############################################################ # # 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=-183 # # 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 -183.000 0.000 329.600 -9.080 5.836 6.138 5.062 -18.140 315.626 -159.637 -168.952 132.600 -183.000 0.000 330.600 -7.259 4.741 8.017 7.033 -32.575 680.147 -388.450 -391.428 328.881 -183.000 0.000 331.600 -1.789 2.362 11.118 9.253 -67.396 1125.566 -535.524 -640.790 496.372 -183.000 0.000 332.600 6.961 -1.305 13.088 10.397 -92.289 353.164 -181.131 -218.355 158.745 -183.000 0.000 333.600 16.131 -4.292 13.899 10.449 -98.048 -622.969 267.617 306.802 -316.352 -183.000 0.000 334.600 25.767 -6.362 12.880 9.110 -78.698 -1311.631 433.486 629.895 -516.993 -183.000 0.000 335.600 36.816 -7.292 10.739 7.284 -51.461 -1406.659 448.318 683.602 -538.121 -183.000 0.000 336.600 44.050 -7.317 7.443 5.399 -26.321 -829.931 265.624 404.670 -299.968 -183.000 0.000 337.600 47.523 -7.159 4.719 4.121 -11.900 -269.612 142.029 164.760 -132.073 -183.000 0.000 338.600 48.883 -6.989 3.303 3.302 -5.844 -72.614 60.907 49.673 -41.296 -183.000 0.000 339.600 49.585 -6.992 2.665 2.898 -3.948 -20.299 28.885 15.529 -14.022 -183.000 0.000 340.600 49.945 -6.962 2.332 2.584 -2.954 -9.222 10.385 6.153 -4.671 -183.000 0.000 341.600 50.147 -6.878 2.156 2.405 -2.634 -6.290 7.032 3.926 -3.640 -183.000 0.000 342.600 50.415 -6.802 1.978 2.203 -2.223 -4.675 4.105 2.840 -2.911 -183.000 0.000 343.600 50.589 -6.691 1.894 2.121 -2.174 -4.743 3.230 2.528 -2.664 -183.000 0.000 344.600 50.725 -6.695 1.803 2.031 -1.903 -3.976 2.997 1.958 -2.396 -183.000 0.000 345.600 50.824 -6.660 1.763 1.953 -1.840 -3.924 2.027 1.896 -1.559 -183.000 0.000 346.000 50.996 -6.662 1.713 1.843 -1.754 -3.971 1.226 1.814 -1.308 -183.000 0.000 348.000 51.498 -6.695 1.344 1.599 -1.203 -2.678 0.870 1.310 -1.046 -183.000 0.000 353.000 51.570 -6.628 0.689 1.168 -0.492 -0.156 0.000 0.132 -0.105 -183.000 0.000 358.000 50.975 -6.565 0.531 0.925 -0.289 -0.025 -0.088 0.010 0.003 -183.000 0.000 363.000 50.416 -6.465 0.456 0.796 -0.191 -0.038 -0.022 0.025 -0.021 -183.000 0.000 373.000 49.400 -6.243 0.415 0.617 -0.104 -0.012 -0.005 0.011 -0.009 -183.000 0.000 388.000 48.226 -5.838 0.357 0.455 -0.040 -0.028 0.002 0.010 -0.004