19x8E (19x8E.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 0.0742 0.0264 0.005 0.332 0.308 3.925 0.037 1.371 35.606 0.08 33326. 0.6104 0.35 0.0193 0.0530 0.0728 0.0266 0.005 0.334 0.302 3.946 0.038 1.345 34.741 0.08 33343. 0.5899 0.70 0.0387 0.1034 0.0713 0.0267 0.005 0.335 0.296 3.964 0.038 1.317 33.874 0.08 33361. 0.5692 1.04 0.0580 0.1511 0.0697 0.0268 0.005 0.336 0.289 3.977 0.038 1.287 33.008 0.08 33380. 0.5484 1.39 0.0774 0.1962 0.0680 0.0268 0.005 0.337 0.282 3.986 0.038 1.257 32.143 0.08 33400. 0.5276 1.74 0.0967 0.2386 0.0662 0.0269 0.005 0.337 0.275 3.990 0.038 1.224 31.279 0.08 33422. 0.5067 2.09 0.1161 0.2785 0.0644 0.0268 0.005 0.337 0.267 3.987 0.038 1.189 30.416 0.08 33444. 0.4857 2.44 0.1354 0.3156 0.0624 0.0268 0.005 0.336 0.259 3.979 0.038 1.153 29.553 0.08 33469. 0.4647 2.78 0.1548 0.3502 0.0604 0.0267 0.005 0.335 0.251 3.963 0.038 1.115 28.690 0.08 33494. 0.4436 3.13 0.1741 0.3821 0.0582 0.0265 0.005 0.333 0.242 3.941 0.038 1.075 27.825 0.08 33521. 0.4225 3.48 0.1934 0.4113 0.0559 0.0263 0.005 0.330 0.232 3.910 0.037 1.034 26.956 0.08 33550. 0.4013 3.83 0.2128 0.4378 0.0536 0.0260 0.005 0.327 0.223 3.870 0.037 0.990 26.081 0.08 33580. 0.3800 4.18 0.2321 0.4614 0.0511 0.0257 0.005 0.323 0.212 3.822 0.036 0.944 25.198 0.08 33612. 0.3586 4.52 0.2515 0.4821 0.0486 0.0253 0.005 0.318 0.202 3.764 0.036 0.897 24.303 0.08 33645. 0.3370 4.87 0.2708 0.4997 0.0459 0.0249 0.005 0.312 0.191 3.696 0.035 0.848 23.393 0.08 33679. 0.3154 5.22 0.2902 0.5141 0.0432 0.0244 0.005 0.306 0.179 3.619 0.035 0.797 22.462 0.08 33716. 0.2937 5.57 0.3095 0.5250 0.0403 0.0238 0.005 0.299 0.168 3.533 0.034 0.745 21.505 0.08 33754. 0.2718 5.92 0.3288 0.5322 0.0374 0.0231 0.005 0.291 0.156 3.438 0.033 0.692 20.517 0.08 33793. 0.2499 6.26 0.3482 0.5353 0.0345 0.0224 0.004 0.282 0.143 3.333 0.032 0.637 19.489 0.08 33835. 0.2278 6.61 0.3675 0.5338 0.0315 0.0217 0.004 0.272 0.131 3.219 0.031 0.581 18.412 0.08 33878. 0.2055 6.96 0.3869 0.5272 0.0284 0.0208 0.004 0.262 0.118 3.096 0.030 0.524 17.275 0.08 33922. 0.1832 7.31 0.4062 0.5147 0.0253 0.0199 0.004 0.250 0.105 2.963 0.028 0.467 16.063 0.08 33969. 0.1607 7.66 0.4256 0.4955 0.0221 0.0190 0.004 0.238 0.092 2.821 0.027 0.408 14.760 0.08 34017. 0.1381 8.01 0.4449 0.4682 0.0189 0.0180 0.004 0.226 0.079 2.671 0.026 0.349 13.342 0.08 34067. 0.1155 8.35 0.4643 0.4314 0.0157 0.0169 0.003 0.212 0.065 2.512 0.024 0.290 11.780 0.08 34119. 0.0929 8.70 0.4836 0.3828 0.0125 0.0158 0.003 0.198 0.052 2.345 0.022 0.231 10.036 0.08 34172. 0.0706 9.05 0.5029 0.3197 0.0093 0.0146 0.003 0.184 0.039 2.171 0.021 0.172 8.058 0.08 34227. 0.0489 9.40 0.5223 0.2379 0.0061 0.0134 0.003 0.168 0.025 1.990 0.019 0.113 5.774 0.08 34284. 0.0284 9.75 0.5416 0.1316 0.0029 0.0121 0.002 0.152 0.012 1.803 0.017 0.054 3.080 0.08 34343. 0.0105 10.09 0.5610 -0.0086 -0.0002 0.0108 0.002 0.136 -0.001 1.610 0.015 -0.003 -0.195 0.08 34403. 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 0.0745 0.0242 0.039 1.214 1.238 28.722 0.137 5.505 19.543 0.15 66652. 0.6714 0.71 0.0197 0.0591 0.0731 0.0243 0.039 1.222 1.214 28.919 0.138 5.398 19.035 0.15 66686. 0.6476 1.42 0.0394 0.1151 0.0715 0.0245 0.039 1.229 1.188 29.087 0.139 5.285 18.529 0.15 66722. 0.6238 2.13 0.0591 0.1680 0.0699 0.0246 0.039 1.235 1.161 29.220 0.140 5.166 18.028 0.15 66761. 0.6000 2.83 0.0787 0.2178 0.0682 0.0247 0.039 1.239 1.133 29.313 0.140 5.039 17.530 0.15 66803. 0.5762 3.54 0.0984 0.2646 0.0664 0.0247 0.039 1.241 1.103 29.361 0.140 4.905 17.037 0.15 66847. 0.5525 4.25 0.1181 0.3084 0.0645 0.0247 0.039 1.241 1.071 29.359 0.140 4.765 16.549 0.15 66893. 0.5289 4.96 0.1378 0.3492 0.0625 0.0247 0.039 1.238 1.038 29.302 0.140 4.616 16.064 0.15 66943. 0.5054 5.67 0.1575 0.3872 0.0604 0.0246 0.039 1.233 1.003 29.186 0.139 4.460 15.584 0.15 66996. 0.4819 6.38 0.1772 0.4222 0.0581 0.0244 0.039 1.226 0.966 29.004 0.138 4.297 15.106 0.15 67051. 0.4585 7.08 0.1969 0.4544 0.0558 0.0242 0.039 1.215 0.927 28.752 0.137 4.125 14.631 0.15 67110. 0.4352 7.79 0.2166 0.4836 0.0534 0.0239 0.038 1.201 0.887 28.425 0.136 3.946 14.157 0.15 67172. 0.4118 8.50 0.2362 0.5099 0.0509 0.0236 0.038 1.184 0.845 28.016 0.134 3.759 13.682 0.15 67237. 0.3885 9.21 0.2559 0.5332 0.0482 0.0232 0.037 1.163 0.801 27.525 0.131 3.565 13.206 0.15 67305. 0.3651 9.92 0.2756 0.5533 0.0455 0.0227 0.036 1.139 0.756 26.951 0.129 3.363 12.725 0.15 67376. 0.3417 10.63 0.2953 0.5701 0.0427 0.0221 0.035 1.111 0.709 26.293 0.126 3.155 12.238 0.15 67451. 0.3183 11.33 0.3150 0.5834 0.0398 0.0215 0.034 1.080 0.661 25.551 0.122 2.942 11.740 0.15 67529. 