17x8N (17x8N.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 0.0803 0.0330 0.004 0.238 0.214 2.813 0.027 0.951 34.457 0.07 29265. 0.5498 0.35 0.0220 0.0522 0.0789 0.0333 0.004 0.240 0.210 2.836 0.027 0.934 33.594 0.07 29281. 0.5315 0.71 0.0440 0.1017 0.0775 0.0335 0.004 0.242 0.206 2.858 0.027 0.917 32.728 0.07 29300. 0.5129 1.06 0.0660 0.1485 0.0759 0.0338 0.004 0.243 0.202 2.876 0.027 0.899 31.860 0.07 29319. 0.4943 1.42 0.0880 0.1926 0.0742 0.0339 0.004 0.244 0.198 2.891 0.028 0.879 30.992 0.07 29340. 0.4755 1.77 0.1101 0.2340 0.0724 0.0341 0.004 0.245 0.193 2.903 0.028 0.858 30.125 0.07 29362. 0.4566 2.13 0.1321 0.2727 0.0705 0.0342 0.004 0.246 0.188 2.910 0.028 0.835 29.260 0.07 29386. 0.4376 2.48 0.1541 0.3088 0.0685 0.0342 0.004 0.246 0.182 2.913 0.028 0.811 28.397 0.07 29412. 0.4186 2.83 0.1761 0.3422 0.0664 0.0342 0.004 0.246 0.177 2.910 0.028 0.786 27.535 0.07 29439. 0.3995 3.19 0.1981 0.3729 0.0641 0.0341 0.004 0.245 0.171 2.902 0.028 0.759 26.675 0.07 29468. 0.3803 3.54 0.2201 0.4010 0.0617 0.0339 0.004 0.244 0.164 2.887 0.028 0.731 25.815 0.07 29499. 0.3612 3.90 0.2421 0.4264 0.0592 0.0336 0.004 0.242 0.158 2.865 0.027 0.701 24.954 0.07 29532. 0.3419 4.25 0.2641 0.4490 0.0566 0.0333 0.004 0.240 0.151 2.836 0.027 0.670 24.089 0.07 29566. 0.3227 4.61 0.2861 0.4689 0.0538 0.0329 0.004 0.237 0.143 2.799 0.027 0.637 23.220 0.07 29602. 0.3034 4.96 0.3081 0.4859 0.0510 0.0323 0.004 0.233 0.136 2.755 0.026 0.604 22.342 0.07 29641. 0.2841 5.31 0.3302 0.4999 0.0480 0.0317 0.004 0.228 0.128 2.703 0.026 0.569 21.453 0.07 29681. 0.2647 5.67 0.3522 0.5107 0.0450 0.0310 0.004 0.223 0.120 2.643 0.025 0.532 20.547 0.07 29723. 0.2454 6.02 0.3742 0.5181 0.0418 0.0302 0.003 0.218 0.111 2.575 0.025 0.495 19.620 0.07 29767. 0.2260 6.38 0.3962 0.5219 0.0386 0.0293 0.003 0.211 0.103 2.499 0.024 0.457 18.664 0.07 29812. 0.2066 6.73 0.4182 0.5215 0.0353 0.0283 0.003 0.204 0.094 2.415 0.023 0.418 17.671 0.07 29860. 0.1871 7.09 0.4402 0.5167 0.0320 0.0273 0.003 0.196 0.085 2.322 0.022 0.379 16.630 0.07 29910. 0.1675 7.44 0.4622 0.5065 0.0286 0.0261 0.003 0.188 0.076 2.222 0.021 0.338 15.528 0.07 29962. 0.1478 7.80 0.4842 0.4903 0.0251 0.0248 0.003 0.179 0.067 2.113 0.020 0.297 14.347 0.07 30016. 0.1280 8.15 0.5062 0.4667 0.0216 0.0234 0.003 0.169 0.057 1.996 0.019 0.256 13.063 0.07 30072. 0.1081 8.50 0.5282 0.4341 0.0180 0.0220 0.003 0.158 0.048 1.871 0.018 0.214 11.644 0.07 30130. 0.0881 8.86 0.5503 0.3902 0.0145 0.0204 0.002 0.147 0.039 1.738 0.017 0.171 10.047 0.07 30190. 0.0680 9.21 0.5723 0.3315 0.0109 0.0187 0.002 0.135 0.029 1.597 0.015 0.129 8.208 0.07 30252. 0.0482 9.57 0.5943 0.2531 0.0072 0.0170 0.002 0.122 0.019 1.448 0.014 0.086 6.035 0.07 30316. 0.0289 9.92 0.6163 0.1471 0.0036 0.0152 0.002 0.109 0.010 1.292 0.012 0.043 3.383 0.07 30382. 0.0115 10.28 0.6383 0.0006 0.0000 0.0133 0.002 0.095 0.000 1.129 0.011 0.000 0.014 0.07 30450. 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 0.0807 0.0290 0.027 0.836 0.859 19.780 0.094 3.821 19.698 0.13 58529. 0.6301 0.71 0.0221 0.0599 0.0793 0.0293 0.027 0.845 0.845 19.993 0.095 3.756 19.159 0.13 58563. 0.6077 1.43 0.0443 0.1164 0.0779 0.0296 0.027 0.853 0.829 20.189 0.096 3.687 18.622 0.13 58599. 0.5852 2.14 0.0664 0.1696 0.0763 0.0299 0.027 0.861 0.812 20.365 0.097 3.613 18.090 0.13 58638. 0.5627 2.85 0.0886 0.2195 0.0746 0.0301 0.028 0.867 0.794 20.515 0.098 3.533 17.562 0.13 58680. 0.5403 3.56 0.1107 0.2663 0.0728 0.0303 0.028 0.872 0.775 20.634 0.099 3.448 17.041 0.13 58725. 0.5179 4.28 0.1328 0.3099 0.0709 0.0304 0.028 0.876 0.755 20.720 0.099 3.358 16.526 0.13 58774. 0.4956 4.99 0.1550 0.3504 0.0689 0.0305 0.028 0.878 0.733 20.765 0.099 3.262 16.017 0.14 58826. 0.4734 5.70 0.1771 0.3879 0.0667 0.0305 0.028 0.878 0.710 20.767 0.099 3.160 15.515 0.14 58881. 0.4513 6.42 0.1993 0.4224 0.0644 0.0304 0.028 0.876 0.686 20.720 0.099 3.052 15.019 0.14 58939. 0.4294 7.13 0.2214 0.4540 0.0620 0.0303 0.028 0.871 0.660 20.619 0.098 2.938 14.529 0.14 59002. 0.4076 7.84 0.2435 0.4828 0.0595 0.0300 0.027 0.865 0.634 20.461 0.098 2.818 14.044 0.14 59067. 0.3858 8.55 0.2657 0.5087 0.0569 0.0297 0.027 0.855 0.605 20.241 0.097 2.692 13.564 0.14 59137. 0.3642 9.27 0.2878 0.5317 0.0541 0.0293 0.027 0.843 0.576 19.957 0.095 2.561 13.087 0.14 59210. 0.3428 9.98 0.3100 0.5517 0.0512 0.0288 0.026 0.829 0.545 19.607 0.094 2.425 12.611 0.14 59287. 0.3214 10.69 0.3321 0.5688 0.0482 0.0282 0.026 0.811 0.513 19.191 0.092 2.284 12.135 0.14 59368. 0.3001 11.41 0.3542 0.5828 0.0452 0.0274 0.025 0.791 0.481 18.707 0.089 2.138 11.656 0.14 59453. 0.2789 12.12 0.3764 0.5935 0.0420 0.0266 0.024 0.767 0.447 18.155 0.087 1.989 11.171 0.14 59542. 0.2578 12.83 0.3985 0.6006 0.0388 0.0257 0.024 0.741 0.413 17.532 0.084 1.836 10.677 0.14 59635. 0.2367 13.54 0.4207 0.6037 0.0355 0.0247 0.023 0.712 0.377 16.839 0.080 1.679 10.168 0.14 59732. 0.2156 14.26 0.4428 0.6024 0.0321 0.0236 0.022 0.679 0.342 16.075 0.077 1.519 9.638 0.14 59832. 