# Steenbergen Pipe Flow with Swirl Data # Wall Jet Case, Re=300,000 # # Reynolds Stresses # x/D= 28.1 # # r/R uu/Ub^2 vv/Ub^2 ww/Ub^2 uv/Ub^2 uw/Ub^2 vw/Ub^2 -0.97000 0.007117 0.001330 0.004698 -0.00025 0.001436 -0.00041 -0.95999 0.006873 0.001411 0.004464 -0.00036 0.001251 -0.00047 -0.94999 0.006720 0.001458 0.004337 -0.00059 0.001098 -0.00050 -0.93000 0.005872 0.001568 0.003772 -0.00063 0.000877 -0.00052 -0.91000 0.005114 0.001492 0.003384 -0.00058 0.000790 -0.00056 -0.88999 0.004582 0.001599 0.002972 -0.00064 0.000585 -0.00046 -0.87 0.003930 0.001552 0.002803 -0.00059 0.000442 -0.00034 -0.85000 0.003548 0.001682 0.002595 -0.00061 0.000406 -0.00029 -0.80000 0.002736 0.001713 0.002469 -0.00050 0.000319 -0.00023 -0.75 0.002063 0.001883 0.002367 -0.00042 0.000188 -0.00001 -0.69999 0.001866 0.002083 0.002429 -0.00037 0.000129 0.000085 -0.64999 0.001681 0.002369 0.002480 -0.00025 0.000124 0.000116 -0.60000 0.001591 0.002502 0.002597 -0.00025 0.000068 0.000190 -0.55000 0.001624 0.002636 0.002727 -0.00023 0.000079 0.000212 -0.5 0.001576 0.002784 0.002597 -0.00018 0.000071 0.000139 -0.44999 0.001641 0.002737 0.002682 -0.00020 0.000120 0.000174 -0.40000 0.001683 0.002625 0.002530 -0.00015 0.000196 0.000038 -0.34999 0.001768 0.002614 0.002471 -0.00019 0.000206 0.000062 -0.30000 0.001774 0.002394 0.002189 -0.00022 0.000230 -0.00001 -0.25 0.001872 0.002297 0.002121 -0.00023 0.000269 -0.00009 -0.2 0.001730 0.002144 0.002061 -0.00024 0.000242 -0.00001 -0.15000 0.001635 0.002052 0.001861 -0.00018 0.000269 -0.00003 -0.1 0.001487 0.002051 0.001821 -0.00017 0.000227 -0.00000 -0.05000 0.001422 0.001969 0.001801 -0.00011 0.000232 0.000088 0 0.001307 0.001996 0.001690 -0.00009 0.000183 0.000014 0.050000 0.001261 0.001998 0.001755 0.000010 0.000226 0.000022 0.1 0.001245 0.001990 0.001793 0.000052 0.000200 0.000064 0.150000 0.001310 0.002037 0.001852 0.000158 0.000206 0.000050 0.2 0.001394 0.002171 0.001891 0.000247 0.000213 0.000069 0.25 0.001548 0.002168 0.002006 0.000263 0.000153 -0.00003 0.300000 0.001735 0.002269 0.002052 0.000370 0.000152 0.000001 0.349999 0.001916 0.002370 0.002066 0.000455 0.000112 -0.00013 0.400000 0.002230 0.002401 0.002110 0.000429 -0.00004 -0.00021 0.449999 0.002441 0.002524 0.002139 0.000592 0.000047 -0.00003 0.5 0.002857 0.002499 0.002260 0.000729 0.000022 -0.00011 0.550000 0.003257 0.002446 0.002171 0.000752 -0.00006 -0.00017 0.600000 0.003661 0.002355 0.002245 0.000821 0.000001 -0.00005 0.649999 0.004372 0.002362 0.002408 0.001033 0.000037 -0.00011 0.699999 0.004914 0.002209 0.002327 0.001100 0.000110 -0.00024 0.75 0.005662 0.002099 0.002441 0.001124 0.000104 -0.00029 0.800000 0.006741 0.001945 0.002976 0.001233 0.000133 -0.00034 0.850000 0.007682 0.001656 0.003815 0.001200 0.000056 -0.00026 0.87 0.008053 0.001645 0.003945 0.001145 -0.00000 -0.00026 0.889999 0.008576 0.001689 0.004120 0.001163 -0.00008 -0.00042 0.910000 0.009085 0.001550 0.004575 0.001099 -0.00020 -0.00031 0.930000 0.009063 0.001354 0.005017 0.000949 -0.00039 -0.00006 0.949999 0.009876 0.001500 0.004971 0.000781 -0.00074 -0.00033 0.959999 0.010112 0.001672 0.004951 0.000806 -0.00082 -0.00048 0.970000 0.009679 0.001609 0.005086 0.000677 -0.00093 -0.00041