0.2949 12.04 0.3347 0.5929 0.0368 0.0208 0.033 1.045 0.612 24.724 0.118 2.723 11.229 0.15 67611. 0.2713 12.75 0.3544 0.5981 0.0338 0.0200 0.032 1.006 0.562 23.813 0.114 2.499 10.700 0.15 67696. 0.2477 13.46 0.3740 0.5987 0.0307 0.0192 0.031 0.964 0.510 22.817 0.109 2.270 10.146 0.15 67785. 0.2238 14.17 0.3937 0.5938 0.0276 0.0183 0.029 0.919 0.458 21.738 0.104 2.038 9.560 0.15 67877. 0.1998 14.88 0.4134 0.5827 0.0244 0.0173 0.028 0.870 0.405 20.574 0.098 1.803 8.934 0.15 67973. 0.1756 15.59 0.4331 0.5639 0.0212 0.0163 0.026 0.817 0.352 19.330 0.092 1.565 8.254 0.15 68072. 0.1512 16.29 0.4528 0.5359 0.0179 0.0151 0.024 0.761 0.298 18.006 0.086 1.325 7.502 0.15 68176. 0.1264 17.00 0.4725 0.4961 0.0147 0.0140 0.022 0.702 0.244 16.606 0.079 1.084 6.656 0.15 68282. 0.1015 17.71 0.4922 0.4411 0.0114 0.0127 0.020 0.640 0.190 15.134 0.072 0.843 5.682 0.15 68393. 0.0764 18.42 0.5118 0.3655 0.0082 0.0114 0.018 0.575 0.136 13.597 0.065 0.604 4.527 0.15 68507. 0.0515 19.13 0.5315 0.2609 0.0050 0.0101 0.016 0.507 0.082 12.001 0.057 0.366 3.111 0.15 68625. 0.0276 19.84 0.5512 0.1131 0.0018 0.0087 0.014 0.437 0.030 10.352 0.049 0.132 1.301 0.15 68746. 0.0069 20.54 0.5709 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 0.0748 0.0232 0.125 2.627 2.797 93.248 0.297 12.442 13.606 0.23 99976. 0.7028 1.06 0.0196 0.0613 0.0734 0.0234 0.126 2.647 2.744 93.949 0.299 12.204 13.246 0.23 100027. 0.6776 2.11 0.0391 0.1194 0.0719 0.0236 0.127 2.664 2.687 94.549 0.301 11.951 12.889 0.23 100081. 0.6525 3.17 0.0587 0.1742 0.0703 0.0237 0.127 2.677 2.627 95.031 0.302 11.683 12.536 0.23 100139. 0.6274 4.23 0.0783 0.2258 0.0686 0.0238 0.128 2.687 2.563 95.379 0.304 11.400 12.187 0.23 100201. 0.6025 5.28 0.0979 0.2742 0.0668 0.0238 0.128 2.693 2.496 95.576 0.304 11.100 11.843 0.23 100266. 0.5778 6.34 0.1174 0.3196 0.0649 0.0238 0.128 2.694 2.425 95.603 0.304 10.785 11.503 0.23 100336. 0.5532 7.39 0.1370 0.3620 0.0629 0.0238 0.128 2.689 2.350 95.444 0.304 10.453 11.167 0.23 100410. 0.5287 8.45 0.1566 0.4014 0.0608 0.0237 0.128 2.679 2.271 95.081 0.303 10.104 10.836 0.23 100488. 0.5043 9.51 0.1761 0.4380 0.0586 0.0236 0.127 2.662 2.189 94.497 0.301 9.738 10.508 0.23 100571. 0.4801 10.56 0.1957 0.4716 0.0563 0.0233 0.126 2.639 2.103 93.675 0.298 9.354 10.183 0.23 100658. 0.4560 11.62 0.2153 0.5023 0.0539 0.0231 0.124 2.609 2.013 92.593 0.295 8.953 9.860 0.23 100750. 0.4320 12.68 0.2348 0.5301 0.0513 0.0227 0.122 2.570 1.919 91.235 0.290 8.535 9.539 0.23 100847. 0.4081 13.73 0.2544 0.5550 0.0487 0.0223 0.120 2.524 1.821 89.593 0.285 8.099 9.218 0.23 100948. 0.3842 14.79 0.2740 0.5768 0.0460 0.0219 0.118 2.470 1.720 87.665 0.279 7.649 8.897 0.23 101055. 0.3603 15.85 0.2936 0.5955 0.0432 0.0213 0.115 2.407 1.615 85.448 0.272 7.183 8.573 0.23 101166. 0.3364 16.90 0.3131 0.6108 0.0403 0.0207 0.111 2.337 1.507 82.940 0.264 6.705 8.244 0.23 101282. 0.3126 17.96 0.3327 0.6226 0.0374 0.0200 0.107 2.258 1.397 80.139 0.255 6.215 7.908 0.23 101404. 0.2887 19.01 0.3523 0.6303 0.0344 0.0192 0.103 2.171 1.284 77.044 0.245 5.713 7.562 0.23 101530. 0.2647 20.07 0.3718 0.6337 0.0313 0.0184 0.099 2.075 1.169 73.655 0.234 5.202 7.202 0.23 101662. 0.2405 21.13 0.3914 0.6320 0.0282 0.0174 0.094 1.971 1.053 69.972 0.223 4.682 6.823 0.23 101799. 0.2162 22.18 0.4110 0.6243 0.0250 0.0165 0.089 1.859 0.934 65.999 0.210 4.155 6.419 0.23 101941. 0.1916 23.24 0.4305 0.6094 0.0218 0.0154 0.083 1.739 0.814 61.740 0.197 3.622 5.982 0.23 102089. 0.1667 24.30 0.4501 0.5857 0.0186 0.0143 0.077 1.612 0.693 57.204 0.182 3.085 5.499 0.23 102242. 0.1414 25.35 0.4697 0.5505 0.0153 0.0131 0.070 1.476 0.572 52.401 0.167 2.545 4.953 0.23 102400. 0.1157 26.41 0.4893 0.5001 0.0121 0.0118 0.063 1.334 0.451 47.346 0.151 2.006 4.320 0.23 102564. 0.0896 27.47 0.5088 0.4286 0.0088 0.0105 0.056 1.185 0.330 42.058 0.134 1.468 3.560 0.23 102734. 0.0632 28.52 0.5284 0.3262 0.0056 0.0091 0.049 1.030 0.210 36.561 0.116 0.935 2.609 0.23 102909. 0.0370 29.58 0.5480 0.1756 0.0025 0.0077 0.041 0.870 0.092 30.879 0.098 0.410 1.354 0.23 103088. 0.0127 30.63 0.5675 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 0.0753 0.0228 0.291 4.579 5.002 216.710 0.517 22.249 10.469 0.30 133297. 0.7231 1.40 0.0194 0.0625 0.0738 0.0230 0.293 4.615 4.907 218.413 0.521 21.827 10.191 0.30 133365. 0.6971 2.80 0.0389 0.1217 0.0723 0.0231 0.295 4.646 4.806 219.878 0.525 21.379 9.915 0.30 133437. 0.6713 4.20 0.0583 0.1775 0.0707 0.0232 0.296 4.671 4.700 221.064 0.528 20.904 9.643 0.30 133514. 