Prediction of a thin-airfoil stall phenomenon using les/rans hybrid methodology with compact difference scheme

34th AIAA Fluid Dynamics Conference and Exhibit

Volumn , Issue , 2004, Pages

  Kawai, Soshi ^a   Fujii, Kozo ^b  

^a UNIVERSITY OF TOKYO   (Japan)

^b JAPAN AEROSPACE EXPLORATION AGENCY   (Japan)

Author keywords

[No Author keywords available]

Indexed keywords

AIRFOILS; ANGLE OF ATTACK; COMPUTATIONAL FLUID DYNAMICS; FLOW SEPARATION; FORECASTING; LAMINAR FLOW; LARGE EDDY SIMULATION; NAVIER STOKES EQUATIONS; NUMERICAL METHODS; REYNOLDS NUMBER; TRANSITION FLOW; TURBULENCE MODELS; VORTEX FLOW;

AERODYNAMIC CHARACTERISTICS; COMPACT DIFFERENCE SCHEME; DIFFERENCING SCHEME; HIGH ORDER COMPACT DIFFERENCE SCHEMES; HIGH REYNOLDS NUMBER; HYBRID METHODOLOGIES; REYNOLDS-AVERAGED NAVIER-STOKES; TIME-AVERAGED FLOW;

AERODYNAMIC STALLING;

EID: 85086613186     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2004-2714     Document Type: Conference Paper

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