20x12 (20x12.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 0.0838 0.0337 0.009 0.547 0.427 6.468 0.062 1.900 29.961 0.08 31277. 0.5746 0.51 0.0271 0.0654 0.0829 0.0344 0.009 0.558 0.423 6.601 0.063 1.881 29.058 0.08 31297. 0.5544 1.03 0.0542 0.1267 0.0820 0.0351 0.009 0.569 0.418 6.732 0.064 1.859 28.158 0.08 31320. 0.5340 1.54 0.0813 0.1840 0.0809 0.0357 0.009 0.580 0.412 6.859 0.065 1.834 27.264 0.08 31346. 0.5136 2.05 0.1084 0.2374 0.0796 0.0363 0.009 0.590 0.406 6.979 0.067 1.806 26.381 0.08 31373. 0.4931 2.57 0.1355 0.2870 0.0782 0.0369 0.010 0.599 0.399 7.090 0.068 1.774 25.511 0.08 31404. 0.4727 3.08 0.1626 0.3329 0.0766 0.0374 0.010 0.608 0.391 7.188 0.069 1.738 24.659 0.08 31437. 0.4522 3.59 0.1897 0.3752 0.0749 0.0379 0.010 0.614 0.382 7.270 0.069 1.699 23.824 0.08 31473. 0.4319 4.11 0.2168 0.4141 0.0729 0.0382 0.010 0.620 0.372 7.333 0.070 1.655 23.009 0.08 31512. 0.4117 4.62 0.2439 0.4498 0.0708 0.0384 0.010 0.623 0.361 7.372 0.070 1.606 22.213 0.08 31555. 0.3916 5.13 0.2710 0.4823 0.0685 0.0385 0.010 0.624 0.349 7.386 0.071 1.553 21.436 0.08 31600. 0.3716 5.64 0.2981 0.5117 0.0659 0.0384 0.010 0.623 0.336 7.371 0.070 1.495 20.678 0.08 31648. 0.3517 6.16 0.3251 0.5382 0.0632 0.0382 0.010 0.619 0.322 7.328 0.070 1.433 19.936 0.08 31700. 0.3319 6.67 0.3522 0.5618 0.0602 0.0378 0.010 0.613 0.307 7.253 0.069 1.366 19.208 0.08 31755. 0.3123 7.18 0.3793 0.5824 0.0572 0.0372 0.010 0.604 0.291 7.149 0.068 1.296 18.490 0.08 31813. 0.2929 7.70 0.4064 0.6000 0.0539 0.0365 0.009 0.593 0.275 7.014 0.067 1.223 17.779 0.08 31875. 0.2735 8.21 0.4335 0.6145 0.0505 0.0357 0.009 0.579 0.258 6.848 0.065 1.146 17.070 0.08 31939. 0.2543 8.72 0.4606 0.6256 0.0471 0.0346 0.009 0.562 0.240 6.653 0.064 1.067 16.358 0.08 32007. 0.2351 9.24 0.4877 0.6332 0.0435 0.0335 0.009 0.543 0.222 6.428 0.061 0.986 15.637 0.08 32078. 0.2160 9.75 0.5148 0.6369 0.0398 0.0321 0.008 0.522 0.203 6.173 0.059 0.902 14.900 0.08 32153. 0.1968 10.26 0.5419 0.6361 0.0360 0.0307 0.008 0.498 0.184 5.888 0.056 0.816 14.136 0.08 32230. 0.1777 10.78 0.5690 0.6300 0.0321 0.0290 0.007 0.471 0.164 5.574 0.053 0.729 13.335 0.08 32311. 0.1584 11.29 0.5961 0.6176 0.0282 0.0272 0.007 0.442 0.144 5.230 0.050 0.640 12.479 0.08 32396. 0.1389 11.80 0.6232 0.5974 0.0242 0.0253 0.007 0.411 0.124 4.858 0.046 0.550 11.544 0.08 32483. 0.1191 12.32 0.6503 0.5669 0.0202 0.0232 0.006 0.377 0.103 4.457 0.043 0.459 10.499 0.08 32574. 0.0989 12.83 0.6774 0.5226 0.0162 0.0210 0.005 0.341 0.083 4.029 0.038 0.367 9.293 0.08 32668. 0.0783 13.34 0.7045 0.4588 0.0121 0.0186 0.005 0.302 0.062 3.574 0.034 0.275 7.844 0.08 32765. 0.0572 13.86 0.7316 0.3656 0.0081 0.0161 0.004 0.261 0.041 3.093 0.030 0.183 6.019 0.08 32866. 0.0358 14.37 0.7587 0.2246 0.0040 0.0135 0.003 0.219 0.020 2.589 0.025 0.091 3.565 0.08 32969. 0.0149 14.88 0.7858 -0.0035 0.0000 0.0107 0.003 0.174 0.000 2.063 0.020 -0.001 -0.054 0.08 33075. 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 0.0842 0.0302 0.062 1.961 1.717 46.409 0.222 7.636 16.777 0.16 62553. 0.6449 1.03 0.0272 0.0733 0.0833 0.0309 0.064 2.009 1.699 47.531 0.227 7.559 16.216 0.16 62594. 0.6202 2.06 0.0545 0.1416 0.0824 0.0317 0.065 2.056 1.680 48.647 0.232 7.471 15.661 0.16 62640. 0.5955 3.09 0.0817 0.2050 0.0813 0.0324 0.067 2.102 1.657 49.737 0.237 7.372 15.115 0.16 62691. 0.5709 4.13 0.1089 0.2637 0.0800 0.0331 0.068 2.146 1.632 50.777 0.242 7.260 14.579 0.16 62747. 0.5465 5.16 0.1361 0.3178 0.0786 0.0337 0.069 2.187 1.604 51.744 0.247 7.133 14.057 0.16 62808. 0.5223 6.19 0.1634 0.3676 0.0771 0.0342 0.071 2.223 1.572 52.611 0.251 6.991 13.550 0.16 62875. 0.4984 7.22 0.1906 0.4133 0.0753 0.0347 0.072 2.255 1.536 53.350 0.255 6.832 13.059 0.16 62948. 0.4748 8.25 0.2178 0.4552 0.0734 0.0351 0.072 2.279 1.496 53.932 0.258 6.655 12.583 0.16 63027. 0.4516 9.28 0.2451 0.4934 0.0712 0.0354 0.073 2.296 1.452 54.331 0.259 6.460 12.124 0.16 63113. 0.4287 10.31 0.2723 0.5282 0.0688 0.0355 0.073 2.304 1.404 54.519 0.260 6.246 11.682 0.16 63204. 0.4061 11.35 0.2995 0.5598 0.0663 0.0355 0.073 2.302 1.352 54.478 0.260 6.013 11.255 0.16 63302. 0.3839 12.38 0.3268 0.5883 0.0635 0.0353 0.073 2.290 1.295 54.192 0.259 5.762 10.842 0.16 63406. 0.3620 13.41 0.3540 0.6138 0.0606 0.0349 0.072 2.268 1.235 53.657 0.256 5.495 10.442 0.16 63517. 0.3405 14.44 0.3812 0.6364 0.0575 0.0344 0.071 2.234 1.172 52.867 0.252 5.212 10.053 0.16 63634. 0.3193 15.47 0.4084 0.6561 0.0542 0.0337 0.069 2.190 1.105 51.822 0.247 4.916 9.674 0.16 63758. 0.2984 16.50 0.4357 0.6729 0.0508 0.0329 0.068 2.135 1.036 50.522 0.241 4.608 9.300 0.16 63889. 