ROLLS-ROYCE APPLIED SCIENCE LABORATORY FLAT PLATE TRANSITIONAL BOUNDARY LAYER FLOW HOT WIRE ANEMOMETRY TEST DATA SINGLE WIRE DATA FOR ERCOFTAC T3C2 TEST CASE RUN NUMBER 1W01906 AXIAL POSITION = 45.0 MM SPAN POSITION = 0.0 MM FREE-STREAM VELOCITY = 5.67 M/S FRICTION VELOCITY = 0.3121 M/S FREE-STREAM TURBULENCE = 2.397 % X-REYNOLDS NUMBER = 1.66 X10**4 FLUID DENSITY = 1.179 KG/M**3 KINEMATIC VISCOSITY = 1.534 X10(-5)MSQ/S BOUNDARY LAYER THICKNESS (99.0%) = 1.62 MM DISPLACEMENT THICKNESS = 0.520 MM MOMENTUM THICKNESS = 0.207 MM ENERGY THICKNESS = 0.328 MM FORM FACTOR H = 2.517 FORM FACTOR E = 1.587 RDELTASTAR = 192.2 RTHETA = 76.4 SKIN FRICTION COEFFICIENT = 0.006062 CALCULATED CF = 0.005149 Y Y/DEL YPLUS U U/UO UPLUS u u/UO u/U u/UTAU MM M/S M/S % % 0.029 0.018 0.590 0.188 0.033 0.603 0.0097 0.17 5.17 0.0312 0.035 0.022 0.717 0.229 0.040 0.733 0.0122 0.21 5.31 0.0389 0.042 0.026 0.844 0.269 0.047 0.863 0.0119 0.21 4.42 0.0381 0.048 0.030 0.972 0.310 0.055 0.993 0.0128 0.23 4.13 0.0410 0.054 0.033 1.099 0.350 0.062 1.122 0.0141 0.25 4.04 0.0453 0.060 0.037 1.226 0.391 0.069 1.252 0.0157 0.28 4.01 0.0502 0.067 0.041 1.353 0.431 0.076 1.382 0.0172 0.30 3.99 0.0551 0.073 0.045 1.480 0.472 0.083 1.512 0.0192 0.34 4.07 0.0616 0.079 0.049 1.607 0.513 0.090 1.642 0.0215 0.38 4.19 0.0687 0.085 0.053 1.735 0.553 0.098 1.772 0.0242 0.43 4.38 0.0777 0.092 0.057 1.862 0.594 0.105 1.902 0.0269 0.47 4.53 0.0861 0.098 0.060 1.989 0.634 0.112 2.032 0.0295 0.52 4.65 0.0945 0.104 0.064 2.116 0.675 0.119 2.162 0.0322 0.57 4.78 0.1032 0.110 0.068 2.243 0.715 0.126 2.292 0.0348 0.61 4.86 0.1114 0.117 0.072 2.370 0.756 0.133 2.422 0.0373 0.66 4.93 0.1195 0.123 0.076 2.498 0.796 0.140 2.552 0.0395 0.70 4.97 0.1267 0.129 0.080 2.625 0.837 0.148 2.681 0.0418 0.74 4.99 0.1339 0.135 0.084 2.752 0.878 0.155 2.811 0.0452 0.80 5.15 0.1449 0.148 0.091 3.006 0.959 0.169 3.071 0.0511 0.90 5.33 0.1636 0.160 0.099 3.261 1.025 0.181 3.285 0.0565 1.00 5.51 0.1809 0.173 0.107 3.515 1.097 0.193 3.513 0.0612 1.08 5.58 0.1959 0.192 0.119 3.896 1.215 0.214 3.891 0.0678 1.20 5.58 0.2172 0.210 0.130 4.278 1.318 0.232 4.223 0.0763 1.35 5.79 0.2446 0.229 0.142 4.659 1.438 0.254 4.608 0.0839 1.48 5.83 0.2688 0.254 0.157 5.168 1.598 0.282 5.118 0.0971 1.71 6.08 0.3111 0.273 0.169 5.550 1.708 0.301 5.471 0.1044 1.84 6.11 0.3344 0.304 0.188 6.185 1.902 0.335 6.092 0.1173 2.07 6.17 0.3759 0.329 0.204 6.694 2.070 0.365 6.633 0.1250 2.21 6.04 0.4006 0.360 0.223 7.330 2.270 0.400 7.273 0.1421 2.51 6.26 0.4552 0.398 0.246 8.093 2.507 0.442 8.032 0.1536 2.71 6.13 0.4920 0.435 0.269 8.856 2.733 0.482 8.756 0.1671 2.95 6.11 0.5352 0.479 0.296 9.746 3.003 0.530 9.620 0.1808 3.19 6.02 0.5791 0.523 0.324 10.636 3.251 0.573 10.415 0.1867 3.29 5.74 0.5980 0.573 0.354 11.653 3.506 0.618 11.232 0.2002 3.53 5.71 0.6414 0.623 0.385 12.671 3.741 0.660 11.986 0.2044 3.60 5.46 0.6547 0.685 0.424 13.942 4.013 0.708 12.857 0.2129 3.75 5.30 0.6820 0.748 0.463 15.214 4.257 0.751 13.638 0.2169 3.83 5.10 0.6949 0.823 0.509 16.740 4.517 0.797 14.472 0.2141 3.78 4.74 0.6859 0.898 0.556 18.266 4.748 0.837 15.212 0.2084 3.68 4.39 0.6676 0.985 0.610 20.046 4.961 0.875 15.894 0.1994 3.52 4.02 0.6389 1.079 0.668 21.954 5.155 0.909 16.515 0.1881 3.32 3.65 0.6026 1.179 0.730 23.989 5.311 0.937 17.014 0.1766 3.12 3.33 0.5659 1.292 0.799 26.278 5.437 0.959 17.420 0.1683 2.97 3.10 0.5392 1.417 0.877 28.821 5.533 0.976 17.726 0.1595 2.81 2.88 0.5109 1.548 0.958 31.491 5.599 0.988 17.938 0.1542 2.72 2.75 0.4939 1.698 1.051 34.543 5.640 0.995 18.068 0.1547 2.73 2.74 0.4956 1.842 1.140 37.468 5.662 0.999 18.141 0.1513 2.67 2.67 0.4849 1.992 1.232 40.520 5.667 0.999 18.155 0.1511 2.67 2.67 0.4842 2.135 1.321 43.445 5.672 1.000 18.171 0.1488 2.62 2.62 0.4768 2.285 1.414 46.497 5.671 1.000 18.168 0.1469 2.59 2.59 0.4707 3.135 1.940 63.791 5.676 1.001 18.185 0.1404 2.48 2.47 0.4497 3.985 2.466 81.086 5.679 1.002 18.196 0.1377 2.43 2.42 0.4411 4.835 2.992 98.381 5.681 1.002 18.200 0.1356 2.39 2.39 0.4346 5.685 3.518 115.675 5.679 1.002 18.196 0.1359 2.40 2.39 0.4354 RUN NUMBER 1W01801 AXIAL POSITION = 95.0 MM SPAN POSITION = 0.0 MM FREE-STREAM VELOCITY = 6.03 M/S FRICTION VELOCITY = 0.2741 M/S FREE-STREAM TURBULENCE = 2.054 % X-REYNOLDS NUMBER = 3.85 X10**4 FLUID DENSITY = 1.214 KG/M**3 KINEMATIC VISCOSITY = 1.490 X10(-5)MSQ/S BOUNDARY LAYER THICKNESS (99.0%) = 2.29 MM DISPLACEMENT THICKNESS = 0.707 MM MOMENTUM THICKNESS = 0.284 MM ENERGY THICKNESS = 0.452 MM FORM FACTOR H = 2.488 FORM FACTOR E = 1.593 RDELTASTAR = 286.1 RTHETA = 115.0 SKIN FRICTION COEFFICIENT = 0.004127 CALCULATED CF = 0.003385 Y Y/DEL YPLUS U U/UO UPLUS u u/UO u/U u/UTAU MM M/S M/S % % 0.029 0.013 0.533 0.150 0.025 0.547 0.0116 0.19 7.77 0.0425 0.035 0.015 0.648 0.182 0.030 0.665 0.0125 0.21 6.86 0.0456 0.042 0.018 0.763 0.214 0.036 0.783 0.0142 0.23 6.61 0.0517 0.048 0.021 0.878 0.247 0.041 0.900 0.0140 0.23 5.67 0.0510 0.054 0.024 0.993 0.279 0.046 1.018 0.0148 0.25 5.31 0.0541 0.060 0.026 1.108 0.311 0.052 1.136 0.0159 0.26 5.10 0.0579 0.067 0.029 1.223 0.344 0.057 1.254 0.0174 0.29 5.05 0.0633 0.073 0.032 1.338 0.376 0.062 1.372 0.0191 0.32 5.09 0.0698 0.079 0.035 1.453 0.408 0.068 1.490 0.0214 0.35 5.23 0.0779 0.085 0.037 1.568 0.441 0.073 1.607 0.0235 0.39 5.33 0.0857 0.092 0.040 1.683 0.473 0.078 1.725 0.0261 0.43 5.52 0.0952 0.098 0.043 1.798 0.505 0.084 1.843 0.0288 0.48 5.70 0.1050 0.104 0.045 1.913 0.538 0.089 1.961 0.0316 0.52 5.88 0.1153 0.110 0.048 2.028 0.570 0.094 2.079 0.0338 0.56 5.93 0.1232 0.117 0.051 2.143 0.602 0.100 2.197 0.0376 0.62 6.24 0.1370 0.129 0.056 2.373 0.667 0.110 2.432 0.0441 0.73 6.61 0.1608 0.142 0.062 2.603 0.731 0.121 2.668 0.0511 0.85 6.98 0.1864 0.154 0.067 2.833 0.796 0.132 2.904 0.0565 0.94 7.10 0.2062 0.173 0.076 3.178 0.893 0.148 3.257 0.0631 1.05 7.06 0.2301 0.192 0.084 3.522 0.972 0.161 3.544 0.0726 1.20 7.47 0.2648 0.210 0.092 3.867 1.057 0.175 3.854 0.0794 1.32 7.52 0.2898 0.235 0.103 4.327 1.171 0.194 4.272 0.0922 1.53 7.88 0.3365 0.260 0.114 4.787 1.286 0.213 4.690 0.1024 1.70 7.96 0.3735 0.285 0.125 5.247 1.406 0.233 5.130 0.1132 1.88 8.05 0.4131 0.317 0.138 5.822 1.570 0.260 5.728 0.1312 2.17 8.36 0.4788 0.348 0.152 6.396 1.729 0.287 6.307 0.1478 2.45 8.55 0.5391 0.385 0.168 7.086 1.929 0.320 7.036 0.1628 2.70 8.44 0.5939 0.429 0.188 7.891 2.166 0.359 7.901 0.1815 3.01 8.38 0.6622 0.473 0.207 8.696 2.376 0.394 8.668 0.1962 3.25 8.26 0.7156 0.523 0.229 9.615 2.607 0.432 9.512 0.2178 3.61 8.35 0.7947 0.579 0.253 10.650 2.874 0.476 10.485 0.2394 3.97 8.33 0.8732 0.642 0.281 11.800 3.173 0.526 11.574 0.2542 4.21 8.01 0.9275 0.704 0.308 12.949 3.450 0.572 12.585 0.2772 4.59 8.03 1.0112 0.779 0.341 14.329 3.747 0.621 13.671 0.2891 4.79 7.71 1.0545 0.860 0.376 15.823 4.050 0.671 14.773 0.2969 4.92 7.33 1.0831 0.954 0.417 17.548 4.358 0.722 15.900 0.2987 4.95 6.85 1.0898 1.054 0.461 19.387 4.642 0.769 16.936 0.2997 4.97 6.46 1.0932 1.167 0.510 21.456 4.934 0.818 17.998 0.2854 4.73 5.79 1.0412 1.292 0.565 23.755 5.203 0.862 18.982 0.2662 4.41 5.12 0.9712 1.423 0.622 26.170 5.420 0.898 19.774 0.2489 4.12 4.59 0.9080 1.573 0.688 28.929 5.618 0.931 20.494 0.2169 3.59 3.86 0.7913 1.742 0.762 32.033 5.759 0.954 21.009 0.1882 3.12 3.27 0.6867 1.923 0.841 35.367 5.871 0.973 21.417 0.1669 2.77 2.84 0.6090 2.129 0.931 39.160 5.944 0.985 21.684 0.1514 2.51 2.55 0.5524 2.348 1.027 43.184 5.996 0.994 21.873 0.1446 2.40 2.41 0.5276 2.598 1.136 47.782 6.021 0.998 21.964 0.1382 2.29 2.30 0.5041 2.842 1.242 52.266 6.034 1.000 22.012 0.1368 2.27 2.27 0.4992 3.092 1.352 56.864 6.035 1.000 22.016 0.1347 2.23 2.23 0.4913 3.342 1.461 61.463 6.036 1.000 22.019 0.1319 2.19 2.19 0.4811 3.585 1.568 65.946 6.043 1.001 22.046 0.1304 2.16 2.16 0.4758 4.885 2.136 89.858 6.041 1.001 22.037 0.1244 2.06 2.06 0.4539 6.185 2.705 113.770 6.042 1.001 22.040 0.1227 2.03 2.03 0.4477 7.485 3.273 137.682 6.044 1.002 22.047 0.1236 2.05 2.05 0.4509 8.785 3.842 161.593 6.054 1.003 22.084 0.1239 2.05 2.05 0.4521 RUN NUMBER 1W01802 AXIAL POSITION = 195.0 