14x8.5E (14x85E.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 0.0930 0.0404 0.002 0.110 0.114 1.304 0.012 0.507 39.625 0.06 18031. 0.5605 0.34 0.0259 0.0581 0.0919 0.0409 0.002 0.112 0.112 1.320 0.013 0.500 38.639 0.06 18043. 0.5431 0.69 0.0517 0.1132 0.0906 0.0414 0.002 0.113 0.111 1.336 0.013 0.493 37.648 0.06 18057. 0.5254 1.03 0.0776 0.1654 0.0892 0.0418 0.002 0.114 0.109 1.351 0.013 0.486 36.657 0.06 18071. 0.5076 1.37 0.1035 0.2145 0.0876 0.0423 0.002 0.115 0.107 1.364 0.013 0.477 35.668 0.06 18088. 0.4896 1.72 0.1294 0.2608 0.0859 0.0426 0.002 0.116 0.105 1.376 0.013 0.468 34.685 0.06 18105. 0.4715 2.06 0.1552 0.3041 0.0841 0.0429 0.002 0.117 0.103 1.385 0.013 0.458 33.709 0.06 18124. 0.4533 2.40 0.1811 0.3447 0.0821 0.0431 0.002 0.118 0.101 1.393 0.013 0.447 32.742 0.06 18144. 0.4351 2.74 0.2070 0.3824 0.0800 0.0433 0.002 0.118 0.098 1.397 0.013 0.435 31.785 0.06 18166. 0.4168 3.09 0.2329 0.4174 0.0776 0.0433 0.002 0.118 0.095 1.398 0.013 0.423 30.838 0.06 18190. 0.3984 3.43 0.2587 0.4496 0.0751 0.0432 0.002 0.118 0.092 1.395 0.013 0.409 29.900 0.06 18215. 0.3800 3.77 0.2846 0.4792 0.0724 0.0430 0.002 0.117 0.089 1.388 0.013 0.394 28.969 0.06 18242. 0.3614 4.12 0.3105 0.5060 0.0695 0.0426 0.002 0.116 0.085 1.376 0.013 0.378 28.043 0.06 18270. 0.3428 4.46 0.3363 0.5301 0.0664 0.0421 0.002 0.115 0.081 1.360 0.013 0.362 27.116 0.06 18300. 0.3240 4.80 0.3622 0.5512 0.0631 0.0415 0.002 0.113 0.077 1.338 0.013 0.344 26.183 0.06 18332. 0.3050 5.15 0.3881 0.5693 0.0596 0.0406 0.002 0.111 0.073 1.311 0.013 0.325 25.238 0.06 18365. 0.2857 5.49 0.4140 0.5840 0.0559 0.0396 0.002 0.108 0.068 1.279 0.012 0.305 24.273 0.06 18400. 0.2662 5.83 0.4398 0.5951 0.0521 0.0385 0.002 0.105 0.064 1.242 0.012 0.284 23.279 0.06 18437. 0.2463 6.17 0.4657 0.6021 0.0481 0.0372 0.002 0.101 0.059 1.200 0.011 0.262 22.244 0.06 18476. 0.2262 6.52 0.4916 0.6044 0.0440 0.0358 0.002 0.098 0.054 1.154 0.011 0.239 21.155 0.06 18516. 0.2057 6.86 0.5175 0.6014 0.0397 0.0342 0.001 0.093 0.049 1.103 0.011 0.216 19.996 0.06 18558. 0.1848 7.20 0.5433 0.5920 0.0354 0.0325 0.001 0.089 0.043 1.049 0.010 0.193 18.748 0.06 18601. 0.1636 7.55 0.5692 0.5752 0.0310 0.0307 0.001 0.084 0.038 0.991 0.009 0.169 17.387 0.06 18646. 0.1420 7.89 0.5951 0.5493 0.0266 0.0288 0.001 0.079 0.033 0.929 0.009 0.145 15.882 0.06 18693. 0.1200 8.23 0.6209 0.5121 0.0221 0.0268 0.001 0.073 0.027 0.864 0.008 0.120 14.191 0.06 18742. 0.0978 8.58 0.6468 0.4608 0.0176 0.0247 0.001 0.067 0.022 0.796 0.008 0.096 12.257 0.06 18792. 0.0753 8.92 0.6727 0.3910 0.0131 0.0225 0.001 0.061 0.016 0.725 0.007 0.071 10.002 0.06 18844. 0.0530 9.26 0.6986 0.2968 0.0086 0.0202 0.001 0.055 0.011 0.652 0.006 0.047 7.309 0.06 18898. 0.0314 9.60 0.7244 0.1688 0.0042 0.0179 0.001 0.049 0.005 0.577 0.006 0.023 4.008 0.06 18953. 0.0120 9.95 0.7503 -0.0078 -0.0002 0.0155 0.001 0.042 0.000 0.501 0.005 -0.001 -0.178 0.06 19010. 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 0.0368 0.013 0.402 0.457 9.502 0.045 2.033 21.819 0.11 36061. 0.6183 0.69 0.0260 0.0641 0.0922 0.0374 0.013 0.408 0.451 9.646 0.046 2.008 21.223 0.11 36086. 0.5976 1.38 0.0520 0.1246 0.0909 0.0379 0.013 0.414 0.445 9.786 0.047 1.980 20.629 0.11 36113. 0.5768 2.07 0.0780 0.1816 0.0895 0.0384 0.013 0.419 0.438 9.919 0.047 1.949 20.038 0.11 36143. 0.5559 2.76 0.1040 0.2351 0.0879 0.0389 0.013 0.424 0.431 10.041 0.048 1.916 19.453 0.11 36175. 0.5350 3.45 0.1299 0.2851 0.0863 0.0393 0.014 0.429 0.422 10.150 0.048 1.879 18.876 0.11 36211. 0.5142 4.13 0.1559 0.3318 0.0844 0.0397 0.014 0.433 0.413 10.242 0.049 1.839 18.307 0.11 36249. 0.4933 4.82 0.1819 0.3753 0.0824 0.0399 0.014 0.436 0.404 10.315 0.049 1.795 17.749 0.11 36290. 0.4726 5.51 0.2079 0.4157 0.0803 0.0401 0.014 0.438 0.393 10.363 0.049 1.748 17.201 0.11 36334. 0.4519 6.20 0.2339 0.4531 0.0779 0.0402 0.014 0.439 0.381 10.384 0.050 1.697 16.664 0.11 36382. 0.4314 6.89 0.2599 0.4875 0.0754 0.0402 0.014 0.438 0.369 10.373 0.050 1.642 16.138 0.11 36432. 0.4109 7.58 0.2859 0.5191 0.0726 0.0400 0.014 0.437 0.356 10.329 0.049 1.582 15.621 0.11 36486. 0.3905 8.27 0.3119 0.5479 0.0697 0.0397 0.014 0.433 0.341 10.247 0.049 1.519 15.113 0.11 36543. 0.3701 8.96 0.3379 0.5738 0.0666 0.0392 0.014 0.428 0.326 10.125 0.048 1.451 14.610 0.11 36604. 0.3497 9.65 0.3638 0.5968 0.0633 0.0386 0.013 0.421 0.310 9.960 0.048 1.378 14.112 0.11 36668. 0.3292 10.34 0.3898 0.6169 0.0598 0.0378 0.013 0.412 0.293 9.749 0.047 1.302 13.614 0.11 36735. 0.3087 11.03 0.4158 0.6338 0.0560 0.0368 0.013 0.401 0.274 9.494 0.045 1.221 13.113 0.11 36806. 0.2879 11.71 0.4418 0.6473 0.0522 0.0356 0.012 0.389 0.256 9.195 0.044 1.136 12.604 0.11 36880. 0.2670 12.40 0.4678 0.6569 0.0482 0.0343 0.012 0.374 0.236 8.854 0.042 1.049 12.081 0.11 36958. 0.2459 13.09 0.4938 0.6622 0.0440 0.0328 0.011 0.358 0.216 8.474 0.040 0.959 11.538 0.11 37039. 0.2245 13.78 0.5198 0.6626 0.0398 0.0312 0.011 0.340 0.195 8.056 0.038 0.866 10.966 0.11 37123. 0.2028 14.47 0.5458 0.6569 0.0354 0.0294 0.010 0.321 0.174 7.602 0.036 0.772 10.355 0.11 37211. 0.1808 15.16 0.5717 0.6441 0.0310 0.0276 0.010 0.301 0.152 7.114 0.034 0.676 9.692 0.11 37302. 0.1584 15.85 0.5977 0.6223 0.0266 0.0255 0.009 0.279 0.130 6.593 0.031 0.579 8.956 0.11 37396. 0.1354 16.54 0.6237 0.5890 0.0221 0.0234 0.008 0.255 0.108 6.041 0.029 0.481 8.124 0.11 37494. 0.1120 17.23 0.6497 0.5404 0.0176 0.0212 0.007 0.231 0.086 5.462 0.026 0.383 7.155 0.11 37596. 0.0880 17.92 0.6757 0.4707 0.0131 0.0188 0.007 0.205 0.064 4.858 0.023 0.285 5.993 0.11 37701. 0.0636 18.61 0.7017 0.3706 0.0087 0.0164 0.006 0.179 0.042 4.232 0.020 0.189 4.543 0.11 37809. 0.0392 19.29 0.7277 0.2238 0.0043 0.0139 0.005 0.152 0.021 3.590 0.017 0.093 2.646 0.11 37921. 0.0161 19.98 0.7537 -0.0004 0.0000 0.0114 0.004 0.124 0.000 2.936 0.014 0.000 -0.005 0.11 38035. 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 0.0936 0.0353 0.041 0.866 1.031 30.727 0.098 4.587 15.222 0.17 54091. 0.6479 1.04 0.0260 0.0672 0.0924 0.0358 0.042 0.880 1.018 31.235 0.099 4.530 14.788 0.17 54128. 