21x13E (21x13E.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 0.0929 0.0362 0.012 0.750 0.576 8.876 0.085 2.561 29.419 0.08 40331. 0.6237 0.53 0.0265 0.0660 0.0917 0.0368 0.012 0.762 0.568 9.016 0.086 2.528 28.593 0.08 40359. 0.6023 1.05 0.0529 0.1281 0.0904 0.0373 0.012 0.773 0.560 9.151 0.087 2.492 27.770 0.08 40390. 0.5808 1.58 0.0794 0.1865 0.0890 0.0379 0.012 0.784 0.551 9.279 0.089 2.452 26.952 0.08 40424. 0.5592 2.10 0.1058 0.2412 0.0874 0.0383 0.013 0.794 0.542 9.398 0.090 2.409 26.142 0.08 40461. 0.5376 2.63 0.1323 0.2923 0.0857 0.0388 0.013 0.803 0.531 9.504 0.091 2.362 25.343 0.08 40501. 0.5160 3.16 0.1588 0.3399 0.0838 0.0391 0.013 0.811 0.519 9.594 0.092 2.311 24.557 0.08 40545. 0.4945 3.68 0.1852 0.3841 0.0818 0.0394 0.013 0.817 0.507 9.666 0.092 2.255 23.785 0.08 40592. 0.4732 4.21 0.2117 0.4250 0.0796 0.0396 0.013 0.821 0.493 9.716 0.093 2.194 23.029 0.08 40643. 0.4519 4.74 0.2382 0.4627 0.0772 0.0397 0.013 0.823 0.479 9.740 0.093 2.129 22.288 0.08 40697. 0.4308 5.26 0.2646 0.4974 0.0747 0.0397 0.013 0.823 0.463 9.735 0.093 2.058 21.562 0.08 40755. 0.4098 5.79 0.2911 0.5291 0.0719 0.0396 0.013 0.820 0.446 9.697 0.093 1.983 20.851 0.08 40817. 0.3890 6.31 0.3175 0.5579 0.0690 0.0393 0.013 0.814 0.428 9.625 0.092 1.902 20.153 0.08 40883. 0.3682 6.84 0.3440 0.5838 0.0659 0.0388 0.013 0.804 0.408 9.514 0.091 1.816 19.465 0.08 40952. 0.3475 7.37 0.3705 0.6067 0.0626 0.0382 0.013 0.791 0.388 9.362 0.089 1.725 18.786 0.08 41026. 0.3268 7.89 0.3969 0.6267 0.0590 0.0374 0.012 0.775 0.366 9.165 0.088 1.628 18.111 0.08 41103. 0.3061 8.42 0.4234 0.6435 0.0553 0.0364 0.012 0.754 0.343 8.924 0.085 1.526 17.435 0.08 41185. 0.2853 8.95 0.4498 0.6570 0.0515 0.0353 0.012 0.730 0.319 8.639 0.083 1.419 16.753 0.08 41270. 0.2644 9.47 0.4763 0.6668 0.0475 0.0339 0.011 0.703 0.294 8.314 0.079 1.309 16.058 0.08 41360. 0.2434 10.00 0.5028 0.6724 0.0434 0.0324 0.011 0.672 0.269 7.949 0.076 1.196 15.340 0.08 41453. 0.2222 10.52 0.5292 0.6731 0.0392 0.0308 0.010 0.638 0.243 7.545 0.072 1.080 14.590 0.08 41551. 0.2008 11.05 0.5557 0.6682 0.0349 0.0290 0.010 0.601 0.216 7.106 0.068 0.961 13.793 0.08 41652. 0.1791 11.58 0.5821 0.6563 0.0305 0.0271 0.009 0.560 0.189 6.631 0.063 0.841 12.931 0.08 41758. 0.1571 12.10 0.6086 0.6357 0.0261 0.0250 0.008 0.518 0.162 6.124 0.058 0.719 11.981 0.08 41867. 0.1346 12.63 0.6351 0.6038 0.0217 0.0228 0.007 0.472 0.134 5.586 0.053 0.597 10.906 0.08 41980. 0.1117 13.16 0.6615 0.5568 0.0172 0.0205 0.007 0.424 0.107 5.020 0.048 0.475 9.654 0.09 42098. 0.0882 13.68 0.6880 0.4884 0.0128 0.0181 0.006 0.374 0.080 4.429 0.042 0.354 8.143 0.09 42219. 0.0642 14.21 0.7145 0.3885 0.0085 0.0156 0.005 0.323 0.053 3.818 0.036 0.234 6.237 0.09 42344. 0.0399 14.73 0.7409 0.2384 0.0042 0.0130 0.004 0.270 0.026 3.190 0.030 0.115 3.690 0.09 42473. 0.0166 15.26 0.7674 0.0007 0.0000 0.0104 0.003 0.216 0.000 2.551 0.024 0.000 0.010 0.09 42606. 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 0.0933 0.0338 0.089 2.801 2.312 66.286 0.316 10.283 15.819 0.17 80660. 0.6721 1.06 0.0266 0.0711 0.0921 0.0344 0.090 2.852 2.282 67.475 0.322 10.152 15.343 0.17 80717. 0.6477 2.11 0.0532 0.1378 0.0908 0.0350 0.092 2.901 2.250 68.634 0.328 10.009 14.870 0.17 80779. 0.6233 3.17 0.0797 0.2002 0.0893 0.0356 0.094 2.947 2.215 69.740 0.333 9.851 14.403 0.17 80848. 0.5989 4.23 0.1063 0.2585 0.0878 0.0361 0.095 2.991 2.176 70.771 0.338 9.678 13.944 0.17 80922. 0.5747 5.29 0.1329 0.3127 0.0860 0.0366 0.096 3.030 2.133 71.703 0.342 9.488 13.494 0.17 81003. 0.5507 6.34 0.1595 0.3630 0.0842 0.0370 0.097 3.064 2.087 72.509 0.346 9.282 13.053 0.17 81091. 0.5269 7.40 0.1860 0.4095 0.0821 0.0373 0.098 3.092 2.036 73.163 0.349 9.057 12.624 0.17 81186. 0.5033 8.46 0.2126 0.4525 0.0799 0.0376 0.099 3.112 1.982 73.637 0.352 8.814 12.205 0.17 81288. 0.4801 9.51 0.2392 0.4921 0.0775 0.0377 0.099 3.123 1.922 73.902 0.353 8.551 11.799 0.17 81397. 0.4571 10.57 0.2658 0.5285 0.0750 0.0377 0.099 3.124 1.859 73.929 0.353 8.267 11.403 0.17 81514. 0.4344 11.63 0.2924 0.5617 0.0722 0.0376 0.099 3.114 1.790 73.691 0.352 7.963 11.019 0.17 81639. 0.4120 12.69 0.3189 0.5920 0.0693 0.0373 0.098 3.092 1.717 73.160 0.349 7.638 10.645 0.17 81772. 