20.5x10PN (205x10PN.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 0.0881 0.0340 0.010 0.625 0.496 7.397 0.071 2.205 30.394 0.08 45252. 0.6125 0.44 0.0227 0.0573 0.0866 0.0344 0.010 0.632 0.488 7.472 0.071 2.169 29.595 0.08 45280. 0.5915 0.88 0.0455 0.1114 0.0851 0.0347 0.010 0.637 0.479 7.541 0.072 2.130 28.797 0.08 45310. 0.5703 1.32 0.0682 0.1625 0.0834 0.0350 0.010 0.643 0.469 7.603 0.073 2.088 28.002 0.08 45342. 0.5491 1.77 0.0909 0.2106 0.0816 0.0352 0.010 0.647 0.459 7.655 0.073 2.043 27.213 0.08 45378. 0.5279 2.21 0.1137 0.2557 0.0797 0.0354 0.010 0.651 0.448 7.697 0.074 1.995 26.429 0.08 45415. 0.5066 2.65 0.1364 0.2978 0.0776 0.0356 0.010 0.653 0.437 7.726 0.074 1.944 25.653 0.08 45456. 0.4853 3.09 0.1591 0.3370 0.0754 0.0356 0.010 0.654 0.425 7.739 0.074 1.889 24.883 0.08 45499. 0.4641 3.53 0.1819 0.3734 0.0731 0.0356 0.010 0.654 0.411 7.736 0.074 1.830 24.121 0.08 45545. 0.4428 3.97 0.2046 0.4069 0.0706 0.0355 0.010 0.652 0.397 7.714 0.074 1.768 23.366 0.08 45593. 0.4216 4.41 0.2273 0.4376 0.0680 0.0353 0.010 0.648 0.383 7.672 0.073 1.702 22.618 0.08 45645. 0.4004 4.85 0.2501 0.4656 0.0652 0.0350 0.010 0.643 0.367 7.607 0.073 1.632 21.874 0.08 45700. 0.3792 5.30 0.2728 0.4907 0.0623 0.0346 0.010 0.636 0.350 7.521 0.072 1.559 21.135 0.08 45758. 0.3581 5.74 0.2956 0.5130 0.0592 0.0341 0.010 0.626 0.333 7.412 0.071 1.483 20.396 0.08 45818. 0.3370 6.18 0.3183 0.5325 0.0561 0.0335 0.010 0.615 0.316 7.280 0.070 1.403 19.657 0.08 45882. 0.3160 6.62 0.3410 0.5489 0.0528 0.0328 0.010 0.602 0.297 7.125 0.068 1.321 18.913 0.08 45949. 0.2951 7.06 0.3638 0.5622 0.0494 0.0320 0.009 0.587 0.278 6.946 0.066 1.237 18.161 0.08 46020. 0.2741 7.50 0.3865 0.5722 0.0459 0.0310 0.009 0.570 0.259 6.743 0.064 1.150 17.396 0.08 46093. 0.2532 7.94 0.4092 0.5785 0.0424 0.0300 0.009 0.551 0.239 6.516 0.062 1.061 16.611 0.08 46170. 0.2322 8.39 0.4320 0.5808 0.0388 0.0288 0.008 0.529 0.218 6.264 0.060 0.970 15.798 0.08 46250. 0.2112 8.83 0.4547 0.5785 0.0351 0.0276 0.008 0.506 0.197 5.987 0.057 0.878 14.949 0.08 46333. 0.1901 9.27 0.4774 0.5709 0.0313 0.0262 0.008 0.481 0.176 5.685 0.054 0.783 14.050 0.08 46420. 0.1688 9.71 0.5002 0.5570 0.0275 0.0247 0.007 0.453 0.155 5.359 0.051 0.688 13.084 0.08 46510. 0.1472 10.15 0.5229 0.5352 0.0236 0.0230 0.007 0.423 0.133 5.007 0.048 0.591 12.028 0.08 46603. 0.1254 10.59 0.5456 0.5037 0.0197 0.0213 0.006 0.391 0.111 4.630 0.044 0.493 10.847 0.08 46700. 0.1033 11.03 0.5684 0.4592 0.0157 0.0195 0.006 0.357 0.089 4.229 0.040 0.394 9.494 0.08 46800. 0.0808 11.48 0.5911 0.3971 0.0118 0.0175 0.005 0.322 0.066 3.805 0.036 0.295 7.894 0.08 46903. 0.0582 11.92 0.6138 0.3099 0.0078 0.0155 0.005 0.284 0.044 3.359 0.032 0.195 5.932 0.08 47010. 0.0356 12.36 0.6366 0.1845 0.0039 0.0133 0.004 0.244 0.022 2.892 0.028 0.097 3.405 0.08 47119. 0.0144 12.80 0.6593 -0.0046 -0.0001 0.0111 0.003 0.203 0.000 2.404 0.023 -0.002 -0.081 0.08 47229. 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 0.0885 0.0308 0.072 2.261 1.993 53.503 0.255 8.864 16.894 0.16 90501. 0.6826 0.89 0.0228 0.0638 0.0871 0.0312 0.073 2.289 1.960 54.164 0.259 8.719 16.415 0.16 90558. 0.6578 1.77 0.0457 0.1239 0.0855 0.0315 0.073 2.315 1.925 54.779 0.262 8.563 15.941 0.16 90619. 0.6331 2.66 0.0685 0.1804 0.0838 0.0318 0.074 2.338 1.888 55.334 0.264 8.396 15.472 0.16 90684. 0.6084 3.55 0.0914 0.2334 0.0820 0.0321 0.075 2.359 1.847 55.815 0.266 8.216 15.011 0.16 90755. 0.5839 4.43 0.1142 0.2829 0.0801 0.0323 0.075 2.375 1.804 56.208 0.268 8.023 14.556 0.16 90831. 0.5596 5.32 0.1370 0.3291 0.0781 0.0325 0.076 2.388 1.757 56.495 0.270 7.817 14.109 0.16 90912. 0.5354 6.21 0.1599 0.3720 0.0759 0.0326 0.076 2.395 1.708 56.661 0.271 7.596 13.670 0.16 90999. 0.5113 7.09 0.1827 0.4117 0.0735 0.0326 0.076 2.396 1.655 56.688 0.271 7.360 13.240 0.16 91092. 0.4875 7.98 0.2055 0.4484 0.0710 0.0325 0.076 2.390 1.598 56.560 0.270 7.109 12.817 0.16 91190. 0.4638 8.87 0.2284 0.4821 0.0683 0.0324 0.075 2.378 1.539 56.263 0.269 6.843 12.403 0.16 91294. 0.4403 9.75 0.2512 0.5129 0.0655 0.0321 0.075 2.358 1.475 55.786 0.266 6.563 11.996 0.16 91405. 0.4171 10.64 0.2741 0.5409 0.0626 0.0317 0.074 2.330 1.409 55.124 0.263 6.268 11.595 0.16 91521. 