Three-dimensional flow prediction and improvement of holes arrangement of a film-cooled turbine blade using a feature-based jet model

Journal of Turbomachinery

Volumn 129, Issue 2, 2007, Pages 258-268

  Burdet, André ^a   Abhari, Reza S ^a  

^a ETH ZURICH   (Switzerland)

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTATIONAL FLUID DYNAMICS; COOLING; GAS TURBINES; JETS; NAVIER STOKES EQUATIONS; NUSSELT NUMBER; REYNOLDS EQUATION; SECONDARY FLOW; THREE DIMENSIONAL;

ADIABATIC FILM-COOLING; COMPUTATIONAL OVERHEAD; FLOW PREDICTION;

TURBOMACHINE BLADES;

COMPUTATIONAL FLUID DYNAMICS; COOLING; GAS TURBINES; JETS; NAVIER STOKES EQUATIONS; NUSSELT NUMBER; REYNOLDS EQUATION; SECONDARY FLOW; THREE DIMENSIONAL; TURBOMACHINE BLADES;

EID: 34249908333     PISSN: 0889504X     EISSN: None     Source Type: Journal    
DOI: 10.1115/1.2437778     Document Type: Article

References (30)

1. Bergeles, G., Gosman, A. D., and Launder, B. E., 1981, "The Prediction of Three-Dimensional Discrete-Hole Cooling Processes - Part 2," ASME J. Heat Transfer, 103, pp. 141-145.
2. Demuren, A. O., Rodi, W., and Schönung, B., 1986, "Systematic Study of Film Cooling With a Three-Dimensional Calculation Procedure," ASME J. Turbomach., 108(3), pp. 124-130.
3. Lakehal, D., 2002, "Near-Wall Modeling of Turbulent Convective Heat Transport in Film Cooling of Turbine Blades With the Aid of Direct Numerical Simulation Data," ASME J. Turbomach., 124(3), pp. 485-498.
4. Leylek, J. H., and Zerkle, R. D., 1994, "Discrete-Jet Film Cooling: A Comparison of Computational Results With Experiments," ASME J. Turbomach., 116(3), pp. 358-368.
5. Walters, D. K., and Leylek, J. H., 2000, "A Detailed Analysis of Film-Cooling Physics - Part I: Streamwise Injection With Cylindrical Holes," ASME J. Turbomach., 122(1), pp. 102-112.
6. Morton, B. R., and Ibbetson, A., 1996, "Jets Deflected in a Crossflow," Exp. Therm. Fluid Sci., 12, pp. 112-133.
7. Garg, V. K., and Abhari, R. S., 1997, "Comparison of Predicted and Experimental Nusselt Number for a Film-Cooled Rotating Blade," Int. J. Heat Fluid Flow, 18, pp. 452-460.
8. Garg, V. K., and Gaugler, R. E., 1997, "Effect of Velocity and Temperature Distribution at the Hole Exit on Film Cooling of Turbine Blades," ASME J. Turbomach., 119(2), pp. 343-445.
9. Heidmann, J. D., Rigby, D. L., and Ameri, A. A., 2000, "A Three-Dimensional Coupled Internal/External Simulation of a Film-Cooled Turbine Vane," ASME J. Turbomach., 122(2), pp. 348-359.
10. Crawford, M. E., Kays, W. M., and Moffat, R. J., 1976, "Heat Transfer to a Full Coverage Film-Cooled Surface With 30° Slant-Hole Injection," NASA Contractor Report No. CR-2786.
11. Schönung, B., and Rodi, W., 1987, "Predictions of Film Cooling by a Row of Holes With a Two-Dimensional Boundary-Layer Procedure," ASME J. Turbomach., 109(4), pp. 579-587.
12. Kulisa, P., Leboeuf, F., and Perrin, G., 1992, "Computation of a Wall Boundary Layer With Discrete Jet Injections," ASME J. Turbomach., 114(4), pp. 756-764.
13. Tafti, D. K., and Yavuzkurt, S., 1990, "Prediction of Heat Transfer Characteristics for Discrete Hole Film Cooling for Turbine Blade Applications," ASME J. Turbomach., 112(3), pp. 504-511.
14. Abhari, R. S., 1996, "Impact of Rotor-Stator Interaction on Turbine Blade Film Cooling," ASME J. Turbomach., 118(1), pp. 123-133.
15. Forest, A. E., White, A. J., Lai, C. C., Guo, S. M., Oldfield, M. L. J., and Lock, G. D., 2004, "Experimentally Aided Development of a Turbine Heat Transfer Prediction Method," Int. J. Heat Fluid Flow, 25, pp. 606-617.
16. Burdet, A., Abhari, R. S., and Rose, M. G., 2005, "Modeling of Film Cooling - Part II: Model for Use in 3D CFD," ASME Paper No. GT2005-68780.
17. Burdet, A., and Abhari, R. S., 2006, "A Competationally Efficient Film Cooling Jet Model Using die Implicit Immerse Boundary Method," Comput. Fluids, submitted.
18. Bernsdorf, S., Rose, M. G., and Abhari, R. S., 2006, "Modeling of Film Cooling - Part I: Experimental Study of Flow Structure," ASME J. Turbomach., 128(1), pp. 141-149.
19. Moussa, Z. M., Trischka, J. W., and Eskain, S., 1977, "The Near Field in the Mixing of a Round Jet With a Cross Stream," J. Fluid Mech., 80(1), pp. 49-80.
20. Burdet, A., 2005, "A Computationally Efficient Feature-Based Jet Model for Film-Cooling Flows Prediction," Ph.D. thesis No. 16163, ETH-Zürich, Switzerland.
21. Majumdar, S., Iaccarino, G., and Durbin, P., 2001, "RANS Solver With Adaptive Structured Boundary Non-Conforming Grids," CTR Annual Research Briefs, pp. 353-366.
22. Abhari, R. S., and Epstein, A. H., 1994, "An Experimental Study of Film Cooling in a Rotating Transonic Turbine," ASME J. Turbomach., 116(1), pp. 63-70.
23. Schultz, D., Jones, T. V., Oldfield, M. L. G., and Daniels, L. C., 1977, "A New Transcient Cascade Facility for the Measurement of Heat Transfer Rates," High Temperature Problems in Gas Turbine Engines, AGARD Conf. Proc. Vol. 229.
24. Ashworth, D. A., 1987, "Unsteady Aerodynamics and Heat Transfer in a Transonic Turbine Stage," Ph.D. thesis, Osney Lab., St. John's College, University of Oxford, England.
25. Rigby, M. J., Johnson, A. B., and Oldfield, M. L. G., 1990, "Gas Turbine Rotor Blade Film Cooling With and Without Simulated NGV Shock Waves and Wakes," ASME Paper No. 90-GT-78.
26. Ni, R. H., 1981, "A Multiple Grid Scheme for Solving the Euler Equations," AIAA J., 20(11), pp. 1565-1571.
27. Hyams, D. G., and Leylek, J. H., 2000, "A Detailed Analysis of Film Cooling Physics - Part III: Streamwise Injection With Shaped Hole," ASME J. Turbomach., 122(1), pp. 122-132.
28. Garg, V. K., 1999, "Heat Transfer on a Film-Cooled Rotating Blade Using Different Turbulence Model," Int. J. Heat Mass Transfer, 42, pp. 789-802.
29. Medic, G., and Durbin, P., 2002, "Toward Improved Film Cooling Prediction," ASME J. Turbomach., 124(2), pp. 193-199.
30. Sellers, J. P., 1963, "Gaseous Film Cooling With Multiple Injection Stations," AIAA J., 1, pp. 2154-2156.