0.1944 14.97 0.4649 0.5959 0.0287 0.0224 0.020 0.644 0.305 15.239 0.073 1.357 9.080 0.14 59937. 0.1731 15.68 0.4871 0.5832 0.0252 0.0210 0.019 0.606 0.268 14.330 0.068 1.192 8.482 0.14 60046. 0.1516 16.40 0.5092 0.5627 0.0216 0.0196 0.018 0.564 0.230 13.349 0.064 1.025 7.829 0.14 60160. 0.1297 17.11 0.5314 0.5325 0.0181 0.0180 0.016 0.520 0.192 12.296 0.059 0.856 7.099 0.14 60277. 0.1075 17.82 0.5535 0.4891 0.0145 0.0164 0.015 0.472 0.154 11.172 0.053 0.686 6.260 0.14 60398. 0.0848 18.53 0.5756 0.4274 0.0109 0.0146 0.013 0.422 0.116 9.978 0.048 0.515 5.260 0.14 60524. 0.0618 19.25 0.5978 0.3387 0.0072 0.0128 0.012 0.368 0.077 8.719 0.042 0.343 4.014 0.14 60653. 0.0385 19.96 0.6199 0.2074 0.0036 0.0108 0.010 0.313 0.039 7.395 0.035 0.172 2.370 0.14 60787. 0.0161 20.67 0.6421 0.0018 0.0000 0.0088 0.008 0.254 0.000 6.010 0.029 0.001 0.019 0.14 60922. 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 0.0810 0.0274 0.085 1.778 1.941 63.109 0.201 8.636 13.954 0.20 87792. 0.6711 1.07 0.0222 0.0637 0.0797 0.0278 0.086 1.799 1.909 63.869 0.203 8.490 13.555 0.20 87842. 0.6464 2.14 0.0444 0.1237 0.0782 0.0281 0.087 1.819 1.874 64.573 0.206 8.334 13.161 0.20 87897. 0.6218 3.22 0.0666 0.1801 0.0766 0.0283 0.087 1.837 1.836 65.205 0.208 8.166 12.771 0.20 87956. 0.5973 4.29 0.0888 0.2329 0.0750 0.0286 0.088 1.852 1.796 65.750 0.209 7.987 12.387 0.20 88020. 0.5729 5.36 0.1110 0.2823 0.0732 0.0288 0.089 1.865 1.753 66.192 0.211 7.795 12.009 0.20 88088. 0.5487 6.43 0.1332 0.3282 0.0712 0.0289 0.089 1.874 1.707 66.516 0.212 7.591 11.637 0.20 88161. 0.5247 7.51 0.1554 0.3709 0.0692 0.0290 0.089 1.879 1.658 66.704 0.212 7.374 11.272 0.20 88239. 0.5009 8.58 0.1776 0.4104 0.0670 0.0290 0.090 1.880 1.606 66.740 0.212 7.143 10.914 0.20 88322. 0.4774 9.65 0.1998 0.4469 0.0647 0.0290 0.089 1.877 1.551 66.608 0.212 6.899 10.562 0.20 88410. 0.4540 10.72 0.2220 0.4802 0.0623 0.0288 0.089 1.868 1.493 66.292 0.211 6.641 10.216 0.20 88504. 0.4308 11.80 0.2442 0.5107 0.0598 0.0286 0.088 1.853 1.432 65.776 0.209 6.370 9.875 0.20 88603. 0.4079 12.87 0.2664 0.5382 0.0571 0.0283 0.087 1.833 1.368 65.046 0.207 6.086 9.540 0.20 88708. 0.3852 13.94 0.2886 0.5628 0.0543 0.0279 0.086 1.806 1.301 64.094 0.204 5.789 9.209 0.20 88819. 0.3626 15.01 0.3109 0.5846 0.0514 0.0273 0.084 1.773 1.232 62.913 0.200 5.480 8.882 0.20 88935. 0.3403 16.09 0.3331 0.6034 0.0484 0.0267 0.082 1.733 1.160 61.500 0.196 5.160 8.556 0.20 89057. 0.3181 17.16 0.3553 0.6191 0.0453 0.0260 0.080 1.686 1.086 59.851 0.191 4.831 8.231 0.20 89185. 0.2961 18.23 0.3775 0.6317 0.0422 0.0252 0.078 1.633 1.010 57.961 0.184 4.493 7.904 0.20 89319. 0.2742 19.30 0.3997 0.6408 0.0389 0.0243 0.075 1.573 0.932 55.826 0.178 4.146 7.573 0.20 89459. 0.2523 20.37 0.4219 0.6462 0.0356 0.0232 0.072 1.506 0.852 53.444 0.170 3.791 7.234 0.20 89605. 0.2305 21.45 0.4441 0.6472 0.0322 0.0221 0.068 1.432 0.771 50.811 0.162 3.430 6.884 0.20 89757. 0.2086 22.52 0.4663 0.6433 0.0287 0.0208 0.064 1.350 0.689 47.926 0.153 3.062 6.516 0.20 89916. 0.1866 23.59 0.4885 0.6333 0.0252 0.0195 0.060 1.262 0.605 44.786 0.143 2.689 6.123 0.20 90080. 0.1643 24.66 0.5107 0.6157 0.0217 0.0180 0.056 1.166 0.520 41.392 0.132 2.311 5.694 0.20 90251. 0.1417 25.74 0.5329 0.5882 0.0181 0.0164 0.051 1.063 0.434 37.745 0.120 1.930 5.213 0.21 90427. 0.1185 26.81 0.5551 0.5470 0.0145 0.0147 0.045 0.954 0.347 33.849 0.108 1.545 4.654 0.21 90611. 0.0947 27.88 0.5773 0.4859 0.0109 0.0129 0.040 0.837 0.260 29.710 0.095 1.158 3.976 0.21 90800. 0.0700 28.95 0.5995 0.3938 0.0072 0.0110 0.034 0.714 0.173 25.337 0.081 0.771 3.103 0.21 90995. 0.0446 30.03 0.6217 0.2487 0.0036 0.0090 0.028 0.584 0.086 20.743 0.066 0.384 1.889 0.21 91197. 0.0192 31.10 0.6439 -0.0012 0.0000 0.0069 0.021 0.449 0.000 15.928 0.051 -0.001 -0.009 0.21 91399. 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 0.0815 0.0266 0.195 3.067 3.470 145.155 0.347 15.434 10.843 0.27 117052. 0.6971 1.43 0.0222 0.0661 0.0801 0.0270 0.197 3.107 3.412 147.018 0.351 15.176 10.526 0.27 117120. 0.6711 2.86 0.0445 0.1282 0.0786 0.0273 0.199 3.143 3.349 148.747 0.355 14.897 10.213 0.27 117193. 0.6451 4.30 0.0667 0.1865 0.0771 0.0276 0.202 3.176 3.282 150.303 0.359 14.599 9.904 0.27 117272. 0.6193 5.73 0.0890 0.2411 0.0754 0.0278 0.203 3.204 3.210 151.651 0.362 14.279 9.601 0.27 117357. 0.5938 7.16 0.1112 0.2921 0.0736 0.0280 0.205 3.228 3.133 152.752 0.365 13.937 9.304 0.27 117448. 0.5684 8.59 0.1334 0.3395 0.0716 0.0282 0.206 3.245 3.051 153.568 0.367 13.572 9.012 0.27 117546. 0.5434 10.02 0.1557 0.3835 0.0696 0.0283 0.207 3.255 2.964 154.057 0.368 13.184 8.727 0.27 117651. 0.5186 11.46 0.1779 0.4243 0.0674 0.0283 0.207 3.258 2.871 154.182 0.368 12.772 8.447 0.27 117762. 0.4940 12.89 0.2002 0.4618 0.0651 0.0282 0.206 3.252 2.773 153.900 0.367 12.336 8.173 0.27 117880. 0.4698 14.32 0.2224 0.4963 0.0627 0.0281 0.205 3.237 2.670 153.174 0.366 11.875 7.906 0.27 118006. 