21x10W (21x10W.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 0.0904 0.0349 0.011 0.724 0.560 8.562 0.082 2.492 29.675 0.08 52431. 0.6206 0.44 0.0221 0.0556 0.0887 0.0352 0.012 0.729 0.550 8.626 0.082 2.445 28.907 0.08 52463. 0.5989 0.88 0.0442 0.1083 0.0869 0.0354 0.012 0.734 0.539 8.681 0.083 2.396 28.143 0.08 52498. 0.5771 1.32 0.0662 0.1581 0.0850 0.0356 0.012 0.738 0.527 8.726 0.083 2.343 27.385 0.08 52536. 0.5554 1.76 0.0883 0.2051 0.0830 0.0357 0.012 0.740 0.514 8.758 0.084 2.287 26.633 0.08 52576. 0.5336 2.20 0.1104 0.2491 0.0808 0.0358 0.012 0.742 0.501 8.777 0.084 2.228 25.887 0.08 52619. 0.5119 2.63 0.1325 0.2904 0.0786 0.0358 0.012 0.742 0.487 8.782 0.084 2.166 25.148 0.08 52664. 0.4903 3.07 0.1546 0.3290 0.0762 0.0358 0.012 0.741 0.472 8.769 0.084 2.100 24.415 0.08 52712. 0.4687 3.51 0.1766 0.3648 0.0736 0.0357 0.012 0.739 0.456 8.739 0.083 2.030 23.688 0.08 52763. 0.4471 3.95 0.1987 0.3979 0.0710 0.0355 0.012 0.734 0.440 8.689 0.083 1.957 22.966 0.08 52817. 0.4257 4.39 0.2208 0.4283 0.0682 0.0352 0.012 0.729 0.423 8.619 0.082 1.881 22.250 0.08 52874. 0.4042 4.83 0.2429 0.4560 0.0653 0.0348 0.011 0.721 0.405 8.528 0.081 1.801 21.536 0.08 52934. 0.3829 5.27 0.2649 0.4810 0.0623 0.0343 0.011 0.711 0.386 8.415 0.080 1.719 20.825 0.08 52996. 0.3617 5.71 0.2870 0.5033 0.0592 0.0338 0.011 0.700 0.367 8.280 0.079 1.633 20.113 0.08 53063. 0.3405 6.15 0.3091 0.5227 0.0560 0.0331 0.011 0.686 0.347 8.121 0.078 1.545 19.397 0.08 53132. 0.3194 6.59 0.3312 0.5392 0.0527 0.0324 0.011 0.671 0.327 7.939 0.076 1.454 18.676 0.08 53204. 0.2984 7.03 0.3533 0.5527 0.0494 0.0316 0.010 0.654 0.306 7.732 0.074 1.361 17.945 0.08 53280. 0.2773 7.46 0.3753 0.5628 0.0459 0.0306 0.010 0.634 0.284 7.501 0.072 1.265 17.200 0.08 53359. 0.2563 7.90 0.3974 0.5694 0.0423 0.0296 0.010 0.612 0.262 7.244 0.069 1.167 16.434 0.08 53442. 0.2352 8.34 0.4195 0.5720 0.0387 0.0284 0.009 0.588 0.240 6.961 0.066 1.068 15.640 0.08 53528. 0.2141 8.78 0.4416 0.5701 0.0350 0.0271 0.009 0.562 0.217 6.652 0.064 0.966 14.809 0.08 53617. 0.1928 9.22 0.4637 0.5630 0.0313 0.0258 0.008 0.534 0.194 6.317 0.060 0.863 13.927 0.08 53710. 0.1714 9.66 0.4857 0.5496 0.0275 0.0243 0.008 0.503 0.170 5.954 0.057 0.758 12.979 0.08 53806. 0.1497 10.10 0.5078 0.5286 0.0236 0.0227 0.007 0.470 0.147 5.565 0.053 0.652 11.941 0.08 53906. 0.1277 10.54 0.5299 0.4980 0.0197 0.0210 0.007 0.435 0.122 5.149 0.049 0.544 10.779 0.08 54009. 0.1054 10.98 0.5520 0.4546 0.0158 0.0192 0.006 0.398 0.098 4.706 0.045 0.436 9.447 0.08 54116. 0.0826 11.42 0.5740 0.3938 0.0119 0.0173 0.006 0.358 0.074 4.237 0.040 0.327 7.870 0.08 54226. 0.0596 11.85 0.5961 0.3082 0.0079 0.0153 0.005 0.316 0.049 3.742 0.036 0.218 5.930 0.08 54340. 0.0367 12.29 0.6182 0.1845 0.0039 0.0132 0.004 0.272 0.024 3.223 0.031 0.108 3.424 0.08 54457. 0.0149 12.73 0.6403 -0.0033 -0.0001 0.0109 0.004 0.226 0.000 2.678 0.026 -0.002 -0.059 0.09 54572. 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 0.0909 0.0318 0.084 2.634 2.253 62.320 0.298 10.019 16.394 0.17 104859. 0.6875 0.88 0.0222 0.0616 0.0892 0.0321 0.084 2.658 2.211 62.892 0.300 9.833 15.944 0.17 104925. 0.6624 1.76 0.0443 0.1198 0.0874 0.0323 0.085 2.679 2.166 63.393 0.303 9.635 15.499 0.17 104995. 0.6374 2.64 0.0665 0.1746 0.0855 0.0325 0.086 2.697 2.119 63.810 0.305 9.424 15.060 0.17 105071. 0.6125 3.53 0.0887 0.2262 0.0834 0.0327 0.086 2.710 2.068 64.130 0.306 9.200 14.628 0.17 105151. 0.5878 4.41 0.1108 0.2745 0.0813 0.0328 0.086 2.719 2.015 64.341 0.307 8.962 14.203 0.17 105237. 0.5633 5.29 0.1330 0.3197 0.0790 0.0329 0.086 2.723 1.958 64.430 0.308 8.710 13.786 0.17 105328. 0.5390 6.17 0.1552 0.3619 0.0766 0.0328 0.086 2.721 1.899 64.383 0.307 8.445 13.375 0.17 105425. 0.5149 7.05 0.1773 0.4011 0.0740 0.0327 0.086 2.713 1.836 64.186 0.306 8.165 12.971 0.17 105528. 0.4910 7.93 0.1995 0.4374 0.0714 0.0326 0.086 2.698 1.770 63.830 0.305 7.871 12.574 0.17 105636. 0.4674 8.82 0.2217 0.4709 0.0686 0.0323 0.085 2.675 1.700 63.304 0.302 7.564 12.184 0.17 105751. 0.4439 9.70 0.2438 0.5016 0.0657 0.0319 0.084 2.646 1.628 62.601 0.299 7.243 11.799 0.17 105871. 0.4207 10.58 0.2660 0.5296 0.0627 0.0315 0.083 2.608 1.554 61.716 0.295 6.911 11.419 0.17 105998. 