24x12E (24x12E.dat) v2022-0915 Simulation Date: 09/22/2022 AIRFOIL AERO DATA GENERATED USING: POLAR DIAGRAMS ====== PERFORMANCE DATA (versus advance ratio and MPH) ====== DEFINITIONS: J=V/nD (advance ratio) Ct=T/(rho * n**2 * D**4) (thrust coef.) Cp=P/(rho * n**3 * D**5) (power coef.) Pe=Ct*J/Cp (efficiency) V (model speed in MPH) Mach (at prop tip) Reyn (at 75% of span) FOM (Figure of Merit) PROP RPM = 1000 V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM (mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - - 0.00 0.0000 0.0000 0.0825 0.0289 0.019 1.169 0.873 13.829 0.132 3.882 28.624 0.10 52921. 0.6538 0.51 0.0223 0.0618 0.0811 0.0292 0.019 1.181 0.858 13.973 0.133 3.816 27.850 0.10 52952. 0.6307 1.01 0.0446 0.1202 0.0797 0.0295 0.019 1.192 0.842 14.106 0.135 3.746 27.082 0.10 52986. 0.6076 1.52 0.0668 0.1753 0.0781 0.0298 0.019 1.202 0.825 14.222 0.136 3.671 26.321 0.10 53022. 0.5846 2.03 0.0891 0.2270 0.0763 0.0300 0.019 1.210 0.807 14.320 0.137 3.591 25.568 0.10 53060. 0.5616 2.53 0.1114 0.2755 0.0745 0.0301 0.019 1.217 0.788 14.396 0.137 3.505 24.826 0.10 53102. 0.5388 3.04 0.1337 0.3208 0.0726 0.0302 0.019 1.221 0.767 14.447 0.138 3.413 24.093 0.10 53146. 0.5160 3.54 0.1559 0.3631 0.0705 0.0303 0.019 1.223 0.746 14.469 0.138 3.316 23.370 0.10 53194. 0.4933 4.05 0.1782 0.4023 0.0683 0.0303 0.019 1.222 0.722 14.459 0.138 3.213 22.658 0.10 53244. 0.4708 4.56 0.2005 0.4386 0.0660 0.0302 0.019 1.218 0.698 14.414 0.138 3.104 21.956 0.10 53298. 0.4484 5.06 0.2228 0.4719 0.0635 0.0300 0.019 1.211 0.672 14.331 0.137 2.988 21.262 0.10 53355. 0.4261 5.57 0.2450 0.5023 0.0609 0.0297 0.019 1.201 0.644 14.205 0.136 2.866 20.575 0.10 53415. 0.4038 6.08 0.2673 0.5298 0.0582 0.0294 0.019 1.186 0.616 14.033 0.134 2.738 19.894 0.10 53478. 0.3816 6.58 0.2896 0.5544 0.0554 0.0289 0.019 1.168 0.585 13.814 0.132 2.603 19.216 0.10 53545. 0.3594 7.09 0.3119 0.5760 0.0524 0.0283 0.018 1.145 0.554 13.546 0.129 2.463 18.538 0.10 53616. 0.3372 7.59 0.3341 0.5944 0.0493 0.0277 0.018 1.118 0.521 13.230 0.126 2.317 17.856 0.10 53690. 0.3150 8.10 0.3564 0.6096 0.0461 0.0269 0.017 1.087 0.487 12.866 0.123 2.166 17.166 0.10 53767. 0.2928 8.61 0.3787 0.6211 0.0428 0.0261 0.017 1.053 0.452 12.454 0.119 2.011 16.462 0.10 53848. 0.2706 9.11 0.4010 0.6288 0.0394 0.0251 0.016 1.014 0.416 11.995 0.115 1.851 15.738 0.10 53933. 0.2482 9.62 0.4232 0.6320 0.0359 0.0240 0.015 0.971 0.380 11.490 0.110 1.689 14.987 0.10 54021. 0.2258 10.13 0.4455 0.6302 0.0324 0.0229 0.015 0.925 0.342 10.938 0.104 1.523 14.197 0.10 54113. 0.2031 10.63 0.4678 0.6226 0.0288 0.0216 0.014 0.874 0.305 10.341 0.099 1.355 13.357 0.10 54208. 0.1802 11.14 0.4901 0.6079 0.0252 0.0203 0.013 0.820 0.266 9.701 0.093 1.184 12.449 0.10 54307. 0.1571 11.64 0.5123 0.5845 0.0215 0.0189 0.012 0.762 0.228 9.018 0.086 1.013 11.451 0.10 54410. 0.1336 12.15 0.5346 0.5502 0.0179 0.0174 0.011 0.701 0.189 8.296 0.079 0.840 10.329 0.10 54517. 0.1098 12.66 0.5569 0.5014 0.0142 0.0158 0.010 0.637 0.150 7.535 0.072 0.668 9.037 0.10 54627. 0.0856 13.16 0.5792 0.4331 0.0105 0.0141 0.009 0.570 0.112 6.741 0.064 0.496 7.505 0.10 54741. 0.0613 13.67 0.6014 0.3368 0.0069 0.0124 0.008 0.500 0.073 5.917 0.057 0.326 5.620 0.10 54859. 0.0372 14.18 0.6237 0.1983 0.0034 0.0106 0.007 0.428 0.036 5.067 0.048 0.159 3.191 0.10 54980. 0.0147 14.68 0.6460 -0.0092 -0.0001 0.0088 0.006 0.355 -0.001 4.194 0.040 -0.006 -0.144 0.10 55103. 0.0000 PROP RPM = 2000 V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM (mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - - 0.00 0.0000 0.0000 0.0829 0.0271 0.139 4.375 3.508 103.522 0.494 15.603 15.369 0.19 105840. 0.7037 1.01 0.0223 0.0664 0.0816 0.0274 0.141 4.428 3.449 104.777 0.500 15.341 14.930 0.19 105902. 0.6779 2.03 0.0446 0.1290 0.0801 0.0277 0.142 4.477 3.386 105.932 0.506 15.060 14.497 0.19 105969. 0.6522 3.04 0.0670 0.1878 0.0785 0.0280 0.143 4.520 3.318 106.961 0.511 14.758 14.070 0.19 106042. 0.6266 4.06 0.0893 0.2429 0.0767 0.0282 0.145 4.557 3.246 107.839 0.515 14.436 13.651 0.19 106119. 