ROLLS-ROYCE APPLIED SCIENCE LABORATORY FLAT PLATE TRANSITIONAL BOUNDARY LAYER FLOW HOT WIRE ANEMOMETRY TEST DATA SINGLE WIRE DATA FOR ERCOFTAC T3A TEST CASE RUN NUMBER 1W01104 AXIAL POSITION = 45.0 MM SPAN POSITION = 0.0 MM FREE-STREAM VELOCITY = 5.05 M/S FRICTION VELOCITY = 0.2575 M/S FREE-STREAM TURBULENCE = 3.043 % X-REYNOLDS NUMBER = 1.52 X10**4 FLUID DENSITY = 1.208 KG/M**3 KINEMATIC VISCOSITY = 1.497 X10(-5)MSQ/S BOUNDARY LAYER THICKNESS (99.0%) = 1.84 MM DISPLACEMENT THICKNESS = 0.620 MM MOMENTUM THICKNESS = 0.236 MM ENERGY THICKNESS = 0.371 MM FORM FACTOR H = 2.621 FORM FACTOR E = 1.570 RDELTASTAR = 209.0 RTHETA = 79.7 SKIN FRICTION COEFFICIENT = 0.005203 CALCULATED CF = 0.005390 Y Y/DEL YPLUS U U/UO UPLUS u u/UO u/U u/UTAU MM M/S M/S % % 0.179 0.097 3.075 0.824 0.163 3.200 0.0539 1.07 6.54 0.2093 0.191 0.104 3.290 0.863 0.171 3.351 0.0580 1.15 6.72 0.2251 0.210 0.114 3.612 0.928 0.184 3.604 0.0650 1.29 7.01 0.2525 0.229 0.124 3.935 1.000 0.198 3.884 0.0717 1.42 7.17 0.2784 0.254 0.138 4.365 1.106 0.219 4.296 0.0807 1.60 7.29 0.3133 0.273 0.148 4.687 1.204 0.239 4.676 0.0909 1.80 7.55 0.3529 0.298 0.161 5.117 1.321 0.262 5.130 0.0999 1.98 7.56 0.3880 0.329 0.178 5.655 1.461 0.289 5.672 0.1122 2.22 7.68 0.4357 0.354 0.192 6.085 1.575 0.312 6.116 0.1216 2.41 7.72 0.4723 0.391 0.212 6.730 1.747 0.346 6.782 0.1385 2.74 7.93 0.5376 0.423 0.229 7.268 1.888 0.374 7.333 0.1454 2.88 7.70 0.5646 0.460 0.250 7.913 2.063 0.408 8.009 0.1590 3.15 7.71 0.6174 0.504 0.273 8.665 2.238 0.443 8.691 0.1735 3.44 7.75 0.6738 0.548 0.297 9.418 2.429 0.481 9.434 0.1821 3.61 7.50 0.7073 0.598 0.324 10.278 2.645 0.524 10.272 0.1971 3.90 7.45 0.7654 0.654 0.355 11.245 2.898 0.574 11.253 0.2131 4.22 7.35 0.8276 0.716 0.389 12.321 3.166 0.627 12.295 0.2228 4.41 7.04 0.8650 0.779 0.423 13.396 3.410 0.675 13.243 0.2273 4.50 6.66 0.8825 0.848 0.460 14.578 3.676 0.728 14.275 0.2347 4.65 6.39 0.9115 0.929 0.504 15.976 3.951 0.783 15.344 0.2318 4.59 5.87 0.9002 1.010 0.548 17.373 4.144 0.821 16.091 0.2246 4.45 5.42 0.8722 1.104 0.599 18.986 4.371 0.866 16.973 0.2123 4.21 4.86 0.8245 1.204 0.653 20.706 4.550 0.901 17.669 0.2052 4.06 4.51 0.7969 1.310 0.711 22.534 4.693 0.930 18.225 0.1961 3.88 4.18 0.7615 1.429 0.775 24.577 4.822 0.955 18.725 0.1835 3.63 3.80 0.7124 1.554 0.843 26.727 4.910 0.972 19.065 0.1794 3.55 3.65 0.6967 1.698 0.921 29.199 4.966 0.984 19.284 0.1751 3.47 3.53 0.6801 1.835 0.996 31.565 4.996 0.990 19.401 0.1730 3.43 3.46 0.6717 1.979 1.074 34.037 5.026 0.995 19.516 0.1714 3.40 3.41 0.6657 2.116 1.148 36.403 5.036 0.998 19.557 0.1691 3.35 3.36 0.6566 2.260 1.226 38.875 5.053 1.001 19.622 0.1690 3.35 3.34 0.6563 3.110 1.688 53.496 5.067 1.004 19.676 0.1594 3.16 3.15 0.6191 3.960 2.149 68.118 5.058 1.002 19.641 0.1558 3.09 3.08 0.6050 4.810 2.610 82.739 5.046 0.999 19.595 0.1552 3.07 3.08 0.6026 5.660 3.071 97.360 5.056 1.001 19.634 0.1536 3.04 3.04 0.5965 RUN NUMBER 1W01105 AXIAL POSITION = 95.0 MM SPAN POSITION = 0.0 MM FREE-STREAM VELOCITY = 5.11 M/S FRICTION VELOCITY = 0.2206 M/S FREE-STREAM TURBULENCE = 2.793 % X-REYNOLDS NUMBER = 3.24 X10**4 FLUID DENSITY = 1.208 KG/M**3 KINEMATIC VISCOSITY = 1.498 X10(-5)MSQ/S BOUNDARY LAYER THICKNESS (99.0%) = 2.71 MM DISPLACEMENT THICKNESS = 0.882 MM MOMENTUM THICKNESS = 0.344 MM ENERGY THICKNESS = 0.545 MM FORM FACTOR H = 2.562 FORM FACTOR E = 1.583 RDELTASTAR = 300.8 RTHETA = 117.4 SKIN FRICTION COEFFICIENT = 0.003723 CALCULATED CF = 0.003688 Y Y/DEL YPLUS U U/UO UPLUS u u/UO u/U u/UTAU MM M/S M/S % % 0.210 0.078 3.096 0.707 0.138 3.207 0.0713 1.39 10.08 0.3233 0.235 0.087 3.464 0.776 0.152 3.520 0.0811 1.59 10.44 0.3676 0.260 0.096 3.832 0.846 0.166 3.836 0.0927 1.81 10.96 0.4203 0.285 0.105 4.200 0.919 0.180 4.169 0.1042 2.04 11.33 0.4725 0.317 0.117 4.660 1.010 0.198 4.580 0.1199 2.35 11.87 0.5438 0.348 0.128 5.120 1.109 0.217 5.029 0.1307 2.56 11.79 0.5927 0.385 0.142 5.672 1.223 0.239 5.544 0.1432 2.80 11.71 0.6491 0.429 0.159 6.317 1.371 0.268 6.217 0.1632 3.19 11.90 0.7399 0.473 0.175 6.961 1.521 0.298 6.898 0.1839 3.60 12.09 0.8338 0.523 0.193 7.697 1.689 0.330 7.657 0.2047 4.00 12.12 0.9280 0.579 0.214 8.525 1.895 0.371 8.590 0.2279 4.46 12.03 1.0334 0.642 0.237 9.445 2.116 0.414 9.592 0.2471 4.83 11.68 1.1203 0.704 0.260 10.366 2.312 0.452 10.485 0.2738 5.36 11.84 1.2414 0.779 0.288 11.470 2.577 0.504 11.687 0.2864 5.60 11.11 1.2985 0.860 0.318 12.666 2.832 0.554 12.839 0.3083 6.03 10.89 1.3978 0.954 0.352 14.047 3.110 0.608 14.100 0.3226 6.31 10.37 1.4625 1.054 0.389 15.519 3.369 0.659 15.274 0.3309 6.47 9.82 1.5004 1.167 0.431 17.176 3.628 0.710 16.450 0.3252 6.36 8.96 1.4744 1.292 0.477 19.016 3.905 0.764 17.707 0.3259 6.38 8.35 1.4777 1.423 0.526 20.949 4.142 0.810 18.781 0.3110 6.08 7.51 1.4102 1.573 0.581 23.157 4.370 0.855 19.814 0.2976 5.82 6.81 1.3492 1.742 0.643 25.642 4.581 0.896 20.771 0.2614 5.11 5.71 1.1851 1.923 0.710 28.311 4.763 0.932 21.594 0.2312 4.52 4.85 1.0483 2.129 0.787 31.348 4.894 0.957 22.189 0.2049 4.01 4.19 0.9292 2.348 0.867 34.568 4.991 0.976 22.628 0.1779 3.48 3.56 0.8066 2.598 0.960 38.249 5.049 0.988 22.894 0.1669 3.27 3.31 0.7569 2.842 1.050 41.838 5.085 0.995 23.054 0.1597 3.12 3.14 0.7239 3.092 1.142 45.519 5.102 0.998 23.132 0.1565 3.06 3.07 0.7096 3.342 1.235 49.201 5.116 1.001 23.197 0.1530 2.99 2.99 0.6936 3.585 1.325 52.789 5.117 1.001 23.202 0.1509 2.95 2.95 0.6840 4.885 1.805 71.931 5.125 1.002 23.236 0.1449 2.84 2.83 0.6572 6.185 2.285 91.072 5.118 1.001 23.205 0.1426 2.79 2.79 0.6466 7.485 2.766 110.213 5.116 1.001 23.197 0.1423 2.78 2.78 0.6452 8.785 3.246 129.355 5.117 1.001 23.203 0.1428 2.79 2.79 0.6473 RUN NUMBER 1W01106 AXIAL POSITION = 195.0 MM SPAN POSITION = 0.0 MM FREE-STREAM VELOCITY = 5.15 M/S FRICTION VELOCITY = 0.1874 M/S FREE-STREAM TURBULENCE = 2.434 % X-REYNOLDS NUMBER = 6.70 X10**4 FLUID DENSITY = 1.205 KG/M**3 KINEMATIC VISCOSITY = 1.501 X10(-5)MSQ/S BOUNDARY LAYER THICKNESS (99.0%) = 4.17 MM DISPLACEMENT THICKNESS = 1.277 MM MOMENTUM THICKNESS = 0.514 MM ENERGY THICKNESS = 0.820 MM FORM FACTOR H = 2.484 FORM FACTOR E = 1.596 RDELTASTAR = 438.4 RTHETA = 176.5 SKIN FRICTION COEFFICIENT = 0.002645 CALCULATED CF = 0.002566 Y Y/DEL YPLUS