############################################################ # # TA1 External Aerodynamics AC5 Ahmed Body Partner 15 University of Poitiers # # CFD11 # CFX Germany (Kuntz, Menter, Durand) # slant - angle = 25 degree # # Turbulence model : SST # Integration down to the wall # CFX5, incompressible # Block structured # 1.3M nodes, stilts ommited # # Results in the boundary layer in the symmetry plane (y=0) # Data at the location x=-223 mm # # M. Kuntz, F. Menter, L. Durand # CFX Germany # # Origin of coordinate system: x=0: end of the car, y=0: symmetry plane, z=0: ground plane # # Kinematic viscosity of air: 15x10-6 m2 s-1 # Bulk velocity: Ub=40 m s-1 # Height of the body: h=288 mm # Reynolds number based on the height of the body: Re=768,000 # Reynolds number based on the length of the body: Re=2.78x10^6 # ############################################################ %AC = 1-05 %Column1Name = x %Column1Units = mm %Column1Type = Real %Column2Name = y %Column2Units = mm %Column2Type = Real %Column3Name = z %Column3Units = mm %Column3Type = Real %Column4Name = U %Column4Units = m s-1 %Column4Type = Real %Column5Name = V %Column5Units = m s-1 %Column5Type = Real %Column6Name = W %Column6Units = m s-1 %Column6Type = Real %Column7Name = k %Column7Units = m2 s-2 %Column7Type = Real %Column8Name = u_rms %Column8Units = m s-1 %Column8Type = Real %Column9Name = v_rms %Column9Units = m s-1 %Column9Type = Real %Column10Name = w_rms %Column10Units = m s-1 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