0.2777 17.53 0.4629 0.6865 0.0473 0.0319 0.066 2.069 0.964 48.966 0.234 4.289 8.931 0.16 64026. 0.2573 18.57 0.4901 0.6970 0.0436 0.0307 0.063 1.993 0.890 47.155 0.225 3.960 8.563 0.16 64169. 0.2370 19.60 0.5174 0.7038 0.0399 0.0294 0.060 1.906 0.814 45.090 0.215 3.622 8.192 0.16 64320. 0.2169 20.63 0.5446 0.7066 0.0361 0.0278 0.057 1.808 0.737 42.770 0.204 3.277 7.814 0.16 64476. 0.1968 21.66 0.5718 0.7048 0.0322 0.0262 0.054 1.699 0.658 40.197 0.192 2.926 7.422 0.16 64640. 0.1766 22.69 0.5991 0.6971 0.0283 0.0243 0.050 1.579 0.577 37.371 0.178 2.568 7.008 0.16 64810. 0.1562 23.72 0.6263 0.6822 0.0243 0.0223 0.046 1.449 0.496 34.297 0.164 2.206 6.559 0.16 64987. 0.1355 24.75 0.6535 0.6574 0.0203 0.0202 0.042 1.309 0.414 30.977 0.148 1.840 6.058 0.16 65170. 0.1143 25.79 0.6807 0.6188 0.0162 0.0178 0.037 1.159 0.331 27.420 0.131 1.472 5.474 0.16 65360. 0.0924 26.82 0.7080 0.5591 0.0121 0.0154 0.032 0.999 0.248 23.633 0.113 1.102 4.756 0.16 65556. 0.0694 27.85 0.7352 0.4645 0.0081 0.0128 0.026 0.830 0.165 19.629 0.094 0.732 3.804 0.16 65759. 0.0453 28.88 0.7624 0.3047 0.0040 0.0100 0.021 0.652 0.082 15.423 0.074 0.364 2.407 0.16 65968. 0.0202 29.91 0.7897 -0.0037 0.0000 0.0072 0.015 0.465 -0.001 11.011 0.053 -0.003 -0.028 0.16 66178. 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 0.0845 0.0289 0.201 4.215 3.878 149.622 0.476 17.251 11.757 0.24 93828. 0.6793 1.55 0.0273 0.0771 0.0837 0.0296 0.206 4.325 3.840 153.522 0.489 17.082 11.346 0.24 93890. 0.6523 3.10 0.0546 0.1487 0.0827 0.0304 0.211 4.435 3.797 157.410 0.501 16.888 10.940 0.24 93959. 0.6254 4.65 0.0818 0.2149 0.0817 0.0311 0.216 4.542 3.747 161.216 0.513 16.668 10.542 0.24 94035. 0.5987 6.20 0.1091 0.2760 0.0804 0.0318 0.221 4.645 3.691 164.865 0.525 16.418 10.155 0.24 94119. 0.5724 7.75 0.1364 0.3322 0.0790 0.0325 0.226 4.741 3.627 168.270 0.536 16.135 9.778 0.24 94212. 0.5464 9.30 0.1637 0.3837 0.0775 0.0330 0.230 4.827 3.556 171.340 0.545 15.817 9.413 0.24 94312. 0.5208 10.85 0.1909 0.4309 0.0757 0.0336 0.233 4.902 3.476 173.977 0.554 15.460 9.061 0.24 94422. 0.4956 12.40 0.2182 0.4741 0.0738 0.0340 0.236 4.961 3.386 176.085 0.560 15.063 8.723 0.24 94541. 0.4709 13.95 0.2455 0.5135 0.0716 0.0342 0.238 5.003 3.288 177.565 0.565 14.623 8.398 0.24 94669. 0.4467 15.50 0.2728 0.5493 0.0693 0.0344 0.239 5.024 3.179 178.329 0.568 14.140 8.086 0.24 94807. 0.4230 17.05 0.3000 0.5819 0.0667 0.0344 0.239 5.024 3.061 178.303 0.568 13.614 7.786 0.24 94954. 0.3996 18.60 0.3273 0.6113 0.0639 0.0342 0.238 4.999 2.933 177.440 0.565 13.048 7.498 0.24 95111. 0.3768 20.15 0.3546 0.6378 0.0610 0.0339 0.236 4.951 2.798 175.713 0.559 12.444 7.221 0.24 95278. 0.3544 21.70 0.3819 0.6614 0.0578 0.0334 0.232 4.877 2.654 173.109 0.551 11.805 6.954 0.24 95455. 0.3324 23.25 0.4091 0.6822 0.0546 0.0327 0.227 4.779 2.503 169.621 0.540 11.135 6.694 0.24 95641. 0.3107 24.80 0.4364 0.7002 0.0511 0.0319 0.222 4.656 2.347 165.246 0.526 10.438 6.441 0.24 95838. 0.2895 26.35 0.4637 0.7152 0.0476 0.0309 0.215 4.507 2.184 159.985 0.509 9.715 6.192 0.24 96044. 0.2685 27.90 0.4910 0.7272 0.0439 0.0297 0.206 4.334 2.017 153.836 0.490 8.971 5.946 0.24 96260. 0.2478 29.45 0.5182 0.7359 0.0402 0.0283 0.197 4.136 1.845 146.799 0.467 8.207 5.701 0.24 96486. 0.2272 31.00 0.5455 0.7409 0.0364 0.0268 0.186 3.913 1.669 138.874 0.442 7.426 5.452 0.24 96722. 0.2067 32.55 0.5728 0.7416 0.0325 0.0251 0.174 3.664 1.490 130.065 0.414 6.630 5.198 0.24 96968. 0.1862 34.09 0.6001 0.7370 0.0285 0.0232 0.161 3.392 1.309 120.377 0.383 5.821 4.931 0.24 97224. 0.1655 35.64 0.6273 0.7257 0.0245 0.0212 0.147 3.094 1.124 109.818 0.350 5.001 4.644 0.24 97490. 0.1445 37.19 0.6546 0.7052 0.0204 0.0190 0.132 2.772 0.938 98.403 0.313 4.174 4.325 0.24 97766. 0.1229 38.74 0.6819 0.6715 0.0164 0.0166 0.116 2.427 0.751 86.156 0.274 3.340 3.953 0.24 98052. 0.1005 40.29 0.7092 0.6169 0.0123 0.0141 0.098 2.060 0.563 73.108 0.233 2.504 3.492 0.24 98347. 0.0769 41.84 0.7365 0.5260 0.0082 0.0114 0.080 1.671 0.375 59.303 0.189 1.667 2.867 0.24 98652. 0.0515 43.39 0.7637 0.3616 0.0041 0.0086 0.060 1.262 0.188 44.796 0.143 0.835 1.901 0.24 98967. 0.0242 44.94 0.7910 0.0031 0.0000 0.0057 0.040 0.832 0.001 29.540 0.094 0.005 0.016 0.25 99281. 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 0.0849 0.0282 0.465 7.322 6.929 346.509 0.827 30.821 9.070 0.32 125100. 0.7005 2.08 0.0275 0.0798 0.0841 0.0290 0.477 7.523 6.863 356.031 0.850 30.524 8.743 0.32 125183. 0.6719 4.16 0.0549 0.1536 0.0832 0.0297 0.490 7.724 6.786 365.544 0.873 30.185 8.420 0.32 125276. 