20.5x10.5PN (205x105PN.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 0.0911 0.0356 0.010 0.654 0.513 7.734 0.074 2.280 30.059 0.08 45241. 0.6159 0.46 0.0235 0.0585 0.0896 0.0360 0.010 0.661 0.504 7.821 0.075 2.244 29.254 0.08 45270. 0.5947 0.91 0.0470 0.1138 0.0881 0.0364 0.011 0.668 0.496 7.902 0.075 2.205 28.451 0.08 45301. 0.5734 1.37 0.0705 0.1659 0.0864 0.0367 0.011 0.674 0.486 7.975 0.076 2.163 27.654 0.08 45336. 0.5519 1.82 0.0940 0.2148 0.0846 0.0370 0.011 0.679 0.476 8.038 0.077 2.117 26.862 0.08 45372. 0.5305 2.28 0.1175 0.2607 0.0826 0.0372 0.011 0.684 0.465 8.089 0.077 2.069 26.078 0.08 45412. 0.5090 2.74 0.1410 0.3036 0.0805 0.0374 0.011 0.687 0.453 8.125 0.078 2.016 25.303 0.08 45455. 0.4876 3.19 0.1645 0.3434 0.0783 0.0375 0.011 0.688 0.441 8.145 0.078 1.960 24.535 0.08 45500. 0.4662 3.65 0.1880 0.3803 0.0759 0.0375 0.011 0.689 0.427 8.146 0.078 1.899 23.777 0.08 45549. 0.4447 4.10 0.2114 0.4144 0.0733 0.0374 0.011 0.687 0.413 8.126 0.078 1.835 23.027 0.08 45600. 0.4233 4.56 0.2349 0.4456 0.0706 0.0372 0.011 0.683 0.397 8.083 0.077 1.766 22.285 0.08 45655. 0.4020 5.02 0.2584 0.4740 0.0677 0.0369 0.011 0.678 0.381 8.016 0.077 1.694 21.549 0.08 45713. 0.3806 5.47 0.2819 0.4995 0.0646 0.0365 0.011 0.670 0.364 7.925 0.076 1.618 20.819 0.08 45774. 0.3594 5.93 0.3054 0.5222 0.0615 0.0359 0.010 0.660 0.346 7.809 0.075 1.539 20.091 0.08 45839. 0.3382 6.39 0.3289 0.5420 0.0582 0.0353 0.010 0.648 0.327 7.669 0.073 1.456 19.363 0.08 45907. 0.3171 6.84 0.3524 0.5588 0.0548 0.0345 0.010 0.634 0.308 7.502 0.072 1.371 18.632 0.08 45978. 0.2960 7.30 0.3759 0.5724 0.0512 0.0336 0.010 0.618 0.288 7.310 0.070 1.283 17.893 0.08 46053. 0.2750 7.75 0.3994 0.5827 0.0476 0.0326 0.010 0.599 0.268 7.092 0.068 1.192 17.143 0.08 46131. 0.2540 8.21 0.4229 0.5893 0.0439 0.0315 0.009 0.579 0.247 6.848 0.065 1.100 16.374 0.08 46212. 0.2330 8.67 0.4464 0.5919 0.0401 0.0303 0.009 0.556 0.226 6.577 0.063 1.005 15.580 0.08 46297. 0.2120 9.12 0.4699 0.5898 0.0363 0.0289 0.008 0.531 0.204 6.279 0.060 0.908 14.750 0.08 46386. 0.1908 9.58 0.4934 0.5824 0.0324 0.0274 0.008 0.503 0.182 5.954 0.057 0.810 13.871 0.08 46478. 0.1694 10.03 0.5169 0.5686 0.0284 0.0258 0.008 0.473 0.160 5.602 0.053 0.710 12.927 0.08 46574. 0.1478 10.49 0.5404 0.5469 0.0243 0.0240 0.007 0.441 0.137 5.223 0.050 0.609 11.893 0.08 46673. 0.1260 10.95 0.5639 0.5152 0.0203 0.0222 0.006 0.407 0.114 4.818 0.046 0.507 10.737 0.08 46776. 0.1038 11.40 0.5874 0.4703 0.0162 0.0202 0.006 0.371 0.091 4.387 0.042 0.405 9.408 0.08 46882. 0.0812 11.86 0.6108 0.4072 0.0121 0.0181 0.005 0.332 0.068 3.932 0.038 0.302 7.834 0.08 46992. 0.0584 12.31 0.6343 0.3181 0.0080 0.0159 0.005 0.292 0.045 3.454 0.033 0.200 5.891 0.08 47105. 0.0357 12.77 0.6578 0.1887 0.0039 0.0136 0.004 0.250 0.022 2.954 0.028 0.098 3.370 0.08 47221. 0.0143 13.23 0.6813 -0.0107 -0.0002 0.0112 0.003 0.205 -0.001 2.429 0.023 -0.004 -0.185 0.08 47332. 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 0.0915 0.0323 0.075 2.370 2.060 56.075 0.268 9.165 16.666 0.16 90480. 0.6847 0.93 0.0240 0.0660 0.0901 0.0327 0.076 2.403 2.028 56.855 0.271 9.019 16.176 0.16 90539. 0.6593 1.86 0.0480 0.1281 0.0885 0.0331 0.077 2.434 1.992 57.583 0.275 8.861 15.691 0.16 90604. 0.6339 2.79 0.0719 0.1863 0.0868 0.0335 0.078 2.461 1.953 58.243 0.278 8.689 15.213 0.16 90674. 0.6086 3.72 0.0959 0.2407 0.0849 0.0338 0.079 2.486 1.912 58.820 0.281 8.504 14.742 0.16 90750. 0.5834 4.66 0.1199 0.2915 0.0829 0.0341 0.080 2.506 1.867 59.294 0.283 8.304 14.280 0.16 90831. 0.5585 5.59 0.1439 0.3387 0.0808 0.0343 0.080 2.521 1.818 59.647 0.285 8.088 13.827 0.16 90919. 0.5337 6.52 0.1679 0.3824 0.0785 0.0344 0.080 2.530 1.766 59.859 0.286 7.856 13.383 0.16 91013. 0.5091 7.45 0.1919 0.4229 0.0760 0.0345 0.080 2.532 1.710 59.909 0.286 7.607 12.948 0.16 91113. 0.4847 8.38 0.2158 0.4601 0.0733 0.0344 0.080 2.526 1.650 59.778 0.285 7.341 12.523 0.16 91219. 0.4605 9.31 0.2398 0.4942 0.0705 0.0342 0.080 2.513 1.587 59.452 0.284 7.058 12.106 0.16 91333. 0.4365 10.24 0.2638 0.5253 0.0675 0.0339 0.079 2.490 1.520 58.922 0.281 6.759 11.698 0.16 91453. 