20.5x14EPN (205x14EPN.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 0.0949 0.0386 0.011 0.708 0.534 8.378 0.080 2.377 28.933 0.08 37544. 0.6054 0.56 0.0288 0.0688 0.0939 0.0393 0.011 0.721 0.529 8.533 0.081 2.352 28.106 0.08 37572. 0.5850 1.12 0.0575 0.1335 0.0928 0.0400 0.012 0.734 0.522 8.687 0.083 2.324 27.276 0.08 37603. 0.5643 1.67 0.0863 0.1942 0.0916 0.0407 0.012 0.747 0.515 8.839 0.084 2.292 26.448 0.08 37638. 0.5435 2.23 0.1150 0.2509 0.0902 0.0413 0.012 0.759 0.508 8.983 0.086 2.258 25.627 0.08 37676. 0.5226 2.79 0.1438 0.3037 0.0886 0.0420 0.012 0.771 0.499 9.117 0.087 2.219 24.815 0.08 37717. 0.5016 3.35 0.1726 0.3527 0.0869 0.0425 0.012 0.781 0.489 9.238 0.088 2.176 24.016 0.08 37763. 0.4808 3.91 0.2013 0.3980 0.0850 0.0430 0.013 0.790 0.478 9.341 0.089 2.128 23.233 0.08 37812. 0.4600 4.47 0.2301 0.4399 0.0829 0.0434 0.013 0.796 0.467 9.423 0.090 2.076 22.466 0.08 37866. 0.4393 5.02 0.2588 0.4784 0.0806 0.0436 0.013 0.801 0.454 9.478 0.091 2.019 21.717 0.08 37924. 0.4188 5.58 0.2876 0.5137 0.0781 0.0437 0.013 0.803 0.440 9.504 0.091 1.956 20.987 0.08 37985. 0.3984 6.14 0.3163 0.5458 0.0754 0.0437 0.013 0.803 0.424 9.497 0.091 1.888 20.274 0.08 38052. 0.3781 6.70 0.3451 0.5750 0.0725 0.0435 0.013 0.799 0.408 9.452 0.090 1.815 19.578 0.08 38122. 0.3579 7.26 0.3739 0.6012 0.0693 0.0431 0.013 0.792 0.390 9.366 0.089 1.736 18.896 0.08 38197. 0.3379 7.82 0.4026 0.6245 0.0659 0.0425 0.012 0.781 0.371 9.236 0.088 1.651 18.227 0.08 38277. 0.3178 8.37 0.4314 0.6449 0.0623 0.0417 0.012 0.766 0.351 9.059 0.087 1.561 17.566 0.08 38361. 0.2978 8.93 0.4601 0.6622 0.0585 0.0407 0.012 0.747 0.329 8.833 0.084 1.465 16.909 0.08 38449. 0.2777 9.49 0.4889 0.6762 0.0545 0.0394 0.011 0.723 0.307 8.558 0.082 1.364 16.252 0.08 38542. 0.2576 10.05 0.5177 0.6867 0.0503 0.0379 0.011 0.696 0.283 8.236 0.079 1.259 15.586 0.08 38640. 0.2373 10.61 0.5464 0.6931 0.0459 0.0362 0.011 0.665 0.259 7.868 0.075 1.150 14.904 0.08 38741. 0.2169 11.17 0.5752 0.6948 0.0415 0.0343 0.010 0.630 0.233 7.458 0.071 1.038 14.194 0.08 38848. 0.1963 11.72 0.6039 0.6909 0.0369 0.0323 0.009 0.592 0.208 7.008 0.067 0.924 13.443 0.08 38958. 0.1754 12.28 0.6327 0.6802 0.0323 0.0300 0.009 0.551 0.182 6.519 0.062 0.808 12.633 0.08 39073. 0.1541 12.84 0.6615 0.6609 0.0276 0.0276 0.008 0.507 0.155 5.995 0.057 0.690 11.740 0.08 39192. 0.1324 13.40 0.6902 0.6301 0.0229 0.0250 0.007 0.460 0.129 5.439 0.052 0.572 10.727 0.08 39316. 0.1101 13.96 0.7190 0.5838 0.0181 0.0223 0.007 0.410 0.102 4.853 0.046 0.454 9.541 0.08 39444. 0.0873 14.52 0.7477 0.5151 0.0135 0.0195 0.006 0.359 0.076 4.242 0.041 0.337 8.095 0.08 39577. 0.0638 15.07 0.7765 0.4124 0.0088 0.0166 0.005 0.305 0.050 3.610 0.034 0.221 6.240 0.08 39713. 0.0398 15.63 0.8053 0.2533 0.0043 0.0136 0.004 0.250 0.024 2.962 0.028 0.107 3.697 0.08 39854. 0.0164 16.19 0.8340 -0.0095 -0.0001 0.0106 0.003 0.195 -0.001 2.304 0.022 -0.003 -0.134 0.08 39999. 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 0.0953 0.0360 0.084 2.642 2.145 62.525 0.299 9.542 15.563 0.16 75087. 0.6524 1.12 0.0289 0.0741 0.0943 0.0367 0.086 2.698 2.123 63.834 0.305 9.443 15.085 0.16 75143. 0.6291 2.24 0.0577 0.1435 0.0932 0.0375 0.087 2.753 2.098 65.142 0.311 9.331 14.607 0.16 75206. 0.6056 3.36 0.0866 0.2082 0.0919 0.0382 0.089 2.807 2.070 66.425 0.317 9.207 14.134 0.16 75275. 0.5820 4.48 0.1154 0.2685 0.0906 0.0389 0.091 2.859 2.039 67.660 0.323 9.068 13.666 0.16 75352. 0.5585 5.60 0.1443 0.3243 0.0890 0.0396 0.092 2.908 2.004 68.818 0.329 8.913 13.207 0.16 75435. 0.5351 6.72 0.1731 0.3759 0.0873 0.0402 0.094 2.953 1.965 69.868 0.334 8.741 12.758 0.16 75527. 0.5119 7.84 0.2020 0.4235 0.0854 0.0407 0.095 2.991 1.922 70.778 0.338 8.551 12.320 0.16 75626. 0.4889 8.96 0.2308 0.4673 0.0833 0.0411 0.096 3.022 1.875 71.515 0.341 8.342 11.894 0.16 75734. 0.4662 10.08 0.2597 0.5075 0.0810 0.0415 0.097 3.045 1.824 72.044 0.344 8.112 11.482 0.16 75850. 0.4438 11.20 0.2885 0.5443 0.0785 0.0416 0.097 3.057 1.767 72.331 0.345 7.861 11.082 0.16 75974. 0.4217 12.32 0.3174 0.5778 0.0758 0.0416 0.097 3.057 1.706 72.344 0.345 7.587 10.695 0.16 76108. 0.3998 13.44 0.3462 0.6082 0.0728 0.0415 0.097 3.045 1.639 72.050 0.344 7.292 10.320 0.16 76250. 