ROLLS-ROYCE APPLIED SCIENCE LABORATORY FLAT PLATE TRANSITIONAL BOUNDARY LAYER FLOW HOT WIRE ANEMOMETRY TEST DATA SINGLE WIRE DATA FOR ERCOFTAC T3C3 TEST CASE RUN NUMBER 1W01907 AXIAL POSITION = 95.0 MM SPAN POSITION = 0.0 MM FREE-STREAM VELOCITY = 4.47 M/S FRICTION VELOCITY = 0.2223 M/S FREE-STREAM TURBULENCE = 2.005 % X-REYNOLDS NUMBER = 2.76 X10**4 FLUID DENSITY = 1.173 KG/M**3 KINEMATIC VISCOSITY = 1.542 X10(-5)MSQ/S BOUNDARY LAYER THICKNESS (99.0%) = 2.65 MM DISPLACEMENT THICKNESS = 0.825 MM MOMENTUM THICKNESS = 0.331 MM ENERGY THICKNESS = 0.526 MM FORM FACTOR H = 2.493 FORM FACTOR E = 1.590 RDELTASTAR = 239.3 RTHETA = 96.0 SKIN FRICTION COEFFICIENT = 0.004936 CALCULATED CF = 0.004000 Y Y/DEL YPLUS U U/UO UPLUS u u/UO u/U u/UTAU MM M/S M/S % % 0.029 0.011 0.418 0.094 0.021 0.421 0.0080 0.18 8.53 0.0359 0.035 0.013 0.508 0.114 0.025 0.512 0.0077 0.17 6.74 0.0345 0.042 0.016 0.598 0.134 0.030 0.603 0.0102 0.23 7.61 0.0459 0.048 0.018 0.688 0.154 0.034 0.694 0.0094 0.21 6.12 0.0425 0.054 0.020 0.778 0.174 0.039 0.785 0.0087 0.19 4.98 0.0391 0.060 0.023 0.868 0.195 0.043 0.875 0.0089 0.20 4.58 0.0401 0.067 0.025 0.958 0.215 0.048 0.966 0.0091 0.20 4.24 0.0410 0.073 0.027 1.048 0.235 0.053 1.057 0.0098 0.22 4.17 0.0440 0.079 0.030 1.139 0.255 0.057 1.148 0.0105 0.23 4.11 0.0471 0.085 0.032 1.229 0.275 0.062 1.239 0.0112 0.25 4.05 0.0502 0.092 0.035 1.319 0.295 0.066 1.329 0.0126 0.28 4.25 0.0565 0.098 0.037 1.409 0.316 0.071 1.420 0.0131 0.29 4.14 0.0588 0.104 0.039 1.499 0.336 0.075 1.511 0.0146 0.33 4.35 0.0657 0.110 0.042 1.589 0.356 0.080 1.602 0.0155 0.35 4.35 0.0696 0.117 0.044 1.679 0.376 0.084 1.693 0.0164 0.37 4.36 0.0738 0.129 0.049 1.859 0.417 0.093 1.874 0.0197 0.44 4.72 0.0885 0.142 0.053 2.039 0.457 0.102 2.056 0.0222 0.50 4.85 0.0997 0.160 0.061 2.310 0.517 0.116 2.328 0.0269 0.60 5.20 0.1210 0.173 0.065 2.490 0.558 0.125 2.510 0.0299 0.67 5.36 0.1346 0.192 0.072 2.760 0.618 0.138 2.782 0.0368 0.82 5.95 0.1656 0.217 0.082 3.120 0.699 0.156 3.145 0.0424 0.95 6.06 0.1906 0.235 0.089 3.390 0.753 0.168 3.388 0.0479 1.07 6.35 0.2153 0.260 0.098 3.751 0.829 0.185 3.731 0.0551 1.23 6.64 0.2479 0.292 0.110 4.201 0.919 0.205 4.134 0.0606 1.35 6.60 0.2727 0.323 0.122 4.651 1.024 0.229 4.607 0.0699 1.56 6.82 0.3143 0.354 0.134 5.102 1.123 0.251 5.054 0.0771 1.72 6.87 0.3471 0.398 0.150 5.732 1.271 0.284 5.716 0.0902 2.02 7.10 0.4060 0.435 0.165 6.273 1.394 0.312 6.273 0.0990 2.21 7.10 0.4452 0.485 0.183 6.993 1.555 0.348 6.996 0.1114 2.49 7.16 0.5011 0.535 0.202 7.714 1.714 0.383 7.713 0.1239 2.77 7.23 0.5573 0.592 0.224 8.525 1.898 0.424 8.538 0.1328 2.97 7.00 0.5973 0.654 0.247 9.425 2.081 0.465 9.363 0.1516 3.39 7.29 0.6821 0.723 0.273 10.416 2.284 0.510 10.274 0.1534 3.43 6.72 0.6902 0.804 0.304 11.587 2.503 0.559 11.262 0.1727 3.86 6.90 0.7771 0.885 0.335 12.758 2.705 0.605 12.170 0.1780 3.98 6.58 0.8007 0.985 0.372 14.199 2.926 0.654 13.164 0.1848 4.13 6.32 0.8315 1.085 0.410 15.641 3.148 0.704 14.161 0.1888 4.22 6.00 0.8493 1.204 0.455 17.352 3.377 0.755 15.193 0.1947 4.35 5.77 0.8759 1.329 0.502 19.153 3.587 0.802 16.140 0.1881 4.21 5.24 0.8465 1.473 0.557 21.225 3.803 0.850 17.108 0.1801 4.02 4.74 0.8101 1.629 0.616 23.477 3.986 0.891 17.931 0.1654 3.70 4.15 0.7440 1.804 0.682 25.999 4.146 0.927 18.653 0.1462 3.27 3.53 0.6576 1.992 0.753 28.701 4.257 0.951 19.152 0.1318 2.95 3.10 0.5928 2.204 0.833 31.764 4.344 0.971 19.543 0.1169 2.61 2.69 0.5260 2.435 0.920 35.097 4.406 0.985 19.824 0.1084 2.42 2.46 0.4875 2.698 1.020 38.880 4.441 0.993 19.982 0.1036 2.32 2.33 0.4662 2.954 1.117 42.573 4.460 0.997 20.065 0.1001 2.24 2.25 0.4505 3.217 1.216 46.356 4.468 0.999 20.101 0.0990 2.21 2.21 0.4452 3.473 1.313 50.049 4.477 1.001 20.140 0.0961 2.15 2.15 0.4325 3.729 1.410 53.742 4.482 1.002 20.163 0.0961 2.15 2.15 0.4325 5.079 1.920 73.198 4.479 1.001 20.153 0.0920 2.06 2.05 0.4139 6.429 2.430 92.654 4.488 1.003 20.191 0.0895 2.00 1.99 0.4025 7.779 2.940 112.110 4.487 1.003 20.186 0.0894 2.00 1.99 0.4020 9.129 3.451 131.566 4.486 1.003 20.182 0.0897 2.01 2.00 0.4036 RUN NUMBER 1W01908 AXIAL POSITION = 195.0 MM SPAN POSITION = 0.0 MM FREE-STREAM VELOCITY = 4.79 M/S FRICTION VELOCITY = 0.1943 M/S FREE-STREAM TURBULENCE = 1.651 % X-REYNOLDS NUMBER = 6.05 X10**4 FLUID DENSITY = 1.172 KG/M**3 KINEMATIC VISCOSITY = 1.543 X10(-5)MSQ/S BOUNDARY LAYER THICKNESS (99.0%) = 3.69 MM DISPLACEMENT THICKNESS = 1.139 MM MOMENTUM THICKNESS = 0.457 MM ENERGY THICKNESS = 0.730 MM FORM FACTOR H = 2.492 FORM FACTOR E = 1.596 RDELTASTAR = 353.2 RTHETA = 141.8 SKIN FRICTION COEFFICIENT = 0.003296 CALCULATED CF = 0.002700 Y Y/DEL YPLUS U U/UO UPLUS u u/UO u/U u/UTAU MM M/S M/S % % 0.029 0.008 0.365 0.071 0.015 0.364 0.0068 0.14 9.61 0.0350 0.035 0.010 0.444 0.086 0.018 0.442 0.0082 0.17 9.55 0.0422 0.042 0.011 0.522 0.101 0.021 0.520 0.0119 0.25 11.77 0.0612 0.048 0.013 0.601 0.116 0.024 0.599 0.0098 0.21 8.45 0.0506 0.054 0.015 0.680 0.132 0.027 0.677 0.0093 0.19 7.08 0.0480 0.060 0.016 0.758 0.147 0.031 0.756 0.0094 0.20 6.43 0.0486 0.067 0.018 0.837 0.162 0.034 0.834 0.0097 0.20 5.98 0.0499 0.073 0.020 0.916 0.177 0.037 0.912 0.0102 0.21 5.76 0.0526 0.079 0.021 0.995 0.192 0.040 0.991 0.0107 0.22 5.56 0.0551 0.085 0.023 1.073 0.208 0.043 1.069 0.0118 0.25 5.70 0.0609 0.092 0.025 1.152 0.223 0.047 1.147 0.0120 0.25 5.37 0.0616 0.098 0.027 1.231 0.238 0.050 1.226 0.0136 0.28 5.70 0.0699 0.104 0.028 1.309 0.253 0.053 1.304 0.0144 0.30 5.67 0.0740 0.117 0.032 1.467 0.284 0.059 1.461 0.0166 0.35 5.83 0.0852 0.129 0.035 1.624 0.314 0.066 1.618 0.0199 0.42 6.34 0.1025 0.142 0.038 1.781 0.345 0.072 1.774 0.0220 0.46 6.37 0.1131 0.160 0.043 2.017 0.390 0.082 2.010 0.0265 0.55 6.79 0.1365 0.179 0.049 2.253 0.436 0.091 2.245 0.0317 0.66 7.26 0.1630 0.198 0.054 2.490 0.482 0.101 2.480 0.0377 0.79 7.83 0.1941 0.217 0.059 2.726 0.527 0.110 2.715 0.0440 0.92 8.35 0.2267 0.242 0.066 3.040 0.588 0.123 3.029 0.0514 1.07 8.74 0.2648 0.273 0.074 3.434 0.654 0.137 3.368 0.0588 1.23 8.98 0.3026 0.304 0.082 3.827 0.727 0.152 3.743 0.0699 1.46 9.62 0.3600 0.335 0.091 4.221 0.805 0.168 4.143 0.0787 1.65 9.78 0.4052 0.379 0.103 4.771 0.903 0.189 4.649 0.0880 1.84 9.74 0.4529 0.417 0.113 5.243 0.997 0.208 5.133 0.0969 2.03 9.72 0.4989 0.467 0.127 5.873 1.127 0.235 5.800 0.1158 2.42 10.28 0.5960 0.523 0.142 6.581 1.277 0.267 6.575 0.1303 2.72 10.20 0.6708 0.579 0.157 7.289 1.425 0.298 7.334 0.1460 3.05 10.25 0.7517 0.648 0.176 8.155 1.604 0.335 8.257 0.1630 3.41 10.16 0.8388 0.717 0.194 9.020 1.776 0.371 9.141 0.1767 3.69 9.95 0.9097 0.798 0.216 10.043 1.982 0.414 10.199 0.1917 4.01 9.67 0.9866 0.892 0.242 11.223 2.210 0.462 11.374 0.2159 4.51 9.77 1.1112 0.992 0.269 12.482 2.439 0.510 12.555 0.2336 4.88 9.58 1.2023 1.104 0.300 13.898 2.672 0.558 13.753 0.2418 5.05 9.05 1.2447 1.229 0.333 15.472 2.927 0.612 15.067 0.2666 5.57 9.11 1.3721 1.367 0.371 17.203 3.187 0.666 16.406 0.2753 5.75 8.64 1.4170 1.523 0.413 19.170 3.437 0.718 17.692 0.2717 5.68 7.90 1.3983 1.698 