19x10E (19x10E.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 0.0863 0.0327 0.007 0.410 0.359 4.852 0.046 1.595 33.511 0.08 33294. 0.6197 0.41 0.0231 0.0594 0.0850 0.0330 0.007 0.414 0.353 4.903 0.047 1.570 32.647 0.08 33315. 0.5990 0.83 0.0461 0.1156 0.0835 0.0333 0.007 0.418 0.347 4.950 0.047 1.543 31.784 0.08 33337. 0.5781 1.24 0.0692 0.1688 0.0820 0.0336 0.007 0.422 0.340 4.993 0.048 1.514 30.925 0.08 33361. 0.5572 1.66 0.0922 0.2188 0.0803 0.0338 0.007 0.425 0.333 5.029 0.048 1.483 30.072 0.08 33387. 0.5363 2.07 0.1153 0.2658 0.0785 0.0340 0.007 0.428 0.326 5.059 0.048 1.450 29.225 0.08 33415. 0.5153 2.49 0.1384 0.3098 0.0766 0.0342 0.007 0.429 0.318 5.080 0.049 1.414 28.388 0.08 33444. 0.4943 2.90 0.1614 0.3509 0.0745 0.0343 0.007 0.430 0.309 5.092 0.049 1.376 27.558 0.08 33476. 0.4734 3.32 0.1845 0.3891 0.0723 0.0343 0.007 0.430 0.300 5.093 0.049 1.335 26.738 0.08 33510. 0.4524 3.73 0.2075 0.4244 0.0699 0.0342 0.007 0.430 0.290 5.082 0.049 1.292 25.927 0.08 33547. 0.4315 4.15 0.2306 0.4570 0.0675 0.0340 0.007 0.428 0.280 5.058 0.048 1.246 25.122 0.08 33585. 0.4106 4.56 0.2537 0.4867 0.0648 0.0338 0.007 0.424 0.269 5.020 0.048 1.197 24.323 0.08 33626. 0.3897 4.98 0.2767 0.5136 0.0620 0.0334 0.007 0.420 0.258 4.967 0.047 1.146 23.528 0.08 33669. 0.3688 5.39 0.2998 0.5375 0.0591 0.0330 0.007 0.414 0.245 4.898 0.047 1.092 22.733 0.08 33715. 0.3478 5.81 0.3228 0.5585 0.0560 0.0324 0.006 0.407 0.233 4.811 0.046 1.035 21.934 0.08 33763. 0.3267 6.22 0.3459 0.5764 0.0528 0.0317 0.006 0.398 0.219 4.708 0.045 0.975 21.126 0.08 33813. 0.3055 6.64 0.3690 0.5909 0.0494 0.0309 0.006 0.388 0.205 4.586 0.044 0.913 20.304 0.08 33866. 0.2841 7.05 0.3920 0.6018 0.0459 0.0299 0.006 0.376 0.191 4.447 0.042 0.849 19.461 0.08 33921. 0.2625 7.47 0.4151 0.6086 0.0424 0.0289 0.006 0.363 0.176 4.292 0.041 0.782 18.589 0.08 33979. 0.2408 7.88 0.4381 0.6109 0.0387 0.0277 0.006 0.348 0.161 4.121 0.039 0.714 17.678 0.08 34039. 0.2188 8.30 0.4612 0.6081 0.0349 0.0265 0.005 0.333 0.145 3.935 0.038 0.645 16.715 0.08 34102. 0.1966 8.71 0.4843 0.5992 0.0311 0.0251 0.005 0.316 0.129 3.733 0.036 0.574 15.687 0.08 34167. 0.1741 9.13 0.5073 0.5831 0.0272 0.0237 0.005 0.297 0.113 3.517 0.034 0.503 14.571 0.08 34235. 0.1513 9.54 0.5304 0.5582 0.0233 0.0221 0.004 0.278 0.097 3.287 0.031 0.430 13.343 0.08 34305. 0.1281 9.96 0.5534 0.5224 0.0193 0.0205 0.004 0.257 0.080 3.044 0.029 0.357 11.966 0.08 34378. 0.1047 10.37 0.5765 0.4725 0.0154 0.0188 0.004 0.236 0.064 2.789 0.027 0.284 10.390 0.08 34453. 0.0811 10.79 0.5996 0.4040 0.0114 0.0170 0.003 0.213 0.048 2.522 0.024 0.211 8.543 0.08 34531. 0.0575 11.20 0.6226 0.3101 0.0075 0.0151 0.003 0.190 0.031 2.247 0.021 0.139 6.313 0.08 34611. 0.0345 11.62 0.6457 0.1797 0.0037 0.0132 0.003 0.166 0.015 1.963 0.019 0.068 3.528 0.08 34694. 0.0135 12.03 0.6687 -0.0060 -0.0001 0.0113 0.002 0.141 0.000 1.673 0.016 -0.002 -0.113 0.08 34779. 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 0.0867 0.0302 0.048 1.516 1.440 35.875 0.171 6.403 18.201 0.15 66588. 0.6744 0.83 0.0231 0.0646 0.0853 0.0306 0.049 1.535 1.417 36.323 0.173 6.304 17.697 0.15 66629. 0.6506 1.67 0.0463 0.1256 0.0839 0.0309 0.049 1.553 1.393 36.742 0.175 6.197 17.198 0.15 66673. 0.6269 2.50 0.0694 0.1830 0.0823 0.0312 0.050 1.569 1.367 37.123 0.177 6.081 16.704 0.15 66722. 0.6032 3.33 0.0926 0.2369 0.0806 0.0315 0.050 1.583 1.339 37.457 0.179 5.957 16.216 0.15 66774. 0.5795 4.16 0.1157 0.2873 0.0788 0.0317 0.051 1.595 1.309 37.734 0.180 5.823 15.736 0.15 66830. 0.5561 5.00 0.1389 0.3345 0.0769 0.0319 0.051 1.604 1.277 37.943 0.181 5.680 15.265 0.15 66890. 0.5327 5.83 0.1620 0.3784 0.0748 0.0320 0.051 1.609 1.242 38.075 0.182 5.527 14.801 0.15 66954. 0.5095 6.66 0.1852 0.4191 0.0726 0.0321 0.051 1.611 1.206 38.119 0.182 5.363 14.347 0.15 67022. 0.4865 7.50 0.2083 0.4569 0.0702 0.0320 0.051 1.609 1.167 38.064 0.182 5.189 13.900 0.15 67095. 0.4636 8.33 0.2315 0.4916 0.0677 0.0319 0.051 1.602 1.125 37.901 0.181 5.004 13.462 0.15 67173. 0.4409 9.16 0.2546 0.5235 0.0651 0.0316 0.050 1.590 1.081 37.620 0.180 4.808 13.031 0.15 67255. 0.4184 10.00 0.2778 0.5524 0.0623 0.0313 0.050 1.573 1.034 37.214 0.178 4.600 12.606 0.15 67342. 0.3959 10.83 0.3009 0.5785 0.0593 0.0309 0.049 1.550 0.985 36.673 0.175 4.382 12.186 0.15 67434. 0.3735 11.66 0.3241 0.6016 0.0562 0.0303 0.048 1.521 0.934 35.988 0.172 4.153 11.768 0.15 67531. 0.3512 12.49 0.3472 0.6217 0.0530 0.0296 0.047 1.486 0.880 35.152 0.168 3.913 11.350 0.15 67632. 0.3288 13.33 0.3704 0.6387 0.0496 0.0287 0.046 1.444 0.823 34.167 0.163 3.663 10.931 0.15 67738. 