16x7E(3D) (16x7E(3D).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 0.0776 0.0295 0.002 0.157 0.162 1.857 0.018 0.721 39.571 0.06 24326. 0.5842 0.30 0.0198 0.0509 0.0762 0.0297 0.003 0.158 0.159 1.867 0.018 0.708 38.641 0.06 24339. 0.5652 0.60 0.0397 0.0994 0.0746 0.0298 0.003 0.159 0.156 1.875 0.018 0.693 37.705 0.06 24353. 0.5460 0.90 0.0595 0.1453 0.0730 0.0299 0.003 0.159 0.153 1.882 0.018 0.679 36.766 0.06 24367. 0.5266 1.20 0.0794 0.1888 0.0713 0.0300 0.003 0.159 0.149 1.886 0.018 0.663 35.824 0.06 24383. 0.5071 1.50 0.0992 0.2298 0.0695 0.0300 0.003 0.160 0.145 1.889 0.018 0.646 34.880 0.06 24399. 0.4875 1.80 0.1190 0.2683 0.0676 0.0300 0.003 0.160 0.141 1.888 0.018 0.628 33.934 0.06 24417. 0.4677 2.10 0.1389 0.3043 0.0656 0.0300 0.003 0.159 0.137 1.885 0.018 0.610 32.985 0.06 24436. 0.4479 2.40 0.1587 0.3377 0.0635 0.0299 0.003 0.159 0.133 1.879 0.018 0.590 32.033 0.06 24456. 0.4279 2.71 0.1785 0.3685 0.0613 0.0297 0.003 0.158 0.128 1.869 0.018 0.570 31.076 0.06 24476. 0.4078 3.01 0.1984 0.3968 0.0590 0.0295 0.002 0.157 0.123 1.855 0.018 0.548 30.112 0.06 24499. 0.3876 3.31 0.2182 0.4224 0.0565 0.0292 0.002 0.155 0.118 1.838 0.018 0.525 29.139 0.06 24522. 0.3672 3.61 0.2381 0.4452 0.0540 0.0289 0.002 0.154 0.113 1.817 0.017 0.502 28.154 0.06 24546. 0.3467 3.91 0.2579 0.4651 0.0513 0.0285 0.002 0.151 0.107 1.791 0.017 0.477 27.153 0.06 24572. 0.3261 4.21 0.2777 0.4821 0.0486 0.0280 0.002 0.149 0.101 1.761 0.017 0.451 26.131 0.06 24599. 0.3052 4.51 0.2976 0.4958 0.0457 0.0274 0.002 0.146 0.095 1.727 0.016 0.425 25.081 0.06 24627. 0.2842 4.81 0.3174 0.5060 0.0428 0.0268 0.002 0.143 0.089 1.687 0.016 0.397 24.000 0.06 24657. 0.2630 5.11 0.3372 0.5125 0.0397 0.0261 0.002 0.139 0.083 1.644 0.016 0.369 22.878 0.06 24688. 0.2416 5.41 0.3571 0.5149 0.0366 0.0254 0.002 0.135 0.076 1.596 0.015 0.340 21.707 0.06 24720. 0.2200 5.71 0.3769 0.5127 0.0334 0.0245 0.002 0.131 0.070 1.545 0.015 0.310 20.477 0.06 24753. 0.1983 6.01 0.3968 0.5054 0.0301 0.0237 0.002 0.126 0.063 1.489 0.014 0.280 19.177 0.06 24788. 0.1764 6.31 0.4166 0.4923 0.0268 0.0227 0.002 0.121 0.056 1.429 0.014 0.249 17.790 0.06 24824. 0.1544 6.61 0.4364 0.4725 0.0235 0.0217 0.002 0.115 0.049 1.365 0.013 0.218 16.298 0.06 24862. 0.1324 6.91 0.4563 0.4449 0.0201 0.0206 0.002 0.110 0.042 1.297 0.012 0.187 14.679 0.06 24900. 0.1103 7.21 0.4761 0.4080 0.0167 0.0195 0.002 0.104 0.035 1.225 0.012 0.155 12.902 0.06 24941. 0.0883 7.51 0.4960 0.3601 0.0133 0.0183 0.002 0.097 0.028 1.150 0.011 0.123 10.931 0.06 24982. 0.0667 7.82 0.5158 0.2986 0.0099 0.0170 0.001 0.091 0.021 1.072 0.010 0.092 8.717 0.06 25025. 0.0459 8.12 0.5356 0.2204 0.0065 0.0158 0.001 0.084 0.014 0.991 0.009 0.060 6.194 0.06 25070. 0.0264 8.42 0.5555 0.1208 0.0031 0.0144 0.001 0.077 0.007 0.908 0.009 0.029 3.275 0.06 25115. 0.0097 8.72 0.5753 -0.0067 -0.0002 0.0131 0.001 0.069 0.000 0.822 0.008 -0.001 -0.175 0.06 25162. 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 0.0779 0.0267 0.018 0.568 0.651 13.452 0.064 2.894 21.937 0.13 48652. 0.6489 0.62 0.0203 0.0577 0.0764 0.0269 0.018 0.572 0.638 13.545 0.065 2.840 21.378 0.13 48679. 0.6264 1.23 0.0406 0.1123 0.0749 0.0271 0.018 0.576 0.625 13.626 0.065 2.782 20.819 0.13 48707. 0.6038 1.85 0.0609 0.1640 0.0732 0.0272 0.018 0.579 0.612 13.692 0.065 2.721 20.263 0.13 48737. 0.5812 2.46 0.0812 0.2126 0.0715 0.0273 0.018 0.581 0.597 13.741 0.066 2.656 19.709 0.13 48769. 0.5585 3.08 0.1015 0.2584 0.0696 0.0274 0.018 0.582 0.582 13.769 0.066 2.587 19.159 0.13 48803. 0.5358 3.69 0.1218 0.3012 0.0677 0.0274 0.018 0.582 0.565 13.775 0.066 2.514 18.612 0.13 48839. 0.5132 4.31 0.1421 0.3412 0.0656 0.0273 0.018 0.581 0.548 13.756 0.066 2.438 18.069 0.13 48878. 0.4905 4.92 0.1624 0.3782 0.0634 0.0272 0.018 0.579 0.530 13.710 0.065 2.357 17.528 0.13 48919. 0.4679 5.54 0.1827 0.4124 0.0611 0.0271 0.018 0.576 0.511 13.633 0.065 2.271 16.990 0.13 48962. 0.4453 6.15 0.2030 0.4438 0.0587 0.0269 0.018 0.572 0.491 13.524 0.065 2.182 16.453 0.13 49008. 0.4226 6.77 0.2233 0.4722 0.0562 0.0266 0.018 0.565 0.470 13.380 0.064 2.088 15.916 0.13 49056. 0.4000 7.38 0.2436 0.4977 0.0536 0.0262 0.018 0.558 0.448 13.199 0.063 1.991 15.378 0.13 49107. 0.3773 8.00 0.2640 0.5202 0.0508 0.0258 0.017 0.549 0.425 12.980 0.062 1.888 14.835 0.13 49160. 0.3545 8.61 0.2843 0.5395 0.0480 0.0253 0.017 0.538 0.401 12.721 0.061 1.782 14.286 0.13 49216. 0.3316 9.23 0.3046 0.5554 0.0450 0.0247 0.017 0.525 0.376 12.420 0.059 1.672 13.726 0.13 49275. 0.3086 9.84 0.3249 0.5677 0.0419 0.0240 0.016 0.510 0.350 12.079 0.058 1.558 13.153 0.13 49336. 0.2855 10.46 0.3452 0.5760 0.0388 0.0232 0.016 0.494 0.324 11.698 0.056 1.441 12.562 0.13 49401. 0.2622 11.07 0.3655 0.5801 0.0356 0.0224 0.015 0.477 0.297 11.278 0.054 1.321 11.948 0.13 49467. 0.2388 11.69 0.3858 0.5793 0.0323 0.0215 0.015 0.457 0.270 10.819 0.052 1.199 11.303 0.13 49537. 0.2152 12.31 0.4061 0.5728 0.0289 0.0205 0.014 0.436 0.242 10.322 0.049 1.075 10.619 0.13 49610. 0.1914 12.92 0.4264 0.5599 0.0255 0.0194 0.013 0.414 0.213 9.787 0.047 0.949 9.885 0.13 49685. 0.1674 13.54 0.4467 0.5392 0.0221 0.0183 0.012 0.389 0.185 9.215 0.044 0.821 9.086 0.13 49763. 0.1432 14.15 0.4670 0.5089 0.0186 0.0171 0.012 0.364 0.156 8.608 0.041 0.693 8.204 0.13 49844. 0.1187 14.77 0.4873 0.4669 0.0152 0.0158 0.011 0.337 0.127 7.967 0.038 0.563 7.212 0.13 49928. 0.0941 15.38 0.5076 0.4096 0.0117 0.0145 0.010 0.308 0.098 7.295 0.035 0.435 6.074 0.13 50015. 0.0696 16.00 0.5279 0.3321 0.0082 0.0131 0.009 0.279 0.069 6.595 0.031 0.306 4.736 0.13 50105. 0.0456 16.61 0.5482 0.2270 0.0048 0.0117 0.008 0.248 0.040 5.869 0.028 0.179 3.118 0.13 50197. 