Integrated simulations for multi-component analysis of gas turbines: RANS boundary conditions

40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit

Volumn , Issue , 2004, Pages

  Kim, Sangho ^a,b   Schlüter, Jorg ^a,c   Wu, Xiaohua ^a,c   Alonso, Juan J ^a,b   Pitsch, Heinz ^a,c  

^a STANFORD UNIVERSITY   (United States)

^b Department of Aeronautics and Astronautics ^*  (United States)

^c Center for Turbulence Research   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

BOUNDARY CONDITIONS; GAS TURBINES; LARGE EDDY SIMULATION; MACH NUMBER; PROPULSION;

INTEGRATED SIMULATIONS; LOW MACH NUMBER APPROXIMATIONS; MULTI-COMPONENT ANALYSIS; MULTIPLE FLOWS; PIPE GEOMETRY; RANS SOLVER; REYNOLDS-AVERAGED NAVIER STOKES SOLVERS; THERMAL COMPUTATIONS;

NAVIER STOKES EQUATIONS;

EID: 85085772977     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2004-3415     Document Type: Conference Paper

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