0.6435 6.24 0.0824 0.2218 0.0821 0.0305 0.503 7.921 6.699 374.872 0.895 29.797 8.105 0.32 125379. 0.6155 8.32 0.1099 0.2846 0.0809 0.0312 0.515 8.111 6.600 383.830 0.916 29.355 7.799 0.32 125492. 0.5878 10.40 0.1373 0.3422 0.0795 0.0319 0.526 8.288 6.487 392.206 0.936 28.853 7.502 0.32 125616. 0.5605 12.49 0.1648 0.3949 0.0779 0.0325 0.536 8.447 6.359 399.771 0.954 28.286 7.215 0.32 125752. 0.5338 14.57 0.1923 0.4432 0.0762 0.0331 0.545 8.585 6.216 406.286 0.970 27.649 6.940 0.32 125901. 0.5076 16.65 0.2198 0.4872 0.0742 0.0335 0.552 8.695 6.056 411.507 0.982 26.938 6.675 0.32 126061. 0.4819 18.73 0.2472 0.5273 0.0721 0.0338 0.557 8.773 5.879 415.195 0.991 26.148 6.422 0.32 126234. 0.4568 20.81 0.2747 0.5638 0.0697 0.0339 0.559 8.814 5.683 417.125 0.996 25.280 6.180 0.32 126420. 0.4322 22.89 0.3022 0.5969 0.0671 0.0339 0.559 8.814 5.470 417.120 0.996 24.332 5.948 0.32 126619. 0.4082 24.97 0.3296 0.6270 0.0642 0.0338 0.557 8.770 5.241 415.061 0.991 23.310 5.727 0.32 126831. 0.3846 27.05 0.3571 0.6540 0.0612 0.0334 0.551 8.682 4.995 410.883 0.981 22.219 5.514 0.32 127057. 0.3616 29.13 0.3846 0.6782 0.0581 0.0329 0.543 8.548 4.736 404.552 0.966 21.066 5.310 0.32 127295. 0.3390 31.21 0.4120 0.6996 0.0547 0.0322 0.531 8.369 4.464 396.053 0.946 19.855 5.112 0.32 127547. 0.3169 33.30 0.4395 0.7182 0.0512 0.0314 0.517 8.143 4.180 385.378 0.920 18.595 4.920 0.32 127813. 0.2951 35.38 0.4670 0.7340 0.0476 0.0303 0.500 7.872 3.887 372.524 0.889 17.289 4.733 0.32 128091. 0.2737 37.46 0.4944 0.7468 0.0439 0.0291 0.479 7.554 3.584 357.488 0.853 15.944 4.548 0.32 128383. 0.2526 39.54 0.5219 0.7565 0.0401 0.0277 0.456 7.190 3.274 340.269 0.812 14.563 4.364 0.32 128689. 0.2317 41.62 0.5494 0.7626 0.0362 0.0261 0.430 6.780 2.957 320.869 0.766 13.152 4.180 0.32 129008. 0.2108 43.70 0.5769 0.7646 0.0323 0.0244 0.401 6.324 2.633 299.294 0.715 11.713 3.991 0.32 129340. 0.1900 45.78 0.6043 0.7614 0.0283 0.0224 0.370 5.823 2.305 275.559 0.658 10.252 3.794 0.32 129686. 0.1690 47.86 0.6318 0.7517 0.0242 0.0203 0.335 5.276 1.972 249.685 0.596 8.772 3.582 0.32 130045. 0.1476 49.94 0.6593 0.7329 0.0201 0.0180 0.297 4.685 1.636 221.713 0.529 7.277 3.347 0.32 130418. 0.1256 52.02 0.6867 0.7004 0.0159 0.0156 0.257 4.051 1.298 191.702 0.458 5.773 3.071 0.32 130804. 0.1026 54.11 0.7142 0.6458 0.0118 0.0130 0.214 3.375 0.959 159.735 0.381 4.265 2.722 0.33 131203. 0.0782 56.19 0.7417 0.5500 0.0076 0.0102 0.169 2.661 0.620 125.928 0.301 2.758 2.233 0.33 131616. 0.0516 58.27 0.7691 0.3626 0.0035 0.0074 0.121 1.911 0.283 90.415 0.216 1.258 1.419 0.33 132040. 0.0221 60.35 0.7966 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 0.0854 0.0279 0.897 11.312 10.892 669.167 1.278 48.446 7.383 0.40 156370. 0.7148 2.59 0.0274 0.0808 0.0847 0.0287 0.923 11.632 10.791 688.113 1.314 48.001 7.113 0.40 156473. 0.6856 5.18 0.0547 0.1556 0.0838 0.0295 0.948 11.953 10.676 707.079 1.350 47.488 6.848 0.40 156588. 0.6565 7.77 0.0821 0.2245 0.0827 0.0302 0.973 12.268 10.544 725.724 1.386 46.900 6.590 0.40 156716. 0.6278 10.36 0.1094 0.2880 0.0815 0.0310 0.997 12.572 10.393 743.679 1.420 46.228 6.339 0.40 156857. 0.5995 12.95 0.1368 0.3461 0.0802 0.0317 1.020 12.856 10.221 760.528 1.453 45.462 6.096 0.40 157011. 0.5717 15.54 0.1641 0.3994 0.0787 0.0323 1.040 13.115 10.026 775.816 1.482 44.595 5.861 0.40 157181. 0.5445 18.13 0.1915 0.4481 0.0769 0.0329 1.058 13.339 9.806 789.071 1.507 43.616 5.637 0.40 157365. 0.5178 20.72 0.2189 0.4925 0.0750 0.0333 1.073 13.520 9.559 799.806 1.528 42.520 5.421 0.40 157564. 0.4917 23.32 0.2462 0.5331 0.0728 0.0336 1.083 13.651 9.285 807.543 1.542 41.301 5.215 0.40 157779. 0.4662 25.91 0.2736 0.5700 0.0705 0.0338 1.089 13.724 8.983 811.837 1.550 39.956 5.019 0.40 158011. 0.4413 28.50 0.3009 0.6036 0.0679 0.0338 1.089 13.732 8.652 812.323 1.551 38.486 4.831 0.40 158258. 0.4169 31.09 0.3283 0.6340 0.0651 0.0337 1.085 13.672 8.295 808.758 1.545 36.897 4.652 0.40 158522. 0.3931 33.68 0.3556 0.6616 0.0621 0.0334 1.074 13.541 7.913 801.003 1.530 35.198 4.481 0.40 158802. 0.3698 36.27 0.3830 0.6863 0.0589 0.0329 1.058 13.337 7.509 788.989 1.507 33.398 4.316 0.40 159098. 0.3470 38.86 0.4104 0.7084 0.0556 0.0322 1.036 13.062 7.084 772.682 1.476 31.508 4.158 0.40 159412. 0.3247 41.45 0.4377 0.7277 0.0521 0.0313 1.009 12.713 6.640 752.069 1.436 29.537 4.005 0.40 159741. 0.3028 44.04 0.4651 0.7444 0.0485 0.0303 0.975 12.292 6.181 727.142 1.389 27.494 3.856 0.40 160087. 0.2812 46.63 0.4924 0.7583 0.0448 0.0291 0.936 11.798 5.708 697.897 1.333 25.387 3.709 0.40 160450. 