Entrance effects on diffused film-cooling holes

Proceedings of the ASME Turbo Expo

Volumn 4, Issue , 1998, Pages

  Kohli, A ^a   Thole, K A ^a  

^a Wisconsin Electric Machines and Power Electronics Consortium   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT ENGINES; COOLANTS; COOLING; FIGHTER AIRCRAFT; HEAT TRANSFER; REYNOLDS NUMBER; TURBINE COMPONENTS; TURBOMACHINE BLADES;

ADIABATIC EFFECTIVENESS; COMPUTATIONAL STUDIES; COOLANT SUPPLY; DENSITY RATIO; ENTRANCE EFFECTS; EXPERIMENTAL RESEARCH; FILM COOLING HOLE; INTERNAL CHANNEL;

GAS TURBINES;

EID: 84973160976     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1115/98-GT-402     Document Type: Conference Paper

References (17)

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