0.3063 14.16 0.3935 0.6522 0.0461 0.0278 0.044 1.396 0.765 33.036 0.158 3.403 10.506 0.15 67850. 0.2838 14.99 0.4167 0.6620 0.0424 0.0267 0.043 1.342 0.705 31.762 0.152 3.137 10.070 0.15 67966. 0.2612 15.83 0.4398 0.6675 0.0387 0.0255 0.041 1.283 0.644 30.349 0.145 2.863 9.620 0.15 68087. 0.2384 16.66 0.4630 0.6682 0.0350 0.0242 0.039 1.217 0.581 28.800 0.138 2.584 9.149 0.15 68214. 0.2154 17.49 0.4861 0.6632 0.0311 0.0228 0.036 1.146 0.517 27.119 0.129 2.300 8.649 0.15 68345. 0.1921 18.33 0.5093 0.6513 0.0272 0.0213 0.034 1.070 0.452 25.310 0.121 2.012 8.107 0.15 68481. 0.1684 19.16 0.5324 0.6308 0.0233 0.0197 0.031 0.988 0.387 23.379 0.112 1.722 7.510 0.15 68623. 0.1443 19.99 0.5556 0.5990 0.0194 0.0179 0.029 0.902 0.321 21.333 0.102 1.430 6.835 0.15 68769. 0.1197 20.82 0.5787 0.5522 0.0154 0.0161 0.026 0.811 0.256 19.179 0.092 1.138 6.049 0.15 68921. 0.0945 21.66 0.6019 0.4843 0.0115 0.0142 0.023 0.715 0.190 16.927 0.081 0.847 5.100 0.15 69078. 0.0687 22.49 0.6250 0.3848 0.0076 0.0123 0.020 0.617 0.126 14.592 0.070 0.559 3.903 0.15 69240. 0.0427 23.32 0.6482 0.2353 0.0037 0.0103 0.016 0.515 0.062 12.187 0.058 0.275 2.301 0.15 69406. 0.0177 24.16 0.6713 -0.0031 0.0000 0.0082 0.013 0.411 -0.001 9.724 0.046 -0.003 -0.029 0.15 69576. 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 0.0870 0.0292 0.157 3.298 3.253 117.069 0.373 14.468 12.602 0.23 99879. 0.7019 1.25 0.0232 0.0672 0.0857 0.0296 0.159 3.343 3.203 118.647 0.378 14.245 12.243 0.23 99941. 0.6766 2.50 0.0464 0.1305 0.0842 0.0299 0.161 3.385 3.148 120.129 0.382 14.003 11.887 0.23 100008. 0.6513 3.76 0.0696 0.1900 0.0827 0.0303 0.163 3.423 3.090 121.482 0.387 13.743 11.536 0.23 100081. 0.6262 5.01 0.0928 0.2457 0.0810 0.0306 0.165 3.456 3.027 122.674 0.390 13.462 11.190 0.23 100159. 0.6012 6.26 0.1160 0.2979 0.0792 0.0308 0.166 3.484 2.959 123.671 0.394 13.161 10.851 0.23 100244. 0.5764 7.51 0.1392 0.3465 0.0772 0.0310 0.167 3.506 2.886 124.439 0.396 12.837 10.519 0.23 100334. 0.5519 8.77 0.1624 0.3918 0.0751 0.0311 0.168 3.520 2.808 124.939 0.398 12.491 10.195 0.23 100431. 0.5276 10.02 0.1856 0.4338 0.0729 0.0312 0.168 3.526 2.725 125.137 0.398 12.121 9.877 0.23 100534. 0.5035 11.27 0.2088 0.4727 0.0705 0.0312 0.168 3.522 2.636 124.996 0.398 11.727 9.567 0.23 100644. 0.4797 12.52 0.2320 0.5085 0.0680 0.0310 0.167 3.507 2.542 124.480 0.396 11.308 9.263 0.23 100761. 0.4561 13.77 0.2552 0.5414 0.0653 0.0308 0.166 3.481 2.442 123.559 0.393 10.864 8.966 0.23 100885. 0.4327 15.03 0.2784 0.5715 0.0625 0.0305 0.164 3.443 2.337 122.200 0.389 10.395 8.675 0.23 101016. 0.4095 16.28 0.3016 0.5986 0.0596 0.0300 0.161 3.391 2.226 120.375 0.383 9.901 8.388 0.23 101154. 0.3865 17.53 0.3248 0.6229 0.0564 0.0294 0.158 3.326 2.109 118.051 0.376 9.382 8.104 0.23 101300. 0.3635 18.78 0.3480 0.6442 0.0532 0.0287 0.154 3.246 1.987 115.203 0.367 8.838 7.823 0.23 101453. 0.3405 20.04 0.3712 0.6624 0.0497 0.0279 0.150 3.151 1.859 111.833 0.356 8.271 7.541 0.23 101613. 0.3176 21.29 0.3944 0.6774 0.0462 0.0269 0.145 3.041 1.728 107.952 0.344 7.684 7.258 0.23 101781. 0.2946 22.54 0.4176 0.6888 0.0426 0.0258 0.139 2.918 1.592 103.571 0.330 7.080 6.971 0.23 101956. 0.2716 23.79 0.4408 0.6962 0.0389 0.0246 0.132 2.781 1.453 98.700 0.314 6.461 6.675 0.23 102138. 0.2484 25.04 0.4640 0.6991 0.0351 0.0233 0.125 2.630 1.310 93.352 0.297 5.829 6.367 0.23 102329. 0.2251 26.30 0.4872 0.6965 0.0312 0.0218 0.117 2.466 1.166 87.537 0.279 5.186 6.041 0.23 102526. 0.2015 27.55 0.5104 0.6873 0.0273 0.0203 0.109 2.290 1.020 81.271 0.259 4.535 5.690 0.23 102732. 0.1774 28.80 0.5336 0.6696 0.0233 0.0186 0.100 2.101 0.872 74.573 0.237 3.878 5.303 0.23 102945. 0.1529 30.05 0.5568 0.6409 0.0194 0.0168 0.090 1.901 0.724 67.467 0.215 3.218 4.865 0.23 103166. 0.1278 31.31 0.5800 0.5969 0.0154 0.0150 0.080 1.690 0.575 59.981 0.191 2.558 4.349 0.23 103394. 0.1019 32.56 0.6032 0.5306 0.0114 0.0130 0.070 1.469 0.427 52.154 0.166 1.901 3.718 0.23 103630. 0.0751 33.81 0.6264 0.4296 0.0075 0.0110 0.059 1.241 0.281 44.030 0.140 1.251 2.898 0.23 103874. 0.0475 35.06 0.6496 0.2691 0.0037 0.0089 0.048 1.005 0.138 35.664 0.114 0.612 1.750 0.23 104125. 0.0201 36.31 0.6728 -0.0085 -0.0001 0.0068 0.036 0.763 -0.003 27.082 0.086 -0.014 -0.054 0.23 104379. 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 0.0875 0.0287 0.366 5.767 5.814 272.915 0.652 25.859 9.662 0.30 133168. 0.7195 1.67 0.0232 0.0687 0.0861 0.0291 0.371 5.848 5.724 276.759 0.661 25.462 9.382 0.30 133251. 