0.461 21.373 3.694 0.772 19.011 0.2712 5.67 7.34 1.3959 1.892 0.513 23.812 3.949 0.825 20.327 0.2594 5.42 6.57 1.3350 2.104 0.571 26.488 4.152 0.867 21.368 0.2374 4.96 5.72 1.2219 2.342 0.635 29.478 4.333 0.905 22.302 0.2151 4.49 4.96 1.1070 2.610 0.708 32.861 4.481 0.936 23.062 0.1798 3.76 4.01 0.9257 2.904 0.788 36.559 4.598 0.961 23.668 0.1488 3.11 3.24 0.7660 3.229 0.876 40.651 4.684 0.979 24.106 0.1206 2.52 2.57 0.6207 3.598 0.976 45.293 4.738 0.990 24.385 0.1014 2.12 2.14 0.5220 3.960 1.075 49.856 4.759 0.994 24.497 0.0927 1.94 1.95 0.4773 4.329 1.175 54.499 4.781 0.999 24.607 0.0890 1.86 1.86 0.4583 4.692 1.273 59.062 4.789 1.001 24.651 0.0862 1.80 1.80 0.4434 5.060 1.373 63.705 4.787 1.000 24.638 0.0839 1.75 1.75 0.4317 6.860 1.861 86.365 4.793 1.002 24.672 0.0798 1.67 1.66 0.4107 8.660 2.350 109.026 4.794 1.002 24.674 0.0791 1.65 1.65 0.4073 10.460 2.838 131.686 4.794 1.002 24.675 0.0789 1.65 1.65 0.4060 12.260 3.327 154.347 4.789 1.001 24.651 0.0790 1.65 1.65 0.4067 RUN NUMBER 1W01909 AXIAL POSITION = 395.0 MM SPAN POSITION = 0.0 MM FREE-STREAM VELOCITY = 5.13 M/S FRICTION VELOCITY = 0.1794 M/S FREE-STREAM TURBULENCE = 1.298 % X-REYNOLDS NUMBER = 13.14 X10**4 FLUID DENSITY = 1.173 KG/M**3 KINEMATIC VISCOSITY = 1.543 X10(-5)MSQ/S BOUNDARY LAYER THICKNESS (99.0%) = 5.25 MM DISPLACEMENT THICKNESS = 1.498 MM MOMENTUM THICKNESS = 0.625 MM ENERGY THICKNESS = 1.005 MM FORM FACTOR H = 2.398 FORM FACTOR E = 1.609 RDELTASTAR = 498.3 RTHETA = 207.8 SKIN FRICTION COEFFICIENT = 0.002447 CALCULATED CF = 0.001832 Y Y/DEL YPLUS U U/UO UPLUS u u/UO u/U u/UTAU MM M/S M/S % % 0.029 0.006 0.337 0.061 0.012 0.341 0.0105 0.21 17.19 0.0586 0.035 0.007 0.410 0.074 0.015 0.415 0.0112 0.22 15.03 0.0623 0.042 0.008 0.483 0.088 0.017 0.488 0.0100 0.19 11.41 0.0557 0.048 0.009 0.555 0.101 0.020 0.562 0.0100 0.19 9.92 0.0557 0.054 0.010 0.628 0.114 0.022 0.635 0.0101 0.20 8.90 0.0565 0.060 0.011 0.701 0.127 0.025 0.709 0.0107 0.21 8.44 0.0598 0.067 0.013 0.774 0.140 0.027 0.782 0.0109 0.21 7.73 0.0605 0.073 0.014 0.846 0.154 0.030 0.856 0.0117 0.23 7.64 0.0654 0.079 0.015 0.919 0.167 0.033 0.929 0.0128 0.25 7.70 0.0716 0.085 0.016 0.992 0.180 0.035 1.003 0.0135 0.26 7.48 0.0750 0.092 0.017 1.064 0.193 0.038 1.076 0.0144 0.28 7.43 0.0800 0.104 0.020 1.210 0.220 0.043 1.223 0.0171 0.33 7.77 0.0951 0.117 0.022 1.355 0.246 0.048 1.371 0.0188 0.37 7.63 0.1046 0.129 0.025 1.501 0.272 0.053 1.518 0.0214 0.42 7.85 0.1191 0.142 0.027 1.646 0.299 0.058 1.665 0.0249 0.49 8.35 0.1390 0.160 0.031 1.864 0.338 0.066 1.885 0.0286 0.56 8.44 0.1592 0.185 0.035 2.155 0.391 0.076 2.179 0.0366 0.71 9.36 0.2040 0.204 0.039 2.373 0.431 0.084 2.400 0.0427 0.83 9.92 0.2380 0.229 0.044 2.664 0.483 0.094 2.694 0.0520 1.01 10.75 0.2897 0.260 0.050 3.027 0.549 0.107 3.062 0.0612 1.19 11.14 0.3411 0.292 0.056 3.391 0.604 0.118 3.365 0.0685 1.34 11.34 0.3817 0.329 0.063 3.827 0.675 0.132 3.762 0.0843 1.64 12.49 0.4698 0.373 0.071 4.336 0.764 0.149 4.258 0.0907 1.77 11.87 0.5055 0.417 0.079 4.845 0.850 0.166 4.736 0.1062 2.07 12.50 0.5918 0.467 0.089 5.427 0.955 0.186 5.321 0.1262 2.46 13.21 0.7031 0.529 0.101 6.154 1.092 0.213 6.083 0.1417 2.76 12.98 0.7897 0.592 0.113 6.881 1.241 0.242 6.918 0.1664 3.24 13.40 0.9274 0.667 0.127 7.753 1.397 0.272 7.787 0.1843 3.59 13.19 1.0268 0.748 0.143 8.698 1.582 0.308 8.815 0.2114 4.12 13.36 1.1779 0.842 0.160 9.789 1.770 0.345 9.865 0.2270 4.43 12.82 1.2650 0.942 0.179 10.952 2.004 0.391 11.169 0.2627 5.12 13.11 1.4638 1.060 0.202 12.334 2.235 0.436 12.456 0.2813 5.48 12.58 1.5675 1.192 0.227 13.861 2.472 0.482 13.777 0.3078 6.00 12.45 1.7152 1.335 0.255 15.533 2.724 0.531 15.181 0.3416 6.66 12.54 1.9037 1.504 0.287 17.496 3.037 0.592 16.927 0.3572 6.96 11.76 1.9909 1.685 0.321 19.604 3.299 0.643 18.383 0.3755 7.32 11.38 2.0923 1.898 0.362 22.076 3.573 0.697 19.912 0.3868 7.54 10.83 2.1557 2.129 0.406 24.766 3.855 0.752 21.485 0.3885 7.57 10.08 2.1648 2.392 0.456 27.820 4.111 0.801 22.909 0.3655 7.12 8.89 2.0368 2.685 0.512 31.237 4.343 0.847 24.202 0.3411 6.65 7.85 1.9011 3.017 0.575 35.090 4.557 0.888 25.394 0.3082 6.01 6.76 1.7175 3.392 0.647 39.453 4.736 0.923 26.391 0.2591 5.05 5.47 1.4437 3.810 0.726 44.324 4.880 0.951 27.193 0.2047 3.99 4.19 1.1405 4.279 0.816 49.777 4.984 0.972 27.776 0.1610 3.14 3.23 0.8971 4.804 0.916 55.884 5.049 0.984 28.135 0.1218 2.37 2.41 0.6789 5.398 1.029 62.791 5.098 0.994 28.409 0.0979 1.91 1.92 0.5454 5.992 1.142 69.698 5.116 0.997 28.513 0.0826 1.61 1.61 0.4604 6.579 1.254 76.532 5.129 1.000 28.583 0.0757 1.48 1.48 0.4217 7.173 1.367 83.439 5.136 1.001 28.621 0.0709 1.38 1.38 0.3951 7.767 1.481 90.346 5.136 1.001 28.621 0.0695 1.35 1.35 0.3872 10.467 1.995 121.755 5.136 1.001 28.624 0.0663 1.29 1.29 0.3692 13.167 2.510 153.164 5.136 1.001 28.620 0.0668 1.30 1.30 0.3722 15.867 3.025 184.572 5.137 1.001 28.628 0.0659 1.29 1.28 0.3674 18.567 3.539 215.981 5.143 1.003 28.659 0.0666 1.30 1.29 0.3709 RUN NUMBER 1W01910 AXIAL POSITION = 595.0 MM SPAN POSITION = 0.0 MM FREE-STREAM VELOCITY = 5.55 M/S FRICTION VELOCITY = 0.1832 M/S FREE-STREAM TURBULENCE = 1.059 % X-REYNOLDS NUMBER = 21.43 X10**4 FLUID DENSITY = 1.174 KG/M**3 KINEMATIC VISCOSITY = 1.541 X10(-5)MSQ/S BOUNDARY LAYER THICKNESS (99.0%) = 6.22 MM DISPLACEMENT THICKNESS = 1.636 MM MOMENTUM THICKNESS = 0.710 MM ENERGY THICKNESS = 1.153 MM FORM FACTOR H = 2.305 FORM FACTOR E = 1.624 RDELTASTAR = 589.1 RTHETA = 255.5 SKIN FRICTION COEFFICIENT = 0.002181 CALCULATED CF = 0.001434 Y Y/DEL YPLUS U U/UO UPLUS u u/UO u/U u/UTAU MM M/S M/S % % 0.029 0.005 0.345 0.063 0.011 0.343 0.0083 0.15 13.23 0.0454 0.035 0.006 0.419 0.076 0.014 0.417 0.0095 0.17 12.38 0.0517 0.042 0.007 0.493 0.090 0.016 0.491 0.0092 0.17 10.26 0.0504 0.048 0.008 0.568 0.104 0.019 0.565 0.0102 0.18 9.86 0.0557 0.054 0.009 0.642 0.117 0.021 0.639 0.0102 0.18 8.75 0.0559 0.060 0.010 0.716 0.131 0.024 0.713 0.0112 0.20 8.59 0.0613 0.067 0.011 0.791 0.144 0.026 0.787 0.0125 0.23 8.67 0.0682 0.073 0.012 0.865 0.158 0.028 0.861 0.0140 0.25 8.88 0.0764 0.079 0.013 0.939 0.171 0.031 0.935 0.0152 0.27 8.86 0.0829 0.085 0.014 1.014 0.185 0.033 1.009 0.0157 0.28 8.50 0.0858 0.092 0.015 1.088 0.198 0.036 1.083 0.0163 0.29 8.24 0.0892 0.104 0.017 1.237 0.226 0.041 1.231 0.0187 0.34 8.30 0.1021 0.117 0.019 1.385 0.253 0.046 1.379 0.0227 0.41 8.98 0.1238 0.135 0.022 1.608 0.293 0.053 1.601 0.0281 0.51 9.59 0.1535 0.154 0.025 1.831 0.334 0.060 1.823 0.0338 0.61 10.12 0.1844 0.173 0.028 2.054 0.375 0.068 2.044 0.0394 0.71 10.53 0.2153 0.192 0.031 2.277 0.415 0.075 2.266 0.0480 0.87 11.57 0.2622 0.223 0.036 2.649 0.483 0.087 2.636 0.0568 1.02 11.75 0.3099 0.248 0.040 2.946 0.537 0.097 2.932 0.0647 1.17 12.04 0.3529 0.279 0.045 3.318 0.605 0.109 3.302 0.0777 1.40 12.85 0.4242 0.317 0.051 3.764 0.674 0.122 3.681 0.0884 1.59 13.11 0.4826 0.354 0.057 4.209 0.752 0.136 4.107 0.1013 1.83 13.46 0.5529 0.404 0.065 4.804 0.878 0.158 4.792 0.1186 2.14 13.51 0.6472 0.454 0.073 5.399 0.984 0.177 5.372 