High Reynolds number des simulations of vortex breakdown over a 70 degree delta wing

21st AIAA Applied Aerodynamics Conference

Volumn , Issue , 2003, Pages

  Morton, Scott ^a  

^a UNITED STATES AIR FORCE ACADEMY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ANGLE OF ATTACK; ANGLE OF ATTACK INDICATORS; CIRCULAR CYLINDERS; COMPUTATIONAL FLUID DYNAMICS; FIGHTER AIRCRAFT; FLOW FIELDS; FLOW SEPARATION; KINETIC ENERGY; KINETICS; REYNOLDS NUMBER; TURBULENT FLOW; VORTEX FLOW; WIND TUNNELS;

ADAPTIVE MESH REFINEMENT; DETACHED EDDY SIMULATIONS; HIGH ANGLE OF ATTACK; HIGH REYNOLDS NUMBER; HYBRID RANS-LES METHODS; LAMINAR TO TURBULENT TRANSITIONS; TURBULENT KINETIC ENERGY; VORTICAL FLOWFIELDS;

DELTA WING AIRCRAFT;

EID: 85067318342     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2003-4217     Document Type: Conference Paper

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