0.4127 11.17 0.2878 0.5534 0.0644 0.0335 0.078 2.459 1.449 58.180 0.278 6.445 11.297 0.16 91579. 0.3892 12.11 0.3118 0.5785 0.0611 0.0329 0.077 2.418 1.375 57.224 0.273 6.118 10.901 0.16 91713. 0.3659 13.04 0.3358 0.6007 0.0577 0.0322 0.075 2.369 1.299 56.049 0.268 5.777 10.511 0.16 91854. 0.3429 13.97 0.3597 0.6198 0.0542 0.0314 0.073 2.310 1.220 54.652 0.261 5.425 10.122 0.16 92001. 0.3200 14.90 0.3837 0.6358 0.0506 0.0305 0.071 2.241 1.138 53.029 0.253 5.062 9.735 0.16 92156. 0.2973 15.83 0.4077 0.6485 0.0468 0.0294 0.069 2.163 1.054 51.176 0.244 4.690 9.345 0.16 92318. 0.2746 16.76 0.4317 0.6576 0.0430 0.0282 0.066 2.075 0.969 49.089 0.234 4.308 8.949 0.16 92487. 0.2521 17.69 0.4557 0.6626 0.0391 0.0269 0.063 1.976 0.881 46.767 0.223 3.918 8.543 0.16 92664. 0.2295 18.62 0.4797 0.6631 0.0352 0.0254 0.059 1.868 0.792 44.206 0.211 3.521 8.122 0.16 92848. 0.2068 19.55 0.5036 0.6581 0.0311 0.0238 0.056 1.750 0.701 41.406 0.198 3.117 7.677 0.16 93039. 0.1840 20.49 0.5276 0.6464 0.0270 0.0221 0.051 1.621 0.609 38.366 0.183 2.708 7.198 0.16 93238. 0.1607 21.42 0.5516 0.6260 0.0229 0.0202 0.047 1.483 0.516 35.091 0.168 2.294 6.668 0.17 93444. 0.1371 22.35 0.5756 0.5940 0.0188 0.0182 0.042 1.335 0.422 31.585 0.151 1.878 6.063 0.17 93657. 0.1127 23.28 0.5996 0.5453 0.0146 0.0160 0.037 1.177 0.328 27.857 0.133 1.460 5.343 0.17 93878. 0.0876 24.21 0.6236 0.4713 0.0104 0.0138 0.032 1.011 0.234 23.919 0.114 1.042 4.441 0.17 94106. 0.0615 25.14 0.6475 0.3554 0.0062 0.0114 0.027 0.836 0.141 19.788 0.094 0.626 3.225 0.17 94341. 0.0346 26.07 0.6715 0.1603 0.0021 0.0089 0.021 0.654 0.048 15.469 0.074 0.213 1.402 0.17 94577. 0.0088 27.00 0.6955 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 0.0920 0.0310 0.244 5.126 4.662 181.957 0.579 20.735 11.620 0.24 135715. 0.7181 1.38 0.0237 0.0681 0.0906 0.0315 0.248 5.203 4.589 184.660 0.588 20.412 11.272 0.24 135803. 0.6911 2.76 0.0473 0.1321 0.0890 0.0319 0.251 5.274 4.510 187.196 0.596 20.062 10.928 0.24 135899. 0.6643 4.13 0.0710 0.1920 0.0874 0.0323 0.254 5.339 4.425 189.511 0.603 19.683 10.591 0.24 136002. 0.6377 5.51 0.0947 0.2480 0.0855 0.0327 0.257 5.397 4.333 191.553 0.610 19.273 10.260 0.24 136114. 0.6113 6.89 0.1183 0.3002 0.0836 0.0329 0.259 5.445 4.234 193.261 0.615 18.832 9.936 0.24 136235. 0.5852 8.27 0.1420 0.3487 0.0815 0.0332 0.261 5.482 4.127 194.572 0.619 18.355 9.620 0.24 136364. 0.5593 9.65 0.1657 0.3938 0.0792 0.0333 0.262 5.506 4.012 195.419 0.622 17.843 9.311 0.24 136502. 0.5338 11.03 0.1893 0.4355 0.0768 0.0334 0.262 5.515 3.888 195.736 0.623 17.294 9.010 0.24 136650. 0.5085 12.40 0.2130 0.4740 0.0742 0.0333 0.262 5.507 3.756 195.458 0.622 16.707 8.716 0.24 136806. 0.4835 13.78 0.2366 0.5093 0.0714 0.0332 0.261 5.481 3.616 194.535 0.619 16.082 8.430 0.24 136973. 0.4588 15.16 0.2603 0.5417 0.0684 0.0329 0.259 5.436 3.467 192.931 0.614 15.421 8.151 0.24 137149. 0.4344 16.54 0.2840 0.5712 0.0654 0.0325 0.256 5.371 3.311 190.624 0.607 14.727 7.878 0.24 137336. 0.4103 17.92 0.3076 0.5978 0.0621 0.0320 0.252 5.285 3.148 187.599 0.597 14.002 7.611 0.25 137532. 0.3865 19.29 0.3313 0.6216 0.0588 0.0313 0.247 5.180 2.978 183.841 0.585 13.248 7.348 0.25 137738. 0.3630 20.67 0.3550 0.6425 0.0553 0.0306 0.240 5.053 2.803 179.338 0.571 12.469 7.090 0.25 137955. 0.3398 22.05 0.3786 0.6606 0.0518 0.0297 0.233 4.904 2.623 174.075 0.554 11.665 6.833 0.25 138182. 0.3167 23.43 0.4023 0.6756 0.0481 0.0286 0.225 4.734 2.437 168.041 0.535 10.839 6.578 0.25 138420. 0.2939 24.81 0.4260 0.6874 0.0444 0.0275 0.216 4.542 2.247 161.222 0.513 9.993 6.321 0.25 138668. 0.2712 26.19 0.4496 0.6957 0.0405 0.0262 0.206 4.328 2.052 153.608 0.489 9.129 6.060 0.25 138927. 0.2485 27.56 0.4733 0.7000 0.0366 0.0248 0.195 4.091 1.854 145.191 0.462 8.248 5.793 0.25 139196. 0.2258 28.94 0.4970 0.6996 0.0326 0.0232 0.182 3.831 1.653 135.965 0.433 7.352 5.514 0.25 139477. 0.2029 30.32 0.5206 0.6936 0.0286 0.0215 0.169 3.548 1.449 125.931 0.401 6.444 5.218 0.25 139768. 0.1798 31.70 0.5443 0.6802 0.0245 0.0196 0.154 3.243 1.242 115.096 0.366 5.525 4.895 0.25 140070. 0.1561 33.08 0.5680 0.6571 0.0204 0.0176 0.139 2.915 1.034 103.473 0.329 4.598 4.532 0.25 140382. 