Effects of hot streak/airfoil ratio in a high-subsonic single-stage turbine

International Journal of Turbo and Jet Engines

Volumn 17, Issue 2, 2000, Pages 119-131

  Dorney, Daniel J ^a   Sondak, Douglas L ^b   Cizmas, Paul G A ^c  

^a Virginia Commonwealth University   (United States)

^b BOSTON UNIVERSITY   (United States)

^c Texas AandM University   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

EID: 0034340979     PISSN: 03340082     EISSN: None     Source Type: Journal    
DOI: 10.1515/TJJ.2000.17.2.119     Document Type: Article

References (16)

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8. nd ASME International Gas Turbine Aeroengine Congress and Exposition, Orlando, FL, June-25, 1997.
9. Shang, T. and Epstein, A.H. "Analysis of Hot Streak Effects on Turbine Rotor Heat Load", ASME paper 96-GT-118, Birmingham, England, June, 1996, also to be published in the ASME Journal of Turbomachinery.
10. Whitney, W.J., Stabe, R.G. and Moffitt, T.P. "Description of the Warm Core Turbine Facility and the Warm Annular Cascade Facility Recently Installed at NASA Lewis Research Center", NASA TM 81562, 1980.
11. Schwab, J.R., Stabe, R.G. and Whitney, W.J. "Analytical and Experimental Study of Flow Through an Axial Turbine Stage with a Nonuniform Inlet Radial Temperature Profile", AIAA Paper 83-1175, Seattle, WA, June, 1983.
12. Stabe, R.G., Whitney, W.J. and Moffitt, T.P. "Performance of a High-Work Low Aspect Ratio turbine Tested with a Realistic Inlet Radial Temperature Profile", AIAA Paper 84-1161, Cincinnati, OH, June, 1984.
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16. Dorney, D.J. and Schwab, J.R. "Unsteady Numerical Simulations of Radial Temperature Profile Redistribution in a Single-Stage Turbine", ASME Paper 95-GT-178, Houston, TX, June, 1995. Also appeared in the ASME Journal of Turbomachinery, 118 (4), 783-791 (1996).