0.3898 13.74 0.3455 0.6194 0.0661 0.0369 0.097 3.056 1.639 72.310 0.345 7.290 10.281 0.17 81912. 0.3678 14.80 0.3721 0.6439 0.0628 0.0363 0.095 3.005 1.556 71.113 0.340 6.921 9.924 0.17 82060. 0.3459 15.86 0.3987 0.6655 0.0592 0.0355 0.093 2.939 1.468 69.546 0.332 6.529 9.574 0.17 82217. 0.3241 16.91 0.4253 0.6842 0.0555 0.0345 0.091 2.857 1.375 67.608 0.323 6.118 9.227 0.17 82381. 0.3024 17.97 0.4518 0.6998 0.0516 0.0333 0.088 2.760 1.279 65.307 0.312 5.689 8.883 0.17 82554. 0.2807 19.03 0.4784 0.7120 0.0476 0.0320 0.084 2.648 1.179 62.655 0.299 5.244 8.535 0.17 82734. 0.2590 20.08 0.5050 0.7204 0.0434 0.0304 0.080 2.521 1.076 59.664 0.285 4.787 8.182 0.17 82923. 0.2372 21.14 0.5316 0.7245 0.0392 0.0287 0.076 2.381 0.971 56.345 0.269 4.319 7.816 0.17 83119. 0.2152 22.20 0.5581 0.7233 0.0348 0.0269 0.071 2.228 0.864 52.712 0.252 3.842 7.433 0.17 83324. 0.1930 23.26 0.5847 0.7159 0.0305 0.0249 0.065 2.061 0.755 48.779 0.233 3.359 7.021 0.17 83536. 0.1705 24.31 0.6113 0.7002 0.0260 0.0227 0.060 1.883 0.645 44.561 0.213 2.871 6.570 0.17 83757. 0.1475 25.37 0.6379 0.6737 0.0216 0.0204 0.054 1.694 0.535 40.078 0.191 2.381 6.058 0.17 83985. 0.1238 26.43 0.6645 0.6320 0.0172 0.0180 0.047 1.494 0.425 35.354 0.169 1.891 5.455 0.17 84222. 0.0994 27.48 0.6910 0.5674 0.0127 0.0155 0.041 1.285 0.316 30.417 0.145 1.405 4.709 0.17 84466. 0.0739 28.54 0.7176 0.4661 0.0084 0.0129 0.034 1.069 0.208 25.300 0.121 0.924 3.725 0.17 84719. 0.0475 29.60 0.7442 0.2992 0.0041 0.0102 0.027 0.847 0.102 20.042 0.096 0.453 2.306 0.17 84979. 0.0206 30.66 0.7708 -0.0055 -0.0001 0.0075 0.020 0.620 -0.001 14.680 0.070 -0.006 -0.041 0.17 85245. 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 0.0937 0.0329 0.292 6.129 5.225 217.530 0.692 23.240 10.894 0.25 120987. 0.6958 1.59 0.0266 0.0735 0.0925 0.0335 0.297 6.245 5.159 221.674 0.706 22.948 10.556 0.25 121072. 0.6699 3.18 0.0532 0.1423 0.0912 0.0341 0.303 6.359 5.087 225.719 0.718 22.626 10.222 0.25 121166. 0.6441 4.76 0.0798 0.2065 0.0898 0.0347 0.308 6.469 5.007 229.591 0.731 22.272 9.892 0.25 121269. 0.6185 6.35 0.1064 0.2664 0.0882 0.0352 0.313 6.571 4.920 233.211 0.742 21.883 9.569 0.25 121381. 0.5930 7.94 0.1331 0.3220 0.0865 0.0357 0.317 6.663 4.824 236.497 0.753 21.458 9.252 0.25 121503. 0.5678 9.53 0.1597 0.3735 0.0846 0.0362 0.321 6.744 4.720 239.357 0.762 20.994 8.944 0.25 121635. 0.5429 11.11 0.1863 0.4211 0.0826 0.0365 0.324 6.810 4.606 241.699 0.769 20.488 8.644 0.25 121778. 0.5184 12.70 0.2129 0.4651 0.0804 0.0368 0.326 6.858 4.483 243.425 0.775 19.940 8.353 0.25 121931. 0.4941 14.29 0.2395 0.5055 0.0780 0.0369 0.328 6.887 4.349 244.436 0.778 19.346 8.071 0.25 122096. 0.4703 15.88 0.2661 0.5427 0.0754 0.0370 0.328 6.892 4.206 244.634 0.779 18.706 7.797 0.25 122272. 0.4468 17.46 0.2927 0.5767 0.0726 0.0369 0.327 6.872 4.051 243.919 0.776 18.019 7.533 0.25 122459. 0.4236 19.05 0.3193 0.6077 0.0697 0.0366 0.325 6.824 3.886 242.199 0.771 17.283 7.277 0.25 122659. 0.4008 20.64 0.3459 0.6359 0.0665 0.0362 0.321 6.744 3.709 239.381 0.762 16.498 7.028 0.25 122870. 0.3782 22.23 0.3725 0.6612 0.0631 0.0356 0.316 6.631 3.521 235.366 0.749 15.663 6.786 0.25 123093. 0.3558 23.81 0.3992 0.6837 0.0596 0.0348 0.309 6.482 3.322 230.073 0.732 14.777 6.549 0.25 123328. 0.3335 25.40 0.4258 0.7034 0.0558 0.0338 0.300 6.297 3.113 223.494 0.711 13.845 6.317 0.25 123576. 0.3114 26.99 0.4524 0.7202 0.0519 0.0326 0.289 6.076 2.894 215.656 0.686 12.873 6.087 0.25 123835. 0.2893 28.58 0.4790 0.7338 0.0478 0.0312 0.277 5.821 2.668 206.597 0.658 11.867 5.857 0.25 124107. 0.2673 30.16 0.5056 0.7438 0.0437 0.0297 0.263 5.532 2.435 196.355 0.625 10.832 5.625 0.25 124390. 0.2453 31.75 0.5322 0.7499 0.0394 0.0280 0.248 5.211 2.197 184.968 0.589 9.772 5.387 0.25 124685. 0.2231 33.34 0.5588 0.7511 0.0350 0.0261 0.231 4.859 1.954 172.480 0.549 8.693 5.139 0.25 124993. 0.2007 34.93 0.5854 0.7464 0.0306 0.0240 0.213 4.478 1.708 158.938 0.506 7.599 4.875 0.25 125312. 0.1780 36.51 0.6120 0.7342 0.0262 0.0218 0.194 4.068 1.460 144.399 0.460 6.495 4.586 0.25 125644. 0.1549 38.10 0.6386 0.7116 0.0217 0.0195 0.173 3.633 1.211 128.931 0.410 5.386 4.260 0.26 125988. 0.1310 39.69 0.6653 0.6742 0.0172 0.0170 0.151 3.173 0.962 112.615 0.358 4.279 3.875 0.26 126343. 