21.5x10.5PN (215x105PN.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 0.0848 0.0319 0.012 0.746 0.580 8.822 0.084 2.579 29.811 0.09 49137. 0.6190 0.45 0.0220 0.0571 0.0834 0.0322 0.012 0.753 0.570 8.907 0.085 2.535 29.027 0.09 49166. 0.5976 0.90 0.0440 0.1111 0.0819 0.0324 0.012 0.759 0.559 8.985 0.086 2.489 28.245 0.09 49197. 0.5761 1.35 0.0661 0.1621 0.0802 0.0327 0.012 0.765 0.548 9.053 0.086 2.438 27.467 0.09 49231. 0.5545 1.80 0.0881 0.2101 0.0785 0.0329 0.012 0.770 0.536 9.111 0.087 2.385 26.693 0.09 49267. 0.5329 2.24 0.1101 0.2550 0.0766 0.0331 0.012 0.774 0.523 9.155 0.087 2.328 25.925 0.09 49306. 0.5114 2.69 0.1321 0.2971 0.0746 0.0332 0.012 0.776 0.510 9.185 0.088 2.267 25.164 0.09 49348. 0.4898 3.14 0.1542 0.3362 0.0724 0.0332 0.012 0.777 0.495 9.197 0.088 2.202 24.410 0.09 49392. 0.4683 3.59 0.1762 0.3725 0.0701 0.0332 0.012 0.777 0.479 9.190 0.088 2.132 23.663 0.09 49439. 0.4467 4.04 0.1982 0.4059 0.0677 0.0331 0.012 0.774 0.463 9.160 0.087 2.059 22.922 0.09 49489. 0.4252 4.49 0.2202 0.4365 0.0652 0.0329 0.012 0.770 0.445 9.107 0.087 1.982 22.188 0.09 49543. 0.4038 4.94 0.2423 0.4644 0.0625 0.0326 0.012 0.763 0.427 9.029 0.086 1.900 21.458 0.09 49599. 0.3824 5.39 0.2643 0.4895 0.0597 0.0322 0.012 0.754 0.408 8.925 0.085 1.815 20.732 0.09 49658. 0.3610 5.83 0.2863 0.5117 0.0568 0.0318 0.012 0.743 0.388 8.795 0.084 1.726 20.007 0.09 49720. 0.3398 6.28 0.3083 0.5311 0.0537 0.0312 0.012 0.730 0.367 8.638 0.082 1.633 19.281 0.09 49785. 0.3186 6.73 0.3303 0.5475 0.0506 0.0305 0.011 0.715 0.346 8.454 0.081 1.538 18.550 0.09 49854. 0.2974 7.18 0.3524 0.5607 0.0474 0.0298 0.011 0.697 0.324 8.242 0.079 1.440 17.812 0.09 49926. 0.2763 7.63 0.3744 0.5706 0.0440 0.0289 0.011 0.676 0.301 8.001 0.076 1.339 17.060 0.09 50001. 0.2552 8.08 0.3964 0.5769 0.0406 0.0279 0.010 0.654 0.278 7.733 0.074 1.235 16.289 0.09 50079. 0.2341 8.53 0.4184 0.5791 0.0372 0.0268 0.010 0.628 0.254 7.435 0.071 1.129 15.492 0.09 50161. 0.2129 8.98 0.4405 0.5768 0.0336 0.0257 0.010 0.601 0.230 7.107 0.068 1.022 14.659 0.09 50246. 0.1916 9.42 0.4625 0.5692 0.0300 0.0244 0.009 0.571 0.205 6.750 0.064 0.912 13.777 0.09 50335. 0.1701 9.87 0.4845 0.5553 0.0263 0.0230 0.009 0.538 0.180 6.363 0.061 0.801 12.829 0.09 50427. 0.1484 10.32 0.5065 0.5337 0.0226 0.0215 0.008 0.503 0.155 5.947 0.057 0.688 11.793 0.09 50522. 0.1264 10.77 0.5286 0.5022 0.0189 0.0199 0.007 0.465 0.129 5.501 0.053 0.574 10.636 0.09 50621. 0.1042 11.22 0.5506 0.4579 0.0151 0.0181 0.007 0.425 0.103 5.025 0.048 0.459 9.310 0.09 50723. 0.0815 11.67 0.5726 0.3961 0.0113 0.0163 0.006 0.382 0.077 4.522 0.043 0.343 7.743 0.09 50829. 0.0587 12.12 0.5946 0.3091 0.0075 0.0144 0.005 0.337 0.051 3.992 0.038 0.228 5.819 0.09 50938. 0.0359 12.57 0.6166 0.1840 0.0037 0.0124 0.005 0.290 0.025 3.437 0.033 0.113 3.339 0.09 51050. 0.0145 13.02 0.6387 -0.0048 -0.0001 0.0103 0.004 0.241 -0.001 2.856 0.027 -0.002 -0.084 0.09 51163. 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 0.0853 0.0288 0.086 2.701 2.332 63.916 0.305 10.372 16.547 0.17 98272. 0.6889 0.90 0.0221 0.0636 0.0839 0.0292 0.087 2.733 2.292 64.661 0.309 10.197 16.080 0.17 98330. 0.6639 1.80 0.0442 0.1235 0.0823 0.0295 0.088 2.762 2.250 65.349 0.312 10.009 15.618 0.17 98393. 0.6388 2.70 0.0664 0.1798 0.0807 0.0298 0.088 2.788 2.205 65.965 0.315 9.808 15.162 0.17 98461. 0.6139 3.61 0.0885 0.2326 0.0789 0.0300 0.089 2.810 2.157 66.492 0.317 9.593 14.712 0.17 98534. 0.5891 4.51 0.1106 0.2820 0.0770 0.0302 0.090 2.828 2.105 66.915 0.319 9.363 14.269 0.17 98613. 0.5645 5.41 0.1327 0.3280 0.0750 0.0303 0.090 2.841 2.050 67.215 0.321 9.118 13.833 0.17 98696. 0.5400 6.31 0.1548 0.3709 0.0728 0.0304 0.090 2.847 1.991 67.372 0.322 8.857 13.405 0.17 98786. 0.5158 7.21 0.1770 0.4106 0.0705 0.0304 0.090 2.847 1.929 67.367 0.322 8.578 12.985 0.17 98881. 