0.3782 14.56 0.3751 0.6357 0.0696 0.0411 0.096 3.018 1.568 71.420 0.341 6.974 9.957 0.16 76401. 0.3568 15.68 0.4040 0.6603 0.0662 0.0405 0.094 2.976 1.491 70.425 0.336 6.632 9.603 0.16 76561. 0.3356 16.80 0.4328 0.6820 0.0626 0.0397 0.093 2.918 1.409 69.037 0.330 6.268 9.258 0.16 76730. 0.3146 17.92 0.4617 0.7009 0.0587 0.0387 0.090 2.842 1.322 67.241 0.321 5.882 8.920 0.16 76908. 0.2936 19.04 0.4905 0.7168 0.0547 0.0374 0.087 2.749 1.231 65.037 0.311 5.476 8.585 0.16 77095. 0.2727 20.17 0.5194 0.7295 0.0505 0.0359 0.084 2.639 1.136 62.436 0.298 5.052 8.252 0.16 77291. 0.2517 21.29 0.5482 0.7385 0.0461 0.0342 0.080 2.513 1.037 59.453 0.284 4.614 7.914 0.17 77496. 0.2307 22.41 0.5771 0.7434 0.0416 0.0323 0.075 2.371 0.936 56.106 0.268 4.164 7.569 0.17 77709. 0.2096 23.53 0.6059 0.7434 0.0370 0.0302 0.070 2.215 0.833 52.412 0.250 3.705 7.208 0.17 77932. 0.1883 24.65 0.6348 0.7373 0.0323 0.0278 0.065 2.045 0.728 48.391 0.231 3.238 6.824 0.17 78163. 0.1666 25.77 0.6636 0.7233 0.0276 0.0254 0.059 1.862 0.622 44.065 0.210 2.767 6.403 0.17 78403. 0.1445 26.89 0.6925 0.6987 0.0229 0.0227 0.053 1.668 0.516 39.457 0.188 2.294 5.927 0.17 78652. 0.1218 28.01 0.7214 0.6590 0.0182 0.0199 0.046 1.462 0.409 34.597 0.165 1.821 5.367 0.17 78910. 0.0983 29.13 0.7502 0.5963 0.0135 0.0170 0.040 1.247 0.304 29.517 0.141 1.352 4.670 0.17 79176. 0.0737 30.25 0.7791 0.4957 0.0089 0.0140 0.033 1.025 0.200 24.257 0.116 0.889 3.738 0.17 79452. 0.0478 31.37 0.8079 0.3246 0.0044 0.0109 0.025 0.797 0.098 18.861 0.090 0.437 2.361 0.17 79735. 0.0212 32.49 0.8368 -0.0031 0.0000 0.0077 0.018 0.565 -0.001 13.375 0.064 -0.003 -0.022 0.17 80026. 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 0.0957 0.0350 0.275 5.777 4.846 205.035 0.653 21.553 10.719 0.24 112627. 0.6754 1.68 0.0289 0.0765 0.0947 0.0357 0.281 5.905 4.796 209.573 0.667 21.332 10.379 0.24 112712. 0.6506 3.36 0.0578 0.1481 0.0936 0.0365 0.287 6.033 4.740 214.116 0.682 21.084 10.041 0.24 112807. 0.6257 5.05 0.0867 0.2147 0.0923 0.0373 0.293 6.158 4.678 218.585 0.696 20.806 9.706 0.24 112911. 0.6008 6.73 0.1155 0.2766 0.0910 0.0380 0.299 6.280 4.608 222.895 0.709 20.495 9.376 0.24 113026. 0.5761 8.41 0.1444 0.3338 0.0894 0.0387 0.304 6.394 4.530 226.948 0.722 20.149 9.053 0.24 113151. 0.5515 10.09 0.1733 0.3867 0.0877 0.0393 0.309 6.498 4.443 230.642 0.734 19.764 8.738 0.24 113289. 0.5272 11.78 0.2022 0.4353 0.0858 0.0399 0.314 6.589 4.347 233.864 0.744 19.337 8.432 0.24 113438. 0.5032 13.46 0.2311 0.4799 0.0837 0.0403 0.317 6.663 4.242 236.498 0.753 18.866 8.135 0.24 113600. 0.4795 15.14 0.2600 0.5209 0.0814 0.0406 0.320 6.717 4.125 238.424 0.759 18.349 7.848 0.24 113775. 0.4562 16.82 0.2889 0.5583 0.0789 0.0408 0.321 6.748 3.998 239.526 0.762 17.783 7.571 0.24 113962. 0.4333 18.50 0.3177 0.5925 0.0762 0.0409 0.321 6.753 3.859 239.687 0.763 17.167 7.303 0.25 114162. 0.4107 20.19 0.3466 0.6236 0.0732 0.0407 0.320 6.728 3.709 238.797 0.760 16.500 7.046 0.25 114376. 0.3884 21.87 0.3755 0.6517 0.0700 0.0404 0.317 6.670 3.548 236.751 0.754 15.781 6.797 0.25 114603. 0.3664 23.55 0.4044 0.6769 0.0666 0.0398 0.313 6.577 3.374 233.449 0.743 15.009 6.556 0.25 114844. 0.3447 25.23 0.4333 0.6994 0.0630 0.0390 0.307 6.446 3.189 228.795 0.728 14.186 6.322 0.25 115098. 0.3232 26.92 0.4622 0.7192 0.0591 0.0380 0.299 6.275 2.993 222.732 0.709 13.312 6.095 0.25 115366. 0.3018 28.60 0.4911 0.7361 0.0550 0.0367 0.289 6.065 2.786 215.256 0.685 12.393 5.871 0.25 115647. 0.2805 30.28 0.5199 0.7499 0.0508 0.0352 0.277 5.815 2.571 206.402 0.657 11.435 5.649 0.25 115941. 0.2593 31.96 0.5488 0.7605 0.0464 0.0335 0.263 5.528 2.348 196.220 0.625 10.443 5.427 0.25 116249. 0.2380 33.65 0.5777 0.7672 0.0418 0.0315 0.248 5.206 2.119 184.766 0.588 9.425 5.202 0.25 116571. 0.2167 35.33 0.6066 0.7694 0.0372 0.0293 0.231 4.849 1.885 172.102 0.548 8.385 4.968 0.25 116905. 0.1952 37.01 0.6355 0.7660 0.0325 0.0270 0.212 4.460 1.648 158.293 0.504 7.329 4.721 0.25 117253. 0.1735 38.69 0.6644 0.7554 0.0278 0.0244 0.192 4.041 1.408 143.414 0.456 6.263 4.453 0.25 117614. 0.1512 40.37 0.6933 0.7348 0.0230 0.0217 0.171 3.594 1.167 127.548 0.406 5.192 4.151 0.25 117988. 0.1284 42.06 0.7221 0.6998 0.0183 0.0189 0.149 3.122 0.927 110.795 0.353 4.124 3.795 0.25 118376. 