0.6932 3.34 0.0464 0.1333 0.0847 0.0295 0.376 5.924 5.628 280.374 0.669 25.033 9.105 0.30 133341. 0.6670 5.01 0.0696 0.1939 0.0831 0.0298 0.380 5.994 5.524 283.682 0.677 24.570 8.832 0.30 133437. 0.6410 6.68 0.0928 0.2507 0.0814 0.0301 0.384 6.056 5.412 286.607 0.684 24.071 8.564 0.30 133542. 0.6153 8.35 0.1160 0.3038 0.0796 0.0304 0.388 6.108 5.291 289.067 0.690 23.535 8.302 0.30 133655. 0.5898 10.02 0.1392 0.3533 0.0777 0.0306 0.390 6.148 5.162 290.974 0.695 22.959 8.046 0.30 133775. 0.5645 11.69 0.1624 0.3994 0.0756 0.0307 0.392 6.175 5.023 292.243 0.698 22.342 7.796 0.30 133905. 0.5396 13.36 0.1856 0.4422 0.0734 0.0308 0.393 6.187 4.875 292.783 0.699 21.682 7.552 0.30 134043. 0.5149 15.03 0.2088 0.4818 0.0710 0.0308 0.392 6.181 4.717 292.508 0.698 20.979 7.314 0.30 134189. 0.4905 16.70 0.2320 0.5183 0.0685 0.0306 0.391 6.156 4.549 291.334 0.696 20.232 7.082 0.30 134346. 0.4664 18.37 0.2552 0.5519 0.0658 0.0304 0.388 6.111 4.371 289.181 0.690 19.440 6.855 0.30 134511. 0.4426 20.03 0.2784 0.5826 0.0629 0.0301 0.384 6.043 4.182 285.976 0.683 18.603 6.633 0.30 134686. 0.4190 21.70 0.3016 0.6105 0.0600 0.0296 0.378 5.951 3.984 281.645 0.672 17.721 6.416 0.30 134870. 0.3955 23.37 0.3248 0.6355 0.0568 0.0290 0.370 5.834 3.776 276.110 0.659 16.794 6.202 0.30 135065. 0.3722 25.04 0.3480 0.6577 0.0535 0.0283 0.361 5.691 3.557 269.309 0.643 15.821 5.991 0.30 135269. 0.3489 26.71 0.3712 0.6769 0.0501 0.0275 0.350 5.520 3.329 261.242 0.624 14.808 5.780 0.30 135483. 0.3257 28.38 0.3944 0.6930 0.0466 0.0265 0.338 5.324 3.093 251.936 0.601 13.760 5.569 0.30 135706. 0.3025 30.05 0.4176 0.7056 0.0429 0.0254 0.324 5.101 2.851 241.415 0.576 12.680 5.356 0.30 135940. 0.2793 31.72 0.4408 0.7145 0.0392 0.0242 0.308 4.854 2.602 229.702 0.548 11.573 5.138 0.30 136184. 0.2559 33.39 0.4640 0.7190 0.0353 0.0228 0.291 4.582 2.348 216.825 0.518 10.443 4.911 0.30 136437. 0.2324 35.06 0.4872 0.7183 0.0314 0.0213 0.272 4.286 2.090 202.811 0.484 9.295 4.673 0.31 136701. 0.2086 36.73 0.5104 0.7113 0.0275 0.0197 0.252 3.966 1.828 187.697 0.448 8.131 4.417 0.31 136975. 0.1844 38.40 0.5336 0.6963 0.0235 0.0180 0.230 3.624 1.564 171.528 0.409 6.957 4.136 0.31 137259. 0.1597 40.07 0.5568 0.6705 0.0195 0.0162 0.207 3.262 1.299 154.361 0.369 5.778 3.817 0.31 137554. 0.1343 41.74 0.5800 0.6296 0.0156 0.0143 0.183 2.879 1.034 136.268 0.325 4.598 3.441 0.31 137858. 0.1080 43.41 0.6032 0.5663 0.0116 0.0123 0.157 2.479 0.770 117.339 0.280 3.424 2.976 0.31 138173. 0.0806 45.08 0.6263 0.4668 0.0077 0.0103 0.131 2.064 0.509 97.687 0.233 2.263 2.362 0.31 138498. 0.0520 46.75 0.6495 0.3026 0.0038 0.0081 0.104 1.636 0.252 77.443 0.185 1.121 1.476 0.31 138833. 0.0229 48.42 0.6727 0.0009 0.0000 0.0060 0.076 1.197 0.001 56.670 0.135 0.002 0.004 0.31 139171. 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 0.0881 0.0285 0.710 8.947 9.145 529.272 1.011 40.677 7.837 0.38 166453. 0.7319 2.10 0.0234 0.0702 0.0867 0.0289 0.720 9.078 9.005 537.013 1.026 40.053 7.605 0.38 166558. 0.7048 4.21 0.0468 0.1361 0.0853 0.0293 0.730 9.201 8.853 544.294 1.040 39.376 7.377 0.38 166671. 0.6778 6.31 0.0702 0.1979 0.0837 0.0297 0.739 9.314 8.688 550.958 1.052 38.645 7.153 0.38 166794. 0.6511 8.42 0.0936 0.2558 0.0820 0.0300 0.747 9.413 8.511 556.847 1.063 37.857 6.933 0.38 166926. 0.6246 10.52 0.1170 0.3098 0.0801 0.0302 0.753 9.497 8.320 561.792 1.073 37.008 6.717 0.38 167069. 0.5984 12.63 0.1403 0.3602 0.0782 0.0305 0.759 9.562 8.115 565.621 1.080 36.095 6.507 0.38 167222. 0.5725 14.73 0.1637 0.4070 0.0760 0.0306 0.762 9.604 7.895 568.151 1.085 35.117 6.303 0.38 167385. 0.5469 16.83 0.1871 0.4504 0.0738 0.0306 0.763 9.622 7.660 569.204 1.087 34.070 6.104 0.38 167560. 0.5217 18.94 0.2105 0.4906 0.0714 0.0306 0.763 9.612 7.408 568.601 1.086 32.953 5.910 0.38 167747. 0.4967 21.04 0.2339 0.5278 0.0688 0.0305 0.759 9.571 7.141 566.170 1.081 31.764 5.721 0.38 167945. 0.4721 23.15 0.2573 0.5619 0.0661 0.0302 0.753 9.496 6.858 561.751 1.073 30.504 5.537 0.38 168155. 0.4478 25.25 0.2807 0.5931 0.0632 0.0299 0.745 9.385 6.558 555.192 1.060 29.171 5.358 0.38 168377. 0.4237 27.36 0.3041 0.6215 0.0601 0.0294 0.733 9.236 6.242 546.344 1.043 27.765 5.182 0.38 168611. 0.3998 29.46 0.3275 0.6470 0.0569 0.0288 0.718 9.045 5.910 535.047 1.022 26.286 5.010 0.38 168857. 0.3761 31.56 0.3509 0.6697 0.0536 0.0281 0.699 8.810 5.561 521.182 0.995 24.735 4.840 0.38 169116. 0.3524 33.67 0.3742 0.6894 0.0501 0.0272 0.677 8.533 5.198 504.758 0.964 23.120 4.671 0.38 169388. 0.3288 35.77 0.3976 0.7060 0.0464 0.0262 0.652 8.213 4.822 485.826 0.928 21.448 4.502 0.38 169672. 