ROLLS-ROYCE APPLIED SCIENCE LABORATORY FLAT PLATE TRANSITIONAL BOUNDARY LAYER FLOW HOT WIRE ANEMOMETRY TEST DATA SINGLE WIRE DATA FOR ERCOFTAC T3C1 TEST CASE RUN NUMBER 1W01708 AXIAL POSITION = 5.0 MM SPAN POSITION = 0.0 MM FREE-STREAM VELOCITY = 6.32 M/S FRICTION VELOCITY = 0.4877 M/S FREE-STREAM TURBULENCE = 7.741 % X-REYNOLDS NUMBER = 0.21 X10**4 FLUID DENSITY = 1.188 KG/M**3 KINEMATIC VISCOSITY = 1.523 X10(-5)MSQ/S BOUNDARY LAYER THICKNESS (99.0%) = 0.58 MM DISPLACEMENT THICKNESS = 0.214 MM MOMENTUM THICKNESS = 0.079 MM ENERGY THICKNESS = 0.122 MM FORM FACTOR H = 2.711 FORM FACTOR E = 1.553 RDELTASTAR = 88.8 RTHETA = 32.7 SKIN FRICTION COEFFICIENT = 0.011904 CALCULATED CF = 0.014576 Y Y/DEL YPLUS U U/UO UPLUS u u/UO u/U u/UTAU MM M/S M/S % % 0.029 0.050 0.929 0.476 0.075 0.976 0.0649 1.03 13.62 0.1330 0.035 0.061 1.129 0.579 0.092 1.187 0.0667 1.05 11.52 0.1367 0.042 0.072 1.329 0.681 0.108 1.397 0.0712 1.13 10.44 0.1459 0.048 0.083 1.529 0.784 0.124 1.608 0.0805 1.27 10.27 0.1651 0.054 0.094 1.729 0.887 0.140 1.818 0.0980 1.55 11.05 0.2009 0.060 0.105 1.929 0.989 0.157 2.029 0.1162 1.84 11.74 0.2382 0.067 0.115 2.129 1.092 0.173 2.239 0.1355 2.14 12.41 0.2779 0.073 0.126 2.330 1.195 0.189 2.450 0.1544 2.44 12.92 0.3165 0.079 0.137 2.530 1.297 0.205 2.660 0.1683 2.66 12.98 0.3452 0.085 0.148 2.730 1.400 0.221 2.870 0.1818 2.88 12.99 0.3728 0.092 0.159 2.930 1.503 0.238 3.081 0.2018 3.19 13.43 0.4137 0.098 0.170 3.130 1.612 0.255 3.306 0.2269 3.59 14.07 0.4653 0.104 0.181 3.330 1.701 0.269 3.487 0.2414 3.82 14.20 0.4950 0.110 0.191 3.530 1.800 0.285 3.692 0.2631 4.16 14.61 0.5394 0.117 0.202 3.731 1.867 0.295 3.829 0.2675 4.23 14.33 0.5485 0.123 0.213 3.931 1.961 0.310 4.021 0.2817 4.46 14.37 0.5776 0.129 0.224 4.131 2.018 0.319 4.137 0.3001 4.75 14.87 0.6154 0.135 0.235 4.331 2.125 0.336 4.357 0.3150 4.98 14.83 0.6460 0.142 0.246 4.531 2.238 0.354 4.589 0.3191 5.05 14.26 0.6544 0.148 0.256 4.731 2.331 0.369 4.779 0.3318 5.25 14.23 0.6803 0.154 0.267 4.931 2.432 0.385 4.987 0.3387 5.36 13.93 0.6944 0.160 0.278 5.131 2.518 0.398 5.163 0.3492 5.52 13.87 0.7161 0.167 0.289 5.332 2.615 0.414 5.361 0.3589 5.68 13.73 0.7358 0.173 0.300 5.532 2.705 0.428 5.547 0.3688 5.83 13.63 0.7562 0.179 0.311 5.732 2.795 0.442 5.731 0.3808 6.02 13.62 0.7808 0.185 0.322 5.932 2.888 0.457 5.922 0.3835 6.07 13.28 0.7863 0.192 0.332 6.132 2.997 0.474 6.144 0.4078 6.45 13.61 0.8363 0.198 0.343 6.332 3.077 0.487 6.308 0.4222 6.68 13.72 0.8657 0.204 0.354 6.532 3.189 0.504 6.538 0.4075 6.45 12.78 0.8356 0.210 0.365 6.733 3.256 0.515 6.677 0.4261 6.74 13.09 0.8738 0.217 0.376 6.933 3.360 0.532 6.890 0.4332 6.85 12.89 0.8883 0.223 0.387 7.133 3.446 0.545 7.066 0.4535 7.17 13.16 0.9299 0.229 0.397 7.333 3.572 0.565 7.324 0.4522 7.15 12.66 0.9272 0.248 0.430 7.933 3.864 0.611 7.922 0.4561 7.22 11.80 0.9352 0.267 0.463 8.534 4.144 0.655 8.496 0.4915 7.78 11.86 1.0079 0.285 0.495 9.134 4.440 0.702 9.104 0.4817 7.62 10.85 0.9877 0.304 0.528 9.735 4.708 0.745 9.653 0.4886 7.73 10.38 1.0019 0.323 0.560 10.335 4.941 0.782 10.132 0.4921 7.78 9.96 1.0091 0.348 0.604 11.135 5.214 0.825 10.690 0.5001 7.91 9.59 1.0254 0.367 0.636 11.736 5.393 0.853 11.057 0.4921 7.79 9.13 1.0091 0.392 0.680 12.536 5.604 0.886 11.490 0.4867 7.70 8.69 0.9979 0.423 0.734 13.537 5.814 0.920 11.921 0.4938 7.81 8.49 1.0126 0.448 0.777 14.338 5.901 0.933 12.100 0.4990 7.89 8.46 1.0232 0.479 0.831 15.338 6.033 0.954 12.371 0.4927 7.79 8.17 1.0103 0.510 0.886 16.339 6.120 0.968 12.549 0.4996 7.90 8.16 1.0243 0.548 0.951 17.540 6.203 0.981 12.720 0.5092 8.06 8.21 1.0442 0.579 1.005 18.540 6.290 0.995 12.898 0.5096 8.06 8.10 1.0450 0.617 1.070 19.741 6.301 0.997 12.920 0.5056 8.00 8.02 1.0367 0.654 1.135 20.942 6.307 0.998 12.932 0.5090 8.05 8.07 1.0436 0.685 1.189 21.943 6.339 1.003 12.998 0.4978 7.87 7.85 1.0207 0.960 1.667 30.749 6.344 1.004 13.008 0.4990 7.89 7.86 1.0231 1.235 2.144 39.555 6.321 1.000 12.961 0.4834 7.65 7.65 0.9912 1.510 2.621 48.360 6.337 1.002 12.993 0.4958 7.84 7.82 1.0166 1.785 3.099 57.166 6.333 1.002 12.985 0.4894 7.74 7.73 1.0034 RUN NUMBER 1W01709 AXIAL POSITION = 15.0 MM SPAN POSITION = 0.0 MM FREE-STREAM VELOCITY = 6.51 M/S FRICTION VELOCITY = 0.4351 M/S FREE-STREAM TURBULENCE = 6.592 % X-REYNOLDS NUMBER = 0.64 X10**4 FLUID DENSITY = 1.189 KG/M**3 KINEMATIC VISCOSITY = 1.521 X10(-5)MSQ/S BOUNDARY LAYER THICKNESS (99.0%) = 0.93 MM DISPLACEMENT THICKNESS = 0.303 MM MOMENTUM THICKNESS = 0.119 MM ENERGY THICKNESS = 0.188 MM FORM FACTOR H = 2.545 FORM FACTOR E = 1.579 RDELTASTAR = 129.6 RTHETA = 50.9 SKIN FRICTION COEFFICIENT = 0.008921 CALCULATED CF = 0.008284 Y Y/DEL YPLUS U U/UO UPLUS u u/UO u/U u/UTAU MM M/S M/S % % 0.029 0.031 0.830 0.380 0.058 0.873 0.0365 0.56 9.62 0.0839 0.035 0.038 1.008 0.462 0.071 1.061 0.0380 0.58 8.23 0.0873 0.042 0.044 1.187 0.543 0.083 1.249 0.0425 0.65 7.82 0.0976 0.048 0.051 1.366 0.625 0.096 1.437 0.0477 0.73 7.64 0.1097 0.054 0.058 1.545 0.707 0.109 1.625 0.0575 0.88 8.14 0.1322 0.060 0.065 1.724 0.789 0.121 1.813 0.0677 1.04 8.58 0.1555 0.067 0.071 1.902 0.871 0.134 2.001 0.0782 1.20 8.98 0.1797 0.073 0.078 2.081 0.952 0.146 2.189 0.0912 1.40 9.58 0.2097 0.079 0.085 2.260 1.034 0.159 2.377 0.0998 1.53 9.65 0.2294 0.085 0.091 2.439 1.116 0.171 2.565 0.1116 1.71 10.00 0.2565 0.092 0.098 2.618 1.198 0.184 2.753 0.1226 1.88 10.23 0.2817 0.098 0.105 2.796 1.280 0.196 2.941 0.1324 2.03 10.35 0.3044 0.104 0.111 2.975 1.362 0.209 3.129 0.1449 2.22 10.64 0.3329 0.110 0.118 3.154 1.419 0.218 3.262 0.1570 2.41 11.06 0.3609 0.117 0.125 3.333 1.492 0.229 3.429 0.1669 2.56 11.19 0.3835 0.123 0.132 3.511 1.547 0.237 3.556 0.1723 2.64 11.14 0.3960 0.129 0.138 3.690 1.611 0.247 3.703 0.1796 2.76 11.15 0.4128 0.135 0.145 3.869 1.694 0.260 3.894 0.1897 2.91 11.19 0.4359 0.142 0.152 4.048 1.761 0.270 4.046 0.2012 3.09 11.43 0.4624 0.148 0.158 4.227 1.841 0.283 4.231 0.2060 3.16 11.19 0.4735 0.154 0.165 4.405 1.905 0.292 4.379 0.2160 3.32 11.34 0.4964 0.160 0.172 4.584 1.971 0.303 4.531 0.2239 3.44 11.36 0.5146 0.167 0.178 4.763 2.039 0.313 4.686 0.2344 3.60 11.50 0.5387 0.173 0.185 4.942 2.119 0.325 4.869 0.2397 3.68 11.31 0.5508 0.185 0.198 5.299 2.256 0.346 5.185 0.2593 3.98 11.49 0.5958 0.198 0.212 5.657 2.389 0.367 5.490 0.2797 4.29 11.71 0.6427 0.217 0.232 6.193 2.592 0.398 5.957 0.3122 4.79 12.04 0.7174 0.235 0.252 6.730 2.817 0.432 6.474 0.3269 5.02 11.60 0.7513 0.254 0.272 7.266 3.050 0.468 7.011 0.3530 5.42 11.57 0.8113 0.273 0.292 7.802 3.259 0.500 7.490 0.3801 5.84 11.67 0.8737 0.292 0.312 8.339 3.485 0.535 8.009 0.3998 6.14 11.47 0.9188 0.317 0.339 9.054 3.783 0.581 8.694 0.4172 6.40 11.03 0.9590 0.342 0.366 9.769 4.066 0.624 9.345 0.4385 6.73 10.79 1.0079 0.373 0.399 10.663 4.385 0.673 10.078 0.4534 6.96 10.34 1.0421 0.404 0.433 11.557 4.684 0.719 10.765 0.4682 7.19 10.00 1.0761 0.435 0.466 12.451 4.914 0.754 11.294 0.4831 7.42 9.83 1.1103 0.473 0.507 13.524 5.164 0.793 11.867 0.4752 7.29 9.20 1.0921 0.510 0.547 14.597 5.400 0.829 12.411 0.4767 7.32 8.83 1.0956 0.548 0.587 15.669 5.613 0.862 12.901 0.4861 7.46 8.66 1.1172 0.592 0.634 16.921 5.814 0.892 13.362 0.4832 7.42 8.31 1.1106 0.642 0.687 18.351 6.004 0.922 13.799 0.4699 7.21 7.83 1.0800 0.692 0.741 19.782 6.127 0.940 14.082 0.4742 7.28 7.74 1.0899 0.748 0.801 21.391 6.259 0.961 14.386 0.4765 7.31 7.61 1.0951 0.810 0.868 23.179 6.337 0.973 14.564 0.4748 7.29 7.49 1.0911 0.879 0.942 25.145 6.434 0.988 14.787 0.4699 7.21 7.30 1.0799 0.948 1.015 27.112 6.473 0.994 14.876 0.4670 7.17 7.21 1.0733 1.017 1.089 29.079 6.472 0.993 14.873 0.4598 7.06 7.10 1.0567 1.092 1.169 31.224 6.502 0.998 14.944 0.4608 7.07 7.09 1.0590 1.160 1.243 33.191 6.535 1.003 15.019 0.4591 7.05 7.03 1.0551 1.229 1.317 35.158 6.517 1.000 14.977 0.4528 6.95 6.95 1.0408 1.704 1.826 48.746 6.555 1.006 15.066 0.4452 6.83 6.79 1.0233 2.179 2.335 62.334 6.503 0.998 14.945 0.4367 6.70 6.72 1.0036 2.654 2.844 75.922 6.541 1.004 15.033 0.4271 6.56 6.53 0.9815 3.129 3.353 89.510 6.536 1.003 15.021 0.4294 6.59 6.57 0.9869 RUN NUMBER 1W01710 AXIAL POSITION = 25.0 MM SPAN POSITION = 0.0 MM FREE-STREAM VELOCITY = 6.65 M/S FRICTION VELOCITY = 0.3885 M/S FREE-STREAM TURBULENCE = 6.160 % X-REYNOLDS NUMBER = 1.09 X10**4 FLUID DENSITY = 1.190 KG/M**3 KINEMATIC VISCOSITY = 1.520 X10(-5)MSQ/S BOUNDARY LAYER THICKNESS (99.0%) = 1.25 MM DISPLACEMENT THICKNESS = 0.390 MM MOMENTUM THICKNESS = 0.155 MM ENERGY THICKNESS = 0.246 MM FORM FACTOR H = 2.520 FORM FACTOR E = 1.587 RDELTASTAR = 170.6 RTHETA = 67.7 SKIN FRICTION COEFFICIENT = 0.006833 CALCULATED CF = 0.006350 Y Y/DEL YPLUS U U/UO UPLUS u u/UO u/U u/UTAU MM M/S M/S % % 0.029 0.023 0.741 0.299 0.045 0.770 0.0307 0.46 10.25 0.0789 0.035 0.028 0.901 0.363 0.055 0.935 0.0324 0.49 8.93 0.0835 0.042 0.033 1.061 0.428 0.064 1.101 0.0369 0.56 8.63 0.0951 0.048 0.038 1.221 0.492 0.074 1.267 0.0428 0.64 8.70 0.1102 0.054 0.043 1.380 0.557 0.084 1.433 0.0489 0.74 8.78 0.1258 0.060 0.048 1.540 0.621 0.093 1.599 0.0556 0.84 8.96 0.1432 0.067 0.053 1.700 0.686 0.103 1.765 0.0627 0.94 9.15 0.1614 0.073 0.058 1.860 0.750 0.113 1.931 0.0693 1.04 9.24 0.1783 0.079 0.063 2.019 0.815 0.123 2.096 0.0797 1.20 9.78 0.2051 0.085 0.068 2.179 0.879 0.132 2.262 0.0855 1.29 9.73 0.2201 0.092 0.073 2.339 0.943 0.142 2.428 0.0949 1.43 10.06 0.2443 0.098 0.078 2.499 1.008 0.152 2.594 0.1101 1.66 10.93 0.2834 0.104 0.083 2.658 1.072 0.161 2.760 0.1183 1.78 11.04 0.3046 0.110 0.088 2.818 1.137 0.171 2.926 0.1288 1.94 11.33 0.3314 0.117 0.093 2.978 1.201 0.181 3.092 0.1348 2.03 11.22 0.3468 0.123 0.098 3.138 1.257 0.189 3.235 0.1432 2.15 11.39 0.3685 0.129 0.103 3.298 1.309 0.197 3.369 0.1491 2.24 11.39 0.3836 0.135 0.109 3.457 1.364 0.205 3.509 0.1599 2.41 11.73 0.4115 0.142 0.114 3.617 1.429 0.215 3.677 0.1708 2.57 11.95 0.4396 0.148 0.119 3.777 1.472 0.221 3.789 0.1732 2.61 11.76 0.4457 0.154 0.124 3.937 1.528 0.230 3.932 0.1849 2.78 12.10 0.4758 0.167 0.134 4.256 1.636 0.246 4.210 0.1975 2.97 12.07 0.5083 0.179 0.144 4.576 1.749 0.263 4.501 0.2131 3.21 12.19 0.5486 0.192 0.154 4.895 1.870 0.281 4.814 0.2299 3.46 12.29 0.5917 0.210 0.169 5.374 2.045 0.308 5.262 0.2544 3.83 12.44 0.6548 0.229 0.184 5.854 2.214 0.333 