0.6456 5.60 0.0778 0.2301 0.0690 0.0233 0.298 4.690 4.587 221.930 0.530 20.402 9.374 0.30 133596. 0.6200 7.00 0.0972 0.2795 0.0672 0.0234 0.298 4.700 4.468 222.437 0.531 19.872 9.110 0.30 133683. 0.5947 8.40 0.1167 0.3258 0.0653 0.0234 0.298 4.702 4.342 222.542 0.531 19.313 8.850 0.30 133775. 0.5695 9.80 0.1361 0.3691 0.0634 0.0234 0.298 4.695 4.210 222.205 0.530 18.725 8.593 0.30 133873. 0.5445 11.20 0.1556 0.4094 0.0613 0.0233 0.297 4.678 4.071 221.385 0.529 18.107 8.340 0.30 133977. 0.5197 12.60 0.1750 0.4468 0.0591 0.0231 0.295 4.650 3.925 220.039 0.525 17.459 8.091 0.30 134086. 0.4950 14.00 0.1945 0.4813 0.0568 0.0229 0.293 4.609 3.773 218.126 0.521 16.781 7.845 0.30 134202. 0.4706 15.40 0.2139 0.5130 0.0544 0.0227 0.289 4.556 3.613 215.598 0.515 16.071 7.601 0.30 134323. 0.4462 16.79 0.2334 0.5418 0.0519 0.0223 0.285 4.488 3.446 212.412 0.507 15.330 7.359 0.30 134451. 0.4219 18.19 0.2528 0.5678 0.0493 0.0219 0.280 4.407 3.273 208.548 0.498 14.559 7.119 0.30 134585. 0.3977 19.59 0.2723 0.5908 0.0466 0.0215 0.274 4.311 3.094 203.997 0.487 13.760 6.878 0.30 134726. 0.3736 20.99 0.2917 0.6108 0.0438 0.0209 0.267 4.200 2.908 198.754 0.474 12.937 6.637 0.30 134873. 0.3496 22.39 0.3111 0.6277 0.0409 0.0203 0.259 4.074 2.718 192.813 0.460 12.089 6.394 0.30 135026. 0.3255 23.79 0.3306 0.6410 0.0380 0.0196 0.250 3.934 2.523 186.168 0.444 11.220 6.146 0.30 135187. 0.3014 25.19 0.3500 0.6507 0.0350 0.0188 0.240 3.778 2.323 178.816 0.427 10.332 5.892 0.30 135354. 0.2773 26.59 0.3695 0.6562 0.0319 0.0180 0.229 3.608 2.119 170.754 0.408 9.425 5.629 0.30 135527. 0.2530 27.99 0.3889 0.6569 0.0288 0.0170 0.217 3.423 1.912 161.986 0.387 8.504 5.353 0.30 135708. 0.2286 29.39 0.4084 0.6520 0.0256 0.0160 0.205 3.223 1.702 152.517 0.364 7.569 5.060 0.30 135896. 0.2039 30.79 0.4278 0.6404 0.0224 0.0150 0.191 3.008 1.489 142.358 0.340 6.623 4.744 0.30 136090. 0.1788 32.19 0.4473 0.6204 0.0192 0.0138 0.176 2.779 1.275 131.527 0.314 5.670 4.396 0.30 136292. 0.1533 33.59 0.4667 0.5895 0.0159 0.0126 0.161 2.537 1.060 120.048 0.287 4.713 4.003 0.30 136501. 0.1273 34.99 0.4862 0.5440 0.0127 0.0114 0.145 2.281 0.844 107.956 0.258 3.755 3.547 0.31 136717. 0.1006 36.39 0.5056 0.4779 0.0095 0.0100 0.128 2.014 0.629 95.295 0.228 2.800 2.996 0.31 136941. 0.0734 37.79 0.5251 0.3811 0.0063 0.0086 0.110 1.735 0.417 82.120 0.196 1.853 2.300 0.31 137171. 0.0459 39.19 0.5445 0.2347 0.0031 0.0072 0.092 1.447 0.206 68.494 0.164 0.918 1.366 0.31 137408. 0.0192 40.59 0.5639 -0.0029 0.0000 0.0057 0.073 1.148 -0.002 54.350 0.130 -0.009 -0.017 0.31 137642. 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 0.0758 0.0226 0.562 7.090 7.874 419.443 0.801 35.024 8.515 0.38 166615. 0.7379 1.75 0.0195 0.0636 0.0744 0.0228 0.567 7.148 7.725 422.840 0.808 34.361 8.286 0.38 166700. 0.7113 3.50 0.0389 0.1237 0.0729 0.0229 0.571 7.197 7.567 425.762 0.813 33.656 8.061 0.38 166790. 0.6848 5.25 0.0584 0.1805 0.0713 0.0231 0.574 7.237 7.399 428.128 0.818 32.910 7.839 0.38 166887. 0.6585 7.00 0.0778 0.2339 0.0696 0.0231 0.576 7.267 7.221 429.858 0.821 32.121 7.620 0.38 166990. 0.6324 8.75 0.0973 0.2842 0.0677 0.0232 0.578 7.284 7.034 430.871 0.823 31.287 7.404 0.38 167099. 0.6065 10.50 0.1168 0.3312 0.0658 0.0232 0.578 7.287 6.836 431.084 0.823 30.408 7.193 0.38 167215. 0.5808 12.26 0.1362 0.3753 0.0638 0.0232 0.577 7.276 6.628 430.416 0.822 29.482 6.985 0.38 167338. 0.5553 14.01 0.1557 0.4163 0.0617 0.0231 0.575 7.248 6.409 428.784 0.819 28.509 6.780 0.38 167468. 0.5301 15.76 0.1751 0.4544 0.0595 0.0229 0.571 7.203 6.180 426.106 0.814 27.489 6.578 0.38 167605. 0.5050 17.51 0.1946 0.4897 0.0572 0.0227 0.566 7.139 5.940 422.296 0.807 26.420 6.380 0.38 167750. 0.4802 19.26 0.2141 0.5221 0.0548 0.0225 0.560 7.054 5.689 417.261 0.797 25.303 6.184 0.38 167903. 0.4555 21.01 0.2335 0.5516 0.0523 0.0221 0.551 6.946 5.426 410.914 0.785 24.135 5.989 0.38 168063. 0.4309 22.76 0.2530 0.5784 0.0496 0.0217 0.541 6.816 5.153 403.214 0.770 22.921 5.797 0.38 168231. 0.4064 24.51 0.2725 0.6022 0.0469 0.0212 0.529 6.663 4.870 394.143 0.753 21.663 5.604 0.38 168407. 0.3820 26.26 0.2919 0.6231 0.0441 0.0207 0.515 6.486 4.578 383.689 0.733 20.364 5.412 0.38 168591. 0.3576 28.01 0.3114 0.6408 0.0412 0.0200 0.499 6.286 4.278 371.837 0.710 19.029 5.218 0.38 168784. 0.3333 29.76 0.3308 0.6552 0.0382 0.0193 0.481 6.062 3.970 358.578 0.685 17.659 5.022 0.38 168984. 0.3090 31.51 0.3503 0.6660 0.0352 0.0185 0.461 5.814 3.655 343.903 0.657 16.258 4.821 0.38 169194. 