0.3940 11.53 0.2969 0.5660 0.0595 0.0312 0.073 2.294 1.340 54.272 0.259 5.961 11.200 0.16 91644. 0.3711 12.41 0.3197 0.5882 0.0563 0.0306 0.071 2.249 1.268 53.226 0.254 5.642 10.809 0.16 91772. 0.3484 13.30 0.3426 0.6076 0.0530 0.0299 0.070 2.197 1.194 51.984 0.248 5.312 10.420 0.16 91908. 0.3259 14.19 0.3654 0.6239 0.0496 0.0291 0.068 2.136 1.118 50.540 0.241 4.972 10.031 0.16 92049. 0.3035 15.07 0.3882 0.6371 0.0462 0.0281 0.066 2.066 1.039 48.893 0.233 4.622 9.640 0.16 92198. 0.2813 15.96 0.4111 0.6468 0.0426 0.0271 0.063 1.988 0.959 47.039 0.225 4.264 9.244 0.16 92352. 0.2591 16.85 0.4339 0.6528 0.0389 0.0259 0.060 1.901 0.876 44.974 0.215 3.898 8.839 0.16 92514. 0.2369 17.73 0.4568 0.6546 0.0352 0.0246 0.057 1.804 0.793 42.697 0.204 3.525 8.420 0.16 92681. 0.2146 18.62 0.4796 0.6514 0.0314 0.0231 0.054 1.699 0.707 40.206 0.192 3.146 7.979 0.16 92856. 0.1921 19.51 0.5024 0.6421 0.0276 0.0216 0.050 1.585 0.621 37.499 0.179 2.761 7.508 0.16 93038. 0.1693 20.39 0.5253 0.6252 0.0237 0.0199 0.046 1.461 0.533 34.578 0.165 2.371 6.993 0.16 93226. 0.1461 21.28 0.5481 0.5983 0.0197 0.0181 0.042 1.329 0.445 31.444 0.150 1.978 6.413 0.17 93421. 0.1224 22.17 0.5709 0.5576 0.0158 0.0162 0.038 1.188 0.356 28.104 0.134 1.581 5.738 0.17 93622. 0.0979 23.05 0.5938 0.4967 0.0118 0.0141 0.033 1.038 0.266 24.564 0.117 1.184 4.914 0.17 93831. 0.0726 23.94 0.6166 0.4040 0.0079 0.0120 0.028 0.881 0.177 20.835 0.099 0.787 3.850 0.17 94046. 0.0463 24.83 0.6395 0.2564 0.0039 0.0097 0.023 0.716 0.088 16.931 0.081 0.391 2.356 0.17 94267. 0.0200 25.71 0.6623 -0.0038 0.0000 0.0074 0.017 0.542 -0.001 12.829 0.061 -0.004 -0.034 0.17 94482. 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 0.0890 0.0296 0.233 4.885 4.509 173.395 0.552 20.056 11.795 0.24 135748. 0.7169 1.33 0.0229 0.0669 0.0876 0.0300 0.236 4.951 4.436 175.724 0.559 19.730 11.449 0.24 135832. 0.6902 2.67 0.0458 0.1298 0.0860 0.0303 0.239 5.012 4.357 177.896 0.566 19.379 11.108 0.24 135924. 0.6637 4.00 0.0687 0.1889 0.0843 0.0307 0.241 5.067 4.272 179.863 0.573 19.001 10.773 0.24 136023. 0.6373 5.33 0.0916 0.2441 0.0825 0.0310 0.244 5.116 4.181 181.578 0.578 18.596 10.443 0.24 136130. 0.6112 6.67 0.1145 0.2957 0.0806 0.0312 0.245 5.156 4.083 182.991 0.582 18.160 10.120 0.24 136244. 0.5853 8.00 0.1373 0.3438 0.0785 0.0314 0.247 5.185 3.978 184.045 0.586 17.694 9.803 0.24 136367. 0.5597 9.33 0.1602 0.3884 0.0763 0.0315 0.248 5.203 3.866 184.681 0.588 17.195 9.494 0.24 136498. 0.5343 10.66 0.1831 0.4298 0.0740 0.0315 0.248 5.208 3.746 184.841 0.588 16.662 9.192 0.24 136637. 0.5092 12.00 0.2060 0.4679 0.0714 0.0314 0.247 5.197 3.618 184.466 0.587 16.094 8.897 0.24 136786. 0.4844 13.33 0.2289 0.5031 0.0688 0.0313 0.246 5.170 3.483 183.509 0.584 15.491 8.608 0.24 136943. 0.4598 14.66 0.2518 0.5353 0.0659 0.0310 0.244 5.126 3.340 181.933 0.579 14.856 8.326 0.24 137109. 0.4355 16.00 0.2747 0.5646 0.0630 0.0306 0.241 5.063 3.190 179.716 0.572 14.189 8.051 0.24 137284. 0.4116 17.33 0.2976 0.5911 0.0599 0.0301 0.237 4.982 3.033 176.842 0.563 13.492 7.780 0.25 137469. 0.3878 18.66 0.3205 0.6148 0.0567 0.0295 0.232 4.882 2.871 173.297 0.552 12.770 7.514 0.25 137664. 0.3644 20.00 0.3434 0.6356 0.0534 0.0288 0.227 4.763 2.703 169.067 0.538 12.022 7.251 0.25 137867. 0.3412 21.33 0.3662 0.6536 0.0499 0.0280 0.220 4.625 2.529 164.140 0.522 11.251 6.990 0.25 138081. 0.3182 22.66 0.3891 0.6685 0.0464 0.0270 0.213 4.466 2.351 158.504 0.505 10.459 6.729 0.25 138304. 0.2953 24.00 0.4120 0.6803 0.0428 0.0259 0.204 4.287 2.169 152.146 0.484 9.648 6.467 0.25 138537. 0.2726 25.33 0.4349 0.6884 0.0391 0.0247 0.195 4.087 1.983 145.056 0.462 8.819 6.200 0.25 138780. 0.2499 26.66 0.4578 0.6926 0.0354 0.0234 0.184 3.866 1.793 137.224 0.437 7.974 5.926 0.25 139033. 0.2271 28.00 0.4807 0.6922 0.0316 0.0219 0.173 3.624 1.600 128.645 0.409 7.115 5.640 0.25 139297. 0.2042 29.33 0.5036 0.6860 0.0277 0.0203 0.160 3.362 1.404 119.316 0.380 6.243 5.335 0.25 139570. 0.1809 30.66 0.5265 0.6726 0.0238 0.0186 0.146 3.078 1.205 109.240 0.348 5.360 5.004 0.25 139853. 0.1572 31.99 0.5494 0.6494 0.0198 0.0168 0.132 2.773 1.005 98.424 0.313 4.469 4.630 0.25 140147. 