0.1062 41.28 0.6919 0.6140 0.0128 0.0144 0.128 2.692 0.715 95.551 0.304 3.180 3.393 0.26 126711. 0.0802 42.86 0.7185 0.5155 0.0084 0.0118 0.104 2.194 0.471 77.856 0.248 2.094 2.743 0.26 127091. 0.0526 44.45 0.7451 0.3433 0.0042 0.0090 0.080 1.681 0.232 59.669 0.190 1.031 1.762 0.26 127482. 0.0237 46.04 0.7717 -0.0026 0.0000 0.0062 0.055 1.158 -0.001 41.109 0.131 -0.005 -0.013 0.26 127881. 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 0.0942 0.0325 0.683 10.761 9.341 509.259 1.216 41.550 8.320 0.33 161309. 0.7105 2.12 0.0266 0.0748 0.0930 0.0331 0.696 10.974 9.226 519.324 1.240 41.036 8.058 0.33 161423. 0.6838 4.24 0.0532 0.1448 0.0917 0.0337 0.710 11.182 9.098 529.164 1.263 40.468 7.798 0.33 161549. 0.6572 6.35 0.0799 0.2101 0.0903 0.0343 0.722 11.381 8.957 538.595 1.286 39.843 7.543 0.33 161686. 0.6308 8.47 0.1065 0.2708 0.0888 0.0349 0.734 11.568 8.803 547.432 1.307 39.155 7.294 0.33 161836. 0.6046 10.59 0.1331 0.3272 0.0871 0.0354 0.745 11.737 8.633 555.469 1.326 38.401 7.050 0.33 161999. 0.5788 12.71 0.1597 0.3794 0.0852 0.0359 0.754 11.886 8.448 562.492 1.343 37.577 6.812 0.33 162175. 0.5532 14.82 0.1863 0.4277 0.0832 0.0362 0.762 12.008 8.246 568.271 1.357 36.679 6.582 0.33 162366. 0.5281 16.94 0.2130 0.4722 0.0809 0.0365 0.768 12.099 8.027 572.571 1.367 35.703 6.358 0.33 162571. 0.5033 19.06 0.2396 0.5132 0.0785 0.0367 0.771 12.153 7.789 575.153 1.373 34.646 6.142 0.33 162791. 0.4790 21.18 0.2662 0.5509 0.0760 0.0367 0.772 12.166 7.533 575.774 1.375 33.505 5.934 0.33 163026. 0.4550 23.29 0.2928 0.5854 0.0732 0.0366 0.770 12.133 7.257 574.201 1.371 32.278 5.732 0.33 163277. 0.4315 25.41 0.3195 0.6169 0.0702 0.0364 0.765 12.049 6.961 570.203 1.361 30.964 5.537 0.33 163543. 0.4082 27.53 0.3461 0.6455 0.0670 0.0359 0.756 11.908 6.646 563.556 1.345 29.561 5.349 0.34 163825. 0.3853 29.65 0.3727 0.6714 0.0636 0.0353 0.743 11.707 6.310 554.023 1.323 28.067 5.166 0.34 164123. 0.3626 31.76 0.3993 0.6946 0.0600 0.0345 0.726 11.440 5.954 541.403 1.293 26.482 4.988 0.34 164438. 0.3401 33.88 0.4259 0.7150 0.0563 0.0335 0.705 11.108 5.579 525.665 1.255 24.814 4.814 0.34 164768. 0.3177 36.00 0.4526 0.7326 0.0523 0.0323 0.680 10.711 5.188 506.875 1.210 23.075 4.642 0.34 165114. 0.2954 38.12 0.4792 0.7472 0.0482 0.0309 0.651 10.251 4.782 485.118 1.158 21.272 4.471 0.34 165477. 0.2732 40.23 0.5058 0.7584 0.0440 0.0294 0.618 9.730 4.365 460.482 1.099 19.417 4.300 0.34 165855. 0.2510 42.35 0.5324 0.7659 0.0397 0.0276 0.581 9.151 3.938 433.060 1.034 17.518 4.125 0.34 166250. 0.2287 44.47 0.5590 0.7688 0.0353 0.0257 0.540 8.515 3.504 402.954 0.962 15.584 3.944 0.34 166660. 0.2063 46.59 0.5857 0.7662 0.0309 0.0236 0.497 7.824 3.063 370.279 0.884 13.623 3.752 0.34 167087. 0.1834 48.70 0.6123 0.7564 0.0264 0.0214 0.449 7.082 2.618 335.172 0.800 11.644 3.543 0.34 167529. 0.1602 50.82 0.6389 0.7368 0.0219 0.0190 0.399 6.293 2.171 297.797 0.711 9.658 3.307 0.34 167988. 0.1362 52.94 0.6655 0.7029 0.0174 0.0165 0.346 5.459 1.725 258.355 0.617 7.673 3.029 0.34 168463. 0.1111 55.06 0.6921 0.6466 0.0129 0.0138 0.291 4.587 1.282 217.086 0.518 5.703 2.679 0.34 168953. 0.0848 57.17 0.7188 0.5512 0.0085 0.0111 0.234 3.683 0.845 174.282 0.416 3.759 2.199 0.34 169460. 0.0565 59.29 0.7454 0.3772 0.0042 0.0083 0.175 2.753 0.417 130.283 0.311 1.854 1.451 0.34 169982. 0.0262 61.41 0.7720 -0.0006 0.0000 0.0054 0.114 1.804 0.000 85.363 0.204 -0.002 -0.002 0.34 170514. 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 0.0949 0.0324 1.329 16.757 14.701 991.287 1.893 65.389 6.726 0.42 201626. 0.7206 2.65 0.0266 0.0756 0.0937 0.0330 1.356 17.097 14.522 1011.418 1.932 64.595 6.513 0.42 201769. 0.6934 5.30 0.0533 0.1463 0.0925 0.0337 1.383 17.431 14.325 1031.117 1.969 63.717 6.301 0.42 201926. 0.6664 7.94 0.0799 0.2122 0.0910 0.0343 1.408 17.750 14.107 1050.020 2.005 62.748 6.094 0.42 202098. 0.6395 10.59 0.1065 0.2735 0.0895 0.0349 1.432 18.050 13.867 1067.755 2.039 61.680 5.890 0.42 202285. 0.6129 13.24 0.1332 0.3304 0.0878 0.0354 1.454 18.323 13.603 1083.915 2.070 60.507 5.692 0.42 202490. 0.5866 15.89 0.1598 0.3831 0.0859 0.0358 1.473 18.562 13.314 1098.062 2.097 59.223 5.500 0.42 202711. 