0.1384 2.49 14.06 0.7555 0.510 0.082 6.067 1.114 0.201 6.080 0.1609 2.90 14.44 0.8781 0.579 0.093 6.885 1.272 0.229 6.945 0.1853 3.34 14.56 1.0113 0.654 0.105 7.777 1.446 0.261 7.890 0.2091 3.77 14.46 1.1410 0.735 0.118 8.743 1.621 0.292 8.846 0.2203 3.97 13.59 1.2023 0.829 0.133 9.858 1.843 0.332 10.059 0.2615 4.71 14.19 1.4274 0.935 0.150 11.121 2.060 0.371 11.241 0.2892 5.21 14.04 1.5784 1.054 0.170 12.533 2.294 0.413 12.522 0.3215 5.79 14.01 1.7549 1.192 0.192 14.168 2.551 0.460 13.924 0.3514 6.33 13.77 1.9177 1.342 0.216 15.952 2.848 0.513 15.544 0.3756 6.77 13.19 2.0498 1.517 0.244 18.033 3.125 0.563 17.054 0.3904 7.04 12.49 2.1307 1.710 0.275 20.337 3.464 0.624 18.905 0.4165 7.51 12.02 2.2732 1.929 0.310 22.938 3.749 0.676 20.462 0.4311 7.77 11.50 2.3528 2.173 0.349 25.837 4.058 0.731 22.145 0.4533 8.17 11.17 2.4740 2.448 0.394 29.107 4.300 0.775 23.466 0.4277 7.71 9.95 2.3341 2.760 0.444 32.823 4.510 0.813 24.614 0.4223 7.61 9.36 2.3046 3.117 0.501 37.059 4.801 0.865 26.201 0.3838 6.92 8.00 2.0948 3.510 0.565 41.741 5.000 0.901 27.289 0.3378 6.09 6.76 1.8434 3.960 0.637 47.092 5.173 0.932 28.231 0.2809 5.06 5.43 1.5332 4.460 0.717 53.038 5.306 0.956 28.958 0.2308 4.16 4.35 1.2595 5.029 0.809 59.801 5.390 0.971 29.415 0.1781 3.21 3.31 0.9722 5.673 0.912 67.456 5.472 0.986 29.866 0.1287 2.32 2.35 0.7021 6.398 1.029 76.077 5.509 0.993 30.066 0.0984 1.77 1.79 0.5371 7.123 1.146 84.698 5.529 0.996 30.174 0.0822 1.48 1.49 0.4489 7.842 1.261 93.245 5.541 0.999 30.242 0.0696 1.25 1.26 0.3796 8.567 1.378 101.866 5.550 1.000 30.291 0.0637 1.15 1.15 0.3477 9.292 1.495 110.487 5.553 1.001 30.305 0.0621 1.12 1.12 0.3388 12.492 2.009 148.539 5.562 1.002 30.352 0.0574 1.03 1.03 0.3134 15.692 2.524 186.590 5.563 1.003 30.359 0.0583 1.05 1.05 0.3179 18.892 3.039 224.642 5.564 1.003 30.364 0.0576 1.04 1.04 0.3145 22.092 3.553 262.694 5.568 1.004 30.389 0.0588 1.06 1.06 0.3208 RUN NUMBER 1W02001 AXIAL POSITION = 695.0 MM SPAN POSITION = 0.0 MM FREE-STREAM VELOCITY = 5.68 M/S FRICTION VELOCITY = 0.1785 M/S FREE-STREAM TURBULENCE = 0.968 % X-REYNOLDS NUMBER = 26.44 X10**4 FLUID DENSITY = 1.212 KG/M**3 KINEMATIC VISCOSITY = 1.493 X10(-5)MSQ/S BOUNDARY LAYER THICKNESS (99.0%) = 6.35 MM DISPLACEMENT THICKNESS = 1.690 MM MOMENTUM THICKNESS = 0.729 MM ENERGY THICKNESS = 1.184 MM FORM FACTOR H = 2.318 FORM FACTOR E = 1.624 RDELTASTAR = 643.0 RTHETA = 277.4 SKIN FRICTION COEFFICIENT = 0.001975 CALCULATED CF = 0.001291 Y Y/DEL YPLUS U U/UO UPLUS u u/UO u/U u/UTAU MM M/S M/S % % 0.029 0.005 0.347 0.062 0.011 0.346 0.0086 0.15 13.95 0.0483 0.035 0.006 0.421 0.075 0.013 0.421 0.0099 0.17 13.19 0.0555 0.042 0.007 0.496 0.088 0.016 0.495 0.0101 0.18 11.48 0.0569 0.048 0.008 0.571 0.102 0.018 0.570 0.0102 0.18 10.06 0.0573 0.054 0.009 0.646 0.115 0.020 0.645 0.0115 0.20 9.96 0.0642 0.060 0.009 0.720 0.128 0.023 0.719 0.0121 0.21 9.40 0.0676 0.067 0.010 0.795 0.142 0.025 0.794 0.0144 0.25 10.14 0.0805 0.073 0.011 0.870 0.155 0.027 0.868 0.0142 0.25 9.15 0.0794 0.079 0.012 0.945 0.168 0.030 0.943 0.0161 0.28 9.57 0.0902 0.085 0.013 1.019 0.182 0.032 1.018 0.0159 0.28 8.74 0.0890 0.098 0.015 1.169 0.208 0.037 1.167 0.0175 0.31 8.41 0.0981 0.110 0.017 1.318 0.235 0.041 1.316 0.0207 0.36 8.80 0.1158 0.123 0.019 1.468 0.261 0.046 1.465 0.0234 0.41 8.94 0.1310 0.135 0.021 1.617 0.288 0.051 1.614 0.0260 0.46 9.03 0.1458 0.154 0.024 1.841 0.328 0.058 1.838 0.0338 0.60 10.31 0.1895 0.179 0.028 2.140 0.381 0.067 2.137 0.0415 0.73 10.90 0.2328 0.198 0.031 2.364 0.421 0.074 2.360 0.0474 0.83 11.25 0.2654 0.229 0.036 2.738 0.488 0.086 2.733 0.0612 1.08 12.54 0.3429 0.254 0.040 3.037 0.541 0.095 3.032 0.0712 1.25 13.16 0.3990 0.292 0.046 3.485 0.604 0.106 3.383 0.0907 1.60 15.01 0.5080 0.329 0.052 3.934 0.669 0.118 3.747 0.0986 1.74 14.75 0.5528 0.367 0.058 4.382 0.760 0.134 4.257 0.1187 2.09 15.62 0.6649 0.417 0.066 4.980 0.856 0.151 4.795 0.1251 2.20 14.62 0.7009 0.473 0.074 5.652 0.973 0.171 5.452 0.1442 2.54 14.82 0.8078 0.535 0.084 6.400 1.141 0.201 6.392 0.1830 3.22 16.05 1.0256 0.604 0.095 7.222 1.311 0.231 7.345 0.2017 3.55 15.38 1.1300 0.679 0.107 8.118 1.448 0.255 8.112 0.2312 4.07 15.97 1.2955 0.773 0.122 9.239 1.682 0.296 9.425 0.2535 4.46 15.07 1.4203 0.873 0.137 10.435 1.907 0.336 10.685 0.2910 5.12 15.26 1.6308 0.985 0.155 11.780 2.137 0.376 11.975 0.3280 5.78 15.35 1.8382 1.110 0.175 13.275 2.384 0.420 13.357 0.3516 6.19 14.75 1.9702 1.254 0.198 14.993 2.679 0.472 15.011 0.3898 6.86 14.55 2.1842 1.417 0.223 16.936 2.952 0.520 16.542 0.4220 7.43 14.30 2.3646 1.598 0.252 19.103 3.251 0.572 18.214 0.4552 8.02 14.00 2.5509 1.810 0.285 21.644 3.597 0.633 20.154 0.4790 8.44 13.32 2.6843 2.042 0.322 24.409 3.906 0.688 21.886 0.4650 8.19 11.91 2.6057 2.304 0.363 27.548 4.190 0.738 23.479 0.4731 8.33 11.29 2.6509 2.604 0.410 31.134 4.496 0.792 25.193 0.4547 8.01 10.11 2.5478 2.942 0.463 35.170 4.725 0.832 26.477 0.4523 7.96 9.57 2.5343 3.323 0.523 39.728 4.983 0.878 27.925 0.3909 6.88 7.84 2.1907 3.754 0.591 44.884 5.165 0.910 28.944 0.3606 6.35 6.98 2.0207 4.242 0.668 50.713 5.347 0.942 29.964 0.2913 5.13 5.45 1.6321 4.785 0.754 57.214 5.476 0.964 30.686 0.2185 3.85 3.99 1.2244 5.410 0.852 64.687 5.556 0.978 31.131 0.1717 3.02 3.09 0.9624 6.104 0.961 72.982 5.613 0.989 31.455 0.1252 2.20 2.23 0.7015 6.898 1.086 82.472 5.647 0.994 31.644 0.0983 1.73 1.74 0.5506 7.685 1.210 91.888 5.681 1.000 31.834 0.0799 1.41 1.41 0.4475 8.479 1.336 101.378 5.653 0.996 31.677 0.0656 1.16 1.16 0.3676 9.267 1.460 110.794 5.670 0.999 31.773 0.0630 1.11 1.11 0.3532 10.054 1.584 120.210 5.666 0.998 31.751 0.0596 1.05 1.05 0.3340 13.504 2.127 161.459 5.696 1.003 31.919 0.0549 0.97 0.96 0.3075 16.954 2.670 202.709 5.673 0.999 31.786 0.0541 0.95 0.95 0.3034 20.404 3.214 243.958 5.727 1.008 32.089 0.0545 0.96 0.95 0.3056 23.854 3.757 285.208 5.694 1.003 31.906 0.0550 0.97 0.97 0.3082 RUN NUMBER 1W02002 AXIAL POSITION = 795.0 MM SPAN POSITION = 0.0 MM FREE-STREAM VELOCITY = 5.81 M/S FRICTION VELOCITY = 0.1729 M/S FREE-STREAM TURBULENCE = 0.908 % X-REYNOLDS NUMBER = 30.96 X10**4 FLUID DENSITY = 1.212 KG/M**3 KINEMATIC VISCOSITY = 1.493 X10(-5)MSQ/S BOUNDARY LAYER THICKNESS (99.0%) = 7.09 MM DISPLACEMENT THICKNESS = 1.814 MM MOMENTUM THICKNESS = 0.787 MM ENERGY THICKNESS = 1.285 MM FORM FACTOR H = 2.305 FORM FACTOR E = 1.632 RDELTASTAR = 706.6 RTHETA = 306.6 SKIN FRICTION COEFFICIENT = 0.001769 CALCULATED CF = 0.001193 Y Y/DEL YPLUS U U/UO UPLUS u u/UO u/U u/UTAU MM M/S M/S % % 0.029 0.004 0.336 0.054 0.009 0.312 0.0095 0.16 17.55 0.0547 0.035 0.005 0.408 0.066 0.011 0.379 0.0093 0.16 14.19 0.0538 0.042 0.006 0.481 0.077 0.013 0.446 0.0116 0.20 15.02 0.0670 0.048 0.007 0.553 0.089 0.015 0.513 0.0104 0.18 11.73 0.0602 0.054 0.008 0.625 0.100 0.017 0.581 0.0117 0.20 11.63 0.0675 0.060 0.008 0.698 0.112 0.019 0.648 0.0128 0.22 11.40 0.0738 0.067 0.009 0.770 0.124 0.021 0.715 0.0130 0.22 10.54 0.0754 0.073 0.010 0.843 0.135 0.023 0.782 0.0141 0.24 10.44 0.0817 0.079 0.011 0.915 0.147 