ROLLS-ROYCE APPLIED SCIENCE LABORATORY FLAT PLATE TRANSITIONAL BOUNDARY LAYER FLOW HOT WIRE ANEMOMETRY TEST DATA SINGLE WIRE DATA FOR ERCOFTAC T3C5 TEST CASE RUN NUMBER 1W02205 AXIAL POSITION = 45.0 MM SPAN POSITION = 0.0 MM FREE-STREAM VELOCITY = 9.65 M/S FRICTION VELOCITY = 0.4595 M/S FREE-STREAM TURBULENCE = 2.455 % X-REYNOLDS NUMBER = 2.91 X10**4 FLUID DENSITY = 1.213 KG/M**3 KINEMATIC VISCOSITY = 1.491 X10(-5)MSQ/S BOUNDARY LAYER THICKNESS (99.0%) = 1.25 MM DISPLACEMENT THICKNESS = 0.398 MM MOMENTUM THICKNESS = 0.158 MM ENERGY THICKNESS = 0.251 MM FORM FACTOR H = 2.513 FORM FACTOR E = 1.588 RDELTASTAR = 257.3 RTHETA = 102.4 SKIN FRICTION COEFFICIENT = 0.004538 CALCULATED CF = 0.003892 Y Y/DEL YPLUS U U/UO UPLUS u u/UO u/U u/UTAU MM M/S M/S % % 0.029 0.023 0.894 0.425 0.044 0.926 0.0264 0.27 6.20 0.0574 0.035 0.028 1.086 0.517 0.054 1.125 0.0325 0.34 6.29 0.0708 0.042 0.033 1.279 0.609 0.063 1.324 0.0355 0.37 5.83 0.0772 0.048 0.038 1.471 0.700 0.073 1.524 0.0385 0.40 5.50 0.0839 0.054 0.043 1.664 0.792 0.082 1.723 0.0444 0.46 5.60 0.0966 0.060 0.048 1.857 0.883 0.092 1.923 0.0524 0.54 5.93 0.1141 0.067 0.053 2.049 0.975 0.101 2.122 0.0600 0.62 6.15 0.1305 0.073 0.058 2.242 1.067 0.111 2.322 0.0699 0.72 6.55 0.1522 0.079 0.063 2.434 1.158 0.120 2.521 0.0774 0.80 6.68 0.1684 0.085 0.068 2.627 1.250 0.130 2.721 0.0859 0.89 6.87 0.1870 0.092 0.073 2.820 1.342 0.139 2.920 0.0920 0.95 6.85 0.2002 0.098 0.078 3.012 1.433 0.149 3.120 0.1033 1.07 7.21 0.2248 0.104 0.083 3.205 1.507 0.156 3.279 0.1062 1.10 7.05 0.2311 0.110 0.088 3.397 1.582 0.164 3.443 0.1145 1.19 7.24 0.2491 0.117 0.093 3.590 1.640 0.170 3.568 0.1166 1.21 7.11 0.2539 0.123 0.098 3.782 1.726 0.179 3.756 0.1268 1.31 7.34 0.2759 0.129 0.103 3.975 1.818 0.188 3.957 0.1328 1.38 7.30 0.2889 0.135 0.108 4.168 1.910 0.198 4.157 0.1418 1.47 7.43 0.3087 0.142 0.113 4.360 1.987 0.206 4.325 0.1502 1.56 7.56 0.3268 0.148 0.118 4.553 2.075 0.215 4.517 0.1525 1.58 7.35 0.3320 0.160 0.128 4.938 2.250 0.233 4.897 0.1683 1.74 7.48 0.3663 0.173 0.138 5.323 2.414 0.250 5.255 0.1847 1.91 7.65 0.4020 0.192 0.153 5.901 2.675 0.277 5.822 0.2056 2.13 7.69 0.4476 0.210 0.168 6.479 2.926 0.303 6.368 0.2266 2.35 7.74 0.4931 0.229 0.183 7.057 3.197 0.331 6.957 0.2499 2.59 7.82 0.5440 0.248 0.198 7.634 3.469 0.360 7.550 0.2745 2.85 7.91 0.5975 0.267 0.213 8.212 3.767 0.390 8.198 0.2960 3.07 7.86 0.6442 0.292 0.233 8.982 4.093 0.424 8.909 0.3212 3.33 7.85 0.6990 0.323 0.258 9.945 4.520 0.469 9.837 0.3522 3.65 7.79 0.7665 0.348 0.278 10.716 4.864 0.504 10.586 0.3766 3.90 7.74 0.8197 0.379 0.303 11.679 5.247 0.544 11.420 0.3932 4.08 7.49 0.8558 0.417 0.333 12.834 5.706 0.592 12.420 0.4158 4.31 7.29 0.9049 0.454 0.362 13.990 6.127 0.635 13.336 0.4303 4.46 7.02 0.9366 0.498 0.397 15.338 6.574 0.682 14.309 0.4439 4.60 6.75 0.9662 0.542 0.432 16.686 6.981 0.724 15.195 0.4550 4.72 6.52 0.9902 0.592 0.472 18.227 7.398 0.767 16.102 0.4405 4.57 5.95 0.9587 0.642 0.512 19.768 7.781 0.807 16.934 0.4311 4.47 5.54 0.9382 0.698 0.557 21.501 8.162 0.846 17.765 0.4172 4.32 5.11 0.9080 0.760 0.607 23.427 8.497 0.881 18.493 0.3972 4.12 4.67 0.8644 0.829 0.662 25.545 8.807 0.913 19.168 0.3634 3.77 4.13 0.7910 0.904 0.722 27.856 9.057 0.939 19.713 0.3367 3.49 3.72 0.7328 0.992 0.792 30.553 9.271 0.961 20.178 0.3080 3.19 3.32 0.6704 1.079 0.861 33.249 9.409 0.975 20.478 0.2887 2.99 3.07 0.6283 1.173 0.936 36.138 9.497 0.985 20.669 0.2816 2.92 2.97 0.6129 1.279 1.021 39.412 9.579 0.993 20.848 0.2739 2.84 2.86 0.5961 1.398 1.116 43.071 9.618 0.997 20.934 0.2705 2.80 2.81 0.5887 1.510 1.206 46.538 9.641 0.999 20.983 0.2674 2.77 2.77 0.5821 1.629 1.301 50.197 9.656 1.001 21.017 0.2629 2.73 2.72 0.5723 1.742 1.390 53.664 9.654 1.001 21.011 0.2623 2.72 2.72 0.5709 1.860 1.485 57.323 9.656 1.001 21.017 0.2576 2.67 2.67 0.5607 2.560 2.044 78.893 9.659 1.001 21.022 0.2472 2.56 2.56 0.5379 3.260 2.603 100.463 9.662 1.002 21.029 0.2412 2.50 2.50 0.5251 3.960 3.162 122.034 9.664 1.002 21.034 0.2392 2.48 2.47 0.5205 4.660 3.721 143.604 9.671 1.003 21.050 0.2368 2.45 2.45 0.5154 RUN NUMBER 1W02206 AXIAL POSITION = 95.0 MM SPAN POSITION = 0.0 MM FREE-STREAM VELOCITY = 10.24 M/S FRICTION VELOCITY = 0.4102 M/S FREE-STREAM TURBULENCE = 2.127 % X-REYNOLDS NUMBER = 6.52 X10**4 FLUID DENSITY = 1.212 KG/M**3 KINEMATIC VISCOSITY = 1.492 X10(-5)MSQ/S BOUNDARY LAYER THICKNESS (99.0%) = 1.76 MM DISPLACEMENT THICKNESS = 0.537 MM MOMENTUM THICKNESS = 0.218 MM ENERGY THICKNESS = 0.348 MM FORM FACTOR H = 2.470 FORM FACTOR E = 1.597 RDELTASTAR = 368.8 RTHETA = 149.3 SKIN FRICTION COEFFICIENT = 0.003211 CALCULATED CF = 0.002601 Y Y/DEL YPLUS U U/UO UPLUS u u/UO u/U u/UTAU MM M/S M/S % % 0.029 0.016 0.797 0.336 0.033 0.819 0.0326 0.32 9.70 0.0795 0.035 0.020 0.969 0.408 0.040 0.995 0.0354 0.35 8.68 0.0864 0.042 0.024 1.141 0.481 0.047 1.172 0.0395 0.39 8.22 0.0963 0.048 0.027 1.313 0.553 0.054 1.348 0.0454 0.44 8.20 0.1106 0.054 0.031 1.485 0.626 0.061 1.525 0.0514 0.50 8.21 0.1253 0.060 0.034 1.657 0.698 0.068 1.701 0.0585 0.57 8.38 0.1426 0.067 0.038 1.828 0.770 0.075 1.878 0.0671 0.66 8.71 0.1636 0.073 0.041 2.000 0.843 0.082 2.054 0.0771 0.75 9.15 0.1879 0.079 0.045 2.172 0.915 0.089 2.231 0.0862 0.84 9.42 0.2101 0.085 0.048 2.344 0.988 0.096 2.407 0.0947 0.92 9.59 0.2308 0.092 0.052 2.516 1.060 0.104 2.584 0.1029 1.00 9.70 0.2508 0.098 0.056 2.688 1.132 0.111 2.760 0.1120 1.09 9.89 0.2731 0.104 0.059 2.859 1.205 0.118 2.937 0.1218 1.19 10.11 0.2968 0.110 0.063 3.031 1.277 0.125 3.113 0.1300 1.27 10.18 0.3169 0.117 0.066 3.203 1.339 0.131 3.265 0.1385 1.35 10.34 0.3376 0.123 0.070 3.375 1.403 0.137 3.421 0.1456 1.42 10.37 0.3549 0.129 0.073 3.547 1.463 0.143 3.567 0.1527 1.49 10.44 0.3723 0.135 0.077 3.719 1.540 0.150 3.754 0.1613 1.58 10.47 0.3932 0.148 0.084 4.062 1.646 0.161 4.014 0.1752 1.71 10.64 0.4270 0.160 0.091 4.406 1.772 0.173 4.319 0.1897 1.85 10.71 0.4625 0.173 0.098 4.750 1.898 0.185 4.626 0.2067 2.02 10.89 0.5038 0.192 0.109 5.265 2.087 0.204 5.088 0.2300 2.25 11.02 0.5606 0.210 0.120 5.781 2.294 0.224 5.591 0.2586 2.53 11.28 0.6305 0.229 0.130 6.296 2.527 0.247 6.160 0.2893 2.83 11.45 0.7053 0.254 0.144 6.984 2.810 0.274 6.850 0.3245 3.17 11.55 0.7910 0.273 0.155 7.499 3.036 0.297 7.401 0.3470 3.39 11.43 0.8458 0.304 0.173 8.358 3.437 0.336 8.379 0.4055 3.96 11.80 0.9886 0.329 0.187 9.046 3.754 0.367 9.150 0.4379 4.28 11.67 1.0675 0.360 0.205 9.905 4.087 0.399 9.963 0.4684 4.58 11.46 1.1419 0.398 0.226 10.936 4.495 0.439 10.957 0.4952 4.84 11.02 1.2073 0.435 0.247 11.967 4.907 0.479 11.962 0.5383 5.26 10.97 1.3122 0.479 0.272 13.170 5.365 0.524 13.078 0.5753 5.62 10.72 1.4024 0.523 0.297 14.373 5.786 0.565 14.105 0.6094 5.95 10.53 1.4854 0.573 0.326 15.748 6.239 0.609 15.209 0.6335 6.19 10.15 1.5444 0.623 0.354 17.122 6.624 0.647 16.148 0.6505 6.35 9.82 1.5858 0.685 0.390 18.841 7.118 0.695 17.351 0.6617 6.46 9.30 1.6129 0.748 0.425 20.559 7.573 0.740 18.460 0.6535 6.38 8.63 1.5931 0.823 0.468 22.621 8.018 0.783 19.545 0.6352 6.20 7.92 1.5484 0.898 0.510 24.683 8.424 0.823 20.535 0.6147 6.00 7.30 1.4984 0.985 0.560 27.089 8.819 0.861 21.499 0.5763 5.63 6.53 1.4049 1.079 0.613 29.667 9.166 0.895 22.343 0.5181 5.06 5.65 1.2631 1.179 0.670 32.416 9.445 0.922 23.023 0.4716 4.61 4.99 1.1496 1.292 0.734 35.509 9.702 0.948 23.651 0.4070 3.98 4.20 0.9922 1.417 0.805 38.946 9.881 0.965 24.088 0.3507 3.42 3.55 0.8548 1.548 0.880 42.555 10.028 0.979 24.445 0.3090 3.02 3.08 0.7533 1.698 0.965 46.679 10.122 0.989 24.674 0.2766 2.70 2.73 0.6742 1.842 1.047 50.632 10.175 0.994 24.804 0.2636 2.57 2.59 0.6427 1.992 1.132 54.756 10.197 0.996 24.857 0.2524 2.47 2.48 0.6154 2.135 1.214 58.708 10.242 1.000 24.968 0.2464 2.41 2.41 0.6006 2.285 1.299 62.832 10.246 1.001 24.976 0.2433 2.38 2.37 0.5931 3.135 1.782 86.203 10.277 1.004 25.053 0.2277 2.22 2.22 0.5551 3.985 2.266 109.573 10.254 1.001 24.996 0.2200 2.15 2.15 0.5363 4.835 2.749 132.944 10.252 1.001 24.991 0.2190 2.14 2.14 0.5340 5.685 3.232 156.314 10.266 1.003 25.025 0.2178 2.13 2.12 0.5308 RUN NUMBER 1W02207 AXIAL POSITION = 145.0 MM SPAN POSITION = 0.0 MM FREE-STREAM VELOCITY = 10.66 M/S FRICTION VELOCITY = 0.3849 M/S FREE-STREAM TURBULENCE = 1.877 % X-REYNOLDS NUMBER = 10.37 X10**4 FLUID DENSITY = 1.214 KG/M**3 KINEMATIC VISCOSITY = 1.490 X10(-5)MSQ/S BOUNDARY LAYER THICKNESS (99.0%) = 2.21 MM DISPLACEMENT THICKNESS = 0.644 MM MOMENTUM THICKNESS = 0.265 MM ENERGY THICKNESS = 0.426 MM FORM FACTOR H = 2.427 FORM FACTOR E = 1.605 RDELTASTAR = 460.7 RTHETA = 189.8 SKIN FRICTION COEFFICIENT = 0.002607 CALCULATED CF = 0.002062 Y Y/DEL YPLUS U U/UO UPLUS u u/UO u/U u/UTAU MM M/S M/S % % 0.029 0.013 0.749 0.289 0.027 0.750 0.0326 0.31 11.29 0.0847 0.035 0.016 0.910 0.351 0.033 0.912 0.0389 0.36 11.08 0.1010 0.042 0.019 1.072 0.413 0.039 1.073 0.0444 0.42 10.74 0.1153 0.048 0.022 1.233 0.475 0.045 1.235 0.0450 0.42 9.46 0.1169 0.054 0.024 1.395 0.538 0.050 1.397 0.0494 0.46 9.20 0.1284 0.060 0.027 1.556 0.600 0.056 1.558 0.0568 0.53 9.48 0.1477 0.067 0.030 1.718 0.662 0.062 1.720 0.0666 0.62 10.06 0.1731 0.073 0.033 1.879 0.724 0.068 1.882 0.0740 0.69 10.21 0.1921 0.079 0.036 2.040 0.787 0.074 2.043 0.0855 0.80 10.87 0.2220 0.085 0.039 2.202 0.849 0.080 2.205 0.0997 0.93 11.74 0.2589 0.092 0.041 2.363 0.911 0.085 2.366 0.1090 1.02 11.96 0.2831 0.098 0.044 2.525 0.973 0.091 2.528 0.1205 1.13 12.38 0.3130 0.104 0.047 2.686 1.035 0.097 2.690 0.1296 1.22 12.52 0.3367 0.110 0.050 2.847 1.098 0.103 2.851 0.1411 1.32 12.86 0.3667 0.117 0.053 3.009 1.160 0.109 3.013 0.1515 1.42 13.07 0.3937 0.123 0.056 3.170 1.221 0.115 3.172 0.1647 1.55 13.49 0.4279 0.135 0.061 3.493 1.337 0.125 3.472 0.1837 1.72 13.75 0.4772 0.148 0.067 3.816 1.454 0.136 3.777 0.2041 1.91 14.03 0.5301 0.167 0.075 4.300 1.642 0.154 4.267 0.2364 2.22 14.39 0.6140 0.179 0.081 4.623 1.757 0.165 4.564 0.2488 2.33 14.16 0.6462 0.198 0.090 5.107 1.950 0.183 5.067 0.2871 2.69 14.72 0.7457 0.223 0.101 5.753 2.214 0.208 5.751 0.3344 3.14 15.11 0.8687 0.242 0.110 6.237 2.401 0.225 6.237 0.3674 3.45 15.30 0.9544 0.267 0.121 6.883 2.658 0.249 6.905 0.4060 3.81 15.27 1.0547 0.298 0.135 7.690 3.001 0.281 7.797 0.4593 4.31 15.30 1.1932 0.329 0.149 8.497 3.241 0.304 