0.1328 33.33 0.5723 0.6125 0.0159 0.0148 0.117 2.448 0.803 86.887 0.277 3.572 4.192 0.25 140451. 0.1075 34.66 0.5951 0.5547 0.0119 0.0127 0.100 2.103 0.601 74.655 0.238 2.673 3.651 0.25 140765. 0.0810 35.99 0.6180 0.4622 0.0079 0.0105 0.083 1.740 0.399 61.768 0.197 1.774 2.929 0.25 141089. 0.0529 37.33 0.6409 0.3042 0.0039 0.0082 0.065 1.360 0.198 48.271 0.154 0.880 1.859 0.25 141421. 0.0237 38.66 0.6638 -0.0088 -0.0001 0.0058 0.046 0.959 -0.004 34.025 0.108 -0.017 -0.052 0.25 141737. 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 0.0897 0.0290 0.541 8.526 8.073 403.488 0.963 35.910 9.075 0.33 180988. 0.7381 1.78 0.0229 0.0687 0.0882 0.0294 0.549 8.646 7.943 409.171 0.977 35.331 8.805 0.33 181102. 0.7103 3.56 0.0459 0.1333 0.0866 0.0298 0.556 8.758 7.803 414.475 0.989 34.706 8.539 0.33 181225. 0.6827 5.34 0.0688 0.1938 0.0850 0.0302 0.562 8.860 7.651 419.289 1.001 34.033 8.277 0.33 181358. 0.6553 7.12 0.0917 0.2504 0.0832 0.0305 0.568 8.949 7.489 423.496 1.011 33.309 8.020 0.33 181500. 0.6282 8.90 0.1146 0.3032 0.0812 0.0307 0.573 9.022 7.314 426.974 1.019 32.532 7.769 0.33 181654. 0.6014 10.68 0.1376 0.3523 0.0791 0.0309 0.576 9.077 7.127 429.587 1.026 31.699 7.524 0.33 181818. 0.5749 12.46 0.1605 0.3980 0.0769 0.0310 0.578 9.111 6.926 431.195 1.029 30.807 7.285 0.33 181993. 0.5488 14.24 0.1834 0.4403 0.0745 0.0310 0.579 9.121 6.712 431.651 1.030 29.854 7.053 0.33 182180. 0.5230 16.02 0.2063 0.4794 0.0720 0.0310 0.578 9.103 6.483 430.819 1.029 28.838 6.826 0.33 182379. 0.4975 17.80 0.2293 0.5155 0.0693 0.0308 0.575 9.056 6.241 428.579 1.023 27.759 6.605 0.33 182589. 0.4723 19.58 0.2522 0.5485 0.0665 0.0306 0.570 8.977 5.985 424.843 1.014 26.621 6.390 0.33 182812. 0.4474 21.36 0.2751 0.5787 0.0635 0.0302 0.563 8.866 5.716 419.558 1.002 25.426 6.180 0.33 183047. 0.4229 23.14 0.2980 0.6061 0.0604 0.0297 0.553 8.720 5.436 412.681 0.985 24.178 5.974 0.33 183294. 0.3987 24.92 0.3210 0.6308 0.0571 0.0291 0.542 8.541 5.144 404.177 0.965 22.882 5.773 0.33 183554. 0.3748 26.70 0.3439 0.6527 0.0538 0.0283 0.528 8.326 4.843 394.014 0.941 21.542 5.575 0.33 183827. 0.3512 28.48 0.3668 0.6717 0.0503 0.0275 0.512 8.075 4.532 382.162 0.912 20.160 5.379 0.33 184113. 0.3278 30.26 0.3897 0.6879 0.0468 0.0265 0.494 7.789 4.213 368.590 0.880 18.741 5.185 0.33 184412. 0.3046 32.04 0.4127 0.7010 0.0432 0.0254 0.474 7.465 3.886 353.267 0.843 17.286 4.990 0.33 184724. 0.2815 33.82 0.4356 0.7107 0.0394 0.0242 0.451 7.103 3.552 336.168 0.803 15.800 4.793 0.33 185049. 0.2585 35.60 0.4585 0.7166 0.0357 0.0228 0.425 6.704 3.211 317.270 0.757 14.284 4.591 0.33 185387. 0.2355 37.39 0.4814 0.7181 0.0318 0.0213 0.398 6.266 2.865 296.559 0.708 12.743 4.382 0.33 185740. 0.2123 39.17 0.5044 0.7143 0.0279 0.0197 0.367 5.790 2.513 274.027 0.654 11.179 4.160 0.33 186105. 0.1888 40.95 0.5273 0.7035 0.0240 0.0180 0.335 5.276 2.157 249.683 0.596 9.596 3.919 0.33 186484. 0.1648 42.73 0.5502 0.6834 0.0200 0.0161 0.300 4.724 1.798 223.546 0.534 7.998 3.648 0.33 186877. 0.1400 44.51 0.5732 0.6498 0.0160 0.0141 0.262 4.134 1.437 195.659 0.467 6.390 3.330 0.33 187284. 0.1143 46.29 0.5961 0.5952 0.0119 0.0119 0.223 3.510 1.074 166.090 0.397 4.778 2.933 0.33 187704. 0.0870 48.07 0.6190 0.5043 0.0079 0.0097 0.181 2.851 0.712 134.935 0.322 3.167 2.393 0.33 188137. 0.0578 49.85 0.6419 0.3408 0.0039 0.0074 0.137 2.162 0.352 102.303 0.244 1.564 1.559 0.33 188581. 0.0265 51.63 0.6649 -0.0177 -0.0001 0.0049 0.091 1.430 -0.012 67.673 0.162 -0.052 -0.078 0.33 188988. 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 0.0905 0.0288 1.050 13.240 12.729 783.231 1.496 56.619 7.371 0.41 226221. 0.7528 2.23 0.0229 0.0698 0.0890 0.0293 1.066 13.432 12.526 794.609 1.518 55.715 7.150 0.41 226364. 0.7243 4.45 0.0459 0.1353 0.0875 0.0297 1.080 13.612 12.306 805.235 1.538 54.737 6.932 0.41 226518. 0.6960 6.68 0.0688 0.1967 0.0858 0.0300 1.093 13.775 12.069 814.881 1.556 53.684 6.718 0.41 226685. 0.6680 8.91 0.0918 0.2541 0.0840 0.0303 1.104 13.918 11.814 823.321 1.572 52.550 6.509 0.41 226864. 0.6403 11.13 0.1147 0.3077 0.0820 0.0306 1.113 14.036 11.540 830.306 1.586 51.332 6.304 0.41 227056. 