0.025 0.849 0.0157 0.27 10.68 0.0907 0.085 0.012 0.987 0.158 0.027 0.917 0.0176 0.30 11.12 0.1019 0.098 0.014 1.132 0.182 0.031 1.051 0.0228 0.39 12.54 0.1317 0.110 0.016 1.277 0.205 0.035 1.185 0.0203 0.35 9.90 0.1174 0.123 0.017 1.422 0.228 0.039 1.320 0.0244 0.42 10.71 0.1414 0.142 0.020 1.639 0.263 0.045 1.521 0.0289 0.50 10.97 0.1669 0.160 0.023 1.856 0.298 0.051 1.723 0.0350 0.60 11.74 0.2022 0.179 0.025 2.073 0.333 0.057 1.924 0.0432 0.74 12.98 0.2497 0.204 0.029 2.363 0.379 0.065 2.193 0.0492 0.85 12.97 0.2845 0.235 0.033 2.725 0.437 0.075 2.529 0.0637 1.10 14.57 0.3685 0.260 0.037 3.014 0.484 0.083 2.798 0.0732 1.26 15.13 0.4232 0.298 0.042 3.448 0.553 0.095 3.201 0.0903 1.55 16.33 0.5226 0.335 0.047 3.883 0.626 0.108 3.619 0.0983 1.69 15.71 0.5685 0.379 0.053 4.389 0.708 0.122 4.097 0.1298 2.23 18.32 0.7506 0.435 0.061 5.041 0.834 0.143 4.823 0.1513 2.60 18.14 0.8751 0.492 0.069 5.692 0.964 0.166 5.578 0.1715 2.95 17.79 0.9921 0.554 0.078 6.416 1.109 0.191 6.415 0.2041 3.51 18.40 1.1806 0.629 0.089 7.285 1.263 0.217 7.306 0.2126 3.66 16.83 1.2297 0.710 0.100 8.226 1.447 0.249 8.370 0.2467 4.24 17.05 1.4272 0.804 0.113 9.312 1.692 0.291 9.786 0.2882 4.96 17.04 1.6673 0.910 0.128 10.542 1.907 0.328 11.029 0.3236 5.57 16.97 1.8720 1.029 0.145 11.917 2.161 0.372 12.500 0.3664 6.30 16.95 2.1192 1.167 0.164 13.510 2.449 0.421 14.167 0.3752 6.45 15.32 2.1702 1.317 0.186 15.247 2.707 0.466 15.658 0.4251 7.31 15.70 2.4589 1.492 0.210 17.274 3.002 0.516 17.364 0.4604 7.92 15.34 2.6634 1.685 0.238 19.518 3.305 0.568 19.117 0.4797 8.25 14.52 2.7750 1.904 0.268 22.051 3.651 0.628 21.121 0.4960 8.53 13.58 2.8692 2.154 0.304 24.947 3.994 0.687 23.101 0.4962 8.54 12.42 2.8702 2.442 0.344 28.277 4.315 0.742 24.963 0.5105 8.78 11.83 2.9530 2.760 0.389 31.968 4.555 0.784 26.347 0.4920 8.46 10.80 2.8458 3.123 0.440 36.167 4.835 0.832 27.968 0.4791 8.24 9.91 2.7716 3.529 0.498 40.872 5.100 0.877 29.502 0.4158 7.15 8.15 2.4053 3.992 0.563 46.228 5.269 0.906 30.476 0.3707 6.38 7.04 2.1440 4.517 0.637 52.308 5.430 0.934 31.409 0.3286 5.65 6.05 1.9005 5.110 0.721 59.185 5.571 0.958 32.224 0.2546 4.38 4.57 1.4727 5.779 0.815 66.930 5.669 0.975 32.791 0.1975 3.40 3.48 1.1423 6.542 0.922 75.761 5.733 0.986 33.164 0.1470 2.53 2.56 0.8504 7.398 1.043 85.678 5.776 0.994 33.409 0.1095 1.88 1.90 0.6336 8.254 1.164 95.595 5.796 0.997 33.525 0.0852 1.47 1.47 0.4928 9.110 1.285 105.512 5.810 0.999 33.607 0.0721 1.24 1.24 0.4172 9.967 1.405 115.428 5.815 1.000 33.636 0.0647 1.11 1.11 0.3741 10.829 1.527 125.417 5.815 1.000 33.638 0.0580 1.00 1.00 0.3354 14.529 2.049 168.269 5.822 1.001 33.676 0.0532 0.92 0.91 0.3078 18.229 2.571 211.121 5.824 1.002 33.687 0.0521 0.90 0.89 0.3011 21.929 3.092 253.973 5.829 1.003 33.716 0.0519 0.89 0.89 0.3005 25.629 3.614 296.826 5.835 1.004 33.753 0.0528 0.91 0.90 0.3053 RUN NUMBER 1W02003 AXIAL POSITION = 895.0 MM SPAN POSITION = 0.0 MM FREE-STREAM VELOCITY = 5.90 M/S FRICTION VELOCITY = 0.1631 M/S FREE-STREAM TURBULENCE = 0.870 % X-REYNOLDS NUMBER = 35.36 X10**4 FLUID DENSITY = 1.212 KG/M**3 KINEMATIC VISCOSITY = 1.493 X10(-5)MSQ/S BOUNDARY LAYER THICKNESS (99.0%) = 7.80 MM DISPLACEMENT THICKNESS = 2.018 MM MOMENTUM THICKNESS = 0.859 MM ENERGY THICKNESS = 1.396 MM FORM FACTOR H = 2.349 FORM FACTOR E = 1.626 RDELTASTAR = 797.1 RTHETA = 339.3 SKIN FRICTION COEFFICIENT = 0.001530 CALCULATED CF = 0.001117 Y Y/DEL YPLUS U U/UO UPLUS u u/UO u/U u/UTAU MM M/S M/S % % 0.029 0.004 0.317 0.049 0.008 0.299 0.0109 0.18 22.31 0.0667 0.035 0.005 0.385 0.059 0.010 0.363 0.0121 0.20 20.39 0.0741 0.042 0.005 0.454 0.070 0.012 0.428 0.0113 0.19 16.19 0.0692 0.048 0.006 0.522 0.080 0.014 0.492 0.0114 0.19 14.19 0.0698 0.054 0.007 0.590 0.091 0.015 0.556 0.0127 0.21 13.94 0.0776 0.060 0.008 0.658 0.101 0.017 0.621 0.0158 0.27 15.56 0.0966 0.067 0.009 0.727 0.112 0.019 0.685 0.0154 0.26 13.79 0.0945 0.073 0.009 0.795 0.122 0.021 0.750 0.0143 0.24 11.73 0.0880 0.079 0.010 0.863 0.133 0.023 0.814 0.0160 0.27 12.02 0.0978 0.085 0.011 0.932 0.143 0.024 0.878 0.0193 0.33 13.50 0.1186 0.098 0.013 1.068 0.164 0.028 1.007 0.0251 0.43 15.29 0.1540 0.110 0.014 1.205 0.185 0.031 1.136 0.0259 0.44 13.97 0.1588 0.129 0.017 1.410 0.217 0.037 1.329 0.0287 0.49 13.25 0.1761 0.142 0.018 1.546 0.238 0.040 1.458 0.0393 0.67 16.53 0.2411 0.167 0.021 1.820 0.280 0.047 1.716 0.0403 0.68 14.39 0.2468 0.185 0.024 2.025 0.311 0.053 1.909 0.0488 0.83 15.68 0.2993 0.210 0.027 2.298 0.353 0.060 2.167 0.0587 0.99 16.60 0.3597 0.242 0.031 2.639 0.406 0.069 2.489 0.0823 1.40 20.28 0.5047 0.273 0.035 2.981 0.458 0.078 2.811 0.1070 1.81 23.34 0.6559 0.310 0.040 3.391 0.522 0.088 3.197 0.1093 1.85 20.97 0.6703 0.354 0.045 3.869 0.605 0.103 3.709 0.1274 2.16 21.06 0.7809 0.398 0.051 4.347 0.679 0.115 4.162 0.1484 2.52 21.85 0.9095 0.454 0.058 4.962 0.764 0.130 4.686 0.1668 2.83 21.82 1.0223 0.510 0.065 5.576 0.883 0.150 5.413 0.1932 3.28 21.88 1.1847 0.579 0.074 6.328 1.017 0.172 6.232 0.2310 3.92 22.72 1.4162 0.660 0.085 7.216 1.179 0.200 7.225 0.2452 4.16 20.80 1.5032 0.748 0.096 8.172 1.350 0.229 8.274 0.2821 4.78 20.90 1.7295 0.848 0.109 9.265 1.531 0.260 9.383 0.2798 4.75 18.28 1.7154 0.960 0.123 10.494 1.765 0.299 10.822 0.3333 5.65 18.88 2.0434 1.092 0.140 11.929 2.060 0.349 12.628 0.3977 6.74 19.31 2.4380 1.235 0.158 13.500 2.249 0.381 13.785 0.4055 6.88 18.04 2.4861 1.404 0.180 15.344 2.574 0.437 15.780 0.4490 7.61 17.44 2.7526 1.592 0.204 17.393 2.902 0.492 17.790 0.5187 8.80 17.87 3.1796 1.798 0.231 19.647 3.209 0.544 19.670 0.5094 8.64 15.88 3.1231 2.042 0.262 22.311 3.576 0.606 21.924 0.5640 9.56 15.77 3.4576 2.317 0.297 25.316 3.916 0.664 24.009 0.5675 9.62 14.49 3.4792 2.623 0.336 28.663 4.253 0.721 26.071 0.5388 9.14 12.67 3.3030 2.973 0.381 32.488 4.597 0.780 28.182 0.5502 9.33 11.97 3.3729 3.367 0.432 36.791 4.903 0.831 30.055 0.4896 8.30 9.99 3.0017 3.817 0.489 41.709 5.139 0.871 31.502 0.4464 7.57 8.69 2.7364 4.329 0.555 47.310 5.336 0.905 32.712 0.4036 6.84 7.56 2.4744 4.904 0.629 53.594 5.504 0.933 33.741 0.3464 5.88 6.29 2.1239 5.560 0.713 60.766 5.641 0.957 34.583 0.2634 4.47 4.67 1.6150 6.304 0.808 68.894 5.747 0.975 35.233 0.2054 3.48 3.57 1.2589 7.142 0.916 78.047 5.815 0.986 35.646 0.1482 2.51 2.55 0.9086 8.098 1.038 88.497 5.857 0.993 35.903 0.1072 1.82 1.83 0.6572 9.048 1.160 98.880 5.878 0.997 36.033 0.0913 1.55 1.55 0.5596 10.004 1.283 109.330 5.890 0.999 36.105 0.0703 1.19 1.19 0.4310 10.954 1.405 119.712 5.903 1.001 36.186 0.0596 1.01 1.01 0.3655 11.910 1.527 130.163 5.901 1.001 36.172 0.0568 0.96 0.96 0.3482 15.960 2.047 174.424 5.904 1.001 36.195 0.0506 0.86 0.86 0.3101 20.010 2.566 218.685 5.906 1.002 36.207 0.0506 0.86 0.86 0.3099 24.060 3.085 262.946 5.916 1.003 36.265 0.0502 0.85 0.85 0.3078 28.110 3.605 307.207 5.919 1.004 36.287 0.0513 0.87 0.87 0.3145 RUN NUMBER 1W02004 AXIAL POSITION = 995.0 MM SPAN POSITION = 0.0 MM FREE-STREAM VELOCITY = 5.84 M/S FRICTION VELOCITY = 0.1465 M/S FREE-STREAM TURBULENCE = 0.835 % X-REYNOLDS