0.6255 2.07 0.0521 0.1304 0.0911 0.0364 0.043 0.894 1.004 31.729 0.101 4.467 14.356 0.17 54169. 0.6030 3.11 0.0781 0.1898 0.0897 0.0370 0.043 0.907 0.989 32.199 0.102 4.398 13.928 0.17 54214. 0.5805 4.14 0.1042 0.2454 0.0882 0.0375 0.044 0.919 0.972 32.635 0.104 4.323 13.506 0.17 54263. 0.5580 5.18 0.1302 0.2973 0.0865 0.0379 0.044 0.930 0.953 33.027 0.105 4.240 13.091 0.17 54316. 0.5357 6.22 0.1563 0.3457 0.0847 0.0383 0.045 0.940 0.933 33.362 0.106 4.150 12.684 0.17 54374. 0.5135 7.25 0.1823 0.3906 0.0827 0.0386 0.045 0.947 0.911 33.629 0.107 4.052 12.286 0.17 54436. 0.4915 8.29 0.2084 0.4323 0.0805 0.0388 0.045 0.953 0.887 33.814 0.108 3.945 11.897 0.17 54502. 0.4696 9.32 0.2344 0.4708 0.0781 0.0389 0.045 0.955 0.861 33.906 0.108 3.830 11.518 0.17 54573. 0.4479 10.36 0.2605 0.5063 0.0756 0.0389 0.045 0.955 0.833 33.891 0.108 3.705 11.147 0.17 54650. 0.4264 11.40 0.2865 0.5389 0.0729 0.0387 0.045 0.951 0.803 33.758 0.107 3.571 10.786 0.17 54731. 0.4050 12.43 0.3126 0.5686 0.0699 0.0384 0.045 0.944 0.770 33.497 0.107 3.427 10.432 0.17 54817. 0.3838 13.47 0.3386 0.5955 0.0668 0.0380 0.044 0.932 0.736 33.097 0.105 3.273 10.085 0.17 54908. 0.3626 14.50 0.3647 0.6195 0.0634 0.0374 0.044 0.917 0.699 32.547 0.104 3.110 9.742 0.17 55005. 0.3414 15.54 0.3907 0.6406 0.0599 0.0365 0.043 0.897 0.660 31.840 0.101 2.936 9.403 0.17 55106. 0.3202 16.58 0.4168 0.6587 0.0562 0.0355 0.042 0.873 0.619 30.975 0.099 2.753 9.064 0.17 55213. 0.2989 17.61 0.4428 0.6735 0.0523 0.0344 0.040 0.844 0.576 29.958 0.095 2.562 8.722 0.17 55324. 0.2775 18.65 0.4689 0.6846 0.0483 0.0330 0.039 0.811 0.532 28.795 0.092 2.365 8.374 0.17 55441. 0.2559 19.68 0.4949 0.6917 0.0441 0.0316 0.037 0.775 0.486 27.492 0.088 2.161 8.015 0.17 55563. 0.2342 20.72 0.5210 0.6940 0.0398 0.0299 0.035 0.734 0.439 26.055 0.083 1.952 7.640 0.17 55690. 0.2121 21.76 0.5470 0.6907 0.0355 0.0281 0.033 0.690 0.391 24.488 0.078 1.739 7.241 0.17 55823. 0.1898 22.79 0.5731 0.6805 0.0311 0.0262 0.031 0.642 0.342 22.798 0.073 1.523 6.810 0.17 55960. 0.1670 23.83 0.5991 0.6616 0.0266 0.0241 0.028 0.591 0.293 20.991 0.067 1.304 6.333 0.17 56102. 0.1437 24.86 0.6252 0.6312 0.0221 0.0219 0.026 0.537 0.244 19.075 0.061 1.083 5.791 0.17 56250. 0.1198 25.90 0.6512 0.5854 0.0176 0.0196 0.023 0.481 0.194 17.059 0.054 0.862 5.155 0.17 56403. 0.0951 26.94 0.6773 0.5173 0.0131 0.0172 0.020 0.421 0.144 14.954 0.048 0.642 4.381 0.17 56561. 0.0698 27.97 0.7033 0.4156 0.0087 0.0147 0.017 0.360 0.095 12.773 0.041 0.425 3.389 0.17 56724. 0.0439 29.01 0.7294 0.2589 0.0043 0.0121 0.014 0.297 0.047 10.532 0.034 0.210 2.036 0.17 56892. 0.0185 30.05 0.7554 0.0014 0.0000 0.0095 0.011 0.232 0.000 8.245 0.026 0.001 0.011 0.17 57064. 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 0.0939 0.0344 0.095 1.502 1.839 71.066 0.170 8.178 11.735 0.22 72120. 0.6669 1.38 0.0261 0.0691 0.0927 0.0350 0.097 1.528 1.816 72.303 0.173 8.077 11.391 0.22 72170. 0.6433 2.77 0.0522 0.1341 0.0914 0.0356 0.099 1.553 1.791 73.508 0.175 7.965 11.050 0.22 72225. 0.6197 4.15 0.0783 0.1949 0.0900 0.0361 0.100 1.578 1.763 74.658 0.178 7.843 10.713 0.22 72285. 0.5962 5.53 0.1044 0.2519 0.0885 0.0367 0.102 1.600 1.733 75.728 0.181 7.709 10.381 0.22 72350. 0.5728 6.92 0.1305 0.3050 0.0868 0.0371 0.103 1.621 1.700 76.692 0.183 7.562 10.055 0.22 72421. 0.5495 8.30 0.1566 0.3544 0.0850 0.0375 0.104 1.638 1.664 77.523 0.185 7.402 9.736 0.22 72498. 0.5264 9.69 0.1826 0.4002 0.0829 0.0379 0.105 1.652 1.625 78.190 0.187 7.227 9.425 0.22 72581. 0.5035 11.07 0.2087 0.4427 0.0808 0.0381 0.105 1.662 1.582 78.663 0.188 7.037 9.122 0.22 72670. 0.4809 12.45 0.2348 0.4819 0.0784 0.0382 0.106 1.667 1.536 78.910 0.188 6.831 8.828 0.22 72765. 0.4585 13.84 0.2609 0.5181 0.0759 0.0382 0.106 1.667 1.486 78.903 0.188 6.609 8.541 0.22 72867. 0.4363 15.22 0.2870 0.5513 0.0731 0.0381 0.105 1.661 1.432 78.611 0.188 6.369 8.262 0.22 72976. 0.4144 16.60 0.3131 0.5816 0.0702 0.0378 0.105 1.648 1.374 78.010 0.186 6.112 7.990 0.22 73091. 0.3926 17.99 0.3392 0.6091 0.0670 0.0373 0.103 1.629 1.313 77.073 0.184 5.838 7.724 0.22 73213. 0.3709 19.37 0.3653 0.6338 0.0637 0.0367 0.102 1.601 1.247 75.776 0.181 5.546 7.463 0.22 73342. 0.3493 20.76 0.3914 0.6556 0.0601 0.0359 0.099 1.566 1.177 74.097 0.177 5.236 7.205 0.22 73478. 0.3276 22.14 0.4175 0.6745 0.0563 0.0349 0.097 1.522 1.104 72.035 0.172 4.909 6.949 0.22 73620. 0.3060 23.52 0.4436 0.6901 0.0524 0.0337 0.093 1.471 1.027 69.604 0.166 4.568 6.692 0.22 73770. 0.2843 24.91 0.4697 0.7023 0.0484 0.0323 0.090 1.412 0.948 66.816 0.160 4.215 6.432 0.22 73926. 0.2624 26.29 0.4958 0.7106 0.0442 0.0308 0.085 1.346 0.866 63.686 0.152 3.851 6.166 0.22 74089. 0.2404 27.67 0.5218 0.7144 0.0399 0.0292 0.081 1.273 0.782 60.226 0.144 3.478 5.888 0.23 74259. 0.2182 29.06 0.5479 0.7127 0.0355 0.0273 0.076 1.193 0.696 56.448 0.135 3.097 5.595 0.23 74436. 0.1957 30.44 0.5740 0.7044 0.0311 0.0254 0.070 1.107 0.609 52.368 0.125 2.711 5.278 0.23 74620. 0.1727 31.82 0.6001 0.6876 0.0266 0.0232 0.064 1.014 0.522 48.000 0.115 2.320 4.929 0.23 74811. 0.1492 33.21 0.6262 0.6597 0.0221 0.0210 0.058 0.916 0.433 43.363 0.104 1.927 4.531 0.23 75008. 0.1250 34.59 0.6523 0.6161 0.0176 0.0186 0.052 0.813 0.345 38.480 0.092 1.533 4.063 0.23 75212. 0.1000 35.98 0.6784 0.5498 0.0131 0.0162 0.045 0.705 0.257 33.377 0.080 1.141 3.486 0.23 75424. 0.0740 37.36 0.7045 0.4476 0.0086 0.0136 0.038 0.594 0.169 28.088 0.067 0.753 2.733 0.23 75642. 0.0471 38.74 0.7306 0.2839 0.0043 0.0110 0.030 0.479 0.083 22.650 0.054 0.371 1.672 0.23 75867. 0.0202 40.13 0.7567 -0.0013 0.0000 0.0083 0.023 0.361 0.000 17.102 0.041 -0.001 -0.007 0.23 76096. 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 0.0942 0.0339 0.183 2.311 2.883 136.719 0.261 12.821 9.563 0.28 90148. 0.6805 1.73 0.0261 0.0704 0.0930 0.0345 0.187 2.353 2.847 139.186 0.266 12.664 9.278 0.28 90210. 0.6561 3.46 0.0522 0.1365 0.0917 0.0351 0.190 2.394 2.808 141.591 0.270 12.490 8.995 0.28 90279. 0.6318 5.19 0.0784 0.1985 0.0903 0.0357 0.193 2.432 2.765 143.890 0.275 12.300 8.717 0.28 90354. 