Film cooling effectiveness predictions for short holes fed by a narrow plenum

Proceedings of the ASME Turbo Expo

Volumn 3, Issue , 1999, Pages

  Hale, C A ^a   Ramadhyani, S ^a   Plesniak, M W ^a  

^a PURDUE UNIVERSITY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ATMOSPHERIC THERMODYNAMICS; BOUNDARY LAYERS; FORECASTING; GAS TURBINES; HEAT TRANSFER; REYNOLDS NUMBER; TURBULENCE MODELS; TURBULENT FLOW;

BOUNDARY-LAYER SEPARATION; COMMERCIAL SOFTWARE; FILM COOLING EFFECTIVENESS; FILM COOLING HOLE; REYNOLDS STRESS TURBULENCE MODEL;

COOLING;

EID: 84928494159     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1115/99-GT-162     Document Type: Conference Paper

References (52)

1. Andreopoulos, J. 1982, "Measurements in a Jet-Pipe FlowIssuing Perpendicularly Into a Cross Stream," ASME J. FluidsEngineering 104, 493-499.
2. Andreopoulos, J. and Rodi, W. 1984, "Experimental Investigation of Jets in a Crossflow," J. Fluid Mech. 138, 93-127.
3. Arnone, A., Liou, M.S. & Povinelli, L.A., 1991,"Multigrid Calculation of Three-dimensional Viscous CascadeFlows," AMA Paper 91-3238.
4. Bergels, G., Gosman, A.D., and Launder, B.E., 1978, 'The Turbulent Jet in a Cross Stream at Low Injection Rates: A Three-dimensional Numerical Treatment," Numerical Heat Transfer, 1, 217-242.
5. Berhe, M.K. and Patankar S.V., 1996, "A Numerical Study of Discrete-Hole Film Cooling," ASME 96-WA/HT-8.
6. Boyle, R.J., Haas, J.E., and Katsanis, T., 1984,"Comparison Between Measured Turbine Stage Performance and the Predicted Performance Using Quasi-3d Flow and Boundary Layer Analysis," NASA TM-83640.
7. Bons, J.P., MacArthur, C.D., and Rivir, R.B., 1994, "The Effect of High Freestream Turbulence on Film Cooling Effectiveness," 1994, ASME Paper 94-GT-51.
8. Burd, S.W., Kaszeta, R.W., and Simon, TN., 1996, "Measurements in Film Cooling Flows: Hole L/D and Turbulence Intensity Effects," 96-WA/HT-7.
9. Burd, S.W., and Simon, T.W., 1997, "The Influence of Film Cooling Supply Geometry on Film Coolant Exit and Surface Adiabatic Effectiveness," ASME Paper 97-GT-25.
10. Burd, S.W. and Simon, T.W., 1998a, "Measurements of Discharge Coefficients in Film Cooling," ASME Paper, 98-Gt-009.
11. Burd, S.W. and Simon, T.W., 1998b, "Turbulence Spectra and Length Scales Measured in Film Coolant Rows Emerging from Discrete Holes," ASME Paper, 98-GT-190.
12. Crabb, D., Durao, D.F.G., and Whitelaw J.H., 1981, "A Round Jet Normal to a Crossflow,"ASME J. of Fluids Engineering, 103, 142-153.
13. Crawford, MX. and Kays, W.M, 1976, "STAN5-A Program for Numerical Computation of Two Dimensional Internal and External Boundary Layer Rows. NASA CR-2742.
14. Crawford, ME., Kays, W.M., and Moffat, R.J., 1980, "Full-Coverage Film Cooling, Part II Heat Transfer Data and Numerical Simulation," ASME J. of Engineering for Power.
15. Demuren, A.E., Rodi, W., and Schonung, B., 1986, "Systematic Study of Film Cooling with a Three-dimensional Calculation Procedure," ASME J. of Turbomachinery, 108, 124-130.
16. Ferguson, J.D., Walters D.K. and Leylek, J.H., 1998, "Performance of Turbulence Models and Near-Wall Treatments in Discrete Jet Film Cooling Simulations," ASME Paper 98-GT-438.