0.1319 34.45 0.5916 0.6202 0.0163 0.0155 0.122 2.566 0.825 91.089 0.290 3.668 4.106 0.25 140706. 0.1067 35.83 0.6153 0.5620 0.0121 0.0133 0.105 2.197 0.615 77.981 0.248 2.736 3.578 0.25 141040. 0.0803 37.21 0.6389 0.4684 0.0080 0.0109 0.086 1.809 0.406 64.200 0.204 1.808 2.872 0.25 141384. 0.0524 38.59 0.6626 0.3071 0.0039 0.0085 0.067 1.403 0.199 49.790 0.158 0.886 1.815 0.25 141734. 0.0232 39.97 0.6863 -0.0306 -0.0003 0.0058 0.046 0.964 -0.013 34.219 0.109 -0.059 -0.174 0.25 142013. 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 0.0927 0.0305 0.568 8.954 8.345 423.747 1.012 37.121 8.933 0.33 180944. 0.7386 1.85 0.0239 0.0703 0.0912 0.0310 0.577 9.095 8.216 430.398 1.027 36.544 8.658 0.33 181063. 0.7103 3.71 0.0477 0.1363 0.0897 0.0314 0.586 9.227 8.075 436.644 1.042 35.918 8.388 0.33 181192. 0.6823 5.56 0.0716 0.1980 0.0880 0.0318 0.593 9.347 7.922 442.352 1.056 35.238 8.123 0.33 181332. 0.6544 7.41 0.0955 0.2555 0.0861 0.0322 0.600 9.454 7.757 447.388 1.068 34.503 7.864 0.33 181483. 0.6269 9.27 0.1193 0.3092 0.0842 0.0325 0.606 9.543 7.578 451.606 1.078 33.708 7.611 0.33 181646. 0.5997 11.12 0.1432 0.3590 0.0820 0.0327 0.610 9.611 7.385 454.850 1.086 32.850 7.365 0.33 181820. 0.5729 12.97 0.1670 0.4052 0.0797 0.0329 0.613 9.656 7.178 456.953 1.091 31.927 7.125 0.33 182007. 0.5464 14.82 0.1909 0.4479 0.0772 0.0329 0.614 9.673 6.955 457.752 1.093 30.935 6.891 0.33 182207. 0.5202 16.68 0.2148 0.4873 0.0746 0.0329 0.613 9.659 6.716 457.087 1.091 29.874 6.665 0.33 182419. 0.4944 18.53 0.2386 0.5235 0.0718 0.0327 0.610 9.611 6.462 454.834 1.086 28.744 6.444 0.33 182645. 0.4689 20.38 0.2625 0.5567 0.0688 0.0324 0.605 9.528 6.193 450.908 1.076 27.548 6.230 0.33 182884. 0.4438 22.24 0.2864 0.5870 0.0656 0.0320 0.597 9.408 5.911 445.253 1.063 26.291 6.021 0.33 183136. 0.4190 24.09 0.3102 0.6144 0.0624 0.0315 0.587 9.252 5.616 437.829 1.045 24.979 5.818 0.33 183402. 0.3946 25.94 0.3341 0.6390 0.0590 0.0308 0.575 9.057 5.309 428.603 1.023 23.615 5.618 0.33 183681. 0.3705 27.80 0.3580 0.6608 0.0554 0.0300 0.560 8.823 4.992 417.542 0.997 22.203 5.422 0.33 183975. 0.3468 29.65 0.3818 0.6797 0.0518 0.0291 0.543 8.550 4.665 404.610 0.966 20.748 5.229 0.33 184282. 0.3233 31.50 0.4057 0.6956 0.0481 0.0280 0.523 8.236 4.329 389.777 0.931 19.253 5.037 0.33 184604. 0.3000 33.36 0.4296 0.7084 0.0442 0.0268 0.500 7.882 3.984 373.012 0.891 17.722 4.845 0.33 184940. 0.2768 35.21 0.4534 0.7178 0.0403 0.0255 0.475 7.486 3.633 354.288 0.846 16.157 4.650 0.33 185291. 0.2537 37.06 0.4773 0.7233 0.0364 0.0240 0.447 7.049 3.274 333.586 0.796 14.563 4.452 0.33 185656. 0.2306 38.91 0.5011 0.7242 0.0323 0.0224 0.417 6.569 2.910 310.894 0.742 12.942 4.245 0.33 186035. 0.2073 40.77 0.5250 0.7195 0.0282 0.0206 0.384 6.048 2.540 286.215 0.683 11.299 4.026 0.33 186429. 0.1836 42.62 0.5489 0.7074 0.0241 0.0187 0.348 5.485 2.167 259.568 0.620 9.638 3.786 0.33 186838. 0.1595 44.47 0.5727 0.6854 0.0199 0.0166 0.310 4.881 1.790 230.994 0.551 7.963 3.515 0.33 187262. 0.1346 46.33 0.5966 0.6487 0.0157 0.0144 0.269 4.238 1.412 200.561 0.479 6.282 3.194 0.33 187700. 0.1087 48.18 0.6205 0.5886 0.0115 0.0121 0.226 3.558 1.035 168.372 0.402 4.602 2.787 0.33 188152. 0.0811 50.03 0.6443 0.4868 0.0073 0.0097 0.180 2.843 0.658 134.554 0.321 2.928 2.219 0.33 188617. 0.0515 51.89 0.6682 0.2963 0.0032 0.0071 0.133 2.096 0.285 99.187 0.237 1.267 1.303 0.33 189089. 0.0199 53.74 0.6921 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 0.0935 0.0303 1.104 13.913 13.156 823.015 1.572 58.517 7.250 0.41 226165. 0.7527 2.30 0.0237 0.0709 0.0921 0.0308 1.121 14.137 12.956 836.290 1.597 57.626 7.027 0.41 226313. 0.7239 4.61 0.0474 0.1374 0.0905 0.0313 1.138 14.348 12.738 848.772 1.621 56.657 6.807 0.41 226474. 0.6953 6.91 0.0712 0.1996 0.0888 0.0317 1.154 14.541 12.501 860.202 1.643 55.605 6.592 0.41 226648. 0.6671 9.21 0.0949 0.2577 0.0870 0.0320 1.167 14.712 12.245 870.316 1.662 54.464 6.381 0.41 226836. 0.6391 11.51 0.1186 0.3117 0.0851 0.0324 1.179 14.856 11.967 878.831 1.678 53.231 6.176 0.41 227039. 0.6116 13.82 0.1423 0.3620 0.0829 0.0326 1.187 14.968 11.668 885.444 1.691 51.900 5.977 0.41 227256. 