20x8E (20x8E.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 0.0707 0.0246 0.006 0.399 0.361 4.717 0.045 1.604 34.671 0.08 36848. 0.6108 0.35 0.0187 0.0524 0.0693 0.0247 0.006 0.401 0.353 4.739 0.045 1.572 33.823 0.08 36865. 0.5899 0.71 0.0373 0.1021 0.0678 0.0248 0.006 0.402 0.346 4.756 0.045 1.538 32.973 0.08 36884. 0.5688 1.06 0.0560 0.1493 0.0662 0.0248 0.006 0.403 0.338 4.769 0.046 1.502 32.123 0.08 36904. 0.5477 1.41 0.0746 0.1937 0.0646 0.0249 0.006 0.404 0.329 4.776 0.046 1.465 31.274 0.08 36925. 0.5265 1.77 0.0933 0.2356 0.0628 0.0249 0.006 0.404 0.320 4.777 0.046 1.425 30.426 0.08 36947. 0.5053 2.12 0.1119 0.2749 0.0610 0.0248 0.006 0.403 0.311 4.772 0.046 1.384 29.578 0.08 36971. 0.4841 2.47 0.1306 0.3115 0.0591 0.0248 0.006 0.402 0.301 4.758 0.045 1.341 28.730 0.08 36996. 0.4627 2.83 0.1492 0.3454 0.0571 0.0247 0.006 0.400 0.291 4.737 0.045 1.295 27.880 0.08 37022. 0.4414 3.18 0.1679 0.3767 0.0550 0.0245 0.006 0.398 0.280 4.707 0.045 1.248 27.028 0.08 37050. 0.4200 3.53 0.1865 0.4053 0.0528 0.0243 0.006 0.394 0.269 4.667 0.045 1.198 26.172 0.08 37079. 0.3985 3.89 0.2052 0.4312 0.0505 0.0240 0.006 0.390 0.258 4.617 0.044 1.146 25.310 0.08 37110. 0.3769 4.24 0.2238 0.4542 0.0482 0.0237 0.006 0.385 0.246 4.558 0.044 1.092 24.439 0.08 37143. 0.3553 4.59 0.2425 0.4743 0.0457 0.0234 0.006 0.379 0.233 4.488 0.043 1.037 23.557 0.08 37177. 0.3337 4.95 0.2611 0.4913 0.0432 0.0230 0.006 0.373 0.220 4.408 0.042 0.979 22.660 0.08 37212. 0.3120 5.30 0.2798 0.5051 0.0406 0.0225 0.006 0.365 0.207 4.317 0.041 0.920 21.743 0.08 37250. 0.2902 5.65 0.2985 0.5155 0.0379 0.0220 0.006 0.356 0.193 4.215 0.040 0.860 20.801 0.08 37289. 0.2683 6.01 0.3171 0.5221 0.0352 0.0214 0.006 0.347 0.179 4.103 0.039 0.798 19.830 0.08 37329. 0.2464 6.36 0.3358 0.5247 0.0324 0.0207 0.005 0.336 0.165 3.980 0.038 0.735 18.821 0.08 37371. 0.2244 6.71 0.3544 0.5228 0.0295 0.0200 0.005 0.325 0.151 3.846 0.037 0.670 17.766 0.08 37415. 0.2023 7.07 0.3731 0.5159 0.0266 0.0193 0.005 0.313 0.136 3.701 0.035 0.604 16.654 0.08 37461. 0.1801 7.42 0.3917 0.5032 0.0237 0.0185 0.005 0.300 0.121 3.545 0.034 0.538 15.472 0.08 37509. 0.1578 7.77 0.4104 0.4840 0.0207 0.0176 0.005 0.286 0.106 3.378 0.032 0.471 14.204 0.08 37558. 0.1355 8.13 0.4290 0.4569 0.0178 0.0167 0.004 0.271 0.091 3.202 0.031 0.403 12.828 0.08 37609. 0.1132 8.48 0.4477 0.4207 0.0148 0.0157 0.004 0.255 0.075 3.015 0.029 0.335 11.317 0.08 37662. 0.0911 8.83 0.4663 0.3730 0.0117 0.0147 0.004 0.238 0.060 2.818 0.027 0.266 9.635 0.08 37716. 0.0692 9.19 0.4850 0.3114 0.0087 0.0136 0.004 0.221 0.045 2.612 0.025 0.198 7.732 0.08 37773. 0.0479 9.54 0.5036 0.2317 0.0057 0.0125 0.003 0.203 0.029 2.398 0.023 0.130 5.542 0.08 37831. 0.0278 9.89 0.5223 0.1286 0.0028 0.0113 0.003 0.184 0.014 2.177 0.021 0.063 2.966 0.08 37891. 0.0104 10.25 0.5409 -0.0072 -0.0001 0.0101 0.003 0.165 -0.001 1.947 0.019 -0.003 -0.160 0.08 37952. 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 0.0710 0.0224 0.046 1.457 1.448 34.487 0.165 6.442 19.048 0.16 73695. 0.6725 0.71 0.0187 0.0576 0.0696 0.0226 0.047 1.466 1.420 34.690 0.166 6.314 18.560 0.16 73730. 0.6488 1.42 0.0374 0.1122 0.0681 0.0227 0.047 1.473 1.389 34.858 0.166 6.179 18.074 0.16 73767. 0.6250 2.12 0.0561 0.1638 0.0665 0.0228 0.047 1.479 1.357 34.985 0.167 6.036 17.592 0.16 73807. 0.6012 2.83 0.0747 0.2124 0.0649 0.0228 0.047 1.482 1.323 35.067 0.167 5.885 17.114 0.16 73849. 0.5776 3.54 0.0934 0.2582 0.0631 0.0228 0.047 1.483 1.288 35.097 0.168 5.727 16.640 0.16 73894. 0.5539 4.25 0.1121 0.3011 0.0613 0.0228 0.047 1.482 1.250 35.071 0.167 5.561 16.169 0.16 73941. 0.5304 4.95 0.1308 0.3411 0.0594 0.0228 0.047 1.478 1.211 34.983 0.167 5.387 15.702 0.16 73992. 0.5070 5.66 0.1495 0.3783 0.0574 0.0227 0.047 1.472 1.170 34.826 0.166 5.204 15.238 0.16 74045. 0.4836 6.37 0.1682 0.4127 0.0553 0.0225 0.046 1.462 1.127 34.595 0.165 5.013 14.777 0.16 74101. 0.4603 7.08 0.1869 0.4443 0.0531 0.0223 0.046 1.449 1.082 34.283 0.164 4.814 14.318 0.16 74160. 0.4370 7.79 0.2056 0.4731 0.0508 0.0221 0.045 1.432 1.035 33.888 0.162 4.606 13.859 0.16 74222. 0.4137 8.49 0.2242 0.4990 0.0484 0.0217 0.045 1.412 0.987 33.407 0.160 4.390 13.400 0.16 74287. 0.3906 9.20 0.2429 0.5220 0.0459 0.0214 0.044 1.388 0.937 32.839 0.157 4.167 12.939 0.16 74355. 0.3674 9.91 0.2616 0.5420 0.0434 0.0209 0.043 1.360 0.885 32.181 0.154 3.937 12.475 0.16 74426. 0.3443 10.62 0.2803 0.5587 0.0408 0.0205 0.042 1.328 0.832 31.432 0.150 3.700 12.004 0.16 74501. 0.3212 11.33 0.2990 0.5722 0.0381 0.0199 0.041 1.293 0.777 30.590 0.146 3.457 11.524 0.16 74579. 