Heat transfer predictions for two turbine nozzle geometries at high reynolds and mach numbers

Journal of Turbomachinery

Volumn 119, Issue 2, 1997, Pages 270-283

  Boyle, R J ^a   Jackson, R ^b  

^a NASA GLENN RESEARCH CENTER   (United States)

^b DRA   (United Kingdom)

Author keywords

[No Author keywords available]

Indexed keywords

EID: 0031497644     PISSN: 0889504X     EISSN: 15288900     Source Type: Journal    
DOI: 10.1115/1.2841110     Document Type: Article

References (32)

1. Ameri, A. A., and Arnone, A., 1992, “Navier-Stokes Heal Transfer Predictions Using Two-Equation Turbulent Closures,” Paper No. AIAA-92-3067.
2. Ameri, A. A., and Arnone, A., 1994, “Prediction of Turbine Blade Passage Heat Transfer Using a Zero and a Two-Equation Turbulent Model,” ASME Paper No. 94-GT-122.
3. Arnone, A., Liou, M.-S., and Povinelli, L. A., 1992, “Navier-Stokes Solution of Transonic Cascade Flows Using Non-periodic C-Type Grids,” AIAA Journal of Propulsion and Power, Vol. 8, No.2, pp. 410-417.
4. Arts, T., Lambert de Rouvroit, M., and Rutherford, A. W., 1990, “Aero-Thermal Investigation of a Highly Loaded Transonic Linear Turbine Guide Vane Cascade,” von Karman Institute for Fluid Dynamics, Technical Note 174.
5. Arts, T., and Heider, R., 1994, “Aerodynamic and Thermal Performance of a Three Dimensional Annular Transonic Nozzle Guide Vane. Part I: Experimental Investigation,” Paper No. A1AA-94-2929.
6. Baldwin, B. S., and Lomax, H., 1978, “Thin-Layer Approximation and Algebraic Model for Separated Turbulent Flows,” Paper No. AIAA-78-257.
7. Blair, M. F., 1974, “An Experimental Study of Heat Transfer and Film Cooling in Large-Scale Turbine Endwalls,” ASME Journal of Heat Transfer, Vol. 96, pp. 525-529.
8. Blair, M. F., 1994, “An Experimental Study of Heat Transfer in a Large-Scale Turbine Rotor Passage,” ASME Journai of Turbomachinery, Vol. 116, pp. 1-13.
9. Boyle, R. J., and Russell, L. M., 1990, “An Experimental Determination of Stator Endwall Heat Transfer,” ASME Journal of Turbomachinf.ry, Vol. 112, pp. 547-558.
10. Boyle, R. J., and Giel, P.W., 1992, “Three-Dimensional Navier-Stokes Heat Transfer Predictions for Turbine Blade Rows,” Paper No. A1AA-92-3068.
11. Boyle, R. J., and Ameri, A., 1997, “Grid Orthogonality Effects on Predicted Turbine Midspan Heal Transfer and Performance,” ASME Journai. of Turboma-cliinery, Vol. 119, pp. 31-38.
12. Chana, K. S., 1992, “Heat Transfer and Aerodynamics of a High Rim Speed Turbine Nozzle Guide Vane With Profiles End Walls,” ASME Paper No. 92-GT-243.
13. Cebeci, T., and Smith, A. M. O., 1974, Analysis of Turbulent Boundary Layers, Academic Press, New York.
14. Chima, R. V., 1987, “Explicit Multigrid Algorithm for Quasi-Three-Dimensional Flows in Turbomachinery,” AIAA Journal of Propulsion and Power, Vol. 3, No. 5, pp. 397-405.
15. Chima, R. V., and Yokota, J. W., 1988, “Numerical Analysis of Three-Dimensional Viscous Internal Flows,” AIAA Paper No. 88-3522; NASA TM-100878.
16. Chima, R. V., 1990, Private Communication.
17. Chima, R. V., 1991, “Viscous Three-Dimensional Calculations of Transonic Fan Performance,” AGARD Propulsion and Energetics Symposium on Computational Fluid Mechanics for Propulsion, San Antonio, TX, May 27-31.
18. Chima, R. V., Giel, P. W., and Boyle, R. J., 1993, “An Algebraic Turbulence Model for Three-Dimensional Viscous Flows,” AIAA Paper No. 93-0083; NASA TM-105931.
19. Choi, D., and Knight, C. J., 1988, “Computations of 3D Viscous Linear Cascade Flows,” AIAA Journal, Vol. 26, No. 12, pp. 1477-1482.
20. Dunn, M. G., Kim, J., Civinskas, K. C., and Boyle, R. J., 1994, “Time-Averaged Heat Transfer and Pressure Measurements and Comparison With Prediction for a Two-Stage Turbine,” ASME Journal of Turbomachinery, Vol. 116, pp. 14-22.
21. Graziani, R. A., Blair, M. F., Taylor, R. J., and Mayle, R. E., 1980, “An Experimental Study of Endwall and Airfoil Surface Heat Transfer in a Large Scale Turbine Blade Cascade,” ASME Journal of Engineering for Power, Vol. 102, No. 2, pp. 1-11
22. Hah, C., 1989, “Numerical Study of Three-Dimensional Flow and Heat Transfer Near the Endwall of a Turbine Blade Row,” AIAA Paper No. 89-1689.
23. Harasgama, S. P., and Wedlake, E. T., 1991, “Heat Transfer and Aerodynamics of a High Rim Speed Turbine Nozzle Guide Vane Tested in the RAE lsentropic Light Piston Cascade (ILPC),” ASME Journal of Turbomachinery, Vol. 113, No. 4, pp. 384-391.
24. Heider, R. and Arts, T., 1994, “Aerodynamic and Thermal Performance of a Three Dimensional Annular Transonic Nozzle Guide Vane. Part II: Assessment of a 3D Navier-Stokes Solver,” Paper No. ATAA-94-2930.
25. Kays, W. M., and Crawford, M. E., 1980, Convective Heat and Mass Transfer, McGraw-Hill, New York.
26. Kingcombe, R. C., Harasgama, S. P., Leversuch, N. P., and Wedlake, E. T., 1989, “Aerodynamic and Heat Transfer Measurements on Blading for a High Rim-Speed Transonic Turbine,” ASME Paper No. 89-GT-228.
27. Mayle, R. E., 1991, “The Role of Laminar-Turbulent Transition in Gas Turbine Engines,” ASME Journal of Turbomachinery, Vol. 113, pp. 509-537.
28. Smith, M. C., and Kuethe, A. M., 1966, “Effects of Turbulence on Laminar Skin Friction and Heat Transfer,” Physics of Fluids, Vol. 9, pp. 2337-2344.
29. Sorenson, R. L., 1980, “A Computer Program to Generate Two-Dimensional Grids About Airfoils and Other Shapes by the Use of Poisson’s Equation,” NASA TM 81198.
30. Strazisar, A. J., 1994, Private Communication.
31. York, R. E., Hylton, L. D., and Mihelc, M.S., 1984, “Experimental Endwall Heat Transfer and Aerodynamics in a Linear Vane Cascade,” ASME Journal of Engineering for Gas Turbines and Power, Vol. 106, pp. 159-167.
32. Young, C. D, Han, J. C., Huang, Y., and River, R. B., 1992, “Influence of Jet-Grid Turbulence on Flat Plate Turbulent Boundary Layer Flow and Heat Transfer,” ASME Journal of Heat Transfer, Vol. 96, pp. 525-529.