MM SPAN POSITION = 0.0 MM FREE-STREAM VELOCITY = 6.50 M/S FRICTION VELOCITY = 0.2426 M/S FREE-STREAM TURBULENCE = 1.687 % X-REYNOLDS NUMBER = 8.50 X10**4 FLUID DENSITY = 1.213 KG/M**3 KINEMATIC VISCOSITY = 1.491 X10(-5)MSQ/S BOUNDARY LAYER THICKNESS (99.0%) = 3.27 MM DISPLACEMENT THICKNESS = 0.972 MM MOMENTUM THICKNESS = 0.394 MM ENERGY THICKNESS = 0.630 MM FORM FACTOR H = 2.467 FORM FACTOR E = 1.599 RDELTASTAR = 423.5 RTHETA = 171.7 SKIN FRICTION COEFFICIENT = 0.002789 CALCULATED CF = 0.002278 Y Y/DEL YPLUS U U/UO UPLUS u u/UO u/U u/UTAU MM M/S M/S % % 0.029 0.009 0.472 0.115 0.018 0.476 0.0119 0.18 10.31 0.0490 0.035 0.011 0.574 0.140 0.022 0.578 0.0125 0.19 8.88 0.0514 0.042 0.013 0.675 0.165 0.025 0.681 0.0142 0.22 8.61 0.0586 0.048 0.015 0.777 0.190 0.029 0.783 0.0150 0.23 7.88 0.0617 0.054 0.017 0.879 0.215 0.033 0.886 0.0163 0.25 7.57 0.0670 0.060 0.018 0.981 0.240 0.037 0.988 0.0176 0.27 7.34 0.0726 0.067 0.020 1.082 0.265 0.041 1.091 0.0190 0.29 7.18 0.0783 0.073 0.022 1.184 0.290 0.045 1.193 0.0207 0.32 7.17 0.0855 0.079 0.024 1.286 0.314 0.048 1.296 0.0234 0.36 7.45 0.0965 0.085 0.026 1.387 0.339 0.052 1.398 0.0254 0.39 7.48 0.1046 0.092 0.028 1.489 0.364 0.056 1.501 0.0288 0.44 7.91 0.1186 0.098 0.030 1.591 0.389 0.060 1.603 0.0298 0.46 7.65 0.1227 0.104 0.032 1.692 0.414 0.064 1.706 0.0329 0.51 7.95 0.1356 0.110 0.034 1.794 0.439 0.068 1.808 0.0362 0.56 8.24 0.1490 0.123 0.038 1.998 0.489 0.075 2.013 0.0430 0.66 8.81 0.1774 0.135 0.041 2.201 0.538 0.083 2.218 0.0518 0.80 9.62 0.2135 0.154 0.047 2.506 0.613 0.094 2.526 0.0601 0.92 9.80 0.2476 0.173 0.053 2.811 0.687 0.106 2.833 0.0700 1.08 10.18 0.2885 0.192 0.059 3.116 0.762 0.117 3.141 0.0811 1.25 10.64 0.3341 0.210 0.064 3.422 0.834 0.128 3.436 0.0938 1.44 11.25 0.3865 0.235 0.072 3.828 0.917 0.141 3.779 0.1042 1.60 11.36 0.4294 0.260 0.080 4.235 1.010 0.155 4.164 0.1180 1.82 11.68 0.4865 0.292 0.089 4.744 1.096 0.169 4.516 0.1330 2.05 12.13 0.5480 0.323 0.099 5.252 1.218 0.187 5.019 0.1480 2.28 12.15 0.6100 0.360 0.110 5.863 1.371 0.211 5.649 0.1685 2.59 12.29 0.6945 0.398 0.122 6.473 1.549 0.238 6.386 0.1940 2.99 12.52 0.7996 0.442 0.135 7.185 1.746 0.269 7.194 0.2238 3.44 12.82 0.9225 0.492 0.150 7.999 1.952 0.300 8.044 0.2450 3.77 12.55 1.0099 0.548 0.168 8.914 2.199 0.338 9.063 0.2774 4.27 12.62 1.1433 0.610 0.187 9.931 2.434 0.374 10.029 0.3014 4.64 12.38 1.2420 0.679 0.208 11.050 2.712 0.417 11.177 0.3322 5.11 12.25 1.3691 0.754 0.231 12.271 3.015 0.464 12.425 0.3581 5.51 11.88 1.4758 0.835 0.256 13.593 3.313 0.510 13.655 0.3840 5.91 11.59 1.5825 0.929 0.284 15.118 3.619 0.557 14.913 0.4102 6.31 11.34 1.6907 1.035 0.317 16.848 3.958 0.609 16.312 0.4353 6.70 11.00 1.7939 1.148 0.351 18.678 4.278 0.658 17.631 0.4463 6.87 10.43 1.8394 1.279 0.391 20.814 4.614 0.710 19.014 0.4578 7.05 9.92 1.8868 1.417 0.433 23.052 4.941 0.760 20.365 0.4436 6.83 8.98 1.8280 1.579 0.483 25.697 5.274 0.812 21.736 0.4206 6.47 7.97 1.7333 1.754 0.537 28.544 5.582 0.859 23.004 0.3955 6.09 7.08 1.6298 1.948 0.596 31.698 5.813 0.895 23.957 0.3556 5.47 6.12 1.4656 2.160 0.661 35.156 6.014 0.926 24.785 0.3089 4.75 5.14 1.2731 2.404 0.736 39.123 6.179 0.951 25.464 0.2531 3.89 4.10 1.0430 2.673 0.818 43.496 6.305 0.970 25.983 0.2032 3.13 3.22 0.8374 2.967 0.908 48.277 6.388 0.983 26.329 0.1682 2.59 2.63 0.6933 3.298 1.009 53.667 6.446 0.992 26.565 0.1434 2.21 2.22 0.5909 3.629 1.110 59.058 6.476 0.997 26.688 0.1300 2.00 2.01 0.5359 3.954 1.210 64.347 6.487 0.998 26.733 0.1223 1.88 1.88 0.5038 4.285 1.311 69.738 6.505 1.001 26.810 0.1183 1.82 1.82 0.4875 4.617 1.413 75.129 6.508 1.002 26.822 0.1168 1.80 1.79 0.4814 6.267 1.918 101.981 6.510 1.002 26.831 0.1106 1.70 1.70 0.4559 7.917 2.422 128.833 6.512 1.002 26.839 0.1084 1.67 1.66 0.4468 9.567 2.927 155.685 6.517 1.003 26.860 0.1101 1.69 1.69 0.4539 11.217 3.432 182.537 6.521 1.004 26.875 0.1096 1.69 1.68 0.4517 RUN NUMBER 1W01803 AXIAL POSITION = 295.0 MM SPAN POSITION = 0.0 MM FREE-STREAM VELOCITY = 6.72 M/S FRICTION VELOCITY = 0.2305 M/S FREE-STREAM TURBULENCE = 1.483 % X-REYNOLDS NUMBER = 13.21 X10**4 FLUID DENSITY = 1.206 KG/M**3 KINEMATIC VISCOSITY = 1.500 X10(-5)MSQ/S BOUNDARY LAYER THICKNESS (99.0%) = 4.06 MM DISPLACEMENT THICKNESS = 1.161 MM MOMENTUM THICKNESS = 0.484 MM ENERGY THICKNESS = 0.778 MM FORM FACTOR H = 2.400 FORM FACTOR E = 1.608 RDELTASTAR = 520.1 RTHETA = 216.7 SKIN FRICTION COEFFICIENT = 0.002353 CALCULATED CF = 0.001827 Y Y/DEL YPLUS U U/UO UPLUS u u/UO u/U u/UTAU MM M/S M/S % % 0.029 0.007 0.446 0.102 0.015 0.442 0.0123 0.18 12.05 0.0533 0.035 0.009 0.542 0.124 0.018 0.537 0.0147 0.22 11.90 0.0639 0.042 0.010 0.638 0.146 0.022 0.633 0.0157 0.23 10.79 0.0683 0.048 0.012 0.734 0.168 0.025 0.728 0.0169 0.25 10.06 0.0732 0.054 0.013 0.830 0.190 0.028 0.823 0.0183 0.27 9.66 0.0795 0.060 0.015 0.926 0.212 0.032 0.919 0.0193 0.29 9.12 0.0838 0.067 0.016 1.022 0.234 0.035 1.014 0.0221 0.33 9.46 0.0959 0.073 0.018 1.118 0.256 0.038 1.109 0.0241 0.36 9.41 0.1044 0.079 0.019 1.214 0.278 0.041 1.205 0.0265 0.39 9.56 0.1151 0.085 0.021 1.310 0.300 0.045 1.300 0.0283 0.42 9.44 0.1227 0.092 0.023 1.406 0.322 0.048 1.395 0.0309 0.46 9.62 0.1342 0.098 0.024 1.502 0.344 0.051 1.490 0.0358 0.53 10.41 0.1551 0.104 0.026 1.598 0.365 0.054 1.586 0.0385 0.57 10.55 0.1672 0.117 0.029 1.790 0.409 0.061 1.776 0.0453 0.67 11.08 0.1968 0.135 0.033 2.078 0.475 0.071 2.062 0.0554 0.82 11.66 0.2404 0.148 0.036 2.270 0.519 0.077 2.253 0.0614 0.91 11.83 0.2666 0.167 0.041 2.558 0.585 0.087 2.539 0.0757 1.13 12.94 0.3285 0.185 0.046 2.846 0.651 0.097 2.825 0.0900 1.34 13.82 0.3904 0.204 0.050 3.135 0.717 0.107 3.110 0.1021 1.52 14.24 0.4429 0.229 0.056 3.519 0.795 0.118 3.448 0.1138 1.69 14.32 0.4937 0.260 0.064 3.999 0.899 0.134 3.900 0.1415 2.11 15.74 0.6138 0.292 0.072 4.479 1.010 0.150 4.383 0.1550 2.31 15.34 0.6725 0.323 0.080 4.959 1.130 0.168 4.901 0.1724 2.57 15.26 0.7479 0.360 0.089 5.535 1.274 0.190 5.527 0.2098 3.12 16.47 0.9102 0.404 0.100 6.208 1.434 0.213 6.222 0.2295 3.42 16.00 0.9958 0.454 0.112 6.976 1.617 0.241 7.018 0.2555 3.80 15.79 1.1084 0.504 0.124 7.744 1.799 0.268 7.806 0.2804 4.17 15.59 1.2167 0.560 0.138 8.608 2.000 0.298 8.677 0.3104 4.62 15.52 1.3469 0.629 0.155 9.665 2.275 0.339 9.873 0.3675 5.47 16.15 1.5947 0.704 0.174 10.817 2.501 0.372 10.852 0.3891 5.79 15.56 1.6884 0.785 0.194 12.066 2.809 0.418 12.188 0.4262 6.34 15.17 1.8493 0.873 0.215 13.410 3.090 0.460 13.405 0.4540 6.76 14.70 1.9700 0.979 0.241 15.043 3.395 0.505 14.732 0.5015 7.46 14.77 2.1759 1.092 0.269 16.771 3.724 0.554 16.159 0.5220 7.77 14.02 2.2650 1.217 0.300 18.692 4.056 0.604 17.596 0.5374 8.00 13.25 2.3319 1.360 0.335 20.901 4.455 0.663 19.330 0.5636 8.39 12.65 2.4455 1.523 0.376 23.397 4.819 0.717 20.910 0.5634 8.38 11.69 2.4445 1.698 0.419 26.086 5.136 0.764 22.282 0.5569 8.29 10.84 2.4161 1.898 0.468 29.159 5.452 0.811 23.657 0.5362 7.98 9.83 2.3264 2.117 0.522 32.521 5.751 0.856 24.953 0.4893 7.28 8.51 2.1231 2.360 0.582 36.266 5.972 0.889 25.913 0.4486 6.68 7.51 1.9465 2.635 0.650 40.491 6.195 0.922 26.878 0.3705 5.51 5.98 1.6075 2.942 0.725 45.197 6.390 0.951 27.724 0.3135 4.67 4.91 1.3603 3.285 0.810 50.479 6.525 0.971 28.313 0.2371 3.53 3.63 1.0286 3.673 0.906 56.433 6.610 0.984 28.679 0.1865 2.78 2.82 0.8092 4.098 1.010 62.963 6.664 0.992 28.914 0.1510 2.25 2.27 0.6551 4.523 1.115 69.493 6.695 0.996 29.047 0.1282 1.91 1.92 0.5563 4.954 1.222 76.120 6.717 1.000 29.145 0.1155 1.72 1.72 0.5013 5.379 1.326 82.650 6.724 1.001 29.176 0.1108 1.65 1.65 0.4805 5.804 1.431 89.180 6.729 1.002 29.198 0.1055 1.57 1.57 0.4576 7.854 1.937 120.679 6.733 1.002 29.215 0.1011 1.50 1.50 0.4385 9.904 2.442 152.178 6.736 1.002 29.226 0.0987 1.47 1.47 0.4283 11.954 2.948 183.677 6.737 1.003 29.230 0.0984 1.47 1.46 0.4271 14.004 3.453 215.176 6.737 1.003 29.233 0.0997 1.48 1.48 0.4324 RUN NUMBER 1W01804 AXIAL POSITION = 395.0 MM SPAN POSITION = 0.0 MM FREE-STREAM VELOCITY = 6.94 M/S FRICTION VELOCITY = 0.2266 M/S FREE-STREAM TURBULENCE = 1.316 % X-REYNOLDS