0.4917 8.11 0.1991 0.4472 0.0681 0.0303 0.090 2.839 1.862 67.182 0.321 8.283 12.572 0.17 98982. 0.4678 9.02 0.2212 0.4809 0.0655 0.0302 0.090 2.823 1.792 66.801 0.319 7.971 12.167 0.17 99089. 0.4441 9.92 0.2433 0.5117 0.0628 0.0299 0.089 2.798 1.718 66.212 0.316 7.642 11.769 0.17 99202. 0.4206 10.82 0.2654 0.5396 0.0600 0.0295 0.088 2.764 1.641 65.409 0.312 7.298 11.377 0.17 99321. 0.3973 11.72 0.2876 0.5647 0.0571 0.0291 0.086 2.721 1.560 64.384 0.307 6.939 10.990 0.17 99447. 0.3743 12.62 0.3097 0.5869 0.0540 0.0285 0.085 2.668 1.476 63.135 0.301 6.567 10.607 0.17 99578. 0.3514 13.52 0.3318 0.6062 0.0508 0.0278 0.083 2.606 1.390 61.654 0.294 6.183 10.226 0.17 99717. 0.3287 14.42 0.3539 0.6225 0.0476 0.0271 0.080 2.533 1.301 59.939 0.286 5.787 9.845 0.17 99862. 0.3062 15.33 0.3760 0.6357 0.0442 0.0262 0.078 2.450 1.210 57.985 0.277 5.380 9.462 0.17 100013. 0.2837 16.23 0.3982 0.6455 0.0408 0.0252 0.075 2.358 1.116 55.786 0.266 4.964 9.073 0.17 100171. 0.2613 17.13 0.4203 0.6515 0.0373 0.0241 0.072 2.254 1.020 53.340 0.255 4.538 8.676 0.17 100336. 0.2389 18.03 0.4424 0.6533 0.0338 0.0229 0.068 2.140 0.923 50.642 0.242 4.104 8.264 0.17 100508. 0.2165 18.93 0.4645 0.6501 0.0301 0.0215 0.064 2.015 0.824 47.691 0.228 3.663 7.832 0.17 100686. 0.1938 19.83 0.4866 0.6408 0.0264 0.0201 0.060 1.880 0.723 44.485 0.212 3.215 7.370 0.17 100871. 0.1708 20.74 0.5088 0.6240 0.0227 0.0185 0.055 1.734 0.621 41.024 0.196 2.762 6.864 0.17 101064. 0.1475 21.64 0.5309 0.5972 0.0189 0.0168 0.050 1.577 0.518 37.311 0.178 2.304 6.296 0.17 101263. 0.1235 22.54 0.5530 0.5566 0.0152 0.0151 0.045 1.409 0.414 33.350 0.159 1.842 5.633 0.17 101469. 0.0988 23.44 0.5751 0.4958 0.0113 0.0132 0.039 1.232 0.310 29.149 0.139 1.379 4.825 0.17 101682. 0.0732 24.34 0.5972 0.4032 0.0075 0.0112 0.033 1.045 0.206 24.721 0.118 0.916 3.778 0.17 101902. 0.0467 25.24 0.6194 0.2554 0.0037 0.0091 0.027 0.849 0.102 20.080 0.096 0.454 2.308 0.17 102128. 0.0201 26.14 0.6415 -0.0053 -0.0001 0.0069 0.020 0.643 -0.002 15.204 0.073 -0.007 -0.046 0.17 102350. 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 0.0858 0.0277 0.278 5.844 5.279 207.417 0.660 23.479 11.543 0.26 147402. 0.7231 1.36 0.0222 0.0666 0.0844 0.0281 0.282 5.918 5.190 210.037 0.669 23.085 11.208 0.26 147490. 0.6962 2.71 0.0443 0.1292 0.0828 0.0284 0.285 5.986 5.095 212.464 0.676 22.662 10.877 0.26 147586. 0.6694 4.07 0.0665 0.1880 0.0812 0.0287 0.288 6.047 4.993 214.643 0.683 22.208 10.551 0.26 147688. 0.6428 5.42 0.0887 0.2431 0.0794 0.0290 0.290 6.100 4.884 216.523 0.689 21.723 10.230 0.26 147798. 0.6164 6.78 0.1108 0.2946 0.0775 0.0292 0.292 6.143 4.767 218.043 0.694 21.204 9.916 0.26 147916. 0.5903 8.13 0.1330 0.3425 0.0755 0.0293 0.294 6.174 4.642 219.141 0.698 20.649 9.609 0.26 148043. 0.5645 9.49 0.1552 0.3871 0.0733 0.0294 0.295 6.191 4.509 219.749 0.699 20.058 9.308 0.26 148177. 0.5389 10.84 0.1773 0.4284 0.0710 0.0294 0.295 6.193 4.368 219.802 0.700 19.428 9.013 0.26 148321. 0.5136 12.20 0.1995 0.4665 0.0686 0.0293 0.294 6.177 4.218 219.233 0.698 18.760 8.726 0.26 148473. 0.4886 13.55 0.2217 0.5017 0.0660 0.0292 0.292 6.142 4.059 217.989 0.694 18.052 8.445 0.26 148634. 0.4639 14.91 0.2438 0.5339 0.0633 0.0289 0.290 6.086 3.891 216.029 0.688 17.308 8.170 0.26 148804. 0.4394 16.26 0.2660 0.5632 0.0604 0.0285 0.286 6.010 3.716 213.327 0.679 16.528 7.900 0.26 148984. 0.4152 17.62 0.2882 0.5897 0.0574 0.0281 0.281 5.913 3.533 209.860 0.668 15.715 7.636 0.26 149173. 0.3914 18.97 0.3103 0.6135 0.0544 0.0275 0.276 5.793 3.344 205.611 0.654 14.872 7.376 0.26 149372. 0.3677 20.33 0.3325 0.6343 0.0512 0.0268 0.269 5.651 3.148 200.562 0.638 14.001 7.118 0.26 149580. 0.3444 21.68 0.3547 0.6523 0.0479 0.0260 0.261 5.485 2.946 194.698 0.620 13.104 6.863 0.26 149798. 