0.4459 15.75 0.2446 0.5279 0.0601 0.0279 0.204 3.211 2.561 151.965 0.363 11.390 7.643 0.27 118139. 0.4222 17.19 0.2669 0.5564 0.0574 0.0276 0.201 3.175 2.446 150.239 0.359 10.882 7.386 0.27 118279. 0.3987 18.62 0.2891 0.5821 0.0546 0.0271 0.198 3.127 2.327 147.976 0.353 10.350 7.133 0.27 118427. 0.3755 20.05 0.3114 0.6050 0.0517 0.0266 0.195 3.067 2.203 145.161 0.347 9.798 6.883 0.27 118583. 0.3526 21.48 0.3336 0.6249 0.0487 0.0260 0.190 2.996 2.074 141.781 0.338 9.227 6.636 0.27 118746. 0.3299 22.91 0.3558 0.6419 0.0456 0.0253 0.185 2.912 1.942 137.828 0.329 8.638 6.390 0.27 118917. 0.3074 24.35 0.3781 0.6558 0.0424 0.0244 0.179 2.817 1.806 133.290 0.318 8.032 6.145 0.27 119097. 0.2850 25.78 0.4003 0.6664 0.0391 0.0235 0.172 2.708 1.666 128.160 0.306 7.412 5.897 0.27 119284. 0.2627 27.21 0.4226 0.6734 0.0358 0.0225 0.164 2.587 1.524 122.427 0.292 6.777 5.645 0.27 119479. 0.2405 28.64 0.4448 0.6762 0.0324 0.0213 0.156 2.453 1.378 116.086 0.277 6.131 5.385 0.27 119683. 0.2182 30.07 0.4670 0.6743 0.0289 0.0200 0.146 2.306 1.230 109.129 0.261 5.473 5.114 0.27 119894. 0.1958 31.51 0.4893 0.6665 0.0254 0.0186 0.136 2.146 1.080 101.554 0.242 4.806 4.825 0.27 120114. 0.1731 32.94 0.5115 0.6513 0.0218 0.0171 0.125 1.973 0.928 93.360 0.223 4.130 4.511 0.27 120343. 0.1500 34.37 0.5338 0.6264 0.0182 0.0155 0.113 1.787 0.775 84.552 0.202 3.447 4.157 0.27 120579. 0.1263 35.80 0.5560 0.5876 0.0146 0.0138 0.101 1.588 0.620 75.139 0.179 2.759 3.744 0.27 120824. 0.1018 37.23 0.5782 0.5283 0.0109 0.0119 0.087 1.376 0.465 65.135 0.155 2.067 3.237 0.27 121077. 0.0762 38.67 0.6005 0.4356 0.0073 0.0100 0.073 1.153 0.309 54.564 0.130 1.375 2.570 0.27 121339. 0.0493 40.10 0.6227 0.2821 0.0036 0.0080 0.058 0.918 0.154 43.457 0.104 0.684 1.605 0.27 121608. 0.0217 41.53 0.6450 -0.0035 0.0000 0.0058 0.043 0.672 -0.001 31.799 0.076 -0.006 -0.019 0.28 121876. 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 0.0820 0.0262 0.374 4.715 5.457 278.897 0.533 24.274 8.875 0.34 146310. 0.7156 1.79 0.0223 0.0677 0.0806 0.0265 0.379 4.778 5.366 282.629 0.540 23.869 8.612 0.34 146395. 0.6886 3.58 0.0445 0.1312 0.0792 0.0269 0.384 4.836 5.268 286.094 0.546 23.434 8.352 0.34 146486. 0.6617 5.38 0.0668 0.1908 0.0776 0.0272 0.388 4.889 5.163 289.218 0.552 22.966 8.097 0.34 146586. 0.6351 7.17 0.0891 0.2466 0.0759 0.0274 0.391 4.935 5.050 291.929 0.558 22.464 7.847 0.34 146692. 0.6087 8.96 0.1113 0.2986 0.0741 0.0276 0.394 4.972 4.930 294.151 0.562 21.928 7.602 0.34 146807. 0.5826 10.75 0.1336 0.3470 0.0722 0.0278 0.397 5.000 4.801 295.806 0.565 21.356 7.362 0.34 146930. 0.5568 12.54 0.1558 0.3920 0.0701 0.0279 0.398 5.018 4.664 296.815 0.567 20.746 7.127 0.34 147061. 0.5313 14.34 0.1781 0.4336 0.0679 0.0279 0.398 5.022 4.519 297.097 0.567 20.099 6.898 0.34 147200. 0.5061 16.13 0.2004 0.4720 0.0656 0.0278 0.398 5.013 4.365 296.575 0.566 19.414 6.675 0.34 147349. 0.4813 17.92 0.2226 0.5073 0.0631 0.0277 0.396 4.990 4.202 295.170 0.564 18.690 6.457 0.34 147506. 0.4568 19.71 0.2449 0.5396 0.0606 0.0275 0.393 4.950 4.030 292.805 0.559 17.927 6.243 0.34 147673. 0.4326 21.50 0.2672 0.5689 0.0579 0.0272 0.388 4.892 3.851 289.416 0.553 17.127 6.035 0.34 147849. 0.4087 23.30 0.2894 0.5954 0.0550 0.0268 0.382 4.817 3.663 284.957 0.544 16.291 5.830 0.34 148034. 0.3851 25.09 0.3117 0.6191 0.0521 0.0262 0.375 4.723 3.467 279.399 0.534 15.422 5.629 0.34 148230. 0.3618 26.88 0.3340 0.6399 0.0491 0.0256 0.366 4.610 3.265 272.719 0.521 14.523 5.430 0.34 148434. 0.3387 28.67 0.3562 0.6579 0.0459 0.0249 0.355 4.478 3.057 264.897 0.506 13.596 5.234 0.34 148649. 0.3158 30.47 0.3785 0.6728 0.0427 0.0240 0.343 4.326 2.842 255.912 0.489 12.642 5.038 0.34 148874. 0.2931 32.26 0.4008 0.6845 0.0394 0.0231 0.330 4.154 2.623 245.745 0.469 11.665 4.841 0.34 149108. 0.2706 34.05 0.4230 0.6928 0.0360 0.0220 0.314 3.962 2.398 234.379 0.448 10.667 4.641 0.34 149353. 0.2481 35.84 0.4453 0.6970 0.0326 0.0208 0.297 3.749 2.169 221.799 0.424 9.649 4.436 0.34 149608. 0.2255 37.63 0.4675 0.6967 0.0291 0.0195 0.279 3.516 1.937 207.994 0.397 8.614 4.223 0.34 149873. 0.2028 39.43 0.4898 0.6908 0.0256 0.0181 0.259 3.262 1.700 192.956 0.369 7.563 3.997 0.34 150149. 0.1799 41.22 0.5121 0.6777 0.0220 0.0166 0.237 2.987 1.461 176.686 0.337 6.498 3.750 0.34 150435. 0.1565 43.01 0.5343 0.6550 0.0183 0.0149 0.213 2.691 1.219 159.192 0.304 5.423 3.474 0.34 150731. 0.1324 44.80 0.5566 0.6187 0.0147 0.0132 0.188 2.375 0.976 140.491 0.268 4.340 3.150 0.34 151038. 0.1074 46.59 0.5789 0.5615 0.0110 0.0113 0.162 2.039 0.731 120.615 0.230 3.251 2.749 0.34 151356. 0.0811 48.39 0.6011 0.4693 0.0073 0.0094 0.134 1.684 0.486 99.610 0.190 2.161 2.213 0.34 151683. 0.0532 50.18 0.6234 0.3106 0.0036 0.0073 0.104 1.311 0.241 77.537 0.148 1.074 1.412 0.34 152020. 0.0239 51.97 0.6457 -0.0057 0.0000 0.0051 0.073 0.919 -0.003 54.345 0.104 -0.013 -0.025 0.34 152354. 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 0.0827 0.0260 0.641 6.739 7.921 478.348 0.761 35.231 7.510 0.40 175563. 