0.2981 12.03 0.3177 0.5820 0.0354 0.0193 0.040 1.253 0.721 29.655 0.142 3.208 11.032 0.16 74661. 0.2749 12.74 0.3364 0.5879 0.0326 0.0186 0.038 1.210 0.664 28.624 0.137 2.954 10.525 0.16 74745. 0.2516 13.45 0.3551 0.5894 0.0297 0.0179 0.037 1.162 0.606 27.499 0.131 2.696 9.996 0.16 74834. 0.2283 14.16 0.3737 0.5859 0.0268 0.0171 0.035 1.111 0.547 26.278 0.125 2.433 9.440 0.16 74925. 0.2048 14.86 0.3924 0.5767 0.0239 0.0162 0.033 1.055 0.487 24.962 0.119 2.166 8.849 0.16 75021. 0.1812 15.57 0.4111 0.5607 0.0209 0.0153 0.032 0.995 0.426 23.553 0.112 1.897 8.213 0.16 75120. 0.1574 16.28 0.4298 0.5365 0.0179 0.0144 0.030 0.932 0.365 22.052 0.105 1.626 7.517 0.16 75222. 0.1333 16.99 0.4485 0.5021 0.0149 0.0133 0.027 0.865 0.304 20.462 0.098 1.353 6.742 0.16 75328. 0.1091 17.70 0.4672 0.4547 0.0119 0.0122 0.025 0.794 0.243 18.788 0.090 1.080 5.861 0.16 75438. 0.0847 18.40 0.4859 0.3900 0.0089 0.0111 0.023 0.720 0.182 17.035 0.081 0.808 4.834 0.16 75551. 0.0604 19.11 0.5046 0.3018 0.0059 0.0099 0.020 0.643 0.121 15.209 0.073 0.537 3.602 0.16 75669. 0.0367 19.82 0.5232 0.1796 0.0030 0.0087 0.018 0.563 0.061 13.318 0.064 0.270 2.067 0.16 75789. 0.0149 20.53 0.5419 0.0041 0.0001 0.0074 0.015 0.480 0.001 11.356 0.054 0.005 0.046 0.16 75909. 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 0.0714 0.0216 0.150 3.155 3.275 111.981 0.356 14.568 13.266 0.24 110539. 0.7044 1.06 0.0187 0.0603 0.0700 0.0217 0.151 3.175 3.210 112.706 0.359 14.278 12.918 0.24 110592. 0.6790 2.13 0.0375 0.1174 0.0684 0.0219 0.152 3.192 3.141 113.310 0.361 13.972 12.574 0.24 110649. 0.6538 3.19 0.0562 0.1713 0.0669 0.0219 0.153 3.205 3.068 113.774 0.362 13.648 12.233 0.24 110709. 0.6287 4.26 0.0749 0.2221 0.0652 0.0220 0.153 3.214 2.992 114.079 0.363 13.308 11.896 0.24 110772. 0.6037 5.32 0.0937 0.2698 0.0634 0.0220 0.153 3.218 2.911 114.207 0.364 12.950 11.562 0.24 110840. 0.5788 6.39 0.1124 0.3146 0.0616 0.0220 0.153 3.216 2.827 114.139 0.363 12.573 11.233 0.24 110911. 0.5541 7.45 0.1312 0.3563 0.0597 0.0220 0.153 3.208 2.738 113.856 0.362 12.179 10.908 0.24 110987. 0.5295 8.52 0.1499 0.3952 0.0576 0.0219 0.152 3.193 2.645 113.335 0.361 11.765 10.586 0.24 111067. 0.5051 9.58 0.1686 0.4312 0.0555 0.0217 0.151 3.171 2.548 112.554 0.358 11.332 10.267 0.24 111152. 0.4808 10.65 0.1874 0.4644 0.0533 0.0215 0.150 3.141 2.446 111.493 0.355 10.880 9.951 0.24 111241. 0.4566 11.71 0.2061 0.4947 0.0510 0.0212 0.148 3.103 2.340 110.140 0.351 10.408 9.637 0.24 111334. 0.4325 12.77 0.2248 0.5222 0.0486 0.0209 0.145 3.057 2.230 108.488 0.345 9.920 9.324 0.24 111432. 0.4085 13.84 0.2436 0.5467 0.0461 0.0205 0.143 3.001 2.116 106.529 0.339 9.414 9.011 0.24 111535. 0.3846 14.90 0.2623 0.5683 0.0436 0.0201 0.140 2.937 1.999 104.255 0.332 8.892 8.697 0.24 111643. 0.3608 15.97 0.2810 0.5867 0.0409 0.0196 0.136 2.864 1.878 101.661 0.324 8.355 8.381 0.24 111756. 0.3370 17.03 0.2998 0.6019 0.0382 0.0190 0.132 2.782 1.755 98.740 0.314 7.804 8.060 0.24 111873. 0.3132 18.10 0.3185 0.6135 0.0355 0.0184 0.128 2.690 1.628 95.489 0.304 7.241 7.732 0.24 111996. 0.2894 19.16 0.3373 0.6213 0.0327 0.0177 0.123 2.589 1.498 91.904 0.293 6.665 7.395 0.24 112124. 0.2656 20.23 0.3560 0.6248 0.0298 0.0170 0.118 2.479 1.367 87.982 0.280 6.079 7.046 0.24 112257. 0.2416 21.29 0.3747 0.6234 0.0269 0.0161 0.112 2.359 1.233 83.724 0.267 5.483 6.679 0.24 112395. 0.2176 22.36 0.3935 0.6163 0.0239 0.0153 0.106 2.229 1.097 79.131 0.252 4.880 6.289 0.24 112539. 0.1932 23.42 0.4122 0.6025 0.0209 0.0143 0.100 2.091 0.960 74.207 0.236 4.270 5.868 0.24 112688. 0.1687 24.49 0.4309 0.5803 0.0179 0.0133 0.092 1.943 0.822 68.960 0.220 3.656 5.406 0.24 112842. 0.1438 25.55 0.4497 0.5474 0.0149 0.0122 0.085 1.786 0.683 63.400 0.202 3.039 4.887 0.24 113002. 0.1185 26.61 0.4684 0.5006 0.0119 0.0111 0.077 1.621 0.544 57.543 0.183 2.421 4.291 0.24 113168. 0.0929 27.68 0.4872 0.4346 0.0088 0.0099 0.069 1.448 0.406 51.407 0.164 1.806 3.582 0.24 113339. 0.0670 28.74 0.5059 0.3410 0.0059 0.0087 0.060 1.268 0.269 45.017 0.143 1.195 2.706 0.24 113515. 0.0412 29.81 0.5246 0.2051 0.0029 0.0074 0.051 1.082 0.133 38.398 0.122 0.591 1.570 0.24 113697. 0.0168 30.87 0.5434 -0.0038 0.0000 0.0061 0.042 0.888 -0.002 31.508 0.100 -0.009 -0.028 0.24 113875. 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 0.0718 0.0212 0.349 5.503 5.861 260.414 0.622 26.070 10.208 0.32 147381. 0.7251 1.42 0.0188 0.0619 0.0704 0.0213 0.352 5.540 5.745 262.184 0.626 25.552 9.938 0.32 147452. 0.6988 2.84 0.0375 0.1205 0.0689 0.0215 0.354 5.571 5.621 263.661 0.629 25.004 9.670 0.32 147528. 