# Steenbergen Pipe Flow with Swirl Data # Wall Jet Case, Re=300,000 # # Reynolds Stresses # x/D= 96.0 # # r/R uu/Ub^2 vv/Ub^2 ww/Ub^2 uv/Ub^2 uw/Ub^2 vw/Ub^2 -0.97000 0.007784 0.001313 0.002905 -0.00032 0.000642 -0.00009 -0.95999 0.007889 0.001403 0.002880 -0.00042 0.000606 -0.00008 -0.94999 0.007910 0.001489 0.002877 -0.00051 0.000560 -0.00011 -0.93000 0.007804 0.001576 0.002808 -0.00054 0.000503 -0.00009 -0.91000 0.007558 0.001497 0.002716 -0.00058 0.000453 -0.00009 -0.88999 0.007327 0.001545 0.002521 -0.00063 0.000408 -0.00014 -0.87 0.006816 0.001615 0.002329 -0.00062 0.000386 -0.00008 -0.85000 0.006429 0.001570 0.002353 -0.00060 0.000422 -0.00005 -0.80000 0.005715 0.001496 0.002217 -0.00054 0.000373 -0.00002 -0.75 0.005065 0.001466 0.002052 -0.00047 0.000394 -0.00000 -0.69999 0.004511 0.001415 0.001886 -0.00040 0.000387 0.000014 -0.64999 0.004143 0.001404 0.001761 -0.00033 0.000400 -0.00001 -0.60000 0.003770 0.001359 0.001675 -0.00031 0.000401 0.000032 -0.55000 0.003471 0.001341 0.001729 -0.00026 0.000413 0.000110 -0.5 0.003167 0.001320 0.001638 -0.00017 0.000436 0.000098 -0.44999 0.002927 0.001290 0.001700 -0.00017 0.000433 0.000109 -0.40000 0.002730 0.001309 0.001622 -0.00014 0.000456 0.000079 -0.34999 0.002540 0.001341 0.001510 -0.00018 0.000400 0.000081 -0.30000 0.002327 0.001280 0.001531 -0.00011 0.000415 0.000098 -0.25 0.002223 0.001307 0.001539 -0.00016 0.000362 0.000124 -0.2 0.002012 0.001282 0.001410 -0.00017 0.000330 0.000058 -0.15000 0.001951 0.001297 0.001383 -0.00017 0.000329 0.000092 -0.1 0.001740 0.001244 0.001349 -0.00015 0.000291 0.000055 -0.05000 0.001619 0.001207 0.001288 -0.00013 0.000273 0.000047 0 0.001502 0.001190 0.001253 -0.00012 0.000258 0.000036 0.050000 0.001396 0.001186 0.001189 -0.00009 0.000252 0.000022 0.1 0.001293 0.001153 0.001137 -0.00006 0.000233 -0.00000 0.150000 0.001160 0.001137 0.001094 -0.00002 0.000176 0.000027 0.2 0.001115 0.001090 0.001097 0.000006 0.000165 0.000012 0.25 0.001169 0.001102 0.001032 0.000068 0.000139 -0.00003 0.300000 0.001340 0.001131 0.001070 0.000138 0.000114 -0.00003 0.349999 0.001549 0.001146 0.001034 0.000182 0.000064 -0.00008 0.400000 0.001871 0.001165 0.001140 0.000254 0.000073 -0.00008 0.449999 0.002306 0.001200 0.001279 0.000321 0.000039 -0.00008 0.5 0.002811 0.001277 0.001432 0.000412 0.000032 -0.00010 0.550000 0.003394 0.001382 0.001552 0.000496 0.000035 -0.00011 0.600000 0.003970 0.001474 0.001694 0.000590 0.000030 -0.00010 0.649999 0.004595 0.001565 0.001917 0.000701 -0.00000 -0.00011 0.699999 0.005237 0.001634 0.002145 0.000758 0.000009 -0.00009 0.75 0.005838 0.001756 0.002249 0.000864 -0.00001 -0.00009 0.800000 0.006545 0.001821 0.002477 0.000926 -0.00002 -0.00011 0.850000 0.007155 0.001847 0.002743 0.000952 -0.00008 -0.00013 0.87 0.007575 0.001844 0.002648 0.001050 0.000022 -0.00009 0.889999 0.007936 0.001830 0.002828 0.000976 -0.00015 -0.00010 0.910000 0.008422 0.001760 0.002874 0.001000 -0.00014 -0.00008 0.930000 0.008834 0.001718 0.002996 0.000977 -0.00018 -0.00010 0.949999 0.009317 0.001718 0.002912 0.000964 -0.00019 -0.00012 0.959999 0.009254 0.001513 0.003137 0.000866 -0.00021 0.000015 0.970000 0.009139 0.001488 0.003128 0.000808 -0.00026 0.000013