0.6130 13.36 0.1376 0.3576 0.0799 0.0308 1.121 14.125 11.246 835.573 1.596 50.024 6.105 0.41 227262. 0.5860 15.59 0.1606 0.4039 0.0777 0.0309 1.125 14.180 10.931 838.839 1.602 48.623 5.911 0.41 227483. 0.5594 17.81 0.1835 0.4468 0.0753 0.0309 1.126 14.197 10.595 839.817 1.604 47.125 5.722 0.41 227717. 0.5331 20.04 0.2065 0.4866 0.0727 0.0309 1.124 14.170 10.235 838.231 1.601 45.527 5.538 0.41 227966. 0.5072 22.27 0.2294 0.5232 0.0700 0.0307 1.118 14.096 9.854 833.842 1.593 43.829 5.360 0.41 228230. 0.4816 24.49 0.2523 0.5569 0.0672 0.0304 1.108 13.971 9.451 826.478 1.578 42.036 5.186 0.41 228510. 0.4564 26.72 0.2753 0.5878 0.0642 0.0300 1.094 13.794 9.027 816.025 1.558 40.153 5.018 0.41 228804. 0.4315 28.95 0.2982 0.6158 0.0610 0.0295 1.076 13.564 8.585 802.399 1.532 38.187 4.853 0.41 229114. 0.4070 31.17 0.3212 0.6412 0.0578 0.0289 1.053 13.279 8.126 785.535 1.500 36.144 4.692 0.41 229440. 0.3828 33.40 0.3441 0.6639 0.0544 0.0282 1.026 12.938 7.651 765.366 1.462 34.030 4.534 0.41 229783. 0.3589 35.63 0.3670 0.6838 0.0509 0.0273 0.995 12.540 7.161 741.832 1.417 31.850 4.378 0.41 230141. 0.3353 37.85 0.3900 0.7009 0.0473 0.0263 0.959 12.085 6.657 714.870 1.365 29.610 4.224 0.41 230515. 0.3119 40.08 0.4129 0.7151 0.0436 0.0252 0.918 11.570 6.141 684.425 1.307 27.315 4.070 0.41 230906. 0.2887 42.31 0.4359 0.7260 0.0399 0.0240 0.872 10.995 5.614 650.441 1.242 24.969 3.915 0.41 231313. 0.2655 44.53 0.4588 0.7334 0.0361 0.0226 0.822 10.360 5.076 612.877 1.171 22.578 3.757 0.41 231738. 0.2422 46.76 0.4817 0.7366 0.0322 0.0211 0.767 9.664 4.529 571.700 1.092 20.145 3.593 0.41 232179. 0.2189 48.99 0.5047 0.7346 0.0282 0.0194 0.707 8.907 3.974 526.900 1.006 17.676 3.421 0.41 232636. 0.1952 51.21 0.5276 0.7261 0.0242 0.0176 0.642 8.089 3.412 478.487 0.914 15.176 3.234 0.41 233111. 0.1710 53.44 0.5506 0.7087 0.0202 0.0157 0.572 7.210 2.845 426.506 0.815 12.653 3.025 0.41 233603. 0.1460 55.67 0.5735 0.6783 0.0162 0.0137 0.498 6.272 2.274 371.041 0.709 10.114 2.779 0.41 234112. 0.1200 57.89 0.5964 0.6272 0.0121 0.0115 0.419 5.278 1.701 312.226 0.596 7.567 2.471 0.41 234637. 0.0923 60.12 0.6194 0.5394 0.0080 0.0092 0.336 4.230 1.129 250.254 0.478 5.023 2.047 0.41 235180. 0.0623 62.35 0.6423 0.3747 0.0040 0.0068 0.249 3.133 0.560 185.347 0.354 2.492 1.371 0.41 235736. 0.0294 64.57 0.6653 -0.0169 -0.0001 0.0043 0.156 1.965 -0.015 116.265 0.222 -0.068 -0.060 0.42 236234. 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 0.0915 0.0289 1.820 19.115 18.537 1356.949 2.160 82.453 6.196 0.49 271444. 0.7636 2.69 0.0231 0.0708 0.0900 0.0293 1.847 19.401 18.243 1377.226 2.192 81.145 6.008 0.49 271616. 0.7345 5.38 0.0462 0.1372 0.0885 0.0298 1.872 19.668 17.924 1396.145 2.222 79.728 5.823 0.49 271804. 0.7057 8.06 0.0692 0.1995 0.0868 0.0301 1.895 19.909 17.581 1413.306 2.249 78.199 5.642 0.49 272006. 0.6771 10.75 0.0923 0.2576 0.0849 0.0304 1.915 20.120 17.210 1428.294 2.273 76.550 5.465 0.49 272224. 0.6489 13.44 0.1154 0.3118 0.0830 0.0307 1.932 20.295 16.811 1440.669 2.293 74.775 5.293 0.49 272457. 0.6211 16.13 0.1385 0.3623 0.0809 0.0309 1.944 20.426 16.382 1449.957 2.308 72.868 5.125 0.49 272708. 0.5937 18.82 0.1615 0.4092 0.0786 0.0310 1.952 20.506 15.922 1455.653 2.317 70.822 4.961 0.49 272975. 0.5666 21.50 0.1846 0.4527 0.0762 0.0311 1.954 20.528 15.430 1457.245 2.319 68.631 4.802 0.49 273260. 0.5400 24.19 0.2077 0.4930 0.0736 0.0310 1.950 20.486 14.904 1454.237 2.314 66.292 4.648 0.49 273563. 0.5136 26.88 0.2308 0.5301 0.0708 0.0308 1.939 20.373 14.345 1446.208 2.302 63.805 4.499 0.49 273884. 0.4877 29.57 0.2538 0.5643 0.0679 0.0305 1.921 20.185 13.754 1432.849 2.280 61.176 4.354 0.49 274223. 0.4621 32.25 0.2769 0.5957 0.0648 0.0301 1.896 19.919 13.133 1413.961 2.250 58.413 4.213 0.49 274581. 0.4370 34.94 0.3000 0.6243 0.0616 0.0296 1.863 19.573 12.484 1389.401 2.211 55.528 4.075 0.49 274958. 0.4121 37.63 0.3231 0.6502 0.0583 0.0290 1.823 19.145 11.809 1359.050 2.163 52.528 3.941 0.49 275354. 0.3877 40.32 0.3461 0.6734 0.0548 0.0282 1.774 18.634 11.111 1322.798 2.105 49.424 3.810 0.49 275770. 0.3635 43.01 0.3692 0.6940 0.0513 0.0273 1.717 18.039 10.392 1280.534 2.038 46.222 3.681 0.49 276205. 