21x10.5PN (21x105PN.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 0.0867 0.0331 0.011 0.685 0.537 8.110 0.077 2.390 30.047 0.08 47153. 0.6154 0.45 0.0225 0.0574 0.0853 0.0334 0.011 0.692 0.528 8.192 0.078 2.350 29.255 0.08 47181. 0.5942 0.90 0.0450 0.1117 0.0837 0.0337 0.011 0.699 0.519 8.267 0.079 2.308 28.464 0.08 47212. 0.5729 1.34 0.0675 0.1629 0.0821 0.0340 0.011 0.704 0.509 8.335 0.080 2.262 27.677 0.08 47246. 0.5515 1.79 0.0900 0.2111 0.0803 0.0342 0.011 0.709 0.498 8.392 0.080 2.213 26.894 0.08 47282. 0.5301 2.24 0.1125 0.2563 0.0784 0.0344 0.011 0.713 0.486 8.438 0.081 2.161 26.118 0.08 47320. 0.5087 2.69 0.1351 0.2985 0.0764 0.0346 0.011 0.716 0.473 8.469 0.081 2.105 25.349 0.08 47361. 0.4873 3.13 0.1576 0.3377 0.0742 0.0346 0.011 0.717 0.460 8.485 0.081 2.046 24.587 0.08 47406. 0.4659 3.58 0.1801 0.3741 0.0719 0.0346 0.011 0.717 0.446 8.481 0.081 1.982 23.832 0.08 47452. 0.4445 4.03 0.2026 0.4077 0.0695 0.0345 0.011 0.715 0.430 8.458 0.081 1.915 23.084 0.08 47502. 0.4232 4.48 0.2251 0.4385 0.0669 0.0343 0.011 0.711 0.414 8.412 0.080 1.843 22.343 0.08 47555. 0.4019 4.92 0.2476 0.4664 0.0641 0.0340 0.011 0.705 0.397 8.342 0.080 1.768 21.607 0.08 47611. 0.3806 5.37 0.2701 0.4916 0.0612 0.0337 0.011 0.697 0.380 8.248 0.079 1.688 20.876 0.08 47670. 0.3594 5.82 0.2926 0.5140 0.0583 0.0332 0.011 0.687 0.361 8.129 0.078 1.606 20.146 0.08 47732. 0.3382 6.27 0.3151 0.5334 0.0551 0.0326 0.011 0.675 0.342 7.984 0.076 1.520 19.415 0.08 47798. 0.3171 6.71 0.3376 0.5499 0.0519 0.0319 0.010 0.660 0.322 7.814 0.075 1.432 18.681 0.08 47866. 0.2961 7.16 0.3602 0.5632 0.0486 0.0311 0.010 0.644 0.301 7.618 0.073 1.340 17.938 0.08 47938. 0.2751 7.61 0.3827 0.5732 0.0452 0.0302 0.010 0.625 0.280 7.396 0.071 1.246 17.183 0.08 48013. 0.2541 8.06 0.4052 0.5796 0.0417 0.0292 0.010 0.604 0.259 7.146 0.068 1.150 16.408 0.08 48091. 0.2331 8.51 0.4277 0.5819 0.0381 0.0280 0.009 0.581 0.236 6.870 0.066 1.052 15.608 0.08 48173. 0.2120 8.95 0.4502 0.5797 0.0345 0.0268 0.009 0.555 0.214 6.566 0.063 0.951 14.771 0.08 48258. 0.1909 9.40 0.4727 0.5722 0.0308 0.0254 0.008 0.527 0.191 6.235 0.060 0.849 13.886 0.08 48347. 0.1695 9.85 0.4952 0.5584 0.0270 0.0240 0.008 0.497 0.168 5.876 0.056 0.745 12.934 0.08 48439. 0.1479 10.30 0.5177 0.5368 0.0232 0.0224 0.007 0.464 0.144 5.489 0.052 0.640 11.894 0.08 48534. 0.1261 10.74 0.5402 0.5054 0.0194 0.0207 0.007 0.429 0.120 5.075 0.048 0.534 10.731 0.08 48633. 0.1039 11.19 0.5627 0.4610 0.0155 0.0189 0.006 0.392 0.096 4.634 0.044 0.427 9.398 0.08 48735. 0.0814 11.64 0.5852 0.3990 0.0116 0.0170 0.006 0.352 0.072 4.167 0.040 0.320 7.821 0.08 48841. 0.0586 12.09 0.6078 0.3117 0.0077 0.0150 0.005 0.311 0.048 3.675 0.035 0.212 5.883 0.08 48950. 0.0359 12.53 0.6303 0.1858 0.0038 0.0129 0.004 0.267 0.024 3.160 0.030 0.105 3.382 0.08 49062. 0.0145 12.98 0.6528 -0.0044 -0.0001 0.0107 0.004 0.222 0.000 2.622 0.025 -0.002 -0.077 0.09 49175. 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 0.0871 0.0300 0.079 2.482 2.160 58.724 0.280 9.609 16.685 0.17 94303. 0.6852 0.90 0.0226 0.0639 0.0857 0.0303 0.080 2.512 2.125 59.442 0.284 9.451 16.212 0.17 94361. 0.6603 1.80 0.0452 0.1241 0.0842 0.0307 0.081 2.540 2.086 60.109 0.287 9.280 15.744 0.17 94423. 0.6354 2.70 0.0678 0.1807 0.0825 0.0310 0.081 2.566 2.045 60.712 0.290 9.098 15.281 0.17 94491. 0.6106 3.60 0.0904 0.2338 0.0807 0.0312 0.082 2.588 2.001 61.235 0.292 8.902 14.824 0.17 94563. 0.5860 4.50 0.1131 0.2834 0.0788 0.0315 0.083 2.606 1.954 61.662 0.294 8.692 14.375 0.17 94641. 0.5615 5.40 0.1357 0.3296 0.0768 0.0316 0.083 2.619 1.904 61.976 0.296 8.468 13.933 0.17 94724. 0.5372 6.30 0.1583 0.3726 0.0746 0.0317 0.083 2.627 1.850 62.157 0.297 8.229 13.499 0.17 94813. 0.5130 7.19 0.1809 0.4124 0.0723 0.0317 0.083 2.628 1.792 62.187 0.297 7.973 13.074 0.17 94907. 