17. Garg, V.K., and Gaugler, R.E., 1994, "Prediction of Film Cooling on Gas Turbine Airfoils," NASA-TM-I06653.
18. Garg, V.K., and Rigby, D.L., 1998, "Heat Transfer on a Film-Cooled Blade - Effect of Hole Physics," ASME Paper 98-GT-404
19. Gogineni, S.F., Rivir, R.B., Pestian, D.J., and Goss, L.P., 1996, "Ply Measurements of Flat Plate Film Cooling Rows With High Free Stream Turbulence," AIAA 96-0617.
20. Goldstein, R.J., Eckert E.R.G., and Burggraf, F., 1974, "Effects of Hle Geometry and Density on Three-dimensional Film Cooling," Int. J. Heat Mass Transfer, 17, 595-607.
21. Gritsch, M., Schulz, A., and Wittig, S., 1997, "Adiabatic Wall Effectiveness Measurements of Film-Cooling Holes with Expanded Exits," ASME Paper 97-GT-164.
22. Haas, W., Rodi, W., and Schonung, B., 1992, "The Influence of Density Difference Between Hot and Coolant Gas on Film Cooling by a Row of Holes: Predictions and Experiments," ASME J. of Turbomachinery,114, 747-755
23. Hale, C.A., Plesniak, MM., and Ramadhyani, S., 1999, "Film Cooling Effectiveness for Short film Cooling Holes Fed by a Narrow Plenum," submitted to ASME TURBO EXPO 1999.
24. ICatsanis, T. and McNally, W.D., 1977, "Revised FORTRAN Program for Calculating Velocities and Streamlines on the Hub-shroud Midchannel Stream Surface of an Axial-, Radial-, or Mixed-flow Turbomachine or Annular Duct," Vol. I User's manual NASA TN D-8430.
25. Kline, S.J. and McClintock, S.J., 1953, "Describing Uncertainties in Single-sample Experiments," Mechanical Engineering January 1953.
26. Kohli, A., and Bogard, D.C., 1995, "Adiabatic Effectiveness, Thermal Fields, and Velocity Fields for Film cooling with Large Angle Injection," ASME Paper 95-GT-219.
27. Kohli, A., and 'Thole, K.A., 1997, "A CFD Investigation on the Effects of Entrance Crossflow Direction to Film- Cooling Holes," ASME Proceeding of the 32s National Heat Transfer Conference, Vol. 12, pp. 223-232.
28. Kohli, A., and Thole, K.A., 1998, "Entrance Effects on Diffused film Cooling Holes," ASME Paper 98-GT-402.
29. Leylek, J.H. and Zerkle, RD., 1994, "Discrete-Jet Film Cooling: A Comparison of Computational Results With Experiments," ASME J. of Turbomachinery 116, 358-368.
30. Lutum E. and Johnson, B.V., 1998, "Influence of the Hole Length-to-diameter Ratio on Film Cooling with Cylindrical Holes," ASME Paper 98-GT-10.
31. Norton, R.J.G., Forest, A.E., White, A.J., Hensshaw, D.G., Epstein, A.H., Schultz, D.L., and Oldfield, M.L.B., 1990, "'Turbine Cooling System Design-Vol.I-Technical Report," Wright Research and Development Center Report No. WRDC-TR-89-2109, Vol. 1
32. PatanIcar, S.V., Basu, D.K., and Alpay, S.A., 1977, "Prediction of the Three-dimensional Velocity Field of a Deflected Turbulent Jet," ASME J. of Fluids Engineering, Vol. 99, 758-762.
33. Pietrzyk, J.R., Bogard, D.G., and Crawford, M.E., 1989, "Hydrodynamic Measurements of Jets in Crossflow for Gas Turbine Film Cooling Applications," ASME J. of Turbomachinery, 111, 139-145.
34. Pietrzyk, J.R., Bogard, D.G., and Crawford, M.E., 1990, "Effects of Density Ratio on the Hydrodynamics of Film Cooling," ASME J. of Turbomachinery, 112, 437-443.