5.697 0.2796 4.21 12.63 0.7197 0.248 0.199 6.333 2.398 0.361 6.172 0.2950 4.44 12.30 0.7593 0.273 0.219 6.972 2.637 0.397 6.788 0.3271 4.92 12.40 0.8419 0.298 0.239 7.611 2.893 0.435 7.445 0.3625 5.45 12.53 0.9331 0.323 0.259 8.250 3.139 0.472 8.079 0.3879 5.84 12.36 0.9984 0.348 0.279 8.889 3.378 0.508 8.694 0.4066 6.12 12.04 1.0464 0.379 0.304 9.688 3.647 0.549 9.386 0.4291 6.45 11.77 1.1043 0.417 0.334 10.647 3.979 0.599 10.240 0.4753 7.15 11.95 1.2234 0.448 0.359 11.446 4.241 0.638 10.915 0.4853 7.30 11.44 1.2491 0.492 0.394 12.564 4.558 0.686 11.730 0.5016 7.55 11.01 1.2910 0.529 0.424 13.522 4.826 0.726 12.420 0.4975 7.48 10.31 1.2804 0.579 0.465 14.801 5.126 0.771 13.192 0.5086 7.65 9.92 1.3091 0.629 0.505 16.079 5.406 0.813 13.914 0.5180 7.79 9.58 1.3333 0.685 0.550 17.517 5.671 0.853 14.596 0.5033 7.57 8.87 1.2952 0.742 0.595 18.954 5.889 0.886 15.157 0.4979 7.49 8.46 1.2815 0.810 0.650 20.712 6.067 0.913 15.615 0.4897 7.37 8.07 1.2604 0.879 0.705 22.469 6.232 0.937 16.038 0.4731 7.12 7.59 1.2175 0.954 0.765 24.386 6.359 0.957 16.365 0.4723 7.11 7.43 1.2156 1.035 0.831 26.463 6.457 0.971 16.618 0.4656 7.00 7.21 1.1984 1.129 0.906 28.860 6.522 0.981 16.785 0.4615 6.94 7.08 1.1877 1.229 0.986 31.416 6.573 0.989 16.916 0.4508 6.78 6.86 1.1602 1.323 1.061 33.813 6.616 0.995 17.027 0.4512 6.79 6.82 1.1612 1.423 1.141 36.369 6.638 0.999 17.085 0.4465 6.72 6.73 1.1492 1.523 1.222 38.925 6.655 1.001 17.129 0.4366 6.57 6.56 1.1236 1.623 1.302 41.481 6.652 1.001 17.121 0.4432 6.67 6.66 1.1406 2.235 1.793 57.138 6.652 1.001 17.120 0.4272 6.43 6.42 1.0994 2.848 2.285 72.795 6.652 1.001 17.119 0.4063 6.11 6.11 1.0457 3.467 2.781 88.612 6.648 1.000 17.110 0.4142 6.23 6.23 1.0660 4.079 3.273 104.269 6.665 1.003 17.153 0.4095 6.16 6.14 1.0538 RUN NUMBER 1W01601 AXIAL POSITION = 45.0 MM SPAN POSITION = 0.0 MM FREE-STREAM VELOCITY = 6.87 M/S FRICTION VELOCITY = 0.3512 M/S FREE-STREAM TURBULENCE = 5.791 % X-REYNOLDS NUMBER = 2.05 X10**4 FLUID DENSITY = 1.200 KG/M**3 KINEMATIC VISCOSITY = 1.508 X10(-5)MSQ/S BOUNDARY LAYER THICKNESS (99.0%) = 1.64 MM DISPLACEMENT THICKNESS = 0.490 MM MOMENTUM THICKNESS = 0.198 MM ENERGY THICKNESS = 0.318 MM FORM FACTOR H = 2.471 FORM FACTOR E = 1.603 RDELTASTAR = 223.0 RTHETA = 90.2 SKIN FRICTION COEFFICIENT = 0.005233 CALCULATED CF = 0.004638 Y Y/DEL YPLUS U U/UO UPLUS u u/UO u/U u/UTAU MM M/S M/S % % 0.029 0.018 0.676 0.238 0.035 0.677 0.0290 0.42 12.19 0.0825 0.035 0.021 0.821 0.289 0.042 0.823 0.0290 0.42 10.04 0.0826 0.042 0.025 0.967 0.340 0.050 0.968 0.0315 0.46 9.27 0.0898 0.048 0.029 1.112 0.391 0.057 1.114 0.0359 0.52 9.18 0.1023 0.054 0.033 1.258 0.443 0.064 1.260 0.0379 0.55 8.56 0.1078 0.060 0.037 1.404 0.494 0.072 1.406 0.0449 0.65 9.08 0.1277 0.067 0.041 1.549 0.545 0.079 1.552 0.0504 0.73 9.24 0.1434 0.073 0.044 1.695 0.596 0.087 1.698 0.0575 0.84 9.64 0.1637 0.079 0.048 1.840 0.648 0.094 1.844 0.0638 0.93 9.85 0.1815 0.085 0.052 1.986 0.699 0.102 1.989 0.0719 1.05 10.29 0.2047 0.092 0.056 2.131 0.750 0.109 2.135 0.0817 1.19 10.89 0.2325 0.098 0.060 2.277 0.801 0.117 2.281 0.0887 1.29 11.08 0.2527 0.104 0.063 2.423 0.852 0.124 2.427 0.0970 1.41 11.38 0.2762 0.110 0.067 2.568 0.904 0.132 2.573 0.1095 1.59 12.11 0.3116 0.117 0.071 2.714 0.955 0.139 2.719 0.1197 1.74 12.53 0.3407 0.123 0.075 2.859 1.006 0.147 2.864 0.1290 1.88 12.82 0.3673 0.129 0.079 3.005 1.057 0.154 3.010 0.1382 2.01 13.07 0.3935 0.135 0.082 3.151 1.104 0.161 3.142 0.1470 2.14 13.32 0.4186 0.142 0.086 3.296 1.156 0.168 3.290 0.1592 2.32 13.77 0.4532 0.154 0.094 3.587 1.252 0.182 3.565 0.1768 2.58 14.12 0.5035 0.167 0.102 3.879 1.343 0.196 3.823 0.1916 2.79 14.27 0.5455 0.185 0.113 4.315 1.488 0.217 4.237 0.2200 3.20 14.78 0.6263 0.204 0.124 4.752 1.647 0.240 4.688 0.2467 3.59 14.98 0.7023 0.223 0.136 5.189 1.801 0.262 5.126 0.2732 3.98 15.17 0.7779 0.242 0.147 5.626 1.955 0.285 5.566 0.3017 4.39 15.43 0.8589 0.267 0.162 6.208 2.163 0.315 6.157 0.3416 4.97 15.80 0.9725 0.292 0.178 6.790 2.380 0.347 6.777 0.3727 5.43 15.66 1.0611 0.317 0.193 7.373 2.590 0.377 7.374 0.4010 5.84 15.48 1.1416 0.348 0.212 8.101 2.876 0.419 8.187 0.4400 6.41 15.30 1.2528 0.379 0.231 8.829 3.161 0.460 9.000 0.4729 6.89 14.96 1.3464 0.417 0.254 9.702 3.443 0.501 9.803 0.5099 7.43 14.81 1.4518 0.454 0.277 10.576 3.740 0.545 10.648 0.5402 7.87 14.44 1.5379 0.498 0.303 11.595 4.050 0.590 11.531 0.5558 8.09 13.72 1.5825 0.548 0.334 12.760 4.353 0.634 12.393 0.5827 8.49 13.38 1.6588 0.598 0.364 13.924 4.692 0.683 13.358 0.5910 8.61 12.60 1.6824 0.654 0.399 15.235 5.004 0.729 14.247 0.5978 8.71 11.94 1.7018 0.717 0.437 16.691 5.297 0.771 15.081 0.5971 8.70 11.27 1.6999 0.779 0.475 18.147 5.564 0.810 15.839 0.5871 8.55 10.55 1.6715 0.854 0.521 19.894 5.805 0.845 16.528 0.5785 8.42 9.96 1.6469 0.935 0.570 21.786 6.039 0.879 17.192 0.5587 8.14 9.25 1.5907 1.023 0.624 23.825 6.242 0.909 17.770 0.5261 7.66 8.43 1.4977 1.117 0.681 26.009 6.425 0.936 18.293 0.5190 7.56 8.08 1.4775 1.223 0.745 28.484 6.533 0.951 18.601 0.4817 7.01 7.37 1.3714 1.335 0.814 31.104 6.639 0.967 18.902 0.4813 7.01 7.25 1.3703 1.460 0.890 34.016 6.724 0.979 19.144 0.4698 6.84 6.99 1.3376 1.598 0.974 37.219 6.793 0.989 19.340 0.4598 6.70 6.77 1.3090 1.735 1.058 40.422 6.824 0.994 19.427 0.4512 6.57 6.61 1.2846 1.873 1.142 43.625 6.853 0.998 19.512 0.4405 6.42 6.43 1.2542 2.004 1.222 46.683 6.876 1.001 19.577 0.4424 6.44 6.43 1.2595 2.142 1.306 49.886 6.866 1.000 19.548 0.4279 6.23 6.23 1.2183 2.942 1.793 68.521 6.877 1.001 19.578 0.4236 6.17 6.16 1.2060 3.742 2.281 87.157 6.885 1.003 19.602 0.4048 5.90 5.88 1.1525 4.542 2.769 105.793 6.872 1.001 19.565 0.4076 5.94 5.93 1.1603 5.342 3.256 124.429 6.881 1.002 19.589 0.3977 5.79 5.78 1.1321 RUN NUMBER 1W01602 AXIAL POSITION = 95.0 MM SPAN POSITION = 0.0 MM FREE-STREAM VELOCITY = 7.17 M/S FRICTION VELOCITY = 0.3161 M/S FREE-STREAM TURBULENCE = 5.067 % X-REYNOLDS NUMBER = 4.52 X10**4 FLUID DENSITY = 1.199 KG/M**3 KINEMATIC VISCOSITY = 1.508 X10(-5)MSQ/S BOUNDARY LAYER THICKNESS (99.0%) = 2.47 MM DISPLACEMENT THICKNESS = 0.674 MM MOMENTUM THICKNESS = 0.287 MM ENERGY THICKNESS = 0.466 MM FORM FACTOR H = 2.346 FORM FACTOR E = 1.620 RDELTASTAR = 320.7 RTHETA = 136.7 SKIN FRICTION COEFFICIENT = 0.003884 CALCULATED CF = 0.003124 Y Y/DEL YPLUS U U/UO UPLUS u u/UO u/U u/UTAU MM M/S M/S % % 0.029 0.012 0.608 0.189 0.026 0.599 0.0307 0.43 16.21 0.0970 0.035 0.014 0.739 0.230 0.032 0.728 0.0401 0.56 17.41 0.1268 0.042 0.017 0.870 0.271 0.038 0.857 0.0440 0.61 16.26 0.1393 0.048 0.019 1.001 0.312 0.043 0.986 0.0501 0.70 16.09 0.1587 0.054 0.022 1.132 0.352 0.049 1.115 0.0546 0.76 15.49 0.1728 0.060 0.024 1.263 0.393 0.055 1.244 0.0640 0.89 16.28 0.2026 0.067 0.027 1.394 0.434 0.061 1.373 0.0701 0.98 16.16 0.2219 0.073 0.029 1.525 0.475 0.066 1.502 0.0723 1.01 15.24 0.2289 0.079 0.032 1.656 0.516 0.072 1.631 0.0796 1.11 15.44 0.2518 0.085 0.035 1.787 0.556 0.078 1.760 0.0714 1.00 12.83 0.2258 0.092 0.037 1.918 0.597 0.083 1.889 0.0780 1.09 13.06 0.2467 0.098 0.040 2.048 0.638 0.089 2.019 0.0860 1.20 13.49 0.2722 0.104 0.042 2.179 0.679 0.095 2.148 0.0958 1.34 14.11 0.3030 0.110 0.045 2.310 0.720 0.100 2.277 0.1039 1.45 14.44 0.3287 0.117 0.047 2.441 0.760 0.106 2.406 0.1147 1.60 15.09 0.3629 0.123 0.050 2.572 0.801 0.112 2.535 0.1268 1.77 15.83 0.4013 0.135 0.055 2.834 0.883 0.123 2.793 0.1445 2.01 16.37 0.4571 0.154 0.062 3.227 1.005 0.140 3.180 0.1751 2.44 17.42 0.5539 0.167 0.068 3.489 1.091 0.152 3.453 0.1946 2.71 17.83 0.6156 0.185 0.075 3.882 1.213 0.169 3.837 0.2271 3.17 18.73 0.7185 0.204 0.083 4.275 1.313 0.183 4.153 0.2464 3.44 18.77 0.7796 0.229 0.093 4.799 1.499 0.209 4.742 0.2969 4.14 19.81 0.9394 0.254 0.103 5.323 1.689 0.235 5.343 0.3323 4.63 19.67 1.0512 0.279 0.113 5.847 1.850 0.258 5.853 0.3621 5.05 19.57 1.1456 0.310 0.126 6.502 2.059 0.287 6.515 0.4144 5.78 20.12 1.3111 0.342 0.138 7.157 2.291 0.320 7.250 0.4584 6.39 20.01 1.4504 0.379 0.154 7.942 2.546 0.355 8.055 0.5034 7.02 19.77 1.5925 0.417 0.169 8.728 2.826 0.394 8.941 0.6185 8.62 21.88 1.9567 0.460 0.187 9.645 3.118 0.435 9.866 0.6695 9.34 21.47 2.1182 0.510 0.207 10.693 3.396 0.473 10.744 0.6997 9.76 20.60 2.2137 0.560 0.227 11.741 3.708 0.517 11.732 0.7225 10.07 19.49 2.2860 0.623 0.252 13.051 4.006 0.559 12.676 0.7626 10.63 19.04 2.4128 0.685 0.278 14.360 4.292 0.598 13.580 0.7447 10.38 17.35 2.3560 0.760 0.308 15.932 4.703 0.656 14.878 0.7957 11.09 16.92 2.5174 0.835 0.339 17.504 5.015 0.699 15.866 0.7490 10.44 14.94 2.3697 0.923 0.374 19.337 5.241 0.731 16.583 0.7105 9.91 13.56 2.2480 1.023 0.415 21.433 5.641 0.786 17.846 0.7066 9.85 12.53 2.2354 1.129 0.458 23.660 5.903 0.823 18.676 0.7588 10.58 12.85 2.4008 1.248 0.506 26.148 6.148 0.857 19.451 0.7093 9.89 11.54 2.2440 1.379 0.559 28.899 6.383 0.890 20.195 0.6798 9.48 10.65 2.1506 1.523 0.617 31.911 6.573 0.917 20.797 0.6169 8.60 9.39 1.9518 1.679 0.681 35.186 6.740 0.940 21.323 0.5839 8.14 8.66 1.8473 1.854 0.752 38.853 6.882 0.960 21.774 0.5346 7.45 7.77 1.6915 2.048 0.830 42.913 6.961 0.971 22.025 0.5133 7.16 7.37 1.6239 2.260 0.916 47.366 7.034 0.981 22.254 0.4590 6.40 6.53 1.4523 2.498 1.013 52.344 7.166 0.999 22.673 0.3728 5.20 5.20 1.1794 2.735 1.109 57.321 7.140 0.996 22.590 0.3523 4.91 4.93 1.1145 2.967 1.203 62.167 7.182 1.001 22.722 0.3543 4.94 4.93 1.1210 3.204 1.299 67.144 7.162 0.999 22.660 0.3413 4.76 4.76 1.0797 3.442 1.395 72.121 7.151 0.997 22.624 0.3981 5.55 5.57 1.2597 4.692 1.902 98.317 7.190 1.002 22.747 0.3753 5.23 5.22 1.1875 5.942 2.409 124.512 7.181 1.001 22.721 0.3732 5.20 5.20 1.1807 7.192 2.916 150.707 7.188 1.002 22.741 0.3704 5.16 5.15 1.1718 8.442 3.423 176.903 7.187 1.002 22.738 0.3634 5.07 5.06 1.1497 RUN NUMBER 1W01603 AXIAL POSITION = 145.0 MM SPAN POSITION = 0.0 MM FREE-STREAM VELOCITY = 7.47 M/S FRICTION VELOCITY = 0.3024 M/S FREE-STREAM TURBULENCE = 4.109 % X-REYNOLDS NUMBER = 7.19 X10**4 FLUID DENSITY = 1.202 KG/M**3 KINEMATIC VISCOSITY = 1.505 X10(-5)MSQ/S BOUNDARY LAYER THICKNESS (99.0%) = 3.20 MM DISPLACEMENT THICKNESS = 0.792 MM MOMENTUM THICKNESS = 0.349 MM ENERGY THICKNESS = 0.572 MM FORM FACTOR H = 2.269 FORM FACTOR E = 1.638 RDELTASTAR = 392.9 RTHETA = 173.2 SKIN FRICTION