0.5607 18.54 0.1864 0.4317 0.0839 0.0362 1.488 18.760 12.999 1109.743 2.119 57.820 5.313 0.42 202950. 0.5352 21.18 0.2130 0.4766 0.0817 0.0365 1.500 18.907 12.656 1118.487 2.136 56.293 5.132 0.42 203207. 0.5101 23.83 0.2397 0.5180 0.0793 0.0367 1.507 18.997 12.284 1123.814 2.146 54.638 4.958 0.42 203482. 0.4855 26.48 0.2663 0.5560 0.0767 0.0367 1.509 19.022 11.882 1125.240 2.149 52.850 4.789 0.42 203777. 0.4613 29.13 0.2929 0.5908 0.0739 0.0366 1.505 18.972 11.449 1122.297 2.143 50.924 4.627 0.42 204091. 0.4374 31.78 0.3196 0.6227 0.0709 0.0364 1.495 18.840 10.985 1114.526 2.129 48.859 4.470 0.42 204425. 0.4140 34.42 0.3462 0.6518 0.0677 0.0360 1.477 18.620 10.488 1101.480 2.104 46.652 4.319 0.42 204778. 0.3908 37.07 0.3728 0.6781 0.0643 0.0353 1.452 18.302 9.960 1082.688 2.068 44.300 4.172 0.42 205152. 0.3679 39.72 0.3995 0.7017 0.0607 0.0345 1.418 17.881 9.398 1057.742 2.020 41.803 4.030 0.42 205546. 0.3452 42.37 0.4261 0.7228 0.0568 0.0335 1.377 17.354 8.807 1026.568 1.961 39.174 3.891 0.42 205959. 0.3227 45.02 0.4527 0.7410 0.0529 0.0323 1.327 16.723 8.190 989.287 1.889 36.429 3.755 0.42 206393. 0.3003 47.66 0.4794 0.7564 0.0487 0.0309 1.269 15.993 7.551 946.067 1.807 33.585 3.620 0.42 206847. 0.2779 50.31 0.5060 0.7686 0.0445 0.0293 1.203 15.165 6.892 897.083 1.713 30.656 3.485 0.42 207320. 0.2556 52.96 0.5326 0.7772 0.0401 0.0275 1.130 14.242 6.218 842.517 1.609 27.656 3.347 0.42 207814. 0.2332 55.61 0.5593 0.7814 0.0357 0.0255 1.049 13.229 5.531 782.571 1.495 24.600 3.205 0.42 208328. 0.2106 58.26 0.5859 0.7804 0.0312 0.0234 0.962 12.129 4.834 717.475 1.370 21.501 3.056 0.42 208862. 0.1877 60.90 0.6125 0.7726 0.0267 0.0211 0.868 10.946 4.131 647.502 1.237 18.374 2.894 0.42 209416. 0.1643 63.55 0.6391 0.7553 0.0221 0.0187 0.768 9.686 3.425 572.983 1.094 15.234 2.711 0.43 209990. 0.1402 66.20 0.6658 0.7242 0.0176 0.0161 0.663 8.356 2.720 494.320 0.944 12.097 2.495 0.43 210584. 0.1150 68.85 0.6924 0.6710 0.0130 0.0134 0.553 6.965 2.019 411.999 0.787 8.982 2.223 0.43 211198. 0.0883 71.50 0.7190 0.5782 0.0086 0.0107 0.438 5.521 1.328 326.608 0.624 5.909 1.845 0.43 211832. 0.0594 74.14 0.7457 0.4023 0.0042 0.0078 0.320 4.037 0.652 238.836 0.456 2.899 1.238 0.43 212485. 0.0279 76.79 0.7723 -0.0080 -0.0001 0.0049 0.200 2.522 -0.008 149.195 0.285 -0.035 -0.024 0.43 213148. 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 0.0957 0.0325 2.305 24.208 21.356 1718.472 2.735 94.992 5.637 0.50 241935. 0.7278 3.17 0.0266 0.0760 0.0946 0.0331 2.352 24.710 21.104 1754.122 2.792 93.871 5.457 0.50 242106. 0.7005 6.35 0.0532 0.1470 0.0933 0.0338 2.399 25.202 20.824 1789.040 2.847 92.627 5.280 0.50 242295. 0.6732 9.52 0.0798 0.2132 0.0919 0.0344 2.444 25.675 20.515 1822.591 2.901 91.250 5.105 0.50 242502. 0.6461 12.70 0.1064 0.2747 0.0904 0.0350 2.486 26.119 20.173 1854.110 2.951 89.729 4.935 0.50 242727. 0.6193 15.87 0.1330 0.3319 0.0887 0.0356 2.525 26.524 19.796 1882.875 2.997 88.054 4.769 0.50 242972. 0.5928 19.05 0.1596 0.3848 0.0869 0.0360 2.559 26.880 19.383 1908.114 3.037 86.214 4.607 0.50 243238. 0.5668 22.22 0.1863 0.4337 0.0848 0.0364 2.587 27.174 18.930 1929.020 3.070 84.202 4.451 0.50 243525. 0.5411 25.40 0.2129 0.4788 0.0826 0.0367 2.608 27.396 18.437 1944.755 3.095 82.007 4.300 0.50 243834. 0.5159 28.57 0.2395 0.5204 0.0802 0.0369 2.621 27.533 17.901 1954.473 3.111 79.623 4.154 0.50 244165. 0.4911 31.75 0.2661 0.5586 0.0776 0.0370 2.625 27.573 17.321 1957.327 3.115 77.042 4.014 0.50 244519. 0.4667 34.92 0.2927 0.5938 0.0748 0.0369 2.618 27.505 16.695 1952.481 3.107 74.260 3.878 0.50 244896. 0.4428 38.10 0.3193 0.6260 0.0718 0.0366 2.600 27.317 16.023 1939.126 3.086 71.272 3.748 0.50 245297. 0.4192 41.27 0.3459 0.6554 0.0686 0.0362 2.570 26.998 15.305 1916.482 3.050 68.075 3.622 0.50 245722. 0.3959 44.45 0.3725 0.6821 0.0652 0.0356 2.526 26.536 14.538 1883.724 2.998 64.665 3.501 0.50 246170. 0.3729 47.62 0.3991 0.7062 0.0615 0.0348 2.468 25.922 13.723 1840.114 2.929 61.041 3.383 0.50 246642. 0.3501 50.80 0.4257 0.7277 0.0577 0.0337 2.394 25.152 12.864 1785.487 2.842 57.220 3.268 0.50 247139. 0.3275 53.97 0.4523 0.7466 0.0536 0.0325 2.307 24.230 11.967 1720.049 2.738 53.227 3.156 0.50 247659. 0.3050 57.15 0.4789 0.7627 0.0495 0.0311 2.205 23.160 11.036 1644.087 2.617 49.087 3.045 0.51 248204. 