ROLLS-ROYCE APPLIED SCIENCE LABORATORY FLAT PLATE TRANSITIONAL BOUNDARY LAYER FLOW HOT WIRE ANEMOMETRY TEST DATA SINGLE WIRE DATA FOR ERCOFTAC T3B TEST CASE RUN NUMBER 1W00907 AXIAL POSITION = 25.0 MM SPAN POSITION = 0.0 MM FREE-STREAM VELOCITY = 9.21 M/S FRICTION VELOCITY = 0.4864 M/S FREE-STREAM TURBULENCE = 5.952 % X-REYNOLDS NUMBER = 1.51 X10**4 FLUID DENSITY = 1.189 KG/M**3 KINEMATIC VISCOSITY = 1.521 X10(-5)MSQ/S BOUNDARY LAYER THICKNESS (99.0%) = 1.04 MM DISPLACEMENT THICKNESS = 0.343 MM MOMENTUM THICKNESS = 0.137 MM ENERGY THICKNESS = 0.216 MM FORM FACTOR H = 2.503 FORM FACTOR E = 1.580 RDELTASTAR = 207.6 RTHETA = 82.9 SKIN FRICTION COEFFICIENT = 0.005574 CALCULATED CF = 0.005396 Y Y/DEL YPLUS U U/UO UPLUS u u/UO u/U u/UTAU MM M/S M/S % % 0.092 0.088 2.926 1.572 0.171 3.231 0.1949 2.12 12.41 0.4008 0.098 0.094 3.125 1.666 0.181 3.425 0.2120 2.30 12.72 0.4358 0.104 0.100 3.325 1.749 0.190 3.596 0.2240 2.43 12.81 0.4605 0.110 0.106 3.525 1.832 0.199 3.766 0.2374 2.58 12.96 0.4882 0.117 0.112 3.725 1.916 0.208 3.940 0.2494 2.71 13.02 0.5128 0.123 0.118 3.925 2.000 0.217 4.112 0.2634 2.86 13.17 0.5415 0.129 0.124 4.125 2.092 0.227 4.300 0.2771 3.01 13.25 0.5697 0.135 0.130 4.324 2.195 0.238 4.513 0.2902 3.15 13.22 0.5966 0.142 0.136 4.524 2.263 0.246 4.652 0.2991 3.25 13.22 0.6150 0.148 0.142 4.724 2.352 0.255 4.836 0.3185 3.46 13.54 0.6549 0.154 0.148 4.924 2.453 0.266 5.043 0.3306 3.59 13.48 0.6797 0.160 0.154 5.124 2.545 0.276 5.233 0.3478 3.77 13.66 0.7150 0.167 0.160 5.324 2.626 0.285 5.399 0.3545 3.85 13.50 0.7289 0.173 0.166 5.523 2.723 0.296 5.598 0.3734 4.05 13.71 0.7677 0.192 0.184 6.123 2.967 0.322 6.099 0.4123 4.47 13.90 0.8476 0.204 0.196 6.523 3.192 0.346 6.562 0.4355 4.73 13.64 0.8953 0.223 0.214 7.122 3.452 0.375 7.098 0.4788 5.20 13.87 0.9843 0.242 0.233 7.722 3.710 0.403 7.627 0.5134 5.57 13.84 1.0555 0.260 0.251 8.321 3.974 0.431 8.169 0.5422 5.88 13.64 1.1147 0.279 0.269 8.921 4.266 0.463 8.770 0.5800 6.30 13.60 1.1924 0.304 0.293 9.720 4.624 0.502 9.507 0.6119 6.64 13.23 1.2581 0.329 0.317 10.519 4.976 0.540 10.231 0.6375 6.92 12.81 1.3107 0.354 0.341 11.319 5.304 0.576 10.905 0.6723 7.30 12.67 1.3822 0.385 0.371 12.318 5.701 0.619 11.722 0.7010 7.61 12.29 1.4412 0.417 0.401 13.317 6.077 0.660 12.494 0.7146 7.76 11.76 1.4692 0.454 0.437 14.516 6.484 0.704 13.331 0.7295 7.92 11.25 1.4999 0.492 0.473 15.715 6.839 0.742 14.061 0.7306 7.93 10.68 1.5020 0.529 0.509 16.914 7.192 0.781 14.786 0.7295 7.92 10.14 1.4998 0.573 0.552 18.313 7.539 0.818 15.499 0.7154 7.77 9.49 1.4709 0.623 0.600 19.912 7.874 0.855 16.188 0.7067 7.67 8.98 1.4529 0.673 0.648 21.510 8.195 0.889 16.849 0.6791 7.37 8.29 1.3962 0.729 0.702 23.309 8.469 0.919 17.412 0.6601 7.16 7.79 1.3570 0.785 0.756 25.107 8.700 0.944 17.886 0.6489 7.04 7.46 1.3341 0.854 0.822 27.305 8.880 0.964 18.258 0.6235 6.77 7.02 1.2819 0.923 0.889 29.504 9.014 0.978 18.532 0.6163 6.69 6.84 1.2670 0.998 0.961 31.902 9.090 0.987 18.688 0.6067 6.58 6.67 1.2473 1.073 1.033 34.300 9.152 0.993 18.815 0.6018 6.53 6.58 1.2373 1.148 1.105 36.698 9.187 0.997 18.887 0.5979 6.49 6.51 1.2293 1.223 1.177 39.096 9.212 1.000 18.940 0.5909 6.41 6.41 1.2148 1.298 1.250 41.494 9.225 1.001 18.967 0.5923 6.43 6.42 1.2178 1.798 1.731 57.480 9.220 1.001 18.955 0.5754 6.25 6.24 1.1830 2.298 2.213 73.467 9.245 1.003 19.007 0.5595 6.07 6.05 1.1503 2.798 2.694 89.454 9.226 1.001 18.969 0.5567 6.04 6.03 1.1445 3.298 3.175 105.441 9.241 1.003 18.999 0.5484 5.95 5.93 1.1275 RUN NUMBER 1W00705 AXIAL POSITION = 45.0 MM SPAN POSITION = 0.0 MM FREE-STREAM VELOCITY = 9.38 M/S FRICTION VELOCITY = 0.4451 M/S FREE-STREAM TURBULENCE = 5.635 % X-REYNOLDS NUMBER = 2.77 X10**4 FLUID DENSITY = 1.188 KG/M**3 KINEMATIC VISCOSITY = 1.523 X10(-5)MSQ/S BOUNDARY LAYER THICKNESS (99.0%) = 1.44 MM DISPLACEMENT THICKNESS = 0.451 MM MOMENTUM THICKNESS = 0.185 MM ENERGY THICKNESS = 0.295 MM FORM FACTOR H = 2.437 FORM FACTOR E = 1.594 RDELTASTAR = 278.0 RTHETA = 114.1 SKIN FRICTION COEFFICIENT = 0.004503 CALCULATED CF = 0.003988 Y Y/DEL YPLUS U U/UO UPLUS u u/UO u/U u/UTAU MM M/S M/S % % 0.104 0.072 3.040 1.405 0.150 3.157 0.2506 2.67 17.83 0.5629 0.110 0.077 3.223 1.459 0.156 3.278 0.2614 2.79 17.92 0.5872 0.117 0.081 3.405 1.543 0.165 3.467 0.2788 2.97 18.06 0.6263 0.123 0.085 3.588 1.605 0.171 3.606 0.2939 3.13 18.31 0.6602 0.129 0.090 3.771 1.664 0.177 3.738 0.3112 3.32 18.70 0.6991 0.135 0.094 3.953 1.739 0.185 3.907 0.3222 3.43 18.53 0.7239 0.142 0.098 4.136 1.809 0.193 4.063 0.3376 3.60 18.67 0.7585 0.148 0.103 4.319 1.878 0.200 4.220 0.3531 3.76 18.80 0.7933 0.167 0.116 4.867 2.090 0.223 4.694 0.3975 4.24 19.02 0.8931 0.179 0.125 5.232 2.236 0.238 5.024 0.4251 4.53 19.01 0.9551 0.198 0.138 5.780 2.444 0.261 5.490 0.4714 5.02 19.29 1.0590 0.217 0.151 6.328 2.655 0.283 5.966 0.5126 5.46 19.30 1.1515 0.235 0.164 6.876 2.895 0.309 6.504 0.5582 5.95 19.28 1.2541 0.254 0.177 7.424 3.113 0.332 6.993 0.6030 6.43 19.37 1.3547 0.279 0.194 8.155 3.424 0.365 7.693 0.6547 6.98 19.12 1.4709 0.304 0.212 8.886 3.681 0.392 8.269 0.6963 7.42 18.92 1.5642 0.335 0.233 9.799 4.062 0.433 9.126 0.7543 8.04 18.57 1.6946 0.367 0.255 10.713 4.443 0.474 9.981 0.7862 8.38 17.70 1.7663 0.398 0.277 11.626 4.808 0.513 10.802 0.8369 8.92 17.40 1.8800 0.435 0.303 12.722 5.203 0.555 11.689 0.8626 9.20 16.58 1.9379 0.479 0.333 14.001 5.663 0.604 12.722 0.9054 9.65 15.99 2.0339 0.523 0.364 15.280 6.073 0.647 13.644 0.9168 9.77 15.10 2.0597 0.567 0.394 16.559 6.467 0.689 14.528 0.9252 9.86 14.31 2.0784 0.623 0.433 18.203 6.867 0.732 15.427 0.9350 9.97 13.62 2.1006 0.679 0.472 19.847 7.262 0.774 16.315 0.9067 9.66 12.48 2.0369 0.742 0.516 21.674 7.622 0.812 17.122 0.8805 9.39 11.55 1.9781 0.810 0.564 23.684 7.961 0.849 17.884 0.8505 9.07 10.68 1.9106 0.885 0.616 25.876 8.292 0.884 18.627 0.8035 8.57 9.69 1.8051 0.967 0.672 28.251 8.561 0.913 19.231 0.7598 8.10 8.88 1.7070 1.054 0.733 30.809 8.769 0.935 19.699 0.7317 7.80 8.34 1.6437 1.148 0.799 33.549 8.972 0.956 20.156 0.6804 7.25 7.58 1.5284 1.254 0.872 36.655 9.114 0.972 20.475 0.6476 6.90 7.11 1.4549 1.373 0.955 40.126 9.236 0.984 20.749 0.6245 6.66 6.76 1.4029 1.498 1.042 43.780 9.331 0.995 20.961 0.6014 6.41 6.44 1.3510 1.623 1.129 47.433 9.348 0.996 21.000 0.5890 6.28 6.30 1.3231 1.748 1.216 51.087 9.386 1.000 21.085 0.5795 6.18 6.17 1.3019 1.873 1.303 54.741 9.400 1.002 21.117 0.5780 6.16 6.15 1.2984 1.998 1.390 58.395 9.400 1.002 21.118 0.5675 6.05 6.04 1.2749 2.748 1.912 80.317 