35. Saxlcar, S. and Bose, T.K., 1995, "Comparison of Different Turbulence Models for Prediction of Slot-film Cooling: Flow and Temperature Field," Numerical Heat Transfer, Pan B 28, 217-238.
36. Sathyamurthy, P.S. and Patanlcar, S.V., 1990, "Prediction of Film Cooling with Lateral Injection, "Heat Transfer in Turbulent Flow: Proceedings of AIAA/ASME Thermophysics and Heat Transfer Conference, ASME, New York, 66-70.
37. Schmidt, F.L., Sen, B., and Bogard, D.G., 1994, "Film Cooling with Compound Angle Holes: Adiabatic Effectiveness," ASME Paper 94-GT-312.
38. Sen, B., Schmidt, D.L., & Bogard, D.G., 1994, "Film Cooling with Compound Angle Holes: Heat Transfer," ASME Paper 94-GT-311.
39. Shonung, B. and Rodi, W., 1987, "Prediction of Film Cooling By a Row of Holes with a Two-dimensional Boundary-Layer Procedure", ASME J. of Turbomachinety, 109, 579-587.
40. Simon, F.F. and Ciancone M.L., 1985, "Flow Visualization Study of the Effect of Injection Hole Geometry on an Inclined Jet in Crossflow," NASA TM 86936.
41. Simoneau, R.J. and Simon, F.F., 1993, "Progress Towards Understanding and Predicting Heat Transfer in the Turbine Gas Path," International Journal of Heat and Fluid Flow, 14, No. 2., 106.
42. Sinha, A.K., Bogard, D.G., and Crawford, M.E., 1991, "Film-Cooling Effectiveness Downstream of a Single Row of Holes With Variable Density Ratio," ASME J. of Turbomachinery, 113, 442-449.
43. Tafti, D.K. and Yavuzkurt, S., 1990, "Prediction of Heat Transfer Characteristics for Discrete Hole Cooling for Turbine Blade Applications," ASME J. of Turbomachinery, 112, 504-511
44. Thole, K.A., Gritsch, M., Schulz, A., and Wittig, S., 1996, "Flowfield Measurements for Cooling Holes with Expanded Exits," ASME Paper 96-GT-174.
45. Thole, K.A., Gritsch, M., Schulz, A., and Wittig, S., 1997, "Effect of a Crossflow at the Entrance to a Film-Cooling Hole," ASME J. of Fluids Engineering, Vol. 119, pp. 533-540.
46. Wang, L., Tsang, H., Simon T.W., and Eckert, E.R.G., 1996, "Measurements of Mean Flow and Eddy Transport Over a Film Cooling Surface," DOE/MC/29061-961C0692 to be presented at 1996 National Heat Transfer Conference, Houston TX.
47. Walters D.K. and Leylek, J.H., 1996, "A Systematic Computational Methodology Applied to a Three-dimensional Film-Cooling Flowfield," ASME Paper 96-GT-351.
48. Walters D.K. and Leylek, J.H., 1997, "A Detailed Analysis of Film-Cooling Physics Part I: Streamwise Injection with Cylindrical Holes," ASME Paper 97-GT-269
49. White, A.J., 1980, "The Prediction of the How and Heat Transfer in the Vicinity of a Jet in Crossflow", presented at the ASME Winter Annual Meeting, Chicago, IL.
50. White, F.M. 1974, Viscous Fluid Flow McGraw-Hill, Inc., New York.
51. Wittig, S., Schulz, A., Gritsch, M., and Thole, K.A., 1996, "Transonic Film-Cooling Investigations: Effects of Hole Shapes and Orientations," ASME Paper 96-GT-222
52. Yoshida, T. & Goldstein, R.J., 1984, "On the Nature of Jets Issuing from a Row of Holes into a Low Reynolds Number Mainstream How," J. Eng. for Gas Turb. and Power, 106, 612-618