0.2600 49.22 0.5198 0.7692 0.0410 0.0277 0.891 11.230 5.221 664.332 1.269 23.224 3.565 0.40 160829. 0.2390 51.81 0.5471 0.7768 0.0371 0.0261 0.840 10.590 4.724 626.450 1.196 21.011 3.420 0.40 161225. 0.2181 54.40 0.5745 0.7807 0.0331 0.0243 0.784 9.877 4.216 584.262 1.116 18.755 3.273 0.40 161638. 0.1972 56.99 0.6018 0.7799 0.0290 0.0224 0.721 9.091 3.701 537.793 1.027 16.462 3.121 0.40 162067. 0.1762 59.58 0.6292 0.7732 0.0249 0.0203 0.653 8.234 3.179 487.087 0.930 14.138 2.960 0.40 162513. 0.1548 62.17 0.6566 0.7582 0.0208 0.0180 0.580 7.306 2.651 432.217 0.825 11.791 2.782 0.41 162976. 0.1329 64.76 0.6839 0.7312 0.0166 0.0156 0.501 6.310 2.119 373.293 0.713 9.427 2.575 0.41 163455. 0.1100 67.36 0.7113 0.6842 0.0124 0.0129 0.416 5.248 1.586 310.476 0.593 7.055 2.317 0.41 163950. 0.0856 69.95 0.7386 0.6003 0.0083 0.0102 0.327 4.124 1.053 243.986 0.466 4.684 1.958 0.41 164462. 0.0589 72.54 0.7660 0.4329 0.0041 0.0073 0.233 2.943 0.522 174.090 0.332 2.324 1.361 0.41 164988. 0.0289 75.13 0.7933 -0.0147 -0.0001 0.0042 0.134 1.692 -0.010 100.119 0.191 -0.044 -0.045 0.41 165503. 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 0.0861 0.0278 1.545 16.233 15.796 1152.334 1.834 70.260 6.217 0.48 187635. 0.7250 3.13 0.0275 0.0822 0.0853 0.0286 1.591 16.709 15.657 1186.129 1.888 69.642 5.987 0.48 187760. 0.6950 6.26 0.0551 0.1581 0.0844 0.0294 1.636 17.187 15.496 1220.038 1.942 68.928 5.761 0.48 187899. 0.6653 9.39 0.0826 0.2281 0.0834 0.0302 1.681 17.657 15.311 1253.440 1.995 68.103 5.540 0.48 188053. 0.6360 12.52 0.1102 0.2923 0.0822 0.0310 1.724 18.111 15.097 1285.667 2.046 67.153 5.326 0.48 188224. 0.6072 15.65 0.1377 0.3512 0.0809 0.0317 1.765 18.538 14.853 1315.959 2.094 66.065 5.119 0.48 188412. 0.5788 18.78 0.1653 0.4051 0.0794 0.0324 1.802 18.926 14.574 1343.489 2.138 64.824 4.920 0.48 188617. 0.5511 21.91 0.1928 0.4543 0.0777 0.0330 1.834 19.262 14.257 1367.384 2.176 63.417 4.729 0.48 188840. 0.5239 25.04 0.2204 0.4991 0.0757 0.0334 1.860 19.535 13.902 1386.757 2.207 61.834 4.547 0.48 189083. 0.4974 28.17 0.2479 0.5400 0.0736 0.0338 1.878 19.732 13.504 1400.736 2.229 60.066 4.373 0.48 189344. 0.4714 31.30 0.2754 0.5773 0.0712 0.0340 1.889 19.842 13.064 1408.509 2.242 58.109 4.207 0.48 189625. 0.4461 34.43 0.3030 0.6112 0.0685 0.0340 1.890 19.855 12.582 1409.414 2.243 55.963 4.049 0.48 189926. 0.4214 37.56 0.3305 0.6420 0.0657 0.0338 1.881 19.764 12.059 1403.018 2.233 53.639 3.898 0.48 190247. 0.3972 40.69 0.3581 0.6698 0.0626 0.0335 1.863 19.568 11.499 1389.076 2.211 51.149 3.755 0.48 190588. 0.3736 43.82 0.3856 0.6949 0.0594 0.0330 1.834 19.264 10.906 1367.468 2.176 48.509 3.617 0.48 190948. 0.3505 46.95 0.4132 0.7173 0.0560 0.0323 1.794 18.851 10.282 1338.143 2.130 45.734 3.485 0.48 191329. 0.3279 50.08 0.4407 0.7371 0.0525 0.0314 1.745 18.328 9.631 1301.084 2.071 42.838 3.357 0.48 191730. 0.3057 53.21 0.4683 0.7543 0.0488 0.0303 1.685 17.697 8.956 1256.282 1.999 39.835 3.233 0.48 192151. 0.2839 56.34 0.4958 0.7687 0.0450 0.0290 1.614 16.957 8.259 1203.736 1.916 36.736 3.112 0.48 192592. 0.2624 59.47 0.5234 0.7802 0.0411 0.0276 1.533 16.108 7.544 1143.447 1.820 33.554 2.992 0.48 193054. 0.2411 62.60 0.5509 0.7885 0.0371 0.0259 1.442 15.150 6.812 1075.422 1.712 30.298 2.873 0.48 193535. 0.2200 65.73 0.5784 0.7930 0.0330 0.0241 1.341 14.083 6.065 999.686 1.591 26.979 2.752 0.48 194037. 0.1988 68.86 0.6060 0.7930 0.0289 0.0221 1.229 12.908 5.307 916.286 1.458 23.604 2.627 0.48 194559. 0.1775 71.99 0.6335 0.7871 0.0247 0.0199 1.107 11.626 4.538 825.309 1.314 20.185 2.494 0.49 195101. 0.1559 75.12 0.6611 0.7730 0.0205 0.0175 0.975 10.240 3.761 726.895 1.157 16.731 2.347 0.49 195663. 0.1335 78.25 0.6886 0.7463 0.0162 0.0150 0.833 8.752 2.980 621.255 0.989 13.253 2.175 0.49 196246. 0.1102 81.38 0.7162 0.6983 0.0120 0.0123 0.682 7.166 2.195 508.694 0.810 9.764 1.957 0.49 196848. 0.0851 84.51 0.7437 0.6088 0.0077 0.0094 0.522 5.489 1.412 389.627 0.620 6.279 1.643 0.49 197470. 0.0573 87.64 0.7713 0.4164 0.0034 0.0064 0.355 3.727 0.632 264.536 0.421 2.812 1.084 0.49 198109. 0.0253 90.77 0.7988 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 0.0868 0.0279 2.460 22.150 21.678 1834.435 2.503 96.422 5.360 0.56 218895. 0.7321 3.63 0.0274 0.0821 0.0861 0.0287 2.534 22.813 21.502 1889.310 2.577 95.639 5.162 0.56 219039. 0.7022 7.26 0.0547 0.1581 0.0852 0.0295 2.608 23.479 21.296 1944.529 2.653 94.726 4.967 0.56 219201. 0.6725 10.89 0.0821 0.2280 0.0843 0.0304 2.681 24.139 21.058 1999.112 2.727 93.665 4.778 0.56 219379. 