COEFFICIENT = 0.003279 CALCULATED CF = 0.002476 Y Y/DEL YPLUS U U/UO UPLUS u u/UO u/U u/UTAU MM M/S M/S % % 0.029 0.009 0.583 0.175 0.023 0.577 0.0382 0.51 21.89 0.1264 0.035 0.011 0.708 0.212 0.028 0.702 0.0364 0.49 17.16 0.1204 0.042 0.013 0.834 0.250 0.033 0.826 0.0362 0.48 14.47 0.1195 0.048 0.015 0.959 0.287 0.038 0.950 0.0386 0.52 13.43 0.1276 0.054 0.017 1.085 0.325 0.044 1.075 0.0429 0.57 13.20 0.1419 0.060 0.019 1.210 0.363 0.049 1.199 0.0473 0.63 13.03 0.1563 0.067 0.021 1.336 0.400 0.054 1.324 0.0550 0.74 13.75 0.1820 0.073 0.023 1.461 0.438 0.059 1.448 0.0617 0.83 14.09 0.2040 0.079 0.025 1.587 0.475 0.064 1.572 0.0728 0.97 15.30 0.2406 0.085 0.027 1.712 0.513 0.069 1.697 0.0808 1.08 15.75 0.2672 0.092 0.029 1.838 0.551 0.074 1.821 0.0910 1.22 16.52 0.3008 0.098 0.031 1.964 0.588 0.079 1.946 0.0980 1.31 16.66 0.3242 0.104 0.032 2.089 0.626 0.084 2.070 0.1252 1.68 20.00 0.4141 0.110 0.034 2.215 0.664 0.089 2.194 0.1285 1.72 19.37 0.4250 0.123 0.038 2.466 0.739 0.099 2.443 0.1532 2.05 20.73 0.5065 0.135 0.042 2.717 0.814 0.109 2.692 0.1766 2.36 21.69 0.5838 0.148 0.046 2.968 0.889 0.119 2.941 0.1995 2.67 22.44 0.6598 0.167 0.052 3.345 1.002 0.134 3.314 0.2320 3.11 23.15 0.7673 0.185 0.058 3.721 1.107 0.148 3.660 0.2686 3.60 24.27 0.8883 0.204 0.064 4.098 1.223 0.164 4.045 0.2989 4.00 24.43 0.9885 0.229 0.072 4.600 1.369 0.183 4.527 0.3471 4.65 25.35 1.1479 0.254 0.079 5.102 1.522 0.204 5.035 0.3843 5.15 25.24 1.2708 0.279 0.087 5.605 1.675 0.224 5.538 0.4279 5.73 25.55 1.4151 0.310 0.097 6.232 1.873 0.251 6.195 0.4845 6.49 25.87 1.6024 0.348 0.109 6.986 2.121 0.284 7.014 0.5312 7.11 25.04 1.7566 0.385 0.120 7.739 2.354 0.315 7.786 0.5969 7.99 25.35 1.9739 0.429 0.134 8.618 2.629 0.352 8.694 0.6383 8.55 24.28 2.1109 0.473 0.148 9.497 2.930 0.392 9.690 0.6959 9.32 23.75 2.3012 0.529 0.165 10.627 3.276 0.439 10.833 0.7693 10.30 23.49 2.5441 0.585 0.183 11.756 3.595 0.481 11.888 0.8143 10.90 22.65 2.6930 0.648 0.202 13.012 3.923 0.525 12.972 0.8430 11.29 21.49 2.7876 0.723 0.226 14.519 4.245 0.568 14.037 0.8672 11.61 20.43 2.8679 0.798 0.249 16.025 4.585 0.614 15.161 0.8781 11.76 19.15 2.9037 0.892 0.279 17.908 4.964 0.665 16.416 0.8953 11.99 18.04 2.9609 0.985 0.308 19.792 5.272 0.706 17.436 0.8677 11.62 16.46 2.8694 1.092 0.341 21.926 5.629 0.754 18.615 0.8660 11.60 15.38 2.8638 1.217 0.380 24.437 5.942 0.796 19.651 0.8340 11.17 14.03 2.7578 1.348 0.421 27.074 6.192 0.829 20.477 0.7945 10.64 12.83 2.6274 1.498 0.468 30.087 6.461 0.865 21.365 0.7600 10.18 11.76 2.5132 1.660 0.519 33.351 6.686 0.895 22.108 0.7062 9.46 10.56 2.3354 1.842 0.575 36.992 6.886 0.922 22.772 0.6339 8.49 9.21 2.0964 2.042 0.638 41.010 7.023 0.940 23.225 0.5618 7.52 8.00 1.8579 2.267 0.708 45.529 7.185 0.962 23.759 0.5216 6.98 7.26 1.7250 2.517 0.786 50.551 7.241 0.970 23.945 0.4626 6.19 6.39 1.5297 2.792 0.872 56.075 7.332 0.982 24.245 0.4218 5.65 5.75 1.3950 3.098 0.968 62.227 7.388 0.989 24.431 0.3759 5.03 5.09 1.2432 3.404 1.064 68.379 7.405 0.991 24.487 0.3515 4.71 4.75 1.1624 3.710 1.159 74.531 7.463 0.999 24.679 0.3482 4.66 4.67 1.1513 4.017 1.255 80.683 7.457 0.999 24.661 0.3271 4.38 4.39 1.0816 4.323 1.351 86.835 7.498 1.004 24.797 0.3303 4.42 4.40 1.0922 5.873 1.835 117.971 7.501 1.004 24.804 0.3160 4.23 4.21 1.0451 7.423 2.320 149.108 7.480 1.002 24.737 0.3073 4.11 4.11 1.0162 8.973 2.804 180.244 7.469 1.000 24.700 0.3014 4.04 4.04 0.9968 10.523 3.288 211.380 7.473 1.001 24.713 0.3068 4.11 4.11 1.0147 RUN NUMBER 1W01604 AXIAL POSITION = 195.0 MM SPAN POSITION = 0.0 MM FREE-STREAM VELOCITY = 7.64 M/S FRICTION VELOCITY = 0.3090 M/S FREE-STREAM TURBULENCE = 3.775 % X-REYNOLDS NUMBER = 9.89 X10**4 FLUID DENSITY = 1.201 KG/M**3 KINEMATIC VISCOSITY = 1.506 X10(-5)MSQ/S BOUNDARY LAYER THICKNESS (99.0%) = 3.75 MM DISPLACEMENT THICKNESS = 0.882 MM MOMENTUM THICKNESS = 0.416 MM ENERGY THICKNESS = 0.690 MM FORM FACTOR H = 2.117 FORM FACTOR E = 1.657 RDELTASTAR = 447.2 RTHETA = 211.2 SKIN FRICTION COEFFICIENT = 0.003274 CALCULATED CF = 0.002111 Y Y/DEL YPLUS U U/UO UPLUS u u/UO u/U u/UTAU MM M/S M/S % % 0.029 0.008 0.595 0.186 0.024 0.601 0.0464 0.61 25.01 0.1503 0.035 0.009 0.723 0.226 0.030 0.731 0.0497 0.65 22.02 0.1609 0.042 0.011 0.852 0.266 0.035 0.860 0.0579 0.76 21.80 0.1875 0.048 0.013 0.980 0.306 0.040 0.990 0.0642 0.84 20.98 0.2077 0.054 0.014 1.108 0.346 0.045 1.119 0.0756 0.99 21.85 0.2445 0.060 0.016 1.237 0.386 0.051 1.249 0.0827 1.08 21.43 0.2676 0.067 0.018 1.365 0.426 0.056 1.378 0.0931 1.22 21.87 0.3014 0.073 0.019 1.493 0.466 0.061 1.508 0.1040 1.36 22.33 0.3367 0.079 0.021 1.621 0.506 0.066 1.637 0.1211 1.58 23.93 0.3918 0.085 0.023 1.750 0.546 0.071 1.767 0.1291 1.69 23.65 0.4178 0.092 0.024 1.878 0.586 0.077 1.896 0.1465 1.92 25.00 0.4740 0.098 0.026 2.006 0.626 0.082 2.026 0.1526 2.00 24.38 0.4940 0.104 0.028 2.135 0.666 0.087 2.155 0.1737 2.27 26.08 0.5620 0.117 0.031 2.391 0.746 0.098 2.414 0.1967 2.57 26.36 0.6365 0.129 0.034 2.648 0.826 0.108 2.673 0.2365 3.10 28.62 0.7652 0.142 0.038 2.904 0.906 0.119 2.932 0.2743 3.59 30.27 0.8878 0.160 0.043 3.289 1.026 0.134 3.321 0.3105 4.07 30.26 1.0048 0.179 0.048 3.674 1.143 0.150 3.698 0.3630 4.75 31.76 1.1748 0.198 0.053 4.059 1.250 0.164 4.046 0.3961 5.19 31.68 1.2819 0.223 0.059 4.572 1.407 0.184 4.554 0.4512 5.91 32.06 1.4602 0.248 0.066 5.085 1.544 0.202 4.995 0.4975 6.51 32.23 1.6099 0.273 0.073 5.598 1.730 0.226 5.597 0.5572 7.29 32.22 1.8030 0.310 0.083 6.368 1.943 0.254 6.286 0.6112 8.00 31.46 1.9777 0.342 0.091 7.009 2.168 0.284 7.016 0.6804 8.91 31.38 2.2019 0.379 0.101 7.779 2.423 0.317 7.840 0.7417 9.71 30.61 2.4001 0.423 0.113 8.677 2.669 0.349 8.635 0.7935 10.39 29.74 2.5677 0.473 0.126 9.703 2.958 0.387 9.572 0.8511 11.14 28.77 2.7541 0.529 0.141 10.857 3.273 0.429 10.592 0.8812 11.54 26.92 2.8515 0.592 0.158 12.140 3.609 0.472 11.678 0.9207 12.05 25.51 2.9793 0.654 0.175 13.423 3.883 0.508 12.564 0.9450 12.37 24.34 3.0580 0.729 0.195 14.962 4.247 0.556 13.743 0.9925 12.99 23.37 3.2116 0.817 0.218 16.758 4.613 0.604 14.927 1.0044 13.15 21.77 3.2503 0.910 0.243 18.682 4.933 0.646 15.964 1.0087 13.21 20.45 3.2642 1.010 0.270 20.735 5.211 0.682 16.862 1.0065 13.18 19.32 3.2570 1.129 0.301 23.172 5.541 0.725 17.929 1.0056 13.16 18.15 3.2540 1.254 0.335 25.737 5.850 0.766 18.930 0.9506 12.44 16.25 3.0760 1.398 0.373 28.688 6.128 0.802 19.829 0.9427 12.34 15.38 3.0506 1.560 0.417 32.023 6.389 0.836 20.676 0.8769 11.48 13.73 2.8377 1.735 0.463 35.615 6.612 0.866 21.397 0.8235 10.78 12.45 2.6647 1.935 0.517 39.719 6.781 0.888 21.944 0.7657 10.02 11.29 2.4779 2.154 0.575 44.209 6.973 0.913 22.566 0.7035 9.21 10.09 2.2764 2.404 0.642 49.340 7.132 0.934 23.080 0.6155 8.06 8.63 1.9916 2.673 0.714 54.856 7.283 0.953 23.567 0.5586 7.31 7.67 1.8076 2.979 0.795 61.142 7.435 0.973 24.059 0.4832 6.33 6.50 1.5635 3.317 0.885 68.069 7.491 0.981 24.240 0.4373 5.73 5.84 1.4152 3.698 0.987 75.893 7.561 0.990 24.467 0.3937 5.15 5.21 1.2740 4.073 1.087 83.590 7.601 0.995 24.597 0.3563 4.66 4.69 1.1529 4.454 1.189 91.415 7.634 0.999 24.704 0.3431 4.49 4.49 1.1102 4.829 1.289 99.111 7.655 1.002 24.772 0.3215 4.21 4.20 1.0402 5.210 1.391 106.936 7.632 0.999 24.697 0.3109 4.07 4.07 1.0062 7.060 1.885 144.906 7.622 0.998 24.665 0.2920 3.82 3.83 0.9449 8.910 2.379 182.876 7.650 1.002 24.756 0.2983 3.91 3.90 0.9653 10.760 2.873 220.846 7.654 1.002 24.769 0.2822 3.69 3.69 0.9131 12.610 3.367 258.815 7.657 1.002 24.777 0.2884 3.78 3.77 0.9332 RUN NUMBER 1W01605 AXIAL POSITION = 295.0 MM SPAN POSITION = 0.0 MM FREE-STREAM VELOCITY = 7.84 M/S FRICTION VELOCITY = 0.3377 M/S FREE-STREAM TURBULENCE = 3.441 % X-REYNOLDS NUMBER = 15.35 X10**4 FLUID DENSITY = 1.201 KG/M**3 KINEMATIC VISCOSITY = 1.506 X10(-5)MSQ/S BOUNDARY LAYER THICKNESS (99.0%) = 5.63 MM DISPLACEMENT THICKNESS = 1.023 MM MOMENTUM THICKNESS = 0.555 MM ENERGY THICKNESS = 0.947 MM FORM FACTOR H = 1.842 FORM FACTOR E = 1.705 RDELTASTAR = 532.4 RTHETA = 289.0 SKIN FRICTION COEFFICIENT = 0.003715 CALCULATED CF = 0.001695 Y Y/DEL YPLUS U U/UO UPLUS u u/UO u/U u/UTAU MM M/S M/S % % 0.029 0.005 0.650 0.221 0.028 0.656 0.0734 0.94 33.14 0.2173 0.035 0.006 0.791 0.269 0.034 0.797 0.0774 0.99 28.76 0.2292 0.042 0.007 0.931 0.317 0.040 0.938 0.0855 1.09 26.98 0.2531 0.048 0.008 1.071 0.365 0.047 1.080 0.1037 1.32 28.44 0.3070 0.054 0.010 1.211 0.412 0.053 1.221 0.1192 1.52 28.92 0.3531 0.060 0.011 1.351 0.460 0.059 1.362 0.1390 1.77 30.21 0.4115 0.067 0.012 1.491 0.508 0.065 1.503 0.1596 2.04 31.44 0.4726 0.073 0.013 1.632 0.555 0.071 1.645 0.1801 2.30 32.43 0.5333 0.079 0.014 1.772 0.603 0.077 1.786 0.1997 2.55 33.11 0.5914 0.085 0.015 1.912 0.651 0.083 1.927 0.2237 2.86 34.37 0.6624 0.092 0.016 2.052 0.699 0.089 2.069 0.2454 3.13 35.13 0.7267 0.104 0.018 2.332 0.794 0.101 2.351 0.2975 3.80 37.46 0.8808 0.117 0.021 2.613 0.890 0.114 2.634 0.3577 4.56 40.21 1.0591 0.129 0.023 2.893 0.985 0.126 2.916 0.3940 5.03 40.00 1.1665 0.148 0.026 3.314 1.128 0.144 3.340 0.4724 6.03 41.88 1.3988 0.167 0.030 3.734 1.273 0.162 3.770 0.5393 6.88 42.35 1.5968 0.185 0.033 4.155 1.376 0.176 4.075 0.5948 7.59 43.22 1.7612 0.210 0.037 4.715 1.567 0.200 4.640 0.6870 8.77 43.83 2.0340 0.235 0.042 5.276 1.751 0.223 5.184 0.7557 9.64 43.16 2.2374 0.260 0.046 5.837 1.931 0.246 5.718 0.8139 10.39 42.15 2.4100 0.298 0.053 6.678 2.193 0.280 6.494 0.9086 11.59 41.42 2.6901 0.335 0.060 7.519 2.455 0.313 7.269 0.9765 12.46 39.77 2.8912 0.373 0.066 8.360 2.713 0.346 8.033 1.0295 13.14 37.95 3.0484 0.423 0.075 9.481 2.991 0.382 8.858 1.0701 13.66 35.77 3.1684 0.473 0.084 10.602 3.269 0.417 9.680 1.1216 14.31 34.31 3.3211 0.529 0.094 11.864 3.558 0.454 10.535 1.1282 14.40 31.71 3.3406 0.598 0.106 13.406 3.913 0.499 11.585 1.1590 14.79 29.62 3.4318 0.673 0.120 15.088 4.208 0.537 12.458 1.1580 14.78 27.52 3.4288 0.754 0.134 16.910 4.490 0.573 13.295 1.1475 14.64 25.56 3.3977 0.848 0.151 19.013 4.820 0.615 14.271 1.1401 14.55 23.66 3.3758 0.954 0.170 21.395 5.124 0.654 15.173 1.1396 14.54 22.24 3.3741 1.073 0.191 24.059 5.366 0.685 15.888 1.1025 14.07 20.55 3.2645 1.204 0.214 27.002 5.663 0.723 16.769 1.0843 13.84 19.15 3.2106 1.354 0.241 30.366 5.964 0.761 17.658 1.0464 13.35 17.55 3.0984 