0.3212 23.04 0.3768 0.6673 0.0445 0.0251 0.252 5.297 2.739 188.000 0.598 12.182 6.608 0.26 150027. 0.2982 24.39 0.3990 0.6791 0.0411 0.0241 0.242 5.084 2.527 180.455 0.574 11.238 6.350 0.26 150265. 0.2752 25.75 0.4212 0.6873 0.0376 0.0230 0.231 4.847 2.310 172.046 0.548 10.274 6.089 0.26 150513. 0.2523 27.10 0.4433 0.6916 0.0340 0.0218 0.218 4.586 2.089 162.764 0.518 9.290 5.820 0.26 150772. 0.2294 28.46 0.4655 0.6912 0.0303 0.0204 0.205 4.299 1.864 152.597 0.486 8.290 5.540 0.26 151041. 0.2062 29.81 0.4877 0.6851 0.0266 0.0189 0.190 3.988 1.636 141.543 0.451 7.276 5.242 0.26 151320. 0.1828 31.17 0.5098 0.6717 0.0228 0.0173 0.174 3.651 1.405 129.601 0.413 6.248 4.916 0.26 151609. 0.1589 32.52 0.5320 0.6487 0.0190 0.0156 0.157 3.290 1.171 116.780 0.372 5.211 4.550 0.26 151909. 0.1343 33.88 0.5542 0.6120 0.0152 0.0138 0.138 2.905 0.937 103.098 0.328 4.166 4.120 0.26 152220. 0.1087 35.23 0.5763 0.5543 0.0114 0.0118 0.119 2.496 0.701 88.583 0.282 3.118 3.589 0.26 152540. 0.0819 36.59 0.5985 0.4619 0.0076 0.0098 0.098 2.065 0.465 73.278 0.233 2.069 2.879 0.26 152871. 0.0536 37.94 0.6207 0.3038 0.0037 0.0077 0.077 1.612 0.230 57.233 0.182 1.025 1.827 0.26 153212. 0.0239 39.30 0.6428 -0.0096 -0.0001 0.0054 0.054 1.136 -0.005 40.310 0.128 -0.022 -0.056 0.26 153540. 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 0.0865 0.0273 0.648 10.214 9.459 483.364 1.154 42.074 8.876 0.34 196527. 0.7443 1.81 0.0222 0.0683 0.0851 0.0276 0.657 10.349 9.301 489.752 1.169 41.372 8.614 0.34 196645. 0.7163 3.62 0.0444 0.1326 0.0835 0.0280 0.665 10.474 9.132 495.674 1.183 40.617 8.356 0.34 196772. 0.6885 5.43 0.0666 0.1928 0.0818 0.0283 0.672 10.586 8.950 501.000 1.196 39.808 8.102 0.34 196910. 0.6609 7.24 0.0888 0.2492 0.0801 0.0285 0.678 10.684 8.755 505.601 1.207 38.941 7.854 0.34 197058. 0.6336 9.05 0.1110 0.3019 0.0782 0.0287 0.683 10.763 8.546 509.334 1.216 38.013 7.610 0.34 197216. 0.6066 10.86 0.1332 0.3509 0.0761 0.0289 0.687 10.820 8.323 512.049 1.222 37.022 7.373 0.34 197385. 0.5800 12.67 0.1554 0.3965 0.0739 0.0290 0.689 10.852 8.085 513.583 1.226 35.964 7.141 0.34 197565. 0.5536 14.48 0.1776 0.4388 0.0716 0.0290 0.689 10.856 7.832 513.773 1.227 34.837 6.914 0.34 197757. 0.5276 16.29 0.1998 0.4779 0.0692 0.0289 0.687 10.829 7.563 512.464 1.223 33.640 6.694 0.34 197961. 0.5019 18.10 0.2220 0.5140 0.0666 0.0287 0.683 10.766 7.278 509.521 1.216 32.372 6.479 0.34 198177. 0.4766 19.91 0.2442 0.5471 0.0638 0.0285 0.677 10.668 6.978 504.847 1.205 31.037 6.269 0.34 198405. 0.4515 21.72 0.2664 0.5773 0.0609 0.0281 0.668 10.531 6.663 498.373 1.190 29.639 6.064 0.34 198646. 0.4268 23.52 0.2886 0.6048 0.0579 0.0276 0.657 10.355 6.336 490.049 1.170 28.181 5.864 0.34 198899. 0.4025 25.33 0.3108 0.6295 0.0548 0.0271 0.643 10.139 5.996 479.830 1.146 26.669 5.668 0.34 199165. 0.3784 27.14 0.3330 0.6514 0.0516 0.0264 0.627 9.882 5.644 467.673 1.116 25.106 5.474 0.34 199444. 0.3546 28.95 0.3552 0.6706 0.0483 0.0256 0.608 9.583 5.282 453.536 1.083 23.496 5.283 0.34 199736. 0.3311 30.76 0.3774 0.6868 0.0449 0.0247 0.587 9.242 4.911 437.380 1.044 21.842 5.092 0.34 200041. 0.3077 32.57 0.3996 0.6999 0.0414 0.0236 0.562 8.857 4.530 419.166 1.001 20.148 4.902 0.34 200360. 0.2844 34.38 0.4218 0.7097 0.0379 0.0225 0.535 8.428 4.141 398.860 0.952 18.417 4.709 0.34 200693. 0.2612 36.19 0.4440 0.7158 0.0342 0.0212 0.505 7.954 3.744 376.431 0.899 16.653 4.511 0.34 201038. 0.2380 38.00 0.4662 0.7174 0.0305 0.0199 0.472 7.435 3.340 351.860 0.840 14.858 4.306 0.35 201398. 0.2146 39.81 0.4884 0.7136 0.0268 0.0183 0.436 6.870 2.931 325.134 0.776 13.037 4.089 0.35 201772. 0.1909 41.62 0.5106 0.7030 0.0230 0.0167 0.397 6.260 2.516 296.255 0.707 11.193 3.853 0.35 202159. 0.1666 43.43 0.5328 0.6830 0.0192 0.0150 0.356 5.605 2.098 265.245 0.633 9.331 3.587 0.35 202560. 