Hybrid LES / RANS simulation of a Mach 5 compression- Corner interaction

46th AIAA Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 2008, Pages

  Edwards, Jack R ^a   Choi, Jung Il ^a   Boles, John A ^a  

^a North Carolina State University   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

BOUNDARY LAYERS; COMPUTATION THEORY; FLOW STRUCTURE; NAVIER STOKES EQUATIONS; REYNOLDS NUMBER; SHOCK WAVES; TURBULENT FLOW;

COMPUTATIONAL RESULTS; COUNTER-ROTATING VORTICES; LOW AND HIGH FREQUENCIES; MEAN FLOW STRUCTURES; REYNOLDS AVERAGED MODELS; REYNOLDS STRESS DISTRIBUTION; SHOCK INDUCED SEPARATION; SHOCK WAVE OSCILLATION;

FORECASTING;

EID: 78149452808     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2008-718     Document Type: Conference Paper

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