NUMBER = 18.26 X10**4 FLUID DENSITY = 1.205 KG/M**3 KINEMATIC VISCOSITY = 1.501 X10(-5)MSQ/S BOUNDARY LAYER THICKNESS (99.0%) = 4.65 MM DISPLACEMENT THICKNESS = 1.274 MM MOMENTUM THICKNESS = 0.545 MM ENERGY THICKNESS = 0.882 MM FORM FACTOR H = 2.339 FORM FACTOR E = 1.619 RDELTASTAR = 588.6 RTHETA = 251.7 SKIN FRICTION COEFFICIENT = 0.002134 CALCULATED CF = 0.001554 Y Y/DEL YPLUS U U/UO UPLUS u u/UO u/U u/UTAU MM M/S M/S % % 0.029 0.006 0.438 0.096 0.014 0.422 0.0135 0.20 14.14 0.0597 0.035 0.008 0.532 0.116 0.017 0.513 0.0165 0.24 14.17 0.0727 0.042 0.009 0.626 0.137 0.020 0.604 0.0167 0.24 12.16 0.0735 0.048 0.010 0.721 0.158 0.023 0.696 0.0179 0.26 11.37 0.0791 0.054 0.012 0.815 0.178 0.026 0.787 0.0197 0.28 11.05 0.0869 0.060 0.013 0.910 0.199 0.029 0.878 0.0217 0.31 10.94 0.0960 0.067 0.014 1.004 0.219 0.032 0.969 0.0251 0.36 11.44 0.1108 0.073 0.016 1.098 0.240 0.035 1.060 0.0269 0.39 11.18 0.1185 0.079 0.017 1.193 0.261 0.038 1.151 0.0289 0.42 11.08 0.1276 0.085 0.018 1.287 0.281 0.041 1.242 0.0310 0.45 11.03 0.1369 0.092 0.020 1.381 0.302 0.044 1.333 0.0335 0.48 11.11 0.1481 0.098 0.021 1.476 0.323 0.047 1.424 0.0387 0.56 11.99 0.1708 0.110 0.024 1.664 0.364 0.052 1.606 0.0426 0.61 11.71 0.1881 0.123 0.026 1.853 0.405 0.058 1.788 0.0513 0.74 12.66 0.2264 0.135 0.029 2.042 0.446 0.064 1.970 0.0574 0.83 12.86 0.2534 0.154 0.033 2.325 0.508 0.073 2.243 0.0684 0.99 13.45 0.3017 0.173 0.037 2.608 0.570 0.082 2.516 0.0810 1.17 14.21 0.3574 0.198 0.043 2.985 0.653 0.094 2.880 0.0962 1.39 14.74 0.4246 0.217 0.047 3.268 0.714 0.103 3.153 0.1105 1.59 15.46 0.4876 0.248 0.053 3.740 0.834 0.120 3.682 0.1361 1.96 16.31 0.6006 0.273 0.059 4.118 0.929 0.134 4.102 0.1546 2.23 16.63 0.6822 0.310 0.067 4.684 1.041 0.150 4.594 0.1675 2.41 16.10 0.7394 0.348 0.075 5.250 1.171 0.169 5.170 0.2025 2.92 17.29 0.8937 0.385 0.083 5.816 1.306 0.188 5.764 0.2226 3.21 17.04 0.9823 0.435 0.094 6.571 1.482 0.214 6.542 0.2590 3.73 17.48 1.1432 0.485 0.104 7.325 1.691 0.244 7.462 0.3023 4.36 17.88 1.3342 0.548 0.118 8.269 1.886 0.272 8.325 0.3314 4.78 17.57 1.4626 0.610 0.131 9.212 2.130 0.307 9.402 0.3700 5.33 17.37 1.6330 0.685 0.147 10.345 2.396 0.345 10.577 0.4207 6.07 17.56 1.8568 0.767 0.165 11.571 2.693 0.388 11.886 0.4554 6.57 16.91 2.0100 0.860 0.185 12.987 2.997 0.432 13.228 0.4752 6.85 15.86 2.0976 0.960 0.207 14.496 3.318 0.478 14.643 0.5200 7.50 15.68 2.2953 1.079 0.232 16.289 3.613 0.521 15.948 0.5745 8.28 15.90 2.5358 1.204 0.259 18.176 3.975 0.573 17.544 0.5973 8.61 15.03 2.6362 1.354 0.291 20.440 4.309 0.621 19.017 0.6274 9.04 14.56 2.7691 1.517 0.326 22.893 4.663 0.672 20.582 0.6298 9.08 13.50 2.7796 1.698 0.365 25.630 5.047 0.728 22.278 0.6259 9.02 12.40 2.7624 1.898 0.408 28.649 5.365 0.773 23.679 0.6056 8.73 11.29 2.6731 2.129 0.458 32.140 5.676 0.818 25.051 0.5830 8.41 10.27 2.5733 2.379 0.512 35.914 5.935 0.856 26.195 0.5499 7.93 9.27 2.4270 2.667 0.574 40.254 6.214 0.896 27.425 0.4886 7.04 7.86 2.1565 2.985 0.642 45.066 6.430 0.927 28.380 0.4120 5.94 6.41 1.8183 3.348 0.720 50.539 6.595 0.951 29.108 0.3540 5.10 5.37 1.5626 3.748 0.806 56.577 6.725 0.970 29.683 0.2816 4.06 4.19 1.2429 4.192 0.902 63.276 6.814 0.982 30.076 0.2183 3.15 3.20 0.9634 4.698 1.011 70.919 6.884 0.993 30.386 0.1580 2.28 2.29 0.6973 5.198 1.118 78.467 6.914 0.997 30.516 0.1323 1.91 1.91 0.5841 5.704 1.227 86.109 6.928 0.999 30.579 0.1175 1.69 1.70 0.5185 6.204 1.335 93.657 6.943 1.001 30.643 0.1046 1.51 1.51 0.4619 6.704 1.443 101.205 6.947 1.002 30.662 0.1002 1.44 1.44 0.4421 9.054 1.948 136.682 6.947 1.001 30.661 0.0922 1.33 1.33 0.4071 11.404 2.454 172.158 6.955 1.003 30.700 0.0921 1.33 1.32 0.4065 13.754 2.959 207.634 6.953 1.002 30.690 0.0913 1.32 1.31 0.4032 16.104 3.465 243.110 6.956 1.003 30.700 0.0913 1.32 1.31 0.4028 RUN NUMBER 1W01805 AXIAL POSITION = 495.0 MM SPAN POSITION = 0.0 MM FREE-STREAM VELOCITY = 7.20 M/S FRICTION VELOCITY = 0.2323 M/S FREE-STREAM TURBULENCE = 1.181 % X-REYNOLDS NUMBER = 23.69 X10**4 FLUID DENSITY = 1.203 KG/M**3 KINEMATIC VISCOSITY = 1.503 X10(-5)MSQ/S BOUNDARY LAYER THICKNESS (99.0%) = 5.26 MM DISPLACEMENT THICKNESS = 1.331 MM MOMENTUM THICKNESS = 0.589 MM ENERGY THICKNESS = 0.961 MM FORM FACTOR H = 2.260 FORM FACTOR E = 1.632 RDELTASTAR = 637.3 RTHETA = 281.9 SKIN FRICTION COEFFICIENT = 0.002086 CALCULATED CF = 0.001364 Y Y/DEL YPLUS U U/UO UPLUS u u/UO u/U u/UTAU MM M/S M/S % % 0.029 0.006 0.448 0.105 0.015 0.450 0.0157 0.22 15.02 0.0676 0.035 0.007 0.545 0.127 0.018 0.547 0.0170 0.24 13.40 0.0734 0.042 0.008 0.641 0.150 0.021 0.644 0.0182 0.25 12.13 0.0782 0.048 0.009 0.738 0.172 0.024 0.742 0.0210 0.29 12.18 0.0903 0.054 0.010 0.835 0.195 0.027 0.839 0.0217 0.30 11.16 0.0936 0.060 0.011 0.931 0.217 0.030 0.936 0.0245 0.34 11.26 0.1054 0.067 0.013 1.028 0.240 0.033 1.033 0.0266 0.37 11.10 0.1147 0.073 0.014 1.124 0.262 0.036 1.130 0.0304 0.42 11.58 0.1308 0.079 0.015 1.221 0.285 0.040 1.227 0.0337 0.47 11.83 0.1451 0.085 0.016 1.318 0.308 0.043 1.324 0.0380 0.53 12.35 0.1635 0.092 0.017 1.414 0.330 0.046 1.421 0.0392 0.55 11.88 0.1688 0.104 0.020 1.608 0.375 0.052 1.615 0.0484 0.67 12.90 0.2084 0.117 0.022 1.801 0.420 0.058 1.809 0.0556 0.77 13.22 0.2392 0.129 0.025 1.994 0.465 0.065 2.003 0.0663 0.92 14.24 0.2852 0.142 0.027 2.187 0.511 0.071 2.197 0.0771 1.07 15.09 0.3317 0.160 0.030 2.477 0.578 0.080 2.488 0.0927 1.29 16.03 0.3989 0.185 0.035 2.863 0.668 0.093 2.877 0.1169 1.62 17.49 0.5031 0.204 0.039 3.153 0.736 0.102 3.168 0.1288 1.79 17.49 0.5542 0.229 0.044 3.540 0.822 0.114 3.537 0.1396 1.94 16.99 0.6008 0.260 0.049 4.023 0.927 0.129 3.989 0.1747 2.43 18.85 0.7519 0.292 0.055 4.506 1.034 0.144 4.452 0.1952 2.71 18.87 0.8400 0.329 0.063 5.085 1.175 0.163 5.055 0.2150 2.99 18.31 0.9255 0.373 0.071 5.762 1.337 0.186 5.754 0.2589 3.60 19.37 1.1144 0.417 0.079 6.438 1.486 0.207 6.397 0.2930 4.07 19.71 1.2611 0.467 0.089 7.211 1.677 0.233 7.217 0.3294 4.58 19.65 1.4178 0.529 0.101 8.177 1.922 0.267 8.271 0.3589 4.99 18.68 1.5446 0.592 0.112 9.143 2.127 0.296 9.155 0.3974 5.52 18.68 1.7102 0.667 0.127 10.302 2.386 0.332 10.271 0.4370 6.07 18.31 1.8809 0.748 0.142 11.558 2.703 0.376 11.635 0.4811 6.69 17.80 2.0708 0.842 0.160 13.007 2.996 0.416 12.895 0.5182 7.20 17.30 2.2302 0.942 0.179 14.553 3.285 0.457 14.139 0.5708 7.93 17.37 2.4566 1.060 0.202 16.388 3.651 0.507 15.716 0.6084 8.46 16.66 2.6184 1.192 0.226 18.417 3.995 0.555 17.195 0.6319 8.78 15.82 2.7198 1.335 0.254 20.639 4.376 0.608 18.834 0.6652 9.25 15.20 2.8630 1.504 0.286 23.247 4.756 0.661 20.469 0.6964 9.68 14.64 2.9974 1.685 0.320 26.049 5.155 0.716 22.187 0.6702 9.31 13.00 2.8843 1.898 0.361 29.333 5.466 0.760 23.527 0.6838 9.50 12.51 2.9431 2.129 0.405 32.908 5.779 0.803 24.871 0.6362 8.84 11.01 2.7380 2.392 0.455 36.965 6.058 0.842 26.074 0.5942 8.26 9.81 2.5575 2.685 0.510 41.505 6.308 0.877 27.149 0.5598 7.78 8.88 2.4095 3.017 0.573 46.625 6.573 0.914 28.289 0.4703 6.54 7.16 2.0241 3.392 0.645 52.422 6.752 0.938 29.061 0.4057 5.64 6.01 1.7462 3.810 0.724 58.894 6.897 0.959 29.686 0.3493 4.85 5.06 1.5034 4.279 0.813 66.140 7.004 0.973 30.142 0.2751 3.82 3.93 1.1838 4.804 0.913 74.254 7.087 0.985 30.502 0.2119 2.95 2.99 0.9122 5.398 1.026 83.432 7.142 0.993 30.740 0.1626 2.26 2.28 0.6998 5.992 1.139 92.609 7.171 0.997 30.865 0.1269 1.76 1.77 0.5462 6.579 1.251 101.690 7.192 1.000 30.954 0.1088 1.51 1.51 0.4682 7.173 1.363 110.868 7.201 1.001 30.993 0.1002 1.39 1.39 0.4312 7.767 1.476 120.045 7.202 1.001 30.997 0.0948 1.32 1.32 0.4078 10.467 1.990 161.779 7.208 1.002 31.020 0.0844 1.17 1.17 0.3631 13.167 2.503 203.512 7.207 1.002 31.019 0.0847 1.18 1.17 0.3643 15.867 3.016 245.245 7.215 1.003 31.054 0.0850 1.18 1.18 0.3660 18.567 3.529 286.979 7.217 1.003 31.063 0.0850 1.18 1.18 0.3657 RUN NUMBER 1W01806 AXIAL POSITION = 595.0 MM SPAN POSITION = 0.0 MM FREE-STREAM VELOCITY = 7.43 M/S FRICTION VELOCITY = 0.2321 M/S FREE-STREAM TURBULENCE = 1.076 % X-REYNOLDS NUMBER = 29.37 X10**4 FLUID DENSITY = 1.201 KG/M**3 KINEMATIC VISCOSITY = 1.506 X10(-5)MSQ/S