0.1417 45.24 0.5550 0.6495 0.0153 0.0131 0.311 4.905 1.676 232.145 0.554 7.456 3.275 0.35 202975. 0.1156 47.05 0.5772 0.5951 0.0115 0.0111 0.264 4.163 1.253 197.029 0.470 5.574 2.885 0.35 203404. 0.0881 48.86 0.5994 0.5042 0.0076 0.0090 0.215 3.381 0.830 159.998 0.382 3.693 2.354 0.35 203847. 0.0585 50.67 0.6216 0.3403 0.0037 0.0068 0.163 2.561 0.409 121.177 0.289 1.820 1.532 0.35 204302. 0.0267 52.48 0.6438 -0.0197 -0.0001 0.0045 0.107 1.691 -0.015 80.026 0.191 -0.067 -0.086 0.35 204728. 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 0.0874 0.0272 1.261 15.890 14.931 939.976 1.795 66.412 7.205 0.43 245642. 0.7591 2.26 0.0222 0.0693 0.0859 0.0275 1.278 16.106 14.684 952.752 1.820 65.314 6.990 0.43 245790. 0.7304 4.53 0.0444 0.1345 0.0844 0.0279 1.294 16.306 14.418 964.595 1.842 64.132 6.780 0.43 245951. 0.7019 6.79 0.0666 0.1956 0.0827 0.0282 1.308 16.486 14.133 975.248 1.863 62.863 6.573 0.43 246123. 0.6738 9.05 0.0888 0.2528 0.0809 0.0284 1.320 16.642 13.827 984.455 1.880 61.502 6.371 0.43 246309. 0.6459 11.31 0.1110 0.3062 0.0790 0.0287 1.330 16.768 13.499 991.931 1.894 60.046 6.173 0.43 246507. 0.6184 13.58 0.1333 0.3559 0.0770 0.0288 1.338 16.860 13.149 997.378 1.905 58.488 5.980 0.43 246720. 0.5912 15.84 0.1555 0.4022 0.0748 0.0289 1.342 16.913 12.775 1000.475 1.911 56.824 5.792 0.43 246946. 0.5644 18.10 0.1777 0.4451 0.0724 0.0289 1.342 16.920 12.377 1000.899 1.912 55.051 5.609 0.43 247187. 0.5380 20.37 0.1999 0.4849 0.0700 0.0288 1.339 16.876 11.953 998.335 1.907 53.166 5.430 0.43 247443. 0.5119 22.63 0.2221 0.5215 0.0673 0.0287 1.331 16.778 11.504 992.519 1.896 51.169 5.257 0.43 247714. 0.4862 24.89 0.2443 0.5553 0.0646 0.0284 1.319 16.621 11.031 983.253 1.878 49.065 5.088 0.43 248000. 0.4608 27.16 0.2665 0.5862 0.0617 0.0280 1.301 16.404 10.535 970.402 1.853 46.860 4.924 0.43 248302. 0.4358 29.42 0.2887 0.6144 0.0586 0.0276 1.279 16.125 10.018 953.863 1.822 44.561 4.764 0.43 248619. 0.4111 31.68 0.3109 0.6398 0.0555 0.0270 1.252 15.781 9.482 933.546 1.783 42.174 4.607 0.43 248953. 0.3868 33.94 0.3331 0.6626 0.0522 0.0263 1.219 15.372 8.927 909.369 1.737 39.707 4.453 0.43 249302. 0.3627 36.21 0.3553 0.6826 0.0489 0.0255 1.182 14.897 8.355 881.249 1.683 37.165 4.300 0.43 249668. 0.3389 38.47 0.3776 0.6998 0.0455 0.0245 1.139 14.354 7.768 849.110 1.622 34.554 4.150 0.43 250051. 0.3154 40.73 0.3998 0.7141 0.0419 0.0235 1.090 13.741 7.167 812.867 1.552 31.879 3.999 0.43 250450. 0.2919 43.00 0.4220 0.7252 0.0383 0.0223 1.036 13.058 6.552 772.460 1.475 29.145 3.847 0.43 250866. 0.2685 45.26 0.4442 0.7327 0.0347 0.0210 0.976 12.304 5.926 727.828 1.390 26.357 3.693 0.43 251299. 0.2451 47.52 0.4664 0.7360 0.0309 0.0196 0.910 11.477 5.288 678.927 1.297 23.522 3.533 0.43 251750. 0.2215 49.78 0.4886 0.7342 0.0272 0.0181 0.839 10.578 4.641 625.736 1.195 20.643 3.364 0.43 252217. 0.1976 52.05 0.5108 0.7259 0.0233 0.0164 0.762 9.606 3.986 568.258 1.085 17.729 3.181 0.43 252702. 0.1732 54.31 0.5330 0.7087 0.0195 0.0146 0.679 8.563 3.324 506.535 0.967 14.786 2.977 0.43 253204. 0.1480 56.57 0.5552 0.6785 0.0156 0.0127 0.591 7.449 2.658 440.652 0.842 11.822 2.736 0.43 253724. 0.1216 58.84 0.5774 0.6277 0.0116 0.0107 0.497 6.267 1.989 370.750 0.708 8.848 2.434 0.43 254261. 0.0936 61.10 0.5996 0.5402 0.0077 0.0086 0.398 5.021 1.321 297.038 0.567 5.874 2.017 0.43 254815. 0.0632 63.36 0.6219 0.3754 0.0038 0.0063 0.295 3.715 0.655 219.765 0.420 2.913 1.352 0.44 255384. 0.0298 65.63 0.6441 -0.0164 -0.0001 0.0040 0.185 2.328 -0.017 137.708 0.263 -0.077 -0.057 0.44 255910. 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 0.0885 0.0273 2.189 22.994 21.776 1632.249 2.598 96.860 6.051 0.51 294745. 0.7699 2.71 0.0222 0.0698 0.0871 0.0277 2.219 23.312 21.421 1654.843 2.634 95.279 5.871 0.51 294924. 