17x8E (17x8E.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 0.0808 0.0307 0.003 0.218 0.213 2.579 0.025 0.946 37.402 0.07 26796. 0.5971 0.34 0.0211 0.0543 0.0794 0.0309 0.003 0.220 0.209 2.597 0.025 0.929 36.488 0.07 26811. 0.5773 0.68 0.0423 0.1058 0.0779 0.0311 0.004 0.221 0.205 2.613 0.025 0.912 35.573 0.07 26827. 0.5575 1.02 0.0634 0.1547 0.0763 0.0313 0.004 0.222 0.201 2.626 0.025 0.893 34.659 0.07 26844. 0.5375 1.36 0.0846 0.2008 0.0746 0.0314 0.004 0.223 0.196 2.636 0.025 0.873 33.747 0.07 26863. 0.5174 1.70 0.1057 0.2442 0.0727 0.0315 0.004 0.223 0.191 2.643 0.025 0.851 32.838 0.07 26883. 0.4972 2.04 0.1268 0.2850 0.0708 0.0315 0.004 0.224 0.186 2.646 0.025 0.828 31.931 0.07 26904. 0.4770 2.38 0.1480 0.3231 0.0687 0.0315 0.004 0.223 0.181 2.644 0.025 0.804 31.027 0.07 26926. 0.4567 2.71 0.1691 0.3585 0.0666 0.0314 0.004 0.223 0.175 2.637 0.025 0.779 30.125 0.07 26950. 0.4364 3.05 0.1902 0.3912 0.0643 0.0313 0.004 0.222 0.169 2.625 0.025 0.752 29.223 0.07 26975. 0.4160 3.39 0.2114 0.4213 0.0619 0.0310 0.003 0.220 0.163 2.607 0.025 0.724 28.321 0.07 27002. 0.3955 3.73 0.2325 0.4486 0.0593 0.0308 0.003 0.218 0.156 2.583 0.025 0.694 27.415 0.07 27030. 0.3749 4.07 0.2537 0.4730 0.0567 0.0304 0.003 0.216 0.149 2.552 0.024 0.663 26.502 0.07 27060. 0.3542 4.41 0.2748 0.4946 0.0539 0.0299 0.003 0.212 0.142 2.514 0.024 0.631 25.579 0.07 27091. 0.3334 4.75 0.2959 0.5131 0.0510 0.0294 0.003 0.209 0.134 2.469 0.024 0.597 24.641 0.07 27124. 0.3124 5.09 0.3171 0.5284 0.0480 0.0288 0.003 0.204 0.126 2.417 0.023 0.561 23.684 0.07 27158. 0.2913 5.43 0.3382 0.5403 0.0449 0.0281 0.003 0.199 0.118 2.358 0.023 0.525 22.702 0.07 27194. 0.2700 5.77 0.3593 0.5484 0.0417 0.0273 0.003 0.194 0.110 2.293 0.022 0.488 21.686 0.07 27232. 0.2485 6.11 0.3805 0.5523 0.0384 0.0264 0.003 0.188 0.101 2.221 0.021 0.449 20.628 0.07 27271. 0.2269 6.45 0.4016 0.5516 0.0350 0.0255 0.003 0.181 0.092 2.142 0.020 0.410 19.519 0.07 27312. 0.2051 6.79 0.4228 0.5457 0.0316 0.0245 0.003 0.174 0.083 2.056 0.020 0.370 18.345 0.07 27354. 0.1831 7.13 0.4439 0.5339 0.0281 0.0234 0.003 0.166 0.074 1.965 0.019 0.329 17.091 0.07 27398. 0.1610 7.46 0.4650 0.5150 0.0246 0.0222 0.003 0.158 0.065 1.867 0.018 0.288 15.738 0.07 27444. 0.1387 7.80 0.4862 0.4879 0.0211 0.0210 0.002 0.149 0.055 1.763 0.017 0.247 14.260 0.07 27492. 0.1162 8.14 0.5073 0.4507 0.0175 0.0197 0.002 0.140 0.046 1.653 0.016 0.205 12.624 0.07 27541. 0.0938 8.48 0.5285 0.4012 0.0139 0.0183 0.002 0.130 0.037 1.539 0.015 0.163 10.788 0.07 27592. 0.0714 8.82 0.5496 0.3362 0.0103 0.0169 0.002 0.120 0.027 1.419 0.014 0.121 8.692 0.07 27644. 0.0496 9.16 0.5707 0.2511 0.0068 0.0154 0.002 0.109 0.018 1.294 0.012 0.079 6.253 0.07 27699. 0.0289 9.50 0.5919 0.1396 0.0033 0.0139 0.002 0.099 0.009 1.166 0.011 0.038 3.351 0.07 27755. 0.0108 9.84 0.6130 -0.0088 -0.0002 0.0123 0.001 0.087 0.000 1.035 0.010 -0.002 -0.204 0.07 27812. 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 0.0811 0.0280 0.025 0.796 0.854 18.838 0.090 3.798 20.558 0.13 53592. 