Numerical prediction of non-reacting and reacting flow in a model gas turbine combustor

Proceedings of the ASME Turbo Expo 2004

Volumn 1, Issue , 2004, Pages 303-312

  Davoudzadeh, Farhad ^a   Liu, Nan Suey ^b  

^a UNIVERSITY OF TOLEDO   (United States)

^b NASA GLENN RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

COMPRESSIBLE FLOW; COMPUTATIONAL FLUID DYNAMICS; COMPUTER SIMULATION; GAS TURBINES; MATHEMATICAL MODELS; NAVIER STOKES EQUATIONS; PARTIAL DIFFERENTIAL EQUATIONS; REYNOLDS NUMBER; TURBULENCE; TURBULENT FLOW; VISCOUS FLOW;

FLOW STRUCTURE; GAS TURBINE COMBUSTORS; MACH NUMBER; REACTING FLOWS; REYNOLDS-AVERAGED NAVIER STOKES (RANS) CODES;

COMBUSTORS;

EID: 10244274177     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1115/gt2004-53496     Document Type: Conference Paper

References (9)

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3. Norris, A.T., 1997, "Automated Simplification of Full Chemical Mechanisms, AIAA Paper No. 97-3115.
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6. th AIAA Aerospace Sciences Meeting & Exhibit, 8-11 January 2001/Reno, NV.
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9. Bowman, C.T., Edwards, C.F., Gerdes J.C., Pitsch, H., Printe, F.B., 2002, "Active Control of Combustion Instability in Air-Breathing Propulsion Systems - A Computational and Experimental Program," Department of Mechanical Engineering, Stanford University, Final Technical Report, NASA-Glenn Grant No. NAG 2-1219.