# Steenbergen Pipe Flow with Swirl Data # Wall Jet Case, Re=50,000 # # Reynolds Stresses # x/D= 55.2 # # r/R uu/Ub^2 vv/Ub^2 ww/Ub^2 uv/Ub^2 uw/Ub^2 vw/Ub^2 -0.97000 0.011946 0.002221 0.004520 -0.00111 0.000793 -0.00006 -0.95999 0.010567 0.002189 0.004518 -0.00110 0.000665 -0.00018 -0.94999 0.009790 0.002319 0.004388 -0.00116 0.000616 -0.00018 -0.93000 0.009100 0.002355 0.004148 -0.00122 0.000565 -0.00010 -0.91000 0.008419 0.002166 0.003949 -0.00112 0.000555 -0.00006 -0.88999 0.007999 0.002368 0.003590 -0.00106 0.000586 -0.00011 -0.87 0.007240 0.002095 0.003392 -0.00093 0.000530 -0.00003 -0.85000 0.006966 0.002043 0.003163 -0.00095 0.000512 -0.00009 -0.80000 0.006226 0.001753 0.002742 -0.00061 0.000576 -0.00005 -0.75 0.005449 0.001664 0.002478 -0.00047 0.000622 0.000062 -0.69999 0.004326 0.001615 0.002196 -0.00031 0.000570 0.000132 -0.64999 0.003952 0.001580 0.002107 -0.00019 0.000612 0.000121 -0.60000 0.003426 0.001684 0.001943 -0.00012 0.000633 0.000114 -0.55000 0.003393 0.001664 0.002062 -0.00002 0.000706 0.000192 -0.5 0.003131 0.001537 0.002110 0.000063 0.000652 0.000230 -0.44999 0.003062 0.001587 0.002134 0.000072 0.000676 0.000245 -0.40000 0.003046 0.001667 0.002161 -0.00005 0.000608 0.000208 -0.34999 0.002876 0.001680 0.002148 -0.00010 0.000548 0.000239 -0.30000 0.002834 0.001723 0.002132 -0.00019 0.000493 0.000202 -0.25 0.002803 0.001659 0.002190 -0.00019 0.000483 0.000154 -0.2 0.002881 0.001755 0.002144 -0.00028 0.000398 0.000157 -0.15000 0.002889 0.001708 0.002136 -0.00034 0.000374 0.000109 -0.1 0.002838 0.001634 0.002123 -0.00037 0.000334 0.000097 -0.05000 0.002868 0.001617 0.002045 -0.00041 0.000277 0.000018 0 0.002839 0.001563 0.001940 -0.00044 0.000248 -0.00000 0.050000 0.002653 0.001584 0.001774 -0.00040 0.000200 -0.00001 0.1 0.002466 0.001443 0.001673 -0.00039 0.000143 -0.00003 0.150000 0.002260 0.001475 0.001517 -0.00039 0.000108 -0.00001 0.2 0.002009 0.001350 0.001437 -0.00029 0.000123 -0.00004 0.25 0.001808 0.001346 0.001307 -0.00030 0.000073 -0.00007 0.300000 0.001658 0.001335 0.001230 -0.00020 0.000053 -0.00008 0.349999 0.001532 0.001275 0.001228 -0.00008 0.000050 -0.00006 0.400000 0.001683 0.001335 0.001191 0.000013 0.000015 -0.00006 0.449999 0.001938 0.001355 0.001284 0.000142 0.000011 -0.00009 0.5 0.002485 0.001489 0.001447 0.000299 -0.00004 -0.00013 0.550000 0.003290 0.001677 0.001601 0.000419 -0.00010 -0.00008 0.600000 0.004088 0.001913 0.001886 0.000611 -0.00014 -0.00015 0.649999 0.005115 0.001902 0.002265 0.000771 -0.00008 -0.00015 0.699999 0.006275 0.002288 0.002663 0.000887 -0.00018 -0.00016 0.75 0.007179 0.002359 0.003021 0.001051 -0.00016 -0.00020 0.800000 0.007901 0.002527 0.003459 0.001198 -0.00017 -0.00020 0.850000 0.008815 0.002715 0.003849 0.001227 -0.00027 -0.00030 0.87 0.009457 0.002750 0.004076 0.001313 -0.00029 -0.00021 0.889999 0.009560 0.002900 0.004211 0.001341 -0.00025 -0.00016 0.910000 0.010054 0.003003 0.004290 0.001278 -0.00031 -0.00000 0.930000 0.010524 0.002749 0.004409 0.001220 -0.00043 -0.00031 0.949999 0.011773 0.002854 0.004759 0.001367 -0.00038 -0.00019 0.959999 0.012998 0.003126 0.004701 0.001424 -0.00045 -0.00011