NUMBER = 38.90 X10**4 FLUID DENSITY = 1.211 KG/M**3 KINEMATIC VISCOSITY = 1.494 X10(-5)MSQ/S BOUNDARY LAYER THICKNESS (99.0%) = 8.73 MM DISPLACEMENT THICKNESS = 2.352 MM MOMENTUM THICKNESS = 0.970 MM ENERGY THICKNESS = 1.569 MM FORM FACTOR H = 2.426 FORM FACTOR E = 1.619 RDELTASTAR = 919.5 RTHETA = 379.0 SKIN FRICTION COEFFICIENT = 0.001260 CALCULATED CF = 0.001065 Y Y/DEL YPLUS U U/UO UPLUS u u/UO u/U u/UTAU MM M/S M/S % % 0.029 0.003 0.285 0.038 0.007 0.259 0.0138 0.24 36.44 0.0944 0.035 0.004 0.346 0.046 0.008 0.315 0.0143 0.25 31.03 0.0977 0.042 0.005 0.407 0.054 0.009 0.371 0.0138 0.24 25.41 0.0942 0.048 0.005 0.468 0.063 0.011 0.427 0.0154 0.26 24.69 0.1053 0.054 0.006 0.530 0.071 0.012 0.482 0.0162 0.28 22.92 0.1106 0.060 0.007 0.591 0.079 0.014 0.538 0.0166 0.28 21.05 0.1133 0.067 0.008 0.652 0.087 0.015 0.594 0.0194 0.33 22.27 0.1323 0.073 0.008 0.714 0.095 0.016 0.650 0.0202 0.35 21.23 0.1380 0.079 0.009 0.775 0.103 0.018 0.706 0.0210 0.36 20.32 0.1434 0.085 0.010 0.836 0.112 0.019 0.762 0.0219 0.37 19.58 0.1491 0.098 0.011 0.959 0.128 0.022 0.873 0.0307 0.53 24.03 0.2098 0.117 0.013 1.143 0.153 0.026 1.041 0.0263 0.45 17.26 0.1796 0.129 0.015 1.266 0.169 0.029 1.152 0.0382 0.65 22.59 0.2603 0.148 0.017 1.450 0.193 0.033 1.320 0.0381 0.65 19.71 0.2601 0.167 0.019 1.634 0.218 0.037 1.487 0.0563 0.96 25.82 0.3840 0.192 0.022 1.879 0.251 0.043 1.711 0.0640 1.10 25.51 0.4364 0.217 0.025 2.124 0.283 0.049 1.934 0.0822 1.41 28.99 0.5606 0.248 0.028 2.431 0.324 0.056 2.213 0.0886 1.52 27.32 0.6047 0.285 0.033 2.799 0.373 0.064 2.548 0.0943 1.61 25.25 0.6435 0.323 0.037 3.167 0.422 0.072 2.883 0.1164 1.99 27.55 0.7942 0.367 0.042 3.596 0.480 0.082 3.274 0.1831 3.14 38.17 1.2496 0.417 0.048 4.086 0.524 0.090 3.575 0.1563 2.68 29.84 1.0669 0.473 0.054 4.638 0.607 0.104 4.145 0.1801 3.08 29.65 1.2289 0.535 0.061 5.251 0.700 0.120 4.776 0.2518 4.31 35.98 1.7183 0.610 0.070 5.987 0.804 0.138 5.490 0.2530 4.33 31.45 1.7264 0.692 0.079 6.784 0.987 0.169 6.735 0.3273 5.61 33.16 2.2334 0.785 0.090 7.704 1.109 0.190 7.571 0.3501 6.00 31.56 2.3892 0.892 0.102 8.747 1.268 0.217 8.650 0.3442 5.90 27.15 2.3489 1.010 0.116 9.912 1.478 0.253 10.086 0.3635 6.23 24.60 2.4807 1.148 0.132 11.261 1.690 0.289 11.532 0.4071 6.97 24.09 2.7779 1.304 0.149 12.794 1.957 0.335 13.354 0.4694 8.04 23.98 3.2030 1.485 0.170 14.572 2.267 0.388 15.468 0.4823 8.26 21.28 3.2911 1.685 0.193 16.534 2.552 0.437 17.414 0.5499 9.42 21.55 3.7526 1.917 0.220 18.803 2.933 0.502 20.015 0.6001 10.28 20.46 4.0953 2.173 0.249 21.317 3.237 0.554 22.090 0.6302 10.79 19.47 4.3004 2.467 0.283 24.199 3.636 0.623 24.815 0.6186 10.59 17.01 4.2213 2.804 0.321 27.510 3.989 0.683 27.221 0.6332 10.84 15.87 4.3207 3.185 0.365 31.251 4.364 0.747 29.780 0.5994 10.27 13.74 4.0904 3.617 0.414 35.482 4.621 0.791 31.530 0.5732 9.82 12.41 3.9117 4.104 0.470 40.265 4.951 0.848 33.784 0.5326 9.12 10.76 3.6344 4.660 0.534 45.722 5.197 0.890 35.463 0.4500 7.71 8.66 3.0711 5.292 0.606 51.915 5.402 0.925 36.859 0.3780 6.47 7.00 2.5792 6.010 0.689 58.967 5.539 0.949 37.795 0.3183 5.45 5.75 2.1718 6.823 0.782 66.938 5.656 0.969 38.598 0.2418 4.14 4.27 1.6500 7.748 0.888 76.014 5.738 0.983 39.154 0.1795 3.07 3.13 1.2250 8.798 1.008 86.315 5.795 0.992 39.541 0.1205 2.06 2.08 0.8220 9.848 1.129 96.617 5.817 0.996 39.698 0.0955 1.64 1.64 0.6515 10.898 1.249 106.919 5.831 0.999 39.791 0.0765 1.31 1.31 0.5218 11.948 1.369 117.220 5.843 1.001 39.870 0.0620 1.06 1.06 0.4233 12.998 1.490 127.522 5.841 1.000 39.862 0.0558 0.95 0.95 0.3804 17.398 1.994 170.690 5.848 1.002 39.909 0.0487 0.83 0.83 0.3321 21.798 2.498 213.859 5.851 1.002 39.928 0.0480 0.82 0.82 0.3279 26.198 3.003 257.028 5.860 1.004 39.986 0.0488 0.84 0.83 0.3329 30.598 3.507 300.197 5.865 1.004 40.023 0.0487 0.83 0.83 0.3326 RUN NUMBER 1W02005 AXIAL POSITION = 1095.0 MM SPAN POSITION = 0.0 MM FREE-STREAM VELOCITY = 5.77 M/S FRICTION VELOCITY = 0.1284 M/S FREE-STREAM TURBULENCE = 0.835 % X-REYNOLDS NUMBER = 42.33 X10**4 FLUID DENSITY = 1.213 KG/M**3 KINEMATIC VISCOSITY = 1.492 X10(-5)MSQ/S BOUNDARY LAYER THICKNESS (99.0%) = 10.22 MM DISPLACEMENT THICKNESS = 2.834 MM MOMENTUM THICKNESS = 1.131 MM ENERGY THICKNESS = 1.824 MM FORM FACTOR H = 2.506 FORM FACTOR E = 1.612 RDELTASTAR = 1095.4 RTHETA = 437.1 SKIN FRICTION COEFFICIENT = 0.000991 CALCULATED CF = 0.001021 Y Y/DEL YPLUS U U/UO UPLUS u u/UO u/U u/UTAU MM M/S M/S % % 0.029 0.003 0.250 0.029 0.005 0.228 0.0153 0.27 52.27 0.1191 0.035 0.003 0.303 0.036 0.006 0.277 0.0200 0.35 56.33 0.1561 0.042 0.004 0.357 0.042 0.007 0.326 0.0187 0.32 44.66 0.1457 0.048 0.005 0.411 0.048 0.008 0.375 0.0232 0.40 48.22 0.1810 0.054 0.005 0.465 0.054 0.009 0.424 0.0240 0.42 44.08 0.1871 0.060 0.006 0.518 0.061 0.011 0.474 0.0277 0.48 45.63 0.2161 0.067 0.007 0.572 0.067 0.012 0.523 0.0248 0.43 36.96 0.1932 0.073 0.007 0.626 0.073 0.013 0.572 0.0309 0.54 42.16 0.2410 0.079 0.008 0.680 0.080 0.014 0.621 0.0360 0.62 45.19 0.2806 0.092 0.009 0.787 0.092 0.016 0.719 0.0364 0.63 39.40 0.2833 0.104 0.010 0.895 0.105 0.018 0.817 0.0571 0.99 54.46 0.4452 0.117 0.011 1.002 0.118 0.020 0.916 0.0612 1.06 52.04 0.4765 0.135 0.013 1.164 0.136 0.024 1.063 0.0732 1.27 53.68 0.5706 0.154 0.015 1.325 0.155 0.027 1.210 0.0672 1.16 43.23 0.5232 0.179 0.018 1.540 0.181 0.031 1.407 0.1020 1.77 56.49 0.7947 0.204 0.020 1.755 0.206 0.036 1.603 0.1175 2.04 57.11 0.9157 0.235 0.023 2.024 0.237 0.041 1.849 0.1375 2.39 57.95 1.0715 0.267 0.026 2.293 0.269 0.047 2.095 0.1634 2.83 60.77 1.2728 0.304 0.030 2.616 0.307 0.053 2.389 0.1760 3.05 57.40 1.3714 0.348 0.034 2.992 0.351 0.061 2.733 0.2061 3.57 58.76 1.6059 0.398 0.039 3.423 0.401 0.070 3.126 0.2507 4.35 62.48 1.9533 0.454 0.044 3.907 0.460 0.080 3.586 0.3245 5.63 70.51 2.5282 0.517 0.051 4.444 0.470 0.082 3.664 0.2333 4.05 49.60 1.8174 0.592 0.058 5.090 0.610 0.106 4.756 0.4039 7.00 66.16 3.1465 0.673 0.066 5.789 0.633 0.110 4.934 0.3243 5.62 51.20 2.5264 0.767 0.075 6.596 0.796 0.138 6.199 0.4403 7.64 55.34 3.4303 0.873 0.085 7.510 0.905 0.157 7.049 0.4344 7.53 48.01 3.3844 0.998 0.098 8.585 1.067 0.185 8.314 0.5025 8.71 47.09 3.9149 1.135 0.111 9.768 1.270 0.220 9.898 0.5313 9.21 41.82 4.1396 1.298 0.127 11.167 1.506 0.261 11.731 0.5673 9.84 37.67 4.4194 1.479 0.145 12.726 1.711 0.297 13.332 0.5712 9.91 33.38 4.4505 1.685 0.165 14.501 1.983 0.344 15.452 0.6451 11.19 32.53 5.0258 1.923 0.188 16.545 2.296 0.398 17.886 0.6191 10.74 26.97 4.8232 2.192 0.214 18.857 2.687 0.466 20.936 0.6843 11.87 25.47 5.3313 2.504 0.245 21.546 3.127 0.542 24.363 0.7436 12.90 23.78 5.7933 2.854 0.279 24.558 3.340 0.579 26.021 0.7216 12.51 21.60 5.6216 3.254 0.318 28.000 3.786 0.657 29.497 0.7058 12.24 18.64 5.4985 3.710 0.363 31.926 4.203 0.729 32.746 0.6975 12.10 16.60 5.4343 4.229 0.414 36.389 4.572 0.793 35.616 0.6833 11.85 14.95 5.3234 4.823 0.472 41.498 4.817 0.835 37.528 0.5836 10.12 12.12 4.5470 5.498 0.538 47.307 5.128 0.889 39.954 0.4962 8.60 9.67 3.8655 6.273 0.614 53.975 5.334 0.925 