0.1046 43.74 0.7510 0.6422 0.0136 0.0159 0.125 2.628 0.689 93.272 0.297 3.064 3.349 0.25 118776. 0.0796 45.42 0.7799 0.5458 0.0090 0.0128 0.101 2.116 0.454 75.115 0.239 2.019 2.741 0.25 119190. 0.0529 47.10 0.8088 0.3719 0.0044 0.0096 0.076 1.591 0.224 56.483 0.180 0.998 1.801 0.25 119616. 0.0244 48.79 0.8377 0.0036 0.0000 0.0064 0.050 1.058 0.001 37.535 0.119 0.006 0.017 0.25 120053. 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 0.0961 0.0345 0.643 10.132 8.655 479.511 1.145 38.500 8.187 0.33 150165. 0.6894 2.25 0.0289 0.0780 0.0952 0.0353 0.658 10.365 8.568 490.505 1.171 38.112 7.923 0.33 150278. 0.6638 4.49 0.0578 0.1508 0.0941 0.0361 0.673 10.598 8.471 501.530 1.197 37.677 7.661 0.33 150404. 0.6382 6.74 0.0868 0.2186 0.0928 0.0369 0.687 10.827 8.361 512.392 1.223 37.189 7.401 0.33 150543. 0.6125 8.98 0.1157 0.2814 0.0915 0.0376 0.701 11.049 8.238 522.885 1.248 36.642 7.146 0.33 150697. 0.5870 11.23 0.1446 0.3394 0.0900 0.0383 0.714 11.258 8.100 532.778 1.272 36.031 6.896 0.33 150865. 0.5618 13.47 0.1735 0.3930 0.0883 0.0390 0.727 11.449 7.947 541.815 1.293 35.350 6.653 0.33 151049. 0.5368 15.72 0.2024 0.4422 0.0864 0.0395 0.737 11.616 7.777 549.726 1.312 34.594 6.417 0.33 151248. 0.5122 17.96 0.2313 0.4874 0.0843 0.0400 0.746 11.753 7.589 556.228 1.328 33.758 6.189 0.33 151465. 0.4880 20.21 0.2603 0.5288 0.0820 0.0403 0.752 11.855 7.383 561.032 1.339 32.838 5.968 0.33 151698. 0.4642 22.46 0.2892 0.5667 0.0795 0.0406 0.756 11.915 7.156 563.851 1.346 31.830 5.756 0.33 151949. 0.4408 24.70 0.3181 0.6012 0.0767 0.0406 0.757 11.926 6.909 564.404 1.347 30.731 5.552 0.33 152217. 0.4177 26.95 0.3470 0.6327 0.0737 0.0404 0.754 11.884 6.641 562.420 1.343 29.540 5.356 0.33 152503. 0.3951 29.19 0.3759 0.6612 0.0705 0.0401 0.748 11.783 6.352 557.645 1.331 28.256 5.167 0.33 152806. 0.3727 31.44 0.4049 0.6870 0.0671 0.0395 0.737 11.618 6.042 549.832 1.313 26.876 4.984 0.33 153128. 0.3507 33.68 0.4338 0.7100 0.0634 0.0387 0.722 11.384 5.711 538.753 1.286 25.402 4.808 0.33 153468. 0.3289 35.93 0.4627 0.7303 0.0595 0.0377 0.703 11.078 5.359 524.261 1.252 23.837 4.636 0.33 153826. 0.3072 38.17 0.4916 0.7479 0.0554 0.0364 0.679 10.699 4.989 506.344 1.209 22.190 4.469 0.33 154202. 0.2857 40.42 0.5205 0.7626 0.0511 0.0349 0.651 10.250 4.603 485.079 1.158 20.473 4.304 0.33 154595. 0.2643 42.67 0.5494 0.7742 0.0467 0.0331 0.618 9.732 4.203 460.584 1.100 18.695 4.139 0.33 155007. 0.2429 44.91 0.5784 0.7822 0.0421 0.0311 0.581 9.149 3.792 432.994 1.034 16.869 3.973 0.33 155437. 0.2214 47.16 0.6073 0.7859 0.0375 0.0289 0.540 8.504 3.373 402.454 0.961 15.004 3.802 0.33 155884. 0.1998 49.40 0.6362 0.7844 0.0327 0.0265 0.495 7.800 2.947 369.124 0.881 13.110 3.622 0.33 156349. 0.1780 51.65 0.6651 0.7760 0.0280 0.0240 0.447 7.040 2.517 333.180 0.795 11.198 3.427 0.33 156831. 0.1556 53.89 0.6940 0.7581 0.0232 0.0212 0.395 6.230 2.086 294.831 0.704 9.278 3.209 0.33 157331. 0.1326 56.14 0.7230 0.7264 0.0184 0.0183 0.341 5.374 1.655 254.318 0.607 7.362 2.952 0.33 157849. 0.1087 58.38 0.7519 0.6726 0.0136 0.0152 0.284 4.478 1.228 211.927 0.506 5.461 2.628 0.33 158384. 0.0833 60.63 0.7808 0.5791 0.0090 0.0121 0.225 3.550 0.807 167.996 0.401 3.589 2.179 0.34 158937. 0.0560 62.88 0.8097 0.4024 0.0044 0.0088 0.165 2.597 0.396 122.916 0.293 1.760 1.460 0.34 159506. 0.0263 65.12 0.8386 -0.0058 0.0000 0.0055 0.103 1.628 -0.003 77.064 0.184 -0.015 -0.020 0.34 160089. 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 0.0967 0.0343 1.250 15.756 13.604 932.081 1.780 60.512 6.620 0.41 187698. 0.6989 2.81 0.0289 0.0788 0.0957 0.0351 1.279 16.127 13.471 953.994 1.822 59.921 6.405 0.41 187839. 0.6729 5.61 0.0578 0.1523 0.0947 0.0359 1.309 16.499 13.322 975.996 1.864 59.255 6.191 0.41 187997. 0.6468 8.42 0.0867 0.2207 0.0935 0.0367 1.338 16.866 13.153 997.709 1.905 58.505 5.980 0.41 188171. 0.6207 11.22 0.1156 0.2840 0.0921 0.0375 1.366 17.221 12.964 1018.725 1.946 57.663 5.772 0.41 188363. 0.5948 14.03 0.1446 0.3426 0.0906 0.0382 1.393 17.557 12.752 1038.575 1.984 56.720 5.569 0.41 188573. 0.5692 16.84 0.1735 0.3965 0.0889 0.0389 1.417 17.864 12.515 1056.753 2.018 55.666 5.372 0.41 188803. 