Film cooling effectiveness and heat transfer on the trailing edge cutback of gas turbine airfoils with various internal cooling designs

Journal of Turbomachinery

Volumn 128, Issue 1, 2006, Pages 196-205

  Martini, P ^a   Schulz, A ^a   Bauer, H J ^a  

^a UNIVERSITY OF KARLSRUHE   (Germany)

Author keywords

[No Author keywords available]

Indexed keywords

AIRFOILS; COOLANTS; COOLING; HEAT TRANSFER; HEAT TRANSFER COEFFICIENTS; REYNOLDS NUMBER; TEMPERATURE; TURBULENCE; WIND TUNNELS;

ADIABATIC FILM COOLING; BLOWING RATIOS; ENGINE REALISTIC DENSITY RATIOS; FILM COOLING; HOT GAS TEMPERATURE; INTERNAL COOLING DESIGNS; TURBULATORS;

GAS TURBINES;

AIRFOILS; COOLANTS; COOLING; GAS TURBINES; HEAT TRANSFER; HEAT TRANSFER COEFFICIENTS; REYNOLDS NUMBER; TEMPERATURE; TURBULENCE; WIND TUNNELS;

EID: 33645757594     PISSN: 0889504X     EISSN: None     Source Type: Journal    
DOI: 10.1115/1.2103094     Document Type: Article

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