8.420 0.4850 4.55 14.96 1.2600 0.360 0.163 9.304 3.562 0.334 9.254 0.5245 4.92 14.72 1.3626 0.398 0.180 10.273 3.993 0.375 10.374 0.5905 5.54 14.79 1.5340 0.435 0.197 11.241 4.392 0.412 11.409 0.6288 5.90 14.32 1.6335 0.485 0.220 12.533 4.847 0.455 12.592 0.7024 6.59 14.49 1.8247 0.535 0.243 13.824 5.315 0.498 13.806 0.7369 6.91 13.86 1.9142 0.585 0.265 15.116 5.759 0.540 14.960 0.7757 7.27 13.47 2.0150 0.648 0.294 16.730 6.253 0.586 16.245 0.8083 7.58 12.93 2.0997 0.717 0.325 18.505 6.763 0.634 17.568 0.8391 7.87 12.41 2.1799 0.785 0.356 20.281 7.235 0.679 18.795 0.8569 8.04 11.84 2.2260 0.867 0.393 22.380 7.734 0.725 20.091 0.8491 7.96 10.98 2.2057 0.954 0.433 24.639 8.218 0.771 21.349 0.8213 7.70 9.99 2.1335 1.054 0.478 27.222 8.683 0.814 22.557 0.7941 7.45 9.15 2.0630 1.160 0.526 29.966 9.093 0.853 23.623 0.7434 6.97 8.18 1.9313 1.279 0.580 33.033 9.468 0.888 24.595 0.6696 6.28 7.07 1.7395 1.410 0.639 36.423 9.782 0.917 25.411 0.5957 5.59 6.09 1.5476 1.554 0.705 40.136 10.050 0.943 26.107 0.5083 4.77 5.06 1.3206 1.717 0.778 44.333 10.249 0.961 26.625 0.4416 4.14 4.31 1.1472 1.892 0.858 48.853 10.410 0.976 27.042 0.3618 3.39 3.48 0.9398 2.085 0.946 53.857 10.523 0.987 27.337 0.3004 2.82 2.85 0.7803 2.298 1.042 59.345 10.592 0.993 27.516 0.2670 2.50 2.52 0.6936 2.510 1.138 64.834 10.635 0.997 27.626 0.2453 2.30 2.31 0.6372 2.723 1.235 70.322 10.661 1.000 27.694 0.2319 2.18 2.18 0.6024 2.935 1.331 75.810 10.672 1.001 27.722 0.2246 2.11 2.11 0.5836 3.148 1.427 81.299 10.674 1.001 27.729 0.2194 2.06 2.06 0.5699 4.298 1.949 111.000 10.683 1.002 27.752 0.2077 1.95 1.94 0.5396 5.448 2.470 140.702 10.680 1.002 27.744 0.2050 1.92 1.92 0.5325 6.598 2.992 170.403 10.680 1.002 27.744 0.2024 1.90 1.90 0.5259 7.748 3.513 200.105 10.684 1.002 27.755 0.2001 1.88 1.87 0.5198 RUN NUMBER 1W02208 AXIAL POSITION = 195.0 MM SPAN POSITION = 0.0 MM FREE-STREAM VELOCITY = 10.93 M/S FRICTION VELOCITY = 0.3700 M/S FREE-STREAM TURBULENCE = 1.744 % X-REYNOLDS NUMBER = 14.30 X10**4 FLUID DENSITY = 1.214 KG/M**3 KINEMATIC VISCOSITY = 1.490 X10(-5)MSQ/S BOUNDARY LAYER THICKNESS (99.0%) = 2.61 MM DISPLACEMENT THICKNESS = 0.730 MM MOMENTUM THICKNESS = 0.307 MM ENERGY THICKNESS = 0.496 MM FORM FACTOR H = 2.377 FORM FACTOR E = 1.615 RDELTASTAR = 535.2 RTHETA = 225.1 SKIN FRICTION COEFFICIENT = 0.002292 CALCULATED CF = 0.001756 Y Y/DEL YPLUS U U/UO UPLUS u u/UO u/U u/UTAU MM M/S M/S % % 0.029 0.011 0.720 0.267 0.024 0.722 0.0426 0.39 15.94 0.1151 0.035 0.014 0.875 0.325 0.030 0.877 0.0479 0.44 14.77 0.1296 0.042 0.016 1.030 0.382 0.035 1.033 0.0514 0.47 13.44 0.1389 0.048 0.018 1.185 0.440 0.040 1.189 0.0590 0.54 13.43 0.1596 0.054 0.021 1.340 0.497 0.046 1.344 0.0652 0.60 13.12 0.1763 0.060 0.023 1.496 0.555 0.051 1.500 0.0741 0.68 13.35 0.2002 0.067 0.025 1.651 0.612 0.056 1.655 0.0852 0.78 13.92 0.2304 0.073 0.028 1.806 0.670 0.061 1.811 0.0935 0.86 13.96 0.2529 0.079 0.030 1.961 0.728 0.067 1.967 0.1091 1.00 15.00 0.2950 0.085 0.033 2.116 0.785 0.072 2.122 0.1173 1.07 14.94 0.3171 0.092 0.035 2.271 0.843 0.077 2.278 0.1271 1.16 15.08 0.3435 0.098 0.037 2.426 0.900 0.082 2.433 0.1407 1.29 15.63 0.3804 0.104 0.040 2.582 0.958 0.088 2.589 0.1554 1.42 16.23 0.4200 0.110 0.042 2.737 1.015 0.093 2.744 0.1649 1.51 16.24 0.4457 0.117 0.045 2.892 1.073 0.098 2.900 0.1776 1.62 16.55 0.4800 0.129 0.049 3.202 1.188 0.109 3.211 0.2076 1.90 17.48 0.5612 0.142 0.054 3.512 1.270 0.116 3.434 0.2225 2.04 17.52 0.6015 0.160 0.061 3.978 1.437 0.132 3.885 0.2573 2.35 17.90 0.6954 0.173 0.066 4.288 1.530 0.140 4.136 0.2690 2.46 17.58 0.7271 0.192 0.073 4.754 1.722 0.158 4.655 0.3219 2.95 18.69 0.8700 0.217 0.083 5.374 1.972 0.180 5.330 0.3666 3.35 18.59 0.9910 0.235 0.090 5.840 2.153 0.197 5.818 0.4073 3.73 18.92 1.1010 0.260 0.100 6.460 2.407 0.220 6.507 0.4569 4.18 18.98 1.2351 0.292 0.112 7.236 2.696 0.247 7.289 0.5204 4.76 19.30 1.4067 0.323 0.124 8.012 2.966 0.271 8.018 0.5534 5.06 18.66 1.4958 0.354 0.136 8.787 3.278 0.300 8.862 0.6097 5.58 18.60 1.6481 0.398 0.152 9.873 3.700 0.339 10.001 0.6912 6.32 18.68 1.8684 0.435 0.167 10.804 4.070 0.372 11.001 0.7371 6.74 18.11 1.9925 0.485 0.186 12.045 4.502 0.412 12.170 0.7933 7.26 17.62 2.1443 0.535 0.205 13.287 4.943 0.452 13.361 0.8320 7.61 16.83 2.2490 0.592 0.227 14.683 5.390 0.493 14.571 0.9003 8.24 16.70 2.4336 0.654 0.251 16.234 5.936 0.543 16.047 0.9396 8.60 15.83 2.5397 0.723 0.277 17.941 6.448 0.590 17.430 0.9835 9.00 15.25 2.6585 0.804 0.308 19.958 6.970 0.638 18.842 1.0216 9.35 14.66 2.7614 0.885 0.339 21.975 7.484 0.685 20.230 0.9918 9.07 13.25 2.6809 0.985 0.378 24.457 7.995 0.732 21.612 1.0009 9.16 12.52 2.7055 1.085 0.416 26.939 8.449 0.773 22.838 0.9823 8.99 11.63 2.6553 1.204 0.461 29.887 8.925 0.817 24.126 0.9358 8.56 10.49 2.5297 1.329 0.509 32.990 9.319 0.853 25.190 0.8754 8.01 9.39 2.3663 1.473 0.564 36.558 9.713 0.889 26.256 0.7926 7.25 8.16 2.1423 1.629 0.624 40.437 10.018 0.917 27.081 0.7041 6.44 7.03 1.9034 1.804 0.691 44.781 10.281 0.941 27.790 0.6074 5.56 5.91 1.6418 1.992 0.763 49.435 10.504 0.961 28.394 0.4960 4.54 4.72 1.3407 2.204 0.845 54.710 10.666 0.976 28.830 0.4005 3.66 3.76 1.0827 2.435 0.933 60.450 10.775 0.986 29.126 0.3326 3.04 3.09 0.8990 2.698 1.034 66.966 10.854 0.993 29.339 0.2817 2.58 2.60 0.7615 2.954 1.132 73.327 10.892 0.997 29.441 0.2424 2.22 2.23 0.6553 3.217 1.233 79.843 10.921 0.999 29.521 0.2281 2.09 2.09 0.6167 3.473 1.331 86.204 10.944 1.001 29.582 0.2150 1.97 1.96 0.5811 3.729 1.429 92.565 10.946 1.002 29.588 0.2080 1.90 1.90 0.5621 5.079 1.946 126.076 10.947 1.002 29.590 0.1954 1.79 1.78 0.5280 6.429 2.464 159.587 10.951 1.002 29.600 0.1920 1.76 1.75 0.5190 7.779 2.981 193.098 10.953 1.002 29.608 0.1919 1.76 1.75 0.5187 9.129 3.498 226.609 10.951 1.002 29.601 0.1906 1.74 1.74 0.5152 RUN NUMBER 1W02209 AXIAL POSITION = 245.0 MM SPAN POSITION = 0.0 MM FREE-STREAM VELOCITY = 11.11 M/S FRICTION VELOCITY = 0.3579 M/S FREE-STREAM TURBULENCE = 1.634 % X-REYNOLDS NUMBER = 18.25 X10**4 FLUID DENSITY = 1.213 KG/M**3 KINEMATIC VISCOSITY = 1.491 X10(-5)MSQ/S BOUNDARY LAYER THICKNESS (99.0%) = 3.03 MM DISPLACEMENT THICKNESS = 0.816 MM MOMENTUM THICKNESS = 0.351 MM ENERGY THICKNESS = 0.570 MM FORM FACTOR H = 2.324 FORM FACTOR E = 1.623 RDELTASTAR = 607.7 RTHETA = 261.5 SKIN FRICTION COEFFICIENT = 0.002076 CALCULATED CF = 0.001554 Y Y/DEL YPLUS U U/UO UPLUS u u/UO u/U u/UTAU MM M/S M/S % % 0.029 0.010 0.696 0.244 0.022 0.682 0.0448 0.40 18.34 0.1250 0.035 0.012 0.846 0.297 0.027 0.828 0.0526 0.47 17.75 0.1470 0.042 0.014 0.996 0.349 0.031 0.975 0.0566 0.51 16.21 0.1581 0.048 0.016 1.146 0.402 0.036 1.122 0.0618 0.56 15.38 0.1726 0.054 0.018 1.296 0.454 0.041 1.269 0.0709 0.64 15.62 0.1982 0.060 0.020 1.446 0.507 0.046 1.416 0.0824 0.74 16.26 0.2302 0.067 0.022 1.596 0.559 0.050 1.563 0.0921 0.83 16.46 0.2573 0.073 0.024 1.747 0.612 0.055 1.710 0.1059 0.95 17.31 0.2959 0.079 0.026 1.897 0.665 0.060 1.857 0.1201 1.08 18.07 0.3355 0.085 0.028 2.047 0.717 0.065 2.004 0.1383 1.24 19.28 0.3864 0.092 0.030 2.197 0.770 0.069 2.150 0.1409 1.27 18.31 0.3937 0.098 0.032 2.347 0.822 0.074 2.297 0.1580 1.42 19.22 0.4415 0.104 0.034 2.497 0.875 0.079 2.444 0.1767 1.59 20.19 0.4936 0.110 0.036 2.647 0.927 0.083 2.591 0.1880 1.69 20.27 0.5252 0.123 0.041 2.947 1.033 0.093 2.885 0.2193 1.97 21.23 0.6125 0.135 0.045 3.247 1.138 0.102 3.179 0.2489 2.24 21.87 0.6953 0.148 0.049 3.547 1.225 0.110 3.422 0.2733 2.46 22.32 0.7636 0.167 0.055 3.997 1.378 0.124 3.849 0.3034 2.73 22.02 0.8477 0.185 0.061 4.447 1.527 0.137 4.266 0.3358 3.02 21.99 0.9382 0.204 0.067 4.897 1.714 0.154 4.790 0.3856 3.47 22.49 1.0773 0.229 0.076 5.498 1.945 0.175 5.434 0.4451 4.01 22.88 1.2435 0.254 0.084 6.098 2.180 0.196 6.091 0.5067 4.56 23.24 1.4156 0.279 0.092 6.698 2.418 0.218 6.756 0.5768 5.19 23.85 1.6115 0.310 0.102 7.448 2.697 0.243 7.534 0.6280 5.65 23.29 1.7546 0.348 0.115 8.349 3.010 0.271 8.410 0.6859 6.17 22.79 1.9163 0.385 0.127 9.249 3.325 0.299 9.290 0.7461 6.72 22.44 2.0845 0.429 0.142 10.299 3.763 0.339 10.514 0.8343 7.51 22.17 2.3309 0.473 0.156 11.349 4.176 0.376 11.668 0.8758 7.88 20.97 2.4469 0.529 0.175 12.700 4.643 0.418 12.973 0.9463 8.52 20.38 2.6438 0.585 0.193 14.050 5.077 0.457 14.183 0.9900 8.91 19.50 2.7657 0.648 0.214 15.551 5.591 0.503 15.621 1.0605 9.55 18.97 2.9628 0.723 0.239 17.351 6.099 0.549 17.040 1.1047 9.94 18.11 3.0864 0.798 0.263 19.152 6.542 0.589 18.277 1.1311 10.18 17.29 3.1600 0.892 0.294 21.402 7.076 0.637 19.767 1.1620 10.46 16.42 3.2463 0.985 0.325 23.653 7.600 0.684 21.233 1.1535 10.38 15.18 3.2225 1.092 0.360 26.204 8.079 0.727 22.570 1.1618 10.46 14.38 3.2457 1.217 0.402 29.205 8.624 0.776 24.094 1.0886 9.80 12.62 3.0411 1.348 0.445 32.356 9.009 0.811 25.170 1.0704 9.64 11.88 2.9904 1.498 0.494 35.957 9.470 0.852 26.457 0.9813 8.83 10.36 2.7416 1.660 0.548 39.858 9.841 0.886 27.492 0.9039 8.14 9.19 2.5252 1.842 0.608 44.209 10.158 0.914 28.378 0.7954 7.16 7.83 2.2222 2.042 0.674 49.011 10.438 0.940 29.161 0.6908 6.22 6.62 1.9298 2.267 0.748 54.412 10.664 0.960 29.791 0.5686 5.12 5.33 1.5886 2.517 0.831 60.414 10.827 0.975 30.249 0.4441 4.00 4.10 1.2408 2.792 0.922 67.016 10.940 0.985 30.563 0.3704 3.33 3.39 1.0348 3.098 1.023 74.368 11.027 0.993 30.805 0.3037 2.73 2.75 0.8485 3.404 1.124 81.721 11.069 0.996 30.924 0.2568 2.31 2.32 0.7174 3.710 1.225 89.073 11.101 0.999 31.014 0.2284 2.06 2.06 0.6381 4.017 1.326 96.425 11.105 1.000 31.025 0.2124 1.91 1.91 0.5934 4.323 1.427 103.777 11.119 1.001 31.063 0.1993 1.79 1.79 0.5569 5.873 1.939 140.988 11.129 1.002 31.092 0.1853 1.67 1.66 0.5176 7.423 2.451 178.199 11.140 1.003 31.122 0.1831 1.65 1.64 0.5115 8.973 2.962 215.411 11.145 1.003 31.136 0.1826 1.64 1.64 0.5102 10.523 3.474 252.622 11.146 1.003 31.138 0.1815 1.63 1.63 0.5070 RUN NUMBER 1W02210 AXIAL POSITION = 295.0 MM SPAN POSITION = 0.0 MM FREE-STREAM VELOCITY = 11.29 M/S FRICTION VELOCITY = 0.3494 M/S FREE-STREAM TURBULENCE = 1.547 % X-REYNOLDS NUMBER = 22.33 X10**4 FLUID DENSITY = 1.213 KG/M**3 KINEMATIC VISCOSITY = 1.492 X10(-5)MSQ/S BOUNDARY LAYER THICKNESS (99.0%) = 3.48 MM DISPLACEMENT THICKNESS = 0.888 MM MOMENTUM THICKNESS = 0.390 MM ENERGY THICKNESS = 0.637 MM FORM FACTOR H = 