16x12E (16x12E.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 0.1022 0.0466 0.004 0.248 0.213 2.931 0.028 0.949 33.020 0.06 23756. 0.5593 0.48 0.0316 0.0675 0.1013 0.0474 0.004 0.252 0.212 2.985 0.028 0.941 32.147 0.06 23776. 0.5422 0.96 0.0632 0.1312 0.1003 0.0483 0.004 0.257 0.209 3.040 0.029 0.932 31.258 0.06 23798. 0.5247 1.44 0.0948 0.1912 0.0992 0.0492 0.004 0.262 0.207 3.095 0.030 0.922 30.359 0.06 23823. 0.5068 1.92 0.1264 0.2473 0.0980 0.0501 0.004 0.266 0.205 3.150 0.030 0.910 29.457 0.06 23851. 0.4886 2.39 0.1580 0.2997 0.0965 0.0509 0.004 0.271 0.202 3.203 0.031 0.897 28.556 0.06 23882. 0.4702 2.87 0.1896 0.3483 0.0950 0.0517 0.004 0.275 0.198 3.252 0.031 0.882 27.661 0.06 23916. 0.4518 3.35 0.2212 0.3934 0.0932 0.0524 0.004 0.279 0.195 3.297 0.031 0.866 26.777 0.06 23953. 0.4332 3.83 0.2528 0.4350 0.0912 0.0530 0.004 0.282 0.190 3.334 0.032 0.847 25.907 0.06 23993. 0.4146 4.31 0.2844 0.4733 0.0890 0.0535 0.005 0.284 0.186 3.364 0.032 0.826 25.053 0.06 24037. 0.3960 4.79 0.3160 0.5083 0.0865 0.0538 0.005 0.286 0.181 3.382 0.032 0.803 24.218 0.06 24085. 0.3774 5.27 0.3476 0.5403 0.0837 0.0539 0.005 0.286 0.175 3.389 0.032 0.778 23.401 0.06 24135. 0.3589 5.75 0.3792 0.5693 0.0807 0.0537 0.005 0.286 0.169 3.382 0.032 0.750 22.603 0.06 24190. 0.3403 6.22 0.4108 0.5954 0.0774 0.0534 0.005 0.284 0.162 3.358 0.032 0.719 21.820 0.06 24247. 0.3216 6.70 0.4424 0.6186 0.0737 0.0527 0.004 0.280 0.154 3.318 0.032 0.685 21.051 0.06 24309. 0.3029 7.18 0.4740 0.6388 0.0698 0.0518 0.004 0.275 0.146 3.258 0.031 0.648 20.291 0.06 24374. 0.2841 7.66 0.5056 0.6559 0.0656 0.0505 0.004 0.269 0.137 3.180 0.030 0.609 19.532 0.06 24442. 0.2651 8.14 0.5372 0.6696 0.0610 0.0490 0.004 0.260 0.127 3.080 0.029 0.567 18.767 0.06 24515. 0.2457 8.62 0.5688 0.6795 0.0562 0.0471 0.004 0.250 0.117 2.962 0.028 0.522 17.984 0.06 24590. 0.2260 9.10 0.6004 0.6848 0.0512 0.0449 0.004 0.239 0.107 2.824 0.027 0.476 17.171 0.06 24669. 0.2059 9.58 0.6320 0.6847 0.0460 0.0424 0.004 0.226 0.096 2.671 0.026 0.427 16.311 0.06 24752. 0.1854 10.05 0.6636 0.6781 0.0406 0.0398 0.003 0.211 0.085 2.502 0.024 0.377 15.383 0.06 24837. 0.1643 10.53 0.6952 0.6631 0.0352 0.0369 0.003 0.196 0.073 2.319 0.022 0.327 14.361 0.07 24927. 0.1427 11.01 0.7268 0.6376 0.0296 0.0338 0.003 0.180 0.062 2.124 0.020 0.275 13.207 0.07 25019. 0.1205 11.49 0.7584 0.5977 0.0240 0.0305 0.003 0.162 0.050 1.918 0.018 0.223 11.866 0.07 25115. 0.0975 11.97 0.7900 0.5381 0.0184 0.0270 0.002 0.144 0.038 1.702 0.016 0.171 10.255 0.07 25215. 0.0738 12.45 0.8216 0.4497 0.0128 0.0235 0.002 0.125 0.027 1.477 0.014 0.119 8.240 0.07 25317. 0.0495 12.93 0.8532 0.3167 0.0074 0.0198 0.002 0.105 0.015 1.246 0.012 0.068 5.588 0.07 25423. 0.0254 13.41 0.8848 0.1087 0.0020 0.0161 0.001 0.085 0.004 1.011 0.010 0.018 1.850 0.07 25532. 0.0044 13.88 0.9164 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 0.1025 0.0430 0.029 0.916 0.856 21.667 0.103 3.808 17.923 0.13 47511. 0.6082 0.94 0.0311 0.0719 0.1016 0.0439 0.030 0.934 0.849 22.112 0.106 3.777 17.419 0.13 47550. 0.5886 1.88 0.0622 0.1396 0.1007 0.0448 0.030 0.954 0.841 22.568 0.108 3.742 16.907 0.13 47594. 0.5687 2.83 0.0933 0.2031 0.0996 0.0458 0.031 0.973 0.832 23.030 0.110 3.702 16.393 0.13 47643. 0.5485 3.77 0.1243 0.2623 0.0984 0.0467 0.031 0.993 0.822 23.489 0.112 3.658 15.879 0.13 47698. 0.5281 4.71 0.1554 0.3173 0.0971 0.0475 0.032 1.012 0.811 23.935 0.114 3.608 15.369 0.13 47758. 0.5076 5.65 0.1865 0.3683 0.0956 0.0484 0.033 1.029 0.798 24.358 0.116 3.551 14.865 0.13 47825. 0.4871 6.59 0.2176 0.4154 0.0938 0.0492 0.033 1.046 0.784 24.746 0.118 3.487 14.370 0.13 47897. 0.4666 7.54 0.2487 0.4587 0.0919 0.0498 0.034 1.060 0.768 25.085 0.120 3.416 13.885 0.13 47976. 0.4462 8.48 0.2798 0.4985 0.0898 0.0504 0.034 1.072 0.750 25.360 0.121 3.336 13.413 0.13 48061. 0.4260 9.42 0.3109 0.5349 0.0874 0.0508 0.034 1.080 0.730 25.559 0.122 3.247 12.954 0.13 48153. 0.4059 10.36 0.3419 0.5682 0.0847 0.0510 0.034 1.085 0.708 25.665 0.123 3.148 12.509 0.13 48252. 0.3859 11.30 0.3730 0.5985 0.0818 0.0510 0.034 1.085 0.683 25.664 0.123 3.040 12.077 0.13 48357. 0.3661 12.25 0.4041 0.6259 0.0786 0.0507 0.034 1.079 0.657 25.542 0.122 2.920 11.659 0.13 48470. 0.3464 13.19 0.4352 0.6505 0.0751 0.0502 0.034 1.069 0.627 25.286 0.121 2.790 11.252 0.13 48589. 0.3268 14.13 0.4663 0.6724 0.0713 0.0494 0.033 1.052 0.596 24.884 0.119 2.649 10.855 0.13 48715. 0.3072 15.07 0.4974 0.6915 0.0672 0.0483 0.033 1.028 0.561 24.327 0.116 2.497 10.466 0.13 48848. 0.2876 16.01 0.5284 0.7077 0.0628 0.0469 0.032 0.998 0.525 23.609 0.113 2.334 10.081 0.13 48988. 0.2678 16.96 0.5595 0.7207 0.0582 0.0452 0.030 0.961 0.486 22.729 0.109 2.161 9.695 0.13 49135. 0.2478 17.90 0.5906 0.7300 0.0533 0.0431 0.029 0.917 0.445 21.696 0.104 1.980 9.304 0.13 49289. 0.2276 18.84 0.6217 0.7351 0.0482 0.0408 0.028 0.867 0.403 20.521 0.098 1.791 8.901 0.13 49449. 0.2071 19.78 0.6528 0.7351 0.0430 0.0382 0.026 0.812 0.359 19.216 0.092 1.597 8.476 0.13 49615. 0.1863 20.72 0.6839 0.7286 0.0377 0.0353 0.024 0.752 0.315 17.791 0.085 1.399 8.019 0.13 49789. 0.1649 21.67 0.7150 0.7138 0.0322 0.0323 0.022 0.687 0.269 16.256 0.078 1.198 7.515 0.13 49969. 0.1430 22.61 0.7460 0.6879 0.0268 0.0290 0.020 0.618 0.224 14.619 0.070 0.995 6.941 0.13 50155. 0.1204 23.55 0.7771 0.6463 0.0213 0.0256 0.017 0.545 0.178 12.893 0.062 0.792 6.261 0.13 50348. 0.0969 24.49 0.8082 0.5813 0.0158 0.0220 0.015 0.469 0.132 11.089 0.053 0.589 5.414 0.13 50547. 0.0722 25.43 0.8393 0.4786 0.0104 0.0183 0.012 0.390 0.087 9.223 0.044 0.388 4.293 0.13 50752. 0.0465 26.38 0.8704 0.3089 0.0052 0.0145 0.010 0.309 0.043 7.310 0.035 0.192 2.672 0.13 50964. 0.0203 27.32 0.9015 0.0007 0.0000 0.0107 0.007 0.227 0.000 5.370 0.026 0.000 0.006 0.13 51182. 