41.554 0.4086 7.09 7.66 3.1831 7.148 0.699 61.504 5.502 0.954 42.865 0.3251 5.64 5.91 2.5329 8.154 0.798 70.163 5.613 0.973 43.727 0.2355 4.08 4.20 1.8348 9.292 0.909 79.951 5.676 0.984 44.219 0.1805 3.13 3.18 1.4062 10.598 1.037 91.191 5.728 0.993 44.626 0.1218 2.11 2.13 0.9492 11.898 1.164 102.377 5.753 0.998 44.824 0.0854 1.48 1.48 0.6654 13.204 1.292 113.617 5.752 0.997 44.809 0.0732 1.27 1.27 0.5700 14.504 1.419 124.803 5.760 0.999 44.873 0.0591 1.02 1.03 0.4602 15.810 1.547 136.043 5.773 1.001 44.973 0.0530 0.92 0.92 0.4127 21.110 2.065 181.648 5.774 1.001 44.985 0.0478 0.83 0.83 0.3727 26.410 2.583 227.252 5.782 1.003 45.044 0.0477 0.83 0.83 0.3720 31.710 3.102 272.857 5.786 1.003 45.073 0.0478 0.83 0.83 0.3725 37.010 3.620 318.462 5.789 1.004 45.100 0.0482 0.84 0.83 0.3751 RUN NUMBER 1W02006 AXIAL POSITION = 1195.0 MM SPAN POSITION = 0.0 MM FREE-STREAM VELOCITY = 5.62 M/S FRICTION VELOCITY = 0.1156 M/S FREE-STREAM TURBULENCE = 0.857 % X-REYNOLDS NUMBER = 45.01 X10**4 FLUID DENSITY = 1.213 KG/M**3 KINEMATIC VISCOSITY = 1.491 X10(-5)MSQ/S BOUNDARY LAYER THICKNESS (99.0%) = 12.20 MM DISPLACEMENT THICKNESS = 3.503 MM MOMENTUM THICKNESS = 1.378 MM ENERGY THICKNESS = 2.211 MM FORM FACTOR H = 2.542 FORM FACTOR E = 1.604 RDELTASTAR = 1319.5 RTHETA = 519.2 SKIN FRICTION COEFFICIENT = 0.000847 CALCULATED CF = 0.000990 Y Y/DEL YPLUS U U/UO UPLUS u u/UO u/U u/UTAU MM M/S M/S % % 0.029 0.002 0.225 0.026 0.005 0.222 0.0283 0.50 99.99 0.2447 0.035 0.003 0.273 0.031 0.006 0.270 0.0299 0.53 95.72 0.2588 0.042 0.003 0.322 0.037 0.007 0.318 0.0322 0.57 87.56 0.2787 0.048 0.004 0.370 0.042 0.008 0.366 0.0394 0.70 92.97 0.3404 0.054 0.004 0.419 0.048 0.009 0.414 0.0365 0.65 76.29 0.3159 0.060 0.005 0.467 0.053 0.010 0.462 0.0416 0.74 77.88 0.3598 0.067 0.005 0.516 0.059 0.010 0.510 0.0415 0.74 70.32 0.3586 0.073 0.006 0.564 0.064 0.011 0.558 0.0512 0.91 79.33 0.4426 0.079 0.006 0.612 0.070 0.012 0.606 0.0533 0.95 76.09 0.4610 0.092 0.007 0.709 0.081 0.014 0.702 0.0605 1.08 74.61 0.5235 0.110 0.009 0.855 0.098 0.017 0.845 0.0674 1.20 68.92 0.5827 0.123 0.010 0.952 0.109 0.019 0.941 0.0897 1.60 82.44 0.7760 0.142 0.012 1.097 0.125 0.022 1.085 0.1115 1.98 88.85 0.9642 0.160 0.013 1.242 0.142 0.025 1.229 0.1181 2.10 83.12 1.0214 0.185 0.015 1.436 0.164 0.029 1.421 0.1440 2.56 87.66 1.2454 0.217 0.018 1.679 0.192 0.034 1.660 0.1862 3.32 97.01 1.6107 0.248 0.020 1.921 0.220 0.039 1.900 0.2279 4.06 99.99 1.9715 0.279 0.023 2.163 0.247 0.044 2.140 0.2606 4.64 99.99 2.2542 0.323 0.026 2.502 0.286 0.051 2.475 0.2817 5.02 98.46 2.4369 0.367 0.030 2.841 0.325 0.058 2.811 0.3725 6.63 99.99 3.2223 0.423 0.035 3.278 0.375 0.067 3.242 0.3763 6.70 99.99 3.2547 0.485 0.040 3.762 0.409 0.073 3.542 0.4158 7.40 99.99 3.5964 0.554 0.045 4.295 0.449 0.080 3.882 0.4836 8.61 99.99 4.1828 0.635 0.052 4.925 0.541 0.096 4.675 0.5299 9.43 98.04 4.5835 0.723 0.059 5.604 0.645 0.115 5.577 0.6148 10.95 95.36 5.3178 0.829 0.068 6.427 0.785 0.140 6.788 0.6770 12.05 86.27 5.8563 0.948 0.078 7.348 0.836 0.149 7.235 0.6786 12.08 81.13 5.8699 1.085 0.089 8.414 0.944 0.168 8.166 0.7343 13.07 77.78 6.3516 1.242 0.102 9.625 1.011 0.180 8.742 0.6959 12.39 68.86 6.0194 1.423 0.117 11.031 1.219 0.217 10.546 0.7230 12.87 59.30 6.2538 1.623 0.133 12.581 1.313 0.234 11.358 0.7332 13.05 55.83 6.3418 1.860 0.152 14.423 1.704 0.303 14.739 0.7990 14.23 46.89 6.9115 2.129 0.174 16.506 1.923 0.342 16.633 0.8426 15.00 43.82 7.2882 2.435 0.200 18.881 2.285 0.407 19.768 0.8605 15.32 37.65 7.4434 2.785 0.228 21.594 2.503 0.446 21.652 0.8526 15.18 34.06 7.3746 3.185 0.261 24.695 3.011 0.536 26.041 0.8484 15.11 28.18 7.3384 3.642 0.298 28.233 3.383 0.602 29.263 0.8597 15.31 25.41 7.4358 4.167 0.341 32.303 3.803 0.677 32.895 0.8188 14.58 21.53 7.0821 4.760 0.390 36.906 4.224 0.752 36.536 0.7661 13.64 18.14 6.6270 5.448 0.446 42.237 4.578 0.815 39.599 0.6885 12.26 15.04 5.9557 6.229 0.510 48.294 4.876 0.868 42.176 0.5887 10.48 12.07 5.0923 7.129 0.584 55.271 5.114 0.910 44.231 0.4791 8.53 9.37 4.1440 8.154 0.668 63.218 5.273 0.939 45.609 0.4112 7.32 7.80 3.5568 9.323 0.764 72.280 5.416 0.964 46.848 0.3096 5.51 5.72 2.6781 10.667 0.874 82.698 5.503 0.980 47.601 0.2408 4.29 4.38 2.0830 12.198 1.000 94.570 5.576 0.993 48.236 0.1372 2.44 2.46 1.1865 13.729 1.125 106.441 5.597 0.996 48.411 0.1077 1.92 1.93 0.9320 15.260 1.251 118.313 5.615 1.000 48.567 0.0728 1.30 1.30 0.6295 16.798 1.377 130.233 5.620 1.001 48.609 0.0648 1.15 1.15 0.5608 18.329 1.502 142.105 5.622 1.001 48.629 0.0540 0.96 0.96 0.4670 24.429 2.002 189.399 5.624 1.001 48.648 0.0484 0.86 0.86 0.4187 30.529 2.502 236.692 5.630 1.002 48.696 0.0483 0.86 0.86 0.4177 36.629 3.002 283.986 5.634 1.003 48.735 0.0480 0.86 0.85 0.4155 42.729 3.502 331.279 5.631 1.003 48.708 0.0481 0.86 0.85 0.4161 RUN NUMBER 1W02010 AXIAL POSITION = 1260.0 MM SPAN POSITION = 0.0 MM FREE-STREAM VELOCITY = 5.53 M/S FRICTION VELOCITY = 0.1409 M/S FREE-STREAM TURBULENCE = 0.881 % X-REYNOLDS NUMBER = 46.74 X10**4 FLUID DENSITY = 1.213 KG/M**3 KINEMATIC VISCOSITY = 1.491 X10(-5)MSQ/S BOUNDARY LAYER THICKNESS (99.0%) = 13.80 MM DISPLACEMENT THICKNESS = 3.824 MM MOMENTUM THICKNESS = 1.598 MM ENERGY THICKNESS = 2.561 MM FORM FACTOR H = 2.393 FORM FACTOR E = 1.603 RDELTASTAR = 1418.4 RTHETA = 592.7 SKIN FRICTION COEFFICIENT = 0.001298 CALCULATED CF = 0.000971 Y Y/DEL YPLUS U U/UO UPLUS u u/UO u/U u/UTAU MM M/S M/S % % 0.029 0.002 0.274 0.039 0.007 0.274 0.0384 0.69 99.31 0.2722 0.035 0.003 0.333 0.047 0.008 0.333 0.0426 0.77 90.75 0.3023 0.042 0.003 0.392 0.055 0.010 0.392 0.0475 0.86 85.96 0.3371 0.048 0.003 0.451 0.064 0.011 0.451 0.0510 0.92 80.13 0.3616 0.054 0.004 0.510 0.072 0.013 0.510 0.0537 0.97 74.61 0.3807 0.060 0.004 0.569 0.080 0.015 0.569 0.0606 1.10 75.57 0.4303 0.067 0.005 0.628 0.089 0.016 0.628 0.0651 1.18 73.50 0.4619 0.073 0.005 0.687 0.097 0.018 0.687 0.0742 1.34 76.59 0.5266 0.085 0.006 0.806 0.114 0.021 0.806 0.0899 1.63 79.21 0.6382 0.098 0.007 0.924 0.130 0.024 0.924 0.1060 1.92 81.39 0.7519 0.110 0.008 1.042 0.147 0.027 1.042 0.1200 2.17 81.75 0.8517 0.129 0.009 1.219 0.172 0.031 1.219 0.1441 2.60 83.86 1.0223 0.148 0.011 1.396 0.197 0.036 1.396 0.1524 2.75 77.44 1.0812 0.167 0.012 1.573 0.222 0.040 1.573 0.1688 3.05 76.11 1.1976 0.192 0.014 1.810 0.255 0.046 1.810 0.2247 4.06 88.11 1.5945 0.223 0.016 2.105 0.297 0.054 2.105 0.2717 4.91 91.58 1.9277 0.254 0.018 2.400 0.338 0.061 2.400 0.3136 5.67 92.70 2.2250 0.298 0.022 2.814 0.397 0.072 2.814 0.4046 7.31 99.99 2.8702 0.335 0.024 3.168 0.447 0.081 3.168 0.4526 8.18 99.99 3.2112 0.392 0.028 3.700 0.490 0.089 3.476 0.5059 9.14 99.99 3.5891 0.448 0.032 4.231 0.509 0.092 3.610 0.5511 9.96 99.99 3.9099 0.510 0.037 4.822 0.641 0.116 4.547 0.6691 12.09 99.99 4.7473 0.585 0.042 5.531 0.609 0.110 4.320 0.6261 11.32 99.99 4.4418 0.673 0.049 6.358 0.659 0.119 4.679 0.6873 12.42 99.99 4.8762 0.773 0.056 7.303 0.769 0.139 5.458 0.7943 14.36 99.99 5.6355 0.885 0.064 8.366 0.871 0.157 6.178 0.8224 14.86 