0.6012 5.07 0.1116 0.2944 0.0749 0.0284 0.146 4.587 3.168 108.540 0.518 14.092 13.239 0.19 106203. 0.5761 6.09 0.1339 0.3426 0.0730 0.0285 0.146 4.608 3.086 109.035 0.521 13.725 12.836 0.19 106292. 0.5512 7.10 0.1562 0.3874 0.0709 0.0286 0.147 4.619 2.998 109.296 0.522 13.334 12.441 0.19 106387. 0.5266 8.12 0.1786 0.4289 0.0687 0.0286 0.147 4.619 2.905 109.295 0.522 12.920 12.054 0.19 106488. 0.5023 9.13 0.2009 0.4674 0.0663 0.0285 0.146 4.607 2.806 109.004 0.520 12.480 11.675 0.19 106596. 0.4781 10.15 0.2232 0.5028 0.0639 0.0284 0.145 4.581 2.701 108.394 0.518 12.016 11.304 0.19 106710. 0.4542 11.16 0.2455 0.5353 0.0613 0.0281 0.144 4.540 2.591 107.434 0.513 11.526 10.940 0.19 106831. 0.4306 12.18 0.2679 0.5648 0.0585 0.0278 0.142 4.484 2.475 106.092 0.507 11.010 10.582 0.19 106959. 0.4070 13.19 0.2902 0.5915 0.0556 0.0273 0.140 4.410 2.353 104.351 0.498 10.468 10.229 0.19 107094. 0.3836 14.20 0.3125 0.6152 0.0526 0.0267 0.137 4.319 2.226 102.205 0.488 9.902 9.880 0.19 107235. 0.3604 15.22 0.3348 0.6360 0.0495 0.0261 0.134 4.211 2.094 99.652 0.476 9.315 9.532 0.19 107384. 0.3373 16.23 0.3571 0.6536 0.0463 0.0253 0.130 4.086 1.958 96.694 0.462 8.709 9.184 0.19 107539. 0.3142 17.25 0.3795 0.6679 0.0430 0.0244 0.125 3.944 1.818 93.331 0.446 8.085 8.833 0.19 107702. 0.2911 18.26 0.4018 0.6786 0.0396 0.0234 0.120 3.785 1.674 89.565 0.428 7.444 8.476 0.19 107872. 0.2681 19.28 0.4241 0.6852 0.0361 0.0223 0.115 3.609 1.527 85.399 0.408 6.790 8.108 0.19 108049. 0.2449 20.29 0.4464 0.6873 0.0326 0.0211 0.108 3.416 1.377 80.839 0.386 6.124 7.726 0.19 108233. 0.2216 21.31 0.4687 0.6839 0.0290 0.0199 0.102 3.207 1.225 75.891 0.362 5.449 7.321 0.19 108425. 0.1981 22.32 0.4911 0.6738 0.0253 0.0185 0.095 2.982 1.071 70.565 0.337 4.765 6.886 0.19 108624. 0.1743 23.34 0.5134 0.6555 0.0217 0.0170 0.087 2.742 0.916 64.876 0.310 4.077 6.407 0.19 108830. 0.1500 24.35 0.5357 0.6263 0.0180 0.0154 0.079 2.487 0.761 58.842 0.281 3.385 5.866 0.19 109044. 0.1251 25.37 0.5580 0.5821 0.0143 0.0137 0.070 2.218 0.606 52.485 0.251 2.694 5.235 0.19 109266. 0.0996 26.38 0.5804 0.5163 0.0107 0.0120 0.061 1.937 0.451 45.834 0.219 2.007 4.465 0.19 109495. 0.0733 27.39 0.6027 0.4173 0.0071 0.0102 0.052 1.645 0.298 38.925 0.186 1.326 3.475 0.19 109731. 0.0464 28.41 0.6250 0.2624 0.0035 0.0083 0.043 1.344 0.148 31.798 0.152 0.657 2.107 0.19 109974. 0.0198 29.42 0.6473 -0.0003 0.0000 0.0064 0.033 1.034 0.000 24.467 0.117 0.000 -0.002 0.19 110220. 0.0000 PROP RPM = 3000 V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM (mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - - 0.00 0.0000 0.0000 0.0835 0.0264 0.457 9.601 7.943 340.777 1.085 35.332 10.573 0.29 158754. 0.7285 1.54 0.0226 0.0693 0.0821 0.0268 0.463 9.726 7.809 345.222 1.099 34.736 10.260 0.29 158849. 0.7010 3.08 0.0452 0.1344 0.0806 0.0271 0.468 9.842 7.665 349.318 1.112 34.095 9.953 0.29 158951. 0.6737 4.62 0.0677 0.1954 0.0789 0.0274 0.473 9.945 7.511 352.974 1.124 33.407 9.651 0.29 159061. 0.6466 6.16 0.0903 0.2526 0.0772 0.0276 0.478 10.033 7.345 356.098 1.133 32.670 9.355 0.29 159180. 0.6199 7.70 0.1129 0.3060 0.0753 0.0278 0.481 10.103 7.168 358.596 1.141 31.881 9.066 0.29 159307. 0.5934 9.24 0.1355 0.3557 0.0733 0.0279 0.483 10.153 6.978 360.367 1.147 31.040 8.783 0.29 159443. 0.5673 10.78 0.1581 0.4020 0.0712 0.0280 0.485 10.180 6.777 361.312 1.150 30.144 8.507 0.29 159589. 0.5415 12.32 0.1806 0.4448 0.0690 0.0280 0.485 10.180 6.563 361.328 1.150 29.192 8.238 0.29 159744. 0.5160 13.86 0.2032 0.4845 0.0666 0.0279 0.483 10.152 6.336 360.314 1.147 28.182 7.976 0.29 159908. 0.4908 15.40 0.2258 0.5210 0.0641 0.0278 0.480 10.091 6.096 358.164 1.140 27.114 7.720 0.29 160083. 0.4660 16.94 0.2484 0.5546 0.0614 0.0275 0.476 9.995 5.842 354.768 1.129 25.986 7.469 0.29 160268. 0.4414 18.48 0.2710 0.5851 0.0586 0.0271 0.469 9.861 5.575 350.014 1.114 24.796 7.224 0.29 160464. 0.4170 20.02 0.2936 0.6128 0.0556 0.0267 0.461 9.687 5.294 343.843 1.094 23.548 6.983 0.29 160670. 