BOUNDARY LAYER THICKNESS (99.0%) = 5.82 MM DISPLACEMENT THICKNESS = 1.404 MM MOMENTUM THICKNESS = 0.634 MM ENERGY THICKNESS = 1.040 MM FORM FACTOR H = 2.216 FORM FACTOR E = 1.641 RDELTASTAR = 693.2 RTHETA = 312.8 SKIN FRICTION COEFFICIENT = 0.001952 CALCULATED CF = 0.001225 Y Y/DEL YPLUS U U/UO UPLUS u u/UO u/U u/UTAU MM M/S M/S % % 0.029 0.005 0.447 0.102 0.014 0.438 0.0197 0.26 19.35 0.0848 0.035 0.006 0.544 0.124 0.017 0.532 0.0210 0.28 17.00 0.0905 0.042 0.007 0.640 0.145 0.020 0.627 0.0250 0.34 17.16 0.1075 0.048 0.008 0.736 0.167 0.023 0.721 0.0259 0.35 15.49 0.1117 0.054 0.009 0.833 0.189 0.025 0.815 0.0277 0.37 14.64 0.1194 0.060 0.010 0.929 0.211 0.028 0.910 0.0296 0.40 14.03 0.1276 0.067 0.011 1.025 0.233 0.031 1.004 0.0328 0.44 14.09 0.1415 0.073 0.012 1.122 0.255 0.034 1.099 0.0344 0.46 13.50 0.1483 0.079 0.014 1.218 0.277 0.037 1.193 0.0373 0.50 13.47 0.1606 0.085 0.015 1.314 0.299 0.040 1.287 0.0425 0.57 14.24 0.1833 0.092 0.016 1.411 0.321 0.043 1.382 0.0507 0.68 15.80 0.2183 0.104 0.018 1.604 0.365 0.049 1.570 0.0577 0.78 15.82 0.2485 0.117 0.020 1.796 0.408 0.055 1.759 0.0763 1.03 18.68 0.3287 0.135 0.023 2.085 0.474 0.064 2.042 0.0839 1.13 17.70 0.3614 0.148 0.025 2.278 0.518 0.070 2.231 0.1042 1.40 20.11 0.4487 0.167 0.029 2.567 0.584 0.079 2.514 0.1127 1.52 19.32 0.4856 0.192 0.033 2.953 0.671 0.090 2.892 0.1298 1.75 19.33 0.5591 0.217 0.037 3.338 0.759 0.102 3.269 0.1669 2.25 21.99 0.7190 0.242 0.041 3.724 0.852 0.115 3.669 0.1836 2.47 21.56 0.7910 0.273 0.047 4.205 0.963 0.130 4.147 0.2066 2.78 21.46 0.8898 0.310 0.053 4.784 1.095 0.147 4.719 0.2437 3.28 22.25 1.0498 0.348 0.060 5.362 1.235 0.166 5.320 0.2610 3.51 21.13 1.1242 0.392 0.067 6.036 1.389 0.187 5.985 0.3058 4.11 22.01 1.3172 0.442 0.076 6.807 1.601 0.215 6.897 0.3555 4.78 22.20 1.5315 0.498 0.086 7.675 1.783 0.240 7.681 0.3674 4.94 20.61 1.5826 0.560 0.096 8.638 2.038 0.274 8.779 0.4319 5.81 21.19 1.8604 0.635 0.109 9.795 2.332 0.314 10.044 0.4694 6.32 20.13 2.0218 0.717 0.123 11.047 2.639 0.355 11.369 0.5153 6.93 19.53 2.2199 0.804 0.138 12.396 2.901 0.390 12.498 0.5551 7.47 19.13 2.3913 0.910 0.156 14.035 3.238 0.436 13.948 0.6193 8.33 19.13 2.6678 1.023 0.176 15.769 3.574 0.481 15.397 0.6484 8.73 18.14 2.7931 1.154 0.198 17.793 3.931 0.529 16.935 0.6925 9.32 17.61 2.9829 1.298 0.223 20.009 4.305 0.579 18.544 0.7073 9.52 16.43 3.0469 1.460 0.251 22.515 4.708 0.634 20.282 0.7322 9.85 15.55 3.1541 1.648 0.283 25.406 5.057 0.680 21.784 0.7572 10.19 14.97 3.2617 1.854 0.319 28.586 5.481 0.738 23.609 0.7089 9.54 12.94 3.0539 2.092 0.359 32.248 5.814 0.782 25.043 0.7089 9.54 12.19 3.0539 2.354 0.404 36.295 6.071 0.817 26.150 0.6830 9.19 11.25 2.9419 2.654 0.456 40.921 6.330 0.852 27.268 0.6333 8.52 10.00 2.7281 2.985 0.513 46.028 6.671 0.898 28.735 0.5491 7.39 8.23 2.3653 3.367 0.578 51.906 6.870 0.924 29.594 0.4705 6.33 6.85 2.0269 3.792 0.651 58.459 7.011 0.944 30.203 0.4220 5.68 6.02 1.8178 4.267 0.733 65.783 7.158 0.963 30.835 0.3370 4.53 4.71 1.4517 4.804 0.825 74.070 7.262 0.977 31.283 0.2648 3.56 3.65 1.1407 5.410 0.930 83.418 7.334 0.987 31.593 0.2008 2.70 2.74 0.8652 6.098 1.048 94.018 7.374 0.992 31.765 0.1633 2.20 2.21 0.7035 6.779 1.165 104.522 7.413 0.997 31.931 0.1205 1.62 1.63 0.5191 7.467 1.283 115.122 7.427 0.999 31.992 0.1048 1.41 1.41 0.4513 8.148 1.400 125.626 7.427 0.999 31.991 0.0928 1.25 1.25 0.3999 8.829 1.517 136.130 7.441 1.001 32.054 0.0855 1.15 1.15 0.3683 11.879 2.041 183.156 7.444 1.002 32.067 0.0799 1.08 1.07 0.3442 14.929 2.565 230.183 7.447 1.002 32.079 0.0794 1.07 1.07 0.3421 17.979 3.089 277.209 7.452 1.003 32.100 0.0808 1.09 1.08 0.3482 21.029 3.613 324.235 7.458 1.004 32.125 0.0800 1.08 1.07 0.3445 RUN NUMBER 1W01807 AXIAL POSITION = 695.0 MM SPAN POSITION = 0.0 MM FREE-STREAM VELOCITY = 7.68 M/S FRICTION VELOCITY = 0.2370 M/S FREE-STREAM TURBULENCE = 0.993 % X-REYNOLDS NUMBER = 35.25 X10**4 FLUID DENSITY = 1.194 KG/M**3 KINEMATIC VISCOSITY = 1.514 X10(-5)MSQ/S BOUNDARY LAYER THICKNESS (99.0%) = 6.35 MM DISPLACEMENT THICKNESS = 1.448 MM MOMENTUM THICKNESS = 0.672 MM ENERGY THICKNESS = 1.111 MM FORM FACTOR H = 2.155 FORM FACTOR E = 1.654 RDELTASTAR = 734.4 RTHETA = 340.8 SKIN FRICTION COEFFICIENT = 0.001904 CALCULATED CF = 0.001118 Y Y/DEL YPLUS U U/UO UPLUS u u/UO u/U u/UTAU MM M/S M/S % % 0.029 0.005 0.454 0.106 0.014 0.449 0.0259 0.34 24.33 0.1092 0.035 0.006 0.552 0.129 0.017 0.546 0.0325 0.42 25.17 0.1373 0.042 0.007 0.649 0.152 0.020 0.642 0.0341 0.44 22.41 0.1440 0.048 0.008 0.747 0.175 0.023 0.739 0.0384 0.50 21.91 0.1619 0.054 0.009 0.845 0.198 0.026 0.836 0.0360 0.47 18.15 0.1517 0.060 0.009 0.943 0.221 0.029 0.933 0.0436 0.57 19.72 0.1839 0.067 0.010 1.041 0.244 0.032 1.029 0.0483 0.63 19.79 0.2038 0.073 0.011 1.138 0.267 0.035 1.126 0.0552 0.72 20.68 0.2328 0.079 0.012 1.236 0.290 0.038 1.223 0.0628 0.82 21.67 0.2650 0.085 0.013 1.334 0.313 0.041 1.320 0.0639 0.83 20.44 0.2697 0.092 0.014 1.432 0.336 0.044 1.416 0.0787 1.03 23.46 0.3323 0.104 0.016 1.627 0.381 0.050 1.610 0.0942 1.23 24.69 0.3974 0.123 0.019 1.921 0.450 0.059 1.900 0.1211 1.58 26.90 0.5112 0.135 0.021 2.116 0.496 0.065 2.094 0.1394 1.81 28.10 0.5882 0.154 0.024 2.410 0.565 0.074 2.384 0.1591 2.07 28.17 0.6715 0.173 0.027 2.703 0.634 0.083 2.674 0.1729 2.25 27.29 0.7298 0.198 0.031 3.094 0.725 0.094 3.061 0.2083 2.71 28.72 0.8790 0.223 0.035 3.485 0.801 0.104 3.380 0.2365 3.08 29.52 0.9980 0.254 0.040 3.974 0.913 0.119 3.855 0.2697 3.51 29.53 1.1382 0.285 0.045 4.463 1.026 0.134 4.329 0.2991 3.89 29.15 1.2620 0.323 0.051 5.050 1.155 0.150 4.876 0.3288 4.28 28.46 1.3878 0.367 0.058 5.735 1.344 0.175 5.672 0.3923 5.11 29.19 1.6556 0.417 0.066 6.517 1.560 0.203 6.583 0.4248 5.53 27.23 1.7926 0.467 0.073 7.300 1.765 0.230 7.450 0.4757 6.19 26.94 2.0074 0.529 0.083 8.277 2.006 0.261 8.465 0.5196 6.77 25.90 2.1926 0.598 0.094 9.353 2.287 0.298 9.652 0.6003 7.82 26.25 2.5335 0.673 0.106 10.527 2.523 0.328 10.646 0.6046 7.87 23.97 2.5516 0.760 0.120 11.896 2.889 0.376 12.192 0.6778 8.83 23.46 2.8604 0.860 0.135 13.461 3.192 0.416 13.470 0.6621 8.62 20.74 2.7942 0.973 0.153 15.221 3.543 0.461 14.950 0.7268 9.46 20.52 3.0671 1.098 0.173 17.177 3.934 0.512 16.602 0.7686 10.01 19.54 3.2434 1.242 0.196 19.426 4.264 0.555 17.993 0.7997 10.41 18.76 3.3750 1.404 0.221 21.969 4.745 0.618 20.025 0.8017 10.44 16.90 3.3834 1.585 0.250 24.805 5.077 0.661 21.427 0.7976 10.39 15.71 3.3658 1.785 0.281 27.935 5.474 0.713 23.101 0.8079 10.52 14.76 3.4094 2.017 0.318 31.553 5.820 0.758 24.561 0.7749 10.09 13.31 3.2702 2.279 0.359 35.661 6.162 0.802 26.006 0.7393 9.63 12.00 3.1200 2.573 0.405 40.257 6.421 0.836 27.096 0.7161 9.32 11.15 3.0221 2.904 0.457 45.440 6.718 0.875 28.349 0.6534 8.51 9.73 2.7573 3.279 0.516 51.308 6.974 0.908 29.431 0.5589 7.28 8.01 2.3586 3.704 0.583 57.958 7.108 0.926 29.996 0.5174 6.74 7.28 2.1834 4.185 0.659 65.488 7.301 0.951 30.812 0.4218 5.49 5.78 1.7800 4.723 0.744 73.899 7.430 0.968 31.357 0.3426 4.46 4.61 1.4456 5.335 0.840 83.483 7.516 0.979 31.717 0.2715 3.54 3.61 1.1460 6.023 0.949 94.241 7.592 0.989 32.039 0.2098 2.73 2.76 0.8853 6.798 1.071 106.367 7.631 0.994 32.206 0.1650 2.15 2.16 0.6964 7.573 1.193 118.494 7.657 0.997 32.314 0.1351 1.76 1.76 0.5700 8.348 1.315 130.621 7.675 0.999 32.390 0.1080 1.41 1.41 0.4559 9.129 1.438 142.846 7.681 1.000 32.413 0.0917 1.19 1.19 0.3872 9.904 1.560 154.972 7.688 1.001 32.445 0.0863 1.12 1.12 0.3641 13.304 2.095 208.174 7.690 1.001 32.454 0.0761 0.99 0.99 0.3212 16.704 2.631 261.375 7.697 1.002 32.483 0.0752 0.98 0.98 0.3175 20.104 3.166 314.576 7.697 1.002 32.484 0.0761 0.99 0.99 0.3213 23.504 3.702 367.778 7.702 1.003 32.503 0.0763 0.99 0.99 0.3219 RUN NUMBER 1W01808 AXIAL POSITION = 795.0 MM SPAN POSITION = 0.0 MM FREE-STREAM VELOCITY = 7.84 M/S FRICTION VELOCITY = 0.2344 M/S FREE-STREAM TURBULENCE = 0.931 % X-REYNOLDS NUMBER = 41.16 X10**4 FLUID DENSITY = 1.194 KG/M**3 KINEMATIC VISCOSITY = 1.514 X10(-5)MSQ/S BOUNDARY LAYER THICKNESS (99.0%) = 6.95 MM DISPLACEMENT THICKNESS = 1.551 MM MOMENTUM THICKNESS = 0.729 MM ENERGY THICKNESS = 1.209 MM FORM FACTOR H = 2.127 FORM FACTOR E = 1.658 RDELTASTAR = 802.9 RTHETA = 377.5 SKIN FRICTION COEFFICIENT = 0.001787 CALCULATED CF = 0.001035 Y Y/DEL YPLUS U U/UO UPLUS u u/UO u/U u/UTAU MM M/S M/S % % 0.029 0.004 0.449 0.107 0.014 0.456 0.0424 0.54 39.65 0.1810 0.035 0.005 0.546 0.130 0.017 0.555 0.0464 0.59 35.67 0.1979 0.042 0.006 0.642 0.153 0.020 0.653 0.0551 0.70 35.98 0.2350 0.048 0.007 0.739 0.176 0.022 0.752 0.0574 0.73 32.59 0.2450 0.054 0.008 0.836 0.199 0.025 0.850 0.0730 0.93 36.64 0.3114 0.060 0.009 0.933 0.222 0.028 0.948 0.0714 0.91 32.11 0.3045 0.067 0.010 1.029 0.245 0.031 1.047 0.0901 1.15 36.75 0.3846 0.073 0.010 1.126 0.268 0.034 1.145 0.0956 1.22 35.60 0.4077 0.079 0.011 1.223 0.291 0.037 1.243 0.1096 1.40 37.62 0.4678 0.085 0.012 1.319 0.314 0.040 1.342 0.1219 1.55 38.76 0.5200 0.098 0.014 1.513 0.361 0.046 1.538 0.1323 1.69 36.70 0.5646 0.110 0.016 1.706 0.407 0.052 1.735 0.1443 1.84 35.47 0.6155 0.123 0.018 1.900 0.453 0.058 1.932 0.1829 2.33 40.38 0.7802 0.142 0.020 2.190 0.522 0.067 2.227 0.1969 2.51 37.72 0.8401 0.160 0.023 2.480 0.591 0.075 2.522 0.2440 3.11 41.28 1.0411 0.179 0.026 2.771 0.660 0.084 2.817 0.2780 3.55 42.10 1.1862 0.204 0.029 3.157 0.753 0.096 3.211 0.3282 4.19 43.61 1.4003 0.229 0.033 3.544 0.818 0.104 3.488 0.3619 4.62 44.27 1.5440 0.260 0.037 4.028 0.950 0.121 4.052 0.4448 5.67 46.83 1.8977 0.298 0.043 4.608 1.055 0.135 4.500 0.4418 5.63 41.89 1.8849 0.335 0.048 5.189 1.198 0.153 5.110 0.4830 6.16 40.33 2.0608 0.379 0.055 5.866 1.355 0.173 5.780 0.5580 7.12 41.20 2.3809 0.429 0.062 6.640 1.534 0.196 6.546 0.5904 7.53 38.48 2.5189 0.485 0.070 7.511 1.774 0.226 7.570 0.6553 8.36 36.93 2.7957 0.548 0.079 8.478 2.002 0.255 8.544 0.6942 8.85 34.67 2.9619 0.623 0.090 9.639 2.309 0.295 9.851 0.7624 9.72 33.02 3.2529 0.704 0.101 10.896 2.574 0.328 10.984 0.7733 9.86 30.04 3.2992 0.798 0.115 12.347 2.888 0.368 12.321 0.8077 10.30 27.97 3.4461 0.904 0.130 13.992 3.261 0.416 13.914 0.8444 10.77 25.89 3.6027 1.017 0.146 15.733 3.609 0.460 15.399 0.8825 11.26 24.45 3.7652 1.154 0.166 17.861 3.998 0.510 17.056 0.8609 10.98 21.53 3.6731 1.304 0.188 20.183 4.387 0.560 18.719 0.8833 11.27 20.13 3.7684 1.473 0.212 22.795 4.758 0.607 20.301 0.8780 11.20 18.45 3.7462 1.667 0.240 25.794 5.178 0.660 22.092 0.8545 10.90 16.50 3.6457 1.885 0.271 29.179 5.572 0.711 23.775 0.8796 11.22 15.78 3.7527 2.135 0.307 33.049 5.917 0.755 25.247 0.8412 10.73 14.21 3.5888 2.410 0.347 37.305 6.252 0.797 26.675 0.8016 10.22 12.82 3.4202 2.729 0.393 42.239 6.576 0.839 28.057 0.7667 9.78 11.66 3.2712 3.085 0.444 47.753 6.824 0.870 29.115 0.7108 9.07 10.42 3.0328 3.492 0.502 54.041 7.066 0.901 30.148 0.6203 7.91 8.78 2.6466 3.948 0.568 61.102 7.258 0.926 30.966 0.5399 6.89 7.44 2.3034 4.460 0.642 69.035 7.417 0.946 31.644 0.4739 6.04 6.39 2.0221 5.048 0.726 78.128 7.538 0.962 32.163 0.3923 5.00 5.20 1.6737 5.704 0.821 88.285 7.672 0.979 32.733 0.2971 3.79 3.87 1.2675 6.454 0.929 99.893 7.741 0.987 33.026 0.2346 2.99 3.03 1.0009 7.298 1.050 112.953 7.785 0.993 33.216 0.1782 2.27 2.29 0.7605 8.142 1.172 126.012 7.809 0.996 33.317 0.1479 1.89 1.89 0.6312 8.985 1.293 139.071 7.829 0.999 33.404 0.1198 1.53 1.53 0.5113 9.829 1.414 152.131 7.842 1.000 33.460 0.0972 1.24 1.24 0.4146 10.673 1.536 165.190 7.846 1.001 33.477 0.0874 1.11 1.11 0.3727 14.323 2.061 221.684 7.856 1.002 33.516 0.0735 0.94 0.94 0.3136 17.973 2.586 278.178 7.859 1.002 33.532 0.0719 0.92 0.91 0.3066 21.623 3.112 334.671 7.865 1.003 33.555 0.0731 0.93 0.93 0.3117 25.273 3.637 391.165 7.870 1.004 33.578 0.0730 0.93 0.93 0.3113 RUN NUMBER 1W01809 AXIAL POSITION = 895.0 MM SPAN POSITION = 0.0 MM FREE-STREAM VELOCITY = 7.91 M/S FRICTION VELOCITY = 0.2368 M/S FREE-STREAM TURBULENCE = 0.888 % X-REYNOLDS NUMBER = 46.75 X10**4 FLUID DENSITY = 1.194 KG/M**3 KINEMATIC VISCOSITY = 1.515 X10(-5)MSQ/S BOUNDARY LAYER THICKNESS (99.0%) = 8.02 MM DISPLACEMENT THICKNESS = 1.694 MM MOMENTUM THICKNESS = 0.825 MM ENERGY THICKNESS = 1.374 MM FORM FACTOR H = 2.053 FORM FACTOR E = 1.665 RDELTASTAR = 884.7 RTHETA = 431.0 SKIN FRICTION COEFFICIENT = 0.001791 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 0.004 0.453 0.109 0.014 0.462 0.0586 0.74 53.62 0.2476 0.035 0.004 0.551 0.133 0.017 0.561 0.0705 0.89 53.01 0.2976 0.042 0.005 0.649 0.156 0.020 0.661 0.0814 1.03 52.01 0.3437 0.048 0.006 0.746 0.180 0.023 0.760 0.0839 1.06 46.57 0.3542 0.054 0.007 0.844 0.204 0.026 0.860 0.0945 1.19 46.39 0.3989 0.060 0.008 0.942 0.227 0.029 0.959 0.1113 1.41 48.99 0.4701 0.067 0.008 1.040 0.251 0.032 1.059 0.1188 1.50 47.38 0.5017 0.073 0.009 1.137 0.274 0.035 1.159 0.1329 1.68 48.43 0.5611 0.079 0.010 1.235 0.298 0.038 1.258 0.1493 1.89 50.11 0.6305 0.085 0.011 1.333 0.321 0.041 1.358 0.1682 2.13 52.31 0.7102 0.098 0.012 1.528 0.369 0.047 1.557 0.1922 2.43 52.15 0.8117 0.110 0.014 1.723 0.416 0.053 1.756 0.2220 2.81 53.40 0.9375 0.129 0.016 2.017 0.486 0.061 2.054 0.2643 3.34 54.34 1.1163 0.142 0.018 2.212 0.534 0.067 2.253 0.3132 3.96 58.69 1.3225 0.167 0.021 2.603 0.628 0.079 2.652 0.3651 4.61 58.15 1.5418 0.185 0.023 2.896 0.699 0.088 2.950 0.4089 5.17 58.54 1.7271 0.210 0.026 3.287 0.793 0.100 3.348 0.4771 6.03 60.18 2.0149 0.242 0.030 3.775 0.927 0.117 3.913 0.5781 7.31 62.39 2.4414 0.273 0.034 4.264 1.023 0.129 4.320 0.6272 7.93 61.32 2.6490 0.310 0.039 4.850 1.110 0.140 4.689 0.6450 8.15 58.09 2.7239 0.354 0.044 5.534 1.303 0.165 5.503 0.7522 9.51 57.73 3.1766 0.398 0.050 6.218 1.499 0.189 6.329 0.8286 10.47 55.29 3.4994 0.454 0.057 7.097 1.626 0.206 6.867 0.8070 10.20 49.63 3.4081 0.510 0.064 7.976 1.862 0.235 7.863 0.8804 11.13 47.29 3.7182 0.579 0.072 9.051 2.203 0.278 9.302 0.9713 12.28 44.10 4.1021 0.660 0.082 10.321 2.472 0.312 10.440 1.0084 12.74 40.79 4.2586 0.748 0.093 11.689 2.726 0.344 11.512 0.9891 12.50 36.28 4.1770 0.848 0.106 13.252 3.035 0.384 12.817 0.9977 12.61 32.88 4.2137 0.960 0.120 15.011 3.282 0.415 13.859 1.0045 12.69 30.61 4.2421 1.092 0.136 17.063 3.799 0.480 16.045 1.0396 13.14 27.36 4.3903 1.235 0.154 19.310 4.012 0.507 16.942 1.0258 12.96 25.57 4.3323 1.404 0.175 21.948 4.469 0.565 18.875 1.0007 12.65 22.39 4.2263 1.592 0.198 24.879 4.839 0.612 20.436 1.0098 12.76 20.87 4.2646 1.798 0.224 28.103 5.246 0.663 22.154 0.9840 12.44 18.76 4.1558 2.042 0.255 31.913 5.591 0.707 23.612 0.9591 12.12 17.15 4.0504 2.317 0.289 36.212 5.950 0.752 25.129 0.9236 11.67 15.52 3.9005 2.623 0.327 41.000 6.282 0.794 26.532 0.8620 10.89 13.72 3.6405 2.973 0.371 46.471 6.550 0.828 27.661 0.8393 10.61 12.81 3.5447 3.367 0.420 52.626 6.854 0.866 28.946 0.7650 9.67 11.16 3.2306 3.817 0.476 59.661 7.089 0.896 29.937 0.6952 8.79 9.81 2.9359 4.329 0.540 67.672 7.279 0.920 30.741 0.5944 7.51 8.17 2.5101 4.904 0.611 76.661 7.462 0.943 31.513 0.5292 6.69 7.09 2.2351 5.560 0.693 86.920 7.610 0.962 32.140 0.4242 5.36 5.57 1.7916 6.304 0.786 98.546 7.690 0.972 32.477 0.3667 4.63 4.77 1.5489 7.142 0.890 111.638 7.788 0.984 32.891 0.2687 3.40 3.45 1.1346 8.098 1.010 126.587 7.846 0.992 33.137 0.1986 2.51 2.53 0.8388 9.048 1.128 141.437 7.877 0.996 33.268 0.1627 2.06 2.07 0.6870 10.004 1.247 156.386 7.899 0.998 33.358 0.1205 1.52 1.53 0.5088 10.954 1.366 171.237 7.913 1.000 33.418 0.1005 1.27 1.27 0.4245 11.910 1.485 186.185 7.924 1.001 33.466 0.0873 1.10 1.10 0.3685 15.960 1.990 249.496 7.931 1.002 33.495 0.0722 0.91 0.91 0.3051 20.010 2.495 312.807 7.936 1.003 33.516 0.0698 0.88 0.88 0.2948 24.060 3.000 376.118 7.943 1.004 33.547 0.0709 0.90 0.89 0.2994 28.110 3.505 439.429 7.944 1.004 33.551 0.0703 0.89 0.88 0.2969 RUN NUMBER 1W01810 AXIAL POSITION = 995.0 MM SPAN POSITION = 0.0 MM FREE-STREAM VELOCITY = 7.86 M/S FRICTION VELOCITY = 0.2494 M/S FREE-STREAM TURBULENCE = 0.881 % X-REYNOLDS NUMBER = 51.59 X10**4 FLUID DENSITY = 1.193 KG/M**3 KINEMATIC VISCOSITY = 1.516 X10(-5)MSQ/S BOUNDARY LAYER THICKNESS (99.0%) = 9.67 MM DISPLACEMENT THICKNESS = 1.918 MM MOMENTUM THICKNESS = 1.004 MM ENERGY THICKNESS = 1.689 MM FORM FACTOR