Film cooling on a gas turbine blade suction side with converging slot-hole
Author:
Funder
National Natural Science Foundation of China
Publisher
Elsevier BV
Subject
General Engineering,Condensed Matter Physics
Reference31 articles.
1. A review of turbine shaped film cooling technology;Bunker;ASME J. Heat Transf.,2005
2. Effects of hole geometry and density on three-dimensional film cooling;Goldstein;Int. J. Heat Mass. Transf.,1974
3. Adiabatic wall effectiveness measurements of film-cooling holes with expanded exits;Gritsch;ASME J. Turbomach.,1998
4. Effect of hole geometry on the thermal performance of fan-shaped film cooling holes;Gritsch;ASME J. Turbomach.,2005
5. Flowfield measurements for film-cooling holes with expanded exits;Thole;ASME J. Turbomach.,1998
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