0.6432 14.52 0.1095 0.2923 0.0832 0.0312 2.752 24.777 20.781 2051.973 2.799 92.436 4.594 0.56 219577. 0.6144 18.15 0.1369 0.3513 0.0819 0.0319 2.819 25.379 20.462 2101.885 2.867 91.017 4.416 0.56 219794. 0.5860 21.77 0.1642 0.4052 0.0804 0.0326 2.880 25.930 20.096 2147.505 2.930 89.389 4.245 0.56 220031. 0.5582 25.40 0.1916 0.4545 0.0788 0.0332 2.933 26.412 19.679 2187.408 2.984 87.533 4.081 0.56 220290. 0.5311 29.03 0.2190 0.4994 0.0769 0.0337 2.977 26.808 19.207 2220.153 3.029 85.434 3.924 0.56 220570. 0.5045 32.66 0.2464 0.5405 0.0748 0.0341 3.010 27.099 18.677 2244.307 3.062 83.077 3.775 0.56 220873. 0.4786 36.29 0.2737 0.5779 0.0724 0.0343 3.029 27.271 18.088 2258.537 3.081 80.456 3.633 0.56 221198. 0.4533 39.92 0.3011 0.6121 0.0698 0.0343 3.033 27.310 17.440 2261.732 3.085 77.572 3.497 0.56 221546. 0.4285 43.55 0.3285 0.6432 0.0670 0.0342 3.022 27.206 16.735 2253.148 3.074 74.436 3.369 0.56 221917. 0.4043 47.18 0.3559 0.6714 0.0639 0.0339 2.994 26.955 15.977 2232.363 3.045 71.066 3.246 0.56 222311. 0.3807 50.81 0.3832 0.6970 0.0607 0.0334 2.949 26.554 15.171 2199.182 3.000 67.483 3.129 0.56 222728. 0.3576 54.44 0.4106 0.7199 0.0573 0.0327 2.888 26.003 14.323 2153.523 2.938 63.708 3.017 0.56 223168. 0.3349 58.07 0.4380 0.7403 0.0538 0.0318 2.810 25.301 13.436 2095.374 2.858 59.761 2.908 0.56 223632. 0.3128 61.69 0.4654 0.7582 0.0501 0.0307 2.715 24.448 12.514 2024.737 2.762 55.663 2.803 0.56 224118. 0.2909 65.32 0.4927 0.7735 0.0463 0.0295 2.604 23.444 11.562 1941.620 2.649 51.430 2.701 0.56 224628. 0.2695 68.95 0.5201 0.7861 0.0424 0.0280 2.476 22.290 10.584 1846.035 2.518 47.077 2.600 0.56 225161. 0.2482 72.58 0.5475 0.7957 0.0383 0.0264 2.331 20.986 9.582 1738.000 2.371 42.619 2.501 0.56 225717. 0.2271 76.21 0.5748 0.8018 0.0343 0.0246 2.169 19.531 8.559 1617.551 2.207 38.069 2.400 0.56 226296. 0.2060 79.84 0.6022 0.8039 0.0301 0.0225 1.991 17.928 7.518 1484.766 2.025 33.441 2.297 0.57 226899. 0.1848 83.47 0.6296 0.8006 0.0259 0.0203 1.797 16.177 6.463 1339.769 1.828 28.747 2.188 0.57 227525. 0.1632 87.10 0.6570 0.7901 0.0216 0.0180 1.586 14.282 5.396 1182.769 1.614 24.002 2.069 0.57 228173. 0.1410 90.73 0.6843 0.7687 0.0173 0.0154 1.360 12.245 4.321 1014.084 1.383 19.219 1.933 0.57 228845. 0.1179 94.36 0.7117 0.7290 0.0130 0.0127 1.119 10.072 3.241 834.171 1.138 14.416 1.762 0.57 229540. 0.0931 97.99 0.7391 0.6542 0.0086 0.0098 0.863 7.772 2.161 643.667 0.878 9.613 1.523 0.57 230258. 0.0657 101.61 0.7665 0.4948 0.0043 0.0067 0.595 5.353 1.086 443.352 0.605 4.829 1.111 0.57 230996. 0.0340 105.24 0.7938 0.0044 0.0000 0.0035 0.310 2.789 0.005 231.019 0.315 0.022 0.010 0.57 231713. 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 0.0876 0.0281 3.702 29.169 28.578 2760.851 3.296 127.113 4.695 0.63 250149. 0.7363 4.15 0.0274 0.0824 0.0869 0.0289 3.815 30.060 28.367 2845.196 3.396 126.177 4.522 0.63 250314. 0.7066 8.31 0.0548 0.1585 0.0862 0.0298 3.930 30.961 28.119 2930.467 3.498 125.074 4.352 0.63 250498. 0.6771 12.46 0.0823 0.2287 0.0853 0.0307 4.043 31.856 27.828 3015.152 3.599 123.778 4.186 0.63 250703. 0.6479 16.62 0.1097 0.2932 0.0842 0.0315 4.154 32.727 27.486 3097.567 3.697 122.260 4.025 0.64 250928. 0.6191 20.77 0.1371 0.3523 0.0830 0.0323 4.259 33.553 27.088 3175.767 3.791 120.489 3.869 0.64 251177. 0.5908 24.92 0.1645 0.4063 0.0816 0.0330 4.355 34.312 26.627 3247.609 3.877 118.437 3.719 0.64 251449. 0.5630 29.08 0.1919 0.4558 0.0800 0.0337 4.440 34.980 26.096 3310.815 3.952 116.076 3.575 0.64 251745. 0.5358 33.23 0.2193 0.5009 0.0781 0.0342 4.510 35.532 25.491 3363.049 4.014 113.384 3.438 0.64 252067. 0.5092 37.39 0.2468 0.5421 0.0760 0.0346 4.562 35.943 24.807 3402.030 4.061 110.340 3.307 0.64 252415. 0.4833 41.54 0.2742 0.5797 0.0737 0.0348 4.594 36.193 24.041 3425.629 4.089 106.933 3.183 0.64 252788. 0.4579 45.70 0.3016 0.6140 0.0711 0.0349 4.602 36.261 23.193 3432.073 4.097 103.165 3.065 0.64 253188. 0.4331 49.85 0.3290 0.6454 0.0682 0.0348 4.587 36.135 22.268 3420.156 4.083 99.047 2.953 0.64 253614. 0.4088 54.00 0.3564 0.6739 0.0652 0.0345 4.545 35.808 21.269 3389.219 4.046 94.606 2.846 0.64 254067. 0.3851 58.16 0.3838 0.6998 0.0619 0.0340 4.478 35.277 20.205 3338.962 3.986 89.871 2.745 0.64 254546. 0.3619 62.31 0.4113 0.7231 0.0585 0.0333 4.384 34.541 19.080 3269.304 3.902 84.870 2.647 0.64 255052. 0.3392 66.47 0.4387 0.7440 0.0549 0.0323 4.265 33.600 17.903 3180.253 3.796 79.633 2.553 0.64 255584. 0.3170 70.62 0.4661 0.7624 0.0511 0.0312 4.119 32.455 16.678 3071.853 3.667 74.186 2.463 0.64 256142. 