0.0230 17.23 0.5685 0.0822 0.0015 0.0102 0.007 0.216 0.012 5.122 0.024 0.055 1.089 0.13 50292. 0.0044 17.84 0.5888 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 0.0782 0.0255 0.058 1.223 1.469 43.396 0.138 6.535 15.355 0.19 72978. 0.6825 0.91 0.0200 0.0595 0.0767 0.0257 0.059 1.232 1.442 43.727 0.139 6.415 14.959 0.19 73016. 0.6588 1.82 0.0399 0.1159 0.0752 0.0259 0.059 1.240 1.413 44.017 0.140 6.287 14.565 0.19 73057. 0.6351 2.72 0.0599 0.1692 0.0736 0.0261 0.059 1.247 1.383 44.258 0.141 6.152 14.174 0.19 73101. 0.6113 3.63 0.0799 0.2194 0.0719 0.0262 0.060 1.252 1.351 44.441 0.141 6.009 13.787 0.19 73149. 0.5877 4.54 0.0998 0.2666 0.0701 0.0262 0.060 1.255 1.317 44.559 0.142 5.857 13.403 0.19 73199. 0.5640 5.45 0.1198 0.3109 0.0681 0.0263 0.060 1.257 1.281 44.603 0.142 5.697 13.024 0.19 73252. 0.5405 6.35 0.1398 0.3523 0.0661 0.0262 0.060 1.256 1.243 44.565 0.142 5.527 12.648 0.19 73309. 0.5171 7.26 0.1597 0.3907 0.0640 0.0262 0.060 1.252 1.203 44.435 0.141 5.349 12.276 0.19 73369. 0.4937 8.17 0.1797 0.4264 0.0617 0.0260 0.059 1.245 1.160 44.206 0.141 5.162 11.907 0.19 73432. 0.4704 9.08 0.1997 0.4592 0.0594 0.0258 0.059 1.236 1.116 43.869 0.140 4.965 11.541 0.19 73499. 0.4472 9.98 0.2196 0.4892 0.0569 0.0256 0.058 1.223 1.070 43.418 0.138 4.759 11.177 0.19 73570. 0.4240 10.89 0.2396 0.5163 0.0543 0.0252 0.057 1.207 1.022 42.846 0.136 4.544 10.814 0.19 73644. 0.4008 11.80 0.2596 0.5406 0.0517 0.0248 0.057 1.187 0.971 42.145 0.134 4.320 10.451 0.19 73722. 0.3777 12.71 0.2795 0.5618 0.0489 0.0243 0.055 1.164 0.919 41.307 0.131 4.086 10.086 0.19 73804. 0.3545 13.61 0.2995 0.5800 0.0460 0.0237 0.054 1.136 0.864 40.331 0.128 3.843 9.717 0.19 73890. 0.3313 14.52 0.3195 0.5948 0.0430 0.0231 0.053 1.105 0.808 39.218 0.125 3.593 9.343 0.19 73979. 0.3079 15.43 0.3394 0.6060 0.0399 0.0223 0.051 1.070 0.750 37.969 0.121 3.336 8.959 0.19 74073. 0.2845 16.34 0.3594 0.6133 0.0367 0.0215 0.049 1.031 0.691 36.586 0.116 3.072 8.563 0.19 74170. 0.2610 17.24 0.3794 0.6162 0.0335 0.0206 0.047 0.988 0.630 35.069 0.112 2.803 8.151 0.19 74272. 0.2373 18.15 0.3993 0.6141 0.0302 0.0197 0.045 0.942 0.569 33.420 0.106 2.529 7.717 0.19 74378. 0.2134 19.06 0.4193 0.6061 0.0269 0.0186 0.042 0.891 0.506 31.640 0.101 2.251 7.254 0.19 74487. 0.1892 19.97 0.4393 0.5912 0.0236 0.0175 0.040 0.838 0.443 29.734 0.095 1.969 6.754 0.19 74601. 0.1648 20.87 0.4592 0.5678 0.0202 0.0163 0.037 0.781 0.379 27.703 0.088 1.686 6.204 0.19 74719. 0.1401 21.78 0.4792 0.5336 0.0167 0.0150 0.034 0.720 0.315 25.555 0.081 1.400 5.587 0.19 74841. 0.1150 22.69 0.4992 0.4854 0.0133 0.0137 0.031 0.656 0.251 23.295 0.074 1.115 4.880 0.19 74968. 0.0896 23.60 0.5191 0.4184 0.0099 0.0123 0.028 0.590 0.187 20.934 0.067 0.830 4.045 0.19 75098. 0.0641 24.50 0.5391 0.3250 0.0066 0.0109 0.025 0.521 0.123 18.481 0.059 0.548 3.026 0.19 75233. 0.0390 25.41 0.5591 0.1927 0.0032 0.0094 0.021 0.449 0.061 15.950 0.051 0.270 1.729 0.19 75372. 0.0156 26.32 0.5790 -0.0029 0.0000 0.0079 0.018 0.376 -0.001 13.342 0.042 -0.003 -0.025 0.19 75511. 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 0.0785 0.0249 0.135 2.120 2.623 100.312 0.239 11.667 11.860 0.25 97301. 0.7044 1.21 0.0200 0.0613 0.0771 0.0251 0.136 2.137 2.575 101.126 0.241 11.453 11.549 0.25 97353. 0.6796 2.42 0.0400 0.1194 0.0755 0.0253 0.137 2.152 2.524 101.842 0.243 11.226 11.240 0.25 97408. 0.6549 3.63 0.0600 0.1742 0.0739 0.0254 0.137 2.165 2.470 102.439 0.245 10.985 10.935 0.25 97467. 0.6302 4.85 0.0800 0.2259 0.0722 0.0256 0.138 2.174 2.412 102.899 0.246 10.729 10.632 0.25 97530. 0.6056 6.06 0.0999 0.2744 0.0704 0.0256 0.138 2.181 2.351 103.201 0.246 10.458 10.334 0.25 97597. 0.5811 7.27 0.1199 0.3199 0.0684 0.0257 0.139 2.183 2.287 103.325 0.247 10.172 10.039 0.25 97668. 0.5568 8.48 0.1399 0.3624 0.0664 0.0256 0.138 2.182 2.219 103.249 0.246 9.870 9.748 0.25 97744. 0.5325 9.69 0.1599 0.4019 0.0643 0.0256 0.138 2.175 2.147 102.953 0.246 9.552 9.461 0.25 97824. 0.5084 10.90 0.1799 0.4386 0.0620 0.0254 0.137 2.164 2.072 102.417 0.245 9.217 9.177 0.25 97909. 0.4845 12.11 0.1999 0.4725 0.0596 0.0252 0.136 2.147 1.993 101.622 0.243 8.866 8.896 0.25 97999. 0.4606 13.33 0.2199 0.5034 0.0572 0.0250 0.135 2.125 1.911 100.549 0.240 8.498 8.618 0.25 98093. 0.4369 14.54 0.2399 0.5316 0.0546 0.0246 0.133 2.096 1.824 99.182 0.237 8.114 8.342 0.25 98193. 0.4132 15.75 0.2598 0.5569 0.0519 0.0242 0.131 2.060 1.734 97.502 0.233 7.713 8.066 0.25 98297. 0.3895 16.96 0.2798 0.5792 0.0491 0.0237 0.128 2.018 1.640 95.491 0.228 7.295 7.790 0.25 98406. 0.3659 18.17 0.2998 0.5984 0.0462 0.0231 0.125 1.968 1.543 93.144 0.222 6.862 7.512 0.26 98521. 0.3422 19.38 0.3198 0.6144 0.0432 0.0225 0.121 1.912 1.442 90.462 0.216 6.415 7.231 0.26 98641. 0.3185 20.59 0.3398 0.6269 0.0401 0.0217 0.117 1.848 1.339 87.449 0.209 5.955 6.944 0.26 98766. 0.2947 21.80 0.3598 0.6356 0.0369 0.0209 0.113 1.777 1.233 84.108 0.201 5.484 6.649 0.26 98896. 0.2708 23.02 0.3798 0.6400 0.0337 0.0200 0.108 1.700 1.125 80.439 0.192 5.003 6.343 0.26 99032. 0.2467 24.23 0.3998 0.6395 0.0304 0.0190 0.103 1.615 1.015 76.447 0.183 4.514 6.021 0.26 99173. 0.2224 25.44 0.4197 0.6333 0.0270 0.0179 0.097 1.524 0.903 72.136 0.172 4.017 5.679 0.26 99319. 0.1979 26.65 0.4397 0.6202 0.0236 0.0168 0.091 1.427 0.790 67.513 0.161 3.515 5.309 0.26 99472. 0.1731 27.86 0.4597 0.5986 0.0202 0.0155 0.084 1.323 0.676 62.587 0.149 3.008 4.901 0.26 99629. 0.1478 29.07 0.4797 0.5661 0.0168 0.0142 0.077 1.212 0.562 57.372 0.137 2.499 4.442 0.26 99792. 0.1221 30.28 0.4997 0.5191 0.0134 0.0129 0.070 1.096 0.447 51.884 0.124 1.990 3.910 0.26 99961. 