0.6727 4.26 0.0563 0.1758 0.0673 0.0215 0.355 5.595 5.491 264.797 0.632 24.426 9.406 0.32 147608. 0.6467 5.68 0.0750 0.2279 0.0656 0.0216 0.356 5.611 5.354 265.552 0.634 23.816 9.145 0.32 147693. 0.6209 7.10 0.0938 0.2768 0.0639 0.0216 0.357 5.618 5.210 265.877 0.635 23.176 8.888 0.32 147784. 0.5952 8.52 0.1125 0.3227 0.0620 0.0216 0.356 5.615 5.059 265.729 0.634 22.502 8.635 0.32 147879. 0.5698 9.95 0.1313 0.3656 0.0601 0.0216 0.355 5.601 4.900 265.057 0.633 21.796 8.385 0.32 147981. 0.5446 11.37 0.1500 0.4055 0.0580 0.0215 0.354 5.574 4.734 263.810 0.630 21.055 8.139 0.32 148088. 0.5195 12.79 0.1688 0.4426 0.0559 0.0213 0.351 5.535 4.559 261.933 0.625 20.280 7.895 0.32 148201. 0.4946 14.21 0.1875 0.4768 0.0537 0.0211 0.348 5.481 4.377 259.379 0.619 19.470 7.654 0.32 148320. 0.4698 15.63 0.2063 0.5081 0.0513 0.0208 0.343 5.412 4.188 256.116 0.611 18.626 7.416 0.32 148445. 0.4452 17.05 0.2251 0.5366 0.0489 0.0205 0.338 5.328 3.991 252.124 0.602 17.750 7.179 0.32 148576. 0.4208 18.47 0.2438 0.5622 0.0464 0.0201 0.332 5.227 3.787 247.385 0.591 16.844 6.943 0.32 148714. 0.3964 19.89 0.2626 0.5849 0.0438 0.0197 0.324 5.111 3.577 241.881 0.577 15.910 6.707 0.32 148858. 0.3722 21.31 0.2813 0.6045 0.0412 0.0192 0.316 4.978 3.361 235.597 0.562 14.948 6.470 0.32 149008. 0.3480 22.73 0.3001 0.6209 0.0385 0.0186 0.306 4.829 3.139 228.518 0.546 13.962 6.230 0.32 149166. 0.3238 24.15 0.3188 0.6339 0.0357 0.0180 0.296 4.662 2.912 220.632 0.527 12.952 5.986 0.32 149330. 0.2997 25.57 0.3376 0.6431 0.0329 0.0172 0.284 4.478 2.680 211.931 0.506 11.921 5.736 0.32 149501. 0.2755 27.00 0.3563 0.6481 0.0300 0.0165 0.271 4.277 2.444 202.409 0.483 10.871 5.477 0.32 149679. 0.2512 28.42 0.3751 0.6484 0.0270 0.0156 0.258 4.058 2.204 192.066 0.459 9.804 5.205 0.32 149863. 0.2267 29.84 0.3938 0.6432 0.0240 0.0147 0.243 3.823 1.961 180.905 0.432 8.724 4.917 0.32 150055. 0.2020 31.26 0.4126 0.6312 0.0210 0.0137 0.227 3.570 1.716 168.937 0.403 7.631 4.606 0.32 150255. 0.1770 32.68 0.4314 0.6109 0.0180 0.0127 0.209 3.300 1.468 156.180 0.373 6.531 4.264 0.32 150461. 0.1516 34.10 0.4501 0.5798 0.0150 0.0116 0.191 3.015 1.220 142.662 0.341 5.426 3.879 0.32 150675. 0.1257 35.52 0.4689 0.5343 0.0119 0.0104 0.172 2.714 0.971 128.417 0.307 4.321 3.431 0.32 150896. 0.0992 36.94 0.4876 0.4684 0.0089 0.0092 0.152 2.398 0.724 113.495 0.271 3.219 2.892 0.32 151124. 0.0722 38.36 0.5064 0.3722 0.0059 0.0080 0.131 2.070 0.478 97.954 0.234 2.126 2.213 0.32 151360. 0.0449 39.78 0.5251 0.2273 0.0029 0.0067 0.110 1.730 0.235 81.859 0.195 1.046 1.303 0.32 151602. 0.0185 41.20 0.5439 -0.0083 -0.0001 0.0053 0.087 1.375 -0.007 65.057 0.155 -0.029 -0.046 0.32 151837. 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 0.0724 0.0210 0.677 8.530 9.235 504.598 0.964 41.079 8.301 0.40 184219. 0.7401 1.78 0.0188 0.0629 0.0710 0.0212 0.681 8.589 9.052 508.112 0.970 40.264 8.081 0.40 184308. 0.7133 3.55 0.0375 0.1225 0.0695 0.0213 0.685 8.639 8.858 511.038 0.976 39.402 7.862 0.40 184402. 0.6865 5.33 0.0563 0.1787 0.0679 0.0214 0.688 8.677 8.654 513.289 0.980 38.492 7.647 0.40 184503. 0.6600 7.11 0.0750 0.2316 0.0662 0.0214 0.690 8.702 8.438 514.775 0.983 37.533 7.435 0.40 184610. 0.6336 8.88 0.0938 0.2814 0.0644 0.0215 0.691 8.713 8.211 515.407 0.984 36.524 7.226 0.40 184724. 0.6075 10.66 0.1126 0.3281 0.0625 0.0215 0.691 8.707 7.973 515.093 0.984 35.464 7.021 0.40 184844. 0.5816 12.44 0.1313 0.3717 0.0606 0.0214 0.689 8.684 7.723 513.736 0.981 34.352 6.818 0.40 184971. 0.5559 14.21 0.1501 0.4124 0.0585 0.0213 0.686 8.642 7.461 511.235 0.976 33.186 6.619 0.40 185106. 0.5304 15.99 0.1688 0.4502 0.0564 0.0211 0.681 8.579 7.186 507.479 0.969 31.964 6.423 0.40 185247. 0.5051 17.77 0.1876 0.4851 0.0541 0.0209 0.674 8.492 6.899 502.372 0.959 30.688 6.229 0.40 185396. 0.4800 19.54 0.2064 0.5172 0.0518 0.0207 0.665 8.382 6.600 495.852 0.947 29.358 6.037 0.40 185553. 0.4551 21.32 0.2251 0.5465 0.0493 0.0203 0.654 8.247 6.290 487.876 0.932 27.978 5.848 0.40 185718. 0.4303 23.09 0.2439 0.5730 0.0468 0.0199 0.642 8.087 5.969 478.407 0.914 26.549 5.659 0.40 185890. 0.4056 24.87 0.2626 0.5965 0.0442 0.0195 0.627 7.901 5.638 467.410 0.893 25.076 5.471 0.40 186071. 0.3811 26.65 0.2814 0.6170 0.0416 0.0189 0.610 7.689 5.297 454.855 0.869 23.560 5.282 0.40 186259. 0.3566 28.42 0.3002 0.6344 0.0388 0.0184 0.591 7.450 4.947 440.712 0.842 22.004 5.091 0.40 186456. 0.3322 30.20 0.3189 0.6485 0.0360 0.0177 0.570 7.184 4.589 424.957 0.812 20.412 4.898 0.40 186662. 