0.2846 33.26 0.3698 0.6727 0.0321 0.0176 0.440 5.541 3.334 327.810 0.626 14.830 4.613 0.38 169411. 0.2601 35.01 0.3892 0.6748 0.0290 0.0167 0.416 5.245 3.007 310.302 0.593 13.377 4.396 0.38 169638. 0.2354 36.77 0.4087 0.6714 0.0258 0.0157 0.391 4.926 2.676 291.390 0.557 11.903 4.166 0.38 169873. 0.2104 38.52 0.4281 0.6614 0.0225 0.0146 0.364 4.583 2.341 271.098 0.518 10.414 3.917 0.38 170117. 0.1851 40.27 0.4476 0.6431 0.0193 0.0134 0.335 4.217 2.004 249.460 0.476 8.912 3.643 0.38 170369. 0.1592 42.02 0.4671 0.6138 0.0160 0.0122 0.304 3.829 1.664 226.527 0.433 7.403 3.332 0.38 170631. 0.1328 43.77 0.4865 0.5698 0.0128 0.0109 0.271 3.421 1.325 202.367 0.386 5.893 2.969 0.38 170902. 0.1055 45.52 0.5060 0.5043 0.0095 0.0095 0.237 2.993 0.987 177.071 0.338 4.388 2.527 0.38 171181. 0.0775 47.27 0.5254 0.4060 0.0063 0.0081 0.202 2.548 0.651 150.750 0.288 2.896 1.959 0.38 171470. 0.0488 49.02 0.5449 0.2526 0.0031 0.0067 0.166 2.088 0.320 123.531 0.236 1.424 1.175 0.38 171766. 0.0205 50.77 0.5644 -0.0093 -0.0001 0.0051 0.128 1.609 -0.009 95.211 0.182 -0.039 -0.042 0.38 172055. 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 0.0765 0.0225 0.970 10.194 11.444 723.677 1.152 50.901 7.172 0.45 199928. 0.7493 2.10 0.0195 0.0643 0.0751 0.0227 0.978 10.278 11.228 729.631 1.161 49.941 6.980 0.45 200030. 0.7223 4.20 0.0389 0.1251 0.0736 0.0229 0.985 10.350 10.998 734.749 1.169 48.920 6.789 0.45 200139. 0.6954 6.30 0.0584 0.1824 0.0719 0.0230 0.991 10.409 10.755 738.883 1.176 47.839 6.602 0.45 200256. 0.6687 8.40 0.0778 0.2364 0.0702 0.0231 0.995 10.451 10.498 741.895 1.181 46.694 6.418 0.45 200380. 0.6422 10.50 0.0973 0.2872 0.0684 0.0232 0.997 10.476 10.226 743.641 1.184 45.485 6.237 0.45 200511. 0.6159 12.61 0.1168 0.3348 0.0665 0.0232 0.998 10.480 9.939 743.977 1.184 44.209 6.059 0.45 200651. 0.5899 14.71 0.1362 0.3794 0.0645 0.0231 0.996 10.463 9.637 742.758 1.182 42.865 5.885 0.45 200799. 0.5642 16.81 0.1557 0.4210 0.0623 0.0231 0.992 10.422 9.320 739.840 1.177 41.453 5.713 0.45 200956. 0.5387 18.91 0.1751 0.4596 0.0601 0.0229 0.986 10.355 8.986 735.079 1.170 39.972 5.545 0.45 201121. 0.5133 21.01 0.1946 0.4954 0.0578 0.0227 0.977 10.260 8.637 728.324 1.159 38.419 5.379 0.45 201295. 0.4882 23.11 0.2141 0.5284 0.0553 0.0224 0.965 10.134 8.272 719.413 1.145 36.795 5.215 0.45 201479. 0.4633 25.21 0.2335 0.5586 0.0528 0.0221 0.950 9.976 7.891 708.193 1.127 35.099 5.054 0.45 201671. 0.4384 27.31 0.2530 0.5859 0.0501 0.0216 0.931 9.785 7.494 694.586 1.105 33.334 4.894 0.45 201874. 0.4137 29.41 0.2724 0.6105 0.0474 0.0211 0.910 9.559 7.083 678.561 1.080 31.505 4.734 0.45 202085. 0.3891 31.51 0.2919 0.6321 0.0445 0.0206 0.885 9.299 6.659 660.094 1.051 29.617 4.575 0.45 202307. 0.3646 33.61 0.3114 0.6506 0.0416 0.0199 0.857 9.004 6.222 639.163 1.017 27.675 4.415 0.45 202538. 0.3401 35.71 0.3308 0.6659 0.0386 0.0192 0.826 8.674 5.774 615.747 0.980 25.683 4.253 0.45 202779. 0.3156 37.82 0.3503 0.6777 0.0356 0.0184 0.791 8.309 5.316 589.834 0.939 23.646 4.088 0.46 203031. 0.2911 39.92 0.3697 0.6855 0.0324 0.0175 0.753 7.909 4.849 561.417 0.894 21.568 3.917 0.46 203292. 0.2664 42.02 0.3892 0.6888 0.0293 0.0165 0.711 7.473 4.374 530.503 0.844 19.454 3.739 0.46 203564. 0.2415 44.12 0.4087 0.6868 0.0260 0.0155 0.667 7.003 3.892 497.111 0.791 17.311 3.551 0.46 203846. 0.2163 46.22 0.4281 0.6783 0.0228 0.0144 0.619 6.498 3.404 461.283 0.734 15.143 3.347 0.46 204139. 0.1907 48.32 0.4476 0.6615 0.0195 0.0132 0.567 5.960 2.913 423.080 0.673 12.957 3.123 0.46 204443. 0.1646 50.42 0.4671 0.6340 0.0162 0.0119 0.513 5.390 2.419 382.591 0.609 10.762 2.868 0.46 204757. 0.1378 52.52 0.4865 0.5915 0.0129 0.0106 0.456 4.789 1.925 339.939 0.541 8.564 2.569 0.46 205082. 0.1101 54.62 0.5060 0.5272 0.0096 0.0092 0.396 4.160 1.433 295.283 0.470 6.375 2.202 0.46 205417. 0.0814 56.72 0.5254 0.4284 0.0063 0.0078 0.334 3.505 0.945 248.824 0.396 4.204 1.723 0.46 205763. 0.0517 58.82 0.5449 0.2700 0.0031 0.0063 0.269 2.828 0.463 200.784 0.320 2.062 1.047 0.46 206120. 0.0220 60.92 0.5644 -0.0127 -0.0001 0.0047 0.202 2.123 -0.016 150.714 0.240 -0.070 -0.048 0.46 206463. 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 0.0774 0.0227 1.548 13.940 15.752 1154.513 1.575 70.067 6.189 0.53 233235. 0.7585 2.45 0.0195 0.0647 0.0760 0.0228 1.561 14.056 15.457 1164.076 1.588 68.751 6.023 0.53 233355. 0.7312 4.90 0.0389 0.1259 0.0744 0.0230 1.572 14.155 15.142 1172.271 1.599 67.352 5.859 0.53 233483. 0.7041 7.35 0.0584 0.1836 0.0728 0.0231 1.581 14.234 14.809 1178.866 1.608 65.869 5.698 0.53 233619. 