2.276 FORM FACTOR E = 1.634 RDELTASTAR = 672.0 RTHETA = 295.3 SKIN FRICTION COEFFICIENT = 0.001914 CALCULATED CF = 0.001405 Y Y/DEL YPLUS U U/UO UPLUS u u/UO u/U u/UTAU MM M/S M/S % % 0.029 0.008 0.679 0.235 0.021 0.672 0.0580 0.51 24.74 0.1662 0.035 0.010 0.826 0.285 0.025 0.816 0.0706 0.63 24.76 0.2021 0.042 0.012 0.972 0.336 0.030 0.961 0.0716 0.63 21.32 0.2049 0.048 0.014 1.118 0.386 0.034 1.106 0.0803 0.71 20.79 0.2298 0.054 0.016 1.265 0.437 0.039 1.250 0.0960 0.85 21.98 0.2749 0.060 0.017 1.411 0.487 0.043 1.395 0.1070 0.95 21.96 0.3063 0.067 0.019 1.558 0.538 0.048 1.540 0.1148 1.02 21.34 0.3286 0.073 0.021 1.704 0.589 0.052 1.685 0.1256 1.11 21.33 0.3594 0.079 0.023 1.850 0.639 0.057 1.829 0.1549 1.37 24.23 0.4432 0.085 0.025 1.997 0.690 0.061 1.974 0.1729 1.53 25.06 0.4948 0.092 0.026 2.143 0.740 0.066 2.119 0.1921 1.70 25.95 0.5498 0.098 0.028 2.289 0.791 0.070 2.264 0.1855 1.64 23.45 0.5309 0.104 0.030 2.436 0.841 0.075 2.408 0.2105 1.86 25.01 0.6024 0.117 0.033 2.729 0.943 0.083 2.698 0.2573 2.28 27.30 0.7365 0.129 0.037 3.021 1.044 0.092 2.987 0.3012 2.67 28.86 0.8621 0.142 0.041 3.314 1.136 0.101 3.251 0.3037 2.69 26.74 0.8694 0.160 0.046 3.753 1.302 0.115 3.727 0.3905 3.46 29.99 1.1177 0.179 0.051 4.192 1.440 0.128 4.122 0.4112 3.64 28.55 1.1770 0.198 0.057 4.632 1.573 0.139 4.502 0.4596 4.07 29.22 1.3157 0.223 0.064 5.217 1.780 0.158 5.095 0.5141 4.55 28.89 1.4716 0.248 0.071 5.803 1.995 0.177 5.711 0.5884 5.21 29.49 1.6841 0.273 0.078 6.388 2.186 0.194 6.256 0.6400 5.67 29.28 1.8319 0.310 0.089 7.266 2.493 0.221 7.137 0.7087 6.28 28.43 2.0287 0.342 0.098 7.998 2.790 0.247 7.985 0.7629 6.76 27.35 2.1837 0.379 0.109 8.877 3.130 0.277 8.959 0.8404 7.44 26.85 2.4055 0.423 0.122 9.901 3.501 0.310 10.021 0.9008 7.98 25.73 2.5784 0.473 0.136 11.072 3.942 0.349 11.285 0.9883 8.75 25.07 2.8289 0.529 0.152 12.390 4.396 0.389 12.584 1.0575 9.36 24.06 3.0271 0.592 0.170 13.854 4.919 0.436 14.080 1.0925 9.67 22.21 3.1273 0.654 0.188 15.318 5.428 0.481 15.537 1.1743 10.40 21.63 3.3613 0.729 0.210 17.074 5.971 0.529 17.090 1.2316 10.91 20.63 3.5252 0.817 0.235 19.124 6.516 0.577 18.652 1.2467 11.04 19.13 3.5685 0.910 0.262 21.319 7.035 0.623 20.138 1.2745 11.29 18.12 3.6482 1.010 0.290 23.661 7.567 0.670 21.661 1.2891 11.41 17.03 3.6898 1.129 0.325 26.443 8.112 0.718 23.220 1.2587 11.15 15.52 3.6029 1.254 0.361 29.370 8.535 0.756 24.430 1.2427 11.00 14.56 3.5571 1.398 0.402 32.737 8.932 0.791 25.568 1.2001 10.63 13.44 3.4352 1.560 0.449 36.543 9.463 0.838 27.086 1.1042 9.78 11.67 3.1607 1.735 0.499 40.642 9.857 0.873 28.216 1.0101 8.94 10.25 2.8912 1.935 0.556 45.326 10.198 0.903 29.190 0.9132 8.09 8.96 2.6140 2.154 0.619 50.450 10.499 0.930 30.051 0.7960 7.05 7.58 2.2785 2.404 0.691 56.305 10.726 0.950 30.701 0.6804 6.02 6.34 1.9475 2.673 0.769 62.599 10.905 0.966 31.213 0.5603 4.96 5.14 1.6038 2.979 0.857 69.772 11.047 0.978 31.621 0.4690 4.15 4.25 1.3424 3.317 0.954 77.677 11.164 0.989 31.955 0.3619 3.20 3.24 1.0359 3.698 1.063 86.606 11.226 0.994 32.133 0.2860 2.53 2.55 0.8187 4.073 1.171 95.389 11.259 0.997 32.229 0.2444 2.16 2.17 0.6996 4.454 1.281 104.319 11.290 1.000 32.317 0.2163 1.92 1.92 0.6191 4.829 1.389 113.102 11.301 1.001 32.348 0.2002 1.77 1.77 0.5730 5.210 1.498 122.031 11.304 1.001 32.356 0.1911 1.69 1.69 0.5471 7.060 2.030 165.361 11.309 1.001 32.372 0.1767 1.57 1.56 0.5059 8.910 2.562 208.690 11.313 1.002 32.383 0.1748 1.55 1.55 0.5004 10.760 3.094 252.020 11.318 1.002 32.398 0.1745 1.55 1.54 0.4994 12.610 3.626 295.349 11.318 1.002 32.396 0.1748 1.55 1.54 0.5002 RUN NUMBER 1W02301 AXIAL POSITION = 345.0 MM SPAN POSITION = 0.0 MM FREE-STREAM VELOCITY = 11.48 M/S FRICTION VELOCITY = 0.3534 M/S FREE-STREAM TURBULENCE = 1.454 % X-REYNOLDS NUMBER = 26.58 X10**4 FLUID DENSITY = 1.214 KG/M**3 KINEMATIC VISCOSITY = 1.490 X10(-5)MSQ/S BOUNDARY LAYER THICKNESS (99.0%) = 3.93 MM DISPLACEMENT THICKNESS = 0.943 MM MOMENTUM THICKNESS = 0.432 MM ENERGY THICKNESS = 0.710 MM FORM FACTOR H = 2.186 FORM FACTOR E = 1.646 RDELTASTAR = 726.8 RTHETA = 332.4 SKIN FRICTION COEFFICIENT = 0.001896 CALCULATED CF = 0.001288 Y Y/DEL YPLUS U U/UO UPLUS u u/UO u/U u/UTAU MM M/S M/S % % 0.029 0.007 0.688 0.243 0.021 0.687 0.0835 0.73 34.42 0.2363 0.035 0.009 0.836 0.295 0.026 0.834 0.0920 0.80 31.20 0.2604 0.042 0.011 0.984 0.347 0.030 0.982 0.1108 0.97 31.93 0.3137 0.048 0.012 1.132 0.399 0.035 1.130 0.1272 1.11 31.85 0.3600 0.054 0.014 1.281 0.452 0.039 1.278 0.1406 1.22 31.12 0.3978 0.060 0.015 1.429 0.504 0.044 1.426 0.1610 1.40 31.95 0.4557 0.067 0.017 1.577 0.556 0.048 1.574 0.1913 1.67 34.38 0.5412 0.073 0.018 1.725 0.609 0.053 1.722 0.1923 1.67 31.59 0.5440 0.079 0.020 1.874 0.661 0.058 1.870 0.2188 1.91 33.11 0.6193 0.085 0.022 2.022 0.713 0.062 2.018 0.2489 2.17 34.90 0.7044 0.092 0.023 2.170 0.765 0.067 2.166 0.2651 2.31 34.63 0.7501 0.098 0.025 2.318 0.818 0.071 2.314 0.2912 2.54 35.62 0.8241 0.104 0.026 2.466 0.870 0.076 2.462 0.2916 2.54 33.51 0.8250 0.117 0.030 2.763 0.975 0.085 2.758 0.3419 2.98 35.08 0.9676 0.135 0.034 3.208 1.131 0.099 3.202 0.4293 3.74 37.94 1.2148 0.148 0.038 3.504 1.240 0.108 3.509 0.4907 4.27 39.57 1.3885 0.167 0.042 3.949 1.395 0.122 3.948 0.5590 4.87 40.07 1.5819 0.185 0.047 4.393 1.533 0.134 4.339 0.5906 5.14 38.51 1.6711 0.210 0.053 4.986 1.730 0.151 4.896 0.6764 5.89 39.10 1.9141 0.235 0.060 5.579 1.885 0.164 5.335 0.7150 6.23 37.93 2.0234 0.260 0.066 6.172 2.156 0.188 6.101 0.8199 7.14 38.03 2.3201 0.292 0.074 6.913 2.420 0.211 6.849 0.8672 7.55 35.83 2.4540 0.329 0.084 7.802 2.756 0.240 7.799 0.9181 8.00 33.31 2.5980 0.367 0.093 8.692 3.116 0.271 8.818 1.0298 8.97 33.05 2.9142 0.410 0.104 9.729 3.490 0.304 9.875 1.0809 9.42 30.97 3.0588 0.454 0.115 10.767 3.850 0.335 10.895 1.1360 9.90 29.50 3.2145 0.510 0.130 12.101 4.395 0.383 12.437 1.2200 10.63 27.76 3.4524 0.573 0.146 13.583 4.800 0.418 13.583 1.2270 10.69 25.56 3.4721 0.635 0.161 15.065 5.266 0.459 14.901 1.2808 11.16 24.32 3.6244 0.710 0.181 16.844 5.776 0.503 16.345 1.3081 11.40 22.65 3.7017 0.798 0.203 18.919 6.293 0.548 17.807 1.3613 11.86 21.63 3.8521 0.892 0.227 21.142 6.870 0.598 19.439 1.3891 12.10 20.22 3.9308 0.992 0.252 23.514 7.350 0.640 20.799 1.3891 12.10 18.90 3.9309 1.110 0.282 26.330 7.876 0.686 22.288 1.3930 12.14 17.69 3.9418 1.242 0.316 29.443 8.403 0.732 23.777 1.3403 11.68 15.95 3.7928 1.385 0.352 32.852 8.874 0.773 25.112 1.3054 11.37 14.71 3.6939 1.548 0.393 36.706 9.338 0.813 26.424 1.2260 10.68 13.13 3.4694 1.729 0.439 41.004 9.730 0.848 27.532 1.1540 10.05 11.86 3.2656 1.935 0.492 45.895 10.100 0.880 28.580 1.0593 9.23 10.49 2.9977 2.160 0.549 51.231 10.399 0.906 29.425 0.9575 8.34 9.21 2.7096 2.410 0.613 57.160 10.694 0.932 30.262 0.8300 7.23 7.76 2.3487 2.698 0.686 63.978 10.924 0.952 30.913 0.6956 6.06 6.37 1.9683 3.010 0.765 71.389 11.101 0.967 31.414 0.5867 5.11 5.28 1.6601 3.367 0.856 79.838 11.248 0.980 31.830 0.4664 4.06 4.15 1.3197 3.760 0.956 89.176 11.344 0.988 32.101 0.3821 3.33 3.37 1.0811 4.198 1.067 99.552 11.407 0.994 32.281 0.3027 2.64 2.65 0.8566 4.635 1.178 109.927 11.443 0.997 32.382 0.2536 2.21 2.22 0.7177 5.079 1.291 120.451 11.470 0.999 32.456 0.2207 1.92 1.92 0.6245 5.517 1.402 130.826 11.482 1.000 32.493 0.1951 1.70 1.70 0.5520 5.954 1.513 141.202 11.492 1.001 32.519 0.1851 1.61 1.61 0.5237 8.054 2.047 191.004 11.504 1.002 32.554 0.1696 1.48 1.47 0.4799 10.154 2.581 240.807 11.505 1.002 32.557 0.1674 1.46 1.46 0.4738 12.254 3.114 290.609 11.503 1.002 32.550 0.1673 1.46 1.45 0.4735 14.354 3.648 340.412 11.502 1.002 32.548 0.1669 1.45 1.45 0.4724 RUN NUMBER 1W02302 AXIAL POSITION = 420.0 MM SPAN POSITION = 0.0 MM FREE-STREAM VELOCITY = 11.77 M/S FRICTION VELOCITY = 0.4039 M/S FREE-STREAM TURBULENCE = 1.350 % X-REYNOLDS NUMBER = 33.14 X10**4 FLUID DENSITY = 1.213 KG/M**3 KINEMATIC VISCOSITY = 1.491 X10(-5)MSQ/S BOUNDARY LAYER THICKNESS (99.0%) = 4.71 MM DISPLACEMENT THICKNESS = 0.956 MM MOMENTUM THICKNESS = 0.487 MM ENERGY THICKNESS = 0.817 MM FORM FACTOR H = 1.963 FORM FACTOR E = 1.678 RDELTASTAR = 754.3 RTHETA = 384.3 SKIN FRICTION COEFFICIENT = 0.002357 CALCULATED CF = 0.001153 Y Y/DEL YPLUS U U/UO UPLUS u u/UO u/U u/UTAU MM M/S M/S % % 0.029 0.006 0.785 0.331 0.028 0.819 0.1492 1.27 45.12 0.3693 0.035 0.007 0.955 0.402 0.034 0.995 0.1856 1.58 46.17 0.4594 0.042 0.009 1.124 0.473 0.040 1.171 0.2227 1.89 47.08 0.5514 0.048 0.010 1.293 0.544 0.046 1.348 0.2679 2.28 49.21 0.6633 0.054 0.011 1.463 0.616 0.052 1.524 0.3079 2.62 50.01 0.7622 0.060 0.013 1.632 0.687 0.058 1.701 0.3527 3.00 51.34 0.8731 0.067 0.014 1.801 0.758 0.064 1.877 0.3940 3.35 51.97 0.9755 0.073 0.015 1.970 0.829 0.070 2.053 0.4231 3.60 51.02 1.0476 0.079 0.017 2.140 0.901 0.077 2.230 0.4687 3.98 52.04 1.1603 0.085 0.018 2.309 0.972 0.083 2.406 0.5072 4.31 52.18 1.2557 0.092 0.019 2.478 1.043 0.089 2.583 0.5462 4.64 52.36 1.3523 0.098 0.021 2.648 1.114 0.095 2.759 0.5669 4.82 50.87 1.4036 0.110 0.023 2.986 1.257 0.107 3.112 0.6347 5.39 50.50 1.5713 0.123 0.026 3.325 1.396 0.119 3.455 0.7214 6.13 51.69 1.7860 0.142 0.030 3.833 1.567 0.133 3.879 0.8077 6.86 51.55 1.9997 0.160 0.034 4.340 1.761 0.150 4.361 0.9157 7.78 51.99 2.2670 0.179 0.038 4.848 1.947 0.165 4.821 0.9816 8.34 50.41 2.4301 0.198 0.042 5.356 2.109 0.179 5.222 1.0602 9.01 50.26 2.6248 0.223 0.047 6.033 2.380 0.202 5.893 1.1604 9.86 48.75 2.8729 0.248 0.053 6.710 2.676 0.227 6.626 1.2680 10.78 47.38 3.1393 0.279 0.059 7.557 2.985 0.254 7.390 1.3374 11.37 44.80 3.3111 0.317 0.067 8.572 3.366 0.286 8.333 1.4365 12.21 42.68 3.5564 0.354 0.075 9.588 3.712 0.315 9.190 1.4861 12.63 40.03 3.6791 0.398 0.084 10.773 4.115 0.350 10.189 1.5240 12.95 37.03 3.7730 0.448 0.095 12.127 4.488 0.381 11.112 1.5466 13.14 34.46 3.8289 0.498 0.106 13.482 4.899 0.416 12.129 1.5542 13.21 31.73 3.8479 0.560 0.119 15.174 5.441 0.462 13.470 1.5904 13.52 29.23 3.9375 0.629 0.134 17.037 5.870 0.499 14.533 1.5720 13.36 26.78 3.8919 0.704 0.150 19.068 6.358 0.540 15.742 1.5439 13.12 24.28 3.8224 0.792 0.168 21.438 6.826 0.580 16.900 1.5517 13.19 22.73 3.8416 0.885 0.188 23.977 7.293 0.620 18.055 1.5353 13.05 21.05 3.8011 0.998 0.212 27.024 7.835 0.666 19.397 1.4924 12.68 19.05 3.6947 1.117 0.237 30.241 