94.44 5.8346 1.017 0.074 9.606 1.031 0.186 7.313 0.9037 16.33 87.68 6.4115 1.167 0.085 11.024 1.058 0.191 7.508 0.8830 15.96 83.44 6.2646 1.342 0.097 12.677 1.191 0.215 8.449 0.9226 16.68 77.47 6.5454 1.535 0.111 14.508 1.304 0.236 9.250 0.9150 16.54 70.19 6.4921 1.767 0.128 16.694 1.512 0.273 10.731 0.9800 17.71 64.80 6.9533 2.023 0.147 19.115 1.712 0.310 12.149 0.9605 17.36 56.09 6.8143 2.323 0.168 21.950 1.949 0.352 13.827 0.9928 17.94 50.94 7.0438 2.660 0.193 25.140 2.349 0.425 16.665 0.9913 17.92 42.20 7.0330 3.054 0.221 28.861 2.561 0.463 18.169 0.9731 17.59 38.00 6.9040 3.504 0.254 33.113 2.981 0.539 21.152 0.9482 17.14 31.80 6.7275 4.017 0.291 37.956 3.356 0.607 23.808 0.9068 16.39 27.02 6.4337 4.610 0.334 43.567 3.592 0.649 25.483 0.9025 16.31 25.13 6.4032 5.285 0.383 49.946 4.158 0.752 29.502 0.8156 14.74 19.61 5.7863 6.060 0.439 57.270 4.485 0.811 31.820 0.7221 13.05 16.10 5.1235 6.954 0.504 65.716 4.760 0.860 33.768 0.6575 11.88 13.81 4.6649 7.973 0.578 75.343 5.032 0.909 35.700 0.5266 9.52 10.47 3.7361 9.148 0.663 86.447 5.215 0.943 36.996 0.4278 7.73 8.20 3.0350 10.492 0.760 99.146 5.343 0.966 37.909 0.3299 5.96 6.17 2.3407 12.029 0.872 113.675 5.421 0.980 38.459 0.2516 4.55 4.64 1.7854 13.798 1.000 130.390 5.487 0.992 38.928 0.1585 2.87 2.89 1.1248 15.567 1.128 147.105 5.518 0.997 39.147 0.1145 2.07 2.08 0.8124 17.329 1.256 163.761 5.520 0.998 39.164 0.0882 1.59 1.60 0.6259 19.098 1.384 180.475 5.531 1.000 39.239 0.0677 1.22 1.22 0.4800 20.867 1.512 197.190 5.539 1.001 39.300 0.0582 1.05 1.05 0.4127 27.767 2.012 262.396 5.541 1.002 39.314 0.0532 0.96 0.96 0.3776 34.667 2.512 327.602 5.550 1.003 39.378 0.0502 0.91 0.90 0.3559 41.567 3.012 392.807 5.554 1.004 39.404 0.0494 0.89 0.89 0.3508 48.467 3.512 458.013 5.553 1.004 39.396 0.0487 0.88 0.88 0.3458 RUN NUMBER 1W02007 AXIAL POSITION = 1295.0 MM SPAN POSITION = 0.0 MM FREE-STREAM VELOCITY = 5.44 M/S FRICTION VELOCITY = 0.1553 M/S FREE-STREAM TURBULENCE = 0.917 % X-REYNOLDS NUMBER = 47.26 X10**4 FLUID DENSITY = 1.213 KG/M**3 KINEMATIC VISCOSITY = 1.491 X10(-5)MSQ/S BOUNDARY LAYER THICKNESS (99.0%) = 15.27 MM DISPLACEMENT THICKNESS = 3.953 MM MOMENTUM THICKNESS = 1.769 MM ENERGY THICKNESS = 2.852 MM FORM FACTOR H = 2.235 FORM FACTOR E = 1.613 RDELTASTAR = 1442.6 RTHETA = 645.4 SKIN FRICTION COEFFICIENT = 0.001629 CALCULATED CF = 0.000966 Y Y/DEL YPLUS U U/UO UPLUS u u/UO u/U u/UTAU MM M/S M/S % % 0.029 0.002 0.302 0.047 0.009 0.302 0.0400 0.73 85.19 0.2573 0.035 0.002 0.367 0.057 0.010 0.367 0.0474 0.87 83.11 0.3051 0.042 0.003 0.432 0.067 0.012 0.432 0.0508 0.93 75.70 0.3272 0.048 0.003 0.497 0.077 0.014 0.497 0.0533 0.98 69.02 0.3433 0.054 0.004 0.562 0.087 0.016 0.562 0.0613 1.13 70.21 0.3949 0.060 0.004 0.628 0.097 0.018 0.628 0.0691 1.27 70.91 0.4450 0.067 0.004 0.693 0.108 0.020 0.693 0.0726 1.33 67.53 0.4677 0.073 0.005 0.758 0.118 0.022 0.758 0.0808 1.48 68.66 0.5202 0.085 0.006 0.888 0.138 0.025 0.888 0.0938 1.72 67.98 0.6036 0.098 0.006 1.018 0.158 0.029 1.018 0.1085 1.99 68.59 0.6983 0.110 0.007 1.148 0.178 0.033 1.148 0.1252 2.30 70.18 0.8058 0.129 0.008 1.344 0.209 0.038 1.344 0.1488 2.73 71.30 0.9579 0.148 0.010 1.539 0.239 0.044 1.539 0.1810 3.32 75.70 1.1650 0.173 0.011 1.799 0.279 0.051 1.799 0.2173 3.99 77.75 1.3989 0.198 0.013 2.060 0.320 0.059 2.060 0.2415 4.44 75.48 1.5546 0.229 0.015 2.385 0.370 0.068 2.385 0.3172 5.83 85.61 2.0418 0.267 0.017 2.776 0.431 0.079 2.776 0.3650 6.71 84.65 2.3496 0.304 0.020 3.166 0.492 0.090 3.166 0.4331 7.96 88.07 2.7885 0.348 0.023 3.622 0.514 0.094 3.308 0.4839 8.89 94.19 3.1156 0.404 0.026 4.208 0.576 0.106 3.706 0.5592 10.27 97.13 3.6002 0.460 0.030 4.794 0.609 0.112 3.920 0.6112 11.23 99.99 3.9347 0.529 0.035 5.510 0.689 0.127 4.437 0.6841 12.57 99.26 4.4040 0.610 0.040 6.356 0.757 0.139 4.873 0.7507 13.79 99.17 4.8329 0.704 0.046 7.332 0.929 0.171 5.982 0.8147 14.97 87.67 5.2447 0.804 0.053 8.374 0.986 0.181 6.347 0.8707 16.00 88.31 5.6057 0.929 0.061 9.676 1.052 0.193 6.771 0.9191 16.89 87.38 5.9170 1.067 0.070 11.108 1.208 0.222 7.780 0.9750 17.91 80.68 6.2771 1.223 0.080 12.735 1.166 0.214 7.506 0.9529 17.51 81.73 6.1347 1.404 0.092 14.623 1.333 0.245 8.579 1.0125 18.60 75.99 6.5187 1.617 0.106 16.836 1.730 0.318 11.138 1.0294 18.91 59.50 6.6270 1.860 0.122 19.375 1.737 0.319 11.182 1.0055 18.48 57.89 6.4735 2.135 0.140 22.239 1.906 0.350 12.269 1.0169 18.68 53.36 6.5468 2.454 0.161 25.559 1.994 0.366 12.836 0.9926 18.24 49.78 6.3901 2.817 0.184 29.335 2.461 0.452 15.844 1.0470 19.24 42.54 6.7402 3.235 0.212 33.696 2.724 0.500 17.536 1.0344 19.01 37.98 6.6594 3.717 0.243 38.708 3.034 0.557 19.533 0.9699 17.82 31.97 6.2444 4.273 0.280 44.502 3.330 0.612 21.440 0.9379 17.23 28.16 6.0381 4.910 0.322 51.141 3.741 0.687 24.086 0.9111 16.74 24.35 5.8658 5.642 0.369 58.758 4.070 0.748 26.205 0.8299 15.25 20.39 5.3429 6.479 0.424 67.480 4.418 0.812 28.442 0.7343 13.49 16.62 4.7273 7.442 0.487 77.505 4.690 0.862 30.194 0.6466 11.88 13.79 4.1626 8.554 0.560 89.092 4.916 0.903 31.647 0.5617 10.32 11.43 3.6160 9.823 0.643 102.306 5.123 0.941 32.983 0.4410 8.10 8.61 2.8392 11.285 0.739 117.539 5.260 0.967 33.865 0.3206 5.89 6.10 2.0642 12.967 0.849 135.049 5.330 0.979 34.313 0.2594 4.77 4.87 1.6697 14.898 0.976 155.164 5.386 0.990 34.676 0.1771 3.25 3.29 1.1404 16.829 1.102 175.278 5.422 0.996 34.904 0.1129 2.07 2.08 0.7270 18.754 1.228 195.328 5.431 0.998 34.961 0.0850 1.56 1.56 0.5469 20.685 1.355 215.442 5.445 1.000 35.051 0.0657 1.21 1.21 0.4227 22.617 1.481 235.556 5.443 1.000 35.044 0.0618 1.13 1.13 0.3975 30.067 1.969 313.150 5.447 1.001 35.066 0.0549 1.01 1.01 0.3536 37.517 2.457 390.744 5.449 1.001 35.079 0.0522 0.96 0.96 0.3363 44.967 2.945 468.337 5.452 1.002 35.100 0.0504 0.93 0.92 0.3245 52.417 3.433 545.931 5.453 1.002 35.104 0.0499 0.92 0.91 0.3211 RUN NUMBER 1W02008 AXIAL POSITION = 1395.0 MM SPAN POSITION = 0.0 MM FREE-STREAM VELOCITY = 5.23 M/S FRICTION VELOCITY = 0.1951 M/S FREE-STREAM TURBULENCE = 0.968 % X-REYNOLDS NUMBER = 48.91 X10**4 FLUID DENSITY = 1.214 KG/M**3 KINEMATIC VISCOSITY = 1.490 X10(-5)MSQ/S BOUNDARY LAYER THICKNESS (99.0%) = 20.24 MM DISPLACEMENT THICKNESS = 4.101 MM MOMENTUM THICKNESS = 2.330 MM ENERGY THICKNESS = 3.904 MM FORM FACTOR H = 1.760 FORM FACTOR E = 1.675 RDELTASTAR = 1437.9 RTHETA = 817.1 SKIN FRICTION COEFFICIENT = 0.002789 CALCULATED CF = 0.000949 Y Y/DEL YPLUS U U/UO UPLUS u u/UO u/U u/UTAU MM M/S M/S % % 0.029 0.001 0.380 0.075 0.014 0.385 0.0438 0.84 58.36 0.2246 0.035 0.002 0.462 0.091 0.017 0.468 0.0487 0.93 53.35 0.2495 0.042 0.002 0.543 0.107 0.021 0.551 0.0518 0.99 48.18 0.2653 0.048 0.002 0.625 0.124 0.024 0.634 0.0587 1.12 47.44 0.3006 0.054 0.003 0.707 0.140 0.027 0.717 0.0623 1.19 44.58 0.3195 0.060 0.003 0.789 0.156 0.030 0.799 0.0667 1.28 42.72 0.3416 0.067 0.003 0.871 0.172 0.033 0.882 0.0747 1.43 43.35 0.3825 0.079 0.004 1.034 0.205 0.039 1.048 0.0883 1.69 43.15 0.4523 0.092 0.005 1.198 0.237 0.045 1.214 0.1069 2.05 45.11 0.5476 0.104 