0.6075 6.93 0.1045 0.2563 0.0888 0.0362 0.196 2.469 2.718 146.035 0.279 12.091 8.443 0.28 90436. 0.5834 8.66 0.1306 0.3102 0.0871 0.0367 0.198 2.501 2.667 147.973 0.283 11.862 8.174 0.28 90525. 0.5594 10.39 0.1567 0.3603 0.0853 0.0371 0.201 2.530 2.610 149.648 0.286 11.611 7.912 0.28 90621. 0.5358 12.12 0.1828 0.4068 0.0833 0.0374 0.202 2.553 2.549 151.002 0.288 11.338 7.656 0.28 90725. 0.5123 13.85 0.2089 0.4498 0.0811 0.0377 0.204 2.569 2.482 151.973 0.290 11.041 7.408 0.28 90837. 0.4892 15.58 0.2351 0.4896 0.0787 0.0378 0.205 2.578 2.410 152.500 0.291 10.718 7.167 0.28 90956. 0.4663 17.31 0.2612 0.5262 0.0762 0.0378 0.205 2.578 2.331 152.522 0.291 10.370 6.933 0.28 91084. 0.4437 19.04 0.2873 0.5598 0.0734 0.0377 0.204 2.569 2.247 151.983 0.290 9.994 6.706 0.28 91220. 0.4213 20.78 0.3134 0.5906 0.0705 0.0374 0.202 2.550 2.156 150.830 0.288 9.591 6.484 0.28 91365. 0.3991 22.51 0.3395 0.6185 0.0673 0.0369 0.200 2.519 2.060 149.013 0.285 9.161 6.269 0.28 91518. 0.3771 24.24 0.3656 0.6437 0.0639 0.0363 0.196 2.476 1.956 146.480 0.280 8.702 6.058 0.28 91679. 0.3551 25.97 0.3918 0.6661 0.0603 0.0355 0.192 2.421 1.847 143.188 0.273 8.215 5.850 0.28 91849. 0.3332 27.70 0.4179 0.6855 0.0566 0.0345 0.187 2.352 1.732 139.136 0.266 7.702 5.645 0.28 92028. 0.3113 29.43 0.4440 0.7019 0.0526 0.0333 0.180 2.271 1.611 134.346 0.257 7.167 5.440 0.28 92215. 0.2894 31.16 0.4701 0.7149 0.0486 0.0319 0.173 2.178 1.487 128.845 0.246 6.612 5.233 0.28 92411. 0.2674 32.89 0.4962 0.7242 0.0444 0.0304 0.164 2.073 1.358 122.658 0.234 6.041 5.022 0.28 92615. 0.2453 34.63 0.5223 0.7291 0.0401 0.0287 0.155 1.958 1.226 115.810 0.221 5.455 4.803 0.28 92828. 0.2229 36.36 0.5485 0.7287 0.0357 0.0269 0.145 1.831 1.092 108.325 0.207 4.857 4.572 0.28 93050. 0.2002 38.09 0.5746 0.7220 0.0312 0.0248 0.134 1.694 0.956 100.233 0.191 4.250 4.324 0.28 93280. 0.1772 39.82 0.6007 0.7071 0.0267 0.0227 0.123 1.548 0.818 91.563 0.175 3.637 4.050 0.28 93518. 0.1535 41.55 0.6268 0.6811 0.0222 0.0204 0.110 1.392 0.679 82.353 0.157 3.020 3.739 0.28 93766. 0.1291 43.28 0.6529 0.6397 0.0176 0.0180 0.097 1.228 0.540 72.648 0.139 2.402 3.371 0.28 94022. 0.1038 45.01 0.6790 0.5752 0.0131 0.0155 0.084 1.057 0.402 62.502 0.119 1.787 2.915 0.28 94286. 0.0774 46.74 0.7052 0.4735 0.0087 0.0129 0.070 0.879 0.265 51.982 0.099 1.178 2.311 0.28 94559. 0.0498 48.48 0.7313 0.3053 0.0043 0.0102 0.055 0.696 0.130 41.166 0.079 0.580 1.437 0.29 94841. 0.0217 50.21 0.7574 -0.0029 0.0000 0.0075 0.040 0.509 -0.001 30.125 0.058 -0.004 -0.013 0.29 95128. 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 0.0946 0.0336 0.314 3.298 4.167 234.103 0.373 18.536 8.074 0.33 108174. 0.6908 2.08 0.0261 0.0714 0.0934 0.0342 0.320 3.359 4.116 238.444 0.379 18.310 7.830 0.33 108250. 0.6659 4.16 0.0523 0.1383 0.0921 0.0348 0.325 3.419 4.061 242.680 0.386 18.061 7.589 0.33 108332. 0.6410 6.24 0.0784 0.2010 0.0907 0.0354 0.331 3.476 3.999 246.733 0.393 17.788 7.352 0.33 108423. 0.6162 8.31 0.1045 0.2595 0.0892 0.0359 0.336 3.529 3.932 250.520 0.399 17.488 7.118 0.33 108521. 0.5915 10.39 0.1307 0.3139 0.0875 0.0364 0.341 3.577 3.858 253.949 0.404 17.158 6.890 0.33 108628. 0.5672 12.47 0.1568 0.3645 0.0857 0.0369 0.345 3.619 3.777 256.921 0.409 16.798 6.667 0.33 108744. 0.5430 14.55 0.1829 0.4115 0.0837 0.0372 0.348 3.653 3.688 259.334 0.413 16.405 6.450 0.33 108868. 0.5192 16.63 0.2091 0.4549 0.0815 0.0375 0.350 3.678 3.592 261.079 0.416 15.976 6.240 0.33 109003. 0.4956 18.71 0.2352 0.4950 0.0791 0.0376 0.351 3.692 3.487 262.049 0.417 15.511 6.036 0.33 109146. 0.4724 20.79 0.2613 0.5320 0.0766 0.0376 0.352 3.693 3.374 262.137 0.417 15.008 5.838 0.33 109300. 0.4495 22.87 0.2875 0.5660 0.0738 0.0375 0.350 3.680 3.252 261.243 0.416 14.466 5.646 0.33 109464. 0.4268 24.94 0.3136 0.5971 0.0708 0.0372 0.348 3.652 3.121 259.274 0.413 13.884 5.460 0.33 109637. 0.4043 27.02 0.3397 0.6254 0.0676 0.0367 0.343 3.608 2.981 256.141 0.408 13.261 5.279 0.34 109821. 0.3821 29.10 0.3658 0.6510 0.0643 0.0361 0.338 3.546 2.832 251.754 0.401 12.598 5.103 0.34 110015. 0.3599 31.18 0.3920 0.6738 0.0607 0.0353 0.330 3.466 2.674 246.035 0.392 11.893 4.929 0.34 110220. 0.3378 33.26 0.4181 0.6938 0.0569 0.0343 0.320 3.367 2.507 238.979 0.380 11.151 4.758 0.34 110434. 0.3158 35.34 0.4442 0.7107 0.0529 0.0331 0.309 3.249 2.333 230.625 0.367 10.376 4.588 0.34 110659. 0.2937 37.42 0.4704 0.7245 0.0488 0.0317 0.296 3.113 2.152 221.018 0.352 9.573 4.417 0.34 110895. 0.2716 39.49 0.4965 0.7345 0.0446 0.0302 0.282 2.961 1.966 210.200 0.335 8.745 4.242 0.34 111140. 0.2493 41.57 0.5226 0.7403 0.0403 0.0284 0.266 2.792 1.775 198.216 0.315 7.896 4.062 0.34 111396. 0.2268 43.65 0.5488 0.7412 0.0359 0.0266 0.248 2.608 1.581 185.108 0.295 7.030 3.873 0.34 111662. 0.2041 45.73 0.5749 0.7358 0.0314 0.0245 0.229 2.408 1.383 170.924 0.272 6.152 3.670 0.34 111939. 0.1809 47.81 0.6010 0.7224 0.0268 0.0223 0.209 2.194 1.183 155.719 0.248 5.263 3.447 0.34 112226. 0.1571 49.89 0.6272 0.6982 0.0223 0.0200 0.187 1.966 0.982 139.559 0.222 4.369 3.193 0.34 112523. 0.1326 51.97 0.6533 0.6588 0.0177 0.0176 0.164 1.726 0.781 122.523 0.195 3.475 2.892 0.34 112830. 0.1071 54.05 0.6794 0.5962 0.0132 0.0150 0.140 1.475 0.581 104.708 0.167 2.584 2.516 0.34 113148. 0.0804 56.12 0.7056 0.4954 0.0087 0.0124 0.116 1.215 0.383 86.231 0.137 1.703 2.013 0.34 113476. 0.0522 58.20 0.7317 0.3240 0.0043 0.0096 0.090 0.947 0.188 67.233 0.107 0.837 1.270 0.34 113815. 0.0231 60.28 0.7578 -0.0044 0.0000 0.0069 0.064 0.674 -0.002 47.835 0.076 -0.008 -0.017 0.34 114159. 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 0.0950 0.0334 0.496 4.467 5.698 369.960 0.505 25.345 6.986 0.39 126199. 0.6989 2.43 0.0261 0.0720 0.0938 0.0341 0.506 4.552 5.629 376.970 0.514 25.040 6.773 0.39 126287. 0.6736 4.85 0.0523 0.1396 0.0926 0.0347 0.515 4.634 5.554 383.816 0.524 24.704 6.563 0.39 126384. 0.6483 7.28 0.0784 0.2028 0.0912 0.0353 0.524 4.714 5.471 390.374 0.533 24.333 6.356 0.39 126489. 0.6231 9.70 0.1046 0.2617 0.0897 0.0358 0.532 4.788 5.379 396.508 0.541 23.926 6.153 0.39 126604. 