U U/UO UPLUS u u/UO u/U u/UTAU MM M/S M/S % % 0.254 0.061 3.172 0.601 0.117 3.209 0.1009 1.96 16.78 0.5383 0.285 0.068 3.562 0.658 0.128 3.509 0.1100 2.14 16.74 0.5872 0.317 0.076 3.952 0.720 0.140 3.844 0.1303 2.53 18.09 0.6954 0.354 0.085 4.421 0.813 0.158 4.336 0.1504 2.92 18.51 0.8028 0.392 0.094 4.889 0.896 0.174 4.781 0.1662 3.23 18.55 0.8868 0.442 0.106 5.513 1.007 0.195 5.374 0.1933 3.75 19.20 1.0316 0.492 0.118 6.138 1.148 0.223 6.124 0.2221 4.31 19.35 1.1851 0.548 0.131 6.840 1.267 0.246 6.760 0.2486 4.82 19.62 1.3265 0.610 0.146 7.621 1.432 0.278 7.644 0.2691 5.22 18.79 1.4361 0.679 0.163 8.479 1.616 0.314 8.622 0.3039 5.90 18.81 1.6218 0.760 0.182 9.494 1.791 0.348 9.557 0.3332 6.47 18.61 1.7782 0.848 0.203 10.587 2.017 0.391 10.762 0.3745 7.27 18.57 1.9983 0.942 0.226 11.757 2.258 0.438 12.051 0.4047 7.85 17.92 2.1598 1.054 0.253 13.162 2.488 0.483 13.276 0.4265 8.28 17.14 2.2759 1.173 0.281 14.645 2.743 0.532 14.641 0.4439 8.62 16.18 2.3692 1.310 0.314 16.362 3.018 0.586 16.106 0.4746 9.21 15.73 2.5330 1.460 0.350 18.235 3.308 0.642 17.655 0.4779 9.27 14.45 2.5503 1.629 0.391 20.343 3.581 0.695 19.109 0.4830 9.37 13.49 2.5776 1.817 0.436 22.684 3.879 0.753 20.703 0.4669 9.06 12.04 2.4919 2.023 0.485 25.260 4.136 0.803 22.074 0.4544 8.82 10.99 2.4252 2.260 0.542 28.226 4.367 0.848 23.304 0.4142 8.04 9.49 2.2106 2.517 0.604 31.426 4.588 0.890 24.485 0.3724 7.23 8.12 1.9875 2.810 0.674 35.094 4.773 0.926 25.473 0.3089 6.00 6.47 1.6487 3.135 0.752 39.153 4.913 0.954 26.219 0.2566 4.98 5.22 1.3694 3.492 0.838 43.602 5.007 0.972 26.719 0.2115 4.11 4.22 1.1288 3.898 0.935 48.675 5.085 0.987 27.135 0.1707 3.31 3.36 0.9108 4.298 1.031 53.670 5.113 0.992 27.287 0.1525 2.96 2.98 0.8138 4.704 1.129 58.743 5.142 0.998 27.440 0.1429 2.77 2.78 0.7628 5.104 1.225 63.738 5.153 1.000 27.501 0.1350 2.62 2.62 0.7206 5.504 1.321 68.734 5.157 1.001 27.519 0.1321 2.56 2.56 0.7051 7.454 1.788 93.085 5.159 1.001 27.533 0.1260 2.45 2.44 0.6725 9.404 2.256 117.436 5.161 1.002 27.540 0.1252 2.43 2.43 0.6680 11.354 2.724 141.788 5.166 1.003 27.569 0.1251 2.43 2.42 0.6675 13.304 3.192 166.139 5.169 1.003 27.584 0.1254 2.43 2.43 0.6692 RUN NUMBER 1W01107 AXIAL POSITION = 295.0 MM SPAN POSITION = 0.0 MM FREE-STREAM VELOCITY = 5.19 M/S FRICTION VELOCITY = 0.1750 M/S FREE-STREAM TURBULENCE = 2.197 % X-REYNOLDS NUMBER = 10.06 X10**4 FLUID DENSITY = 1.188 KG/M**3 KINEMATIC VISCOSITY = 1.523 X10(-5)MSQ/S BOUNDARY LAYER THICKNESS (99.0%) = 5.68 MM DISPLACEMENT THICKNESS = 1.576 MM MOMENTUM THICKNESS = 0.660 MM ENERGY THICKNESS = 1.064 MM FORM FACTOR H = 2.390 FORM FACTOR E = 1.613 RDELTASTAR = 537.4 RTHETA = 224.9 SKIN FRICTION COEFFICIENT = 0.002272 CALCULATED CF = 0.002094 Y Y/DEL YPLUS U U/UO UPLUS u u/UO u/U u/UTAU MM M/S M/S % % 0.292 0.051 3.350 0.560 0.108 3.202 0.1164 2.24 20.77 0.6650 0.329 0.058 3.781 0.628 0.121 3.591 0.1415 2.73 22.53 0.8088 0.367 0.065 4.211 0.697 0.134 3.981 0.1600 3.08 22.97 0.9143 0.410 0.072 4.714 0.801 0.154 4.580 0.1951 3.76 24.34 1.1150 0.460 0.081 5.289 0.893 0.172 5.105 0.2253 4.34 25.22 1.2876 0.523 0.092 6.007 1.032 0.199 5.897 0.2658 5.12 25.77 1.5193 0.585 0.103 6.725 1.182 0.228 6.758 0.2861 5.51 24.20 1.6354 0.654 0.115 7.515 1.321 0.255 7.551 0.3025 5.83 22.89 1.7287 0.735 0.129 8.449 1.506 0.290 8.609 0.3570 6.88 23.70 2.0403 0.829 0.146 9.526 1.707 0.329 9.758 0.3911 7.53 22.91 2.2351 0.929 0.164 10.675 1.906 0.367 10.894 0.4311 8.31 22.62 2.4641 1.048 0.184 12.040 2.154 0.415 12.310 0.4880 9.40 22.66 2.7892 1.173 0.206 13.476 2.377 0.458 13.585 0.5194 10.01 21.85 2.9685 1.317 0.232 15.128 2.636 0.508 15.066 0.5283 10.18 20.04 3.0192 1.479 0.260 16.995 2.921 0.563 16.696 0.5447 10.49 18.65 3.1133 1.660 0.292 19.078 3.193 0.615 18.247 0.5678 10.94 17.78 3.2449 1.867 0.329 21.448 3.482 0.671 19.899 0.5803 11.18 16.67 3.3168 2.098 0.369 24.105 3.774 0.727 21.570 0.5609 10.81 14.86 3.2058 2.354 0.414 27.050 4.027 0.776 23.015 0.5401 10.40 13.41 3.0869 2.642 0.465 30.354 4.226 0.814 24.152 0.5144 9.91 12.17 2.9398 2.967 0.522 34.088 4.466 0.860 25.527 0.4708 9.07 10.54 2.6906 3.335 0.587 38.326 4.697 0.905 26.846 0.4092 7.88 8.71 2.3385 3.742 0.659 42.994 4.875 0.939 27.862 0.3421 6.59 7.02 1.9553 4.204 0.740 48.308 4.979 0.959 28.457 0.2766 5.33 5.56 1.5808 4.717 0.830 54.198 5.048 0.972 28.850 0.2183 4.20 4.32 1.2474 5.298 0.933 60.877 5.111 0.985 29.209 0.1682 3.24 3.29 0.9612 5.879 1.035 67.556 5.197 1.001 29.700 0.1408 2.71 2.71 0.8046 6.454 1.136 74.163 5.171 0.996 29.553 0.1295 2.49 2.50 0.7399 7.035 1.238 80.842 5.169 0.996 29.542 0.1223 2.36 2.37 0.6991 7.617 1.341 87.522 5.186 0.999 29.636 0.1202 2.32 2.32 0.6871 10.267 1.807 117.973 5.210 1.004 29.776 0.1128 2.17 2.17 0.6448 12.917 2.274 148.424 5.226 1.007 29.866 0.1135 2.19 2.17 0.6489 15.567 2.740 178.876 5.195 1.001 29.688 0.1130 2.18 2.17 0.6456 18.217 3.207 209.327 5.177 0.997 29.588 0.1140 2.20 2.20 0.6517 RUN NUMBER 1W01108 AXIAL POSITION = 395.0 MM SPAN POSITION = 0.0 MM FREE-STREAM VELOCITY = 5.20 M/S FRICTION VELOCITY = 0.1683 M/S FREE-STREAM TURBULENCE = 2.001 % X-REYNOLDS NUMBER = 13.48 X10**4 FLUID DENSITY = 1.188 KG/M**3 KINEMATIC VISCOSITY = 1.523 X10(-5)MSQ/S BOUNDARY LAYER THICKNESS (99.0%) = 6.86 MM DISPLACEMENT THICKNESS = 1.820 MM MOMENTUM THICKNESS = 0.798 MM ENERGY THICKNESS = 1.297 MM FORM FACTOR H = 2.281 FORM FACTOR E = 1.626 RDELTASTAR = 621.2 RTHETA = 272.3 SKIN FRICTION COEFFICIENT = 0.002098 CALCULATED CF = 0.001808 Y Y/DEL YPLUS U U/UO UPLUS u u/UO u/U u/UTAU MM M/S M/S % % 0.279 0.041 3.085 0.539 0.104 3.201 0.1493 2.87 27.72 0.8872 0.317 0.046 3.499 0.601 0.116 3.573 0.1980 3.81 32.92 1.1761 0.354 0.052 3.914 0.666 0.128 3.955 0.1978 3.81 29.72 1.1753 0.398 0.058 4.398 0.742 0.143 4.407 0.2277 4.38 30.69 1.3524 0.448 0.065 4.950 0.839 0.161 4.985 0.2705 5.20 32.23 1.6067 0.510 0.074 5.641 0.940 0.181 5.582 0.2951 5.68 31.41 1.7530 0.573 0.083 6.332 1.074 0.207 6.379 0.3391 6.52 31.58 2.0142 0.648 0.094 7.162 1.187 0.228 7.052 0.3536 6.80 29.79 2.1009 0.729 0.106 8.060 1.391 0.268 8.261 0.4204 8.09 30.23 2.4976 0.823 0.120 9.096 1.542 0.297 9.162 0.4490 8.64 29.11 2.6673 0.929 0.135 10.271 1.754 0.337 10.418 0.4870 9.37 27.77 