0.3977 11.46 0.2882 0.5548 0.0596 0.0309 0.081 2.563 1.476 60.641 0.290 6.567 11.042 0.17 106131. 0.3749 12.34 0.3103 0.5773 0.0563 0.0303 0.080 2.509 1.396 59.372 0.283 6.212 10.668 0.17 106271. 0.3523 13.22 0.3325 0.5969 0.0530 0.0295 0.078 2.447 1.314 57.903 0.276 5.846 10.295 0.17 106417. 0.3298 14.11 0.3547 0.6135 0.0496 0.0287 0.075 2.376 1.230 56.227 0.268 5.471 9.921 0.17 106570. 0.3074 14.99 0.3768 0.6271 0.0461 0.0277 0.073 2.297 1.143 54.341 0.259 5.086 9.544 0.17 106729. 0.2851 15.87 0.3990 0.6373 0.0426 0.0266 0.070 2.208 1.055 52.239 0.249 4.693 9.160 0.17 106895. 0.2629 16.75 0.4212 0.6438 0.0389 0.0255 0.067 2.110 0.965 49.917 0.238 4.291 8.766 0.17 107069. 0.2406 17.63 0.4433 0.6461 0.0352 0.0242 0.064 2.002 0.873 47.371 0.226 3.883 8.358 0.17 107249. 0.2182 18.51 0.4655 0.6434 0.0314 0.0227 0.060 1.885 0.779 44.598 0.213 3.467 7.927 0.17 107435. 0.1955 19.40 0.4877 0.6348 0.0276 0.0212 0.056 1.758 0.685 41.596 0.199 3.045 7.466 0.17 107629. 0.1726 20.28 0.5098 0.6187 0.0237 0.0196 0.051 1.621 0.589 38.365 0.183 2.619 6.960 0.17 107830. 0.1492 21.16 0.5320 0.5927 0.0198 0.0178 0.047 1.475 0.492 34.905 0.167 2.187 6.390 0.17 108038. 0.1252 22.04 0.5542 0.5531 0.0159 0.0159 0.042 1.319 0.394 31.219 0.149 1.752 5.724 0.17 108254. 0.1004 22.92 0.5763 0.4935 0.0119 0.0139 0.037 1.154 0.296 27.310 0.130 1.315 4.910 0.17 108476. 0.0746 23.80 0.5985 0.4024 0.0080 0.0118 0.031 0.980 0.197 23.187 0.111 0.877 3.856 0.17 108705. 0.0478 24.69 0.6207 0.2565 0.0040 0.0096 0.025 0.797 0.099 18.856 0.090 0.438 2.370 0.17 108940. 0.0208 25.57 0.6428 -0.0028 0.0000 0.0073 0.019 0.603 -0.001 14.273 0.068 -0.003 -0.025 0.17 109166. 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 0.0914 0.0306 0.272 5.710 5.099 202.680 0.645 22.680 11.410 0.25 157283. 0.7199 1.33 0.0222 0.0644 0.0897 0.0309 0.275 5.767 5.005 204.706 0.652 22.260 11.089 0.25 157382. 0.6931 2.65 0.0444 0.1252 0.0879 0.0312 0.277 5.818 4.904 206.489 0.657 21.812 10.772 0.25 157488. 0.6665 3.98 0.0666 0.1823 0.0860 0.0314 0.279 5.860 4.797 207.983 0.662 21.335 10.461 0.25 157602. 0.6401 5.30 0.0889 0.2360 0.0839 0.0316 0.280 5.893 4.683 209.148 0.666 20.829 10.155 0.25 157723. 0.6140 6.63 0.1111 0.2863 0.0818 0.0317 0.282 5.915 4.562 209.937 0.668 20.291 9.856 0.25 157852. 0.5882 7.95 0.1333 0.3333 0.0795 0.0318 0.282 5.925 4.434 210.306 0.669 19.722 9.563 0.25 157990. 0.5626 9.28 0.1555 0.3772 0.0771 0.0318 0.282 5.922 4.299 210.207 0.669 19.121 9.276 0.25 158136. 0.5374 10.60 0.1777 0.4181 0.0745 0.0317 0.281 5.905 4.156 209.595 0.667 18.488 8.995 0.25 158291. 0.5124 11.93 0.1999 0.4559 0.0718 0.0315 0.280 5.872 4.007 208.429 0.663 17.823 8.720 0.25 158454. 0.4877 13.25 0.2221 0.4909 0.0690 0.0312 0.277 5.823 3.850 206.678 0.658 17.127 8.450 0.25 158627. 0.4633 14.58 0.2443 0.5231 0.0661 0.0309 0.274 5.756 3.687 204.317 0.650 16.401 8.186 0.25 158808. 0.4392 15.90 0.2666 0.5526 0.0631 0.0304 0.270 5.672 3.518 201.322 0.641 15.648 7.926 0.25 159000. 0.4154 17.23 0.2888 0.5793 0.0599 0.0299 0.265 5.569 3.343 197.673 0.629 14.868 7.670 0.25 159200. 0.3918 18.55 0.3110 0.6033 0.0567 0.0292 0.259 5.447 3.162 193.348 0.615 14.063 7.417 0.25 159411. 0.3685 19.88 0.3332 0.6245 0.0533 0.0285 0.253 5.306 2.975 188.327 0.599 13.235 7.166 0.25 159631. 0.3454 21.20 0.3554 0.6429 0.0499 0.0276 0.245 5.144 2.784 182.591 0.581 12.384 6.916 0.25 159861. 0.3224 22.53 0.3776 0.6583 0.0464 0.0266 0.236 4.962 2.588 176.123 0.561 11.512 6.665 0.25 160101. 0.2996 23.85 0.3998 0.6706 0.0428 0.0255 0.227 4.759 2.388 168.904 0.538 10.621 6.412 0.25 160352. 0.2769 25.18 0.4221 0.6793 0.0391 0.0243 0.216 4.534 2.183 160.920 0.512 9.712 6.154 0.25 160612. 0.2541 26.50 0.4443 0.6841 0.0354 0.0230 0.204 4.287 1.975 152.158 0.484 8.786 5.888 0.25 160883. 0.2312 27.83 0.4665 0.6843 0.0316 0.0216 0.191 4.018 1.764 142.606 0.454 7.844 5.609 0.25 161165. 0.2081 29.16 0.4887 0.6789 0.0278 0.0200 0.177 3.726 1.549 132.259 0.421 6.889 5.311 0.25 161457. 0.1847 30.48 0.5109 0.6662 0.0239 0.0183 0.162 3.412 1.331 121.114 0.386 5.922 4.986 0.25 161760. 0.1607 31.81 0.5331 0.6440 0.0199 0.0165 0.146 3.076 1.112 109.172 0.348 4.945 4.619 0.25 162073. 