Detached-eddy simulation of fighter aircraft at high alpha

40th AIAA Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 2002, Pages

  Forsythe, James R ^a   Squires, Kyle D ^b   Wurtzler, Kenneth E ^c   Spalart, Philippe R ^d  

^a UNITED STATES AIR FORCE ACADEMY   (United States)

^b ARIZONA STATE UNIVERSITY   (United States)

^c Cobalt Solution LLC ^*  (United States)

^d BOEING COMPANY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ANGLE OF ATTACK; ANGLE OF ATTACK INDICATORS; BOUNDARY LAYERS; CELLS; CYTOLOGY; DRAG; FLIGHT CONTROL SYSTEMS; FLOW SEPARATION; FORECASTING; MESH GENERATION; REYNOLDS NUMBER; SUPERSONIC AIRCRAFT;

CHORD-BASED REYNOLDS NUMBER; DETACHED EDDY SIMULATIONS; MASSIVELY SEPARATED FLOW; PITCHING MOMENT COEFFICIENTS; REYNOLDS AVERAGED NAVIER STOKES (RANS)EQUATIONS; SPALART-ALLMARAS MODEL; STABILITY AND CONTROL; THREE-DIMENSIONAL STRUCTURE;

NAVIER STOKES EQUATIONS;

EID: 85085403070     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2002-591     Document Type: Conference Paper

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