0.6576 0.68 0.0212 0.0598 0.0797 0.0283 0.025 0.803 0.839 19.004 0.091 3.731 20.021 0.13 53622. 0.6348 1.36 0.0424 0.1163 0.0782 0.0285 0.026 0.809 0.823 19.153 0.091 3.660 19.487 0.13 53654. 0.6119 2.04 0.0636 0.1697 0.0766 0.0287 0.026 0.815 0.806 19.280 0.092 3.584 18.958 0.13 53689. 0.5891 2.72 0.0848 0.2201 0.0749 0.0289 0.026 0.819 0.788 19.382 0.093 3.504 18.433 0.13 53726. 0.5663 3.40 0.1060 0.2673 0.0730 0.0290 0.026 0.822 0.768 19.454 0.093 3.418 17.915 0.13 53765. 0.5436 4.08 0.1272 0.3116 0.0711 0.0290 0.026 0.824 0.748 19.493 0.093 3.327 17.402 0.13 53808. 0.5210 4.77 0.1484 0.3530 0.0690 0.0290 0.026 0.824 0.726 19.496 0.093 3.230 16.895 0.13 53853. 0.4984 5.45 0.1696 0.3914 0.0668 0.0290 0.026 0.822 0.703 19.457 0.093 3.128 16.393 0.13 53901. 0.4759 6.13 0.1909 0.4270 0.0645 0.0288 0.026 0.819 0.679 19.374 0.093 3.020 15.897 0.13 53951. 0.4535 6.81 0.2121 0.4598 0.0621 0.0286 0.026 0.813 0.654 19.242 0.092 2.907 15.405 0.13 54005. 0.4311 7.49 0.2333 0.4897 0.0596 0.0284 0.026 0.805 0.627 19.058 0.091 2.788 14.916 0.13 54062. 0.4088 8.17 0.2545 0.5167 0.0569 0.0280 0.025 0.795 0.599 18.818 0.090 2.663 14.428 0.13 54121. 0.3864 8.85 0.2757 0.5409 0.0541 0.0276 0.025 0.783 0.569 18.518 0.088 2.532 13.941 0.13 54184. 0.3641 9.53 0.2969 0.5620 0.0512 0.0270 0.024 0.767 0.538 18.157 0.087 2.395 13.451 0.14 54250. 0.3417 10.21 0.3181 0.5800 0.0481 0.0264 0.024 0.750 0.507 17.736 0.085 2.253 12.956 0.14 54319. 0.3192 10.89 0.3393 0.5947 0.0450 0.0257 0.023 0.729 0.474 17.256 0.082 2.107 12.453 0.14 54392. 0.2967 11.57 0.3605 0.6057 0.0418 0.0249 0.022 0.706 0.440 16.715 0.080 1.957 11.939 0.14 54467. 0.2741 12.25 0.3817 0.6128 0.0385 0.0240 0.022 0.681 0.405 16.116 0.077 1.803 11.407 0.14 54546. 0.2514 12.93 0.4029 0.6155 0.0352 0.0230 0.021 0.653 0.370 15.459 0.074 1.645 10.854 0.14 54628. 0.2285 13.62 0.4241 0.6131 0.0317 0.0219 0.020 0.623 0.334 14.743 0.070 1.485 10.271 0.14 54714. 0.2054 14.30 0.4453 0.6048 0.0282 0.0208 0.019 0.590 0.297 13.971 0.067 1.322 9.649 0.14 54802. 0.1821 14.98 0.4665 0.5894 0.0247 0.0196 0.018 0.555 0.260 13.144 0.063 1.157 8.978 0.14 54895. 0.1585 15.66 0.4877 0.5656 0.0212 0.0183 0.016 0.518 0.223 12.262 0.059 0.991 8.239 0.14 54990. 0.1346 16.34 0.5089 0.5309 0.0176 0.0169 0.015 0.479 0.185 11.330 0.054 0.824 7.412 0.14 55089. 0.1104 17.02 0.5301 0.4823 0.0140 0.0154 0.014 0.437 0.147 10.350 0.049 0.656 6.464 0.14 55192. 0.0859 17.70 0.5513 0.4150 0.0105 0.0139 0.013 0.394 0.110 9.325 0.045 0.489 5.349 0.14 55298. 0.0614 18.38 0.5726 0.3218 0.0069 0.0123 0.011 0.349 0.073 8.261 0.039 0.324 3.994 0.14 55407. 0.0373 19.06 0.5938 0.1906 0.0034 0.0107 0.010 0.303 0.036 7.163 0.034 0.160 2.281 0.14 55520. 0.0150 19.74 0.6150 -0.0008 0.0000 0.0090 0.008 0.255 0.000 6.033 0.029 -0.001 -0.009 0.14 55634. 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 0.0814 0.0269 0.082 1.720 1.928 61.056 0.194 8.577 14.325 0.20 80386. 0.6886 1.02 0.0212 0.0625 0.0800 0.0272 0.083 1.737 1.895 61.651 0.196 8.427 13.939 0.20 80431. 0.6642 2.05 0.0425 0.1216 0.0785 0.0274 0.083 1.752 1.859 62.185 0.198 8.267 13.557 0.20 80480. 