############################################################ # # TA1 External Aerodynamics AC5 Ahmed Body Partner 15 University of Poitiers # # Measurements MOVA- project : Ahmed Car Model # slant - angle = 35 degree # # Hot wire measurements in the boundary layer in the symmetry plane (y=0) # (Only u-w components) # # Data at the location x=-23 # # 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 -23.000 0.000 228.000 2.411 -1.690 3.116 2.169 -4.592 -45.946 9.949 23.610 -15.458 -23.000 0.000 229.000 2.227 -1.509 3.394 2.337 -3.714 -53.048 26.580 19.097 -11.626 -23.000 0.000 231.000 1.900 -1.128 3.856 2.573 -5.105 -78.308 16.197 32.340 -23.345 -23.000 0.000 233.000 1.323 -0.680 4.333 2.695 -6.196 -98.573 18.394 40.020 -27.189 -23.000 0.000 235.000 0.847 -0.190 4.772 2.878 -7.137 -124.366 20.596 46.047 -30.553 -23.000 0.000 237.000 0.304 0.172 4.963 3.000 -7.284 -121.834 20.965 44.500 -31.098 -23.000 0.000 239.000 -0.028 0.549 5.156 3.166 -8.685 -116.441 21.889 47.335 -32.539 -23.000 0.000 241.000 -0.571 1.021 5.281 3.312 -9.706 -110.616 28.205 50.466 -37.475 -23.000 0.000 243.000 -1.076 1.503 5.382 3.397 -9.802 -88.166 20.722 34.841 -27.594 -23.000 0.000 245.000 -1.185 1.776 5.343 3.404 -9.415 -77.112 21.645 30.468 -27.368 -23.000 0.000 248.000 -1.687 2.376 5.204 3.481 -8.965 -41.507 15.796 18.362 -19.560 -23.000 0.000 253.000 -2.429 3.089 5.060 3.506 -8.151 -15.835 13.945 9.126 -13.933 -23.000 0.000 258.000 -3.258 3.844 4.683 3.559 -6.727 2.149 7.040 3.789 -11.377 -23.000 0.000 263.000 -3.865 4.308 4.268 3.683 -5.115 13.406 9.477 0.950 -8.810 -23.000 0.000 268.000 -4.519 4.518 3.815 3.668 -3.313 14.571 0.753 1.454 -4.247 -23.000 0.000 273.000 -4.992 4.344 3.353 3.837 -1.451 8.494 -11.469 -0.221 -6.208 -23.000 0.000 278.000 -5.330 4.147 3.133 3.997 -0.807 5.474 -22.602 1.722 -2.534 -23.000 0.000 283.000 -5.588 3.858 3.025 4.046 -0.407 2.430 -16.924 -2.697 0.350 -23.000 0.000 293.000 -4.934 2.689 3.688 4.405 -2.768 31.147 -48.913 -30.119 25.561 -23.000 0.000 303.000 -0.785 0.703 5.928 5.626 -15.129 102.414 -108.690 -83.177 68.199 -23.000 0.000 313.000 9.132 -2.185 7.155 6.492 -23.452 -47.836 -6.919 18.346 -19.779 -23.000 0.000 323.000 21.142 -3.816 7.143 6.276 -22.934 -69.286 51.135 50.802 -48.828 -23.000 0.000 333.000 34.445 -4.764 5.742 4.671 -13.191 -184.285 86.522 85.391 -75.627 -23.000 0.000 343.000 41.961 -4.870 2.332 2.272 -1.707 -15.711 15.684 8.968 -8.324 -23.000 0.000 353.000 43.895 -4.895 0.999 1.113 -0.131 -0.441 1.226 0.452 -0.221 -23.000 0.000 363.000 43.948 -4.783 0.589 0.628 0.004 -0.083 0.163 0.033 -0.003 -23.000 0.000 373.000 43.795 -4.583 0.478 0.474 0.005 -0.089 0.061 0.006 -0.003 -23.000 0.000 388.000 43.604 -4.267 0.427 0.408 0.013 -0.073 0.037 -0.002 0.002