# Steenbergen Pipe Flow with Swirl Data # Wall Jet Case, Re=300,000 # # 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 0.007667 0.001393 0.003457 -0.00028 0.001104 -0.00028 -0.95999 0.007518 0.001421 0.003333 -0.00040 0.000978 -0.00036 -0.94999 0.007391 0.001388 0.003190 -0.00051 0.000861 -0.00026 -0.93000 0.006800 0.001463 0.003008 -0.00055 0.000788 -0.00033 -0.91000 0.006071 0.001373 0.002766 -0.00056 0.000684 -0.00024 -0.88999 0.005837 0.001426 0.002617 -0.00059 0.000701 -0.00026 -0.87 0.005048 0.001368 0.002355 -0.00044 0.000580 -0.00020 -0.85000 0.004701 0.001416 0.002284 -0.00053 0.000509 -0.00021 -0.80000 0.003860 0.001302 0.002045 -0.00043 0.000424 -0.00008 -0.75 0.002942 0.001295 0.001896 -0.00036 0.000381 -0.00002 -0.69999 0.002496 0.001359 0.001876 -0.00023 0.000383 0.000006 -0.64999 0.002022 0.001370 0.001888 -0.00016 0.000326 0.000023 -0.60000 0.001899 0.001422 0.001912 -0.00015 0.000346 0.000096 -0.55000 0.001664 0.001485 0.001903 -0.00010 0.000326 0.000141 -0.5 0.001662 0.001562 0.001946 -0.00011 0.000269 0.000167 -0.44999 0.001698 0.001653 0.001890 -0.00009 0.000259 0.000148 -0.40000 0.001826 0.001663 0.001950 -0.00014 0.000263 0.000170 -0.34999 0.001943 0.001648 0.001933 -0.00019 0.000237 0.000152 -0.30000 0.002068 0.001637 0.001921 -0.00024 0.000229 0.000087 -0.25 0.002197 0.001661 0.001899 -0.00024 0.000241 0.000124 -0.2 0.002326 0.001692 0.001835 -0.00032 0.000238 0.000027 -0.15000 0.002314 0.001611 0.001808 -0.00030 0.000225 0.000057 -0.1 0.002313 0.001607 0.001745 -0.00030 0.000219 0.000006 -0.05000 0.002236 0.001523 0.001699 -0.00034 0.000198 -0.00001 0 0.002119 0.001482 0.001602 -0.00034 0.000159 -0.00001 0.050000 0.001872 0.001465 0.001515 -0.00032 0.000143 -0.00003 0.1 0.001662 0.001416 0.001454 -0.00027 0.000137 -0.00008 0.150000 0.001423 0.001383 0.001355 -0.00024 0.000101 -0.00004 0.2 0.001234 0.001278 0.001298 -0.00022 0.000062 -0.00004 0.25 0.001099 0.001222 0.001249 -0.00015 0.000026 -0.00005 0.300000 0.001094 0.001188 0.001178 -0.00009 0.000031 -0.00003 0.349999 0.001015 0.001197 0.001150 -0.00003 -0.00001 -0.00008 0.400000 0.001110 0.001159 0.001150 -0.00000 -0.00001 -0.00005 0.449999 0.001325 0.001207 0.001158 0.000092 -0.00006 -0.00009 0.5 0.001522 0.001135 0.001168 0.000141 -0.00006 -0.00003 0.550000 0.001876 0.001178 0.001275 0.000205 -0.00010 -0.00010 0.600000 0.002406 0.001218 0.001386 0.000342 -0.00011 -0.00012 0.649999 0.003173 0.001291 0.001544 0.000487 -0.00011 -0.00013 0.699999 0.004010 0.001370 0.001762 0.000576 -0.00013 -0.00018 0.75 0.004914 0.001461 0.001937 0.000703 -0.00013 -0.00024 0.800000 0.005670 0.001605 0.002257 0.000784 -0.00016 -0.00025 0.850000 0.006648 0.001605 0.002617 0.000786 -0.00026 -0.00026 0.87 0.007053 0.001681 0.002708 0.000854 -0.00035 -0.00026 0.889999 0.007411 0.001635 0.002880 0.000822 -0.00040 -0.00028 0.910000 0.007619 0.001585 0.002961 0.000635 -0.00047 -0.00024 0.930000 0.008302 0.001666 0.003111 0.000722 -0.00058 -0.00039 0.949999 0.008417 0.001614 0.003246 0.000505 -0.00075 -0.00029 0.959999 0.015281 0.031034 -0.00136 0.010719 -0.00025 0.003169 0.970000 0.008419 0.001351 0.003340 0.000309 -0.00070 -0.00022