0.3078 31.98 0.3377 0.6589 0.0331 0.0170 0.547 6.890 4.223 407.573 0.778 18.786 4.700 0.40 186876. 0.2834 33.75 0.3564 0.6652 0.0302 0.0162 0.521 6.568 3.851 388.547 0.742 17.130 4.496 0.40 187099. 0.2588 35.53 0.3752 0.6670 0.0272 0.0153 0.493 6.219 3.473 367.879 0.703 15.447 4.282 0.40 187330. 0.2341 37.31 0.3940 0.6632 0.0242 0.0144 0.463 5.842 3.090 345.577 0.660 13.743 4.055 0.40 187570. 0.2091 39.08 0.4127 0.6529 0.0212 0.0134 0.431 5.438 2.702 321.662 0.614 12.020 3.811 0.40 187820. 0.1838 40.86 0.4315 0.6343 0.0181 0.0123 0.397 5.007 2.312 296.170 0.566 10.285 3.541 0.40 188078. 0.1580 42.64 0.4502 0.6049 0.0151 0.0112 0.361 4.550 1.921 269.155 0.514 8.542 3.236 0.40 188345. 0.1316 44.41 0.4690 0.5609 0.0120 0.0100 0.323 4.069 1.529 240.691 0.460 6.799 2.880 0.40 188622. 0.1045 46.19 0.4878 0.4956 0.0089 0.0088 0.283 3.565 1.138 210.875 0.403 5.062 2.448 0.40 188908. 0.0766 47.97 0.5065 0.3981 0.0059 0.0075 0.241 3.040 0.750 179.827 0.343 3.338 1.893 0.40 189202. 0.0481 49.74 0.5253 0.2463 0.0029 0.0062 0.198 2.496 0.368 147.676 0.282 1.636 1.129 0.40 189506. 0.0201 51.52 0.5440 -0.0132 -0.0001 0.0047 0.153 1.927 -0.015 114.013 0.218 -0.065 -0.058 0.40 189794. 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 0.0732 0.0210 1.169 12.284 13.440 872.019 1.388 59.781 6.991 0.48 221050. 0.7519 2.13 0.0188 0.0636 0.0718 0.0212 1.178 12.370 13.174 878.143 1.398 58.598 6.805 0.48 221158. 0.7246 4.26 0.0375 0.1237 0.0702 0.0213 1.184 12.442 12.893 883.228 1.406 57.347 6.621 0.48 221272. 0.6975 6.39 0.0563 0.1805 0.0686 0.0214 1.190 12.497 12.596 887.116 1.412 56.025 6.440 0.48 221394. 0.6705 8.53 0.0750 0.2341 0.0669 0.0214 1.193 12.533 12.283 889.650 1.416 54.633 6.262 0.48 221523. 0.6439 10.66 0.0938 0.2844 0.0651 0.0215 1.194 12.547 11.953 890.676 1.418 53.167 6.087 0.48 221660. 0.6174 12.79 0.1125 0.3316 0.0632 0.0215 1.194 12.538 11.607 890.028 1.417 51.626 5.915 0.48 221804. 0.5912 14.92 0.1313 0.3758 0.0612 0.0214 1.190 12.503 11.243 887.541 1.413 50.009 5.746 0.48 221958. 0.5652 17.05 0.1501 0.4171 0.0592 0.0213 1.184 12.439 10.862 883.036 1.405 48.313 5.579 0.48 222119. 0.5395 19.18 0.1688 0.4554 0.0570 0.0211 1.175 12.345 10.463 876.319 1.395 46.538 5.415 0.48 222290. 0.5139 21.32 0.1876 0.4909 0.0547 0.0209 1.163 12.217 10.045 867.219 1.380 44.681 5.254 0.48 222469. 0.4885 23.45 0.2063 0.5236 0.0524 0.0206 1.147 12.053 9.610 855.624 1.362 42.746 5.094 0.48 222658. 0.4633 25.58 0.2251 0.5536 0.0499 0.0203 1.128 11.854 9.159 841.459 1.339 40.737 4.937 0.48 222856. 0.4383 27.71 0.2438 0.5807 0.0473 0.0199 1.106 11.617 8.691 824.659 1.312 38.659 4.780 0.48 223064. 0.4135 29.84 0.2626 0.6050 0.0447 0.0194 1.080 11.342 8.209 805.162 1.281 36.514 4.624 0.48 223281. 0.3887 31.97 0.2814 0.6263 0.0420 0.0189 1.050 11.029 7.713 782.913 1.246 34.306 4.468 0.48 223508. 0.3641 34.10 0.3001 0.6446 0.0392 0.0183 1.016 10.676 7.204 757.862 1.206 32.041 4.311 0.48 223744. 0.3395 36.24 0.3189 0.6596 0.0364 0.0176 0.979 10.283 6.682 729.966 1.162 29.722 4.152 0.48 223991. 0.3149 38.37 0.3376 0.6710 0.0335 0.0169 0.938 9.850 6.150 699.195 1.113 27.354 3.989 0.48 224249. 0.2902 40.50 0.3564 0.6785 0.0305 0.0160 0.892 9.375 5.608 665.528 1.059 24.942 3.822 0.48 224516. 0.2655 42.63 0.3751 0.6815 0.0275 0.0152 0.843 8.860 5.057 628.963 1.001 22.491 3.646 0.48 224794. 0.2406 44.76 0.3939 0.6791 0.0245 0.0142 0.791 8.305 4.498 589.515 0.938 20.008 3.461 0.48 225082. 0.2153 46.89 0.4127 0.6703 0.0214 0.0132 0.734 7.709 3.934 547.221 0.871 17.498 3.261 0.48 225382. 0.1897 49.02 0.4314 0.6533 0.0183 0.0121 0.673 7.074 3.365 502.145 0.799 14.970 3.040 0.48 225692. 0.1636 51.16 0.4502 0.6256 0.0152 0.0110 0.609 6.401 2.795 454.384 0.723 12.431 2.790 0.48 226013. 0.1368 53.29 0.4689 0.5831 0.0121 0.0097 0.542 5.692 2.223 404.067 0.643 9.890 2.496 0.48 226345. 0.1092 55.42 0.4877 0.5188 0.0090 0.0085 0.471 4.950 1.654 351.367 0.559 7.358 2.135 0.48 226688. 0.0806 57.55 0.5064 0.4206 0.0059 0.0071 0.398 4.177 1.090 296.499 0.472 4.847 1.667 0.48 227041. 0.0510 59.68 0.5252 0.2633 0.0029 0.0058 0.321 3.377 0.532 239.693 0.381 2.366 1.007 0.48 227405. 0.0215 61.81 0.5440 -0.0185 -0.0001 0.0043 0.241 2.536 -0.027 180.031 0.287 -0.121 -0.068 0.48 227745. 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 0.0742 0.0212 1.870 16.836 18.532 1394.301 1.902 82.432 6.029 0.56 257874. 0.7614 2.49 0.0187 0.0639 0.0727 0.0213 1.883 16.954 18.167 1404.064 1.915 80.808 5.869 0.56 258000. 0.7339 4.97 0.0375 0.1244 0.0712 0.0214 1.894 17.051 17.781 1412.126 1.926 79.088 5.711 0.56 258134. 