8.282 0.704 20.505 1.4491 12.32 17.50 3.5876 1.254 0.266 33.965 8.715 0.741 21.575 1.4067 11.95 16.14 3.4827 1.404 0.298 38.027 9.118 0.775 22.575 1.3745 11.68 15.07 3.4029 1.573 0.334 42.598 9.532 0.810 23.599 1.3060 11.10 13.70 3.2334 1.767 0.375 47.846 9.891 0.841 24.488 1.2268 10.43 12.40 3.0371 1.979 0.420 53.601 10.198 0.867 25.249 1.1677 9.92 11.45 2.8910 2.217 0.471 60.034 10.510 0.893 26.019 1.0666 9.06 10.15 2.6407 2.485 0.528 67.313 10.784 0.916 26.699 0.9645 8.20 8.94 2.3879 2.785 0.592 75.439 11.005 0.935 27.245 0.8535 7.25 7.76 2.1130 3.123 0.663 84.580 11.243 0.956 27.836 0.7181 6.10 6.39 1.7777 3.504 0.744 94.906 11.387 0.968 28.191 0.6043 5.14 5.31 1.4962 3.929 0.835 106.417 11.516 0.979 28.510 0.5001 4.25 4.34 1.2380 4.404 0.936 119.283 11.599 0.986 28.715 0.4141 3.52 3.57 1.0252 4.935 1.048 133.672 11.690 0.993 28.942 0.3235 2.75 2.77 0.8009 5.473 1.163 148.230 11.738 0.998 29.059 0.2516 2.14 2.14 0.6228 6.004 1.275 162.619 11.747 0.998 29.083 0.2179 1.85 1.85 0.5394 6.535 1.388 177.008 11.767 1.000 29.133 0.1952 1.66 1.66 0.4832 7.067 1.501 191.397 11.773 1.001 29.147 0.1783 1.51 1.51 0.4413 9.542 2.027 258.433 11.784 1.001 29.174 0.1609 1.37 1.37 0.3983 12.010 2.551 325.299 11.797 1.003 29.206 0.1584 1.35 1.34 0.3922 14.479 3.076 392.165 11.800 1.003 29.213 0.1581 1.34 1.34 0.3914 16.948 3.600 459.032 11.807 1.003 29.230 0.1589 1.35 1.35 0.3934 RUN NUMBER 1W02303 AXIAL POSITION = 495.0 MM SPAN POSITION = 0.0 MM FREE-STREAM VELOCITY = 12.13 M/S FRICTION VELOCITY = 0.4779 M/S FREE-STREAM TURBULENCE = 1.260 % X-REYNOLDS NUMBER = 40.24 X10**4 FLUID DENSITY = 1.212 KG/M**3 KINEMATIC VISCOSITY = 1.493 X10(-5)MSQ/S BOUNDARY LAYER THICKNESS (99.0%) = 5.78 MM DISPLACEMENT THICKNESS = 0.983 MM MOMENTUM THICKNESS = 0.562 MM ENERGY THICKNESS = 0.965 MM FORM FACTOR H = 1.748 FORM FACTOR E = 1.716 RDELTASTAR = 798.7 RTHETA = 457.0 SKIN FRICTION COEFFICIENT = 0.003102 CALCULATED CF = 0.001047 Y Y/DEL YPLUS U U/UO UPLUS u u/UO u/U u/UTAU MM M/S M/S % % 0.029 0.005 0.928 0.446 0.037 0.934 0.1947 1.60 43.62 0.4075 0.035 0.006 1.129 0.543 0.045 1.136 0.2309 1.90 42.55 0.4831 0.042 0.007 1.329 0.639 0.053 1.337 0.2806 2.31 43.92 0.5872 0.048 0.008 1.529 0.735 0.061 1.538 0.3375 2.78 45.91 0.7063 0.054 0.009 1.729 0.831 0.069 1.740 0.3906 3.22 46.98 0.8173 0.060 0.010 1.929 0.928 0.076 1.941 0.4477 3.69 48.26 0.9367 0.067 0.012 2.129 1.024 0.084 2.142 0.5224 4.31 51.03 1.0932 0.073 0.013 2.329 1.120 0.092 2.344 0.5756 4.74 51.39 1.2044 0.079 0.014 2.529 1.216 0.100 2.545 0.6121 5.04 50.33 1.2809 0.085 0.015 2.729 1.312 0.108 2.746 0.6557 5.40 49.96 1.3721 0.092 0.016 2.929 1.409 0.116 2.948 0.7236 5.96 51.36 1.5141 0.104 0.018 3.330 1.601 0.132 3.350 0.8163 6.73 50.98 1.7080 0.117 0.020 3.730 1.775 0.146 3.714 0.9203 7.58 51.85 1.9258 0.135 0.023 4.330 2.004 0.165 4.193 1.0460 8.62 52.20 2.1888 0.148 0.026 4.730 2.138 0.176 4.474 1.1211 9.24 52.43 2.3459 0.167 0.029 5.331 2.437 0.201 5.100 1.2557 10.35 51.52 2.6276 0.192 0.033 6.131 2.767 0.228 5.789 1.3808 11.38 49.91 2.8894 0.217 0.037 6.931 3.078 0.254 6.442 1.5066 12.42 48.94 3.1525 0.242 0.042 7.732 3.394 0.280 7.103 1.5783 13.01 46.50 3.3027 0.273 0.047 8.732 3.824 0.315 8.001 1.7128 14.12 44.79 3.5841 0.310 0.054 9.933 4.209 0.347 8.807 1.7678 14.57 42.00 3.6991 0.348 0.060 11.134 4.669 0.385 9.770 1.8465 15.22 39.55 3.8638 0.392 0.068 12.534 5.001 0.412 10.464 1.8460 15.21 36.92 3.8628 0.442 0.076 14.135 5.489 0.452 11.485 1.8343 15.12 33.42 3.8382 0.498 0.086 15.936 5.871 0.484 12.285 1.8076 14.90 30.79 3.7824 0.560 0.097 17.937 6.345 0.523 13.277 1.7577 14.49 27.70 3.6779 0.635 0.110 20.338 6.754 0.557 14.132 1.7052 14.05 25.25 3.5682 0.717 0.124 22.939 7.172 0.591 15.008 1.6675 13.74 23.25 3.4892 0.804 0.139 25.741 7.596 0.626 15.896 1.6388 13.51 21.57 3.4291 0.910 0.158 29.143 8.044 0.663 16.832 1.5802 13.02 19.64 3.3066 1.023 0.177 32.744 8.398 0.692 17.573 1.5250 12.57 18.16 3.1910 1.154 0.200 36.946 8.829 0.728 18.475 1.4617 12.05 16.56 3.0586 1.298 0.225 41.549 9.185 0.757 19.219 1.4186 11.69 15.45 2.9685 1.460 0.253 46.751 9.541 0.786 19.964 1.3614 11.22 14.27 2.8488 1.648 0.285 52.754 9.881 0.814 20.675 1.2977 10.69 13.13 2.7155 1.854 0.321 59.358 10.157 0.837 21.253 1.2539 10.33 12.35 2.6238 2.092 0.362 66.961 10.451 0.861 21.868 1.1938 9.84 11.42 2.4981 2.354 0.408 75.366 10.698 0.882 22.387 1.1097 9.15 10.37 2.3221 2.654 0.460 84.970 10.941 0.902 22.893 1.0336 8.52 9.45 2.1628 2.985 0.517 95.576 11.204 0.923 23.445 0.9195 7.58 8.21 1.9240 3.367 0.583 107.782 11.416 0.941 23.888 0.8178 6.74 7.16 1.7113 3.792 0.656 121.389 11.606 0.956 24.286 0.6998 5.77 6.03 1.4643 4.267 0.739 136.596 11.747 0.968 24.581 0.5978 4.93 5.09 1.2509 4.804 0.832 153.805 11.884 0.979 24.868 0.4764 3.93 4.01 0.9969 5.410 0.937 173.215 11.975 0.987 25.058 0.3719 3.06 3.11 0.7781 6.098 1.056 195.226 12.049 0.993 25.213 0.2858 2.36 2.37 0.5980 6.779 1.174 217.037 12.096 0.997 25.311 0.2318 1.91 1.92 0.4851 7.467 1.293 239.048 12.127 0.999 25.375 0.1945 1.60 1.60 0.4070 8.148 1.411 260.858 12.132 1.000 25.386 0.1724 1.42 1.42 0.3607 8.829 1.529 282.669 12.145 1.001 25.413 0.1639 1.35 1.35 0.3429 11.879 2.057 380.318 12.155 1.002 25.434 0.1528 1.26 1.26 0.3197 14.929 2.585 477.967 12.159 1.002 25.443 0.1501 1.24 1.23 0.3142 17.979 3.113 575.616 12.171 1.003 25.468 0.1521 1.25 1.25 0.3182 21.029 3.641 673.265 12.174 1.003 25.473 0.1529 1.26 1.26 0.3200 RUN NUMBER 1W02304 AXIAL POSITION = 570.0 MM SPAN POSITION = 0.0 MM FREE-STREAM VELOCITY = 12.46 M/S FRICTION VELOCITY = 0.5159 M/S FREE-STREAM TURBULENCE = 1.174 % X-REYNOLDS NUMBER = 47.39 X10**4 FLUID DENSITY = 1.207 KG/M**3 KINEMATIC VISCOSITY = 1.499 X10(-5)MSQ/S BOUNDARY LAYER THICKNESS (99.0%) = 6.84 MM DISPLACEMENT THICKNESS = 1.045 MM MOMENTUM THICKNESS = 0.649 MM ENERGY THICKNESS = 1.134 MM FORM FACTOR H = 1.609 FORM FACTOR E = 1.746 RDELTASTAR = 868.6 RTHETA = 539.9 SKIN FRICTION COEFFICIENT = 0.003428 CALCULATED CF = 0.000965 Y Y/DEL YPLUS U U/UO UPLUS u u/UO u/U u/UTAU MM M/S M/S % % 0.029 0.004 0.998 0.519 0.042 1.006 0.2122 1.70 40.86 0.4112 0.035 0.005 1.213 0.631 0.051 1.223 0.2518 2.02 39.90 0.4880 0.042 0.006 1.428 0.743 0.060 1.440 0.2986 2.40 40.19 0.5789 0.048 0.007 1.644 0.855 0.069 1.657 0.3535 2.84 41.35 0.6852 0.054 0.008 1.859 0.967 0.078 1.874 0.4057 3.26 41.97 0.7864 0.060 0.009 2.074 1.079 0.087 2.091 0.4484 3.60 41.57 0.8693 0.067 0.010 2.289 1.191 0.096 2.308 0.4985 4.00 41.87 0.9664 0.073 0.011 2.504 1.302 0.105 2.525 0.5628 4.52 43.21 1.0910 0.079 0.012 2.719 1.414 0.114 2.742 0.6127 4.92 43.32 1.1877 0.085 0.012 2.934 1.526 0.122 2.959 0.6738 5.41 44.15 1.3061 0.098 0.014 3.364 1.750 0.140 3.392 0.7767 6.23 44.38 1.5056 0.110 0.016 3.795 1.953 0.157 3.785 0.8769 7.04 44.90 1.6997 0.123 0.018 4.225 2.183 0.175 4.232 0.9860 7.91 45.16 1.9112 0.142 0.021 4.870 2.481 0.199 4.810 1.1291 9.06 45.50 2.1886 0.160 0.023 5.516 2.780 0.223 5.389 1.2704 10.20 45.70 2.4626 0.179 0.026 6.161 3.074 0.247 5.958 1.3959 11.20 45.41 2.7059 0.204 0.030 7.022 3.478 0.279 6.742 1.5188 12.19 43.67 2.9440 0.229 0.033 7.882 3.906 0.313 7.570 1.6416 13.17 42.03 3.1822 0.260 0.038 8.958 4.326 0.347 8.386 1.7377 13.95 40.17 3.3684 0.292 0.043 10.033 4.682 0.376 9.075 1.8224 14.63 38.93 3.5326 0.335 0.049 11.539 5.267 0.423 10.209 1.8671 14.98 35.45 3.6193 0.379 0.055 13.045 5.675 0.455 11.001 1.9055 15.29 33.58 3.6937 0.429 0.063 14.766 6.222 0.499 12.060 1.8674 14.99 30.01 3.6197 0.485 0.071 16.702 6.609 0.530 12.811 1.8375 14.75 27.80 3.5617 0.548 0.080 18.853 7.039 0.565 13.645 1.7762 14.25 25.23 3.4430 0.617 0.090 21.220 7.352 0.590 14.252 1.7339 13.91 23.58 3.3610 0.698 0.102 24.016 7.787 0.625 15.094 1.6652 13.36 21.39 3.2278 0.792 0.116 27.243 8.112 0.651 15.724 1.5951 12.80 19.66 3.0919 0.892 0.130 30.685 8.474 0.680 16.426 1.5066 12.09 17.78 2.9204 1.010 0.148 34.772 8.743 0.702 16.947 1.4533 11.66 16.62 2.8171 1.142 0.167 39.290 9.091 0.730 17.621 1.4011 11.24 15.41 2.7159 1.292 0.189 44.453 9.389 0.753 18.200 1.3816 11.09 14.71 2.6781 1.460 0.213 50.261 9.697 0.778 18.796 1.3307 10.68 13.72 2.5795 1.654 0.242 56.930 9.978 0.801 19.342 1.2785 10.26 12.81 2.4783 1.867 0.273 64.244 10.234 0.821 19.838 1.2358 9.92 12.07 2.3954 2.110 0.308 72.633 10.530 0.845 20.412 1.1842 9.50 11.25 2.2954 2.385 0.349 82.099 10.723 0.861 20.786 1.1398 9.15 10.63 2.2093 2.698 0.394 92.855 10.989 0.882 21.301 1.0629 8.53 9.67 2.0604 3.048 0.445 104.902 11.234 0.901 21.775 0.9849 7.90 8.77 1.9092 3.448 0.504 118.669 11.450 0.919 22.195 0.9000 7.22 7.86 1.7445 3.898 0.570 134.158 11.670 0.936 22.620 0.8052 6.46 6.90 1.5608 4.404 0.644 151.583 11.867 0.952 23.002 0.6923 5.56 5.83 1.3419 4.979 0.728 171.374 12.024 0.965 23.308 0.5924 4.75 4.93 1.1484 5.629 0.823 193.746 12.188 0.978 23.624 0.4625 3.71 3.80 0.8966 6.367 0.931 219.131 12.295 0.987 23.833 0.3619 2.90 2.94 0.7015 7.198 1.052 247.742 12.380 0.993 23.997 0.2642 2.12 2.13 0.5121 8.029 1.174 276.353 12.418 0.997 24.071 0.2074 1.66 1.67 0.4019 8.860 1.295 304.964 12.445 0.999 24.124 0.1759 1.41 1.41 0.3410 9.685 1.416 333.360 12.463 1.000 24.158 0.1600 1.28 1.28 0.3101 10.517 1.537 361.971 12.468 1.001 24.168 0.1525 1.22 1.22 0.2955 14.117 2.063 485.881 12.481 1.002 24.194 0.1453 1.17 1.16 0.2816 17.717 2.590 609.790 12.491 1.002 24.213 0.1444 1.16 1.16 0.2798 21.317 3.116 733.700 12.501 1.003 24.232 0.1455 1.17 1.16 0.2820 24.917 3.642 857.609 12.502 1.003 24.234 0.1463 1.17 1.17 0.2836 RUN NUMBER 1W02305 AXIAL POSITION = 645.0 MM SPAN POSITION = 0.0 MM FREE-STREAM VELOCITY = 12.77 M/S FRICTION VELOCITY = 0.6277 M/S FREE-STREAM TURBULENCE = 1.095 % X-REYNOLDS NUMBER = 54.91 X10**4 FLUID DENSITY = 1.206 KG/M**3 KINEMATIC VISCOSITY = 1.500 X10(-5)MSQ/S BOUNDARY LAYER THICKNESS (99.0%) = 7.87 MM DISPLACEMENT THICKNESS = 1.163 MM MOMENTUM THICKNESS = 0.757 MM ENERGY THICKNESS = 1.332 MM FORM FACTOR H = 1.535 FORM FACTOR E = 1.759 RDELTASTAR = 990.0 RTHETA = 644.8 SKIN FRICTION COEFFICIENT = 0.004831 CALCULATED CF = 0.003954 LAW OF THE WALL OFFSET = 5.20 KARMAN CONSTANT = 0.410 FORM FACTOR G = 7.094 CLAUSER DELTA = 23.661 MM WAKE FACTOR PI = 0.239 1 Y Y/DEL YPLUS U U/UO UPLUS u u/UO u/U u/UTAU MM M/S M/S % % 0.029 0.004 1.213 0.628 0.049 1.000 0.2057 1.61 32.77 0.3277 0.035 0.004 1.475 0.763 0.060 1.216 0.2456 1.92 32.19 0.3912 0.042 0.005 1.736 0.898 0.070 1.431 0.2875 2.25 32.00 0.4579 0.048 0.006 1.998 1.034 0.081 1.647 0.3499 2.74 33.86 0.5575 0.054 0.007 2.259 1.169 0.092 1.862 0.3953 3.10 33.82 0.6298 0.060 0.008 2.521 1.304 0.102 2.078 0.4526 3.54 34.71 0.7210 0.067 0.008 2.782 1.439 0.113 2.293 0.5094 3.99 35.39 0.8114 0.073 0.009 3.044 1.575 0.123 2.509 0.5546 4.34 35.22 0.8835 0.079 0.010 3.305 1.710 0.134 2.724 0.6087 4.77 35.60 0.9697 0.085 0.011 3.567 1.794 0.140 2.858 0.6652 5.21 37.08 1.0598 0.098 0.012 4.090 2.008 0.157 3.199 0.7628 5.97 37.98 1.2152 0.110 0.014 4.613 2.192 0.172 3.492 0.8481 6.64 38.69 1.3511 0.129 0.016 5.397 2.518 0.197 4.012 0.9873 7.73 39.20 1.5728 0.142 0.018 5.920 2.748 0.215 4.377 1.0730 8.40 39.05 1.7094 0.167 0.021 6.966 3.136 0.246 4.996 1.2307 9.64 39.24 1.9605 0.185 0.024 7.751 3.465 0.271 5.520 1.3461 10.54 38.85 2.1445 0.210 0.027 8.797 3.836 0.300 6.111 1.4625 11.45 38.12 2.3299 0.242 0.031 10.104 4.289 0.336 6.833 1.5768 12.35 36.76 2.5120 0.273 0.035 11.412 4.831 0.378 7.696 1.6797 13.15 34.77 2.6760 0.310 0.039 12.981 5.354 0.419 8.530 1.7407 13.63 32.51 2.7731 0.348 0.044 14.550 5.793 0.454 9.229 1.7910 14.02 30.91 2.8531 0.398 0.051 16.642 6.263 0.490 9.978 1.7821 13.95 28.45 2.8391 0.448 0.057 18.734 6.756 0.529 10.763 1.7373 13.60 25.71 2.7677 0.510 0.065 21.349 7.160 0.561 11.406 1.7132 13.41 23.93 2.7293 0.579 0.074 24.225 7.537 0.590 12.007 1.6639 13.03 22.08 2.6507 0.654 0.083 27.363 7.907 0.619 12.596 1.6070 12.58 20.32 2.5601 0.742 0.094 31.024 8.244 0.645 13.133 1.5213 11.91 18.45 2.4235 0.842 0.107 35.208 8.559 0.670 13.635 1.4656 11.48 17.12 2.3349 0.954 0.121 39.915 8.879 0.695 14.145 1.4069 11.01 15.84 2.2412 1.079 0.137 45.145 9.126 0.715 14.539 1.3529 10.59 14.82 2.1552 1.223 0.155 51.160 9.387 0.735 14.955 1.2980 10.16 13.83 2.0678 1.392 0.177 58.220 9.656 0.756 15.383 1.2509 9.79 12.96 1.9928 1.573 0.200 65.804 9.893 0.775 15.761 1.2257 9.60 12.39 1.9527 1.785 0.227 74.695 10.134 0.793 16.144 1.1792 9.23 11.64 1.8786 2.023 0.257 84.632 10.348 0.810 16.486 1.1581 9.07 11.19 1.8449 2.292 0.291 95.876 10.583 0.829 16.859 1.1150 8.73 10.54 1.7763 2.598 0.330 108.690 10.830 0.848 17.252 1.0858 8.50 10.03 1.7298 2.942 0.374 123.072 11.086 0.868 17.661 1.0278 8.05 9.27 1.6373 3.335 0.424 139.547 11.319 0.886 18.032 0.9572 7.49 8.46 1.5249 3.779 0.480 158.113 11.567 0.906 18.427 0.8960 7.02 7.75 1.4275 4.279 0.544 179.033 11.806 0.924 18.808 0.8218 6.43 6.96 1.3093 4.854 0.617 203.091 12.033 0.942 19.169 0.7176 5.62 5.96 1.1431 5.498 0.699 230.026 12.243 0.959 19.504 0.6095 4.77 4.98 0.9709 6.229 0.792 260.621 12.432 0.973 19.805 0.4946 3.87 3.98 0.7879 7.060 0.897 295.401 12.567 0.984 20.021 0.3872 3.03 3.08 0.6168 7.998 1.017 334.625 12.665 0.992 20.177 0.2823 2.21 2.23 0.4497 8.935 1.136 373.850 12.728 0.997 20.276 0.2122 1.66 1.67 0.3380 9.873 1.255 413.075 12.759 0.999 20.326 0.1758 1.38 1.38 0.2800 10.817 1.375 452.562 12.785 1.001 20.367 0.1553 1.22 1.21 0.2474 11.754 1.494 491.787 12.786 1.001 20.370 0.1467 1.15 1.15 0.2337 15.754 2.002 659.147 12.792 1.002 20.378 0.1391 1.09 1.09 0.2216 19.754 2.511 826.506 12.804 1.002 20.398 0.1396 1.09 1.09 0.2223 23.754 3.019 993.866 12.810 1.003 20.407 0.1391 1.09 1.09 0.2216 27.754 3.528 1161.226 12.821 1.004 20.424 0.1398 1.09 1.09 0.2227 RUN NUMBER 1W02306 AXIAL POSITION = 720.0 MM SPAN POSITION = 0.0 MM FREE-STREAM VELOCITY = 13.03 M/S FRICTION VELOCITY = 0.6318 M/S FREE-STREAM TURBULENCE = 1.040 % X-REYNOLDS NUMBER = 62.44 X10**4 FLUID DENSITY = 1.204 KG/M**3 KINEMATIC VISCOSITY = 1.503 X10(-5)MSQ/S BOUNDARY LAYER THICKNESS (99.0%) = 8.96 MM DISPLACEMENT THICKNESS = 1.302 MM MOMENTUM THICKNESS = 0.880 MM ENERGY THICKNESS = 1.555 MM FORM FACTOR H = 1.480 FORM FACTOR E = 1.768 RDELTASTAR = 1129.0 RTHETA = 763.0 SKIN FRICTION COEFFICIENT = 0.004702 CALCULATED CF = 0.004123 LAW OF THE WALL OFFSET = 5.20 KARMAN CONSTANT = 0.410 FORM FACTOR G = 6.686 CLAUSER DELTA = 26.850 MM WAKE FACTOR PI = 0.169 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 1.219 0.689 0.053 1.090 0.2136 1.64 31.01 0.3381 0.035 0.004 1.482 0.837 0.064 1.325 0.2661 2.04 31.78 0.4212 0.042 0.005 1.745 0.986 0.076 1.560 0.3225 2.47 32.71 0.5104 0.048 0.005 2.008 1.134 0.087 1.795 0.3831 2.94 33.78 0.6064 0.054 0.006 2.271 1.283 0.098 2.030 0.4382 3.36 34.16 0.6936 0.060 0.007 2.533 1.431 0.110 2.265 0.4991 3.83 34.87 0.7899 0.067 0.007 2.796 1.580 0.121 2.500 0.5447 4.18 34.48 0.8621 0.073 0.008 3.059 1.728 0.133 2.735 0.5934 4.55 34.34 0.9393 0.079 0.009 3.322 1.877 0.144 2.970 0.6330 4.86 33.73 1.0019 0.092 0.010 3.847 2.095 0.161 3.316 0.7356 5.65 35.11 1.1643 0.104 0.012 4.373 2.334 0.179 3.694 0.8196 6.29 35.12 1.2973 0.117 0.013 4.899 2.604 0.200 4.122 0.9283 7.12 35.65 1.4693 0.135 0.015 5.687 2.941 0.226 4.655 1.0580 8.12 35.98 1.6747 0.154 0.017 6.475 3.271 0.251 5.177 1.1765 9.03 35.97 1.8622 0.173 0.019 7.264 3.611 0.277 5.716 1.2842 9.86 35.56 2.0326 0.198 0.022 8.315 4.017 0.308 6.358 1.4021 10.76 34.91 2.2193 0.223 0.025 9.366 4.443 0.341 7.033 1.4934 11.46 33.61 2.3638 0.254 0.028 10.680 4.924 0.378 7.794 1.5972 12.26 32.44 2.5280 0.292 0.033 12.257 5.503 0.422 8.711 1.6587 12.73 30.14 2.6254 0.329 0.037 13.834 5.974 0.459 9.456 1.6896 12.97 28.28 2.6744 0.373 0.042 15.673 6.481 0.497 10.258 1.6908 12.98 26.09 2.6762 0.429 0.048 18.038 6.950 0.533 11.001 1.6638 12.77 23.94 2.6335 0.485 0.054 20.404 7.355 0.564 11.642 1.6341 12.54 22.22 2.5865 0.554 0.062 23.294 7.722 0.593 12.222 1.5798 12.12 20.46 2.5006 0.629 0.070 26.448 8.077 0.620 12.785 1.5193 11.66 18.81 2.4047 0.717 0.080 30.127 8.364 0.642 13.239 1.4647 11.24 17.51 2.3183 0.817 0.091 34.332 8.651 0.664 13.692 1.3925 10.69 16.10 2.2041 0.929 0.104 39.062 8.897 0.683 14.083 1.3353 10.25 15.01 2.1135 1.054 0.118 44.318 9.127 0.700 14.446 1.2760 9.79 13.98 2.0197 1.198 0.134 50.362 9.380 0.720 14.846 1.2365 9.49 13.18 1.9571 1.367 0.153 57.458 9.594 0.736 15.185 1.1880 9.12 12.38 1.8804 1.554 0.173 65.342 9.809 0.753 15.526 1.1518 8.84 11.74 1.8231 1.767 0.197 74.277 10.051 0.771 15.909 1.1259 8.64 11.20 1.7822 2.010 0.224 84.526 10.270 0.788 16.255 1.1004 8.45 10.72 1.7418 2.285 0.255 96.089 10.515 0.807 16.643 1.0716 8.22 10.19 1.6962 2.598 0.290 109.229 10.736 0.824 16.993 1.0266 7.88 9.56 1.6249 2.954 0.330 124.208 10.976 0.842 17.372 0.9876 7.58 9.00 1.5631 3.360 0.375 141.290 11.237 0.862 17.786 0.9516 7.30 8.47 1.5062 3.823 0.427 160.737 11.502 0.883 18.205 0.8969 6.88 7.80 1.4197 4.348 0.485 182.812 11.766 0.903 18.624 0.8427 6.47 7.16 1.3339 4.942 0.552 207.777 12.019 0.922 19.023 0.7681 5.90 6.39 1.2158 5.623 0.628 236.422 12.287 0.943 19.448 0.6737 5.17 5.48 1.0663 6.392 0.713 268.746 12.494 0.959 19.775 0.5738 4.40 4.59 0.9082 7.267 0.811 305.538 12.689 0.974 20.084 0.4610 3.54 3.63 0.7297 8.267 0.923 347.585 12.855 0.987 20.346 0.3373 2.59 2.62 0.5339 9.398 1.049 395.151 12.948 0.994 20.494 0.2424 1.86 1.87 0.3836 10.529 1.175 442.717 12.998 0.998 20.573 0.1831 1.41 1.41 0.2898 11.667 1.302 490.546 13.016 0.999 20.603 0.1565 1.20 1.20 0.2477 12.798 1.428 538.112 13.035 1.000 20.631 0.1438 1.10 1.10 0.2275 13.929 1.555 585.678 13.029 1.000 20.622 0.1378 1.06 1.06 0.2181 18.629 2.079 783.301 13.043 1.001 20.645 0.1340 1.03 1.03 0.2121 23.329 2.604 980.924 13.058 1.002 20.669 0.1337 1.03 1.02 0.2116 28.029 3.128 1178.547 13.064 1.003 20.678 0.1349 1.04 1.03 0.2135 32.729 3.653 1376.170 13.076 1.004 20.696 0.1355 1.04 1.04 0.2145 RUN NUMBER 1W02307 AXIAL POSITION = 795.0 MM SPAN POSITION = 0.0 MM FREE-STREAM VELOCITY = 13.25 M/S FRICTION VELOCITY = 0.6315 M/S FREE-STREAM TURBULENCE = 0.994 % X-REYNOLDS NUMBER = 70.01 X10**4 FLUID DENSITY = 1.202 KG/M**3 KINEMATIC VISCOSITY = 1.504 X10(-5)MSQ/S BOUNDARY LAYER THICKNESS (99.0%) = 9.93 MM DISPLACEMENT THICKNESS = 1.456 MM MOMENTUM THICKNESS = 1.001 MM ENERGY THICKNESS = 1.772 MM FORM FACTOR H = 1.455 FORM FACTOR E = 1.770 RDELTASTAR = 1282.6 RTHETA = 881.6 SKIN FRICTION COEFFICIENT = 0.004545 CALCULATED CF = 0.004123 LAW OF THE WALL OFFSET = 5.20 KARMAN CONSTANT = 0.410 FORM FACTOR G = 6.557 CLAUSER DELTA = 30.549 MM WAKE FACTOR PI = 0.152 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 1.218 0.701 0.053 1.109 0.2028 1.53 28.95 0.3211 0.035 0.004 1.480 0.851 0.064 1.348 0.2250 1.70 26.43 0.3563 0.042 0.004 1.742 1.002 0.076 1.587 0.2806 2.12 27.99 0.4443 0.048 0.005 2.005 1.153 0.087 1.826 0.3301 2.49 28.62 0.5227 0.054 0.005 2.267 1.304 0.098 2.065 0.3989 3.01 30.58 0.6316 0.060 0.006 2.530 1.455 0.110 2.305 0.4538 3.43 31.18 0.7186 0.067 0.007 2.792 1.606 0.121 2.544 0.5198 3.92 32.36 0.8230 0.073 0.007 3.054 1.757 0.133 2.783 0.5797 4.38 32.99 0.9179 0.079 0.008 3.317 1.908 0.144 3.022 0.6266 4.73 32.84 0.9922 0.092 0.009 3.842 2.154 0.163 3.411 0.7304 5.51 33.91 1.1566 0.104 0.010 4.366 2.409 0.182 3.815 0.8324 6.28 34.55 1.3180 0.117 0.012 4.891 2.665 0.201 4.221 0.9315 7.03 34.95 1.4749 0.135 0.014 5.678 3.061 0.231 4.847 1.0679 8.06 34.89 1.6909 0.154 0.016 6.466 3.432 0.259 5.435 1.1909 8.99 34.70 1.8857 0.179 0.018 7.515 3.878 0.293 6.141 1.3300 10.04 34.29 2.1059 0.204 0.021 8.565 4.349 0.328 6.886 1.4282 10.78 32.84 2.2614 0.235 0.024 9.877 4.853 0.366 7.685 1.5339 11.58 31.60 2.4288 0.267 0.027 11.189 5.321 0.402 8.425 1.5982 12.06 30.04 2.5306 0.304 0.031 12.763 5.868 0.443 9.292 1.6335 12.33 27.84 2.5866 0.348 0.035 14.600 6.420 0.485 10.165 1.6494 12.45 25.69 2.6117 0.398 0.040 16.699 6.831 0.516 10.816 1.6399 12.38 24.01 2.5967 0.448 0.045 18.799 7.237 0.546 11.459 1.5938 12.03 22.02 2.5237 0.517 0.052 21.685 7.629 0.576 12.079 1.5576 11.76 20.42 2.4663 0.585 0.059 24.572 7.953 0.600 12.593 1.5053 11.36 18.93 2.3836 0.667 0.067 27.983 8.274 0.625 13.102 1.4494 10.94 17.52 2.2951 0.760 0.077 31.919 8.544 0.645 13.530 1.3772 10.40 16.12 2.1807 0.867 0.087 36.380 8.785 0.663 13.911 1.3258 10.01 15.09 2.0993 0.992 0.100 41.628 9.017 0.681 14.278 1.2704 9.59 14.09 2.0116 1.129 0.114 47.401 9.233 0.697 14.619 1.2143 9.17 13.15 1.9228 1.292 0.130 54.224 9.442 0.713 14.951 1.1771 8.89 12.47 1.8639 1.473 0.148 61.833 9.660 