9.402 1.002 21.122 0.5538 5.90 5.89 1.2441 3.498 2.433 102.240 9.385 1.000 21.083 0.5409 5.77 5.76 1.2151 4.248 2.955 124.163 9.378 1.000 21.067 0.5358 5.71 5.71 1.2037 4.998 3.477 146.085 9.404 1.002 21.126 0.5287 5.64 5.62 1.1877 RUN NUMBER 1W00903 AXIAL POSITION = 70.0 MM SPAN POSITION = 0.0 MM FREE-STREAM VELOCITY = 9.36 M/S FRICTION VELOCITY = 0.3958 M/S FREE-STREAM TURBULENCE = 5.442 % X-REYNOLDS NUMBER = 4.31 X10**4 FLUID DENSITY = 1.190 KG/M**3 KINEMATIC VISCOSITY = 1.521 X10(-5)MSQ/S BOUNDARY LAYER THICKNESS (99.0%) = 1.96 MM DISPLACEMENT THICKNESS = 0.555 MM MOMENTUM THICKNESS = 0.237 MM ENERGY THICKNESS = 0.382 MM FORM FACTOR H = 2.340 FORM FACTOR E = 1.613 RDELTASTAR = 341.6 RTHETA = 146.0 SKIN FRICTION COEFFICIENT = 0.003573 CALCULATED CF = 0.003198 Y Y/DEL YPLUS U U/UO UPLUS u u/UO u/U u/UTAU MM M/S M/S % % 0.110 0.056 2.870 1.296 0.138 3.273 0.3209 3.43 24.77 0.8109 0.117 0.059 3.033 1.344 0.143 3.394 0.3292 3.52 24.50 0.8317 0.123 0.063 3.195 1.397 0.149 3.529 0.3443 3.68 24.65 0.8698 0.129 0.066 3.358 1.453 0.155 3.671 0.3639 3.89 25.05 0.9194 0.142 0.072 3.683 1.559 0.166 3.939 0.4040 4.31 25.91 1.0208 0.154 0.078 4.009 1.683 0.180 4.251 0.4320 4.61 25.67 1.0914 0.173 0.088 4.497 1.855 0.198 4.685 0.4870 5.20 26.26 1.2303 0.185 0.094 4.822 1.960 0.209 4.953 0.5124 5.47 26.13 1.2944 0.204 0.104 5.310 2.138 0.228 5.402 0.5702 6.09 26.67 1.4407 0.229 0.117 5.961 2.393 0.256 6.045 0.6423 6.86 26.85 1.6228 0.248 0.126 6.449 2.589 0.277 6.542 0.6838 7.30 26.41 1.7276 0.273 0.139 7.100 2.848 0.304 7.196 0.7542 8.05 26.48 1.9055 0.304 0.155 7.914 3.151 0.336 7.961 0.8239 8.80 26.15 2.0814 0.329 0.168 8.564 3.386 0.362 8.554 0.8525 9.10 25.18 2.1538 0.367 0.187 9.541 3.788 0.405 9.570 0.9268 9.90 24.47 2.3415 0.404 0.206 10.517 4.169 0.445 10.534 0.9802 10.47 23.51 2.4765 0.442 0.225 11.493 4.549 0.486 11.494 1.0312 11.01 22.67 2.6052 0.485 0.247 12.632 4.934 0.527 12.466 1.0740 11.47 21.77 2.7135 0.535 0.273 13.933 5.404 0.577 13.652 1.1009 11.76 20.37 2.7813 0.585 0.298 15.235 5.806 0.620 14.670 1.1246 12.01 19.37 2.8413 0.642 0.327 16.699 6.221 0.664 15.718 1.1356 12.13 18.25 2.8690 0.710 0.362 18.489 6.649 0.710 16.800 1.1137 11.89 16.75 2.8136 0.779 0.397 20.279 7.008 0.748 17.704 1.1097 11.85 15.84 2.8036 0.854 0.435 22.231 7.379 0.788 18.641 1.0721 11.45 14.53 2.7086 0.942 0.480 24.509 7.740 0.826 19.554 1.0461 11.17 13.52 2.6430 1.029 0.524 26.787 8.028 0.857 20.283 0.9944 10.62 12.39 2.5124 1.135 0.578 29.552 8.319 0.888 21.016 0.9199 9.82 11.06 2.3240 1.248 0.636 32.481 8.577 0.916 21.670 0.8669 9.26 10.11 2.1901 1.373 0.699 35.735 8.807 0.940 22.250 0.7851 8.38 8.91 1.9834 1.504 0.766 39.152 8.975 0.958 22.675 0.7252 7.74 8.08 1.8321 1.654 0.843 43.056 9.109 0.973 23.014 0.6698 7.15 7.35 1.6922 1.817 0.926 47.287 9.206 0.983 23.259 0.6310 6.74 6.85 1.5942 1.998 1.018 52.005 9.296 0.993 23.486 0.6001 6.41 6.46 1.5161 2.179 1.110 56.723 9.342 0.998 23.603 0.5752 6.14 6.16 1.4532 2.354 1.199 61.279 9.363 1.000 23.654 0.5654 6.04 6.04 1.4285 2.535 1.292 65.997 9.364 1.000 23.658 0.5497 5.87 5.87 1.3888 2.717 1.384 70.715 9.380 1.002 23.697 0.5416 5.78 5.77 1.3683 3.717 1.894 96.747 9.390 1.003 23.723 0.5261 5.62 5.60 1.3293 4.717 2.403 122.778 9.362 1.000 23.653 0.5182 5.53 5.53 1.3092 5.717 2.913 148.810 9.387 1.002 23.716 0.5122 5.47 5.46 1.2941 6.717 3.422 174.842 9.397 1.004 23.742 0.5096 5.44 5.42 1.2875 RUN NUMBER 1W00706 AXIAL POSITION = 95.0 MM SPAN POSITION = 0.0 MM FREE-STREAM VELOCITY = 9.47 M/S FRICTION VELOCITY = 0.3920 M/S FREE-STREAM TURBULENCE = 5.244 % X-REYNOLDS NUMBER = 5.91 X10**4 FLUID DENSITY = 1.188 KG/M**3 KINEMATIC VISCOSITY = 1.523 X10(-5)MSQ/S BOUNDARY LAYER THICKNESS (99.0%) = 2.52 MM DISPLACEMENT THICKNESS = 0.644 MM MOMENTUM THICKNESS = 0.292 MM ENERGY THICKNESS = 0.477 MM FORM FACTOR H = 2.207 FORM FACTOR E = 1.636 RDELTASTAR = 400.1 RTHETA = 181.3 SKIN FRICTION COEFFICIENT = 0.003430 CALCULATED CF = 0.002732 Y Y/DEL YPLUS U U/UO UPLUS u u/UO u/U u/UTAU MM M/S M/S % % 0.117 0.046 2.999 1.238 0.131 3.158 0.3826 4.04 30.91 0.9760 0.123 0.049 3.160 1.285 0.136 3.278 0.4037 4.26 31.42 1.0298 0.135 0.054 3.482 1.396 0.147 3.561 0.4550 4.81 32.59 1.1605 0.154 0.061 3.965 1.583 0.167 4.038 0.5203 5.50 32.87 1.3273 0.167 0.066 4.286 1.698 0.179 4.331 0.5705 6.03 33.60 1.4552 0.185 0.074 4.769 1.864 0.197 4.755 0.6255 6.61 33.56 1.5956 0.204 0.081 5.252 2.045 0.216 5.215 0.6859 7.25 33.55 1.7495 0.229 0.091 5.895 2.284 0.241 5.826 0.7636 8.07 33.43 1.9478 0.254 0.101 6.539 2.550 0.269 6.504 0.8409 8.88 32.98 2.1450 0.279 0.111 7.182 2.789 0.295 7.114 0.9102 9.61 32.64 2.3217 0.310 0.123 7.987 3.094 0.327 7.893 0.9652 10.20 31.19 2.4620 0.342 0.136 8.791 3.423 0.362 8.731 1.0554 11.15 30.83 2.6920 0.379 0.151 9.757 3.788 0.400 9.661 1.1049 11.67 29.17 2.8185 0.417 0.166 10.722 4.137 0.437 10.552 1.1622 12.28 28.10 2.9647 0.460 0.183 11.849 4.469 0.472 11.399 1.1926 12.60 26.69 3.0421 0.510 0.203 13.136 4.889 0.516 12.471 1.2289 12.98 25.14 3.1348 0.560 0.223 14.423 5.260 0.556 13.417 1.2596 13.31 23.95 3.2129 0.623 0.248 16.032 5.699 0.602 14.538 1.2782 13.50 22.43 3.2605 0.685 0.272 17.641 6.076 0.642 15.499 1.2721 13.44 20.94 3.2448 0.760 0.302 19.572 6.487 0.685 16.548 1.2695 13.41 19.57 3.2381 0.835 0.332 21.502 6.810 0.719 17.371 1.2706 13.42 18.66 3.2412 0.923 0.367 23.755 7.167 0.757 18.281 1.2380 13.08 17.27 3.1579 1.023 0.407 26.329 7.533 0.796 19.215 1.1872 12.54 15.76 3.0283 1.129 0.449 29.065 7.831 0.827 19.975 1.1518 12.17 14.71 2.9380 1.248 0.496 32.122 8.166 0.863 20.831 1.0769 11.38 13.19 2.7469 1.379 0.548 35.501 8.425 0.890 21.490 1.0032 10.60 11.91 2.5591 1.523 0.605 39.201 8.673 0.916 22.122 0.9381 9.91 10.82 2.3929 1.679 0.668 43.224 8.883 0.938 22.659 0.8392 8.86 9.45 2.1406 1.854 0.737 47.729 9.056 0.957 23.100 0.7746 8.18 8.55 1.9758 2.048 0.814 52.717 9.199 0.972 23.464 0.7073 7.47 7.69 1.8041 2.260 0.899 58.187 9.315 0.984 23.760 0.6382 6.74 6.85 1.6280 2.498 0.993 64.301 9.368 0.990 23.895 0.5973 6.31 6.38 1.5237 2.735 1.087 70.416 9.433 0.996 24.063 0.5658 5.98 6.00 1.4431 2.967 1.179 76.369 9.442 0.997 24.084 0.5483 5.79 5.81 1.3987 3.204 1.274 82.483 9.466 1.000 24.147 0.5334 5.63 5.63 1.3605 3.442 1.368 88.597 9.462 1.000 24.137 0.5350 5.65 5.65 1.3648 4.692 1.865 120.777 9.470 1.000 24.157 0.5058 5.34 5.34 1.2902 5.942 2.362 152.956 9.486 1.002 24.198 0.5043 5.33 5.32 1.2864 7.192 2.859 185.136 9.478 1.001 24.175 0.4975 5.26 5.25 1.2690 8.442 3.356 