2.8932 1.048 0.153 11.584 1.897 0.365 11.271 0.5209 10.02 27.46 3.0947 1.179 0.172 13.035 2.171 0.418 12.899 0.5690 10.95 26.20 3.3801 1.329 0.194 14.693 2.454 0.472 14.577 0.6000 11.54 24.45 3.5642 1.498 0.218 16.559 2.741 0.527 16.284 0.6277 12.08 22.90 3.7290 1.685 0.246 18.632 2.989 0.575 17.755 0.6304 12.13 21.09 3.7453 1.904 0.277 21.051 3.238 0.623 19.238 0.6581 12.66 20.32 3.9094 2.142 0.312 23.676 3.493 0.672 20.748 0.6403 12.32 18.33 3.8039 2.417 0.352 26.717 3.728 0.717 22.150 0.6445 12.40 17.29 3.8290 2.723 0.397 30.103 3.969 0.764 23.577 0.6102 11.74 15.37 3.6249 3.073 0.448 33.972 4.270 0.822 25.366 0.5487 10.56 12.85 3.2594 3.460 0.504 38.257 4.476 0.861 26.590 0.5129 9.87 11.46 3.0471 3.904 0.569 43.163 4.691 0.903 27.870 0.4531 8.72 9.66 2.6916 4.398 0.641 48.621 4.856 0.934 28.849 0.3771 7.26 7.77 2.2402 4.954 0.722 54.771 4.972 0.957 29.537 0.3110 5.98 6.26 1.8477 5.585 0.814 61.750 5.047 0.971 29.980 0.2425 4.66 4.80 1.4404 6.298 0.918 69.628 5.088 0.979 30.224 0.1902 3.66 3.74 1.1300 7.004 1.020 77.436 5.156 0.992 30.630 0.1493 2.87 2.90 0.8872 7.717 1.124 85.314 5.218 1.004 30.997 0.1334 2.57 2.56 0.7923 8.429 1.228 93.191 5.215 1.003 30.982 0.1172 2.25 2.25 0.6962 9.135 1.331 100.999 5.187 0.998 30.814 0.1123 2.16 2.17 0.6674 12.285 1.790 135.826 5.171 0.995 30.722 0.1040 2.00 2.01 0.6181 15.435 2.249 170.652 5.183 0.997 30.789 0.1041 2.00 2.01 0.6182 18.585 2.708 205.478 5.209 1.002 30.943 0.1031 1.98 1.98 0.6127 21.735 3.167 240.305 5.241 1.008 31.138 0.1040 2.00 1.98 0.6177 RUN NUMBER 1W01109 AXIAL POSITION = 495.0 MM SPAN POSITION = 0.0 MM FREE-STREAM VELOCITY = 5.20 M/S FRICTION VELOCITY = 0.1729 M/S FREE-STREAM TURBULENCE = 1.882 % X-REYNOLDS NUMBER = 16.92 X10**4 FLUID DENSITY = 1.188 KG/M**3 KINEMATIC VISCOSITY = 1.522 X10(-5)MSQ/S BOUNDARY LAYER THICKNESS (99.0%) = 8.11 MM DISPLACEMENT THICKNESS = 2.002 MM MOMENTUM THICKNESS = 0.944 MM ENERGY THICKNESS = 1.555 MM FORM FACTOR H = 2.120 FORM FACTOR E = 1.646 RDELTASTAR = 684.3 RTHETA = 322.8 SKIN FRICTION COEFFICIENT = 0.002209 CALCULATED CF = 0.001614 Y Y/DEL YPLUS U U/UO UPLUS u u/UO u/U u/UTAU MM M/S M/S % % 0.273 0.034 3.098 0.571 0.110 3.302 0.2400 4.61 42.03 1.3878 0.310 0.038 3.524 0.640 0.123 3.701 0.2785 5.35 43.51 1.6105 0.354 0.044 4.021 0.723 0.139 4.182 0.3248 6.24 44.92 1.8786 0.404 0.050 4.588 0.805 0.155 4.658 0.3730 7.17 46.30 2.1569 0.460 0.057 5.227 0.919 0.177 5.318 0.4049 7.78 44.04 2.3416 0.517 0.064 5.866 1.025 0.197 5.928 0.4637 8.91 45.23 2.6816 0.592 0.073 6.718 1.186 0.228 6.861 0.5133 9.87 43.26 2.9684 0.667 0.082 7.570 1.250 0.240 7.228 0.5076 9.76 40.61 2.9356 0.760 0.094 8.635 1.462 0.281 8.455 0.5797 11.14 39.65 3.3524 0.860 0.106 9.770 1.642 0.316 9.495 0.5866 11.27 35.73 3.3924 0.979 0.121 11.119 1.903 0.366 11.007 0.6186 11.89 32.50 3.5772 1.110 0.137 12.610 2.107 0.405 12.187 0.6646 12.77 31.54 3.8434 1.254 0.155 14.242 2.311 0.444 13.368 0.6820 13.11 29.51 3.9442 1.423 0.176 16.159 2.578 0.496 14.910 0.6853 13.17 26.58 3.9633 1.617 0.199 18.359 2.806 0.539 16.227 0.7103 13.65 25.32 4.1079 1.835 0.226 20.844 3.082 0.592 17.824 0.7045 13.54 22.86 4.0741 2.079 0.256 23.612 3.286 0.632 19.004 0.7014 13.48 21.34 4.0563 2.360 0.291 26.807 3.524 0.677 20.381 0.7064 13.58 20.04 4.0853 2.673 0.330 30.356 3.793 0.729 21.937 0.6719 12.91 17.71 3.8856 3.035 0.374 34.473 4.064 0.781 23.505 0.6411 12.32 15.77 3.7078 3.442 0.425 39.087 4.273 0.821 24.713 0.6100 11.72 14.28 3.5278 3.904 0.482 44.340 4.475 0.860 25.877 0.5436 10.45 12.15 3.1436 4.423 0.546 50.232 4.626 0.889 26.756 0.4739 9.11 10.24 2.7407 5.017 0.619 56.975 4.766 0.916 27.563 0.4012 7.71 8.42 2.3203 5.692 0.702 64.641 4.900 0.942 28.339 0.3364 6.47 6.87 1.9457 6.454 0.796 73.302 5.026 0.966 29.065 0.2659 5.11 5.29 1.5378 7.317 0.903 83.098 5.111 0.982 29.556 0.2199 4.23 4.30 1.2720 8.298 1.024 94.242 5.190 0.998 30.015 0.1656 3.18 3.19 0.9574 9.279 1.145 105.387 5.180 0.996 29.957 0.1378 2.65 2.66 0.7971 10.260 1.266 116.531 5.203 1.000 30.087 0.1103 2.12 2.12 0.6381 11.235 1.386 127.605 5.175 0.995 29.928 0.1089 2.09 2.11 0.6300 12.217 1.507 138.749 5.190 0.998 30.018 0.1014 1.95 1.95 0.5862 16.367 2.019 185.883 5.222 1.004 30.200 0.0972 1.87 1.86 0.5620 20.517 2.531 233.017 5.222 1.004 30.200 0.0973 1.87 1.86 0.5626 24.667 3.043 280.151 5.222 1.004 30.200 0.0973 1.87 1.86 0.5630 28.817 3.555 327.285 5.222 1.004 30.200 0.0979 1.88 1.87 0.5662 RUN NUMBER 1W01110 AXIAL POSITION = 595.0 MM SPAN POSITION = 0.0 MM FREE-STREAM VELOCITY = 5.21 M/S FRICTION VELOCITY = 0.1915 M/S FREE-STREAM TURBULENCE = 1.760 % X-REYNOLDS NUMBER = 20.35 X10**4 FLUID DENSITY = 1.188 KG/M**3 KINEMATIC VISCOSITY = 1.523 X10(-5)MSQ/S BOUNDARY LAYER THICKNESS (99.0%) = 10.47 MM DISPLACEMENT THICKNESS = 2.132 MM MOMENTUM THICKNESS = 1.124 MM ENERGY THICKNESS = 1.891 MM FORM FACTOR H = 1.896 FORM FACTOR E = 1.682 RDELTASTAR = 729.1 RTHETA = 384.5 SKIN FRICTION COEFFICIENT = 0.002703 CALCULATED CF = 0.001472 Y Y/DEL YPLUS U U/UO UPLUS u u/UO u/U u/UTAU MM M/S M/S % % 0.248 0.024 3.115 0.666 0.128 3.478 0.3369 6.47 50.59 1.7596 0.279 0.027 3.508 0.733 0.141 3.827 0.3859 7.41 52.67 2.0154 0.317 0.030 3.980 0.785 0.151 4.101 0.4227 8.12 53.83 2.2076 0.360 0.034 4.530 0.884 0.170 4.617 0.4777 9.17 54.04 2.4951 0.410 0.039 5.159 1.039 0.199 5.425 0.5449 10.46 52.46 2.8457 0.467 0.045 5.866 1.159 0.222 6.052 0.6085 11.68 52.51 3.1778 0.529 0.051 6.652 1.217 0.234 6.358 0.6075 11.66 49.90 3.1726 0.604 0.058 7.595 1.421 0.273 7.422 0.6697 12.86 47.12 3.4975 0.685 0.065 8.617 1.568 0.301 8.191 0.6933 13.31 44.21 3.6208 0.779 0.074 9.796 1.790 0.344 9.347 0.7590 14.57 42.41 3.9640 0.885 0.085 11.132 1.935 0.372 10.108 0.7592 14.58 39.23 3.9652 1.004 0.096 12.625 2.157 0.414 11.264 0.7680 14.74 35.61 4.0108 1.142 0.109 14.354 2.306 0.443 12.045 0.7792 14.96 33.79 4.0696 1.298 0.124 16.319 2.510 0.482 13.107 0.7639 14.67 30.44 3.9896 1.473 0.141 18.519 2.784 0.535 14.541 0.7958 15.28 28.58 4.1562 1.673 0.160 21.034 2.939 0.564 15.348 0.7641 14.67 26.00 3.9908 1.898 0.181 23.863 3.244 0.623 16.945 0.7572 14.54 23.34 3.9545 2.154 0.206 27.086 3.430 0.659 17.914 0.7514 14.43 21.91 3.9245 2.448 0.234 30.779 3.621 0.695 