Enhancement of USM3D unstructured flow solver for high-speed high-temperature shear flows

47th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition

Volumn , Issue , 2009, Pages

  Pandya, Mohagna J ^a   Abdol Hamid, Khaled S ^b   Frink, Neal T ^b  

^a ANALYTICAL SERVICES AND MATERIALS INC   (United States)

^b NASA LANGLEY RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

FLOW SIMULATION; NASA; NAVIER STOKES EQUATIONS; SUPERSONIC AERODYNAMICS; SUPERSONIC AIRCRAFT; TURBULENCE MODELS;

AXISYMMETRIC JET; COMPRESSIBILITY CORRECTION; NAVIER-STOKES FLOW SOLVER; SIMPLE MODIFICATIONS; TEMPERATURE AND PRESSURES; TURBULENCE TRANSPORTS; TWO-EQUATION TURBULENCE MODELS; UNSTRUCTURED FLOW;

SHEAR FLOW;

EID: 78549266851     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2009-1329     Document Type: Conference Paper

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