0.5439 19.64 0.2024 0.4461 0.0871 0.0395 1.439 18.134 12.251 1072.719 2.049 54.493 5.180 0.41 189053. 0.5190 22.45 0.2313 0.4916 0.0850 0.0400 1.456 18.357 11.959 1085.903 2.074 53.193 4.995 0.41 189324. 0.4944 25.26 0.2602 0.5333 0.0827 0.0403 1.469 18.523 11.637 1095.731 2.093 51.760 4.817 0.41 189616. 0.4703 28.06 0.2891 0.5715 0.0802 0.0406 1.477 18.622 11.283 1101.625 2.104 50.186 4.645 0.41 189929. 0.4466 30.87 0.3180 0.6064 0.0774 0.0406 1.479 18.646 10.897 1103.024 2.107 48.469 4.481 0.41 190265. 0.4234 33.67 0.3469 0.6381 0.0745 0.0405 1.474 18.585 10.477 1099.387 2.100 46.603 4.323 0.41 190622. 0.4005 36.48 0.3758 0.6670 0.0712 0.0401 1.462 18.429 10.024 1090.204 2.082 44.589 4.171 0.41 191002. 0.3780 39.29 0.4048 0.6931 0.0678 0.0396 1.442 18.172 9.538 1074.984 2.053 42.423 4.024 0.41 191405. 0.3557 42.09 0.4337 0.7165 0.0641 0.0388 1.412 17.805 9.017 1053.270 2.012 40.107 3.883 0.41 191830. 0.3337 44.90 0.4626 0.7374 0.0601 0.0377 1.374 17.323 8.463 1024.759 1.957 37.645 3.746 0.41 192277. 0.3119 47.71 0.4915 0.7556 0.0560 0.0364 1.327 16.726 7.881 989.413 1.890 35.053 3.613 0.41 192747. 0.2903 50.51 0.5204 0.7710 0.0517 0.0349 1.270 16.015 7.272 947.377 1.809 32.348 3.482 0.41 193240. 0.2687 53.32 0.5493 0.7835 0.0472 0.0331 1.205 15.195 6.642 898.881 1.717 29.546 3.352 0.41 193755. 0.2473 56.12 0.5782 0.7925 0.0426 0.0311 1.132 14.271 5.995 844.190 1.612 26.665 3.221 0.41 194292. 0.2257 58.93 0.6071 0.7975 0.0379 0.0289 1.051 13.246 5.333 783.592 1.497 23.722 3.087 0.41 194851. 0.2040 61.74 0.6360 0.7976 0.0331 0.0264 0.962 12.127 4.661 717.399 1.370 20.732 2.947 0.41 195432. 0.1821 64.54 0.6650 0.7912 0.0283 0.0238 0.866 10.920 3.982 645.968 1.234 17.713 2.796 0.42 196035. 0.1597 67.35 0.6939 0.7759 0.0235 0.0210 0.764 9.631 3.301 569.710 1.088 14.681 2.628 0.42 196660. 0.1366 70.16 0.7228 0.7473 0.0186 0.0180 0.656 8.268 2.620 489.111 0.934 11.655 2.430 0.42 197307. 0.1126 72.96 0.7517 0.6972 0.0138 0.0149 0.543 6.842 1.945 404.742 0.773 8.652 2.180 0.42 197976. 0.0870 75.77 0.7806 0.6079 0.0091 0.0117 0.425 5.364 1.280 317.284 0.606 5.695 1.830 0.42 198666. 0.0593 78.57 0.8095 0.4330 0.0045 0.0084 0.305 3.846 0.631 227.524 0.435 2.805 1.257 0.42 199378. 0.0286 81.38 0.8384 0.0001 0.0000 0.0050 0.183 2.303 0.000 136.215 0.260 0.000 0.000 0.42 200105. 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 0.0974 0.0344 2.163 22.720 19.731 1612.861 2.567 87.764 5.549 0.49 225225. 0.7055 3.37 0.0289 0.0792 0.0965 0.0352 2.215 23.266 19.546 1651.573 2.629 86.939 5.368 0.49 225394. 0.6793 6.73 0.0578 0.1532 0.0954 0.0360 2.267 23.814 19.336 1690.510 2.691 86.006 5.188 0.49 225583. 0.6529 10.10 0.0867 0.2219 0.0943 0.0368 2.319 24.357 19.099 1729.002 2.752 84.951 5.010 0.49 225793. 0.6267 13.47 0.1156 0.2855 0.0929 0.0376 2.369 24.882 18.832 1766.318 2.811 83.763 4.836 0.49 226023. 0.6006 16.84 0.1445 0.3443 0.0915 0.0384 2.416 25.380 18.531 1801.638 2.867 82.426 4.665 0.49 226276. 0.5748 20.20 0.1734 0.3985 0.0898 0.0391 2.460 25.837 18.194 1834.059 2.919 80.928 4.499 0.49 226552. 0.5493 23.57 0.2024 0.4483 0.0879 0.0397 2.498 26.239 17.818 1862.615 2.964 79.255 4.339 0.49 226852. 0.5242 26.94 0.2313 0.4941 0.0859 0.0402 2.530 26.572 17.400 1886.297 3.002 77.395 4.184 0.49 227178. 0.4995 30.30 0.2602 0.5360 0.0836 0.0406 2.553 26.823 16.938 1904.077 3.030 75.338 4.035 0.49 227528. 0.4753 33.67 0.2891 0.5744 0.0811 0.0408 2.568 26.976 16.429 1914.931 3.048 73.075 3.891 0.49 227905. 0.4514 37.04 0.3180 0.6095 0.0783 0.0409 2.572 27.017 15.872 1917.856 3.052 70.599 3.754 0.49 228308. 0.4280 40.41 0.3469 0.6415 0.0753 0.0407 2.564 26.933 15.267 1911.897 3.043 67.905 3.622 0.49 228738. 0.4050 43.77 0.3758 0.6707 0.0721 0.0404 2.543 26.711 14.611 1896.148 3.018 64.991 3.495 0.49 229195. 0.3824 47.14 0.4047 0.6971 0.0686 0.0398 2.507 26.339 13.906 1869.743 2.976 61.853 3.373 0.49 229679. 0.3600 50.51 0.4336 0.7209 0.0649 0.0390 2.457 25.806 13.150 1831.870 2.916 58.492 3.256 0.49 230189. 0.3380 53.87 0.4625 0.7422 0.0609 0.0380 2.390 25.103 12.346 1781.983 2.836 54.916 3.143 0.49 230727. 0.3161 57.24 0.4914 0.7609 0.0568 0.0367 2.307 24.230 11.499 1719.990 2.737 51.147 3.032 0.49 231292. 0.2943 60.61 0.5203 0.7770 0.0524 0.0351 2.208 23.189 10.613 1646.135 2.620 47.208 2.924 0.49 231883. 