0.729 15.296 1.1277 8.51 11.67 1.7856 1.679 0.169 70.493 9.876 0.746 15.638 1.0863 8.20 11.00 1.7201 1.910 0.192 80.202 10.111 0.763 16.011 1.0562 7.97 10.45 1.6724 2.179 0.219 91.485 10.332 0.780 16.360 1.0376 7.83 10.04 1.6429 2.485 0.250 104.343 10.561 0.797 16.722 0.9974 7.53 9.44 1.5793 2.829 0.285 118.775 10.780 0.814 17.070 0.9671 7.30 8.97 1.5314 3.229 0.325 135.569 11.052 0.834 17.500 0.9367 7.07 8.48 1.4832 3.679 0.370 154.462 11.298 0.853 17.890 0.9124 6.89 8.08 1.4447 4.198 0.423 176.242 11.598 0.876 18.366 0.8707 6.57 7.51 1.3787 4.785 0.482 200.908 11.853 0.895 18.769 0.8185 6.18 6.91 1.2960 5.454 0.549 228.986 12.137 0.916 19.218 0.7552 5.70 6.22 1.1959 6.217 0.626 260.999 12.425 0.938 19.674 0.6720 5.07 5.41 1.0640 7.085 0.713 297.474 12.687 0.958 20.090 0.5647 4.26 4.45 0.8942 8.079 0.813 339.196 12.904 0.974 20.433 0.4564 3.45 3.54 0.7227 9.210 0.927 386.692 13.066 0.986 20.690 0.3320 2.51 2.54 0.5256 10.498 1.057 440.747 13.176 0.995 20.864 0.2321 1.75 1.76 0.3675 11.785 1.186 494.803 13.222 0.998 20.937 0.1720 1.30 1.30 0.2724 13.073 1.316 548.858 13.234 0.999 20.956 0.1451 1.10 1.10 0.2298 14.360 1.445 602.914 13.243 1.000 20.969 0.1368 1.03 1.03 0.2166 15.654 1.576 657.232 13.250 1.000 20.980 0.1328 1.00 1.00 0.2102 20.904 2.104 877.653 13.261 1.001 20.998 0.1296 0.98 0.98 0.2051 26.154 2.633 1098.073 13.271 1.002 21.014 0.1303 0.98 0.98 0.2063 31.404 3.161 1318.494 13.278 1.002 21.025 0.1311 0.99 0.99 0.2075 36.654 3.690 1538.915 13.289 1.003 21.043 0.1317 0.99 0.99 0.2085 RUN NUMBER 1W02308 AXIAL POSITION = 895.0 MM SPAN POSITION = 0.0 MM FREE-STREAM VELOCITY = 13.40 M/S FRICTION VELOCITY = 0.6172 M/S FREE-STREAM TURBULENCE = 0.941 % X-REYNOLDS NUMBER = 80.25 X10**4 FLUID DENSITY = 1.210 KG/M**3 KINEMATIC VISCOSITY = 1.494 X10(-5)MSQ/S BOUNDARY LAYER THICKNESS (99.0%) = 11.32 MM DISPLACEMENT THICKNESS = 1.735 MM MOMENTUM THICKNESS = 1.198 MM ENERGY THICKNESS = 2.116 MM FORM FACTOR H = 1.448 FORM FACTOR E = 1.766 RDELTASTAR = 1555.9 RTHETA = 1074.2 SKIN FRICTION COEFFICIENT = 0.004244 CALCULATED CF = 0.003950 LAW OF THE WALL OFFSET = 5.20 KARMAN CONSTANT = 0.410 FORM FACTOR G = 6.720 CLAUSER DELTA = 37.667 MM WAKE FACTOR PI = 0.223 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 1.198 0.655 0.049 1.062 0.2050 1.53 31.28 0.3321 0.035 0.003 1.456 0.797 0.059 1.291 0.2211 1.65 27.76 0.3583 0.042 0.004 1.714 0.938 0.070 1.519 0.2625 1.96 27.99 0.4253 0.048 0.004 1.972 1.079 0.081 1.748 0.3173 2.37 29.41 0.5141 0.054 0.005 2.230 1.220 0.091 1.977 0.3672 2.74 30.09 0.5950 0.060 0.005 2.489 1.361 0.102 2.206 0.4233 3.16 31.09 0.6858 0.067 0.006 2.747 1.503 0.112 2.435 0.4745 3.54 31.57 0.7688 0.073 0.006 3.005 1.644 0.123 2.664 0.5378 4.01 32.71 0.8713 0.079 0.007 3.263 1.785 0.133 2.893 0.5863 4.38 32.84 0.9500 0.092 0.008 3.779 1.986 0.148 3.219 0.6811 5.08 34.29 1.1035 0.104 0.009 4.296 2.192 0.164 3.551 0.7658 5.72 34.94 1.2408 0.123 0.011 5.070 2.564 0.191 4.155 0.9029 6.74 35.21 1.4630 0.142 0.013 5.845 2.938 0.219 4.761 1.0437 7.79 35.52 1.6911 0.160 0.014 6.619 3.317 0.248 5.374 1.1605 8.66 34.99 1.8804 0.185 0.016 7.652 3.812 0.284 6.176 1.3076 9.76 34.31 2.1187 0.210 0.019 8.684 4.267 0.319 6.914 1.4135 10.55 33.12 2.2902 0.242 0.021 9.975 4.803 0.359 7.783 1.5156 11.31 31.55 2.4557 0.273 0.024 11.266 5.250 0.392 8.507 1.5735 11.74 29.97 2.5495 0.310 0.027 12.815 5.750 0.429 9.317 1.6124 12.04 28.04 2.6126 0.354 0.031 14.622 6.218 0.464 10.075 1.6219 12.11 26.08 2.6280 0.410 0.036 16.945 6.731 0.502 10.906 1.5991 11.94 23.76 2.5910 0.467 0.041 19.269 7.123 0.532 11.541 1.5780 11.78 22.15 2.5568 0.535 0.047 22.108 7.489 0.559 12.134 1.5343 11.45 20.49 2.4860 0.610 0.054 25.206 7.805 0.583 12.646 1.4782 11.03 18.94 2.3951 0.698 0.062 28.820 8.093 0.604 13.113 1.4196 10.60 17.54 2.3002 0.792 0.070 32.693 8.376 0.625 13.571 1.3578 10.14 16.21 2.2001 0.910 0.080 37.598 8.620 0.643 13.966 1.2996 9.70 15.08 2.1057 1.035 0.091 42.761 8.847 0.660 14.334 1.2515 9.34 14.15 2.0279 1.185 0.105 48.957 9.076 0.677 14.707 1.1927 8.90 13.14 1.9326 1.354 0.120 55.927 9.258 0.691 15.001 1.1478 8.57 12.40 1.8597 1.542 0.136 63.671 9.492 0.709 15.380 1.1079 8.27 11.67 1.7951 1.760 0.156 72.707 9.681 0.723 15.687 1.0724 8.00 11.08 1.7376 2.017 0.178 83.291 9.932 0.741 16.093 1.0421 7.78 10.49 1.6886 2.298 0.203 94.908 10.126 0.756 16.407 1.0208 7.62 10.08 1.6539 2.629 0.232 108.590 10.349 0.772 16.769 0.9955 7.43 9.62 1.6129 2.998 0.265 123.822 10.606 0.792 17.185 0.9681 7.23 9.13 1.5687 3.423 0.302 141.376 10.877 0.812 17.623 0.9349 6.98 8.60 1.5148 3.910 0.345 161.512 11.147 0.832 18.062 0.9102 6.79 8.16 1.4747 4.467 0.395 184.488 11.427 0.853 18.516 0.8748 6.53 7.66 1.4174 5.098 0.450 210.562 11.732 0.876 19.009 0.8262 6.17 7.04 1.3388 5.823 0.514 240.508 12.034 0.898 19.498 0.7706 5.75 6.40 1.2485 6.648 0.587 274.584 12.342 0.921 19.997 0.7072 5.28 5.73 1.1459 7.592 0.671 313.566 12.629 0.943 20.463 0.6289 4.69 4.98 1.0189 8.667 0.766 357.969 12.909 0.964 20.916 0.5204 3.88 4.03 0.8432 9.892 0.874 408.567 13.130 0.980 21.275 0.3970 2.96 3.02 0.6432 11.298 0.998 466.652 13.286 0.992 21.527 0.2713 2.02 2.04 0.4396 12.698 1.122 524.479 13.360 0.997 21.647 0.1934 1.44 1.45 0.3134 14.104 1.246 582.564 13.392 1.000 21.700 0.1525 1.14 1.14 0.2472 15.504 1.370 640.390 13.401 1.000 21.713 0.1357 1.01 1.01 0.2199 16.910 1.494 698.475 13.405 1.001 21.720 0.1300 0.97 0.97 0.2107 22.560 1.993 931.848 13.418 1.002 21.741 0.1252 0.93 0.93 0.2029 28.210 2.492 1165.220 13.426 1.002 21.754 0.1251 0.93 0.93 0.2027 33.860 2.991 1398.593 13.441 1.003 21.778 0.1270 0.95 0.94 0.2057 39.510 3.490 1631.965 13.448 1.004 21.790 0.1261 0.94 0.94 0.2043 RUN NUMBER 1W02309 AXIAL POSITION = 995.0 MM SPAN POSITION = 0.0 MM FREE-STREAM VELOCITY = 13.36 M/S FRICTION VELOCITY = 0.5933 M/S FREE-STREAM TURBULENCE = 0.923 % X-REYNOLDS NUMBER = 88.95 X10**4 FLUID DENSITY = 1.210 KG/M**3 KINEMATIC VISCOSITY = 1.495 X10(-5)MSQ/S BOUNDARY LAYER THICKNESS (99.0%) = 13.27 MM DISPLACEMENT THICKNESS = 2.091 MM MOMENTUM THICKNESS = 1.448 MM ENERGY THICKNESS = 2.550 MM FORM FACTOR H = 1.444 FORM FACTOR E = 1.761 RDELTASTAR = 1868.9 RTHETA = 1294.4 SKIN FRICTION COEFFICIENT = 0.003943 CALCULATED CF = 0.003784 LAW OF THE WALL OFFSET = 5.20 KARMAN CONSTANT = 0.410 FORM FACTOR G = 6.923 CLAUSER DELTA = 47.086 MM WAKE FACTOR PI = 0.329 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 1.151 0.607 0.045 1.023 0.1919 1.44 31.60 0.3235 0.035 0.003 1.399 0.738 0.055 1.244 0.2071 1.55 28.05 0.3490 0.042 0.003 1.647 0.869 0.065 1.465 0.2475 1.85 28.49 0.4172 0.048 0.004 1.895 1.000 0.075 1.685 0.2911 2.18 29.11 0.4906 0.054 0.004 2.143 1.131 0.085 1.906 0.3322 2.49 29.38 0.5599 0.060 0.005 2.391 1.262 0.094 2.126 0.3861 2.89 30.60 0.6507 0.067 0.005 2.639 1.392 0.104 2.347 0.4456 3.33 32.00 0.7511 0.073 0.005 2.888 1.523 0.114 2.568 0.5024 3.76 32.98 0.8468 0.085 0.006 3.384 1.785 0.134 3.009 0.6127 4.59 34.33 1.0328 0.098 0.007 3.880 2.007 0.150 3.383 0.7030 5.26 35.03 1.1849 0.110 0.008 4.376 2.255 0.169 3.801 0.8025 6.01 35.58 1.3526 0.123 0.009 4.872 2.504 0.187 4.220 0.9000 6.74 35.95 1.5170 0.142 0.011 5.616 2.890 0.216 4.871 1.0369 7.76 35.88 1.7478 0.167 0.013 6.609 3.350 0.251 5.646 1.1994 8.98 35.81 2.0217 0.192 0.014 7.601 3.832 0.287 6.459 1.3194 9.87 34.43 2.2239 0.217 0.016 8.593 4.247 0.318 7.158 1.4100 10.55 33.20 2.3766 0.248 0.019 9.834 4.735 0.354 7.981 1.4968 11.20 31.61 2.5230 0.285 0.022 11.322 5.283 0.395 8.905 1.5650 11.71 29.62 2.6378 0.329 0.025 13.058 5.749 0.430 9.690 1.5664 11.72 27.25 2.6403 0.373 0.028 14.795 6.148 0.460 10.363 1.5760 11.79 25.63 2.6564 0.429 0.032 17.028 6.570 0.492 11.074 1.5524 11.62 23.63 2.6166 0.492 0.037 19.508 6.941 0.519 11.700 1.5298 11.45 22.04 2.5785 0.567 0.043 22.485 7.304 0.547 12.312 1.4785 11.06 20.24 2.4920 0.648 0.049 25.710 7.593 0.568 12.799 1.4281 10.69 18.81 2.4072 0.742 0.056 29.431 7.854 0.588 13.239 1.3687 10.24 17.43 2.3070 0.848 0.064 33.648 8.116 0.607 13.680 1.3123 9.82 16.17 2.2120 0.973 0.073 38.610 8.337 0.624 14.053 1.2651 9.47 15.17 2.1325 1.110 0.084 44.067 8.556 0.640 14.422 1.2113 9.07 14.16 2.0418 1.273 0.096 50.517 8.749 0.655 14.747 1.1763 8.80 13.44 1.9827 1.460 0.110 57.959 8.945 0.669 15.077 1.1368 8.51 12.71 1.9162 1.667 0.126 66.146 9.174 0.687 15.462 1.1034 8.26 12.03 1.8599 1.910 0.144 75.820 9.370 0.701 15.793 1.0675 7.99 11.39 1.7994 2.185 0.165 86.735 9.583 0.717 16.152 1.0502 7.86 10.96 1.7702 2.504 0.189 99.387 9.809 0.734 16.533 1.0209 7.64 10.41 1.7209 2.867 0.216 113.775 10.056 0.753 16.951 1.0044 7.52 9.99 1.6929 3.285 0.248 130.396 10.300 0.771 17.362 0.9729 7.28 9.45 1.6398 3.760 0.283 149.249 10.544 0.789 17.772 0.9548 7.15 9.06 1.6094 4.304 0.324 170.831 10.840 0.811 18.272 0.9233 6.91 8.52 1.5563 4.929 0.372 195.638 11.135 0.833 18.769 0.8916 6.67 8.01 1.5028 5.642 0.425 223.919 11.458 0.858 19.314 0.8514 6.37 7.43 1.4352 6.460 0.487 256.416 11.791 0.882 19.875 0.7949 5.95 6.74 1.3399 7.392 0.557 293.378 12.136 0.908 20.456 0.7381 5.52 6.08 1.2441 8.467 0.638 336.047 12.459 0.932 21.000 0.6520 4.88 5.23 1.0990 9.692 0.731 384.668 12.765 0.955 21.517 0.5569 4.17 4.36 0.9387 11.092 0.836 440.236 13.030 0.975 21.963 0.4257 3.19 3.27 0.7176 12.698 0.957 503.990 13.215 0.989 22.275 0.2875 2.15 2.18 0.4846 14.304 1.078 567.745 13.305 0.996 22.426 0.1988 1.49 1.49 0.3351 15.910 1.199 631.499 13.345 0.999 22.494 0.1510 1.13 1.13 0.2545 17.517 1.320 695.253 13.347 0.999 22.497 0.1330 1.00 1.00 0.2242 19.117 1.441 758.759 13.358 1.000 22.516 0.1259 0.94 0.94 0.2122 25.467 1.920 1010.799 13.370 1.001 22.535 0.1220 0.91 0.91 0.2057 31.817 2.398 1262.839 13.379 1.001 22.551 0.1214 0.91 0.91 0.2047 38.167 2.877 1514.879 13.391 1.002 22.571 0.1217 0.91 0.91 0.2051 44.517 3.356 1766.918 13.400 1.003 22.586 0.1234 0.92 0.92 0.2079 RUN NUMBER 1W02310 AXIAL POSITION = 1095.0 MM SPAN POSITION = 0.0 MM FREE-STREAM VELOCITY = 13.09 M/S FRICTION VELOCITY = 0.5585 M/S FREE-STREAM TURBULENCE = 0.925 % X-REYNOLDS NUMBER = 95.85 X10**4 FLUID DENSITY = 1.209 KG/M**3 KINEMATIC VISCOSITY = 1.496 X10(-5)MSQ/S BOUNDARY LAYER THICKNESS (99.0%) = 15.16 MM DISPLACEMENT THICKNESS = 2.532 MM MOMENTUM THICKNESS = 1.742 MM ENERGY THICKNESS = 3.049 MM FORM FACTOR H = 1.454 FORM FACTOR E = 1.751 RDELTASTAR = 2216.3 RTHETA = 1524.7 SKIN FRICTION COEFFICIENT = 0.003639 CALCULATED CF = 0.003567 LAW OF THE WALL OFFSET = 5.20 KARMAN CONSTANT = 0.410 FORM FACTOR G = 7.316 CLAUSER DELTA = 59.355 MM WAKE FACTOR PI = 0.470 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 1.083 0.574 0.044 1.027 0.1794 1.37 31.27 0.3213 0.035 0.002 1.316 0.697 0.053 1.249 0.2050 1.57 29.39 0.3670 0.042 0.003 1.550 0.821 0.063 1.470 0.2466 1.88 30.03 0.4415 0.048 0.003 1.783 0.945 0.072 1.692 0.2919 2.23 30.90 0.5227 0.054 0.004 2.016 1.068 0.082 1.913 0.3415 2.61 31.97 0.6115 0.060 0.004 2.250 1.192 0.091 2.134 0.3848 2.94 32.28 0.6890 0.067 0.004 2.483 1.316 0.100 2.356 0.4371 3.34 33.22 0.7826 0.073 0.005 2.716 1.439 0.110 2.577 0.4867 3.72 33.82 0.8715 0.085 0.006 3.183 1.687 0.129 3.020 0.5861 4.48 34.75 1.0494 0.098 0.006 3.650 1.899 0.145 3.401 0.6776 5.18 35.67 1.2132 0.110 0.007 4.117 2.128 0.163 3.810 0.7788 5.95 36.60 1.3944 0.129 0.009 4.817 2.475 0.189 4.431 0.9056 6.92 36.59 1.6214 0.148 0.010 5.517 2.804 0.214 5.021 1.0343 7.90 36.88 1.8519 0.173 0.011 6.451 3.238 0.247 5.798 1.1723 8.95 36.20 2.0990 0.198 0.013 7.384 3.609 0.276 6.462 1.2702 9.70 35.19 2.2744 0.229 0.015 8.551 4.069 0.311 7.285 1.3720 10.48 33.72 2.4565 0.267 0.018 9.951 4.589 0.350 8.216 1.4578 11.13 31.77 2.6102 0.304 0.020 11.351 5.065 0.387 9.068 1.4967 11.43 29.55 2.6798 0.354 0.023 13.218 5.507 0.421 9.860 1.5076 11.51 27.38 2.6994 0.404 0.027 15.085 5.909 0.451 10.580 1.5095 11.53 25.54 2.7027 0.467 0.031 17.419 6.295 0.481 11.271 1.4850 11.34 23.59 2.6589 0.535 0.035 19.986 6.625 0.506 11.862 1.4560 11.12 21.98 2.6069 0.617 0.041 23.020 6.911 0.528 12.374 1.4051 10.73 20.33 2.5158 0.704 0.046 26.287 7.179 0.548 12.853 1.3645 10.42 19.01 2.4432 0.810 0.053 30.255 7.436 0.568 13.314 1.3198 10.08 17.75 2.3631 0.935 0.062 34.922 7.666 0.586 13.726 1.2792 9.77 16.69 2.2904 1.073 0.071 40.057 7.877 0.602 14.103 1.2203 9.32 15.49 2.1850 1.235 0.081 46.124 8.096 0.618 14.495 1.1810 9.02 14.59 2.1146 1.417 0.093 52.892 8.283 0.633 14.831 1.1436 8.73 13.81 2.0476 1.629 0.107 60.827 8.514 0.650 15.244 1.1119 8.49 13.06 1.9909 1.873 0.124 69.929 8.714 0.666 15.602 1.0893 8.32 12.50 1.9503 2.154 0.142 80.431 8.905 0.680 15.945 1.0640 8.13 11.95 1.9050 2.473 0.163 92.333 9.132 0.697 16.351 1.0373 7.92 11.36 1.8572 2.848 0.188 106.335 9.346 0.714 16.735 1.0223 7.81 10.94 1.8305 3.273 0.216 122.205 9.604 0.734 17.197 1.0039 7.67 10.45 1.7975 3.760 0.248 140.408 9.848 0.752 17.632 0.9911 7.57 10.06 1.7746 4.317 0.285 161.179 10.133 0.774 18.143 0.9623 7.35 9.50 1.7230 4.960 0.327 185.217 10.431 0.797 18.677 0.9383 7.17 9.00 1.6801 5.704 0.376 212.988 10.761 0.822 19.267 0.8991 6.87 8.36 1.6097 6.554 0.432 244.727 11.086 0.847 19.849 0.8637 6.60 7.79 1.5464 7.535 0.497 281.368 11.439 0.874 20.481 0.8108 6.19 7.09 1.4518 8.654 0.571 323.142 11.812 0.902 21.150 0.7422 5.67 6.28 1.3289 9.948 0.656 371.451 12.179 0.930 21.806 0.6606 5.05 5.42 1.1827 11.429 0.754 426.761 12.540 0.958 22.452 0.5380 4.11 4.29 0.9633 13.135 0.866 490.473 12.812 0.978 22.939 0.3956 3.02 3.09 0.7083 15.098 0.996 563.753 12.989 0.992 23.256 0.2578 1.97 1.98 0.4615 17.054 1.125 636.799 13.067 0.998 23.397 0.1702 1.30 1.30 0.3048 19.017 1.254 710.079 13.088 1.000 23.433 0.1365 1.04 1.04 0.2444 20.973 1.383 783.126 13.097 1.000 23.451 0.1241 0.95 0.95 0.2223 22.935 1.513 856.406 13.103 1.001 23.461 0.1205 0.92 0.92 0.2158 30.485 2.011 1138.325 13.116 1.002 23.484 0.1191 0.91 0.91 0.2133 38.035 2.509 1420.243 13.126 1.002 23.502 0.1192 0.91 0.91 0.2134 45.585 3.007 1702.161 13.126 1.003 23.503 0.1200 0.92 0.91 0.2148 53.135 3.505 1984.079 13.127 1.003 23.503 0.1211 0.93 0.92 0.2169 RUN NUMBER 1W02401 AXIAL POSITION = 1195.0 MM SPAN POSITION = 0.0 MM FREE-STREAM VELOCITY = 12.77 M/S FRICTION VELOCITY = 0.5223 M/S FREE-STREAM TURBULENCE = 0.931 % X-REYNOLDS NUMBER = 101.82 X10**4 FLUID DENSITY = 1.207 KG/M**3 KINEMATIC VISCOSITY = 1.499 X10(-5)MSQ/S BOUNDARY LAYER THICKNESS (99.0%) = 17.56 MM DISPLACEMENT THICKNESS = 3.112 MM MOMENTUM THICKNESS = 2.111 MM ENERGY THICKNESS = 3.673 MM FORM FACTOR H = 1.474 FORM FACTOR E = 1.740 RDELTASTAR = 2651.2 RTHETA = 1798.3 SKIN FRICTION COEFFICIENT = 0.003346 CALCULATED CF = 0.003304 LAW OF THE WALL OFFSET = 5.20 KARMAN CONSTANT = 0.410 FORM FACTOR G = 7.865 CLAUSER DELTA = 76.074 MM WAKE FACTOR PI = 0.614 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 1.011 0.464 0.036 0.889 0.1638 1.28 35.26 0.3136 0.035 0.002 1.228 0.565 0.044 1.081 0.1800 1.41 31.89 0.3447 0.042 0.002 1.446 0.665 0.052 1.273 0.2097 1.64 31.55 0.4016 0.048 0.003 1.664 0.765 0.060 1.464 0.2401 1.88 31.39 0.4597 0.054 0.003 1.882 0.865 0.068 1.656 0.2729 2.14 31.55 0.5225 0.060 0.003 2.100 0.965 0.076 1.848 0.3137 2.46 32.50 0.6006 0.067 0.004 2.318 1.065 0.083 2.039 0.3460 2.71 32.48 0.6624 0.073 0.004 2.535 1.165 0.091 2.231 0.3841 3.01 32.96 0.7354 0.085 0.005 2.971 1.365 0.107 2.615 0.4727 3.70 34.62 0.9051 0.098 0.006 3.407 1.566 0.123 2.998 0.5588 4.38 35.69 1.0699 0.117 0.007 4.060 1.828 0.143 3.501 0.6829 5.35 37.35 1.3076 0.135 0.008 4.713 2.085 0.163 3.992 0.7806 6.11 37.44 1.4946 0.154 0.009 5.367 2.334 0.183 4.470 0.8804 6.90 37.72 1.6858 0.179 0.010 6.238 2.675 0.210 5.122 1.0054 7.87 37.58 1.9250 0.210 0.012 7.327 3.085 0.242 5.907 1.1393 8.92 36.93 2.1815 0.242 0.014 8.416 3.516 0.275 6.732 1.2448 9.75 35.40 2.3834 0.279 0.016 9.723 3.960 0.310 7.582 1.3394 10.49 33.82 2.5645 0.323 0.018 11.248 4.456 0.349 8.532 1.3865 10.86 31.12 2.6548 0.373 0.021 12.990 4.918 0.385 9.417 1.4349 11.24 29.18 2.7475 0.429 0.024 14.951 5.365 0.420 10.272 1.4473 11.33 26.98 2.7712 0.492 0.028 17.129 5.728 0.449 10.968 1.4312 11.21 24.99 2.7405 0.567 0.032 19.743 6.082 0.476 11.645 1.4086 11.03 23.16 2.6971 0.654 0.037 22.792 6.407 0.502 12.268 1.3680 10.71 21.35 2.6193 0.754 0.043 26.277 6.685 0.524 12.800 1.3136 10.29 19.65 2.5151 0.873 0.050 30.416 6.929 0.543 13.267 1.2722 9.96 18.36 2.4359 1.004 0.057 34.990 7.170 0.562 13.728 1.2158 9.52 16.96 2.3279 1.160 0.066 40.435 7.381 0.578 14.133 1.1837 9.27 16.04 2.2664 1.335 0.076 46.534 7.566 0.593 14.487 1.1531 9.03 15.24 2.2080 1.535 0.087 53.504 7.798 0.611 14.930 1.1178 8.75 14.34 2.1403 1.773 0.101 61.781 7.969 0.624 15.258 1.0862 8.51 13.63 2.0799 2.042 0.116 71.147 8.159 0.639 15.622 1.0690 8.37 13.10 2.0469 2.354 0.134 82.037 8.341 0.653 15.971 1.0504 8.23 12.59 2.0112 2.717 0.155 94.671 8.570 0.671 16.409 1.0335 8.09 12.06 1.9790 3.129 0.178 109.046 8.797 0.689 16.844 1.0273 8.05 11.68 1.9670 3.610 0.206 125.818 9.044 0.708 17.318 1.0126 7.93 11.20 1.9388 4.160 0.237 144.986 9.320 0.730 17.845 0.9876 7.73 10.60 1.8910 4.792 0.273 166.985 9.571 0.750 18.327 0.9741 7.63 10.18 1.8651 5.523 0.314 192.469 9.880 0.774 18.917 0.9558 7.49 9.67 1.8301 6.367 0.362 221.874 10.194 0.798 19.518 0.9215 7.22 9.04 1.7645 7.335 0.418 255.635 10.548 0.826 20.196 0.8875 6.95 8.41 1.6994 8.460 0.482 294.842 10.933 0.856 20.934 0.8340 6.53 7.63 1.5969 9.748 0.555 339.711 11.318 0.886 21.670 0.7783 6.10 6.88 1.4903 11.235 0.640 391.551 11.731 0.919 22.462 0.6904 5.41 5.89 1.3220 12.948 0.737 451.232 12.113 0.949 23.193 0.5744 4.50 4.74 1.0998 14.923 0.850 520.061 12.434 0.974 23.808 0.4261 3.34 3.43 0.8159 17.198 0.979 599.346 12.659 0.991 24.238 0.2593 2.03 2.05 0.4966 19.473 1.109 678.630 12.738 0.998 24.390 0.1690 1.32 1.33 0.3236 21.748 1.238 757.914 12.766 1.000 24.443 0.1324 1.04 1.04 0.2535 24.023 1.368 837.199 12.776 1.001 24.464 0.1209 0.95 0.95 0.2314 26.298 1.497 916.483 12.779 1.001 24.470 0.1173 0.92 0.92 0.2246 34.898 1.987 1216.195 12.790 1.002 24.489 0.1157 0.91 0.90 0.2216 43.498 2.477 1515.907 12.798 1.002 24.505 0.1165 0.91 0.91 0.2230 52.098 2.966 1815.619 12.803 1.003 24.515 0.1180 0.92 0.92 0.2258 60.698 3.456 2115.331 12.806 1.003 24.521 0.1189 0.93 0.93 0.2277 RUN NUMBER 1W02402 AXIAL POSITION = 1295.0 MM SPAN POSITION = 0.0 MM FREE-STREAM VELOCITY = 12.35 M/S FRICTION VELOCITY = 0.4808 M/S FREE-STREAM TURBULENCE = 0.940 % X-REYNOLDS NUMBER = 106.72 X10**4 FLUID DENSITY = 1.207 KG/M**3 KINEMATIC VISCOSITY = 1.498 X10(-5)MSQ/S BOUNDARY LAYER THICKNESS (99.0%) = 20.84 MM DISPLACEMENT THICKNESS = 3.843 MM MOMENTUM THICKNESS = 2.573 MM ENERGY THICKNESS = 4.446 MM FORM FACTOR H = 1.493 FORM FACTOR E = 1.728 RDELTASTAR = 3166.7 RTHETA = 2120.6 SKIN FRICTION COEFFICIENT = 0.003034 CALCULATED CF = 0.003069 LAW OF THE WALL OFFSET = 5.20 KARMAN CONSTANT = 0.410 FORM FACTOR G = 8.482 CLAUSER DELTA = 98.663 MM WAKE FACTOR PI = 0.878 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 0.931 0.420 0.034 0.874 0.1631 1.32 38.81 0.3391 0.035 0.002 1.131 0.511 0.041 1.062 0.1866 1.51 36.53 0.3880 0.042 0.002 1.332 0.601 0.049 1.251 0.2124 1.72 35.33 0.4418 0.048 0.002 1.533 0.692 0.056 1.439 0.2467 2.00 35.66 0.5132 0.054 0.003 1.733 0.782 0.063 1.627 0.2792 2.26 35.68 0.5806 0.060 0.003 1.934 0.873 0.071 1.816 0.3108 2.52 35.60 0.6464 0.067 0.003 2.134 0.964 0.078 2.004 0.3458 2.80 35.89 0.7192 0.079 0.004 2.536 1.145 0.093 2.381 0.4217 3.42 36.84 0.8771 0.092 0.004 2.937 1.326 0.107 2.757 0.4874 3.95 36.76 1.0137 0.104 0.005 3.338 1.507 0.122 3.134 0.5592 4.53 37.11 1.1631 0.123 0.006 3.940 1.713 0.139 3.564 0.6493 5.26 37.89 1.3504 0.142 0.007 4.542 1.928 0.156 4.009 0.7463 6.05 38.72 1.5521 0.160 0.008 5.143 2.153 0.174 4.478 0.8418 6.82 39.10 1.7508 0.185 0.009 5.946 2.459 0.199 5.114 0.9533 7.72 38.77 1.9826 0.217 0.010 6.949 2.846 0.231 5.920 1.0794 8.74 37.92 2.2450 0.254 0.012 8.152 3.293 0.267 6.849 1.1872 9.62 36.05 2.4691 0.292 0.014 9.356 3.704 0.300 7.703 1.2665 10.26 34.19 2.6341 0.335 0.016 10.760 4.100 0.332 8.528 1.3284 10.76 32.40 2.7628 0.392 0.019 12.566 4.568 0.370 9.501 1.3592 11.01 29.76 2.8269 0.448 0.021 14.371 4.893 0.396 10.177 1.3659 11.06 27.91 2.8408 0.523 0.025 16.778 5.250 0.425 10.919 1.3516 10.95 25.74 2.8110 0.604 0.029 19.386 5.605 0.454 11.658 1.3215 10.70 23.58 2.7485 0.698 0.033 22.395 5.878 0.476 12.226 1.2843 10.40 21.85 2.6710 0.804 0.039 25.805 6.135 0.497 12.760 1.2515 10.14 20.40 2.6028 0.929 0.045 29.817 6.356 0.515 13.220 1.2288 