0.3053 37.88 0.4210 0.7192 0.0427 0.0250 0.623 7.851 4.435 464.434 0.887 19.727 4.331 0.38 169968. 0.2817 39.98 0.4444 0.7287 0.0389 0.0237 0.591 7.449 4.039 440.630 0.842 17.964 4.157 0.38 170278. 0.2580 42.08 0.4678 0.7338 0.0350 0.0223 0.556 7.006 3.634 414.467 0.792 16.165 3.977 0.38 170600. 0.2341 44.19 0.4912 0.7337 0.0310 0.0208 0.518 6.525 3.223 386.004 0.737 14.336 3.787 0.38 170935. 0.2100 46.29 0.5146 0.7272 0.0270 0.0191 0.476 6.006 2.807 355.317 0.679 12.485 3.583 0.38 171282. 0.1854 48.40 0.5380 0.7123 0.0230 0.0174 0.432 5.452 2.387 322.503 0.616 10.618 3.357 0.38 171643. 0.1602 50.50 0.5614 0.6862 0.0189 0.0155 0.386 4.863 1.966 287.683 0.549 8.744 3.099 0.38 172017. 0.1342 52.61 0.5848 0.6438 0.0149 0.0135 0.337 4.243 1.545 251.013 0.479 6.871 2.791 0.38 172403. 0.1071 54.71 0.6081 0.5762 0.0108 0.0115 0.285 3.595 1.126 212.687 0.406 5.010 2.402 0.38 172803. 0.0787 56.81 0.6315 0.4658 0.0069 0.0093 0.232 2.924 0.713 172.946 0.330 3.172 1.870 0.38 173216. 0.0488 58.92 0.6549 0.2729 0.0030 0.0071 0.177 2.232 0.308 132.064 0.252 1.368 1.056 0.38 173640. 0.0181 61.02 0.6783 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 0.0888 0.0285 1.226 12.879 13.278 914.258 1.455 59.062 6.587 0.45 199733. 0.7413 2.51 0.0232 0.0702 0.0875 0.0289 1.244 13.070 13.078 927.824 1.477 58.172 6.393 0.45 199858. 0.7140 5.01 0.0464 0.1363 0.0860 0.0293 1.261 13.250 12.861 940.596 1.497 57.207 6.202 0.45 199993. 0.6869 7.52 0.0696 0.1982 0.0845 0.0297 1.277 13.415 12.627 952.307 1.516 56.164 6.014 0.45 200139. 0.6600 10.02 0.0928 0.2562 0.0828 0.0300 1.291 13.561 12.374 962.681 1.532 55.038 5.830 0.45 200297. 0.6333 12.53 0.1161 0.3103 0.0809 0.0303 1.303 13.685 12.101 971.432 1.546 53.825 5.650 0.45 200467. 0.6070 15.04 0.1393 0.3609 0.0790 0.0305 1.312 13.781 11.808 978.261 1.557 52.521 5.475 0.45 200649. 0.5810 17.54 0.1625 0.4079 0.0769 0.0306 1.318 13.846 11.493 982.854 1.564 51.122 5.304 0.45 200844. 0.5553 20.05 0.1857 0.4515 0.0746 0.0307 1.321 13.874 11.157 984.902 1.568 49.624 5.138 0.45 201052. 0.5300 22.55 0.2089 0.4920 0.0722 0.0307 1.320 13.863 10.797 984.098 1.566 48.026 4.976 0.45 201274. 0.5050 25.06 0.2321 0.5294 0.0697 0.0305 1.314 13.807 10.415 980.145 1.560 46.324 4.819 0.45 201509. 0.4803 27.56 0.2553 0.5639 0.0669 0.0303 1.304 13.703 10.009 972.764 1.548 44.518 4.667 0.45 201759. 0.4559 30.07 0.2785 0.5956 0.0641 0.0300 1.290 13.547 9.579 961.693 1.531 42.608 4.518 0.45 202022. 0.4318 32.58 0.3018 0.6245 0.0610 0.0295 1.270 13.336 9.126 946.679 1.507 40.594 4.373 0.45 202300. 0.4079 35.08 0.3250 0.6506 0.0579 0.0289 1.244 13.065 8.650 927.447 1.476 38.473 4.230 0.45 202593. 0.3842 37.59 0.3482 0.6740 0.0545 0.0282 1.212 12.731 8.149 903.770 1.438 36.248 4.090 0.45 202900. 0.3606 40.09 0.3714 0.6945 0.0510 0.0273 1.174 12.335 7.628 875.639 1.394 33.929 3.951 0.46 203222. 0.3370 42.60 0.3946 0.7121 0.0474 0.0263 1.131 11.877 7.088 843.136 1.342 31.527 3.813 0.46 203559. 0.3135 45.11 0.4178 0.7265 0.0437 0.0251 1.081 11.359 6.532 806.343 1.283 29.053 3.674 0.46 203910. 0.2900 47.61 0.4410 0.7374 0.0399 0.0238 1.026 10.781 5.961 765.343 1.218 26.515 3.533 0.46 204277. 0.2664 50.12 0.4642 0.7442 0.0360 0.0224 0.966 10.146 5.379 720.223 1.146 23.924 3.387 0.46 204659. 0.2426 52.62 0.4875 0.7463 0.0320 0.0209 0.900 9.454 4.786 671.083 1.068 21.290 3.235 0.46 205055. 0.2186 55.13 0.5107 0.7425 0.0280 0.0193 0.829 8.706 4.186 618.048 0.984 18.620 3.072 0.46 205467. 0.1941 57.64 0.5339 0.7311 0.0239 0.0175 0.753 7.907 3.581 561.278 0.893 15.927 2.894 0.46 205894. 0.1691 60.14 0.5571 0.7095 0.0199 0.0156 0.672 7.057 2.972 500.975 0.797 13.220 2.691 0.46 206337. 0.1433 62.65 0.5803 0.6731 0.0158 0.0136 0.587 6.162 2.364 437.398 0.696 10.513 2.451 0.46 206794. 0.1164 65.15 0.6035 0.6141 0.0118 0.0116 0.497 5.224 1.758 370.870 0.590 7.820 2.150 0.46 207267. 0.0880 67.66 0.6267 0.5167 0.0078 0.0094 0.405 4.251 1.159 301.792 0.480 5.156 1.742 0.46 207756. 0.0579 70.16 0.6499 0.3452 0.0038 0.0072 0.309 3.249 0.571 230.639 0.367 2.538 1.122 0.46 208259. 0.0262 72.67 0.6732 -0.0062 0.0000 0.0049 0.211 2.219 -0.007 157.535 0.251 -0.030 -0.019 0.46 208763. 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 0.0897 0.0286 1.957 17.621 18.255 1459.341 1.991 81.199 5.674 0.53 233006. 0.7487 2.94 0.0233 0.0709 0.0884 0.0291 1.987 17.888 17.982 1481.484 2.021 79.986 5.505 0.53 233152. 0.7210 5.88 0.0467 0.1376 0.0869 0.0295 2.015 18.140 17.686 1502.326 2.049 78.667 5.340 0.53 233312. 