0.5844 16.12 0.1661 0.4087 0.0806 0.0328 1.193 15.042 11.346 889.830 1.699 50.466 5.783 0.41 227488. 0.5576 18.42 0.1898 0.4518 0.0782 0.0328 1.196 15.073 10.999 891.666 1.703 48.925 5.595 0.41 227736. 0.5311 20.72 0.2135 0.4917 0.0755 0.0328 1.194 15.056 10.628 890.644 1.701 47.274 5.412 0.41 228000. 0.5050 23.03 0.2372 0.5285 0.0727 0.0326 1.189 14.986 10.233 886.510 1.693 45.514 5.235 0.41 228280. 0.4793 25.33 0.2609 0.5622 0.0697 0.0324 1.179 14.861 9.814 879.091 1.679 43.651 5.063 0.41 228576. 0.4540 27.63 0.2847 0.5931 0.0666 0.0320 1.164 14.678 9.373 868.276 1.658 41.692 4.896 0.41 228889. 0.4291 29.93 0.3084 0.6212 0.0633 0.0314 1.145 14.436 8.913 853.986 1.631 39.645 4.734 0.41 229219. 0.4045 32.24 0.3321 0.6466 0.0599 0.0308 1.121 14.135 8.434 836.154 1.597 37.515 4.575 0.41 229566. 0.3803 34.54 0.3558 0.6692 0.0564 0.0300 1.093 13.772 7.939 814.716 1.556 35.311 4.420 0.41 229930. 0.3564 36.84 0.3796 0.6891 0.0528 0.0291 1.059 13.348 7.428 789.608 1.508 33.038 4.267 0.41 230311. 0.3328 39.14 0.4033 0.7062 0.0491 0.0280 1.020 12.860 6.902 760.766 1.453 30.702 4.115 0.41 230709. 0.3095 41.45 0.4270 0.7203 0.0452 0.0268 0.976 12.309 6.364 728.131 1.391 28.308 3.964 0.41 231126. 0.2863 43.75 0.4507 0.7313 0.0413 0.0255 0.928 11.692 5.814 691.650 1.321 25.861 3.813 0.41 231560. 0.2631 46.05 0.4745 0.7386 0.0373 0.0240 0.873 11.010 5.253 651.283 1.244 23.366 3.658 0.41 232012. 0.2400 48.35 0.4982 0.7418 0.0333 0.0224 0.814 10.261 4.683 607.006 1.159 20.830 3.499 0.41 232482. 0.2167 50.66 0.5219 0.7399 0.0292 0.0206 0.749 9.447 4.105 558.819 1.067 18.257 3.332 0.41 232970. 0.1932 52.96 0.5456 0.7314 0.0250 0.0187 0.680 8.566 3.520 506.754 0.968 15.655 3.150 0.41 233476. 0.1692 55.26 0.5693 0.7140 0.0208 0.0166 0.605 7.622 2.930 450.884 0.861 13.031 2.947 0.41 233999. 0.1444 57.57 0.5931 0.6836 0.0166 0.0144 0.525 6.615 2.337 391.335 0.747 10.395 2.709 0.41 234541. 0.1185 59.87 0.6168 0.6324 0.0124 0.0121 0.440 5.550 1.744 328.295 0.627 7.757 2.409 0.41 235101. 0.0911 62.17 0.6405 0.5440 0.0082 0.0096 0.351 4.429 1.153 262.011 0.500 5.128 1.996 0.41 235677. 0.0613 64.47 0.6642 0.3768 0.0040 0.0071 0.258 3.257 0.566 192.691 0.368 2.519 1.333 0.42 236263. 0.0287 66.78 0.6880 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 0.0945 0.0304 1.913 20.094 19.152 1426.406 2.270 85.190 6.090 0.49 271375. 0.7629 2.76 0.0237 0.0714 0.0931 0.0309 1.945 20.427 18.866 1450.020 2.308 83.918 5.901 0.49 271553. 0.7337 5.52 0.0474 0.1384 0.0916 0.0314 1.974 20.739 18.554 1472.233 2.343 82.530 5.716 0.49 271747. 0.7048 8.28 0.0711 0.2010 0.0899 0.0318 2.002 21.026 18.215 1492.584 2.376 81.021 5.535 0.49 271956. 0.6762 11.04 0.0948 0.2595 0.0881 0.0322 2.026 21.280 17.847 1510.611 2.404 79.382 5.359 0.49 272183. 0.6479 13.81 0.1185 0.3139 0.0861 0.0325 2.046 21.494 17.448 1525.816 2.428 77.607 5.187 0.49 272426. 0.6201 16.57 0.1422 0.3646 0.0840 0.0328 2.062 21.661 17.016 1537.660 2.447 75.688 5.019 0.49 272688. 0.5926 19.33 0.1659 0.4116 0.0817 0.0329 2.073 21.773 16.551 1545.582 2.460 73.618 4.857 0.49 272967. 0.5656 22.09 0.1896 0.4551 0.0792 0.0330 2.077 21.821 16.050 1549.010 2.465 71.391 4.700 0.49 273266. 0.5389 24.85 0.2134 0.4954 0.0766 0.0330 2.075 21.798 15.513 1547.400 2.463 69.002 4.547 0.49 273583. 0.5126 27.61 0.2371 0.5325 0.0737 0.0328 2.066 21.698 14.940 1540.299 2.451 66.453 4.399 0.49 273920. 0.4867 30.37 0.2608 0.5667 0.0707 0.0325 2.048 21.517 14.333 1527.397 2.431 63.752 4.256 0.49 274276. 0.4612 33.13 0.2845 0.5981 0.0676 0.0321 2.023 21.250 13.694 1508.502 2.401 60.910 4.117 0.49 274652. 0.4361 35.90 0.3082 0.6267 0.0643 0.0316 1.989 20.898 13.025 1483.474 2.361 57.936 3.982 0.49 275048. 0.4114 38.66 0.3319 0.6526 0.0609 0.0309 1.947 20.457 12.330 1452.202 2.311 54.842 3.851 0.49 275465. 0.3870 41.42 0.3556 0.6759 0.0573 0.0301 1.897 19.927 11.609 1414.576 2.251 51.637 3.722 0.49 275902. 0.3630 44.18 0.3793 0.6965 0.0536 0.0292 1.838 19.306 10.866 1370.489 2.181 48.332 3.596 0.49 276360. 0.3393 46.94 0.4030 0.7144 0.0499 0.0281 1.770 18.593 10.102 1319.830 2.101 44.933 3.472 0.49 276839. 0.3158 49.70 0.4267 0.7294 0.0460 0.0269 1.693 17.785 9.319 1262.499 2.009 41.449 3.348 0.49 277339. 