0.7409 5.42 0.0444 0.1354 0.0855 0.0280 2.247 23.607 21.037 1675.774 2.667 93.575 5.694 0.51 295117. 0.7121 8.14 0.0666 0.1969 0.0838 0.0283 2.272 23.872 20.626 1694.593 2.697 91.744 5.521 0.51 295325. 0.6836 10.85 0.0887 0.2545 0.0820 0.0286 2.294 24.101 20.184 1710.846 2.723 89.778 5.351 0.51 295548. 0.6555 13.56 0.1109 0.3083 0.0801 0.0288 2.312 24.287 19.710 1724.043 2.744 87.672 5.186 0.51 295787. 0.6277 16.27 0.1331 0.3585 0.0781 0.0290 2.325 24.422 19.204 1733.655 2.759 85.417 5.024 0.51 296043. 0.6003 18.99 0.1553 0.4051 0.0758 0.0291 2.332 24.499 18.662 1739.127 2.768 83.008 4.867 0.51 296316. 0.5733 21.70 0.1775 0.4485 0.0735 0.0291 2.333 24.510 18.084 1739.889 2.769 80.438 4.714 0.51 296605. 0.5466 24.41 0.1997 0.4886 0.0710 0.0290 2.327 24.447 17.469 1735.394 2.762 77.703 4.566 0.51 296913. 0.5203 27.12 0.2218 0.5258 0.0684 0.0288 2.313 24.303 16.818 1725.166 2.746 74.805 4.422 0.51 297239. 0.4944 29.84 0.2440 0.5600 0.0656 0.0286 2.292 24.073 16.130 1708.858 2.720 71.748 4.281 0.51 297583. 0.4689 32.55 0.2662 0.5915 0.0626 0.0282 2.261 23.754 15.410 1686.230 2.684 68.543 4.145 0.51 297945. 0.4437 35.26 0.2884 0.6202 0.0596 0.0277 2.222 23.344 14.658 1657.106 2.637 65.200 4.012 0.51 298327. 0.4188 37.97 0.3106 0.6463 0.0564 0.0271 2.174 22.840 13.878 1621.329 2.580 61.728 3.882 0.51 298727. 0.3943 40.69 0.3328 0.6698 0.0531 0.0264 2.117 22.240 13.070 1578.759 2.513 58.137 3.755 0.52 299147. 0.3702 43.40 0.3549 0.6906 0.0497 0.0256 2.051 21.543 12.238 1529.253 2.434 54.436 3.630 0.52 299587. 0.3462 46.11 0.3771 0.7087 0.0463 0.0246 1.975 20.746 11.383 1472.676 2.344 50.633 3.506 0.52 300046. 0.3225 48.82 0.3993 0.7240 0.0427 0.0236 1.889 19.847 10.507 1408.896 2.242 46.736 3.383 0.52 300525. 0.2990 51.54 0.4215 0.7362 0.0391 0.0224 1.794 18.846 9.611 1337.793 2.129 42.752 3.259 0.52 301024. 0.2755 54.25 0.4437 0.7451 0.0354 0.0211 1.689 17.739 8.698 1259.266 2.004 38.689 3.133 0.52 301544. 0.2519 56.96 0.4659 0.7500 0.0316 0.0196 1.573 16.527 7.769 1173.238 1.867 34.555 3.003 0.52 302084. 0.2282 59.67 0.4880 0.7501 0.0277 0.0180 1.448 15.209 6.825 1079.669 1.718 30.358 2.867 0.52 302644. 0.2042 62.39 0.5102 0.7441 0.0239 0.0164 1.312 13.785 5.869 978.564 1.557 26.107 2.721 0.52 303225. 0.1797 65.10 0.5324 0.7297 0.0199 0.0145 1.167 12.256 4.904 869.993 1.385 21.813 2.557 0.52 303827. 0.1544 67.81 0.5546 0.7030 0.0160 0.0126 1.011 10.623 3.932 754.102 1.200 17.488 2.365 0.52 304450. 0.1278 70.52 0.5768 0.6566 0.0120 0.0106 0.846 8.891 2.955 631.136 1.004 13.145 2.124 0.52 305093. 0.0996 73.24 0.5990 0.5747 0.0080 0.0084 0.672 7.064 1.979 501.457 0.798 8.802 1.790 0.52 305756. 0.0687 75.95 0.6211 0.4158 0.0041 0.0061 0.490 5.149 1.006 365.508 0.582 4.476 1.249 0.52 306438. 0.0342 78.66 0.6433 0.0205 0.0001 0.0037 0.298 3.126 0.029 221.910 0.353 0.129 0.060 0.52 307088. 0.0003 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 0.0899 0.0276 3.521 31.704 30.109 2625.674 3.582 133.924 5.201 0.60 343831. 0.7782 3.17 0.0222 0.0702 0.0885 0.0280 3.571 32.151 29.624 2662.658 3.632 131.768 5.046 0.60 344041. 0.7489 6.34 0.0445 0.1361 0.0869 0.0284 3.617 32.564 29.101 2696.872 3.679 129.439 4.894 0.60 344269. 0.7199 9.52 0.0667 0.1979 0.0852 0.0287 3.658 32.935 28.537 2727.578 3.721 126.932 4.745 0.60 344514. 0.6912 12.69 0.0889 0.2558 0.0834 0.0290 3.693 33.254 27.931 2754.033 3.757 124.236 4.600 0.60 344776. 0.6629 15.86 0.1112 0.3099 0.0815 0.0292 3.722 33.512 27.280 2775.434 3.786 121.341 4.458 0.60 345058. 0.6349 19.03 0.1334 0.3604 0.0794 0.0294 3.743 33.699 26.583 2790.918 3.807 118.239 4.320 0.60 345359. 0.6073 22.20 0.1556 0.4074 0.0771 0.0295 3.754 33.804 25.836 2799.589 3.819 114.919 4.186 0.60 345680. 0.5801 25.37 0.1779 0.4511 0.0748 0.0295 3.756 33.815 25.039 2800.515 3.820 111.374 4.055 0.60 346021. 