Effects of aeroderivative combustor turbulence on endwall heat transfer distributions acquired in a linear vane cascade

Journal of Turbomachinery

Volumn 125, Issue 2, 2003, Pages 210-220

  Ames, Forrest E ^a   Barbot, Pierre A ^b   Wang, Chao ^b  

^a Mem ASME   (United States)

^b University of North Dakota   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

BOUNDARY LAYER FLOW; CHANNEL FLOW; HEAT TRANSFER; INTAKE SYSTEMS; REYNOLDS NUMBER; TURBULENT FLOW; VANE PUMPS; VORTEX FLOW; WALL FLOW;

FLOW FIELDS;

COMBUSTORS;

COMBUSTOR; HEAT TRANSFER; TURBOMACHINERY; TURBULENCE;

EID: 0037641108     PISSN: 0889504X     EISSN: None     Source Type: Journal    
DOI: 10.1115/1.1559897     Document Type: Article

References (25)

1. Sieverding, C. H., 1985, "Recent Progress in the Understanding of Basic Aspects of Secondary Flow in Turbine Blade Passages," ASME J. Eng. Gas Turbines Power, 107, pp. 248-257.
2. Klein, A., 1966, "Investigation of the Entry Boundary Layer on the Secondary Flows in the Blading of Axial Turbines," BHRA T 1004.
3. Langston, L. S., Nice, M. L., and Hooper, R. M., 1977, "Three-Dimensional Flow Within a Turbine Cascade Passage," ASME J. Eng. Power, pp. 21-28.
4. Marchal, P., and Sieverding, C. H., 1977, "Secondary Flows Within Turbomachinery Bladings," AGARD Conf. Proc., AGARD CP 214.
5. Ames, F. E., Hylton, L. D., and York, R. E., 1986, unpublished work on the impact of the inlet endwall boundary layer on secondary losses and velocity vectors in a compressible turbine cascade, Allison Gas Turbine Division of General Motors.
6. Zess, G. A., and Thole, K. A., 2001, "Computational Design and Experimental Evaluation of Using an Inlet Fillet on a Gas Turbine Vane," ASME Paper No. 2001-GT-404.
7. Burd, S. W., and Simon, T. W., 2000, "Flow Measurements in a Nozzle Guide Vane Passage With a Low Aspect Ratio and Endwall Contouring," ASME J. Turbomach., 122, pp. 659-666.
8. York, R. E., Hylton, L. D., and Milelc, M. S., 1984, "An Experimental Investigation of Endwall Heat Transfer and Aerodynamics in a Linear Vane Cascade," ASME J. Eng. Gas Turbines Power, 106, p. 159.
9. Harasgama, S. P., and Wedlake, E. T., 1989, "Heat Transfer and Aerodynamics of a High Rim Speed Turbine Nozzle Guide Vane Tested in the RAE Isentropic Light Piston Cascade," ASME J. Turbomach., 113, pp. 384-391.
10. Spencer, M. C., Jones, T. V., Lock, G. D., 1996, "Endwall Heat Transfer Measurements in an Annular Cascade of Nozzle Guide Vanes at Engine Representative Reynolds and Mach Numbers," Int. J. Heat Fluid Flow, 17, pp. 139-147.
11. Arts, T., and Heider, R., 1994, "Aerodynamic and Thermal Performance of a Three Dimensional Annular Transonic Nozzle Guide Vane, Part-I Experimental Investigation," Paper No. 1994-31, 30th AIAA/ASME/SAE/ASEE Joint propulsion conference.
12. Radomsky, R., and Thole, K. A., 2000, "High Freestream Turbulence Effects in the Endwall Leading Edge Region," ASME J. Turbomach., 122, pp. 699-708.
13. Goldstein, R. J., and Spores, R. A., 1988, "Turbulent Transport on the Endwall in the Region Between Adjacent Turbine Blades," ASME J. Heat Transfer, 110, pp. 862-869.
14. Giel, P. W., Thurman, D. R., Van Fossen, G. J., Hippensteele, A. A., and Boyle, R. J., 1996, "Endwall Heat Transfer Measurements in a Transonic Turbine Cascade," ASME Paper No. 96-GT-180.
15. Boyle, R. J., and Lucci, B. L., 1996, "Predicted Turbine Heat Transfer for a Range of Test Conditions," ASME Paper No. 96-GT-304.
16. FLUENT 5.5, 2000, FLUENT 5.5 User's Guide, Fluent, Inc., Lebanon, N.H.
17. Hippensteele, S. A., Russell, L. M., and Torres, F. J., 1985, "Local Heat-Transfer Measurements on a Large, Scale-Model Turbine Blade Airfoil Using a Composite of a Heater Element and Liquid Crystals," MASA Technical Memo. 86900.
18. Hippensteele, S. A., Russell, L. M., and Torres, F. J., 1986, "Use of a Liquid-Crystal, Heater-Element Composite for Quantitative High-Resolution Heat Transfer Coefficients on a Turbine Airfoil, Including Turbulence and Surface Roughness Effects," NASA Tech. Memo., 87355.
19. Hippensteele, S. A., 1988, "High-Resolution Liquid-Crystal Heat-Transfer Measurements on the End Wall of a Turbine Passage with Variations in Reynolds Number," NASA Tech. Memo., 100827.
20. Jones, T. V., and Hippensteele, S. A., 1988, "High-Resolution Heat-Transfer-Coefficient Maps Applicable to Compound-Curve Surface Using Liquid Crystals in a transient wind tunnel," NASA Tech. Memo., 89855.
21. Camei, C., Glezer, B., Owen, J. M., Pilbrow, R. G., and Syson, B. J., 1998, "Application of Thermochromic Liquid Crystal to Rotating Surfaces," ASME J. Turbomach., 120, pp. 100-103.
22. Moffat, R. J., 1988, "Describing the Uncertainties in Experimental Results," Exp. Therm. Fluid Sci., 1, pp. 3-17.
23. Ames, F. E., Kwon, O., and Moffat, R. J., 1999, "An Algebratic Model for High Intensity Large Scale Turbulence," ASME Paper No. 99-GT-160.
24. Ames, F. E., and Plesniak, M. W., 1997, "The Influence of Large Scale, High Intensity Turbulence on Vane Aerodynamic Losses, Wake Growth, and Exit Turbulence Parameters," ASME J. Turbomach., 119, pp. 182.
25. Kays, W. M., and Crawford, M. E., 1993, Convective Heat and Mass Transfer, 3rd Edition, McGraw-Hill, New York.