0.7065 7.46 0.0562 0.1816 0.0695 0.0215 1.902 17.125 17.372 1418.230 1.935 77.272 5.556 0.56 258277. 0.6794 9.94 0.0750 0.2355 0.0678 0.0216 1.907 17.172 16.942 1422.127 1.940 75.357 5.403 0.56 258429. 0.6525 12.43 0.0937 0.2862 0.0660 0.0216 1.909 17.189 16.488 1423.563 1.942 73.340 5.253 0.56 258589. 0.6258 14.91 0.1125 0.3338 0.0641 0.0216 1.907 17.173 16.012 1422.276 1.940 71.220 5.106 0.56 258759. 0.5994 17.40 0.1312 0.3784 0.0621 0.0215 1.902 17.122 15.511 1417.999 1.934 68.994 4.962 0.56 258938. 0.5733 19.88 0.1500 0.4201 0.0600 0.0214 1.891 17.031 14.987 1410.444 1.924 66.660 4.819 0.56 259128. 0.5474 22.37 0.1687 0.4589 0.0578 0.0212 1.876 16.896 14.437 1399.302 1.909 64.215 4.680 0.56 259328. 0.5216 24.85 0.1875 0.4949 0.0555 0.0210 1.856 16.715 13.862 1384.292 1.888 61.658 4.542 0.56 259538. 0.4961 27.34 0.2062 0.5281 0.0531 0.0207 1.831 16.485 13.263 1365.226 1.862 58.992 4.406 0.56 259759. 0.4708 29.82 0.2250 0.5586 0.0506 0.0204 1.800 16.204 12.640 1341.986 1.831 56.223 4.272 0.56 259990. 0.4456 32.31 0.2437 0.5863 0.0480 0.0200 1.763 15.872 11.996 1314.466 1.793 53.357 4.139 0.56 260233. 0.4206 34.79 0.2624 0.6112 0.0454 0.0195 1.720 15.487 11.331 1282.570 1.750 50.399 4.007 0.56 260487. 0.3957 37.28 0.2812 0.6333 0.0426 0.0189 1.671 15.047 10.646 1246.208 1.700 47.355 3.875 0.56 260752. 0.3709 39.76 0.2999 0.6523 0.0398 0.0183 1.616 14.554 9.944 1205.301 1.644 44.230 3.742 0.56 261029. 0.3462 42.25 0.3187 0.6682 0.0369 0.0176 1.555 14.004 9.225 1159.783 1.582 41.031 3.608 0.56 261317. 0.3215 44.74 0.3374 0.6806 0.0340 0.0168 1.488 13.398 8.490 1109.603 1.514 37.763 3.470 0.56 261617. 0.2967 47.22 0.3562 0.6892 0.0310 0.0160 1.414 12.735 7.741 1054.730 1.439 34.434 3.329 0.56 261930. 0.2717 49.71 0.3749 0.6933 0.0279 0.0151 1.335 12.016 6.981 995.159 1.358 31.051 3.182 0.56 262254. 0.2466 52.19 0.3937 0.6923 0.0249 0.0141 1.248 11.240 6.210 930.916 1.270 27.622 3.026 0.56 262591. 0.2212 54.68 0.4124 0.6849 0.0217 0.0131 1.156 10.409 5.431 862.061 1.176 24.156 2.857 0.56 262940. 0.1954 57.16 0.4312 0.6695 0.0186 0.0120 1.058 9.523 4.646 788.699 1.076 20.664 2.672 0.56 263301. 0.1689 59.65 0.4499 0.6435 0.0154 0.0108 0.953 8.585 3.857 710.986 0.970 17.157 2.461 0.56 263676. 0.1418 62.13 0.4687 0.6025 0.0123 0.0096 0.844 7.597 3.068 629.134 0.858 13.647 2.212 0.56 264063. 0.1137 64.62 0.4874 0.5395 0.0091 0.0083 0.729 6.562 2.282 543.426 0.741 10.150 1.905 0.56 264463. 0.0844 67.10 0.5061 0.4411 0.0060 0.0069 0.609 5.484 1.502 454.211 0.620 6.679 1.500 0.56 264875. 0.0539 69.59 0.5249 0.2795 0.0029 0.0055 0.485 4.369 0.731 361.868 0.494 3.252 0.916 0.56 265299. 0.0230 72.07 0.5436 -0.0238 -0.0002 0.0040 0.355 3.195 -0.044 264.573 0.361 -0.196 -0.075 0.56 265688. 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 0.0754 0.0215 2.829 22.287 24.593 2109.448 2.518 109.389 5.288 0.63 294688. 0.7693 2.84 0.0187 0.0640 0.0739 0.0216 2.848 22.441 24.111 2124.028 2.535 107.245 5.149 0.63 294833. 0.7417 5.67 0.0375 0.1247 0.0723 0.0217 2.864 22.567 23.600 2135.975 2.550 104.975 5.011 0.63 294987. 0.7143 8.51 0.0562 0.1820 0.0707 0.0218 2.876 22.662 23.061 2144.899 2.560 102.575 4.877 0.63 295152. 0.6871 11.35 0.0749 0.2360 0.0689 0.0219 2.884 22.720 22.492 2150.418 2.567 100.044 4.744 0.63 295326. 0.6601 14.19 0.0936 0.2870 0.0671 0.0219 2.886 22.738 21.892 2152.151 2.569 97.378 4.614 0.63 295510. 0.6334 17.02 0.1124 0.3348 0.0652 0.0219 2.883 22.712 21.262 2149.697 2.566 94.573 4.486 0.64 295705. 0.6069 19.86 0.1311 0.3797 0.0631 0.0218 2.873 22.638 20.600 2142.653 2.558 91.627 4.361 0.64 295912. 0.5807 22.70 0.1498 0.4217 0.0610 0.0217 2.857 22.510 19.905 2130.593 2.543 88.537 4.237 0.64 296129. 0.5546 25.54 0.1685 0.4608 0.0588 0.0215 2.834 22.325 19.177 2113.052 2.522 85.299 4.116 0.64 296358. 0.5289 28.37 0.1873 0.4972 0.0564 0.0213 2.802 22.077 18.415 2089.587 2.494 81.911 3.997 0.64 296600. 0.5033 31.21 0.2060 0.5309 0.0540 0.0210 2.762 21.764 17.621 2059.917 2.459 78.378 3.880 0.64 296853. 0.4778 34.05 0.2247 0.5619 0.0515 0.0206 2.714 21.383 16.796 2023.853 2.416 74.708 3.764 0.64 297118. 0.4526 36.89 0.2434 0.5901 0.0488 0.0202 2.657 20.932 15.941 1981.241 2.365 70.907 3.649 0.64 297396. 0.4275 39.72 0.2622 0.6157 0.0461 0.0197 2.591 20.412 15.059 1931.940 2.306 66.982 3.535 0.64 297687. 0.4025 42.56 0.2809 0.6384 0.0434 0.0191 2.516 19.819 14.151 1875.820 2.239 62.943 3.422 0.64 297990. 0.3776 45.40 0.2996 0.6582 0.0405 0.0184 2.431 19.152 13.218 1812.760 2.164 58.795 3.307 0.64 298307. 0.3528 48.24 0.3184 0.6749 0.0376 0.0177 2.337 18.412 12.263 1742.666 2.080 54.547 3.192 0.64 298637. 