0.6398 3.07 0.0637 0.1773 0.0769 0.0276 0.084 1.765 1.820 62.645 0.199 8.096 13.179 0.20 80532. 0.6155 4.09 0.0850 0.2297 0.0751 0.0278 0.085 1.776 1.779 63.019 0.201 7.914 12.806 0.20 80588. 0.5913 5.11 0.1062 0.2789 0.0733 0.0279 0.085 1.783 1.736 63.292 0.201 7.720 12.438 0.20 80648. 0.5673 6.14 0.1274 0.3249 0.0714 0.0280 0.085 1.788 1.689 63.452 0.202 7.514 12.076 0.20 80711. 0.5434 7.16 0.1487 0.3679 0.0693 0.0280 0.085 1.789 1.640 63.484 0.202 7.296 11.720 0.20 80779. 0.5196 8.18 0.1699 0.4078 0.0671 0.0280 0.085 1.786 1.589 63.375 0.202 7.066 11.369 0.20 80851. 0.4960 9.21 0.1912 0.4448 0.0648 0.0278 0.085 1.778 1.534 63.112 0.201 6.822 11.023 0.20 80927. 0.4726 10.23 0.2124 0.4790 0.0623 0.0276 0.084 1.766 1.476 62.682 0.200 6.566 10.682 0.20 81008. 0.4493 11.25 0.2336 0.5102 0.0598 0.0274 0.083 1.749 1.416 62.070 0.198 6.297 10.345 0.20 81093. 0.4261 12.27 0.2549 0.5386 0.0571 0.0270 0.082 1.726 1.352 61.263 0.195 6.014 10.010 0.20 81183. 0.4029 13.30 0.2761 0.5641 0.0543 0.0266 0.081 1.697 1.285 60.247 0.192 5.718 9.678 0.20 81278. 0.3798 14.32 0.2974 0.5867 0.0514 0.0260 0.079 1.663 1.216 59.021 0.188 5.409 9.346 0.20 81377. 0.3568 15.34 0.3186 0.6061 0.0483 0.0254 0.077 1.622 1.144 57.583 0.183 5.089 9.012 0.20 81481. 0.3337 16.36 0.3398 0.6224 0.0452 0.0247 0.075 1.576 1.070 55.935 0.178 4.759 8.675 0.20 81590. 0.3106 17.39 0.3611 0.6352 0.0420 0.0239 0.073 1.524 0.993 54.078 0.172 4.419 8.333 0.20 81704. 0.2875 18.41 0.3823 0.6441 0.0387 0.0229 0.070 1.465 0.915 52.013 0.166 4.071 7.981 0.20 81822. 0.2643 19.43 0.4036 0.6488 0.0353 0.0219 0.067 1.401 0.835 49.741 0.158 3.715 7.616 0.20 81946. 0.2409 20.46 0.4248 0.6486 0.0318 0.0208 0.063 1.332 0.754 47.264 0.150 3.352 7.233 0.20 82075. 0.2174 21.48 0.4460 0.6427 0.0283 0.0197 0.060 1.256 0.671 44.587 0.142 2.985 6.826 0.20 82208. 0.1936 22.50 0.4673 0.6300 0.0248 0.0184 0.056 1.175 0.587 41.712 0.133 2.612 6.386 0.20 82347. 0.1694 23.52 0.4885 0.6086 0.0212 0.0170 0.052 1.089 0.503 38.648 0.123 2.237 5.902 0.20 82491. 0.1449 24.55 0.5098 0.5764 0.0177 0.0156 0.047 0.997 0.418 35.402 0.113 1.859 5.356 0.20 82640. 0.1199 25.57 0.5310 0.5296 0.0141 0.0141 0.043 0.901 0.333 31.984 0.102 1.482 4.724 0.20 82794. 0.0944 26.59 0.5522 0.4626 0.0105 0.0125 0.038 0.800 0.249 28.410 0.090 1.106 3.968 0.20 82953. 0.0685 27.62 0.5735 0.3662 0.0070 0.0109 0.033 0.696 0.165 24.697 0.079 0.733 3.025 0.21 83118. 0.0425 28.64 0.5947 0.2239 0.0035 0.0092 0.028 0.588 0.082 20.864 0.066 0.365 1.784 0.21 83287. 0.0177 29.66 0.6160 0.0024 0.0000 0.0075 0.023 0.477 0.001 16.917 0.054 0.003 0.018 0.21 83458. 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 0.0818 0.0264 0.190 2.992 3.444 141.611 0.338 15.319 11.031 0.27 107179. 0.7087 1.37 0.0213 0.0642 0.0804 0.0266 0.192 3.023 3.384 143.069 0.342 15.052 10.728 0.27 107239. 0.6832 2.73 0.0425 0.1249 0.0789 0.0269 0.194 3.051 3.320 144.382 0.345 14.766 10.429 0.27 107304. 0.6578 4.10 0.0638 0.1820 0.0772 0.0271 0.195 3.075 3.251 145.519 0.347 14.461 10.134 0.27 107374. 