0.2925 52.46 0.4504 0.7415 0.0420 0.0255 1.607 16.882 8.518 1198.403 1.907 37.887 3.224 0.49 277860. 0.2693 55.22 0.4741 0.7501 0.0380 0.0240 1.512 15.883 7.701 1127.475 1.794 34.255 3.098 0.49 278402. 0.2461 57.98 0.4978 0.7547 0.0339 0.0224 1.408 14.787 6.871 1049.666 1.671 30.561 2.969 0.49 278966. 0.2227 60.75 0.5215 0.7546 0.0298 0.0206 1.294 13.594 6.028 964.982 1.536 26.813 2.833 0.49 279551. 0.1991 63.51 0.5452 0.7483 0.0255 0.0186 1.171 12.305 5.176 873.473 1.390 23.021 2.688 0.50 280158. 0.1750 66.27 0.5689 0.7336 0.0213 0.0165 1.040 10.921 4.316 775.266 1.234 19.197 2.525 0.50 280786. 0.1501 69.03 0.5926 0.7065 0.0170 0.0143 0.899 9.446 3.452 670.579 1.067 15.353 2.335 0.50 281436. 0.1241 71.79 0.6163 0.6596 0.0128 0.0119 0.751 7.885 2.587 559.742 0.891 11.505 2.096 0.50 282107. 0.0965 74.55 0.6401 0.5768 0.0085 0.0094 0.594 6.243 1.724 443.189 0.705 7.670 1.765 0.50 282797. 0.0663 77.31 0.6638 0.4155 0.0043 0.0068 0.431 4.526 0.868 321.298 0.511 3.863 1.226 0.50 283501. 0.0327 80.07 0.6875 -0.0164 -0.0001 0.0040 0.252 2.649 -0.019 188.015 0.299 -0.086 -0.047 0.50 283996. 0.0000 PROP RPM = 7000 V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM (mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - - 0.00 0.0000 0.0000 0.0958 0.0307 3.068 27.628 26.417 2288.093 3.121 117.501 5.237 0.57 316570. 0.7704 3.23 0.0238 0.0719 0.0944 0.0312 3.121 28.098 26.030 2327.053 3.175 115.783 5.074 0.57 316779. 0.7409 6.46 0.0476 0.1392 0.0929 0.0317 3.170 28.541 25.608 2363.692 3.225 113.903 4.914 0.57 317007. 0.7117 9.69 0.0713 0.2022 0.0912 0.0322 3.215 28.946 25.147 2397.251 3.270 111.852 4.758 0.57 317253. 0.6829 12.92 0.0951 0.2609 0.0894 0.0326 3.255 29.305 24.645 2426.966 3.311 109.619 4.606 0.57 317519. 0.6544 16.15 0.1189 0.3157 0.0874 0.0329 3.288 29.607 24.099 2452.020 3.345 107.194 4.458 0.57 317806. 0.6264 19.39 0.1427 0.3667 0.0852 0.0332 3.314 29.843 23.509 2471.531 3.372 104.567 4.314 0.57 318114. 0.5987 22.62 0.1664 0.4140 0.0829 0.0333 3.332 30.000 22.870 2484.583 3.389 101.726 4.175 0.57 318443. 0.5715 25.85 0.1902 0.4578 0.0804 0.0334 3.339 30.069 22.182 2490.228 3.397 98.664 4.040 0.57 318794. 0.5446 29.08 0.2140 0.4984 0.0777 0.0334 3.336 30.037 21.442 2487.579 3.394 95.375 3.910 0.57 319168. 0.5182 32.31 0.2378 0.5359 0.0749 0.0332 3.320 29.896 20.652 2475.896 3.378 91.860 3.783 0.57 319564. 0.4921 35.54 0.2615 0.5704 0.0718 0.0329 3.292 29.639 19.814 2454.670 3.349 88.131 3.661 0.57 319983. 0.4665 38.77 0.2853 0.6022 0.0686 0.0325 3.250 29.264 18.930 2423.589 3.306 84.201 3.543 0.57 320426. 0.4412 42.00 0.3091 0.6312 0.0653 0.0320 3.195 28.767 18.005 2382.436 3.250 80.087 3.428 0.57 320892. 0.4163 45.23 0.3329 0.6576 0.0618 0.0313 3.126 28.146 17.042 2331.043 3.180 75.803 3.316 0.57 321382. 0.3918 48.46 0.3566 0.6813 0.0582 0.0305 3.043 27.400 16.044 2269.236 3.096 71.364 3.207 0.57 321896. 0.3677 51.70 0.3804 0.7025 0.0544 0.0295 2.946 26.526 15.014 2196.854 2.997 66.783 3.100 0.57 322435. 0.3438 54.93 0.4042 0.7211 0.0506 0.0284 2.835 25.523 13.955 2113.730 2.884 62.072 2.994 0.57 322997. 0.3202 58.16 0.4280 0.7368 0.0467 0.0271 2.708 24.387 12.869 2019.705 2.755 57.240 2.890 0.57 323585. 0.2967 61.39 0.4517 0.7496 0.0426 0.0257 2.568 23.119 11.758 1914.634 2.612 52.300 2.785 0.58 324197. 0.2734 64.62 0.4755 0.7591 0.0385 0.0241 2.412 21.715 10.625 1798.404 2.453 47.260 2.680 0.58 324834. 0.2500 67.85 0.4993 0.7648 0.0343 0.0224 2.241 20.176 9.472 1670.953 2.279 42.134 2.571 0.58 325497. 0.2265 71.08 0.5231 0.7659 0.0301 0.0206 2.055 18.502 8.303 1532.280 2.090 36.931 2.458 0.58 326184. 0.2027 74.31 0.5469 0.7609 0.0258 0.0186 1.854 16.693 7.119 1382.481 1.886 31.667 2.336 0.58 326897. 0.1784 77.54 0.5706 0.7478 0.0215 0.0164 1.638 14.752 5.925 1221.772 1.667 26.356 2.200 0.58 327634. 0.1533 80.77 0.5944 0.7225 0.0171 0.0141 1.409 12.685 4.725 1050.516 1.433 21.018 2.040 0.58 328397. 0.1269 84.00 0.6182 0.6772 0.0128 0.0117 1.166 10.496 3.524 869.268 1.186 15.675 1.839 0.58 329184. 0.0988 87.24 0.6420 0.5947 0.0084 0.0091 0.910 8.196 2.327 678.747 0.926 10.350 1.555 0.58 329994. 