0.3279 51.07 0.3371 0.6883 0.0346 0.0169 2.233 17.596 11.288 1665.459 1.988 50.207 3.074 0.64 298980. 0.3030 53.91 0.3558 0.6979 0.0315 0.0161 2.120 16.705 10.293 1581.096 1.887 45.785 2.953 0.64 299337. 0.2779 56.75 0.3745 0.7032 0.0284 0.0152 1.998 15.738 9.283 1489.573 1.778 41.290 2.827 0.64 299708. 0.2527 59.58 0.3933 0.7035 0.0253 0.0141 1.865 14.696 8.258 1390.926 1.660 36.733 2.693 0.64 300093. 0.2270 62.42 0.4120 0.6975 0.0221 0.0131 1.724 13.579 7.223 1285.250 1.534 32.127 2.549 0.64 300492. 0.2010 65.26 0.4307 0.6837 0.0189 0.0119 1.573 12.390 6.179 1172.708 1.400 27.484 2.390 0.64 300905. 0.1743 68.10 0.4494 0.6594 0.0157 0.0107 1.413 11.131 5.130 1053.532 1.258 22.820 2.209 0.64 301332. 0.1468 70.93 0.4682 0.6202 0.0125 0.0094 1.245 9.805 4.081 928.053 1.108 18.152 1.995 0.64 301774. 0.1182 73.77 0.4869 0.5588 0.0093 0.0081 1.068 8.417 3.035 796.700 0.951 13.499 1.728 0.64 302230. 0.0883 76.61 0.5056 0.4608 0.0061 0.0067 0.885 6.973 1.997 660.014 0.788 8.881 1.372 0.64 302701. 0.0569 79.45 0.5243 0.2958 0.0030 0.0053 0.695 5.479 0.971 518.576 0.619 4.319 0.849 0.64 303184. 0.0246 82.28 0.5431 -0.0281 -0.0002 0.0038 0.495 3.900 -0.063 369.151 0.441 -0.282 -0.078 0.64 303619. 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 0.0768 0.0219 4.112 28.794 31.735 3065.985 3.253 141.156 4.695 0.71 331487. 0.7759 3.19 0.0187 0.0639 0.0753 0.0220 4.139 28.988 31.118 3086.655 3.275 138.413 4.573 0.71 331652. 0.7484 6.37 0.0374 0.1244 0.0738 0.0222 4.162 29.145 30.464 3103.419 3.293 135.503 4.452 0.71 331827. 0.7210 9.56 0.0561 0.1817 0.0721 0.0223 4.178 29.261 29.772 3115.697 3.306 132.427 4.334 0.71 332013. 0.6938 12.75 0.0748 0.2357 0.0703 0.0223 4.188 29.329 29.042 3122.946 3.314 129.179 4.218 0.71 332211. 0.6669 15.93 0.0935 0.2867 0.0685 0.0223 4.190 29.344 28.272 3124.599 3.315 125.755 4.104 0.71 332420. 0.6402 19.12 0.1122 0.3347 0.0665 0.0223 4.184 29.302 27.462 3120.085 3.311 122.152 3.992 0.71 332641. 0.6138 22.31 0.1309 0.3797 0.0644 0.0222 4.169 29.196 26.611 3108.820 3.299 118.366 3.882 0.71 332874. 0.5876 25.50 0.1496 0.4219 0.0623 0.0221 4.144 29.021 25.718 3090.194 3.279 114.392 3.775 0.71 333120. 0.5616 28.68 0.1683 0.4614 0.0600 0.0219 4.108 28.771 24.781 3063.544 3.251 110.226 3.669 0.72 333379. 0.5358 31.87 0.1870 0.4981 0.0576 0.0216 4.061 28.439 23.801 3028.225 3.213 105.866 3.565 0.72 333652. 0.5102 35.06 0.2057 0.5321 0.0552 0.0213 4.001 28.022 22.778 2983.803 3.166 101.317 3.463 0.72 333938. 0.4848 38.24 0.2244 0.5636 0.0526 0.0209 3.929 27.517 21.715 2930.011 3.109 96.587 3.361 0.72 334237. 0.4596 41.43 0.2431 0.5924 0.0499 0.0205 3.844 26.922 20.613 2866.635 3.042 91.688 3.262 0.72 334551. 0.4344 44.62 0.2618 0.6185 0.0472 0.0200 3.746 26.235 19.476 2793.478 2.964 86.627 3.162 0.72 334879. 0.4094 47.80 0.2805 0.6419 0.0443 0.0194 3.635 25.454 18.304 2710.357 2.876 81.416 3.063 0.72 335221. 0.3845 50.99 0.2992 0.6625 0.0414 0.0187 3.510 24.578 17.101 2617.112 2.777 76.063 2.964 0.72 335578. 0.3596 54.18 0.3178 0.6801 0.0384 0.0180 3.371 23.606 15.868 2513.604 2.667 70.580 2.863 0.72 335949. 0.3346 57.37 0.3365 0.6944 0.0354 0.0171 3.218 22.537 14.608 2399.735 2.546 64.976 2.761 0.72 336336. 0.3096 60.55 0.3552 0.7050 0.0323 0.0163 3.051 21.370 13.324 2275.458 2.414 59.264 2.656 0.72 336737. 0.2844 63.74 0.3739 0.7115 0.0291 0.0153 2.871 20.105 12.018 2140.786 2.271 53.456 2.546 0.72 337154. 0.2590 66.93 0.3926 0.7131 0.0259 0.0143 2.676 18.743 10.694 1995.806 2.118 47.566 2.430 0.72 337587. 0.2332 70.11 0.4113 0.7085 0.0227 0.0131 2.468 17.287 9.355 1840.691 1.953 41.610 2.305 0.72 338035. 0.2068 73.30 0.4300 0.6962 0.0194 0.0120 2.247 15.737 8.005 1675.727 1.778 35.605 2.167 0.72 338499. 0.1798 76.49 0.4487 0.6735 0.0161 0.0107 2.013 14.100 6.648 1501.326 1.593 29.570 2.008 0.72 338979. 0.1519 79.67 0.4674 0.6358 0.0128 0.0094 1.768 12.378 5.290 1318.057 1.399 23.528 1.820 0.72 339475. 0.1228 82.86 0.4861 0.5754 0.0095 0.0080 1.511 10.581 3.935 1126.661 1.195 17.503 1.584 0.72 339987. 0.0922 86.05 0.5048 0.4775 0.0063 0.0066 1.245 8.716 2.590 928.068 0.985 11.521 1.266 0.72 340515. 0.0598 89.24 0.5235 0.3094 0.0031 0.0052 0.970 6.793 1.261 723.297 0.767 5.610 0.791 0.72 341058. 0.0261 92.42 0.5422 -0.0294 -0.0002 0.0036 0.680 4.764 -0.081 507.263 0.538 -0.360 -0.072 0.72 341541. 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 0.0787 0.0228 5.875 37.026 40.122 4380.631 4.183 178.464 4.154 0.79 368267. 0.7720 3.53 0.0186 0.0628 0.0772 0.0229 5.901 37.191 39.352 4400.117 4.202 175.038 4.056 0.79 368452. 