0.1361 33.13 0.5553 0.6082 0.0160 0.0146 0.129 2.717 0.890 96.444 0.307 3.960 4.187 0.25 162397. 0.1104 34.46 0.5775 0.5516 0.0120 0.0125 0.111 2.337 0.668 82.944 0.264 2.970 3.652 0.25 162732. 0.0834 35.78 0.5998 0.4605 0.0080 0.0104 0.092 1.936 0.445 68.698 0.219 1.978 2.936 0.25 163077. 0.0547 37.11 0.6220 0.3043 0.0040 0.0081 0.072 1.514 0.222 53.730 0.171 0.986 1.871 0.25 163430. 0.0246 38.43 0.6442 -0.0088 -0.0001 0.0057 0.051 1.065 -0.004 37.802 0.120 -0.019 -0.052 0.26 163758. 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 0.0921 0.0302 0.634 9.993 9.136 472.931 1.129 40.636 8.762 0.33 209700. 0.7400 1.77 0.0222 0.0660 0.0904 0.0305 0.641 10.098 8.968 477.885 1.141 39.888 8.511 0.33 209832. 0.7122 3.54 0.0445 0.1282 0.0886 0.0307 0.647 10.190 8.788 482.251 1.151 39.089 8.265 0.33 209974. 0.6846 5.31 0.0667 0.1867 0.0867 0.0310 0.652 10.268 8.596 485.923 1.160 38.237 8.024 0.33 210127. 0.6574 7.08 0.0890 0.2417 0.0846 0.0312 0.655 10.329 8.393 488.796 1.167 37.331 7.788 0.33 210289. 0.6304 8.85 0.1112 0.2931 0.0825 0.0313 0.658 10.370 8.177 490.763 1.172 36.370 7.557 0.33 210462. 0.6038 10.62 0.1335 0.3412 0.0801 0.0313 0.659 10.390 7.948 491.715 1.174 35.353 7.331 0.33 210647. 0.5775 12.39 0.1557 0.3861 0.0777 0.0313 0.659 10.386 7.706 491.536 1.173 34.277 7.111 0.33 210842. 0.5516 14.16 0.1780 0.4279 0.0751 0.0312 0.657 10.356 7.451 490.115 1.170 33.143 6.896 0.33 211049. 0.5259 15.93 0.2002 0.4667 0.0724 0.0311 0.654 10.298 7.183 487.355 1.163 31.951 6.685 0.33 211269. 0.5006 17.69 0.2224 0.5027 0.0696 0.0308 0.648 10.210 6.903 483.180 1.154 30.704 6.480 0.33 211500. 0.4757 19.46 0.2447 0.5358 0.0667 0.0304 0.640 10.090 6.611 477.527 1.140 29.404 6.279 0.33 211743. 0.4511 21.23 0.2669 0.5662 0.0636 0.0300 0.631 9.939 6.307 470.340 1.123 28.054 6.082 0.33 211999. 0.4268 23.00 0.2892 0.5939 0.0604 0.0294 0.619 9.753 5.993 461.566 1.102 26.656 5.889 0.33 212268. 0.4028 24.77 0.3114 0.6189 0.0572 0.0288 0.605 9.533 5.668 451.155 1.077 25.212 5.699 0.33 212549. 0.3791 26.54 0.3337 0.6412 0.0538 0.0280 0.589 9.278 5.334 439.060 1.048 23.727 5.510 0.34 212844. 0.3556 28.31 0.3559 0.6608 0.0503 0.0271 0.570 8.985 4.991 425.233 1.015 22.201 5.324 0.34 213152. 0.3323 30.08 0.3782 0.6775 0.0468 0.0261 0.549 8.656 4.640 409.630 0.978 20.637 5.137 0.34 213474. 0.3092 31.85 0.4004 0.6912 0.0432 0.0250 0.526 8.288 4.280 392.209 0.936 19.039 4.950 0.34 213809. 0.2861 33.62 0.4226 0.7015 0.0395 0.0238 0.500 7.880 3.913 372.935 0.890 17.407 4.760 0.34 214157. 0.2631 35.39 0.4449 0.7081 0.0357 0.0224 0.472 7.433 3.540 351.774 0.840 15.746 4.564 0.34 214520. 0.2399 37.16 0.4671 0.7104 0.0319 0.0210 0.441 6.946 3.160 328.701 0.785 14.057 4.361 0.34 214897. 0.2166 38.93 0.4894 0.7073 0.0280 0.0194 0.407 6.417 2.775 303.701 0.725 12.343 4.144 0.34 215287. 0.1929 40.70 0.5116 0.6973 0.0241 0.0176 0.371 5.848 2.385 276.766 0.661 10.608 3.908 0.34 215692. 0.1687 42.47 0.5339 0.6781 0.0201 0.0158 0.332 5.238 1.991 247.903 0.592 8.855 3.643 0.34 216111. 0.1436 44.24 0.5561 0.6456 0.0161 0.0138 0.291 4.588 1.594 217.134 0.518 7.089 3.329 0.34 216545. 0.1174 46.01 0.5784 0.5922 0.0120 0.0118 0.247 3.899 1.194 184.499 0.440 5.313 2.936 0.34 216992. 0.0897 47.78 0.6006 0.5028 0.0080 0.0096 0.201 3.171 0.794 150.056 0.358 3.533 2.401 0.34 217453. 0.0598 49.54 0.6229 0.3410 0.0040 0.0073 0.153 2.406 0.394 113.867 0.272 1.753 1.570 0.34 217926. 0.0275 51.31 0.6451 -0.0191 -0.0001 0.0048 0.101 1.586 -0.014 75.064 0.179 -0.063 -0.085 0.34 218340. 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 0.0931 0.0300 1.234 15.559 14.418 920.424 1.758 64.132 7.105 0.42 262106. 0.7538 2.21 0.0223 0.0669 0.0914 0.0304 1.248 15.727 14.155 930.342 1.777 62.960 6.901 0.42 262272. 0.7254 4.43 0.0445 0.1300 0.0895 0.0307 1.259 15.875 13.873 939.086 1.794 61.706 6.700 0.42 262451. 0.6973 6.64 0.0668 0.1893 0.0876 0.0309 1.269 15.999 13.572 946.444 1.808 60.369 6.504 0.42 262642. 0.6695 8.85 0.0890 0.2450 0.0855 0.0311 1.277 16.097 13.252 952.206 1.819 58.946 6.313 0.42 262846. 0.6421 11.06 0.1113 0.2971 0.0833 0.0312 1.282 16.163 12.913 956.161 1.826 57.435 6.125 0.42 263064. 