0.7296 2.15 0.0223 0.0687 0.0813 0.0264 0.650 6.831 7.790 484.938 0.772 34.648 7.286 0.40 175665. 0.7019 4.30 0.0446 0.1333 0.0798 0.0267 0.659 6.918 7.648 491.061 0.782 34.020 7.064 0.40 175776. 0.6743 6.46 0.0668 0.1938 0.0782 0.0270 0.666 6.995 7.496 496.583 0.790 33.344 6.847 0.40 175896. 0.6471 8.61 0.0891 0.2504 0.0765 0.0272 0.672 7.063 7.334 501.379 0.798 32.620 6.634 0.40 176024. 0.6201 10.76 0.1114 0.3032 0.0747 0.0275 0.678 7.118 7.159 505.315 0.804 31.844 6.426 0.40 176162. 0.5935 12.91 0.1337 0.3523 0.0728 0.0276 0.682 7.160 6.973 508.252 0.809 31.016 6.223 0.40 176310. 0.5672 15.07 0.1560 0.3979 0.0707 0.0277 0.684 7.185 6.775 510.052 0.812 30.133 6.024 0.41 176468. 0.5412 17.22 0.1783 0.4401 0.0685 0.0277 0.685 7.193 6.564 510.575 0.813 29.196 5.831 0.41 176636. 0.5156 19.37 0.2005 0.4791 0.0662 0.0277 0.683 7.180 6.340 509.683 0.811 28.202 5.642 0.41 176815. 0.4904 21.52 0.2228 0.5150 0.0637 0.0276 0.680 7.146 6.104 507.240 0.807 27.153 5.459 0.41 177005. 0.4655 23.67 0.2451 0.5479 0.0611 0.0273 0.675 7.087 5.856 503.109 0.801 26.047 5.279 0.41 177205. 0.4409 25.83 0.2674 0.5779 0.0584 0.0270 0.667 7.004 5.595 497.178 0.791 24.885 5.104 0.41 177417. 0.4167 27.98 0.2897 0.6050 0.0555 0.0266 0.656 6.894 5.322 489.366 0.779 23.672 4.933 0.41 177640. 0.3928 30.13 0.3119 0.6294 0.0526 0.0261 0.643 6.756 5.038 479.621 0.763 22.411 4.765 0.41 177875. 0.3691 32.28 0.3342 0.6509 0.0495 0.0254 0.627 6.591 4.745 467.901 0.745 21.104 4.599 0.41 178122. 0.3458 34.44 0.3565 0.6697 0.0464 0.0247 0.609 6.398 4.442 454.172 0.723 19.757 4.436 0.41 178380. 0.3227 36.59 0.3788 0.6855 0.0431 0.0238 0.588 6.176 4.130 438.397 0.698 18.372 4.273 0.41 178650. 0.2998 38.74 0.4011 0.6981 0.0398 0.0229 0.564 5.924 3.811 420.544 0.669 16.953 4.111 0.41 178933. 0.2770 40.89 0.4234 0.7074 0.0364 0.0218 0.537 5.643 3.485 400.581 0.638 15.502 3.946 0.41 179227. 0.2543 43.04 0.4456 0.7129 0.0329 0.0206 0.508 5.332 3.153 378.483 0.602 14.023 3.778 0.41 179534. 0.2315 45.20 0.4679 0.7140 0.0294 0.0192 0.475 4.990 2.814 354.228 0.564 12.518 3.603 0.41 179853. 0.2086 47.35 0.4902 0.7097 0.0258 0.0178 0.440 4.618 2.471 327.805 0.522 10.990 3.419 0.41 180184. 0.1855 49.50 0.5125 0.6984 0.0222 0.0163 0.401 4.215 2.123 299.214 0.476 9.443 3.218 0.41 180528. 0.1618 51.65 0.5348 0.6778 0.0185 0.0146 0.360 3.782 1.772 268.468 0.427 7.880 2.993 0.41 180885. 0.1375 53.81 0.5571 0.6437 0.0148 0.0128 0.316 3.319 1.418 235.601 0.375 6.305 2.729 0.41 181253. 0.1121 55.96 0.5793 0.5887 0.0111 0.0109 0.269 2.827 1.062 200.666 0.319 4.723 2.400 0.41 181635. 0.0854 58.11 0.6016 0.4978 0.0074 0.0089 0.220 2.307 0.705 163.747 0.261 3.138 1.954 0.41 182028. 0.0566 60.26 0.6239 0.3356 0.0037 0.0068 0.168 1.760 0.350 124.951 0.199 1.556 1.270 0.41 182434. 0.0259 62.42 0.6462 -0.0084 -0.0001 0.0046 0.113 1.185 -0.006 84.145 0.134 -0.025 -0.031 0.41 182831. 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 0.0834 0.0260 1.018 9.165 10.883 759.030 1.035 48.410 6.504 0.47 204811. 0.7405 2.51 0.0223 0.0695 0.0821 0.0263 1.032 9.294 10.705 769.724 1.050 47.616 6.308 0.47 204931. 0.7124 5.03 0.0446 0.1347 0.0806 0.0267 1.046 9.414 10.512 779.655 1.064 46.759 6.116 0.47 205061. 0.6844 7.54 0.0669 0.1959 0.0790 0.0270 1.058 9.522 10.305 788.611 1.076 45.837 5.927 0.47 205201. 0.6567 10.05 0.0892 0.2530 0.0773 0.0273 1.068 9.616 10.082 796.389 1.086 44.846 5.742 0.47 205352. 0.6293 12.56 0.1115 0.3063 0.0755 0.0275 1.077 9.693 9.844 802.768 1.095 43.786 5.562 0.47 205513. 0.6023 15.08 0.1338 0.3560 0.0735 0.0276 1.083 9.751 9.589 807.529 1.102 42.652 5.386 0.47 205687. 0.5756 17.59 0.1561 0.4021 0.0714 0.0277 1.087 9.786 9.317 810.447 1.106 41.443 5.214 0.47 205872. 0.5494 20.10 0.1784 0.4448 0.0692 0.0278 1.088 9.796 9.028 811.296 1.107 40.158 5.047 0.47 206069. 0.5235 22.61 0.2007 0.4843 0.0669 0.0277 1.086 9.779 8.722 809.852 1.105 38.795 4.885 0.47 206278. 0.4979 25.13 0.2230 0.5206 0.0644 0.0276 1.081 9.731 8.398 805.897 1.099 37.355 4.727 0.47 206500. 0.4728 27.64 0.2453 0.5540 0.0618 0.0273 1.072 9.650 8.057 799.215 1.090 35.837 4.572 0.47 206735. 0.4480 30.15 0.2676 0.5845 0.0590 0.0270 1.059 9.534 7.698 789.619 1.077 34.242 4.422 0.47 206983. 0.4235 32.66 0.2899 0.6122 0.0562 0.0266 1.042 9.382 7.323 776.980 1.060 32.575 4.275 0.47 207245. 0.3993 35.18 0.3122 0.6371 0.0532 0.0260 1.021 9.191 6.934 761.214 1.038 30.841 4.131 0.47 207520. 0.3755 37.69 0.3345 0.6593 0.0501 0.0254 0.995 8.962 6.530 742.256 1.013 29.045 3.990 0.47 207808. 0.3519 40.20 0.3567 0.6787 0.0469 0.0246 0.966 8.694 6.113 720.046 0.982 27.192 3.851 0.48 208110. 0.3286 42.71 0.3790 0.6952 0.0436 0.0238 0.931 8.386 5.685 694.530 0.947 25.287 3.713 0.48 208426. 0.3055 45.23 0.4013 0.7088 0.0402 0.0228 0.893 8.038 5.246 665.654 0.908 23.335 3.575 0.48 208756. 0.2826 47.74 0.4236 0.7190 0.0368 0.0217 0.849 7.648 4.797 633.368 0.864 21.338 3.435 0.48 209101. 0.2597 50.25 0.4459 0.7256 0.0333 0.0204 0.801 7.216 4.340 597.630 0.815 19.302 3.294 0.48 209459. 