Improvement of delayed-detached eddy simulation applied to separated flow over missile fin

AIAA Journal

Volumn 47, Issue 2, 2009, Pages 345-360

  Riou, Jacques ^a,b   Garnier, Eric ^a,b   Deck, Sébastien ^a,b   Basdevan, Claude ^b,c  

^a ONERA   (France)

^b UNIVERSITÉ PARIS 13   (France)

^c Laboratoire Analyse   (France)

Author keywords

[No Author keywords available]

Indexed keywords

BACKWARD FACING STEPS; BOUNDARY-LAYER FLOWS; COMPUTATIONAL SIMULATIONS; DELAYED-DETACHED EDDY SIMULATIONS; EDDY SIMULATION METHODS; EDDY VISCOSITIES; EXPERIMENTAL DATUM; LARGE EDDIES; LEADING-EDGE VORTICES; MISSILE FINS; PRESSURE SENSITIVE PAINTS; REYNOLDS; REYNOLDS AVERAGED NAVIER-STOKES; SEPARATED FLOWS;

AERODYNAMICS; ANGLE OF ATTACK; BOUNDARY LAYER FLOW; FINS (HEAT EXCHANGE); FLOW SEPARATION; LARGE EDDY SIMULATION; MISSILES; SYSTEMS ENGINEERING; TRANSIENTS; VORTEX FLOW;

FLOW SIMULATION;

EID: 60149111579     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/1.37742     Document Type: Article

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