0.7466 7.06 0.0373 0.1226 0.0756 0.0230 5.920 37.315 38.534 4414.825 4.216 171.401 3.959 0.79 368648. 0.7210 10.60 0.0559 0.1794 0.0739 0.0230 5.933 37.393 37.669 4423.985 4.225 167.550 3.862 0.79 368857. 0.6954 14.13 0.0746 0.2333 0.0721 0.0231 5.936 37.417 36.754 4426.827 4.227 163.481 3.766 0.79 369078. 0.6698 17.66 0.0932 0.2842 0.0702 0.0230 5.931 37.380 35.788 4422.547 4.223 159.187 3.670 0.79 369313. 0.6442 21.19 0.1119 0.3322 0.0682 0.0230 5.914 37.277 34.771 4410.312 4.212 154.664 3.576 0.79 369560. 0.6186 24.73 0.1305 0.3775 0.0661 0.0229 5.886 37.099 33.702 4389.263 4.191 149.906 3.483 0.79 369821. 0.5932 28.26 0.1492 0.4200 0.0639 0.0227 5.845 36.839 32.579 4358.486 4.162 144.910 3.390 0.79 370096. 0.5677 31.79 0.1678 0.4598 0.0616 0.0225 5.789 36.488 31.401 4316.997 4.122 139.670 3.299 0.79 370386. 0.5424 35.32 0.1865 0.4969 0.0592 0.0222 5.718 36.039 30.166 4263.835 4.072 134.181 3.209 0.79 370690. 0.5171 38.85 0.2051 0.5314 0.0566 0.0219 5.630 35.486 28.878 4198.401 4.009 128.448 3.120 0.80 371009. 0.4919 42.39 0.2238 0.5633 0.0540 0.0215 5.525 34.825 27.537 4120.212 3.935 122.485 3.031 0.80 371343. 0.4667 45.92 0.2424 0.5926 0.0513 0.0210 5.403 34.053 26.147 4028.872 3.847 116.302 2.944 0.80 371692. 0.4416 49.45 0.2611 0.6192 0.0485 0.0204 5.262 33.167 24.711 3924.060 3.747 109.913 2.856 0.80 372058. 0.4166 52.98 0.2797 0.6431 0.0456 0.0198 5.103 32.166 23.231 3805.611 3.634 103.331 2.769 0.80 372438. 0.3915 56.52 0.2984 0.6642 0.0426 0.0191 4.926 31.048 21.710 3673.352 3.508 96.566 2.681 0.80 372835. 0.3664 60.05 0.3170 0.6821 0.0395 0.0184 4.730 29.813 20.151 3527.223 3.368 89.632 2.591 0.80 373248. 0.3413 63.58 0.3357 0.6967 0.0364 0.0175 4.516 28.461 18.557 3367.260 3.215 82.544 2.500 0.80 373677. 0.3159 67.11 0.3543 0.7075 0.0332 0.0166 4.283 26.993 16.932 3193.611 3.050 75.314 2.405 0.80 374123. 0.2903 70.64 0.3730 0.7138 0.0300 0.0157 4.032 25.412 15.278 3006.557 2.871 67.959 2.305 0.80 374586. 0.2643 74.18 0.3916 0.7148 0.0267 0.0146 3.764 23.721 13.601 2806.477 2.680 60.496 2.198 0.80 375066. 0.2378 77.71 0.4103 0.7090 0.0233 0.0135 3.479 21.925 11.903 2593.940 2.477 52.944 2.081 0.80 375562. 0.2107 81.24 0.4289 0.6947 0.0200 0.0123 3.178 20.029 10.190 2369.713 2.263 45.326 1.950 0.80 376077. 0.1827 84.77 0.4476 0.6686 0.0166 0.0111 2.863 18.044 8.468 2134.784 2.039 37.664 1.799 0.80 376608. 0.1536 88.30 0.4662 0.6262 0.0132 0.0098 2.535 15.978 6.742 1890.350 1.805 29.987 1.618 0.80 377158. 0.1232 91.84 0.4849 0.5596 0.0098 0.0085 2.196 13.844 5.019 1637.879 1.564 22.325 1.390 0.80 377725. 0.0914 95.37 0.5035 0.4548 0.0065 0.0072 1.849 11.656 3.307 1379.072 1.317 14.711 1.088 0.80 378309. 0.0580 98.90 0.5222 0.2846 0.0032 0.0058 1.496 9.430 1.615 1115.722 1.065 7.182 0.656 0.80 378910. 0.0245 102.43 0.5408 -0.0213 -0.0002 0.0044 1.128 7.108 -0.088 840.914 0.803 -0.391 -0.047 0.81 379461. 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 0.0809 0.0259 8.861 50.773 49.928 6607.695 5.736 222.081 3.427 0.87 405020. 0.7105 3.89 0.0187 0.0575 0.0794 0.0258 8.835 50.624 48.990 6588.394 5.720 217.907 3.373 0.87 405226. 0.6926 7.77 0.0373 0.1130 0.0778 0.0257 8.801 50.426 47.991 6562.623 5.697 213.463 3.317 0.87 405446. 0.6741 11.66 0.0560 0.1667 0.0761 0.0255 8.757 50.174 46.931 6529.739 5.669 208.748 3.260 0.87 405679. 0.6552 15.55 0.0746 0.2183 0.0742 0.0254 8.702 49.861 45.808 6489.029 5.633 203.753 3.202 0.87 405925. 0.6358 19.44 0.0933 0.2678 0.0723 0.0252 8.636 49.482 44.621 6439.739 5.590 198.473 3.143 0.87 406187. 0.6159 23.32 0.1119 0.3152 0.0703 0.0250 8.557 49.031 43.368 6381.068 5.540 192.901 3.083 0.87 406462. 0.5956 27.21 0.1306 0.3604 0.0682 0.0247 8.465 48.502 42.049 6312.174 5.480 187.032 3.021 0.87 406753. 0.5748 31.10 0.1493 0.4034 0.0659 0.0244 8.357 47.886 40.661 6232.083 5.410 180.860 2.959 0.87 407060. 0.5536 34.98 0.1679 0.4442 0.0635 0.0240 8.233 47.177 39.204 6139.719 5.330 174.380 2.896 0.87 407382. 0.5320 38.87 0.1866 0.4826 0.0611 0.0236 8.092 46.364 37.676 6033.886 5.238 167.584 2.832 0.87 407720. 0.5100 42.76 0.2052 0.5187 0.0585 0.0231 7.930 45.440 36.079 5913.639 5.134 160.478 2.767 0.87 408074. 0.4876 46.64 0.2239 0.5522 0.0558 0.0226 7.752 44.417 34.414 5780.565 5.018 153.075 2.700 0.87 408446. 0.4647 50.53 0.2426 0.5827 0.0530 0.0221 7.559 43.309 32.687 5636.397 4.893 145.391 2.630 0.88 408834. 0.4412 54.42 0.2612 0.6103 0.0501 0.0214 7.347 42.097 30.900 5478.637 4.756 137.443 2.558 0.88 409238. 0.4172 58.31 0.2799 0.6347 0.0471 0.0208 7.118 40.784 29.057 5307.779 4.608 129.246 2.483 0.88 409661. 