Transonic aerodynamic losses due to turbine airfoil, suction surface film cooling

Proceedings of the ASME Turbo Expo

Volumn 3, Issue , 1999, Pages

  Jackson, D J ^a,c   Lee, K L ^a   Ligrani, P M ^a   Johnson, P D ^b   Soechting, F O ^b  

^a University of Utah   (United States)

^b PRATT AND WHITNEY   (United States)

^c BOEING COMPANY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT ENGINES; AIRFOILS; COOLING; GAS TURBINES; GEOMETRY; HEAT TRANSFER; KINETIC ENERGY; KINETICS; MACH NUMBER; MIXING; SHOCK WAVES; TRANSONIC AERODYNAMICS;

DISCHARGE COEFFICIENTS; EXPERIMENTAL APPARATUS; FREESTREAM MACH NUMBER; KINETIC ENERGY DISTRIBUTIONS; MACH-NUMBER DISTRIBUTIONS; MOMENTUM FLUX RATIOS; TOTAL-PRESSURE LOSS; TURBULENT DIFFUSION;

AERODYNAMICS;

EID: 84928471491     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1115/99-GT-260     Document Type: Conference Paper

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