0.5981 12.13 0.1307 0.3166 0.0880 0.0363 0.539 4.855 5.279 402.071 0.548 23.479 5.955 0.39 126729. 0.5734 14.55 0.1568 0.3676 0.0862 0.0368 0.546 4.913 5.168 406.905 0.555 22.989 5.761 0.39 126864. 0.5489 16.98 0.1830 0.4149 0.0842 0.0371 0.551 4.961 5.048 410.843 0.560 22.454 5.573 0.39 127010. 0.5248 19.41 0.2091 0.4586 0.0820 0.0374 0.555 4.995 4.917 413.709 0.564 21.871 5.391 0.39 127167. 0.5010 21.83 0.2353 0.4991 0.0796 0.0375 0.557 5.015 4.775 415.331 0.567 21.237 5.214 0.39 127335. 0.4775 24.26 0.2614 0.5363 0.0770 0.0375 0.557 5.017 4.620 415.536 0.567 20.551 5.043 0.39 127515. 0.4543 26.68 0.2875 0.5706 0.0742 0.0374 0.555 5.001 4.454 414.161 0.565 19.811 4.878 0.39 127706. 0.4314 29.11 0.3137 0.6020 0.0713 0.0371 0.551 4.963 4.275 411.055 0.561 19.016 4.717 0.39 127909. 0.4088 31.54 0.3398 0.6306 0.0681 0.0367 0.545 4.903 4.084 406.076 0.554 18.165 4.562 0.39 128123. 0.3864 33.96 0.3659 0.6565 0.0647 0.0361 0.535 4.819 3.880 399.078 0.544 17.258 4.410 0.39 128350. 0.3640 36.39 0.3921 0.6797 0.0611 0.0352 0.523 4.708 3.663 389.932 0.532 16.294 4.261 0.39 128589. 0.3418 38.81 0.4182 0.7001 0.0573 0.0342 0.508 4.572 3.435 378.629 0.517 15.278 4.115 0.39 128840. 0.3196 41.24 0.4444 0.7176 0.0533 0.0330 0.490 4.410 3.196 365.227 0.498 14.217 3.969 0.39 129103. 0.2974 43.66 0.4705 0.7319 0.0492 0.0316 0.469 4.224 2.949 349.798 0.477 13.116 3.824 0.39 129378. 0.2752 46.09 0.4966 0.7427 0.0449 0.0300 0.446 4.014 2.694 332.410 0.453 11.982 3.676 0.39 129664. 0.2528 48.52 0.5228 0.7494 0.0405 0.0283 0.420 3.781 2.432 313.131 0.427 10.819 3.523 0.39 129963. 0.2303 50.94 0.5489 0.7512 0.0361 0.0264 0.392 3.526 2.166 292.032 0.398 9.633 3.364 0.39 130274. 0.2075 53.37 0.5751 0.7470 0.0316 0.0243 0.361 3.250 1.895 269.189 0.367 8.428 3.193 0.40 130597. 0.1842 55.79 0.6012 0.7350 0.0270 0.0221 0.328 2.955 1.621 244.691 0.334 7.211 3.005 0.40 130932. 0.1604 58.22 0.6273 0.7125 0.0224 0.0198 0.293 2.640 1.346 218.645 0.298 5.986 2.792 0.40 131279. 0.1357 60.65 0.6535 0.6749 0.0178 0.0173 0.256 2.308 1.070 191.177 0.261 4.759 2.539 0.40 131638. 0.1101 63.07 0.6796 0.6142 0.0133 0.0147 0.218 1.961 0.796 162.446 0.222 3.539 2.221 0.40 132009. 0.0830 65.50 0.7058 0.5145 0.0087 0.0120 0.178 1.602 0.524 132.644 0.181 2.331 1.792 0.40 132392. 0.0544 67.92 0.7319 0.3409 0.0043 0.0092 0.137 1.232 0.257 101.999 0.139 1.145 1.145 0.40 132787. 0.0243 70.35 0.7580 -0.0056 0.0000 0.0064 0.095 0.854 -0.003 70.704 0.096 -0.013 -0.018 0.40 133189. 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 0.0955 0.0334 0.740 5.826 7.482 551.462 0.658 33.278 6.154 0.44 144222. 0.7054 2.77 0.0261 0.0725 0.0944 0.0340 0.754 5.939 7.393 562.103 0.671 32.884 5.966 0.44 144323. 0.6798 5.55 0.0523 0.1405 0.0931 0.0346 0.768 6.049 7.295 572.505 0.683 32.448 5.780 0.44 144433. 0.6542 8.32 0.0784 0.2041 0.0917 0.0353 0.781 6.154 7.187 582.476 0.695 31.968 5.596 0.44 144554. 0.6288 11.09 0.1046 0.2634 0.0902 0.0358 0.794 6.253 7.068 591.813 0.706 31.439 5.417 0.44 144686. 0.6036 13.86 0.1307 0.3186 0.0885 0.0363 0.805 6.342 6.937 600.293 0.717 30.857 5.242 0.44 144829. 0.5786 16.64 0.1568 0.3698 0.0867 0.0368 0.815 6.420 6.794 607.676 0.725 30.219 5.071 0.44 144983. 0.5540 19.41 0.1830 0.4173 0.0847 0.0371 0.823 6.484 6.637 613.708 0.733 29.521 4.905 0.45 145150. 0.5296 22.18 0.2091 0.4613 0.0825 0.0374 0.829 6.531 6.466 618.124 0.738 28.759 4.744 0.45 145330. 0.5056 24.95 0.2353 0.5020 0.0801 0.0376 0.832 6.557 6.279 620.657 0.741 27.930 4.589 0.45 145522. 0.4819 27.73 0.2614 0.5395 0.0776 0.0376 0.833 6.562 6.077 621.049 0.741 27.032 4.438 0.45 145728. 0.4586 30.50 0.2876 0.5740 0.0748 0.0375 0.830 6.540 5.859 619.050 0.739 26.063 4.293 0.45 145946. 0.4355 33.27 0.3137 0.6057 0.0718 0.0372 0.824 6.492 5.625 614.430 0.733 25.020 4.152 0.45 146178. 0.4128 36.04 0.3398 0.6346 0.0686 0.0367 0.814 6.413 5.374 606.973 0.725 23.904 4.016 0.45 146424. 0.3902 38.82 0.3660 0.6608 0.0652 0.0361 0.800 6.302 5.106 596.459 0.712 22.713 3.883 0.45 146684. 0.3678 41.59 0.3921 0.6843 0.0615 0.0353 0.781 6.156 4.822 582.691 0.696 21.447 3.753 0.45 146957. 0.3454 44.36 0.4183 0.7051 0.0577 0.0342 0.759 5.976 4.522 565.646 0.675 20.112 3.626 0.45 147244. 0.3231 47.13 0.4444 0.7231 0.0537 0.0330 0.731 5.762 4.208 545.412 0.651 18.717 3.499 0.45 147545. 0.3009 49.91 0.4705 0.7379 0.0496 0.0316 0.700 5.516 3.882 522.095 0.623 17.269 3.373 0.45 147859. 0.2785 52.68 0.4967 0.7494 0.0453 0.0300 0.665 5.238 3.547 495.799 0.592 15.777 3.245 0.45 148187. 0.2561 55.45 0.5228 0.7568 0.0409 0.0282 0.626 4.930 3.203 466.626 0.557 14.246 3.113 0.45 148529. 0.2335 58.22 0.5490 0.7595 0.0364 0.0263 0.583 4.593 2.852 434.682 0.519 12.685 2.976 0.45 148885. 0.2106 61.00 0.5751 0.7564 0.0318 0.0242 0.537 4.227 2.495 400.083 0.478 11.099 2.829 0.45 149254. 0.1873 63.77 0.6012 0.7458 0.0272 0.0220 0.487 3.835 2.135 362.965 0.433 9.495 2.668 0.45 149637. 0.1634 66.54 0.6274 0.7248 0.0226 0.0196 0.434 3.418 1.772 323.487 0.386 7.882 2.485 0.45 150033. 0.1386 69.31 0.6535 0.6889 0.0180 0.0171 0.378 2.978 1.409 281.847 0.336 6.266 2.267 0.45 150444. 0.1128 72.09 0.6797 0.6300 0.0134 0.0144 0.320 2.518 1.047 238.284 0.284 4.658 1.994 0.45 150868. 0.0855 74.86 0.7058 0.5317 0.0088 0.0117 0.259 2.040 0.690 193.091 0.230 3.068 1.620 0.46 151306. 0.0564 77.63 0.7319 0.3564 0.0043 0.0089 0.197 1.549 0.339 146.619 0.175 1.506 1.047 0.46 151757. 0.0255 80.40 0.7581 -0.0068 -0.0001 0.0060 0.133 1.048 -0.004 99.156 0.118 -0.019 -0.019 0.46 152216. 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 0.0961 0.0334 1.055 7.385 9.526 786.353 0.834 42.373 5.495 0.50 162243. 0.7108 3.12 0.0261 0.0728 0.0949 0.0341 1.075 7.530 9.415 801.773 0.851 41.879 5.326 0.50 162356. 0.6850 6.24 0.0523 0.1411 0.0937 0.0347 1.095 7.671 9.293 816.858 0.867 41.334 5.160 0.50 162480. 0.6592 9.36 0.0784 0.2049 0.0923 0.0353 1.115 7.807 9.157 831.331 0.882 40.730 4.996 0.50 162616. 0.6336 12.48 0.1046 0.2645 0.0908 0.0359 1.133 7.935 9.007 844.897 0.896 40.065 4.836 0.50 162765. 