0.2368 52.76 0.4682 0.7279 0.0297 0.0191 0.749 6.743 3.874 558.407 0.762 17.231 3.147 0.48 209832. 0.2138 55.28 0.4905 0.7249 0.0261 0.0176 0.692 6.227 3.401 515.681 0.703 15.128 2.991 0.48 210220. 0.1904 57.79 0.5128 0.7153 0.0224 0.0161 0.630 5.668 2.922 469.450 0.640 12.998 2.823 0.48 210622. 0.1666 60.30 0.5351 0.6966 0.0187 0.0144 0.563 5.068 2.438 419.736 0.573 10.846 2.635 0.48 211038. 0.1420 62.82 0.5574 0.6647 0.0150 0.0125 0.492 4.426 1.951 366.593 0.500 8.677 2.414 0.48 211469. 0.1164 65.33 0.5797 0.6120 0.0112 0.0106 0.416 3.744 1.461 310.111 0.423 6.498 2.137 0.48 211915. 0.0891 67.84 0.6020 0.5226 0.0074 0.0086 0.336 3.024 0.970 250.423 0.342 4.316 1.757 0.48 212375. 0.0597 70.35 0.6243 0.3581 0.0037 0.0064 0.252 2.266 0.481 187.706 0.256 2.137 1.161 0.48 212848. 0.0278 72.87 0.6466 -0.0117 -0.0001 0.0042 0.163 1.469 -0.010 121.664 0.166 -0.044 -0.037 0.48 213308. 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 0.0844 0.0261 1.527 12.030 14.375 1138.606 1.359 63.941 5.726 0.54 234053. 0.7494 2.87 0.0223 0.0700 0.0830 0.0265 1.549 12.202 14.142 1154.938 1.379 62.904 5.554 0.54 234191. 0.7209 5.75 0.0446 0.1356 0.0815 0.0268 1.569 12.362 13.890 1170.097 1.397 61.783 5.384 0.54 234340. 0.6926 8.62 0.0669 0.1972 0.0799 0.0271 1.587 12.507 13.619 1183.761 1.413 60.575 5.218 0.54 234501. 0.6647 11.49 0.0892 0.2547 0.0782 0.0274 1.603 12.632 13.327 1195.613 1.427 59.277 5.056 0.54 234674. 0.6370 14.37 0.1115 0.3084 0.0764 0.0276 1.616 12.735 13.014 1205.325 1.439 57.884 4.897 0.54 234860. 0.6097 17.24 0.1339 0.3584 0.0744 0.0278 1.626 12.811 12.678 1212.558 1.447 56.394 4.743 0.54 235058. 0.5829 20.11 0.1562 0.4049 0.0723 0.0279 1.632 12.858 12.321 1216.969 1.453 54.804 4.592 0.54 235271. 0.5563 22.99 0.1785 0.4480 0.0701 0.0279 1.634 12.871 11.941 1218.219 1.454 53.112 4.446 0.54 235497. 0.5302 25.86 0.2008 0.4879 0.0677 0.0279 1.631 12.847 11.537 1215.970 1.451 51.316 4.303 0.54 235738. 0.5045 28.73 0.2231 0.5246 0.0652 0.0277 1.622 12.783 11.110 1209.889 1.444 49.417 4.165 0.54 235993. 0.4792 31.61 0.2454 0.5584 0.0626 0.0275 1.609 12.675 10.660 1199.651 1.432 47.414 4.030 0.54 236262. 0.4542 34.48 0.2677 0.5893 0.0598 0.0272 1.589 12.520 10.186 1184.973 1.414 45.309 3.899 0.54 236547. 0.4295 37.35 0.2900 0.6175 0.0569 0.0267 1.563 12.316 9.691 1165.658 1.391 43.107 3.771 0.54 236847. 0.4052 40.22 0.3123 0.6429 0.0539 0.0262 1.531 12.061 9.176 1141.579 1.363 40.816 3.646 0.54 237162. 0.3812 43.10 0.3346 0.6657 0.0507 0.0255 1.492 11.755 8.643 1112.641 1.328 38.442 3.523 0.54 237493. 0.3575 45.97 0.3570 0.6857 0.0475 0.0247 1.447 11.397 8.092 1078.752 1.288 35.993 3.402 0.54 237839. 0.3341 48.84 0.3793 0.7029 0.0442 0.0238 1.394 10.986 7.526 1039.834 1.241 33.474 3.283 0.54 238201. 0.3108 51.72 0.4016 0.7172 0.0408 0.0228 1.335 10.521 6.945 995.805 1.189 30.891 3.163 0.54 238580. 0.2877 54.59 0.4239 0.7283 0.0373 0.0217 1.269 10.001 6.351 946.591 1.130 28.250 3.043 0.54 238974. 0.2647 57.46 0.4462 0.7359 0.0337 0.0205 1.196 9.426 5.745 892.129 1.065 25.556 2.921 0.54 239385. 0.2417 60.34 0.4685 0.7393 0.0301 0.0191 1.116 8.794 5.129 832.369 0.994 22.814 2.795 0.55 239812. 0.2185 63.21 0.4908 0.7377 0.0264 0.0176 1.029 8.107 4.503 767.282 0.916 20.030 2.662 0.55 240255. 0.1950 66.08 0.5131 0.7296 0.0227 0.0160 0.935 7.363 3.869 696.867 0.832 17.210 2.518 0.55 240715. 0.1710 68.96 0.5354 0.7127 0.0190 0.0142 0.833 6.563 3.228 621.159 0.741 14.360 2.357 0.55 241192. 0.1462 71.83 0.5577 0.6828 0.0152 0.0124 0.724 5.708 2.583 540.237 0.645 11.488 2.168 0.55 241686. 0.1203 74.70 0.5801 0.6323 0.0114 0.0104 0.609 4.799 1.934 454.240 0.542 8.601 1.931 0.55 242196. 0.0927 77.58 0.6024 0.5448 0.0075 0.0083 0.487 3.839 1.283 363.373 0.434 5.709 1.602 0.55 242722. 0.0626 80.45 0.6247 0.3789 0.0037 0.0061 0.359 2.831 0.635 267.907 0.320 2.822 1.074 0.55 243264. 0.0295 83.32 0.6470 -0.0160 -0.0001 0.0038 0.224 1.767 -0.016 167.248 0.200 -0.072 -0.044 0.55 243783. 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 0.0855 0.0264 2.196 15.381 18.435 1637.779 1.738 81.998 5.105 0.61 263286. 0.7566 3.23 0.0223 0.0702 0.0841 0.0268 2.228 15.605 18.140 1661.635 1.763 80.687 4.952 0.61 263442. 0.7279 6.47 0.0446 0.1361 0.0827 0.0271 2.258 15.813 17.821 1683.767 1.787 79.268 4.801 0.61 263611. 0.6995 9.70 0.0670 0.1979 0.0811 0.0274 2.285 16.000 17.476 1703.696 1.808 77.735 4.653 0.61 263793. 0.6713 12.94 0.0893 0.2557 0.0793 0.0277 2.308 16.162 17.106 1720.958 1.826 76.086 4.508 0.61 263989. 0.6436 16.17 0.1116 0.3096 0.0775 0.0279 2.327 16.295 16.707 1735.071 1.841 74.313 4.367 0.61 264199. 0.6162 19.40 0.1339 0.3599 0.0755 0.0281 2.341 16.393 16.280 1745.545 1.852 72.414 4.230 0.61 264424. 0.5891 22.64 0.1562 0.4066 0.0734 0.0282 2.349 16.453 15.824 1751.882 1.859 70.385 4.097 0.61 264664. 0.5625 25.87 0.1786 0.4500 0.0711 0.0282 2.352 16.469 15.338 1753.591 1.861 68.224 3.967 0.61 264920. 