18.910 0.7358 14.13 20.32 3.8431 2.779 0.265 34.945 3.800 0.730 19.847 0.6788 13.03 17.86 3.5454 3.154 0.301 39.660 4.016 0.771 20.975 0.6417 12.32 15.98 3.3516 3.579 0.342 45.004 4.164 0.799 21.746 0.6243 11.99 14.99 3.2607 4.067 0.388 51.134 4.360 0.837 22.772 0.5850 11.23 13.42 3.0552 4.610 0.440 57.972 4.555 0.874 23.788 0.5227 10.04 11.48 2.7301 5.235 0.500 65.831 4.682 0.899 24.454 0.4804 9.22 10.26 2.5090 5.948 0.568 74.790 4.840 0.929 25.276 0.4111 7.89 8.49 2.1471 6.748 0.644 84.850 4.938 0.948 25.788 0.3546 6.81 7.18 1.8522 7.660 0.731 96.324 5.015 0.963 26.191 0.2836 5.44 5.66 1.4811 8.698 0.830 109.370 5.067 0.973 26.464 0.2196 4.22 4.33 1.1471 9.735 0.929 122.416 5.122 0.983 26.749 0.1757 3.37 3.43 0.9176 10.767 1.028 135.384 5.175 0.993 27.026 0.1386 2.66 2.68 0.7241 11.804 1.127 148.430 5.211 1.000 27.215 0.1181 2.27 2.27 0.6169 12.842 1.226 161.476 5.227 1.004 27.300 0.1051 2.02 2.01 0.5491 17.192 1.641 216.175 5.220 1.002 27.261 0.0920 1.77 1.76 0.4803 21.542 2.057 270.874 5.202 0.999 27.170 0.0913 1.75 1.76 0.4770 25.892 2.472 325.574 5.201 0.998 27.162 0.0897 1.72 1.72 0.4683 30.242 2.887 380.273 5.226 1.003 27.294 0.0917 1.76 1.75 0.4789 RUN NUMBER 1W01201 AXIAL POSITION = 695.0 MM SPAN POSITION = 0.0 MM FREE-STREAM VELOCITY = 5.22 M/S FRICTION VELOCITY = 0.2274 M/S FREE-STREAM TURBULENCE = 1.647 % X-REYNOLDS NUMBER = 23.84 X10**4 FLUID DENSITY = 1.189 KG/M**3 KINEMATIC VISCOSITY = 1.521 X10(-5)MSQ/S BOUNDARY LAYER THICKNESS (99.0%) = 12.89 MM DISPLACEMENT THICKNESS = 2.230 MM MOMENTUM THICKNESS = 1.330 MM ENERGY THICKNESS = 2.287 MM FORM FACTOR H = 1.677 FORM FACTOR E = 1.719 RDELTASTAR = 765.0 RTHETA = 456.3 SKIN FRICTION COEFFICIENT = 0.003801 CALCULATED CF = 0.001360 Y Y/DEL YPLUS U U/UO UPLUS u u/UO u/U u/UTAU MM M/S M/S % % 0.210 0.016 3.144 0.770 0.148 3.385 0.3414 6.54 44.34 1.5010 0.242 0.019 3.611 0.847 0.162 3.726 0.3929 7.53 46.37 1.7275 0.273 0.021 4.078 0.949 0.182 4.171 0.4544 8.71 47.89 1.9977 0.317 0.025 4.733 1.057 0.203 4.647 0.5040 9.66 47.68 2.2160 0.360 0.028 5.387 1.197 0.230 5.265 0.5664 10.86 47.30 2.4904 0.410 0.032 6.134 1.351 0.259 5.939 0.6254 11.99 46.30 2.7495 0.473 0.037 7.069 1.491 0.286 6.555 0.6714 12.87 45.03 2.9519 0.542 0.042 8.097 1.657 0.318 7.284 0.7241 13.88 43.70 3.1836 0.617 0.048 9.219 1.884 0.361 8.285 0.7753 14.86 41.14 3.4086 0.704 0.055 10.527 2.045 0.392 8.991 0.7931 15.20 38.78 3.4868 0.804 0.062 12.022 2.279 0.437 10.018 0.8062 15.45 35.38 3.5447 0.923 0.072 13.798 2.433 0.466 10.697 0.8234 15.78 33.84 3.6200 1.054 0.082 15.760 2.599 0.498 11.427 0.8061 15.45 31.01 3.5441 1.204 0.093 18.003 2.767 0.530 12.166 0.8068 15.46 29.16 3.5470 1.373 0.106 20.527 2.976 0.570 13.084 0.7848 15.04 26.37 3.4505 1.573 0.122 23.517 3.152 0.604 13.858 0.7717 14.79 24.48 3.3930 1.798 0.139 26.882 3.310 0.635 14.555 0.7223 13.85 21.82 3.1758 2.054 0.159 30.714 3.458 0.663 15.203 0.7099 13.61 20.53 3.1214 2.342 0.182 35.013 3.652 0.700 16.056 0.6723 12.89 18.41 2.9559 2.679 0.208 40.059 3.820 0.732 16.796 0.6495 12.45 17.00 2.8555 3.060 0.237 45.760 3.926 0.753 17.261 0.6489 12.44 16.53 2.8529 3.498 0.271 52.302 4.073 0.781 17.910 0.6105 11.70 14.99 2.6840 3.998 0.310 59.778 4.241 0.813 18.648 0.5760 11.04 13.58 2.5323 4.567 0.354 68.283 4.369 0.837 19.209 0.5495 10.53 12.58 2.4160 5.217 0.405 78.003 4.496 0.862 19.766 0.5120 9.81 11.39 2.2510 5.960 0.462 89.124 4.624 0.886 20.330 0.4683 8.98 10.13 2.0592 6.810 0.528 101.834 4.766 0.914 20.954 0.4169 7.99 8.75 1.8331 7.779 0.603 116.320 4.881 0.936 21.460 0.3596 6.89 7.37 1.5809 8.885 0.689 132.861 4.993 0.957 21.954 0.2912 5.58 5.83 1.2801 10.148 0.787 151.740 5.075 0.973 22.312 0.2281 4.37 4.50 1.0030 11.598 0.900 173.422 5.142 0.986 22.606 0.1667 3.19 3.24 0.7328 13.042 1.012 195.010 5.172 0.991 22.738 0.1343 2.57 2.60 0.5904 14.492 1.124 216.692 5.192 0.995 22.828 0.1075 2.06 2.07 0.4727 15.935 1.236 238.280 5.207 0.998 22.892 0.0949 1.82 1.82 0.4174 17.379 1.348 259.869 5.208 0.998 22.897 0.0902 1.73 1.73 0.3966 23.179 1.798 346.596 5.225 1.002 22.973 0.0858 1.65 1.64 0.3774 28.979 2.248 433.324 5.237 1.004 23.025 0.0864 1.66 1.65 0.3800 34.779 2.698 520.052 5.245 1.005 23.060 0.0869 1.67 1.66 0.3822 40.579 3.148 606.779 5.251 1.007 23.088 0.0859 1.65 1.64 0.3777 RUN NUMBER 1W01202 AXIAL POSITION = 795.0 MM SPAN POSITION = 0.0 MM FREE-STREAM VELOCITY = 5.23 M/S FRICTION VELOCITY = 0.2575 M/S FREE-STREAM TURBULENCE = 1.538 % X-REYNOLDS NUMBER = 27.35 X10**4 FLUID DENSITY = 1.190 KG/M**3 KINEMATIC VISCOSITY = 1.520 X10(-5)MSQ/S BOUNDARY LAYER THICKNESS (99.0%) = 15.27 MM DISPLACEMENT THICKNESS = 2.454 MM MOMENTUM THICKNESS = 1.567 MM ENERGY THICKNESS = 2.734 MM FORM FACTOR H = 1.567 FORM FACTOR E = 1.745 RDELTASTAR = 844.3 RTHETA = 538.9 SKIN FRICTION COEFFICIENT = 0.004849 CALCULATED CF = 0.003951 LAW OF THE WALL OFFSET = 5.20 KARMAN CONSTANT = 0.410 FORM FACTOR G = 7.346 CLAUSER DELTA = 49.848 MM WAKE FACTOR PI = 0.393 1 Y Y/DEL YPLUS U U/UO UPLUS u u/UO u/U u/UTAU MM M/S M/S % % 0.192 0.013 3.244 0.766 0.147 2.977 0.2833 5.42 36.96 1.1001 0.223 0.015 3.773 0.876 0.168 3.403 0.3314 6.34 37.83 1.2873 0.254 0.017 4.302 0.959 0.183 3.726 0.3892 7.44 40.57 1.5114 0.292 0.019 4.938 1.089 0.208 4.228 0.4343 8.31 39.90 1.6868 0.335 0.022 5.679 1.219 0.233 4.733 0.4943 9.45 40.56 1.9196 0.385 0.025 6.526 1.404 0.269 5.454 0.5524 10.56 39.34 2.1456 0.442 0.029 7.478 1.582 0.302 6.143 0.6133 11.73 38.78 2.3820 0.504 0.033 8.537 1.752 0.335 6.804 0.6654 12.72 37.98 2.5841 0.579 0.038 9.807 1.975 0.378 7.670 0.7058 13.50 35.74 2.7411 0.660 0.043 11.184 2.172 0.415 8.437 0.7318 14.00 33.69 2.8422 0.760 0.050 12.877 2.372 0.454 9.211 0.7373 14.10 31.09 2.8634 0.873 0.057 14.783 2.562 0.490 9.951 0.7448 14.24 29.07 2.8927 0.998 0.065 16.900 2.780 0.532 10.797 0.7365 14.08 26.49 2.8604 1.142 0.075 19.335 2.939 0.562 11.413 0.7360 14.08 25.05 2.8587 1.310 0.086 22.193 3.089 0.591 11.998 0.7131 13.64 23.09 2.7697 1.504 0.099 25.475 3.239 0.619 12.578 0.6982 13.35 21.56 2.7119 1.723 0.113 29.181 3.360 0.643 13.050 0.6834 13.07 20.34 2.6543 1.973 0.129 33.415 3.504 0.670 13.611 0.6472 12.38 18.47 2.5135 2.260 0.148 38.285 3.627 0.694 14.088 0.6313 12.07 