0.4891 8.09 0.2035 0.4491 0.0698 0.0316 0.083 2.622 1.731 62.046 0.296 7.701 12.656 0.17 95008. 0.4653 8.99 0.2261 0.4828 0.0672 0.0315 0.083 2.608 1.667 61.721 0.295 7.413 12.247 0.17 95114. 0.4417 9.89 0.2487 0.5137 0.0645 0.0312 0.082 2.586 1.598 61.200 0.292 7.109 11.845 0.17 95227. 0.4184 10.79 0.2713 0.5417 0.0616 0.0308 0.081 2.556 1.526 60.475 0.289 6.790 11.449 0.17 95346. 0.3952 11.69 0.2939 0.5668 0.0586 0.0304 0.080 2.516 1.452 59.542 0.284 6.457 11.058 0.17 95471. 0.3723 12.59 0.3166 0.5891 0.0554 0.0298 0.078 2.468 1.374 58.396 0.279 6.112 10.672 0.17 95603. 0.3495 13.49 0.3392 0.6084 0.0522 0.0291 0.076 2.410 1.294 57.033 0.272 5.754 10.288 0.17 95741. 0.3270 14.39 0.3618 0.6248 0.0488 0.0283 0.074 2.343 1.211 55.449 0.265 5.386 9.905 0.17 95886. 0.3045 15.29 0.3844 0.6380 0.0454 0.0274 0.072 2.267 1.126 53.641 0.256 5.008 9.520 0.17 96037. 0.2822 16.19 0.4070 0.6479 0.0419 0.0263 0.069 2.181 1.039 51.605 0.246 4.620 9.129 0.17 96195. 0.2600 17.09 0.4296 0.6540 0.0383 0.0252 0.066 2.085 0.950 49.337 0.236 4.224 8.730 0.17 96360. 0.2377 17.99 0.4522 0.6558 0.0346 0.0239 0.063 1.979 0.859 46.835 0.224 3.820 8.317 0.17 96532. 0.2154 18.89 0.4748 0.6527 0.0309 0.0225 0.059 1.864 0.766 44.097 0.211 3.409 7.883 0.17 96710. 0.1928 19.78 0.4974 0.6435 0.0271 0.0210 0.055 1.738 0.673 41.121 0.196 2.992 7.420 0.17 96896. 0.1700 20.68 0.5201 0.6268 0.0233 0.0193 0.051 1.602 0.578 37.909 0.181 2.570 6.912 0.17 97088. 0.1468 21.58 0.5427 0.6001 0.0194 0.0176 0.046 1.456 0.482 34.462 0.165 2.143 6.342 0.17 97287. 0.1230 22.48 0.5653 0.5595 0.0155 0.0157 0.041 1.301 0.385 30.786 0.147 1.714 5.677 0.17 97493. 0.0985 23.38 0.5879 0.4987 0.0116 0.0137 0.036 1.136 0.288 26.889 0.128 1.283 4.865 0.17 97706. 0.0730 24.28 0.6105 0.4059 0.0077 0.0116 0.031 0.963 0.192 22.781 0.109 0.852 3.813 0.17 97926. 0.0466 25.18 0.6331 0.2576 0.0038 0.0094 0.025 0.781 0.095 18.478 0.088 0.423 2.333 0.17 98152. 0.0201 26.08 0.6557 -0.0048 -0.0001 0.0071 0.019 0.590 -0.001 13.962 0.067 -0.006 -0.042 0.17 98377. 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 0.0876 0.0288 0.255 5.366 4.889 190.461 0.606 21.746 11.643 0.25 141450. 0.7193 1.35 0.0227 0.0670 0.0862 0.0292 0.259 5.437 4.809 192.984 0.614 21.390 11.302 0.25 141537. 0.6925 2.70 0.0453 0.1300 0.0847 0.0295 0.262 5.503 4.723 195.338 0.622 21.006 10.966 0.25 141631. 0.6659 4.06 0.0680 0.1891 0.0830 0.0298 0.265 5.564 4.630 197.471 0.629 20.595 10.635 0.25 141733. 0.6394 5.41 0.0906 0.2444 0.0812 0.0301 0.267 5.616 4.531 199.331 0.634 20.153 10.310 0.25 141842. 0.6132 6.76 0.1133 0.2960 0.0793 0.0304 0.269 5.659 4.424 200.864 0.639 19.679 9.991 0.25 141959. 0.5872 8.11 0.1360 0.3441 0.0773 0.0305 0.271 5.691 4.310 202.007 0.643 19.173 9.678 0.25 142084. 0.5614 9.46 0.1586 0.3888 0.0751 0.0306 0.272 5.711 4.189 202.696 0.645 18.631 9.373 0.25 142218. 0.5360 10.81 0.1813 0.4302 0.0728 0.0307 0.272 5.716 4.059 202.866 0.646 18.053 9.074 0.25 142361. 0.5108 12.17 0.2039 0.4685 0.0703 0.0306 0.271 5.704 3.920 202.452 0.644 17.438 8.783 0.25 142512. 0.4859 13.52 0.2266 0.5037 0.0677 0.0304 0.270 5.674 3.774 201.401 0.641 16.785 8.498 0.25 142673. 0.4613 14.87 0.2493 0.5359 0.0649 0.0302 0.268 5.626 3.619 199.673 0.636 16.096 8.220 0.25 142843. 0.4369 16.22 0.2719 0.5652 0.0620 0.0298 0.265 5.557 3.456 197.243 0.628 15.374 7.948 0.25 143022. 0.4129 17.57 0.2946 0.5918 0.0589 0.0293 0.260 5.468 3.287 194.090 0.618 14.620 7.681 0.25 143211. 0.3891 18.93 0.3172 0.6155 0.0558 0.0287 0.255 5.359 3.111 190.200 0.605 13.837 7.419 0.25 143409. 0.3656 20.28 0.3399 0.6364 0.0525 0.0280 0.249 5.228 2.929 185.558 0.591 13.028 7.159 0.25 143617. 0.3423 21.63 0.3626 0.6545 0.0491 0.0272 0.242 5.076 2.741 180.149 0.573 12.193 6.902 0.25 143835. 