0.2951 74.77 0.4935 0.7783 0.0472 0.0299 3.948 31.106 15.412 2944.155 3.514 68.552 2.374 0.64 256728. 0.2735 78.93 0.5209 0.7916 0.0432 0.0285 3.751 29.553 14.109 2797.199 3.339 62.755 2.288 0.64 257340. 0.2521 83.08 0.5483 0.8020 0.0391 0.0268 3.528 27.798 12.773 2631.029 3.141 56.812 2.202 0.64 257978. 0.2309 87.24 0.5758 0.8091 0.0350 0.0249 3.280 25.840 11.408 2445.714 2.919 50.743 2.116 0.65 258643. 0.2096 91.39 0.6032 0.8123 0.0307 0.0228 3.006 23.681 10.019 2241.380 2.675 44.565 2.027 0.65 259334. 0.1883 95.54 0.6306 0.8104 0.0264 0.0205 2.706 21.323 8.610 2018.227 2.409 38.295 1.935 0.65 260052. 0.1666 99.70 0.6580 0.8016 0.0220 0.0181 2.382 18.770 7.184 1776.579 2.121 31.953 1.834 0.65 260796. 0.1442 103.85 0.6854 0.7822 0.0176 0.0154 2.034 16.027 5.746 1516.930 1.811 25.558 1.718 0.65 261567. 0.1208 108.01 0.7128 0.7450 0.0132 0.0126 1.663 13.101 4.301 1239.993 1.480 19.133 1.573 0.65 262364. 0.0957 112.16 0.7403 0.6729 0.0088 0.0096 1.270 10.003 2.856 946.759 1.130 12.705 1.368 0.65 263186. 0.0679 116.31 0.7677 0.5133 0.0043 0.0065 0.856 6.745 1.417 638.442 0.762 6.302 1.007 0.65 264033. 0.0352 120.47 0.7951 -0.0333 -0.0001 0.0031 0.414 3.261 -0.043 308.684 0.368 -0.191 -0.063 0.65 264822. 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 0.0884 0.0290 5.441 38.107 36.529 4057.616 4.305 162.483 4.083 0.71 281397. 0.7241 4.68 0.0274 0.0808 0.0879 0.0298 5.601 39.222 36.296 4176.342 4.431 161.443 3.942 0.71 281582. 0.6967 9.36 0.0549 0.1559 0.0872 0.0307 5.762 40.351 36.016 4296.591 4.559 160.201 3.802 0.71 281788. 0.6694 14.03 0.0823 0.2255 0.0864 0.0315 5.922 41.474 35.683 4416.205 4.686 158.718 3.665 0.71 282018. 0.6423 18.71 0.1098 0.2896 0.0854 0.0324 6.079 42.569 35.287 4532.792 4.809 156.956 3.531 0.71 282271. 0.6154 23.39 0.1372 0.3487 0.0843 0.0332 6.227 43.610 34.818 4643.575 4.927 154.870 3.401 0.71 282551. 0.5887 28.07 0.1646 0.4030 0.0830 0.0339 6.364 44.567 34.267 4745.513 5.035 152.418 3.275 0.71 282857. 0.5625 32.74 0.1921 0.4527 0.0814 0.0345 6.484 45.411 33.624 4835.347 5.130 149.560 3.154 0.72 283191. 0.5366 37.42 0.2195 0.4983 0.0796 0.0351 6.584 46.109 32.882 4909.742 5.209 146.261 3.038 0.72 283554. 0.5111 42.10 0.2470 0.5401 0.0776 0.0355 6.659 46.632 32.035 4965.393 5.268 142.494 2.926 0.72 283946. 0.4859 46.78 0.2744 0.5782 0.0752 0.0357 6.704 46.949 31.079 4999.148 5.304 138.239 2.820 0.72 284368. 0.4612 51.45 0.3019 0.6131 0.0727 0.0358 6.716 47.035 30.012 5008.292 5.314 133.495 2.718 0.72 284820. 0.4369 56.13 0.3293 0.6449 0.0698 0.0357 6.693 46.871 28.839 4990.888 5.295 128.278 2.621 0.72 285301. 0.4129 60.81 0.3567 0.6740 0.0667 0.0353 6.632 46.448 27.567 4945.774 5.248 122.620 2.528 0.72 285813. 0.3894 65.49 0.3842 0.7003 0.0634 0.0348 6.534 45.758 26.205 4872.361 5.170 116.560 2.439 0.72 286354. 0.3664 70.16 0.4116 0.7242 0.0600 0.0341 6.397 44.801 24.761 4770.391 5.062 110.139 2.354 0.72 286926. 0.3437 74.84 0.4391 0.7456 0.0563 0.0331 6.222 43.574 23.246 4639.775 4.923 103.396 2.272 0.72 287527. 0.3214 79.52 0.4665 0.7646 0.0525 0.0320 6.008 42.078 21.666 4480.509 4.754 96.369 2.193 0.72 288158. 0.2995 84.20 0.4939 0.7811 0.0485 0.0307 5.757 40.314 20.029 4292.651 4.555 89.088 2.116 0.72 288819. 0.2779 88.87 0.5214 0.7952 0.0444 0.0291 5.466 38.282 18.342 4076.303 4.325 81.586 2.041 0.72 289510. 0.2564 93.55 0.5488 0.8065 0.0402 0.0274 5.138 35.984 16.611 3831.572 4.065 73.886 1.966 0.72 290231. 0.2351 98.23 0.5763 0.8146 0.0359 0.0254 4.772 33.420 14.841 3558.565 3.776 66.015 1.892 0.73 290981. 0.2138 102.91 0.6037 0.8190 0.0316 0.0233 4.368 30.592 13.038 3257.476 3.456 57.994 1.815 0.73 291762. 0.1923 107.58 0.6312 0.8186 0.0271 0.0209 3.927 27.504 11.207 2928.615 3.107 49.848 1.736 0.73 292571. 0.1705 112.26 0.6586 0.8116 0.0226 0.0184 3.450 24.159 9.353 2572.464 2.729 41.600 1.649 0.73 293411. 0.1480 116.94 0.6860 0.7945 0.0181 0.0156 2.936 20.565 7.482 2189.747 2.323 33.278 1.550 0.73 294280. 0.1244 121.62 0.7135 0.7602 0.0136 0.0127 2.389 16.731 5.601 1781.547 1.890 24.911 1.426 0.73 295179. 0.0990 126.29 0.7409 0.6918 0.0090 0.0096 1.810 12.674 3.717 1349.489 1.432 16.535 1.249 0.73 296106. 0.0707 130.97 0.7684 0.5350 0.0045 0.0064 1.201 8.412 1.840 895.766 0.950 8.185 0.932 0.74 297060. 0.0371 135.65 0.7958 -0.0532 -0.0002 0.0029 0.546 3.823 -0.080 407.111 0.432 -0.357 -0.090 0.74 297909. 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 0.0893 0.0321 8.258 52.046 45.532 6157.658 5.880 202.528 3.354 0.79 312637. 0.6640 5.20 0.0275 0.0742 0.0888 0.0329 8.467 53.364 45.292 6313.556 6.029 201.459 3.254 0.79 312841. 