17.41 2.4520 2.592 0.170 43.896 3.755 0.718 14.585 0.6024 11.52 16.04 2.3395 2.973 0.195 50.353 3.898 0.745 15.139 0.5778 11.05 14.82 2.2439 3.404 0.223 57.658 4.013 0.767 15.585 0.5473 10.47 13.64 2.1257 3.904 0.256 66.127 4.105 0.785 15.944 0.5358 10.25 13.05 2.0808 4.473 0.293 75.761 4.220 0.807 16.391 0.5178 9.90 12.27 2.0109 5.123 0.336 86.771 4.361 0.834 16.939 0.4985 9.53 11.43 1.9360 5.873 0.385 99.475 4.477 0.856 17.388 0.4621 8.84 10.32 1.7947 6.729 0.441 113.978 4.611 0.882 17.907 0.4318 8.26 9.37 1.6772 7.710 0.505 130.599 4.719 0.902 18.327 0.3970 7.59 8.41 1.5417 8.835 0.579 149.655 4.848 0.927 18.828 0.3512 6.72 7.25 1.3642 10.123 0.663 171.463 4.960 0.949 19.265 0.2959 5.66 5.97 1.1493 11.604 0.760 196.553 5.057 0.967 19.640 0.2314 4.42 4.57 0.8985 13.298 0.871 225.242 5.136 0.982 19.946 0.1728 3.30 3.36 0.6711 14.992 0.982 253.931 5.174 0.989 20.095 0.1306 2.50 2.52 0.5073 16.685 1.093 282.621 5.202 0.995 20.204 0.1035 1.98 1.99 0.4018 18.379 1.204 311.310 5.214 0.997 20.250 0.0908 1.74 1.74 0.3527 20.073 1.315 339.999 5.217 0.998 20.260 0.0863 1.65 1.65 0.3350 26.723 1.750 452.639 5.226 0.999 20.296 0.0817 1.56 1.56 0.3174 33.373 2.186 565.279 5.239 1.002 20.347 0.0814 1.56 1.55 0.3162 40.023 2.621 677.919 5.247 1.003 20.378 0.0800 1.53 1.53 0.3109 46.673 3.057 790.560 5.259 1.006 20.424 0.0804 1.54 1.53 0.3123 RUN NUMBER 1W01203 AXIAL POSITION = 895.0 MM SPAN POSITION = 0.0 MM FREE-STREAM VELOCITY = 5.25 M/S FRICTION VELOCITY = 0.2587 M/S FREE-STREAM TURBULENCE = 1.451 % X-REYNOLDS NUMBER = 30.93 X10**4 FLUID DENSITY = 1.191 KG/M**3 KINEMATIC VISCOSITY = 1.519 X10(-5)MSQ/S BOUNDARY LAYER THICKNESS (99.0%) = 17.65 MM DISPLACEMENT THICKNESS = 2.740 MM MOMENTUM THICKNESS = 1.816 MM ENERGY THICKNESS = 3.186 MM FORM FACTOR H = 1.509 FORM FACTOR E = 1.755 RDELTASTAR = 946.6 RTHETA = 627.5 SKIN FRICTION COEFFICIENT = 0.004861 CALCULATED CF = 0.004153 LAW OF THE WALL OFFSET = 5.20 KARMAN CONSTANT = 0.410 FORM FACTOR G = 6.839 CLAUSER DELTA = 55.568 MM WAKE FACTOR PI = 0.187 1 Y Y/DEL YPLUS U U/UO UPLUS u u/UO u/U u/UTAU MM M/S M/S % % 0.179 0.010 3.049 0.800 0.152 3.093 0.2735 5.21 34.18 1.0572 0.204 0.012 3.475 0.874 0.167 3.380 0.3103 5.91 35.49 1.1993 0.235 0.013 4.008 0.982 0.187 3.794 0.3571 6.80 36.38 1.3803 0.273 0.015 4.646 1.096 0.209 4.237 0.4106 7.82 37.46 1.5870 0.317 0.018 5.392 1.258 0.240 4.861 0.4767 9.08 37.90 1.8425 0.367 0.021 6.244 1.445 0.275 5.586 0.5280 10.06 36.53 2.0408 0.417 0.024 7.095 1.591 0.303 6.151 0.5723 10.91 35.96 2.2120 0.485 0.027 8.267 1.800 0.343 6.958 0.6298 12.00 34.98 2.4342 0.554 0.031 9.438 2.009 0.383 7.767 0.6646 12.66 33.07 2.5687 0.642 0.036 10.928 2.207 0.421 8.532 0.6776 12.91 30.70 2.6190 0.742 0.042 12.632 2.411 0.459 9.320 0.7030 13.40 29.16 2.7173 0.854 0.048 14.548 2.600 0.495 10.048 0.7023 13.38 27.02 2.7146 0.979 0.055 16.678 2.822 0.538 10.907 0.6953 13.25 24.64 2.6874 1.129 0.064 19.233 2.989 0.570 11.553 0.6902 13.15 23.09 2.6676 1.304 0.074 22.215 3.161 0.602 12.216 0.6623 12.62 20.95 2.5598 1.498 0.085 25.515 3.280 0.625 12.678 0.6438 12.27 19.63 2.4884 1.729 0.098 29.455 3.413 0.650 13.191 0.6148 11.72 18.01 2.3763 1.985 0.112 33.820 3.549 0.676 13.718 0.5864 11.17 16.52 2.2665 2.292 0.130 39.037 3.649 0.695 14.104 0.5597 10.67 15.34 2.1635 2.635 0.149 44.893 3.753 0.715 14.506 0.5408 10.31 14.41 2.0903 3.035 0.172 51.708 3.851 0.734 14.887 0.5267 10.04 13.67 2.0356 3.498 0.198 59.587 3.933 0.749 15.200 0.5015 9.56 12.75 1.9383 4.029 0.228 68.637 4.053 0.772 15.664 0.4892 9.32 12.07 1.8910 4.635 0.263 78.965 4.164 0.793 16.093 0.4764 9.08 11.44 1.8414 5.342 0.303 90.996 4.264 0.813 16.482 0.4546 8.66 10.66 1.7573 6.148 0.348 104.731 4.406 0.840 17.029 0.4357 8.30 9.89 1.6839 7.079 0.401 120.596 4.506 0.859 17.415 0.4211 8.02 9.35 1.6275 8.148 0.462 138.803 4.634 0.883 17.911 0.3941 7.51 8.51 1.5234 9.385 0.532 159.884 4.767 0.908 18.424 0.3596 6.85 7.54 1.3898 10.804 0.612 184.054 4.900 0.934 18.940 0.3121 5.95 6.37 1.2062 12.442 0.705 211.949 5.025 0.958 19.422 0.2535 4.83 5.04 0.9797 14.329 0.812 244.104 5.106 0.973 19.734 0.2007 3.82 3.93 0.7758 16.498 0.934 281.050 5.190 0.989 20.060 0.1357 2.59 2.61 0.5244 18.667 1.057 317.997 5.220 0.995 20.177 0.1007 1.92 1.93 0.3892 20.835 1.180 354.943 5.228 0.996 20.208 0.0880 1.68 1.68 0.3401 23.004 1.303 391.889 5.229 0.996 20.209 0.0808 1.54 1.55 0.3124 25.173 1.426 428.835 5.237 0.998 20.244 0.0787 1.50 1.50 0.3041 33.423 1.893 569.379 5.250 1.000 20.290 0.0774 1.47 1.47 0.2992 41.673 2.360 709.924 5.263 1.003 20.341 0.0768 1.46 1.46 0.2967 49.923 2.828 850.468 5.273 1.005 20.382 0.0764 1.46 1.45 0.2952 58.173 3.295 991.013 5.283 1.007 20.419 0.0761 1.45 1.44 0.2942 RUN NUMBER 1W01204 AXIAL POSITION = 995.0 MM SPAN POSITION = 0.0 MM FREE-STREAM VELOCITY = 5.26 M/S FRICTION VELOCITY = 0.2555 M/S FREE-STREAM TURBULENCE = 1.361 % X-REYNOLDS NUMBER = 34.47 X10**4 FLUID DENSITY = 1.192 KG/M**3 KINEMATIC VISCOSITY = 1.518 X10(-5)MSQ/S BOUNDARY LAYER THICKNESS (99.0%) = 19.66 MM DISPLACEMENT THICKNESS = 3.054 MM MOMENTUM THICKNESS = 2.051 MM ENERGY THICKNESS = 3.604 MM FORM FACTOR H = 1.489 FORM FACTOR E = 1.757 RDELTASTAR = 1058.1 RTHETA = 710.5 SKIN FRICTION COEFFICIENT = 0.004722 CALCULATED CF = 0.004140 LAW OF THE WALL OFFSET = 5.20 KARMAN CONSTANT = 0.410 FORM FACTOR G = 6.761 CLAUSER DELTA = 62.861 MM WAKE FACTOR PI = 0.156 1 Y Y/DEL YPLUS U U/UO UPLUS u u/UO u/U u/UTAU MM M/S M/S % % 0.179 0.009 3.013 0.764 0.145 2.990 0.2438 4.64 31.91 0.9541 0.210 0.011 3.539 0.851 0.162 3.331 0.2882 5.48 33.87 1.1281 0.242 0.012 4.065 0.958 0.182 3.748 0.3338 6.35 34.86 1.3065 0.279 0.014 4.696 1.093 0.208 4.278 0.3967 7.54 36.29 1.5525 0.323 0.016 5.432 1.240 0.236 4.851 0.4479 8.52 36.13 1.7531 0.373 0.019 6.274 1.419 0.270 5.555 0.5128 9.75 36.13 2.0071 0.429 0.022 7.221 1.610 0.306 6.301 0.5733 10.90 35.62 2.2440 0.498 0.025 8.378 1.832 0.348 7.171 0.6142 11.68 33.53 2.4041 0.573 0.029 9.640 2.029 0.386 7.941 0.6429 12.23 31.69 2.5165 0.660 0.034 11.113 2.223 0.423 8.702 0.6733 12.81 30.28 2.6354 0.760 0.039 12.796 2.472 0.470 9.674 0.6889 13.10 27.87 2.6964 0.879 0.045 14.795 2.637 0.501 10.321 0.6927 13.17 26.27 2.7113 1.017 