0.3193 22.98 0.3852 0.6695 0.0457 0.0263 0.233 4.901 2.549 173.959 0.554 11.336 6.645 0.25 144063. 0.2964 24.33 0.4079 0.6813 0.0421 0.0252 0.224 4.704 2.351 166.976 0.532 10.457 6.386 0.25 144302. 0.2736 25.69 0.4305 0.6895 0.0385 0.0241 0.213 4.485 2.149 159.187 0.507 9.560 6.124 0.25 144550. 0.2508 27.04 0.4532 0.6939 0.0348 0.0228 0.202 4.243 1.943 150.582 0.479 8.645 5.854 0.25 144808. 0.2280 28.39 0.4759 0.6935 0.0311 0.0213 0.189 3.977 1.734 141.154 0.449 7.714 5.572 0.25 145077. 0.2050 29.74 0.4985 0.6875 0.0273 0.0198 0.176 3.688 1.522 130.900 0.417 6.769 5.273 0.25 145356. 0.1818 31.09 0.5212 0.6743 0.0234 0.0181 0.161 3.376 1.307 119.821 0.381 5.813 4.947 0.25 145646. 0.1580 32.44 0.5438 0.6514 0.0195 0.0163 0.145 3.041 1.090 107.925 0.344 4.847 4.580 0.25 145946. 0.1336 33.80 0.5665 0.6147 0.0156 0.0144 0.128 2.683 0.871 95.231 0.303 3.875 4.149 0.25 146256. 0.1082 35.15 0.5891 0.5571 0.0117 0.0124 0.110 2.304 0.652 81.767 0.260 2.899 3.616 0.25 146577. 0.0816 36.50 0.6118 0.4647 0.0078 0.0102 0.091 1.904 0.433 67.572 0.215 1.924 2.904 0.25 146909. 0.0534 37.85 0.6345 0.3062 0.0038 0.0080 0.071 1.485 0.214 52.698 0.168 0.954 1.845 0.25 147249. 0.0239 39.20 0.6571 -0.0087 -0.0001 0.0056 0.050 1.043 -0.004 37.036 0.118 -0.018 -0.050 0.26 147582. 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 0.0883 0.0283 0.595 9.372 8.757 443.541 1.059 38.951 8.955 0.33 188591. 0.7404 1.81 0.0227 0.0688 0.0869 0.0287 0.603 9.502 8.614 449.693 1.074 38.317 8.689 0.33 188708. 0.7125 3.61 0.0454 0.1334 0.0853 0.0290 0.611 9.624 8.461 455.436 1.087 37.633 8.426 0.33 188834. 0.6848 5.42 0.0681 0.1939 0.0837 0.0294 0.618 9.734 8.296 460.647 1.100 36.899 8.168 0.33 188970. 0.6574 7.22 0.0908 0.2506 0.0819 0.0297 0.624 9.830 8.118 465.202 1.111 36.111 7.915 0.33 189116. 0.6302 9.03 0.1135 0.3034 0.0800 0.0299 0.629 9.910 7.928 468.966 1.120 35.266 7.668 0.33 189273. 0.6033 10.83 0.1362 0.3526 0.0779 0.0301 0.633 9.969 7.725 471.792 1.126 34.361 7.427 0.33 189440. 0.5767 12.64 0.1589 0.3983 0.0757 0.0302 0.635 10.006 7.507 473.523 1.130 33.392 7.191 0.33 189620. 0.5505 14.44 0.1815 0.4407 0.0734 0.0302 0.636 10.016 7.275 474.001 1.132 32.358 6.961 0.33 189811. 0.5246 16.25 0.2042 0.4799 0.0709 0.0302 0.634 9.996 7.027 473.070 1.129 31.257 6.737 0.33 190014. 0.4990 18.05 0.2269 0.5159 0.0682 0.0300 0.631 9.944 6.764 470.600 1.123 30.088 6.520 0.33 190229. 0.4738 19.86 0.2496 0.5491 0.0654 0.0297 0.626 9.857 6.487 466.494 1.114 28.854 6.307 0.33 190456. 0.4489 21.66 0.2723 0.5793 0.0625 0.0294 0.618 9.735 6.196 460.688 1.100 27.560 6.100 0.33 190696. 0.4243 23.47 0.2950 0.6068 0.0594 0.0289 0.608 9.575 5.892 453.134 1.082 26.209 5.898 0.33 190949. 0.4000 25.27 0.3177 0.6315 0.0562 0.0283 0.595 9.378 5.577 443.793 1.059 24.805 5.699 0.33 191215. 0.3761 27.08 0.3404 0.6534 0.0529 0.0276 0.580 9.142 5.250 432.628 1.033 23.353 5.504 0.34 191493. 0.3524 28.88 0.3631 0.6725 0.0496 0.0268 0.563 8.867 4.914 419.605 1.002 21.856 5.311 0.34 191785. 0.3290 30.69 0.3858 0.6888 0.0461 0.0258 0.543 8.551 4.568 404.690 0.966 20.318 5.120 0.34 192090. 0.3057 32.49 0.4085 0.7019 0.0425 0.0247 0.520 8.196 4.214 387.851 0.926 18.743 4.928 0.34 192409. 0.2826 34.30 0.4312 0.7118 0.0388 0.0235 0.495 7.798 3.852 369.057 0.881 17.132 4.734 0.34 192741. 0.2596 36.10 0.4539 0.7178 0.0351 0.0222 0.467 7.359 3.483 348.283 0.831 15.491 4.535 0.34 193087. 0.2365 37.91 0.4766 0.7195 0.0313 0.0208 0.437 6.878 3.107 325.513 0.777 13.821 4.330 0.34 193447. 0.2132 39.71 0.4993 0.7158 0.0275 0.0192 0.403 6.355 2.726 300.738 0.718 12.126 4.112 0.34 193820. 0.1897 41.52 0.5219 0.7053 0.0236 0.0175 0.367 5.789 2.340 273.962 0.654 10.410 3.875 0.34 194207. 0.1656 43.32 0.5446 0.6854 0.0197 0.0156 0.329 5.181 1.951 245.207 0.585 8.678 3.609 0.34 194609. 