0.6935 8.81 0.0700 0.2001 0.0853 0.0299 2.040 18.371 17.365 1521.421 2.076 77.240 5.177 0.53 233484. 0.6662 11.75 0.0933 0.2585 0.0836 0.0302 2.063 18.575 17.018 1538.322 2.099 75.696 5.018 0.53 233670. 0.6393 14.69 0.1166 0.3132 0.0818 0.0305 2.082 18.747 16.644 1552.553 2.118 74.031 4.862 0.53 233870. 0.6126 17.63 0.1400 0.3641 0.0798 0.0307 2.097 18.880 16.240 1563.615 2.133 72.237 4.711 0.53 234085. 0.5863 20.57 0.1633 0.4115 0.0777 0.0308 2.107 18.969 15.807 1570.999 2.143 70.309 4.564 0.53 234315. 0.5603 23.51 0.1866 0.4555 0.0754 0.0309 2.111 19.008 15.343 1574.191 2.147 68.244 4.421 0.53 234560. 0.5347 26.44 0.2100 0.4964 0.0730 0.0309 2.109 18.990 14.846 1572.684 2.145 66.036 4.282 0.53 234822. 0.5095 29.38 0.2333 0.5342 0.0704 0.0307 2.100 18.909 14.317 1565.995 2.136 63.684 4.147 0.53 235099. 0.4846 32.32 0.2566 0.5690 0.0676 0.0305 2.083 18.760 13.756 1553.661 2.119 61.186 4.016 0.53 235393. 0.4600 35.26 0.2799 0.6010 0.0647 0.0301 2.059 18.538 13.161 1535.256 2.094 58.541 3.888 0.53 235704. 0.4356 38.20 0.3033 0.6303 0.0616 0.0296 2.025 18.237 12.533 1510.367 2.060 55.749 3.764 0.53 236032. 0.4115 41.13 0.3266 0.6568 0.0583 0.0290 1.983 17.853 11.872 1478.543 2.017 52.808 3.642 0.53 236377. 0.3875 44.07 0.3499 0.6806 0.0549 0.0282 1.930 17.381 11.178 1439.424 1.964 49.721 3.522 0.53 236739. 0.3637 47.01 0.3733 0.7016 0.0514 0.0273 1.868 16.820 10.455 1393.004 1.900 46.502 3.404 0.53 237119. 0.3399 49.95 0.3966 0.7197 0.0477 0.0263 1.796 16.173 9.705 1339.419 1.827 43.168 3.286 0.53 237516. 0.3162 52.89 0.4199 0.7346 0.0439 0.0251 1.715 15.441 8.933 1278.804 1.745 39.733 3.168 0.53 237930. 0.2924 55.83 0.4432 0.7460 0.0400 0.0238 1.624 14.626 8.141 1211.296 1.652 36.211 3.048 0.53 238362. 0.2686 58.76 0.4666 0.7535 0.0360 0.0223 1.525 13.729 7.332 1137.037 1.551 32.614 2.925 0.53 238812. 0.2446 61.70 0.4899 0.7562 0.0320 0.0207 1.416 12.753 6.510 1056.201 1.441 28.956 2.796 0.53 239279. 0.2203 64.64 0.5132 0.7530 0.0279 0.0190 1.299 11.700 5.677 968.996 1.322 25.250 2.657 0.53 239765. 0.1955 67.58 0.5366 0.7421 0.0238 0.0172 1.174 10.574 4.836 875.694 1.195 21.512 2.505 0.54 240268. 0.1701 70.52 0.5599 0.7208 0.0196 0.0152 1.041 9.378 3.992 776.638 1.059 17.757 2.331 0.54 240789. 0.1439 73.45 0.5832 0.6840 0.0155 0.0132 0.902 8.117 3.148 672.269 0.917 14.003 2.124 0.54 241328. 0.1164 76.39 0.6065 0.6229 0.0113 0.0110 0.755 6.800 2.309 563.140 0.768 10.271 1.860 0.54 241885. 0.0873 79.33 0.6299 0.5188 0.0073 0.0088 0.603 5.433 1.480 449.935 0.614 6.582 1.492 0.54 242460. 0.0560 82.27 0.6532 0.3266 0.0033 0.0065 0.447 4.026 0.666 333.453 0.455 2.961 0.905 0.54 243052. 0.0228 85.21 0.6765 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 0.0908 0.0289 2.951 23.253 24.132 2200.878 2.627 107.338 4.973 0.60 266270. 0.7545 3.34 0.0232 0.0706 0.0895 0.0294 2.997 23.609 23.779 2234.580 2.667 105.771 4.827 0.60 266437. 0.7269 6.67 0.0464 0.1370 0.0880 0.0298 3.039 23.944 23.396 2266.324 2.705 104.067 4.682 0.60 266619. 0.6995 10.01 0.0695 0.1993 0.0865 0.0302 3.078 24.252 22.981 2295.426 2.740 102.220 4.541 0.60 266815. 0.6723 13.35 0.0927 0.2576 0.0848 0.0305 3.113 24.524 22.531 2321.221 2.771 100.219 4.403 0.60 267027. 0.6454 16.68 0.1159 0.3121 0.0829 0.0308 3.142 24.754 22.045 2342.986 2.797 98.058 4.268 0.60 267255. 0.6188 20.02 0.1391 0.3630 0.0810 0.0310 3.165 24.934 21.521 2359.976 2.817 95.727 4.136 0.60 267499. 0.5926 23.36 0.1623 0.4104 0.0788 0.0312 3.180 25.055 20.958 2371.427 2.831 93.220 4.008 0.60 267760. 0.5667 26.69 0.1855 0.4546 0.0766 0.0312 3.187 25.109 20.353 2376.566 2.837 90.530 3.884 0.60 268039. 0.5412 30.03 0.2086 0.4955 0.0741 0.0312 3.184 25.089 19.706 2374.630 2.835 87.653 3.764 0.60 268336. 0.5160 33.37 0.2318 0.5335 0.0715 0.0311 3.171 24.986 19.016 2364.886 2.823 84.584 3.647 0.60 268652. 0.4912 36.70 0.2550 0.5686 0.0688 0.0308 3.147 24.793 18.283 2346.649 2.801 81.322 3.534 0.60 268986. 0.4666 40.04 0.2782 0.6009 0.0659 0.0305 3.110 24.504 17.506 2319.273 2.768 77.865 3.423 0.61 269338. 0.4424 43.38 0.3014 0.6306 0.0628 0.0300 3.060 24.112 16.685 2282.147 2.724 74.213 3.316 0.61 269710. 0.4183 46.71 0.3245 0.6576 0.0595 0.0294 2.997 23.609 15.820 2234.617 2.667 70.366 3.211 0.61 270101. 0.3944 50.05 0.3477 0.6819 0.0561 0.0286 2.918 22.991 14.911 2176.096 2.598 66.324 3.108 0.61 270512. 0.3706 53.39 0.3709 0.7036 0.0525 0.0277 2.825 22.256 13.962 2106.518 2.514 62.104 3.006 0.61 270942. 0.3469 56.72 0.3941 0.7225 0.0488 0.0266 2.717 21.406 12.978 2026.080 2.418 57.728 2.905 0.61 271392. 