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 0.1027 0.0416 0.095 1.989 1.931 70.597 0.225 8.591 12.408 0.19 71265. 0.6324 1.42 0.0312 0.0748 0.1019 0.0425 0.097 2.032 1.916 72.135 0.230 8.521 12.046 0.19 71324. 0.6114 2.83 0.0623 0.1450 0.1010 0.0434 0.099 2.077 1.898 73.718 0.235 8.443 11.679 0.19 71391. 0.5901 4.25 0.0935 0.2107 0.0999 0.0443 0.101 2.122 1.878 75.323 0.240 8.355 11.311 0.19 71465. 0.5685 5.67 0.1246 0.2718 0.0987 0.0453 0.103 2.167 1.856 76.921 0.245 8.255 10.944 0.19 71547. 0.5468 7.08 0.1558 0.3285 0.0974 0.0462 0.105 2.211 1.831 78.481 0.250 8.143 10.580 0.19 71638. 0.5250 8.50 0.1870 0.3808 0.0959 0.0471 0.107 2.253 1.802 79.963 0.255 8.016 10.222 0.19 71737. 0.5033 9.91 0.2181 0.4290 0.0942 0.0479 0.109 2.291 1.770 81.327 0.259 7.873 9.871 0.19 71846. 0.4816 11.33 0.2493 0.4734 0.0922 0.0486 0.111 2.325 1.734 82.527 0.263 7.712 9.529 0.19 71965. 0.4602 12.75 0.2804 0.5140 0.0901 0.0492 0.112 2.353 1.693 83.514 0.266 7.532 9.197 0.19 72094. 0.4389 14.16 0.3116 0.5511 0.0877 0.0496 0.113 2.373 1.648 84.238 0.268 7.332 8.875 0.19 72232. 0.4179 15.58 0.3427 0.5850 0.0850 0.0498 0.114 2.385 1.598 84.647 0.269 7.109 8.565 0.19 72381. 0.3971 17.00 0.3739 0.6158 0.0821 0.0498 0.114 2.386 1.543 84.690 0.270 6.864 8.264 0.19 72540. 0.3765 18.41 0.4051 0.6437 0.0789 0.0496 0.113 2.376 1.482 84.316 0.268 6.594 7.975 0.19 72709. 0.3561 19.83 0.4362 0.6689 0.0753 0.0491 0.112 2.352 1.416 83.481 0.266 6.300 7.695 0.19 72889. 0.3358 21.24 0.4674 0.6914 0.0715 0.0484 0.110 2.314 1.344 82.144 0.261 5.980 7.424 0.19 73079. 0.3157 22.66 0.4985 0.7112 0.0674 0.0473 0.108 2.262 1.267 80.274 0.256 5.636 7.159 0.19 73280. 0.2955 24.08 0.5297 0.7282 0.0630 0.0458 0.104 2.193 1.184 77.846 0.248 5.267 6.899 0.19 73491. 0.2753 25.49 0.5609 0.7422 0.0583 0.0441 0.100 2.109 1.096 74.855 0.238 4.875 6.641 0.19 73712. 0.2550 26.91 0.5920 0.7529 0.0534 0.0420 0.096 2.010 1.004 71.332 0.227 4.464 6.382 0.19 73943. 0.2345 28.33 0.6232 0.7596 0.0483 0.0396 0.090 1.897 0.908 67.316 0.214 4.038 6.117 0.19 74185. 0.2137 29.74 0.6543 0.7615 0.0430 0.0370 0.084 1.771 0.809 62.843 0.200 3.599 5.840 0.19 74436. 0.1927 31.16 0.6855 0.7575 0.0377 0.0341 0.078 1.633 0.709 57.948 0.184 3.151 5.546 0.19 74697. 0.1712 32.58 0.7167 0.7458 0.0323 0.0310 0.071 1.484 0.606 52.662 0.168 2.697 5.223 0.20 74968. 0.1491 33.99 0.7478 0.7236 0.0268 0.0277 0.063 1.325 0.503 47.020 0.150 2.239 4.856 0.20 75249. 0.1263 35.41 0.7790 0.6862 0.0213 0.0242 0.055 1.157 0.400 41.061 0.131 1.780 4.421 0.20 75539. 0.1026 36.82 0.8101 0.6255 0.0158 0.0205 0.047 0.981 0.298 34.828 0.111 1.323 3.874 0.20 75839. 0.0775 38.24 0.8413 0.5254 0.0104 0.0167 0.038 0.799 0.196 28.374 0.090 0.872 3.134 0.20 76149. 0.0509 39.66 0.8725 0.3503 0.0051 0.0128 0.029 0.613 0.097 21.758 0.069 0.430 2.015 0.20 76468. 0.0230 41.07 0.9036 0.0008 0.0000 0.0089 0.020 0.424 0.000 15.045 0.048 0.001 0.005 0.20 76795. 0.0000 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 0.1030 0.0408 0.220 3.468 3.443 164.114 0.392 15.314 9.515 0.25 95018. 0.6475 1.89 0.0312 0.0765 0.1022 0.0417 0.225 3.546 3.416 167.825 0.401 15.192 9.231 0.25 95097. 0.6256 3.78 0.0624 0.1483 0.1013 0.0426 0.230 3.627 3.385 171.651 0.410 15.055 8.944 0.25 95186. 0.6034 5.67 0.0936 0.2153 0.1002 0.0436 0.235 3.709 3.350 175.534 0.419 14.901 8.656 0.25 95285. 0.5810 7.56 0.1248 0.2775 0.0991 0.0446 0.241 3.791 3.311 179.408 0.428 14.726 8.370 0.25 95395. 0.5585 9.46 0.1560 0.3352 0.0977 0.0455 0.246 3.871 3.266 183.194 0.437 14.527 8.086 0.25 95516. 0.5359 11.35 0.1872 0.3884 0.0962 0.0464 0.251 3.947 3.216 186.803 0.446 14.303 7.808 0.25 95649. 0.5135 13.24 0.2184 0.4373 0.0945 0.0472 0.255 4.018 3.159 190.131 0.454 14.050 7.535 0.25 95795. 0.4911 15.13 0.2496 0.4822 0.0926 0.0479 0.259 4.080 3.095 193.071 0.461 13.765 7.270 0.25 95954. 0.4690 17.02 0.2808 0.5233 0.0905 0.0485 0.262 4.131 3.023 195.504 0.467 13.446 7.013 0.25 96125. 0.4472 18.91 0.3120 0.5608 0.0881 0.0490 0.265 4.169 2.943 197.309 0.471 13.090 6.765 0.26 96311. 0.4256 20.80 0.3432 0.5951 0.0854 0.0493 0.266 4.191 2.854 198.360 0.474 12.694 6.525 0.26 96509. 0.4043 22.69 0.3744 0.6262 0.0825 0.0493 0.266 4.195 2.755 198.531 0.474 12.256 6.295 0.26 96722. 0.3832 24.58 0.4056 0.6545 0.0792 0.0491 0.265 4.178 2.647 197.703 0.472 11.775 6.073 0.26 96949. 0.3624 26.47 0.4368 0.6801 0.0757 0.0486 0.263 4.137 2.529 195.764 0.467 11.249 5.860 0.26 97189. 0.3417 28.37 0.4680 0.7030 0.0718 0.0478 0.258 4.070 2.401 192.616 0.460 10.678 5.653 0.26 97444. 0.3212 30.26 0.4992 0.7233 0.0677 0.0467 0.252 3.976 2.262 188.183 0.449 10.063 5.453 0.26 97712. 0.3008 32.15 0.5304 0.7408 0.0633 0.0453 0.245 3.854 2.114 182.402 0.435 9.403 5.257 0.26 97994. 0.2803 34.04 0.5616 0.7556 0.0585 0.0435 0.235 3.703 1.956 175.261 0.418 8.703 5.063 0.26 98290. 0.2597 35.93 0.5928 0.7671 0.0536 0.0414 0.224 3.525 1.791 166.830 0.398 7.968 4.870 0.26 98599. 0.2390 37.82 0.6240 0.7749 0.0485 0.0390 0.211 3.322 1.620 157.202 0.375 7.205 4.674 0.26 98921. 0.2182 39.71 0.6552 0.7783 0.0432 0.0364 0.196 3.095 1.444 146.463 0.350 6.421 4.471 0.26 99257. 0.1970 41.60 0.6864 0.7761 0.0378 0.0334 0.181 2.846 1.264 134.692 0.322 5.621 4.255 0.26 99606. 0.1754 43.49 0.7176 0.7667 0.0324 0.0303 0.164 2.577 1.081 121.968 0.291 4.809 4.021 0.26 99969. 0.1533 45.38 0.7488 0.7472 0.0269 0.0269 0.145 2.290 0.897 108.374 0.259 3.991 3.755 0.26 100344. 0.1305 47.28 0.7800 0.7130 0.0213 0.0233 0.126 1.986 0.713 94.005 0.224 3.172 3.440 0.26 100732. 0.1065 49.17 0.8112 0.6559 0.0159 0.0196 0.106 1.669 0.530 78.967 0.189 2.356 3.043 0.26 101133. 0.0812 51.06 0.8424 0.5587 0.0104 0.0157 0.085 1.339 0.349 63.388 0.151 1.552 2.496 0.26 101547. 