9.95 19.33 2.5556 1.079 0.052 34.632 6.566 0.532 13.656 1.1819 9.57 18.00 2.4580 1.248 0.060 40.048 6.789 0.550 14.119 1.1471 9.29 16.90 2.3857 1.442 0.069 46.267 6.982 0.566 14.520 1.1095 8.99 15.89 2.3076 1.667 0.080 53.488 7.178 0.581 14.929 1.0837 8.78 15.10 2.2540 1.923 0.092 61.713 7.343 0.595 15.272 1.0600 8.59 14.44 2.2046 2.223 0.107 71.342 7.531 0.610 15.662 1.0454 8.47 13.88 2.1743 2.567 0.123 82.375 7.725 0.626 16.067 1.0335 8.37 13.38 2.1495 2.973 0.143 95.414 7.936 0.643 16.506 1.0276 8.32 12.95 2.1371 3.435 0.165 110.259 8.158 0.661 16.967 1.0202 8.26 12.51 2.1218 3.967 0.190 127.310 8.389 0.680 17.448 1.0021 8.12 11.94 2.0841 4.585 0.220 147.169 8.623 0.698 17.934 0.9941 8.05 11.53 2.0675 5.298 0.254 170.038 8.906 0.721 18.523 0.9781 7.92 10.98 2.0343 6.123 0.294 196.517 9.209 0.746 19.152 0.9654 7.82 10.48 2.0079 7.079 0.340 227.209 9.528 0.772 19.815 0.9382 7.60 9.85 1.9513 8.179 0.392 262.515 9.913 0.803 20.618 0.9014 7.30 9.09 1.8748 9.454 0.454 303.438 10.290 0.833 21.401 0.8675 7.03 8.43 1.8043 10.929 0.524 350.780 10.709 0.867 22.273 0.8039 6.51 7.51 1.6719 12.629 0.606 405.343 11.126 0.901 23.139 0.7286 5.90 6.55 1.5154 14.598 0.700 468.533 11.580 0.938 24.084 0.6128 4.96 5.29 1.2745 16.873 0.810 541.552 11.956 0.968 24.866 0.4542 3.68 3.80 0.9447 19.498 0.936 625.804 12.207 0.989 25.388 0.2783 2.25 2.28 0.5789 22.123 1.062 710.057 12.305 0.997 25.591 0.1696 1.37 1.38 0.3528 24.748 1.188 794.310 12.329 0.999 25.642 0.1303 1.06 1.06 0.2709 27.379 1.314 878.763 12.333 0.999 25.651 0.1189 0.96 0.96 0.2474 30.004 1.440 963.016 12.344 1.000 25.674 0.1147 0.93 0.93 0.2386 39.754 1.908 1275.954 12.351 1.000 25.688 0.1145 0.93 0.93 0.2381 49.504 2.375 1588.892 12.361 1.001 25.708 0.1145 0.93 0.93 0.2382 59.254 2.843 1901.830 12.369 1.002 25.725 0.1158 0.94 0.94 0.2407 69.004 3.311 2214.769 12.372 1.002 25.731 0.1160 0.94 0.94 0.2413 RUN NUMBER 1W02403 AXIAL POSITION = 1395.0 MM SPAN POSITION = 0.0 MM FREE-STREAM VELOCITY = 11.90 M/S FRICTION VELOCITY = 0.4365 M/S FREE-STREAM TURBULENCE = 0.961 % X-REYNOLDS NUMBER = 110.83 X10**4 FLUID DENSITY = 1.208 KG/M**3 KINEMATIC VISCOSITY = 1.497 X10(-5)MSQ/S BOUNDARY LAYER THICKNESS (99.0%) = 24.85 MM DISPLACEMENT THICKNESS = 4.884 MM MOMENTUM THICKNESS = 3.187 MM ENERGY THICKNESS = 5.452 MM FORM FACTOR H = 1.532 FORM FACTOR E = 1.710 RDELTASTAR = 3880.5 RTHETA = 2532.4 SKIN FRICTION COEFFICIENT = 0.002692 CALCULATED CF = 0.002753 LAW OF THE WALL OFFSET = 5.20 KARMAN CONSTANT = 0.410 FORM FACTOR G = 9.469 CLAUSER DELTA = 133.123 MM WAKE FACTOR PI = 1.169 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 0.845 0.330 0.028 0.756 0.1190 1.00 36.05 0.2726 0.035 0.001 1.028 0.401 0.034 0.919 0.1347 1.13 33.57 0.3086 0.042 0.002 1.210 0.472 0.040 1.082 0.1511 1.27 31.98 0.3461 0.048 0.002 1.392 0.544 0.046 1.245 0.1691 1.42 31.12 0.3875 0.054 0.002 1.574 0.615 0.052 1.408 0.1960 1.65 31.88 0.4490 0.060 0.002 1.756 0.686 0.058 1.571 0.2249 1.89 32.79 0.5152 0.067 0.003 1.938 0.757 0.064 1.734 0.2543 2.14 33.59 0.5826 0.079 0.003 2.303 0.899 0.076 2.060 0.3138 2.64 34.89 0.7189 0.092 0.004 2.667 1.042 0.088 2.386 0.3776 3.17 36.25 0.8651 0.104 0.004 3.032 1.184 0.100 2.712 0.4435 3.73 37.46 1.0160 0.123 0.005 3.578 1.397 0.117 3.201 0.5436 4.57 38.90 1.2455 0.148 0.006 4.307 1.642 0.138 3.761 0.6593 5.54 40.16 1.5106 0.167 0.007 4.853 1.818 0.153 4.166 0.7392 6.21 40.66 1.6937 0.198 0.008 5.764 2.106 0.177 4.826 0.8507 7.15 40.39 1.9491 0.229 0.009 6.675 2.403 0.202 5.506 0.9547 8.03 39.72 2.1873 0.267 0.011 7.768 2.783 0.234 6.376 1.0718 9.01 38.52 2.4556 0.310 0.012 9.044 3.196 0.269 7.321 1.1602 9.75 36.31 2.6581 0.354 0.014 10.319 3.547 0.298 8.128 1.2109 10.18 34.14 2.7744 0.417 0.017 12.141 4.012 0.337 9.192 1.2604 10.60 31.42 2.8878 0.479 0.019 13.963 4.337 0.365 9.936 1.2695 10.67 29.27 2.9085 0.560 0.023 16.331 4.657 0.391 10.670 1.2752 10.72 27.38 2.9215 0.648 0.026 18.882 4.966 0.417 11.379 1.2542 10.54 25.25 2.8735 0.754 0.030 21.979 5.239 0.440 12.004 1.2182 10.24 23.25 2.7911 0.873 0.035 25.441 5.481 0.461 12.557 1.1890 9.99 21.69 2.7241 1.010 0.041 29.449 5.696 0.479 13.051 1.1592 9.74 20.35 2.6558 1.173 0.047 34.186 5.907 0.497 13.534 1.1353 9.54 19.22 2.6011 1.360 0.055 39.651 6.089 0.512 13.952 1.1022 9.27 18.10 2.5253 1.579 0.064 46.028 6.282 0.528 14.392 1.0766 9.05 17.14 2.4667 1.835 0.074 53.497 6.463 0.543 14.808 1.0560 8.88 16.34 2.4195 2.129 0.086 62.060 6.627 0.557 15.182 1.0418 8.76 15.72 2.3870 2.467 0.099 71.898 6.812 0.573 15.607 1.0267 8.63 15.07 2.3523 2.860 0.115 83.376 7.014 0.590 16.069 1.0177 8.55 14.51 2.3317 3.317 0.133 96.676 7.215 0.606 16.529 1.0073 8.47 13.96 2.3079 3.848 0.155 112.162 7.417 0.624 16.994 1.0072 8.47 13.58 2.3075 4.467 0.180 130.198 7.659 0.644 17.548 1.0034 8.43 13.10 2.2988 5.179 0.208 150.968 7.890 0.663 18.078 0.9978 8.39 12.65 2.2862 6.004 0.242 175.016 8.178 0.687 18.736 0.9927 8.34 12.14 2.2743 6.967 0.280 203.073 8.492 0.714 19.456 0.9766 8.21 11.50 2.2376 8.079 0.325 235.502 8.846 0.744 20.268 0.9496 7.98 10.73 2.1756 9.367 0.377 273.033 9.204 0.774 21.087 0.9262 7.79 10.06 2.1221 10.867 0.437 316.758 9.648 0.811 22.106 0.8848 7.44 9.17 2.0272 12.604 0.507 367.406 10.068 0.846 23.067 0.8312 6.99 8.26 1.9043 14.617 0.588 426.070 10.576 0.889 24.230 0.7452 6.26 7.05 1.7074 16.948 0.682 494.026 11.045 0.928 25.305 0.6282 5.28 5.69 1.4393 19.660 0.791 573.095 11.461 0.963 26.258 0.4750 3.99 4.14 1.0883 22.798 0.918 664.553 11.748 0.988 26.915 0.2731 2.30 2.32 0.6256 25.935 1.044 756.011 11.849 0.996 27.149 0.1601 1.35 1.35 0.3668 29.079 1.170 847.651 11.875 0.998 27.208 0.1241 1.04 1.05 0.2843 32.217 1.297 939.109 11.886 0.999 27.232 0.1162 0.98 0.98 0.2663 35.354 1.423 1030.567 11.890 0.999 27.241 0.1139 0.96 0.96 0.2609 43.873 1.766 1278.888 11.903 1.001 27.272 0.1126 0.95 0.95 0.2580 52.392 2.109 1527.209 11.912 1.001 27.292 0.1146 0.96 0.96 0.2626 60.910 2.451 1775.530 11.926 1.003 27.324 0.1130 0.95 0.95 0.2590 69.429 2.794 2023.851 11.925 1.002 27.322 0.1143 0.96 0.96 0.2618 RUN NUMBER 1W02404 AXIAL POSITION = 1495.0 MM SPAN POSITION = 0.0 MM FREE-STREAM VELOCITY = 11.29 M/S FRICTION VELOCITY = 0.3803 M/S FREE-STREAM TURBULENCE = 1.000 % X-REYNOLDS NUMBER = 112.75 X10**4 FLUID DENSITY = 1.208 KG/M**3 KINEMATIC VISCOSITY = 1.497 X10(-5)MSQ/S BOUNDARY LAYER THICKNESS (99.0%) = 29.25 MM DISPLACEMENT THICKNESS = 6.343 MM MOMENTUM THICKNESS = 3.984 MM ENERGY THICKNESS = 6.717 MM FORM FACTOR H = 1.592 FORM FACTOR E = 1.686 RDELTASTAR = 4783.8 RTHETA = 3004.8 SKIN FRICTION COEFFICIENT = 0.002268 CALCULATED CF = 0.002396 LAW OF THE WALL OFFSET = 5.20 KARMAN CONSTANT = 0.410 FORM FACTOR G = 9.999 CLAUSER DELTA = 188.349 MM WAKE FACTOR PI = 1.722 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 0.737 0.269 0.024 0.708 0.0967 0.86 35.89 0.2543 0.035 0.001 0.895 0.327 0.029 0.861 0.1064 0.94 32.51 0.2799 0.042 0.001 1.054 0.386 0.034 1.014 0.1225 1.08 31.77 0.3221 0.048 0.002 1.213 0.444 0.039 1.167 0.1320 1.17 29.75 0.3470 0.054 0.002 1.372 0.502 0.044 1.319 0.1511 1.34 30.11 0.3973 0.060 0.002 1.530 0.560 0.050 1.472 0.1708 1.51 30.51 0.4491 0.067 0.002 1.689 0.618 0.055 1.625 0.1977 1.75 32.01 0.5200 0.079 0.003 2.007 0.734 0.065 1.930 0.2531 2.24 34.49 0.6656 0.092 0.003 2.324 0.850 0.075 2.235 0.3000 2.66 35.29 0.7889 0.110 0.004 2.800 1.024 0.091 2.693 0.3974 3.52 38.80 1.0451 0.129 0.004 3.276 1.198 0.106 3.152 0.4874 4.32 40.67 1.2817 0.148 0.005 3.753 1.351 0.120 3.553 0.5672 5.02 41.99 1.4916 0.173 0.006 4.388 1.535 0.136 4.037 0.6603 5.85 43.01 1.7364 0.204 0.007 5.181 1.757 0.156 4.621 0.7471 6.62 42.52 1.9648 0.242 0.008 6.134 2.065 0.183 5.431 0.8720 7.72 42.22 2.2930 0.279 0.010 7.086 2.345 0.208 6.168 0.9538 8.45 40.67 2.5083 0.323 0.011 8.197 2.654 0.235 6.978 1.0326 9.14 38.91 2.7154 0.379 0.013 9.626 3.036 0.269 7.984 1.0980 9.72 36.16 2.8874 0.442 0.015 11.214 3.363 0.298 8.844 1.1398 10.09 33.89 2.9974 0.517 0.018 13.118 3.724 0.330 9.794 1.1582 10.26 31.10 3.0456 0.598 0.020 15.182 4.051 0.359 10.654 1.1670 10.34 28.80 3.0689 0.698 0.024 17.722 4.285 0.379 11.268 1.1443 10.13 26.71 3.0092 0.810 0.028 20.579 4.524 0.401 11.896 1.1382 10.08 25.16 2.9932 0.942 0.032 23.913 4.726 0.419 12.427 1.1080 9.81 23.45 2.9136 1.098 0.038 27.882 4.910 0.435 12.913 1.0912 9.66 22.22 2.8695 1.279 0.044 32.485 5.099 0.452 13.408 1.0611 9.40 20.81 2.7904 1.492 0.051 37.882 5.254 0.465 13.816 1.0467 9.27 19.92 2.7526 1.735 0.059 44.073 5.418 0.480 14.247 1.0197 9.03 18.82 2.6816 2.017 0.069 51.217 5.601 0.496 14.729 1.0185 9.02 18.18 2.6782 2.348 0.080 59.630 5.755 0.510 15.133 1.0086 8.93 17.53 2.6524 2.735 0.094 69.472 5.931 0.525 15.598 1.0004 8.86 16.87 2.6307 3.185 0.109 80.901 6.132 0.543 16.126 1.0037 8.89 16.37 2.6396 3.704 0.127 94.077 6.295 0.558 16.555 0.9882 8.75 15.70 2.5987 4.310 0.147 109.475 6.494 0.575 17.077 0.9978 8.84 15.37 2.6239 5.017 0.171 127.413 6.728 0.596 17.693 1.0011 8.87 14.88 2.6325 5.842 0.200 148.367 6.988 0.619 18.375 0.9929 8.79 14.21 2.6110 6.798 0.232 172.655 7.279 0.645 19.141 1.0025 8.88 13.77 2.6362 7.910 0.270 200.911 7.578 0.671 19.929 0.9911 8.78 13.08 2.6063 9.204 0.315 233.770 7.932 0.702 20.859 0.9768 8.65 12.31 2.5686 10.710 0.366 272.027 8.336 0.738 21.922 0.9509 8.42 11.41 2.5006 12.460 0.426 316.475 8.757 0.776 23.027 0.9199 8.15 10.51 2.4192 14.504 0.496 368.384 9.248 0.819 24.319 0.8663 7.67 9.37 2.2782 16.879 0.577 428.706 9.784 0.866 25.729 0.7928 7.02 8.10 2.0848 19.642 0.671 498.870 10.316 0.914 27.128 0.6733 5.96 6.53 1.7706 22.854 0.781 580.464 10.806 0.957 28.417 0.5028 4.45 4.65 1.3222 26.598 0.909 675.551 11.138 0.986 29.291 0.2873 2.54 2.58 0.7555 30.335 1.037 770.479 11.254 0.997 29.595 0.1627 1.44 1.45 0.4278 34.079 1.165 865.565 11.282 0.999 29.669 0.1229 1.09 1.09 0.3233 37.823 1.293 960.652 11.289 1.000 29.687 0.1147 1.02 1.02 0.3016 41.560 1.421 1055.580 11.286 1.000 29.678 0.1118 0.99 0.99 0.2941 48.529 1.659 1232.578 11.298 1.001 29.711 0.1131 1.00 1.00 0.2973 55.492 1.897 1409.417 11.303 1.001 29.724 0.1110 0.98 0.98 0.2918 62.454 2.135 1586.256 11.308 1.001 29.736 0.1119 0.99 0.99 0.2944 69.423 2.373 1763.254 11.311 1.002 29.744 0.1129 1.00 1.00 0.2968