0.6150 13.28 0.1335 0.3459 0.0810 0.0313 1.285 16.196 12.553 958.091 1.830 55.834 5.943 0.42 263295. 0.5883 15.49 0.1558 0.3915 0.0786 0.0313 1.284 16.191 12.172 957.767 1.829 54.141 5.764 0.42 263541. 0.5619 17.70 0.1780 0.4339 0.0760 0.0312 1.281 16.143 11.771 954.968 1.824 52.356 5.591 0.42 263801. 0.5359 19.92 0.2003 0.4733 0.0732 0.0310 1.273 16.051 11.349 949.500 1.813 50.478 5.421 0.42 264076. 0.5103 22.13 0.2226 0.5099 0.0704 0.0307 1.262 15.911 10.907 941.210 1.798 48.513 5.256 0.42 264366. 0.4850 24.34 0.2448 0.5437 0.0674 0.0304 1.247 15.721 10.446 929.972 1.776 46.463 5.095 0.42 264671. 0.4601 26.56 0.2671 0.5748 0.0643 0.0299 1.228 15.479 9.967 915.675 1.749 44.333 4.937 0.42 264993. 0.4355 28.77 0.2893 0.6032 0.0611 0.0293 1.205 15.184 9.471 898.218 1.715 42.127 4.783 0.42 265330. 0.4112 30.98 0.3116 0.6290 0.0578 0.0286 1.177 14.834 8.959 877.501 1.676 39.850 4.631 0.42 265683. 0.3873 33.19 0.3338 0.6521 0.0544 0.0279 1.144 14.427 8.432 853.429 1.630 37.505 4.481 0.42 266052. 0.3636 35.41 0.3561 0.6726 0.0509 0.0270 1.108 13.962 7.890 825.910 1.577 35.096 4.333 0.42 266438. 0.3401 37.62 0.3784 0.6903 0.0473 0.0259 1.066 13.437 7.335 794.857 1.518 32.628 4.186 0.42 266841. 0.3168 39.83 0.4006 0.7052 0.0437 0.0248 1.019 12.851 6.768 760.187 1.452 30.103 4.038 0.42 267261. 0.2935 42.05 0.4229 0.7168 0.0399 0.0236 0.968 12.202 6.189 721.828 1.379 27.527 3.889 0.42 267698. 0.2703 44.26 0.4451 0.7249 0.0361 0.0222 0.912 11.490 5.599 679.717 1.298 24.903 3.736 0.42 268152. 0.2470 46.47 0.4674 0.7288 0.0323 0.0207 0.850 10.714 4.999 633.802 1.210 22.235 3.577 0.42 268624. 0.2235 48.69 0.4896 0.7277 0.0283 0.0191 0.783 9.873 4.390 584.052 1.115 19.528 3.410 0.42 269113. 0.1996 50.90 0.5119 0.7201 0.0244 0.0173 0.711 8.967 3.774 530.453 1.013 16.787 3.227 0.42 269620. 0.1752 53.11 0.5341 0.7036 0.0203 0.0154 0.634 7.996 3.152 473.018 0.903 14.018 3.022 0.42 270145. 0.1499 55.32 0.5564 0.6742 0.0163 0.0134 0.552 6.961 2.524 411.792 0.786 11.226 2.780 0.42 270687. 0.1234 57.54 0.5787 0.6244 0.0122 0.0113 0.465 5.863 1.893 346.852 0.662 8.420 2.475 0.42 271247. 0.0952 59.75 0.6009 0.5380 0.0081 0.0091 0.373 4.705 1.260 278.319 0.532 5.606 2.054 0.42 271824. 0.0644 61.96 0.6232 0.3751 0.0041 0.0067 0.277 3.488 0.628 206.314 0.394 2.793 1.381 0.42 272415. 0.0306 64.18 0.6454 -0.0197 -0.0001 0.0042 0.173 2.177 -0.020 128.779 0.246 -0.088 -0.070 0.43 272917. 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 0.0942 0.0302 2.144 22.526 21.024 1599.046 2.545 93.513 5.963 0.50 314497. 0.7640 2.68 0.0224 0.0679 0.0925 0.0305 2.168 22.775 20.640 1616.720 2.573 91.807 5.791 0.50 314700. 0.7351 5.35 0.0448 0.1319 0.0907 0.0308 2.189 22.994 20.229 1632.278 2.598 89.979 5.621 0.50 314917. 0.7064 8.03 0.0673 0.1920 0.0887 0.0311 2.206 23.178 19.790 1645.323 2.619 88.026 5.456 0.50 315150. 0.6781 10.70 0.0897 0.2484 0.0866 0.0313 2.220 23.321 19.322 1655.485 2.635 85.946 5.294 0.50 315399. 0.6502 13.38 0.1121 0.3012 0.0844 0.0314 2.229 23.418 18.825 1662.385 2.646 83.734 5.136 0.50 315664. 0.6227 16.05 0.1345 0.3507 0.0820 0.0315 2.234 23.464 18.298 1665.627 2.651 81.388 4.983 0.50 315946. 0.5955 18.73 0.1570 0.3968 0.0795 0.0314 2.233 23.452 17.739 1664.806 2.650 78.904 4.833 0.50 316245. 0.5688 21.40 0.1794 0.4398 0.0769 0.0313 2.225 23.378 17.150 1659.521 2.641 76.283 4.687 0.50 316562. 0.5424 24.08 0.2018 0.4798 0.0741 0.0312 2.212 23.236 16.530 1649.426 2.625 73.524 4.545 0.50 316897. 0.5164 26.76 0.2242 0.5170 0.0712 0.0309 2.192 23.022 15.880 1634.245 2.601 70.634 4.407 0.50 317250. 0.4907 29.43 0.2467 0.5513 0.0681 0.0305 2.164 22.733 15.202 1613.758 2.568 67.618 4.273 0.50 317623. 0.4655 32.11 0.2691 0.5829 0.0650 0.0300 2.129 22.367 14.497 1587.773 2.527 64.483 4.141 0.50 318014. 0.4406 34.78 0.2915 0.6119 0.0617 0.0294 2.087 21.921 13.767 1556.111 2.477 61.235 4.013 0.50 318425. 0.4160 37.46 0.3139 0.6382 0.0583 0.0287 2.036 21.393 13.013 1518.595 2.417 57.881 3.887 0.50 318855. 0.3917 40.13 0.3364 0.6620 0.0548 0.0279 1.978 20.779 12.236 1475.063 2.348 54.427 3.763 0.50 319305. 0.3678 42.81 0.3588 0.6831 0.0513 0.0269 1.911 20.079 11.439 1425.348 2.269 50.879 3.640 0.50 319775. 