0.3232 60.06 0.4173 0.7384 0.0450 0.0254 2.595 20.444 11.964 1934.990 2.310 53.216 2.804 0.61 271861. 0.2996 63.40 0.4404 0.7510 0.0411 0.0241 2.459 19.371 10.923 1833.458 2.189 48.586 2.702 0.61 272350. 0.2758 66.73 0.4636 0.7599 0.0371 0.0226 2.309 18.190 9.859 1721.695 2.055 43.854 2.597 0.61 272859. 0.2519 70.07 0.4868 0.7643 0.0330 0.0210 2.146 16.904 8.776 1599.955 1.910 39.037 2.488 0.61 273388. 0.2276 73.41 0.5100 0.7632 0.0289 0.0193 1.969 15.516 7.679 1468.547 1.753 34.155 2.372 0.61 273937. 0.2030 76.74 0.5332 0.7551 0.0247 0.0175 1.781 14.029 6.570 1327.865 1.585 29.225 2.244 0.61 274506. 0.1777 80.08 0.5564 0.7373 0.0205 0.0155 1.580 12.450 5.456 1178.411 1.407 24.269 2.100 0.61 275095. 0.1515 83.42 0.5795 0.7054 0.0163 0.0134 1.369 10.785 4.341 1020.827 1.219 19.310 1.929 0.61 275704. 0.1241 86.75 0.6027 0.6513 0.0122 0.0113 1.148 9.043 3.231 855.920 1.022 14.373 1.712 0.61 276334. 0.0951 90.09 0.6259 0.5581 0.0080 0.0090 0.918 7.234 2.133 684.696 0.817 9.488 1.413 0.61 276983. 0.0637 93.43 0.6491 0.3851 0.0040 0.0067 0.682 5.371 1.054 508.348 0.607 4.687 0.940 0.62 277653. 0.0298 96.76 0.6723 -0.0034 0.0000 0.0043 0.439 3.456 -0.006 327.118 0.390 -0.026 -0.008 0.62 278322. 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 0.0921 0.0294 4.268 29.891 30.981 3182.841 3.377 137.805 4.415 0.68 299523. 0.7589 3.75 0.0232 0.0705 0.0908 0.0298 4.334 30.355 30.540 3232.220 3.429 135.842 4.286 0.68 299712. 0.7314 7.50 0.0463 0.1368 0.0894 0.0303 4.397 30.792 30.059 3278.748 3.479 133.700 4.158 0.68 299917. 0.7040 11.25 0.0695 0.1990 0.0878 0.0307 4.454 31.193 29.535 3321.411 3.524 131.372 4.033 0.68 300139. 0.6769 15.01 0.0927 0.2573 0.0861 0.0310 4.505 31.548 28.967 3359.214 3.564 128.845 3.911 0.68 300378. 0.6501 18.76 0.1158 0.3118 0.0843 0.0313 4.548 31.847 28.352 3391.102 3.598 126.108 3.792 0.68 300635. 0.6236 22.51 0.1390 0.3628 0.0823 0.0315 4.581 32.081 27.687 3415.973 3.624 123.151 3.676 0.68 300911. 0.5974 26.26 0.1622 0.4103 0.0802 0.0317 4.603 32.238 26.970 3432.702 3.642 119.964 3.564 0.68 301206. 0.5715 30.01 0.1853 0.4545 0.0779 0.0318 4.613 32.308 26.200 3440.160 3.650 116.539 3.454 0.68 301522. 0.5461 33.76 0.2085 0.4956 0.0754 0.0317 4.609 32.280 25.375 3437.234 3.647 112.869 3.348 0.68 301857. 0.5209 37.51 0.2317 0.5338 0.0728 0.0316 4.590 32.145 24.494 3422.851 3.632 108.948 3.246 0.68 302213. 0.4961 41.27 0.2548 0.5691 0.0700 0.0314 4.554 31.893 23.555 3396.004 3.603 104.775 3.146 0.68 302590. 0.4715 45.02 0.2780 0.6018 0.0671 0.0310 4.500 31.515 22.560 3355.764 3.561 100.347 3.049 0.68 302988. 0.4473 48.77 0.3012 0.6318 0.0639 0.0305 4.427 31.003 21.508 3301.247 3.503 95.665 2.955 0.68 303407. 0.4232 52.52 0.3243 0.6592 0.0606 0.0298 4.334 30.348 20.397 3231.522 3.429 90.728 2.863 0.68 303848. 0.3993 56.27 0.3475 0.6840 0.0572 0.0290 4.218 29.543 19.230 3145.729 3.338 85.536 2.773 0.68 304311. 0.3755 60.02 0.3707 0.7062 0.0535 0.0281 4.082 28.585 18.010 3043.728 3.229 80.110 2.684 0.68 304796. 0.3517 63.77 0.3938 0.7257 0.0498 0.0270 3.924 27.477 16.745 2925.812 3.104 74.480 2.596 0.68 305302. 0.3280 67.53 0.4170 0.7424 0.0459 0.0258 3.745 26.224 15.438 2792.301 2.963 68.669 2.508 0.68 305831. 0.3043 71.28 0.4402 0.7558 0.0419 0.0244 3.545 24.826 14.097 2643.495 2.805 62.702 2.419 0.68 306382. 0.2804 75.03 0.4633 0.7656 0.0378 0.0229 3.325 23.288 12.725 2479.724 2.631 56.601 2.328 0.69 306955. 0.2564 78.78 0.4865 0.7711 0.0337 0.0212 3.086 21.613 11.328 2301.357 2.442 50.389 2.233 0.69 307550. 0.2321 82.53 0.5097 0.7713 0.0295 0.0195 2.828 19.805 9.912 2108.849 2.238 44.087 2.132 0.69 308168. 0.2073 86.28 0.5328 0.7647 0.0252 0.0176 2.552 17.870 8.481 1902.778 2.019 37.722 2.022 0.69 308808. 0.1818 90.03 0.5560 0.7486 0.0209 0.0155 2.258 15.814 7.041 1683.886 1.787 31.320 1.897 0.69 309470. 0.1554 93.79 0.5792 0.7187 0.0166 0.0134 1.949 13.647 5.600 1453.130 1.542 24.911 1.748 0.69 310155. 0.1278 97.54 0.6023 0.6667 0.0124 0.0112 1.625 11.380 4.166 1211.747 1.286 18.529 1.559 0.69 310863. 0.0983 101.29 0.6255 0.5752 0.0082 0.0089 1.289 9.028 2.746 961.285 1.020 12.212 1.295 0.69 311594. 0.0663 105.04 0.6487 0.4006 0.0040 0.0065 0.944 6.608 1.349 703.609 0.747 6.002 0.870 0.69 312346. 0.0312 108.79 0.6718 -0.0110 -0.0001 0.0041 0.589 4.123 -0.022 439.002 0.466 -0.099 -0.023 0.69 313094. 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 0.0937 0.0303 6.043 38.090 38.900 4506.492 4.303 173.026 3.915 0.75 332760. 0.7541 4.16 0.0231 0.0695 0.0924 0.0308 6.127 38.619 38.364 4569.120 4.363 170.644 3.808 0.75 332971. 