Heat transfer and flow on the squealer tip of a gas turbine blade

Proceedings of the ASME Turbo Expo

Volumn 3, Issue , 2000, Pages

  Azad, Gm S ^a   Han, Je Chin ^a   Boyle, Robert J ^b  

^a Texas AandM University   (United States)

^b NASA GLENN RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

FIGHTER AIRCRAFT; GAS TURBINE LOCOMOTIVES; GAS TURBINES; HEAT TRANSFER; HEAT TRANSFER COEFFICIENTS; LIQUID CRYSTALS; REYNOLDS NUMBER; TURBOMACHINE BLADES; TURBULENCE;

AIRCRAFT GAS TURBINE ENGINES; EXPERIMENTAL INVESTIGATIONS; HEAT TRANSFER MEASUREMENTS; LOCAL HEAT TRANSFER COEFFICIENT; OVERALL HEAT TRANSFER COEFFICIENT; STATIC PRESSURE MEASUREMENTS; STATIONARY LINEAR CASCADES; TRANSIENT LIQUID CRYSTAL TECHNIQUE;

TURBINE COMPONENTS;

EID: 84955477678     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1115/2000-GT-0195     Document Type: Conference Paper

References (20)

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