0.3396 45.69 0.3923 0.7117 0.0476 0.0263 1.652 17.357 9.652 1232.154 1.961 42.932 3.553 0.49 276659. 0.3159 48.38 0.4154 0.7266 0.0439 0.0251 1.579 16.588 8.894 1177.554 1.874 39.560 3.426 0.49 277134. 0.2924 51.07 0.4385 0.7384 0.0401 0.0238 1.497 15.730 8.119 1116.645 1.777 36.114 3.298 0.49 277629. 0.2690 53.76 0.4615 0.7466 0.0362 0.0224 1.407 14.782 7.329 1049.347 1.670 32.599 3.168 0.49 278144. 0.2455 56.45 0.4846 0.7507 0.0322 0.0208 1.308 13.744 6.525 975.613 1.553 29.024 3.034 0.49 278679. 0.2218 59.13 0.5077 0.7498 0.0282 0.0191 1.201 12.614 5.710 895.424 1.425 25.396 2.892 0.49 279235. 0.1978 61.82 0.5308 0.7423 0.0241 0.0172 1.085 11.394 4.884 808.806 1.287 21.724 2.739 0.49 279811. 0.1732 64.51 0.5538 0.7258 0.0200 0.0153 0.960 10.084 4.051 715.845 1.139 18.017 2.567 0.50 280408. 0.1478 67.20 0.5769 0.6959 0.0159 0.0131 0.827 8.688 3.212 616.704 0.982 14.287 2.362 0.50 281026. 0.1212 69.88 0.6000 0.6441 0.0117 0.0109 0.686 7.207 2.371 511.639 0.814 10.548 2.102 0.50 281664. 0.0927 72.57 0.6231 0.5513 0.0076 0.0085 0.538 5.649 1.532 401.009 0.638 6.815 1.733 0.50 282321. 0.0614 75.26 0.6461 0.3659 0.0034 0.0061 0.382 4.018 0.697 285.199 0.454 3.102 1.109 0.50 282995. 0.0265 77.95 0.6692 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 0.0928 0.0292 2.918 26.278 25.579 2176.320 2.969 113.777 5.331 0.57 316652. 0.7717 3.12 0.0230 0.0707 0.0913 0.0296 2.963 26.677 25.182 2209.302 3.014 112.012 5.170 0.57 316854. 0.7426 6.24 0.0459 0.1371 0.0898 0.0301 3.004 27.048 24.752 2240.075 3.056 110.097 5.012 0.57 317072. 0.7137 9.36 0.0689 0.1993 0.0881 0.0304 3.041 27.385 24.287 2267.985 3.094 108.026 4.857 0.57 317308. 0.6851 12.48 0.0919 0.2575 0.0862 0.0308 3.074 27.680 23.784 2292.381 3.127 105.791 4.706 0.57 317562. 0.6569 15.60 0.1148 0.3118 0.0843 0.0310 3.101 27.923 23.242 2312.554 3.155 103.382 4.559 0.57 317834. 0.6290 18.72 0.1378 0.3624 0.0822 0.0312 3.122 28.107 22.660 2327.750 3.175 100.790 4.415 0.57 318126. 0.6016 21.84 0.1608 0.4095 0.0799 0.0314 3.134 28.220 22.034 2337.169 3.188 98.006 4.276 0.57 318437. 0.5745 24.97 0.1837 0.4532 0.0775 0.0314 3.138 28.254 21.363 2339.988 3.192 95.023 4.141 0.57 318769. 0.5478 28.09 0.2067 0.4937 0.0749 0.0313 3.132 28.199 20.646 2335.418 3.186 91.834 4.010 0.57 319121. 0.5215 31.21 0.2296 0.5312 0.0721 0.0312 3.115 28.047 19.883 2322.767 3.169 88.441 3.883 0.57 319494. 0.4955 34.33 0.2526 0.5658 0.0692 0.0309 3.086 27.790 19.076 2301.537 3.140 84.850 3.759 0.57 319889. 0.4700 37.45 0.2756 0.5975 0.0661 0.0305 3.046 27.426 18.227 2271.402 3.099 81.074 3.640 0.57 320305. 0.4448 40.57 0.2985 0.6266 0.0629 0.0300 2.993 26.952 17.339 2232.132 3.045 77.126 3.523 0.57 320742. 0.4199 43.69 0.3215 0.6531 0.0595 0.0293 2.928 26.366 16.416 2183.552 2.979 73.019 3.410 0.57 321202. 0.3955 46.81 0.3445 0.6770 0.0561 0.0285 2.850 25.664 15.460 2125.485 2.900 68.766 3.299 0.57 321685. 0.3713 49.93 0.3674 0.6983 0.0525 0.0276 2.760 24.847 14.473 2057.769 2.807 64.378 3.190 0.57 322189. 0.3474 53.05 0.3904 0.7170 0.0488 0.0266 2.656 23.911 13.459 1980.238 2.701 59.866 3.083 0.57 322717. 0.3237 56.17 0.4134 0.7329 0.0450 0.0254 2.538 22.854 12.419 1892.731 2.582 55.240 2.976 0.57 323267. 0.3002 59.29 0.4363 0.7458 0.0412 0.0241 2.407 21.675 11.356 1795.105 2.449 50.510 2.869 0.57 323840. 0.2767 62.41 0.4593 0.7555 0.0372 0.0226 2.263 20.373 10.271 1687.240 2.302 45.684 2.761 0.58 324437. 0.2533 65.53 0.4823 0.7613 0.0332 0.0211 2.104 18.946 9.167 1569.052 2.140 40.774 2.650 0.58 325057. 0.2296 68.66 0.5052 0.7625 0.0292 0.0193 1.932 17.394 8.046 1440.504 1.965 35.788 2.533 0.58 325701. 0.2057 71.78 0.5282 0.7577 0.0251 0.0175 1.746 15.717 6.911 1301.630 1.776 30.739 2.408 0.58 326368. 0.1812 74.90 0.5512 0.7448 0.0209 0.0155 1.546 13.917 5.764 1152.554 1.572 25.639 2.268 0.58 327059. 0.1559 78.02 0.5741 0.7198 0.0167 0.0133 1.332 11.996 4.610 993.519 1.355 20.504 2.105 0.58 327774. 0.1293 81.14 0.5971 0.6751 0.0125 0.0111 1.106 9.961 3.452 824.914 1.125 15.353 1.898 0.58 328512. 0.1009 84.26 0.6201 0.5939 0.0083 0.0087 0.868 7.816 2.294 647.294 0.883 10.205 1.608 0.58 329273. 0.0697 87.38 0.6430 0.4304 0.0041 0.0062 0.619 5.570 1.143 461.306 0.629 5.083 1.124 0.58 330053. 