0.6771 9.80 0.0778 0.2380 0.0710 0.0232 1.587 14.292 14.456 1183.634 1.615 64.299 5.539 0.53 233764. 0.6504 12.25 0.0973 0.2892 0.0692 0.0233 1.591 14.325 14.082 1186.343 1.618 62.638 5.384 0.53 233919. 0.6240 14.70 0.1167 0.3372 0.0673 0.0233 1.591 14.330 13.688 1186.761 1.619 60.886 5.232 0.53 234082. 0.5978 17.15 0.1362 0.3821 0.0652 0.0232 1.589 14.304 13.273 1184.652 1.616 59.040 5.082 0.53 234256. 0.5718 19.60 0.1556 0.4241 0.0631 0.0231 1.582 14.245 12.837 1179.786 1.609 57.100 4.935 0.53 234439. 0.5461 22.05 0.1751 0.4632 0.0608 0.0230 1.572 14.151 12.379 1171.929 1.599 55.063 4.791 0.53 234633. 0.5206 24.50 0.1945 0.4994 0.0585 0.0228 1.557 14.017 11.899 1160.844 1.584 52.928 4.649 0.53 234837. 0.4953 26.95 0.2140 0.5328 0.0560 0.0225 1.537 13.841 11.397 1146.268 1.564 50.695 4.510 0.53 235051. 0.4702 29.40 0.2334 0.5635 0.0534 0.0221 1.513 13.620 10.872 1127.951 1.539 48.361 4.372 0.53 235277. 0.4452 31.85 0.2529 0.5914 0.0507 0.0217 1.483 13.352 10.326 1105.764 1.508 45.932 4.236 0.53 235513. 0.4204 34.30 0.2723 0.6166 0.0480 0.0212 1.448 13.036 9.760 1079.656 1.473 43.414 4.100 0.53 235760. 0.3956 36.75 0.2918 0.6389 0.0451 0.0206 1.408 12.673 9.176 1049.588 1.432 40.815 3.965 0.53 236019. 0.3709 39.20 0.3113 0.6582 0.0421 0.0199 1.362 12.262 8.575 1015.524 1.385 38.140 3.830 0.53 236289. 0.3463 41.65 0.3307 0.6743 0.0391 0.0192 1.311 11.802 7.958 977.433 1.333 35.396 3.693 0.53 236571. 0.3217 44.10 0.3502 0.6870 0.0360 0.0184 1.254 11.293 7.327 935.295 1.276 32.589 3.553 0.53 236865. 0.2970 46.55 0.3696 0.6958 0.0328 0.0174 1.192 10.736 6.683 889.098 1.213 29.726 3.409 0.53 237170. 0.2722 49.00 0.3891 0.7002 0.0296 0.0165 1.125 10.129 6.028 838.852 1.144 26.813 3.259 0.53 237488. 0.2471 51.45 0.4085 0.6994 0.0264 0.0154 1.052 9.474 5.364 784.594 1.070 23.859 3.101 0.53 237817. 0.2218 53.90 0.4280 0.6923 0.0231 0.0143 0.974 8.771 4.692 726.386 0.991 20.870 2.930 0.53 238159. 0.1960 56.35 0.4474 0.6771 0.0197 0.0130 0.891 8.022 4.015 664.330 0.906 17.857 2.741 0.53 238513. 0.1696 58.80 0.4669 0.6513 0.0164 0.0117 0.803 7.228 3.334 598.571 0.817 14.830 2.526 0.53 238879. 0.1425 61.25 0.4863 0.6104 0.0130 0.0104 0.710 6.391 2.653 529.308 0.722 11.800 2.273 0.53 239258. 0.1143 63.70 0.5058 0.5474 0.0097 0.0090 0.613 5.516 1.974 456.801 0.623 8.781 1.960 0.53 239649. 0.0850 66.15 0.5252 0.4487 0.0064 0.0075 0.511 4.605 1.301 381.378 0.520 5.786 1.547 0.53 240053. 0.0545 68.60 0.5447 0.2862 0.0031 0.0060 0.407 3.663 0.637 303.404 0.414 2.832 0.952 0.54 240468. 0.0234 71.05 0.5641 -0.0163 -0.0001 0.0044 0.298 2.681 -0.026 221.996 0.303 -0.114 -0.052 0.54 240864. 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 0.0785 0.0229 2.335 18.398 20.857 1741.355 2.079 92.772 5.433 0.60 266533. 0.7662 2.80 0.0194 0.0649 0.0770 0.0231 2.355 18.550 20.468 1755.766 2.096 91.041 5.287 0.60 266671. 0.7387 5.60 0.0389 0.1262 0.0754 0.0232 2.371 18.680 20.054 1768.071 2.110 89.199 5.144 0.60 266818. 0.7115 8.39 0.0583 0.1841 0.0738 0.0234 2.384 18.784 19.614 1777.913 2.122 87.245 5.004 0.60 266975. 0.6844 11.19 0.0778 0.2388 0.0720 0.0235 2.394 18.859 19.149 1784.948 2.131 85.175 4.866 0.60 267142. 0.6576 13.99 0.0972 0.2901 0.0702 0.0235 2.399 18.899 18.657 1788.822 2.135 82.985 4.731 0.60 267319. 0.6310 16.79 0.1166 0.3384 0.0682 0.0235 2.399 18.903 18.137 1789.180 2.136 80.672 4.598 0.60 267507. 0.6047 19.59 0.1361 0.3836 0.0662 0.0235 2.395 18.866 17.589 1785.671 2.131 78.235 4.468 0.60 267706. 0.5786 22.38 0.1555 0.4259 0.0640 0.0234 2.384 18.784 17.012 1777.941 2.122 75.671 4.340 0.60 267917. 0.5528 25.18 0.1750 0.4653 0.0617 0.0232 2.368 18.654 16.407 1765.638 2.108 72.979 4.215 0.60 268139. 0.5272 27.98 0.1944 0.5019 0.0593 0.0230 2.345 18.472 15.773 1748.405 2.087 70.158 4.092 0.60 268373. 0.5019 30.78 0.2138 0.5358 0.0568 0.0227 2.314 18.234 15.109 1725.852 2.060 67.204 3.971 0.60 268618. 0.4767 33.58 0.2333 0.5669 0.0542 0.0223 2.277 17.936 14.415 1697.594 2.026 64.117 3.851 0.60 268877. 0.4516 36.37 0.2527 0.5954 0.0515 0.0219 2.231 17.575 13.692 1663.424 1.986 60.903 3.733 0.60 269148. 0.4266 39.17 0.2721 0.6211 0.0487 0.0213 2.177 17.150 12.943 1623.267 1.938 57.570 3.616 0.61 269431. 0.4018 41.97 0.2916 0.6440 0.0458 0.0207 2.115 16.662 12.169 1577.064 1.882 54.128 3.500 0.61 269727. 0.3770 44.77 0.3110 0.6640 0.0428 0.0200 2.045 16.110 11.373 1524.767 1.820 50.585 3.383 0.61 270037. 0.3523 47.57 0.3305 0.6809 0.0397 0.0193 1.966 15.492 10.555 1466.329 1.750 46.950 3.265 0.61 270359. 0.3276 50.37 0.3499 0.6944 0.0366 0.0184 1.880 14.810 9.719 1401.716 1.673 43.230 3.145 0.61 270695. 