0.052 17.109 2.827 0.538 11.065 0.6824 12.98 24.14 2.6708 1.167 0.059 19.634 2.987 0.568 11.693 0.6637 12.62 22.22 2.5976 1.348 0.069 22.685 3.140 0.597 12.291 0.6421 12.21 20.45 2.5131 1.554 0.079 26.156 3.285 0.625 12.856 0.6111 11.62 18.61 2.3920 1.792 0.091 30.154 3.411 0.649 13.352 0.5881 11.18 17.24 2.3016 2.067 0.105 34.783 3.503 0.666 13.709 0.5689 10.82 16.24 2.2265 2.385 0.121 40.148 3.627 0.690 14.197 0.5292 10.06 14.59 2.0711 2.748 0.140 46.249 3.724 0.708 14.577 0.5062 9.63 13.59 1.9811 3.173 0.161 53.403 3.823 0.727 14.964 0.4905 9.33 12.83 1.9198 3.654 0.186 61.503 3.919 0.745 15.338 0.4677 8.89 11.93 1.8305 4.217 0.214 70.971 4.002 0.761 15.666 0.4527 8.61 11.31 1.7718 4.860 0.247 81.806 4.109 0.781 16.082 0.4385 8.34 10.67 1.7162 5.604 0.285 94.325 4.215 0.802 16.497 0.4247 8.08 10.07 1.6621 6.460 0.329 108.737 4.327 0.823 16.937 0.4142 7.88 9.57 1.6211 7.448 0.379 125.358 4.438 0.844 17.369 0.4005 7.62 9.03 1.5677 8.592 0.437 144.610 4.576 0.870 17.912 0.3777 7.18 8.25 1.4783 9.904 0.504 166.701 4.701 0.894 18.399 0.3488 6.63 7.42 1.3651 11.417 0.581 192.159 4.844 0.921 18.961 0.3121 5.94 6.44 1.2215 13.160 0.669 221.510 4.963 0.944 19.424 0.2747 5.22 5.53 1.0750 15.179 0.772 255.489 5.091 0.968 19.927 0.2128 4.05 4.18 0.8330 17.498 0.890 294.517 5.179 0.985 20.270 0.1517 2.89 2.93 0.5938 19.817 1.008 333.546 5.214 0.992 20.408 0.1113 2.12 2.13 0.4356 22.142 1.126 372.679 5.235 0.996 20.489 0.0881 1.68 1.68 0.3448 24.460 1.244 411.708 5.242 0.997 20.519 0.0785 1.49 1.50 0.3072 26.779 1.362 450.737 5.246 0.998 20.533 0.0755 1.44 1.44 0.2954 35.529 1.807 598.014 5.267 1.002 20.616 0.0731 1.39 1.39 0.2862 44.279 2.252 745.292 5.279 1.004 20.662 0.0725 1.38 1.37 0.2838 53.029 2.698 892.569 5.287 1.006 20.695 0.0727 1.38 1.38 0.2847 61.779 3.143 1039.847 5.293 1.007 20.718 0.0715 1.36 1.35 0.2800 RUN NUMBER 1W01205 AXIAL POSITION = 1095.0 MM SPAN POSITION = 0.0 MM FREE-STREAM VELOCITY = 5.27 M/S FRICTION VELOCITY = 0.2515 M/S FREE-STREAM TURBULENCE = 1.295 % X-REYNOLDS NUMBER = 38.22 X10**4 FLUID DENSITY = 1.198 KG/M**3 KINEMATIC VISCOSITY = 1.510 X10(-5)MSQ/S BOUNDARY LAYER THICKNESS (99.0%) = 21.71 MM DISPLACEMENT THICKNESS = 3.370 MM MOMENTUM THICKNESS = 2.282 MM ENERGY THICKNESS = 4.013 MM FORM FACTOR H = 1.477 FORM FACTOR E = 1.759 RDELTASTAR = 1176.4 RTHETA = 796.5 SKIN FRICTION COEFFICIENT = 0.004553 CALCULATED CF = 0.004094 LAW OF THE WALL OFFSET = 5.20 KARMAN CONSTANT = 0.410 FORM FACTOR G = 6.767 CLAUSER DELTA = 70.639 MM WAKE FACTOR PI = 0.196 1 Y Y/DEL YPLUS U U/UO UPLUS u u/UO u/U u/UTAU MM M/S M/S % % 0.185 0.009 3.085 0.777 0.147 3.091 0.2558 4.85 32.90 1.0169 0.217 0.010 3.605 0.881 0.167 3.504 0.3072 5.83 34.87 1.2216 0.254 0.012 4.230 1.009 0.191 4.013 0.3639 6.90 36.06 1.4469 0.292 0.013 4.854 1.131 0.215 4.497 0.4140 7.85 36.61 1.6463 0.335 0.015 5.583 1.280 0.243 5.088 0.4678 8.88 36.56 1.8602 0.392 0.018 6.520 1.466 0.278 5.830 0.5181 9.83 35.33 2.0601 0.454 0.021 7.561 1.656 0.314 6.586 0.5690 10.79 34.35 2.2625 0.523 0.024 8.705 1.846 0.350 7.340 0.6151 11.67 33.32 2.4459 0.604 0.028 10.059 2.062 0.391 8.199 0.6461 12.26 31.33 2.5691 0.704 0.032 11.724 2.284 0.433 9.083 0.6589 12.50 28.84 2.6198 0.810 0.037 13.493 2.491 0.473 9.905 0.6798 12.90 27.29 2.7031 0.942 0.043 15.679 2.695 0.511 10.716 0.6704 12.72 24.87 2.6655 1.085 0.050 18.073 2.863 0.543 11.383 0.6598 12.52 23.05 2.6233 1.254 0.058 20.883 3.033 0.575 12.060 0.6438 12.21 21.23 2.5599 1.454 0.067 24.214 3.172 0.602 12.611 0.6240 11.84 19.67 2.4811 1.679 0.077 27.961 3.303 0.627 13.132 0.5896 11.18 17.85 2.3442 1.942 0.089 32.332 3.423 0.649 13.611 0.5641 10.70 16.48 2.2431 2.248 0.104 37.432 3.513 0.667 13.970 0.5365 10.18 15.27 2.1332 2.598 0.120 43.261 3.609 0.685 14.349 0.5108 9.69 14.15 2.0311 3.004 0.138 50.026 3.709 0.704 14.748 0.4804 9.11 12.95 1.9100 3.473 0.160 57.832 3.818 0.724 15.181 0.4573 8.67 11.98 1.8182 4.010 0.185 66.784 3.914 0.742 15.561 0.4447 8.44 11.36 1.7682 4.642 0.214 77.296 4.002 0.759 15.913 0.4284 8.13 10.70 1.7032 5.367 0.247 89.370 4.110 0.780 16.341 0.4113 7.80 10.01 1.6352 6.204 0.286 103.317 4.222 0.801 16.789 0.4000 7.59 9.47 1.5906 7.173 0.330 119.449 4.326 0.821 17.202 0.3909 7.42 9.04 1.5543 8.292 0.382 138.080 4.448 0.844 17.684 0.3790 7.19 8.52 1.5069 9.585 0.441 159.625 4.578 0.868 18.203 0.3557 6.75 7.77 1.4142 11.079 0.510 184.501 4.727 0.897 18.795 0.3267 6.20 6.91 1.2988 12.810 0.590 213.332 4.860 0.922 19.324 0.3027 5.74 6.23 1.2035 14.810 0.682 246.638 5.003 0.949 19.892 0.2532 4.80 5.06 1.0067 17.123 0.789 285.149 5.114 0.970 20.336 0.1998 3.79 3.91 0.7943 19.798 0.912 329.696 5.197 0.986 20.663 0.1390 2.64 2.67 0.5527 22.473 1.035 374.244 5.237 0.994 20.825 0.1023 1.94 1.95 0.4068 25.142 1.158 418.687 5.256 0.997 20.901 0.0817 1.55 1.56 0.3250 27.817 1.281 463.234 5.256 0.997 20.900 0.0741 1.41 1.41 0.2946 30.492 1.404 507.782 5.258 0.997 20.906 0.0713 1.35 1.36 0.2833 40.392 1.860 672.649 5.277 1.001 20.982 0.0695 1.32 1.32 0.2764 50.292 2.316 837.516 5.288 1.003 21.028 0.0692 1.31 1.31 0.2752 60.192 2.772 1002.383 5.297 1.005 21.063 0.0688 1.31 1.30 0.2737 70.092 3.228 1167.250 5.299 1.005 21.070 0.0683 1.30 1.29 0.2714 RUN NUMBER 1W01206 AXIAL POSITION = 1195.0 MM SPAN POSITION = 0.0 MM FREE-STREAM VELOCITY = 5.29 M/S FRICTION VELOCITY = 0.2488 M/S FREE-STREAM TURBULENCE = 1.227 % X-REYNOLDS NUMBER = 41.89 X10**4 FLUID DENSITY = 1.198 KG/M**3 KINEMATIC VISCOSITY = 1.510 X10(-5)MSQ/S BOUNDARY LAYER THICKNESS (99.0%) = 24.14 MM DISPLACEMENT THICKNESS = 3.751 MM MOMENTUM THICKNESS = 2.559 MM ENERGY THICKNESS = 4.502 MM FORM FACTOR H = 1.466 FORM FACTOR E = 1.759 RDELTASTAR = 1314.8 RTHETA = 897.0 SKIN FRICTION COEFFICIENT = 0.004418 CALCULATED CF = 0.004035 LAW OF THE WALL OFFSET = 5.20 KARMAN CONSTANT = 0.410 FORM FACTOR G = 6.760 CLAUSER DELTA = 79.801 MM WAKE FACTOR PI = 0.189 1 Y Y/DEL YPLUS U U/UO UPLUS u u/UO u/U u/UTAU MM M/S M/S % % 0.192 0.008 3.155 0.774 0.146 3.112 0.2578 4.87 33.30 1.0365 0.223 0.009 3.670 0.864 0.163 3.474 0.2990 5.65 34.60 1.2018 0.260 0.011 4.288 0.981 0.185 3.943 0.3503 6.62 35.71 1.4080 0.304 0.013 5.009 1.140 0.215 4.583 0.4074 7.70 35.73 1.6377 0.348 0.014 