0.2727 63.98 0.5493 0.7902 0.0479 0.0333 2.093 21.987 9.695 1560.822 2.484 43.125 2.817 0.50 232501. 0.2511 67.34 0.5782 0.8002 0.0432 0.0312 1.964 20.631 8.751 1464.515 2.331 38.925 2.710 0.50 233146. 0.2295 70.71 0.6071 0.8063 0.0384 0.0289 1.821 19.126 7.786 1357.721 2.161 34.631 2.601 0.50 233818. 0.2077 74.08 0.6360 0.8077 0.0336 0.0264 1.664 17.482 6.805 1240.995 1.975 30.268 2.487 0.50 234515. 0.1857 77.44 0.6649 0.8030 0.0287 0.0238 1.495 15.707 5.814 1114.966 1.775 25.859 2.365 0.50 235239. 0.1632 80.81 0.6938 0.7897 0.0238 0.0209 1.315 13.810 4.818 980.363 1.560 21.430 2.229 0.50 235989. 0.1400 84.18 0.7227 0.7637 0.0189 0.0179 1.124 11.806 3.824 838.048 1.334 17.007 2.069 0.50 236766. 0.1158 87.55 0.7516 0.7167 0.0140 0.0147 0.924 9.707 2.837 689.043 1.097 12.619 1.867 0.50 237568. 0.0900 90.91 0.7805 0.6307 0.0092 0.0114 0.717 7.530 1.865 534.561 0.851 8.296 1.582 0.50 238397. 0.0619 94.28 0.8094 0.4563 0.0045 0.0080 0.504 5.297 0.915 376.011 0.598 4.071 1.104 0.50 239251. 0.0302 97.65 0.8383 -0.0057 0.0000 0.0046 0.288 3.025 -0.006 214.714 0.342 -0.028 -0.013 0.50 240122. 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 0.0982 0.0346 3.457 31.125 27.086 2577.728 3.516 120.477 4.766 0.57 262744. 0.7099 3.93 0.0289 0.0794 0.0973 0.0354 3.541 31.886 26.844 2640.759 3.602 119.401 4.611 0.57 262942. 0.6837 7.85 0.0578 0.1534 0.0963 0.0363 3.626 32.653 26.569 2704.276 3.689 118.178 4.456 0.57 263162. 0.6575 11.78 0.0867 0.2222 0.0952 0.0371 3.711 33.413 26.257 2767.199 3.775 116.790 4.304 0.57 263406. 0.6312 15.70 0.1156 0.2860 0.0939 0.0380 3.793 34.151 25.903 2828.335 3.858 115.218 4.154 0.57 263675. 0.6051 19.63 0.1445 0.3449 0.0925 0.0387 3.871 34.851 25.504 2886.335 3.937 113.440 4.008 0.57 263970. 0.5793 23.56 0.1733 0.3992 0.0908 0.0394 3.942 35.496 25.054 2939.716 4.010 111.439 3.866 0.57 264292. 0.5538 27.48 0.2022 0.4491 0.0890 0.0401 4.005 36.066 24.549 2986.889 4.075 109.194 3.728 0.57 264643. 0.5287 31.41 0.2311 0.4950 0.0870 0.0406 4.058 36.540 23.986 3026.190 4.128 106.689 3.595 0.57 265023. 0.5040 35.33 0.2600 0.5371 0.0847 0.0410 4.098 36.899 23.361 3055.931 4.169 103.908 3.467 0.57 265433. 0.4797 39.26 0.2889 0.5756 0.0822 0.0413 4.123 37.123 22.671 3074.426 4.194 100.838 3.345 0.57 265873. 0.4558 43.18 0.3178 0.6109 0.0795 0.0413 4.130 37.190 21.913 3080.030 4.202 97.470 3.227 0.57 266344. 0.4324 47.11 0.3467 0.6432 0.0765 0.0412 4.119 37.083 21.087 3071.179 4.190 93.795 3.114 0.57 266846. 0.4093 51.04 0.3756 0.6726 0.0732 0.0409 4.085 36.784 20.191 3046.390 4.156 89.810 3.006 0.57 267379. 0.3866 54.96 0.4045 0.6994 0.0697 0.0403 4.029 36.275 19.225 3004.266 4.098 85.511 2.902 0.57 267944. 0.3643 58.89 0.4334 0.7235 0.0659 0.0395 3.947 35.541 18.188 2943.479 4.015 80.899 2.803 0.57 268540. 0.3421 62.81 0.4622 0.7452 0.0619 0.0384 3.839 34.571 17.083 2863.112 3.906 75.985 2.706 0.58 269168. 0.3202 66.74 0.4911 0.7645 0.0577 0.0371 3.705 33.362 15.916 2762.975 3.769 70.796 2.613 0.58 269827. 0.2984 70.67 0.5200 0.7812 0.0533 0.0355 3.545 31.919 14.696 2643.451 3.606 65.366 2.522 0.58 270517. 0.2767 74.59 0.5489 0.7951 0.0487 0.0336 3.360 30.249 13.429 2505.185 3.418 59.732 2.431 0.58 271239. 0.2550 78.52 0.5778 0.8059 0.0440 0.0315 3.150 28.363 12.125 2348.938 3.204 53.930 2.341 0.58 271991. 0.2333 82.44 0.6067 0.8131 0.0391 0.0292 2.917 26.269 10.790 2175.533 2.968 47.994 2.250 0.58 272774. 0.2115 86.37 0.6356 0.8157 0.0342 0.0266 2.663 23.979 9.433 1985.881 2.709 41.956 2.154 0.58 273588. 0.1894 90.30 0.6645 0.8126 0.0292 0.0239 2.388 21.505 8.060 1781.002 2.430 35.852 2.053 0.58 274432. 0.1668 94.22 0.6934 0.8013 0.0242 0.0210 2.095 18.862 6.681 1562.091 2.131 29.715 1.940 0.58 275307. 0.1435 98.15 0.7223 0.7777 0.0192 0.0179 1.784 16.066 5.302 1330.552 1.815 23.584 1.807 0.58 276212. 0.1191 102.07 0.7511 0.7338 0.0143 0.0146 1.459 13.138 3.934 1088.064 1.484 17.498 1.640 0.59 277147. 0.0931 106.00 0.7800 0.6514 0.0094 0.0112 1.122 10.102 2.586 836.616 1.141 11.501 1.402 0.59 278113. 0.0645 109.92 0.8089 0.4789 0.0046 0.0078 0.776 6.986 1.268 578.539 0.789 5.639 0.994 0.59 279109. 0.0320 113.85 0.8378 -0.0081 0.0000 0.0042 0.424 3.815 -0.011 315.982 0.431 -0.050 -0.016 0.59 280123. 