1.523 0.271 34.151 6.183 0.789 18.308 1.0116 12.91 16.36 2.9953 1.710 0.304 38.356 6.409 0.818 18.976 0.9583 12.23 14.95 2.8373 1.923 0.342 43.122 6.605 0.843 19.558 0.9046 11.54 13.69 2.6784 2.160 0.384 48.448 6.810 0.869 20.164 0.8479 10.82 12.45 2.5104 2.429 0.432 54.475 6.980 0.891 20.668 0.7768 9.91 11.13 2.2999 2.729 0.485 61.203 7.110 0.907 21.052 0.7185 9.17 10.11 2.1275 3.067 0.545 68.772 7.289 0.930 21.583 0.6518 8.32 8.94 1.9298 3.448 0.613 77.323 7.405 0.945 21.926 0.5917 7.55 7.99 1.7520 3.873 0.688 86.854 7.527 0.961 22.286 0.5098 6.51 6.77 1.5096 4.354 0.774 97.647 7.624 0.973 22.573 0.4672 5.96 6.13 1.3833 4.892 0.869 109.702 7.704 0.983 22.810 0.4106 5.24 5.33 1.2156 5.498 0.977 123.298 7.749 0.989 22.945 0.3690 4.71 4.76 1.0925 6.104 1.085 136.895 7.784 0.993 23.046 0.3262 4.16 4.19 0.9660 6.710 1.192 150.491 7.816 0.997 23.143 0.3037 3.88 3.89 0.8993 7.310 1.299 163.947 7.861 1.003 23.275 0.2990 3.82 3.80 0.8855 7.917 1.407 177.544 7.825 0.999 23.169 0.2841 3.63 3.63 0.8412 10.667 1.895 239.218 7.856 1.002 23.259 0.2695 3.44 3.43 0.7980 13.417 2.384 300.892 7.846 1.001 23.230 0.2631 3.36 3.35 0.7789 16.167 2.872 362.566 7.840 1.001 23.215 0.2636 3.36 3.36 0.7805 18.917 3.361 424.241 7.861 1.003 23.277 0.2696 3.44 3.43 0.7983 RUN NUMBER 1W01606 AXIAL POSITION = 395.0 MM SPAN POSITION = 0.0 MM FREE-STREAM VELOCITY = 8.18 M/S FRICTION VELOCITY = 0.3838 M/S FREE-STREAM TURBULENCE = 3.115 % X-REYNOLDS NUMBER = 21.39 X10**4 FLUID DENSITY = 1.198 KG/M**3 KINEMATIC VISCOSITY = 1.510 X10(-5)MSQ/S BOUNDARY LAYER THICKNESS (99.0%) = 7.29 MM DISPLACEMENT THICKNESS = 1.137 MM MOMENTUM THICKNESS = 0.700 MM ENERGY THICKNESS = 1.224 MM FORM FACTOR H = 1.624 FORM FACTOR E = 1.749 RDELTASTAR = 615.7 RTHETA = 379.1 SKIN FRICTION COEFFICIENT = 0.004407 CALCULATED CF = 0.001436 Y Y/DEL YPLUS U U/UO UPLUS u u/UO u/U u/UTAU MM M/S M/S % % 0.029 0.004 0.737 0.285 0.035 0.742 0.0869 1.06 30.50 0.2263 0.035 0.005 0.896 0.346 0.042 0.902 0.0892 1.09 25.77 0.2323 0.042 0.006 1.055 0.407 0.050 1.062 0.1017 1.24 24.96 0.2650 0.048 0.007 1.214 0.469 0.057 1.221 0.1168 1.43 24.91 0.3043 0.054 0.007 1.373 0.530 0.065 1.381 0.1370 1.68 25.84 0.3569 0.060 0.008 1.532 0.592 0.072 1.541 0.1570 1.92 26.54 0.4091 0.067 0.009 1.691 0.653 0.080 1.701 0.1853 2.27 28.38 0.4827 0.073 0.010 1.850 0.714 0.087 1.861 0.2068 2.53 28.95 0.5387 0.079 0.011 2.008 0.776 0.095 2.021 0.2358 2.88 30.39 0.6142 0.085 0.012 2.167 0.837 0.102 2.181 0.2645 3.23 31.60 0.6891 0.092 0.013 2.326 0.898 0.110 2.341 0.2959 3.62 32.94 0.7710 0.104 0.014 2.644 1.021 0.125 2.660 0.3516 4.30 34.44 0.9161 0.123 0.017 3.121 1.205 0.147 3.140 0.4429 5.42 36.74 1.1538 0.135 0.019 3.439 1.323 0.162 3.446 0.5021 6.14 37.95 1.3080 0.154 0.021 3.915 1.494 0.183 3.891 0.5740 7.02 38.43 1.4955 0.173 0.024 4.392 1.679 0.205 4.375 0.6599 8.07 39.29 1.7191 0.198 0.027 5.028 1.904 0.233 4.960 0.7531 9.21 39.56 1.9621 0.223 0.031 5.663 2.159 0.264 5.624 0.8493 10.39 39.34 2.2127 0.254 0.035 6.458 2.392 0.292 6.231 0.9326 11.40 38.99 2.4296 0.285 0.039 7.252 2.655 0.325 6.916 1.0015 12.25 37.73 2.6092 0.323 0.044 8.205 2.968 0.363 7.733 1.0641 13.01 35.85 2.7723 0.367 0.050 9.318 3.303 0.404 8.605 1.1206 13.70 33.93 2.9195 0.410 0.056 10.430 3.608 0.441 9.399 1.1553 14.13 32.02 3.0098 0.467 0.064 11.860 3.886 0.475 10.125 1.1957 14.62 30.77 3.1151 0.523 0.072 13.290 4.247 0.519 11.064 1.1965 14.63 28.17 3.1171 0.592 0.081 15.038 4.538 0.555 11.823 1.1985 14.66 26.41 3.1225 0.673 0.092 17.104 4.826 0.590 12.573 1.1798 14.43 24.45 3.0736 0.754 0.103 19.169 5.070 0.620 13.209 1.1618 14.21 22.92 3.0269 0.854 0.117 21.712 5.350 0.654 13.939 1.1316 13.84 21.15 2.9482 0.967 0.133 24.572 5.584 0.683 14.548 1.0944 13.38 19.60 2.8512 1.092 0.150 27.750 5.821 0.712 15.164 1.0566 12.92 18.15 2.7526 1.229 0.169 31.246 6.021 0.736 15.685 1.0227 12.51 16.99 2.6644 1.385 0.190 35.218 6.214 0.760 16.189 0.9860 12.06 15.87 2.5687 1.567 0.215 39.826 6.419 0.785 16.723 0.9345 11.43 14.56 2.4346 1.767 0.242 44.911 6.598 0.807 17.189 0.8976 10.98 13.60 2.3384 1.998 0.274 50.790 6.726 0.822 17.523 0.8678 10.61 12.90 2.2609 2.254 0.309 57.305 6.890 0.843 17.951 0.8189 10.01 11.88 2.1333 2.542 0.349 64.614 7.034 0.860 18.324 0.7818 9.56 11.12 2.0369 2.873 0.394 73.035 7.211 0.882 18.787 0.7356 9.00 10.20 1.9164 3.242 0.445 82.410 7.341 0.898 19.124 0.6888 8.42 9.38 1.7946 3.654 0.501 92.898 7.484 0.915 19.496 0.6397 7.82 8.55 1.6665 4.129 0.567 104.974 7.647 0.935 19.923 0.5889 7.20 7.70 1.5343 4.660 0.639 118.480 7.745 0.947 20.176 0.5241 6.41 6.77 1.3654 5.260 0.722 133.734 7.849 0.960 20.449 0.4821 5.90 6.14 1.2560 5.935 0.814 150.895 7.960 0.973 20.738 0.4188 5.12 5.26 1.0911 6.698 0.919 170.281 8.055 0.985 20.985 0.3740 4.57 4.64 0.9743 7.460 1.024 189.666 8.108 0.992 21.123 0.3344 4.09 4.12 0.8712 8.223 1.128 209.051 8.157 0.998 21.252 0.2979 3.64 3.65 0.7760 8.985 1.233 228.437 8.176 1.000 21.301 0.2841 3.47 3.47 0.7402 9.748 1.338 247.822 8.187 1.001 21.330 0.2744 3.36 3.35 0.7149 13.098 1.797 332.991 8.222 1.005 21.421 0.2521 3.08 3.07 0.6569 16.448 2.257 418.160 8.176 1.000 21.302 0.2492 3.05 3.05 0.6493 19.798 2.717 503.329 8.203 1.003 21.372 0.2485 3.04 3.03 0.6473 23.148 3.176 588.498 8.188 1.001 21.332 0.2548 3.12 3.11 0.6637 RUN NUMBER 1W01607 AXIAL POSITION = 495.0 MM SPAN POSITION = 0.0 MM FREE-STREAM VELOCITY = 8.47 M/S FRICTION VELOCITY = 0.4447 M/S FREE-STREAM TURBULENCE = 2.777 % X-REYNOLDS NUMBER = 27.81 X10**4 FLUID DENSITY = 1.200 KG/M**3 KINEMATIC VISCOSITY = 1.507 X10(-5)MSQ/S BOUNDARY LAYER THICKNESS (99.0%) = 9.22 MM DISPLACEMENT THICKNESS = 1.309 MM MOMENTUM THICKNESS = 0.856 MM ENERGY THICKNESS = 1.515 MM FORM FACTOR H = 1.529 FORM FACTOR E = 1.769 RDELTASTAR = 735.7 RTHETA = 481.0 SKIN FRICTION COEFFICIENT = 0.005516 CALCULATED CF = 0.004317 LAW OF THE WALL OFFSET = 5.20 KARMAN CONSTANT = 0.410 FORM FACTOR G = 6.592 CLAUSER DELTA = 24.934 MM WAKE FACTOR PI = -0.021 1 Y Y/DEL YPLUS U U/UO UPLUS u u/UO u/U u/UTAU MM M/S M/S % % 0.029 0.003 0.856 0.314 0.037 0.705 0.0870 1.03 27.74 0.1956 0.035 0.004 1.040 0.381 0.045 0.857 0.0897 1.06 23.53 0.2016 0.042 0.005 1.224 0.449 0.053 1.009 0.1055 1.25 23.52 0.2373 0.048 0.005 1.409 0.516 0.061 1.161 0.1206 1.42 23.37 0.2713 0.054 0.006 1.593 0.584 0.069 1.313 0.1403 1.66 24.03 0.3155 0.060 0.007 1.778 0.651 0.077 1.465 0.1675 1.98 25.71 0.3766 0.067 0.007 1.962 0.719 0.085 1.617 0.1985 2.34 27.60 0.4463 0.073 0.008 2.146 0.787 0.093 1.769 0.2216 2.62 28.18 0.4984 0.079 0.009 2.331 0.854 0.101 1.921 0.2469 2.92 28.90 0.5551 0.085 0.009 2.515 0.922 0.109 2.073 0.2735 3.23 29.67 0.6149 0.098 0.011 2.884 1.057 0.125 2.376 0.3279 3.87 31.02 0.7373 0.110 0.012 3.253 1.192 0.141 2.680 0.3820 4.51 32.05 0.8590 0.129 0.014 3.806 1.395 0.165 3.136 0.4792 5.66 34.36 1.0776 0.148 0.016 4.359 1.580 0.187 3.553 0.5614 6.63 35.54 1.2625 0.167 0.018 4.913 1.762 0.208 3.963 0.6378 7.53 36.19 1.4342 0.185 0.020 5.466 1.968 0.232 4.425 0.7083 8.36 36.00 1.5928 0.217 0.023 6.388 2.289 0.270 5.147 0.8179 9.66 35.74 1.8392 0.242 0.026 7.125 2.532 0.299 5.694 0.8960 10.58 35.38 2.0148 0.273 0.030 8.048 2.785 0.329 6.263 0.9709 11.47 34.86 2.1832 0.310 0.034 9.154 3.117 0.368 7.008 1.0383 12.26 33.31 2.3347 0.354 0.038 10.445 3.437 0.406 7.728 1.0885 12.85 31.67 2.4475 0.404 0.044 11.920 3.815 0.450 8.578 1.1346 13.40 29.74 2.5512 0.460 0.050 13.580 4.154 0.491 9.342 1.1509 13.59 27.70 2.5880 0.517 0.056 15.239 4.468 0.528 10.047 1.1690 13.80 26.16 2.6286 0.592 0.064 17.452 4.826 0.570 10.852 1.1649 13.76 24.14 2.6193 0.667 0.072 19.665 5.093 0.601 11.452 1.1440 13.51 22.46 2.5725 0.760 0.082 22.431 5.376 0.635 12.089 1.1084 13.09 20.62 2.4924 0.860 0.093 25.382 5.604 0.662 12.601 1.0836 12.80 19.34 2.4365 0.979 0.106 28.886 5.797 0.685 13.035 1.0429 12.32 17.99 2.3451 1.110 0.120 32.758 6.040 0.713 13.583 0.9998 11.81 16.55 2.2482 1.254 0.136 36.999 6.180 0.730 13.897 0.9527 11.25 15.42 2.1424 1.423 0.154 41.978 6.379 0.753 14.345 0.9064 10.70 14.21 2.0382 1.617 0.175 47.695 6.547 0.773 14.722 0.8689 10.26 13.27 1.9539 1.835 0.199 54.149 6.703 0.791 15.072 0.8231 9.72 12.28 1.8509 2.079 0.226 61.341 6.855 0.810 15.415 0.7875 9.30 11.49 1.7709 2.360 0.256 69.640 6.992 0.826 15.721 0.7472 8.82 10.69 1.6803 2.673 0.290 78.860 7.156 0.845 16.091 0.7251 8.56 10.13 1.6304 3.035 0.329 89.555 7.315 0.864 16.448 0.6909 8.16 9.45 1.5536 3.442 0.373 101.542 7.434 0.878 16.716 0.6586 7.78 8.86 1.4810 3.904 0.424 115.188 7.573 0.894 17.029 0.6232 7.36 8.23 1.4013 4.423 0.480 130.494 7.714 0.911 17.346 0.5883 6.95 7.63 1.3229 5.017 0.544 148.013 7.855 0.928 17.663 0.5413 6.39 6.89 1.2171 5.692 0.618 167.929 8.015 0.946 18.023 0.4954 5.85 6.18 1.1140 6.454 0.700 190.426 8.135 0.961 18.292 0.4486 5.30 5.52 1.0088 7.317 0.794 215.874 8.222 0.971 18.489 0.3884 4.59 4.72 0.8733 8.298 0.900 244.826 8.316 0.982 18.700 0.3382 3.99 4.07 0.7604 9.279 1.007 273.778 8.395 0.991 18.878 0.2986 3.53 3.56 0.6715 10.260 1.113 302.730 8.446 0.997 18.993 0.2757 3.26 3.26 0.6199 11.235 1.219 331.498 8.452 0.998 19.005 0.2605 3.08 3.08 0.5858 12.217 1.326 360.450 8.485 1.002 19.081 0.2571 3.04 3.03 0.5780 16.367 1.776 482.896 8.487 1.002 19.085 0.2372 2.80 2.79 0.5333 20.517 2.226 605.342 8.512 1.005 19.141 0.2319 2.74 2.72 0.5214 24.667 2.677 727.789 8.492 1.003 19.095 0.2323 2.74 2.74 0.5223 28.817 3.127 850.235 8.476 1.001 19.060 0.2351 2.78 2.77 0.5288 RUN NUMBER 1W01608 AXIAL POSITION = 595.0 MM SPAN POSITION = 0.0 MM FREE-STREAM VELOCITY = 8.78 M/S FRICTION VELOCITY = 0.4511 M/S FREE-STREAM TURBULENCE = 2.478 % X-REYNOLDS NUMBER = 34.69 X10**4 FLUID DENSITY = 1.201 KG/M**3 KINEMATIC VISCOSITY = 1.506 X10(-5)MSQ/S BOUNDARY LAYER THICKNESS (99.0%) = 10.77 MM DISPLACEMENT THICKNESS = 1.476 MM MOMENTUM THICKNESS = 0.991 MM ENERGY THICKNESS = 1.759 MM FORM FACTOR H = 1.490 FORM FACTOR E = 1.775 RDELTASTAR = 860.8 RTHETA = 577.9 SKIN FRICTION COEFFICIENT = 0.005276 CALCULATED CF = 0.004373 LAW OF THE WALL OFFSET = 5.20 KARMAN CONSTANT = 0.410 FORM FACTOR G = 6.400 CLAUSER DELTA = 28.743 MM WAKE FACTOR PI = -0.016 1 Y Y/DEL YPLUS U U/UO UPLUS u u/UO u/U u/UTAU MM M/S M/S % % 0.029 0.003 0.869 0.336 0.038 0.745 