0.0541 52.95 0.8736 0.3813 0.0051 0.0118 0.064 1.002 0.172 47.416 0.113 0.764 1.643 0.26 101974. 0.0250 54.84 0.9049 -0.0005 0.0000 0.0077 0.042 0.659 0.000 31.207 0.075 -0.001 -0.002 0.26 102411. 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 0.1034 0.0403 0.425 5.358 5.396 316.971 0.605 24.003 7.722 0.32 118770. 0.6579 2.36 0.0312 0.0776 0.1026 0.0412 0.435 5.483 5.355 324.325 0.619 23.817 7.488 0.32 118869. 0.6355 4.73 0.0624 0.1504 0.1016 0.0422 0.445 5.611 5.307 331.917 0.634 23.607 7.253 0.32 118980. 0.6127 7.09 0.0936 0.2182 0.1006 0.0432 0.455 5.741 5.254 339.632 0.649 23.369 7.016 0.32 119104. 0.5898 9.46 0.1248 0.2812 0.0995 0.0442 0.466 5.872 5.193 347.341 0.663 23.100 6.782 0.32 119241. 0.5668 11.82 0.1561 0.3395 0.0981 0.0451 0.476 5.999 5.124 354.887 0.678 22.794 6.549 0.32 119393. 0.5437 14.19 0.1873 0.3932 0.0967 0.0460 0.486 6.121 5.047 362.092 0.692 22.447 6.321 0.32 119559. 0.5208 16.55 0.2185 0.4425 0.0950 0.0469 0.495 6.234 4.958 368.755 0.704 22.055 6.099 0.32 119742. 0.4980 18.92 0.2497 0.4878 0.0931 0.0476 0.502 6.333 4.859 374.658 0.716 21.612 5.882 0.32 119940. 0.4755 21.28 0.2809 0.5292 0.0909 0.0483 0.509 6.416 4.747 379.569 0.725 21.115 5.673 0.32 120155. 0.4533 23.65 0.3121 0.5671 0.0885 0.0487 0.514 6.479 4.622 383.244 0.732 20.560 5.470 0.32 120387. 0.4313 26.01 0.3433 0.6016 0.0859 0.0490 0.517 6.516 4.483 385.434 0.736 19.942 5.276 0.32 120636. 0.4097 28.37 0.3745 0.6330 0.0829 0.0491 0.517 6.523 4.330 385.890 0.737 19.258 5.089 0.32 120902. 0.3883 30.74 0.4058 0.6616 0.0797 0.0489 0.515 6.498 4.160 384.370 0.734 18.505 4.909 0.32 121185. 0.3672 33.10 0.4370 0.6874 0.0761 0.0484 0.510 6.435 3.975 380.654 0.727 17.681 4.737 0.32 121486. 0.3463 35.47 0.4682 0.7106 0.0723 0.0476 0.502 6.332 3.774 374.547 0.715 16.787 4.570 0.32 121805. 0.3256 37.83 0.4994 0.7313 0.0681 0.0465 0.491 6.185 3.557 365.891 0.699 15.821 4.409 0.32 122140. 0.3050 40.20 0.5306 0.7494 0.0637 0.0451 0.475 5.994 3.324 354.563 0.677 14.786 4.252 0.32 122493. 0.2843 42.56 0.5618 0.7647 0.0589 0.0433 0.457 5.757 3.077 340.534 0.650 13.686 4.098 0.32 122863. 0.2636 44.93 0.5930 0.7769 0.0540 0.0412 0.434 5.476 2.817 323.937 0.619 12.531 3.945 0.32 123250. 0.2428 47.29 0.6242 0.7857 0.0488 0.0388 0.409 5.155 2.548 304.952 0.582 11.333 3.790 0.32 123654. 0.2218 49.66 0.6554 0.7902 0.0435 0.0361 0.381 4.797 2.271 283.748 0.542 10.101 3.630 0.32 124074. 0.2006 52.02 0.6867 0.7895 0.0381 0.0331 0.349 4.403 1.988 260.480 0.497 8.844 3.462 0.32 124511. 0.1790 54.38 0.7179 0.7819 0.0326 0.0299 0.316 3.978 1.701 235.306 0.449 7.568 3.280 0.33 124964. 0.1569 56.75 0.7491 0.7648 0.0270 0.0265 0.279 3.523 1.412 208.390 0.398 6.282 3.074 0.33 125433. 0.1340 59.11 0.7803 0.7336 0.0215 0.0229 0.241 3.041 1.123 179.918 0.344 4.995 2.831 0.33 125919. 0.1100 61.48 0.8115 0.6800 0.0160 0.0191 0.201 2.537 0.835 150.108 0.287 3.714 2.523 0.33 126421. 0.0845 63.84 0.8427 0.5865 0.0105 0.0152 0.160 2.015 0.551 119.213 0.228 2.450 2.095 0.33 126939. 0.0570 66.21 0.8739 0.4100 0.0052 0.0111 0.117 1.480 0.273 87.530 0.167 1.213 1.413 0.33 127472. 0.0271 68.57 0.9051 0.0070 0.0001 0.0070 0.074 0.936 0.003 55.371 0.106 0.013 0.023 0.33 128019. 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 0.1037 0.0401 0.730 7.671 7.799 544.536 0.867 34.692 6.496 0.38 142520. 0.6653 2.84 0.0312 0.0784 0.1030 0.0410 0.748 7.853 7.741 557.433 0.887 34.430 6.298 0.38 142638. 0.6426 5.68 0.0625 0.1519 0.1021 0.0420 0.765 8.040 7.674 570.765 0.908 34.134 6.098 0.38 142772. 0.6195 8.52 0.0937 0.2203 0.1011 0.0430 0.784 8.232 7.599 584.331 0.930 33.799 5.898 0.38 142920. 0.5963 11.36 0.1250 0.2838 0.0999 0.0440 0.802 8.423 7.513 597.904 0.952 33.417 5.699 0.38 143085. 0.5729 14.20 0.1562 0.3426 0.0986 0.0450 0.820 8.610 7.415 611.210 0.973 32.982 5.503 0.38 143268. 0.5495 17.04 0.1874 0.3967 0.0971 0.0459 0.837 8.789 7.304 623.935 0.993 32.489 5.310 0.38 143468. 0.5263 19.88 0.2187 0.4464 0.0955 0.0468 0.853 8.956 7.178 635.727 1.012 31.929 5.121 0.38 143687. 0.5032 22.72 0.2499 0.4919 0.0936 0.0475 0.867 9.103 7.036 646.200 1.028 31.296 4.939 0.38 143926. 0.4804 25.56 0.2812 0.5336 0.0914 0.0482 0.878 9.226 6.876 654.943 1.042 30.583 4.762 0.38 144184. 0.4579 28.40 0.3124 0.5716 0.0891 0.0487 0.887 9.319 6.696 661.527 1.053 29.785 4.591 0.38 144463. 0.4357 31.24 0.3436 0.6064 0.0864 0.0490 0.892 9.375 6.496 665.511 1.059 28.895 4.427 0.38 144762. 0.4138 34.08 0.3749 0.6380 0.0834 0.0490 0.894 9.388 6.274 666.456 1.061 27.908 4.270 0.38 145083. 0.3922 36.92 0.4061 0.6668 0.0802 0.0489 0.890 9.353 6.030 663.936 1.057 26.821 4.119 0.38 145424. 0.3710 39.76 0.4374 0.6928 0.0766 0.0484 0.882 9.263 5.762 657.558 1.047 25.630 3.975 0.38 145786. 0.3499 42.60 0.4686 0.7163 0.0728 0.0476 0.868 9.114 5.471 646.980 1.030 24.335 3.835 0.39 146169. 0.3290 45.44 0.4999 0.7373 0.0686 0.0465 0.847 8.902 5.156 631.922 1.006 22.936 3.701 0.39 146572. 0.3082 48.28 0.5311 0.7558 0.0641 0.0450 0.821 8.624 4.819 612.163 0.974 21.435 3.571 0.39 146997. 0.2874 51.12 0.5623 0.7715 0.0593 0.0432 0.788 8.278 4.460 587.651 0.935 19.839 3.443 0.39 147442. 0.2666 53.96 0.5936 0.7844 0.0543 0.0411 0.749 7.869 4.084 558.614 0.889 18.164 3.316 0.39 147907. 0.2457 56.80 0.6248 0.7939 0.0491 0.0387 0.705 7.401 3.693 525.364 0.836 16.425 3.188 0.39 148393. 0.2247 59.64 0.6561 0.7993 0.0438 0.0359 0.655 6.877 3.290 488.195 0.777 14.636 3.057 0.39 148898. 0.2034 62.48 0.6873 0.7997 0.0383 0.0329 0.600 6.302 2.880 447.380 0.712 12.809 2.920 0.39 149423. 0.1817 65.32 0.7185 0.7935 0.0328 0.0297 0.541 5.680 2.463 403.193 0.642 10.957 2.771 0.39 149968. 0.1595 68.16 0.7498 0.7781 0.0272 0.0262 0.477 5.014 2.043 355.928 0.566 9.089 2.604 0.39 150533. 