0.6082 15.59 0.1307 0.3199 0.0892 0.0364 1.150 8.051 8.843 857.234 0.910 39.333 4.679 0.50 162926. 0.5831 18.71 0.1568 0.3713 0.0873 0.0369 1.164 8.152 8.662 867.995 0.921 38.528 4.526 0.50 163100. 0.5583 21.83 0.1830 0.4190 0.0853 0.0373 1.176 8.234 8.464 876.809 0.930 37.646 4.378 0.50 163288. 0.5338 24.95 0.2091 0.4632 0.0832 0.0375 1.185 8.295 8.247 883.293 0.937 36.682 4.235 0.50 163490. 0.5097 28.07 0.2352 0.5040 0.0808 0.0377 1.190 8.331 8.011 887.062 0.941 35.633 4.096 0.50 163707. 0.4859 31.19 0.2614 0.5417 0.0782 0.0377 1.190 8.337 7.755 887.736 0.942 34.494 3.962 0.50 163938. 0.4625 34.31 0.2875 0.5765 0.0754 0.0376 1.187 8.311 7.478 884.953 0.939 33.263 3.833 0.50 164185. 0.4393 37.43 0.3137 0.6083 0.0724 0.0373 1.178 8.249 7.181 878.381 0.932 31.939 3.708 0.50 164446. 0.4164 40.54 0.3398 0.6375 0.0692 0.0369 1.164 8.149 6.861 867.706 0.921 30.520 3.587 0.50 164723. 0.3938 43.66 0.3659 0.6640 0.0658 0.0362 1.143 8.007 6.521 852.611 0.905 29.004 3.469 0.50 165016. 0.3713 46.78 0.3921 0.6878 0.0621 0.0354 1.117 7.821 6.158 832.808 0.884 27.392 3.354 0.50 165323. 0.3488 49.90 0.4182 0.7090 0.0582 0.0344 1.084 7.591 5.776 808.254 0.858 25.690 3.241 0.50 165646. 0.3265 53.02 0.4443 0.7274 0.0542 0.0331 1.045 7.317 5.376 779.073 0.827 23.911 3.130 0.50 165985. 0.3041 56.14 0.4705 0.7428 0.0500 0.0317 1.000 7.001 4.960 745.418 0.791 22.064 3.018 0.51 166339. 0.2817 59.26 0.4966 0.7549 0.0457 0.0301 0.949 6.644 4.532 707.438 0.751 20.159 2.906 0.51 166708. 0.2593 62.38 0.5228 0.7630 0.0413 0.0283 0.892 6.248 4.093 665.283 0.706 18.205 2.790 0.51 167093. 0.2366 65.49 0.5489 0.7666 0.0368 0.0263 0.830 5.814 3.644 619.103 0.657 16.211 2.670 0.51 167493. 0.2136 68.61 0.5750 0.7645 0.0322 0.0242 0.763 5.344 3.189 569.069 0.604 14.185 2.542 0.51 167909. 0.1902 71.73 0.6012 0.7551 0.0275 0.0219 0.691 4.840 2.728 515.376 0.547 12.136 2.401 0.51 168340. 0.1662 74.85 0.6273 0.7356 0.0228 0.0195 0.615 4.304 2.265 458.257 0.486 10.074 2.242 0.51 168786. 0.1414 77.97 0.6535 0.7014 0.0182 0.0169 0.534 3.738 1.801 397.996 0.422 8.009 2.052 0.51 169248. 0.1154 81.09 0.6796 0.6443 0.0135 0.0142 0.449 3.146 1.338 334.944 0.355 5.953 1.812 0.51 169725. 0.0879 84.21 0.7057 0.5474 0.0089 0.0115 0.361 2.531 0.881 269.529 0.286 3.919 1.483 0.51 170218. 0.0583 87.33 0.7319 0.3711 0.0044 0.0086 0.271 1.900 0.432 202.262 0.215 1.923 0.969 0.51 170725. 0.0267 90.44 0.7580 -0.0082 -0.0001 0.0057 0.179 1.254 -0.006 133.553 0.142 -0.027 -0.021 0.51 171241. 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 0.0967 0.0336 1.452 9.155 11.841 1083.112 1.034 52.670 4.959 0.56 180260. 0.7152 3.46 0.0261 0.0730 0.0956 0.0342 1.481 9.337 11.707 1104.671 1.055 52.071 4.807 0.56 180386. 0.6893 6.93 0.0523 0.1414 0.0944 0.0349 1.510 9.515 11.557 1125.781 1.075 51.406 4.656 0.56 180524. 0.6634 10.39 0.0784 0.2054 0.0930 0.0355 1.537 9.687 11.391 1146.049 1.094 50.669 4.508 0.56 180676. 0.6377 13.86 0.1045 0.2651 0.0916 0.0361 1.562 9.847 11.208 1165.068 1.113 49.855 4.363 0.56 180841. 0.6123 17.32 0.1307 0.3206 0.0899 0.0366 1.586 9.994 11.006 1182.387 1.129 48.956 4.222 0.56 181020. 0.5871 20.79 0.1568 0.3722 0.0881 0.0371 1.606 10.122 10.784 1197.517 1.144 47.967 4.085 0.56 181214. 0.5622 24.25 0.1829 0.4201 0.0861 0.0375 1.623 10.227 10.540 1209.944 1.155 46.882 3.951 0.56 181423. 0.5376 27.71 0.2090 0.4644 0.0839 0.0378 1.635 10.304 10.273 1219.128 1.164 45.694 3.822 0.56 181648. 0.5134 31.18 0.2352 0.5054 0.0815 0.0379 1.642 10.350 9.982 1224.531 1.169 44.398 3.697 0.56 181889. 0.4896 34.64 0.2613 0.5432 0.0789 0.0380 1.644 10.359 9.665 1225.618 1.170 42.990 3.577 0.56 182147. 0.4660 38.11 0.2874 0.5781 0.0761 0.0379 1.639 10.328 9.322 1221.885 1.167 41.466 3.461 0.56 182421. 0.4428 41.57 0.3136 0.6102 0.0731 0.0376 1.626 10.251 8.953 1212.861 1.158 39.824 3.348 0.56 182712. 0.4199 45.04 0.3397 0.6396 0.0699 0.0371 1.607 10.127 8.557 1198.112 1.144 38.063 3.240 0.56 183020. 0.3972 48.50 0.3658 0.6664 0.0664 0.0365 1.579 9.950 8.134 1177.198 1.124 36.180 3.134 0.56 183345. 0.3746 51.97 0.3920 0.6905 0.0628 0.0356 1.542 9.718 7.683 1149.713 1.098 34.176 3.031 0.56 183687. 0.3521 55.43 0.4181 0.7121 0.0589 0.0346 1.496 9.429 7.208 1115.581 1.065 32.059 2.930 0.56 184047. 0.3297 58.89 0.4442 0.7309 0.0548 0.0333 1.442 9.086 6.709 1074.973 1.027 29.844 2.831 0.56 184423. 0.3073 62.36 0.4704 0.7468 0.0506 0.0319 1.379 8.690 6.192 1028.101 0.982 27.543 2.732 0.56 184817. 0.2849 65.82 0.4965 0.7594 0.0462 0.0302 1.308 8.242 5.658 975.176 0.931 25.168 2.632 0.56 185227. 0.2624 69.29 0.5226 0.7683 0.0417 0.0284 1.229 7.746 5.111 916.406 0.875 22.732 2.529 0.56 185655. 0.2397 72.75 0.5488 0.7727 0.0372 0.0264 1.143 7.201 4.551 852.002 0.814 20.244 2.423 0.56 186100. 0.2166 76.22 0.5749 0.7716 0.0325 0.0242 1.049 6.611 3.983 782.202 0.747 17.715 2.309 0.56 186562. 0.1932 79.68 0.6010 0.7634 0.0278 0.0219 0.948 5.978 3.408 707.279 0.675 15.157 2.185 0.57 187040. 0.1691 83.14 0.6271 0.7452 0.0231 0.0194 0.842 5.304 2.829 627.560 0.599 12.582 2.044 0.57 187536. 0.1441 86.61 0.6533 0.7127 0.0184 0.0168 0.729 4.593 2.249 543.444 0.519 10.003 1.877 0.57 188049. 0.1180 90.07 0.6794 0.6574 0.0137 0.0141 0.611 3.849 1.672 455.422 0.435 7.435 1.665 0.57 188579. 0.0902 93.54 0.7055 0.5621 0.0090 0.0113 0.488 3.077 1.100 364.094 0.348 4.894 1.371 0.57 189127. 0.0603 97.00 0.7317 0.3851 0.0044 0.0084 0.362 2.284 0.539 270.183 0.258 2.399 0.906 0.57 189690. 0.0279 100.47 0.7578 -0.0095 -0.0001 0.0054 0.234 1.473 -0.008 174.254 0.166 -0.037 -0.022 0.57 190263. 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 0.0975 0.0338 1.946 11.151 14.439 1451.217 1.260 64.224 4.513 0.61 198274. 0.7187 3.81 0.0261 0.0730 0.0964 0.0345 1.985 11.376 14.279 1480.521 1.285 63.512 4.374 0.61 198413. 0.6928 7.62 0.0522 0.1415 0.0952 0.0351 2.024 11.597 14.101 1509.241 1.310 62.720 4.238 0.61 198565. 0.6669 11.43 0.0784 0.2056 0.0939 0.0358 2.061 11.809 13.903 1536.845 1.334 61.841 4.103 0.61 198732. 0.6412 15.24 0.1045 0.2653 0.0924 0.0364 2.096 12.008 13.684 1562.777 1.357 60.867 3.972 0.61 198913. 