0.0344 90.50 0.6660 -0.0207 -0.0001 0.0035 0.351 3.164 -0.030 262.053 0.357 -0.134 -0.052 0.58 330714. 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 0.0943 0.0297 4.431 34.912 33.968 3304.409 3.944 151.089 4.663 0.65 361841. 0.7778 3.57 0.0230 0.0708 0.0929 0.0302 4.500 35.451 33.453 3355.407 4.005 148.797 4.522 0.65 362073. 0.7486 7.14 0.0460 0.1373 0.0913 0.0306 4.563 35.953 32.892 3402.971 4.062 146.304 4.384 0.65 362325. 0.7197 10.71 0.0690 0.1996 0.0896 0.0310 4.621 36.409 32.284 3446.074 4.113 143.599 4.249 0.65 362596. 0.6911 14.28 0.0920 0.2578 0.0878 0.0313 4.672 36.806 31.626 3483.693 4.158 140.672 4.118 0.65 362889. 0.6628 17.85 0.1150 0.3123 0.0858 0.0316 4.713 37.134 30.915 3514.732 4.195 137.510 3.990 0.65 363203. 0.6349 21.43 0.1380 0.3630 0.0837 0.0318 4.745 37.380 30.148 3538.037 4.223 134.100 3.865 0.65 363539. 0.6074 25.00 0.1610 0.4103 0.0814 0.0319 4.764 37.532 29.323 3552.380 4.240 130.431 3.744 0.65 363897. 0.5803 28.57 0.1839 0.4542 0.0789 0.0320 4.769 37.576 28.438 3556.508 4.245 126.492 3.627 0.65 364279. 0.5536 32.14 0.2069 0.4950 0.0763 0.0319 4.760 37.498 27.490 3549.204 4.237 122.275 3.513 0.65 364685. 0.5272 35.71 0.2299 0.5327 0.0735 0.0317 4.733 37.289 26.480 3529.411 4.213 117.782 3.403 0.65 365115. 0.5012 39.28 0.2529 0.5676 0.0705 0.0314 4.689 36.940 25.409 3496.357 4.173 113.020 3.296 0.65 365569. 0.4756 42.85 0.2759 0.5998 0.0674 0.0310 4.626 36.446 24.282 3449.551 4.118 108.007 3.193 0.65 366047. 0.4503 46.42 0.2989 0.6293 0.0641 0.0305 4.544 35.802 23.103 3388.659 4.045 102.760 3.092 0.65 366551. 0.4254 49.99 0.3219 0.6563 0.0607 0.0298 4.443 35.007 21.875 3313.425 3.955 97.299 2.994 0.65 367080. 0.4009 53.56 0.3449 0.6807 0.0572 0.0290 4.323 34.058 20.603 3223.604 3.848 91.640 2.899 0.65 367634. 0.3766 57.13 0.3679 0.7026 0.0536 0.0280 4.183 32.953 19.289 3118.963 3.723 85.799 2.805 0.65 368214. 0.3526 60.70 0.3909 0.7219 0.0498 0.0270 4.022 31.688 17.938 2999.255 3.580 79.790 2.713 0.66 368820. 0.3289 64.28 0.4139 0.7386 0.0460 0.0257 3.841 30.262 16.553 2864.251 3.419 73.626 2.621 0.66 369452. 0.3052 67.85 0.4369 0.7524 0.0420 0.0244 3.639 28.671 15.135 2713.739 3.239 67.321 2.530 0.66 370110. 0.2817 71.42 0.4599 0.7630 0.0380 0.0229 3.416 26.916 13.689 2547.542 3.041 60.887 2.437 0.66 370795. 0.2581 74.99 0.4829 0.7700 0.0339 0.0213 3.172 24.993 12.216 2365.536 2.824 54.336 2.342 0.66 371506. 0.2343 78.56 0.5058 0.7725 0.0298 0.0195 2.907 22.902 10.720 2167.667 2.587 47.684 2.243 0.66 372245. 0.2102 82.13 0.5288 0.7693 0.0256 0.0176 2.620 20.645 9.205 1953.991 2.332 40.945 2.137 0.66 373010. 0.1856 85.70 0.5518 0.7583 0.0213 0.0155 2.313 18.222 7.674 1724.698 2.059 34.136 2.018 0.66 373802. 0.1600 89.27 0.5748 0.7355 0.0170 0.0133 1.985 15.638 6.133 1480.163 1.767 27.278 1.879 0.66 374622. 0.1332 92.84 0.5978 0.6933 0.0127 0.0110 1.637 12.900 4.585 1220.989 1.457 20.396 1.703 0.66 375468. 0.1044 96.41 0.6208 0.6146 0.0084 0.0085 1.271 10.016 3.039 948.039 1.132 13.518 1.454 0.66 376340. 0.0725 99.98 0.6438 0.4502 0.0042 0.0060 0.888 6.998 1.500 662.322 0.791 6.671 1.027 0.66 377234. 0.0360 103.56 0.6668 -0.0940 -0.0004 0.0030 0.453 3.569 -0.154 337.819 0.403 -0.686 -0.207 0.67 377187. 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 0.0962 0.0307 6.525 45.695 43.851 4865.658 5.163 195.050 4.088 0.73 407006. 0.7748 4.04 0.0231 0.0704 0.0948 0.0312 6.617 46.343 43.204 4934.651 5.236 192.173 3.971 0.73 407270. 0.7471 8.09 0.0463 0.1367 0.0932 0.0316 6.704 46.947 42.497 4998.952 5.304 189.027 3.856 0.73 407557. 0.7195 12.13 0.0694 0.1990 0.0915 0.0319 6.782 47.493 41.726 5057.123 5.366 185.599 3.742 0.73 407867. 0.6919 16.17 0.0926 0.2574 0.0897 0.0322 6.850 47.968 40.889 5107.696 5.419 181.873 3.631 0.73 408201. 0.6646 20.21 0.1157 0.3121 0.0877 0.0325 6.905 48.357 39.980 5149.062 5.463 177.832 3.522 0.73 408560. 0.6374 24.26 0.1388 0.3632 0.0855 0.0327 6.946 48.642 38.997 5179.477 5.496 173.459 3.415 0.73 408944. 0.6104 28.30 0.1620 0.4108 0.0832 0.0328 6.969 48.808 37.936 5197.089 5.514 168.739 3.311 0.73 409354. 0.5837 32.34 0.1851 0.4550 0.0807 0.0328 6.973 48.835 36.793 5199.955 5.517 163.656 3.209 0.73 409791. 