0.1408 45.13 0.5673 0.6521 0.0157 0.0137 0.288 4.533 1.559 214.516 0.512 6.934 3.296 0.34 195024. 0.1150 46.93 0.5900 0.5978 0.0118 0.0116 0.244 3.845 1.166 181.958 0.434 5.184 2.905 0.34 195453. 0.0876 48.74 0.6127 0.5071 0.0078 0.0094 0.198 3.120 0.772 147.633 0.352 3.436 2.373 0.34 195896. 0.0583 50.54 0.6354 0.3431 0.0038 0.0071 0.150 2.359 0.381 111.662 0.267 1.695 1.548 0.34 196351. 0.0267 52.35 0.6581 -0.0173 -0.0001 0.0047 0.099 1.556 -0.012 73.626 0.176 -0.054 -0.075 0.34 196786. 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 0.0892 0.0281 1.156 14.568 13.814 861.756 1.646 61.445 7.271 0.42 235724. 0.7551 2.26 0.0227 0.0698 0.0877 0.0285 1.172 14.776 13.591 874.062 1.669 60.453 7.053 0.42 235870. 0.7265 4.52 0.0454 0.1354 0.0862 0.0289 1.188 14.970 13.351 885.551 1.691 59.385 6.838 0.42 236028. 0.6981 6.77 0.0681 0.1968 0.0845 0.0292 1.202 15.146 13.092 895.979 1.711 58.234 6.628 0.42 236199. 0.6701 9.03 0.0908 0.2542 0.0827 0.0295 1.214 15.300 12.814 905.099 1.729 56.999 6.422 0.42 236382. 0.6423 11.29 0.1135 0.3078 0.0808 0.0298 1.224 15.428 12.516 912.644 1.743 55.673 6.220 0.42 236579. 0.6149 13.55 0.1362 0.3577 0.0787 0.0300 1.231 15.524 12.197 918.322 1.754 54.251 6.024 0.42 236790. 0.5878 15.80 0.1589 0.4041 0.0765 0.0301 1.236 15.583 11.855 921.823 1.761 52.729 5.833 0.42 237015. 0.5611 18.06 0.1816 0.4471 0.0741 0.0301 1.238 15.600 11.489 922.830 1.762 51.103 5.647 0.42 237255. 0.5348 20.32 0.2043 0.4869 0.0716 0.0301 1.235 15.570 11.099 921.037 1.759 49.370 5.466 0.42 237509. 0.5088 22.58 0.2270 0.5236 0.0690 0.0299 1.229 15.488 10.686 916.179 1.750 47.530 5.290 0.42 237779. 0.4832 24.83 0.2498 0.5573 0.0661 0.0296 1.218 15.350 10.249 908.063 1.734 45.587 5.119 0.42 238064. 0.4579 27.09 0.2725 0.5882 0.0632 0.0293 1.202 15.156 9.790 896.560 1.712 43.546 4.953 0.42 238365. 0.4330 29.35 0.2952 0.6164 0.0601 0.0288 1.182 14.903 9.311 881.575 1.684 41.416 4.791 0.42 238682. 0.4084 31.61 0.3179 0.6418 0.0569 0.0282 1.157 14.589 8.813 863.027 1.648 39.202 4.632 0.42 239015. 0.3842 33.86 0.3406 0.6645 0.0536 0.0274 1.128 14.214 8.298 840.850 1.606 36.911 4.476 0.42 239365. 0.3603 36.12 0.3633 0.6846 0.0501 0.0266 1.093 13.777 7.767 814.970 1.556 34.549 4.323 0.42 239730. 0.3366 38.38 0.3860 0.7018 0.0466 0.0256 1.053 13.275 7.222 785.322 1.500 32.122 4.171 0.42 240113. 0.3132 40.64 0.4087 0.7160 0.0430 0.0245 1.008 12.709 6.662 751.841 1.436 29.635 4.019 0.42 240512. 0.2899 42.89 0.4314 0.7271 0.0393 0.0233 0.958 12.078 6.091 714.468 1.365 27.092 3.867 0.42 240928. 0.2666 45.15 0.4541 0.7346 0.0355 0.0220 0.903 11.379 5.508 673.154 1.286 24.500 3.711 0.42 241361. 0.2434 47.41 0.4768 0.7380 0.0317 0.0205 0.842 10.614 4.915 627.864 1.199 21.862 3.551 0.42 241811. 0.2199 49.67 0.4995 0.7362 0.0278 0.0189 0.776 9.781 4.313 578.582 1.105 19.185 3.381 0.42 242279. 0.1962 51.92 0.5222 0.7280 0.0239 0.0171 0.704 8.880 3.704 525.315 1.003 16.475 3.198 0.42 242764. 0.1720 54.18 0.5449 0.7109 0.0199 0.0153 0.628 7.913 3.089 468.107 0.894 13.739 2.993 0.42 243266. 0.1470 56.44 0.5676 0.6808 0.0159 0.0133 0.546 6.881 2.469 407.042 0.777 10.983 2.752 0.42 243786. 0.1208 58.70 0.5903 0.6301 0.0119 0.0112 0.459 5.786 1.848 342.260 0.654 8.219 2.449 0.42 244323. 0.0930 60.95 0.6130 0.5426 0.0079 0.0089 0.367 4.631 1.227 273.961 0.523 5.456 2.031 0.42 244877. 0.0628 63.21 0.6357 0.3777 0.0039 0.0066 0.271 3.421 0.608 202.389 0.387 2.705 1.363 0.42 245447. 0.0297 65.47 0.6584 -0.0151 -0.0001 0.0041 0.170 2.139 -0.015 126.561 0.242 -0.065 -0.053 0.43 245985. 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 0.0902 0.0282 2.004 21.055 20.131 1494.661 2.379 89.541 6.109 0.50 282845. 0.7658 2.72 0.0228 0.0705 0.0888 0.0286 2.034 21.363 19.809 1516.499 2.414 88.111 5.925 0.50 283022. 