0.5363 29.11 0.2009 0.4901 0.0687 0.0282 2.347 16.437 14.822 1750.181 1.857 65.929 3.841 0.61 265192. 0.5104 32.34 0.2232 0.5272 0.0662 0.0280 2.335 16.352 14.276 1741.178 1.847 63.499 3.719 0.61 265480. 0.4850 35.57 0.2455 0.5614 0.0635 0.0278 2.315 16.211 13.699 1726.111 1.831 60.934 3.600 0.61 265785. 0.4599 38.81 0.2679 0.5927 0.0607 0.0274 2.286 16.008 13.093 1704.569 1.809 58.237 3.484 0.61 266107. 0.4351 42.04 0.2902 0.6213 0.0578 0.0270 2.248 15.742 12.458 1676.268 1.779 55.414 3.371 0.61 266445. 0.4107 45.28 0.3125 0.6472 0.0547 0.0264 2.201 15.411 11.797 1641.025 1.741 52.475 3.261 0.61 266801. 0.3866 48.51 0.3348 0.6705 0.0515 0.0257 2.144 15.014 11.113 1598.707 1.696 49.429 3.153 0.61 267175. 0.3628 51.74 0.3571 0.6911 0.0483 0.0249 2.077 14.549 10.406 1549.190 1.644 46.284 3.047 0.61 267566. 0.3392 54.98 0.3795 0.7090 0.0449 0.0240 2.001 14.015 9.678 1492.358 1.583 43.049 2.941 0.61 267975. 0.3158 58.21 0.4018 0.7240 0.0414 0.0230 1.915 13.412 8.932 1428.100 1.515 39.731 2.837 0.61 268401. 0.2926 61.45 0.4241 0.7359 0.0379 0.0218 1.819 12.738 8.169 1356.310 1.439 36.337 2.732 0.61 268846. 0.2695 64.68 0.4464 0.7444 0.0343 0.0206 1.712 11.992 7.391 1276.897 1.355 32.874 2.625 0.61 269309. 0.2463 67.92 0.4687 0.7489 0.0306 0.0192 1.596 11.174 6.598 1189.790 1.262 29.349 2.515 0.61 269791. 0.2230 71.15 0.4911 0.7485 0.0269 0.0176 1.468 10.283 5.793 1094.948 1.162 25.768 2.400 0.61 270291. 0.1994 74.38 0.5134 0.7419 0.0231 0.0160 1.331 9.320 4.978 992.369 1.053 22.141 2.275 0.61 270810. 0.1752 77.62 0.5357 0.7267 0.0193 0.0142 1.183 8.284 4.153 882.104 0.936 18.474 2.136 0.62 271347. 0.1502 80.85 0.5580 0.6988 0.0154 0.0123 1.025 7.178 3.322 764.268 0.811 14.777 1.972 0.62 271903. 0.1240 84.09 0.5804 0.6506 0.0115 0.0103 0.857 6.002 2.487 639.065 0.678 11.061 1.765 0.62 272477. 0.0961 87.32 0.6027 0.5651 0.0077 0.0082 0.680 4.759 1.650 506.794 0.538 7.337 1.476 0.62 273070. 0.0654 90.55 0.6250 0.3984 0.0038 0.0059 0.493 3.455 0.814 367.851 0.390 3.621 1.004 0.62 273680. 0.0313 93.79 0.6473 -0.0215 -0.0001 0.0036 0.297 2.077 -0.025 221.120 0.235 -0.113 -0.052 0.62 274256. 0.0000 PROP RPM = 10000 V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM (mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - - 0.00 0.0000 0.0000 0.0868 0.0268 3.061 19.291 23.112 2282.312 2.179 102.803 4.593 0.67 292509. 0.7622 3.60 0.0223 0.0702 0.0855 0.0272 3.106 19.574 22.750 2315.828 2.211 101.191 4.456 0.67 292683. 0.7335 7.19 0.0447 0.1362 0.0840 0.0275 3.147 19.837 22.356 2346.941 2.241 99.440 4.321 0.67 292872. 0.7051 10.79 0.0670 0.1980 0.0824 0.0279 3.185 20.074 21.930 2374.968 2.268 97.547 4.188 0.67 293075. 0.6770 14.38 0.0893 0.2559 0.0807 0.0282 3.217 20.279 21.471 2399.226 2.291 95.503 4.059 0.67 293294. 0.6492 17.98 0.1117 0.3100 0.0788 0.0284 3.244 20.446 20.976 2419.022 2.310 93.303 3.933 0.67 293530. 0.6218 21.57 0.1340 0.3604 0.0768 0.0286 3.264 20.570 20.446 2433.645 2.324 90.942 3.811 0.67 293781. 0.5947 25.17 0.1563 0.4073 0.0747 0.0287 3.275 20.644 19.878 2442.392 2.332 88.415 3.691 0.68 294050. 0.5681 28.76 0.1787 0.4509 0.0724 0.0287 3.278 20.662 19.271 2444.568 2.334 85.720 3.576 0.68 294336. 0.5418 32.36 0.2010 0.4913 0.0700 0.0286 3.271 20.619 18.627 2439.500 2.330 82.853 3.463 0.68 294640. 0.5159 35.95 0.2233 0.5287 0.0674 0.0285 3.254 20.510 17.944 2426.523 2.317 79.815 3.354 0.68 294962. 0.4904 39.55 0.2457 0.5631 0.0647 0.0282 3.225 20.328 17.223 2404.988 2.297 76.606 3.248 0.68 295303. 0.4653 43.14 0.2680 0.5948 0.0619 0.0279 3.184 20.068 16.463 2374.321 2.267 73.228 3.145 0.68 295662. 0.4404 46.74 0.2903 0.6238 0.0589 0.0274 3.130 19.729 15.668 2334.128 2.229 69.690 3.045 0.68 296040. 0.4159 50.33 0.3127 0.6502 0.0558 0.0268 3.063 19.306 14.839 2284.160 2.181 66.003 2.947 0.68 296437. 0.3918 53.93 0.3350 0.6740 0.0525 0.0261 2.983 18.800 13.979 2224.232 2.124 62.180 2.851 0.68 296854. 0.3679 57.52 0.3573 0.6951 0.0492 0.0253 2.889 18.208 13.092 2154.188 2.057 58.232 2.756 0.68 297290. 0.3442 61.12 0.3797 0.7137 0.0458 0.0243 2.781 17.529 12.178 2073.871 1.980 54.168 2.663 0.68 297746. 0.3208 64.71 0.4020 0.7294 0.0422 0.0233 2.659 16.762 11.241 1983.129 1.894 49.999 2.571 0.68 298222. 0.2975 68.31 0.4243 0.7421 0.0386 0.0221 2.524 15.906 10.282 1881.818 1.797 45.733 2.478 0.68 298718. 0.2743 71.90 0.4467 0.7515 0.0350 0.0208 2.373 14.959 9.303 1769.814 1.690 41.378 2.384 0.68 299234. 0.2510 75.50 0.4690 0.7571 0.0312 0.0193 2.209 13.921 8.306 1647.025 1.573 36.944 2.287 0.68 299770. 0.2275 79.10 0.4913 0.7579 0.0274 0.0178 2.029 12.792 7.293 1513.390 1.445 32.439 2.186 0.68 300327. 0.2037 82.69 0.5137 0.7527 0.0235 0.0161 1.836 11.570 6.266 1368.909 1.307 27.873 2.076 0.68 300904. 0.1794 86.29 0.5360 0.7392 0.0196 0.0142 1.628 10.258 5.229 1213.653 1.159 23.256 1.954 0.68 301502. 0.1542 89.88 0.5583 0.7133 0.0157 0.0123 1.405 8.856 4.182 1047.790 1.001 18.600 1.810 0.68 302121. 