0.7285 8.33 0.0463 0.1351 0.0910 0.0311 6.207 39.119 37.778 4628.210 4.420 168.037 3.702 0.75 333200. 0.7028 12.49 0.0694 0.1969 0.0894 0.0315 6.279 39.577 37.138 4682.460 4.471 165.192 3.597 0.75 333447. 0.6770 16.65 0.0925 0.2550 0.0877 0.0318 6.344 39.984 36.442 4730.524 4.517 162.093 3.494 0.75 333714. 0.6514 20.81 0.1157 0.3095 0.0859 0.0321 6.398 40.325 35.685 4770.957 4.556 158.725 3.393 0.75 334001. 0.6259 24.98 0.1388 0.3605 0.0839 0.0323 6.440 40.590 34.864 4802.222 4.586 155.076 3.293 0.75 334309. 0.6005 29.14 0.1619 0.4082 0.0818 0.0325 6.467 40.763 33.977 4822.712 4.605 151.132 3.196 0.75 334639. 0.5752 33.30 0.1851 0.4526 0.0795 0.0325 6.478 40.831 33.022 4830.787 4.613 146.882 3.100 0.75 334990. 0.5502 37.46 0.2082 0.4940 0.0770 0.0325 6.470 40.780 31.996 4824.796 4.607 142.317 3.008 0.76 335364. 0.5254 41.63 0.2314 0.5324 0.0744 0.0323 6.441 40.597 30.897 4803.122 4.587 137.432 2.918 0.76 335761. 0.5009 45.79 0.2545 0.5681 0.0716 0.0321 6.389 40.268 29.726 4764.210 4.549 132.221 2.830 0.76 336181. 0.4765 49.95 0.2776 0.6010 0.0686 0.0317 6.312 39.781 28.481 4706.618 4.494 126.684 2.745 0.76 336624. 0.4524 54.11 0.3008 0.6314 0.0654 0.0312 6.208 39.125 27.163 4628.983 4.420 120.821 2.662 0.76 337092. 0.4284 58.28 0.3239 0.6592 0.0621 0.0305 6.075 38.288 25.771 4529.919 4.326 114.630 2.580 0.76 337583. 0.4045 62.44 0.3470 0.6846 0.0585 0.0297 5.911 37.259 24.306 4408.148 4.209 108.111 2.501 0.76 338098. 0.3808 66.60 0.3702 0.7074 0.0548 0.0287 5.717 36.035 22.772 4263.416 4.071 101.292 2.423 0.76 338637. 0.3570 70.76 0.3933 0.7275 0.0510 0.0276 5.493 34.622 21.179 4096.151 3.912 94.206 2.345 0.76 339201. 0.3333 74.93 0.4164 0.7449 0.0470 0.0263 5.239 33.022 19.534 3906.857 3.731 86.887 2.268 0.76 339788. 0.3095 79.09 0.4396 0.7592 0.0430 0.0249 4.956 31.240 17.843 3696.062 3.529 79.364 2.190 0.76 340401. 0.2856 83.25 0.4627 0.7699 0.0388 0.0233 4.646 29.281 16.112 3464.332 3.308 71.665 2.109 0.76 341037. 0.2615 87.41 0.4858 0.7764 0.0345 0.0216 4.308 27.152 14.348 3212.346 3.068 63.820 2.026 0.76 341698. 0.2370 91.58 0.5090 0.7775 0.0302 0.0198 3.944 24.858 12.558 2940.944 2.808 55.857 1.937 0.76 342384. 0.2119 95.74 0.5321 0.7718 0.0259 0.0178 3.555 22.409 10.748 2651.208 2.532 47.806 1.839 0.76 343094. 0.1862 99.90 0.5552 0.7563 0.0215 0.0158 3.144 19.817 8.926 2344.531 2.239 39.703 1.727 0.77 343829. 0.1593 104.06 0.5784 0.7265 0.0171 0.0136 2.712 17.096 7.101 2022.685 1.932 31.585 1.592 0.77 344589. 0.1310 108.23 0.6015 0.6735 0.0127 0.0114 2.264 14.266 5.282 1687.895 1.612 23.495 1.419 0.77 345375. 0.1007 112.39 0.6246 0.5792 0.0084 0.0090 1.801 11.350 3.480 1342.893 1.282 15.480 1.175 0.77 346185. 0.0677 116.55 0.6478 0.3993 0.0041 0.0067 1.329 8.375 1.707 990.893 0.946 7.594 0.781 0.77 347019. 0.0315 120.71 0.6709 -0.0137 -0.0001 0.0043 0.848 5.346 -0.036 632.533 0.604 -0.160 -0.026 0.77 347848. 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 0.0955 0.0333 8.842 50.663 47.989 6593.433 5.724 213.455 3.301 0.83 365978. 0.7062 4.59 0.0232 0.0651 0.0942 0.0336 8.916 51.087 47.359 6648.559 5.772 210.651 3.231 0.83 366212. 0.6866 9.19 0.0464 0.1273 0.0929 0.0339 8.982 51.465 46.664 6697.817 5.814 207.562 3.160 0.83 366466. 0.6666 13.78 0.0696 0.1866 0.0913 0.0341 9.038 51.787 45.902 6739.706 5.851 204.171 3.089 0.83 366740. 0.6463 18.37 0.0928 0.2431 0.0897 0.0342 9.082 52.040 45.067 6772.700 5.880 200.458 3.018 0.83 367037. 0.6257 22.97 0.1161 0.2968 0.0879 0.0344 9.113 52.213 44.155 6795.218 5.899 196.401 2.947 0.83 367356. 0.6048 27.56 0.1393 0.3476 0.0859 0.0344 9.126 52.293 43.162 6805.561 5.908 191.984 2.877 0.83 367699. 0.5836 32.16 0.1625 0.3956 0.0837 0.0344 9.122 52.265 42.084 6801.951 5.905 187.190 2.806 0.83 368065. 0.5622 36.75 0.1857 0.4408 0.0814 0.0343 9.096 52.116 40.918 6782.557 5.888 182.002 2.736 0.83 368457. 0.5405 41.34 0.2089 0.4833 0.0789 0.0341 9.046 51.832 39.661 6745.514 5.856 176.411 2.667 0.83 368873. 0.5187 45.94 0.2321 0.5232 0.0762 0.0338 8.970 51.397 38.311 6688.938 5.807 170.407 2.598 0.83 369314. 0.4966 50.53 0.2553 0.5603 0.0734 0.0334 8.866 50.798 36.867 6611.004 5.739 163.984 2.529 0.83 369782. 0.4743 55.12 0.2785 0.5948 0.0703 0.0329 8.730 50.021 35.329 6509.917 5.651 157.141 2.461 0.83 370275. 0.4518 59.72 0.3017 0.6268 0.0671 0.0323 8.561 49.053 33.696 6383.867 5.542 149.879 2.394 0.83 370795. 0.4292 64.31 0.3249 0.6561 0.0636 0.0315 8.356 47.878 31.969 6230.966 5.409 142.197 2.327 0.83 371341. 0.4063 68.90 0.3482 0.6828 0.0600 0.0306 8.112 46.481 30.147 6049.224 5.251 134.094 2.260 0.83 371914. 