0.6158 19.05 0.1306 0.3209 0.0907 0.0369 2.127 12.190 13.442 1586.421 1.377 59.790 3.843 0.61 199111. 0.5905 22.85 0.1567 0.3725 0.0889 0.0374 2.155 12.349 13.175 1607.114 1.395 58.601 3.718 0.61 199324. 0.5656 26.66 0.1828 0.4205 0.0870 0.0378 2.178 12.480 12.881 1624.156 1.410 57.293 3.597 0.61 199555. 0.5411 30.47 0.2090 0.4649 0.0848 0.0381 2.195 12.577 12.558 1636.812 1.421 55.859 3.480 0.61 199803. 0.5169 34.28 0.2351 0.5060 0.0824 0.0383 2.205 12.635 12.206 1644.346 1.427 54.291 3.367 0.61 200068. 0.4930 38.09 0.2612 0.5440 0.0798 0.0383 2.207 12.648 11.822 1646.030 1.429 52.585 3.258 0.61 200352. 0.4695 41.90 0.2873 0.5791 0.0770 0.0382 2.201 12.611 11.406 1641.175 1.425 50.736 3.152 0.61 200654. 0.4462 45.71 0.3134 0.6113 0.0740 0.0379 2.185 12.518 10.958 1629.140 1.414 48.741 3.051 0.61 200975. 0.4233 49.52 0.3396 0.6410 0.0707 0.0375 2.158 12.366 10.476 1609.336 1.397 46.598 2.953 0.61 201314. 0.4005 53.33 0.3657 0.6680 0.0672 0.0368 2.120 12.150 9.961 1581.176 1.373 44.305 2.857 0.61 201672. 0.3780 57.14 0.3918 0.6925 0.0635 0.0359 2.071 11.865 9.411 1544.098 1.340 41.862 2.765 0.62 202049. 0.3555 60.95 0.4179 0.7144 0.0596 0.0349 2.009 11.510 8.831 1497.983 1.300 39.278 2.674 0.62 202444. 0.3330 64.75 0.4440 0.7336 0.0555 0.0336 1.935 11.088 8.222 1443.054 1.253 36.572 2.584 0.62 202859. 0.3106 68.56 0.4702 0.7500 0.0512 0.0321 1.850 10.601 7.590 1379.602 1.198 33.759 2.495 0.62 203292. 0.2881 72.37 0.4963 0.7632 0.0468 0.0304 1.754 10.050 6.937 1307.914 1.135 30.854 2.406 0.62 203744. 0.2655 76.18 0.5224 0.7728 0.0423 0.0286 1.647 9.438 6.266 1228.275 1.066 27.872 2.314 0.62 204214. 0.2428 79.99 0.5485 0.7780 0.0377 0.0266 1.530 8.767 5.581 1140.977 0.991 24.825 2.219 0.62 204704. 0.2197 83.80 0.5746 0.7779 0.0330 0.0244 1.403 8.040 4.885 1046.339 0.908 21.728 2.117 0.62 205212. 0.1961 87.61 0.6007 0.7708 0.0282 0.0220 1.267 7.259 4.180 944.733 0.820 18.593 2.007 0.62 205738. 0.1720 91.42 0.6269 0.7540 0.0234 0.0195 1.122 6.428 3.470 836.605 0.726 15.436 1.881 0.62 206284. 0.1469 95.23 0.6530 0.7231 0.0186 0.0168 0.969 5.552 2.759 722.498 0.627 12.273 1.732 0.62 206848. 0.1206 99.04 0.6791 0.6697 0.0138 0.0140 0.809 4.634 2.051 603.079 0.524 9.122 1.542 0.62 207430. 0.0926 102.85 0.7052 0.5762 0.0091 0.0112 0.643 3.682 1.350 479.170 0.416 6.005 1.278 0.63 208032. 0.0622 106.65 0.7313 0.3989 0.0045 0.0082 0.472 2.703 0.662 351.761 0.305 2.943 0.853 0.63 208652. 0.0291 110.46 0.7575 -0.0105 -0.0001 0.0052 0.297 1.703 -0.011 221.613 0.192 -0.047 -0.022 0.63 209280. 0.0000 PROP RPM = 12000 V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM (mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - - 0.00 0.0000 0.0000 0.0983 0.0341 2.550 13.396 17.332 1901.907 1.513 77.094 4.133 0.67 216284. 0.7212 4.15 0.0261 0.0730 0.0973 0.0348 2.603 13.670 17.147 1940.743 1.544 76.268 4.007 0.67 216435. 0.6955 8.31 0.0522 0.1414 0.0961 0.0355 2.654 13.938 16.939 1978.881 1.575 75.346 3.883 0.67 216602. 0.6697 12.46 0.0783 0.2054 0.0948 0.0361 2.703 14.197 16.708 2015.603 1.604 74.319 3.760 0.67 216783. 0.6441 16.61 0.1044 0.2651 0.0933 0.0368 2.749 14.440 16.452 2050.165 1.631 73.176 3.640 0.67 216982. 0.6187 20.76 0.1305 0.3206 0.0917 0.0373 2.792 14.663 16.167 2081.735 1.657 71.909 3.522 0.67 217197. 0.5936 24.92 0.1566 0.3723 0.0899 0.0378 2.829 14.858 15.851 2109.415 1.679 70.507 3.408 0.67 217431. 0.5687 29.07 0.1827 0.4203 0.0879 0.0382 2.859 15.019 15.504 2132.276 1.697 68.960 3.298 0.67 217683. 0.5442 33.22 0.2088 0.4648 0.0858 0.0385 2.882 15.139 15.121 2149.338 1.710 67.259 3.191 0.67 217953. 0.5201 37.38 0.2349 0.5060 0.0834 0.0387 2.896 15.211 14.702 2159.622 1.719 65.397 3.088 0.67 218243. 0.4962 41.53 0.2610 0.5441 0.0808 0.0388 2.899 15.229 14.246 2162.152 1.721 63.365 2.988 0.67 218553. 0.4727 45.68 0.2871 0.5793 0.0780 0.0387 2.891 15.186 13.750 2156.011 1.716 61.158 2.893 0.67 218883. 0.4495 49.83 0.3132 0.6118 0.0750 0.0384 2.870 15.076 13.214 2140.341 1.703 58.774 2.800 0.67 219233. 0.4266 53.99 0.3393 0.6416 0.0717 0.0379 2.835 14.893 12.637 2114.360 1.683 56.209 2.711 0.67 219604. 0.4039 58.14 0.3655 0.6689 0.0682 0.0372 2.786 14.632 12.019 2077.302 1.653 53.460 2.624 0.67 219995. 0.3813 62.29 0.3916 0.6937 0.0644 0.0364 2.720 14.287 11.360 2028.418 1.614 50.528 2.540 0.67 220407. 0.3588 66.45 0.4177 0.7160 0.0605 0.0353 2.638 13.858 10.662 1967.516 1.566 47.424 2.458 0.67 220839. 0.3364 70.60 0.4438 0.7356 0.0563 0.0340 2.541 13.347 9.930 1894.887 1.508 44.168 2.377 0.67 221291. 0.3139 74.75 0.4699 0.7525 0.0520 0.0325 2.428 12.755 9.168 1810.919 1.441 40.781 2.296 0.67 221764. 0.2914 78.90 0.4960 0.7663 0.0475 0.0308 2.301 12.087 8.382 1716.003 1.366 37.281 2.215 0.67 222257. 0.2688 83.06 0.5221 0.7766 0.0430 0.0289 2.160 11.344 7.573 1610.516 1.282 33.686 2.133 0.68 222770. 0.2460 87.21 0.5482 0.7827 0.0383 0.0268 2.005 10.529 6.747 1494.849 1.190 30.010 2.047 0.68 223304. 0.2229 91.36 0.5743 0.7835 0.0335 0.0246 1.836 9.646 5.906 1369.427 1.090 26.270 1.956 0.68 223858. 0.1992 95.52 0.6004 0.7775 0.0287 0.0221 1.656 8.697 5.055 1234.747 0.983 22.484 1.857 0.68 224432. 0.1750 99.67 0.6265 0.7622 0.0238 0.0196 1.464 7.687 4.197 1091.399 0.869 18.670 1.744 0.68 225027. 0.1498 103.82 0.6526 0.7330 0.0189 0.0169 1.261 6.622 3.338 940.106 0.748 14.846 1.610 0.68 225642. 0.1233 107.97 0.6787 0.6814 0.0141 0.0140 1.048 5.506 2.481 781.766 0.622 11.036 1.440 0.68 226277. 0.0950 112.13 0.7048 0.5897 0.0093 0.0111 0.828 4.349 1.633 617.501 0.491 7.265 1.200 0.68 226933. 0.0643 116.28 0.7309 0.4125 0.0045 0.0080 0.602 3.160 0.800 448.688 0.357 3.560 0.809 0.68 227608. 0.0303 120.43 0.7570 -0.0114 -0.0001 0.0050 0.371 1.947 -0.013 276.412 0.220 -0.059 -0.022 0.69 228293. 0.0000 PROP RPM = 13000 V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM (mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - - 0.00 0.0000 0.0000 0.0993 0.0347 3.301 16.003 20.537 2461.306 1.808 91.348 3.785 0.72 234289. 0.7188 4.49 0.0261 0.0724 0.0982 0.0354 3.366 16.317 20.326 2509.714 1.844 90.412 3.673 0.72 234453. 