Leading edge film-cooling effects on turbine blade heat transfer

Numerical Heat Transfer; Part A: Applications

Volumn 30, Issue 2, 1996, Pages 165-187

  Garg, Vijay K ^a   Gaugler, Raymond E ^a  

^a NASA GLENN RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

COOLANTS; COOLING; HEAT TRANSFER COEFFICIENTS; MASS TRANSFER; NAVIER STOKES EQUATIONS; SURFACES; TEMPERATURE; THERMAL EFFECTS; THREE DIMENSIONAL; TURBINES; TURBOMACHINE BLADES;

ADIABATIC EFFECTIVENESS; DISCRETE JET FILM COOLING; FILM COOLED TURBINE VANE; INLET TEMPERATURE; PRESSURE SURFACE; SHOWER HEAD HOLES; SPANWISE PITCH; SUCTION SURFACE;

HEAT TRANSFER;

EID: 0030576484     PISSN: 10407782     EISSN: 15210634     Source Type: Journal    
DOI: 10.1080/10407789608913834     Document Type: Article

References (30)

1. R. J. Goldstein, Film Cooling, in T. F. Irvine, Jr. And J. P. Hartnett (eds.), Advances in Heat Transfer, vol. 7, pp. 321-379, Academic, New York, 1971.
2. V. K. Garg and R. E. Gaugler, Heat Transfer in Film-Cooled Turbine Blades, ASME Paper 93-GT-81,1993.
3. V. K. Garg and R. E. Gaugler, Prediction of Film Cooling on Gas Turbine Airfoils, ASME Paper 94-GT-16, 1994.
4. J. P. Bons, C. D. MacArthur, and R. B. Rivir, The Effect of High Freestream Turbulence on Film Cooling Effectiveness, ASME Paper 94-GT-51, 1994.
5. J. S. Lee, S. T. Ro, and H. J. Seo, Mass Transfer Effects of Free-Stream Turbulence and Horseshoe Vortex Formed at the Upstream Edge of Film Cooling Jets About a Cylindrical Surface, ASME Paper 94-GT-18, 1994.
6. M. Y. Jabbari, K. C. Marston, E. R. G. Eckert, and R. J. Goldstein, Film Cooling of the Gas Turbine Endwall by Discrete-Hole Injection, ASME Paper 94-GT-67, 1994.
7. B. Sen, D. L. Schmidt, and D. G. Bogard, Film Cooling with Compound Angle Holes: Heat Transfer, ASME Paper 94-GT-311, 1994.
8. D. L. Schmidt, B. Sen, and D. G. Bogard, Film Cooling with Compound Angle Holes: Adiabatic Effectiveness, ASME Paper 94-GT-312, 1994.
9. Y. W. Kim, W. Abdel-Messeh, J. P. Downs, F. O. Soechting, G. D. Steuber, and S. Tanrikut, A Summary of the Cooled Turbine Blade Tip Heat Transfer and Film Effectiveness Investigations Performed by Dr. D. E. Metzger, ASME Paper 94-GT-167, 1994.
10. N. Hay, D. Lampard, and A. Khaldi, The Coefficient of Discharge of 30° Inclined Film Cooling Holes with Rounded Entries or Exits, ASME Paper 94-GT-180, 1994.
11. J. M. Fougeres and R. Heider, Three-Dimensional Navier-Stokes Prediction of Heat Transfer with Film Cooling, ASME Paper 94-GT-14, 1994.
12. B. Weigand and S. P. Harasgama, Computations of a Film Cooled Turbine Rotor Blade with Non-Uniform Inlet Temperature Distribution Using a Three-Dimensional Viscous Procedure, ASME Paper 94-GT-15, 1994.
13. W. N. Dawes, The Extension of a Solution-Adaptive Three-Dimensional Navier-Stokes Solver Toward Geometries of Arbitrary Complexity, J. Turbomach., vol. 115, pp. 283-295, 1993.
14. E. J. Hall, D. A. Topp, and R. A. Delaney, Aerodynamic/Heat Transfer Analysis of Discrete Site Film-Cooled Turbine Airfoils, AIAA Paper 94-3070, 1994.
15. R. J. Boyle and P. Giel, Three-Dimensional Navier-Stokes Heat Transfer Predictions for Turbine Blade Rows, AIAA Paper 92-3068, 1992.
16. A. Arnone, M.-S. Liou, and L. A. Povinelli, Multigrid Calculation of Three-Dimensional Viscous Cascade Flows, AIAA Paper 91-3238, 1991.
17. L. D. Hylton, V. Nirmalan, B. K. Sultanian, and R. M. Kaufman, The Effects of Leading Edge and Downstream Film Cooling on Turbine Vane Heat Transfer, NASA CR 182133, 1988.
18. J. S. Liu, R. Utz, and R. Bozzola, Aerodynamic Design and Analysis of a Gas Producer Turbine Stator with Film Cooling Injection, AIAA Paper 94-2928, 1994.
19. J. H. Leylek and R. D. Zerkle, Discrete-Jet Film Cooling: A Comparison of Computational Results with Experiments, J. Turbomach., vol, 116, pp. 358-368, 1994.
20. H. Schlichting, Boundary Layer Theory, 7th ed., p. 328, McGraw-Hill, New York, 1979.
21. B. S. Baldwin and H. Lomax, Thin-Layer Approximation and Algebraic Model for Separated Turbulent Flows, AIAA Paper 78-257, 1978.
22. A. A. Ameri and A. Arnone, Transition Modeling Effects on Turbine Rotor Blade Heat Transfer Predictions, ASME Paper 94-GT-22, 1994.
23. A. A. Ameri and A. Amone, Prediction of Turbine Blade Passage Heat Transfer Using a Zero and a Two-Equation Turbulence Model, ASME Paper 94-GT-122, 1994.
24. R. J. Boyle and A. A. Ameri, Grid Orthogonality Effects on Predicted Turbine Midspan Heat Transfer and Performance, ASME Paper 94-GT-123, 1994.
25. R. A. Graziani, M. F. Blair, J. R. Taylor, and R. E. Mayle, An Experimental Study of Endwall and Airfoil Surface Heat Transfer in a Large Scale Turbine Blade Cascade, J. Eng. Power, vol. 102, pp. 257-267, 1980.
26. A. A. Amer, B. A. Jubran, and M. A. Hamdan, Comparison of Different Two-Equation Turbulence Models for Prediction of Film Cooling from Two Rows of Holes, Numer. Heat Transfer Pan A, vol. 21, pp. 143-162, 1992.
27. S.-W. Kim and T. J. Benson, Calculation of a Circular Jet in Cross Flow with a Multiple-Time-Scale Turbulence Model, Int. J. Heat Mass Transfer, vol. 35, pp. 2357-2365, 1992.
28. V. K. Garg and R. E. Gaugler, Effect of Velocity and Temperature Distribution at the Hole Exit on Film Cooling of Turbine Blades, ASME Paper 95-GT-2, 1995.
29. A. Jameson, W. Schmidt, and E. Türkei, Numerical Solutions of the Euler Equations by Finite Volume Methods Using Runge-Kutta Time-Stepping Schemes, AIAA Paper 81-1259, 1981.
30. W. Haas, W. Rodi, and B. Schönung, The Influence of Density Difference Between Hot and Coolant Gas on Film Cooling by a Row of Holes: Predictions and Experiments, ASME Paper 91-GT-255, 1991.