0.0959 31.50 0.5197 0.4523 0.0100 0.0115 0.062 0.975 0.333 46.146 0.110 1.482 3.275 0.26 100136. 0.0693 32.71 0.5397 0.3564 0.0066 0.0100 0.054 0.849 0.220 40.186 0.096 0.980 2.486 0.26 100316. 0.0428 33.92 0.5597 0.2158 0.0033 0.0085 0.046 0.719 0.109 34.036 0.081 0.484 1.451 0.26 100501. 0.0176 35.13 0.5796 -0.0022 0.0000 0.0069 0.037 0.585 -0.001 27.690 0.066 -0.004 -0.014 0.26 100686. 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 0.0789 0.0246 0.259 3.265 4.120 193.126 0.369 18.326 9.676 0.32 121623. 0.7203 1.52 0.0200 0.0626 0.0775 0.0248 0.261 3.292 4.045 194.755 0.372 17.991 9.420 0.32 121688. 0.6948 3.03 0.0400 0.1219 0.0759 0.0249 0.263 3.316 3.965 196.189 0.375 17.634 9.166 0.32 121757. 0.6693 4.55 0.0601 0.1778 0.0743 0.0251 0.265 3.337 3.879 197.390 0.377 17.255 8.914 0.32 121831. 0.6439 6.07 0.0801 0.2304 0.0726 0.0252 0.266 3.352 3.789 198.316 0.379 16.854 8.666 0.32 121910. 0.6186 7.58 0.1001 0.2799 0.0707 0.0253 0.267 3.363 3.693 198.930 0.380 16.428 8.421 0.32 121994. 0.5935 9.10 0.1201 0.3263 0.0688 0.0253 0.267 3.367 3.592 199.188 0.380 15.979 8.180 0.32 122084. 0.5686 10.62 0.1401 0.3696 0.0668 0.0253 0.267 3.365 3.486 199.050 0.380 15.504 7.943 0.32 122179. 0.5438 12.13 0.1601 0.4100 0.0646 0.0252 0.266 3.355 3.373 198.474 0.379 15.003 7.708 0.32 122280. 0.5192 13.65 0.1802 0.4474 0.0623 0.0251 0.265 3.337 3.255 197.419 0.377 14.477 7.478 0.32 122386. 0.4947 15.16 0.2002 0.4820 0.0600 0.0249 0.263 3.311 3.131 195.848 0.374 13.925 7.250 0.32 122499. 0.4704 16.68 0.2202 0.5137 0.0575 0.0246 0.260 3.275 3.000 193.724 0.370 13.346 7.025 0.32 122617. 0.4462 18.20 0.2402 0.5426 0.0549 0.0243 0.256 3.229 2.864 191.013 0.365 12.741 6.802 0.32 122742. 0.4222 19.71 0.2602 0.5687 0.0521 0.0239 0.252 3.173 2.723 187.678 0.358 12.110 6.580 0.32 122873. 0.3981 21.23 0.2802 0.5918 0.0493 0.0234 0.246 3.105 2.575 183.684 0.351 11.453 6.358 0.32 123010. 0.3741 22.75 0.3003 0.6118 0.0464 0.0228 0.240 3.026 2.422 179.018 0.342 10.771 6.135 0.32 123154. 0.3501 24.26 0.3203 0.6287 0.0433 0.0221 0.233 2.936 2.263 173.683 0.332 10.067 5.911 0.32 123304. 0.3261 25.78 0.3403 0.6422 0.0402 0.0213 0.225 2.835 2.101 167.686 0.320 9.344 5.682 0.32 123461. 0.3020 27.30 0.3603 0.6519 0.0370 0.0205 0.216 2.722 1.934 161.029 0.308 8.603 5.448 0.32 123624. 0.2779 28.81 0.3803 0.6575 0.0338 0.0195 0.206 2.599 1.764 153.719 0.294 7.847 5.205 0.32 123794. 0.2535 30.33 0.4003 0.6582 0.0305 0.0185 0.195 2.464 1.591 145.760 0.278 7.076 4.951 0.32 123971. 0.2290 31.85 0.4204 0.6534 0.0271 0.0174 0.184 2.319 1.415 137.161 0.262 6.295 4.680 0.32 124155. 0.2042 33.36 0.4404 0.6417 0.0237 0.0163 0.172 2.163 1.238 127.936 0.244 5.504 4.387 0.32 124346. 0.1790 34.88 0.4604 0.6215 0.0203 0.0150 0.158 1.996 1.058 118.105 0.226 4.707 4.064 0.32 124543. 0.1533 36.40 0.4804 0.5903 0.0168 0.0137 0.144 1.820 0.878 107.693 0.206 3.907 3.699 0.32 124748. 0.1271 37.91 0.5004 0.5442 0.0134 0.0123 0.130 1.635 0.698 96.736 0.185 3.106 3.274 0.32 124959. 0.1003 39.43 0.5205 0.4772 0.0099 0.0108 0.114 1.442 0.519 85.279 0.163 2.309 2.761 0.32 125178. 0.0729 40.94 0.5405 0.3790 0.0065 0.0093 0.098 1.240 0.342 73.379 0.140 1.519 2.111 0.32 125404. 0.0452 42.46 0.5605 0.2303 0.0032 0.0078 0.082 1.033 0.167 61.102 0.117 0.741 1.237 0.32 125636. 0.0185 43.98 0.5805 -0.0108 -0.0001 0.0062 0.065 0.818 -0.006 48.407 0.092 -0.027 -0.056 0.32 125866. 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 0.0794 0.0244 0.444 4.667 5.971 331.292 0.527 26.559 8.175 0.38 145942. 0.7326 1.84 0.0202 0.0640 0.0780 0.0246 0.448 4.708 5.861 334.180 0.532 26.070 7.955 0.38 146021. 0.7063 3.67 0.0404 0.1246 0.0764 0.0248 0.452 4.743 5.744 336.720 0.536 25.549 7.737 0.38 146105. 0.6800 5.51 0.0606 0.1817 0.0747 0.0249 0.454 4.773 5.619 338.839 0.539 24.995 7.522 0.38 146195. 0.6539 7.35 0.0808 0.2354 0.0730 0.0251 0.457 4.796 5.487 340.468 0.542 24.408 7.310 0.38 146292. 0.6280 9.18 0.1010 0.2859 0.0711 0.0251 0.458 4.811 5.347 341.534 0.544 23.785 7.102 0.38 146394. 0.6022 11.02 0.1212 0.3332 0.0692 0.0252 0.459 4.817 5.199 341.962 0.544 23.127 6.896 0.38 146503. 0.5767 12.86 0.1414 0.3773 0.0671 0.0251 0.458 4.813 5.043 341.677 0.544 22.431 6.694 0.38 146619. 0.5513 14.69 0.1616 0.4184 0.0649 0.0251 0.457 4.798 4.878 340.605 0.542 21.697 6.496 0.38 146742. 0.5261 16.53 0.1818 0.4565 0.0626 0.0249 0.454 4.771 4.704 338.674 0.539 20.925 6.300 0.38 146872. 0.5011 18.37 0.2020 0.4918 0.0601 0.0247 0.450 4.731 4.522 335.813 0.534 20.114 6.108 0.38 147009. 0.4763 20.20 0.2222 0.5241 0.0576 0.0244 0.445 4.676 4.331 331.957 0.528 19.264 5.918 0.38 147153. 0.4516 22.04 0.2424 0.5536 0.0549 0.0241 0.439 4.607 4.131 327.045 0.521 18.376 5.729 0.38 147305. 0.4271 23.88 0.2626 0.5801 0.0522 0.0236 0.430 4.522 3.923 321.010 0.511 17.448 5.543 0.38 147465. 0.4026 25.71 0.2828 0.6038 0.0493 0.0231 0.421 4.420 3.706 313.791 0.499 16.483 5.356 0.38 147632. 0.3781 27.55 0.3030 0.6243 0.0463 0.0225 0.410 4.302 3.480 305.367 0.486 15.481 5.170 0.38 147807. 0.3537 29.39 0.3232 0.6417 0.0432 0.0218 0.397 4.166 3.248 295.747 0.471 14.447 4.981 0.38 147991. 0.3292 31.22 0.3434 0.6556 0.0400 0.0210 0.382 4.014 3.009 284.939 0.453 13.385 4.790 0.38 148182. 0.3047 33.06 0.3636 0.6658 0.0368 0.0201 0.366 3.845 2.765 272.951 0.434 12.297 4.594 0.38 148381. 0.2801 34.89 0.3838 0.6717 0.0334 0.0191 0.348 3.660 2.515 259.789 0.413 11.186 4.391 0.38 148589. 0.2554 36.73 0.4040 0.6727 0.0301 0.0181 0.329 3.458 2.261 245.465 0.391 10.057 4.178 0.38 148805. 0.2304 38.57 0.4242 0.6680 0.0266 0.0169 0.308 3.240 2.003 229.996 0.366 8.910 3.951 0.38 149029. 0.2051 40.40 0.4444 0.6561 0.0232 0.0157 0.286 3.006 1.743 213.408 0.340 7.752 3.704 0.38 149262. 