0.7368 5.43 0.0455 0.1368 0.0872 0.0290 2.061 21.650 19.462 1536.871 2.446 86.566 5.744 0.50 283213. 0.7080 8.15 0.0683 0.1988 0.0855 0.0294 2.086 21.910 19.088 1555.346 2.475 84.902 5.566 0.50 283419. 0.6795 10.86 0.0910 0.2568 0.0837 0.0297 2.107 22.138 18.685 1571.489 2.501 83.111 5.393 0.50 283641. 0.6514 13.58 0.1138 0.3109 0.0818 0.0299 2.125 22.326 18.252 1584.823 2.522 81.187 5.224 0.50 283879. 0.6236 16.29 0.1366 0.3614 0.0797 0.0301 2.139 22.467 17.788 1594.835 2.538 79.122 5.059 0.50 284134. 0.5962 19.01 0.1593 0.4082 0.0775 0.0302 2.147 22.553 17.291 1600.978 2.548 76.909 4.899 0.50 284406. 0.5691 21.72 0.1821 0.4517 0.0751 0.0303 2.149 22.577 16.759 1602.686 2.551 74.542 4.743 0.50 284696. 0.5425 24.44 0.2048 0.4920 0.0726 0.0302 2.145 22.531 16.191 1599.422 2.546 72.017 4.591 0.50 285004. 0.5162 27.16 0.2276 0.5291 0.0699 0.0300 2.133 22.408 15.588 1590.711 2.532 69.334 4.445 0.50 285330. 0.4903 29.87 0.2504 0.5634 0.0670 0.0298 2.114 22.204 14.950 1576.213 2.509 66.498 4.302 0.50 285675. 0.4648 32.59 0.2731 0.5948 0.0640 0.0294 2.086 21.915 14.280 1555.698 2.476 63.519 4.164 0.50 286038. 0.4396 35.30 0.2959 0.6235 0.0609 0.0289 2.050 21.539 13.581 1529.001 2.433 60.407 4.029 0.50 286421. 0.4148 38.02 0.3186 0.6495 0.0576 0.0283 2.006 21.074 12.853 1495.987 2.381 57.171 3.897 0.50 286824. 0.3904 40.73 0.3414 0.6729 0.0542 0.0275 1.953 20.518 12.100 1456.534 2.318 53.822 3.768 0.50 287246. 0.3662 43.45 0.3641 0.6936 0.0508 0.0266 1.892 19.870 11.324 1410.519 2.245 50.368 3.641 0.50 287687. 0.3424 46.17 0.3869 0.7116 0.0472 0.0257 1.821 19.128 10.526 1357.828 2.161 46.818 3.516 0.50 288149. 0.3187 48.88 0.4097 0.7267 0.0435 0.0245 1.741 18.290 9.708 1298.347 2.066 43.179 3.391 0.50 288631. 0.2952 51.60 0.4324 0.7388 0.0398 0.0233 1.652 17.355 8.871 1231.975 1.961 39.459 3.266 0.50 289133. 0.2718 54.31 0.4552 0.7474 0.0359 0.0219 1.554 16.322 8.018 1158.627 1.844 35.665 3.139 0.51 289656. 0.2483 57.03 0.4779 0.7520 0.0320 0.0204 1.446 15.189 7.150 1078.242 1.716 31.805 3.008 0.51 290199. 0.2247 59.74 0.5007 0.7517 0.0281 0.0187 1.329 13.957 6.269 990.791 1.577 27.886 2.870 0.51 290763. 0.2008 62.46 0.5235 0.7451 0.0241 0.0169 1.202 12.626 5.377 896.293 1.426 23.918 2.721 0.51 291348. 0.1763 65.17 0.5462 0.7299 0.0201 0.0150 1.066 11.197 4.477 794.823 1.265 19.912 2.555 0.51 291954. 0.1510 67.89 0.5690 0.7019 0.0160 0.0130 0.921 9.671 3.570 686.540 1.093 15.877 2.358 0.51 292580. 0.1245 70.61 0.5917 0.6531 0.0119 0.0108 0.767 8.053 2.659 571.692 0.910 11.829 2.110 0.51 293228. 0.0961 73.32 0.6145 0.5661 0.0078 0.0085 0.604 6.348 1.750 450.646 0.717 7.784 1.761 0.51 293896. 0.0651 76.04 0.6373 0.3944 0.0038 0.0061 0.434 4.562 0.845 323.838 0.515 3.757 1.183 0.51 294583. 0.0304 78.75 0.6600 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 0.0916 0.0286 3.219 28.986 27.803 2400.608 3.275 123.670 5.253 0.58 329951. 0.7740 3.16 0.0227 0.0707 0.0901 0.0290 3.267 29.417 27.368 2436.227 3.323 121.731 5.095 0.58 330158. 0.7448 6.33 0.0455 0.1370 0.0886 0.0294 3.312 29.817 26.896 2469.429 3.369 119.632 4.940 0.58 330382. 0.7158 9.49 0.0682 0.1992 0.0869 0.0297 3.352 30.181 26.386 2499.515 3.410 117.366 4.788 0.58 330623. 0.6872 12.66 0.0909 0.2574 0.0851 0.0300 3.387 30.498 25.837 2525.780 3.446 114.924 4.640 0.58 330883. 0.6590 15.82 0.1136 0.3118 0.0831 0.0303 3.416 30.760 25.247 2547.452 3.475 112.297 4.495 0.58 331162. 0.6311 18.98 0.1364 0.3624 0.0810 0.0305 3.438 30.956 24.612 2563.709 3.497 109.473 4.354 0.58 331461. 0.6036 22.15 0.1591 0.4095 0.0788 0.0306 3.451 31.076 23.931 2573.676 3.511 106.444 4.217 0.58 331779. 0.5765 25.31 0.1818 0.4532 0.0764 0.0306 3.455 31.110 23.202 2576.438 3.515 103.201 4.085 0.58 332119. 0.5497 28.48 0.2046 0.4938 0.0738 0.0306 3.448 31.045 22.423 2571.119 3.507 99.737 3.956 0.58 332479. 