The mean flowfield structure of a supersonic three-dimensional base flow

46th AIAA Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 2008, Pages

  Gaitonde, Datta V ^a  

^a AIR FORCE RESEARCH LABORATORY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AFTERBODY; BASE SURFACE; BASEFLOWS; DETACHED EDDY SIMULATIONS; EXPERIMENTAL DATA; HIGH-SPEED; LATERAL PLANE; LONGITUDINAL VORTICES; MEAN FLOW; PREDICTIVE CAPABILITIES; REYNOLDS AVERAGED NAVIER-STOKES EQUATIONS; SURFACE OIL FLOW; SURFACE PRESSURES; TWO-EQUATION TURBULENCE MODELS; VELOCITY VECTORS; VORTEX CORES; VORTICITY DISTRIBUTION; WAKE REGION; WAVE STRUCTURES;

AEROSPACE ENGINEERING; BOUNDARY LAYERS; CIRCULAR CYLINDERS; COMPUTATIONAL FLUID DYNAMICS; FLIGHT DYNAMICS; FLOW FIELDS; GROUNDWATER FLOW; THREE DIMENSIONAL; TURBULENCE MODELS; VORTEX FLOW;

NAVIER STOKES EQUATIONS;

EID: 78149422259     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

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