0.0908 1.03 27.00 0.2012 0.035 0.003 1.056 0.409 0.047 0.906 0.0945 1.08 23.13 0.2095 0.042 0.004 1.243 0.481 0.055 1.066 0.1121 1.28 23.31 0.2486 0.048 0.004 1.430 0.554 0.063 1.227 0.1311 1.49 23.68 0.2906 0.054 0.005 1.617 0.626 0.071 1.388 0.1511 1.72 24.14 0.3349 0.060 0.006 1.804 0.698 0.080 1.548 0.1764 2.01 25.25 0.3910 0.067 0.006 1.992 0.771 0.088 1.709 0.2050 2.33 26.60 0.4545 0.073 0.007 2.179 0.843 0.096 1.869 0.2352 2.68 27.89 0.5214 0.079 0.007 2.366 0.916 0.104 2.030 0.2626 2.99 28.68 0.5822 0.092 0.008 2.740 1.061 0.121 2.351 0.3222 3.67 30.37 0.7142 0.104 0.010 3.115 1.206 0.137 2.673 0.3869 4.40 32.09 0.8576 0.123 0.011 3.676 1.423 0.162 3.154 0.4793 5.46 33.68 1.0624 0.142 0.013 4.238 1.619 0.184 3.589 0.5599 6.37 34.58 1.2411 0.160 0.015 4.799 1.810 0.206 4.012 0.6352 7.23 35.09 1.4080 0.179 0.017 5.361 1.983 0.226 4.395 0.7021 7.99 35.41 1.5563 0.210 0.020 6.297 2.305 0.262 5.110 0.8165 9.30 35.42 1.8100 0.235 0.022 7.045 2.534 0.289 5.618 0.8951 10.19 35.32 1.9843 0.273 0.025 8.168 2.953 0.336 6.545 0.9953 11.33 33.71 2.2063 0.310 0.029 9.292 3.274 0.373 7.258 1.0636 12.11 32.48 2.3576 0.354 0.033 10.602 3.632 0.413 8.051 1.1189 12.74 30.81 2.4804 0.404 0.038 12.099 4.000 0.455 8.868 1.1557 13.16 28.89 2.5618 0.460 0.043 13.784 4.337 0.494 9.614 1.1696 13.32 26.97 2.5927 0.529 0.049 15.843 4.694 0.534 10.405 1.1813 13.45 25.17 2.6186 0.604 0.056 18.089 5.018 0.571 11.123 1.1561 13.16 23.04 2.5627 0.692 0.064 20.709 5.340 0.608 11.838 1.1357 12.93 21.27 2.5174 0.785 0.073 23.517 5.553 0.632 12.308 1.1002 12.53 19.81 2.4388 0.898 0.083 26.886 5.789 0.659 12.832 1.0533 11.99 18.20 2.3350 1.023 0.095 30.630 6.019 0.685 13.343 1.0077 11.47 16.74 2.2338 1.173 0.109 35.122 6.234 0.710 13.819 0.9611 10.94 15.42 2.1306 1.335 0.124 39.989 6.428 0.732 14.249 0.9017 10.27 14.03 1.9988 1.523 0.141 45.604 6.577 0.749 14.579 0.8569 9.76 13.03 1.8994 1.742 0.162 52.155 6.741 0.767 14.942 0.8143 9.27 12.08 1.8050 1.985 0.184 59.455 6.850 0.780 15.183 0.7886 8.98 11.51 1.7480 2.267 0.210 67.878 7.015 0.799 15.551 0.7589 8.64 10.82 1.6823 2.592 0.241 77.612 7.176 0.817 15.907 0.7149 8.14 9.96 1.5847 2.960 0.275 88.655 7.332 0.835 16.253 0.6935 7.90 9.46 1.5374 3.373 0.313 101.009 7.480 0.852 16.581 0.6583 7.50 8.80 1.4593 3.854 0.358 115.422 7.648 0.871 16.953 0.6303 7.18 8.24 1.3973 4.398 0.408 131.706 7.803 0.888 17.298 0.5994 6.82 7.68 1.3288 5.017 0.466 150.237 7.978 0.908 17.686 0.5665 6.45 7.10 1.2557 5.729 0.532 171.575 8.136 0.926 18.035 0.5232 5.96 6.43 1.1598 6.542 0.608 195.908 8.290 0.944 18.377 0.4808 5.47 5.80 1.0657 7.467 0.693 223.611 8.429 0.960 18.684 0.4303 4.90 5.10 0.9538 8.517 0.791 255.057 8.559 0.975 18.974 0.3765 4.29 4.40 0.8345 9.723 0.903 291.182 8.645 0.984 19.163 0.3231 3.68 3.74 0.7162 11.098 1.031 332.361 8.726 0.993 19.343 0.2821 3.21 3.23 0.6253 12.473 1.158 373.541 8.751 0.996 19.399 0.2524 2.87 2.88 0.5596 13.848 1.286 414.720 8.784 1.000 19.471 0.2382 2.71 2.71 0.5281 15.217 1.413 455.712 8.800 1.002 19.507 0.2301 2.62 2.61 0.5100 16.592 1.541 496.891 8.787 1.000 19.478 0.2304 2.62 2.62 0.5106 22.142 2.056 663.106 8.808 1.003 19.525 0.2204 2.51 2.50 0.4886 27.692 2.572 829.320 8.814 1.003 19.538 0.2166 2.47 2.46 0.4801 33.242 3.087 995.535 8.795 1.001 19.496 0.2202 2.51 2.50 0.4882 38.792 3.603 1161.749 8.786 1.000 19.476 0.2176 2.48 2.48 0.4824 RUN NUMBER 1W01609 AXIAL POSITION = 695.0 MM SPAN POSITION = 0.0 MM FREE-STREAM VELOCITY = 9.03 M/S FRICTION VELOCITY = 0.4517 M/S FREE-STREAM TURBULENCE = 2.287 % X-REYNOLDS NUMBER = 41.67 X10**4 FLUID DENSITY = 1.202 KG/M**3 KINEMATIC VISCOSITY = 1.505 X10(-5)MSQ/S BOUNDARY LAYER THICKNESS (99.0%) = 12.07 MM DISPLACEMENT THICKNESS = 1.675 MM MOMENTUM THICKNESS = 1.142 MM ENERGY THICKNESS = 2.027 MM FORM FACTOR H = 1.466 FORM FACTOR E = 1.775 RDELTASTAR = 1004.0 RTHETA = 684.8 SKIN FRICTION COEFFICIENT = 0.005010 CALCULATED CF = 0.004334 LAW OF THE WALL OFFSET = 5.20 KARMAN CONSTANT = 0.410 FORM FACTOR G = 6.353 CLAUSER DELTA = 33.457 MM WAKE FACTOR PI = 0.028 1 Y Y/DEL YPLUS U U/UO UPLUS u u/UO u/U u/UTAU MM M/S M/S % % 0.029 0.002 0.870 0.365 0.040 0.807 0.0935 1.04 25.64 0.2070 0.035 0.003 1.058 0.443 0.049 0.981 0.1106 1.23 24.95 0.2449 0.042 0.003 1.245 0.522 0.058 1.155 0.1291 1.43 24.73 0.2857 0.048 0.004 1.433 0.600 0.067 1.329 0.1550 1.72 25.82 0.3432 0.054 0.004 1.620 0.679 0.075 1.503 0.1889 2.09 27.82 0.4183 0.060 0.005 1.808 0.758 0.084 1.677 0.2188 2.42 28.87 0.4843 0.067 0.006 1.996 0.836 0.093 1.851 0.2535 2.81 30.31 0.5612 0.073 0.006 2.183 0.915 0.101 2.025 0.2846 3.15 31.10 0.6300 0.085 0.007 2.558 1.072 0.119 2.373 0.3394 3.76 31.66 0.7513 0.098 0.008 2.933 1.229 0.136 2.721 0.4086 4.53 33.24 0.9045 0.110 0.009 3.308 1.386 0.154 3.069 0.4675 5.18 33.72 1.0349 0.123 0.010 3.684 1.513 0.168 3.349 0.5221 5.78 34.51 1.1558 0.142 0.012 4.246 1.684 0.187 3.728 0.5892 6.53 34.99 1.3043 0.167 0.014 4.996 1.942 0.215 4.298 0.6856 7.60 35.31 1.5178 0.192 0.016 5.747 2.200 0.244 4.871 0.7817 8.66 35.53 1.7305 0.217 0.018 6.497 2.453 0.272 5.431 0.8719 9.66 35.54 1.9302 0.254 0.021 7.622 2.808 0.311 6.216 0.9679 10.72 34.47 2.1427 0.285 0.024 8.560 3.069 0.340 6.794 1.0366 11.49 33.78 2.2950 0.329 0.027 9.873 3.464 0.384 7.669 1.1003 12.19 31.76 2.4360 0.379 0.031 11.373 3.825 0.424 8.467 1.1438 12.67 29.91 2.5322 0.435 0.036 13.061 4.220 0.468 9.343 1.1678 12.94 27.67 2.5852 0.498 0.041 14.937 4.538 0.503 10.046 1.1861 13.14 26.14 2.6259 0.573 0.047 17.188 4.938 0.547 10.932 1.1815 13.09 23.93 2.6157 0.654 0.054 19.626 5.220 0.578 11.557 1.1569 12.82 22.16 2.5613 0.748 0.062 22.439 5.485 0.608 12.144 1.1270 12.49 20.54 2.4949 0.860 0.071 25.815 5.757 0.638 12.745 1.0784 11.95 18.73 2.3873 0.985 0.082 29.566 5.964 0.661 13.203 1.0281 11.39 17.24 2.2760 1.129 0.094 33.880 6.166 0.683 13.650 0.9796 10.85 15.89 2.1686 1.292 0.107 38.756 6.366 0.705 14.093 0.9259 10.26 14.55 2.0499 1.479 0.123 44.383 6.540 0.725 14.479 0.8780 9.73 13.42 1.9437 1.698 0.141 50.947 6.692 0.741 14.815 0.8347 9.25 12.47 1.8480 1.942 0.161 58.262 6.845 0.758 15.155 0.7965 8.83 11.64 1.7633 2.223 0.184 66.702 6.997 0.775 15.491 0.7692 8.52 10.99 1.7028 2.548 0.211 76.455 7.151 0.792 15.832 0.7301 8.09 10.21 1.6163 2.917 0.242 87.521 7.305 0.809 16.173 0.7060 7.82 9.66 1.5630 3.342 0.277 100.274 7.499 0.831 16.602 0.6794 7.53 9.06 1.5041 3.829 0.317 114.904 7.662 0.849 16.963 0.6552 7.26 8.55 1.4505 4.385 0.363 131.596 7.806 0.865 17.280 0.6270 6.95 8.03 1.3881 5.023 0.416 150.727 8.005 0.887 17.722 0.5911 6.55 7.38 1.3085 5.754 0.477 172.671 8.162 0.904 18.070 0.5550 6.15 6.80 1.2287 6.592 0.546 197.803 8.349 0.925 18.484 0.5147 5.70 6.17 1.1395 7.554 0.626 226.687 8.548 0.947 18.924 0.4577 5.07 5.35 1.0133 8.648 0.716 259.509 8.681 0.962 19.218 0.4108 4.55 4.73 0.9096 9.910 0.821 297.395 8.823 0.978 19.533 0.3537 3.92 4.01 0.7831 11.348 0.940 340.533 8.917 0.988 19.742 0.3022 3.35 3.39 0.6689 12.998 1.077 390.047 8.968 0.994 19.854 0.2563 2.84 2.86 0.5674 14.648 1.213 439.562 9.010 0.998 19.948 0.2378 2.64 2.64 0.5265 16.298 1.350 489.076 9.025 1.000 19.980 0.2216 2.46 2.46 0.4905 17.948 1.487 538.591 9.054 1.003 20.044 0.2173 2.41 2.40 0.4811 19.592 1.623 587.918 9.050 1.003 20.036 0.2119 2.35 2.34 0.4691 26.092 2.161 782.975 9.024 1.000 19.978 0.2115 2.34 2.34 0.4683 32.592 2.700 978.033 9.038 1.001 20.010 0.2081 2.31 2.30 0.4608 39.092 3.238 1173.090 9.027 1.000 19.984 0.2057 2.28 2.28 0.4553 45.592 3.776 1368.147 9.029 1.000 19.988 0.2064 2.29 2.29 0.4570 RUN NUMBER 1W01610 AXIAL POSITION = 795.0 MM SPAN POSITION = 0.0 MM FREE-STREAM VELOCITY = 9.18 M/S FRICTION VELOCITY = 0.4485 M/S FREE-STREAM TURBULENCE = 2.143 % X-REYNOLDS NUMBER = 48.62 X10**4 FLUID DENSITY = 1.204 KG/M**3 KINEMATIC VISCOSITY = 1.502 X10(-5)MSQ/S BOUNDARY LAYER THICKNESS (99.0%) = 13.29 MM DISPLACEMENT THICKNESS = 1.866 MM MOMENTUM THICKNESS = 1.276 MM ENERGY THICKNESS = 2.265 MM FORM FACTOR H = 1.463 FORM FACTOR E = 1.775 RDELTASTAR = 1141.3 RTHETA = 780.4 SKIN FRICTION COEFFICIENT = 0.004769 CALCULATED CF = 0.004209 LAW OF THE WALL OFFSET = 5.20 KARMAN CONSTANT = 0.410 FORM FACTOR G = 6.476 CLAUSER DELTA = 38.214 MM WAKE FACTOR PI = 0.096 1 Y Y/DEL YPLUS U U/UO UPLUS u u/UO u/U u/UTAU MM M/S M/S % % 0.029 0.002 0.866 0.332 0.036 0.739 0.0966 1.05 29.13 0.2154 0.035 0.003 1.053 0.403 0.044 0.899 0.0990 1.08 24.56 0.2207 0.042 0.003 1.239 0.474 0.052 1.058 0.1165 1.27 24.55 0.2597 0.048 0.004 1.426 0.546 0.059 1.217 0.1349 1.47 24.71 0.3007 0.054 0.004 1.613 0.617 0.067 1.376 0.1595 1.74 25.83 0.3555 0.060 0.005 1.799 0.689 0.075 1.536 0.1868 2.03 27.12 0.4166 0.067 0.005 1.986 0.760 0.083 1.695 0.2157 2.35 28.37 0.4809 0.073 0.005 2.173 0.832 0.091 1.854 0.2491 2.71 29.95 0.5554 0.085 0.006 2.546 0.975 0.106 2.173 0.3051 3.32 31.31 0.6804 0.098 0.007 2.919 1.118 0.122 2.492 0.3647 3.97 32.63 0.8131 0.110 0.008 3.293 1.260 0.137 2.810 0.4097 4.46 32.50 0.9134 0.129 0.010 3.853 1.438 0.157 3.205 0.4960 5.40 34.51 1.1060 0.148 0.011 4.413 1.594 0.174 3.554 0.5646 6.15 35.42 1.2588 0.173 0.013 5.159 1.855 0.202 4.137 0.6674 7.27 35.97 1.4880 0.198 0.015 5.906 2.112 0.230 4.708 0.7538 8.21 35.70 1.6806 0.223 0.017 6.653 2.353 0.256 5.246 0.8460 9.21 35.96 1.8863 0.260 0.020 7.773 2.728 0.297 6.083 0.9583 10.43 35.12 2.1366 0.298 0.022 8.893 3.039 0.331 6.775 1.0295 11.21 33.88 2.2954 0.342 0.026 10.199 3.425 0.373 7.637 1.1054 12.04 32.27 2.4646 0.392 0.029 11.692 3.849 0.419 8.583 1.1571 12.60 30.06 2.5798 0.448 0.034 13.372 4.198 0.457 9.359 1.1817 12.87 28.15 2.6347 0.517 0.039 15.426 4.588 0.500 10.230 1.1865 12.92 25.86 2.6454 0.592 0.045 17.666 4.926 0.536 10.984 1.1783 12.83 23.92 2.6272 0.679 0.051 20.279 5.242 0.571 11.687 1.1562 12.59 22.06 2.5778 0.779 0.059 23.265 5.520 0.601 12.307 1.1218 12.21 20.32 2.5013 0.898 0.068 26.812 5.796 0.631 12.922 1.0748 11.70 18.55 2.3965 1.029 0.077 30.732 6.001 0.653 13.379 1.0301 11.22 17.17 2.2968 1.179 0.089 35.212 6.195 0.674 13.812 0.9701 10.56 15.66 2.1630 1.354 0.102 40.438 6.359 0.692 14.178 0.9283 10.11 14.60 2.0697 1.554 0.117 46.411 6.534 0.711 14.568 0.8819 9.60 13.50 1.9664 1.779 0.134 53.131 6.700 0.729 14.938 0.8400 9.15 12.54 1.8729 