0.1278 93.48 0.5807 0.6673 0.0118 0.0102 1.169 7.367 3.129 871.622 0.832 13.918 1.628 0.69 302760. 0.0994 97.07 0.6030 0.5840 0.0078 0.0080 0.919 5.795 2.074 685.610 0.655 9.226 1.372 0.69 303420. 0.0682 100.67 0.6253 0.4168 0.0038 0.0058 0.658 4.145 1.021 490.367 0.468 4.542 0.944 0.69 304099. 0.0329 104.26 0.6477 -0.0291 -0.0001 0.0033 0.381 2.400 -0.040 283.902 0.271 -0.177 -0.064 0.69 304725. 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 0.0884 0.0277 4.206 24.101 28.470 3136.622 2.723 126.636 4.117 0.74 321717. 0.7582 3.95 0.0223 0.0693 0.0871 0.0280 4.261 24.415 28.036 3177.487 2.758 124.705 4.002 0.74 321910. 0.7314 7.90 0.0446 0.1347 0.0856 0.0284 4.312 24.706 27.563 3215.340 2.791 122.602 3.888 0.74 322119. 0.7046 11.86 0.0670 0.1963 0.0840 0.0287 4.357 24.967 27.050 3249.323 2.821 120.318 3.776 0.74 322344. 0.6778 15.81 0.0893 0.2540 0.0823 0.0289 4.397 25.192 26.494 3278.571 2.846 117.846 3.665 0.74 322587. 0.6512 19.76 0.1116 0.3081 0.0804 0.0291 4.428 25.373 25.894 3302.175 2.867 115.178 3.557 0.74 322847. 0.6247 23.71 0.1339 0.3587 0.0784 0.0293 4.451 25.504 25.249 3319.165 2.881 112.307 3.450 0.74 323126. 0.5984 27.67 0.1562 0.4059 0.0762 0.0294 4.464 25.576 24.557 3328.577 2.890 109.228 3.346 0.74 323423. 0.5723 31.62 0.1786 0.4498 0.0740 0.0294 4.465 25.583 23.817 3329.439 2.890 105.936 3.245 0.74 323740. 0.5465 35.57 0.2009 0.4905 0.0715 0.0293 4.453 25.516 23.028 3320.787 2.883 102.430 3.145 0.74 324076. 0.5210 39.52 0.2232 0.5282 0.0689 0.0291 4.428 25.370 22.191 3301.665 2.866 98.707 3.049 0.74 324432. 0.4957 43.48 0.2455 0.5631 0.0662 0.0288 4.387 25.135 21.306 3271.123 2.840 94.770 2.954 0.74 324808. 0.4707 47.43 0.2678 0.5952 0.0633 0.0285 4.329 24.806 20.373 3228.314 2.803 90.621 2.862 0.74 325205. 0.4459 51.38 0.2902 0.6246 0.0602 0.0280 4.255 24.378 19.395 3172.606 2.754 86.271 2.773 0.74 325623. 0.4215 55.33 0.3125 0.6515 0.0571 0.0274 4.162 23.848 18.375 3103.594 2.694 81.734 2.685 0.75 326061. 0.3973 59.29 0.3348 0.6758 0.0538 0.0266 4.051 23.213 17.317 3021.002 2.623 77.026 2.600 0.75 326521. 0.3734 63.24 0.3571 0.6975 0.0504 0.0258 3.922 22.472 16.223 2924.607 2.539 72.160 2.516 0.75 327002. 0.3498 67.19 0.3794 0.7167 0.0469 0.0248 3.774 21.624 15.096 2814.195 2.443 67.149 2.433 0.75 327505. 0.3263 71.14 0.4018 0.7332 0.0433 0.0237 3.607 20.666 13.940 2689.592 2.335 62.006 2.351 0.75 328029. 0.3030 75.10 0.4241 0.7468 0.0396 0.0225 3.420 19.599 12.756 2550.619 2.214 56.740 2.268 0.75 328576. 0.2796 79.05 0.4464 0.7572 0.0359 0.0211 3.215 18.419 11.547 2397.114 2.081 51.363 2.185 0.75 329144. 0.2563 83.00 0.4687 0.7638 0.0320 0.0197 2.989 17.127 10.316 2229.020 1.935 45.885 2.099 0.75 329735. 0.2327 86.95 0.4910 0.7659 0.0281 0.0180 2.744 15.724 9.064 2046.318 1.776 40.318 2.009 0.75 330348. 0.2088 90.91 0.5134 0.7620 0.0242 0.0163 2.480 14.208 7.795 1849.099 1.605 34.672 1.912 0.75 330983. 0.1843 94.86 0.5357 0.7499 0.0202 0.0144 2.196 12.583 6.511 1637.604 1.422 28.960 1.803 0.75 331641. 0.1588 98.81 0.5580 0.7255 0.0162 0.0125 1.894 10.852 5.215 1412.263 1.226 23.196 1.675 0.75 332322. 0.1320 102.76 0.5803 0.6809 0.0121 0.0104 1.574 9.019 3.911 1173.734 1.019 17.397 1.511 0.75 333025. 0.1032 106.72 0.6026 0.5986 0.0081 0.0081 1.238 7.092 2.604 922.958 0.801 11.581 1.280 0.76 333750. 0.0713 110.67 0.6250 0.4318 0.0040 0.0058 0.887 5.080 1.297 661.136 0.574 5.771 0.890 0.76 334496. 0.0350 114.62 0.6473 -0.0092 0.0000 0.0034 0.519 2.971 -0.016 386.719 0.336 -0.069 -0.018 0.76 335202. 0.0000 PROP RPM = 12000 V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM (mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - - 0.00 0.0000 0.0000 0.0902 0.0301 5.937 31.183 34.580 4427.209 3.523 153.812 3.543 0.81 350907. 0.7191 4.31 0.0223 0.0655 0.0889 0.0303 5.984 31.432 34.074 4462.500 3.551 151.560 3.463 0.81 351119. 0.6978 8.63 0.0447 0.1279 0.0875 0.0305 6.026 31.649 33.519 4493.290 3.576 149.093 3.384 0.81 351348. 0.6761 12.94 0.0670 0.1874 0.0859 0.0307 6.060 31.828 32.914 4518.695 3.596 146.402 3.304 0.81 351596. 0.6542 17.25 0.0893 0.2438 0.0842 0.0308 6.085 31.962 32.256 4537.786 3.611 143.474 3.224 0.81 351863. 0.6320 21.56 0.1116 0.2973 0.0823 0.0309 6.101 32.045 31.543 4549.624 3.620 140.301 3.145 0.81 352149. 0.6096 25.88 0.1340 0.3477 0.0803 0.0309 6.106 32.071 30.772 4553.225 3.623 136.874 3.065 0.81 352456. 0.5869 30.19 0.1563 0.3953 0.0781 0.0309 6.098 32.031 29.943 4547.515 3.619 133.187 2.987 0.81 352783. 0.5641 34.50 0.1786 0.4399 0.0758 0.0308 6.077 31.917 29.054 4531.401 3.606 129.233 2.908 0.81 353132. 0.5411 38.82 0.2009 0.4816 0.0733 0.0306 6.040 31.722 28.105 4503.768 3.584 125.011 2.830 0.81 353501. 0.5179 43.13 0.2233 0.5206 0.0707 0.0303 5.986 31.439 27.095 4463.514 3.552 120.519 2.753 0.81 353893. 0.4947 47.44 0.2456 0.5567 0.0679 0.0300 5.913 31.059 26.024 4409.519 3.509 115.757 2.677 0.81 354306. 0.4713 51.75 0.2679 0.5902 0.0650 0.0295 5.821 30.574 24.894 4340.706 3.454 110.730 2.601 0.81 354742. 