0.6325 5.46 0.0851 0.2357 0.0755 0.0273 0.196 3.095 3.178 146.447 0.350 14.136 9.843 0.27 107449. 0.6075 6.83 0.1064 0.2861 0.0737 0.0274 0.197 3.109 3.100 147.134 0.351 13.791 9.558 0.27 107529. 0.5826 8.19 0.1276 0.3333 0.0717 0.0275 0.198 3.118 3.018 147.547 0.352 13.423 9.277 0.27 107614. 0.5579 9.56 0.1489 0.3772 0.0696 0.0275 0.198 3.120 2.930 147.652 0.352 13.034 9.001 0.27 107705. 0.5334 10.93 0.1702 0.4182 0.0674 0.0274 0.198 3.115 2.838 147.417 0.352 12.622 8.731 0.27 107801. 0.5091 12.29 0.1914 0.4561 0.0651 0.0273 0.197 3.102 2.740 146.809 0.350 12.187 8.465 0.27 107903. 0.4850 13.66 0.2127 0.4911 0.0626 0.0271 0.196 3.081 2.637 145.796 0.348 11.729 8.203 0.27 108011. 0.4611 15.02 0.2340 0.5233 0.0601 0.0269 0.194 3.050 2.529 144.344 0.345 11.247 7.945 0.27 108125. 0.4374 16.39 0.2552 0.5525 0.0574 0.0265 0.191 3.009 2.415 142.419 0.340 10.741 7.691 0.27 108245. 0.4137 17.75 0.2765 0.5789 0.0545 0.0261 0.188 2.958 2.296 139.989 0.334 10.211 7.438 0.27 108372. 0.3901 19.12 0.2978 0.6024 0.0516 0.0255 0.184 2.896 2.172 137.046 0.327 9.659 7.187 0.27 108505. 0.3666 20.49 0.3191 0.6229 0.0485 0.0249 0.179 2.823 2.043 133.589 0.319 9.087 6.936 0.27 108644. 0.3432 21.85 0.3403 0.6403 0.0454 0.0241 0.174 2.739 1.910 129.621 0.309 8.496 6.684 0.27 108789. 0.3198 23.22 0.3616 0.6542 0.0421 0.0233 0.168 2.644 1.773 125.141 0.299 7.888 6.428 0.27 108942. 0.2963 24.58 0.3829 0.6645 0.0388 0.0224 0.161 2.539 1.633 120.153 0.287 7.265 6.166 0.27 109100. 0.2728 25.95 0.4041 0.6706 0.0354 0.0213 0.154 2.423 1.490 114.659 0.274 6.629 5.895 0.27 109266. 0.2491 27.31 0.4254 0.6720 0.0319 0.0202 0.146 2.296 1.345 108.665 0.259 5.981 5.612 0.27 109438. 0.2253 28.68 0.4467 0.6679 0.0284 0.0190 0.137 2.159 1.197 102.178 0.244 5.323 5.312 0.27 109616. 0.2012 30.05 0.4680 0.6570 0.0249 0.0177 0.128 2.012 1.047 95.209 0.227 4.657 4.988 0.27 109802. 0.1767 31.41 0.4892 0.6377 0.0213 0.0163 0.118 1.855 0.896 87.774 0.210 3.986 4.631 0.27 109994. 0.1517 32.78 0.5105 0.6074 0.0177 0.0149 0.107 1.688 0.745 79.895 0.191 3.312 4.227 0.27 110193. 0.1263 34.14 0.5318 0.5622 0.0141 0.0133 0.096 1.513 0.593 71.597 0.171 2.637 3.756 0.27 110399. 0.1001 35.51 0.5530 0.4958 0.0105 0.0117 0.084 1.329 0.442 62.916 0.150 1.965 3.185 0.27 110612. 0.0733 36.87 0.5743 0.3974 0.0069 0.0100 0.072 1.139 0.292 53.894 0.129 1.299 2.458 0.27 110832. 0.0460 38.24 0.5956 0.2466 0.0034 0.0083 0.060 0.942 0.145 44.582 0.106 0.643 1.471 0.27 111059. 0.0194 39.61 0.6168 -0.0016 0.0000 0.0065 0.047 0.739 -0.001 34.982 0.084 -0.003 -0.009 0.27 111286. 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 0.0823 0.0260 0.367 4.622 5.412 273.395 0.522 24.074 8.979 0.34 133969. 0.7231 1.71 0.0213 0.0654 0.0809 0.0263 0.371 4.671 5.318 276.312 0.528 23.656 8.730 0.34 134045. 0.6969 3.42 0.0426 0.1271 0.0793 0.0266 0.374 4.715 5.218 278.943 0.533 23.208 8.484 0.34 134126. 0.6708 5.12 0.0639 0.1852 0.0777 0.0268 0.377 4.754 5.110 281.224 0.537 22.730 8.242 0.34 134214. 0.6449 6.83 0.0851 0.2398 0.0760 0.0270 0.380 4.786 4.996 283.092 0.541 22.220 8.004 0.34 134308. 