0.1365 71.00 0.7810 0.7491 0.0216 0.0225 0.410 4.309 1.623 305.913 0.487 7.220 2.407 0.39 151116. 0.1124 73.84 0.8123 0.6979 0.0160 0.0187 0.340 3.572 1.205 253.533 0.404 5.360 2.156 0.39 151720. 0.0868 76.68 0.8435 0.6065 0.0105 0.0147 0.267 2.807 0.793 199.242 0.317 3.525 1.804 0.39 152342. 0.0589 79.52 0.8747 0.4284 0.0052 0.0106 0.193 2.022 0.389 143.568 0.228 1.730 1.229 0.40 152984. 0.0281 82.36 0.9060 -0.0045 0.0000 0.0064 0.117 1.226 -0.002 87.063 0.139 -0.011 -0.012 0.40 153640. 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 0.1042 0.0400 1.157 10.421 10.661 863.048 1.177 47.418 5.603 0.44 166267. 0.6708 3.31 0.0312 0.0789 0.1034 0.0410 1.185 10.672 10.583 883.829 1.206 47.074 5.431 0.44 166405. 0.6479 6.63 0.0625 0.1528 0.1026 0.0419 1.214 10.932 10.495 905.339 1.235 46.682 5.258 0.44 166561. 0.6247 9.94 0.0937 0.2216 0.1016 0.0430 1.243 11.196 10.395 927.261 1.265 46.237 5.085 0.44 166734. 0.6012 13.26 0.1250 0.2855 0.1005 0.0440 1.273 11.462 10.281 949.227 1.295 45.729 4.912 0.44 166927. 0.5776 16.57 0.1562 0.3445 0.0992 0.0450 1.302 11.722 10.150 970.796 1.324 45.149 4.742 0.44 167140. 0.5541 19.88 0.1875 0.3989 0.0977 0.0459 1.330 11.972 10.002 991.461 1.353 44.488 4.576 0.45 167374. 0.5307 23.20 0.2187 0.4488 0.0961 0.0468 1.355 12.203 9.833 1010.649 1.379 43.735 4.413 0.45 167630. 0.5074 26.51 0.2500 0.4945 0.0942 0.0476 1.378 12.410 9.641 1027.737 1.402 42.882 4.255 0.45 167908. 0.4845 29.83 0.2812 0.5364 0.0921 0.0483 1.397 12.582 9.424 1042.058 1.422 41.919 4.102 0.45 168210. 0.4618 33.14 0.3125 0.5746 0.0897 0.0488 1.412 12.714 9.181 1052.912 1.436 40.837 3.955 0.45 168536. 0.4395 36.45 0.3437 0.6095 0.0871 0.0491 1.421 12.794 8.909 1059.588 1.445 39.629 3.814 0.45 168885. 0.4175 39.77 0.3750 0.6413 0.0841 0.0492 1.423 12.816 8.608 1061.369 1.448 38.286 3.678 0.45 169259. 0.3958 43.08 0.4062 0.6703 0.0809 0.0490 1.418 12.770 8.274 1057.567 1.443 36.804 3.549 0.45 169658. 0.3744 46.40 0.4375 0.6965 0.0773 0.0485 1.405 12.649 7.909 1047.542 1.429 35.179 3.424 0.45 170081. 0.3532 49.71 0.4687 0.7203 0.0734 0.0478 1.382 12.446 7.511 1030.736 1.406 33.408 3.305 0.45 170528. 0.3322 53.03 0.5000 0.7416 0.0692 0.0466 1.350 12.155 7.080 1006.694 1.373 31.494 3.190 0.45 171000. 0.3113 56.34 0.5312 0.7604 0.0647 0.0452 1.308 11.773 6.618 975.060 1.330 29.438 3.079 0.45 171496. 0.2904 59.65 0.5624 0.7766 0.0599 0.0434 1.255 11.299 6.126 935.734 1.277 27.250 2.970 0.45 172015. 0.2695 62.97 0.5937 0.7900 0.0548 0.0412 1.192 10.735 5.610 889.077 1.213 24.952 2.862 0.45 172559. 0.2486 66.28 0.6249 0.8002 0.0496 0.0387 1.121 10.089 5.073 835.587 1.140 22.565 2.754 0.45 173126. 0.2275 69.60 0.6562 0.8065 0.0442 0.0359 1.040 9.367 4.521 775.735 1.058 20.108 2.643 0.45 173716. 0.2061 72.91 0.6874 0.8079 0.0387 0.0329 0.952 8.573 3.957 709.964 0.969 17.599 2.528 0.45 174329. 0.1844 76.22 0.7187 0.8031 0.0331 0.0296 0.857 7.712 3.384 638.716 0.871 15.053 2.403 0.46 174965. 0.1621 79.54 0.7499 0.7894 0.0274 0.0261 0.754 6.792 2.807 562.464 0.767 12.487 2.264 0.46 175624. 0.1391 82.85 0.7812 0.7624 0.0218 0.0223 0.646 5.817 2.229 481.746 0.657 9.916 2.099 0.46 176306. 0.1149 86.17 0.8124 0.7138 0.0162 0.0184 0.533 4.796 1.655 397.184 0.542 7.360 1.890 0.46 177010. 0.0891 89.48 0.8437 0.6252 0.0106 0.0143 0.415 3.737 1.088 309.519 0.422 4.838 1.594 0.46 177736. 0.0610 92.79 0.8749 0.4477 0.0052 0.0102 0.295 2.652 0.533 219.618 0.300 2.370 1.100 0.46 178485. 0.0295 96.11 0.9062 -0.0074 0.0000 0.0059 0.172 1.550 -0.005 128.370 0.175 -0.022 -0.018 0.46 179251. 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 0.1047 0.0400 1.730 13.628 13.991 1289.921 1.540 62.231 4.920 0.51 190011. 0.6748 3.79 0.0312 0.0791 0.1039 0.0410 1.772 13.961 13.894 1321.408 1.577 61.799 4.769 0.51 190169. 0.6519 7.57 0.0625 0.1533 0.1031 0.0420 1.816 14.306 13.783 1354.051 1.616 61.307 4.617 0.51 190347. 0.6286 11.36 0.0937 0.2223 0.1022 0.0431 1.861 14.658 13.657 1387.379 1.656 60.745 4.465 0.51 190545. 0.6051 15.14 0.1249 0.2863 0.1011 0.0441 1.905 15.012 13.512 1420.832 1.696 60.100 4.313 0.51 190765. 0.5815 18.93 0.1562 0.3455 0.0998 0.0451 1.950 15.359 13.346 1453.744 1.735 59.362 4.164 0.51 191008. 0.5578 22.71 0.1874 0.4000 0.0984 0.0461 1.992 15.693 13.156 1485.340 1.773 58.517 4.017 0.51 191275. 0.5344 26.50 0.2186 0.4501 0.0968 0.0470 2.031 16.004 12.939 1514.750 1.808 57.551 3.874 0.51 191568. 0.5111 30.29 0.2499 0.4960 0.0950 0.0478 2.067 16.281 12.692 1541.021 1.839 56.452 3.736 0.51 191886. 0.4880 34.07 0.2811 0.5380 0.0929 0.0485 2.096 16.515 12.412 1563.132 1.866 55.208 3.601 0.51 192231. 0.4653 37.86 0.3123 0.5763 0.0905 0.0490 2.119 16.693 12.096 1580.016 1.886 53.805 3.472 0.51 192603. 0.4429 41.64 0.3436 0.6113 0.0879 0.0494 2.133 16.805 11.743 1590.583 1.899 52.234 3.349 0.51 193003. 0.4208 45.43 0.3748 0.6433 0.0849 0.0495 2.137 16.838 11.350 1593.742 1.902 50.484 3.230 0.51 193431. 0.3991 49.21 0.4060 0.6724 0.0817 0.0493 2.130 16.782 10.915 1588.437 1.896 48.549 3.117 0.51 193886. 0.3776 53.00 0.4373 0.6989 0.0781 0.0488 2.110 16.627 10.437 1573.693 1.878 46.422 3.008 0.51 194370. 0.3564 56.79 0.4685 0.7229 0.0742 0.0481 2.077 16.362 9.915 1548.654 1.849 44.102 2.904 0.51 194881. 0.3353 60.57 0.4997 0.7445 0.0700 0.0470 2.028 15.981 9.350 1512.625 1.806 41.589 2.804 0.51 195420. 0.3144 64.36 0.5310 0.7637 0.0654 0.0455 1.965 15.479 8.743 1465.059 1.749 38.887 2.707 0.51 195987. 0.2935 68.14 0.5622 0.7803 0.0606 0.0436 1.885 14.853 8.096 1405.786 1.678 36.009 2.612 0.52 196581. 0.2726 71.93 0.5934 0.7942 0.0555 0.0414 1.791 14.108 7.415 1335.331 1.594 32.983 2.519 0.52 197202. 0.2515 75.71 0.6246 0.8051 0.0502 0.0389 1.682 13.254 6.708 1254.440 1.497 29.837 2.425 0.52 197850. 