217.316 9.494 1.003 24.217 0.4965 5.24 5.23 1.2664 RUN NUMBER 1W00904 AXIAL POSITION = 145.0 MM SPAN POSITION = 0.0 MM FREE-STREAM VELOCITY = 9.37 M/S FRICTION VELOCITY = 0.4359 M/S FREE-STREAM TURBULENCE = 5.019 % X-REYNOLDS NUMBER = 8.93 X10**4 FLUID DENSITY = 1.189 KG/M**3 KINEMATIC VISCOSITY = 1.521 X10(-5)MSQ/S BOUNDARY LAYER THICKNESS (99.0%) = 3.69 MM DISPLACEMENT THICKNESS = 0.751 MM MOMENTUM THICKNESS = 0.395 MM ENERGY THICKNESS = 0.667 MM FORM FACTOR H = 1.900 FORM FACTOR E = 1.687 RDELTASTAR = 462.4 RTHETA = 243.4 SKIN FRICTION COEFFICIENT = 0.004330 CALCULATED CF = 0.002222 Y Y/DEL YPLUS U U/UO UPLUS u u/UO u/U u/UTAU MM M/S M/S % % 0.104 0.028 2.980 1.330 0.142 3.052 0.5230 5.58 39.31 1.1998 0.117 0.032 3.339 1.473 0.157 3.379 0.6037 6.44 41.00 1.3851 0.129 0.035 3.697 1.604 0.171 3.681 0.6643 7.09 41.41 1.5240 0.142 0.038 4.055 1.726 0.184 3.959 0.7229 7.72 41.89 1.6585 0.160 0.043 4.592 1.938 0.207 4.447 0.8136 8.69 41.97 1.8667 0.179 0.049 5.130 2.118 0.226 4.859 0.8961 9.57 42.31 2.0560 0.198 0.054 5.667 2.288 0.244 5.249 0.9552 10.20 41.75 2.1915 0.223 0.060 6.383 2.519 0.269 5.779 1.0308 11.00 40.92 2.3649 0.248 0.067 7.100 2.754 0.294 6.319 1.1246 12.00 40.83 2.5801 0.279 0.076 7.995 3.046 0.325 6.989 1.1855 12.65 38.92 2.7199 0.310 0.084 8.891 3.339 0.356 7.661 1.2647 13.50 37.87 2.9016 0.348 0.094 9.966 3.707 0.396 8.504 1.3160 14.05 35.50 3.0193 0.385 0.104 11.040 4.053 0.433 9.298 1.3564 14.48 33.47 3.1120 0.429 0.116 12.294 4.412 0.471 10.121 1.4011 14.96 31.76 3.2145 0.479 0.130 13.727 4.771 0.509 10.946 1.4276 15.24 29.92 3.2753 0.535 0.145 15.339 5.184 0.553 11.894 1.4272 15.24 27.53 3.2745 0.598 0.162 17.130 5.525 0.590 12.675 1.4355 15.32 25.98 3.2934 0.667 0.181 19.100 5.844 0.624 13.407 1.4320 15.29 24.51 3.2854 0.748 0.203 21.428 6.184 0.660 14.188 1.3971 14.91 22.59 3.2053 0.829 0.225 23.757 6.478 0.691 14.862 1.3780 14.71 21.27 3.1614 0.929 0.252 26.623 6.808 0.727 15.619 1.3341 14.24 19.60 3.0608 1.035 0.281 29.667 7.105 0.758 16.300 1.3050 13.93 18.37 2.9939 1.148 0.311 32.891 7.355 0.785 16.874 1.2613 13.46 17.15 2.8937 1.285 0.348 36.832 7.643 0.816 17.534 1.1999 12.81 15.70 2.7528 1.429 0.387 40.951 7.871 0.840 18.058 1.1590 12.37 14.73 2.6592 1.592 0.431 45.608 8.072 0.862 18.520 1.1041 11.79 13.68 2.5332 1.779 0.482 50.981 8.321 0.888 19.089 1.0147 10.83 12.20 2.3281 1.979 0.536 56.713 8.533 0.911 19.577 0.9569 10.21 11.21 2.1953 2.210 0.599 63.340 8.695 0.928 19.948 0.8795 9.39 10.11 2.0177 2.460 0.667 70.504 8.875 0.947 20.363 0.7926 8.46 8.93 1.8184 2.742 0.743 78.564 9.010 0.962 20.671 0.7415 7.91 8.23 1.7011 3.054 0.828 87.519 9.129 0.974 20.944 0.6659 7.11 7.29 1.5278 3.404 0.923 97.549 9.224 0.985 21.162 0.6080 6.49 6.59 1.3948 3.798 1.029 108.833 9.289 0.992 21.312 0.5599 5.98 6.03 1.2845 4.185 1.134 119.938 9.357 0.999 21.467 0.5355 5.72 5.72 1.2287 4.579 1.241 131.222 9.363 0.999 21.482 0.5148 5.50 5.50 1.1812 4.967 1.346 142.326 9.379 1.001 21.518 0.4979 5.31 5.31 1.1423 5.360 1.453 153.610 9.383 1.002 21.528 0.4896 5.23 5.22 1.1233 7.260 1.968 208.059 9.400 1.003 21.566 0.4737 5.06 5.04 1.0868 9.160 2.483 262.508 9.392 1.003 21.548 0.4705 5.02 5.01 1.0795 11.060 2.998 316.956 9.396 1.003 21.558 0.4666 4.98 4.97 1.0706 12.960 3.513 371.405 9.352 0.998 21.455 0.4702 5.02 5.03 1.0788 RUN NUMBER 1W00707 AXIAL POSITION = 195.0 MM SPAN POSITION = 0.0 MM FREE-STREAM VELOCITY = 9.50 M/S FRICTION VELOCITY = 0.5088 M/S FREE-STREAM TURBULENCE = 4.714 % X-REYNOLDS NUMBER = 12.45 X10**4 FLUID DENSITY = 1.215 KG/M**3 KINEMATIC VISCOSITY = 1.488 X10(-5)MSQ/S BOUNDARY LAYER THICKNESS (99.0%) = 5.38 MM DISPLACEMENT THICKNESS = 0.866 MM MOMENTUM THICKNESS = 0.528 MM ENERGY THICKNESS = 0.918 MM FORM FACTOR H = 1.639 FORM FACTOR E = 1.738 RDELTASTAR = 553.0 RTHETA = 337.4 SKIN FRICTION COEFFICIENT = 0.005732 CALCULATED CF = 0.004000 LAW OF THE WALL OFFSET = 5.20 KARMAN CONSTANT = 0.410 FORM FACTOR G = 7.284 CLAUSER DELTA = 16.174 MM WAKE FACTOR PI = 0.186 1 Y Y/DEL YPLUS U U/UO UPLUS u u/UO u/U u/UTAU MM M/S M/S % % 0.092 0.017 3.128 1.532 0.161 3.010 0.5766 6.07 37.64 1.1332 0.098 0.018 3.342 1.601 0.168 3.147 0.6208 6.53 38.77 1.2200 0.110 0.021 3.769 1.764 0.186 3.467 0.6879 7.24 39.00 1.3520 0.129 0.024 4.410 2.002 0.211 3.934 0.7967 8.38 39.79 1.5657 0.142 0.026 4.838 2.150 0.226 4.226 0.8493 8.94 39.49 1.6691 0.160 0.030 5.479 2.392 0.252 4.701 0.9476 9.97 39.62 1.8624 0.179 0.033 6.120 2.644 0.278 5.196 1.0309 10.85 38.99 2.0262 0.204 0.038 6.975 2.911 0.306 5.721 1.1192 11.78 38.45 2.1997 0.229 0.043 7.829 3.189 0.336 6.268 1.1893 12.51 37.29 2.3375 0.254 0.047 8.684 3.458 0.364 6.796 1.2699 13.36 36.72 2.4959 0.285 0.053 9.753 3.806 0.400 7.480 1.3296 13.99 34.93 2.6132 0.323 0.060 11.035 4.182 0.440 8.219 1.3746 14.46 32.87 2.7016 0.367 0.068 12.531 4.525 0.476 8.894 1.4090 14.82 31.14 2.7693 0.410 0.076 14.026 4.874 0.513 9.580 1.4182 14.92 29.10 2.7873 0.460 0.086 15.736 5.154 0.542 10.129 1.4242 14.98 27.64 2.7991 0.517 0.096 17.659 5.492 0.578 10.793 1.4109 14.84 25.69 2.7730 0.579 0.108 19.796 5.811 0.611 11.421 1.4017 14.75 24.12 2.7549 0.648 0.120 22.147 6.059 0.637 11.907 1.3849 14.57 22.86 2.7218 0.729 0.136 24.924 6.359 0.669 12.498 1.3371 14.07 21.03 2.6279 0.817 0.152 27.916 6.619 0.696 13.010 1.3062 13.74 19.73 2.5672 0.917 0.170 31.335 6.876 0.723 13.514 1.2625 13.28 18.36 2.4813 1.029 0.191 35.181 7.111 0.748 13.975 1.2243 12.88 17.22 2.4061 1.160 0.216 39.669 7.339 0.772 14.423 1.1743 12.35 16.00 2.3079 1.298 0.241 44.370 7.514 0.791 14.767 1.1331 11.92 15.08 2.2269 1.460 0.272 49.926 7.740 0.814 15.213 1.0906 11.47 14.09 2.1433 1.635 0.304 55.909 7.922 0.833 15.570 1.0451 11.00 13.19 2.0540 1.842 0.342 62.961 8.096 0.852 15.912 0.9987 10.51 12.34 1.9628 2.067 0.384 70.653 8.269 0.870 16.252 0.9564 10.06 11.57 1.8796 2.317 0.431 79.201 8.424 0.886 16.556 0.9127 9.60 10.84 1.7939 2.598 0.483 88.817 8.601 0.905 16.904 0.8496 8.94 9.88 1.6697 2.917 0.542 99.715 8.792 0.925 17.279 0.7909 8.32 9.00 1.5544 3.273 0.609 111.895 8.950 0.942 17.590 0.7377 7.76 8.24 1.4498 3.679 0.684 125.785 9.102 0.958 17.889 0.6778 7.13 7.45 1.3321 4.123 0.767 140.956 9.212 0.969 18.105 0.6188 6.51 6.72 1.2161 4.629 0.861 158.265 9.325 0.981 18.328 0.5751 6.05 6.17 1.1302 5.198 0.967 177.711 9.390 0.988 18.455 0.5284 5.56 5.63 1.0385 5.760 1.071 196.942 9.450 0.994 18.573 0.5054 5.32 5.35 0.9932 6.329 1.177 216.388 9.473 0.997 18.619 0.4797 5.05 5.06 0.9429 6.898 1.283 235.833 9.502 