2.042 0.154 60.971 6.856 0.747 15.287 0.8058 8.77 11.75 1.7967 2.348 0.177 70.117 7.031 0.765 15.676 0.7679 8.36 10.92 1.7122 2.692 0.203 80.384 7.185 0.782 16.019 0.7480 8.14 10.41 1.6677 3.085 0.232 92.143 7.369 0.802 16.429 0.7132 7.77 9.68 1.5902 3.542 0.267 105.769 7.522 0.819 16.770 0.6914 7.53 9.19 1.5416 4.067 0.306 121.449 7.712 0.840 17.195 0.6648 7.24 8.62 1.4822 4.667 0.351 139.368 7.882 0.858 17.573 0.6406 6.97 8.13 1.4282 5.348 0.402 159.714 8.081 0.880 18.018 0.6077 6.62 7.52 1.3548 6.142 0.462 183.420 8.253 0.899 18.401 0.5732 6.24 6.95 1.2780 7.042 0.530 210.299 8.459 0.921 18.861 0.5332 5.81 6.30 1.1888 8.079 0.608 241.285 8.618 0.938 19.215 0.4886 5.32 5.67 1.0895 9.273 0.698 276.937 8.781 0.956 19.579 0.4299 4.68 4.90 0.9585 10.635 0.800 317.629 8.939 0.973 19.929 0.3558 3.87 3.98 0.7932 12.198 0.918 364.295 9.055 0.986 20.190 0.3087 3.36 3.41 0.6882 13.998 1.053 418.053 9.121 0.993 20.336 0.2564 2.79 2.81 0.5718 15.792 1.188 471.625 9.181 1.000 20.469 0.2326 2.53 2.53 0.5186 17.592 1.324 525.383 9.189 1.000 20.487 0.2131 2.32 2.32 0.4751 19.385 1.459 578.954 9.178 0.999 20.463 0.2076 2.26 2.26 0.4628 21.185 1.594 632.713 9.200 1.002 20.512 0.1985 2.16 2.16 0.4426 28.185 2.121 841.773 9.191 1.001 20.493 0.2006 2.18 2.18 0.4473 35.185 2.648 1050.833 9.204 1.002 20.522 0.1988 2.16 2.16 0.4433 42.185 3.175 1259.893 9.190 1.001 20.491 0.1985 2.16 2.16 0.4427 49.185 3.701 1468.953 9.207 1.002 20.528 0.1968 2.14 2.14 0.4388 RUN NUMBER 1W01701 AXIAL POSITION = 895.0 MM SPAN POSITION = 0.0 MM FREE-STREAM VELOCITY = 9.25 M/S FRICTION VELOCITY = 0.4409 M/S FREE-STREAM TURBULENCE = 2.071 % X-REYNOLDS NUMBER = 55.14 X10**4 FLUID DENSITY = 1.204 KG/M**3 KINEMATIC VISCOSITY = 1.502 X10(-5)MSQ/S BOUNDARY LAYER THICKNESS (99.0%) = 14.74 MM DISPLACEMENT THICKNESS = 2.126 MM MOMENTUM THICKNESS = 1.474 MM ENERGY THICKNESS = 2.615 MM FORM FACTOR H = 1.443 FORM FACTOR E = 1.774 RDELTASTAR = 1309.7 RTHETA = 907.9 SKIN FRICTION COEFFICIENT = 0.004540 CALCULATED CF = 0.004170 LAW OF THE WALL OFFSET = 5.20 KARMAN CONSTANT = 0.410 FORM FACTOR G = 6.439 CLAUSER DELTA = 44.616 MM WAKE FACTOR PI = 0.160 1 Y Y/DEL YPLUS U U/UO UPLUS u u/UO u/U u/UTAU MM M/S M/S % % 0.029 0.002 0.851 0.349 0.038 0.792 0.1036 1.12 29.66 0.2350 0.035 0.002 1.035 0.425 0.046 0.963 0.1230 1.33 28.98 0.2791 0.042 0.003 1.218 0.500 0.054 1.134 0.1421 1.54 28.43 0.3223 0.048 0.003 1.402 0.575 0.062 1.304 0.1632 1.76 28.38 0.3702 0.054 0.004 1.585 0.650 0.070 1.475 0.1843 1.99 28.33 0.4180 0.060 0.004 1.769 0.726 0.078 1.646 0.2136 2.31 29.43 0.4844 0.067 0.005 1.952 0.801 0.087 1.817 0.2381 2.57 29.72 0.5400 0.073 0.005 2.136 0.876 0.095 1.987 0.2693 2.91 30.74 0.6108 0.085 0.006 2.503 1.027 0.111 2.329 0.3327 3.60 32.41 0.7547 0.098 0.007 2.869 1.177 0.127 2.670 0.3910 4.23 33.21 0.8869 0.110 0.007 3.236 1.328 0.144 3.012 0.4551 4.92 34.28 1.0324 0.129 0.009 3.787 1.512 0.163 3.430 0.5378 5.81 35.56 1.2198 0.148 0.010 4.337 1.691 0.183 3.835 0.6155 6.65 36.40 1.3961 0.173 0.012 5.071 1.945 0.210 4.411 0.7157 7.74 36.80 1.6234 0.198 0.013 5.805 2.179 0.235 4.941 0.8018 8.66 36.80 1.8185 0.229 0.016 6.722 2.485 0.269 5.636 0.9018 9.75 36.29 2.0454 0.260 0.018 7.640 2.808 0.303 6.369 0.9863 10.66 35.13 2.2372 0.304 0.021 8.924 3.196 0.345 7.248 1.0697 11.56 33.47 2.4262 0.348 0.024 10.208 3.538 0.382 8.025 1.1243 12.15 31.78 2.5501 0.398 0.027 11.676 3.910 0.423 8.870 1.1680 12.62 29.87 2.6492 0.460 0.031 13.511 4.262 0.461 9.667 1.1807 12.76 27.70 2.6780 0.523 0.035 15.345 4.605 0.498 10.444 1.1723 12.67 25.46 2.6590 0.604 0.041 17.730 4.911 0.531 11.140 1.1648 12.59 23.72 2.6419 0.692 0.047 20.299 5.213 0.563 11.824 1.1374 12.29 21.82 2.5797 0.798 0.054 23.418 5.470 0.591 12.407 1.0995 11.88 20.10 2.4939 0.917 0.062 26.904 5.711 0.617 12.954 1.0603 11.46 18.57 2.4049 1.054 0.072 30.940 5.921 0.640 13.431 1.0078 10.89 17.02 2.2859 1.210 0.082 35.527 6.108 0.660 13.853 0.9623 10.40 15.76 2.1827 1.392 0.094 40.847 6.293 0.680 14.273 0.9174 9.91 14.58 2.0808 1.598 0.108 46.902 6.431 0.695 14.586 0.8749 9.46 13.61 1.9844 1.835 0.125 53.874 6.591 0.712 14.950 0.8390 9.07 12.73 1.9030 2.104 0.143 61.763 6.751 0.730 15.313 0.8044 8.69 11.91 1.8245 2.417 0.164 70.936 6.884 0.744 15.613 0.7814 8.44 11.35 1.7724 2.773 0.188 81.394 7.072 0.764 16.040 0.7630 8.25 10.79 1.7306 3.185 0.216 93.503 7.203 0.778 16.338 0.7296 7.88 10.13 1.6548 3.660 0.248 107.447 7.414 0.801 16.816 0.7118 7.69 9.60 1.6145 4.204 0.285 123.408 7.597 0.821 17.231 0.6934 7.49 9.13 1.5727 4.829 0.328 141.755 7.778 0.841 17.643 0.6667 7.20 8.57 1.5121 5.542 0.376 162.671 7.984 0.863 18.109 0.6425 6.94 8.05 1.4574 6.367 0.432 186.888 8.191 0.885 18.578 0.6039 6.53 7.37 1.3698 7.310 0.496 214.592 8.376 0.905 18.998 0.5711 6.17 6.82 1.2954 8.398 0.570 246.516 8.591 0.928 19.486 0.5161 5.58 6.01 1.1706 9.642 0.654 283.026 8.742 0.945 19.829 0.4711 5.09 5.39 1.0685 11.073 0.751 325.040 8.929 0.965 20.252 0.3972 4.29 4.45 0.9009 12.710 0.862 373.109 9.045 0.977 20.515 0.3354 3.62 3.71 0.7608 14.598 0.990 428.517 9.175 0.992 20.811 0.2693 2.91 2.93 0.6108 16.479 1.118 483.741 9.225 0.997 20.924 0.2334 2.52 2.53 0.5293 18.367 1.246 539.148 9.227 0.997 20.929 0.2137 2.31 2.32 0.4847 20.254 1.374 594.556 9.275 1.002 21.038 0.2049 2.21 2.21 0.4647 22.135 1.502 649.780 9.278 1.003 21.045 0.1985 2.15 2.14 0.4503 29.435 1.997 864.071 9.285 1.003 21.061 0.1886 2.04 2.03 0.4278 36.735 2.492 1078.362 9.281 1.003 21.052 0.1904 2.06 2.05 0.4318 44.035 2.987 1292.654 9.264 1.001 21.013 0.1910 2.06 2.06 0.4333 51.335 3.483 1506.945 9.268 1.002 21.022 0.1916 2.07 2.07 0.4346 RUN NUMBER 1W01702 AXIAL POSITION = 995.0 MM SPAN POSITION = 0.0 MM FREE-STREAM VELOCITY = 9.25 M/S FRICTION VELOCITY = 0.4257 M/S FREE-STREAM TURBULENCE = 1.952 % X-REYNOLDS NUMBER = 61.30 X10**4 FLUID DENSITY = 1.204 KG/M**3 KINEMATIC VISCOSITY = 1.502 X10(-5)MSQ/S BOUNDARY LAYER THICKNESS (99.0%) = 16.92 MM DISPLACEMENT THICKNESS = 2.504 MM MOMENTUM THICKNESS = 1.733 MM ENERGY THICKNESS = 3.064 MM FORM FACTOR H = 1.444 FORM FACTOR E = 1.768 RDELTASTAR = 1542.7 RTHETA = 1068.0 SKIN FRICTION COEFFICIENT = 0.004233 CALCULATED CF = 0.003980 LAW OF THE WALL OFFSET = 5.20 KARMAN CONSTANT = 0.410 FORM FACTOR G = 6.688 CLAUSER DELTA = 54.427 MM WAKE FACTOR PI = 0.284 1 Y Y/DEL YPLUS U U/UO UPLUS u u/UO u/U u/UTAU MM M/S M/S % % 0.029 0.002 0.822 0.325 0.035 0.763 0.0938 1.01 28.86 0.2203 0.035 0.002 0.999 0.395 0.043 0.928 0.1064 1.15 26.93 0.2499 0.042 0.002 1.176 0.465 0.050 1.092 0.1250 1.35 26.87 0.2935 0.048 0.003 1.353 0.535 0.058 1.257 0.1489 1.61 27.82 0.3497 0.054 0.003 1.531 0.605 0.065 1.421 0.1688 1.82 27.89 0.3965 0.060 0.004 1.708 0.675 0.073 1.586 0.1932 2.09 28.61 0.4538 0.067 0.004 1.885 0.745 0.081 1.750 0.2242 2.42 30.08 0.5266 0.073 0.004 2.062 0.815 0.088 1.915 0.2521 2.72 30.93 0.5922 0.085 0.005 2.416 0.955 0.103 2.244 0.3106 3.36 32.51 0.7295 0.098 0.006 2.771 1.095 0.118 2.573 0.3695 3.99 33.73 0.8678 0.117 0.007 3.302 1.306 0.141 3.067 0.4585 4.95 35.12 1.0770 0.129 0.008 3.656 1.427 0.154 3.351 0.5153 5.57 36.12 1.2104 0.154 0.009 4.365 1.662 0.180 3.904 0.6174 6.67 37.14 1.4502 0.173 0.010 4.896 1.820 0.197 4.274 0.6805 7.35 37.40 1.5985 0.198 0.012 5.605 2.070 0.224 4.862 0.7747 8.37 37.43 1.8196 0.229 0.014 6.491 2.359 0.255 5.542 0.8703 9.40 36.89 2.0443 0.267 0.016 7.554 2.698 0.292 6.338 0.9718 10.50 36.02 2.2827 0.304 0.018 8.617 2.997 0.324 7.040 1.0249 11.07 34.20 2.4073 0.354 0.021 10.034 3.379 0.365 7.937 1.1072 11.96 32.77 2.6007 0.404 0.024 11.451 3.745 0.405 8.798 1.1402 12.32 30.44 2.6782 0.467 0.028 13.223 4.087 0.442 9.601 1.1674 12.62 28.56 2.7422 0.535 0.032 15.171 4.399 0.475 10.333 1.1644 12.58 26.47 2.7352 0.617 0.036 17.474 4.706 0.509 11.055 1.1491 12.42 24.42 2.6992 0.710 0.042 20.132 5.001 0.540 11.748 1.1228 12.13 22.45 2.6374 0.817 0.048 23.143 5.228 0.565 12.280 1.0931 11.81 20.91 2.5676 0.942 0.056 26.686 5.459 0.590 12.823 1.0518 11.37 19.27 2.4705 1.079 0.064 30.584 5.666 0.612 13.310 1.0108 10.92 17.84 2.3742 1.242 0.073 35.189 5.860 0.633 13.766 0.9727 10.51 16.60 2.2848 1.429 0.084 40.504 6.048 0.654 14.206 0.9253 10.00 15.30 2.1735 1.642 0.097 46.527 6.196 0.670 14.553 0.8766 9.47 14.15 2.0591 1.892 0.112 53.613 6.364 0.688 14.948 0.8498 9.18 13.35 1.9960 2.173 0.128 61.585 6.522 0.705 15.320 0.8242 8.91 12.64 1.9360 2.498 0.148 70.797 6.650 0.719 15.620 0.8006 8.65 12.04 1.8805 2.873 0.170 81.426 6.833 0.738 16.050 0.7776 8.40 11.38 1.8264 3.304 0.195 93.650 7.012 0.758 16.471 0.7631 8.25 10.88 1.7925 3.798 0.224 107.645 7.173 0.775 16.848 0.7341 7.93 10.23 1.7243 4.367 0.258 123.766 7.358 0.795 17.282 0.7171 7.75 9.75 1.6845 5.017 0.296 142.189 7.543 0.815 17.718 0.7079 7.65 9.39 1.6628 5.767 0.341 163.448 7.752 0.838 18.208 0.6823 7.37 8.80 1.6028 6.629 0.392 187.895 7.969 0.861 18.720 0.6504 7.03 8.16 1.5278 7.623 0.450 216.062 8.182 0.884 19.218 0.6167 6.66 7.54 1.4486 8.760 0.518 248.304 8.410 0.909 19.754 0.5696 6.15 6.77 1.3379 10.073 0.595 285.505 8.611 0.930 20.226 0.5134 5.55 5.96 1.2059 11.579 0.684 328.199 8.828 0.954 20.737 0.4576 4.94 5.18 1.0748 13.310 0.787 377.270 8.970 0.969 21.069 0.3797 4.10 4.23 0.8918 15.298 0.904 433.605 9.116 0.985 21.412 0.3172 3.43 3.48 0.7450 17.285 1.022 489.939 9.175 0.992 21.552 0.2567 2.77 2.80 0.6029 19.273 1.139 546.273 9.232 0.998 21.685 0.2228 2.41 2.41 0.5234 21.267 1.257 602.785 9.252 1.000 21.732 0.2034 2.20 2.20 0.4778 23.254 1.374 659.119 9.270 1.002 21.775 0.1997 2.16 2.15 0.4691 30.904 1.826 875.954 9.284 1.003 21.809 0.1874 2.02 2.02 0.4401 38.554 2.278 1092.788 9.276 1.002 21.789 0.1860 2.01 2.01 0.4370 46.204 2.731 1309.622 9.272 1.002 21.779 0.1830 1.98 1.97 0.4299 53.854 3.183 1526.456 9.270 1.002 21.775 0.1807 1.95 1.95 0.4244 RUN NUMBER 1W01703 AXIAL POSITION = 1095.0 MM SPAN POSITION = 0.0 MM FREE-STREAM VELOCITY = 9.10 M/S FRICTION VELOCITY = 0.4044 M/S FREE-STREAM TURBULENCE = 1.976 % X-REYNOLDS NUMBER = 65.81 X10**4 FLUID DENSITY = 1.194 KG/M**3 KINEMATIC VISCOSITY = 1.515 X10(-5)MSQ/S BOUNDARY LAYER THICKNESS (99.0%) = 19.26 MM DISPLACEMENT THICKNESS = 2.968 MM MOMENTUM THICKNESS = 2.045 MM ENERGY THICKNESS = 3.600 MM FORM