H = 1.911 FORM FACTOR E = 1.683 RDELTASTAR = 994.6 RTHETA = 520.5 SKIN FRICTION COEFFICIENT = 0.002013 CALCULATED CF = 0.000924 Y Y/DEL YPLUS U U/UO UPLUS u u/UO u/U u/UTAU MM M/S M/S % % 0.029 0.003 0.477 0.125 0.016 0.500 0.0783 1.00 62.78 0.3141 0.035 0.004 0.580 0.152 0.019 0.608 0.0872 1.11 57.48 0.3496 0.042 0.004 0.683 0.179 0.023 0.716 0.1023 1.30 57.29 0.4102 0.048 0.005 0.785 0.205 0.026 0.824 0.1115 1.42 54.26 0.4470 0.054 0.006 0.888 0.232 0.030 0.932 0.1282 1.63 55.16 0.5139 0.060 0.006 0.991 0.259 0.033 1.040 0.1449 1.84 55.90 0.5811 0.067 0.007 1.094 0.286 0.036 1.147 0.1620 2.06 56.60 0.6494 0.073 0.008 1.197 0.313 0.040 1.255 0.1819 2.31 58.12 0.7295 0.079 0.008 1.299 0.340 0.043 1.363 0.1964 2.50 57.78 0.7876 0.092 0.009 1.505 0.394 0.050 1.579 0.2418 3.08 61.42 0.9697 0.104 0.011 1.711 0.448 0.057 1.794 0.2820 3.59 63.02 1.1308 0.117 0.012 1.916 0.501 0.064 2.010 0.3359 4.27 67.01 1.3469 0.129 0.013 2.122 0.555 0.071 2.226 0.3599 4.58 64.83 1.4429 0.148 0.015 2.430 0.636 0.081 2.549 0.4424 5.63 69.58 1.7737 0.173 0.018 2.841 0.743 0.095 2.980 0.5099 6.49 68.60 2.0445 0.198 0.020 3.252 0.851 0.108 3.412 0.5914 7.52 69.50 2.3713 0.223 0.023 3.664 0.949 0.121 3.805 0.6679 8.49 70.38 2.6778 0.254 0.026 4.178 0.998 0.127 4.003 0.7105 9.04 71.17 2.8488 0.292 0.030 4.794 1.164 0.148 4.668 0.8184 10.41 70.30 3.2815 0.329 0.034 5.411 1.256 0.160 5.037 0.8952 11.39 71.26 3.5894 0.373 0.039 6.131 1.455 0.185 5.833 0.9894 12.58 68.01 3.9670 0.423 0.044 6.953 1.732 0.220 6.945 1.0926 13.90 63.08 4.3810 0.485 0.050 7.981 1.910 0.243 7.657 1.1483 14.61 60.13 4.6041 0.548 0.057 9.009 2.110 0.268 8.461 1.1912 15.15 56.45 4.7763 0.629 0.065 10.345 2.417 0.307 9.690 1.2357 15.72 51.13 4.9545 0.710 0.073 11.682 2.664 0.339 10.681 1.2381 15.75 46.47 4.9641 0.810 0.084 13.327 2.982 0.379 11.958 1.2612 16.04 42.29 5.0567 0.923 0.095 15.177 3.175 0.404 12.732 1.2456 15.84 39.23 4.9942 1.048 0.108 17.233 3.592 0.457 14.403 1.2401 15.77 34.52 4.9725 1.192 0.123 19.597 3.857 0.491 15.465 1.1986 15.25 31.08 4.8059 1.354 0.140 22.270 4.154 0.528 16.657 1.1403 14.50 27.45 4.5719 1.542 0.159 25.354 4.472 0.569 17.931 1.1337 14.42 25.35 4.5455 1.754 0.181 28.849 4.851 0.617 19.450 1.0922 13.89 22.52 4.3793 1.992 0.206 32.755 5.175 0.658 20.750 1.0861 13.81 20.99 4.3548 2.267 0.234 37.278 5.535 0.704 22.194 1.0083 12.83 18.22 4.0429 2.579 0.267 42.418 5.903 0.751 23.668 0.9721 12.36 16.47 3.8977 2.929 0.303 48.174 6.162 0.784 24.707 0.9679 12.31 15.71 3.8808 3.329 0.344 54.753 6.459 0.822 25.898 0.8719 11.09 13.50 3.4959 3.785 0.392 62.258 6.685 0.850 26.804 0.8294 10.55 12.41 3.3256 4.304 0.445 70.790 6.965 0.886 27.927 0.7577 9.64 10.88 3.0382 4.898 0.507 80.555 7.170 0.912 28.748 0.6579 8.37 9.18 2.6380 5.567 0.576 91.555 7.358 0.936 29.502 0.5701 7.25 7.75 2.2858 6.329 0.655 104.096 7.486 0.952 30.017 0.4941 6.29 6.60 1.9813 7.192 0.744 118.282 7.617 0.969 30.543 0.3952 5.03 5.19 1.5847 8.179 0.846 134.523 7.700 0.979 30.875 0.3105 3.95 4.03 1.2450 9.298 0.962 152.924 7.772 0.988 31.161 0.2363 3.01 3.04 0.9474 10.417 1.078 171.324 7.821 0.995 31.359 0.1626 2.07 2.08 0.6521 11.535 1.193 189.725 7.839 0.997 31.432 0.1299 1.65 1.66 0.5207 12.654 1.309 208.126 7.854 0.999 31.489 0.1022 1.30 1.30 0.4099 13.773 1.425 226.526 7.859 1.000 31.512 0.0894 1.14 1.14 0.3586 18.423 1.906 303.007 7.874 1.002 31.573 0.0710 0.90 0.90 0.2845 23.073 2.387 379.487 7.879 1.002 31.591 0.0683 0.87 0.87 0.2739 27.723 2.868 455.968 7.881 1.002 31.599 0.0687 0.87 0.87 0.2754 32.373 3.349 532.448 7.889 1.003 31.632 0.0693 0.88 0.88 0.2777 RUN NUMBER 1W01901 AXIAL POSITION = 1095.0 MM SPAN POSITION = 0.0 MM FREE-STREAM VELOCITY = 7.77 M/S FRICTION VELOCITY = 0.2928 M/S FREE-STREAM TURBULENCE = 0.888 % X-REYNOLDS NUMBER = 56.19 X10**4 FLUID DENSITY = 1.194 KG/M**3 KINEMATIC VISCOSITY = 1.515 X10(-5)MSQ/S BOUNDARY LAYER THICKNESS (99.0%) = 12.18 MM DISPLACEMENT THICKNESS = 2.160 MM MOMENTUM THICKNESS = 1.266 MM ENERGY THICKNESS = 2.167 MM FORM FACTOR H = 1.706 FORM FACTOR E = 1.712 RDELTASTAR = 1108.4 RTHETA = 649.8 SKIN FRICTION COEFFICIENT = 0.002838 CALCULATED CF = 0.000886 Y Y/DEL YPLUS U U/UO UPLUS u u/UO u/U u/UTAU MM M/S M/S % % 0.029 0.002 0.561 0.168 0.022 0.573 0.0870 1.12 51.84 0.2969 0.035 0.003 0.681 0.204 0.026 0.696 0.0955 1.23 46.85 0.3262 0.042 0.003 0.802 0.240 0.031 0.820 0.1093 1.41 45.53 0.3732 0.048 0.004 0.923 0.276 0.036 0.943 0.1230 1.58 44.55 0.4201 0.054 0.004 1.044 0.312 0.040 1.067 0.1398 1.80 44.75 0.4773 0.060 0.005 1.165 0.348 0.045 1.190 0.1546 1.99 44.35 0.5278 0.067 0.005 1.286 0.385 0.049 1.313 0.1804 2.32 46.90 0.6160 0.073 0.006 1.406 0.421 0.054 1.437 0.1988 2.56 47.26 0.6790 0.079 0.006 1.527 0.457 0.059 1.560 0.2236 2.88 48.94 0.7636 0.092 0.008 1.769 0.529 0.068 1.807 0.2639 3.39 49.86 0.9011 0.104 0.009 2.011 0.602 0.077 2.054 0.3143 4.04 52.26 1.0734 0.123 0.010 2.373 0.710 0.091 2.424 0.3971 5.11 55.93 1.3559 0.142 0.012 2.736 0.818 0.105 2.795 0.4607 5.93 56.29 1.5731 0.160 0.013 3.098 0.927 0.119 3.165 0.5354 6.89 57.77 1.8284 0.185 0.015 3.581 0.991 0.128 3.385 0.6178 7.95 62.32 2.1096 0.210 0.017 4.065 1.180 0.152 4.029 0.7260 9.34 61.54 2.4791 0.242 0.020 4.669 1.300 0.167 4.438 0.8174 10.51 62.89 2.7912 0.279 0.023 5.394 1.470 0.189 5.020 0.9159 11.78 62.30 3.1276 0.317 0.026 6.119 1.616 0.208 5.519 1.0167 13.08 62.91 3.4717 0.367 0.030 7.085 1.944 0.250 6.640 1.1168 14.37 57.43 3.8136 0.417 0.034 8.052 2.161 0.278 7.378 1.1829 15.22 54.75 4.0395 0.473 0.039 9.139 2.330 0.300 7.956 1.2535 16.13 53.80 4.2804 0.542 0.044 10.469 2.630 0.338 8.982 1.3085 16.83 49.74 4.4681 0.623 0.051 12.039 2.879 0.370 9.830 1.3300 17.11 46.20 4.5415 0.710 0.058 13.731 3.057 0.393 10.440 1.3399 17.24 43.82 4.5755 0.817 0.067 15.785 3.295 0.424 11.253 1.3454 17.31 40.83 4.5944 0.929 0.076 17.960 3.546 0.456 12.109 1.3134 16.90 37.04 4.4848 1.067 0.088 20.618 3.806 0.490 12.995 1.2836 16.51 33.73 4.3831 1.217 0.100 23.518 4.082 0.525 13.939 1.2543 16.13 30.73 4.2830 1.392 0.114 26.901 4.263 0.548 14.556 1.2243 15.75 28.72 4.1807 1.592 0.131 30.768 4.631 0.596 15.814 1.1521 14.82 24.88 3.9341 1.817 0.149 35.118 4.887 0.629 16.689 1.1074 14.25 22.66 3.7814 2.079 0.171 40.192 5.103 0.656 17.425 1.0880 14.00 21.32 3.7153 2.373 0.195 45.871 5.394 0.694 18.420 1.0190 13.11 18.89 3.4795 2.710 0.222 52.396 5.693 0.732 19.441 0.9884 12.71 17.36 3.3751 3.104 0.255 60.008 5.914 0.761 20.195 0.9815 12.63 16.60 3.3516 3.548 0.291 68.587 6.171 0.794 21.071 0.9363 12.04 15.17 3.1973 4.054 0.333 78.374 6.437 0.828 21.979 0.8904 11.45 13.83 3.0405 4.629 0.380 89.490 6.663 0.857 22.754 0.8205 10.55 12.31 2.8018 5.292 0.434 102.298 6.856 0.882 23.410 0.7767 9.99 11.33 2.6522 6.048 0.496 116.918 7.046 0.906 24.060 0.6917 8.90 9.82 2.3619 6.917 0.568 133.714 7.229 0.930 24.685 0.5983 7.70 8.28 2.0431 7.904 0.649 152.805 7.384 0.950 25.215 0.5035 6.48 6.82 1.7193 9.029 0.741 174.554 7.520 0.967 25.679 0.4006 5.15 5.33 1.3679 10.323 0.847 199.565 7.613 0.979 25.996 0.3038 3.91 3.99 1.0375 11.798 0.968 228.081 7.692 0.990 26.267 0.2067 2.66 2.69 0.7059 13.273 1.090 256.596 7.731 0.994 26.398 0.1454 1.87 1.88 0.4966 14.748 1.211 285.112 7.756 0.998 26.484 0.1097 1.41 1.41 0.3747 16.223 1.332 313.627 7.764 0.999 26.513 0.0879 1.13 1.13 0.3003 17.698 1.453 342.143 7.774 1.000 26.547 0.0785 1.01 1.01 0.2681 23.598 1.937 456.205 7.784 1.001 26.582 0.0708 0.91 0.91 0.2419 29.498 2.421 570.267 7.791 1.002 26.605 0.0693 0.89 0.89 0.2367 35.398 2.906 684.329 7.793 1.003 26.612 0.0697 0.90 0.89 0.2379 41.298 3.390 798.391 7.796 1.003 26.621 0.0690 0.89 0.89 0.2356 RUN NUMBER 1W01902 AXIAL POSITION = 1195.0 MM SPAN POSITION = 0.0 MM FREE-STREAM VELOCITY = 7.55 M/S FRICTION VELOCITY = 0.3177 M/S FREE-STREAM TURBULENCE = 0.915 % X-REYNOLDS NUMBER = 59.57 X10**4 FLUID DENSITY = 1.194 KG/M**3 KINEMATIC VISCOSITY = 1.514 X10(-5)MSQ/S BOUNDARY LAYER THICKNESS (99.0%) = 14.79 MM DISPLACEMENT THICKNESS = 2.513 MM MOMENTUM THICKNESS = 1.594 MM ENERGY THICKNESS = 2.760 MM FORM