Novel blade cooling engineering solution

Proceedings of the ASME Turbo Expo

Volumn 3, Issue , 2000, Pages

  Moser, Siegfried ^a   Ivanisin, Mario ^a   Woisetschläger, Jakob ^a   Jericha, Herbert ^a  

^a GRAZ UNIVERSITY OF TECHNOLOGY   (Austria)

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTATIONAL FLUID DYNAMICS; FIGHTER AIRCRAFT; FINITE ELEMENT METHOD; GAS DYNAMICS; HEAT CONDUCTION; HEAT TRANSFER; KINETIC ENERGY; KINETICS; NAVIER STOKES EQUATIONS; TURBINE COMPONENTS; TURBINES; TURBOMACHINE BLADES; TURBULENCE; TURBULENT FLOW;

COMPUTATION FLUID DYNAMICS; COOLING EFFICIENCY; ENGINEERING DESIGN; INJECTION ANGLES; SOLID HEAT CONDUCTIONS; TURBINE INLET TEMPERATURE; TURBULENCE INTENSITY; TURBULENT KINETIC ENERGY;

COOLING;

EID: 84955165858     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1115/2000-GT-0242     Document Type: Conference Paper

References (17)

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