0.5572 36.38 0.2083 0.4962 0.0780 0.0327 6.955 48.706 35.567 5186.206 5.503 158.203 3.111 0.73 410255. 0.5310 40.43 0.2314 0.5343 0.0751 0.0325 6.912 48.405 34.257 5154.164 5.469 152.377 3.015 0.73 410746. 0.5050 44.47 0.2545 0.5696 0.0721 0.0322 6.843 47.920 32.867 5102.586 5.414 146.193 2.922 0.73 411266. 0.4794 48.51 0.2777 0.6021 0.0689 0.0318 6.746 47.245 31.401 5030.655 5.338 139.673 2.831 0.73 411813. 0.4541 52.56 0.3008 0.6321 0.0655 0.0312 6.622 46.373 29.865 4937.793 5.239 132.841 2.743 0.74 412388. 0.4291 56.60 0.3239 0.6595 0.0620 0.0305 6.469 45.300 28.265 4823.577 5.118 125.724 2.658 0.74 412993. 0.4044 60.64 0.3471 0.6844 0.0584 0.0296 6.286 44.023 26.606 4687.630 4.974 118.344 2.574 0.74 413626. 0.3801 64.68 0.3702 0.7068 0.0546 0.0286 6.074 42.539 24.892 4529.612 4.806 110.721 2.493 0.74 414288. 0.3560 68.73 0.3934 0.7267 0.0507 0.0275 5.832 40.845 23.129 4349.201 4.615 102.876 2.412 0.74 414980. 0.3320 72.77 0.4165 0.7440 0.0468 0.0262 5.560 38.937 21.319 4146.061 4.399 94.826 2.332 0.74 415701. 0.3082 76.81 0.4396 0.7585 0.0427 0.0247 5.257 36.813 19.467 3919.888 4.159 86.587 2.252 0.74 416452. 0.2845 80.86 0.4628 0.7699 0.0386 0.0232 4.922 34.471 17.576 3670.455 3.894 78.177 2.172 0.74 417234. 0.2606 84.90 0.4859 0.7776 0.0343 0.0215 4.556 31.908 15.650 3397.635 3.605 69.612 2.089 0.74 418045. 0.2366 88.94 0.5091 0.7809 0.0300 0.0196 4.159 29.127 13.694 3101.440 3.291 60.911 2.003 0.74 418887. 0.2121 92.98 0.5322 0.7784 0.0257 0.0176 3.731 26.127 11.712 2782.065 2.952 52.095 1.909 0.74 419759. 0.1870 97.03 0.5553 0.7677 0.0213 0.0154 3.272 22.915 9.709 2439.974 2.589 43.186 1.805 0.74 420662. 0.1610 101.07 0.5785 0.7446 0.0169 0.0131 2.784 19.496 7.692 2075.992 2.203 34.212 1.680 0.74 421595. 0.1334 105.11 0.6016 0.7003 0.0124 0.0107 2.268 15.885 5.667 1691.402 1.795 25.206 1.520 0.75 422559. 0.1035 109.15 0.6248 0.6139 0.0080 0.0081 1.727 12.096 3.643 1287.997 1.367 16.205 1.283 0.75 423552. 0.0701 113.20 0.6479 0.4225 0.0036 0.0055 1.164 8.150 1.629 867.774 0.921 7.245 0.851 0.75 424567. 0.0311 117.24 0.6710 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 0.0984 0.0340 9.901 62.403 55.397 7383.069 7.050 246.408 3.403 0.81 452135. 0.7250 4.48 0.0231 0.0654 0.0971 0.0343 9.984 62.929 54.626 7445.230 7.110 242.977 3.328 0.81 452430. 0.7040 8.96 0.0462 0.1278 0.0955 0.0345 10.057 63.387 53.776 7499.400 7.161 239.197 3.252 0.81 452750. 0.6827 13.45 0.0693 0.1873 0.0939 0.0347 10.117 63.764 52.844 7544.062 7.204 235.050 3.177 0.81 453096. 0.6611 17.93 0.0924 0.2438 0.0921 0.0349 10.162 64.049 51.825 7577.727 7.236 230.516 3.102 0.81 453469. 0.6392 22.41 0.1154 0.2974 0.0901 0.0350 10.190 64.226 50.713 7598.668 7.256 225.572 3.027 0.81 453870. 0.6170 26.89 0.1385 0.3481 0.0880 0.0350 10.198 64.279 49.505 7605.008 7.262 220.198 2.953 0.81 454300. 0.5946 31.37 0.1616 0.3959 0.0856 0.0350 10.185 64.192 48.195 7594.647 7.252 214.372 2.878 0.81 454758. 0.5719 35.86 0.1847 0.4409 0.0831 0.0348 10.145 63.944 46.780 7565.280 7.224 208.076 2.805 0.81 455247. 0.5491 40.34 0.2078 0.4831 0.0804 0.0346 10.077 63.515 45.255 7514.627 7.176 201.296 2.732 0.81 455765. 0.5260 44.82 0.2309 0.5225 0.0775 0.0342 9.978 62.890 43.622 7440.630 7.105 194.030 2.659 0.82 456314. 0.5027 49.30 0.2540 0.5593 0.0744 0.0338 9.845 62.055 41.883 7341.786 7.011 186.294 2.587 0.82 456893. 0.4793 53.79 0.2771 0.5934 0.0711 0.0332 9.678 61.001 40.044 7217.101 6.892 178.115 2.517 0.82 457504. 0.4558 58.27 0.3001 0.6250 0.0677 0.0325 9.476 59.723 38.113 7065.891 6.747 169.528 2.447 0.82 458146. 0.4323 62.75 0.3232 0.6540 0.0641 0.0317 9.236 58.215 36.098 6887.532 6.577 160.566 2.377 0.82 458820. 0.4088 67.23 0.3463 0.6804 0.0604 0.0308 8.960 56.473 34.006 6681.378 6.380 151.259 2.309 0.82 459525. 0.3853 71.71 0.3694 0.7043 0.0566 0.0297 8.645 54.489 31.842 6446.713 6.156 141.635 2.240 0.82 460263. 0.3618 76.20 0.3925 0.7257 0.0526 0.0285 8.291 52.259 29.613 6182.830 5.904 131.720 2.172 0.82 461032. 0.3384 80.68 0.4156 0.7442 0.0485 0.0271 7.899 49.784 27.324 5890.026 5.625 121.537 2.104 0.82 461835. 0.3148 85.16 0.4387 0.7597 0.0444 0.0256 7.466 47.058 24.979 5567.476 5.317 111.106 2.035 0.82 462670. 