0.0679 90.47 0.6657 0.4269 0.0041 0.0064 0.643 5.790 1.138 479.540 0.654 5.062 1.076 0.58 330819. 0.0329 93.70 0.6895 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 0.0973 0.0312 4.660 36.710 35.055 3474.602 4.147 155.923 4.576 0.65 361746. 0.7755 3.73 0.0240 0.0724 0.0959 0.0318 4.741 37.355 34.555 3535.588 4.220 153.699 4.433 0.65 361988. 0.7459 7.45 0.0480 0.1402 0.0944 0.0323 4.818 37.961 34.004 3592.973 4.289 151.252 4.293 0.65 362252. 0.7165 11.18 0.0720 0.2037 0.0927 0.0328 4.889 38.516 33.401 3645.524 4.352 148.568 4.156 0.65 362538. 0.6874 14.91 0.0960 0.2628 0.0909 0.0332 4.951 39.007 32.742 3692.006 4.407 145.634 4.022 0.65 362847. 0.6588 18.63 0.1200 0.3180 0.0889 0.0335 5.003 39.420 32.022 3731.101 4.454 142.435 3.893 0.65 363181. 0.6305 22.36 0.1440 0.3692 0.0867 0.0338 5.044 39.740 31.240 3761.407 4.490 138.956 3.767 0.65 363539. 0.6027 26.08 0.1680 0.4169 0.0844 0.0340 5.071 39.952 30.392 3781.452 4.514 135.184 3.645 0.65 363922. 0.5752 29.81 0.1919 0.4610 0.0818 0.0341 5.082 40.040 29.475 3789.750 4.524 131.105 3.528 0.65 364331. 0.5482 33.54 0.2159 0.5019 0.0791 0.0340 5.076 39.989 28.487 3784.893 4.518 126.712 3.414 0.65 364766. 0.5215 37.26 0.2399 0.5397 0.0762 0.0339 5.050 39.786 27.430 3765.733 4.495 122.009 3.304 0.65 365228. 0.4953 40.99 0.2639 0.5746 0.0730 0.0335 5.004 39.424 26.306 3731.488 4.454 117.009 3.198 0.65 365717. 0.4694 44.72 0.2879 0.6067 0.0697 0.0331 4.937 38.898 25.120 3681.698 4.395 111.734 3.095 0.65 366232. 0.4440 48.44 0.3119 0.6360 0.0663 0.0325 4.849 38.205 23.877 3616.052 4.316 106.205 2.995 0.65 366776. 0.4189 52.17 0.3359 0.6628 0.0627 0.0318 4.740 37.341 22.582 3534.311 4.219 100.445 2.898 0.65 367347. 0.3942 55.89 0.3599 0.6870 0.0590 0.0309 4.608 36.305 21.239 3436.243 4.102 94.473 2.804 0.65 367945. 0.3698 59.62 0.3839 0.7086 0.0551 0.0299 4.454 35.094 19.853 3321.609 3.965 88.307 2.711 0.66 368572. 0.3457 63.35 0.4079 0.7276 0.0512 0.0287 4.278 33.705 18.427 3190.174 3.808 81.962 2.620 0.66 369228. 0.3219 67.07 0.4319 0.7438 0.0471 0.0273 4.079 32.136 16.964 3041.698 3.631 75.454 2.530 0.66 369912. 0.2982 70.80 0.4559 0.7571 0.0429 0.0259 3.857 30.386 15.467 2875.983 3.433 68.797 2.439 0.66 370624. 0.2746 74.53 0.4799 0.7671 0.0387 0.0242 3.611 28.451 13.940 2692.864 3.214 62.007 2.348 0.66 371366. 0.2509 78.25 0.5039 0.7734 0.0344 0.0224 3.342 26.331 12.387 2492.254 2.975 55.097 2.254 0.66 372137. 0.2271 81.98 0.5279 0.7749 0.0300 0.0204 3.050 24.027 10.811 2274.186 2.715 48.085 2.156 0.66 372937. 0.2029 85.70 0.5519 0.7703 0.0256 0.0183 2.734 21.541 9.215 2038.835 2.434 40.990 2.050 0.66 373766. 0.1781 89.43 0.5758 0.7571 0.0211 0.0161 2.396 18.876 7.607 1786.581 2.133 33.834 1.931 0.66 374624. 0.1524 93.16 0.5998 0.7309 0.0166 0.0136 2.036 16.039 5.990 1518.056 1.812 26.644 1.790 0.66 375511. 0.1254 96.88 0.6238 0.6825 0.0121 0.0111 1.655 13.040 4.373 1234.197 1.473 19.450 1.607 0.66 376426. 0.0962 100.61 0.6478 0.5903 0.0077 0.0084 1.255 9.891 2.762 936.175 1.117 12.286 1.338 0.66 377367. 0.0637 104.34 0.6718 0.3860 0.0032 0.0056 0.838 6.598 1.162 624.533 0.745 5.168 0.844 0.67 378316. 0.0260 108.06 0.6958 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 0.0991 0.0325 6.904 48.346 45.197 5147.955 5.462 201.036 3.982 0.73 406897. 0.7663 4.19 0.0240 0.0710 0.0978 0.0330 7.014 49.117 44.585 5230.049 5.549 198.316 3.867 0.73 407170. 0.7390 8.37 0.0479 0.1378 0.0963 0.0335 7.117 49.839 43.908 5306.854 5.631 195.301 3.753 0.73 407467. 0.7117 12.56 0.0719 0.2005 0.0947 0.0339 7.210 50.495 43.160 5376.712 5.705 191.974 3.641 0.73 407790. 0.6846 16.75 0.0959 0.2593 0.0929 0.0343 7.292 51.070 42.337 5437.961 5.770 188.315 3.531 0.73 408140. 0.6577 20.94 0.1198 0.3143 0.0909 0.0347 7.361 51.548 41.436 5488.836 5.824 184.305 3.424 0.73 408516. 0.6309 25.12 0.1438 0.3656 0.0887 0.0349 7.412 51.910 40.451 5527.414 5.865 179.924 3.319 0.73 408921. 0.6043 29.31 0.1678 0.4134 0.0864 0.0351 7.445 52.138 39.378 5551.658 5.890 175.155 3.217 0.73 409354. 0.5779 33.50 0.1917 0.4579 0.0838 0.0351 7.455 52.211 38.215 5559.441 5.899 169.980 3.118 0.73 409817. 