Analysis of delta wing vortical substructures using detached-eddy simulation

32nd AIAA Fluid Dynamics Conference and Exhibit

Volumn , Issue , 2002, Pages

  Mitchell, Anthony ^a   Morton, Scott ^a   Forsythe, James ^a  

^a UNITED STATES AIR FORCE ACADEMY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTATIONAL RESULTS; DETACHED EDDY SIMULATIONS; HIGH ANGLE OF ATTACK; HIGH REYNOLDS NUMBER; HYBRID RANS-LES METHODS; LASER DOPPLER VELOCIMETRY; LEADING-EDGE VORTICES; VORTICAL STRUCTURES;

ANGLE OF ATTACK INDICATORS; DELTA WING AIRCRAFT; REYNOLDS NUMBER; SHEAR FLOW; TURBULENCE MODELS;

FLOW FIELDS;

EID: 84896823858     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

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