Measurements and Predictions of Surface Roughness Effects on Turbine Vane Aerodynamics

American Society of Mechanical Engineers, International Gas Turbine Institute, Turbo Expo (Publication) IGTI

Volumn 6 A, Issue , 2003, Pages 291-303

  Boyle, R J ^a   Senyitko, R G ^b  

^a NASA GLENN RESEARCH CENTER   (United States)

^b QSS GROUP INC   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

CERAMIC VANES; KINETIC LOSS COEFFICIENT; SUCTION SURFACE;

AERODYNAMICS; ASPECT RATIO; BOUNDARY CONDITIONS; CASCADES (FLUID MECHANICS); CERAMIC COATINGS; COMPUTATIONAL FLUID DYNAMICS; NAVIER STOKES EQUATIONS; PRESSURE MEASUREMENT; REYNOLDS NUMBER; STATORS; SURFACE ROUGHNESS; TURBOMACHINE BLADES; TURBULENCE; TURBULENT FLOW;

TURBINES;

EID: 0347595224     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1115/GT2003-38580     Document Type: Conference Paper

References (35)

1. Kind, R.J., Serjak, P.J., and Abbott, M.W.P., 1998, "Measurements and Prediction of the Effects of Surface Roughness on Profile Losses and Deviation in a Turbine Cascade," ASME Journal of Turbomachinery, Vol. 120, pp. 20-27.
2. Boynton, J.L., Tabibzadeh, R., and Hudson, S.T., 1992, "Investigation of Rotor Blade Roughness Effects on Turbine Performance," ASME Journal of Turbomachinery, Vol. 115, pp. 614-620.
3. Bammert, K., and Stanstede, H., 1972, "Measurements Concerning the Influence of Surface Roughness and Profile Changes on the Performance of Gas Turbines," ASME Journal of Engineering for Power, Vol. 94, pp. 207-213.
4. Bammert, K., and Stanstede, H., 1976, "Influences of Manufacturing Tolerances and Surface Roughness of Blades on the Performance of Turbines, " ASME Journal of Engineering for Power, Vol. 98, pp. 29-36.
5. Harbecke, U.G., Riess, W. and Seume, J.R., 2002, "The Effect of Milling Process Induced Coarse Surface Texture on Aerodynamic Turbine Profile Losses," ASME paper GT-2002-3033
6. Stabe, R.G., and Liebert, C.H., 1975, "Aerodynamic Performance of a Ceramic-Coated Core Turbine Vane Tested with Cold Air in a Two-Dimensional Cascade", NASA TM X=3191.
7. Bons, J.P., Taylor, R.P., McClain, S.T., and River, R.B., 2001, "The Many Faces of Turbine Surface Roughness, ASME Journal of Turbomachinery, Vol. 123, pp. 739-748.
8. Taylor, R.P., 1990, "Surface Roughness Measurements on Gas Turbine Blades," ASME Journal of Turbomachinery, Vol. 112, pp. 175-180.
9. El-Batsh, H., and Haselbacher, H., 2002, "Numerical Investigation of the Effects of Ash Particle Deposition on the Flow Field Through Turbine Cascades," ASME paper GT-2002-30600
10. Taylor, R.P, Coleman, H.W., and Hodge, B.k., 1985, "Predictions of Turbulent Rough-Wall Skin Friction Using a Discete Element Approach," ASME Journal of Fliuds Engineering, Vol. 107, pp. 251-257.
11. Cebeci, T., and Chang, K.C., 1978, "Calculation of Incompressible Rough-Wall Boundary Layer Flows," AIAA Journal, Vol. 16, No. 7, pp 730-735.
12. Wilcox, D.C., 1994, Turbulence Modeling for CFD, DCW Industries, Inc, La Canada, CA.
13. Boyle, R.J., Lucci, B.L, and Senyitko, R.G., 2002, "Aero-dynamic Performance and Turbulence Measurements in a Turbine Vane Cascade", ASME paper GT-2002-30434
