Simulations and measurements on impulse blades for heat transfer prediction in supersonic turbine applications

Proceedings of the ASME Turbo Expo

Volumn 4, Issue , 1998, Pages

  Hall, U ^a   Larsson, J ^a   Bario, F ^b   Kulisa, P ^b   Slimanr, J ^b   Begin, V ^c   Eriksson, L E ^d   Wahlen U ^d  

^a CHALMERS UNIVERSITY OF TECHNOLOGY   (Sweden)

^b LABORATOIRE DE MÉCANIQUE DES FLUIDES ET D ACOUSTIQUE   (France)

^c SNECMA   (France)

^d VOLVO AERO CORPORATION   (Sweden)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT ENGINES; BOOSTERS (ROCKET); BOUNDARY LAYERS; FORECASTING; GAS TURBINES; HEAT TRANSFER; NAVIER STOKES EQUATIONS; NUMERICAL METHODS; ROCKET ENGINES; ROCKETS; TURBOMACHINE BLADES; VELOCITY;

BOUNDARY LAYER METHODS; FLOW AND HEAT TRANSFER; HEAT TRANSFER PREDICTIONS; IMPULSE TURBINES; SEPARATION BUBBLE; SIMULATIONS AND MEASUREMENTS; TURBINE APPLICATIONS; TWO-EQUATION MODEL;

TURBINE COMPONENTS;

EID: 84973129530     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1115/98-GT-154     Document Type: Conference Paper

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