5.730 1.283 0.242 5.157 0.4571 8.64 35.63 1.8373 0.404 0.017 6.656 1.468 0.277 5.899 0.5140 9.71 35.03 2.0664 0.473 0.020 7.789 1.675 0.317 6.734 0.5840 11.03 34.86 2.3475 0.548 0.023 9.025 1.877 0.355 7.546 0.6125 11.57 32.63 2.4623 0.635 0.026 10.466 2.115 0.400 8.502 0.6460 12.21 30.54 2.5969 0.735 0.030 12.114 2.309 0.436 9.280 0.6674 12.61 28.91 2.6828 0.854 0.035 14.071 2.507 0.474 10.076 0.6779 12.81 27.04 2.7249 0.992 0.041 16.336 2.691 0.508 10.816 0.6589 12.45 24.49 2.6487 1.148 0.048 18.910 2.863 0.541 11.509 0.6527 12.33 22.80 2.6238 1.329 0.055 21.897 3.036 0.574 12.204 0.6230 11.77 20.52 2.5042 1.542 0.064 25.398 3.176 0.600 12.768 0.6097 11.52 19.20 2.4510 1.785 0.074 29.414 3.293 0.622 13.239 0.5816 10.99 17.66 2.3380 2.067 0.086 34.048 3.422 0.646 13.754 0.5538 10.46 16.18 2.2260 2.392 0.099 39.402 3.503 0.662 14.082 0.5131 9.69 14.65 2.0627 2.773 0.115 45.684 3.620 0.684 14.552 0.4887 9.23 13.50 1.9644 3.217 0.133 52.995 3.709 0.701 14.908 0.4808 9.08 12.97 1.9329 3.723 0.154 61.336 3.803 0.719 15.289 0.4550 8.60 11.96 1.8292 4.317 0.179 71.119 3.892 0.735 15.647 0.4334 8.19 11.13 1.7421 5.004 0.207 82.446 3.988 0.753 16.030 0.4216 7.97 10.57 1.6947 5.792 0.240 95.421 4.082 0.771 16.409 0.4085 7.72 10.01 1.6421 6.717 0.278 110.661 4.190 0.792 16.844 0.3988 7.53 9.52 1.6031 7.779 0.322 128.167 4.305 0.813 17.305 0.3839 7.25 8.92 1.5432 9.010 0.373 148.453 4.447 0.840 17.876 0.3584 6.77 8.06 1.4405 10.442 0.433 172.035 4.580 0.865 18.411 0.3432 6.48 7.49 1.3795 12.098 0.501 199.323 4.720 0.892 18.972 0.3240 6.12 6.87 1.3025 14.017 0.581 230.937 4.855 0.917 19.517 0.2914 5.51 6.00 1.1713 16.242 0.673 267.596 4.999 0.944 20.093 0.2481 4.69 4.96 0.9974 18.817 0.780 310.022 5.123 0.968 20.594 0.1908 3.60 3.72 0.7669 21.798 0.903 359.141 5.215 0.985 20.962 0.1280 2.42 2.45 0.5145 24.779 1.027 408.260 5.259 0.994 21.139 0.0907 1.71 1.72 0.3646 27.767 1.150 457.482 5.276 0.997 21.210 0.0755 1.43 1.43 0.3035 30.748 1.274 506.601 5.285 0.999 21.245 0.0706 1.33 1.34 0.2837 33.729 1.397 555.721 5.288 0.999 21.257 0.0683 1.29 1.29 0.2745 44.629 1.849 735.310 5.305 1.002 21.326 0.0663 1.25 1.25 0.2665 55.529 2.301 914.899 5.309 1.003 21.341 0.0657 1.24 1.24 0.2640 66.429 2.752 1094.488 5.312 1.004 21.353 0.0659 1.25 1.24 0.2651 77.329 3.204 1274.077 5.308 1.003 21.338 0.0649 1.23 1.22 0.2610 RUN NUMBER 1W01207 AXIAL POSITION = 1295.0 MM SPAN POSITION = 0.0 MM FREE-STREAM VELOCITY = 5.30 M/S FRICTION VELOCITY = 0.2454 M/S FREE-STREAM TURBULENCE = 1.206 % X-REYNOLDS NUMBER = 45.48 X10**4 FLUID DENSITY = 1.199 KG/M**3 KINEMATIC VISCOSITY = 1.508 X10(-5)MSQ/S BOUNDARY LAYER THICKNESS (99.0%) = 26.20 MM DISPLACEMENT THICKNESS = 4.079 MM MOMENTUM THICKNESS = 2.791 MM ENERGY THICKNESS = 4.909 MM FORM FACTOR H = 1.461 FORM FACTOR E = 1.759 RDELTASTAR = 1432.5 RTHETA = 980.2 SKIN FRICTION COEFFICIENT = 0.004292 CALCULATED CF = 0.003966 LAW OF THE WALL OFFSET = 5.20 KARMAN CONSTANT = 0.410 FORM FACTOR G = 6.816 CLAUSER DELTA = 88.057 MM WAKE FACTOR PI = 0.225 1 Y Y/DEL YPLUS U U/UO UPLUS u u/UO u/U u/UTAU MM M/S M/S % % 0.198 0.008 3.217 0.775 0.146 3.157 0.2579 4.87 33.30 1.0511 0.229 0.009 3.725 0.872 0.165 3.554 0.3052 5.76 35.00 1.2437 0.267 0.010 4.335 0.978 0.185 3.985 0.3496 6.60 35.75 1.4248 0.310 0.012 5.047 1.120 0.211 4.565 0.4060 7.66 36.24 1.6546 0.360 0.014 5.860 1.276 0.241 5.199 0.4561 8.61 35.75 1.8586 0.417 0.016 6.775 1.464 0.276 5.968 0.5233 9.88 35.74 2.1328 0.485 0.019 7.894 1.664 0.314 6.781 0.5686 10.73 34.17 2.3173 0.560 0.021 9.114 1.847 0.349 7.527 0.6057 11.43 32.79 2.4683 0.654 0.025 10.639 2.086 0.394 8.501 0.6395 12.07 30.66 2.6062 0.760 0.029 12.367 2.292 0.433 9.342 0.6543 12.35 28.54 2.6663 0.879 0.034 14.299 2.495 0.471 10.169 0.6647 12.55 26.64 2.7087 1.023 0.039 16.638 2.698 0.509 10.996 0.6630 12.52 24.57 2.7019 1.185 0.045 19.281 2.846 0.537 11.597 0.6428 12.14 22.59 2.6196 1.379 0.053 22.433 3.010 0.568 12.267 0.6194 11.69 20.58 2.5241 1.598 0.061 25.991 3.137 0.592 12.783 0.5925 11.19 18.89 2.4148 1.854 0.071 30.160 3.301 0.623 13.454 0.5637 10.64 17.08 2.2974 2.154 0.082 35.040 3.399 0.642 13.852 0.5400 10.19 15.89 2.2006 2.498 0.095 40.632 3.479 0.657 14.180 0.5079 9.59 14.60 2.0699 2.898 0.111 47.139 3.572 0.674 14.556 0.4920 9.29 13.78 2.0051 3.360 0.128 54.663 3.686 0.696 15.022 0.4649 8.78 12.61 1.8944 3.898 0.149 63.407 3.753 0.708 15.293 0.4500 8.50 11.99 1.8338 4.523 0.173 73.574 3.873 0.731 15.785 0.4283 8.09 11.06 1.7455 5.248 0.200 85.368 3.961 0.748 16.140 0.4095 7.73 10.34 1.6688 6.092 0.232 99.094 4.053 0.765 16.518 0.4030 7.61 9.94 1.6423 7.067 0.270 114.955 4.167 0.787 16.983 0.3922 7.40 9.41 1.5983 8.198 0.313 133.357 4.286 0.809 17.466 0.3806 7.19 8.88 1.5511 9.510 0.363 154.708 4.416 0.834 17.995 0.3586 6.77 8.12 1.4615 11.035 0.421 179.516 4.549 0.859 18.539 0.3451 6.51 7.59 1.4063 12.804 0.489 208.290 4.682 0.884 19.081 0.3257 6.15 6.96 1.3275 14.854 0.567 241.638 4.836 0.913 19.710 0.2893 5.46 5.98 1.1790 17.235 0.658 280.375 4.980 0.940 20.297 0.2537 4.79 5.09 1.0339 19.992 0.763 325.213 5.114 0.965 20.841 0.1945 3.67 3.80 0.7927 23.198 0.885 377.371 5.208 0.983 21.225 0.1359 2.57 2.61 0.5538 26.398 1.008 429.427 5.255 0.992 21.414 0.0933 1.76 1.78 0.3803 29.604 1.130 481.585 5.279 0.997 21.513 0.0748 1.41 1.42 0.3048 32.804 1.252 533.641 5.288 0.998 21.549 0.0686 1.30 1.30 0.2796 36.004 1.374 585.697 5.291 0.999 21.562 0.0663 1.25 1.25 0.2702 46.842 1.788 761.996 5.306 1.002 21.625 0.0645 1.22 1.22 0.2628 57.679 2.201 938.296 5.314 1.003 21.657 0.0634 1.20 1.19 0.2584 68.517 2.615 1114.596 5.320 1.004 21.681 0.0628 1.19 1.18 0.2559 79.360 3.029 1290.997 5.323 1.005 21.692 0.0639 1.21 1.20 0.2604 RUN NUMBER 1W01208 AXIAL POSITION = 1395.0 MM SPAN POSITION = 0.0 MM FREE-STREAM VELOCITY = 5.30 M/S FRICTION VELOCITY = 0.2433 M/S FREE-STREAM TURBULENCE = 1.141 % X-REYNOLDS NUMBER = 49.08 X10**4 FLUID DENSITY = 1.200 KG/M**3 KINEMATIC VISCOSITY = 1.508 X10(-5)MSQ/S BOUNDARY LAYER THICKNESS (99.0%) = 27.58 MM DISPLACEMENT THICKNESS = 4.361 MM MOMENTUM THICKNESS = 2.998 MM ENERGY THICKNESS = 5.270 MM FORM FACTOR H = 1.455 FORM FACTOR E = 1.758 RDELTASTAR = 1534.5 RTHETA = 1054.6 SKIN FRICTION