Minimization of coolant mass flow rate in internally cooled gas turbine blades

Proceedings of the ASME Turbo Expo

Volumn 3, Issue , 1999, Pages

  Martin, Thomas J ^a,b   Dulikravich, George S ^a   Han, Zhen Xue ^a,c   Dennis, Brian H ^a  

^a The Pennsylvania State University   (United States)

^b NASA LANGLEY RESEARCH CENTER   (United States)

^c School of Electronics and Information   (China)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; ALGORITHMS; BOUNDARY ELEMENT METHOD; COMPUTATIONAL FLUID DYNAMICS; CONSTRAINED OPTIMIZATION; CONSTRAINT THEORY; COOLANTS; DESIGN; FLOW OF GASES; FLOW RATE; GAS TURBINES; HEAT CONDUCTION; HEAT CONVECTION; HEAT FLUX; HEAT TRANSFER; INLET FLOW; ITERATIVE METHODS; MASS TRANSFER; NAVIER STOKES EQUATIONS; ONE DIMENSIONAL; OPTIMIZATION; REYNOLDS EQUATION; SAILING VESSELS; SERPENTINE; SILICATE MINERALS; SIMULATED ANNEALING; THERMAL BARRIER COATINGS; TURBINE COMPONENTS; TURBOJET ENGINES;

EVOLUTIONARY OPTIMIZATIONS; FINITE VOLUME REYNOLDS AVERAGED NAVIER-STOKES; HEAT CONVECTION COEFFICIENT; HYBRID OPTIMIZATION ALGORITHM; QUASI-ONE-DIMENSIONAL ANALYSIS; QUASI-ONE-DIMENSIONAL SYSTEMS; TURBINE INLET TEMPERATURE; WALL THICKNESS DISTRIBUTION;

TURBOMACHINE BLADES;

EID: 84921766822     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1115/99-GT-146     Document Type: Conference Paper

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