FACTOR H = 1.577 FORM FACTOR E = 1.732 RDELTASTAR = 1253.0 RTHETA = 794.5 SKIN FRICTION COEFFICIENT = 0.003542 CALCULATED CF = 0.000860 Y Y/DEL YPLUS U U/UO UPLUS u u/UO u/U u/UTAU MM M/S M/S % % 0.029 0.002 0.608 0.193 0.026 0.608 0.0769 1.02 39.80 0.2422 0.035 0.002 0.740 0.235 0.031 0.740 0.0864 1.14 36.75 0.2718 0.042 0.003 0.871 0.277 0.037 0.871 0.0991 1.31 35.80 0.3117 0.048 0.003 1.002 0.318 0.042 1.002 0.1120 1.48 35.19 0.3526 0.054 0.004 1.133 0.360 0.048 1.133 0.1277 1.69 35.46 0.4018 0.060 0.004 1.264 0.402 0.053 1.264 0.1463 1.94 36.43 0.4605 0.067 0.004 1.395 0.443 0.059 1.395 0.1678 2.22 37.85 0.5281 0.073 0.005 1.526 0.485 0.064 1.526 0.1831 2.43 37.76 0.5764 0.085 0.006 1.789 0.568 0.075 1.789 0.2269 3.01 39.93 0.7142 0.098 0.007 2.051 0.652 0.086 2.051 0.2685 3.56 41.20 0.8449 0.110 0.007 2.313 0.735 0.097 2.313 0.3222 4.27 43.83 1.0139 0.129 0.009 2.706 0.860 0.114 2.706 0.3862 5.12 44.92 1.2156 0.148 0.010 3.100 0.985 0.130 3.100 0.4542 6.02 46.12 1.4297 0.173 0.012 3.624 1.096 0.145 3.448 0.5391 7.14 49.20 1.6966 0.198 0.013 4.149 1.269 0.168 3.995 0.6142 8.14 48.39 1.9331 0.229 0.015 4.805 1.420 0.188 4.468 0.7127 9.44 50.20 2.2430 0.260 0.018 5.460 1.616 0.214 5.087 0.7848 10.39 48.55 2.4699 0.298 0.020 6.247 1.755 0.232 5.523 0.8727 11.56 49.73 2.7466 0.342 0.023 7.165 2.043 0.271 6.429 0.9568 12.67 46.84 3.0114 0.398 0.027 8.345 2.351 0.311 7.399 1.0549 13.97 44.87 3.3200 0.454 0.031 9.525 2.526 0.335 7.951 1.1002 14.57 43.55 3.4626 0.523 0.035 10.968 2.776 0.368 8.738 1.1476 15.20 41.33 3.6118 0.598 0.040 12.541 3.078 0.408 9.687 1.1381 15.07 36.98 3.5818 0.692 0.047 14.508 3.280 0.435 10.324 1.1531 15.27 35.15 3.6292 0.792 0.054 16.606 3.479 0.461 10.948 1.1798 15.63 33.91 3.7131 0.910 0.062 19.098 3.743 0.496 11.780 1.1470 15.19 30.65 3.6100 1.042 0.070 21.851 3.918 0.519 12.330 1.1395 15.09 29.09 3.5864 1.198 0.081 25.129 4.164 0.552 13.105 1.0653 14.11 25.58 3.3528 1.379 0.093 28.932 4.379 0.580 13.781 1.0307 13.65 23.54 3.2439 1.579 0.107 33.128 4.514 0.598 14.206 1.0383 13.75 23.00 3.2677 1.817 0.123 38.111 4.700 0.623 14.792 0.9990 13.23 21.26 3.1442 2.085 0.141 43.750 4.939 0.654 15.546 0.9493 12.57 19.22 2.9878 2.392 0.162 50.175 5.152 0.682 16.215 0.9279 12.29 18.01 2.9203 2.748 0.186 57.649 5.330 0.706 16.774 0.9214 12.20 17.29 2.8998 3.154 0.213 66.173 5.511 0.730 17.343 0.9123 12.08 16.56 2.8712 3.623 0.245 76.007 5.704 0.755 17.951 0.9128 12.09 16.00 2.8728 4.160 0.281 87.284 5.950 0.788 18.728 0.8771 11.62 14.74 2.7605 4.773 0.323 100.135 6.134 0.812 19.305 0.8342 11.05 13.60 2.6253 5.479 0.370 114.952 6.320 0.837 19.891 0.8072 10.69 12.77 2.5406 6.292 0.425 131.999 6.529 0.865 20.549 0.7639 10.12 11.70 2.4043 7.223 0.488 151.537 6.742 0.893 21.219 0.6836 9.05 10.14 2.1515 8.292 0.561 173.960 6.937 0.919 21.834 0.6119 8.11 8.82 1.9260 9.517 0.643 199.662 7.098 0.940 22.341 0.5127 6.79 7.22 1.6138 10.923 0.739 229.165 7.277 0.964 22.902 0.3962 5.25 5.44 1.2470 12.542 0.848 263.128 7.387 0.978 23.249 0.2919 3.87 3.95 0.9187 14.398 0.974 302.073 7.474 0.990 23.523 0.1994 2.64 2.67 0.6276 16.254 1.099 341.018 7.515 0.995 23.651 0.1294 1.71 1.72 0.4074 18.110 1.225 379.963 7.539 0.999 23.727 0.0989 1.31 1.31 0.3114 19.967 1.350 418.908 7.540 0.999 23.732 0.0823 1.09 1.09 0.2591 21.817 1.475 457.722 7.547 1.000 23.753 0.0766 1.01 1.01 0.2410 29.017 1.962 608.782 7.554 1.001 23.775 0.0700 0.93 0.93 0.2205 36.217 2.449 759.843 7.562 1.002 23.801 0.0690 0.91 0.91 0.2171 43.417 2.936 910.903 7.566 1.002 23.814 0.0685 0.91 0.90 0.2155 50.617 3.422 1061.963 7.573 1.003 23.836 0.0690 0.91 0.91 0.2173 RUN NUMBER 1W01903 AXIAL POSITION = 1295.0 MM SPAN POSITION = 0.0 MM FREE-STREAM VELOCITY = 7.34 M/S FRICTION VELOCITY = 0.3229 M/S FREE-STREAM TURBULENCE = 0.930 % X-REYNOLDS NUMBER = 62.74 X10**4 FLUID DENSITY = 1.194 KG/M**3 KINEMATIC VISCOSITY = 1.515 X10(-5)MSQ/S BOUNDARY LAYER THICKNESS (99.0%) = 17.84 MM DISPLACEMENT THICKNESS = 3.026 MM MOMENTUM THICKNESS = 1.976 MM ENERGY THICKNESS = 3.430 MM FORM FACTOR H = 1.531 FORM FACTOR E = 1.736 RDELTASTAR = 1465.9 RTHETA = 957.3 SKIN FRICTION COEFFICIENT = 0.003874 CALCULATED CF = 0.003579 LAW OF THE WALL OFFSET = 5.20 KARMAN CONSTANT = 0.410 FORM FACTOR G = 7.883 CLAUSER DELTA = 68.755 MM WAKE FACTOR PI = 0.748 1 Y Y/DEL YPLUS U U/UO UPLUS u u/UO u/U u/UTAU MM M/S M/S % % 0.029 0.002 0.618 0.184 0.025 0.568 0.0647 0.88 35.22 0.2002 0.035 0.002 0.752 0.223 0.030 0.691 0.0695 0.95 31.16 0.2154 0.042 0.002 0.885 0.263 0.036 0.814 0.0793 1.08 30.17 0.2454 0.048 0.003 1.018 0.302 0.041 0.936 0.0910 1.24 30.11 0.2818 0.054 0.003 1.151 0.342 0.047 1.059 0.1039 1.42 30.39 0.3217 0.060 0.003 1.285 0.381 0.052 1.181 0.1192 1.62 31.26 0.3692 0.067 0.004 1.418 0.421 0.057 1.304 0.1337 1.82 31.75 0.4139 0.073 0.004 1.551 0.461 0.063 1.426 0.1521 2.07 33.03 0.4711 0.085 0.005 1.818 0.540 0.074 1.671 0.1875 2.56 34.75 0.5807 0.104 0.006 2.217 0.658 0.090 2.039 0.2493 3.40 37.86 0.7719 0.117 0.007 2.484 0.738 0.101 2.284 0.2809 3.83 38.09 0.8699 0.135 0.008 2.884 0.856 0.117 2.651 0.3421 4.66 39.96 1.0594 0.160 0.009 3.417 1.014 0.138 3.141 0.4114 5.61 40.55 1.2738 0.185 0.010 3.950 1.148 0.156 3.554 0.4831 6.58 42.09 1.4960 0.210 0.012 4.483 1.275 0.174 3.947 0.5498 7.49 43.13 1.7026 0.242 0.014 5.149 1.444 0.197 4.470 0.6151 8.38 42.61 1.9048 0.285 0.016 6.082 1.668 0.227 5.165 0.7162 9.76 42.94 2.2176 0.329 0.018 7.015 1.888 0.257 5.845 0.7833 10.68 41.50 2.4255 0.379 0.021 8.081 2.156 0.294 6.676 0.8517 11.61 39.50 2.6373 0.435 0.024 9.280 2.428 0.331 7.517 0.9077 12.37 37.39 2.8108 0.504 0.028 10.746 2.715 0.370 8.406 0.9543 13.01 35.15 2.9549 0.579 0.032 12.345 2.971 0.405 9.200 0.9841 13.41 33.12 3.0473 0.667 0.037 14.210 3.224 0.439 9.984 0.9888 13.48 30.67 3.0620 0.773 0.043 16.476 3.461 0.472 10.717 0.9860 13.44 28.49 3.0532 0.892 0.050 19.008 3.653 0.498 11.311 0.9809 13.37 26.85 3.0374 1.029 0.058 21.939 3.903 0.532 12.086 0.9453 12.88 24.22 2.9272 1.185 0.066 25.271 4.048 0.552 12.536 0.9375 12.78 23.16 2.9030 1.373 0.077 29.268 4.226 0.576 13.085 0.8881 12.10 21.02 2.7500 1.585 0.089 33.799 4.391 0.598 13.596 0.8587 11.70 19.56 2.6588 1.829 0.103 38.996 4.534 0.618 14.039 0.8641 11.78 19.06 2.6758 2.104 0.118 44.859 4.658 0.635 14.424 0.8363 11.40 17.95 2.5896 2.429 0.136 51.789 4.835 0.659 14.971 0.8016 10.92 16.58 2.4822 2.804 0.157 59.784 4.991 0.680 15.456 0.8030 10.94 16.09 2.4866 3.235 0.181 68.979 5.126 0.699 15.873 0.8119 11.06 15.84 2.5140 3.735 0.209 79.639 5.304 0.723 16.424 0.7823 10.66 14.75 2.4223 4.310 0.242 91.899 5.464 0.745 16.918 0.7981 10.88 14.61 2.4712 4.973 0.279 106.024 5.640 0.769 17.464 0.7797 10.63 13.82 2.4143 5.735 0.322 122.281 5.841 0.796 18.086 0.7847 10.69 13.43 2.4298 6.617 0.371 141.071 6.057 0.825 18.756 0.7368 10.04 12.16 2.2815 7.635 0.428 162.791 6.267 0.854 19.407 0.7067 9.63 11.28 2.1884 8.804 0.494 187.710 6.474 0.882 20.047 0.6470 8.82 9.99 2.0035 10.160 0.570 216.627 6.685 0.911 20.701 0.5797 7.90 8.67 1.7951 11.723 0.657 249.941 6.910 0.942 21.396 0.4824 6.57 6.98 1.4937 13.523 0.758 288.319 7.065 0.963 21.877 0.3797 5.18 5.37 1.1758 15.598 0.875 332.560 7.204 0.982 22.307 0.2620 3.57 3.64 0.8111 17.998 1.009 383.731 7.285 0.993 22.558 0.1590 2.17 2.18 0.4925 20.392 1.143 434.768 7.319 0.997 22.663 0.1097 1.50 1.50 0.3398 22.792 1.278 485.938 7.330 0.999 22.698 0.0841 1.15 1.15 0.2603 25.185 1.412 536.976 7.339 1.000 22.725 0.0761 1.04 1.04 0.2356 27.585 1.547 588.146 7.341 1.000 22.732 0.0732 1.00 1.00 0.2268 36.585 2.051 780.036 7.350 1.002 22.761 0.0697 0.95 0.95 0.2159 45.585 2.556 971.925 7.358 1.003 22.783 0.0683 0.93 0.93 0.2115 54.585 3.061 1163.814 7.360 1.003 22.790 0.0677 0.92 0.92 0.2097 63.585 3.565 1355.704 7.357 1.003 22.782 0.0682 0.93 0.93 0.2113 RUN NUMBER 1W01904 AXIAL POSITION = 1395.0 MM SPAN POSITION = 0.0 MM FREE-STREAM VELOCITY = 7.05 M/S FRICTION VELOCITY = 0.2978 M/S FREE-STREAM TURBULENCE = 0.957 % X-REYNOLDS NUMBER = 64.94 X10**4 FLUID DENSITY = 1.194 KG/M**3 KINEMATIC VISCOSITY = 