0.1793 42.24 0.4647 0.6352 0.0197 0.0144 0.262 2.757 1.480 195.739 0.312 6.584 3.430 0.38 149503. 0.1530 44.08 0.4849 0.6024 0.0162 0.0130 0.237 2.494 1.217 177.040 0.282 5.412 3.117 0.39 149753. 0.1261 45.91 0.5051 0.5532 0.0127 0.0116 0.211 2.217 0.954 157.378 0.250 4.242 2.748 0.39 150011. 0.0984 47.75 0.5253 0.4800 0.0092 0.0101 0.184 1.928 0.692 136.841 0.218 3.077 2.293 0.39 150278. 0.0699 49.59 0.5455 0.3695 0.0058 0.0085 0.155 1.628 0.433 115.538 0.184 1.926 1.700 0.39 150554. 0.0410 51.42 0.5657 0.1949 0.0024 0.0069 0.125 1.318 0.178 93.584 0.149 0.794 0.865 0.39 150836. 0.0134 53.26 0.5859 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 0.0800 0.0243 0.704 6.340 8.190 525.058 0.716 36.427 7.075 0.44 170258. 0.7425 2.15 0.0202 0.0647 0.0786 0.0245 0.710 6.396 8.039 529.711 0.723 35.758 6.883 0.44 170350. 0.7157 4.29 0.0405 0.1259 0.0770 0.0247 0.716 6.445 7.879 533.798 0.728 35.044 6.694 0.44 170449. 0.6891 6.44 0.0607 0.1836 0.0753 0.0249 0.720 6.487 7.708 537.203 0.733 34.286 6.508 0.44 170555. 0.6626 8.58 0.0809 0.2380 0.0736 0.0250 0.724 6.518 7.527 539.813 0.736 33.480 6.324 0.44 170668. 0.6363 10.73 0.1011 0.2890 0.0717 0.0251 0.726 6.539 7.335 541.511 0.739 32.627 6.144 0.44 170788. 0.6102 12.87 0.1214 0.3367 0.0697 0.0251 0.727 6.547 7.132 542.174 0.740 31.723 5.966 0.44 170916. 0.5843 15.02 0.1416 0.3814 0.0676 0.0251 0.726 6.541 6.917 541.682 0.739 30.768 5.792 0.44 171052. 0.5587 17.16 0.1618 0.4230 0.0654 0.0250 0.724 6.519 6.691 539.914 0.737 29.761 5.621 0.44 171196. 0.5332 19.31 0.1821 0.4616 0.0631 0.0249 0.720 6.481 6.452 536.753 0.732 28.700 5.452 0.45 171348. 0.5079 21.46 0.2023 0.4973 0.0606 0.0247 0.714 6.425 6.202 532.087 0.726 27.586 5.287 0.45 171508. 0.4828 23.60 0.2225 0.5301 0.0580 0.0244 0.705 6.349 5.939 525.809 0.717 26.419 5.123 0.45 171678. 0.4579 25.75 0.2428 0.5601 0.0554 0.0240 0.694 6.252 5.665 517.818 0.706 25.198 4.962 0.45 171856. 0.4331 27.89 0.2630 0.5872 0.0526 0.0235 0.681 6.134 5.378 508.012 0.693 23.923 4.802 0.45 172043. 0.4084 30.04 0.2832 0.6114 0.0496 0.0230 0.666 5.992 5.080 496.286 0.677 22.596 4.643 0.45 172239. 0.3838 32.18 0.3034 0.6326 0.0466 0.0224 0.647 5.827 4.770 482.609 0.658 21.219 4.483 0.45 172444. 0.3591 34.33 0.3237 0.6506 0.0435 0.0216 0.626 5.639 4.451 466.994 0.637 19.798 4.323 0.45 172659. 0.3345 36.48 0.3439 0.6652 0.0403 0.0208 0.603 5.427 4.122 449.454 0.613 18.337 4.160 0.45 172883. 0.3098 38.62 0.3641 0.6762 0.0370 0.0199 0.577 5.192 3.786 429.999 0.587 16.841 3.994 0.45 173116. 0.2850 40.77 0.3844 0.6829 0.0336 0.0189 0.548 4.934 3.443 408.642 0.557 15.314 3.821 0.45 173359. 0.2600 42.91 0.4046 0.6849 0.0302 0.0179 0.517 4.654 3.093 385.400 0.526 13.760 3.641 0.45 173612. 0.2348 45.06 0.4248 0.6811 0.0268 0.0167 0.483 4.351 2.739 360.302 0.492 12.184 3.448 0.45 173874. 0.2093 47.20 0.4451 0.6703 0.0233 0.0154 0.447 4.026 2.381 333.391 0.455 10.590 3.239 0.45 174147. 0.1833 49.35 0.4653 0.6505 0.0197 0.0141 0.409 3.679 2.020 304.727 0.416 8.985 3.007 0.45 174429. 0.1567 51.49 0.4855 0.6187 0.0162 0.0127 0.368 3.313 1.658 274.396 0.374 7.374 2.740 0.45 174721. 0.1294 53.64 0.5057 0.5700 0.0127 0.0112 0.325 2.928 1.296 242.507 0.331 5.765 2.424 0.45 175023. 0.1012 55.79 0.5260 0.4965 0.0091 0.0097 0.281 2.526 0.936 209.207 0.285 4.165 2.030 0.45 175336. 0.0720 57.93 0.5462 0.3829 0.0057 0.0081 0.234 2.109 0.581 174.673 0.238 2.583 1.508 0.45 175658. 0.0421 60.08 0.5664 0.1984 0.0023 0.0064 0.187 1.679 0.231 139.093 0.190 1.027 0.753 0.45 175989. 0.0133 62.22 0.5867 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 0.0808 0.0244 1.054 8.302 10.794 785.789 0.938 48.011 6.230 0.51 194570. 0.7507 2.44 0.0202 0.0650 0.0793 0.0246 1.063 8.376 10.597 792.788 0.946 47.135 6.063 0.51 194676. 0.7238 4.89 0.0403 0.1264 0.0777 0.0248 1.071 8.441 10.387 798.932 0.954 46.201 5.897 0.51 194789. 0.6970 7.33 0.0605 0.1843 0.0760 0.0250 1.078 8.495 10.164 804.042 0.960 45.208 5.733 0.51 194910. 0.6703 9.78 0.0807 0.2388 0.0743 0.0251 1.083 8.536 9.927 807.950 0.964 44.154 5.573 0.51 195039. 0.6439 12.22 0.1008 0.2901 0.0724 0.0252 1.087 8.563 9.675 810.479 0.967 43.036 5.415 0.51 195176. 0.6177 14.66 0.1210 0.3381 0.0704 0.0252 1.088 8.573 9.409 811.448 0.969 41.852 5.259 0.51 195322. 0.5916 17.11 0.1411 0.3830 0.0683 0.0252 1.087 8.565 9.128 810.674 0.968 40.601 5.107 0.51 195477. 0.5658 19.55 0.1613 0.4249 0.0661 0.0251 1.084 8.537 8.831 807.978 0.964 39.281 4.957 0.51 195641. 0.5403 22.00 0.1815 0.4639 0.0637 0.0249 1.077 8.486 8.519 803.181 0.959 37.890 4.811 0.51 195815. 0.5149 24.44 0.2016 0.5000 0.0613 0.0247 1.068 8.411 8.190 796.116 0.950 36.430 4.666 0.51 195998. 0.4897 26.88 0.2218 0.5332 0.0587 0.0244 1.055 8.311 7.846 786.624 0.939 34.899 4.524 0.51 196191. 0.4647 29.33 0.2420 0.5636 0.0560 0.0240 1.039 8.183 7.486 774.554 0.925 33.298 4.384 0.51 196394. 0.4399 31.77 0.2621 0.5913 0.0532 0.0236 1.019 8.027 7.110 759.752 0.907 31.627 4.245 0.51 196607. 0.4151 34.22 0.2823 0.6160 0.0503 0.0230 0.995 7.840 6.719 742.060 0.886 29.885 4.107 0.51 196831. 0.3904 36.66 0.3024 0.6378 0.0472 0.0224 0.967 7.622 6.313 721.424 0.861 28.078 3.969 0.51 197064. 0.3657 39.10 0.3226 0.6566 0.0441 0.0217 0.936 7.373 5.893 697.861 0.833 26.212 3.830 0.51 197309. 0.3410 41.55 0.3428 0.6721 0.0409 0.0208 0.900 7.093 5.462 671.389 0.801 24.294 3.690 0.51 197564. 0.3162 43.99 0.3629 0.6840 0.0376 0.0199 0.861 6.783 5.020 642.025 0.766 22.330 3.547 0.51 197829. 0.2914 46.44 0.3831 0.6919 0.0342 0.0189 0.818 6.443 4.569 609.787 0.728 20.324 3.399 0.51 198106. 