0.2826 60.32 0.5056 0.7758 0.0452 0.0294 2.089 21.946 10.076 1557.913 2.479 44.820 2.934 0.51 248772. 0.2602 63.50 0.5322 0.7854 0.0408 0.0276 1.960 20.593 9.094 1461.848 2.327 40.448 2.821 0.51 249364. 0.2377 66.67 0.5588 0.7909 0.0363 0.0256 1.819 19.106 8.092 1356.245 2.159 35.991 2.706 0.51 249981. 0.2151 69.85 0.5854 0.7915 0.0317 0.0235 1.665 17.489 7.075 1241.510 1.976 31.470 2.585 0.51 250621. 0.1921 73.02 0.6120 0.7855 0.0271 0.0211 1.499 15.751 6.049 1118.126 1.780 26.905 2.454 0.51 251285. 0.1686 76.20 0.6386 0.7705 0.0225 0.0186 1.323 13.899 5.018 986.675 1.570 22.319 2.307 0.51 251973. 0.1444 79.37 0.6652 0.7423 0.0179 0.0160 1.137 11.944 3.988 847.868 1.349 17.738 2.133 0.51 252685. 0.1190 82.55 0.6918 0.6926 0.0133 0.0133 0.942 9.897 2.965 702.568 1.118 13.186 1.914 0.51 253420. 0.0921 85.72 0.7184 0.6038 0.0088 0.0104 0.740 7.774 1.955 551.819 0.878 8.695 1.607 0.51 254180. 0.0628 88.90 0.7450 0.4301 0.0043 0.0075 0.532 5.590 0.966 396.849 0.632 4.295 1.104 0.51 254963. 0.0303 92.07 0.7716 0.0011 0.0000 0.0045 0.320 3.361 0.001 238.583 0.380 0.006 0.003 0.51 255757. 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 0.0967 0.0328 3.692 33.243 29.379 2753.142 3.756 130.677 4.840 0.58 282234. 0.7330 3.70 0.0266 0.0761 0.0956 0.0334 3.770 33.947 29.044 2811.413 3.835 129.190 4.686 0.58 282434. 0.7056 7.40 0.0532 0.1472 0.0944 0.0341 3.847 34.637 28.672 2868.569 3.913 127.533 4.534 0.58 282655. 0.6783 11.11 0.0798 0.2135 0.0930 0.0348 3.921 35.301 28.258 2923.555 3.988 125.692 4.384 0.58 282896. 0.6512 14.81 0.1064 0.2751 0.0915 0.0354 3.990 35.925 27.799 2975.283 4.059 123.652 4.238 0.58 283160. 0.6243 18.51 0.1330 0.3324 0.0899 0.0360 4.053 36.496 27.292 3022.562 4.123 121.397 4.096 0.58 283446. 0.5978 22.21 0.1596 0.3854 0.0880 0.0365 4.109 36.998 26.734 3064.122 4.180 118.913 3.957 0.58 283757. 0.5717 25.92 0.1862 0.4344 0.0860 0.0369 4.155 37.415 26.121 3098.639 4.227 116.187 3.824 0.58 284093. 0.5460 29.62 0.2128 0.4797 0.0838 0.0372 4.190 37.730 25.451 3124.743 4.263 113.205 3.694 0.58 284454. 0.5207 33.32 0.2394 0.5215 0.0814 0.0374 4.212 37.927 24.721 3141.041 4.285 109.958 3.570 0.58 284841. 0.4959 37.02 0.2660 0.5599 0.0788 0.0374 4.219 37.989 23.929 3146.153 4.292 106.435 3.450 0.59 285255. 0.4715 40.73 0.2926 0.5953 0.0760 0.0373 4.209 37.899 23.073 3138.713 4.282 102.630 3.334 0.59 285696. 0.4475 44.43 0.3192 0.6278 0.0729 0.0371 4.181 37.642 22.153 3117.410 4.253 98.536 3.223 0.59 286164. 0.4239 48.13 0.3458 0.6575 0.0697 0.0367 4.132 37.202 21.166 3080.979 4.203 94.148 3.116 0.59 286661. 0.4006 51.83 0.3723 0.6846 0.0662 0.0360 4.061 36.563 20.113 3028.094 4.131 89.462 3.013 0.59 287185. 0.3775 55.53 0.3989 0.7091 0.0625 0.0352 3.966 35.711 18.992 2957.534 4.035 84.475 2.913 0.59 287736. 0.3547 59.24 0.4255 0.7311 0.0586 0.0341 3.847 34.642 17.808 2868.975 3.914 79.210 2.815 0.59 288316. 0.3320 62.94 0.4521 0.7506 0.0546 0.0329 3.705 33.359 16.570 2762.735 3.769 73.702 2.720 0.59 288924. 0.3094 66.64 0.4787 0.7674 0.0503 0.0314 3.539 31.868 15.284 2639.288 3.600 67.983 2.627 0.59 289560. 0.2869 70.34 0.5053 0.7812 0.0460 0.0297 3.351 30.176 13.958 2499.142 3.409 62.086 2.533 0.59 290224. 0.2644 74.05 0.5319 0.7918 0.0415 0.0279 3.142 28.289 12.598 2342.825 3.196 56.038 2.439 0.59 290915. 0.2419 77.75 0.5585 0.7984 0.0369 0.0258 2.911 26.213 11.211 2170.916 2.962 49.869 2.342 0.59 291634. 0.2191 81.45 0.5851 0.8003 0.0323 0.0236 2.661 23.957 9.804 1984.080 2.707 43.606 2.241 0.59 292381. 0.1961 85.15 0.6117 0.7959 0.0276 0.0212 2.391 21.530 8.381 1783.105 2.432 37.280 2.132 0.59 293156. 0.1725 88.86 0.6383 0.7829 0.0229 0.0187 2.104 18.944 6.952 1568.944 2.140 30.923 2.010 0.60 293958. 0.1481 92.56 0.6649 0.7571 0.0182 0.0160 1.801 16.213 5.523 1342.760 1.832 24.568 1.866 0.60 294789. 0.1225 96.26 0.6915 0.7102 0.0135 0.0132 1.483 13.354 4.104 1105.970 1.509 18.252 1.683 0.60 295647. 0.0953 99.96 0.7181 0.6243 0.0089 0.0102 1.154 10.388 2.702 860.293 1.174 12.019 1.425 0.60 296532. 0.0654 103.67 0.7447 0.4507 0.0044 0.0072 0.815 7.338 1.329 607.757 0.829 5.911 0.992 0.60 297445. 0.0319 107.37 0.7713 -0.0059 0.0000 0.0042 0.469 4.224 -0.010 349.797 0.477 -0.043 -0.013 0.60 298369. 