0.3440 45.48 0.3812 0.7015 0.0476 0.0259 1.836 19.289 10.621 1369.299 2.179 47.242 3.518 0.50 320266. 0.3204 48.16 0.4036 0.7170 0.0439 0.0247 1.752 18.409 9.785 1306.771 2.080 43.522 3.396 0.50 320777. 0.2968 50.84 0.4261 0.7294 0.0400 0.0234 1.660 17.435 8.931 1237.637 1.970 39.725 3.273 0.50 321309. 0.2733 53.51 0.4485 0.7383 0.0361 0.0219 1.558 16.366 8.062 1161.787 1.849 35.858 3.147 0.50 321862. 0.2497 56.19 0.4709 0.7431 0.0322 0.0204 1.447 15.202 7.178 1079.135 1.717 31.926 3.017 0.51 322437. 0.2258 58.86 0.4933 0.7428 0.0282 0.0187 1.327 13.941 6.281 989.626 1.575 27.937 2.879 0.51 323032. 0.2016 61.54 0.5157 0.7360 0.0241 0.0169 1.198 12.583 5.373 893.245 1.422 23.898 2.728 0.51 323650. 0.1767 64.21 0.5382 0.7201 0.0200 0.0149 1.059 11.129 4.455 790.020 1.257 19.817 2.558 0.51 324288. 0.1509 66.89 0.5606 0.6906 0.0158 0.0128 0.912 9.580 3.531 680.043 1.082 15.705 2.355 0.51 324948. 0.1236 69.57 0.5830 0.6386 0.0117 0.0106 0.756 7.938 2.601 563.470 0.897 11.571 2.094 0.51 325630. 0.0944 72.24 0.6054 0.5446 0.0075 0.0083 0.591 6.206 1.670 440.526 0.701 7.429 1.720 0.51 326331. 0.0621 74.92 0.6279 0.3537 0.0033 0.0059 0.418 4.387 0.739 311.392 0.496 3.289 1.077 0.51 327049. 0.0259 77.59 0.6503 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 0.0957 0.0306 3.450 31.065 29.059 2572.742 3.510 129.257 5.123 0.58 366869. 0.7717 3.10 0.0223 0.0676 0.0940 0.0309 3.489 31.411 28.540 2601.387 3.549 126.944 4.976 0.58 367106. 0.7428 6.20 0.0445 0.1313 0.0921 0.0312 3.522 31.715 27.982 2626.582 3.583 124.463 4.832 0.58 367359. 0.7142 9.30 0.0668 0.1913 0.0902 0.0315 3.551 31.970 27.386 2647.709 3.612 121.811 4.691 0.58 367631. 0.6860 12.40 0.0891 0.2476 0.0881 0.0317 3.573 32.169 26.750 2664.179 3.634 118.983 4.554 0.58 367920. 0.6581 15.50 0.1114 0.3004 0.0859 0.0318 3.588 32.304 26.073 2675.382 3.650 115.974 4.420 0.58 368229. 0.6307 18.60 0.1336 0.3499 0.0835 0.0319 3.595 32.368 25.355 2680.694 3.657 112.780 4.290 0.58 368557. 0.6036 21.70 0.1559 0.3961 0.0810 0.0319 3.593 32.354 24.595 2679.482 3.655 109.397 4.163 0.58 368905. 0.5769 24.80 0.1782 0.4393 0.0783 0.0318 3.582 32.253 23.791 2671.106 3.644 105.823 4.040 0.58 369273. 0.5506 27.90 0.2004 0.4795 0.0756 0.0316 3.560 32.058 22.945 2655.002 3.622 102.060 3.920 0.58 369662. 0.5246 31.00 0.2227 0.5169 0.0726 0.0313 3.528 31.765 22.058 2630.729 3.589 98.115 3.803 0.58 370073. 0.4991 34.10 0.2450 0.5516 0.0696 0.0309 3.484 31.369 21.132 2597.932 3.544 93.994 3.689 0.58 370505. 0.4739 37.20 0.2673 0.5837 0.0664 0.0304 3.428 30.867 20.168 2556.314 3.487 89.709 3.579 0.59 370958. 0.4490 40.30 0.2895 0.6131 0.0631 0.0298 3.360 30.254 19.170 2505.606 3.418 85.268 3.470 0.59 371434. 0.4245 43.40 0.3118 0.6401 0.0597 0.0291 3.280 29.529 18.138 2445.535 3.336 80.679 3.364 0.59 371933. 0.4003 46.50 0.3341 0.6646 0.0562 0.0283 3.186 28.687 17.075 2375.847 3.241 75.951 3.260 0.59 372454. 0.3764 49.60 0.3563 0.6865 0.0526 0.0273 3.079 27.727 15.983 2296.290 3.133 71.093 3.157 0.59 372998. 0.3527 52.71 0.3786 0.7059 0.0489 0.0263 2.959 26.644 14.863 2206.624 3.010 66.112 3.055 0.59 373565. 0.3291 55.81 0.4009 0.7226 0.0452 0.0251 2.825 25.437 13.717 2106.623 2.874 61.015 2.953 0.59 374157. 0.3056 58.91 0.4232 0.7363 0.0413 0.0237 2.677 24.102 12.548 1996.086 2.723 55.811 2.851 0.59 374772. 0.2822 62.01 0.4454 0.7468 0.0374 0.0223 2.514 22.638 11.355 1874.839 2.558 50.509 2.747 0.59 375411. 0.2587 65.11 0.4677 0.7535 0.0334 0.0207 2.337 21.043 10.143 1742.740 2.377 45.116 2.640 0.59 376074. 0.2349 68.21 0.4900 0.7556 0.0293 0.0190 2.145 19.316 8.912 1599.695 2.182 39.641 2.527 0.59 376761. 0.2108 71.31 0.5122 0.7518 0.0252 0.0172 1.939 17.456 7.665 1445.667 1.972 34.095 2.405 0.59 377474. 0.1860 74.41 0.5345 0.7399 0.0211 0.0152 1.717 15.464 6.405 1280.694 1.747 28.489 2.268 0.59 378210. 0.1604 77.51 0.5568 0.7161 0.0169 0.0131 1.482 13.341 5.134 1104.898 1.507 22.836 2.108 0.59 378972. 0.1334 80.61 0.5791 0.6728 0.0127 0.0109 1.232 11.091 3.856 918.512 1.253 17.150 1.904 0.59 379757. 0.1045 83.71 0.6013 0.5934 0.0085 0.0086 0.968 8.716 2.574 721.878 0.985 11.448 1.617 0.59 380567. 