0.6424 10.40 0.0549 0.1439 0.0883 0.0337 8.677 54.690 45.001 6470.445 6.179 200.164 3.155 0.79 313069. 0.6208 15.61 0.0824 0.2091 0.0876 0.0345 8.884 55.996 44.648 6624.946 6.326 198.592 3.057 0.79 313323. 0.5992 20.81 0.1099 0.2701 0.0867 0.0353 9.083 57.249 44.219 6773.277 6.468 196.687 2.961 0.79 313604. 0.5777 26.01 0.1373 0.3270 0.0857 0.0360 9.268 58.415 43.702 6911.164 6.600 194.387 2.868 0.79 313914. 0.5563 31.21 0.1648 0.3801 0.0845 0.0366 9.433 59.454 43.082 7034.091 6.717 191.631 2.778 0.79 314254. 0.5350 36.41 0.1923 0.4296 0.0830 0.0372 9.571 60.327 42.346 7137.430 6.816 188.356 2.691 0.79 314626. 0.5138 41.62 0.2197 0.4756 0.0814 0.0376 9.678 60.997 41.481 7216.714 6.891 184.510 2.607 0.80 315030. 0.4926 46.82 0.2472 0.5185 0.0794 0.0378 9.746 61.429 40.478 7267.761 6.940 180.048 2.526 0.80 315467. 0.4715 52.02 0.2747 0.5583 0.0771 0.0379 9.772 61.590 39.330 7286.868 6.958 174.941 2.448 0.80 315937. 0.4504 57.22 0.3021 0.5952 0.0746 0.0379 9.751 61.457 38.035 7271.045 6.943 169.180 2.373 0.80 316441. 0.4293 62.42 0.3296 0.6293 0.0718 0.0376 9.680 61.012 36.597 7218.392 6.893 162.783 2.300 0.80 316979. 0.4081 67.63 0.3571 0.6607 0.0687 0.0371 9.559 60.248 35.024 7128.050 6.807 155.788 2.229 0.80 317550. 0.3870 72.83 0.3845 0.6895 0.0654 0.0365 9.387 59.164 33.329 6999.781 6.684 148.247 2.160 0.80 318155. 0.3658 78.03 0.4120 0.7157 0.0618 0.0356 9.164 57.760 31.523 6833.687 6.526 140.214 2.092 0.80 318793. 0.3446 83.23 0.4395 0.7394 0.0581 0.0345 8.891 56.038 29.618 6629.898 6.331 131.742 2.026 0.80 319465. 0.3235 88.43 0.4669 0.7604 0.0542 0.0333 8.567 53.997 27.626 6388.497 6.101 122.881 1.961 0.80 320170. 0.3025 93.64 0.4944 0.7789 0.0501 0.0318 8.193 51.638 25.557 6109.386 5.834 113.676 1.897 0.80 320908. 0.2814 98.84 0.5219 0.7946 0.0459 0.0302 7.768 48.958 23.419 5792.306 5.531 104.168 1.834 0.80 321679. 0.2604 104.04 0.5493 0.8075 0.0416 0.0283 7.291 45.954 21.221 5436.885 5.192 94.393 1.770 0.81 322483. 0.2393 109.24 0.5768 0.8172 0.0372 0.0263 6.763 42.623 18.971 5042.805 4.816 84.384 1.706 0.81 323320. 0.2180 114.44 0.6043 0.8232 0.0327 0.0240 6.182 38.964 16.675 4609.843 4.402 74.172 1.641 0.81 324190. 0.1966 119.65 0.6317 0.8242 0.0281 0.0216 5.551 34.986 14.340 4139.230 3.953 63.786 1.571 0.81 325093. 0.1746 124.85 0.6592 0.8184 0.0235 0.0189 4.870 30.698 11.973 3631.902 3.468 53.257 1.495 0.81 326028. 0.1518 130.05 0.6867 0.8019 0.0188 0.0161 4.143 26.116 9.582 3089.782 2.951 42.619 1.407 0.81 326997. 0.1277 135.25 0.7141 0.7668 0.0141 0.0131 3.374 21.265 7.174 2515.895 2.403 31.908 1.293 0.81 327998. 0.1016 140.45 0.7416 0.6942 0.0093 0.0100 2.568 16.183 4.759 1914.661 1.828 21.168 1.127 0.82 329030. 0.0722 145.66 0.7691 0.5265 0.0046 0.0067 1.732 10.918 2.348 1291.746 1.234 10.445 0.825 0.82 330093. 0.0371 150.86 0.7965 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 0.0896 0.0383 13.126 75.207 55.281 9787.694 8.497 245.892 2.562 0.87 343892. 0.5588 5.77 0.0277 0.0631 0.0892 0.0391 13.409 76.830 55.055 9998.821 8.680 244.883 2.497 0.87 344115. 0.5437 11.53 0.0554 0.1230 0.0888 0.0400 13.693 78.460 54.776 10211.029 8.864 243.645 2.433 0.87 344365. 0.5283 17.30 0.0831 0.1797 0.0882 0.0408 13.972 80.060 54.433 10419.260 9.045 242.119 2.370 0.87 344643. 0.5129 23.07 0.1107 0.2334 0.0875 0.0415 14.237 81.577 54.009 10616.674 9.217 240.231 2.307 0.87 344952. 0.4975 28.84 0.1384 0.2841 0.0867 0.0422 14.477 82.949 53.484 10795.234 9.372 237.897 2.247 0.87 345293. 0.4821 34.60 0.1661 0.3321 0.0856 0.0428 14.679 84.108 52.838 10946.097 9.503 235.024 2.189 0.87 345668. 0.4669 40.37 0.1938 0.3778 0.0844 0.0433 14.832 84.986 52.050 11060.292 9.602 231.519 2.135 0.87 346079. 0.4518 46.14 0.2215 0.4212 0.0828 0.0435 14.925 85.518 51.100 11129.504 9.662 227.292 2.083 0.87 346527. 0.4368 51.91 0.2492 0.4627 0.0810 0.0436 14.948 85.650 49.971 11146.764 9.677 222.270 2.033 0.88 347013. 0.4217 57.67 0.2768 0.5023 0.0789 0.0435 14.895 85.344 48.650 11106.931 9.642 216.395 1.987 0.88 347536. 0.4065 63.44 0.3045 0.5402 0.0764 0.0431 14.761 84.576 47.132 11007.030 9.555 209.643 1.942 0.88 348098. 0.3912 69.21 0.3322 0.5763 0.0736 0.0424 14.546 83.344 45.420 10846.611 9.416 202.026 1.899 0.88 348699. 0.3755 74.98 0.3599 0.6106 0.0705 0.0416 14.251 81.659 43.523 10627.337 9.226 193.591 1.858 0.88 349337. 0.3595 80.74 0.3876 0.6430 0.0672 0.0405 13.882 79.544 41.458 10352.137 8.987 184.404 1.816 0.88 350014. 0.3431 86.51 0.4153 0.6734 0.0636 0.0392 13.443 77.026 39.239 10024.360 8.702 174.536 1.775 0.88 350728. 