1.515 X10(-5)MSQ/S BOUNDARY LAYER THICKNESS (99.0%) = 21.98 MM DISPLACEMENT THICKNESS = 3.889 MM MOMENTUM THICKNESS = 2.560 MM ENERGY THICKNESS = 4.430 MM FORM FACTOR H = 1.519 FORM FACTOR E = 1.731 RDELTASTAR = 1810.4 RTHETA = 1191.5 SKIN FRICTION COEFFICIENT = 0.003566 CALCULATED CF = 0.003439 LAW OF THE WALL OFFSET = 5.20 KARMAN CONSTANT = 0.410 FORM FACTOR G = 8.096 CLAUSER DELTA = 92.106 MM WAKE FACTOR PI = 0.804 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 0.570 0.170 0.024 0.570 0.0604 0.86 35.60 0.2029 0.035 0.002 0.693 0.206 0.029 0.693 0.0662 0.94 32.09 0.2223 0.042 0.002 0.816 0.243 0.034 0.816 0.0751 1.07 30.93 0.2522 0.048 0.002 0.939 0.279 0.040 0.938 0.0857 1.21 30.65 0.2876 0.054 0.002 1.061 0.316 0.045 1.061 0.0979 1.39 30.99 0.3289 0.060 0.003 1.184 0.353 0.050 1.184 0.1109 1.57 31.45 0.3724 0.067 0.003 1.307 0.389 0.055 1.307 0.1230 1.74 31.61 0.4131 0.079 0.004 1.553 0.462 0.066 1.553 0.1489 2.11 32.21 0.5001 0.092 0.004 1.799 0.536 0.076 1.798 0.1794 2.54 33.49 0.6023 0.104 0.005 2.044 0.609 0.086 2.044 0.2169 3.07 35.63 0.7282 0.123 0.006 2.413 0.718 0.102 2.412 0.2732 3.87 38.03 0.9174 0.142 0.006 2.781 0.828 0.117 2.781 0.3219 4.56 38.87 1.0809 0.167 0.008 3.273 0.974 0.138 3.272 0.3891 5.52 39.93 1.3065 0.192 0.009 3.764 1.089 0.154 3.657 0.4461 6.33 40.96 1.4980 0.223 0.010 4.378 1.262 0.179 4.236 0.5202 7.38 41.24 1.7469 0.254 0.012 4.993 1.386 0.197 4.655 0.5760 8.17 41.55 1.9342 0.298 0.014 5.853 1.578 0.224 5.298 0.6536 9.27 41.42 2.1946 0.342 0.016 6.712 1.784 0.253 5.989 0.7216 10.23 40.45 2.4229 0.398 0.018 7.818 2.043 0.290 6.860 0.7748 10.99 37.93 2.6018 0.460 0.021 9.047 2.303 0.327 7.735 0.8314 11.79 36.09 2.7918 0.535 0.024 10.521 2.547 0.361 8.551 0.8661 12.28 34.01 2.9084 0.617 0.028 12.118 2.797 0.397 9.392 0.8805 12.48 31.48 2.9567 0.717 0.033 14.083 3.059 0.434 10.271 0.8896 12.61 29.08 2.9873 0.829 0.038 16.295 3.246 0.460 10.902 0.8742 12.40 26.93 2.9355 0.960 0.044 18.875 3.417 0.484 11.473 0.8772 12.44 25.67 2.9457 1.110 0.051 21.823 3.614 0.512 12.135 0.8474 12.01 23.45 2.8454 1.292 0.059 25.386 3.782 0.536 12.699 0.8225 11.66 21.75 2.7619 1.492 0.068 29.317 3.931 0.557 13.201 0.8055 11.42 20.49 2.7049 1.729 0.079 33.985 4.072 0.577 13.674 0.7822 11.09 19.21 2.6266 1.998 0.091 39.267 4.191 0.594 14.071 0.7526 10.67 17.96 2.5272 2.310 0.105 45.410 4.321 0.613 14.508 0.7455 10.57 17.26 2.5034 2.679 0.122 52.658 4.458 0.632 14.971 0.7459 10.58 16.73 2.5045 3.098 0.141 60.889 4.579 0.649 15.377 0.7213 10.23 15.75 2.4222 3.585 0.163 70.471 4.715 0.669 15.834 0.7091 10.05 15.04 2.3810 4.148 0.189 81.528 4.857 0.689 16.309 0.7224 10.24 14.87 2.4258 4.804 0.219 94.427 5.023 0.712 16.867 0.7115 10.09 14.16 2.3891 5.560 0.253 109.291 5.177 0.734 17.385 0.7064 10.02 13.64 2.3721 6.435 0.293 126.490 5.363 0.760 18.007 0.6939 9.84 12.94 2.3302 7.448 0.339 146.392 5.566 0.789 18.691 0.6922 9.82 12.44 2.3245 8.617 0.392 169.365 5.773 0.818 19.384 0.6838 9.70 11.85 2.2961 9.973 0.454 196.023 6.014 0.853 20.196 0.6365 9.03 10.58 2.1375 11.542 0.525 226.858 6.258 0.887 21.014 0.5817 8.25 9.29 1.9532 13.354 0.608 262.484 6.483 0.919 21.771 0.5061 7.18 7.81 1.6994 15.454 0.703 303.761 6.695 0.949 22.481 0.4064 5.76 6.07 1.3645 17.885 0.814 351.550 6.861 0.973 23.037 0.2887 4.09 4.21 0.9696 20.698 0.942 406.832 6.974 0.989 23.417 0.1742 2.47 2.50 0.5851 23.510 1.070 462.114 7.020 0.995 23.574 0.1121 1.59 1.60 0.3765 26.323 1.198 517.396 7.041 0.998 23.643 0.0836 1.19 1.19 0.2808 29.135 1.325 572.678 7.047 0.999 23.664 0.0757 1.07 1.07 0.2540 31.948 1.453 627.960 7.044 0.999 23.654 0.0726 1.03 1.03 0.2436 41.354 1.881 812.848 7.061 1.001 23.710 0.0687 0.97 0.97 0.2308 50.767 2.310 997.858 7.066 1.002 23.728 0.0676 0.96 0.96 0.2270 60.173 2.738 1182.746 7.068 1.002 23.733 0.0662 0.94 0.94 0.2222 69.585 3.166 1367.757 7.073 1.003 23.751 0.0675 0.96 0.95 0.2267 RUN NUMBER 1W01905 AXIAL POSITION = 1495.0 MM SPAN POSITION = 0.0 MM FREE-STREAM VELOCITY = 6.71 M/S FRICTION VELOCITY = 0.2660 M/S FREE-STREAM TURBULENCE = 0.980 % X-REYNOLDS NUMBER = 65.60 X10**4 FLUID DENSITY = 1.183 KG/M**3 KINEMATIC VISCOSITY = 1.529 X10(-5)MSQ/S BOUNDARY LAYER THICKNESS (99.0%) = 25.52 MM DISPLACEMENT THICKNESS = 5.023 MM MOMENTUM THICKNESS = 3.229 MM ENERGY THICKNESS = 5.526 MM FORM FACTOR H = 1.556 FORM FACTOR E = 1.711 RDELTASTAR = 2203.9 RTHETA = 1416.7 SKIN FRICTION COEFFICIENT = 0.003144 CALCULATED CF = 0.003102 LAW OF THE WALL OFFSET = 5.20 KARMAN CONSTANT = 0.410 FORM FACTOR G = 9.007 CLAUSER DELTA = 126.672 MM WAKE FACTOR PI = 1.024 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 0.505 0.129 0.019 0.484 0.0461 0.69 35.84 0.1734 0.035 0.001 0.613 0.156 0.023 0.588 0.0488 0.73 31.22 0.1836 0.042 0.002 0.722 0.184 0.027 0.692 0.0568 0.85 30.83 0.2134 0.048 0.002 0.831 0.212 0.032 0.796 0.0627 0.93 29.60 0.2357 0.054 0.002 0.939 0.240 0.036 0.901 0.0700 1.04 29.23 0.2633 0.060 0.002 1.048 0.267 0.040 1.005 0.0775 1.16 28.99 0.2914 0.067 0.003 1.157 0.295 0.044 1.109 0.0879 1.31 29.79 0.3304 0.079 0.003 1.374 0.350 0.052 1.318 0.1068 1.59 30.46 0.4014 0.092 0.004 1.592 0.406 0.061 1.526 0.1325 1.97 32.63 0.4980 0.110 0.004 1.918 0.489 0.073 1.839 0.1723 2.57 35.22 0.6477 0.129 0.005 2.244 0.572 0.085 2.152 0.2124 3.17 37.11 0.7985 0.148 0.006 2.571 0.656 0.098 2.465 0.2598 3.87 39.64 0.9768 0.173 0.007 3.006 0.766 0.114 2.882 0.3089 4.61 40.31 1.1614 0.204 0.008 3.549 0.905 0.135 3.403 0.3803 5.67 42.02 1.4298 0.235 0.009 4.093 1.032 0.154 3.881 0.4430 6.60 42.92 1.6655 0.273 0.011 4.745 1.172 0.175 4.407 0.5088 7.59 43.41 1.9131 0.317 0.012 5.506 1.360 0.203 5.112 0.5821 8.68 42.81 2.1883 0.367 0.014 6.376 1.569 0.234 5.901 0.6534 9.74 41.63 2.4566 0.429 0.017 7.464 1.774 0.265 6.671 0.7010 10.45 39.51 2.6355 0.498 0.020 8.660 2.037 0.304 7.657 0.7546 11.25 37.06 2.8372 0.579 0.023 10.073 2.292 0.342 8.617 0.7928 11.82 34.59 2.9805 0.679 0.027 11.813 2.522 0.376 9.482 0.8056 12.01 31.94 3.0288 0.785 0.031 13.662 2.727 0.406 10.252 0.8068 12.03 29.59 3.0333 0.917 0.036 15.945 2.905 0.433 10.923 0.7973 11.89 27.44 2.9974 1.067 0.042 18.555 3.079 0.459 11.574 0.7858 11.71 25.52 2.9542 1.235 0.048 21.491 3.216 0.479 12.092 0.7778 11.59 24.18 2.9241 1.435 0.056 24.971 3.387 0.505 12.735 0.7577 11.30 22.37 2.8489 1.673 0.066 29.103 3.504 0.522 13.175 0.7315 10.91 20.88 2.7504 1.942 0.076 33.778 3.623 0.540 13.621 0.7111 10.60 19.63 2.6735 2.260 0.089 39.324 3.754 0.560 14.115 0.6971 10.39 18.57 2.6209 2.623 0.103 45.631 3.853 0.574 14.487 0.6936 10.34 18.00 2.6079 3.048 0.119 53.025 3.964 0.591 14.905 0.6809 10.15 17.18 2.5600 3.542 0.139 61.615 4.119 0.614 15.487 0.6747 10.06 16.38 2.5367 4.117 0.161 71.619 4.232 0.631 15.910 0.6705 10.00 15.84 2.5209 4.785 0.188 83.254 4.374 0.652 16.447 0.6619 9.87 15.13 2.4885 5.567 0.218 96.846 4.516 0.673 16.978 0.6661 9.93 14.75 2.5045 6.467 0.253 112.505 4.707 0.702 17.698 0.6816 10.16 14.48 2.5625 7.517 0.295 130.773 4.868 0.726 18.304 0.6670 9.94 13.70 2.5076 8.735 0.342 151.977 5.082 0.758 19.105 0.6639 9.90 13.06 2.4960 10.148 0.398 176.551 5.311 0.792 19.969 0.6476 9.65 12.19 2.4348 11.792 0.462 205.150 5.562 0.829 20.912 0.6199 9.24 11.15 2.3308 13.704 0.537 238.423 5.841 0.871 21.962 0.5741 8.56 9.83 2.1585 15.929 0.624 277.134 6.091 0.908 22.901 0.5115 7.63 8.40 1.9232 18.510 0.725 322.043 6.346 0.946 23.859 0.4022 6.00 6.34 1.5122 21.510 0.843 374.237 6.532 0.974 24.559 0.2758 4.11 4.22 1.0370 24.998 0.980 434.913 6.653 0.992 25.013 0.1585 2.36 2.38 0.5959 28.485 1.116 495.589 6.693 0.998 25.165 0.1000 1.49 1.49 0.3760 31.973 1.253 556.265 6.708 1.000 25.221 0.0772 1.15 1.15 0.2901 35.460 1.390 616.941 6.714 1.001 25.241 0.0728 1.08 1.08 0.2736 38.942 1.526 677.508 6.715 1.001 25.247 0.0700 1.04 1.04 0.2632 46.598 1.826 810.712 6.720 1.002 25.267 0.0676 1.01 1.01 0.2540 54.254 2.126 943.916 6.723 1.002 25.276 0.0667 0.99 0.99 0.2509 61.910 2.426 1077.120 6.725 1.003 25.284 0.0668 1.00 0.99 0.2510 69.567 2.726 1210.324 6.721 1.002 25.267 0.0658 0.98 0.98 0.2472