0.4480 56.07 0.2902 0.6210 0.0619 0.0289 5.708 29.979 23.708 4256.250 3.387 105.452 2.526 0.81 355201. 0.4246 60.38 0.3126 0.6491 0.0586 0.0282 5.573 29.270 22.468 4155.579 3.307 99.940 2.452 0.81 355682. 0.4012 64.69 0.3349 0.6747 0.0553 0.0274 5.415 28.443 21.181 4038.226 3.214 94.213 2.379 0.81 356186. 0.3779 69.01 0.3572 0.6977 0.0518 0.0265 5.235 27.496 19.849 3903.751 3.107 88.288 2.306 0.81 356714. 0.3546 73.32 0.3795 0.7179 0.0482 0.0255 5.032 26.429 18.476 3752.218 2.986 82.182 2.233 0.82 357265. 0.3314 77.63 0.4019 0.7352 0.0445 0.0243 4.805 25.238 17.066 3583.175 2.851 75.910 2.160 0.82 357839. 0.3080 81.94 0.4242 0.7495 0.0408 0.0231 4.554 23.921 15.622 3396.208 2.703 69.485 2.086 0.82 358438. 0.2846 86.26 0.4465 0.7602 0.0369 0.0217 4.280 22.478 14.146 3191.362 2.540 62.920 2.010 0.82 359060. 0.2610 90.57 0.4688 0.7670 0.0330 0.0202 3.981 20.907 12.641 2968.317 2.362 56.228 1.932 0.82 359706. 0.2370 94.88 0.4912 0.7686 0.0290 0.0185 3.657 19.210 11.111 2727.342 2.170 49.421 1.848 0.82 360377. 0.2126 99.20 0.5135 0.7635 0.0249 0.0168 3.311 17.391 9.558 2469.134 1.965 42.514 1.756 0.82 361072. 0.1874 103.51 0.5358 0.7489 0.0208 0.0149 2.943 15.458 7.986 2194.577 1.746 35.521 1.650 0.82 361791. 0.1610 107.82 0.5581 0.7201 0.0167 0.0129 2.554 13.417 6.398 1904.867 1.516 28.459 1.523 0.82 362535. 0.1330 112.13 0.5805 0.6682 0.0125 0.0109 2.148 11.281 4.800 1601.569 1.274 21.349 1.359 0.82 363303. 0.1028 116.45 0.6028 0.5750 0.0083 0.0087 1.725 9.062 3.195 1286.625 1.024 14.212 1.126 0.82 364095. 0.0695 120.76 0.6251 0.3969 0.0041 0.0065 1.290 6.778 1.590 962.313 0.766 7.074 0.750 0.83 364910. 0.0326 125.07 0.6474 -0.0088 -0.0001 0.0043 0.841 4.416 -0.022 626.930 0.499 -0.099 -0.016 0.83 365686. 0.0000 PROP RPM = 13000 V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM (mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - - 0.00 0.0000 0.0000 0.0920 0.0354 8.883 43.067 41.389 6623.882 4.866 184.099 2.834 0.88 380083. 0.6293 4.68 0.0224 0.0573 0.0908 0.0355 8.901 43.153 40.827 6637.123 4.875 181.599 2.790 0.88 380312. 0.6153 9.37 0.0448 0.1128 0.0894 0.0355 8.905 43.174 40.204 6640.421 4.878 178.830 2.746 0.88 380562. 0.6010 14.05 0.0671 0.1664 0.0879 0.0354 8.895 43.125 39.518 6632.883 4.872 175.776 2.702 0.88 380832. 0.5863 18.73 0.0895 0.2183 0.0862 0.0353 8.869 43.001 38.765 6613.799 4.858 172.425 2.658 0.88 381123. 0.5713 23.42 0.1119 0.2684 0.0843 0.0352 8.827 42.798 37.941 6582.528 4.835 168.762 2.614 0.88 381436. 0.5558 28.10 0.1343 0.3166 0.0824 0.0349 8.768 42.511 37.045 6538.467 4.803 164.777 2.570 0.88 381772. 0.5399 32.78 0.1566 0.3628 0.0802 0.0346 8.691 42.138 36.075 6481.035 4.761 160.463 2.525 0.88 382131. 0.5234 37.46 0.1790 0.4071 0.0779 0.0342 8.595 41.674 35.030 6409.624 4.708 155.812 2.479 0.88 382512. 0.5064 42.15 0.2014 0.4494 0.0754 0.0338 8.480 41.114 33.908 6323.565 4.645 150.822 2.432 0.88 382918. 0.4888 46.83 0.2238 0.4895 0.0727 0.0332 8.344 40.454 32.710 6222.109 4.571 145.494 2.384 0.88 383347. 0.4707 51.51 0.2461 0.5275 0.0699 0.0326 8.186 39.689 31.436 6104.396 4.484 139.827 2.336 0.88 383800. 0.4520 56.20 0.2685 0.5632 0.0669 0.0319 8.005 38.812 30.087 5969.501 4.385 133.827 2.286 0.88 384278. 0.4328 60.88 0.2909 0.5966 0.0637 0.0311 7.800 37.818 28.667 5816.671 4.273 127.510 2.235 0.88 384780. 0.4131 65.56 0.3133 0.6277 0.0604 0.0302 7.571 36.705 27.180 5645.375 4.147 120.896 2.184 0.88 385307. 0.3930 70.25 0.3357 0.6563 0.0570 0.0291 7.316 35.468 25.632 5455.241 4.007 114.010 2.131 0.88 385859. 0.3724 74.93 0.3580 0.6824 0.0534 0.0280 7.035 34.108 24.027 5245.938 3.853 106.874 2.077 0.88 386436. 0.3515 79.61 0.3804 0.7059 0.0497 0.0268 6.728 32.620 22.372 5017.115 3.685 99.510 2.023 0.88 387038. 0.3302 84.29 0.4028 0.7259 0.0459 0.0255 6.400 31.028 20.669 4772.273 3.506 91.934 1.964 0.88 387666. 0.3082 88.98 0.4252 0.7422 0.0421 0.0241 6.049 29.326 18.922 4510.465 3.313 84.166 1.903 0.88 388320. 0.2857 93.66 0.4475 0.7541 0.0381 0.0226 5.675 27.515 17.136 4232.006 3.109 76.221 1.837 0.89 388999. 0.2624 98.34 0.4699 0.7576 0.0340 0.0211 5.300 25.698 15.312 3952.469 2.903 68.107 1.757 0.89 389704. 0.2373 103.03 0.4923 0.7540 0.0299 0.0195 4.903 23.770 13.455 3655.997 2.686 59.849 1.669 0.89 390436. 0.2113 107.71 0.5147 0.7412 0.0257 0.0179 4.483 21.737 11.570 3343.285 2.456 51.465 1.570 0.89 391194. 0.1843 112.39 0.5370 0.7157 0.0215 0.0161 4.046 19.615 9.661 3016.858 2.216 42.974 1.453 0.89 391978. 0.1558 117.08 0.5594 0.6720 0.0172 0.0143 3.593 17.418 7.733 2678.978 1.968 34.398 1.309 0.89 392788. 0.1257 121.76 0.5818 0.6012 0.0129 0.0125 3.128 15.166 5.793 2332.563 1.713 25.765 1.126 0.89 393625. 0.0936 126.44 0.6042 0.4881 0.0085 0.0106 2.656 12.879 3.846 1980.901 1.455 17.107 0.881 0.89 394488. 0.0596 131.12 0.6266 0.3047 0.0042 0.0087 2.182 10.581 1.902 1627.352 1.195 8.460 0.530 0.89 395375. 0.0252 135.81 0.6489 -0.0097 -0.0001 0.0068 1.701 8.246 -0.046 1268.307 0.932 -0.204 -0.016 0.90 396238. 0.0000