0.0725 86.81 0.6236 0.4326 0.0043 0.0061 0.691 6.223 1.292 515.348 0.703 5.745 1.137 0.59 381397. 0.0361 89.91 0.6459 -0.0198 -0.0001 0.0035 0.391 3.517 -0.032 291.311 0.397 -0.144 -0.050 0.60 382051. 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 0.0975 0.0313 5.260 41.442 38.674 3922.490 4.682 172.024 4.472 0.67 419216. 0.7771 3.55 0.0223 0.0676 0.0958 0.0316 5.319 41.907 37.993 3966.490 4.735 168.995 4.345 0.67 419488. 0.7482 7.10 0.0446 0.1313 0.0939 0.0319 5.371 42.315 37.261 4005.135 4.781 165.737 4.220 0.67 419781. 0.7197 10.65 0.0669 0.1912 0.0920 0.0322 5.414 42.657 36.476 4037.431 4.819 162.247 4.098 0.67 420094. 0.6915 14.19 0.0892 0.2476 0.0898 0.0324 5.448 42.921 35.638 4062.460 4.849 158.519 3.979 0.67 420429. 0.6637 17.74 0.1115 0.3005 0.0876 0.0325 5.470 43.099 34.745 4079.272 4.869 154.545 3.863 0.67 420785. 0.6363 21.29 0.1338 0.3501 0.0852 0.0326 5.481 43.180 33.795 4086.929 4.878 150.320 3.751 0.67 421164. 0.6092 24.84 0.1561 0.3965 0.0827 0.0326 5.477 43.154 32.788 4084.454 4.875 145.840 3.641 0.67 421565. 0.5825 28.39 0.1784 0.4399 0.0800 0.0324 5.459 43.010 31.722 4070.869 4.859 141.101 3.534 0.67 421990. 0.5562 31.94 0.2007 0.4803 0.0771 0.0322 5.425 42.740 30.599 4045.295 4.829 136.105 3.431 0.67 422439. 0.5303 35.48 0.2230 0.5180 0.0742 0.0319 5.374 42.336 29.420 4007.048 4.783 130.860 3.330 0.67 422912. 0.5047 39.03 0.2453 0.5531 0.0711 0.0315 5.305 41.792 28.188 3955.605 4.722 125.379 3.232 0.67 423410. 0.4795 42.58 0.2677 0.5855 0.0678 0.0310 5.217 41.105 26.905 3890.523 4.644 119.673 3.137 0.67 423932. 0.4546 46.13 0.2900 0.6155 0.0645 0.0304 5.111 40.269 25.575 3811.408 4.550 113.755 3.043 0.67 424480. 0.4300 49.68 0.3123 0.6430 0.0610 0.0296 4.986 39.281 24.199 3717.880 4.438 107.639 2.952 0.67 425054. 0.4058 53.23 0.3346 0.6680 0.0574 0.0288 4.840 38.136 22.782 3609.558 4.309 101.334 2.863 0.67 425654. 0.3818 56.77 0.3569 0.6906 0.0538 0.0278 4.675 36.831 21.325 3486.073 4.161 94.852 2.775 0.67 426280. 0.3580 60.32 0.3792 0.7106 0.0500 0.0267 4.488 35.363 19.830 3347.073 3.995 88.204 2.687 0.67 426932. 0.3344 63.87 0.4015 0.7281 0.0461 0.0254 4.281 33.727 18.300 3192.220 3.810 81.400 2.600 0.67 427612. 0.3108 67.42 0.4238 0.7427 0.0422 0.0241 4.052 31.920 16.738 3021.212 3.606 74.451 2.513 0.67 428319. 0.2873 70.97 0.4461 0.7542 0.0382 0.0226 3.800 29.940 15.145 2833.790 3.383 67.367 2.424 0.67 429053. 0.2636 74.52 0.4684 0.7621 0.0341 0.0210 3.527 27.784 13.525 2629.743 3.139 60.160 2.333 0.67 429814. 0.2397 78.07 0.4907 0.7655 0.0300 0.0192 3.230 25.451 11.880 2408.933 2.875 52.843 2.237 0.67 430604. 0.2154 81.61 0.5130 0.7633 0.0257 0.0173 2.912 22.940 10.213 2171.304 2.592 45.427 2.133 0.68 431421. 0.1905 85.16 0.5353 0.7533 0.0215 0.0153 2.571 20.253 8.527 1916.915 2.288 37.929 2.018 0.68 432267. 0.1646 88.71 0.5576 0.7316 0.0172 0.0131 2.207 17.390 6.827 1645.961 1.965 30.366 1.881 0.68 433140. 0.1373 92.26 0.5799 0.6907 0.0129 0.0108 1.822 14.356 5.116 1358.803 1.622 22.757 1.708 0.68 434041. 0.1079 95.81 0.6022 0.6134 0.0086 0.0084 1.416 11.157 3.400 1055.973 1.260 15.124 1.460 0.68 434969. 0.0752 99.36 0.6245 0.4507 0.0042 0.0059 0.990 7.797 1.683 738.006 0.881 7.488 1.035 0.68 435920. 0.0375 102.90 0.6468 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 0.0997 0.0326 7.820 54.763 50.071 5831.231 6.187 222.714 3.895 0.75 471526. 0.7700 4.02 0.0225 0.0669 0.0980 0.0329 7.893 55.276 49.205 5885.855 6.245 218.865 3.792 0.75 471838. 0.7432 8.04 0.0449 0.1301 0.0962 0.0332 7.956 55.718 48.271 5932.936 6.295 214.708 3.690 0.75 472173. 0.7164 12.07 0.0674 0.1899 0.0942 0.0334 8.007 56.077 47.266 5971.097 6.336 210.238 3.590 0.75 472532. 0.6897 16.09 0.0899 0.2463 0.0920 0.0336 8.045 56.339 46.188 5999.043 6.365 205.444 3.492 0.75 472915. 0.6631 20.11 0.1124 0.2994 0.0897 0.0337 8.067 56.494 45.036 6015.466 6.383 200.320 3.396 0.75 473324. 0.6367 24.13 0.1348 0.3492 0.0873 0.0337 8.072 56.526 43.808 6018.957 6.386 194.858 3.301 0.75 473758. 0.6105 28.15 0.1573 0.3960 0.0847 0.0336 8.057 56.424 42.503 6008.078 6.375 189.053 3.209 0.75 474219. 0.5845 32.18 0.1798 0.4398 0.0819 0.0335 8.021 56.173 41.120 5981.347 6.346 182.901 3.118 0.75 474707. 