0.2304 79.50 0.6559 0.8122 0.0447 0.0361 1.561 12.296 5.980 1163.833 1.389 26.597 2.330 0.52 198524. 0.2090 83.29 0.6871 0.8147 0.0392 0.0330 1.427 11.243 5.235 1064.181 1.270 23.286 2.231 0.52 199225. 0.1872 87.07 0.7183 0.8111 0.0335 0.0297 1.282 10.102 4.479 956.156 1.141 19.925 2.125 0.52 199951. 0.1649 90.86 0.7496 0.7991 0.0278 0.0261 1.127 8.880 3.717 840.480 1.003 16.535 2.006 0.52 200704. 0.1418 94.64 0.7808 0.7743 0.0221 0.0223 0.963 7.586 2.954 717.969 0.857 13.139 1.866 0.52 201483. 0.1176 98.43 0.8120 0.7284 0.0164 0.0183 0.791 6.229 2.194 589.576 0.704 9.760 1.688 0.52 202287. 0.0917 102.22 0.8433 0.6433 0.0108 0.0142 0.612 4.822 1.445 456.432 0.545 6.425 1.435 0.53 203117. 0.0633 106.00 0.8745 0.4685 0.0053 0.0099 0.429 3.379 0.711 319.865 0.382 3.163 1.008 0.53 203971. 0.0312 109.79 0.9057 -0.0001 0.0000 0.0056 0.243 1.915 0.000 181.244 0.216 0.000 0.000 0.53 204846. 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 0.1052 0.0402 2.473 17.319 17.803 1844.095 1.957 79.186 4.379 0.57 213752. 0.6775 4.26 0.0312 0.0792 0.1045 0.0412 2.534 17.747 17.686 1889.674 2.005 78.666 4.245 0.57 213930. 0.6547 8.52 0.0624 0.1534 0.1038 0.0422 2.598 18.191 17.552 1937.026 2.055 78.072 4.110 0.57 214129. 0.6315 12.77 0.0937 0.2226 0.1028 0.0433 2.663 18.646 17.399 1985.467 2.107 77.390 3.975 0.57 214352. 0.6080 17.03 0.1249 0.2867 0.1018 0.0443 2.728 19.104 17.222 2034.199 2.158 76.604 3.840 0.57 214599. 0.5844 21.29 0.1561 0.3460 0.1006 0.0454 2.792 19.555 17.019 2082.247 2.209 75.700 3.707 0.57 214873. 0.5609 25.55 0.1873 0.4006 0.0992 0.0464 2.854 19.989 16.785 2128.483 2.258 74.658 3.577 0.57 215173. 0.5374 29.81 0.2186 0.4507 0.0976 0.0473 2.912 20.395 16.516 2171.630 2.304 73.463 3.450 0.57 215502. 0.5141 34.06 0.2498 0.4967 0.0958 0.0482 2.964 20.758 16.209 2210.294 2.345 72.097 3.326 0.57 215861. 0.4911 38.32 0.2810 0.5388 0.0937 0.0489 3.008 21.065 15.859 2242.980 2.380 70.542 3.207 0.57 216249. 0.4684 42.58 0.3122 0.5772 0.0914 0.0494 3.042 21.301 15.464 2268.125 2.407 68.783 3.092 0.57 216668. 0.4460 46.84 0.3435 0.6124 0.0888 0.0498 3.063 21.451 15.019 2284.126 2.424 66.806 2.982 0.57 217118. 0.4239 51.09 0.3747 0.6445 0.0858 0.0499 3.070 21.501 14.523 2289.392 2.429 64.598 2.877 0.58 217600. 0.4021 55.35 0.4059 0.6738 0.0826 0.0498 3.061 21.435 13.972 2282.375 2.422 62.148 2.777 0.58 218112. 0.3806 59.61 0.4371 0.7005 0.0790 0.0493 3.033 21.240 13.365 2261.645 2.400 59.450 2.680 0.58 218657. 0.3594 63.87 0.4684 0.7247 0.0751 0.0485 2.985 20.905 12.702 2225.954 2.362 56.500 2.588 0.58 219233. 0.3383 68.13 0.4996 0.7466 0.0708 0.0474 2.916 20.420 11.983 2174.281 2.307 53.300 2.500 0.58 219840. 0.3173 72.38 0.5308 0.7661 0.0663 0.0459 2.824 19.777 11.208 2105.834 2.234 49.855 2.414 0.58 220478. 0.2964 76.64 0.5620 0.7831 0.0614 0.0440 2.709 18.974 10.382 2020.334 2.144 46.180 2.331 0.58 221146. 0.2754 80.90 0.5933 0.7976 0.0562 0.0418 2.573 18.017 9.512 1918.514 2.036 42.310 2.249 0.58 221845. 0.2544 85.16 0.6245 0.8090 0.0509 0.0393 2.416 16.918 8.607 1801.457 1.911 38.284 2.167 0.58 222574. 0.2332 89.42 0.6557 0.8169 0.0454 0.0364 2.240 15.686 7.674 1670.205 1.772 34.133 2.084 0.58 223333. 0.2117 93.67 0.6869 0.8203 0.0397 0.0333 2.046 14.329 6.720 1525.739 1.619 29.889 1.998 0.58 224122. 0.1899 97.93 0.7182 0.8179 0.0340 0.0298 1.836 12.857 5.750 1369.039 1.453 25.578 1.905 0.59 224939. 0.1675 102.19 0.7494 0.8074 0.0282 0.0262 1.611 11.281 4.773 1201.156 1.274 21.228 1.802 0.59 225786. 0.1444 106.45 0.7806 0.7844 0.0224 0.0223 1.372 9.610 3.792 1023.281 1.086 16.868 1.681 0.59 226662. 0.1200 110.71 0.8118 0.7410 0.0167 0.0182 1.122 7.859 2.817 836.809 0.888 12.529 1.527 0.59 227566. 0.0940 114.96 0.8431 0.6586 0.0110 0.0140 0.863 6.042 1.854 643.394 0.683 8.245 1.307 0.59 228500. 0.0652 119.22 0.8743 0.4854 0.0054 0.0097 0.597 4.179 0.911 444.992 0.472 4.053 0.929 0.59 229461. 0.0325 123.48 0.9055 -0.0026 0.0000 0.0053 0.327 2.288 -0.003 243.604 0.258 -0.012 -0.005 0.59 230445. 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 0.1059 0.0405 3.416 21.528 22.110 2547.022 2.432 98.345 3.937 0.63 237489. 0.6789 4.73 0.0312 0.0792 0.1052 0.0415 3.501 22.065 21.975 2610.590 2.493 97.744 3.818 0.63 237686. 0.6564 9.46 0.0624 0.1533 0.1045 0.0425 3.590 22.625 21.820 2676.820 2.556 97.053 3.697 0.63 237907. 0.6333 14.19 0.0936 0.2224 0.1036 0.0436 3.681 23.200 21.640 2744.776 2.621 96.256 3.576 0.63 238154. 0.6101 18.92 0.1248 0.2866 0.1026 0.0447 3.773 23.779 21.433 2813.331 2.687 95.332 3.455 0.64 238429. 0.5867 23.65 0.1561 0.3458 0.1015 0.0458 3.864 24.352 21.192 2881.122 2.751 94.262 3.336 0.64 238732. 0.5632 28.37 0.1873 0.4004 0.1001 0.0468 3.951 24.905 20.913 2946.542 2.814 93.021 3.219 0.64 239066. 0.5399 33.10 0.2185 0.4506 0.0986 0.0478 4.034 25.423 20.591 3007.785 2.872 91.588 3.105 0.64 239432. 0.5167 37.83 0.2497 0.4966 0.0968 0.0487 4.107 25.888 20.220 3062.872 2.925 89.939 2.994 0.64 239830. 0.4938 42.56 0.2809 0.5388 0.0948 0.0494 4.170 26.284 19.796 3109.672 2.970 88.054 2.887 0.64 240262. 0.4711 47.29 0.3121 0.5773 0.0925 0.0500 4.219 26.591 19.314 3145.970 3.004 85.910 2.785 0.64 240728. 0.4488 52.02 0.3433 0.6126 0.0899 0.0504 4.250 26.789 18.770 3169.498 3.027 83.489 2.686 0.64 241228. 0.4268 56.75 0.3745 0.6448 0.0870 0.0505 4.262 26.861 18.160 3177.987 3.035 80.774 2.592 0.64 241763. 0.4050 61.48 0.4058 0.6743 0.0837 0.0504 4.250 26.787 17.480 3169.251 3.026 77.753 2.502 0.64 242334. 0.3836 66.21 0.4370 0.7011 0.0801 0.0499 4.213 26.551 16.730 3141.261 3.000 74.415 2.416 0.64 242939. 0.3624 70.94 0.4682 0.7256 0.0762 0.0491 4.147 26.136 15.908 3092.248 2.953 70.757 2.333 0.64 243579. 0.3413 75.67 0.4994 0.7478 0.0719 0.0480 4.051 25.532 15.014 3020.777 2.885 66.781 2.254 0.64 244254. 