0.3927 62.19 0.2985 0.6553 0.0440 0.0201 6.874 39.387 27.162 5125.950 4.450 120.815 2.403 0.88 410100. 0.3675 66.08 0.3172 0.6712 0.0409 0.0193 6.620 37.932 25.217 4936.521 4.285 112.164 2.317 0.88 410557. 0.3413 69.97 0.3358 0.6827 0.0376 0.0185 6.348 36.373 23.227 4733.633 4.109 103.316 2.226 0.88 411032. 0.3147 73.85 0.3545 0.6893 0.0344 0.0177 6.056 34.702 21.198 4516.255 3.921 94.288 2.129 0.88 411526. 0.2876 77.74 0.3732 0.6902 0.0310 0.0168 5.747 32.928 19.133 4285.413 3.720 85.102 2.025 0.88 412037. 0.2599 81.63 0.3918 0.6840 0.0276 0.0158 5.421 31.063 17.037 4042.656 3.510 75.779 1.911 0.88 412567. 0.2315 85.52 0.4105 0.6693 0.0242 0.0148 5.081 29.116 14.915 3789.268 3.290 66.344 1.785 0.88 413115. 0.2023 89.40 0.4291 0.6439 0.0207 0.0138 4.730 27.100 12.775 3526.866 3.062 56.824 1.643 0.88 413683. 0.1723 93.29 0.4478 0.6050 0.0172 0.0127 4.368 25.029 10.623 3257.369 2.828 47.251 1.479 0.88 414269. 0.1414 97.18 0.4664 0.5485 0.0137 0.0117 4.000 22.921 8.467 2983.004 2.590 37.660 1.287 0.88 414875. 0.1099 101.06 0.4851 0.4690 0.0102 0.0106 3.629 20.794 6.315 2706.164 2.349 28.091 1.059 0.88 415500. 0.0780 104.95 0.5038 0.3590 0.0068 0.0095 3.258 18.667 4.179 2429.322 2.109 18.588 0.780 0.88 416144. 0.0468 108.84 0.5224 0.2077 0.0034 0.0084 2.889 16.556 2.068 2154.639 1.870 9.197 0.435 0.88 416806. 0.0184 112.73 0.5411 -0.0052 -0.0001 0.0073 2.509 14.374 -0.043 1870.694 1.624 -0.192 -0.010 0.89 417449. 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 0.0824 0.0323 14.360 75.424 60.525 10708.284 8.521 269.214 2.564 0.95 441782. 0.5851 4.34 0.0191 0.0483 0.0810 0.0320 14.247 74.828 59.454 10623.678 8.454 264.451 2.538 0.95 442010. 0.5742 8.67 0.0382 0.0956 0.0794 0.0317 14.111 74.119 58.301 10522.933 8.374 259.322 2.513 0.95 442255. 0.5629 13.01 0.0573 0.1419 0.0777 0.0314 13.954 73.293 57.064 10405.718 8.281 253.822 2.487 0.95 442515. 0.5513 17.35 0.0763 0.1872 0.0759 0.0310 13.775 72.349 55.742 10271.701 8.174 247.939 2.461 0.95 442792. 0.5391 21.69 0.0954 0.2315 0.0740 0.0305 13.572 71.285 54.331 10120.642 8.054 241.664 2.435 0.95 443086. 0.5266 26.02 0.1145 0.2747 0.0720 0.0300 13.346 70.100 52.830 9952.316 7.920 234.988 2.408 0.95 443397. 0.5134 30.36 0.1336 0.3167 0.0698 0.0294 13.097 68.791 51.238 9766.547 7.772 227.906 2.380 0.95 443726. 0.4997 34.70 0.1527 0.3575 0.0675 0.0288 12.824 67.358 49.553 9563.069 7.610 220.411 2.350 0.95 444073. 0.4854 39.03 0.1718 0.3969 0.0651 0.0282 12.527 65.797 47.773 9341.455 7.434 212.496 2.320 0.95 444438. 0.4704 43.37 0.1908 0.4349 0.0625 0.0274 12.205 64.104 45.898 9101.046 7.242 204.154 2.287 0.95 444822. 0.4547 47.71 0.2099 0.4713 0.0598 0.0266 11.857 62.275 43.929 8841.495 7.036 195.394 2.254 0.95 445225. 0.4382 52.05 0.2290 0.5060 0.0570 0.0258 11.483 60.313 41.870 8562.943 6.814 186.238 2.218 0.95 445647. 0.4210 56.38 0.2481 0.5385 0.0541 0.0249 11.091 58.252 39.727 8270.346 6.581 176.707 2.179 0.95 446088. 0.4029 60.72 0.2672 0.5678 0.0511 0.0240 10.695 56.176 37.504 7975.524 6.347 166.820 2.133 0.96 446549. 0.3832 65.06 0.2863 0.5937 0.0480 0.0231 10.288 54.038 35.208 7672.019 6.105 156.605 2.081 0.96 447030. 0.3624 69.39 0.3053 0.6154 0.0447 0.0222 9.876 51.873 32.843 7364.650 5.861 146.087 2.023 0.96 447530. 0.3401 73.73 0.3244 0.6309 0.0414 0.0213 9.478 49.782 30.414 7067.797 5.624 135.283 1.952 0.96 448050. 0.3158 78.07 0.3435 0.6338 0.0380 0.0206 9.170 48.164 27.921 6838.112 5.442 124.191 1.852 0.96 448591. 0.2871 82.41 0.3626 0.6287 0.0346 0.0199 8.869 46.582 25.376 6613.472 5.263 112.874 1.740 0.96 449152. 0.2572 86.74 0.3817 0.6160 0.0310 0.0192 8.558 44.947 22.790 6381.355 5.078 101.372 1.620 0.96 449734. 0.2269 91.08 0.4008 0.5946 0.0275 0.0185 8.239 43.276 20.171 6144.126 4.889 89.721 1.489 0.96 450337. 0.1962 95.42 0.4198 0.5633 0.0239 0.0178 7.918 41.587 17.528 5904.291 4.698 77.965 1.347 0.96 450961. 0.1654 99.75 0.4389 0.5207 0.0203 0.0171 7.597 39.905 14.872 5665.420 4.508 66.150 1.191 0.96 451606. 0.1347 104.09 0.4580 0.4657 0.0166 0.0164 7.280 38.237 12.216 5428.684 4.320 54.335 1.021 0.96 452273. 0.1047 108.43 0.4771 0.3972 0.0130 0.0157 6.968 36.598 9.573 5196.039 4.135 42.580 0.836 0.96 452962. 0.0759 112.77 0.4962 0.3140 0.0095 0.0150 6.664 35.000 6.959 4969.083 3.954 30.952 0.635 0.96 453673. 0.0492 117.10 0.5153 0.2151 0.0060 0.0143 6.368 33.447 4.387 4748.594 3.779 19.515 0.419 0.96 454408. 0.0258 121.44 0.5343 0.0993 0.0025 0.0137 6.076 31.915 1.864 4531.058 3.606 8.291 0.187 0.97 455170. 0.0075 125.78 0.5534