1.000 18.674 0.4716 4.96 4.96 0.9269 7.460 1.388 255.065 9.505 1.000 18.681 0.4693 4.94 4.94 0.9223 10.060 1.871 343.959 9.517 1.001 18.705 0.4538 4.77 4.77 0.8919 12.660 2.355 432.853 9.524 1.002 18.719 0.4452 4.68 4.67 0.8749 15.260 2.838 521.746 9.527 1.002 18.725 0.4474 4.71 4.70 0.8793 17.860 3.322 610.640 9.537 1.003 18.743 0.4480 4.71 4.70 0.8806 RUN NUMBER 1W00708 AXIAL POSITION = 295.0 MM SPAN POSITION = 0.0 MM FREE-STREAM VELOCITY = 9.51 M/S FRICTION VELOCITY = 0.4947 M/S FREE-STREAM TURBULENCE = 4.334 % X-REYNOLDS NUMBER = 18.85 X10**4 FLUID DENSITY = 1.216 KG/M**3 KINEMATIC VISCOSITY = 1.488 X10(-5)MSQ/S BOUNDARY LAYER THICKNESS (99.0%) = 8.03 MM DISPLACEMENT THICKNESS = 1.183 MM MOMENTUM THICKNESS = 0.786 MM ENERGY THICKNESS = 1.389 MM FORM FACTOR H = 1.506 FORM FACTOR E = 1.768 RDELTASTAR = 755.9 RTHETA = 502.1 SKIN FRICTION COEFFICIENT = 0.005414 CALCULATED CF = 0.004430 LAW OF THE WALL OFFSET = 5.20 KARMAN CONSTANT = 0.410 FORM FACTOR G = 6.454 CLAUSER DELTA = 22.736 MM WAKE FACTOR PI = 0.018 1 Y Y/DEL YPLUS U U/UO UPLUS u u/UO u/U u/UTAU MM M/S M/S % % 0.098 0.012 3.250 1.523 0.160 3.079 0.5147 5.41 33.79 1.0403 0.117 0.015 3.873 1.747 0.184 3.532 0.6151 6.47 35.20 1.2433 0.129 0.016 4.289 1.912 0.201 3.865 0.6762 7.11 35.37 1.3668 0.148 0.018 4.912 2.196 0.231 4.438 0.7945 8.35 36.18 1.6058 0.173 0.022 5.744 2.537 0.267 5.127 0.9037 9.50 35.63 1.8266 0.192 0.024 6.367 2.798 0.294 5.656 0.9877 10.39 35.30 1.9964 0.223 0.028 7.406 3.182 0.335 6.431 1.0915 11.48 34.31 2.2063 0.248 0.031 8.237 3.489 0.367 7.052 1.1558 12.15 33.13 2.3361 0.285 0.036 9.484 3.881 0.408 7.844 1.2256 12.89 31.58 2.4773 0.323 0.040 10.731 4.255 0.447 8.601 1.2685 13.34 29.81 2.5639 0.367 0.046 12.186 4.566 0.480 9.228 1.2873 13.54 28.20 2.6020 0.417 0.052 13.848 4.916 0.517 9.937 1.2974 13.64 26.39 2.6224 0.479 0.060 15.926 5.303 0.558 10.718 1.2959 13.63 24.44 2.6193 0.542 0.067 18.004 5.563 0.585 11.244 1.2781 13.44 22.98 2.5833 0.617 0.077 20.498 5.868 0.617 11.861 1.2513 13.16 21.32 2.5292 0.698 0.087 23.199 6.083 0.640 12.295 1.2164 12.79 20.00 2.4587 0.798 0.099 26.524 6.356 0.668 12.847 1.1701 12.30 18.41 2.3650 0.904 0.113 30.057 6.575 0.691 13.289 1.1263 11.84 17.13 2.2766 1.029 0.128 34.213 6.807 0.716 13.758 1.0807 11.37 15.88 2.1845 1.167 0.145 38.785 6.963 0.732 14.074 1.0394 10.93 14.93 2.1009 1.329 0.166 44.187 7.171 0.754 14.495 0.9927 10.44 13.84 2.0065 1.504 0.187 50.006 7.324 0.770 14.803 0.9520 10.01 13.00 1.9242 1.710 0.213 56.863 7.503 0.789 15.166 0.9173 9.65 12.23 1.8541 1.948 0.243 64.760 7.652 0.805 15.467 0.8785 9.24 11.48 1.7756 2.210 0.275 73.488 7.819 0.822 15.805 0.8508 8.95 10.88 1.7196 2.510 0.313 83.462 7.992 0.840 16.154 0.8287 8.71 10.37 1.6750 2.854 0.355 94.892 8.155 0.858 16.484 0.8004 8.42 9.81 1.6179 3.242 0.404 107.775 8.350 0.878 16.878 0.7670 8.07 9.19 1.5502 3.685 0.459 122.530 8.542 0.898 17.265 0.7346 7.73 8.60 1.4848 4.185 0.521 139.154 8.684 0.913 17.553 0.7049 7.41 8.12 1.4249 4.754 0.592 158.064 8.882 0.934 17.954 0.6507 6.84 7.33 1.3152 5.404 0.673 179.676 9.034 0.950 18.261 0.6102 6.42 6.75 1.2334 6.135 0.764 203.989 9.181 0.966 18.558 0.5531 5.82 6.02 1.1180 6.973 0.868 231.834 9.313 0.979 18.824 0.5058 5.32 5.43 1.0223 7.917 0.986 263.213 9.408 0.989 19.015 0.4704 4.95 5.00 0.9507 8.998 1.121 299.163 9.459 0.995 19.119 0.4450 4.68 4.70 0.8994 10.073 1.255 334.905 9.501 0.999 19.204 0.4266 4.49 4.49 0.8622 11.154 1.389 370.855 9.497 0.999 19.196 0.4241 4.46 4.47 0.8572 12.229 1.523 406.598 9.512 1.000 19.227 0.4126 4.34 4.34 0.8339 13.304 1.657 442.340 9.503 0.999 19.209 0.4149 4.36 4.37 0.8387 17.804 2.217 591.959 9.514 1.001 19.231 0.4122 4.34 4.33 0.8332 22.304 2.778 741.578 9.527 1.002 19.258 0.4083 4.29 4.29 0.8253 26.804 3.338 891.197 9.530 1.002 19.264 0.4120 4.33 4.32 0.8327 31.304 3.899 1040.816 9.536 1.003 19.276 0.4121 4.33 4.32 0.8329 RUN NUMBER 1W00709 AXIAL POSITION = 395.0 MM SPAN POSITION = 0.0 MM FREE-STREAM VELOCITY = 9.54 M/S FRICTION VELOCITY = 0.4754 M/S FREE-STREAM TURBULENCE = 4.031 % X-REYNOLDS NUMBER = 25.30 X10**4 FLUID DENSITY = 1.215 KG/M**3 KINEMATIC VISCOSITY = 1.489 X10(-5)MSQ/S BOUNDARY LAYER THICKNESS (99.0%) = 10.19 MM DISPLACEMENT THICKNESS = 1.517 MM MOMENTUM THICKNESS = 1.030 MM ENERGY THICKNESS = 1.821 MM FORM FACTOR H = 1.474 FORM FACTOR E = 1.769 RDELTASTAR = 971.8 RTHETA = 659.4 SKIN FRICTION COEFFICIENT = 0.004970 CALCULATED CF = 0.004327 LAW OF THE WALL OFFSET = 5.20 KARMAN CONSTANT = 0.410 FORM FACTOR G = 6.449 CLAUSER DELTA = 30.436 MM WAKE FACTOR PI = 0.079 1 Y Y/DEL YPLUS U U/UO UPLUS u u/UO u/U u/UTAU MM M/S M/S % % 0.104 0.010 3.321 1.551 0.163 3.263 0.5368 5.63 34.60 1.1292 0.123 0.012 3.919 1.774 0.186 3.732 0.6270 6.58 35.34 1.3189 0.142 0.014 4.518 2.020 0.212 4.250 0.7303 7.66 36.15 1.5363 0.160 0.016 5.117 2.243 0.235 4.719 0.8108 8.50 36.15 1.7057 0.179 0.018 5.715 2.452 0.257 5.159 0.8847 9.28 36.08 1.8611 0.210 0.021 6.713 2.831 0.297 5.956 1.0008 10.50 35.35 2.1053 0.235 0.023 7.511 3.093 0.324 6.507 1.0664 11.18 34.48 2.2434 0.273 0.027 8.709 3.495 0.367 7.352 1.1445 12.00 32.75 2.4077 0.310 0.030 9.906 3.854 0.404 8.107 1.1936 12.52 30.97 2.5110 0.354 0.035 11.303 4.199 0.440 8.834 1.2383 12.99 29.49 2.6050 0.404 0.040 12.899 4.515 0.473 9.498 1.2628 13.24 27.97 2.6566 0.460 0.045 14.695 4.873 0.511 10.252 1.2554 13.17 25.76 2.6408 0.529 0.052 16.890 5.187 0.544 10.912 1.2440 13.05 23.98 2.6169 0.604 0.059 19.285 5.479 0.575 11.525 1.2247 12.84 22.35 2.5764 0.692 0.068 22.079 5.781 0.606 12.162 1.1974 12.56 20.71 2.5188 0.785 0.077 25.072 6.017 0.631 12.658 1.1444 12.00 19.02 2.4075 0.898 0.088 28.664 6.272 0.658 13.195 1.1028 11.57 17.58 2.3200 1.023 0.100 32.655 6.454 0.677 13.578 1.0590 11.11 16.41 2.2277 1.173 0.115 37.445 6.650 0.697 13.988 1.0067 10.56 15.14 2.1177 1.335 0.131 42.633 6.842 0.718 14.394 0.9745 10.22 14.24 2.0500 1.523 0.149 48.620 6.972 0.731 14.666 0.9295 9.75 13.33 1.9553 1.742 0.171 55.604 7.163 0.751 15.068 0.9020 9.46 12.59 1.8976 1.985 0.195 63.387 7.331 0.769 15.422 0.8630 9.05 11.77 1.8155 2.267 0.222 72.367 7.486 0.785 15.747 0.8369 8.78 11.18 1.7606 2.592 0.254 82.744 7.643 0.802 16.079 0.8133 8.53 10.64 1.7110 2.960 0.290 94.518 7.829 0.821 16.469 0.7903 8.29 10.09 1.6625 3.373 0.331 107.689 8.018 0.841 16.868 0.7672 8.05 9.57 1.6138 3.854 0.378 123.054 8.206 0.861 17.263 0.7412 7.77 9.03 1.5593 4.398 0.431 140.416 8.385 0.879 17.640 0.7161 7.51 8.54 1.5063 5.017 0.492 160.172 8.579 