0.2664 48.88 0.4033 0.6951 0.0307 0.0178 0.771 6.072 4.110 574.701 0.686 18.282 3.244 0.51 198393. 0.2412 51.32 0.4234 0.6929 0.0273 0.0167 0.720 5.672 3.644 536.810 0.641 16.211 3.079 0.51 198692. 0.2156 53.77 0.4436 0.6838 0.0237 0.0154 0.665 5.242 3.174 496.175 0.592 14.116 2.901 0.51 199001. 0.1895 56.21 0.4638 0.6661 0.0202 0.0141 0.607 4.785 2.699 452.887 0.541 12.005 2.703 0.51 199322. 0.1629 58.66 0.4839 0.6368 0.0166 0.0126 0.546 4.301 2.223 407.070 0.486 9.886 2.476 0.51 199654. 0.1354 61.10 0.5041 0.5912 0.0131 0.0111 0.481 3.792 1.746 358.889 0.428 7.768 2.207 0.51 199998. 0.1070 63.54 0.5242 0.5212 0.0095 0.0096 0.414 3.260 1.273 308.559 0.368 5.661 1.871 0.51 200352. 0.0774 65.99 0.5444 0.4116 0.0060 0.0080 0.344 2.708 0.804 256.347 0.306 3.577 1.423 0.52 200719. 0.0468 68.43 0.5646 0.2306 0.0026 0.0063 0.272 2.140 0.343 202.541 0.242 1.527 0.769 0.52 201095. 0.0165 70.88 0.5847 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 0.0816 0.0246 1.511 10.579 13.807 1126.415 1.195 61.414 5.560 0.57 218877. 0.7576 2.72 0.0200 0.0646 0.0801 0.0248 1.524 10.672 13.559 1136.392 1.206 60.309 5.412 0.57 218995. 0.7308 5.45 0.0399 0.1257 0.0786 0.0250 1.536 10.754 13.294 1145.141 1.215 59.132 5.265 0.57 219122. 0.7041 8.17 0.0599 0.1835 0.0769 0.0251 1.545 10.823 13.013 1152.416 1.223 57.880 5.121 0.57 219257. 0.6775 10.89 0.0799 0.2378 0.0752 0.0252 1.553 10.875 12.714 1157.975 1.229 56.550 4.980 0.57 219401. 0.6512 13.62 0.0999 0.2890 0.0733 0.0253 1.558 10.909 12.397 1161.571 1.232 55.141 4.841 0.57 219555. 0.6250 16.34 0.1198 0.3370 0.0713 0.0254 1.560 10.922 12.061 1162.951 1.234 53.648 4.704 0.57 219718. 0.5991 19.07 0.1398 0.3820 0.0692 0.0253 1.558 10.911 11.707 1161.854 1.233 52.071 4.570 0.57 219891. 0.5734 21.79 0.1598 0.4240 0.0670 0.0252 1.553 10.875 11.332 1158.029 1.229 50.406 4.439 0.57 220074. 0.5480 24.51 0.1798 0.4631 0.0647 0.0251 1.544 10.812 10.938 1151.227 1.221 48.653 4.310 0.57 220267. 0.5227 27.24 0.1997 0.4995 0.0622 0.0249 1.530 10.718 10.524 1141.210 1.211 46.812 4.183 0.57 220471. 0.4976 29.96 0.2197 0.5330 0.0596 0.0246 1.512 10.591 10.090 1127.755 1.197 44.881 4.058 0.57 220686. 0.4727 32.68 0.2397 0.5639 0.0570 0.0242 1.489 10.431 9.636 1110.651 1.178 42.861 3.935 0.57 220911. 0.4480 35.41 0.2597 0.5920 0.0542 0.0238 1.461 10.234 9.162 1089.683 1.156 40.754 3.814 0.57 221148. 0.4233 38.13 0.2796 0.6174 0.0512 0.0232 1.428 9.998 8.668 1064.630 1.130 38.557 3.693 0.57 221396. 0.3987 40.86 0.2996 0.6399 0.0482 0.0226 1.388 9.724 8.156 1035.383 1.099 36.276 3.573 0.57 221656. 0.3742 43.58 0.3196 0.6595 0.0451 0.0218 1.344 9.410 7.626 1001.962 1.063 33.920 3.452 0.57 221927. 0.3496 46.30 0.3396 0.6760 0.0419 0.0210 1.293 9.057 7.081 964.397 1.023 31.497 3.330 0.57 222210. 0.3250 49.03 0.3595 0.6891 0.0386 0.0201 1.237 8.666 6.523 922.710 0.979 29.013 3.206 0.57 222504. 0.3003 51.75 0.3795 0.6985 0.0352 0.0191 1.176 8.236 5.952 876.926 0.930 26.476 3.079 0.58 222811. 0.2755 54.47 0.3995 0.7035 0.0318 0.0180 1.109 7.767 5.371 827.080 0.878 23.892 2.946 0.58 223129. 0.2504 57.20 0.4194 0.7033 0.0283 0.0169 1.037 7.262 4.782 773.228 0.820 21.269 2.805 0.58 223460. 0.2249 59.92 0.4394 0.6969 0.0247 0.0156 0.959 6.719 4.185 715.452 0.759 18.615 2.653 0.58 223802. 0.1990 62.64 0.4594 0.6826 0.0212 0.0143 0.877 6.141 3.583 653.870 0.694 15.938 2.486 0.58 224158. 0.1725 65.37 0.4794 0.6577 0.0176 0.0128 0.789 5.528 2.978 588.648 0.625 13.248 2.295 0.58 224525. 0.1453 68.09 0.4993 0.6180 0.0140 0.0113 0.697 4.884 2.373 520.005 0.552 10.557 2.070 0.58 224905. 0.1170 70.82 0.5193 0.5563 0.0105 0.0098 0.601 4.210 1.771 448.231 0.476 7.876 1.792 0.58 225298. 0.0874 73.54 0.5393 0.4593 0.0069 0.0081 0.501 3.509 1.174 373.687 0.396 5.220 1.425 0.58 225703. 0.0566 76.26 0.5593 0.2992 0.0035 0.0065 0.398 2.787 0.586 296.789 0.315 2.605 0.895 0.58 226119. 0.0251 78.99 0.5792 0.0032 0.0000 0.0047 0.291 2.040 0.004 217.250 0.231 0.019 0.009 0.58 226529. 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 0.0826 0.0248 2.095 13.203 17.259 1562.109 1.492 76.769 5.011 0.63 243177. 0.7635 3.03 0.0200 0.0647 0.0812 0.0250 2.113 13.320 16.951 1575.925 1.505 75.396 4.879 0.63 243309. 0.7366 6.05 0.0399 0.1260 0.0796 0.0252 2.130 13.422 16.621 1588.005 1.516 73.932 4.747 0.63 243451. 0.7098 9.08 0.0599 0.1838 0.0779 0.0254 2.143 13.507 16.271 1597.997 1.526 72.374 4.618 0.63 243602. 0.6832 12.11 0.0799 0.2384 0.0761 0.0255 2.153 13.571 15.899 1605.572 1.533 70.719 4.491 0.63 243763. 0.6568 15.13 0.0999 0.2897 0.0742 0.0256 2.160 13.611 15.504 1610.379 1.538 68.962 4.367 0.63 243935. 0.6306 18.16 0.1198 0.3379 0.0722 0.0256 2.162 13.626 15.086 1612.060 1.539 67.102 4.245 0.64 244117. 0.6046 21.18 0.1398 0.3831 0.0701 0.0256 2.159 13.610 14.643 1610.258 1.538 65.133 4.125 0.64 244310. 0.5788 24.21 0.1598 0.4253 0.0679 0.0255 2.152 13.563 14.176 1604.620 1.532 63.056 4.007 0.64 244514. 0.5533 27.24 0.1798 0.4647 0.0655 0.0253 2.139 13.480 13.684 1594.798 1.523 60.867 3.892 0.64 244730. 0.5280 30.26 0.1997 0.5013 0.0630 0.0251 2.119 13.358 13.167 1580.464 1.509 58.566 3.779 0.64 244958. 0.5028 33.29 0.2197 0.5352 0.0604 0.0248 2.094 13.197 12.624 1561.308 1.491 56.153 3.667 0.64 245197. 0.4779 36.32 0.2397 0.5664 0.0577 0.0244 2.061 12.991 12.057 1537.034 1.468 53.629 3.558 0.64 245449. 0.4531 39.34 0.2597 0.5950 0.0549 0.0240 2.021 12.741 11.464 1507.353 1.439 50.993 3.450 0.64 245713. 0.4283 42.37 0.2796 0.6208 0.0519 0.0234 1.974 12.441 10.846 1471.953 1.406 48.245 3.342 0.64 245990. 0.4037 45.39 0.2996 0.6438 0.0489 0.0227 1.919 12.092 10.205 1430.678 1.366 45.391 3.235 0.64 246279. 