Effects of surface roughness on heat transfer and aerodynamic performance of turbine airfoils

Journal of Turbomachinery

Volumn 120, Issue 3, 1998, Pages 522-529

  Abuaf, N ^a   Bunker, R S ^a   Lee, C P ^b  

^a GENERAL ELECTRIC COMPANY   (United States)

^b GE AVIATION   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; FRICTION; HEAT TRANSFER; HEAT TRANSFER COEFFICIENTS; REYNOLDS NUMBER; SURFACE ROUGHNESS; THERMAL VARIABLES MEASUREMENT;

AERODYNAMIC FLOW PATH LOSSES; ENGINE PERFORMANCE; SKIN FRICTION COEFFICIENTS;

AIRFOILS;

AEROFOIL; HEAT TRANSFER; SURFACE ROUGHNESS;

EID: 0032124970     PISSN: 0889504X     EISSN: 15288900     Source Type: Journal    
DOI: 10.1115/1.2841749     Document Type: Article

References (27)

1. Abuaf, N., Bunker, R., and Lee, P. C., 1997, “Heat Transfer and Film Cooling Effectiveness in a Linear Airfoil Cascade,” ASME Journal of Turbo machinery, Vol. 119, pp. 302-309.
2. Bammert, K., and Sandstede, H., 1975, “Influences of Manufacturing Tolerances and Surface Roughness of Blades on the Performance of Turbines,” ASME Paper No. 75-GT-35.
3. Barlow, D. N., Kim, Y. W., and Florschuetz, L. W., 1997, “Transient Liquid Crystal Technique for Convective Heat Transfer on Rough Surfaces,” ASME Journal of Turbo machinery, Vol. 119, pp. 14-22.
4. Blair, M. F., 1994, “An Experimental Study of Heat Transfer in a Large-Scale Turbine Rotor Passage,” ASME Journal of Turbo machinery, Vol. 116, pp. 1-13.
5. Bogard, D. G., Schmidt, D. L., and Tabbita, M., 1998, “Characterization and Laboratory Simulation of Turbine Airfoil Surface Roughness,” ASME Journal of Turbo machinery, Vol. 120, pp. 337-342.
6. Boyle R. J., 1994, “Prediction of Surface Roughness and Incidence Effects on Turbine Performance,” ASME Journal of Turbo machinery, Vol. 116, pp. 745-751.
7. Boudreau, B. D., Raja, J., Sannreddy, H., and Caber, P. J., 1995, “A Comparative Study of Surface Texture Measurement Using White Light Scanning Interfer-ometry and Contact Stylus Techniques,” Proc. American Society for Precision Engineering 1995 Annual Meeting, Vol. 12, pp. 120-124, Oct. 15-20.
8. Chakroun, W., and Taylor, R. P., 1993, “Heat Transfer and Fluid Dynamics Measurements in Accelerated Rough Wall Boundary Layer,” ASME Paper No. 93-GT-78.
9. Dipprey, R. B., and Sabersky, R. H., 1963, “Heat and Mass Transfer in Smooth and Rough Tubes at Various Prandtl Numbers,” Int. J. Heat Mass Transfer, Vol. 6, pp. 329-353.
10. Dunn, M. G., Kim, J., Civinskas, K. C., and Boyle, R. J., 1994, “Time-Averaged Heat Transfer and Pressure Measurements and Comparison With Prediction for a Two-Stage Turbine,” ASME Journal of Turbo machinery, Vol. 116, pp. 14-22.
11. Forster, V. T., 1967, “Performance Loss of Modem Steam Turbine Plant Due to Surface Roughness,” Proc. Instn. Mech. Engrs. 1966-67, Vol. 181, Pt. 1, pp. 391-405.
12. Guo, S. M., Jones, T. V., Lock, G. D., and Dancer, S. N., 1998, “Computational Prediction of Heat Transfer to Gas Turbine Nozzle Guide Vanes With Roughened Surfaces,” ASME Journal of Turbo machinery, Vol. 120, pp. 343-350.
13. Han, L. S., 1985, “Turbulent Flow Over Rough Turbine Airfoils,” AFWAL-TR-85-2056, Final Contractor Report, The Ohio State University.
14. Han, L. S., and Delpassand, M., 1990, “A Heat Transfer Analysis of Rough Turbine Airfoils,” WRDC-TR-89-2135, Final Contractor Report, Ohio State University.
15. Hoffs, A., Drost, U., and Boles, A., 1996, “Heat Transfer Measurements on a Turbine Airfoil at Various Reynolds Numbers and Turbulence Intensities Including Effects of Surface Roughness,” ASME Paper No. 96-GT-169.
16. Hosni, M. H., Coleman, H. W., and Taylor, R. P., 1991, “Measurements and Calculations of Rough Wall Heat Transfer in the Turbulent Boundary Layer,” Int. J. Heat Mass Transfer, Vol. 34, No. 4/5, pp. 1067-1082.
17. Kadar, B. A., and Yaglom, A. M., 1972, “Heat and Mass Transfer Laws of Fully Turbulent Wall Flows,” Int. J. Heat Mass Transfer, Vol. 15, pp. 2329-2351.
18. Kline, S. J., and McClintock, F. A., 1953, “Describing Uncertainties in Single Sample Experiments,” Mechanical Engineering, Vol. 75, Jan., pp. 3-8.
19. 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.
20. Lander, R. D., Fish, R. W., and Suo, M., 1972, “External Heat Transfer Distribution on Film Cooled Turbine Vane,” J. Aircraft, Vol. 9, No. 10, pp. 707-714.
21. Pinson, M., and Wang, T., 1994, “Effects of Leading Edge Roughness on Fluid Flow and Heat Transfer in the Transitional Boundary Layer Over a Flat Plate,” ASME Paper No. 94-GT-326.
22. Schlichting, H., 1968, Boundary Layer Theory, McGraw-Hill, New York.
23. Seidman, M. H., 1978, “Rough Wall Heat Transfer in a Compressible Turbulent Boundary Layer,” AIAA Paper No. 78-163.
24. 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.
25. Tarada, F. H. A., 1990, “Prediction of Rough Wall Boundary Layers Using a Low-Reynolds Number fc-Epsilon Model,” Int. J. Heat Fluid Flow, Vol. 11, pp. 331-345.
26. Turner, A. B., Tarada, F. H. A., and Bayley, F. J., 1985, “Effects of Surface Roughness on Heat Transfer to Gas Turbine Blades,” AGARD-CP-390.
27. Zerkle, R. D., and Lounsbury, R. J., 1989, “Free Stream Turbulence Effect on Turbine Airfoil Heat Transfer,” J. Propulsion, Vol. 5, No. 1, pp. 82-88.