0.900 18.047 0.6827 7.16 7.96 1.4362 5.729 0.562 182.921 8.774 0.920 18.457 0.6487 6.80 7.39 1.3647 6.542 0.642 208.864 8.968 0.940 18.866 0.6011 6.30 6.70 1.2644 7.467 0.732 238.398 9.150 0.960 19.248 0.5447 5.71 5.95 1.1459 8.517 0.835 271.923 9.282 0.973 19.525 0.5078 5.33 5.47 1.0683 9.723 0.954 310.438 9.413 0.987 19.801 0.4580 4.80 4.87 0.9634 11.098 1.089 354.340 9.484 0.995 19.950 0.4196 4.40 4.42 0.8827 12.473 1.224 398.243 9.516 0.998 20.018 0.4026 4.22 4.23 0.8470 13.848 1.358 442.145 9.537 1.000 20.062 0.3919 4.11 4.11 0.8244 15.217 1.493 485.848 9.527 0.999 20.041 0.3879 4.07 4.07 0.8160 16.592 1.628 529.750 9.536 1.000 20.061 0.3858 4.05 4.05 0.8116 22.142 2.172 706.956 9.545 1.001 20.080 0.3838 4.03 4.02 0.8074 27.692 2.717 884.162 9.545 1.001 20.078 0.3807 3.99 3.99 0.8009 33.242 3.261 1061.368 9.565 1.003 20.120 0.3821 4.01 3.99 0.8037 38.792 3.806 1238.575 9.565 1.003 20.122 0.3843 4.03 4.02 0.8085 RUN NUMBER 1W00710 AXIAL POSITION = 495.0 MM SPAN POSITION = 0.0 MM FREE-STREAM VELOCITY = 9.57 M/S FRICTION VELOCITY = 0.4605 M/S FREE-STREAM TURBULENCE = 3.724 % X-REYNOLDS NUMBER = 31.81 X10**4 FLUID DENSITY = 1.214 KG/M**3 KINEMATIC VISCOSITY = 1.490 X10(-5)MSQ/S BOUNDARY LAYER THICKNESS (99.0%) = 13.65 MM DISPLACEMENT THICKNESS = 1.910 MM MOMENTUM THICKNESS = 1.320 MM ENERGY THICKNESS = 2.341 MM FORM FACTOR H = 1.447 FORM FACTOR E = 1.773 RDELTASTAR = 1227.8 RTHETA = 848.5 SKIN FRICTION COEFFICIENT = 0.004625 CALCULATED CF = 0.004217 LAW OF THE WALL OFFSET = 5.20 KARMAN CONSTANT = 0.410 FORM FACTOR G = 6.424 CLAUSER DELTA = 39.725 MM WAKE FACTOR PI = 0.152 1 Y Y/DEL YPLUS U U/UO UPLUS u u/UO u/U u/UTAU MM M/S M/S % % 0.098 0.007 3.021 1.378 0.144 2.992 0.4635 4.84 33.64 1.0066 0.110 0.008 3.408 1.519 0.159 3.299 0.5288 5.52 34.81 1.1484 0.129 0.009 3.987 1.736 0.181 3.770 0.6131 6.40 35.32 1.3315 0.148 0.011 4.567 1.929 0.201 4.190 0.6935 7.24 35.95 1.5062 0.167 0.012 5.146 2.133 0.223 4.632 0.7773 8.12 36.44 1.6880 0.192 0.014 5.919 2.414 0.252 5.243 0.8668 9.05 35.90 1.8825 0.223 0.016 6.885 2.739 0.286 5.949 0.9723 10.15 35.50 2.1117 0.254 0.019 7.850 3.041 0.318 6.604 1.0501 10.97 34.53 2.2805 0.292 0.021 9.009 3.398 0.355 7.380 1.1176 11.67 32.89 2.4273 0.335 0.025 10.362 3.790 0.396 8.232 1.1834 12.36 31.22 2.5702 0.379 0.028 11.714 4.081 0.426 8.862 1.2086 12.62 29.62 2.6249 0.435 0.032 13.452 4.446 0.464 9.656 1.2237 12.78 27.52 2.6577 0.504 0.037 15.577 4.787 0.500 10.397 1.2262 12.81 25.61 2.6630 0.573 0.042 17.702 5.130 0.536 11.142 1.2275 12.82 23.93 2.6658 0.660 0.048 20.406 5.430 0.567 11.793 1.1927 12.46 21.96 2.5904 0.754 0.055 23.304 5.685 0.594 12.347 1.1531 12.04 20.28 2.5043 0.867 0.063 26.781 5.933 0.620 12.885 1.1126 11.62 18.75 2.4163 0.992 0.073 30.644 6.153 0.643 13.363 1.0642 11.11 17.30 2.3112 1.135 0.083 35.087 6.351 0.663 13.792 1.0163 10.61 16.00 2.2072 1.304 0.096 40.303 6.516 0.681 14.152 0.9746 10.18 14.96 2.1166 1.498 0.110 46.291 6.706 0.700 14.564 0.9312 9.73 13.89 2.0223 1.710 0.125 52.859 6.874 0.718 14.929 0.9001 9.40 13.09 1.9548 1.960 0.144 60.586 7.031 0.734 15.270 0.8628 9.01 12.27 1.8738 2.248 0.165 69.472 7.181 0.750 15.596 0.8476 8.85 11.80 1.8408 2.579 0.189 79.710 7.353 0.768 15.968 0.8220 8.59 11.18 1.7852 2.954 0.216 91.300 7.529 0.786 16.350 0.7939 8.29 10.55 1.7242 3.385 0.248 104.628 7.710 0.805 16.745 0.7827 8.17 10.15 1.7000 3.879 0.284 119.889 7.884 0.823 17.121 0.7621 7.96 9.67 1.6551 4.442 0.325 137.274 8.104 0.846 17.601 0.7388 7.72 9.12 1.6045 5.092 0.373 157.364 8.298 0.867 18.021 0.7179 7.50 8.65 1.5591 5.835 0.427 180.351 8.500 0.888 18.461 0.6794 7.10 7.99 1.4755 6.685 0.490 206.622 8.688 0.907 18.868 0.6437 6.72 7.41 1.3981 7.660 0.561 236.756 8.897 0.929 19.323 0.5972 6.24 6.71 1.2970 8.773 0.643 271.141 9.112 0.952 19.788 0.5477 5.72 6.01 1.1894 10.054 0.736 310.740 9.250 0.966 20.090 0.4888 5.10 5.28 1.0615 11.517 0.843 355.942 9.381 0.980 20.374 0.4419 4.61 4.71 0.9596 13.198 0.967 407.905 9.460 0.988 20.546 0.4104 4.29 4.34 0.8912 14.873 1.089 459.674 9.525 0.995 20.687 0.3790 3.96 3.98 0.8231 16.554 1.212 511.637 9.551 0.997 20.742 0.3729 3.89 3.90 0.8098 18.235 1.336 563.599 9.555 0.998 20.752 0.3618 3.78 3.79 0.7858 19.910 1.458 615.369 9.561 0.999 20.764 0.3532 3.69 3.69 0.7671 26.510 1.942 819.356 9.584 1.001 20.815 0.3507 3.66 3.66 0.7617 33.110 2.425 1023.343 9.589 1.001 20.826 0.3508 3.66 3.66 0.7618 39.710 2.908 1227.330 9.620 1.005 20.892 0.3506 3.66 3.64 0.7614 46.310 3.392 1431.317 9.614 1.004 20.880 0.3566 3.72 3.71 0.7744 RUN NUMBER 1W00801 AXIAL POSITION = 595.0 MM SPAN POSITION = 0.0 MM FREE-STREAM VELOCITY = 9.60 M/S FRICTION VELOCITY = 0.4541 M/S FREE-STREAM TURBULENCE = 3.484 % X-REYNOLDS NUMBER = 38.22 X10**4 FLUID DENSITY = 1.210 KG/M**3 KINEMATIC VISCOSITY = 1.495 X10(-5)MSQ/S BOUNDARY LAYER THICKNESS (99.0%) = 15.33 MM DISPLACEMENT THICKNESS = 2.170 MM MOMENTUM THICKNESS = 1.521 MM ENERGY THICKNESS = 2.704 MM FORM FACTOR H = 1.427 FORM FACTOR E = 1.778 RDELTASTAR = 1394.1 RTHETA = 977.2 SKIN FRICTION COEFFICIENT = 0.004474 CALCULATED CF = 0.004191 LAW OF THE WALL OFFSET = 5.20 KARMAN CONSTANT = 0.410 FORM FACTOR G = 6.323 CLAUSER DELTA = 45.886 MM WAKE FACTOR PI = 0.160 1 Y Y/DEL YPLUS U U/UO UPLUS u u/UO u/U u/UTAU MM M/S M/S % % 0.117 0.008 3.539 1.520 0.158 3.347 0.5304 5.52 34.90 1.1681 0.129 0.008 3.919 1.654 0.172 3.642 0.5849 6.09 35.37 1.2881 0.154 0.010 4.679 1.940 0.202 4.272 0.6970 7.26 35.93 1.5349 0.173 0.011 5.248 2.161 0.225 4.758 0.7969 8.30 36.88 1.7549 0.198 0.013 6.008 2.424 0.252 5.338 0.8830 9.20 36.43 1.9445 0.229 0.015 6.957 2.778 0.289 6.117 0.9768 10.17 35.17 2.1512 0.267 0.017 8.097 3.123 0.325 6.876 1.0697 11.14 34.26 2.3556 0.304 0.020 9.236 3.452 0.360 7.602 1.1329 11.80 32.82 2.4948 0.354 0.023 10.755 3.867 0.403 8.516 1.1977 12.47 30.97 2.6376 0.404 0.026 12.274 4.225 0.440 9.305 1.2163 12.67 28.79 2.6786 0.467 0.030 14.173 4.562 0.475 10.046 1.2235 12.74 26.82 2.6942 0.535 0.035 16.261 4.876 0.508 10.738 1.2169 12.67 24.96 2.6799 0.617 0.040 18.730 5.213 0.543 11.479 1.1965 12.46 22.95 2.6350 0.710 0.046 21.578 5.494 0.572 12.100 1.1681 12.17 21.26 2.5723 0.817 0.053 24.806 5.747 0.599 12.655 1.1276 11.74 19.62 2.4831 0.942 0.061 28.604 5.970 0.622 13.146 1.0761 11.21 18.03 2.3697 1.079 0.070 32.781 6.179 0.644 13.607 1.0304 10.73 16.67 2.2690 1.242 0.081 37.718 6.346 0.661 13.974 0.9958 10.37 15.69 2.1929 1.429 0.093 43.414 6.529 0.680 14.379 0.9614 10.01 14.72 2.1172 1.642 0.107 