############################################################ # # 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=-203 # # 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 -203.000 0.000 339.600 45.216 -0.872 3.328 1.612 -3.222 -14.873 1.657 5.241 -2.946 -203.000 0.000 340.600 47.181 -1.398 2.759 1.503 -2.582 -7.059 0.432 2.279 -1.096 -203.000 0.000 341.600 48.118 -1.704 2.454 1.463 -2.342 -4.466 0.464 1.619 -0.924 -203.000 0.000 342.600 48.653 -1.923 2.270 1.432 -2.202 -3.849 0.258 1.572 -1.127 -203.000 0.000 343.600 49.105 -2.201 2.121 1.389 -2.069 -4.368 0.388 1.836 -1.040 -203.000 0.000 345.600 49.869 -2.564 1.843 1.254 -1.682 -3.377 0.304 1.406 -0.940 -203.000 0.000 347.600 50.363 -2.870 1.617 1.142 -1.414 -2.996 0.575 1.161 -0.974 -203.000 0.000 349.600 50.527 -3.147 1.519 1.089 -1.285 -3.541 0.604 1.465 -1.237 -203.000 0.000 351.600 50.721 -3.359 1.332 1.035 -1.081 -3.374 0.846 1.417 -1.309 -203.000 0.000 353.600 50.800 -3.568 1.120 0.912 -0.796 -2.628 0.794 1.134 -1.096 -203.000 0.000 355.600 50.695 -3.752 0.934 0.810 -0.563 -1.680 0.513 0.729 -0.689 -203.000 0.000 357.600 50.578 -3.894 0.809 0.704 -0.404 -1.174 0.105 0.450 -0.407 -203.000 0.000 359.600 50.524 -4.010 0.678 0.628 -0.285 -0.470 0.023 0.216 -0.218 -203.000 0.000 361.600 50.401 -4.121 0.574 0.577 -0.212 -0.113 0.061 0.099 -0.067 -203.000 0.000 363.000 50.280 -4.185 0.513 0.533 -0.162 -0.038 0.012 0.012 0.000 -203.000 0.000 373.000 49.329 -4.415 0.450 0.461 -0.104 -0.011 0.016 0.006 -0.004 -203.000 0.000 388.000 48.223 -4.465 0.373 0.386 -0.050 -0.032 0.018 0.013 -0.006