Detached-eddy simulations of a 70 degree delta wing in the onera F2 wind tunnel

ECCOMAS 2004 - European Congress on Computational Methods in Applied Sciences and Engineering

Volumn , Issue , 2004, Pages

  Morton, Scott A ^a  

^a UNITED STATES AIR FORCE ACADEMY   (United States)

Author keywords

Delta wings; Detached eddy simulation; Large eddy simulation; Vortex breakdown; Vortical flows

Indexed keywords

DELTA WINGS; DETACHED EDDY SIMULATIONS; HIGH REYNOLDS NUMBER; HYBRID RANS-LES METHODS; LAMINAR TO TURBULENT TRANSITIONS; TURBULENT KINETIC ENERGY; VORTEX BREAKDOWN; VORTICAL FLOWS;

ANGLE OF ATTACK INDICATORS; CIRCULAR CYLINDERS; COMPUTATIONAL FLUID DYNAMICS; COMPUTATIONAL METHODS; FLOW FIELDS; KINETICS; LANDING GEAR (AIRCRAFT); LARGE EDDY SIMULATION; REYNOLDS NUMBER; WIND TUNNELS;

DELTA WING AIRCRAFT;

EID: 84893491228     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (16)

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