0.3928 21.55 0.3161 0.6375 0.0526 0.0261 0.451 9.473 5.001 336.235 1.070 22.245 6.746 0.29 160886. 0.3689 23.09 0.3387 0.6593 0.0494 0.0254 0.439 9.218 4.697 327.185 1.041 20.893 6.512 0.29 161114. 0.3450 24.63 0.3613 0.6780 0.0461 0.0245 0.425 8.922 4.383 316.690 1.008 19.497 6.278 0.29 161352. 0.3213 26.17 0.3839 0.6934 0.0427 0.0236 0.409 8.586 4.060 304.753 0.970 18.060 6.043 0.29 161601. 0.2977 27.71 0.4065 0.7052 0.0392 0.0226 0.391 8.209 3.729 291.379 0.927 16.587 5.805 0.29 161861. 0.2741 29.25 0.4290 0.7131 0.0356 0.0214 0.371 7.792 3.391 276.580 0.880 15.082 5.561 0.29 162133. 0.2503 30.79 0.4516 0.7164 0.0320 0.0202 0.349 7.336 3.047 260.375 0.829 13.552 5.307 0.29 162415. 0.2265 32.33 0.4742 0.7143 0.0283 0.0188 0.326 6.840 2.698 242.790 0.773 11.999 5.040 0.29 162709. 0.2024 33.87 0.4968 0.7055 0.0246 0.0174 0.300 6.307 2.345 223.865 0.713 10.430 4.751 0.29 163014. 0.1779 35.41 0.5194 0.6880 0.0209 0.0158 0.273 5.738 1.990 203.652 0.648 8.851 4.432 0.29 163330. 0.1528 36.95 0.5419 0.6588 0.0172 0.0141 0.244 5.134 1.634 182.220 0.580 7.267 4.067 0.29 163658. 0.1271 38.49 0.5645 0.6129 0.0134 0.0124 0.214 4.498 1.279 159.659 0.508 5.687 3.632 0.29 163997. 0.1004 40.03 0.5871 0.5414 0.0097 0.0105 0.182 3.834 0.926 136.079 0.433 4.117 3.085 0.29 164348. 0.0726 41.57 0.6097 0.4274 0.0061 0.0087 0.150 3.145 0.577 111.615 0.355 2.567 2.345 0.29 164710. 0.0436 43.11 0.6323 0.2331 0.0025 0.0067 0.116 2.435 0.235 86.420 0.275 1.045 1.233 0.29 165083. 0.0146 44.65 0.6549 PROP RPM = 4000 V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM (mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - - 0.00 0.0000 0.0000 0.0842 0.0262 1.074 16.930 14.245 801.198 1.913 63.362 8.064 0.38 211661. 0.7441 2.03 0.0224 0.0697 0.0828 0.0266 1.089 17.156 14.009 811.916 1.938 62.313 7.826 0.38 211787. 0.7162 4.07 0.0447 0.1353 0.0813 0.0269 1.102 17.365 13.755 821.814 1.962 61.183 7.592 0.38 211922. 0.6884 6.10 0.0671 0.1968 0.0797 0.0272 1.114 17.553 13.483 830.676 1.983 59.971 7.362 0.38 212068. 0.6609 8.13 0.0894 0.2544 0.0780 0.0274 1.124 17.714 13.191 838.287 2.001 58.672 7.137 0.38 212224. 0.6337 10.16 0.1118 0.3082 0.0761 0.0276 1.132 17.843 12.878 844.421 2.016 57.283 6.917 0.38 212392. 0.6069 12.20 0.1342 0.3584 0.0742 0.0278 1.138 17.937 12.545 848.848 2.026 55.800 6.703 0.38 212572. 0.5805 14.23 0.1565 0.4051 0.0721 0.0278 1.142 17.989 12.190 851.329 2.032 54.220 6.494 0.38 212764. 0.5544 16.26 0.1789 0.4485 0.0698 0.0278 1.142 17.995 11.812 851.626 2.033 52.541 6.291 0.38 212968. 0.5286 18.30 0.2013 0.4887 0.0675 0.0278 1.139 17.950 11.412 849.497 2.028 50.761 6.093 0.38 213185. 0.5033 20.33 0.2236 0.5258 0.0650 0.0276 1.133 17.849 10.989 844.700 2.017 48.877 5.900 0.38 213415. 0.4782 22.36 0.2460 0.5600 0.0623 0.0274 1.122 17.686 10.541 836.975 1.998 46.887 5.712 0.38 213659. 0.4534 24.39 0.2683 0.5913 0.0595 0.0270 1.108 17.455 10.069 826.055 1.972 44.788 5.529 0.38 213916. 0.4289 26.43 0.2907 0.6197 0.0566 0.0265 1.089 17.153 9.574 811.775 1.938 42.585 5.349 0.38 214187. 0.4047 28.46 0.3131 0.6454 0.0535 0.0260 1.065 16.779 9.057 794.078 1.896 40.284 5.173 0.38 214471. 0.3806 30.49 0.3354 0.6683 0.0504 0.0253 1.037 16.333 8.519 772.944 1.845 37.894 4.999 0.38 214770. 0.3567 32.53 0.3578 0.6883 0.0471 0.0245 1.004 15.813 7.964 748.367 1.787 35.424 4.827 0.38 215083. 0.3330 34.56 0.3801 0.7052 0.0437 0.0236 0.966 15.221 7.392 720.347 1.720 32.881 4.655 0.38 215410. 0.3094 36.59 0.4025 0.7188 0.0402 0.0225 0.924 14.557 6.806 688.895 1.645 30.272 4.481 0.38 215751. 0.2858 38.62 0.4249 0.7288 0.0367 0.0214 0.877 13.820 6.207 654.034 1.561 27.607 4.304 0.38 216107. 0.2622 40.66 0.4472 0.7347 0.0331 0.0201 0.826 13.012 5.596 615.802 1.470 24.893 4.122 0.38 216478. 0.2384 42.69 0.4696 0.7357 0.0294 0.0188 0.770 12.134 4.977 574.260 1.371 22.138 3.931 0.39 216863. 0.2144 44.72 0.4919 0.7307 0.0257 0.0173 0.710 11.188 4.351 529.492 1.264 19.353 3.727 0.39 217262. 0.1901 46.76 0.5143 0.7181 0.0220 0.0157 0.646 10.177 3.720 481.616 1.150 16.547 3.503 0.39 217677. 