0.6193 8.54 0.1064 0.2910 0.0741 0.0271 0.381 4.809 4.874 284.483 0.543 21.678 7.770 0.34 134408. 0.5938 10.25 0.1277 0.3389 0.0721 0.0272 0.383 4.823 4.744 285.329 0.545 21.101 7.541 0.34 134515. 0.5686 11.96 0.1490 0.3836 0.0700 0.0272 0.383 4.827 4.606 285.566 0.545 20.489 7.317 0.34 134628. 0.5436 13.67 0.1703 0.4252 0.0678 0.0272 0.382 4.820 4.461 285.126 0.545 19.842 7.096 0.34 134749. 0.5188 15.37 0.1916 0.4638 0.0655 0.0271 0.381 4.800 4.307 283.944 0.542 19.159 6.881 0.34 134877. 0.4943 17.08 0.2128 0.4994 0.0630 0.0269 0.378 4.766 4.146 281.958 0.539 18.439 6.669 0.34 135013. 0.4700 18.79 0.2341 0.5322 0.0604 0.0266 0.374 4.718 3.975 279.101 0.533 17.682 6.460 0.34 135156. 0.4459 20.50 0.2554 0.5621 0.0577 0.0262 0.369 4.654 3.797 275.301 0.526 16.887 6.255 0.34 135306. 0.4219 22.21 0.2767 0.5892 0.0549 0.0258 0.363 4.573 3.609 270.497 0.517 16.054 6.052 0.34 135465. 0.3980 23.92 0.2980 0.6134 0.0519 0.0252 0.355 4.474 3.414 264.671 0.505 15.186 5.851 0.34 135631. 0.3742 25.62 0.3193 0.6347 0.0488 0.0246 0.346 4.358 3.212 257.820 0.492 14.285 5.650 0.34 135805. 0.3505 27.33 0.3406 0.6529 0.0457 0.0238 0.335 4.225 3.003 249.947 0.477 13.356 5.449 0.34 135988. 0.3268 29.04 0.3618 0.6678 0.0424 0.0230 0.323 4.075 2.788 241.053 0.460 12.399 5.245 0.34 136178. 0.3032 30.75 0.3831 0.6791 0.0390 0.0220 0.310 3.907 2.567 231.142 0.441 11.419 5.038 0.34 136377. 0.2794 32.46 0.4044 0.6864 0.0356 0.0210 0.295 3.723 2.342 220.219 0.421 10.418 4.824 0.34 136584. 0.2556 34.17 0.4257 0.6891 0.0321 0.0198 0.279 3.521 2.113 208.295 0.398 9.398 4.601 0.34 136799. 0.2315 35.87 0.4470 0.6865 0.0286 0.0186 0.262 3.303 1.880 195.384 0.373 8.363 4.365 0.34 137023. 0.2072 37.58 0.4683 0.6772 0.0250 0.0173 0.243 3.068 1.645 181.509 0.347 7.316 4.110 0.34 137255. 0.1825 39.29 0.4896 0.6596 0.0214 0.0159 0.224 2.818 1.407 166.701 0.318 6.261 3.830 0.34 137496. 0.1573 41.00 0.5108 0.6312 0.0178 0.0144 0.202 2.553 1.169 151.001 0.288 5.200 3.512 0.34 137746. 0.1314 42.71 0.5321 0.5877 0.0141 0.0128 0.180 2.273 0.931 134.465 0.257 4.139 3.139 0.34 138004. 0.1048 44.42 0.5534 0.5223 0.0105 0.0112 0.157 1.981 0.693 117.163 0.224 3.082 2.683 0.34 138270. 0.0773 46.12 0.5747 0.4232 0.0070 0.0094 0.133 1.677 0.458 99.181 0.189 2.035 2.093 0.34 138545. 0.0490 47.83 0.5960 0.2663 0.0034 0.0077 0.108 1.363 0.226 80.620 0.154 1.004 1.270 0.34 138829. 0.0209 49.54 0.6173 -0.0045 0.0000 0.0059 0.082 1.039 -0.003 61.466 0.117 -0.012 -0.021 0.34 139112. 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 0.0829 0.0259 0.631 6.623 7.848 470.181 0.748 34.909 7.571 0.40 160756. 0.7342 2.05 0.0213 0.0662 0.0814 0.0262 0.637 6.696 7.713 475.320 0.756 34.306 7.360 0.40 160847. 0.7075 4.10 0.0426 0.1286 0.0799 0.0265 0.644 6.761 7.567 479.958 0.764 33.659 7.151 0.40 160946. 0.6810 6.15 0.0639 0.1873 0.0783 0.0267 0.649 6.818 7.412 483.981 0.770 32.969 6.946 0.40 161051. 0.6546 8.20 0.0852 0.2425 0.0765 0.0269 0.653 6.864 7.246 487.280 0.776 32.232 6.745 0.40 161164. 0.6285 10.25 0.1064 0.2943 0.0747 0.0270 0.657 6.899 7.070 489.739 0.779 31.447 6.548 0.40 161284. 