Overall effectiveness for a film cooled turbine blade leading edge with varying hole pitch

Journal of Turbomachinery

Volumn 135, Issue 3, 2013, Pages

  Dyson, Thomas E ^a   Bogard, David G ^a   Piggush, Justin D ^b   Kohli, Atul ^b  

^a UNIVERSITY OF TEXAS AT AUSTIN   (United States)

^b PRATT AND WHITNEY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

CONVECTIVE COOLING; CYLINDRICAL HOLES; ENGINE CONDITIONS; HIGH-CONDUCTIVITY MATERIALS; IMPINGEMENT COOLING; MASS FLOW RATE; OVERALL EFFECTIVENESS; TURBINE BLADE;

COOLANTS; COOLING; TURBINES; TURBOMACHINE BLADES;

COMPUTER SIMULATION;

EID: 84888019299     PISSN: 0889504X     EISSN: 15288900     Source Type: Journal    
DOI: 10.1115/1.4006872     Document Type: Article

References (11)

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3. Albert, J. E., Bogard, D. G., and Cunha, F., 2004, "Adiabatic and Overall Effectiveness for a Film Cooled Blade," ASME Turbo Expo, Vienna, Austria, June 14-17, ASME Paper No. GT2004-53998.
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9. Moffat, R. J., 1985, "Using Uncertainty Analysis in the Planning of an Experiment," ASME J. Fluids Eng., 107(2), pp. 173-178.
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11. Dobrowolski, L. D., 2009, "Numerical Simulation of a Film Cooled Turbine Blade Leading Edge Including Heat Transfer Effects," M.S. thesis, University of Texas at Austin, Austin, TX.