0.5234 31.64 0.2273 0.5313 0.0711 0.0304 3.429 30.874 21.595 2556.955 3.488 96.053 3.831 0.58 332860. 0.4974 34.80 0.2500 0.5660 0.0682 0.0301 3.397 30.590 20.718 2533.386 3.456 92.155 3.709 0.58 333263. 0.4718 37.97 0.2727 0.5978 0.0652 0.0297 3.353 30.187 19.797 2500.034 3.411 88.056 3.592 0.59 333688. 0.4465 41.13 0.2955 0.6270 0.0620 0.0292 3.294 29.663 18.834 2456.645 3.351 83.771 3.477 0.59 334136. 0.4216 44.30 0.3182 0.6536 0.0587 0.0286 3.222 29.015 17.831 2403.005 3.278 79.314 3.366 0.59 334606. 0.3971 47.46 0.3409 0.6776 0.0553 0.0278 3.137 28.242 16.794 2338.927 3.191 74.698 3.257 0.59 335098. 0.3729 50.62 0.3637 0.6990 0.0518 0.0269 3.036 27.340 15.723 2264.225 3.089 69.936 3.150 0.59 335614. 0.3490 53.79 0.3864 0.7178 0.0481 0.0259 2.922 26.307 14.622 2178.712 2.972 65.038 3.044 0.59 336153. 0.3252 56.95 0.4091 0.7338 0.0444 0.0248 2.792 25.142 13.493 2082.217 2.841 60.016 2.939 0.59 336715. 0.3017 60.12 0.4318 0.7469 0.0406 0.0235 2.648 23.842 12.338 1974.580 2.694 54.880 2.834 0.59 337300. 0.2782 63.28 0.4546 0.7567 0.0367 0.0221 2.488 22.406 11.160 1855.662 2.531 49.640 2.728 0.59 337910. 0.2546 66.44 0.4773 0.7628 0.0328 0.0205 2.314 20.833 9.961 1725.366 2.354 44.308 2.619 0.59 338543. 0.2309 69.61 0.5000 0.7642 0.0288 0.0188 2.124 19.122 8.744 1583.648 2.160 38.893 2.504 0.59 339201. 0.2069 72.77 0.5228 0.7597 0.0247 0.0170 1.918 17.273 7.511 1430.528 1.952 33.408 2.381 0.59 339882. 0.1824 75.94 0.5455 0.7471 0.0206 0.0151 1.698 15.288 6.265 1266.128 1.727 27.866 2.244 0.59 340588. 0.1570 79.10 0.5682 0.7225 0.0165 0.0130 1.463 13.170 5.010 1090.694 1.488 22.285 2.083 0.59 341318. 0.1303 82.26 0.5910 0.6782 0.0123 0.0108 1.213 10.923 3.751 904.625 1.234 16.682 1.880 0.59 342072. 0.1018 85.43 0.6137 0.5973 0.0082 0.0084 0.950 8.555 2.491 708.505 0.967 11.081 1.595 0.59 342850. 0.0703 88.59 0.6364 0.4333 0.0041 0.0060 0.675 6.074 1.237 503.046 0.686 5.503 1.116 0.59 343650. 0.0347 91.76 0.6591 -0.0216 -0.0001 0.0034 0.381 3.430 -0.034 284.099 0.388 -0.150 -0.054 0.60 344375. 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 0.0932 0.0291 4.898 38.586 36.966 3652.139 4.359 164.423 4.591 0.67 377036. 0.7799 3.62 0.0227 0.0707 0.0918 0.0295 4.971 39.166 36.399 3707.036 4.425 161.903 4.454 0.67 377274. 0.7508 7.24 0.0455 0.1370 0.0902 0.0300 5.040 39.706 35.784 3758.197 4.486 159.166 4.319 0.67 377532. 0.7218 10.86 0.0682 0.1993 0.0885 0.0303 5.102 40.196 35.118 3804.521 4.541 156.203 4.187 0.67 377810. 0.6932 14.48 0.0910 0.2575 0.0867 0.0306 5.156 40.623 34.398 3844.906 4.590 153.002 4.058 0.67 378110. 0.6650 18.10 0.1137 0.3119 0.0848 0.0309 5.201 40.974 33.622 3878.139 4.629 149.550 3.932 0.67 378431. 0.6371 21.71 0.1365 0.3627 0.0827 0.0311 5.234 41.236 32.786 3902.962 4.659 145.832 3.810 0.67 378775. 0.6096 25.33 0.1592 0.4100 0.0804 0.0312 5.254 41.395 31.888 3918.024 4.677 141.837 3.691 0.67 379142. 0.5825 28.95 0.1820 0.4539 0.0780 0.0313 5.259 41.436 30.924 3921.932 4.681 137.552 3.576 0.67 379533. 0.5557 32.57 0.2047 0.4947 0.0754 0.0312 5.248 41.346 29.894 3913.338 4.671 132.968 3.465 0.67 379947. 0.5293 36.19 0.2275 0.5326 0.0726 0.0310 5.218 41.110 28.796 3891.071 4.645 128.086 3.357 0.67 380387. 0.5033 39.81 0.2502 0.5675 0.0697 0.0307 5.169 40.721 27.633 3854.261 4.601 122.914 3.252 0.67 380850. 0.4776 43.43 0.2730 0.5998 0.0666 0.0303 5.099 40.173 26.409 3802.342 4.539 117.469 3.150 0.67 381340. 0.4524 47.05 0.2957 0.6294 0.0634 0.0298 5.009 39.461 25.128 3734.933 4.458 111.772 3.052 0.67 381854. 0.4274 50.67 0.3185 0.6565 0.0600 0.0291 4.897 38.582 23.795 3651.736 4.359 105.841 2.956 0.67 382394. 0.4028 54.29 0.3412 0.6810 0.0565 0.0283 4.764 37.533 22.413 3552.481 4.240 99.694 2.862 0.67 382960. 