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 0.0980 0.0332 5.592 44.059 38.860 4170.147 4.978 172.849 4.227 0.67 322520. 0.7362 4.23 0.0266 0.0758 0.0969 0.0339 5.712 45.006 38.440 4259.800 5.085 170.980 4.093 0.67 322749. 0.7090 8.45 0.0531 0.1468 0.0957 0.0347 5.831 45.938 37.969 4347.988 5.190 168.885 3.961 0.67 323001. 0.6819 12.68 0.0797 0.2130 0.0944 0.0353 5.945 46.837 37.443 4433.070 5.292 166.546 3.831 0.67 323277. 0.6550 16.91 0.1063 0.2746 0.0929 0.0360 6.052 47.684 36.857 4513.307 5.387 163.940 3.704 0.67 323579. 0.6283 21.14 0.1329 0.3317 0.0913 0.0366 6.151 48.461 36.206 4586.823 5.475 161.046 3.580 0.67 323907. 0.6019 25.36 0.1594 0.3847 0.0895 0.0371 6.238 49.146 35.487 4651.618 5.552 157.844 3.460 0.67 324263. 0.5759 29.59 0.1860 0.4338 0.0875 0.0375 6.310 49.716 34.693 4705.602 5.617 154.314 3.344 0.67 324647. 0.5503 33.82 0.2126 0.4791 0.0853 0.0378 6.365 50.150 33.822 4746.652 5.666 150.440 3.232 0.67 325060. 0.5252 38.04 0.2391 0.5210 0.0829 0.0380 6.400 50.424 32.870 4772.614 5.697 146.205 3.124 0.67 325504. 0.5004 42.27 0.2657 0.5596 0.0803 0.0381 6.412 50.516 31.834 4781.338 5.707 141.597 3.020 0.67 325978. 0.4761 46.50 0.2923 0.5952 0.0774 0.0380 6.398 50.404 30.712 4770.738 5.695 136.605 2.920 0.67 326483. 0.4521 50.72 0.3188 0.6279 0.0744 0.0378 6.355 50.067 29.501 4738.801 5.657 131.222 2.824 0.67 327019. 0.4285 54.95 0.3454 0.6579 0.0711 0.0373 6.281 49.484 28.202 4683.592 5.591 125.441 2.731 0.67 327587. 0.4052 59.18 0.3720 0.6854 0.0676 0.0367 6.173 48.633 26.811 4603.116 5.495 119.255 2.642 0.67 328187. 0.3822 63.41 0.3986 0.7103 0.0639 0.0358 6.029 47.496 25.328 4495.474 5.366 112.660 2.555 0.67 328818. 0.3594 67.63 0.4251 0.7329 0.0599 0.0347 5.847 46.065 23.760 4360.049 5.204 105.686 2.472 0.67 329482. 0.3366 71.86 0.4517 0.7529 0.0558 0.0335 5.629 44.346 22.117 4197.312 5.010 98.377 2.390 0.67 330177. 0.3141 76.09 0.4783 0.7704 0.0515 0.0319 5.375 42.346 20.409 4008.001 4.784 90.778 2.310 0.67 330904. 0.2915 80.31 0.5048 0.7850 0.0470 0.0302 5.086 40.073 18.645 3792.906 4.527 82.933 2.230 0.67 331663. 0.2690 84.54 0.5314 0.7965 0.0424 0.0283 4.764 37.537 16.834 3552.853 4.241 74.879 2.149 0.68 332453. 0.2464 88.77 0.5580 0.8043 0.0378 0.0262 4.410 34.747 14.985 3288.747 3.926 66.655 2.067 0.68 333274. 0.2235 93.00 0.5845 0.8075 0.0330 0.0239 4.025 31.713 13.107 3001.610 3.583 58.300 1.981 0.68 334128. 0.2004 97.22 0.6111 0.8047 0.0283 0.0215 3.611 28.449 11.208 2692.656 3.214 49.854 1.888 0.68 335012. 0.1766 101.45 0.6377 0.7937 0.0234 0.0188 3.169 24.970 9.299 2363.360 2.821 41.360 1.785 0.68 335929. 0.1520 105.68 0.6643 0.7703 0.0186 0.0161 2.703 21.294 7.388 2015.510 2.406 32.863 1.663 0.68 336876. 0.1263 109.90 0.6908 0.7264 0.0138 0.0132 2.214 17.447 5.489 1651.328 1.971 24.415 1.508 0.68 337856. 0.0987 114.13 0.7174 0.6439 0.0091 0.0101 1.708 13.455 3.613 1273.547 1.520 16.072 1.287 0.68 338866. 0.0683 118.36 0.7440 0.4717 0.0045 0.0071 1.187 9.355 1.775 885.458 1.057 7.894 0.909 0.68 339908. 0.0338 122.58 0.7705 -0.0091 0.0000 0.0039 0.656 5.171 -0.018 489.411 0.584 -0.081 -0.017 0.69 340961. 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 0.0994 0.0345 8.271 57.920 49.906 6167.338 6.544 221.984 3.670 0.75 362790. 0.7245 4.75 0.0265 0.0742 0.0984 0.0352 8.432 59.051 49.405 6287.823 6.672 219.754 3.564 0.75 363047. 0.6999 9.49 0.0530 0.1439 0.0973 0.0359 8.591 60.165 48.839 6406.394 6.797 217.237 3.458 0.75 363330. 0.6752 14.24 0.0796 0.2093 0.0960 0.0365 8.745 61.240 48.202 6520.849 6.919 214.404 3.353 0.75 363641. 0.6504 18.99 0.1061 0.2705 0.0946 0.0371 8.889 62.254 47.488 6628.875 7.033 211.225 3.249 0.75 363980. 0.6256 23.74 0.1326 0.3275 0.0930 0.0377 9.022 63.185 46.689 6727.926 7.139 207.671 3.148 0.75 364350. 0.6009 28.48 0.1591 0.3806 0.0912 0.0381 9.139 64.005 45.799 6815.248 7.231 203.712 3.048 0.75 364750. 0.5763 33.23 0.1857 0.4299 0.0893 0.0386 9.237 64.687 44.811 6887.920 7.308 199.321 2.951 0.75 365183. 0.5519 37.98 0.2122 0.4756 0.0871 0.0389 9.311 65.203 43.722 6942.865 7.367 194.474 2.856 0.75 365649. 0.5277 42.73 0.2387 0.5178 0.0847 0.0391 9.356 65.523 42.524 6976.937 7.403 189.149 2.765 0.75 366148. 