0.3790 48.42 0.3196 0.6640 0.0457 0.0220 1.855 11.694 9.542 1383.559 1.321 42.442 3.128 0.64 246581. 0.3544 51.45 0.3396 0.6811 0.0424 0.0211 1.784 11.247 8.860 1330.636 1.271 39.408 3.020 0.64 246896. 0.3297 54.47 0.3595 0.6949 0.0391 0.0202 1.706 10.751 8.160 1271.943 1.215 36.298 2.910 0.64 247224. 0.3049 57.50 0.3795 0.7050 0.0357 0.0192 1.619 10.206 7.446 1207.518 1.153 33.120 2.797 0.64 247565. 0.2799 60.53 0.3995 0.7109 0.0322 0.0181 1.525 9.614 6.718 1137.410 1.086 29.883 2.679 0.64 247919. 0.2547 63.55 0.4194 0.7117 0.0286 0.0169 1.424 8.974 5.979 1061.698 1.014 26.596 2.554 0.64 248287. 0.2291 66.58 0.4394 0.7064 0.0250 0.0156 1.315 8.287 5.232 980.497 0.936 23.270 2.420 0.64 248668. 0.2030 69.61 0.4594 0.6932 0.0214 0.0142 1.199 7.556 4.477 893.977 0.854 19.915 2.272 0.64 249063. 0.1763 72.63 0.4794 0.6695 0.0178 0.0128 1.076 6.782 3.719 802.368 0.766 16.543 2.102 0.64 249472. 0.1487 75.66 0.4993 0.6309 0.0142 0.0112 0.947 5.967 2.961 705.981 0.674 13.169 1.902 0.64 249894. 0.1200 78.68 0.5193 0.5700 0.0106 0.0096 0.812 5.115 2.205 605.224 0.578 9.808 1.652 0.64 250330. 0.0900 81.71 0.5393 0.4727 0.0070 0.0080 0.671 4.231 1.456 500.606 0.478 6.478 1.320 0.64 250781. 0.0584 84.74 0.5593 0.3084 0.0034 0.0062 0.527 3.319 0.719 392.717 0.375 3.198 0.830 0.64 251244. 0.0258 87.76 0.5792 -0.0070 -0.0001 0.0045 0.377 2.375 -0.011 280.936 0.268 -0.050 -0.018 0.65 251695. 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 0.0839 0.0252 2.832 16.225 21.190 2111.522 1.833 94.254 4.552 0.70 267469. 0.7684 3.33 0.0200 0.0646 0.0824 0.0254 2.856 16.367 20.815 2130.056 1.849 92.583 4.432 0.70 267616. 0.7416 6.65 0.0399 0.1258 0.0808 0.0256 2.878 16.491 20.413 2146.192 1.863 90.799 4.314 0.70 267772. 0.7148 9.98 0.0599 0.1836 0.0791 0.0258 2.896 16.593 19.986 2159.462 1.875 88.899 4.198 0.70 267940. 0.6882 13.30 0.0798 0.2382 0.0773 0.0259 2.909 16.669 19.532 2169.410 1.883 86.879 4.084 0.70 268118. 0.6619 16.63 0.0998 0.2895 0.0754 0.0260 2.917 16.717 19.050 2175.563 1.889 84.733 3.972 0.70 268308. 0.6357 19.95 0.1197 0.3378 0.0734 0.0260 2.920 16.731 18.538 2177.438 1.890 82.459 3.862 0.70 268509. 0.6097 23.28 0.1397 0.3831 0.0712 0.0260 2.916 16.709 17.997 2174.550 1.888 80.052 3.754 0.70 268723. 0.5840 26.61 0.1596 0.4255 0.0690 0.0259 2.905 16.646 17.426 2166.421 1.881 77.509 3.648 0.70 268948. 0.5585 29.93 0.1796 0.4652 0.0666 0.0257 2.887 16.540 16.823 2152.583 1.869 74.829 3.545 0.70 269187. 0.5332 33.26 0.1995 0.5020 0.0641 0.0255 2.860 16.387 16.189 2132.592 1.851 72.010 3.443 0.70 269438. 0.5081 36.58 0.2195 0.5362 0.0614 0.0251 2.824 16.182 15.524 2106.028 1.828 69.053 3.343 0.70 269702. 0.4831 39.91 0.2395 0.5678 0.0587 0.0247 2.779 15.925 14.828 2072.505 1.799 65.957 3.245 0.70 269980. 0.4583 43.24 0.2594 0.5967 0.0558 0.0243 2.724 15.611 14.101 2031.630 1.764 62.723 3.148 0.70 270271. 0.4335 46.56 0.2794 0.6230 0.0528 0.0237 2.659 15.237 13.343 1982.991 1.721 59.351 3.052 0.70 270576. 0.4089 49.89 0.2993 0.6466 0.0497 0.0230 2.583 14.802 12.556 1926.367 1.672 55.848 2.956 0.70 270895. 0.3842 53.21 0.3193 0.6673 0.0465 0.0222 2.497 14.306 11.742 1861.791 1.616 52.227 2.860 0.70 271227. 0.3595 56.54 0.3392 0.6851 0.0431 0.0214 2.400 13.749 10.904 1789.327 1.553 48.499 2.764 0.70 271574. 0.3347 59.86 0.3592 0.6996 0.0397 0.0204 2.292 13.132 10.044 1709.025 1.484 44.677 2.666 0.70 271935. 0.3098 63.19 0.3791 0.7105 0.0363 0.0194 2.174 12.455 9.166 1620.939 1.407 40.770 2.565 0.70 272310. 0.2848 66.52 0.3991 0.7173 0.0327 0.0182 2.045 11.719 8.271 1525.140 1.324 36.790 2.460 0.70 272700. 0.2594 69.84 0.4191 0.7192 0.0291 0.0170 1.907 10.924 7.362 1421.737 1.234 32.748 2.349 0.70 273105. 0.2337 73.17 0.4390 0.7150 0.0255 0.0157 1.758 10.073 6.442 1310.906 1.138 28.656 2.229 0.70 273524. 0.2075 76.49 0.4590 0.7031 0.0218 0.0142 1.600 9.166 5.514 1192.892 1.036 24.527 2.097 0.71 273958. 0.1806 79.82 0.4789 0.6808 0.0181 0.0128 1.432 8.207 4.581 1068.037 0.927 20.376 1.945 0.71 274408. 0.1527 83.15 0.4989 0.6436 0.0144 0.0112 1.256 7.198 3.647 936.803 0.813 16.221 1.766 0.71 274872. 0.1237 86.47 0.5188 0.5839 0.0107 0.0095 1.073 6.146 2.716 799.795 0.694 12.081 1.540 0.71 275351. 0.0931 89.80 0.5388 0.4869 0.0071 0.0079 0.882 5.054 1.794 657.777 0.571 7.979 1.237 0.71 275846. 0.0608 93.12 0.5587 0.3203 0.0035 0.0061 0.686 3.931 0.885 511.636 0.444 3.936 0.784 0.71 276354. 0.0271 96.45 0.5787 -0.0083 -0.0001 0.0043 0.483 2.770 -0.016 360.511 0.313 -0.069 -0.020 0.71 276848. 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 0.0853 0.0258 3.765 19.776 25.653 2807.746 2.234 114.105 4.144 0.76 291750. 0.7697 3.62 0.0199 0.0642 0.0838 0.0260 3.795 19.932 25.204 2829.856 2.252 112.105 4.040 0.76 291911. 0.7437 7.25 0.0399 0.1250 0.0822 0.0262 3.821 20.067 24.723 2849.053 2.267 109.968 3.936 0.76 292084. 0.7177 10.87 0.0598 0.1826 0.0805 0.0263 3.842 20.178 24.211 2864.715 2.280 107.689 3.833 0.76 292268. 0.6917 14.49 0.0797 0.2371 0.0787 0.0265 3.857 20.259 23.665 2876.218 2.289 105.263 3.732 0.76 292463. 0.6658 18.11 0.0996 0.2884 0.0768 0.0265 3.866 20.306 23.086 2882.904 2.294 102.685 3.632 0.76 292672. 0.6400 21.74 0.1196 0.3368 0.0747 0.0265 3.868 20.314 22.470 2884.104 2.295 99.948 3.534 0.76 292893. 0.6143 25.36 0.1395 0.3821 0.0725 0.0265 3.861 20.279 21.819 2879.130 2.291 97.050 3.437 0.76 293127. 0.5888 28.98 0.1594 0.4247 0.0703 0.0264 3.845 20.196 21.130 2867.299 2.282 93.986 3.342 0.76 293374. 0.5635 32.61 0.1793 0.4645 0.0678 0.0262 3.819 20.060 20.403 2847.948 2.266 90.753 3.249 0.76 293635. 0.5383 36.23 0.1993 0.5016 0.0653 0.0259 3.782 19.866 19.638 2820.448 2.244 87.352 3.158 0.76 293910. 