0.1652 48.79 0.5367 0.6952 0.0182 0.0141 0.578 9.103 3.087 430.785 1.028 13.730 3.250 0.39 218107. 0.1396 50.82 0.5590 0.6575 0.0145 0.0123 0.506 7.970 2.454 377.199 0.900 10.916 2.951 0.39 218551. 0.1130 52.85 0.5814 0.5973 0.0108 0.0105 0.431 6.785 1.825 321.109 0.767 8.118 2.578 0.39 219010. 0.0851 54.89 0.6038 0.4995 0.0071 0.0086 0.352 5.554 1.203 262.825 0.627 5.350 2.076 0.39 219485. 0.0557 56.92 0.6261 0.3300 0.0035 0.0066 0.272 4.283 0.591 202.704 0.484 2.629 1.322 0.39 219973. 0.0249 58.95 0.6485 -0.0094 -0.0001 0.0046 0.189 2.973 -0.011 140.684 0.336 -0.050 -0.036 0.39 220459. 0.0000 PROP RPM = 5000 V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM (mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - - 0.00 0.0000 0.0000 0.0852 0.0263 2.104 26.517 22.513 1568.630 2.996 100.138 6.510 0.48 264558. 0.7551 2.54 0.0223 0.0703 0.0838 0.0266 2.132 26.879 22.144 1590.073 3.037 98.498 6.317 0.48 264715. 0.7267 5.08 0.0447 0.1364 0.0823 0.0270 2.159 27.214 21.747 1609.875 3.075 96.731 6.127 0.48 264885. 0.6986 7.62 0.0670 0.1984 0.0807 0.0273 2.183 27.514 21.320 1627.605 3.108 94.833 5.941 0.48 265068. 0.6707 10.16 0.0894 0.2565 0.0789 0.0275 2.203 27.771 20.862 1642.838 3.138 92.796 5.760 0.48 265264. 0.6432 12.70 0.1117 0.3108 0.0771 0.0277 2.220 27.979 20.372 1655.119 3.161 90.616 5.583 0.48 265475. 0.6161 15.24 0.1341 0.3614 0.0751 0.0279 2.231 28.129 19.849 1663.988 3.178 88.286 5.410 0.48 265700. 0.5893 17.78 0.1564 0.4085 0.0730 0.0279 2.238 28.213 19.290 1668.969 3.187 85.803 5.242 0.48 265941. 0.5629 20.32 0.1788 0.4524 0.0707 0.0280 2.239 28.223 18.696 1669.585 3.189 83.161 5.079 0.48 266197. 0.5369 22.85 0.2011 0.4930 0.0683 0.0279 2.233 28.152 18.066 1665.361 3.181 80.358 4.920 0.48 266469. 0.5113 25.39 0.2235 0.5306 0.0658 0.0277 2.220 27.991 17.399 1655.812 3.162 77.390 4.766 0.48 266757. 0.4860 27.93 0.2458 0.5652 0.0632 0.0275 2.200 27.731 16.693 1640.425 3.133 74.252 4.616 0.48 267062. 0.4611 30.47 0.2682 0.5970 0.0603 0.0271 2.171 27.363 15.949 1618.664 3.091 70.941 4.469 0.48 267384. 0.4364 33.01 0.2905 0.6261 0.0574 0.0266 2.132 26.881 15.167 1590.188 3.037 67.463 4.326 0.48 267723. 0.4119 35.55 0.3129 0.6524 0.0543 0.0260 2.085 26.284 14.350 1554.871 2.970 63.828 4.186 0.48 268079. 0.3877 38.09 0.3352 0.6760 0.0511 0.0253 2.029 25.571 13.501 1512.673 2.889 60.052 4.048 0.48 268453. 0.3637 40.63 0.3576 0.6968 0.0478 0.0245 1.963 24.741 12.623 1463.577 2.795 56.146 3.912 0.48 268845. 0.3398 43.17 0.3799 0.7146 0.0443 0.0236 1.888 23.795 11.718 1407.588 2.688 52.123 3.776 0.48 269254. 0.3160 45.71 0.4022 0.7293 0.0408 0.0225 1.803 22.732 10.790 1344.726 2.568 47.995 3.640 0.48 269681. 0.2923 48.25 0.4246 0.7406 0.0372 0.0213 1.710 21.554 9.842 1275.033 2.435 43.777 3.501 0.48 270126. 0.2685 50.79 0.4469 0.7478 0.0336 0.0201 1.607 20.262 8.876 1198.590 2.289 39.479 3.359 0.48 270589. 0.2446 53.33 0.4693 0.7505 0.0299 0.0187 1.496 18.857 7.895 1115.513 2.130 35.117 3.210 0.48 271070. 0.2205 55.87 0.4916 0.7474 0.0261 0.0172 1.376 17.344 6.903 1025.973 1.959 30.704 3.052 0.48 271570. 0.1960 58.41 0.5140 0.7370 0.0223 0.0156 1.247 15.725 5.903 930.200 1.777 26.257 2.878 0.48 272088. 0.1710 60.95 0.5363 0.7167 0.0185 0.0139 1.111 14.005 4.900 828.507 1.582 21.794 2.682 0.48 272624. 0.1452 63.49 0.5587 0.6820 0.0147 0.0121 0.967 12.193 3.897 721.292 1.378 17.333 2.450 0.48 273179. 0.1183 66.03 0.5810 0.6250 0.0110 0.0102 0.817 10.296 2.900 609.062 1.163 12.897 2.159 0.48 273753. 0.0899 68.56 0.6034 0.5296 0.0072 0.0082 0.660 8.324 1.913 492.438 0.940 8.509 1.762 0.48 274346. 0.0596 71.10 0.6257 0.3582 0.0036 0.0062 0.499 6.291 0.943 372.148 0.711 4.194 1.149 0.49 274956. 0.0273 73.64 0.6481 -0.0075 0.0000 0.0042 0.333 4.192 -0.013 247.995 0.474 -0.056 -0.023 0.49 275560. 0.0000 PROP RPM = 6000 V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM (mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - - 0.00 0.0000 0.0000 0.0864 0.0266 3.675 38.608 32.893 2740.686 4.362 146.307 5.444 0.57 317439. 