0.3785 57.90 0.3640 0.7031 0.0529 0.0274 4.609 36.312 20.987 3436.898 4.102 93.349 2.770 0.67 383552. 0.3545 61.52 0.3867 0.7226 0.0492 0.0263 4.432 34.915 19.519 3304.725 3.945 86.822 2.679 0.67 384171. 0.3307 65.14 0.4095 0.7394 0.0454 0.0251 4.232 33.341 18.014 3155.706 3.767 80.125 2.589 0.67 384816. 0.3070 68.76 0.4322 0.7534 0.0415 0.0238 4.009 31.586 16.473 2989.617 3.569 73.274 2.499 0.67 385488. 0.2834 72.38 0.4550 0.7643 0.0376 0.0224 3.763 29.649 14.901 2806.225 3.350 66.282 2.409 0.67 386187. 0.2598 76.00 0.4777 0.7715 0.0335 0.0208 3.494 27.527 13.301 2605.419 3.110 59.162 2.316 0.67 386913. 0.2360 79.62 0.5005 0.7743 0.0294 0.0190 3.201 25.221 11.675 2387.118 2.849 51.931 2.218 0.67 387667. 0.2118 83.24 0.5232 0.7715 0.0253 0.0171 2.885 22.730 10.028 2151.364 2.568 44.603 2.114 0.68 388448. 0.1871 86.86 0.5460 0.7608 0.0211 0.0151 2.546 20.056 8.363 1898.335 2.266 37.198 1.998 0.68 389257. 0.1615 90.48 0.5687 0.7386 0.0169 0.0130 2.184 17.205 6.685 1628.410 1.944 29.736 1.862 0.68 390093. 0.1345 94.09 0.5915 0.6971 0.0126 0.0107 1.800 14.181 5.001 1342.215 1.602 22.243 1.690 0.68 390957. 0.1056 97.71 0.6142 0.6191 0.0084 0.0083 1.396 10.995 3.316 1040.679 1.242 14.750 1.445 0.68 391848. 0.0735 101.33 0.6369 0.4553 0.0041 0.0058 0.972 7.659 1.638 724.954 0.865 7.286 1.025 0.68 392764. 0.0367 104.95 0.6597 -0.0439 -0.0002 0.0031 0.516 4.067 -0.081 384.983 0.460 -0.360 -0.095 0.68 393528. 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 0.0952 0.0303 7.271 50.917 47.794 5421.649 5.753 212.590 3.998 0.75 424092. 0.7724 4.09 0.0228 0.0697 0.0938 0.0307 7.365 51.577 47.085 5491.975 5.827 209.432 3.889 0.75 424363. 0.7456 8.18 0.0457 0.1355 0.0922 0.0311 7.452 52.190 46.310 5557.247 5.896 205.986 3.780 0.75 424657. 0.7187 12.26 0.0685 0.1974 0.0906 0.0314 7.531 52.742 45.467 5615.951 5.959 202.237 3.672 0.75 424974. 0.6918 16.35 0.0914 0.2556 0.0887 0.0317 7.599 53.217 44.553 5666.566 6.012 198.170 3.566 0.75 425316. 0.6651 20.44 0.1142 0.3102 0.0868 0.0319 7.654 53.601 43.562 5707.439 6.056 193.765 3.462 0.75 425682. 0.6384 24.53 0.1370 0.3612 0.0846 0.0321 7.693 53.876 42.493 5736.730 6.087 189.007 3.360 0.75 426075. 0.6119 28.61 0.1599 0.4089 0.0823 0.0322 7.714 54.024 41.339 5752.470 6.104 183.877 3.260 0.75 426493. 0.5856 32.70 0.1827 0.4533 0.0799 0.0322 7.714 54.025 40.099 5752.568 6.104 178.360 3.162 0.75 426939. 0.5594 36.79 0.2055 0.4945 0.0772 0.0321 7.691 53.859 38.769 5734.956 6.085 172.445 3.066 0.75 427412. 0.5334 40.88 0.2284 0.5328 0.0744 0.0319 7.641 53.510 37.349 5697.776 6.046 166.130 2.973 0.75 427912. 0.5077 44.96 0.2512 0.5682 0.0714 0.0316 7.563 52.964 35.843 5639.613 5.984 159.428 2.883 0.75 428441. 0.4822 49.05 0.2741 0.6009 0.0682 0.0311 7.455 52.211 34.254 5559.496 5.899 152.362 2.795 0.75 428998. 0.4570 53.14 0.2969 0.6311 0.0649 0.0305 7.318 51.246 32.589 5456.737 5.790 144.958 2.709 0.75 429584. 0.4321 57.23 0.3197 0.6586 0.0615 0.0298 7.149 50.063 30.855 5330.792 5.656 137.243 2.625 0.75 430199. 0.4075 61.31 0.3426 0.6837 0.0579 0.0290 6.948 48.658 29.056 5181.156 5.497 129.242 2.544 0.75 430844. 0.3831 65.40 0.3654 0.7064 0.0542 0.0280 6.715 47.026 27.198 5007.380 5.313 120.977 2.464 0.75 431518. 0.3590 69.49 0.3883 0.7265 0.0504 0.0269 6.449 45.163 25.285 4809.026 5.103 112.469 2.385 0.76 432221. 0.3351 73.58 0.4111 0.7441 0.0465 0.0257 6.150 43.067 23.322 4585.751 4.866 103.737 2.307 0.76 432955. 0.3113 77.66 0.4339 0.7588 0.0425 0.0243 5.816 40.733 21.313 4337.270 4.602 94.799 2.229 0.76 433719. 0.2875 81.75 0.4568 0.7705 0.0384 0.0227 5.449 38.161 19.261 4063.365 4.311 85.672 2.150 0.76 434513. 0.2636 85.84 0.4796 0.7787 0.0342 0.0211 5.048 35.348 17.171 3763.925 3.994 76.376 2.069 0.76 435338. 0.2396 89.93 0.5024 0.7824 0.0300 0.0192 4.612 32.297 15.047 3438.995 3.649 66.929 1.985 0.76 436194. 