Purge flow and interface gap geometry influence on the aero-thermal performance of a rotor blade cascade

Author:

Barigozzi Giovanna,Franchini Giuseppe,Perdichizzi Antonio,Maritano Massimiliano,Abram Roberto

Publisher

Elsevier BV

Subject

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

Reference38 articles.

1. Barigozzi, G., Franchini, G., Perdichizzi, A., 2007. Inlet turbulence intensity effect on endwall film cooling. In: Proceedings of the 7th European Conference on Turbomachinery Fluid Dynamics and Thermodynamics, Athens, Greece, March 5–9, 1105–1116.

2. Influence of coolant flow rate on aero-thermal performance of a rotor blade cascade with endwall film cooling;Barigozzi;ASME J. Turbomach.,2012

3. Barigozzi, G., Franchini, G., Perdichizzi, A., Maritano, M., Abram, R., 2013. Aero-thermal Performance of a Rotor Blade Cascade with Stator–rotor Seal Purge Flow. ASME Paper GT2013-94692.

4. Exit plane and suction surface flows in an annular turbine cascade with a skewed inlet boundary layer;Bindon;Int. J. Heat and Fluid Flow,1980

5. An experimental study of heat transfer and film cooling on large-scale turbine endwalls;Blair;J. Heat Transfer,1974

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