0.3263 92.28 0.4429 0.7015 0.0598 0.0377 12.937 74.127 36.884 9647.055 8.375 164.060 1.734 0.88 351480. 0.3090 98.05 0.4706 0.7274 0.0558 0.0361 12.367 70.864 34.408 9222.388 8.006 153.045 1.692 0.88 352269. 0.2912 103.81 0.4983 0.7506 0.0516 0.0342 11.737 67.250 31.824 8752.139 7.598 141.554 1.649 0.88 353095. 0.2730 109.58 0.5260 0.7710 0.0472 0.0322 11.046 63.291 29.147 8236.825 7.151 129.644 1.605 0.88 353958. 0.2542 115.35 0.5537 0.7884 0.0428 0.0300 10.294 58.983 26.386 7676.165 6.664 117.364 1.559 0.89 354857. 0.2350 121.12 0.5814 0.8023 0.0382 0.0277 9.480 54.321 23.552 7069.478 6.137 104.758 1.511 0.89 355794. 0.2151 126.88 0.6090 0.8122 0.0335 0.0251 8.604 49.301 20.654 6416.172 5.570 91.871 1.460 0.89 356767. 0.1947 132.65 0.6367 0.8162 0.0287 0.0224 7.672 43.957 17.703 5720.737 4.966 78.742 1.404 0.89 357776. 0.1733 138.42 0.6644 0.8041 0.0238 0.0197 6.747 38.658 14.697 5031.054 4.368 65.374 1.325 0.89 358822. 0.1490 144.19 0.6921 0.7748 0.0189 0.0169 5.784 33.143 11.656 4313.368 3.745 51.846 1.226 0.89 359905. 0.1228 149.95 0.7198 0.7168 0.0139 0.0140 4.792 27.456 8.590 3573.159 3.102 38.209 1.090 0.90 361023. 0.0938 155.72 0.7475 0.6056 0.0089 0.0110 3.780 21.660 5.514 2818.894 2.447 24.524 0.887 0.90 362176. 0.0611 161.49 0.7751 0.3801 0.0040 0.0081 2.765 15.843 2.441 2061.892 1.790 10.857 0.537 0.90 363361. 0.0246 167.25 0.8028 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 0.0874 0.0440 19.592 102.902 64.171 14609.407 11.626 285.434 1.992 0.95 375216. 0.4682 6.31 0.0278 0.0540 0.0871 0.0448 19.928 104.671 63.945 14860.527 11.826 284.426 1.952 0.95 375458. 0.4579 12.63 0.0556 0.1057 0.0867 0.0456 20.277 106.500 63.672 15120.268 12.032 283.214 1.910 0.95 375728. 0.4471 18.94 0.0833 0.1551 0.0863 0.0464 20.629 108.351 63.341 15382.985 12.241 281.740 1.868 0.95 376029. 0.4361 25.25 0.1111 0.2020 0.0857 0.0471 20.976 110.172 62.934 15641.559 12.447 279.929 1.825 0.95 376363. 0.4247 31.57 0.1389 0.2467 0.0850 0.0479 21.305 111.901 62.431 15887.044 12.643 277.694 1.782 0.95 376732. 0.4132 37.88 0.1667 0.2890 0.0842 0.0485 21.602 113.463 61.810 16108.832 12.819 274.933 1.740 0.95 377138. 0.4014 44.19 0.1944 0.3292 0.0831 0.0491 21.849 114.761 61.045 16293.146 12.966 271.529 1.699 0.95 377582. 0.3895 50.51 0.2222 0.3675 0.0819 0.0495 22.032 115.720 60.112 16429.297 13.074 267.380 1.660 0.95 378067. 0.3775 56.82 0.2500 0.4038 0.0803 0.0497 22.134 116.256 58.989 16505.291 13.134 262.384 1.621 0.96 378592. 0.3653 63.13 0.2778 0.4384 0.0785 0.0498 22.139 116.285 57.655 16509.416 13.138 256.450 1.584 0.96 379160. 0.3529 69.45 0.3056 0.4714 0.0764 0.0495 22.035 115.735 56.096 16431.375 13.076 249.513 1.548 0.96 379769. 0.3402 75.76 0.3333 0.5030 0.0740 0.0490 21.809 114.551 54.305 16263.228 12.942 241.548 1.515 0.96 380422. 0.3274 82.07 0.3611 0.5333 0.0712 0.0482 21.456 112.694 52.285 15999.588 12.732 232.564 1.482 0.96 381117. 0.3144 88.39 0.3889 0.5624 0.0682 0.0471 20.970 110.140 50.043 15637.046 12.444 222.591 1.452 0.96 381855. 0.3013 94.70 0.4167 0.5905 0.0648 0.0457 20.349 106.880 47.588 15174.153 12.075 211.673 1.422 0.96 382635. 0.2879 101.01 0.4445 0.6177 0.0612 0.0440 19.595 102.918 44.933 14611.720 11.628 199.862 1.395 0.96 383457. 0.2743 107.33 0.4722 0.6437 0.0573 0.0421 18.712 98.283 42.091 13953.674 11.104 187.220 1.368 0.96 384322. 0.2604 113.64 0.5000 0.6686 0.0532 0.0398 17.711 93.024 39.078 13206.970 10.510 173.820 1.342 0.96 385228. 0.2461 119.95 0.5278 0.6919 0.0489 0.0373 16.602 87.202 35.912 12380.401 9.852 159.739 1.316 0.97 386176. 0.2313 126.27 0.5556 0.7131 0.0444 0.0346 15.399 80.880 32.612 11482.896 9.138 145.058 1.288 0.97 387165. 0.2158 132.58 0.5833 0.7314 0.0398 0.0317 14.110 74.113 29.194 10522.087 8.373 129.856 1.258 0.97 388195. 0.1995 138.89 0.6111 0.7462 0.0350 0.0286 12.745 66.941 25.677 9503.923 7.563 114.211 1.225 0.97 389265. 0.1822 145.21 0.6389 0.7555 0.0301 0.0254 11.314 59.426 22.076 8437.006 6.714 98.196 1.187 0.97 390375. 0.1636 151.52 0.6667 0.7468 0.0250 0.0224 9.949 52.257 18.391 7419.148 5.904 81.802 1.124 0.97 391526. 0.1415 157.83 0.6945 0.6965 0.0199 0.0198 8.832 46.387 14.615 6585.732 5.241 65.006 1.007 0.97 392716. 0.1129 164.15 0.7222 0.6103 0.0147 0.0174 7.749 40.700 10.804 5778.402 4.598 48.058 0.848 0.98 393945. 0.0818 170.46 0.7500 0.4739 0.0095 0.0151 6.706 35.222 6.992 5000.657 3.979 31.101 0.634 0.98 395213. 0.0492 176.77 0.7778 0.2653 0.0044 0.0128 5.710 29.988 3.214 4257.575 3.388 14.294 0.342 0.98 396520. 0.0180 183.09 0.8056