49.870 6.690 0.697 14.734 0.9215 9.60 13.77 2.0293 1.892 0.123 57.465 6.845 0.713 15.073 0.8854 9.22 12.94 1.9498 2.173 0.142 66.010 7.006 0.730 15.427 0.8563 8.92 12.22 1.8858 2.498 0.163 75.884 7.204 0.750 15.865 0.8345 8.69 11.58 1.8378 2.873 0.187 87.277 7.373 0.768 16.238 0.8189 8.53 11.11 1.8034 3.304 0.216 100.379 7.543 0.786 16.612 0.8014 8.35 10.62 1.7649 3.798 0.248 115.379 7.706 0.803 16.971 0.7785 8.11 10.10 1.7144 4.367 0.285 132.658 7.901 0.823 17.400 0.7633 7.95 9.66 1.6809 5.017 0.327 152.406 8.100 0.844 17.838 0.7465 7.77 9.22 1.6438 5.767 0.376 175.192 8.315 0.866 18.311 0.7249 7.55 8.72 1.5963 6.629 0.432 201.395 8.507 0.886 18.733 0.6799 7.08 7.99 1.4972 7.623 0.497 231.586 8.713 0.907 19.187 0.6436 6.70 7.39 1.4174 8.760 0.571 266.144 8.913 0.928 19.627 0.5990 6.24 6.72 1.3191 10.073 0.657 306.019 9.108 0.949 20.058 0.5467 5.69 6.00 1.2040 11.579 0.755 351.781 9.284 0.967 20.446 0.4844 5.04 5.22 1.0667 13.310 0.868 404.378 9.411 0.980 20.724 0.4267 4.44 4.53 0.9397 15.298 0.998 464.760 9.504 0.990 20.930 0.3844 4.00 4.04 0.8464 17.285 1.128 525.142 9.550 0.995 21.031 0.3568 3.72 3.74 0.7856 19.273 1.257 585.524 9.568 0.997 21.070 0.3502 3.65 3.66 0.7712 21.267 1.387 646.096 9.586 0.998 21.111 0.3386 3.53 3.53 0.7457 23.254 1.517 706.478 9.596 0.999 21.133 0.3389 3.53 3.53 0.7464 30.904 2.016 938.892 9.611 1.001 21.166 0.3315 3.45 3.45 0.7301 38.554 2.515 1171.306 9.630 1.003 21.208 0.3320 3.46 3.45 0.7312 46.204 3.014 1403.720 9.626 1.003 21.198 0.3349 3.49 3.48 0.7375 53.854 3.513 1636.134 9.642 1.004 21.234 0.3345 3.48 3.47 0.7366 RUN NUMBER 1W00802 AXIAL POSITION = 695.0 MM SPAN POSITION = 0.0 MM FREE-STREAM VELOCITY = 9.61 M/S FRICTION VELOCITY = 0.4456 M/S FREE-STREAM TURBULENCE = 3.276 % X-REYNOLDS NUMBER = 44.69 X10**4 FLUID DENSITY = 1.210 KG/M**3 KINEMATIC VISCOSITY = 1.495 X10(-5)MSQ/S BOUNDARY LAYER THICKNESS (99.0%) = 16.73 MM DISPLACEMENT THICKNESS = 2.436 MM MOMENTUM THICKNESS = 1.705 MM ENERGY THICKNESS = 3.021 MM FORM FACTOR H = 1.429 FORM FACTOR E = 1.773 RDELTASTAR = 1566.2 RTHETA = 1095.9 SKIN FRICTION COEFFICIENT = 0.004297 CALCULATED CF = 0.004049 LAW OF THE WALL OFFSET = 5.20 KARMAN CONSTANT = 0.410 FORM FACTOR G = 6.478 CLAUSER DELTA = 52.552 MM WAKE FACTOR PI = 0.184 1 Y Y/DEL YPLUS U U/UO UPLUS u u/UO u/U u/UTAU MM M/S M/S % % 0.117 0.007 3.472 1.451 0.151 3.257 0.5091 5.30 35.08 1.1425 0.135 0.008 4.031 1.654 0.172 3.712 0.5952 6.19 35.99 1.3358 0.154 0.009 4.590 1.854 0.193 4.161 0.6737 7.01 36.34 1.5121 0.179 0.011 5.335 2.124 0.221 4.767 0.7817 8.13 36.80 1.7543 0.210 0.013 6.266 2.424 0.252 5.441 0.8851 9.21 36.51 1.9865 0.242 0.014 7.198 2.756 0.287 6.186 0.9715 10.11 35.25 2.1803 0.279 0.017 8.315 3.093 0.322 6.941 1.0571 11.00 34.18 2.3725 0.323 0.019 9.619 3.464 0.360 7.774 1.1246 11.70 32.47 2.5240 0.373 0.022 11.109 3.841 0.400 8.620 1.1752 12.23 30.60 2.6375 0.429 0.026 12.786 4.197 0.437 9.420 1.2060 12.55 28.73 2.7067 0.492 0.029 14.649 4.498 0.468 10.096 1.2125 12.61 26.95 2.7211 0.567 0.034 16.884 4.812 0.501 10.800 1.1965 12.45 24.86 2.6854 0.654 0.039 19.492 5.147 0.535 11.551 1.1785 12.26 22.90 2.6449 0.754 0.045 22.472 5.431 0.565 12.189 1.1400 11.86 20.99 2.5586 0.873 0.052 26.011 5.691 0.592 12.771 1.1079 11.53 19.47 2.4863 1.004 0.060 29.923 5.910 0.615 13.263 1.0583 11.01 17.91 2.3751 1.160 0.069 34.580 6.123 0.637 13.743 1.0167 10.58 16.60 2.2819 1.335 0.080 39.795 6.304 0.656 14.148 0.9766 10.16 15.49 2.1918 1.535 0.092 45.756 6.479 0.674 14.540 0.9388 9.77 14.49 2.1070 1.773 0.106 52.835 6.604 0.687 14.822 0.9069 9.44 13.73 2.0354 2.042 0.122 60.844 6.802 0.708 15.265 0.8752 9.11 12.87 1.9642 2.354 0.141 70.158 6.954 0.723 15.607 0.8499 8.84 12.22 1.9073 2.717 0.162 80.962 7.107 0.739 15.950 0.8281 8.61 11.65 1.8584 3.129 0.187 93.256 7.287 0.758 16.355 0.8080 8.41 11.09 1.8135 3.610 0.216 107.599 7.464 0.777 16.752 0.7930 8.25 10.62 1.7798 4.160 0.249 123.991 7.623 0.793 17.108 0.7741 8.05 10.16 1.7374 4.792 0.286 142.804 7.839 0.815 17.592 0.7664 7.97 9.78 1.7201 5.523 0.330 164.598 8.034 0.836 18.032 0.7403 7.70 9.21 1.6614 6.367 0.381 189.745 8.254 0.859 18.525 0.7209 7.50 8.73 1.6179 7.335 0.438 218.618 8.474 0.882 19.018 0.6818 7.09 8.05 1.5302 8.460 0.506 252.147 8.663 0.901 19.443 0.6519 6.78 7.52 1.4630 9.748 0.583 290.519 8.892 0.925 19.955 0.6031 6.27 6.78 1.3535 11.235 0.671 334.852 9.102 0.947 20.428 0.5398 5.62 5.93 1.2115 12.948 0.774 385.891 9.290 0.966 20.850 0.4868 5.06 5.24 1.0924 14.923 0.892 444.753 9.431 0.981 21.166 0.4239 4.41 4.49 0.9513 17.198 1.028 512.557 9.535 0.992 21.400 0.3754 3.91 3.94 0.8424 19.473 1.164 580.360 9.585 0.997 21.511 0.3465 3.60 3.62 0.7776 21.748 1.300 648.163 9.611 1.000 21.570 0.3291 3.42 3.42 0.7386 24.023 1.436 715.967 9.601 0.999 21.548 0.3261 3.39 3.40 0.7318 26.298 1.572 783.770 9.626 1.001 21.603 0.3157 3.28 3.28 0.7084 34.898 2.086 1040.082 9.633 1.002 21.618 0.3159 3.29 3.28 0.7090 43.498 2.600 1296.394 9.639 1.003 21.632 0.3160 3.29 3.28 0.7092 52.098 3.114 1552.706 9.644 1.003 21.644 0.3136 3.26 3.25 0.7038 60.698 3.628 1809.017 9.638 1.003 21.630 0.3149 3.28 3.27 0.7068 RUN NUMBER 1W00803 AXIAL POSITION = 895.0 MM SPAN POSITION = 0.0 MM FREE-STREAM VELOCITY = 9.69 M/S FRICTION VELOCITY = 0.4338 M/S FREE-STREAM TURBULENCE = 2.965 % X-REYNOLDS NUMBER = 57.94 X10**4 FLUID DENSITY = 1.208 KG/M**3 KINEMATIC VISCOSITY = 1.497 X10(-5)MSQ/S BOUNDARY LAYER THICKNESS (99.0%) = 21.58 MM DISPLACEMENT THICKNESS = 3.107 MM MOMENTUM THICKNESS = 2.213 MM ENERGY THICKNESS = 3.932 MM FORM FACTOR H = 1.404 FORM FACTOR E = 1.777 RDELTASTAR = 2011.2 RTHETA = 1432.5 SKIN FRICTION COEFFICIENT = 0.004007 CALCULATED CF = 0.003919 LAW OF THE WALL OFFSET = 5.20 KARMAN CONSTANT = 0.410 FORM FACTOR G = 6.428 CLAUSER DELTA = 69.410 MM WAKE FACTOR PI = 0.247 1 Y Y/DEL YPLUS U U/UO UPLUS u u/UO u/U u/UTAU MM M/S M/S % % 0.123 0.006 3.557 1.449 0.149 3.340 0.5103 5.27 35.23 1.1764 0.142 0.007 4.100 1.634 0.169 3.766 0.5891 6.08 36.06 1.3582 0.167 0.008 4.824 1.905 0.197 4.391 0.7015 7.24 36.83 1.6172 0.192 0.009 5.549 2.152 0.222 4.961 0.7915 8.17 36.78 1.8247 0.223 0.010 6.454 2.450 0.253 5.648 0.8964 9.25 36.59 2.0666 0.260 0.012 7.541 2.773 0.286 6.393 0.9905 10.22 35.71 2.2834 0.298 0.014 8.627 3.102 0.320 7.151 1.0591 10.93 34.14 2.4416 0.348 0.016 10.076 3.516 0.363 8.106 1.1249 11.61 31.99 2.5933 0.404 0.019 11.706 3.895 0.402 8.980 1.1664 12.04 29.94 2.6889 0.467 0.022 13.517 4.244 0.438 9.783 1.1788 12.16 