0.5037 47.47 0.2652 0.5568 0.0821 0.0391 9.370 65.617 41.216 6986.916 7.413 183.328 2.676 0.75 366683. 0.4800 52.22 0.2918 0.5928 0.0793 0.0390 9.346 65.454 39.792 6969.611 7.395 176.996 2.590 0.75 367252. 0.4564 56.97 0.3183 0.6260 0.0762 0.0387 9.282 65.006 38.252 6921.899 7.344 170.144 2.507 0.75 367856. 0.4332 61.71 0.3448 0.6564 0.0729 0.0383 9.174 64.244 36.592 6840.712 7.258 162.763 2.426 0.75 368495. 0.4101 66.46 0.3713 0.6843 0.0693 0.0376 9.016 63.138 34.812 6722.931 7.133 154.845 2.349 0.75 369171. 0.3872 71.21 0.3979 0.7098 0.0656 0.0367 8.804 61.659 32.910 6565.447 6.966 146.385 2.274 0.76 369882. 0.3644 75.96 0.4244 0.7328 0.0615 0.0356 8.538 59.794 30.894 6366.934 6.756 137.414 2.201 0.76 370629. 0.3418 80.70 0.4509 0.7536 0.0573 0.0343 8.218 57.550 28.775 6127.940 6.502 127.993 2.130 0.76 371411. 0.3192 85.45 0.4774 0.7718 0.0529 0.0327 7.844 54.936 26.569 5849.586 6.207 118.180 2.060 0.76 372228. 0.2967 90.20 0.5040 0.7873 0.0484 0.0310 7.420 51.964 24.288 5533.115 5.871 108.031 1.991 0.76 373082. 0.2742 94.95 0.5305 0.7997 0.0437 0.0290 6.946 48.646 21.942 5179.893 5.496 97.597 1.921 0.76 373970. 0.2515 99.69 0.5570 0.8086 0.0389 0.0268 6.425 44.998 19.544 4791.430 5.084 86.930 1.850 0.76 374893. 0.2285 104.44 0.5835 0.8129 0.0341 0.0245 5.860 41.036 17.104 4369.500 4.636 76.078 1.775 0.76 375852. 0.2052 109.19 0.6101 0.8113 0.0292 0.0219 5.252 36.779 14.635 3916.270 4.155 65.095 1.695 0.76 376845. 0.1812 113.94 0.6366 0.8014 0.0242 0.0192 4.606 32.254 12.148 3434.428 3.644 54.036 1.604 0.76 377874. 0.1562 118.68 0.6631 0.7786 0.0192 0.0164 3.926 27.492 9.659 2927.358 3.106 42.961 1.497 0.77 378938. 0.1300 123.43 0.6896 0.7345 0.0143 0.0134 3.217 22.532 7.180 2399.267 2.546 31.936 1.357 0.77 380037. 0.1016 128.18 0.7162 0.6496 0.0094 0.0104 2.488 17.424 4.729 1855.272 1.969 21.033 1.156 0.77 381171. 0.0702 132.92 0.7427 0.4719 0.0046 0.0073 1.745 12.222 2.323 1301.428 1.381 10.335 0.810 0.77 382340. 0.0345 137.67 0.7692 -0.0092 0.0000 0.0042 0.995 6.971 -0.025 742.266 0.788 -0.111 -0.015 0.77 383521. 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 0.1010 0.0389 12.775 80.520 62.588 9526.521 9.097 278.392 2.980 0.83 403038. 0.6587 5.27 0.0265 0.0673 0.1001 0.0394 12.953 81.643 62.025 9659.327 9.224 275.885 2.912 0.83 403323. 0.6409 10.54 0.0530 0.1314 0.0990 0.0399 13.123 82.714 61.381 9786.096 9.345 273.025 2.845 0.83 403637. 0.6228 15.80 0.0795 0.1924 0.0979 0.0404 13.281 83.710 60.650 9903.824 9.457 269.771 2.778 0.83 403981. 0.6044 21.07 0.1060 0.2504 0.0965 0.0408 13.423 84.601 59.820 10009.327 9.558 266.081 2.711 0.83 404358. 0.5858 26.34 0.1324 0.3053 0.0950 0.0412 13.544 85.363 58.883 10099.455 9.644 261.912 2.644 0.83 404769. 0.5670 31.61 0.1589 0.3573 0.0933 0.0415 13.639 85.967 57.829 10170.890 9.712 257.223 2.579 0.83 405215. 0.5480 36.87 0.1854 0.4064 0.0914 0.0417 13.706 86.384 56.649 10220.273 9.760 251.976 2.514 0.83 405696. 0.5287 42.14 0.2119 0.4526 0.0893 0.0418 13.738 86.586 55.336 10244.176 9.782 246.137 2.450 0.83 406215. 0.5092 47.41 0.2384 0.4961 0.0869 0.0418 13.731 86.544 53.883 10239.119 9.778 239.673 2.387 0.84 406772. 0.4896 52.68 0.2649 0.5368 0.0844 0.0416 13.681 86.226 52.284 10201.573 9.742 232.558 2.325 0.84 407367. 0.4696 57.94 0.2914 0.5749 0.0815 0.0413 13.582 85.604 50.533 10127.982 9.672 224.771 2.263 0.84 408001. 0.4495 63.21 0.3179 0.6103 0.0785 0.0409 13.430 84.648 48.628 10014.825 9.563 216.297 2.202 0.84 408675. 0.4291 68.48 0.3444 0.6432 0.0751 0.0402 13.221 83.328 46.566 9858.633 9.414 207.124 2.142 0.84 409388. 0.4085 73.75 0.3708 0.6735 0.0715 0.0394 12.949 81.612 44.345 9655.697 9.221 197.244 2.083 0.84 410140. 0.3876 79.02 0.3973 0.7012 0.0677 0.0384 12.608 79.468 41.962 9402.044 8.978 186.648 2.024 0.84 410932. 0.3664 84.28 0.4238 0.7265 0.0636 0.0371 12.197 76.877 39.427 9095.496 8.686 175.372 1.966 0.84 411764. 0.3450 89.55 0.4503 0.7491 0.0593 0.0356 11.716 73.844 36.756 8736.591 8.343 163.491 1.908 0.84 412634. 0.3233 94.82 0.4768 0.7688 0.0548 0.0340 11.171 70.408 33.966 8330.050 7.955 151.080 1.849 0.84 413544. 0.3012 100.09 0.5033 0.7852 0.0501 0.0321 10.562 66.570 31.073 7875.999 7.521 138.212 1.789 0.84 414493. 