0.3028 53.16 0.3693 0.7042 0.0334 0.0175 1.785 14.062 8.866 1330.919 1.589 39.434 3.021 0.61 271044. 0.2778 55.96 0.3888 0.7097 0.0301 0.0165 1.682 13.248 7.997 1253.953 1.497 35.573 2.893 0.61 271407. 0.2526 58.76 0.4082 0.7101 0.0268 0.0154 1.570 12.371 7.117 1170.871 1.398 31.654 2.757 0.61 271783. 0.2271 61.56 0.4277 0.7044 0.0234 0.0142 1.451 11.429 6.225 1081.768 1.291 27.690 2.610 0.61 272174. 0.2011 64.36 0.4471 0.6908 0.0200 0.0130 1.323 10.426 5.327 986.805 1.178 23.693 2.448 0.61 272578. 0.1745 67.15 0.4665 0.6665 0.0166 0.0116 1.188 9.363 4.424 886.199 1.058 19.676 2.264 0.61 272997. 0.1471 69.95 0.4860 0.6274 0.0132 0.0103 1.046 8.244 3.520 780.257 0.931 15.655 2.046 0.61 273429. 0.1185 72.75 0.5054 0.5659 0.0099 0.0088 0.898 7.072 2.619 669.377 0.799 11.647 1.774 0.61 273876. 0.0887 75.55 0.5249 0.4677 0.0065 0.0073 0.743 5.854 1.725 554.060 0.661 7.672 1.412 0.61 274337. 0.0573 78.35 0.5443 0.3020 0.0032 0.0057 0.583 4.595 0.843 434.871 0.519 3.749 0.879 0.61 274811. 0.0249 81.14 0.5637 -0.0197 -0.0001 0.0041 0.416 3.278 -0.038 310.250 0.370 -0.168 -0.055 0.61 275259. 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 0.0798 0.0233 3.380 23.669 26.835 2520.269 2.674 119.361 4.829 0.68 299821. 0.7726 3.14 0.0194 0.0648 0.0783 0.0235 3.407 23.863 26.338 2540.971 2.696 117.153 4.701 0.68 299977. 0.7451 6.29 0.0388 0.1261 0.0767 0.0236 3.431 24.028 25.810 2558.560 2.715 114.802 4.575 0.68 300144. 0.7179 9.43 0.0583 0.1841 0.0751 0.0237 3.450 24.159 25.248 2572.513 2.730 112.304 4.452 0.68 300321. 0.6908 12.58 0.0777 0.2388 0.0733 0.0238 3.463 24.252 24.653 2582.330 2.740 109.656 4.330 0.68 300510. 0.6640 15.72 0.0971 0.2902 0.0714 0.0239 3.470 24.300 24.023 2587.494 2.745 106.853 4.211 0.68 300711. 0.6374 18.87 0.1165 0.3386 0.0694 0.0239 3.470 24.300 23.357 2587.491 2.745 103.891 4.094 0.68 300924. 0.6111 22.01 0.1359 0.3840 0.0673 0.0238 3.462 24.247 22.655 2581.807 2.739 100.768 3.980 0.68 301149. 0.5850 25.16 0.1553 0.4265 0.0651 0.0237 3.446 24.135 21.915 2569.937 2.727 97.480 3.868 0.68 301387. 0.5592 28.30 0.1748 0.4662 0.0628 0.0236 3.421 23.961 21.139 2551.372 2.707 94.026 3.758 0.68 301637. 0.5336 31.44 0.1942 0.5032 0.0604 0.0233 3.387 23.719 20.325 2525.605 2.680 90.404 3.650 0.68 301901. 0.5082 34.59 0.2136 0.5374 0.0579 0.0230 3.342 23.404 19.472 2492.075 2.644 86.611 3.544 0.68 302179. 0.4830 37.73 0.2330 0.5690 0.0552 0.0226 3.286 23.011 18.580 2450.229 2.600 82.645 3.439 0.68 302471. 0.4578 40.88 0.2524 0.5979 0.0525 0.0222 3.218 22.537 17.651 2399.746 2.546 78.513 3.336 0.68 302776. 0.4329 44.02 0.2719 0.6241 0.0496 0.0216 3.139 21.981 16.688 2340.514 2.483 74.226 3.234 0.68 303096. 0.4080 47.17 0.2913 0.6476 0.0466 0.0210 3.047 21.342 15.692 2272.459 2.411 69.798 3.132 0.68 303430. 0.3832 50.31 0.3107 0.6683 0.0436 0.0203 2.944 20.619 14.667 2195.515 2.330 65.238 3.030 0.68 303778. 0.3584 53.46 0.3301 0.6860 0.0405 0.0195 2.829 19.812 13.615 2109.621 2.238 60.557 2.927 0.68 304141. 0.3335 56.60 0.3495 0.7004 0.0373 0.0186 2.702 18.921 12.537 2014.733 2.138 55.767 2.823 0.68 304519. 0.3086 59.74 0.3689 0.7111 0.0340 0.0176 2.562 17.945 11.438 1910.839 2.027 50.877 2.715 0.68 304912. 0.2836 62.89 0.3884 0.7177 0.0307 0.0166 2.411 16.885 10.319 1797.963 1.908 45.900 2.603 0.68 305320. 0.2583 66.03 0.4078 0.7194 0.0273 0.0155 2.248 15.742 9.184 1676.186 1.778 40.849 2.485 0.68 305744. 0.2326 69.18 0.4272 0.7150 0.0239 0.0143 2.073 14.516 8.035 1545.649 1.640 35.738 2.358 0.68 306183. 0.2064 72.32 0.4466 0.7030 0.0204 0.0130 1.886 13.210 6.876 1406.580 1.492 30.583 2.217 0.69 306637. 0.1795 75.47 0.4660 0.6805 0.0170 0.0116 1.689 11.827 5.710 1259.311 1.336 25.400 2.057 0.69 307108. 0.1518 78.61 0.4855 0.6432 0.0135 0.0102 1.481 10.371 4.544 1104.302 1.172 20.211 1.866 0.69 307594. 0.1229 81.75 0.5049 0.5833 0.0100 0.0087 1.263 8.848 3.381 942.162 1.000 15.037 1.628 0.69 308096. 0.0924 84.90 0.5243 0.4859 0.0066 0.0071 1.038 7.266 2.227 773.667 0.821 9.905 1.305 0.69 308614. 0.0602 88.04 0.5437 0.3176 0.0032 0.0055 0.804 5.632 1.088 599.699 0.636 4.839 0.823 0.69 309146. 0.0265 91.19 0.5631 -0.0222 -0.0002 0.0039 0.560 3.924 -0.051 417.781 0.443 -0.228 -0.056 0.69 309645. 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 0.0814 0.0239 4.757 29.983 33.795 3547.348 3.387 150.320 4.321 0.75 333094. 0.7758 3.49 0.0194 0.0644 0.0799 0.0241 4.792 30.206 33.177 3573.730 3.413 147.573 4.211 0.75 333268. 0.7490 6.98 0.0388 0.1254 0.0783 0.0242 4.822 30.395 32.519 3596.044 3.434 144.644 4.102 0.75 333455. 