Prediction of relaminarization effects on turbine blade heat transfer

Proceedings of the ASME Turbo Expo

Volumn 3, Issue , 2001, Pages

  Boyle, R J ^a   Giel, P W ^b  

^a NASA GLENN RESEARCH CENTER   (United States)

^b Dynacs Engineering Co   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

HELICOPTER ROTORS; REYNOLDS NUMBER; TURBINES; TURBOMACHINE BLADES; TURBULENCE MODELS;

FAVORABLE PRESSURE GRADIENTS; HIGH REYNOLDS NUMBER; MODERATE REYNOLDS NUMBERS; PRESSURE SIDE; PRESSURE SURFACE; ROTOR COOLING; SURFACE HEAT TRANSFER; TURBINE BLADE;

HEAT TRANSFER;

EID: 84905728030     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1115/2001-GT-0162     Document Type: Conference Paper

References (30)

1. Zhang, L., and Han. J.-C., 1994, "Inuence of Main-stream Turbulence on Heat Transfer Coecients From a Gas Turbine Blade," ASME Journal of Heat Transfer, Vol. 116, pp. 896-902.
2. Brown, A., and Martin, B.W., 1982, "Flow Transition Phenomena and Heat Transfer Over the Pressure Surfaces of Gas Turbine Blades," ASME Journal of Engineering for Power, Vol. 104, pp. 360-367.
3. Nicholson, J.H., Forest, A.E., Oldfleld, M.L.G., and Schultz, D.L., 1984, "Heat Transfer Optimized Turbine Blades-An Experimental Study Using Transient Techniques," ASME Journal of Engineering for Gas Turbines and Power, Vol. 106, pp. 173-181.
4. Cebeci, T., and Smith, A.M.O., 1974, Analysis of Turbulent Boundary Layers, Academic Press, N.Y.
5. Crawford, M.E. and Kays, W.M., 1976, "STAN5 - A Program for Numerical Computation of Two-Dimensional Internal and External Boundary Layer Flows," NASA CR-2742.
6. Kays, W.M. and Cra wford, M.E., 1980, "Convective Heat and Mass Transfer," Second Edition, McGraw-Hill, New York.
7. Mayle, R.E., 1991, "The Role of Laminar-Turbulent Transition in Gas Turbine Engines," ASME Journal of Turbomachinery, Vol. 113, pp. 509-537.
8. Boyle, R.J, and Simon, F.F., 1999, "Mach Number Effects on Turbine Blade Transition Length Prediction," ASME Journal of Turbomachinery, Vol. 121, pp. 694-702.
9. Solomon, W.J., Walker, G.J., and Gostelow, J.P., 1995 "Transition Length Prediction For Flows With Rapidly Changing Pressure Gradients", ASME paper 95-GT-241.
10. Dunham, J., 1972, "Predictions of Boundary Layer Transition on Turbomachinery Blades," AGARD-AG-164.
11. Steelant, J. and Dick, E., 1999 "Prediction of By-Pass Transition By Means of a Turbulence Weighting Factor - Part I: Theory and Validation," ASME paper 99-GT-29.
12. 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.
13. Chima, R.V., and Yokota, J.W., 1990, "Numerical Analysis of Three-Dimensional Viscous Internal Flows," AIAA Journal, Vol. 28, No. 5, pp. 798-806.
14. 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.
15. 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.
16. Chima, R.V., Giel, P.W., and Boyle, R.J., 1993, "An Algebraic Turbulence Model for Three-Dimensional Viscous Flows," AAIA paper 93-0083, (NASA TM-105931).
17. Ameri, A.A. and Arnone, A., 1992 "Navier-Stokes Heat Transfer Predictions Using Two-Equation Turbulence Closures," AIAA paper 92-3067.
18. Chima, R.V., 1996, "Application of the κ ω Turbulence Model to Quasi-Three-Dimensional Turbomachinery Flows," AIAA Journal of Propulsion and Power, Vol. 12, No. 6, pp. 1176-1179.
19. 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.
20. Arts, T., Duboue, J.-M., and Rollin, G., 1998, "Aero-Thermal Performance Measurements and Analysis of a Two-Dimensional High Turning Rotor Blade," ASME Journal of Turbomachinery, Vol. 120, pp. 494-499.
21. Blair, M.F., 1983, "Inuence of Free-Stream Turbulence on Turbulent Boundary Layer Heat Transfer and Mean Profile Development, Part II-Analysis of Results," ASME Journal of Heat Transfer, Vol. 105, pp. 41-47.
22. Arts, T., Lambert de Rouvroit, M., and Rutherford, A.W., 1990, "Aero-Thermal In vestigation of a Highly Loaded Transonic Linear Turbine Guide Vane Cascade," VKI Technical Note 174.
23. Dring, R.P., Blair, M.F., Joslyn, H.D., Power, G.D., and Verdon, J.M., 1986, "The Effects of Inlet Turbulence and Rotor/Stator Interactions on the Aerodynamics and Heat Transfer of a Large-Scale Rotating Turbine Model - I-Final Report," NASA CR 4079.
24. Giel, P.W., Van Fossen, G.J., Boyle, R.J., Thurman, D.R, and Civinskas, K.C, 1999, "Blade Heat Transfer Measurements and Predictions in a Transonic Turbine Cascade," ASME paper 99-GT-125.
25. Giel, P.W., Bunker, R.S., Van Fossen, G.J., and Boyle, R.J., 2000, "Heat Transfer Measurements and Predictions on a Power Generation Gas Turbine Blade," ASME paper 2000-GT-209.
26. Blair, M.F., 1994, "An Experimental Study of Heat Transfer in a Large-Scale Turbine Rotor Passage," ASME Journal of Turbomachinery, Vol. 116, pp. 1-13.
27. 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.
28. VanFossen, G.J., Simoneau, R.J., and Ching, C.Y., 1995, "Inuence of Turbulence Parameters, Reynolds Number, and Body Shape on Stagnation-Region Heat Transfer," ASME Journal of Heat Transfer, Vol. 117, pp. 597-603, also NASA TP 3487, 1994.
29. Dullenkopf, K. and Mayle, R.E.,1994, "The Effects of Incident Turbulence and Moving Wakes on Laminar Heat Transfer in Gas Turbines," ASME Journal of Turbomachinery, Vol. 116, pp. 23-28.
30. Dullenkopf, K. and Mayle, R.E.,1995, "An Account of Free-Stream- Turbulence Length Scale on Laminar Heat Transfer," ASME Journal of Turbomachinery, Vol. 117, pp. 401-406.