0.7633 3.05 0.0223 0.0705 0.0850 0.0269 3.726 39.144 32.362 2778.722 4.422 143.948 5.282 0.57 317629. 0.7347 6.09 0.0447 0.1368 0.0835 0.0273 3.773 39.639 31.790 2813.838 4.478 141.401 5.124 0.57 317834. 0.7064 9.14 0.0670 0.1991 0.0819 0.0276 3.816 40.081 31.173 2845.257 4.528 138.659 4.969 0.57 318054. 0.6783 12.18 0.0893 0.2573 0.0802 0.0278 3.852 40.461 30.511 2872.215 4.571 135.715 4.818 0.57 318291. 0.6507 15.23 0.1117 0.3118 0.0783 0.0280 3.881 40.767 29.802 2893.918 4.606 132.558 4.671 0.57 318545. 0.6234 18.27 0.1340 0.3627 0.0763 0.0282 3.902 40.987 29.042 2909.542 4.631 129.180 4.527 0.57 318817. 0.5965 21.32 0.1563 0.4101 0.0742 0.0283 3.913 41.110 28.232 2918.244 4.645 125.575 4.388 0.57 319107. 0.5700 24.37 0.1787 0.4542 0.0719 0.0283 3.915 41.123 27.369 2919.183 4.646 121.736 4.252 0.57 319416. 0.5439 27.41 0.2010 0.4952 0.0695 0.0282 3.904 41.015 26.452 2911.510 4.634 117.658 4.121 0.57 319743. 0.5182 30.46 0.2234 0.5332 0.0669 0.0280 3.881 40.773 25.480 2894.380 4.607 113.335 3.993 0.57 320090. 0.4928 33.50 0.2457 0.5682 0.0642 0.0278 3.845 40.386 24.452 2866.897 4.563 108.763 3.869 0.57 320458. 0.4677 36.55 0.2680 0.6005 0.0614 0.0274 3.793 39.840 23.367 2828.117 4.501 103.934 3.747 0.57 320845. 0.4429 39.59 0.2904 0.6300 0.0584 0.0269 3.725 39.125 22.225 2777.403 4.420 98.856 3.629 0.57 321253. 0.4183 42.64 0.3127 0.6569 0.0553 0.0263 3.640 38.240 21.031 2714.515 4.320 93.546 3.514 0.57 321682. 0.3940 45.69 0.3350 0.6811 0.0520 0.0256 3.539 37.181 19.789 2639.384 4.201 88.024 3.401 0.57 322131. 0.3699 48.73 0.3574 0.7026 0.0486 0.0247 3.422 35.950 18.505 2551.987 4.062 82.308 3.289 0.57 322602. 0.3459 51.78 0.3797 0.7213 0.0451 0.0238 3.289 34.546 17.181 2452.337 3.903 76.419 3.178 0.58 323094. 0.3220 54.82 0.4020 0.7369 0.0416 0.0227 3.139 32.970 15.821 2340.470 3.725 70.374 3.066 0.58 323607. 0.2982 57.87 0.4244 0.7492 0.0379 0.0215 2.972 31.224 14.432 2216.470 3.528 64.192 2.953 0.58 324141. 0.2743 60.92 0.4467 0.7578 0.0342 0.0202 2.790 29.308 13.015 2080.477 3.311 57.892 2.837 0.58 324697. 0.2503 63.96 0.4690 0.7618 0.0304 0.0187 2.592 27.226 11.577 1932.699 3.076 51.494 2.717 0.58 325275. 0.2260 67.01 0.4914 0.7604 0.0266 0.0172 2.378 24.983 10.122 1773.442 2.823 45.021 2.589 0.58 325875. 0.2013 70.05 0.5137 0.7520 0.0227 0.0155 2.150 22.583 8.654 1603.117 2.551 38.495 2.449 0.58 326496. 0.1761 73.10 0.5361 0.7339 0.0189 0.0138 1.907 20.036 7.181 1422.277 2.264 31.942 2.290 0.58 327140. 0.1500 76.14 0.5584 0.7018 0.0150 0.0119 1.652 17.350 5.709 1231.638 1.960 25.392 2.102 0.58 327806. 0.1228 79.19 0.5807 0.6475 0.0111 0.0100 1.384 14.539 4.244 1032.100 1.643 18.876 1.865 0.58 328494. 0.0939 82.24 0.6031 0.5540 0.0073 0.0080 1.106 11.619 2.795 824.785 1.313 12.430 1.537 0.58 329205. 0.0628 85.28 0.6254 0.3801 0.0036 0.0059 0.819 8.607 1.369 610.997 0.972 6.091 1.017 0.58 329936. 0.0291 88.33 0.6477 -0.0164 -0.0001 0.0038 0.523 5.494 -0.037 390.028 0.621 -0.162 -0.042 0.58 330654. 0.0000 PROP RPM = 7000 V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM (mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - - 0.00 0.0000 0.0000 0.0880 0.0271 5.951 53.583 45.595 4437.671 6.054 202.806 4.660 0.67 370300. 0.7693 3.54 0.0223 0.0703 0.0866 0.0275 6.034 54.335 44.877 4499.923 6.139 199.612 4.523 0.67 370522. 0.7408 7.09 0.0446 0.1364 0.0851 0.0278 6.112 55.028 44.100 4557.347 6.217 196.155 4.389 0.67 370762. 0.7126 10.63 0.0668 0.1985 0.0835 0.0281 6.180 55.648 43.261 4608.676 6.287 192.427 4.258 0.67 371021. 0.6847 14.18 0.0891 0.2567 0.0818 0.0284 6.239 56.179 42.359 4652.667 6.347 188.413 4.129 0.67 371298. 0.6571 17.72 0.1114 0.3111 0.0799 0.0286 6.287 56.606 41.390 4688.018 6.395 184.102 4.005 0.67 371596. 0.6299 21.27 0.1337 0.3620 0.0779 0.0288 6.321 56.912 40.351 4713.361 6.430 179.482 3.883 0.67 371914. 0.6030 24.81 0.1560 0.4095 0.0757 0.0288 6.339 57.081 39.240 4727.352 6.449 174.542 3.765 0.67 372253. 0.5766 28.36 0.1782 0.4538 0.0735 0.0289 6.341 57.096 38.056 4728.604 6.451 169.273 3.650 0.67 372614. 