0.2787 105.35 0.5298 0.7977 0.0453 0.0301 9.893 62.356 28.092 7377.488 7.045 124.954 1.727 0.84 415481. 0.2558 110.62 0.5563 0.8056 0.0404 0.0279 9.168 57.787 25.038 6836.862 6.529 111.371 1.661 0.85 416507. 0.2322 115.89 0.5828 0.8078 0.0354 0.0255 8.388 52.870 21.927 6255.178 5.973 97.532 1.590 0.85 417572. 0.2080 121.16 0.6092 0.8023 0.0303 0.0230 7.560 47.649 18.773 5637.382 5.383 83.503 1.510 0.85 418676. 0.1829 126.42 0.6357 0.7856 0.0252 0.0204 6.691 42.170 15.592 4989.233 4.764 69.355 1.417 0.85 419818. 0.1564 131.69 0.6622 0.7521 0.0200 0.0176 5.791 36.498 12.402 4318.151 4.124 55.164 1.303 0.85 420998. 0.1282 136.96 0.6887 0.6914 0.0149 0.0148 4.871 30.700 9.222 3632.155 3.468 41.018 1.152 0.85 422218. 0.0977 142.23 0.7152 0.5841 0.0098 0.0120 3.944 24.856 6.073 2940.755 2.808 27.015 0.937 0.85 423475. 0.0645 147.50 0.7417 0.3879 0.0048 0.0092 3.023 19.050 2.981 2253.879 2.152 13.258 0.600 0.86 424771. 0.0289 152.76 0.7682 -0.0078 -0.0001 0.0064 2.116 13.336 -0.040 1577.827 1.507 -0.180 -0.012 0.86 426087. 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 0.1013 0.0468 20.489 117.396 75.994 15278.297 13.263 338.022 2.256 0.92 443321. 0.5495 5.83 0.0266 0.0566 0.1006 0.0474 20.720 118.722 75.435 15450.802 13.413 335.533 2.214 0.92 443630. 0.5374 11.66 0.0533 0.1110 0.0997 0.0478 20.931 119.933 74.784 15608.490 13.550 332.641 2.173 0.92 443971. 0.5251 17.48 0.0799 0.1635 0.0987 0.0483 21.114 120.982 74.031 15744.977 13.668 329.288 2.133 0.92 444347. 0.5127 23.31 0.1066 0.2139 0.0976 0.0486 21.260 121.819 73.158 15853.870 13.763 325.409 2.093 0.92 444760. 0.5002 29.14 0.1332 0.2625 0.0962 0.0488 21.361 122.395 72.154 15928.819 13.828 320.940 2.055 0.92 445211. 0.4876 34.97 0.1598 0.3092 0.0947 0.0489 21.408 122.664 71.002 15963.842 13.858 315.816 2.017 0.92 445702. 0.4750 40.79 0.1865 0.3543 0.0929 0.0489 21.394 122.585 69.689 15953.582 13.850 309.978 1.981 0.92 446234. 0.4621 46.62 0.2131 0.3978 0.0909 0.0487 21.314 122.123 68.204 15893.501 13.797 303.371 1.946 0.92 446808. 0.4491 52.45 0.2398 0.4397 0.0887 0.0484 21.161 121.249 66.534 15779.728 13.699 295.945 1.912 0.92 447425. 0.4359 58.28 0.2664 0.4801 0.0862 0.0479 20.932 119.938 64.671 15609.146 13.551 287.658 1.879 0.92 448087. 0.4223 64.10 0.2930 0.5189 0.0835 0.0471 20.624 118.171 62.607 15379.117 13.351 278.477 1.846 0.92 448792. 0.4082 69.93 0.3197 0.5561 0.0805 0.0463 20.232 115.927 60.336 15087.071 13.097 268.373 1.814 0.92 449542. 0.3937 75.76 0.3463 0.5916 0.0771 0.0452 19.755 113.194 57.853 14731.389 12.789 257.329 1.781 0.92 450337. 0.3786 81.59 0.3730 0.6253 0.0736 0.0439 19.192 109.965 55.158 14311.118 12.424 245.341 1.748 0.92 451176. 0.3628 87.41 0.3996 0.6569 0.0697 0.0424 18.538 106.221 52.247 13823.960 12.001 232.396 1.714 0.92 452059. 0.3462 93.24 0.4262 0.6865 0.0655 0.0407 17.795 101.962 49.133 13269.645 11.520 218.542 1.679 0.92 452987. 0.3289 99.07 0.4529 0.7137 0.0611 0.0388 16.965 97.207 45.835 12650.807 10.982 203.876 1.643 0.93 453958. 0.3109 104.90 0.4795 0.7383 0.0565 0.0367 16.056 91.999 42.378 11973.086 10.394 188.499 1.605 0.93 454973. 0.2920 110.72 0.5062 0.7581 0.0517 0.0345 15.104 86.541 38.780 11262.750 9.777 172.492 1.562 0.93 456032. 0.2717 116.55 0.5328 0.7727 0.0468 0.0322 14.102 80.804 35.062 10516.021 9.129 155.955 1.512 0.93 457133. 0.2502 122.38 0.5595 0.7786 0.0417 0.0299 13.093 75.022 31.241 9763.564 8.476 138.961 1.451 0.93 458276. 0.2267 128.21 0.5861 0.7704 0.0364 0.0277 12.129 69.495 27.332 9044.289 7.852 121.574 1.371 0.93 459463. 0.2002 134.04 0.6127 0.7504 0.0312 0.0254 11.131 63.777 23.369 8300.186 7.206 103.944 1.277 0.93 460692. 0.1725 139.86 0.6394 0.7143 0.0258 0.0231 10.115 57.959 19.374 7542.899 6.548 86.175 1.165 0.94 461963. 0.1433 145.69 0.6660 0.6566 0.0205 0.0208 9.097 52.123 15.375 6783.409 5.889 68.388 1.028 0.94 463277. 0.1126 151.52 0.6927 0.5693 0.0152 0.0185 8.094 46.378 11.404 6035.750 5.240 50.726 0.857 0.94 464633. 0.0809 157.35 0.7193 0.4416 0.0100 0.0163 7.122 40.810 7.497 5311.141 4.611 33.346 0.640 0.94 466032. 0.0490 163.17 0.7459 0.2592 0.0049 0.0142 6.195 35.495 3.690 4619.461 4.010 16.415 0.362 0.94 467474. 0.0194 169.00 0.7726 0.0001 0.0000 0.0121 5.303 30.387 0.001 3954.699 3.433 0.003 0.000 0.94 468963. 0.0000