Heat transfer on a film-cooled rotating blade

International Journal of Heat and Fluid Flow

Volumn 21, Issue 2, 2000, Pages 134-145

  Garg, V K ^a  

^a NASA GLENN RESEARCH CENTER   (United States)

Author keywords

Adiabatic effectiveness; Film cooling; Heat transfer; Rotating turbine blade

Indexed keywords

COOLING; HEAT TRANSFER COEFFICIENTS; MATHEMATICAL MODELS; NAVIER STOKES EQUATIONS; THERMODYNAMICS; TURBOMACHINE BLADES;

ADIABATIC EFFECTIVENESS; FILM-COOLED TURBINE BLADES;

HEAT TRANSFER;

FILM; HEAT TRANSFER; ROTATING BLADE ROW; TURBINE;

EID: 0034021128     PISSN: 0142727X     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0142-727X(99)00072-7     Document Type: Article

References (24)

1. Ameri, A.A., Steinthorsson, E., Rigby, D.L., 1997. Effect of squealer tip on rotor heat transfer and efficiency, ASME Paper 97-GT-128.
2. Boyle, R.J., Giel, P., 1992. Three-dimensional Navier-Stokes heat transfer predictions for turbine blade rows, AIAA Paper 92-3068.
3. Chima, R.V., 1996. A k-ω turbulence model for quasi-three-dimensional turbomachinery flows, AIAA Paper 96-0248.
4. Garg V.K. Adiabatic effectiveness and heat transfer coefficient on a film-cooled rotating blade. Numer. Heat Transfer, Part A. 32:1997;811-830.
5. Garg V.K. Heat transfer on a film-cooled rotating blade using a two-equation turbulence model. Int. J. Rotating Machinery. 4(3):1998;201-216.
6. Garg V.K. Heat transfer on a film-cooled rotating blade using different turbulence models. Int. J. Heat Mass Transfer. 42(5):1999;789-802.
7. Garg, V.K., 1999b, Heat transfer on a film-cooled rotating blade, ASME Paper 99-GT-44.
8. Garg V.K., Abhari R.S. Comparison of predicted and experimental Nusselt number for a film-cooled rotating blade. Int. J. Heat & Fluid Flow. 18:1997;452-460.
9. Garg V.K., Ameri A.A. Comparison of two-equation turbulence models for prediction of heat transfer on film-cooled turbine blades. Numer. Heat Transfer, Part A. 32:1997;347-371.
10. Garg, V.K., Gaugler, R.E., 1993. Heat transfer in film-cooled turbine blades, ASME Paper 93-GT-81.
11. Garg, V.K., Gaugler, R.E., 1994. Prediction of film cooling on gas turbine airfoils, ASME Paper 94-GT-16.
12. Garg V.K., Gaugler R.E. Leading edge film cooling effects on turbine blade heat transfer. Numer. Heat Transfer, Part A. 30:1996;165-187.
13. Garg V.K., Gaugler R.E. Effect of coolant temperature and mass flow on film cooling of turbine blades. Int. J. Heat Mass Transfer. 40:1997;435-445.
14. Garg V.K., Gaugler R.E. Effect of velocity and temperature distribution at the hole exit on film cooling of turbine blades. J. Turbomachinery. 119:1997;343-351.
15. Garg V.K., Rigby D.L. Heat transfer on a film-cooled blade-effect of hole physics. Int. J. Heat & Fluid Flow. 20:1999;10-25.
16. Goldstein, R.J., 1971. Film Cooling, Advances in Heat Transfer, vol. 7, Academic Press, New York, pp. 321-379.
17. Jameson, A., Schmidt, W., Turkel, E., 1981. Numerical solutions of the Euler equations by finite volume methods using Runge-Kutta time-stepping schemes, AIAA Paper 81-1259.
18. Menter, F.R., 1993. Zonal two-equation k-ω turbulence models for aerodynamic flows, AIAA Paper 93-2906.
19. TM/az3000 - User's Guide and Reference Manual, White Plains, NY.
20. Rigby, D.L., 1996. Method of weakest descent for automatic block merging, in: Proceedings of the 15th International Conference on Numerical Methods in Fluid Dynamics, Monterey, CA.
21. Rigby, D.L., Steinthorsson, E., Coirier, W.J., 1997. Automatic block merging using the method of weakest descent, AIAA Paper 97-0197.
22. Steinthorsson, E., Ameri, A.A., Rigby, D.L., 1997. TRAF3D.MB-A multi-block flow solver for turbomachinery flows, AIAA Paper 97-0996.
23. Steinthorsson, E., Liou, M.S., Povinelli, L.A., 1993. Development of an explicit multiblock/multigrid flow solver for viscous flows in complex geometries, AIAA Paper 93-2380.
24. Wilcox D.C. Simulation of transition with a two-equation turbulence model. AIAA J. 32:1994;247-255.