0.5533 28.55 0.2001 0.4916 0.0722 0.0294 3.745 33.722 24.190 2792.801 3.810 107.597 3.929 0.60 346383. 0.5268 31.72 0.2223 0.5292 0.0695 0.0292 3.722 33.515 23.289 2775.675 3.787 103.590 3.806 0.60 346767. 0.5008 34.89 0.2446 0.5638 0.0667 0.0289 3.686 33.188 22.338 2748.564 3.750 99.360 3.686 0.60 347171. 0.4750 38.06 0.2668 0.5957 0.0637 0.0285 3.636 32.735 21.340 2711.086 3.698 94.922 3.570 0.60 347598. 0.4497 41.23 0.2890 0.6250 0.0606 0.0280 3.571 32.154 20.299 2662.958 3.633 90.288 3.457 0.60 348046. 0.4247 44.40 0.3113 0.6516 0.0574 0.0274 3.492 31.442 19.216 2603.943 3.552 85.475 3.347 0.60 348517. 0.4001 47.58 0.3335 0.6756 0.0540 0.0267 3.398 30.595 18.097 2533.818 3.457 80.494 3.239 0.60 349010. 0.3757 50.75 0.3557 0.6971 0.0506 0.0258 3.289 29.611 16.942 2452.359 3.345 75.358 3.133 0.60 349526. 0.3517 53.92 0.3780 0.7160 0.0470 0.0248 3.164 28.488 15.755 2359.354 3.219 70.080 3.029 0.60 350066. 0.3278 57.09 0.4002 0.7320 0.0434 0.0237 3.023 27.223 14.539 2254.590 3.076 64.669 2.925 0.60 350628. 0.3041 60.26 0.4225 0.7452 0.0397 0.0225 2.867 25.814 13.295 2137.883 2.916 59.136 2.821 0.60 351214. 0.2804 63.43 0.4447 0.7550 0.0359 0.0212 2.694 24.259 12.026 2009.067 2.741 53.492 2.715 0.60 351824. 0.2567 66.61 0.4669 0.7611 0.0321 0.0197 2.505 22.556 10.735 1868.021 2.548 47.748 2.606 0.60 352457. 0.2329 69.78 0.4892 0.7625 0.0281 0.0181 2.299 20.704 9.423 1714.685 2.339 41.915 2.493 0.60 353115. 0.2086 72.95 0.5114 0.7580 0.0242 0.0163 2.077 18.704 8.095 1549.071 2.113 36.007 2.370 0.61 353796. 0.1839 76.12 0.5336 0.7454 0.0202 0.0144 1.839 16.558 6.753 1371.292 1.871 30.037 2.234 0.61 354502. 0.1583 79.29 0.5559 0.7206 0.0161 0.0124 1.585 14.267 5.401 1181.598 1.612 24.022 2.073 0.61 355232. 0.1314 82.46 0.5781 0.6762 0.0121 0.0103 1.315 11.838 4.043 980.396 1.337 17.983 1.870 0.61 355986. 0.1025 85.64 0.6003 0.5951 0.0080 0.0081 1.030 9.277 2.685 768.291 1.048 11.943 1.585 0.61 356763. 0.0708 88.81 0.6226 0.4309 0.0040 0.0057 0.732 6.593 1.332 546.011 0.745 5.926 1.107 0.61 357562. 0.0348 91.98 0.6448 -0.0263 -0.0001 0.0032 0.413 3.721 -0.044 308.169 0.420 -0.197 -0.065 0.61 358257. 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 0.0917 0.0282 5.370 42.306 40.088 4004.245 4.780 178.313 4.541 0.68 392894. 0.7839 3.63 0.0223 0.0701 0.0902 0.0286 5.446 42.904 39.457 4060.830 4.847 175.505 4.407 0.68 393136. 0.7548 7.26 0.0445 0.1360 0.0886 0.0290 5.516 43.457 38.773 4113.211 4.910 172.463 4.276 0.68 393399. 0.7259 10.88 0.0668 0.1978 0.0870 0.0293 5.579 43.954 38.035 4160.225 4.966 169.178 4.147 0.68 393681. 0.6973 14.51 0.0890 0.2558 0.0851 0.0296 5.633 44.382 37.238 4200.687 5.014 165.636 4.021 0.68 393984. 0.6690 18.14 0.1113 0.3100 0.0832 0.0299 5.677 44.727 36.382 4233.342 5.053 161.827 3.898 0.68 394309. 0.6411 21.77 0.1335 0.3606 0.0811 0.0300 5.709 44.975 35.462 4256.831 5.081 157.735 3.779 0.68 394656. 0.6135 25.39 0.1558 0.4077 0.0788 0.0301 5.726 45.111 34.476 4269.756 5.097 153.348 3.662 0.68 395026. 0.5863 29.02 0.1780 0.4516 0.0764 0.0301 5.727 45.121 33.421 4270.666 5.098 148.656 3.549 0.68 395419. 0.5595 32.65 0.2003 0.4924 0.0738 0.0300 5.710 44.989 32.296 4258.188 5.083 143.651 3.440 0.68 395836. 0.5330 36.28 0.2225 0.5302 0.0711 0.0298 5.674 44.703 31.100 4231.131 5.051 138.332 3.334 0.68 396277. 0.5069 39.91 0.2448 0.5652 0.0682 0.0295 5.617 44.254 29.836 4188.618 5.000 132.712 3.231 0.68 396743. 0.4812 43.53 0.2670 0.5975 0.0652 0.0291 5.539 43.635 28.509 4130.067 4.930 126.807 3.131 0.69 397234. 0.4558 47.16 0.2893 0.6272 0.0620 0.0286 5.438 42.843 27.122 4055.069 4.840 120.638 3.034 0.69 397749. 0.4308 50.79 0.3115 0.6544 0.0587 0.0280 5.315 41.873 25.680 3963.283 4.731 114.224 2.939 0.69 398291. 0.4061 54.42 0.3338 0.6790 0.0553 0.0272 5.169 40.723 24.187 3854.391 4.601 107.584 2.846 0.69 398858. 