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 0.0992 0.0350 5.219 41.115 35.730 3891.483 4.645 158.925 4.164 0.65 300254. 0.7125 4.48 0.0289 0.0792 0.0984 0.0359 5.348 42.135 35.432 3988.095 4.760 157.602 4.030 0.65 300480. 0.6866 8.96 0.0577 0.1531 0.0974 0.0367 5.479 43.168 35.092 4085.793 4.877 156.088 3.896 0.65 300731. 0.6605 13.45 0.0866 0.2218 0.0963 0.0376 5.609 44.194 34.703 4182.911 4.993 154.359 3.763 0.65 301010. 0.6345 17.93 0.1154 0.2855 0.0951 0.0385 5.736 45.194 34.259 4277.580 5.106 152.386 3.633 0.65 301317. 0.6086 22.41 0.1443 0.3444 0.0937 0.0393 5.857 46.146 33.755 4367.701 5.214 150.141 3.505 0.65 301654. 0.5829 26.89 0.1732 0.3987 0.0921 0.0400 5.969 47.025 33.183 4450.927 5.313 147.598 3.381 0.65 302022. 0.5575 31.38 0.2020 0.4486 0.0903 0.0407 6.068 47.806 32.538 4524.770 5.401 144.728 3.262 0.65 302423. 0.5325 35.86 0.2309 0.4945 0.0883 0.0412 6.151 48.459 31.814 4586.636 5.475 141.507 3.146 0.65 302857. 0.5079 40.34 0.2597 0.5367 0.0861 0.0417 6.214 48.958 31.006 4633.885 5.531 137.915 3.035 0.65 303326. 0.4837 44.82 0.2886 0.5754 0.0836 0.0419 6.254 49.275 30.110 4663.888 5.567 133.931 2.928 0.65 303829. 0.4599 49.30 0.3175 0.6109 0.0809 0.0420 6.268 49.383 29.124 4674.091 5.579 129.542 2.826 0.65 304368. 0.4365 53.79 0.3463 0.6433 0.0779 0.0419 6.252 49.256 28.043 4662.072 5.565 124.737 2.728 0.65 304942. 0.4135 58.27 0.3752 0.6730 0.0746 0.0416 6.203 48.870 26.868 4625.539 5.521 119.510 2.635 0.66 305552. 0.3909 62.75 0.4041 0.7001 0.0711 0.0410 6.118 48.203 25.598 4562.350 5.446 113.858 2.545 0.66 306198. 0.3685 67.23 0.4329 0.7246 0.0673 0.0402 5.995 47.232 24.231 4470.473 5.336 107.780 2.458 0.66 306880. 0.3464 71.71 0.4618 0.7468 0.0632 0.0391 5.831 45.943 22.772 4348.456 5.191 101.289 2.375 0.66 307598. 0.3244 76.20 0.4906 0.7665 0.0589 0.0377 5.627 44.331 21.228 4195.941 5.009 94.421 2.295 0.66 308351. 0.3026 80.68 0.5195 0.7838 0.0544 0.0361 5.382 42.404 19.609 4013.477 4.791 87.222 2.216 0.66 309140. 0.2809 85.16 0.5484 0.7985 0.0498 0.0342 5.099 40.170 17.927 3802.061 4.538 79.741 2.139 0.66 309964. 0.2592 89.64 0.5772 0.8101 0.0450 0.0320 4.778 37.643 16.193 3562.860 4.253 72.026 2.061 0.66 310824. 0.2374 94.13 0.6061 0.8183 0.0400 0.0296 4.422 34.835 14.416 3297.156 3.936 64.123 1.983 0.66 311718. 0.2155 98.61 0.6349 0.8223 0.0350 0.0270 4.032 31.763 12.607 3006.343 3.589 56.077 1.902 0.66 312647. 0.1933 103.09 0.6638 0.8206 0.0299 0.0242 3.610 28.442 10.777 2692.002 3.213 47.935 1.816 0.66 313611. 0.1706 107.57 0.6927 0.8112 0.0248 0.0212 3.159 24.892 8.935 2355.969 2.812 39.743 1.720 0.67 314610. 0.1472 112.05 0.7215 0.7901 0.0197 0.0180 2.683 21.135 7.093 2000.413 2.388 31.551 1.608 0.67 315643. 0.1226 116.54 0.7504 0.7493 0.0146 0.0146 2.183 17.200 5.264 1627.940 1.943 23.414 1.467 0.67 316711. 0.0963 121.02 0.7792 0.6706 0.0096 0.0112 1.665 13.119 3.460 1241.686 1.482 15.391 1.264 0.67 317813. 0.0673 125.50 0.8081 0.5008 0.0047 0.0076 1.134 8.932 1.696 845.368 1.009 7.546 0.910 0.67 318949. 0.0339 129.98 0.8370 -0.0091 0.0000 0.0040 0.593 4.675 -0.016 442.473 0.528 -0.069 -0.016 0.67 320105. 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 0.1003 0.0361 7.658 53.629 45.727 5710.413 6.059 203.396 3.632 0.73 337752. 0.7030 5.03 0.0288 0.0777 0.0995 0.0369 7.837 54.882 45.383 5843.836 6.201 201.863 3.522 0.73 338005. 0.6792 10.07 0.0576 0.1506 0.0987 0.0378 8.018 56.153 44.985 5979.162 6.344 200.093 3.412 0.73 338287. 0.6551 15.10 0.0865 0.2187 0.0977 0.0386 8.199 57.420 44.526 6114.112 6.487 198.053 3.303 0.73 338600. 0.6309 20.14 0.1153 0.2821 0.0965 0.0394 8.376 58.660 43.998 6246.126 6.627 195.704 3.195 0.73 338944. 0.6066 25.17 0.1441 0.3409 0.0952 0.0402 8.545 59.845 43.392 6372.289 6.761 193.006 3.089 0.73 339323. 0.5823 30.21 0.1729 0.3952 0.0937 0.0410 8.702 60.944 42.698 6489.345 6.885 189.921 2.984 0.73 339737. 0.5582 35.24 0.2017 0.4454 0.0919 0.0416 8.842 61.925 41.909 6593.768 6.996 186.410 2.883 0.73 340188. 0.5342 40.28 0.2305 0.4916 0.0900 0.0422 8.960 62.751 41.016 6681.808 7.090 182.439 2.784 0.73 340676. 0.5104 45.31 0.2594 0.5341 0.0878 0.0426 9.051 63.388 40.013 6749.607 7.162 177.976 2.689 0.73 341203. 