Film-cooling effectiveness on a rotating blade platform

Journal of Turbomachinery

Volumn 131, Issue 1, 2009, Pages

  Suryanarayanan, A ^a   Mhetras, S P ^a   Schobeiri, M T ^a   Han, J C ^a  

^a Department of Electrical and Computer Engineering   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMIC MEASUREMENTS; BLADE PLATFORM; COOLANT INJECTION; EXPERIMENTAL INVESTIGATIONS; FILM COOLING; FILM COOLING EFFECTIVENESS; FLOW RESEARCHES; INCIDENCE ANGLES; MAINSTREAM FLOW; MASS FLOW RATIOS; PRESSURE SENSITIVE PAINT TECHNIQUE; ROTATING BLADES; ROTATING CONDITIONS; ROTATION SPEED; ROTATIONAL SPEED; ROTOR BLADES; TURBINE ROTOR; TURBINE SPEED; WHEEL-SPACE CAVITY;

COOLANTS; COOLING; HELICOPTER ROTORS; MASS TRANSFER; RESEARCH LABORATORIES; ROTATION; SPEED; STAGES; STATORS; TURBINES;

TURBOMACHINE BLADES;

EID: 77953197121     PISSN: 0889504X     EISSN: 15288900     Source Type: Journal    
DOI: 10.1115/1.2752184     Document Type: Article

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