0.3817 58.04 0.3560 0.7011 0.0518 0.0263 4.999 39.388 22.647 3728.073 4.450 100.733 2.755 0.69 399451. 0.3575 61.67 0.3783 0.7207 0.0482 0.0253 4.806 37.866 21.063 3584.015 4.278 93.689 2.666 0.69 400070. 0.3336 65.30 0.4005 0.7376 0.0444 0.0241 4.589 36.153 19.439 3421.898 4.085 86.465 2.577 0.69 400716. 0.3098 68.93 0.4228 0.7517 0.0406 0.0229 4.347 34.247 17.778 3241.463 3.869 79.075 2.488 0.69 401388. 0.2860 72.55 0.4450 0.7626 0.0368 0.0215 4.080 32.144 16.082 3042.458 3.632 71.534 2.398 0.69 402088. 0.2622 76.18 0.4673 0.7699 0.0328 0.0199 3.788 29.844 14.356 2824.714 3.372 63.856 2.305 0.69 402814. 0.2381 79.81 0.4895 0.7728 0.0288 0.0183 3.471 27.344 12.603 2588.134 3.089 56.056 2.209 0.69 403568. 0.2138 83.44 0.5118 0.7699 0.0247 0.0165 3.128 24.646 10.826 2332.732 2.784 48.152 2.105 0.69 404349. 0.1888 87.07 0.5341 0.7593 0.0206 0.0145 2.761 21.751 9.029 2058.700 2.457 40.163 1.989 0.69 405158. 0.1630 90.69 0.5563 0.7370 0.0165 0.0125 2.369 18.663 7.219 1766.436 2.109 32.111 1.854 0.69 405994. 0.1358 94.32 0.5786 0.6954 0.0123 0.0103 1.953 15.390 5.401 1456.616 1.739 24.024 1.682 0.69 406858. 0.1066 97.95 0.6008 0.6172 0.0082 0.0080 1.516 11.941 3.582 1130.249 1.349 15.932 1.437 0.70 407748. 0.0742 101.58 0.6231 0.4531 0.0040 0.0056 1.058 8.332 1.769 788.586 0.941 7.869 1.018 0.70 408663. 0.0369 105.20 0.6453 -0.0528 -0.0002 0.0029 0.560 4.410 -0.105 417.373 0.498 -0.468 -0.114 0.70 409342. 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 0.0938 0.0298 8.064 56.472 51.927 6013.125 6.380 230.971 3.917 0.77 441925. 0.7696 4.10 0.0223 0.0685 0.0924 0.0301 8.153 57.098 51.135 6079.819 6.451 227.449 3.815 0.77 442201. 0.7438 8.19 0.0447 0.1333 0.0908 0.0304 8.235 57.670 50.273 6140.693 6.515 223.613 3.713 0.77 442500. 0.7179 12.29 0.0670 0.1946 0.0891 0.0307 8.307 58.173 49.337 6194.258 6.572 219.451 3.613 0.77 442822. 0.6919 16.38 0.0893 0.2523 0.0873 0.0309 8.367 58.593 48.324 6238.983 6.620 214.946 3.513 0.77 443167. 0.6659 20.48 0.1117 0.3066 0.0853 0.0311 8.413 58.914 47.230 6273.204 6.656 210.080 3.415 0.77 443538. 0.6399 24.57 0.1340 0.3575 0.0832 0.0312 8.442 59.120 46.051 6295.088 6.679 204.837 3.318 0.77 443934. 0.6140 28.67 0.1563 0.4051 0.0809 0.0312 8.452 59.191 44.784 6302.650 6.687 199.199 3.223 0.77 444356. 0.5881 32.77 0.1787 0.4495 0.0784 0.0312 8.440 59.107 43.424 6293.773 6.678 193.151 3.129 0.77 444805. 0.5623 36.86 0.2010 0.4909 0.0758 0.0310 8.403 58.850 41.970 6266.395 6.649 186.684 3.038 0.77 445280. 0.5366 40.96 0.2233 0.5294 0.0730 0.0308 8.339 58.402 40.422 6218.653 6.598 179.797 2.948 0.77 445783. 0.5111 45.05 0.2456 0.5650 0.0701 0.0305 8.246 57.749 38.783 6149.107 6.524 172.506 2.861 0.77 446314. 0.4858 49.15 0.2680 0.5979 0.0669 0.0300 8.122 56.881 37.058 6056.748 6.426 164.834 2.775 0.77 446873. 0.4606 53.24 0.2903 0.6283 0.0637 0.0294 7.967 55.792 35.254 5940.813 6.303 156.808 2.692 0.77 447461. 0.4357 57.34 0.3126 0.6560 0.0603 0.0287 7.779 54.476 33.376 5800.636 6.155 148.455 2.610 0.77 448077. 0.4111 61.44 0.3350 0.6813 0.0568 0.0279 7.557 52.926 31.430 5635.596 5.980 139.801 2.530 0.77 448722. 0.3867 65.53 0.3573 0.7041 0.0531 0.0270 7.302 51.137 29.422 5445.102 5.777 130.867 2.451 0.77 449397. 0.3625 69.63 0.3796 0.7243 0.0494 0.0259 7.012 49.103 27.355 5228.563 5.548 121.675 2.373 0.77 450101. 0.3384 73.72 0.4020 0.7420 0.0456 0.0247 6.686 46.821 25.234 4985.488 5.290 112.243 2.296 0.77 450835. 0.3145 77.82 0.4243 0.7568 0.0417 0.0234 6.324 44.285 23.064 4715.493 5.003 102.590 2.218 0.78 451599. 0.2905 81.91 0.4466 0.7686 0.0377 0.0219 5.925 41.494 20.848 4418.349 4.688 92.734 2.140 0.78 452393. 0.2665 86.01 0.4690 0.7766 0.0336 0.0203 5.490 38.448 18.591 4094.012 4.344 82.694 2.060 0.78 453218. 0.2422 90.11 0.4913 0.7802 0.0294 0.0185 5.019 35.149 16.297 3742.659 3.971 72.491 1.975 0.78 454073. 