COEFFICIENT = 0.004207 CALCULATED CF = 0.003929 LAW OF THE WALL OFFSET = 5.20 KARMAN CONSTANT = 0.410 FORM FACTOR G = 6.818 CLAUSER DELTA = 95.102 MM WAKE FACTOR PI = 0.215 1 Y Y/DEL YPLUS U U/UO UPLUS u u/UO u/U u/UTAU MM M/S M/S % % 0.198 0.007 3.191 0.768 0.145 3.156 0.2542 4.79 33.11 1.0450 0.235 0.009 3.796 0.891 0.168 3.661 0.3119 5.88 35.03 1.2821 0.273 0.010 4.401 1.004 0.189 4.128 0.3536 6.67 35.21 1.4535 0.317 0.011 5.107 1.149 0.217 4.724 0.4149 7.82 36.10 1.7052 0.367 0.013 5.913 1.325 0.250 5.447 0.4774 9.00 36.03 1.9625 0.429 0.016 6.922 1.499 0.283 6.163 0.5314 10.02 35.44 2.1841 0.498 0.018 8.031 1.700 0.320 6.986 0.5734 10.81 33.74 2.3570 0.579 0.021 9.342 1.934 0.365 7.949 0.6145 11.58 31.78 2.5260 0.673 0.024 10.855 2.121 0.400 8.716 0.6448 12.15 30.41 2.6504 0.779 0.028 12.569 2.304 0.434 9.472 0.6487 12.23 28.15 2.6666 0.910 0.033 14.687 2.541 0.479 10.446 0.6491 12.24 25.54 2.6681 1.054 0.038 17.006 2.698 0.509 11.089 0.6541 12.33 24.25 2.6888 1.229 0.045 19.830 2.844 0.536 11.691 0.6236 11.76 21.93 2.5634 1.429 0.052 23.057 3.022 0.570 12.420 0.6093 11.49 20.16 2.5043 1.660 0.060 26.788 3.154 0.594 12.963 0.5880 11.08 18.65 2.4170 1.929 0.070 31.124 3.256 0.614 13.383 0.5545 10.45 17.03 2.2792 2.242 0.081 36.166 3.390 0.639 13.936 0.5275 9.94 15.56 2.1684 2.604 0.094 42.015 3.483 0.657 14.316 0.5114 9.64 14.68 2.1022 3.023 0.110 48.772 3.564 0.672 14.648 0.4896 9.23 13.74 2.0124 3.517 0.128 56.738 3.652 0.688 15.011 0.4601 8.67 12.60 1.8911 4.085 0.148 65.915 3.763 0.709 15.468 0.4422 8.34 11.75 1.8176 4.742 0.172 76.504 3.852 0.726 15.833 0.4243 8.00 11.02 1.7442 5.510 0.200 88.907 3.933 0.741 16.166 0.4136 7.80 10.52 1.6999 6.404 0.232 103.328 4.047 0.763 16.636 0.3935 7.42 9.72 1.6174 7.442 0.270 120.068 4.145 0.781 17.038 0.3900 7.35 9.41 1.6029 8.642 0.313 139.430 4.263 0.804 17.523 0.3801 7.17 8.92 1.5624 10.042 0.364 162.019 4.401 0.830 18.091 0.3584 6.76 8.14 1.4732 11.667 0.423 188.238 4.534 0.855 18.635 0.3409 6.43 7.52 1.4010 13.554 0.492 218.693 4.672 0.881 19.205 0.3205 6.04 6.86 1.3174 15.748 0.571 254.088 4.822 0.909 19.822 0.2908 5.48 6.03 1.1954 18.298 0.664 295.232 4.976 0.938 20.455 0.2530 4.77 5.08 1.0400 21.260 0.771 343.032 5.117 0.965 21.032 0.1978 3.73 3.87 0.8132 24.698 0.896 398.496 5.221 0.984 21.462 0.1343 2.53 2.57 0.5520 28.135 1.020 453.960 5.275 0.994 21.684 0.0904 1.70 1.71 0.3717 31.573 1.145 509.423 5.285 0.996 21.724 0.0730 1.38 1.38 0.3003 35.017 1.270 564.988 5.296 0.998 21.769 0.0658 1.24 1.24 0.2703 38.454 1.395 620.452 5.309 1.001 21.821 0.0636 1.20 1.20 0.2613 48.692 1.766 785.633 5.315 1.002 21.847 0.0621 1.17 1.17 0.2551 58.923 2.137 950.713 5.316 1.002 21.851 0.0608 1.15 1.14 0.2499 69.160 2.508 1115.894 5.319 1.003 21.864 0.0600 1.13 1.13 0.2468 79.398 2.879 1281.075 5.323 1.003 21.881 0.0605 1.14 1.14 0.2488 RUN NUMBER 1W01209 AXIAL POSITION = 1495.0 MM SPAN POSITION = 0.0 MM FREE-STREAM VELOCITY = 5.30 M/S FRICTION VELOCITY = 0.2391 M/S FREE-STREAM TURBULENCE = 1.101 % X-REYNOLDS NUMBER = 52.73 X10**4 FLUID DENSITY = 1.205 KG/M**3 KINEMATIC VISCOSITY = 1.501 X10(-5)MSQ/S BOUNDARY LAYER THICKNESS (99.0%) = 29.50 MM DISPLACEMENT THICKNESS = 4.692 MM MOMENTUM THICKNESS = 3.222 MM ENERGY THICKNESS = 5.661 MM FORM FACTOR H = 1.456 FORM FACTOR E = 1.757 RDELTASTAR = 1654.8 RTHETA = 1136.6 SKIN FRICTION COEFFICIENT = 0.004079 CALCULATED CF = 0.003845 LAW OF THE WALL OFFSET = 5.20 KARMAN CONSTANT = 0.410 FORM FACTOR G = 6.935 CLAUSER DELTA = 103.893 MM WAKE FACTOR PI = 0.282 1 Y Y/DEL YPLUS U U/UO UPLUS u u/UO u/U u/UTAU MM M/S M/S % % 0.204 0.007 3.249 0.744 0.141 3.112 0.2479 4.68 33.30 1.0365 0.235 0.008 3.747 0.839 0.159 3.510 0.2972 5.61 35.41 1.2430 0.279 0.009 4.444 0.982 0.186 4.108 0.3604 6.81 36.69 1.5070 0.323 0.011 5.141 1.117 0.211 4.673 0.4111 7.76 36.79 1.7191 0.379 0.013 6.037 1.272 0.240 5.319 0.4663 8.81 36.66 1.9499 0.442 0.015 7.032 1.460 0.276 6.104 0.5227 9.87 35.81 2.1857 0.510 0.017 8.127 1.663 0.314 6.953 0.5671 10.71 34.11 2.3716 0.598 0.020 9.521 1.873 0.354 7.832 0.6102 11.52 32.58 2.5516 0.692 0.023 11.014 2.063 0.390 8.626 0.6368 12.03 30.87 2.6629 0.804 0.027 12.806 2.297 0.434 9.605 0.6523 12.32 28.40 2.7278 0.942 0.032 14.997 2.464 0.465 10.302 0.6499 12.27 26.38 2.7177 1.092 0.037 17.386 2.693 0.509 11.262 0.6380 12.05 23.69 2.6681 1.273 0.043 20.273 2.839 0.536 11.873 0.6169 11.65 21.73 2.5796 1.479 0.050 23.558 2.993 0.565 12.515 0.6051 11.43 20.22 2.5303 1.723 0.058 27.441 3.105 0.586 12.986 0.5824 11.00 18.76 2.4356 2.004 0.068 31.920 3.227 0.609 13.494 0.5517 10.42 17.10 2.3069 2.335 0.079 37.197 3.349 0.632 14.005 0.5177 9.78 15.46 2.1649 2.717 0.092 43.269 3.437 0.649 14.372 0.4964 9.37 14.44 2.0758 3.160 0.107 50.338 3.526 0.666 14.746 0.4722 8.92 13.39 1.9747 3.673 0.124 58.501 3.607 0.681 15.082 0.4523 8.54 12.54 1.8914 4.273 0.145 68.058 3.708 0.700 15.506 0.4395 8.30 11.85 1.8380 4.973 0.169 79.208 3.816 0.721 15.957 0.4221 7.97 11.06 1.7653 5.785 0.196 92.150 3.911 0.739 16.353 0.4149 7.83 10.61 1.7349 6.735 0.228 107.282 4.021 0.759 16.815 0.3976 7.51 9.89 1.6627 7.835 0.266 124.803 4.124 0.779 17.244 0.3841 7.25 9.31 1.6061 9.117 0.309 145.211 4.238 0.800 17.723 0.3717 7.02 8.77 1.5544 10.604 0.359 168.904 4.366 0.825 18.259 0.3611 6.82 8.27 1.5102 12.335 0.418 196.480 4.508 0.851 18.850 0.3394 6.41 7.53 1.4194 14.354 0.487 228.636 4.658 0.880 19.478 0.3168 5.98 6.80 1.3249 16.698 0.566 265.968 4.801 0.907 20.076 0.2898 5.47 6.04 1.2119 19.429 0.659 309.472 4.958 0.936 20.732 0.2525 4.77 5.09 1.0560 22.604 0.766 360.045 5.099 0.963 21.322 0.1983 3.75 3.89 0.8293 26.298 0.891 418.880 5.209 0.984 21.783 0.1352 2.55 2.60 0.5653 29.992 1.017 477.716 5.260 0.993 21.998 0.0910 1.72 1.73 0.3804 33.685 1.142 536.551 5.280 0.997 22.081 0.0689 1.30 1.30 0.2879 37.379 1.267 595.387 5.290 0.999 22.120 0.0640 1.21 1.21 0.2674 41.073 1.392 654.222 5.291 0.999 22.125 0.0614 1.16 1.16 0.2566 50.629 1.716 806.438 5.307 1.002 22.193 0.0601 1.14 1.13 0.2514 60.192 2.040 958.753 5.308 1.002 22.195 0.0588 1.11 1.11 0.2459 69.748 2.364 1110.968 5.311 1.003 22.210 0.0587 1.11 1.11 0.2455 79.310 2.688 1263.283 5.314 1.004 22.224 0.0583 1.10 1.10 0.2437