Numerical prediction of film cooling and heat transfer with different film-hole arrangements on the plane and squealer TIP of a gas turbine blade

Proceedings of the ASME Turbo Expo 2004

Volumn 3, Issue , 2004, Pages 177-187

  Yang, Huitao ^a   Chen, Hamn Ching ^b   Han, Je Chin ^a  

^a Texas AandM University   (United States)

^b TEXAS A AND M UNIVERSITY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

DATA REDUCTION; GAS TURBINES; LIQUID CRYSTALS; OXIDATION; POWER GENERATION; PRESSURE DISTRIBUTION; THERMAL LOAD; TURBOMACHINE BLADES;

FILM COOLING; FILM-HOLE ARRANGEMENTS; LEAKAGE FLOW; LIQUID CRYSTAL TECHNIQUES (LCT);

HEAT TRANSFER;

EID: 10244237765     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1115/gt2004-53199     Document Type: Conference Paper

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