0.2174 94.20 0.5136 0.7778 0.0252 0.0167 4.512 31.599 13.972 3364.734 3.570 62.145 1.883 0.78 454960. 0.1919 98.30 0.5360 0.7670 0.0210 0.0147 3.971 27.808 11.619 2961.052 3.142 51.683 1.780 0.78 455877. 0.1654 102.39 0.5583 0.7434 0.0167 0.0125 3.397 23.787 9.248 2532.884 2.687 41.134 1.656 0.78 456825. 0.1373 106.49 0.5806 0.6981 0.0124 0.0103 2.792 19.553 6.864 2082.052 2.209 30.533 1.495 0.78 457804. 0.1068 110.58 0.6029 0.6113 0.0081 0.0080 2.160 15.129 4.478 1610.987 1.709 19.919 1.261 0.78 458813. 0.0728 114.68 0.6253 0.4264 0.0038 0.0056 1.505 10.542 2.099 1122.522 1.191 9.337 0.848 0.78 459848. 0.0335 118.78 0.6476 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 0.0963 0.0348 12.941 81.563 65.829 9649.817 9.215 292.809 3.094 0.85 490913. 0.6845 4.54 0.0223 0.0605 0.0949 0.0350 12.980 81.813 64.888 9679.440 9.243 288.624 3.041 0.85 491221. 0.6678 9.07 0.0445 0.1188 0.0934 0.0350 13.005 81.965 63.856 9697.473 9.260 284.030 2.987 0.85 491554. 0.6507 13.61 0.0668 0.1750 0.0918 0.0350 13.011 82.009 62.727 9702.643 9.265 279.009 2.932 0.85 491914. 0.6332 18.15 0.0890 0.2289 0.0900 0.0350 12.999 81.933 61.497 9693.650 9.257 273.539 2.877 0.85 492300. 0.6153 22.68 0.1113 0.2806 0.0880 0.0349 12.966 81.725 60.161 9668.998 9.233 267.596 2.822 0.85 492714. 0.5968 27.22 0.1336 0.3301 0.0859 0.0348 12.910 81.369 58.713 9626.939 9.193 261.157 2.766 0.85 493157. 0.5779 31.76 0.1558 0.3773 0.0836 0.0345 12.828 80.851 57.149 9565.581 9.134 254.200 2.710 0.85 493629. 0.5586 36.29 0.1781 0.4221 0.0812 0.0342 12.717 80.151 55.464 9482.855 9.055 246.706 2.653 0.85 494131. 0.5387 40.83 0.2004 0.4646 0.0785 0.0339 12.574 79.254 53.656 9376.715 8.954 238.661 2.595 0.86 494663. 0.5184 45.37 0.2226 0.5047 0.0757 0.0334 12.398 78.144 51.723 9245.307 8.829 230.065 2.538 0.86 495225. 0.4976 49.90 0.2449 0.5424 0.0727 0.0328 12.186 76.807 49.670 9087.216 8.678 220.934 2.479 0.86 495818. 0.4764 54.44 0.2671 0.5777 0.0695 0.0321 11.937 75.238 47.504 8901.521 8.500 211.299 2.421 0.86 496442. 0.4549 58.98 0.2894 0.6106 0.0662 0.0314 11.650 73.430 45.233 8687.583 8.296 201.196 2.362 0.86 497097. 0.4331 63.51 0.3117 0.6410 0.0627 0.0305 11.325 71.377 42.864 8444.727 8.064 190.661 2.302 0.86 497784. 0.4110 68.05 0.3339 0.6690 0.0591 0.0295 10.959 69.074 40.406 8172.213 7.804 179.728 2.243 0.86 498502. 0.3887 72.59 0.3562 0.6945 0.0554 0.0284 10.553 66.512 37.866 7869.165 7.514 168.427 2.183 0.86 499253. 0.3662 77.12 0.3785 0.7171 0.0516 0.0272 10.109 63.713 35.248 7538.023 7.198 156.784 2.121 0.86 500036. 0.3433 81.66 0.4007 0.7367 0.0476 0.0259 9.623 60.655 32.560 7176.206 6.853 144.825 2.058 0.86 500852. 0.3202 86.20 0.4230 0.7530 0.0436 0.0245 9.098 57.342 29.805 6784.230 6.478 132.575 1.993 0.86 501701. 0.2966 90.73 0.4452 0.7650 0.0395 0.0230 8.536 53.801 26.990 6365.350 6.078 120.054 1.923 0.86 502583. 0.2724 95.27 0.4675 0.7713 0.0353 0.0214 7.944 50.067 24.119 5923.502 5.657 107.281 1.847 0.86 503498. 0.2473 99.81 0.4898 0.7718 0.0310 0.0197 7.309 46.070 21.198 5450.594 5.205 94.288 1.764 0.86 504446. 0.2214 104.34 0.5120 0.7644 0.0267 0.0179 6.637 41.831 18.233 4949.086 4.726 81.102 1.671 0.86 505428. 0.1946 108.88 0.5343 0.7459 0.0223 0.0160 5.929 37.372 15.232 4421.521 4.222 67.753 1.563 0.87 506444. 0.1663 113.42 0.5566 0.7109 0.0179 0.0140 5.192 32.722 12.203 3871.383 3.697 54.280 1.430 0.87 507494. 0.1362 117.95 0.5788 0.6502 0.0134 0.0119 4.429 27.917 9.156 3302.904 3.154 40.728 1.257 0.87 508577. 0.1037 122.49 0.6011 0.5463 0.0089 0.0098 3.649 23.000 6.103 2721.124 2.598 27.148 1.017 0.87 509694. 0.0685 127.03 0.6233 0.3623 0.0045 0.0077 2.858 18.015 3.057 2131.344 2.035 13.599 0.651 0.87 510841. 0.0310 131.56 0.6456 -0.0028 0.0000 0.0055 2.041 12.864 -0.016 1521.955 1.453 -0.072 -0.005 0.87 511914. 0.0000