0.3203 80.39 0.5306 0.7676 0.0673 0.0465 3.923 24.729 14.049 2925.733 2.794 62.491 2.178 0.64 244964. 0.2994 85.12 0.5618 0.7851 0.0623 0.0446 3.764 23.723 13.019 2806.685 2.680 57.907 2.104 0.64 245707. 0.2784 89.85 0.5930 0.8001 0.0571 0.0423 3.573 22.522 11.932 2664.615 2.545 53.074 2.031 0.65 246484. 0.2573 94.58 0.6242 0.8121 0.0517 0.0397 3.354 21.139 10.800 2501.035 2.388 48.038 1.959 0.65 247294. 0.2361 99.31 0.6555 0.8208 0.0461 0.0368 3.108 19.587 9.632 2317.418 2.213 42.843 1.885 0.65 248138. 0.2146 104.04 0.6867 0.8251 0.0404 0.0336 2.836 17.878 8.436 2115.140 2.020 37.524 1.809 0.65 249014. 0.1927 108.77 0.7179 0.8239 0.0346 0.0301 2.542 16.022 7.221 1895.588 1.810 32.118 1.728 0.65 249922. 0.1703 113.50 0.7491 0.8147 0.0287 0.0264 2.226 14.033 5.994 1660.243 1.585 26.659 1.637 0.65 250863. 0.1470 118.23 0.7803 0.7936 0.0228 0.0224 1.892 11.924 4.763 1410.783 1.347 21.184 1.531 0.65 251836. 0.1225 122.96 0.8115 0.7525 0.0169 0.0183 1.541 9.713 3.537 1149.177 1.097 15.733 1.396 0.66 252840. 0.0963 127.69 0.8427 0.6729 0.0111 0.0140 1.177 7.419 2.326 877.769 0.838 10.348 1.202 0.66 253877. 0.0672 132.41 0.8739 0.5015 0.0055 0.0095 0.804 5.066 1.141 599.336 0.572 5.077 0.864 0.66 254944. 0.0338 137.14 0.9051 -0.0065 0.0000 0.0050 0.425 2.677 -0.008 316.749 0.302 -0.034 -0.011 0.66 256036. 0.0000 PROP RPM = 11000 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 0.1065 0.0411 4.616 26.448 26.926 3442.082 2.988 119.765 3.548 0.70 261221. 0.6752 5.20 0.0312 0.0785 0.1060 0.0421 4.728 27.093 26.776 3526.022 3.061 119.098 3.444 0.70 261437. 0.6536 10.40 0.0624 0.1522 0.1053 0.0431 4.846 27.768 26.602 3613.792 3.137 118.327 3.339 0.70 261680. 0.6315 15.59 0.0936 0.2210 0.1045 0.0442 4.967 28.462 26.401 3704.193 3.216 117.430 3.233 0.70 261951. 0.6091 20.79 0.1248 0.2850 0.1035 0.0453 5.090 29.166 26.165 3795.776 3.295 116.384 3.127 0.70 262252. 0.5865 25.99 0.1559 0.3443 0.1025 0.0464 5.212 29.865 25.890 3886.755 3.374 115.160 3.021 0.70 262586. 0.5638 31.19 0.1871 0.3989 0.1012 0.0475 5.331 30.543 25.569 3975.003 3.451 113.731 2.918 0.70 262952. 0.5410 36.39 0.2183 0.4492 0.0997 0.0485 5.442 31.182 25.194 4058.094 3.523 112.065 2.816 0.70 263354. 0.5184 41.59 0.2495 0.4953 0.0980 0.0494 5.543 31.760 24.760 4133.325 3.588 110.134 2.717 0.70 263792. 0.4958 46.78 0.2807 0.5376 0.0960 0.0501 5.629 32.255 24.260 4197.779 3.644 107.908 2.621 0.70 264267. 0.4735 51.98 0.3119 0.5763 0.0937 0.0507 5.697 32.644 23.687 4248.372 3.688 105.361 2.529 0.70 264779. 0.4514 57.18 0.3431 0.6117 0.0912 0.0511 5.742 32.901 23.037 4281.896 3.717 102.467 2.440 0.70 265330. 0.4295 62.38 0.3743 0.6441 0.0883 0.0513 5.760 33.003 22.304 4295.142 3.729 99.207 2.355 0.70 265919. 0.4079 67.58 0.4055 0.6737 0.0850 0.0512 5.746 32.925 21.484 4284.971 3.720 95.563 2.274 0.70 266547. 0.3866 72.77 0.4366 0.7008 0.0814 0.0507 5.697 32.645 20.576 4248.501 3.688 91.521 2.197 0.70 267213. 0.3654 77.97 0.4678 0.7256 0.0775 0.0499 5.610 32.144 19.577 4183.279 3.632 87.078 2.123 0.71 267918. 0.3444 83.17 0.4990 0.7480 0.0732 0.0488 5.481 31.406 18.488 4087.330 3.548 82.234 2.052 0.71 268660. 0.3235 88.37 0.5302 0.7683 0.0685 0.0473 5.309 30.421 17.310 3959.129 3.437 76.997 1.983 0.71 269441. 0.3026 93.57 0.5614 0.7862 0.0635 0.0453 5.093 29.184 16.050 3798.031 3.297 71.389 1.917 0.71 270259. 0.2816 98.76 0.5926 0.8017 0.0582 0.0430 4.835 27.703 14.718 3605.303 3.130 65.464 1.852 0.71 271114. 0.2605 103.96 0.6238 0.8144 0.0527 0.0404 4.537 25.994 13.328 3383.000 2.937 59.281 1.787 0.71 272005. 0.2392 109.16 0.6550 0.8238 0.0471 0.0374 4.202 24.075 11.891 3133.134 2.720 52.893 1.721 0.71 272933. 0.2177 114.36 0.6862 0.8291 0.0412 0.0341 3.832 21.957 10.419 2857.607 2.481 46.346 1.654 0.71 273896. 0.1958 119.56 0.7173 0.8291 0.0353 0.0305 3.431 19.658 8.922 2558.326 2.221 39.684 1.582 0.72 274895. 0.1733 124.76 0.7485 0.8214 0.0293 0.0267 3.000 17.191 7.408 2237.342 1.942 32.951 1.502 0.72 275929. 0.1499 129.95 0.7797 0.8021 0.0233 0.0227 2.544 14.577 5.889 1897.076 1.647 26.193 1.408 0.72 276998. 0.1253 135.15 0.8109 0.7631 0.0173 0.0184 2.066 11.836 4.374 1540.415 1.337 19.457 1.288 0.72 278102. 0.0988 140.35 0.8421 0.6858 0.0114 0.0140 1.570 8.997 2.877 1170.897 1.016 12.799 1.115 0.72 279241. 0.0693 145.55 0.8733 0.5152 0.0056 0.0095 1.063 6.092 1.411 792.819 0.688 6.278 0.807 0.72 280414. 0.0352 150.75 0.9045 -0.0082 0.0000 0.0049 0.551 3.156 -0.011 410.702 0.357 -0.050 -0.012 0.73 281613. 0.0000 PROP RPM = 12000 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 0.1072 0.0429 6.251 32.835 32.254 4661.724 3.710 143.467 3.138 0.76 284948. 0.6536 5.66 0.0311 0.0758 0.1067 0.0438 6.391 33.570 32.095 4766.111 3.793 142.757 3.054 0.76 285182. 0.6346 11.33 0.0623 0.1474 0.1061 0.0448 6.538 34.339 31.909 4875.216 3.880 141.932 2.969 0.76 285446. 0.6150 16.99 0.0934 0.2147 0.1054 0.0459 6.688 35.130 31.692 4987.496 3.969 140.966 2.882 0.76 285740. 0.5950 22.65 0.1246 0.2776 0.1045 0.0469 6.841 35.930 31.436 5101.069 4.059 139.829 2.795 0.76 286068. 0.5747 28.31 0.1557 0.3362 0.1035 0.0480 6.992 36.722 31.134 5213.611 4.149 138.484 2.709 0.76 286431. 0.5542 33.98 0.1869 0.3907 0.1023 0.0490 7.137 37.489 30.777 5322.400 4.235 136.897 2.623 0.76 286830. 0.5336 39.64 0.2180 0.4411 0.1009 0.0499 7.274 38.206 30.357 5424.307 4.317 135.027 2.538 0.76 287267. 0.5129 45.30 0.2492 0.4877 0.0993 0.0507 7.397 38.852 29.864 5515.924 4.389 132.836 2.456 0.76 287744. 0.4921 50.97 0.2803 0.5307 0.0974 0.0514 7.501 39.399 29.291 5593.604 4.451 130.286 2.375 0.76 288261. 0.4714 56.63 0.3115 0.5702 0.0952 0.0520 7.582 39.821 28.629 5653.528 4.499 127.342 2.297 0.77 288820. 0.4507 62.29 0.3426 0.6065 0.0927 0.0523 7.633 40.090 27.871 5691.761 4.529 123.971 2.221 0.77 289420. 