0.3833 73.50 0.3714 0.7068 0.0562 0.0295 7.830 44.865 28.238 5838.851 5.069 125.602 2.194 0.83 372513. 0.3600 78.09 0.3946 0.7277 0.0522 0.0283 7.512 43.044 26.251 5601.928 4.863 116.766 2.125 0.84 373139. 0.3363 82.69 0.4178 0.7452 0.0482 0.0270 7.159 41.020 24.197 5338.512 4.634 107.628 2.056 0.84 373792. 0.3123 87.28 0.4410 0.7591 0.0439 0.0255 6.771 38.796 22.083 5049.054 4.383 98.226 1.984 0.84 374471. 0.2879 91.87 0.4642 0.7687 0.0396 0.0239 6.348 36.374 19.918 4733.799 4.109 88.597 1.908 0.84 375177. 0.2630 96.47 0.4874 0.7732 0.0352 0.0222 5.892 33.762 17.711 4393.823 3.814 78.777 1.828 0.84 375911. 0.2376 101.06 0.5106 0.7711 0.0308 0.0204 5.406 30.976 15.468 4031.257 3.500 68.802 1.740 0.84 376671. 0.2114 105.65 0.5338 0.7600 0.0263 0.0184 4.893 28.036 13.200 3648.709 3.168 58.712 1.641 0.84 377458. 0.1841 110.25 0.5570 0.7365 0.0217 0.0164 4.357 24.965 10.915 3249.062 2.821 48.550 1.524 0.84 378273. 0.1555 114.84 0.5803 0.6945 0.0172 0.0143 3.803 21.791 8.625 2835.956 2.462 38.366 1.380 0.84 379115. 0.1251 119.44 0.6035 0.6241 0.0126 0.0122 3.237 18.546 6.343 2413.574 2.095 28.214 1.192 0.84 379984. 0.0927 124.03 0.6267 0.5067 0.0081 0.0100 2.664 15.265 4.082 1986.591 1.725 18.155 0.932 0.85 380881. 0.0581 128.62 0.6499 0.3044 0.0037 0.0079 2.092 11.988 1.857 1560.138 1.354 8.259 0.540 0.85 381804. 0.0227 133.22 0.6731 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 0.0969 0.0398 13.712 72.018 57.955 10224.697 8.137 257.783 2.571 0.90 399196. 0.6044 5.01 0.0232 0.0556 0.0958 0.0399 13.752 72.233 57.267 10255.159 8.161 254.723 2.533 0.90 399448. 0.5919 10.02 0.0464 0.1096 0.0945 0.0400 13.774 72.348 56.500 10271.536 8.174 251.314 2.495 0.90 399724. 0.5792 15.03 0.0696 0.1619 0.0931 0.0400 13.775 72.351 55.650 10271.952 8.174 247.530 2.457 0.90 400023. 0.5661 20.04 0.0928 0.2125 0.0915 0.0399 13.752 72.229 54.709 10254.669 8.160 243.344 2.420 0.90 400346. 0.5527 25.04 0.1160 0.2616 0.0897 0.0398 13.703 71.971 53.671 10218.035 8.131 238.728 2.382 0.91 400695. 0.5390 30.05 0.1392 0.3090 0.0878 0.0396 13.625 71.566 52.531 10160.507 8.085 233.657 2.345 0.91 401069. 0.5249 35.06 0.1624 0.3547 0.0858 0.0393 13.518 71.003 51.283 10080.633 8.022 228.109 2.307 0.91 401470. 0.5103 40.07 0.1856 0.3987 0.0835 0.0389 13.379 70.273 49.924 9977.013 7.939 222.063 2.270 0.91 401898. 0.4952 45.08 0.2088 0.4410 0.0810 0.0384 13.207 69.366 48.449 9848.246 7.837 215.503 2.231 0.91 402354. 0.4797 50.09 0.2320 0.4815 0.0783 0.0378 12.998 68.272 46.856 9692.870 7.713 208.415 2.193 0.91 402838. 0.4635 55.10 0.2552 0.5201 0.0755 0.0370 12.752 66.980 45.142 9509.419 7.567 200.790 2.153 0.91 403351. 0.4468 60.11 0.2784 0.5567 0.0724 0.0362 12.467 65.484 43.307 9296.999 7.398 192.628 2.113 0.91 403892. 0.4294 65.12 0.3016 0.5913 0.0691 0.0353 12.142 63.775 41.351 9054.388 7.205 183.931 2.071 0.91 404462. 0.4114 70.12 0.3248 0.6237 0.0657 0.0342 11.774 61.843 39.276 8780.176 6.987 174.700 2.029 0.91 405060. 0.3927 75.13 0.3480 0.6538 0.0620 0.0330 11.362 59.677 37.081 8472.607 6.742 164.935 1.985 0.91 405688. 0.3733 80.14 0.3712 0.6815 0.0581 0.0317 10.904 57.273 34.774 8131.324 6.471 154.675 1.940 0.91 406344. 0.3532 85.15 0.3944 0.7062 0.0541 0.0302 10.408 54.665 32.368 7761.060 6.176 143.975 1.892 0.91 407030. 0.3324 90.16 0.4176 0.7262 0.0500 0.0287 9.890 51.947 29.874 7375.152 5.869 132.881 1.837 0.91 407745. 0.3101 95.17 0.4408 0.7408 0.0457 0.0272 9.353 49.124 27.303 6974.292 5.550 121.443 1.776 0.91 408488. 0.2865 100.18 0.4640 0.7473 0.0412 0.0256 8.815 46.301 24.662 6573.572 5.231 109.697 1.702 0.91 409260. 0.2610 105.19 0.4872 0.7450 0.0367 0.0240 8.270 43.435 21.964 6166.665 4.907 97.695 1.615 0.92 410062. 0.2338 110.19 0.5104 0.7337 0.0321 0.0224 7.698 40.432 19.222 5740.340 4.568 85.498 1.519 0.92 410893. 0.2056 115.20 0.5336 0.7110 0.0275 0.0206 7.107 37.327 16.448 5299.441 4.217 73.159 1.408 0.92 411753. 0.1763 120.21 0.5568 0.6730 0.0228 0.0189 6.504 34.162 13.655 4850.098 3.860 60.735 1.277 0.92 412642. 0.1457 125.22 0.5800 0.6148 0.0182 0.0171 5.897 30.971 10.857 4397.065 3.499 48.293 1.120 0.92 413561. 0.1140 130.23 0.6032 0.5297 0.0135 0.0154 5.292 27.796 8.073 3946.263 3.140 35.907 0.928 0.92 414509. 0.0814 135.24 0.6264 0.4084 0.0089 0.0136 4.699 24.680 5.322 3503.890 2.788 23.671 0.689 0.92 415487. 0.0491 140.25 0.6496 0.2381 0.0044 0.0120 4.124 21.661 2.625 3075.270 2.447 11.677 0.387 0.92 416495. 0.0194 145.26 0.6728 -0.0019 0.0000 0.0103 3.558 18.688 -0.018 2653.225 2.111 -0.080 -0.003 0.92 417521. 0.0000