Film cooling subject to bulk flow pulsations: effects of blowing ratio, freestream velocity, and pulsation frequency

Author:

Bell C.M,Ligrani P.M,Hull W.A,Norton C.M

Publisher

Elsevier BV

Subject

Fluid Flow and Transfer Processes,Mechanical Engineering,Condensed Matter Physics

Reference19 articles.

1. Gas turbine rotor blade film cooling with and without simulated NGV shock waves and wakes;Rigby,1990

2. An experimental study of film cooling in a rotating transonic turbine;Abhari;ASME Transactions—J. Turbomachinery,1994

3. Flowfield measurements in supersonic film cooling including effect of shock-wave interaction;Juhany;AIAA Journal,1994

4. Experimental studies of supersonic film cooling with shock wave interaction;Kanda;AIAA Journal,1996

5. Impact of rotor-stator interaction on turbine blade film cooling;Abhari;ASME Transactions—J. Turbomachinery,1996

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2. NUMERICAL INVESTIGATION OF FILM COOLING SUBJECT TO BULK FLOW PULSATIONS;Heat Transfer Research;2019

3. Experimental Investigation of Louver Cooling Scheme on Gas Turbine Stator;Heat Transfer Engineering;2015-07-30

4. Effect of trench width and blowing ratio on double-jet film cooling embedded in trenches;Proceedings of the Institution of Mechanical Engineers, Part A: Journal of Power and Energy;2015-02-04

5. Film-Cooling Jets Analyzed with Proper Orthogonal Decomposition and Dynamic Mode Decomposition;43rd Fluid Dynamics Conference;2013-06-22

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