0.4300 67.95 0.3738 0.6398 0.0898 0.0525 7.650 40.178 27.011 5704.294 4.539 120.146 2.148 0.77 290062. 0.4094 73.62 0.4049 0.6704 0.0866 0.0523 7.627 40.058 26.044 5687.147 4.526 115.843 2.077 0.77 290747. 0.3887 79.28 0.4360 0.6983 0.0830 0.0518 7.559 39.701 24.966 5636.501 4.485 111.048 2.009 0.77 291473. 0.3681 84.94 0.4672 0.7237 0.0791 0.0510 7.441 39.084 23.775 5548.871 4.416 105.751 1.943 0.77 292242. 0.3475 90.61 0.4983 0.7468 0.0747 0.0499 7.270 38.185 22.472 5421.337 4.314 99.955 1.880 0.77 293052. 0.3268 96.27 0.5295 0.7676 0.0700 0.0483 7.042 36.989 21.059 5251.539 4.179 93.669 1.819 0.77 293903. 0.3061 101.93 0.5606 0.7861 0.0650 0.0463 6.756 35.487 19.541 5038.186 4.009 86.918 1.759 0.77 294795. 0.2852 107.60 0.5918 0.8023 0.0596 0.0440 6.413 33.686 17.933 4782.534 3.806 79.768 1.701 0.77 295727. 0.2641 113.26 0.6229 0.8157 0.0540 0.0413 6.017 31.606 16.252 4487.190 3.571 72.290 1.643 0.78 296698. 0.2429 118.92 0.6541 0.8259 0.0483 0.0382 5.572 29.266 14.512 4154.980 3.306 64.549 1.584 0.78 297709. 0.2213 124.58 0.6852 0.8321 0.0423 0.0348 5.081 26.686 12.726 3788.719 3.015 56.603 1.523 0.78 298759. 0.1993 130.25 0.7164 0.8328 0.0363 0.0312 4.548 23.887 10.905 3391.352 2.699 48.505 1.458 0.78 299847. 0.1766 135.91 0.7475 0.8256 0.0301 0.0273 3.978 20.893 9.062 2966.230 2.360 40.309 1.386 0.78 300974. 0.1530 141.57 0.7787 0.8063 0.0240 0.0232 3.376 17.731 7.210 2517.307 2.003 32.069 1.299 0.78 302138. 0.1279 147.24 0.8098 0.7658 0.0178 0.0188 2.748 14.435 5.361 2049.420 1.631 23.844 1.186 0.79 303340. 0.1007 152.90 0.8409 0.6842 0.0117 0.0144 2.103 11.047 3.530 1568.396 1.248 15.700 1.021 0.79 304580. 0.0703 158.56 0.8721 0.5054 0.0058 0.0099 1.450 7.615 1.733 1081.141 0.860 7.708 0.727 0.79 305856. 0.0351 164.22 0.9032 -0.0075 0.0000 0.0055 0.798 4.189 -0.014 594.746 0.473 -0.060 -0.010 0.79 307162. 0.0000 PROP RPM = 13000 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 0.1079 0.0469 8.702 42.190 38.082 6488.995 4.767 169.387 2.662 0.83 308668. 0.6024 6.13 0.0311 0.0699 0.1074 0.0478 8.869 43.002 37.919 6613.944 4.858 168.665 2.600 0.83 308920. 0.5872 12.26 0.0622 0.1364 0.1069 0.0488 9.044 43.847 37.730 6743.862 4.954 167.822 2.538 0.83 309205. 0.5716 18.39 0.0934 0.1995 0.1063 0.0497 9.222 44.709 37.506 6876.543 5.051 166.827 2.474 0.83 309523. 0.5556 24.52 0.1245 0.2590 0.1055 0.0507 9.400 45.573 37.240 7009.344 5.149 165.642 2.410 0.83 309876. 0.5393 30.65 0.1556 0.3152 0.1046 0.0516 9.574 46.416 36.921 7139.026 5.244 164.226 2.346 0.83 310268. 0.5227 36.78 0.1867 0.3680 0.1035 0.0525 9.738 47.214 36.540 7261.827 5.334 162.532 2.282 0.83 310699. 0.5059 42.91 0.2179 0.4176 0.1022 0.0533 9.888 47.941 36.086 7373.538 5.416 160.509 2.220 0.83 311172. 0.4890 49.04 0.2490 0.4640 0.1007 0.0540 10.017 48.566 35.545 7469.672 5.487 158.106 2.158 0.83 311688. 0.4719 55.17 0.2801 0.5075 0.0989 0.0546 10.119 49.059 34.909 7545.611 5.543 155.273 2.098 0.83 312248. 0.4547 61.30 0.3112 0.5482 0.0968 0.0550 10.187 49.391 34.164 7596.669 5.580 151.962 2.040 0.83 312853. 0.4372 67.43 0.3423 0.5861 0.0944 0.0551 10.216 49.533 33.303 7618.419 5.596 148.131 1.983 0.83 313503. 0.4196 73.56 0.3735 0.6214 0.0916 0.0550 10.200 49.455 32.316 7606.452 5.587 143.743 1.927 0.83 314200. 0.4017 79.69 0.4046 0.6542 0.0884 0.0547 10.133 49.130 31.197 7556.485 5.551 138.766 1.873 0.83 314942. 0.3836 85.82 0.4357 0.6845 0.0848 0.0540 10.010 48.531 29.942 7464.382 5.483 133.180 1.819 0.83 315730. 0.3651 91.95 0.4668 0.7124 0.0809 0.0530 9.825 47.634 28.546 7326.405 5.382 126.973 1.767 0.83 316563. 0.3463 98.08 0.4980 0.7379 0.0765 0.0516 9.574 46.417 27.011 7139.246 5.244 120.146 1.716 0.84 317442. 0.3271 104.21 0.5291 0.7610 0.0718 0.0499 9.253 44.863 25.339 6900.175 5.069 112.708 1.666 0.84 318365. 0.3075 110.34 0.5602 0.7815 0.0667 0.0478 8.861 42.961 23.536 6607.559 4.854 104.689 1.616 0.84 319332. 0.2874 116.47 0.5913 0.7995 0.0613 0.0453 8.399 40.719 21.620 6262.773 4.600 96.165 1.566 0.84 320343. 0.2670 122.60 0.6224 0.8142 0.0556 0.0425 7.874 38.175 19.610 5871.590 4.313 87.224 1.515 0.84 321397. 0.2460 128.73 0.6536 0.8249 0.0496 0.0393 7.292 35.354 17.524 5437.652 3.994 77.945 1.462 0.84 322492. 0.2244 134.86 0.6847 0.8306 0.0436 0.0359 6.658 32.281 15.378 4965.058 3.647 68.400 1.405 0.84 323630. 0.2020 140.99 0.7158 0.8296 0.0374 0.0322 5.976 28.974 13.187 4456.355 3.273 58.655 1.342 0.85 324808. 0.1787 147.12 0.7469 0.8189 0.0311 0.0283 5.253 25.469 10.965 3917.236 2.877 48.774 1.270 0.85 326028. 0.1542 153.25 0.7781 0.7929 0.0247 0.0243 4.499 21.810 8.729 3354.549 2.464 38.825 1.180 0.85 327289. 0.1279 159.38 0.8092 0.7411 0.0184 0.0201 3.723 18.052 6.493 2776.492 2.040 28.879 1.061 0.85 328590. 0.0991 165.52 0.8403 0.6418 0.0121 0.0159 2.940 14.255 4.276 2192.439 1.610 19.018 0.885 0.85 329932. 0.0671 171.65 0.8714 0.4441 0.0059 0.0117 2.163 10.486 2.099 1612.803 1.185 9.335 0.590 0.86 331314. 0.0314 177.78 0.9026 -0.0063 -0.0001 0.0076 1.404 6.808 -0.019 1047.073 0.769 -0.083 -0.008 0.86 332728. 0.0000 PROP RPM = 14000 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 0.1078 0.0532 12.308 55.413 44.147 9178.418 6.261 196.364 2.182 0.89 332408. 0.5316 6.62 0.0312 0.0620 0.1075 0.0541 12.520 56.367 43.993 9336.507 6.368 195.682 2.137 0.89 332677. 0.5199 13.24 0.0624 0.1214 0.1070 0.0550 12.740 57.357 43.814 9500.390 6.480 194.883 2.092 0.89 332981. 0.5078 19.86 0.0936 0.1781 0.1065 0.0560 12.963 58.361 43.600 9666.680 6.594 193.931 2.046 0.89 333321. 0.4954 26.47 0.1248 0.2321 0.1059 0.0569 13.184 59.354 43.341 9831.186 6.706 192.783 2.000 0.89 333700. 0.4828 33.09 0.1560 0.2835 0.1051 0.0579 13.395 60.305 43.028 9988.762 6.813 191.387 1.954 0.89 334120. 