14. Boyle, R.J., Lucci, B.L., Verhoff, V.G., Camperchioli, W.P., and La, H., 1998, "Aerodynamics of a Transitioning Turbine Stator Over a Range of Reynolds Numbers," ASME paper 98-GT-285.
15. Price, J., Jimenez, O., Miriyala, N., Kimmel, J.B., Leroux, D.R., and Fahme, T., 2001, "Ceramic Stationary Gas Turbine Development Program - Eighth Annual Summary," ASME paper 2001-GT-0517.
16. Schwab, J.R., 1982, "Aerodynamic Performance of High Turning Core Turbine Vanes in a Two-Dimensional Cascade," NASA TM 82894.
17. Abuaf, N., Bunker, R.S., and Lee, C.P., 1998, "Effects of Surface Roughness on Heat Transfer and Aerodynamic Performance of Turbine Airfoils," ASME Journal of Turbomachinery, Vol. 120, pp. 522-529.
18. f Augmentation for Real Turbine Roughness with Elevated Freestream Turbulence," ASME paper GT-2002-30198.
19. Sigal, A., and Danberg, J.E., 1990, "New Correlation of Roughness Density Effect on the Turbulent Boundary Layer." AIAA Journal, Vol. 28, No. 3, pp 554-556.
20. van Rij, J.A., Belnap, B.J., and Ligrani, P.M., 2002, "Analysis and Experiments on Three-Dimensional, Irregular Surface Roughness," ASME Journal of Fluids Engineering, Vol. 124, pp. 671-677.
21. Dvorak, F.A., 1969, "Calculation of Turbulent Boundary Layers on Rough Surfaces in Pressure Gradient," AIAA Journal, Vol. 7, No. 9, pp 1752-1759.
22. Dirling, R.B., 1973, "A Method for Computing Roughwall Heat Transfer Rates on Re-Entry Nosetips," AIAA paper 73-763
23. Waigh, D.R., and Kind, R.J., 1998, "Improved Aerodynamic Characterization of Regular Three-Dimensional Roughness," AIAA Journal, Vol. 36, No. 6, pp 1117-1119.
24. Boyle, R.J., Spuckler, C.M. and Lucci, B.L., 2000, "Comparison of Predicted and Measured Turbine Vane Rough Surface Heat Transfer," ASME paper 2000-GT-0217
25. Koch, C.C., and Smith, L.H., 1976, "Loss Sources and Magnitudes in Axial-Flow Compressors," ASME Journal of Engineering for Power, Vol. 98, pp. 411-424.
26. 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.
27. 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.
28. Ameri, A.A., and Bunker, R.S., 1999, "Heat Transfer and Flow on the First Stage Blade Tip of a Power Generation Gas Turbine; Part 2: Simulation Results," ASME paper 99-GT-283, (NASA CR-1999-209151).
29. Chima, R.V., Giel, P.W., and Boyle, R.J., 1993 "An Algebraic Turbulence Model for Three-Dimensional Viscous Flows," AIAA paper 93-0083, (NASA TM-105931).
30. Chima, R.V., 1996, "Application of the k - ω Turbulence Model to Quasi-Three-Dimensional Turbomachinery Flows," AIAA Journal of Propulsion and Power, Vol. 12, No. 6, pp. 1176-1179.
31. Pinson, M.W., and Wang, T., 2000 "Effect of Two-Scale Roughness on Boundary Layer Transition over a Heated Flat Plate: Part 1 - Surface Heat Transfer," ASME Journal of Turbomachinery, Vol. 122, pp. 301-307.
32. Mayle, R.E., 1991, "The Role of Laminar-Turbulent Transition in Gas Turbine Engines", ASME Journal of Turbomachinery, Vol. 113, pp. 509-537.
33. 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.
34. 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.
35. Menter, F., 1994, "Influence of Freestream Values on k- ω Turbulence Model Predictions," AIAA Journal, Vol. 32. No. 8, pp. 1598-1605.