0.5505 31.90 0.2005 0.4949 0.0710 0.0288 6.324 56.941 36.796 4715.755 6.433 163.667 3.539 0.67 372997. 0.5249 35.44 0.2228 0.5331 0.0684 0.0286 6.286 56.599 35.458 4687.436 6.395 157.719 3.431 0.67 373403. 0.4995 38.99 0.2451 0.5685 0.0657 0.0283 6.225 56.053 34.042 4642.217 6.333 151.421 3.326 0.67 373832. 0.4745 42.53 0.2674 0.6012 0.0628 0.0279 6.140 55.285 32.546 4578.589 6.246 144.763 3.224 0.67 374285. 0.4497 46.08 0.2896 0.6312 0.0598 0.0274 6.028 54.281 30.969 4495.428 6.133 137.751 3.125 0.67 374761. 0.4251 49.62 0.3119 0.6586 0.0566 0.0268 5.890 53.036 29.319 4392.315 5.992 130.411 3.028 0.67 375261. 0.4008 53.17 0.3342 0.6835 0.0533 0.0260 5.725 51.548 27.601 4269.142 5.824 122.769 2.932 0.67 375786. 0.3767 56.71 0.3565 0.7057 0.0498 0.0252 5.533 49.819 25.821 4125.893 5.628 114.853 2.839 0.67 376334. 0.3526 60.26 0.3787 0.7252 0.0463 0.0242 5.314 47.847 23.986 3962.597 5.406 106.688 2.745 0.67 376907. 0.3287 63.80 0.4010 0.7418 0.0427 0.0231 5.068 45.634 22.100 3779.328 5.156 98.301 2.652 0.67 377505. 0.3048 67.34 0.4233 0.7553 0.0389 0.0218 4.796 43.182 20.170 3576.232 4.879 89.718 2.558 0.67 378127. 0.2809 70.89 0.4456 0.7651 0.0351 0.0205 4.497 40.493 18.203 3353.535 4.575 80.965 2.462 0.67 378774. 0.2568 74.43 0.4679 0.7707 0.0313 0.0190 4.173 37.571 16.203 3111.584 4.245 72.071 2.362 0.67 379447. 0.2324 77.98 0.4901 0.7711 0.0274 0.0174 3.823 34.423 14.178 2850.873 3.889 63.065 2.256 0.67 380144. 0.2077 81.52 0.5124 0.7649 0.0234 0.0157 3.449 31.057 12.136 2572.073 3.509 53.981 2.140 0.68 380867. 0.1823 85.07 0.5347 0.7494 0.0195 0.0139 3.052 27.483 10.084 2276.076 3.105 44.855 2.010 0.68 381616. 0.1560 88.61 0.5570 0.7205 0.0155 0.0120 2.634 23.715 8.032 1964.044 2.679 35.725 1.855 0.68 382390. 0.1285 92.16 0.5793 0.6702 0.0116 0.0100 2.196 19.772 5.989 1637.474 2.234 26.639 1.659 0.68 383190. 0.0993 95.70 0.6015 0.5814 0.0077 0.0079 1.741 15.676 3.967 1298.244 1.771 17.644 1.386 0.68 384015. 0.0675 99.24 0.6238 0.4113 0.0038 0.0058 1.272 11.454 1.977 948.583 1.294 8.794 0.945 0.68 384865. 0.0325 102.79 0.6461 0.0061 0.0000 0.0036 0.789 7.103 0.018 588.241 0.802 0.078 0.014 0.68 385707. 0.0000 PROP RPM = 8000 V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM (mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - - 0.00 0.0000 0.0000 0.0900 0.0282 9.244 72.833 60.923 6893.605 8.229 270.984 4.008 0.76 423132. 0.7649 4.04 0.0222 0.0691 0.0887 0.0285 9.357 73.722 59.995 6977.744 8.329 266.858 3.900 0.76 423387. 0.7385 8.09 0.0445 0.1345 0.0872 0.0288 9.461 74.542 58.987 7055.338 8.422 262.376 3.792 0.76 423663. 0.7121 12.13 0.0667 0.1961 0.0856 0.0291 9.554 75.273 57.897 7124.528 8.504 257.524 3.686 0.76 423961. 0.6857 16.18 0.0890 0.2540 0.0838 0.0294 9.633 75.896 56.718 7183.476 8.575 252.282 3.581 0.76 424280. 0.6594 20.22 0.1112 0.3084 0.0819 0.0296 9.696 76.389 55.448 7230.198 8.630 246.634 3.478 0.76 424622. 0.6333 24.27 0.1335 0.3593 0.0799 0.0297 9.739 76.732 54.083 7262.599 8.669 240.562 3.378 0.76 424988. 0.6073 28.31 0.1557 0.4070 0.0778 0.0298 9.761 76.900 52.620 7278.540 8.688 234.052 3.279 0.76 425378. 0.5815 32.36 0.1780 0.4515 0.0754 0.0297 9.757 76.871 51.055 7275.797 8.685 227.092 3.183 0.76 425793. 0.5560 36.40 0.2002 0.4929 0.0730 0.0296 9.725 76.621 49.387 7252.149 8.657 219.672 3.089 0.76 426234. 0.5307 40.45 0.2225 0.5314 0.0704 0.0295 9.662 76.126 47.613 7205.312 8.601 211.782 2.997 0.76 426700. 0.5056 44.49 0.2447 0.5672 0.0676 0.0292 9.565 75.362 45.731 7132.944 8.514 203.413 2.908 0.76 427193. 0.4808 48.54 0.2669 0.6003 0.0646 0.0287 9.431 74.301 43.739 7032.528 8.394 194.553 2.821 0.76 427712. 0.4561 52.58 0.2892 0.6307 0.0615 0.0282 9.256 72.922 41.638 6902.014 8.239 185.207 2.736 0.76 428258. 0.4317 56.62 0.3114 0.6587 0.0583 0.0276 9.039 71.215 39.435 6740.500 8.046 175.405 2.654 0.77 428832. 0.4074 60.67 0.3337 0.6842 0.0549 0.0268 8.781 69.179 37.137 6547.790 7.816 165.186 2.573 0.77 429433. 