Discrete conservation principles in large-eddy simulation with application to separation control over an airfoil

Physics of Fluids

Volumn 20, Issue 10, 2008, Pages

  You, Donghyun ^a   Ham, Frank ^a   Moin, Parviz ^a  

^a STANFORD UNIVERSITY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRFOILS; ANGLE OF ATTACK; FIGHTER AIRCRAFT; FINITE VOLUME METHOD; FLOW SEPARATION; JETS; KINETIC ENERGY; KINETICS; LOCATION; NAVIER STOKES EQUATIONS; REYNOLDS NUMBER; SHEAR FLOW;

CONSERVATION PRINCIPLES; FINITE VOLUME DISCRETIZATIONS; FREE-STREAM VELOCITY; HIGH REYNOLDS NUMBER; INCOMPRESSIBLE NAVIER STOKES EQUATIONS; LARGE EDDY SIMULATION TECHNIQUES; MOMENTUM CONSERVATIONS; SEPARATED SHEAR LAYERS;

LARGE EDDY SIMULATION;

EID: 55849122245     PISSN: 10706631     EISSN: None     Source Type: Journal    
DOI: 10.1063/1.3006077     Document Type: Conference Paper

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