0.2151 94.01 0.5253 0.7804 0.0257 0.0173 4.142 29.009 12.894 3088.866 3.277 57.353 1.893 0.76 437080. 0.1900 98.10 0.5481 0.7703 0.0213 0.0152 3.640 25.490 10.717 2714.146 2.880 47.671 1.791 0.76 437998. 0.1638 102.19 0.5710 0.7479 0.0170 0.0130 3.106 21.749 8.523 2315.852 2.457 37.912 1.669 0.76 438947. 0.1362 106.28 0.5938 0.7045 0.0126 0.0106 2.542 17.801 6.319 1895.511 2.011 28.109 1.512 0.76 439927. 0.1062 110.36 0.6166 0.6205 0.0082 0.0081 1.952 13.667 4.114 1455.242 1.544 18.301 1.282 0.76 440937. 0.0727 114.45 0.6395 0.4374 0.0038 0.0056 1.338 9.368 1.917 997.549 1.058 8.528 0.872 0.77 441974. 0.0337 118.54 0.6623 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 0.0976 0.0344 11.317 71.331 60.484 8439.293 8.059 269.035 3.251 0.83 471108. 0.7064 4.52 0.0227 0.0632 0.0962 0.0346 11.384 71.754 59.640 8489.312 8.107 265.279 3.186 0.83 471410. 0.6876 9.05 0.0455 0.1238 0.0947 0.0348 11.439 72.099 58.711 8530.159 8.146 261.149 3.122 0.83 471738. 0.6684 13.57 0.0682 0.1818 0.0931 0.0349 11.480 72.355 57.695 8560.442 8.175 256.628 3.057 0.83 472092. 0.6488 18.09 0.0910 0.2373 0.0913 0.0350 11.504 72.509 56.586 8578.646 8.192 251.693 2.992 0.83 472473. 0.6288 22.61 0.1137 0.2901 0.0894 0.0350 11.510 72.547 55.378 8583.113 8.196 246.321 2.926 0.83 472882. 0.6085 27.14 0.1365 0.3403 0.0872 0.0350 11.495 72.452 54.067 8571.941 8.186 240.488 2.861 0.83 473319. 0.5878 31.66 0.1592 0.3879 0.0849 0.0349 11.456 72.207 52.647 8542.991 8.158 234.172 2.795 0.83 473786. 0.5667 36.18 0.1819 0.4329 0.0825 0.0347 11.391 71.794 51.113 8494.041 8.111 227.353 2.729 0.83 474283. 0.5452 40.70 0.2047 0.4753 0.0798 0.0344 11.295 71.191 49.464 8422.771 8.043 220.014 2.664 0.83 474811. 0.5234 45.23 0.2274 0.5151 0.0770 0.0340 11.167 70.383 47.696 8327.128 7.952 212.153 2.598 0.84 475369. 0.5013 49.75 0.2502 0.5523 0.0739 0.0335 11.004 69.355 45.815 8205.477 7.836 203.785 2.532 0.84 475958. 0.4790 54.27 0.2729 0.5870 0.0707 0.0329 10.804 68.098 43.826 8056.746 7.694 194.939 2.467 0.84 476578. 0.4564 58.79 0.2956 0.6192 0.0673 0.0322 10.567 66.605 41.737 7880.165 7.525 185.648 2.402 0.84 477230. 0.4337 63.32 0.3184 0.6489 0.0638 0.0313 10.292 64.872 39.557 7675.070 7.329 175.948 2.338 0.84 477914. 0.4108 67.84 0.3411 0.6761 0.0602 0.0304 9.978 62.891 37.291 7440.740 7.105 165.873 2.273 0.84 478630. 0.3879 72.36 0.3639 0.7007 0.0564 0.0293 9.624 60.657 34.949 7176.381 6.853 155.451 2.209 0.84 479378. 0.3649 76.88 0.3866 0.7227 0.0525 0.0281 9.229 58.171 32.534 6882.344 6.572 144.711 2.144 0.84 480158. 0.3417 81.41 0.4094 0.7418 0.0485 0.0268 8.795 55.434 30.053 6558.438 6.263 133.676 2.078 0.84 480972. 0.3184 85.93 0.4321 0.7578 0.0444 0.0253 8.319 52.432 27.511 6203.279 5.924 122.371 2.012 0.84 481818. 0.2948 90.45 0.4548 0.7700 0.0402 0.0237 7.803 49.183 24.913 5818.939 5.557 110.814 1.942 0.84 482698. 0.2708 94.97 0.4776 0.7778 0.0359 0.0221 7.249 45.690 22.264 5405.631 5.162 99.029 1.868 0.84 483611. 0.2463 99.50 0.5003 0.7804 0.0316 0.0202 6.653 41.932 19.569 4961.106 4.738 87.042 1.789 0.84 484558. 0.2211 104.02 0.5231 0.7759 0.0272 0.0183 6.018 37.928 16.834 4487.292 4.285 74.877 1.702 0.84 485538. 0.1951 108.54 0.5458 0.7616 0.0227 0.0163 5.346 33.693 14.066 3986.263 3.807 62.564 1.600 0.85 486552. 0.1677 113.06 0.5686 0.7322 0.0182 0.0141 4.641 29.252 11.272 3460.905 3.305 50.138 1.477 0.85 487601. 0.1386 117.59 0.5913 0.6788 0.0137 0.0119 3.909 24.637 8.462 2914.876 2.784 37.639 1.317 0.85 488683. 0.1070 122.11 0.6140 0.5827 0.0091 0.0096 3.155 19.885 5.646 2352.639 2.247 25.115 1.089 0.85 489798. 0.0723 126.63 0.6368 0.4016 0.0046 0.0073 2.386 15.038 2.837 1779.140 1.699 12.620 0.723 0.85 490944. 0.0340 131.16 0.6595 0.0008 0.0000 0.0048 1.590 10.020 0.004 1185.507 1.132 0.017 0.001 0.85 492028. 0.0000