FACTOR H = 1.451 FORM FACTOR E = 1.760 RDELTASTAR = 1783.7 RTHETA = 1229.2 SKIN FRICTION COEFFICIENT = 0.003947 CALCULATED CF = 0.003794 LAW OF THE WALL OFFSET = 5.20 KARMAN CONSTANT = 0.410 FORM FACTOR G = 6.998 CLAUSER DELTA = 66.809 MM WAKE FACTOR PI = 0.432 1 Y Y/DEL YPLUS U U/UO UPLUS u u/UO u/U u/UTAU MM M/S M/S % % 0.029 0.002 0.774 0.274 0.030 0.678 0.0876 0.96 31.97 0.2168 0.035 0.002 0.941 0.333 0.037 0.824 0.0909 1.00 27.28 0.2248 0.042 0.002 1.108 0.392 0.043 0.970 0.1058 1.16 26.97 0.2616 0.048 0.002 1.275 0.451 0.050 1.116 0.1210 1.33 26.81 0.2992 0.054 0.003 1.442 0.510 0.056 1.262 0.1415 1.55 27.72 0.3500 0.060 0.003 1.609 0.570 0.063 1.408 0.1599 1.76 28.07 0.3954 0.067 0.003 1.775 0.629 0.069 1.555 0.1786 1.96 28.42 0.4418 0.079 0.004 2.109 0.747 0.082 1.847 0.2314 2.54 30.99 0.5723 0.092 0.005 2.443 0.865 0.095 2.139 0.2765 3.04 31.97 0.6838 0.104 0.005 2.777 0.983 0.108 2.431 0.3354 3.69 34.12 0.8296 0.117 0.006 3.110 1.101 0.121 2.723 0.3839 4.22 34.86 0.9495 0.135 0.007 3.611 1.278 0.140 3.162 0.4630 5.09 36.22 1.1451 0.160 0.008 4.278 1.499 0.165 3.707 0.5678 6.24 37.88 1.4042 0.185 0.010 4.946 1.708 0.188 4.225 0.6566 7.21 38.44 1.6239 0.217 0.011 5.780 2.017 0.222 4.987 0.7642 8.40 37.90 1.8899 0.248 0.013 6.615 2.313 0.254 5.720 0.8628 9.48 37.30 2.1336 0.285 0.015 7.616 2.616 0.287 6.470 0.9526 10.47 36.41 2.3559 0.329 0.017 8.784 2.987 0.328 7.387 1.0281 11.30 34.42 2.5425 0.385 0.020 10.286 3.343 0.367 8.266 1.0873 11.95 32.53 2.6889 0.442 0.023 11.788 3.699 0.406 9.148 1.1199 12.30 30.27 2.7697 0.510 0.026 13.623 4.038 0.444 9.986 1.1324 12.44 28.04 2.8005 0.592 0.031 15.792 4.342 0.477 10.739 1.1194 12.30 25.78 2.7683 0.685 0.036 18.295 4.642 0.510 11.481 1.0927 12.01 23.54 2.7023 0.785 0.041 20.965 4.854 0.533 12.005 1.0790 11.85 22.23 2.6685 0.910 0.047 24.303 5.081 0.558 12.567 1.0425 11.45 20.52 2.5782 1.054 0.055 28.141 5.279 0.580 13.056 1.0017 11.01 18.98 2.4774 1.217 0.063 32.479 5.501 0.604 13.605 0.9581 10.53 17.41 2.3693 1.404 0.073 37.485 5.656 0.621 13.987 0.9206 10.11 16.28 2.2768 1.623 0.084 43.326 5.794 0.637 14.329 0.8821 9.69 15.22 2.1814 1.873 0.097 50.000 5.944 0.653 14.699 0.8539 9.38 14.37 2.1117 2.160 0.112 57.676 6.107 0.671 15.103 0.8364 9.19 13.70 2.0685 2.498 0.130 66.687 6.260 0.688 15.482 0.8110 8.91 12.95 2.0056 2.885 0.150 77.033 6.410 0.704 15.852 0.7907 8.69 12.33 1.9553 3.329 0.173 88.881 6.598 0.725 16.318 0.7815 8.59 11.84 1.9328 3.842 0.199 102.564 6.778 0.745 16.761 0.7712 8.47 11.38 1.9073 4.435 0.230 118.416 6.969 0.766 17.236 0.7407 8.14 10.63 1.8318 5.123 0.266 136.772 7.129 0.783 17.631 0.7275 7.99 10.20 1.7992 5.917 0.307 157.964 7.396 0.813 18.292 0.7166 7.87 9.69 1.7722 6.835 0.355 182.493 7.581 0.833 18.749 0.6868 7.55 9.06 1.6985 7.892 0.410 210.694 7.811 0.858 19.316 0.6579 7.23 8.42 1.6269 9.110 0.473 243.233 8.056 0.885 19.922 0.6214 6.83 7.71 1.5368 10.517 0.546 280.779 8.278 0.909 20.471 0.5690 6.25 6.87 1.4071 12.148 0.631 324.331 8.550 0.939 21.145 0.5020 5.51 5.87 1.2414 14.023 0.728 374.392 8.742 0.960 21.619 0.4181 4.59 4.78 1.0340 16.192 0.841 432.295 8.885 0.976 21.972 0.3462 3.80 3.90 0.8561 18.698 0.971 499.209 9.010 0.990 22.283 0.2693 2.96 2.99 0.6661 21.198 1.101 565.956 9.069 0.996 22.427 0.2296 2.52 2.53 0.5677 23.704 1.231 632.870 9.099 1.000 22.503 0.2039 2.24 2.24 0.5043 26.210 1.361 699.784 9.117 1.002 22.548 0.1922 2.11 2.11 0.4753 28.710 1.491 766.531 9.111 1.001 22.533 0.1900 2.09 2.08 0.4698 38.060 1.976 1016.166 9.101 1.000 22.508 0.1842 2.02 2.02 0.4554 47.410 2.462 1265.800 9.105 1.000 22.518 0.1807 1.99 1.98 0.4469 56.760 2.948 1515.435 9.104 1.000 22.514 0.1812 1.99 1.99 0.4481 66.110 3.433 1765.069 9.109 1.001 22.528 0.1798 1.98 1.97 0.4447 RUN NUMBER 1W01704 AXIAL POSITION = 1195.0 MM SPAN POSITION = 0.0 MM FREE-STREAM VELOCITY = 8.86 M/S FRICTION VELOCITY = 0.3786 M/S FREE-STREAM TURBULENCE = 1.971 % X-REYNOLDS NUMBER = 69.82 X10**4 FLUID DENSITY = 1.193 KG/M**3 KINEMATIC VISCOSITY = 1.516 X10(-5)MSQ/S BOUNDARY LAYER THICKNESS (99.0%) = 21.84 MM DISPLACEMENT THICKNESS = 3.573 MM MOMENTUM THICKNESS = 2.438 MM ENERGY THICKNESS = 4.266 MM FORM FACTOR H = 1.465 FORM FACTOR E = 1.750 RDELTASTAR = 2087.6 RTHETA = 1424.7 SKIN FRICTION COEFFICIENT = 0.003656 CALCULATED CF = 0.003567 LAW OF THE WALL OFFSET = 5.20 KARMAN CONSTANT = 0.410 FORM FACTOR G = 7.427 CLAUSER DELTA = 83.564 MM WAKE FACTOR PI = 0.573 1 Y Y/DEL YPLUS U U/UO UPLUS u u/UO u/U u/UTAU MM M/S M/S % % 0.029 0.001 0.724 0.250 0.028 0.661 0.0803 0.91 32.06 0.2121 0.035 0.002 0.881 0.304 0.034 0.804 0.0870 0.98 28.57 0.2297 0.042 0.002 1.037 0.358 0.040 0.947 0.0990 1.12 27.61 0.2614 0.048 0.002 1.193 0.412 0.047 1.089 0.1106 1.25 26.82 0.2921 0.054 0.002 1.349 0.466 0.053 1.232 0.1276 1.44 27.35 0.3369 0.060 0.003 1.505 0.520 0.059 1.374 0.1453 1.64 27.93 0.3837 0.067 0.003 1.661 0.574 0.065 1.517 0.1689 1.91 29.40 0.4460 0.079 0.004 1.974 0.682 0.077 1.802 0.2122 2.40 31.10 0.5604 0.092 0.004 2.286 0.790 0.089 2.087 0.2571 2.90 32.53 0.6789 0.104 0.005 2.598 0.898 0.101 2.372 0.3095 3.49 34.46 0.8173 0.123 0.006 3.067 1.060 0.120 2.800 0.3882 4.38 36.62 1.0253 0.142 0.006 3.535 1.222 0.138 3.227 0.4590 5.18 37.56 1.2123 0.160 0.007 4.003 1.382 0.156 3.649 0.5248 5.93 37.99 1.3862 0.192 0.009 4.784 1.599 0.181 4.222 0.6204 7.01 38.81 1.6385 0.217 0.010 5.409 1.760 0.199 4.648 0.6922 7.82 39.33 1.8282 0.254 0.012 6.345 2.074 0.234 5.477 0.7966 9.00 38.41 2.1040 0.292 0.013 7.282 2.367 0.267 6.252 0.8820 9.96 37.26 2.3296 0.342 0.016 8.531 2.702 0.305 7.136 0.9573 10.81 35.43 2.5284 0.392 0.018 9.780 2.998 0.339 7.917 1.0125 11.43 33.78 2.6741 0.454 0.021 11.342 3.359 0.379 8.871 1.0446 11.80 31.10 2.7588 0.529 0.024 13.215 3.671 0.415 9.695 1.0690 12.07 29.12 2.8235 0.610 0.028 15.245 3.956 0.447 10.447 1.0616 11.99 26.84 2.8039 0.704 0.032 17.587 4.222 0.477 11.151 1.0565 11.93 25.02 2.7903 0.817 0.037 20.398 4.500 0.508 11.885 1.0283 11.61 22.85 2.7160 0.942 0.043 23.520 4.692 0.530 12.393 1.0060 11.36 21.44 2.6569 1.092 0.050 27.268 4.906 0.554 12.956 0.9667 10.92 19.71 2.5531 1.260 0.058 31.483 5.052 0.570 13.342 0.9417 10.63 18.64 2.4872 1.460 0.067 36.480 5.228 0.590 13.809 0.8976 10.14 17.17 2.3706 1.692 0.077 42.257 5.399 0.610 14.260 0.8747 9.88 16.20 2.3102 1.954 0.089 48.814 5.566 0.629 14.700 0.8504 9.60 15.28 2.2459 2.260 0.103 56.465 5.719 0.646 15.105 0.8279 9.35 14.48 2.1865 2.617 0.120 65.365 5.836 0.659 15.413 0.8102 9.15 13.88 2.1400 3.023 0.138 75.514 5.984 0.676 15.804 0.7849 8.86 13.12 2.0731 3.498 0.160 87.380 6.159 0.695 16.265 0.7840 8.85 12.73 2.0705 4.042 0.185 100.964 6.335 0.715 16.731 0.7674 8.67 12.11 2.0267 4.679 0.214 116.890 6.494 0.733 17.152 0.7501 8.47 11.55 1.9811 5.410 0.248 135.158 6.686 0.755 17.658 0.7407 8.36 11.08 1.9562 6.254 0.286 156.236 6.930 0.783 18.303 0.7315 8.26 10.56 1.9319 7.235 0.331 180.749 7.116 0.804 18.794 0.7160 8.09 10.06 1.8910 8.367 0.383 209.010 7.379 0.833 19.489 0.6824 7.71 9.25 1.8023 9.673 0.443 241.642 7.625 0.861 20.139 0.6544 7.39 8.58 1.7283 11.185 0.512 279.427 7.869 0.889 20.782 0.6129 6.92 7.79 1.6188 12.935 0.592 323.145 8.132 0.918 21.478 0.5565 6.28 6.84 1.4699 14.954 0.685 373.577 8.372 0.945 22.112 0.4755 5.37 5.68 1.2559 17.292 0.792 431.972 8.568 0.968 22.630 0.3903 4.41 4.56 1.0308 19.998 0.916 499.579 8.723 0.985 23.039 0.3075 3.47 3.53 0.8122 22.698 1.039 567.030 8.812 0.995 23.273 0.2418 2.73 2.74 0.6385 25.404 1.163 634.636 8.840 0.998 23.348 0.2165 2.44 2.45 0.5718 28.110 1.287 702.243 8.860 1.000 23.400 0.1950 2.20 2.20 0.5149 30.810 1.411 769.694 8.859 1.000 23.398 0.1842 2.08 2.08 0.4865 40.529 1.855 1012.485 8.859 1.000 23.399 0.1785 2.02 2.02 0.4716 50.242 2.300 1255.121 8.874 1.002 23.438 0.1763 1.99 1.99 0.4658 59.954 2.745 1497.756 8.873 1.002 23.434 0.1747 1.97 1.97 0.4614 69.673 3.190 1740.547 8.866 1.001 23.416 0.1746 1.97 1.97 0.4611 RUN NUMBER 1W01705 AXIAL POSITION = 1295.0 MM SPAN POSITION = 0.0 MM FREE-STREAM VELOCITY = 8.61 M/S FRICTION VELOCITY = 0.3511 M/S FREE-STREAM TURBULENCE = 2.006 % X-REYNOLDS NUMBER = 73.49 X10**4 FLUID DENSITY = 1.192 KG/M**3 KINEMATIC VISCOSITY = 1.518 X10(-5)MSQ/S BOUNDARY LAYER THICKNESS (99.0%) = 25.79 MM DISPLACEMENT THICKNESS = 4.399 MM MOMENTUM THICKNESS = 2.972 MM ENERGY THICKNESS = 5.168 MM FORM FACTOR H = 1.480 FORM FACTOR E = 1.739 RDELTASTAR = 2496.6 RTHETA = 1686.4 SKIN FRICTION COEFFICIENT = 0.003324 CALCULATED CF = 0.003329 LAW OF THE WALL OFFSET = 5.20 KARMAN CONSTANT = 0.410 FORM FACTOR G = 7.961 CLAUSER DELTA = 107.922 MM WAKE FACTOR PI = 0.837 1 Y Y/DEL YPLUS U U/UO UPLUS u u/UO u/U u/UTAU MM M/S M/S % % 0.029 0.001 0.671 0.222 0.026 0.633 0.0717 0.83 32.26 0.2041 0.035 0.001 0.815 0.270 0.031 0.769 0.0821 0.95 30.38 0.2337 0.042 0.002 0.960 0.318 0.037 0.906 0.0946 1.10 29.75 0.2694 0.048 0.002 1.105 0.366 0.042 1.042 0.1058 1.23 28.92 0.3014 0.054 0.002 1.249 0.414 0.048 1.178 0.1192 1.38 28.80 0.3394 0.060 0.002 1.394 0.462 0.054 1.315 0.1372 1.59 29.73 0.3908 0.067 0.003 1.538 0.510 0.059 1.451 0.1559 1.81 30.59 0.4440 0.079 0.003 1.828 0.605 0.070 1.724 0.1975 2.29 32.63 0.5626 0.092 0.004 2.117 0.701 0.081 1.997 0.2374 2.76 33.87 0.6762 0.110 0.004 2.550 0.845 0.098 2.406 0.3113 3.61 36.85 0.8866 0.129 0.005 2.984 0.988 0.115 2.815 0.3724 4.32 37.67 1.0606 0.148 0.006 3.418 1.132 0.131 3.224 0.4328 5.03 38.23 1.2327 0.173 0.007 3.996 1.278 0.148 3.638 0.5043 5.85 39.47 1.4362 0.198 0.008 4.575 1.446 0.168 4.119 0.5801 6.73 40.11 1.6521 0.229 0.009 5.298 1.650 0.192 4.699 0.6634 7.70 40.21 1.8894 0.273 0.011 6.310 1.938 0.225 5.520 0.7704 8.94 39.75 2.1940 0.317 0.012 7.322 2.250 0.261 6.407 0.8582 9.96 38.15 2.4441 0.367 0.014 8.478 2.560 0.297 7.290 0.9311 10.81 36.37 2.6518 0.423 0.016 9.780 2.843 0.330 8.096 0.9762 11.33 34.34 2.7802 0.492 0.019 11.370 3.133 0.364 8.923 0.9929 11.53 31.69 2.8276 0.573 0.022 13.250 3.462 0.402 9.861 1.0129 11.76 29.25 2.8846 0.667 0.026 15.418 3.737 0.434 10.644 1.0084 11.71 26.98 2.8718 0.773 0.030 17.876 3.975 0.462 11.321 0.9902 11.50 24.91 2.8201 0.898 0.035 20.768 4.224 0.490 12.030 0.9835 11.42 23.28 2.8009 1.048 0.041 24.238 4.396 0.510 12.519 0.9626 11.18 21.90 2.7415 