0.5517 37.69 0.2157 0.4991 0.0811 0.0350 7.441 52.110 36.958 5548.718 5.887 164.389 3.021 0.73 410309. 0.5257 41.87 0.2397 0.5373 0.0781 0.0348 7.399 51.819 35.608 5517.714 5.854 158.386 2.927 0.73 410831. 0.4999 46.06 0.2636 0.5727 0.0750 0.0345 7.329 51.326 34.170 5465.179 5.799 151.988 2.836 0.73 411383. 0.4745 50.25 0.2876 0.6052 0.0716 0.0340 7.229 50.623 32.649 5390.317 5.719 145.222 2.747 0.73 411965. 0.4493 54.44 0.3116 0.6351 0.0681 0.0334 7.097 49.705 31.052 5292.590 5.616 138.118 2.661 0.74 412579. 0.4244 58.62 0.3355 0.6624 0.0645 0.0327 6.935 48.568 29.385 5171.555 5.487 130.705 2.577 0.74 413223. 0.3999 62.81 0.3595 0.6871 0.0607 0.0317 6.741 47.209 27.655 5026.795 5.334 123.009 2.495 0.74 413899. 0.3756 67.00 0.3835 0.7094 0.0567 0.0307 6.515 45.622 25.867 4857.875 5.154 115.055 2.415 0.74 414606. 0.3516 71.19 0.4074 0.7291 0.0527 0.0295 6.255 43.805 24.025 4664.399 4.949 106.865 2.336 0.74 415345. 0.3278 75.37 0.4314 0.7462 0.0486 0.0281 5.962 41.754 22.135 4446.004 4.717 98.457 2.258 0.74 416115. 0.3041 79.56 0.4554 0.7605 0.0443 0.0265 5.636 39.466 20.201 4202.409 4.459 89.853 2.180 0.74 416918. 0.2805 83.75 0.4793 0.7716 0.0400 0.0248 5.275 36.940 18.226 3933.391 4.173 81.069 2.102 0.74 417754. 0.2568 87.94 0.5033 0.7792 0.0356 0.0230 4.880 34.174 16.215 3638.829 3.861 72.126 2.021 0.74 418621. 0.2330 92.12 0.5273 0.7823 0.0311 0.0210 4.450 31.168 14.174 3318.737 3.521 63.045 1.937 0.74 419521. 0.2087 96.31 0.5512 0.7798 0.0266 0.0188 3.987 27.924 12.107 2973.389 3.155 53.850 1.847 0.74 420454. 0.1839 100.50 0.5752 0.7691 0.0220 0.0164 3.491 24.449 10.020 2603.391 2.762 44.570 1.746 0.74 421419. 0.1582 104.69 0.5992 0.7463 0.0174 0.0140 2.963 20.753 7.922 2209.761 2.345 35.238 1.626 0.75 422416. 0.1310 108.87 0.6232 0.7025 0.0128 0.0113 2.406 16.848 5.822 1794.029 1.904 25.895 1.472 0.75 423445. 0.1016 113.06 0.6471 0.6171 0.0082 0.0086 1.821 12.755 3.728 1358.211 1.441 16.584 1.245 0.75 424503. 0.0688 117.25 0.6711 0.4250 0.0036 0.0057 1.212 8.487 1.647 903.721 0.959 7.327 0.827 0.75 425573. 0.0304 121.44 0.6951 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 0.1012 0.0365 10.627 66.979 56.962 7924.369 7.567 253.367 3.260 0.81 452016. 0.7043 4.62 0.0238 0.0645 0.1000 0.0369 10.742 67.705 56.256 8010.308 7.649 250.229 3.185 0.81 452316. 0.6839 9.24 0.0476 0.1260 0.0986 0.0372 10.843 68.344 55.467 8085.867 7.721 246.716 3.111 0.81 452644. 0.6632 13.86 0.0714 0.1846 0.0970 0.0375 10.928 68.877 54.587 8148.957 7.782 242.803 3.038 0.81 453001. 0.6425 18.48 0.0952 0.2403 0.0953 0.0377 10.993 69.289 53.611 8197.669 7.828 238.462 2.966 0.81 453387. 0.6217 23.10 0.1190 0.2932 0.0933 0.0379 11.037 69.563 52.533 8230.087 7.859 233.667 2.895 0.81 453804. 0.6006 27.72 0.1428 0.3433 0.0912 0.0379 11.056 69.682 51.347 8244.212 7.873 228.393 2.825 0.81 454252. 0.5794 32.34 0.1666 0.3906 0.0889 0.0379 11.047 69.629 50.048 8237.935 7.867 222.615 2.756 0.81 454732. 0.5580 36.96 0.1904 0.4353 0.0864 0.0378 11.009 69.385 48.631 8209.090 7.839 216.313 2.687 0.81 455245. 0.5363 41.58 0.2142 0.4774 0.0837 0.0375 10.937 68.932 47.093 8155.517 7.788 209.471 2.619 0.82 455790. 0.5145 46.20 0.2380 0.5168 0.0807 0.0372 10.829 68.255 45.435 8075.364 7.711 202.093 2.552 0.82 456368. 0.4923 50.81 0.2618 0.5537 0.0776 0.0367 10.684 67.342 43.659 7967.388 7.608 194.197 2.485 0.82 456979. 0.4701 55.43 0.2856 0.5880 0.0742 0.0360 10.501 66.188 41.776 7830.839 7.478 185.818 2.420 0.82 457624. 0.4476 60.05 0.3094 0.6199 0.0707 0.0353 10.279 64.788 39.792 7665.241 7.320 176.993 2.355 0.82 458302. 0.4251 64.67 0.3331 0.6493 0.0670 0.0344 10.018 63.140 37.716 7470.198 7.134 167.760 2.290 0.82 459015. 0.4025 69.29 0.3569 0.6762 0.0632 0.0333 9.716 61.239 35.556 7245.287 6.919 158.153 2.226 0.82 459761. 0.3799 73.91 0.3807 0.7006 0.0592 0.0322 9.374 59.081 33.320 6990.008 6.675 148.205 2.162 0.82 460542. 0.3572 78.53 0.4045 0.7224 0.0551 0.0309 8.990 56.662 31.013 6703.736 6.402 137.944 2.098 0.82 461357. 0.3345 83.15 0.4283 0.7416 0.0509 0.0294 8.563 53.974 28.642 6385.780 6.098 127.397 2.034 0.82 462207. 0.3116 87.77 0.4521 0.7580 0.0466 0.0278 8.094 51.012 26.212 6035.377 5.763 116.589 1.970 0.82 463092. 