0.5587 36.20 0.2022 0.4808 0.0790 0.0332 7.962 55.760 39.659 5937.348 6.300 176.403 3.030 0.75 475222. 0.5331 40.22 0.2247 0.5189 0.0759 0.0329 7.878 55.174 38.123 5874.954 6.234 169.570 2.943 0.75 475764. 0.5078 44.24 0.2472 0.5545 0.0727 0.0324 7.769 54.407 36.515 5793.292 6.147 162.418 2.859 0.75 476335. 0.4827 48.26 0.2697 0.5874 0.0694 0.0319 7.633 53.452 34.839 5691.625 6.039 154.965 2.776 0.75 476934. 0.4579 52.28 0.2921 0.6179 0.0659 0.0312 7.469 52.303 33.100 5569.301 5.909 147.229 2.696 0.75 477563. 0.4333 56.31 0.3146 0.6459 0.0623 0.0304 7.276 50.955 31.301 5425.689 5.757 139.226 2.617 0.75 478220. 0.4090 60.33 0.3371 0.6715 0.0587 0.0294 7.054 49.400 29.445 5260.186 5.581 130.973 2.539 0.75 478907. 0.3850 64.35 0.3595 0.6947 0.0549 0.0284 6.802 47.635 27.537 5072.193 5.382 122.484 2.462 0.75 479624. 0.3610 68.37 0.3820 0.7154 0.0510 0.0272 6.519 45.653 25.579 4861.141 5.158 113.774 2.387 0.76 480371. 0.3373 72.39 0.4045 0.7335 0.0470 0.0259 6.204 43.449 23.574 4626.526 4.909 104.856 2.311 0.76 481148. 0.3135 76.42 0.4270 0.7488 0.0429 0.0244 5.857 41.021 21.525 4367.908 4.634 95.744 2.235 0.76 481957. 0.2898 80.44 0.4494 0.7610 0.0387 0.0229 5.478 38.363 19.436 4084.901 4.334 86.453 2.158 0.76 482796. 0.2658 84.46 0.4719 0.7697 0.0345 0.0211 5.065 35.473 17.311 3777.233 4.008 76.998 2.079 0.76 483667. 0.2416 88.48 0.4944 0.7739 0.0302 0.0193 4.620 32.351 15.152 3444.802 3.655 67.394 1.995 0.76 484569. 0.2170 92.50 0.5168 0.7722 0.0258 0.0173 4.141 28.998 12.963 3087.707 3.276 57.661 1.904 0.76 485503. 0.1916 96.53 0.5393 0.7624 0.0214 0.0151 3.629 25.416 10.750 2706.346 2.872 47.816 1.802 0.76 486468. 0.1651 100.55 0.5618 0.7399 0.0170 0.0129 3.086 21.614 8.517 2301.458 2.442 37.884 1.679 0.76 487465. 0.1369 104.57 0.5843 0.6956 0.0125 0.0105 2.513 17.601 6.270 1874.181 1.989 27.890 1.517 0.76 488494. 0.1062 108.59 0.6067 0.6081 0.0080 0.0080 1.912 13.393 4.016 1426.058 1.513 17.864 1.277 0.76 489553. 0.0715 112.61 0.6292 0.4112 0.0035 0.0054 1.285 9.002 1.760 958.540 1.017 7.829 0.833 0.76 490634. 0.0309 116.63 0.6517 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 0.1024 0.0369 12.122 76.406 63.474 9039.746 8.632 282.331 3.185 0.83 523785. 0.7090 4.46 0.0224 0.0611 0.1007 0.0370 12.157 76.623 62.424 9065.463 8.657 277.661 3.123 0.83 524134. 0.6895 8.93 0.0449 0.1198 0.0989 0.0370 12.176 76.741 61.284 9079.323 8.670 272.590 3.062 0.83 524510. 0.6697 13.39 0.0673 0.1761 0.0969 0.0370 12.176 76.746 60.052 9079.968 8.671 267.109 3.000 0.83 524913. 0.6495 17.85 0.0898 0.2299 0.0948 0.0370 12.158 76.628 58.724 9066.008 8.657 261.204 2.938 0.83 525343. 0.6291 22.31 0.1122 0.2813 0.0925 0.0369 12.118 76.375 57.299 9036.064 8.629 254.864 2.876 0.83 525802. 0.6083 26.78 0.1346 0.3304 0.0900 0.0367 12.054 75.975 55.774 8988.752 8.584 248.081 2.814 0.83 526289. 0.5873 31.24 0.1571 0.3770 0.0874 0.0364 11.965 75.416 54.147 8922.649 8.521 240.846 2.752 0.83 526806. 0.5659 35.70 0.1795 0.4211 0.0846 0.0361 11.850 74.687 52.418 8836.305 8.438 233.157 2.691 0.83 527353. 0.5443 40.16 0.2020 0.4629 0.0816 0.0356 11.705 73.773 50.588 8728.235 8.335 225.015 2.629 0.83 527930. 0.5224 44.63 0.2244 0.5022 0.0785 0.0351 11.529 72.666 48.659 8597.235 8.210 216.435 2.567 0.84 528539. 0.5003 49.09 0.2468 0.5392 0.0752 0.0344 11.321 71.357 46.636 8442.354 8.062 207.435 2.506 0.84 529178. 0.4781 53.55 0.2693 0.5738 0.0718 0.0337 11.080 69.838 44.524 8262.693 7.890 198.041 2.444 0.84 529849. 0.4557 58.01 0.2917 0.6060 0.0683 0.0329 10.805 68.102 42.328 8057.307 7.694 188.274 2.383 0.84 530552. 0.4332 62.48 0.3142 0.6359 0.0646 0.0319 10.494 66.141 40.053 7825.227 7.473 178.156 2.322 0.84 531286. 0.4105 66.94 0.3366 0.6634 0.0608 0.0309 10.146 63.946 37.704 7565.555 7.225 167.708 2.260 0.84 532054. 0.3878 71.40 0.3591 0.6884 0.0569 0.0297 9.759 61.510 35.285 7277.378 6.949 156.950 2.199 0.84 532854. 0.3650 75.87 0.3815 0.7110 0.0529 0.0284 9.333 58.826 32.802 6959.770 6.646 145.902 2.138 0.84 533688. 0.3421 80.33 0.4039 0.7309 0.0488 0.0270 8.866 55.884 30.257 6611.747 6.314 134.582 2.076 0.84 534555. 0.3190 84.79 0.4264 0.7481 0.0446 0.0254 8.358 52.677 27.655 6232.367 5.951 123.009 2.013 0.84 535456. 