0.005 1.362 0.269 0.052 1.380 0.1213 2.32 45.06 0.6218 0.117 0.006 1.525 0.302 0.058 1.546 0.1426 2.73 47.26 0.7306 0.142 0.007 1.853 0.366 0.070 1.878 0.1858 3.56 50.72 0.9522 0.160 0.008 2.098 0.415 0.079 2.126 0.2170 4.15 52.31 1.1122 0.185 0.009 2.426 0.480 0.092 2.458 0.2559 4.90 53.35 1.3114 0.217 0.011 2.835 0.561 0.107 2.873 0.3221 6.16 57.45 1.6503 0.248 0.012 3.244 0.642 0.123 3.287 0.3648 6.98 56.87 1.8694 0.285 0.014 3.735 0.714 0.137 3.660 0.4232 8.10 59.24 2.1684 0.335 0.017 4.390 0.833 0.159 4.268 0.5089 9.74 61.10 2.6077 0.385 0.019 5.044 0.966 0.185 4.948 0.5909 11.31 61.20 3.0281 0.448 0.022 5.863 1.099 0.210 5.632 0.6514 12.47 59.27 3.3381 0.517 0.026 6.763 1.229 0.235 6.300 0.7220 13.82 58.72 3.6998 0.598 0.030 7.827 1.343 0.257 6.882 0.7657 14.65 57.01 3.9238 0.692 0.034 9.054 1.531 0.293 7.847 0.8164 15.62 53.31 4.1835 0.798 0.039 10.446 1.648 0.315 8.446 0.8554 16.37 51.90 4.3836 0.923 0.046 12.082 1.756 0.336 8.999 0.8829 16.89 50.27 4.5241 1.067 0.053 13.965 1.919 0.367 9.834 0.8869 16.97 46.21 4.5446 1.229 0.061 16.092 2.023 0.387 10.367 0.9158 17.52 45.27 4.6927 1.423 0.070 18.629 2.158 0.413 11.059 0.8997 17.22 41.69 4.6104 1.642 0.081 21.494 2.229 0.427 11.422 0.9195 17.60 41.25 4.7118 1.898 0.094 24.849 2.486 0.476 12.739 0.8738 16.72 35.15 4.4776 2.192 0.108 28.695 2.526 0.483 12.943 0.8840 16.92 35.00 4.5299 2.535 0.125 33.196 2.665 0.510 13.658 0.8719 16.68 32.71 4.4677 2.929 0.145 38.352 2.807 0.537 14.386 0.8777 16.79 31.26 4.4974 3.379 0.167 44.244 2.987 0.572 15.309 0.8696 16.64 29.11 4.4561 3.904 0.193 51.118 3.218 0.616 16.488 0.8383 16.04 26.05 4.2957 4.510 0.223 59.057 3.387 0.648 17.354 0.8349 15.98 24.65 4.2783 5.210 0.257 68.222 3.601 0.689 18.451 0.8424 16.12 23.40 4.3167 6.023 0.298 78.861 3.838 0.734 19.667 0.8130 15.56 21.18 4.1659 6.954 0.344 91.055 4.075 0.780 20.879 0.7629 14.60 18.72 3.9092 8.035 0.397 105.212 4.334 0.829 22.207 0.7292 13.95 16.83 3.7366 9.285 0.459 121.580 4.515 0.864 23.135 0.6565 12.56 14.54 3.3642 10.723 0.530 140.402 4.737 0.907 24.275 0.5644 10.80 11.91 2.8922 12.392 0.612 162.253 4.900 0.938 25.110 0.4513 8.64 9.21 2.3125 14.310 0.707 187.376 5.015 0.960 25.697 0.3591 6.87 7.16 1.8401 16.529 0.816 216.428 5.101 0.976 26.138 0.2582 4.94 5.06 1.3231 19.098 0.943 250.063 5.167 0.989 26.475 0.1569 3.00 3.04 0.8039 21.660 1.070 283.616 5.195 0.994 26.618 0.1120 2.14 2.16 0.5739 24.229 1.197 317.251 5.213 0.998 26.712 0.0760 1.46 1.46 0.3896 26.792 1.323 350.804 5.217 0.998 26.735 0.0670 1.28 1.28 0.3433 29.360 1.450 384.439 5.222 0.999 26.761 0.0630 1.21 1.21 0.3228 38.910 1.922 509.486 5.230 1.001 26.801 0.0555 1.06 1.06 0.2844 48.460 2.394 634.532 5.237 1.002 26.835 0.0511 0.98 0.98 0.2619 58.010 2.866 759.578 5.249 1.004 26.896 0.0507 0.97 0.97 0.2599 67.560 3.337 884.625 5.244 1.003 26.871 0.0506 0.97 0.96 0.2592 RUN NUMBER 1W02009 AXIAL POSITION = 1495.0 MM SPAN POSITION = 0.0 MM FREE-STREAM VELOCITY = 4.96 M/S FRICTION VELOCITY = 0.2046 M/S FREE-STREAM TURBULENCE = 1.023 % X-REYNOLDS NUMBER = 49.71 X10**4 FLUID DENSITY = 1.213 KG/M**3 KINEMATIC VISCOSITY = 1.491 X10(-5)MSQ/S BOUNDARY LAYER THICKNESS (99.0%) = 25.18 MM DISPLACEMENT THICKNESS = 4.743 MM MOMENTUM THICKNESS = 2.974 MM ENERGY THICKNESS = 5.082 MM FORM FACTOR H = 1.595 FORM FACTOR E = 1.709 RDELTASTAR = 1577.2 RTHETA = 988.9 SKIN FRICTION COEFFICIENT = 0.003407 CALCULATED CF = 0.003213 LAW OF THE WALL OFFSET = 5.20 KARMAN CONSTANT = 0.410 FORM FACTOR G = 9.037 CLAUSER DELTA = 114.921 MM WAKE FACTOR PI = 1.156 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 0.398 0.084 0.017 0.409 0.0345 0.70 41.26 0.1689 0.035 0.001 0.484 0.102 0.021 0.497 0.0370 0.75 36.31 0.1807 0.042 0.002 0.570 0.120 0.024 0.586 0.0409 0.82 34.12 0.1998 0.048 0.002 0.655 0.138 0.028 0.674 0.0464 0.94 33.69 0.2270 0.054 0.002 0.741 0.156 0.031 0.762 0.0507 1.02 32.53 0.2479 0.060 0.002 0.827 0.174 0.035 0.850 0.0564 1.14 32.41 0.2756 0.067 0.003 0.913 0.192 0.039 0.939 0.0623 1.26 32.45 0.3045 0.079 0.003 1.084 0.228 0.046 1.115 0.0742 1.50 32.51 0.3625 0.092 0.004 1.256 0.264 0.053 1.291 0.0899 1.81 34.01 0.4392 0.110 0.004 1.513 0.318 0.064 1.556 0.1118 2.26 35.13 0.5466 0.123 0.005 1.685 0.354 0.071 1.732 0.1321 2.66 37.27 0.6457 0.148 0.006 2.028 0.427 0.086 2.085 0.1697 3.42 39.78 0.8296 0.173 0.007 2.371 0.499 0.101 2.438 0.2030 4.10 40.70 0.9923 0.198 0.008 2.714 0.571 0.115 2.791 0.2377 4.80 41.64 1.1620 0.229 0.009 3.143 0.661 0.133 3.232 0.2835 5.72 42.87 1.3854 0.267 0.011 3.657 0.751 0.151 3.669 0.3392 6.84 45.18 1.6578 0.310 0.012 4.258 0.834 0.168 4.075 0.3902 7.87 46.81 1.9073 0.360 0.014 4.944 0.979 0.198 4.787 0.4537 9.15 46.33 2.2177 0.423 0.017 5.802 1.115 0.225 5.450 0.4983 10.05 44.69 2.4357 0.492 0.020 6.745 1.309 0.264 6.400 0.5697 11.49 43.51 2.7844 0.573 0.023 7.860 1.433 0.289 7.005 0.6203 12.51 43.28 3.0318 0.660 0.026 9.061 1.597 0.322 7.808 0.6498 13.11 40.68 3.1759 0.767 0.030 10.519 1.792 0.361 8.759 0.6749 13.61 37.66 3.2986 0.892 0.035 12.235 1.965 0.396 9.605 0.6860 13.84 34.91 3.3530 1.035 0.041 14.208 2.082 0.420 10.174 0.6892 13.90 33.11 3.3684 1.204 0.048 16.523 2.288 0.461 11.181 0.6763 13.64 29.56 3.3055 1.398 0.056 19.182 2.365 0.477 11.561 0.6692 13.50 28.29 3.2707 1.629 0.065 22.356 2.506 0.505 12.247 0.6508 13.13 25.97 3.1808 1.885 0.075 25.873 2.583 0.521 12.623 0.6546 13.20 25.34 3.1993 2.192 0.087 30.076 2.704 0.546 13.218 0.6612 13.34 24.45 3.2317 2.548 0.101 34.965 2.782 0.561 13.596 0.6590 13.29 23.69 3.2208 2.954 0.117 40.540 2.875 0.580 14.052 0.6513 13.14 22.65 3.1834 3.435 0.136 47.145 2.977 0.600 14.548 0.6542 13.20 21.98 3.1977 3.985 0.158 54.693 3.131 0.632 15.304 0.6417 12.94 20.49 3.1363 4.629 0.184 63.528 3.241 0.654 15.839 0.6450 13.01 19.90 3.1523 5.373 0.213 73.735 3.335 0.673 16.298 0.6678 13.47 20.03 3.2642 6.235 0.248 85.571 3.499 0.706 17.103 0.6615 13.34 18.91 3.2334 7.242 0.288 99.381 3.668 0.740 17.930 0.6826 13.77 18.61 3.3365 8.404 0.334 115.335 3.825 0.771 18.693 0.6647 13.41 17.38 3.2486 9.760 0.388 133.948 4.018 0.811 19.639 0.6355 12.82 15.82 3.1062 11.329 0.450 155.477 4.213 0.850 20.593 0.5971 12.05 14.17 2.9186 13.154 0.522 180.523 4.392 0.886 21.468 0.5661 11.42 12.89 2.7667 15.273 0.606 209.600 4.578 0.923 22.376 0.4630 9.34 10.11 2.2632 17.729 0.704 243.309 4.728 0.954 23.111 0.3614 7.29 7.64 1.7662 20.585 0.817 282.508 4.824 0.973 23.580 0.2628 5.30 5.45 1.2845 23.898 0.949 327.968 4.905 0.989 23.972 0.1549 3.13 3.16 0.7573 27.210 1.081 373.428 4.939 0.996 24.138 0.0943 1.90 1.91 0.4610 30.523 1.212 418.889 4.949 0.998 24.190 0.0756 1.53 1.53 0.3695 33.835 1.344 464.349 4.952 0.999 24.205 0.0669 1.35 1.35 0.3270 37.148 1.475 509.809 4.957 1.000 24.226 0.0604 1.22 1.22 0.2950 45.235 1.796 620.800 4.962 1.001 24.252 0.0562 1.13 1.13 0.2746 53.317 2.117 731.706 4.965 1.002 24.268 0.0535 1.08 1.08 0.2616 61.404 2.438 842.697 4.968 1.002 24.284 0.0514 1.04 1.04 0.2514 69.492 2.759 953.688 4.967 1.002 24.275 0.0507 1.02 1.02 0.2480