0.2887 92.39 0.4759 0.7713 0.0422 0.0260 7.579 47.771 23.729 5651.852 5.397 105.545 1.904 0.82 464013. 0.2655 97.01 0.4997 0.7809 0.0377 0.0241 7.022 44.257 21.197 5236.067 5.000 94.286 1.836 0.82 464968. 0.2420 101.63 0.5235 0.7861 0.0331 0.0220 6.421 40.469 18.624 4787.941 4.572 82.841 1.764 0.82 465959. 0.2179 106.25 0.5473 0.7853 0.0285 0.0198 5.778 36.417 16.015 4308.581 4.114 71.236 1.686 0.83 466985. 0.1931 110.87 0.5711 0.7765 0.0238 0.0175 5.093 32.101 13.378 3797.973 3.627 59.506 1.598 0.83 468046. 0.1673 115.49 0.5949 0.7556 0.0191 0.0150 4.370 27.541 10.722 3258.393 3.112 47.691 1.492 0.83 469142. 0.1399 120.11 0.6187 0.7145 0.0143 0.0124 3.612 22.764 8.057 2693.277 2.572 35.838 1.357 0.83 470273. 0.1102 124.73 0.6425 0.6351 0.0096 0.0097 2.826 17.810 5.396 2107.166 2.012 24.001 1.161 0.83 471436. 0.0772 129.35 0.6663 0.4698 0.0049 0.0069 2.017 12.713 2.748 1504.062 1.436 12.221 0.829 0.83 472620. 0.0393 133.97 0.6901 -0.0124 -0.0001 0.0038 1.121 7.063 -0.039 835.644 0.798 -0.173 -0.021 0.83 473331. 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 0.1025 0.0443 17.188 98.482 69.774 12816.737 11.126 310.356 2.469 0.89 497150. 0.5904 5.11 0.0239 0.0543 0.1014 0.0447 17.317 99.225 69.024 12913.494 11.210 307.017 2.424 0.89 497476. 0.5765 10.22 0.0479 0.1067 0.1001 0.0449 17.421 99.819 68.173 12990.759 11.278 303.232 2.380 0.89 497834. 0.5625 15.34 0.0718 0.1571 0.0987 0.0451 17.492 100.229 67.212 13044.085 11.324 298.959 2.337 0.89 498224. 0.5484 20.45 0.0958 0.2058 0.0971 0.0452 17.526 100.421 66.131 13069.107 11.346 294.150 2.295 0.89 498649. 0.5342 25.56 0.1197 0.2526 0.0953 0.0452 17.516 100.364 64.919 13061.678 11.339 288.758 2.254 0.90 499108. 0.5199 30.67 0.1436 0.2978 0.0933 0.0450 17.457 100.029 63.565 13018.024 11.301 282.737 2.215 0.90 499603. 0.5054 35.79 0.1676 0.3414 0.0911 0.0447 17.346 99.391 62.061 12935.031 11.229 276.046 2.176 0.90 500135. 0.4907 40.90 0.1915 0.3834 0.0887 0.0443 17.179 98.432 60.398 12810.289 11.121 268.652 2.139 0.90 500705. 0.4757 46.01 0.2155 0.4239 0.0860 0.0437 16.953 97.140 58.572 12642.083 10.975 260.530 2.101 0.90 501311. 0.4603 51.12 0.2394 0.4628 0.0831 0.0430 16.668 95.507 56.582 12429.518 10.790 251.678 2.065 0.90 501956. 0.4446 56.24 0.2634 0.5000 0.0799 0.0421 16.324 93.534 54.433 12172.761 10.567 242.120 2.028 0.90 502639. 0.4283 61.35 0.2873 0.5357 0.0766 0.0411 15.922 91.230 52.135 11872.947 10.307 231.899 1.992 0.90 503359. 0.4116 66.46 0.3112 0.5696 0.0730 0.0399 15.464 88.608 49.700 11531.739 10.011 221.067 1.955 0.90 504118. 0.3945 71.57 0.3352 0.6017 0.0692 0.0386 14.954 85.682 47.140 11150.915 9.680 209.679 1.917 0.90 504915. 0.3768 76.69 0.3591 0.6318 0.0653 0.0371 14.392 82.462 44.465 10731.848 9.317 197.781 1.879 0.90 505750. 0.3587 81.80 0.3831 0.6599 0.0612 0.0355 13.779 78.954 41.686 10275.368 8.920 185.418 1.840 0.90 506623. 0.3400 86.91 0.4070 0.6857 0.0570 0.0338 13.118 75.164 38.811 9782.082 8.492 172.632 1.800 0.90 507535. 0.3209 92.02 0.4309 0.7090 0.0526 0.0320 12.407 71.090 35.849 9251.848 8.032 159.458 1.758 0.90 508486. 0.3012 97.14 0.4549 0.7297 0.0482 0.0300 11.645 66.727 32.808 8684.026 7.539 145.929 1.714 0.90 509475. 0.2809 102.25 0.4788 0.7474 0.0436 0.0279 10.832 62.067 29.694 8077.642 7.012 132.078 1.667 0.90 510503. 0.2601 107.36 0.5028 0.7616 0.0389 0.0257 9.966 57.106 26.514 7431.924 6.452 117.935 1.618 0.91 511570. 0.2385 112.47 0.5267 0.7701 0.0342 0.0234 9.065 51.943 23.276 6760.046 5.869 103.532 1.562 0.91 512676. 0.2157 117.59 0.5507 0.7674 0.0293 0.0211 8.165 46.783 19.984 6088.493 5.286 88.887 1.489 0.91 513821. 0.1905 122.70 0.5746 0.7482 0.0244 0.0188 7.279 41.709 16.646 5428.142 4.712 74.042 1.391 0.91 515005. 0.1624 127.81 0.5985 0.7110 0.0195 0.0164 6.367 36.483 13.283 4747.995 4.122 59.081 1.269 0.91 516227. 0.1324 132.92 0.6225 0.6459 0.0145 0.0140 5.437 31.151 9.908 4054.100 3.519 44.069 1.108 0.91 517487. 0.0999 138.04 0.6464 0.5348 0.0096 0.0116 4.499 25.779 6.537 3354.992 2.913 29.076 0.884 0.91 518783. 0.0647 143.15 0.6704 0.3408 0.0047 0.0092 3.565 20.425 3.183 2658.178 2.308 14.156 0.543 0.91 520101. 0.0277 148.26 0.6943