27.78 2.7175 0.542 0.025 15.690 4.571 0.472 10.538 1.1842 12.22 25.91 2.7300 0.629 0.029 18.226 4.918 0.508 11.338 1.1775 12.15 23.94 2.7145 0.729 0.034 21.123 5.184 0.535 11.951 1.1361 11.72 21.91 2.6191 0.848 0.039 24.564 5.488 0.566 12.653 1.1084 11.44 20.20 2.5554 0.979 0.045 28.367 5.684 0.587 13.104 1.0636 10.98 18.71 2.4520 1.135 0.053 32.894 5.882 0.607 13.559 1.0238 10.56 17.41 2.3602 1.317 0.061 38.146 6.062 0.626 13.974 0.9791 10.10 16.15 2.2573 1.529 0.071 44.304 6.240 0.644 14.387 0.9324 9.62 14.94 2.1496 1.767 0.082 51.185 6.424 0.663 14.809 0.9031 9.32 14.06 2.0819 2.048 0.095 59.335 6.608 0.682 15.235 0.8812 9.09 13.34 2.0316 2.373 0.110 68.752 6.757 0.697 15.577 0.8469 8.74 12.53 1.9524 2.748 0.127 79.617 6.916 0.714 15.943 0.8292 8.56 11.99 1.9116 3.185 0.148 92.294 7.074 0.730 16.309 0.8057 8.31 11.39 1.8575 3.685 0.171 106.782 7.243 0.747 16.698 0.7960 8.21 10.99 1.8351 4.273 0.198 123.805 7.401 0.764 17.062 0.7825 8.08 10.57 1.8040 4.948 0.229 143.363 7.607 0.785 17.536 0.7642 7.89 10.05 1.7617 5.729 0.265 166.001 7.787 0.804 17.951 0.7563 7.80 9.71 1.7436 6.635 0.307 192.260 8.003 0.826 18.449 0.7367 7.60 9.21 1.6984 7.685 0.356 222.684 8.193 0.846 18.889 0.7166 7.39 8.75 1.6520 8.904 0.413 257.998 8.451 0.872 19.483 0.6874 7.09 8.13 1.5846 10.317 0.478 298.926 8.695 0.897 20.044 0.6427 6.63 7.39 1.4816 11.948 0.554 346.192 8.888 0.917 20.491 0.5944 6.13 6.69 1.3703 13.835 0.641 400.883 9.117 0.941 21.019 0.5383 5.56 5.90 1.2411 16.023 0.742 464.267 9.316 0.961 21.478 0.4720 4.87 5.07 1.0882 18.560 0.860 537.792 9.481 0.978 21.858 0.4097 4.23 4.32 0.9445 21.498 0.996 622.908 9.591 0.990 22.112 0.3469 3.58 3.62 0.7996 24.435 1.132 708.023 9.656 0.996 22.262 0.3107 3.21 3.22 0.7163 27.373 1.268 793.139 9.667 0.998 22.285 0.2960 3.05 3.06 0.6825 30.304 1.404 878.073 9.685 0.999 22.328 0.2926 3.02 3.02 0.6745 33.242 1.540 963.189 9.682 0.999 22.320 0.2850 2.94 2.94 0.6569 43.992 2.038 1274.675 9.705 1.002 22.375 0.2871 2.96 2.96 0.6620 54.742 2.536 1586.162 9.719 1.003 22.406 0.2837 2.93 2.92 0.6540 65.492 3.034 1897.649 9.708 1.002 22.380 0.2860 2.95 2.95 0.6592 76.242 3.533 2209.135 9.701 1.001 22.365 0.2873 2.96 2.96 0.6623 RUN NUMBER 1W00804 AXIAL POSITION = 1095.0 MM SPAN POSITION = 0.0 MM FREE-STREAM VELOCITY = 9.60 M/S FRICTION VELOCITY = 0.4238 M/S FREE-STREAM TURBULENCE = 2.749 % X-REYNOLDS NUMBER = 70.18 X10**4 FLUID DENSITY = 1.208 KG/M**3 KINEMATIC VISCOSITY = 1.498 X10(-5)MSQ/S BOUNDARY LAYER THICKNESS (99.0%) = 24.02 MM DISPLACEMENT THICKNESS = 3.533 MM MOMENTUM THICKNESS = 2.533 MM ENERGY THICKNESS = 4.502 MM FORM FACTOR H = 1.395 FORM FACTOR E = 1.777 RDELTASTAR = 2264.4 RTHETA = 1623.2 SKIN FRICTION COEFFICIENT = 0.003900 CALCULATED CF = 0.003843 LAW OF THE WALL OFFSET = 5.20 KARMAN CONSTANT = 0.410 FORM FACTOR G = 6.413 CLAUSER DELTA = 80.016 MM WAKE FACTOR PI = 0.224 1 Y Y/DEL YPLUS U U/UO UPLUS u u/UO u/U u/UTAU MM M/S M/S % % 0.110 0.005 3.120 1.263 0.132 2.979 0.4346 4.53 34.43 1.0255 0.129 0.005 3.651 1.431 0.149 3.376 0.5087 5.30 35.55 1.2002 0.148 0.006 4.181 1.603 0.167 3.782 0.5881 6.13 36.69 1.3876 0.173 0.007 4.889 1.834 0.191 4.326 0.6813 7.10 37.16 1.6075 0.198 0.008 5.596 2.092 0.218 4.937 0.7759 8.08 37.08 1.8306 0.235 0.010 6.657 2.427 0.253 5.726 0.8917 9.29 36.74 2.1038 0.273 0.011 7.719 2.757 0.287 6.504 0.9751 10.16 35.37 2.3008 0.317 0.013 8.957 3.083 0.321 7.274 1.0477 10.92 33.98 2.4721 0.367 0.015 10.372 3.459 0.360 8.161 1.1035 11.50 31.90 2.6036 0.423 0.018 11.964 3.824 0.398 9.023 1.1444 11.92 29.92 2.7000 0.492 0.020 13.909 4.186 0.436 9.875 1.1704 12.19 27.96 2.7615 0.573 0.024 16.208 4.565 0.476 10.770 1.1638 12.12 25.50 2.7458 0.667 0.028 18.862 4.874 0.508 11.500 1.1459 11.94 23.51 2.7037 0.773 0.032 21.868 5.152 0.537 12.155 1.1216 11.69 21.77 2.6463 0.904 0.038 25.583 5.411 0.564 12.768 1.0777 11.23 19.92 2.5428 1.048 0.044 29.651 5.614 0.585 13.245 1.0416 10.85 18.56 2.4576 1.217 0.051 34.426 5.837 0.608 13.771 0.9925 10.34 17.00 2.3416 1.417 0.059 40.086 6.018 0.627 14.200 0.9496 9.89 15.78 2.2404 1.642 0.068 46.453 6.159 0.642 14.532 0.9098 9.48 14.77 2.1467 1.910 0.080 54.059 6.362 0.663 15.011 0.8921 9.29 14.02 2.1048 2.217 0.092 62.726 6.495 0.677 15.323 0.8553 8.91 13.17 2.0179 2.573 0.107 72.807 6.630 0.691 15.643 0.8275 8.62 12.48 1.9525 2.992 0.125 84.658 6.789 0.707 16.017 0.8142 8.48 11.99 1.9211 3.473 0.145 98.277 6.958 0.725 16.418 0.8021 8.36 11.53 1.8924 4.035 0.168 114.195 7.119 0.742 16.798 0.7876 8.21 11.06 1.8582 4.685 0.195 132.590 7.285 0.759 17.189 0.7747 8.07 10.63 1.8277 5.442 0.227 153.991 7.479 0.779 17.646 0.7692 8.01 10.29 1.8149 6.323 0.263 178.930 7.653 0.797 18.057 0.7447 7.76 9.73 1.7571 7.342 0.306 207.760 7.863 0.819 18.552 0.7324 7.63 9.31 1.7279 8.523 0.355 241.189 8.101 0.844 19.113 0.7053 7.35 8.71 1.6641 9.904 0.412 280.277 8.316 0.866 19.621 0.6766 7.05 8.14 1.5965 11.498 0.479 325.379 8.535 0.889 20.139 0.6450 6.72 7.56 1.5219 13.354 0.556 377.910 8.753 0.912 20.653 0.5922 6.17 6.77 1.3973 15.510 0.646 438.931 8.978 0.935 21.182 0.5508 5.74 6.13 1.2995 18.017 0.750 509.856 9.201 0.959 21.708 0.4796 5.00 5.21 1.1316 20.923 0.871 592.101 9.368 0.976 22.102 0.4073 4.24 4.35 0.9609 24.298 1.012 687.612 9.513 0.991 22.446 0.3400 3.54 3.57 0.8022 27.673 1.152 783.122 9.555 0.996 22.545 0.2982 3.11 3.12 0.7036 31.048 1.293 878.633 9.586 0.999 22.617 0.2837 2.96 2.96 0.6694 34.423 1.433 974.143 9.602 1.000 22.655 0.2708 2.82 2.82 0.6389 37.798 1.574 1069.654 9.621 1.002 22.699 0.2625 2.74 2.73 0.6194 48.185 2.006 1363.614 9.626 1.003 22.711 0.2657 2.77 2.76 0.6269 58.567 2.438 1657.397 9.626 1.003 22.711 0.2644 2.75 2.75 0.6237 68.954 2.871 1951.357 9.633 1.004 22.728 0.2644 2.75 2.74 0.6238 79.342 3.303 2245.317 9.624 1.003 22.708 0.2638 2.75 2.74 0.6225 RUN NUMBER 1W00805 AXIAL POSITION = 1295.0 MM SPAN POSITION = 0.0 MM FREE-STREAM VELOCITY = 9.61 M/S FRICTION VELOCITY = 0.4161 M/S FREE-STREAM TURBULENCE = 2.548 % X-REYNOLDS NUMBER = 83.10 X10**4 FLUID DENSITY = 1.207 KG/M**3 KINEMATIC VISCOSITY = 1.498 X10(-5)MSQ/S BOUNDARY LAYER THICKNESS (99.0%) = 29.37 MM DISPLACEMENT THICKNESS = 4.116 MM MOMENTUM THICKNESS = 2.980 MM ENERGY THICKNESS = 5.308 MM FORM FACTOR H = 1.381 FORM FACTOR E = 1.781 RDELTASTAR = 2641.1 RTHETA = 1911.9 SKIN FRICTION COEFFICIENT = 0.003746 CALCULATED CF = 0.003758 LAW OF THE WALL OFFSET = 5.20 KARMAN CONSTANT = 0.410 FORM FACTOR G = 6.380 CLAUSER DELTA = 95.110 MM WAKE FACTOR PI = 0.283 1 Y