0.3833 64.71 0.3559 0.7072 0.0514 0.0258 8.481 66.814 34.754 6323.933 7.549 154.587 2.493 0.77 430061. 0.3593 68.76 0.3782 0.7275 0.0477 0.0248 8.139 64.122 32.294 6069.083 7.244 143.644 2.413 0.77 430717. 0.3353 72.80 0.4004 0.7450 0.0440 0.0236 7.756 61.104 29.764 5783.504 6.904 132.390 2.334 0.77 431401. 0.3113 76.85 0.4227 0.7594 0.0402 0.0223 7.332 57.767 27.172 5467.604 6.526 120.863 2.254 0.77 432113. 0.2873 80.89 0.4449 0.7703 0.0362 0.0209 6.869 54.115 24.527 5121.963 6.114 109.097 2.172 0.77 432853. 0.2630 84.94 0.4672 0.7769 0.0323 0.0194 6.366 50.158 21.837 4747.418 5.667 97.131 2.086 0.77 433621. 0.2384 88.98 0.4894 0.7782 0.0282 0.0178 5.827 45.907 19.111 4345.102 5.187 85.004 1.995 0.77 434418. 0.2132 93.03 0.5116 0.7726 0.0242 0.0160 5.252 41.380 16.358 3916.554 4.675 72.761 1.894 0.77 435243. 0.1873 97.07 0.5339 0.7573 0.0201 0.0142 4.645 36.596 13.590 3463.760 4.135 60.450 1.780 0.77 436098. 0.1604 101.12 0.5561 0.7277 0.0160 0.0122 4.009 31.583 10.819 2989.279 3.568 48.124 1.642 0.77 436981. 0.1320 105.16 0.5784 0.6750 0.0119 0.0102 3.348 26.374 8.058 2496.303 2.980 35.844 1.464 0.77 437893. 0.1016 109.20 0.6006 0.5812 0.0079 0.0081 2.667 21.011 5.323 1988.704 2.374 23.677 1.214 0.78 438834. 0.0685 113.25 0.6229 0.4025 0.0039 0.0060 1.973 15.541 2.629 1470.949 1.756 11.694 0.811 0.78 439803. 0.0321 117.29 0.6451 -0.0070 0.0000 0.0039 1.264 9.957 -0.028 942.399 1.125 -0.126 -0.014 0.78 440759. 0.0000 PROP RPM = 9000 V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM (mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - - 0.00 0.0000 0.0000 0.0925 0.0326 15.227 106.639 79.208 11354.955 12.048 352.315 3.164 0.86 475922. 0.6884 4.55 0.0222 0.0619 0.0912 0.0327 15.289 107.069 78.069 11400.812 12.097 347.251 3.106 0.86 476211. 0.6709 9.10 0.0445 0.1215 0.0897 0.0328 15.334 107.386 76.824 11434.477 12.132 341.712 3.047 0.86 476524. 0.6530 13.65 0.0667 0.1788 0.0881 0.0329 15.360 107.569 75.467 11454.066 12.153 335.678 2.988 0.86 476862. 0.6347 18.19 0.0889 0.2336 0.0864 0.0329 15.365 107.603 73.993 11457.589 12.157 329.120 2.929 0.86 477224. 0.6160 22.74 0.1112 0.2861 0.0845 0.0329 15.345 107.465 72.395 11442.990 12.141 322.014 2.870 0.86 477613. 0.5969 27.29 0.1334 0.3362 0.0825 0.0328 15.299 107.138 70.669 11408.150 12.104 314.335 2.810 0.86 478029. 0.5775 31.84 0.1557 0.3838 0.0803 0.0326 15.222 106.601 68.809 11350.906 12.044 306.063 2.750 0.86 478472. 0.5576 36.39 0.1779 0.4290 0.0780 0.0324 15.112 105.832 66.813 11269.029 11.957 297.182 2.689 0.86 478943. 0.5374 40.94 0.2001 0.4717 0.0755 0.0320 14.966 104.809 64.676 11160.134 11.841 287.677 2.629 0.86 479443. 0.5168 45.48 0.2224 0.5120 0.0729 0.0316 14.780 103.510 62.396 11021.796 11.694 277.536 2.568 0.86 479973. 0.4959 50.03 0.2446 0.5498 0.0700 0.0312 14.552 101.909 59.971 10851.340 11.514 266.750 2.507 0.86 480532. 0.4746 54.58 0.2668 0.5852 0.0670 0.0306 14.276 99.977 57.397 10645.645 11.295 255.301 2.445 0.86 481121. 0.4530 59.13 0.2891 0.6180 0.0638 0.0299 13.949 97.688 54.674 10401.875 11.037 243.192 2.384 0.86 481740. 0.4310 63.68 0.3113 0.6483 0.0605 0.0290 13.569 95.028 51.812 10118.626 10.736 230.460 2.322 0.86 482390. 0.4087 68.23 0.3336 0.6762 0.0570 0.0281 13.136 91.992 48.821 9795.415 10.393 217.156 2.261 0.86 483070. 0.3862 72.77 0.3558 0.7009 0.0534 0.0271 12.657 88.638 45.712 9438.241 10.014 203.326 2.197 0.86 483781. 0.3631 77.32 0.3780 0.7221 0.0496 0.0260 12.134 84.979 42.495 9048.585 9.601 189.019 2.130 0.86 484523. 0.3395 81.87 0.4003 0.7395 0.0458 0.0248 11.567 81.008 39.182 8625.759 9.152 174.281 2.060 0.86 485296. 0.3153 86.42 0.4225 0.7524 0.0418 0.0235 10.960 76.753 35.782 8172.704 8.672 159.159 1.986 0.86 486100. 0.2904 90.97 0.4447 0.7604 0.0377 0.0221 10.307 72.179 32.308 7685.687 8.155 143.706 1.907 0.87 486936. 0.2650 95.52 0.4670 0.7627 0.0336 0.0206 9.608 67.288 28.771 7164.823 7.602 127.973 1.821 0.87 487802. 0.2388 100.07 0.4892 0.7576 0.0294 0.0190 8.869 62.114 25.183 6613.926 7.018 112.015 1.727 0.87 488701. 