0.7223 10.46 0.0582 0.1832 0.0766 0.0243 4.846 30.542 31.819 3613.533 3.451 141.529 3.994 0.75 333654. 0.6957 13.95 0.0775 0.2378 0.0748 0.0244 4.862 30.643 31.075 3625.462 3.462 138.223 3.888 0.75 333866. 0.6693 17.44 0.0969 0.2892 0.0729 0.0244 4.869 30.691 30.288 3631.066 3.467 134.719 3.783 0.75 334090. 0.6430 20.93 0.1163 0.3377 0.0709 0.0244 4.867 30.678 29.454 3629.575 3.466 131.013 3.681 0.75 334328. 0.6169 24.42 0.1357 0.3832 0.0688 0.0244 4.855 30.599 28.575 3620.211 3.457 127.101 3.580 0.75 334580. 0.5910 27.90 0.1551 0.4259 0.0666 0.0242 4.831 30.447 27.648 3602.211 3.440 122.980 3.481 0.75 334845. 0.5653 31.39 0.1745 0.4658 0.0642 0.0241 4.794 30.215 26.674 3574.811 3.414 118.647 3.384 0.75 335125. 0.5398 34.88 0.1939 0.5030 0.0618 0.0238 4.744 29.898 25.652 3537.262 3.378 114.101 3.289 0.76 335420. 0.5145 38.37 0.2132 0.5375 0.0592 0.0235 4.679 29.488 24.581 3488.780 3.332 109.338 3.196 0.76 335730. 0.4893 41.85 0.2326 0.5695 0.0565 0.0231 4.598 28.979 23.461 3428.583 3.274 104.355 3.104 0.76 336055. 0.4643 45.34 0.2520 0.5989 0.0537 0.0226 4.501 28.367 22.293 3356.198 3.205 99.160 3.013 0.76 336395. 0.4393 48.83 0.2714 0.6257 0.0508 0.0220 4.387 27.651 21.081 3271.465 3.124 93.767 2.923 0.76 336751. 0.4144 52.32 0.2908 0.6498 0.0477 0.0214 4.257 26.830 19.828 3174.315 3.031 88.193 2.833 0.76 337123. 0.3896 55.81 0.3102 0.6712 0.0446 0.0206 4.110 25.903 18.536 3064.683 2.927 82.450 2.743 0.76 337510. 0.3648 59.29 0.3295 0.6896 0.0414 0.0198 3.946 24.871 17.210 2942.537 2.810 76.552 2.653 0.76 337914. 0.3399 62.78 0.3489 0.7048 0.0382 0.0189 3.765 23.733 15.853 2807.871 2.681 70.513 2.561 0.76 338334. 0.3149 66.27 0.3683 0.7164 0.0348 0.0179 3.568 22.489 14.466 2660.742 2.541 64.347 2.466 0.76 338771. 0.2897 69.76 0.3877 0.7240 0.0314 0.0168 3.354 21.141 13.055 2501.274 2.389 58.068 2.367 0.76 339224. 0.2642 73.25 0.4071 0.7265 0.0280 0.0157 3.124 19.691 11.622 2329.693 2.225 51.693 2.263 0.76 339695. 0.2382 76.73 0.4265 0.7230 0.0245 0.0144 2.878 18.141 10.171 2146.345 2.050 45.238 2.149 0.76 340182. 0.2117 80.22 0.4459 0.7115 0.0210 0.0131 2.617 16.496 8.706 1951.730 1.864 38.725 2.023 0.76 340686. 0.1844 83.71 0.4652 0.6894 0.0174 0.0118 2.342 14.762 7.233 1746.520 1.668 32.174 1.878 0.76 341208. 0.1560 87.20 0.4846 0.6518 0.0139 0.0103 2.054 12.945 5.758 1531.603 1.463 25.610 1.705 0.76 341747. 0.1264 90.68 0.5040 0.5908 0.0103 0.0088 1.754 11.056 4.286 1308.107 1.249 19.063 1.486 0.76 342304. 0.0950 94.17 0.5234 0.4909 0.0068 0.0073 1.445 9.106 2.825 1077.406 1.029 12.564 1.189 0.76 342878. 0.0617 97.66 0.5428 0.3190 0.0033 0.0057 1.128 7.109 1.381 841.036 0.803 6.145 0.745 0.76 343468. 0.0270 101.15 0.5622 -0.0208 -0.0001 0.0040 0.798 5.032 -0.062 595.388 0.569 -0.274 -0.047 0.77 344021. 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 0.0833 0.0257 6.807 39.004 41.885 5076.133 4.407 186.302 3.743 0.83 366345. 0.7480 3.83 0.0193 0.0615 0.0819 0.0257 6.825 39.106 41.134 5089.355 4.418 182.965 3.666 0.83 366539. 0.7261 7.65 0.0387 0.1204 0.0803 0.0258 6.836 39.169 40.332 5097.540 4.425 179.399 3.589 0.83 366747. 0.7038 11.48 0.0580 0.1767 0.0786 0.0258 6.839 39.187 39.478 5099.878 4.427 175.599 3.511 0.83 366968. 0.6813 15.31 0.0773 0.2304 0.0768 0.0258 6.833 39.154 38.570 5095.563 4.424 171.560 3.433 0.83 367202. 0.6585 19.13 0.0967 0.2814 0.0748 0.0257 6.817 39.063 37.606 5083.730 4.413 167.272 3.355 0.83 367451. 0.6354 22.96 0.1160 0.3299 0.0728 0.0256 6.790 38.907 36.585 5063.483 4.396 162.730 3.277 0.83 367714. 0.6122 26.79 0.1353 0.3757 0.0707 0.0255 6.751 38.680 35.506 5033.896 4.370 157.929 3.199 0.83 367993. 0.5887 30.61 0.1547 0.4189 0.0684 0.0253 6.697 38.373 34.367 4994.024 4.335 152.864 3.121 0.83 368287. 0.5651 34.44 0.1740 0.4595 0.0660 0.0250 6.629 37.980 33.169 4942.891 4.291 147.534 3.044 0.83 368597. 0.5413 38.27 0.1933 0.4976 0.0635 0.0247 6.544 37.493 31.910 4879.512 4.236 141.935 2.966 0.83 368922. 0.5174 42.09 0.2127 0.5331 0.0609 0.0243 6.441 36.904 30.590 4802.790 4.169 136.064 2.889 0.83 369265. 0.4934 45.92 0.2320 0.5660 0.0581 0.0238 6.318 36.203 29.208 4711.551 4.090 129.917 2.812 0.83 369623. 0.4693 49.74 0.2513 0.5963 0.0553 0.0233 6.176 35.387 27.766 4605.428 3.998 123.501 2.735 0.83 369999. 0.4450 53.57 0.2707 0.6238 0.0523 0.0227 6.015 34.464 26.267 4485.247 3.894 116.835 2.656 0.83 370391. 0.4204 57.40 0.2900 0.6484 0.0492 0.0220 5.834 33.429 24.716 4350.562 3.777 109.937 2.577 0.83 370801. 