0.6027 12.30 0.1277 0.3427 0.0727 0.0271 0.659 6.920 6.882 491.242 0.782 30.613 6.355 0.40 161413. 0.5771 14.35 0.1490 0.3879 0.0706 0.0271 0.659 6.926 6.683 491.674 0.783 29.728 6.165 0.40 161550. 0.5518 16.40 0.1703 0.4300 0.0683 0.0271 0.658 6.916 6.473 490.917 0.781 28.791 5.980 0.40 161695. 0.5267 18.45 0.1916 0.4691 0.0660 0.0270 0.656 6.887 6.250 488.858 0.778 27.801 5.799 0.40 161849. 0.5019 20.50 0.2129 0.5053 0.0635 0.0268 0.651 6.838 6.016 485.383 0.773 26.758 5.621 0.40 162012. 0.4773 22.55 0.2342 0.5386 0.0609 0.0265 0.644 6.767 5.769 480.378 0.765 25.660 5.447 0.40 162184. 0.4529 24.60 0.2555 0.5690 0.0582 0.0261 0.635 6.673 5.510 473.716 0.754 24.507 5.275 0.40 162365. 0.4287 26.65 0.2768 0.5967 0.0553 0.0257 0.624 6.555 5.238 465.291 0.741 23.299 5.106 0.40 162556. 0.4045 28.71 0.2981 0.6215 0.0523 0.0251 0.610 6.411 4.955 455.065 0.724 22.040 4.939 0.41 162756. 0.3806 30.76 0.3193 0.6434 0.0492 0.0244 0.594 6.241 4.661 443.035 0.705 20.733 4.772 0.41 162965. 0.3567 32.81 0.3406 0.6623 0.0460 0.0237 0.576 6.046 4.358 429.202 0.683 19.384 4.605 0.41 163185. 0.3328 34.86 0.3619 0.6780 0.0427 0.0228 0.555 5.826 4.046 413.570 0.658 17.996 4.437 0.41 163414. 0.3090 36.91 0.3832 0.6903 0.0393 0.0218 0.531 5.580 3.726 396.143 0.630 16.573 4.266 0.41 163652. 0.2851 38.96 0.4045 0.6986 0.0359 0.0208 0.505 5.310 3.399 376.931 0.600 15.120 4.090 0.41 163901. 0.2611 41.01 0.4258 0.7025 0.0324 0.0196 0.477 5.014 3.066 355.952 0.567 13.640 3.907 0.41 164160. 0.2369 43.06 0.4471 0.7011 0.0288 0.0184 0.447 4.694 2.729 333.232 0.530 12.137 3.714 0.41 164429. 0.2124 45.11 0.4684 0.6933 0.0252 0.0170 0.414 4.350 2.387 308.811 0.491 10.617 3.506 0.41 164707. 0.1875 47.16 0.4897 0.6773 0.0216 0.0156 0.379 3.983 2.042 282.742 0.450 9.084 3.276 0.41 164997. 0.1621 49.21 0.5109 0.6505 0.0179 0.0141 0.342 3.594 1.696 255.100 0.406 7.544 3.015 0.41 165296. 0.1359 51.26 0.5322 0.6087 0.0143 0.0125 0.303 3.183 1.350 225.982 0.360 6.003 2.709 0.41 165606. 0.1089 53.31 0.5535 0.5447 0.0106 0.0108 0.262 2.754 1.005 195.513 0.311 4.469 2.331 0.41 165926. 0.0809 55.36 0.5748 0.4454 0.0070 0.0090 0.220 2.308 0.663 163.848 0.261 2.949 1.835 0.41 166256. 0.0517 57.41 0.5961 0.2841 0.0034 0.0072 0.176 1.848 0.326 131.164 0.209 1.452 1.129 0.41 166597. 0.0223 59.46 0.6174 -0.0067 -0.0001 0.0054 0.131 1.372 -0.006 97.407 0.155 -0.025 -0.026 0.41 166934. 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 0.0836 0.0259 1.002 9.020 10.773 747.044 1.019 47.916 6.541 0.47 187539. 0.7431 2.39 0.0213 0.0667 0.0821 0.0262 1.013 9.121 10.587 755.348 1.030 47.093 6.358 0.47 187646. 0.7161 4.78 0.0426 0.1295 0.0806 0.0265 1.023 9.211 10.389 762.838 1.041 46.210 6.177 0.47 187761. 0.6892 7.18 0.0639 0.1887 0.0789 0.0267 1.032 9.289 10.177 769.335 1.050 45.267 6.000 0.47 187884. 0.6626 9.57 0.0851 0.2444 0.0772 0.0269 1.039 9.354 9.950 774.659 1.057 44.260 5.826 0.47 188016. 0.6362 11.96 0.1064 0.2965 0.0753 0.0270 1.044 9.402 9.709 778.627 1.062 43.186 5.656 0.47 188158. 