############################################################ # # TA1 External Aerodynamics AC5 Ahmed Body Partner 15 University of Poitiers # # Measurements MOVA- project : Ahmed Car Model # slant - angle = 25 degree # # Hot wire measurements in the boundary layer in the symmetry plane (y=0) # (Only u-w components) # # Data at the location x=-223 # # H. Lienhart/Th. Schenk # Institute of Fluid Mechanics # University Erlangen-Nuremberg # # 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 # ############################################################ %AC = 1-05 %Column1Name = x %Column1Units = m %Column1Type = Real %Column2Name = y %Column2Units = m %Column2Type = Real %Column3Name = z %Column3Units = m %Column3Type = Real %Column4Name = U %Column4Units = m s-1 %Column4Type = Real %Column5Name = W %Column5Units = m s-1 %Column5Type = Real %Column6Name = u_rms %Column6Units = m s-1 %Column6Type = Real %Column7Name = w_rms %Column7Units = m s-1 %Column7Type = Real %Column8Name = uw %Column8Units = m2 s-2 %Column8Type = Real %Column9Name = uuu %Column9Units = m3 s-3 %Column9Type = Real %Column10Name = www %Column10Units = m3 s-3 %Column10Type = Real %Column11Name = uuw %Column11Units = m3 s-3 %Column11Type = Real %Column12Name = uww %Column12Units = m3 s-3 %Column12Type = Real %End Of Metadata -223.000 0.000 339.700 38.375 0.251 3.364 1.954 -2.830 -8.599 2.108 4.012 -2.341 -223.000 0.000 340.700 40.929 -0.062 2.983 1.866 -2.362 -7.945 1.457 3.471 -1.734 -223.000 0.000 341.700 42.532 -0.298 2.748 1.822 -2.159 -7.453 1.333 2.740 -1.471 -223.000 0.000 342.700 43.745 -0.516 2.517 1.762 -1.900 -5.062 1.344 2.002 -1.424 -223.000 0.000 343.700 44.674 -0.663 2.395 1.724 -1.790 -5.678 1.506 2.042 -1.385 -223.000 0.000 345.700 46.231 -0.955 2.110 1.592 -1.471 -4.902 1.632 1.956 -1.564 -223.000 0.000 347.700 47.514 -1.248 1.800 1.400 -1.045 -4.012 1.316 1.586 -1.346 -223.000 0.000 349.700 48.483 -1.453 1.549 1.229 -0.792 -3.999 1.326 1.513 -1.276 -223.000 0.000 351.700 49.259 -1.652 1.218 1.013 -0.475 -2.637 0.974 0.971 -0.908 -223.000 0.000 353.700 49.689 -1.839 0.879 0.804 -0.236 -1.268 0.559 0.502 -0.439 -223.000 0.000 355.700 49.866 -2.030 0.652 0.623 -0.107 -0.465 0.275 0.185 -0.159 -223.000 0.000 357.700 49.848 -2.196 0.546 0.499 -0.051 -0.168 0.128 0.068 -0.036 -223.000 0.000 359.700 49.749 -2.366 0.498 0.416 -0.035 -0.111 0.027 0.017 0.003 -223.000 0.000 361.700 49.572 -2.502 0.492 0.387 -0.030 -0.102 0.024 0.012 0.000 -223.000 0.000 363.700 49.445 -2.637 0.462 0.367 -0.028 -0.079 0.015 0.012 -0.002