0.3956 61.22 0.3093 0.6699 0.0460 0.0212 5.633 32.278 23.117 4200.794 3.647 102.825 2.496 0.83 371228. 0.3706 65.05 0.3287 0.6882 0.0427 0.0204 5.413 31.013 21.474 4036.127 3.504 95.518 2.413 0.83 371672. 0.3454 68.88 0.3480 0.7029 0.0394 0.0195 5.171 29.629 19.791 3856.069 3.348 88.030 2.328 0.83 372134. 0.3198 72.70 0.3673 0.7136 0.0360 0.0185 4.909 28.130 18.071 3660.864 3.178 80.380 2.239 0.83 372614. 0.2939 76.53 0.3867 0.7196 0.0325 0.0175 4.628 26.518 16.319 3451.092 2.996 72.586 2.145 0.84 373112. 0.2676 80.36 0.4060 0.7197 0.0289 0.0163 4.328 24.801 14.538 3227.637 2.802 64.667 2.043 0.84 373628. 0.2406 84.18 0.4253 0.7126 0.0253 0.0151 4.012 22.985 12.735 2991.380 2.597 56.645 1.931 0.84 374163. 0.2128 88.01 0.4447 0.6962 0.0217 0.0139 3.679 21.081 10.914 2743.493 2.382 48.544 1.804 0.84 374717. 0.1841 91.84 0.4640 0.6672 0.0181 0.0126 3.333 19.098 9.080 2485.431 2.158 40.390 1.657 0.84 375289. 0.1542 95.66 0.4833 0.6208 0.0144 0.0112 2.976 17.050 7.242 2218.955 1.926 32.214 1.480 0.84 375880. 0.1230 99.49 0.5027 0.5497 0.0108 0.0098 2.610 14.953 5.407 1946.051 1.689 24.051 1.260 0.84 376490. 0.0905 103.32 0.5220 0.4411 0.0071 0.0084 2.238 12.824 3.584 1669.012 1.449 15.941 0.974 0.84 377118. 0.0569 107.14 0.5413 0.2730 0.0035 0.0070 1.864 10.682 1.782 1390.212 1.207 7.924 0.581 0.84 377765. 0.0240 110.97 0.5607 -0.0022 0.0000 0.0056 1.483 8.497 -0.011 1105.765 0.960 -0.049 -0.004 0.84 378394. 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 0.0853 0.0304 10.452 54.897 51.037 7793.945 6.202 227.012 2.970 0.90 399582. 0.6553 4.19 0.0194 0.0539 0.0839 0.0302 10.402 54.635 50.158 7756.721 6.173 223.102 2.933 0.90 399796. 0.6415 8.38 0.0388 0.1064 0.0823 0.0300 10.340 54.311 49.213 7710.810 6.136 218.901 2.895 0.90 400025. 0.6272 12.57 0.0582 0.1574 0.0806 0.0298 10.266 53.923 48.202 7655.625 6.092 214.404 2.856 0.90 400269. 0.6123 16.76 0.0776 0.2070 0.0788 0.0296 10.179 53.464 47.123 7590.495 6.040 209.601 2.816 0.90 400528. 0.5969 20.96 0.0971 0.2549 0.0769 0.0293 10.077 52.930 45.972 7514.728 5.980 204.482 2.775 0.90 400804. 0.5810 25.15 0.1165 0.3012 0.0748 0.0289 9.961 52.316 44.748 7427.569 5.911 199.038 2.733 0.91 401095. 0.5645 29.34 0.1359 0.3459 0.0727 0.0285 9.827 51.617 43.449 7328.312 5.832 193.263 2.689 0.91 401404. 0.5474 33.53 0.1553 0.3887 0.0704 0.0281 9.677 50.828 42.076 7216.224 5.742 187.152 2.645 0.91 401729. 0.5298 37.72 0.1747 0.4297 0.0679 0.0276 9.509 49.943 40.626 7090.563 5.642 180.703 2.599 0.91 402072. 0.5115 41.91 0.1941 0.4688 0.0654 0.0271 9.321 48.956 39.099 6950.536 5.531 173.913 2.551 0.91 402433. 0.4927 46.10 0.2135 0.5058 0.0627 0.0265 9.112 47.862 37.495 6795.149 5.407 166.778 2.503 0.91 402812. 0.4733 50.29 0.2329 0.5407 0.0599 0.0258 8.882 46.651 35.812 6623.199 5.271 159.292 2.452 0.91 403208. 0.4532 54.49 0.2524 0.5734 0.0569 0.0251 8.628 45.318 34.053 6433.985 5.120 151.468 2.401 0.91 403624. 0.4326 58.68 0.2718 0.6037 0.0539 0.0243 8.351 43.864 32.223 6227.558 4.956 143.328 2.347 0.91 404058. 0.4114 62.87 0.2912 0.6304 0.0507 0.0234 8.065 42.361 30.327 6014.231 4.786 134.893 2.287 0.91 404510. 0.3890 67.06 0.3106 0.6529 0.0474 0.0226 7.769 40.806 28.369 5793.408 4.610 126.184 2.221 0.91 404982. 0.3653 71.25 0.3300 0.6711 0.0441 0.0217 7.462 39.191 26.354 5564.103 4.428 117.225 2.148 0.91 405473. 0.3406 75.44 0.3494 0.6824 0.0406 0.0208 7.159 37.604 24.287 5338.817 4.248 108.029 2.063 0.91 405983. 0.3140 79.63 0.3688 0.6873 0.0371 0.0199 6.850 35.980 22.173 5108.171 4.065 98.626 1.969 0.91 406512. 0.2863 83.82 0.3882 0.6859 0.0335 0.0189 6.523 34.263 20.019 4864.430 3.871 89.044 1.867 0.91 407062. 0.2579 88.02 0.4077 0.6770 0.0298 0.0180 6.181 32.467 17.831 4609.424 3.668 79.311 1.755 0.91 407631. 0.2288 92.21 0.4271 0.6588 0.0261 0.0169 5.827 30.608 15.615 4345.514 3.458 69.454 1.630 0.91 408220. 0.1989 96.40 0.4465 0.6293 0.0224 0.0159 5.465 28.703 13.378 4075.033 3.243 59.506 1.489 0.91 408829. 0.1682 100.59 0.4659 0.5858 0.0186 0.0148 5.096 26.766 11.130 3800.083 3.024 49.504 1.328 0.91 409459. 0.1369 104.78 0.4853 0.5250 0.0148 0.0137 4.725 24.817 8.878 3523.310 2.804 39.491 1.143 0.92 410109. 0.1052 108.97 0.5047 0.4427 0.0111 0.0126 4.355 22.874 6.635 3247.486 2.584 29.513 0.927 0.92 410780. 0.0737 113.16 0.5241 0.3337 0.0074 0.0116 3.990 20.958 4.412 2975.426 2.368 19.626 0.673 0.92 411472. 0.0436 117.35 0.5435 0.1914 0.0037 0.0106 3.633 19.081 2.222 2709.070 2.156 9.882 0.372 0.92 412183. 0.0171 121.55 0.5629 0.0045 0.0001 0.0095 3.268 17.165 0.046 2436.992 1.939 0.204 0.009 0.92 412897. 0.0001