0.2911 89.64 0.4618 0.7719 0.0401 0.0240 6.993 44.076 22.583 5214.665 4.980 100.448 1.964 0.82 463538. 0.2672 94.12 0.4849 0.7801 0.0358 0.0222 6.480 40.842 20.140 4832.100 4.614 89.584 1.890 0.82 464439. 0.2428 98.61 0.5079 0.7834 0.0314 0.0203 5.926 37.352 17.657 4419.238 4.220 78.539 1.812 0.82 465373. 0.2180 103.09 0.5310 0.7802 0.0269 0.0183 5.334 33.618 15.138 3977.347 3.798 67.336 1.726 0.82 466341. 0.1923 107.57 0.5541 0.7677 0.0224 0.0161 4.705 29.652 12.591 3508.197 3.350 56.004 1.628 0.83 467342. 0.1653 112.05 0.5772 0.7408 0.0178 0.0139 4.042 25.476 10.022 3014.102 2.878 44.577 1.508 0.83 468377. 0.1367 116.54 0.6003 0.6901 0.0132 0.0115 3.350 21.115 7.440 2498.187 2.386 33.094 1.351 0.83 469445. 0.1055 121.02 0.6234 0.5950 0.0086 0.0090 2.634 16.603 4.857 1964.346 1.876 21.603 1.121 0.83 470545. 0.0707 125.50 0.6465 0.4019 0.0041 0.0065 1.900 11.975 2.282 1416.821 1.353 10.150 0.730 0.83 471671. 0.0316 129.98 0.6696 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 0.1003 0.0414 16.071 92.083 68.281 11983.891 10.403 303.714 2.584 0.89 497254. 0.6112 4.93 0.0231 0.0550 0.0990 0.0416 16.125 92.395 67.443 12024.598 10.439 299.988 2.544 0.89 497574. 0.5980 9.85 0.0461 0.1082 0.0977 0.0417 16.153 92.554 66.506 12045.272 10.457 295.820 2.504 0.89 497924. 0.5846 14.78 0.0692 0.1598 0.0961 0.0416 16.150 92.540 65.463 12043.428 10.455 291.177 2.465 0.89 498303. 0.5709 19.71 0.0923 0.2097 0.0944 0.0416 16.115 92.337 64.305 12017.026 10.432 286.027 2.427 0.89 498713. 0.5571 24.64 0.1154 0.2581 0.0925 0.0414 16.044 91.932 63.025 11964.342 10.386 280.337 2.389 0.90 499154. 0.5429 29.56 0.1384 0.3048 0.0905 0.0411 15.936 91.313 61.618 11883.766 10.317 274.076 2.352 0.90 499628. 0.5284 34.49 0.1615 0.3500 0.0882 0.0407 15.789 90.468 60.076 11773.790 10.221 267.217 2.314 0.90 500135. 0.5134 39.42 0.1846 0.3935 0.0857 0.0402 15.600 89.386 58.394 11632.984 10.099 259.734 2.277 0.90 500675. 0.4980 44.35 0.2077 0.4353 0.0831 0.0396 15.368 88.058 56.567 11460.112 9.949 251.611 2.239 0.90 501250. 0.4820 49.27 0.2307 0.4753 0.0802 0.0389 15.092 86.476 54.596 11254.250 9.770 242.843 2.200 0.90 501858. 0.4654 54.20 0.2538 0.5135 0.0771 0.0381 14.771 84.638 52.484 11015.063 9.562 233.451 2.161 0.90 502500. 0.4481 59.13 0.2769 0.5499 0.0738 0.0372 14.406 82.546 50.241 10742.798 9.326 223.470 2.121 0.90 503177. 0.4303 64.06 0.3000 0.5842 0.0703 0.0361 13.998 80.204 47.874 10437.970 9.061 212.946 2.080 0.90 503889. 0.4120 68.98 0.3230 0.6165 0.0667 0.0349 13.546 77.614 45.396 10100.916 8.769 201.921 2.038 0.90 504635. 0.3931 73.91 0.3461 0.6466 0.0629 0.0337 13.050 74.776 42.814 9731.601 8.448 190.438 1.995 0.90 505416. 0.3737 78.84 0.3692 0.6744 0.0589 0.0323 12.511 71.686 40.137 9329.443 8.099 178.531 1.951 0.90 506232. 0.3539 83.77 0.3923 0.6999 0.0549 0.0308 11.927 68.340 37.373 8893.906 7.721 166.233 1.906 0.90 507083. 0.3335 88.69 0.4153 0.7228 0.0507 0.0291 11.297 64.732 34.528 8424.447 7.313 153.579 1.859 0.90 507970. 0.3127 93.62 0.4384 0.7422 0.0464 0.0274 10.632 60.921 31.608 7928.478 6.883 140.594 1.808 0.90 508893. 0.2910 98.55 0.4615 0.7570 0.0420 0.0256 9.935 56.925 28.621 7408.375 6.431 127.307 1.752 0.90 509852. 0.2683 103.48 0.4846 0.7654 0.0375 0.0238 9.219 52.821 25.571 6874.298 5.968 113.739 1.687 0.91 510846. 0.2442 108.40 0.5076 0.7622 0.0330 0.0220 8.518 48.806 22.460 6351.758 5.514 99.902 1.604 0.91 511877. 0.2176 113.33 0.5307 0.7496 0.0283 0.0201 7.782 44.590 19.302 5803.024 5.038 85.857 1.509 0.91 512944. 0.1897 118.26 0.5538 0.7238 0.0236 0.0181 7.017 40.208 16.106 5232.791 4.543 71.640 1.396 0.91 514047. 0.1604 123.18 0.5769 0.6790 0.0189 0.0161 6.231 35.706 12.882 4646.822 4.034 57.298 1.257 0.91 515186. 0.1292 128.11 0.5999 0.6064 0.0142 0.0140 5.432 31.124 9.642 4050.591 3.516 42.888 1.080 0.91 516362. 0.0960 133.04 0.6230 0.4909 0.0094 0.0119 4.628 26.516 6.403 3450.812 2.996 28.481 0.842 0.91 517573. 0.0610 137.97 0.6461 0.3058 0.0047 0.0099 3.827 21.928 3.181 2853.725 2.477 14.149 0.506 0.91 518816. 0.0258 142.89 0.6692 -0.0092 -0.0001 0.0077 2.997 17.175 -0.072 2235.161 1.940 -0.322 -0.015 0.91 519962. 0.0000