0.6101 14.35 0.1277 0.3453 0.0733 0.0271 1.047 9.431 9.452 781.049 1.065 42.045 5.489 0.47 188308. 0.5842 16.74 0.1490 0.3910 0.0712 0.0271 1.048 9.439 9.180 781.737 1.066 40.833 5.326 0.47 188468. 0.5586 19.13 0.1703 0.4334 0.0690 0.0271 1.047 9.424 8.891 780.503 1.065 39.549 5.167 0.47 188638. 0.5334 21.53 0.1916 0.4729 0.0666 0.0270 1.042 9.384 8.587 777.164 1.060 38.193 5.011 0.47 188818. 0.5083 23.92 0.2129 0.5095 0.0641 0.0268 1.035 9.316 8.265 771.537 1.053 36.763 4.859 0.47 189009. 0.4835 26.31 0.2342 0.5432 0.0615 0.0265 1.024 9.218 7.927 763.439 1.041 35.258 4.709 0.47 189210. 0.4590 28.70 0.2554 0.5741 0.0587 0.0261 1.009 9.088 7.571 752.666 1.027 33.676 4.563 0.47 189422. 0.4346 31.09 0.2767 0.6022 0.0558 0.0257 0.991 8.924 7.198 739.044 1.008 32.019 4.418 0.47 189644. 0.4103 33.49 0.2980 0.6276 0.0528 0.0251 0.969 8.724 6.810 722.508 0.986 30.290 4.275 0.47 189878. 0.3862 35.88 0.3193 0.6501 0.0497 0.0244 0.943 8.489 6.406 703.051 0.959 28.496 4.133 0.47 190123. 0.3621 38.27 0.3406 0.6696 0.0465 0.0236 0.913 8.219 5.990 680.676 0.929 26.643 3.991 0.47 190379. 0.3382 40.66 0.3619 0.6861 0.0431 0.0228 0.879 7.914 5.561 655.387 0.894 24.736 3.849 0.47 190647. 0.3142 43.05 0.3832 0.6991 0.0397 0.0218 0.841 7.573 5.122 627.193 0.856 22.781 3.704 0.47 190925. 0.2902 45.44 0.4045 0.7083 0.0362 0.0207 0.799 7.198 4.673 596.109 0.813 20.784 3.555 0.47 191216. 0.2660 47.84 0.4257 0.7132 0.0327 0.0195 0.754 6.788 4.215 562.163 0.767 18.749 3.401 0.47 191518. 0.2417 50.23 0.4470 0.7130 0.0291 0.0182 0.705 6.344 3.751 525.398 0.717 16.684 3.238 0.48 191832. 0.2171 52.62 0.4683 0.7065 0.0255 0.0169 0.652 5.867 3.281 485.876 0.663 14.593 3.063 0.48 192157. 0.1920 55.01 0.4896 0.6921 0.0218 0.0154 0.595 5.357 2.807 443.687 0.605 12.486 2.870 0.48 192495. 0.1664 57.40 0.5109 0.6669 0.0181 0.0139 0.535 4.817 2.331 398.950 0.544 10.368 2.650 0.48 192844. 0.1401 59.80 0.5322 0.6268 0.0144 0.0122 0.472 4.248 1.855 351.824 0.480 8.250 2.391 0.48 193206. 0.1127 62.19 0.5535 0.5643 0.0107 0.0105 0.406 3.653 1.380 302.511 0.413 6.140 2.070 0.48 193579. 0.0842 64.58 0.5747 0.4653 0.0071 0.0087 0.337 3.034 0.911 251.263 0.343 4.050 1.644 0.48 193964. 0.0543 66.97 0.5960 0.3006 0.0035 0.0069 0.266 2.395 0.448 198.374 0.271 1.992 1.024 0.48 194361. 0.0237 69.36 0.6173 -0.0088 -0.0001 0.0050 0.193 1.735 -0.009 143.707 0.196 -0.041 -0.029 0.48 194754. 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 0.0844 0.0261 1.503 11.843 14.211 1120.906 1.338 63.212 5.751 0.54 214317. 0.7504 2.73 0.0213 0.0670 0.0830 0.0264 1.520 11.976 13.969 1133.510 1.353 62.135 5.590 0.54 214439. 0.7232 5.46 0.0426 0.1301 0.0814 0.0266 1.535 12.096 13.709 1144.875 1.367 60.978 5.431 0.54 214572. 0.6961 8.20 0.0638 0.1896 0.0798 0.0269 1.549 12.200 13.431 1154.723 1.378 59.741 5.276 0.54 214713. 0.6693 10.93 0.0851 0.2455 0.0780 0.0270 1.559 12.285 13.134 1162.781 1.388 58.420 5.123 0.54 214865. 0.6427 13.66 0.1064 0.2979 0.0761 0.0272 1.567 12.348 12.817 1168.770 1.395 57.010 4.974 0.54 215026. 0.6164 16.39 0.1277 0.3470 0.0741 0.0273 1.572 12.387 12.480 1172.405 1.399 55.510 4.828 0.54 215199. 