0.6941 8.99 0.0522 0.1404 0.0971 0.0361 3.430 16.627 20.090 2557.389 1.879 89.361 3.563 0.72 234633. 0.6694 13.48 0.0782 0.2042 0.0958 0.0367 3.491 16.927 19.826 2603.443 1.912 88.185 3.454 0.72 234830. 0.6446 17.98 0.1043 0.2638 0.0944 0.0373 3.550 17.210 19.531 2646.948 1.944 86.872 3.347 0.72 235045. 0.6199 22.47 0.1304 0.3194 0.0928 0.0379 3.603 17.469 19.202 2686.863 1.974 85.409 3.241 0.72 235279. 0.5953 26.97 0.1565 0.3711 0.0910 0.0384 3.650 17.698 18.836 2722.051 2.000 83.784 3.139 0.72 235532. 0.5709 31.46 0.1826 0.4192 0.0891 0.0388 3.690 17.888 18.432 2751.277 2.021 81.985 3.039 0.72 235805. 0.5468 35.96 0.2086 0.4637 0.0869 0.0391 3.719 18.031 17.986 2773.258 2.037 80.001 2.942 0.72 236099. 0.5229 40.45 0.2347 0.5051 0.0846 0.0393 3.737 18.118 17.496 2786.663 2.047 77.822 2.848 0.72 236413. 0.4992 44.95 0.2608 0.5433 0.0820 0.0394 3.742 18.141 16.960 2790.169 2.050 75.439 2.757 0.72 236750. 0.4759 49.44 0.2869 0.5787 0.0792 0.0392 3.731 18.091 16.377 2782.497 2.044 72.844 2.670 0.72 237108. 0.4528 53.94 0.3130 0.6113 0.0761 0.0390 3.705 17.961 15.745 2762.462 2.029 70.034 2.585 0.73 237487. 0.4299 58.43 0.3391 0.6414 0.0728 0.0385 3.660 17.743 15.064 2729.008 2.005 67.006 2.504 0.73 237889. 0.4073 62.93 0.3651 0.6690 0.0693 0.0378 3.595 17.432 14.334 2681.136 1.969 63.756 2.425 0.73 238313. 0.3848 67.42 0.3912 0.6941 0.0655 0.0369 3.511 17.021 13.553 2617.874 1.923 60.284 2.348 0.73 238759. 0.3623 71.92 0.4173 0.7168 0.0615 0.0358 3.405 16.507 12.725 2538.922 1.865 56.602 2.273 0.73 239228. 0.3399 76.41 0.4434 0.7369 0.0573 0.0345 3.278 15.894 11.856 2444.646 1.796 52.735 2.200 0.73 239718. 0.3174 80.91 0.4695 0.7543 0.0529 0.0329 3.132 15.185 10.951 2335.562 1.716 48.709 2.127 0.73 240231. 0.2950 85.40 0.4955 0.7688 0.0484 0.0312 2.967 14.383 10.014 2212.188 1.625 44.543 2.053 0.73 240765. 0.2723 89.90 0.5216 0.7798 0.0437 0.0293 2.783 13.491 9.051 2075.026 1.524 40.260 1.978 0.73 241321. 0.2495 94.39 0.5477 0.7867 0.0390 0.0271 2.581 12.513 8.066 1924.596 1.414 35.879 1.901 0.73 241899. 0.2263 98.89 0.5738 0.7885 0.0341 0.0248 2.362 11.453 7.063 1761.492 1.294 31.418 1.819 0.73 242499. 0.2026 103.38 0.5999 0.7836 0.0292 0.0224 2.127 10.314 6.047 1586.420 1.165 26.899 1.729 0.73 243121. 0.1782 107.88 0.6259 0.7695 0.0243 0.0197 1.878 9.104 5.023 1400.242 1.029 22.343 1.627 0.74 243765. 0.1528 112.37 0.6520 0.7415 0.0193 0.0170 1.615 7.828 3.996 1204.036 0.884 17.773 1.505 0.74 244430. 0.1261 116.87 0.6781 0.6911 0.0144 0.0141 1.340 6.496 2.971 999.160 0.734 13.217 1.349 0.74 245117. 0.0974 121.36 0.7042 0.5998 0.0095 0.0111 1.056 5.119 1.957 787.309 0.578 8.703 1.127 0.74 245827. 0.0661 125.86 0.7303 0.4208 0.0046 0.0080 0.765 3.710 0.959 570.544 0.419 4.267 0.763 0.74 246557. 0.0313 130.35 0.7563 -0.0114 -0.0001 0.0049 0.470 2.279 -0.015 350.541 0.257 -0.069 -0.020 0.74 247298. 0.0000 PROP RPM = 14000 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 0.0362 4.302 19.367 24.065 3207.830 2.188 107.043 3.403 0.78 252288. 0.6996 4.83 0.0260 0.0702 0.0993 0.0368 4.376 19.699 23.832 3262.950 2.226 106.006 3.313 0.78 252464. 0.6778 9.67 0.0521 0.1366 0.0982 0.0375 4.448 20.025 23.569 3316.909 2.262 104.837 3.223 0.78 252658. 0.6558 14.50 0.0781 0.1992 0.0970 0.0380 4.517 20.338 23.274 3368.667 2.298 103.521 3.134 0.78 252870. 0.6336 19.34 0.1042 0.2581 0.0956 0.0386 4.582 20.630 22.941 3417.123 2.331 102.043 3.045 0.78 253101. 0.6113 24.17 0.1302 0.3134 0.0941 0.0391 4.641 20.896 22.569 3461.060 2.361 100.388 2.958 0.78 253353. 0.5889 29.00 0.1563 0.3651 0.0923 0.0395 4.692 21.126 22.154 3499.155 2.387 98.541 2.872 0.78 253626. 0.5665 33.84 0.1823 0.4135 0.0904 0.0399 4.734 21.312 21.692 3529.996 2.408 96.487 2.787 0.78 253920. 0.5441 38.67 0.2084 0.4585 0.0883 0.0401 4.763 21.445 21.181 3552.087 2.423 94.211 2.705 0.78 254237. 0.5217 43.51 0.2344 0.5004 0.0859 0.0402 4.779 21.516 20.616 3563.875 2.431 91.702 2.624 0.78 254576. 0.4993 48.34 0.2604 0.5394 0.0833 0.0402 4.779 21.516 19.997 3563.786 2.431 88.948 2.545 0.78 254938. 0.4770 53.17 0.2865 0.5754 0.0805 0.0401 4.761 21.434 19.321 3550.274 2.422 85.941 2.468 0.78 255324. 0.4547 58.01 0.3125 0.6087 0.0775 0.0398 4.723 21.263 18.587 3521.852 2.402 82.674 2.394 0.78 255734. 0.4325 62.84 0.3386 0.6394 0.0742 0.0393 4.663 20.992 17.793 3477.118 2.372 79.145 2.321 0.78 256167. 0.4103 67.68 0.3646 0.6676 0.0706 0.0386 4.579 20.615 16.940 3414.669 2.329 75.349 2.250 0.78 256624. 0.3882 72.51 0.3907 0.6933 0.0668 0.0376 4.470 20.123 16.026 3333.107 2.273 71.286 2.181 0.78 257104. 0.3659 77.34 0.4167 0.7165 0.0627 0.0365 4.334 19.511 15.056 3231.804 2.204 66.968 2.113 0.78 257609. 0.3436 82.18 0.4428 0.7371 0.0585 0.0351 4.172 18.783 14.035 3111.089 2.122 62.426 2.046 0.79 258137. 0.3213 87.01 0.4688 0.7551 0.0541 0.0336 3.985 17.940 12.970 2971.566 2.027 57.689 1.980 0.79 258689. 0.2988 91.85 0.4948 0.7702 0.0495 0.0318 3.773 16.988 11.866 2813.881 1.919 52.782 1.913 0.79 259264. 0.2762 96.68 0.5209 0.7818 0.0447 0.0298 3.539 15.931 10.731 2638.830 1.800 47.731 1.844 0.79 259862. 0.2532 101.51 0.5469 0.7892 0.0399 0.0276 3.282 14.775 9.568 2447.218 1.669 42.559 1.773 0.79 260484. 0.2299 106.35 0.5730 0.7914 0.0349 0.0253 3.004 13.524 8.383 2240.007 1.528 37.288 1.697 0.79 261130. 0.2060 111.18 0.5990 0.7866 0.0299 0.0228 2.707 12.186 7.181 2018.377 1.377 31.943 1.614 0.79 261798. 0.1813 116.01 0.6251 0.7719 0.0249 0.0201 2.392 10.769 5.969 1783.752 1.217 26.548 1.518 0.79 262490. 0.1554 120.85 0.6511 0.7423 0.0198 0.0174 2.062 9.285 4.751 1537.929 1.049 21.132 1.401 0.79 263206. 0.1280 125.68 0.6771 0.6886 0.0147 0.0145 1.721 7.746 3.535 1283.102 0.875 15.725 1.250 0.80 263945. 0.0985 130.52 0.7032 0.5917 0.0097 0.0115 1.370 6.170 2.330 1021.903 0.697 10.363 1.034 0.80 264707. 0.0662 135.35 0.7292 0.4063 0.0048 0.0086 1.016 4.573 1.143 757.410 0.517 5.086 0.685 0.80 265492. 0.0307 140.18 0.7553 -0.0098 -0.0001 0.0056 0.660 2.971 -0.017 492.118 0.336 -0.077 -0.016 0.80 266289. 