0.4868 50.35 0.2882 0.5732 0.0853 0.0429 9.110 63.798 38.893 6793.252 7.208 172.995 2.597 0.73 341770. 0.4635 55.38 0.3170 0.6090 0.0826 0.0430 9.131 63.945 37.652 6808.854 7.224 167.475 2.508 0.74 342376. 0.4405 60.42 0.3458 0.6418 0.0796 0.0429 9.109 63.792 36.287 6792.646 7.207 161.404 2.423 0.74 343022. 0.4178 65.45 0.3746 0.6718 0.0763 0.0426 9.040 63.307 34.795 6741.006 7.152 154.770 2.341 0.74 343709. 0.3953 70.49 0.4034 0.6992 0.0728 0.0420 8.918 62.457 33.177 6650.495 7.056 147.570 2.263 0.74 344436. 0.3730 75.52 0.4323 0.7242 0.0689 0.0412 8.741 61.212 31.431 6517.858 6.916 139.803 2.187 0.74 345203. 0.3510 80.56 0.4611 0.7468 0.0648 0.0400 8.503 59.548 29.561 6340.697 6.728 131.485 2.115 0.74 346011. 0.3291 85.59 0.4899 0.7671 0.0605 0.0386 8.205 57.460 27.576 6118.355 6.492 122.659 2.044 0.74 346858. 0.3073 90.63 0.5187 0.7850 0.0559 0.0369 7.847 54.954 25.491 5851.583 6.209 113.386 1.976 0.74 347746. 0.2855 95.66 0.5475 0.8004 0.0512 0.0350 7.432 52.046 23.321 5541.857 5.880 103.730 1.909 0.74 348673. 0.2638 100.70 0.5763 0.8130 0.0462 0.0328 6.961 48.750 21.078 5190.973 5.508 93.754 1.842 0.74 349639. 0.2420 105.73 0.6052 0.8222 0.0412 0.0303 6.438 45.087 18.777 4800.943 5.094 83.518 1.774 0.75 350644. 0.2200 110.76 0.6340 0.8273 0.0360 0.0276 5.866 41.078 16.431 4374.007 4.641 73.083 1.704 0.75 351688. 0.1977 115.80 0.6628 0.8270 0.0308 0.0247 5.247 36.746 14.053 3912.759 4.152 62.508 1.629 0.75 352771. 0.1748 120.83 0.6916 0.8190 0.0256 0.0216 4.587 32.121 11.658 3420.274 3.629 51.854 1.546 0.75 353892. 0.1511 125.87 0.7204 0.7991 0.0203 0.0183 3.889 27.238 9.260 2900.299 3.077 41.187 1.448 0.75 355052. 0.1261 130.90 0.7492 0.7591 0.0151 0.0149 3.161 22.139 6.875 2357.427 2.501 30.579 1.323 0.75 356251. 0.0993 135.94 0.7781 0.6798 0.0099 0.0113 2.410 16.879 4.520 1797.248 1.907 20.106 1.141 0.75 357487. 0.0694 140.97 0.8069 0.5063 0.0049 0.0077 1.645 11.518 2.215 1226.400 1.301 9.852 0.819 0.76 358762. 0.0349 146.01 0.8357 -0.0112 -0.0001 0.0041 0.873 6.116 -0.025 651.262 0.691 -0.112 -0.018 0.76 360059. 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 0.1015 0.0397 11.578 72.977 57.110 8634.064 8.245 254.025 3.000 0.81 375236. 0.6489 5.58 0.0287 0.0716 0.1008 0.0405 11.797 74.353 56.736 8796.849 8.400 252.363 2.925 0.81 375515. 0.6307 11.16 0.0575 0.1394 0.1000 0.0412 12.016 75.734 56.300 8960.217 8.556 250.423 2.850 0.81 375827. 0.6121 16.74 0.0862 0.2036 0.0991 0.0420 12.231 77.092 55.792 9120.859 8.710 248.161 2.774 0.81 376172. 0.5932 22.32 0.1150 0.2642 0.0981 0.0427 12.438 78.395 55.199 9275.096 8.857 245.525 2.699 0.81 376553. 0.5740 27.90 0.1437 0.3211 0.0969 0.0434 12.631 79.611 54.510 9418.868 8.994 242.459 2.625 0.81 376972. 0.5547 33.48 0.1725 0.3745 0.0954 0.0439 12.804 80.700 53.711 9547.754 9.117 238.909 2.552 0.81 377431. 0.5352 39.06 0.2012 0.4246 0.0938 0.0445 12.950 81.624 52.792 9657.141 9.222 234.819 2.480 0.81 377931. 0.5157 44.64 0.2300 0.4715 0.0919 0.0448 13.065 82.345 51.740 9742.376 9.303 230.141 2.409 0.82 378472. 0.4959 50.23 0.2587 0.5152 0.0898 0.0451 13.140 82.822 50.546 9798.766 9.357 224.826 2.340 0.82 379057. 0.4761 55.81 0.2875 0.5559 0.0874 0.0452 13.171 83.016 49.199 9821.738 9.379 218.838 2.272 0.82 379686. 0.4561 61.39 0.3162 0.5936 0.0847 0.0451 13.151 82.890 47.695 9806.849 9.365 212.146 2.206 0.82 380360. 0.4360 66.97 0.3450 0.6286 0.0818 0.0449 13.075 82.408 46.027 9749.811 9.310 204.728 2.141 0.82 381077. 0.4158 72.55 0.3737 0.6609 0.0785 0.0444 12.936 81.534 44.193 9646.469 9.212 196.570 2.078 0.82 381840. 0.3954 78.13 0.4025 0.6905 0.0750 0.0437 12.730 80.235 42.191 9492.711 9.065 187.665 2.016 0.82 382647. 0.3748 83.71 0.4312 0.7175 0.0711 0.0427 12.451 78.474 40.021 9284.377 8.866 178.012 1.955 0.82 383500. 0.3540 89.29 0.4600 0.7420 0.0670 0.0415 12.093 76.221 37.686 9017.844 8.611 167.627 1.895 0.82 384396. 0.3331 94.87 0.4887 0.7639 0.0625 0.0400 11.656 73.464 35.198 8691.637 8.300 156.563 1.837 0.82 385337. 0.3119 100.45 0.5174 0.7832 0.0579 0.0382 11.141 70.220 32.575 8307.859 7.933 144.893 1.778 0.82 386322. 0.2905 106.03 0.5462 0.7995 0.0530 0.0362 10.551 66.499 29.834 7867.573 7.513 132.704 1.720 0.83 387350. 