steady and Unsteady Flows in a Film-Cooling Arrangement using a Two-Layer Algebraic Stress Model," Numerical Heat Transfer, Part A, 26, pp. 237-258.
    • (1994) Numerical Heat Transfer, Part A , vol.26 , pp. 237-258
    • Jansson, L.S.1    Davidson, L.2    Olsson, E.3
  • 2
    • 0030131308 scopus 로고
    • Numerical prediction of periodic vortex shedding in subsonic and transonic turbine cascade flows
    • Mensink, C., 1995, "Numerical Prediction of Periodic Vortex Shedding in Subsonic and Transonic Turbine Cascade Flows," International Journal for Numerical Methods in Fluids, 22, pp. 881-897.
    • (1995) International Journal for Numerical Methods in Fluids , vol.22 , pp. 881-897
    • Mensink, C.1
  • 3
    • 0025418242 scopus 로고
    • The influence of boundary layer state on vortex shedding from flat plates and turbine cascades
    • Sieverding, C. H. and Heinemann, H., 1990, "The Influence of Boundary Layer State on Vortex Shedding from Flat Plates and Turbine Cascades," ASME Journal of Turbomachinery, 112, pp. 181-187.
    • (1990) ASME Journal of Turbomachinery , vol.112 , pp. 181-187
    • Sieverding, C.H.1    Heinemann, H.2
  • 4
    • 0032704704 scopus 로고    scopus 로고
    • Simulation of vortex shedding in a turbine stage
    • Sondak, D. L. and Dorney, D. J., 1999, "Simulation of Vortex Shedding in a Turbine Stage," ASME Journal of Turbomachinery, 121, pp. 428-435.
    • (1999) ASME Journal of Turbomachinery , vol.121 , pp. 428-435
    • Sondak, D.L.1    Dorney, D.J.2
  • 5
    • 0031404629 scopus 로고    scopus 로고
    • The effects of vortex shedding on the unsteady pressure distribution around the trailing edge of a turbine blade
    • Cicatelli, G. and Sieverding, C. H., 1997, "The Effects of Vortex Shedding on the Unsteady Pressure Distribution Around the Trailing Edge of a Turbine Blade," ASME Journal of Turbomachinery, 119, pp. 810-819.
    • (1997) ASME Journal of Turbomachinery , vol.119 , pp. 810-819
    • Cicatelli, G.1    Sieverding, C.H.2
  • 6
    • 85080663831 scopus 로고    scopus 로고
    • Trailing edge film cooling under realistic engine conditions: A 3-D computational study of flow unsteadiness
    • Undergraduate Honors Thesis, Mechanical Engineering Department, Clemson University, Clemson, SC
    • Sommers, A. D., 2001, "Trailing Edge Film Cooling under Realistic Engine Conditions: A 3-D Computational Study of Flow Unsteadiness," Undergraduate Honors Thesis, Mechanical Engineering Department, Clemson University, Clemson, SC.
    • (2001)
    • Sommers, A.D.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.