0.0000 PROP RPM = 15000 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 0.1014 0.0395 5.768 24.236 27.922 4301.039 2.738 124.195 2.945 0.83 270280. 0.6521 5.22 0.0262 0.0659 0.1004 0.0400 5.844 24.558 27.668 4358.211 2.775 123.068 2.879 0.83 270470. 0.6348 10.44 0.0525 0.1288 0.0994 0.0405 5.918 24.866 27.380 4412.823 2.809 121.786 2.814 0.83 270679. 0.6172 15.66 0.0787 0.1887 0.0982 0.0410 5.986 25.151 27.053 4463.514 2.842 120.332 2.749 0.83 270909. 0.5993 20.88 0.1050 0.2456 0.0969 0.0414 6.047 25.407 26.683 4508.909 2.870 118.686 2.684 0.83 271159. 0.5811 26.09 0.1312 0.2997 0.0954 0.0417 6.098 25.625 26.266 4547.525 2.895 116.829 2.620 0.83 271432. 0.5627 31.31 0.1575 0.3508 0.0936 0.0420 6.139 25.795 25.796 4577.849 2.914 114.741 2.556 0.83 271728. 0.5441 36.53 0.1837 0.3992 0.0917 0.0422 6.166 25.911 25.270 4598.298 2.927 112.402 2.493 0.83 272048. 0.5252 41.75 0.2099 0.4448 0.0896 0.0423 6.178 25.961 24.684 4607.232 2.933 109.796 2.430 0.83 272392. 0.5060 46.97 0.2362 0.4877 0.0873 0.0423 6.173 25.937 24.034 4602.991 2.930 106.905 2.368 0.84 272761. 0.4866 52.19 0.2624 0.5279 0.0846 0.0421 6.147 25.829 23.317 4583.901 2.918 103.716 2.307 0.84 273156. 0.4669 57.41 0.2887 0.5655 0.0818 0.0418 6.099 25.629 22.531 4548.328 2.896 100.218 2.247 0.84 273576. 0.4470 62.63 0.3149 0.6005 0.0787 0.0413 6.027 25.327 21.673 4494.693 2.861 96.403 2.187 0.84 274022. 0.4267 67.84 0.3412 0.6329 0.0753 0.0406 5.929 24.914 20.744 4421.480 2.815 92.269 2.128 0.84 274494. 0.4062 73.06 0.3674 0.6628 0.0717 0.0397 5.803 24.382 19.741 4327.070 2.755 87.810 2.069 0.84 274991. 0.3853 78.28 0.3936 0.6901 0.0678 0.0386 5.645 23.721 18.665 4209.797 2.680 83.023 2.011 0.84 275515. 0.3641 83.50 0.4199 0.7149 0.0636 0.0374 5.457 22.928 17.520 4068.938 2.590 77.929 1.953 0.84 276064. 0.3426 88.72 0.4461 0.7369 0.0592 0.0359 5.237 22.005 16.313 3905.170 2.486 72.561 1.895 0.84 276640. 0.3207 93.94 0.4724 0.7557 0.0546 0.0342 4.990 20.966 15.053 3720.749 2.369 66.955 1.835 0.84 277240. 0.2984 99.16 0.4986 0.7708 0.0499 0.0323 4.715 19.812 13.746 3516.072 2.238 61.144 1.773 0.84 277866. 0.2756 104.38 0.5249 0.7817 0.0450 0.0302 4.415 18.552 12.400 3292.292 2.096 55.157 1.708 0.84 278518. 0.2521 109.59 0.5511 0.7874 0.0400 0.0280 4.090 17.188 11.021 3050.260 1.942 49.022 1.639 0.85 279194. 0.2280 114.81 0.5773 0.7866 0.0349 0.0256 3.742 15.725 9.615 2790.766 1.777 42.770 1.563 0.85 279896. 0.2031 120.03 0.6036 0.7768 0.0297 0.0231 3.374 14.179 8.190 2516.293 1.602 36.427 1.476 0.85 280624. 0.1771 125.25 0.6298 0.7542 0.0245 0.0205 2.989 12.561 6.750 2229.234 1.419 30.026 1.373 0.85 281376. 0.1496 130.47 0.6561 0.7122 0.0193 0.0177 2.592 10.890 5.306 1932.660 1.230 23.600 1.245 0.85 282154. 0.1202 135.69 0.6823 0.6395 0.0140 0.0150 2.186 9.186 3.864 1630.301 1.038 17.189 1.075 0.85 282957. 0.0886 140.91 0.7086 0.5148 0.0088 0.0122 1.778 7.473 2.437 1326.205 0.844 10.839 0.833 0.85 283785. 0.0545 146.12 0.7348 0.2932 0.0038 0.0094 1.374 5.774 1.034 1024.749 0.652 4.600 0.458 0.86 284638. 0.0195 151.34 0.7610 PROP RPM = 16000 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 0.1020 0.0447 7.928 31.230 31.980 5911.864 3.528 142.249 2.454 0.89 288276. 0.5815 5.58 0.0263 0.0589 0.1012 0.0452 8.008 31.547 31.720 5971.839 3.564 141.091 2.409 0.89 288478. 0.5687 11.15 0.0526 0.1156 0.1003 0.0456 8.081 31.834 31.421 6026.070 3.597 139.760 2.365 0.89 288700. 0.5556 16.73 0.0789 0.1703 0.0992 0.0459 8.144 32.080 31.078 6072.677 3.624 138.233 2.321 0.89 288944. 0.5423 22.31 0.1052 0.2228 0.0979 0.0462 8.193 32.276 30.685 6109.804 3.647 136.488 2.278 0.89 289211. 0.5289 27.88 0.1315 0.2733 0.0965 0.0464 8.228 32.412 30.238 6135.598 3.662 134.497 2.235 0.89 289503. 0.5152 33.46 0.1577 0.3217 0.0949 0.0465 8.245 32.479 29.730 6148.226 3.669 132.237 2.193 0.89 289819. 0.5012 39.04 0.1840 0.3683 0.0930 0.0465 8.242 32.467 29.156 6145.884 3.668 129.684 2.152 0.89 290161. 0.4869 44.62 0.2103 0.4128 0.0910 0.0463 8.216 32.366 28.510 6126.787 3.657 126.813 2.111 0.89 290529. 0.4723 50.19 0.2366 0.4555 0.0887 0.0461 8.165 32.166 27.788 6088.961 3.634 123.602 2.070 0.89 290925. 0.4573 55.77 0.2629 0.4962 0.0861 0.0456 8.088 31.860 26.986 6031.153 3.600 120.034 2.029 0.89 291348. 0.4419 61.35 0.2892 0.5349 0.0833 0.0450 7.982 31.442 26.100 5951.858 3.552 116.094 1.989 0.89 291799. 0.4259 66.92 0.3155 0.5716 0.0802 0.0443 7.845 30.902 25.129 5849.784 3.491 111.774 1.948 0.89 292277. 0.4094 72.50 0.3418 0.6063 0.0768 0.0433 7.676 30.237 24.071 5723.811 3.416 107.067 1.907 0.89 292784. 0.3922 78.08 0.3681 0.6387 0.0731 0.0422 7.473 29.439 22.925 5572.775 3.326 101.970 1.866 0.89 293318. 0.3744 83.65 0.3944 0.6687 0.0692 0.0408 7.235 28.501 21.691 5395.292 3.220 96.481 1.823 0.90 293880. 0.3559 89.23 0.4207 0.6964 0.0650 0.0393 6.961 27.422 20.373 5190.976 3.098 90.620 1.780 0.90 294470. 0.3368 94.81 0.4470 0.7214 0.0606 0.0375 6.652 26.205 18.982 4960.648 2.961 84.431 1.736 0.90 295087. 0.3169 100.39 0.4732 0.7429 0.0559 0.0356 6.315 24.876 17.525 4709.040 2.811 77.953 1.688 0.90 295732. 0.2962 105.96 0.4995 0.7598 0.0511 0.0336 5.955 23.457 16.012 4440.301 2.650 71.221 1.636 0.90 296404. 0.2743 111.54 0.5258 0.7714 0.0461 0.0314 5.572 21.948 14.450 4154.775 2.480 64.273 1.577 0.90 297102. 0.2513 117.12 0.5521 0.7740 0.0410 0.0292 5.183 20.417 12.845 3864.825 2.307 57.135 1.507 0.90 297828. 0.2264 122.69 0.5784 0.7675 0.0358 0.0269 4.777 18.819 11.208 3562.390 2.126 49.851 1.427 0.90 298581. 0.2002 128.27 0.6047 0.7499 0.0305 0.0246 4.354 17.153 9.546 3247.109 1.938 42.462 1.333 0.90 299360. 0.1727 133.85 0.6310 0.7164 0.0251 0.0221 3.921 15.445 7.870 2923.747 1.745 35.005 1.221 0.91 300166. 0.1435 139.42 0.6573 0.6608 0.0197 0.0196 3.481 13.715 6.188 2596.140 1.549 27.525 1.081 0.91 300999. 0.1127 145.00 0.6836 0.5733 0.0144 0.0172 3.043 11.988 4.512 2269.265 1.354 20.071 0.902 0.91 301859. 0.0803 150.58 0.7099 0.4388 0.0091 0.0147 2.613 10.294 2.856 1948.644 1.163 12.702 0.665 0.91 302746. 0.0471 156.16 0.7362 0.2335 0.0039 0.0124 2.198 8.659 1.233 1639.103 0.978 5.483 0.341 0.91 303659. 0.0159 161.73 0.7625