0.4700 39.71 0.1872 0.3323 0.1042 0.0587 13.589 61.179 42.645 10133.444 6.912 189.685 1.909 0.89 334583. 0.4571 46.33 0.2184 0.3788 0.1030 0.0594 13.757 61.935 42.179 10258.625 6.997 187.613 1.865 0.89 335092. 0.4442 52.95 0.2496 0.4230 0.1017 0.0600 13.890 62.531 41.615 10357.489 7.065 185.105 1.822 0.89 335648. 0.4311 59.57 0.2808 0.4652 0.1000 0.0604 13.978 62.929 40.938 10423.325 7.110 182.092 1.781 0.89 336252. 0.4180 66.19 0.3120 0.5054 0.0980 0.0605 14.013 63.087 40.132 10449.443 7.127 178.509 1.742 0.89 336905. 0.4047 72.80 0.3432 0.5439 0.0957 0.0604 13.987 62.970 39.185 10430.149 7.114 174.294 1.704 0.89 337608. 0.3912 79.42 0.3744 0.5805 0.0930 0.0600 13.895 62.555 38.085 10361.400 7.067 169.400 1.667 0.89 338362. 0.3773 86.04 0.4056 0.6153 0.0900 0.0593 13.731 61.815 36.822 10238.853 6.984 163.785 1.631 0.90 339165. 0.3630 92.66 0.4368 0.6483 0.0865 0.0583 13.489 60.728 35.390 10058.776 6.861 157.417 1.596 0.90 340019. 0.3482 99.28 0.4680 0.6793 0.0825 0.0569 13.166 59.275 33.785 9818.160 6.697 150.277 1.561 0.90 340923. 0.3327 105.90 0.4992 0.7083 0.0782 0.0551 12.760 57.444 32.007 9514.900 6.490 142.366 1.526 0.90 341876. 0.3166 112.52 0.5304 0.7351 0.0734 0.0530 12.267 55.227 30.057 9147.564 6.239 133.694 1.490 0.90 342877. 0.2996 119.13 0.5616 0.7595 0.0683 0.0505 11.688 52.620 27.945 8715.729 5.945 124.300 1.454 0.90 343926. 0.2819 125.75 0.5928 0.7813 0.0628 0.0476 11.026 49.640 25.691 8222.277 5.608 114.274 1.417 0.90 345022. 0.2634 132.37 0.6240 0.7997 0.0570 0.0445 10.292 46.335 23.319 7674.802 5.235 103.722 1.378 0.91 346164. 0.2440 138.99 0.6552 0.8126 0.0509 0.0411 9.509 42.809 20.848 7090.768 4.837 92.734 1.334 0.91 347351. 0.2233 145.61 0.6864 0.8180 0.0447 0.0375 8.687 39.107 18.300 6477.620 4.418 81.398 1.281 0.91 348584. 0.2010 152.23 0.7176 0.8102 0.0383 0.0339 7.860 35.384 15.688 5860.939 3.998 69.780 1.214 0.91 349861. 0.1763 158.85 0.7488 0.7892 0.0319 0.0302 6.998 31.504 13.038 5218.210 3.559 57.994 1.133 0.91 351182. 0.1501 165.46 0.7800 0.7477 0.0253 0.0264 6.119 27.546 10.370 4562.705 3.112 46.124 1.031 0.92 352548. 0.1217 172.08 0.8112 0.6751 0.0188 0.0226 5.237 23.577 7.704 3905.280 2.664 34.269 0.895 0.92 353956. 0.0911 178.70 0.8425 0.5525 0.0124 0.0189 4.372 19.681 5.069 3259.902 2.224 22.547 0.705 0.92 355409. 0.0582 185.32 0.8737 0.3482 0.0061 0.0153 3.539 15.933 2.494 2639.026 1.800 11.091 0.429 0.92 356904. 0.0248 191.94 0.9049 0.0008 0.0000 0.0119 2.750 12.380 0.004 2050.501 1.399 0.020 0.001 0.92 358441. 0.0000 PROP RPM = 15000 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 0.1056 0.0583 16.600 69.751 49.640 12378.463 7.880 220.798 1.819 0.95 356221. 0.4700 7.18 0.0316 0.0562 0.1053 0.0592 16.864 70.859 49.495 12575.199 8.006 220.156 1.785 0.95 356509. 0.4606 14.35 0.0631 0.1101 0.1050 0.0602 17.144 72.037 49.329 12784.180 8.139 219.414 1.750 0.95 356834. 0.4508 21.53 0.0947 0.1617 0.1046 0.0612 17.436 73.263 49.132 13001.893 8.277 218.538 1.714 0.95 357198. 0.4406 28.70 0.1263 0.2110 0.1040 0.0623 17.733 74.513 48.895 13223.628 8.418 217.483 1.677 0.95 357604. 0.4301 35.88 0.1579 0.2579 0.1034 0.0633 18.028 75.750 48.605 13443.227 8.558 216.193 1.640 0.95 358055. 0.4193 43.05 0.1894 0.3025 0.1027 0.0643 18.309 76.932 48.248 13652.884 8.692 214.605 1.603 0.95 358553. 0.4083 50.23 0.2210 0.3449 0.1017 0.0652 18.564 78.004 47.807 13843.257 8.813 212.645 1.566 0.95 359100. 0.3972 57.40 0.2526 0.3852 0.1006 0.0659 18.779 78.908 47.264 14003.580 8.915 210.230 1.531 0.96 359699. 0.3860 64.58 0.2841 0.4237 0.0992 0.0665 18.938 79.575 46.599 14122.028 8.990 207.272 1.497 0.96 360351. 0.3747 71.75 0.3157 0.4605 0.0974 0.0668 19.024 79.936 45.791 14186.141 9.031 203.680 1.464 0.96 361057. 0.3633 78.93 0.3473 0.4959 0.0954 0.0668 19.021 79.922 44.821 14183.603 9.030 199.364 1.433 0.96 361819. 0.3519 86.10 0.3788 0.5301 0.0929 0.0664 18.913 79.469 43.669 14103.160 8.978 194.238 1.404 0.96 362638. 0.3403 93.28 0.4104 0.5632 0.0901 0.0656 18.688 78.525 42.317 13935.564 8.872 188.228 1.377 0.96 363512. 0.3286 100.45 0.4420 0.5953 0.0867 0.0644 18.337 77.052 40.754 13674.208 8.705 181.276 1.352 0.96 364443. 0.3165 107.63 0.4736 0.6263 0.0829 0.0627 17.856 75.030 38.971 13315.475 8.477 173.345 1.327 0.96 365430. 0.3039 114.80 0.5051 0.6562 0.0787 0.0605 17.242 72.451 36.964 12857.648 8.185 164.415 1.304 0.96 366471. 0.2907 121.98 0.5367 0.6847 0.0739 0.0579 16.500 69.331 34.736 12304.059 7.833 154.506 1.280 0.97 367567. 0.2768 129.15 0.5683 0.7114 0.0687 0.0549 15.636 65.700 32.301 11659.674 7.423 143.673 1.257 0.97 368715. 0.2619 136.33 0.5998 0.7360 0.0632 0.0515 14.662 61.609 29.684 10933.598 6.961 132.037 1.231 0.97 369916. 0.2460 143.50 0.6314 0.7578 0.0573 0.0477 13.592 57.114 26.919 10135.824 6.453 119.736 1.205 0.97 371167. 0.2292 150.68 0.6630 0.7738 0.0511 0.0438 12.476 52.422 24.029 9303.162 5.923 106.880 1.172 0.97 372469. 0.2106 157.85 0.6945 0.7804 0.0448 0.0398 11.347 47.679 21.039 8461.528 5.387 93.580 1.128 0.97 373819. 0.1897 165.03 0.7261 0.7621 0.0382 0.0364 10.366 43.556 17.953 7729.792 4.921 79.854 1.053 0.98 375218. 0.1637 172.20 0.7577 0.7221 0.0315 0.0331 9.424 39.598 14.820 7027.371 4.474 65.921 0.957 0.98 376665. 0.1350 179.38 0.7893 0.6580 0.0249 0.0298 8.492 35.684 11.683 6332.818 4.032 51.965 0.837 0.98 378160. 0.1049 186.55 0.8208 0.5621 0.0183 0.0267 7.595 31.914 8.582 5663.759 3.606 38.172 0.687 0.98 379703. 0.0738 193.73 0.8524 0.4262 0.0118 0.0237 6.745 28.340 5.565 5029.504 3.202 24.751 0.502 0.99 381294. 0.0434 200.90 0.8840 0.2408 0.0057 0.0209 5.954 25.019 2.676 4440.032 2.827 11.903 0.273 0.99 382938. 0.0164 208.08 0.9155 -0.0086 -0.0002 0.0183 5.213 21.903 -0.081 3887.141 2.475 -0.361 -0.009 0.99 384681. 0.0000