1.217 0.047 28.142 4.586 0.532 13.060 0.9178 10.66 20.01 2.6139 1.410 0.055 32.624 4.756 0.552 13.543 0.8971 10.42 18.86 2.5549 1.642 0.064 37.973 4.886 0.567 13.916 0.8641 10.03 17.68 2.4610 1.904 0.074 44.046 5.052 0.587 14.387 0.8440 9.80 16.71 2.4035 2.210 0.086 51.130 5.183 0.602 14.760 0.8165 9.48 15.75 2.3253 2.567 0.100 59.372 5.328 0.619 15.175 0.8061 9.36 15.13 2.2958 2.979 0.115 68.914 5.480 0.636 15.606 0.7919 9.19 14.45 2.2553 3.460 0.134 80.047 5.617 0.652 15.997 0.7862 9.13 14.00 2.2391 4.023 0.156 93.060 5.796 0.673 16.507 0.7714 8.96 13.31 2.1969 4.673 0.181 108.096 5.975 0.694 17.017 0.7668 8.90 12.83 2.1837 5.423 0.210 125.446 6.154 0.714 17.527 0.7569 8.79 12.30 2.1557 6.298 0.244 145.688 6.343 0.736 18.064 0.7510 8.72 11.84 2.1387 7.317 0.284 169.255 6.579 0.764 18.736 0.7405 8.60 11.26 2.1090 8.498 0.329 196.581 6.811 0.791 19.396 0.7233 8.40 10.62 2.0599 9.867 0.383 228.245 7.072 0.821 20.140 0.7041 8.17 9.96 2.0053 11.460 0.444 265.114 7.356 0.854 20.950 0.6550 7.60 8.90 1.8654 13.304 0.516 307.766 7.617 0.884 21.694 0.6233 7.24 8.18 1.7751 15.454 0.599 357.502 7.900 0.917 22.498 0.5545 6.44 7.02 1.5793 17.942 0.696 415.047 8.150 0.946 23.211 0.4792 5.56 5.88 1.3647 20.835 0.808 481.989 8.373 0.972 23.846 0.3703 4.30 4.42 1.0546 24.198 0.938 559.774 8.508 0.988 24.231 0.2767 3.21 3.25 0.7881 27.554 1.068 637.416 8.574 0.995 24.419 0.2248 2.61 2.62 0.6403 30.917 1.199 715.201 8.608 0.999 24.516 0.1942 2.26 2.26 0.5532 34.279 1.329 792.987 8.598 0.998 24.486 0.1819 2.11 2.12 0.5181 37.635 1.459 870.628 8.619 1.001 24.546 0.1791 2.08 2.08 0.5102 45.654 1.770 1056.129 8.618 1.001 24.544 0.1740 2.02 2.02 0.4954 53.673 2.081 1241.629 8.627 1.002 24.569 0.1735 2.01 2.01 0.4942 61.692 2.392 1427.130 8.618 1.001 24.545 0.1741 2.02 2.02 0.4959 69.710 2.703 1612.630 8.645 1.004 24.621 0.1728 2.01 2.00 0.4921 RUN NUMBER 1W01706 AXIAL POSITION = 1395.0 MM SPAN POSITION = 0.0 MM FREE-STREAM VELOCITY = 8.29 M/S FRICTION VELOCITY = 0.3200 M/S FREE-STREAM TURBULENCE = 2.045 % X-REYNOLDS NUMBER = 76.18 X10**4 FLUID DENSITY = 1.192 KG/M**3 KINEMATIC VISCOSITY = 1.518 X10(-5)MSQ/S BOUNDARY LAYER THICKNESS (99.0%) = 30.17 MM DISPLACEMENT THICKNESS = 5.511 MM MOMENTUM THICKNESS = 3.651 MM ENERGY THICKNESS = 6.293 MM FORM FACTOR H = 1.510 FORM FACTOR E = 1.724 RDELTASTAR = 3009.8 RTHETA = 1993.8 SKIN FRICTION COEFFICIENT = 0.002981 CALCULATED CF = 0.003042 LAW OF THE WALL OFFSET = 5.20 KARMAN CONSTANT = 0.410 FORM FACTOR G = 8.743 CLAUSER DELTA = 142.759 MM WAKE FACTOR PI = 1.104 1 Y Y/DEL YPLUS U U/UO UPLUS u u/UO u/U u/UTAU MM M/S M/S % % 0.029 0.001 0.611 0.185 0.022 0.580 0.0791 0.95 42.64 0.2471 0.035 0.001 0.743 0.225 0.027 0.704 0.0915 1.10 40.57 0.2858 0.042 0.001 0.875 0.265 0.032 0.829 0.1011 1.22 38.09 0.3159 0.048 0.002 1.007 0.305 0.037 0.954 0.1187 1.43 38.87 0.3709 0.054 0.002 1.138 0.345 0.042 1.079 0.1334 1.61 38.64 0.4170 0.060 0.002 1.270 0.385 0.046 1.204 0.1513 1.83 39.26 0.4728 0.067 0.002 1.402 0.425 0.051 1.329 0.1686 2.03 39.64 0.5268 0.079 0.003 1.666 0.505 0.061 1.579 0.2006 2.42 39.71 0.6269 0.092 0.003 1.929 0.585 0.071 1.829 0.2315 2.79 39.57 0.7235 0.110 0.004 2.324 0.705 0.085 2.203 0.2800 3.38 39.71 0.8748 0.129 0.004 2.720 0.825 0.100 2.578 0.3299 3.98 39.99 1.0310 0.154 0.005 3.247 0.985 0.119 3.078 0.3888 4.69 39.47 1.2148 0.179 0.006 3.774 1.119 0.135 3.498 0.4561 5.50 40.75 1.4251 0.204 0.007 4.301 1.253 0.151 3.916 0.5240 6.32 41.81 1.6373 0.242 0.008 5.092 1.463 0.177 4.572 0.6081 7.34 41.56 1.9002 0.279 0.009 5.882 1.662 0.201 5.195 0.6953 8.39 41.82 2.1725 0.329 0.011 6.936 1.940 0.234 6.063 0.7801 9.41 40.21 2.4377 0.379 0.013 7.990 2.214 0.267 6.917 0.8450 10.19 38.17 2.6405 0.442 0.015 9.308 2.485 0.300 7.765 0.8991 10.85 36.18 2.8095 0.517 0.017 10.889 2.820 0.340 8.813 0.9418 11.36 33.39 2.9430 0.604 0.020 12.734 3.106 0.375 9.707 0.9419 11.36 30.32 2.9433 0.698 0.023 14.711 3.335 0.402 10.420 0.9425 11.37 28.26 2.9450 0.817 0.027 17.214 3.598 0.434 11.242 0.9460 11.41 26.30 2.9561 0.948 0.031 19.981 3.780 0.456 11.813 0.9290 11.21 24.57 2.9028 1.104 0.037 23.275 3.958 0.477 12.369 0.9072 10.94 22.92 2.8347 1.285 0.043 27.097 4.144 0.500 12.949 0.8878 10.71 21.43 2.7743 1.498 0.050 31.577 4.306 0.519 13.455 0.8596 10.37 19.96 2.6860 1.748 0.058 36.848 4.402 0.531 13.755 0.8408 10.14 19.10 2.6274 2.035 0.067 42.909 4.596 0.554 14.362 0.8259 9.96 17.97 2.5807 2.367 0.078 49.893 4.717 0.569 14.739 0.8043 9.70 17.05 2.5132 2.754 0.091 58.062 4.838 0.584 15.117 0.7840 9.46 16.20 2.4497 3.210 0.106 67.681 4.967 0.599 15.522 0.7834 9.45 15.77 2.4478 3.735 0.124 78.750 5.113 0.617 15.977 0.7783 9.39 15.22 2.4320 4.348 0.144 91.663 5.288 0.638 16.523 0.7713 9.30 14.59 2.4100 5.060 0.168 106.684 5.424 0.654 16.948 0.7754 9.35 14.30 2.4228 5.892 0.195 124.210 5.626 0.679 17.579 0.7676 9.26 13.64 2.3985 6.854 0.227 144.502 5.791 0.699 18.095 0.7538 9.09 13.02 2.3554 7.979 0.264 168.220 6.034 0.728 18.854 0.7449 8.99 12.35 2.3277 9.292 0.308 195.891 6.262 0.755 19.568 0.7417 8.95 11.84 2.3176 10.817 0.358 228.042 6.514 0.786 20.355 0.7186 8.67 11.03 2.2455 12.585 0.417 265.333 6.821 0.823 21.313 0.6953 8.39 10.19 2.1726 14.654 0.486 308.948 7.119 0.859 22.245 0.6570 7.93 9.23 2.0530 17.054 0.565 359.547 7.433 0.897 23.226 0.5923 7.15 7.97 1.8510 19.854 0.658 418.579 7.738 0.933 24.179 0.5093 6.14 6.58 1.5914 23.110 0.766 487.230 7.966 0.961 24.892 0.4103 4.95 5.15 1.2822 26.898 0.891 567.081 8.144 0.982 25.448 0.2979 3.59 3.66 0.9310 30.685 1.017 646.932 8.234 0.993 25.728 0.2307 2.78 2.80 0.7209 34.473 1.143 726.783 8.279 0.999 25.871 0.1933 2.33 2.33 0.6039 38.267 1.268 806.766 8.283 0.999 25.883 0.1816 2.19 2.19 0.5673 42.054 1.394 886.617 8.297 1.001 25.925 0.1762 2.13 2.12 0.5505 48.960 1.623 1032.221 8.310 1.002 25.968 0.1726 2.08 2.08 0.5392 55.873 1.852 1177.956 8.315 1.003 25.983 0.1726 2.08 2.08 0.5392 62.779 2.081 1323.559 8.297 1.001 25.927 0.1718 2.07 2.07 0.5369 69.692 2.310 1469.294 8.302 1.001 25.942 0.1695 2.05 2.04 0.5298 RUN NUMBER 1W01707 AXIAL POSITION = 1495.0 MM SPAN POSITION = 0.0 MM FREE-STREAM VELOCITY = 7.84 M/S FRICTION VELOCITY = 0.2812 M/S FREE-STREAM TURBULENCE = 2.198 % X-REYNOLDS NUMBER = 77.22 X10**4 FLUID DENSITY = 1.191 KG/M**3 KINEMATIC VISCOSITY = 1.519 X10(-5)MSQ/S BOUNDARY LAYER THICKNESS (99.0%) = 35.97 MM DISPLACEMENT THICKNESS = 7.092 MM MOMENTUM THICKNESS = 4.542 MM ENERGY THICKNESS = 7.734 MM FORM FACTOR H = 1.561 FORM FACTOR E = 1.703 RDELTASTAR = 3663.4 RTHETA = 2346.3 SKIN FRICTION COEFFICIENT = 0.002571 CALCULATED CF = 0.002686 LAW OF THE WALL OFFSET = 5.20 KARMAN CONSTANT = 0.410 FORM FACTOR G = 9.999 CLAUSER DELTA = 197.796 MM WAKE FACTOR PI = 1.617 1 Y Y/DEL YPLUS U U/UO UPLUS u u/UO u/U u/UTAU MM M/S M/S % % 0.029 0.001 0.537 0.140 0.018 0.499 0.0533 0.68 38.00 0.1895 0.035 0.001 0.653 0.170 0.022 0.606 0.0557 0.71 32.69 0.1981 0.042 0.001 0.769 0.201 0.026 0.713 0.0618 0.79 30.81 0.2198 0.048 0.001 0.884 0.231 0.029 0.821 0.0704 0.90 30.51 0.2505 0.054 0.002 1.000 0.261 0.033 0.928 0.0774 0.99 29.66 0.2754 0.060 0.002 1.116 0.291 0.037 1.036 0.0882 1.12 30.28 0.3137 0.073 0.002 1.347 0.352 0.045 1.251 0.1053 1.34 29.94 0.3744 0.085 0.002 1.579 0.412 0.053 1.465 0.1305 1.66 31.65 0.4639 0.098 0.003 1.810 0.473 0.060 1.680 0.1547 1.97 32.74 0.5502 0.117 0.003 2.158 0.563 0.072 2.003 0.1991 2.54 35.35 0.7080 0.135 0.004 2.505 0.654 0.083 2.325 0.2496 3.18 38.17 0.8875 0.160 0.004 2.968 0.775 0.099 2.755 0.3126 3.98 40.34 1.1114 0.185 0.005 3.431 0.896 0.114 3.185 0.3729 4.75 41.64 1.3259 0.217 0.006 4.010 1.029 0.131 3.658 0.4488 5.72 43.63 1.5958 0.254 0.007 4.704 1.208 0.154 4.294 0.5326 6.79 44.10 1.8938 0.298 0.008 5.515 1.414 0.180 5.027 0.6191 7.89 43.79 2.2012 0.348 0.010 6.441 1.632 0.208 5.803 0.7052 8.99 43.21 2.5076 0.410 0.011 7.598 1.886 0.240 6.707 0.7689 9.80 40.76 2.7340 0.479 0.013 8.872 2.171 0.277 7.720 0.8279 10.55 38.13 2.9438 0.560 0.016 10.376 2.401 0.306 8.535 0.8420 10.73 35.08 2.9939 0.654 0.018 12.113 2.636 0.336 9.371 0.8648 11.03 32.81 3.0750 0.767 0.021 14.196 2.871 0.366 10.210 0.8841 11.27 30.79 3.1434 0.898 0.025 16.627 3.082 0.393 10.958 0.8665 11.05 28.11 3.0809 1.048 0.029 19.405 3.258 0.415 11.585 0.8607 10.97 26.42 3.0601 1.229 0.034 22.762 3.434 0.438 12.210 0.8495 10.83 24.74 3.0203 1.435 0.040 26.582 3.574 0.456 12.709 0.8336 10.63 23.32 2.9641 1.679 0.047 31.097 3.736 0.476 13.285 0.8144 10.38 21.80 2.8958 1.960 0.055 36.306 3.843 0.490 13.665 0.8019 10.22 20.86 2.8511 2.298 0.064 42.556 3.973 0.507 14.127 0.7904 10.08 19.89 2.8102 2.685 0.075 49.733 4.157 0.530 14.781 0.7773 9.91 18.70 2.7638 3.142 0.087 58.183 4.213 0.537 14.980 0.7700 9.82 18.28 2.7378 3.667 0.102 67.907 4.374 0.558 15.551 0.7606 9.70 17.39 2.7045 4.292 0.119 79.482 4.513 0.575 16.046 0.7571 9.65 16.78 2.6921 5.017 0.139 92.910 4.657 0.594 16.560 0.7719 9.84 16.57 2.7446 5.867 0.163 108.653 4.817 0.614 17.128 0.7618 9.71 15.82 2.7088 6.854 0.191 126.942 5.068 0.646 18.018 0.7755 9.89 15.30 2.7572 8.017 0.223 148.473 5.219 0.665 18.556 0.7600 9.69 14.56 2.7024 9.373 0.261 173.592 5.469 0.697 19.444 0.7641 9.74 13.97 2.7167 10.954 0.305 202.878 5.699 0.727 20.263 0.7529 9.60 13.21 2.6770 12.810 0.356 237.258 5.997 0.764 21.322 0.7272 9.27 12.13 2.5858 14.973 0.416 277.309 6.319 0.806 22.467 0.7091 9.04 11.22 2.5212 17.504 0.487 324.190 6.644 0.847 23.622 0.6643 8.47 10.00 2.3619 20.467 0.569 379.058 6.986 0.891 24.839 0.6073 7.74 8.69 2.1594 23.923 0.665 443.071 7.316 0.933 26.012 0.5096 6.50 6.97 1.8119 27.967 0.778 517.965 7.537 0.961 26.798 0.4037 5.15 5.36 1.4355 32.698 0.909 605.592 7.729 0.985 27.480 0.2725 3.47 3.53 0.9689 37.423 1.040 693.103 7.813 0.996 27.779 0.2014 2.57 2.58 0.7160 42.154 1.172 780.731 7.840 0.999 27.876 0.1845 2.35 2.35 0.6560 46.879 1.303 868.242 7.843 1.000 27.886 0.1755 2.24 2.24 0.6239 51.610 1.435 955.869 7.856 1.002 27.934 0.1718 2.19 2.19 0.6107 56.029 1.558 1037.708 7.855 1.001 27.927 0.1711 2.18 2.18 0.6085 60.448 1.681 1119.547 7.853 1.001 27.923 0.1694 2.16 2.16 0.6023 64.867 1.803 1201.387 7.853 1.001 27.921 0.1690 2.15 2.15 0.6007 69.285 1.926 1283.226 7.840 0.999 27.875 0.1724 2.20 2.20 0.6130