Study of hot streak phenomena in subsonic and transonic flows

International Journal of Turbo and Jet Engines

Volumn 13, Issue 2, 1996, Pages 131-141

  Dorney, Daniel J ^a   Sondak, Douglas L ^b  

^a WESTERN MICHIGAN UNIVERSITY   (United States)

^b UNITED TECHNOLOGIES RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

EID: 0030375667     PISSN: 03340082     EISSN: None     Source Type: Journal    
DOI: 10.1515/TJJ.1996.13.2.131     Document Type: Article

References (20)

1. Baldwin, B.S. and Lomax, H., "Thin-layer approximation and algebraic model for separated turbulent flows", AIAA Paper 78-257, Huntsville, AL, 1978.
2. Butler, T.L., Sharma, O.P., Joslyn, H.D., and Dring, R.P., "Redistribution of an inlet temperature distortion in an axial flow turbine stage", AIAA Journal of Propulsion and Power, 5, 64-71 (January-February, 1989).
3. Chakravarthy, S., and Osher, S., "Numerical experiments with the Osher upwind scheme for the Euler equations", AIAA Paper 82-0975, 1982.
4. Dorney, D.J., Davis, R.L., and Sharma, O.P., "Two-dimensional inlet temperature profile attenuation in a turbine stage", ASME Paper 91-GT-406, Orlando, FL, June, 1991.
5. Dorney, D.J., Davis, R.L., Edwards, D.E., and Madavan, N.K., "Unsteady analysis of hot streak migration in a turbine stage", AIAA Journal of Propulsion and Power, 8 (2), 520-529 (1992).
6. Dorney, D.J., and Davis, R.L., "Numerical simulation of turbine 'hot spot' alleviation using film cooling", AIAA Journal of Propulsion and Power, 9 (3), 329-336 (1993).
7. Dorney, D.J., and Schwab, J.R., "Unsteady numerical simulations of radial temperature profile redistribution in a single-stage turbine", ASPE Paper 95-GT-178, also to appear in the ASME Journal of Turbomachinery.
8. Dunn, M.G., Bennett, W.A., Delaney, R.A., and Rao, K.V., "Investigation of unsteady flow through a transonic turbine stage: Data/ prediction comparison for time-averaged and phase-resolved pressure data", ASME Journal of Turbomachinery, 114, 91-99 (1992).
9. Harasgama, S.P., "Combustor exit temperature distortion effects on heat transfer and aerodynamics within a rotating turbine blade passage", ASME Paper 90-GT-174, Brussels, Belgium, 1990.
10. Johnson, A.B., Rigby, M.J., Oldfield, M.L.G., Ainsworth, R.W., and Oliver, M.J., "Surface heat transfer fluctuations on a turbine rotor blade due to upstream shock wave passing", ASME 88-GT-172, Amsterdam, The Netherlands, 1988.
11. Kirtley, K.R., Celestina, M.L., and Adamczyk, J.J., "The effect of unsteadiness on the time-mean thermal loads in a turbine stage", SAE Paper 931375 (also to appear in the ASME Journal of Turbomachinery).
12. Krouthen, B., and Giles, M.B., "Numerical investigation of hot streaks in turbines", AIAA Paper 88-3015, Boston, MA, 1988.
13. Rai, M.M., and Dring, R.P., "Navier-Stokes analyses of the redistribution of inlet temperature distortions in a turbine", AIAA Journal of Propulsion and Power, 6, 276-282 (1990).
14. Rao, K.V., Delaney, R.A., and Dunn, M.G., "Vaneblade interaction in a transonic turbine, Part I -Aerodynamics", AIAA Journal of Propulsion and Power, 10 (3), 305-311 (1994).
15. Roback, R.J., and Dring, R.P., "Hot streaks and phantom cooling in a turbine rotor passage: Part 1 - Separate effects", ASME Paper 92-GT-75, Cologne, Germany, 1992.
16. Saxer, A.P., and Giles, M.B., "Inlet radial temperature redistribution in a transonic turbine stage", AIAA Paper 90-1543, Seattle, WA, 1990.
17. Saxer, A.P., and Felici, H.M., "Numerical analysis of 3-D unsteady hot streak migration and shock interaction in a turbine stage", ASME Paper 94-GT-76, The Hague, Netherlands, 1994 (also to appear in ASME Journal of Turbomachinery).
18. Takahashi, R.K. and Ni, R.H., "Unsteady Euler analysis of the redistribution of an inlet temperature distortion in a turbine", AIAA Paper 90-2262, Orlando, FL, 1990.
19. Takahashi, R.K. and Ni, R.H., "Unsteady hot streak migration through a 1-1/2 stage turbine", AIAA Paper 91-3382, Sacramento, CA, 1991.
20. Weigand, B., and Harasgama, S.P., "Computations of a film-cooled turbine rotor blade with non-uniform inlet temperature distribution using a three-dimensional inlet temperature distribution using a three-dimensional viscous procedure", ASME Paper 94-GT-15, The Hague, Netherlands, 1994.