Y/DEL YPLUS U U/UO UPLUS u u/UO u/U u/UTAU MM M/S M/S % % 0.129 0.004 3.582 1.384 0.144 3.326 0.4961 5.16 35.86 1.1925 0.154 0.005 4.276 1.606 0.167 3.860 0.5887 6.12 36.66 1.4150 0.179 0.006 4.971 1.821 0.189 4.376 0.6828 7.10 37.50 1.6411 0.210 0.007 5.838 2.091 0.218 5.026 0.7765 8.08 37.13 1.8663 0.242 0.008 6.706 2.339 0.243 5.622 0.8616 8.96 36.83 2.0708 0.285 0.010 7.921 2.727 0.284 6.554 0.9701 10.09 35.58 2.3316 0.335 0.011 9.310 3.103 0.323 7.459 1.0546 10.97 33.98 2.5347 0.385 0.013 10.698 3.454 0.359 8.302 1.1080 11.53 32.08 2.6632 0.454 0.015 12.607 3.878 0.403 9.320 1.1430 11.89 29.48 2.7472 0.529 0.018 14.690 4.256 0.443 10.228 1.1585 12.05 27.22 2.7845 0.617 0.021 17.120 4.581 0.476 11.010 1.1482 11.94 25.06 2.7596 0.717 0.024 19.897 4.870 0.507 11.706 1.1203 11.65 23.00 2.6928 0.835 0.028 23.194 5.133 0.534 12.338 1.0875 11.31 21.19 2.6139 0.979 0.033 27.186 5.397 0.561 12.973 1.0581 11.01 19.60 2.5430 1.142 0.039 31.699 5.647 0.587 13.572 1.0135 10.54 17.95 2.4359 1.329 0.045 36.905 5.786 0.602 13.907 0.9652 10.04 16.68 2.3198 1.548 0.053 42.980 5.964 0.620 14.333 0.9324 9.70 15.63 2.2409 1.804 0.061 50.096 6.155 0.640 14.794 0.8931 9.29 14.51 2.1466 2.104 0.072 58.426 6.310 0.656 15.167 0.8682 9.03 13.76 2.0868 2.454 0.084 68.146 6.444 0.670 15.488 0.8329 8.66 12.93 2.0019 2.854 0.097 79.253 6.614 0.688 15.896 0.8171 8.50 12.35 1.9638 3.329 0.113 92.444 6.783 0.706 16.303 0.8112 8.44 11.96 1.9497 3.879 0.132 107.717 6.902 0.718 16.590 0.7936 8.25 11.50 1.9074 4.523 0.154 125.593 7.101 0.739 17.068 0.7714 8.02 10.86 1.8540 5.273 0.180 146.420 7.263 0.756 17.458 0.7666 7.97 10.55 1.8426 6.142 0.209 170.544 7.468 0.777 17.948 0.7585 7.89 10.16 1.8231 7.160 0.244 198.834 7.669 0.798 18.433 0.7377 7.67 9.62 1.7730 8.348 0.284 231.810 7.853 0.817 18.875 0.7259 7.55 9.24 1.7447 9.723 0.331 269.993 8.084 0.841 19.431 0.6965 7.24 8.61 1.6739 11.335 0.386 314.771 8.287 0.862 19.918 0.6749 7.02 8.14 1.6221 13.210 0.450 366.838 8.524 0.887 20.488 0.6298 6.55 7.39 1.5138 15.398 0.524 427.583 8.764 0.912 21.065 0.5820 6.05 6.64 1.3987 17.942 0.611 498.221 8.999 0.936 21.629 0.5265 5.48 5.85 1.2654 20.910 0.712 580.660 9.208 0.958 22.131 0.4561 4.74 4.95 1.0964 24.367 0.830 676.638 9.387 0.976 22.563 0.3834 3.99 4.08 0.9215 28.398 0.967 788.582 9.505 0.989 22.847 0.3118 3.24 3.28 0.7494 32.429 1.104 900.527 9.550 0.993 22.954 0.2762 2.87 2.89 0.6639 36.454 1.241 1012.298 9.591 0.998 23.053 0.2582 2.69 2.69 0.6207 40.485 1.379 1124.242 9.603 0.999 23.081 0.2517 2.62 2.62 0.6049 44.517 1.516 1236.187 9.613 1.000 23.105 0.2475 2.57 2.57 0.5948 53.235 1.813 1478.299 9.627 1.001 23.139 0.2446 2.54 2.54 0.5878 61.954 2.110 1720.412 9.637 1.002 23.162 0.2447 2.55 2.54 0.5882 70.673 2.407 1962.524 9.642 1.003 23.174 0.2482 2.58 2.57 0.5964 79.398 2.704 2204.810 9.647 1.003 23.188 0.2450 2.55 2.54 0.5888 RUN NUMBER 1W00806 AXIAL POSITION = 1495.0 MM SPAN POSITION = 0.0 MM FREE-STREAM VELOCITY = 9.60 M/S FRICTION VELOCITY = 0.4093 M/S FREE-STREAM TURBULENCE = 2.400 % X-REYNOLDS NUMBER = 95.70 X10**4 FLUID DENSITY = 1.207 KG/M**3 KINEMATIC VISCOSITY = 1.499 X10(-5)MSQ/S BOUNDARY LAYER THICKNESS (99.0%) = 30.78 MM DISPLACEMENT THICKNESS = 4.467 MM MOMENTUM THICKNESS = 3.238 MM ENERGY THICKNESS = 5.756 MM FORM FACTOR H = 1.380 FORM FACTOR E = 1.778 RDELTASTAR = 2859.7 RTHETA = 2072.7 SKIN FRICTION COEFFICIENT = 0.003639 CALCULATED CF = 0.003687 LAW OF THE WALL OFFSET = 5.20 KARMAN CONSTANT = 0.410 FORM FACTOR G = 6.451 CLAUSER DELTA = 104.727 MM WAKE FACTOR PI = 0.303 1 Y Y/DEL YPLUS U U/UO UPLUS u u/UO u/U u/UTAU MM M/S M/S % % 0.117 0.004 3.181 1.371 0.143 3.349 0.4994 5.20 36.43 1.2201 0.135 0.004 3.693 1.547 0.161 3.780 0.5760 6.00 37.23 1.4073 0.154 0.005 4.205 1.729 0.180 4.225 0.6517 6.79 37.68 1.5921 0.185 0.006 5.059 1.996 0.208 4.876 0.7482 7.80 37.49 1.8279 0.217 0.007 5.912 2.262 0.236 5.527 0.8339 8.69 36.86 2.0372 0.254 0.008 6.936 2.568 0.268 6.274 0.9311 9.70 36.26 2.2748 0.292 0.009 7.960 2.893 0.302 7.068 1.0019 10.44 34.63 2.4477 0.342 0.011 9.325 3.249 0.339 7.938 1.0730 11.18 33.02 2.6215 0.404 0.013 11.032 3.616 0.377 8.835 1.1123 11.59 30.76 2.7175 0.473 0.015 12.909 4.006 0.418 9.787 1.1371 11.85 28.38 2.7780 0.548 0.018 14.957 4.297 0.448 10.497 1.1415 11.90 26.57 2.7888 0.642 0.021 17.517 4.605 0.480 11.251 1.1376 11.86 24.70 2.7793 0.748 0.024 20.419 4.864 0.507 11.884 1.1015 11.48 22.64 2.6910 0.879 0.029 24.002 5.142 0.536 12.563 1.0689 11.14 20.79 2.6113 1.023 0.033 27.928 5.358 0.558 13.090 1.0334 10.77 19.29 2.5247 1.198 0.039 32.706 5.587 0.582 13.651 0.9926 10.34 17.76 2.4249 1.398 0.045 38.168 5.741 0.598 14.027 0.9454 9.85 16.47 2.3096 1.635 0.053 44.653 5.914 0.616 14.449 0.9256 9.65 15.65 2.2613 1.910 0.062 52.162 6.102 0.636 14.907 0.8851 9.22 14.51 2.1623 2.229 0.072 60.866 6.234 0.650 15.231 0.8626 8.99 13.84 2.1074 2.604 0.085 71.106 6.393 0.666 15.620 0.8430 8.79 13.19 2.0596 3.042 0.099 83.053 6.519 0.679 15.925 0.8108 8.45 12.44 1.9808 3.554 0.115 97.048 6.714 0.700 16.403 0.8089 8.43 12.05 1.9762 4.148 0.135 113.261 6.883 0.717 16.816 0.7902 8.24 11.48 1.9305 4.848 0.158 132.376 7.033 0.733 17.183 0.7903 8.24 11.24 1.9308 5.660 0.184 154.562 7.221 0.753 17.641 0.7686 8.01 10.64 1.8777 6.610 0.215 180.503 7.400 0.771 18.080 0.7593 7.91 10.26 1.8550 7.723 0.251 210.882 7.615 0.794 18.604 0.7465 7.78 9.80 1.8237 9.017 0.293 246.210 7.805 0.813 19.069 0.7263 7.57 9.31 1.7744 10.529 0.342 287.511 8.031 0.837 19.621 0.6937 7.23 8.64 1.6948 12.298 0.400 335.810 8.244 0.859 20.140 0.6737 7.02 8.17 1.6459 14.360 0.467 392.129 8.469 0.883 20.690 0.6351 6.62 7.50 1.5517 16.773 0.545 458.007 8.744 0.911 21.363 0.5977 6.23 6.83 1.4601 19.585 0.636 534.806 8.955 0.933 21.879 0.5393 5.62 6.02 1.3176 22.873 0.743 624.577 9.204 0.959 22.487 0.4649 4.85 5.05 1.1358 26.717 0.868 729.537 9.378 0.977 22.910 0.3788 3.95 4.04 0.9255 31.198 1.014 851.904 9.510 0.991 23.235 0.3112 3.24 3.27 0.7603 35.679 1.159 974.272 9.586 0.999 23.419 0.2641 2.75 2.76 0.6452 40.167 1.305 1096.810 9.607 1.001 23.471 0.2466 2.57 2.57 0.6025 44.648 1.451 1219.178 9.618 1.002 23.498 0.2338 2.44 2.43 0.5713 49.129 1.596 1341.545 9.618 1.002 23.498 0.2323 2.42 2.41 0.5674 56.667 1.841 1547.369 9.614 1.002 23.489 0.2305 2.40 2.40 0.5632 64.198 2.086 1753.022 9.594 1.000 23.439 0.2294 2.39 2.39 0.5604 71.735 2.331 1958.845 9.618 1.002 23.498 0.2287 2.38 2.38 0.5587 79.273 2.576 2164.669 9.591 1.000 23.432 0.2303 2.40 2.40 0.5627