Measurements of heat transfer coefficients and friction factors in rib-Roughened channels simulating leading-edge cavities of a modern turbine blade

Journal of Turbomachinery

Volumn 119, Issue 3, 1997, Pages 601-609

  Taslim, M E ^a   Li, T ^a   Spring, S D ^b  

^a Northeastern University   (United States)

^b GE AVIATION   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

CAVITATION CORROSION; CHANNEL FLOW; FRICTION; GAS TURBINES; HEAT TRANSFER; SIMULATION; SURFACE ROUGHNESS;

LEADING EDGE CAVITIES;

TURBOMACHINE BLADES;

BLADES; FRICTION; HEAT TRANSFER; TURBINES;

EID: 0031190841     PISSN: 0889504X     EISSN: 15288900     Source Type: Journal    
DOI: 10.1115/1.2841164     Document Type: Article

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