0.2119 104.61 0.5114 0.7428 0.0252 0.0173 8.097 56.701 21.558 6037.570 6.406 95.890 1.620 0.87 489631. 0.1838 109.16 0.5337 0.7146 0.0209 0.0156 7.296 51.094 17.910 5440.509 5.773 79.665 1.493 0.87 490594. 0.1545 113.71 0.5559 0.6676 0.0166 0.0139 6.475 45.346 14.256 4828.417 5.123 63.409 1.339 0.87 491588. 0.1236 118.26 0.5782 0.5931 0.0124 0.0121 5.643 39.518 10.613 4207.859 4.465 47.206 1.144 0.87 492615. 0.0911 122.81 0.6004 0.4769 0.0082 0.0103 4.809 33.676 7.003 3585.876 3.805 31.147 0.886 0.87 493674. 0.0573 127.36 0.6226 0.2939 0.0040 0.0085 3.982 27.890 3.447 2969.696 3.151 15.332 0.526 0.87 494764. 0.0239 131.90 0.6449 -0.0065 -0.0001 0.0068 3.158 22.113 -0.059 2354.568 2.498 -0.261 -0.011 0.87 495852. 0.0000 PROP RPM = 10000 V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM (mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - - 0.00 0.0000 0.0000 0.0932 0.0414 26.509 167.079 98.514 19767.455 18.877 438.190 2.260 0.95 528763. 0.5485 5.12 0.0225 0.0500 0.0920 0.0414 26.558 167.389 97.317 19804.145 18.912 432.868 2.229 0.95 529081. 0.5376 10.24 0.0450 0.0986 0.0908 0.0415 26.562 167.418 95.983 19807.561 18.915 426.933 2.198 0.95 529426. 0.5265 15.36 0.0676 0.1459 0.0894 0.0414 26.516 167.125 94.501 19772.854 18.882 420.339 2.168 0.95 529800. 0.5152 20.47 0.0901 0.1919 0.0878 0.0412 26.412 166.472 92.859 19695.580 18.808 413.038 2.138 0.95 530204. 0.5038 25.59 0.1126 0.2367 0.0861 0.0410 26.246 165.426 91.048 19571.832 18.690 404.981 2.110 0.95 530639. 0.4922 30.71 0.1351 0.2804 0.0842 0.0406 26.014 163.960 89.057 19398.408 18.524 396.125 2.082 0.95 531106. 0.4804 35.83 0.1576 0.3228 0.0822 0.0401 25.711 162.054 86.878 19172.887 18.309 386.432 2.055 0.95 531606. 0.4684 40.95 0.1802 0.3642 0.0799 0.0395 25.337 159.694 84.503 18893.738 18.042 375.871 2.029 0.95 532139. 0.4559 46.07 0.2027 0.4043 0.0775 0.0388 24.890 156.875 81.929 18560.117 17.724 364.419 2.002 0.95 532706. 0.4431 51.18 0.2252 0.4433 0.0749 0.0380 24.369 153.591 79.150 18171.648 17.353 352.058 1.976 0.95 533307. 0.4297 56.30 0.2477 0.4810 0.0720 0.0371 23.774 149.843 76.163 17728.160 16.929 338.775 1.949 0.95 533943. 0.4158 61.42 0.2703 0.5172 0.0690 0.0361 23.104 145.624 72.965 17228.982 16.452 324.550 1.921 0.96 534614. 0.4012 66.54 0.2928 0.5519 0.0658 0.0349 22.360 140.931 69.557 16673.746 15.922 309.389 1.892 0.96 535321. 0.3858 71.66 0.3153 0.5850 0.0624 0.0336 21.542 135.778 65.950 16064.095 15.340 293.346 1.862 0.96 536062. 0.3697 76.78 0.3378 0.6161 0.0588 0.0322 20.655 130.185 62.162 15402.416 14.708 276.495 1.831 0.96 536839. 0.3529 81.90 0.3603 0.6452 0.0551 0.0307 19.701 124.171 58.208 14690.865 14.029 258.910 1.797 0.96 537651. 0.3352 87.01 0.3829 0.6711 0.0512 0.0292 18.706 117.902 54.102 13949.240 13.321 240.648 1.759 0.96 538498. 0.3164 92.13 0.4054 0.6915 0.0472 0.0276 17.715 111.652 49.859 13209.757 12.614 221.774 1.712 0.96 539380. 0.2955 97.25 0.4279 0.7047 0.0430 0.0261 16.741 105.513 45.495 12483.474 11.921 202.360 1.653 0.96 540298. 0.2726 102.37 0.4504 0.7050 0.0388 0.0248 15.882 100.101 41.016 11843.129 11.309 182.437 1.571 0.96 541251. 0.2460 107.49 0.4729 0.6920 0.0345 0.0236 15.096 95.146 36.446 11256.900 10.750 162.110 1.468 0.96 542239. 0.2167 112.61 0.4955 0.6685 0.0301 0.0223 14.291 90.075 31.817 10656.920 10.177 141.522 1.354 0.96 543263. 0.1867 117.72 0.5180 0.6324 0.0257 0.0210 13.479 84.957 27.152 10051.388 9.598 120.774 1.225 0.96 544323. 0.1561 122.84 0.5405 0.5811 0.0213 0.0198 12.672 79.869 22.480 9449.391 9.024 99.992 1.079 0.97 545419. 0.1251 127.96 0.5630 0.5121 0.0169 0.0185 11.880 74.875 17.830 8858.609 8.459 79.306 0.913 0.97 546551. 0.0942 133.08 0.5856 0.4228 0.0125 0.0173 11.109 70.020 13.235 8284.176 7.911 58.871 0.725 0.97 547720. 0.0645 138.20 0.6081 0.3104 0.0083 0.0162 10.368 65.346 8.734 7731.208 7.383 38.848 0.512 0.97 548927. 0.0370 143.32 0.6306 0.1724 0.0041 0.0151 9.657 60.868 4.356 7201.422 6.877 19.374 0.274 0.97 550176. 0.0140 148.43 0.6531 0.0018 0.0000 0.0139 8.922 56.237 0.040 6653.467 6.354 0.179 0.003 0.97 551503. 0.0000