0.2689 111.61 0.5749 0.8125 0.0480 0.0339 9.888 62.322 26.995 7373.410 7.041 120.076 1.661 0.83 388422. 0.2470 117.19 0.6037 0.8217 0.0428 0.0314 9.156 57.711 24.076 6827.908 6.520 107.089 1.599 0.83 389536. 0.2246 122.77 0.6324 0.8260 0.0375 0.0287 8.360 52.692 21.093 6234.128 5.953 93.820 1.535 0.83 390694. 0.2017 128.35 0.6612 0.8237 0.0321 0.0258 7.506 47.309 18.064 5597.214 5.345 80.346 1.464 0.83 391894. 0.1781 133.93 0.6899 0.8117 0.0267 0.0227 6.602 41.614 15.006 4923.455 4.702 66.747 1.382 0.83 393136. 0.1533 139.51 0.7187 0.7848 0.0212 0.0194 5.660 35.673 11.939 4220.511 4.030 53.104 1.283 0.83 394420. 0.1269 145.10 0.7474 0.7327 0.0158 0.0161 4.690 29.560 8.882 3497.342 3.340 39.508 1.152 0.84 395747. 0.0983 150.68 0.7762 0.6350 0.0104 0.0127 3.707 23.364 5.858 2764.254 2.640 26.058 0.961 0.84 397116. 0.0666 156.26 0.8049 0.4421 0.0051 0.0094 2.726 17.181 2.892 2032.716 1.941 12.864 0.645 0.84 398526. 0.0314 161.84 0.8337 0.0018 0.0000 0.0060 1.762 11.103 0.008 1313.574 1.254 0.033 0.003 0.84 399967. 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 0.1019 0.0473 18.361 105.206 69.412 13691.786 11.886 308.744 2.299 0.89 412736. 0.5483 6.17 0.0289 0.0609 0.1014 0.0481 18.645 106.834 69.049 13903.654 12.070 307.128 2.253 0.89 413040. 0.5357 12.33 0.0577 0.1192 0.1008 0.0488 18.924 108.432 68.617 14111.607 12.251 305.210 2.205 0.89 413379. 0.5229 18.50 0.0866 0.1751 0.1000 0.0495 19.189 109.952 68.105 14309.533 12.422 302.930 2.159 0.89 413757. 0.5099 24.66 0.1155 0.2284 0.0991 0.0501 19.432 111.345 67.495 14490.712 12.580 300.217 2.113 0.90 414175. 0.4968 30.83 0.1444 0.2794 0.0980 0.0507 19.643 112.552 66.771 14647.807 12.716 296.996 2.068 0.90 414635. 0.4836 37.00 0.1732 0.3282 0.0968 0.0511 19.811 113.515 65.915 14773.196 12.825 293.189 2.024 0.90 415140. 0.4703 43.16 0.2021 0.3749 0.0953 0.0514 19.927 114.177 64.909 14859.390 12.900 288.715 1.981 0.90 415691. 0.4569 49.33 0.2310 0.4196 0.0936 0.0515 19.980 114.485 63.736 14899.354 12.934 283.498 1.940 0.90 416290. 0.4434 55.49 0.2599 0.4624 0.0916 0.0515 19.964 114.389 62.381 14886.859 12.924 277.469 1.901 0.90 416937. 0.4297 61.66 0.2887 0.5033 0.0893 0.0512 19.869 113.849 60.829 14816.646 12.863 270.566 1.862 0.90 417635. 0.4157 67.83 0.3176 0.5425 0.0867 0.0508 19.692 112.833 59.070 14684.422 12.748 262.742 1.825 0.90 418382. 0.4014 73.99 0.3465 0.5799 0.0838 0.0501 19.427 111.314 57.095 14486.716 12.576 253.960 1.788 0.90 419179. 0.3866 80.16 0.3754 0.6153 0.0806 0.0492 19.070 109.270 54.900 14220.707 12.345 244.195 1.751 0.90 420027. 0.3714 86.32 0.4042 0.6488 0.0771 0.0480 18.619 106.682 52.481 13883.964 12.053 233.436 1.714 0.90 420926. 0.3555 92.49 0.4331 0.6802 0.0732 0.0466 18.069 103.533 49.838 13474.029 11.697 221.679 1.678 0.90 421874. 0.3390 98.65 0.4620 0.7095 0.0690 0.0449 17.418 99.804 46.974 12988.763 11.276 208.942 1.640 0.90 422872. 0.3218 104.82 0.4909 0.7363 0.0645 0.0430 16.668 95.504 43.907 12429.180 10.790 195.299 1.602 0.91 423919. 0.3039 110.99 0.5197 0.7604 0.0597 0.0408 15.823 90.666 40.658 11799.537 10.243 180.849 1.563 0.91 425015. 0.2852 117.15 0.5486 0.7805 0.0547 0.0384 14.909 85.426 37.251 11117.590 9.651 165.692 1.520 0.91 426159. 0.2655 123.32 0.5775 0.7960 0.0495 0.0359 13.925 79.791 33.710 10384.226 9.015 149.941 1.472 0.91 427351. 0.2447 129.48 0.6064 0.8050 0.0441 0.0332 12.891 73.864 30.057 9612.945 8.345 133.693 1.418 0.91 428590. 0.2225 135.65 0.6352 0.8034 0.0386 0.0306 11.847 67.880 26.311 8834.146 7.669 117.032 1.351 0.91 429876. 0.1983 141.82 0.6641 0.7901 0.0330 0.0278 10.770 61.709 22.502 8030.984 6.972 100.087 1.271 0.91 431209. 0.1725 147.98 0.6930 0.7623 0.0274 0.0249 9.658 55.337 18.656 7201.727 6.252 82.982 1.175 0.92 432588. 0.1453 154.15 0.7219 0.7134 0.0217 0.0220 8.530 48.873 14.803 6360.465 5.522 65.844 1.056 0.92 434014. 0.1163 160.31 0.7507 0.6334 0.0161 0.0191 7.405 42.432 10.973 5522.237 4.794 48.809 0.901 0.92 435487. 0.0855 166.48 0.7796 0.5070 0.0106 0.0163 6.306 36.130 7.201 4702.023 4.082 32.031 0.695 0.92 437005. 0.0534 172.65 0.8085 0.3092 0.0052 0.0135 5.249 30.075 3.525 3914.048 3.398 15.681 0.409 0.92 438570. 0.0220 178.81 0.8374 -0.0027 0.0000 0.0109 4.243 24.313 -0.024 3164.225 2.747 -0.107 -0.003 0.93 440179. 0.0000