0.5133 39.85 0.2192 0.5361 0.0626 0.0256 3.734 19.611 18.835 2784.215 2.216 83.780 3.068 0.76 294200. 0.4884 43.47 0.2391 0.5680 0.0598 0.0252 3.673 19.290 17.995 2738.727 2.179 80.040 2.980 0.76 294504. 0.4636 47.10 0.2590 0.5973 0.0569 0.0247 3.599 18.901 17.116 2683.493 2.135 76.131 2.893 0.76 294822. 0.4389 50.72 0.2790 0.6240 0.0539 0.0241 3.511 18.440 16.199 2617.992 2.083 72.054 2.807 0.76 295156. 0.4142 54.34 0.2989 0.6481 0.0507 0.0234 3.409 17.904 15.246 2541.930 2.023 67.815 2.720 0.77 295504. 0.3896 57.97 0.3188 0.6694 0.0474 0.0226 3.293 17.295 14.261 2455.382 1.954 63.431 2.634 0.77 295867. 0.3648 61.59 0.3387 0.6878 0.0440 0.0217 3.163 16.612 13.246 2358.475 1.877 58.917 2.547 0.77 296246. 0.3400 65.21 0.3587 0.7029 0.0406 0.0207 3.019 15.857 12.205 2251.334 1.792 54.286 2.459 0.77 296640. 0.3150 68.83 0.3786 0.7145 0.0370 0.0196 2.862 15.032 11.140 2134.100 1.698 49.551 2.368 0.77 297049. 0.2898 72.46 0.3985 0.7218 0.0334 0.0185 2.691 14.136 10.055 2006.957 1.597 44.724 2.272 0.77 297475. 0.2643 76.08 0.4184 0.7242 0.0298 0.0172 2.508 13.173 8.952 1870.160 1.488 39.821 2.171 0.77 297916. 0.2382 79.70 0.4384 0.7203 0.0261 0.0159 2.312 12.143 7.836 1724.059 1.372 34.854 2.061 0.77 298373. 0.2116 83.33 0.4583 0.7084 0.0223 0.0144 2.104 11.052 6.709 1569.127 1.249 29.840 1.939 0.77 298846. 0.1842 86.95 0.4782 0.6855 0.0185 0.0129 1.885 9.903 5.575 1405.988 1.119 24.797 1.798 0.77 299335. 0.1557 90.57 0.4981 0.6471 0.0148 0.0114 1.657 8.702 4.439 1235.444 0.983 19.746 1.630 0.77 299841. 0.1259 94.19 0.5181 0.5852 0.0110 0.0097 1.419 7.456 3.307 1058.503 0.842 14.711 1.417 0.77 300363. 0.0945 97.82 0.5380 0.4848 0.0073 0.0081 1.175 6.173 2.185 876.391 0.697 9.717 1.131 0.77 300901. 0.0613 101.44 0.5579 0.3148 0.0036 0.0064 0.926 4.864 1.078 690.496 0.549 4.793 0.708 0.77 301455. 0.0269 105.06 0.5778 -0.0081 -0.0001 0.0046 0.670 3.519 -0.019 499.592 0.398 -0.087 -0.018 0.77 301993. 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 0.0870 0.0274 5.083 24.643 30.714 3790.198 2.784 136.616 3.676 0.83 316017. 0.7470 3.92 0.0199 0.0618 0.0855 0.0275 5.102 24.738 30.185 3804.793 2.795 134.261 3.598 0.83 316193. 0.7250 7.84 0.0398 0.1210 0.0839 0.0276 5.117 24.810 29.618 3815.913 2.803 131.740 3.520 0.83 316381. 0.7026 11.76 0.0597 0.1775 0.0822 0.0277 5.127 24.855 29.013 3822.884 2.808 129.048 3.442 0.83 316582. 0.6799 15.68 0.0796 0.2312 0.0804 0.0277 5.129 24.869 28.367 3825.014 2.810 126.177 3.364 0.83 316796. 0.6570 19.60 0.0995 0.2823 0.0784 0.0276 5.125 24.847 27.680 3821.577 2.807 123.121 3.285 0.83 317023. 0.6339 23.52 0.1194 0.3306 0.0764 0.0276 5.112 24.783 26.950 3811.797 2.800 119.874 3.207 0.83 317265. 0.6105 27.44 0.1393 0.3763 0.0742 0.0275 5.089 24.673 26.176 3794.880 2.788 116.430 3.129 0.83 317520. 0.5870 31.36 0.1592 0.4194 0.0718 0.0273 5.056 24.512 25.356 3770.005 2.769 112.784 3.051 0.83 317790. 0.5633 35.28 0.1791 0.4598 0.0694 0.0270 5.011 24.293 24.491 3736.345 2.745 108.935 2.973 0.83 318075. 0.5396 39.20 0.1990 0.4976 0.0668 0.0267 4.953 24.011 23.579 3693.091 2.713 104.879 2.896 0.83 318374. 0.5157 43.12 0.2189 0.5329 0.0641 0.0263 4.881 23.663 22.621 3639.461 2.673 100.617 2.819 0.83 318690. 0.4917 47.04 0.2388 0.5655 0.0612 0.0259 4.795 23.245 21.616 3575.271 2.626 96.149 2.742 0.83 319020. 0.4676 50.96 0.2587 0.5954 0.0583 0.0253 4.693 22.755 20.566 3499.814 2.571 91.477 2.665 0.83 319367. 0.4433 54.88 0.2786 0.6226 0.0552 0.0247 4.576 22.187 19.469 3412.458 2.507 86.600 2.588 0.83 319729. 0.4187 58.80 0.2985 0.6469 0.0519 0.0240 4.442 21.538 18.329 3312.674 2.433 81.527 2.510 0.83 320107. 0.3940 62.72 0.3184 0.6682 0.0486 0.0232 4.292 20.809 17.148 3200.531 2.351 76.275 2.430 0.83 320502. 0.3691 66.64 0.3383 0.6863 0.0451 0.0223 4.125 19.999 15.932 3075.965 2.259 70.864 2.349 0.83 320913. 0.3439 70.56 0.3582 0.7008 0.0416 0.0213 3.942 19.110 14.683 2939.291 2.159 65.310 2.266 0.83 321341. 0.3184 74.48 0.3781 0.7114 0.0380 0.0202 3.742 18.145 13.406 2790.766 2.050 59.628 2.179 0.83 321785. 0.2925 78.40 0.3980 0.7171 0.0343 0.0190 3.528 17.105 12.103 2630.871 1.933 53.834 2.087 0.83 322246. 0.2662 82.31 0.4179 0.7171 0.0305 0.0178 3.299 15.996 10.779 2460.233 1.807 47.944 1.987 0.83 322724. 0.2393 86.23 0.4378 0.7098 0.0267 0.0165 3.057 14.822 9.437 2279.737 1.675 41.974 1.877 0.83 323219. 0.2115 90.15 0.4577 0.6931 0.0229 0.0151 2.803 13.590 8.081 2090.257 1.535 35.946 1.754 0.83 323731. 0.1828 94.07 0.4776 0.6638 0.0190 0.0137 2.538 12.307 6.717 1892.935 1.390 29.879 1.610 0.83 324261. 0.1530 97.99 0.4975 0.6172 0.0152 0.0122 2.265 10.982 5.350 1689.167 1.241 23.799 1.437 0.84 324808. 0.1219 101.91 0.5174 0.5457 0.0113 0.0107 1.985 9.626 3.987 1480.572 1.088 17.733 1.221 0.84 325373. 0.0894 105.83 0.5373 0.4367 0.0075 0.0092 1.702 8.251 2.633 1269.018 0.932 11.713 0.941 0.84 325955. 0.0560 109.75 0.5572 0.2681 0.0037 0.0076 1.417 6.869 1.298 1056.484 0.776 5.774 0.557 0.84 326553. 0.0233 113.67 0.5771 -0.0066 -0.0001 0.0061 1.127 5.466 -0.025 840.755 0.618 -0.109 -0.013 0.84 327141. 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 0.0888 0.0312 7.221 32.509 36.356 5384.671 3.673 161.711 3.062 0.89 340271. 0.6772 4.23 0.0200 0.0560 0.0873 0.0311 7.202 32.423 35.747 5370.482 3.663 159.001 3.019 0.89 340463. 0.6620 8.47 0.0399 0.1104 0.0857 0.0310 7.176 32.307 35.092 5351.192 3.650 156.089 2.974 0.89 340668. 0.6462 12.70 0.0599 0.1631 0.0840 0.0308 7.143 32.156 34.391 5326.233 3.633 152.969 2.929 0.89 340887. 0.6298 16.94 0.0799 0.2140 0.0822 0.0307 7.101 31.967 33.640 5294.929 3.612 149.632 2.882 0.89 341120. 0.6129 21.17 0.0998 0.2630 0.0802 0.0304 7.049 31.736 32.839 5256.596 3.585 146.070 2.834 0.89 341368. 