0.2957 89.25 0.4488 0.7615 0.0403 0.0238 7.813 49.244 24.999 5826.141 5.564 111.197 1.946 0.84 536390. 0.2719 93.72 0.4713 0.7702 0.0360 0.0220 7.234 45.592 22.294 5394.053 5.151 99.163 1.875 0.84 537360. 0.2473 98.18 0.4937 0.7735 0.0315 0.0201 6.614 41.689 19.543 4932.309 4.710 86.929 1.797 0.84 538363. 0.2220 102.64 0.5161 0.7697 0.0270 0.0181 5.957 37.548 16.753 4442.404 4.242 74.517 1.710 0.84 539401. 0.1956 107.10 0.5386 0.7555 0.0225 0.0160 5.265 33.187 13.928 3926.360 3.749 61.951 1.609 0.85 540474. 0.1678 111.57 0.5610 0.7255 0.0179 0.0138 4.541 28.624 11.075 3386.533 3.234 49.259 1.483 0.85 541582. 0.1379 116.03 0.5835 0.6694 0.0132 0.0115 3.790 23.887 8.200 2826.120 2.699 36.474 1.316 0.85 542724. 0.1053 120.49 0.6059 0.5660 0.0086 0.0092 3.016 19.007 5.313 2248.804 2.147 23.632 1.072 0.85 543899. 0.0690 124.95 0.6283 0.3626 0.0039 0.0068 2.223 14.014 2.420 1657.973 1.583 10.764 0.662 0.85 545100. 0.0288 129.42 0.6508 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 0.1041 0.0452 19.767 113.264 78.051 14740.538 12.797 347.172 2.402 0.92 576066. 0.5929 4.90 0.0224 0.0509 0.1026 0.0452 19.758 113.213 76.913 14733.903 12.791 342.109 2.368 0.92 576443. 0.5802 9.80 0.0448 0.1003 0.1009 0.0451 19.714 112.959 75.659 14700.777 12.762 336.531 2.334 0.92 576850. 0.5673 14.70 0.0672 0.1483 0.0991 0.0449 19.631 112.481 74.284 14638.628 12.708 330.417 2.302 0.92 577288. 0.5543 19.60 0.0896 0.1950 0.0971 0.0446 19.506 111.764 72.783 14545.272 12.627 323.739 2.270 0.92 577757. 0.5410 24.49 0.1120 0.2403 0.0949 0.0442 19.337 110.796 71.151 14419.278 12.518 316.479 2.238 0.92 578259. 0.5275 29.39 0.1344 0.2844 0.0925 0.0437 19.123 109.572 69.385 14260.060 12.379 308.623 2.207 0.92 578794. 0.5136 34.29 0.1568 0.3271 0.0900 0.0431 18.864 108.088 67.482 14066.937 12.212 300.160 2.176 0.92 579363. 0.4994 39.19 0.1792 0.3685 0.0873 0.0424 18.559 106.339 65.441 13839.240 12.014 291.083 2.145 0.92 579966. 0.4848 44.09 0.2016 0.4085 0.0844 0.0416 18.206 104.320 63.262 13576.535 11.786 281.392 2.113 0.92 580603. 0.4697 48.99 0.2240 0.4471 0.0813 0.0407 17.807 102.033 60.949 13278.905 11.528 271.100 2.082 0.92 581275. 0.4541 53.89 0.2463 0.4842 0.0780 0.0397 17.362 99.483 58.506 12947.032 11.240 260.236 2.050 0.92 581982. 0.4380 58.79 0.2687 0.5198 0.0746 0.0386 16.872 96.677 55.943 12581.776 10.922 248.835 2.017 0.92 582723. 0.4215 63.69 0.2911 0.5536 0.0710 0.0374 16.339 93.618 53.266 12183.669 10.577 236.928 1.983 0.92 583500. 0.4044 68.59 0.3135 0.5858 0.0673 0.0360 15.761 90.306 50.482 11752.701 10.203 224.546 1.948 0.92 584313. 0.3868 73.48 0.3359 0.6161 0.0635 0.0346 15.138 86.739 47.598 11288.513 9.800 211.714 1.912 0.92 585161. 0.3687 78.38 0.3583 0.6445 0.0595 0.0331 14.471 82.915 44.618 10790.802 9.368 198.462 1.875 0.92 586045. 0.3500 83.28 0.3807 0.6707 0.0554 0.0315 13.758 78.831 41.551 10259.366 8.906 184.818 1.837 0.92 586966. 0.3309 88.18 0.4031 0.6946 0.0512 0.0297 13.000 74.486 38.401 9693.814 8.415 170.809 1.797 0.92 587923. 0.3111 93.08 0.4255 0.7160 0.0469 0.0279 12.194 69.872 35.176 9093.409 7.894 156.461 1.755 0.92 588916. 0.2908 97.98 0.4479 0.7340 0.0425 0.0259 11.347 65.017 31.879 8461.489 7.346 141.798 1.709 0.93 589947. 0.2696 102.88 0.4703 0.7421 0.0380 0.0241 10.538 60.381 28.507 7858.167 6.822 126.801 1.645 0.93 591015. 0.2455 107.78 0.4927 0.7364 0.0334 0.0224 9.782 56.047 25.065 7294.168 6.332 111.490 1.559 0.93 592120. 0.2180 112.68 0.5151 0.7198 0.0288 0.0206 9.003 51.586 21.569 6713.557 5.828 95.938 1.457 0.93 593262. 0.1891 117.57 0.5375 0.6884 0.0240 0.0188 8.210 47.040 18.026 6121.946 5.315 80.180 1.336 0.93 594442. 0.1584 122.47 0.5599 0.6371 0.0193 0.0169 7.405 42.432 14.447 5522.261 4.794 64.259 1.187 0.93 595659. 0.1260 127.37 0.5823 0.5580 0.0145 0.0151 6.599 37.813 10.842 4921.140 4.272 48.223 0.999 0.93 596914. 0.0919 132.27 0.6047 0.4395 0.0096 0.0133 5.798 33.220 7.224 4323.385 3.753 32.133 0.758 0.93 598205. 0.0569 137.17 0.6271 0.2635 0.0048 0.0114 5.008 28.693 3.608 3734.181 3.242 16.047 0.438 0.93 599527. 0.0233 142.07 0.6495 -0.0084 -0.0001 0.0095 4.162 23.847 -0.092 3103.552 2.694 -0.409 -0.013 0.94 600738. 0.0000