Time-averaged heat flux for a recessed tip, lip, and platform of a transonic turbine blade

Proceedings of the ASME Turbo Expo

Volumn 3, Issue , 2000, Pages

  Dunn, M G ^a   Haldeman, C W ^a  

^a OHIO STATE UNIVERSITY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

GAS TURBINES; HEAT FLUX; HEAT TRANSFER; TURBINES; TURBOMACHINE BLADES;

BLADE SUCTION SURFACE; BLADE TIP REGION; EXPERIMENTAL RESEARCH; ROTATING TURBINES; STATIC-PRESSURE RATIO; STATIONARY SHROUD; SUCTION SURFACES; TRANSONIC TURBINE;

TURBINE COMPONENTS;

EID: 84955252575     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1115/1.1311285     Document Type: Conference Paper

References (32)

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