0.5955 25.41 0.1198 0.3101 0.0781 0.0302 6.987 31.457 31.986 5210.464 3.554 142.273 2.784 0.89 341631. 0.5775 29.64 0.1397 0.3553 0.0759 0.0299 6.914 31.127 31.078 5155.758 3.517 138.235 2.734 0.89 341910. 0.5590 33.88 0.1597 0.3984 0.0736 0.0295 6.828 30.740 30.115 5091.687 3.473 133.952 2.683 0.89 342204. 0.5399 38.11 0.1797 0.4394 0.0711 0.0291 6.729 30.292 29.096 5017.485 3.422 129.419 2.630 0.89 342515. 0.5203 42.35 0.1996 0.4783 0.0685 0.0286 6.614 29.778 28.020 4932.395 3.364 124.634 2.577 0.89 342842. 0.5002 46.58 0.2196 0.5150 0.0657 0.0280 6.485 29.194 26.888 4835.662 3.298 119.598 2.522 0.89 343186. 0.4796 50.81 0.2396 0.5494 0.0628 0.0274 6.338 28.536 25.700 4726.528 3.224 114.312 2.466 0.89 343546. 0.4585 55.05 0.2595 0.5811 0.0597 0.0267 6.178 27.813 24.455 4606.913 3.142 108.777 2.408 0.89 343923. 0.4367 59.28 0.2795 0.6097 0.0566 0.0259 6.003 27.027 23.155 4476.581 3.053 102.993 2.346 0.89 344318. 0.4140 63.52 0.2994 0.6350 0.0533 0.0251 5.814 26.177 21.800 4335.851 2.957 96.968 2.281 0.89 344730. 0.3905 67.75 0.3194 0.6567 0.0498 0.0242 5.612 25.264 20.397 4184.580 2.854 90.726 2.211 0.89 345159. 0.3662 71.99 0.3394 0.6737 0.0463 0.0233 5.399 24.306 18.949 4025.986 2.746 84.287 2.135 0.89 345607. 0.3408 76.22 0.3593 0.6851 0.0427 0.0224 5.180 23.322 17.462 3862.915 2.635 77.670 2.050 0.89 346071. 0.3142 80.46 0.3793 0.6912 0.0389 0.0214 4.947 22.274 15.939 3689.335 2.516 70.899 1.960 0.89 346554. 0.2869 84.69 0.3993 0.6912 0.0351 0.0203 4.700 21.161 14.387 3505.002 2.391 63.993 1.862 0.90 347055. 0.2590 88.93 0.4192 0.6840 0.0313 0.0192 4.440 19.990 12.808 3311.084 2.258 56.972 1.755 0.90 347574. 0.2303 93.16 0.4392 0.6679 0.0274 0.0180 4.169 18.770 11.209 3109.051 2.121 49.859 1.635 0.90 348111. 0.2008 97.39 0.4591 0.6405 0.0234 0.0168 3.890 17.514 9.595 2900.963 1.979 42.677 1.500 0.90 348667. 0.1704 101.63 0.4791 0.5992 0.0195 0.0156 3.605 16.230 7.971 2688.323 1.834 35.454 1.345 0.90 349241. 0.1392 105.86 0.4991 0.5400 0.0155 0.0143 3.317 14.931 6.345 2473.170 1.687 28.221 1.164 0.90 349835. 0.1075 110.10 0.5190 0.4581 0.0115 0.0131 3.028 13.631 4.724 2257.783 1.540 21.015 0.949 0.90 350447. 0.0757 114.33 0.5390 0.3469 0.0076 0.0118 2.742 12.343 3.120 2044.521 1.395 13.876 0.692 0.90 351078. 0.0448 118.57 0.5590 0.1977 0.0038 0.0106 2.461 11.081 1.539 1835.396 1.252 6.846 0.380 0.90 351727. 0.0173 122.80 0.5789 -0.0039 -0.0001 0.0094 2.177 9.801 -0.026 1623.465 1.107 -0.114 -0.007 0.90 352376. 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 0.0898 0.0373 10.616 44.609 42.178 7916.701 5.040 187.608 2.417 0.95 364543. 0.5755 4.59 0.0202 0.0481 0.0884 0.0371 10.558 44.362 41.525 7872.822 5.012 184.701 2.392 0.95 364748. 0.5653 9.17 0.0404 0.0952 0.0869 0.0368 10.483 44.050 40.814 7817.516 4.977 181.541 2.368 0.95 364968. 0.5548 13.76 0.0605 0.1413 0.0852 0.0365 10.393 43.671 40.045 7750.219 4.934 178.120 2.344 0.95 365204. 0.5439 18.34 0.0807 0.1865 0.0834 0.0361 10.286 43.221 39.214 7670.288 4.883 174.425 2.319 0.95 365456. 0.5325 22.93 0.1009 0.2306 0.0815 0.0357 10.161 42.696 38.319 7577.193 4.824 170.443 2.294 0.95 365725. 0.5207 27.51 0.1211 0.2736 0.0795 0.0352 10.018 42.094 37.357 7470.413 4.756 166.165 2.268 0.95 366011. 0.5084 32.10 0.1412 0.3155 0.0773 0.0346 9.856 41.413 36.327 7349.555 4.679 161.582 2.242 0.95 366315. 0.4955 36.68 0.1614 0.3562 0.0750 0.0340 9.675 40.651 35.227 7214.309 4.593 156.688 2.215 0.95 366636. 0.4821 41.27 0.1816 0.3956 0.0725 0.0333 9.474 39.807 34.055 7064.435 4.497 151.478 2.187 0.95 366975. 0.4679 45.85 0.2018 0.4336 0.0698 0.0325 9.253 38.879 32.813 6899.760 4.393 145.951 2.157 0.95 367332. 0.4531 50.44 0.2219 0.4701 0.0670 0.0316 9.012 37.866 31.499 6720.069 4.278 140.109 2.126 0.95 367708. 0.4376 55.02 0.2421 0.5050 0.0641 0.0307 8.750 36.768 30.116 6525.113 4.154 133.954 2.093 0.95 368103. 0.4213 59.61 0.2623 0.5380 0.0610 0.0297 8.468 35.582 28.663 6314.600 4.020 127.491 2.059 0.96 368516. 0.4042 64.20 0.2825 0.5684 0.0578 0.0287 8.173 34.344 27.140 6094.943 3.880 120.717 2.020 0.96 368948. 0.3859 68.78 0.3026 0.5955 0.0544 0.0276 7.869 33.065 25.550 5868.010 3.736 113.645 1.975 0.96 369399. 0.3661 73.37 0.3228 0.6185 0.0509 0.0265 7.560 31.766 23.899 5637.482 3.589 106.304 1.923 0.96 369869. 0.3447 77.95 0.3430 0.6366 0.0472 0.0254 7.247 30.450 22.195 5403.854 3.440 98.723 1.863 0.96 370359. 0.3219 82.54 0.3632 0.6465 0.0435 0.0244 6.959 29.240 20.440 5189.142 3.304 90.918 1.787 0.96 370868. 0.2962 87.12 0.3833 0.6445 0.0397 0.0236 6.719 28.232 18.639 5010.206 3.190 82.905 1.687 0.96 371396. 0.2672 91.71 0.4035 0.6350 0.0358 0.0227 6.471 27.190 16.803 4825.273 3.072 74.738 1.579 0.96 371944. 0.2374 96.29 0.4237 0.6170 0.0318 0.0218 6.217 26.121 14.938 4635.702 2.951 66.445 1.462 0.96 372512. 0.2072 100.88 0.4439 0.5893 0.0278 0.0209 5.958 25.035 13.053 4442.855 2.828 58.059 1.333 0.96 373100. 0.1766 105.46 0.4640 0.5506 0.0237 0.0200 5.698 23.942 11.155 4248.909 2.705 49.617 1.191 0.96 373707. 0.1458 110.05 0.4842 0.4992 0.0197 0.0191 5.439 22.855 9.254 4056.112 2.582 41.160 1.035 0.96 374336. 0.1154 114.64 0.5044 0.4339 0.0157 0.0182 5.186 21.789 7.360 3866.899 2.462 32.739 0.863 0.96 374984. 0.0859 119.22 0.5246 0.3533 0.0117 0.0173 4.938 20.749 5.487 3682.353 2.344 24.407 0.676 0.97 375654. 0.0581 123.81 0.5447 0.2563 0.0078 0.0165 4.699 19.743 3.647 3503.819 2.231 16.223 0.472 0.97 376345. 0.0331 128.39 0.5649 0.1418 0.0039 0.0157 4.467 18.771 1.851 3331.205 2.121 8.231 0.252 0.97 377060. 0.0126 132.98 0.5851 0.0057 0.0001 0.0148 4.219 17.728 0.068 3146.222 2.003 0.303 0.010 0.97 377816. 0.0001