0.5904 19.13 0.1490 0.3929 0.0720 0.0273 1.574 12.397 12.122 1173.396 1.401 53.917 4.686 0.54 215383. 0.5647 21.86 0.1702 0.4357 0.0697 0.0272 1.571 12.377 11.742 1171.459 1.398 52.228 4.546 0.54 215577. 0.5393 24.59 0.1915 0.4755 0.0674 0.0271 1.564 12.322 11.341 1166.316 1.392 50.443 4.410 0.54 215784. 0.5141 27.32 0.2128 0.5124 0.0648 0.0269 1.552 12.231 10.917 1157.694 1.382 48.560 4.277 0.54 216002. 0.4892 30.06 0.2341 0.5464 0.0622 0.0266 1.536 12.101 10.471 1145.313 1.367 46.577 4.147 0.54 216232. 0.4645 32.79 0.2553 0.5777 0.0594 0.0263 1.514 11.927 10.003 1128.871 1.347 44.493 4.019 0.54 216475. 0.4400 35.52 0.2766 0.6063 0.0565 0.0258 1.486 11.707 9.512 1108.094 1.323 42.307 3.893 0.54 216730. 0.4157 38.25 0.2979 0.6321 0.0534 0.0252 1.452 11.441 8.999 1082.881 1.293 40.027 3.769 0.54 216998. 0.3914 40.99 0.3192 0.6552 0.0503 0.0245 1.412 11.128 8.467 1053.220 1.257 37.660 3.646 0.54 217278. 0.3673 43.72 0.3405 0.6753 0.0470 0.0237 1.367 10.767 7.917 1019.116 1.216 35.214 3.523 0.54 217571. 0.3432 46.45 0.3617 0.6924 0.0437 0.0228 1.315 10.360 7.351 980.575 1.170 32.696 3.400 0.54 217877. 0.3191 49.18 0.3830 0.7062 0.0402 0.0218 1.257 9.906 6.770 937.612 1.119 30.114 3.275 0.54 218196. 0.2950 51.92 0.4043 0.7163 0.0367 0.0207 1.194 9.406 6.177 890.250 1.063 27.475 3.147 0.54 218528. 0.2708 54.65 0.4256 0.7222 0.0331 0.0195 1.124 8.859 5.573 838.531 1.001 24.787 3.014 0.54 218873. 0.2463 57.38 0.4469 0.7231 0.0295 0.0182 1.049 8.268 4.959 782.521 0.934 22.057 2.874 0.54 219232. 0.2216 60.11 0.4681 0.7178 0.0258 0.0168 0.969 7.631 4.338 722.315 0.862 19.295 2.724 0.54 219604. 0.1964 62.85 0.4894 0.7048 0.0220 0.0153 0.882 6.952 3.711 658.050 0.785 16.508 2.558 0.54 219990. 0.1706 65.58 0.5107 0.6812 0.0183 0.0137 0.791 6.233 3.082 589.909 0.704 13.708 2.370 0.54 220389. 0.1440 68.31 0.5320 0.6428 0.0146 0.0121 0.695 5.474 2.452 518.131 0.618 10.907 2.146 0.55 220802. 0.1164 71.04 0.5532 0.5818 0.0108 0.0103 0.594 4.681 1.825 443.027 0.529 8.116 1.868 0.55 221229. 0.0874 73.78 0.5745 0.4836 0.0071 0.0085 0.489 3.856 1.203 364.984 0.436 5.352 1.495 0.55 221669. 0.0568 76.51 0.5958 0.3161 0.0035 0.0066 0.381 3.005 0.591 284.451 0.340 2.629 0.942 0.55 222122. 0.0251 79.24 0.6171 -0.0107 -0.0001 0.0047 0.270 2.125 -0.014 201.161 0.240 -0.061 -0.031 0.55 222569. 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 0.0854 0.0263 2.161 15.133 18.199 1611.322 1.710 80.951 5.123 0.61 241088. 0.7565 3.07 0.0213 0.0671 0.0840 0.0266 2.185 15.304 17.892 1629.591 1.729 79.584 4.980 0.61 241227. 0.7292 6.14 0.0425 0.1303 0.0824 0.0269 2.207 15.459 17.562 1646.046 1.747 78.117 4.839 0.61 241376. 0.7020 9.22 0.0638 0.1899 0.0808 0.0271 2.226 15.592 17.209 1660.281 1.762 76.545 4.701 0.61 241536. 0.6751 12.29 0.0851 0.2460 0.0790 0.0273 2.242 15.702 16.831 1671.907 1.774 74.864 4.566 0.61 241707. 0.6485 15.36 0.1063 0.2986 0.0771 0.0275 2.254 15.782 16.428 1680.509 1.783 73.070 4.434 0.61 241890. 0.6221 18.43 0.1276 0.3478 0.0751 0.0275 2.261 15.831 15.998 1685.676 1.789 71.159 4.305 0.61 242085. 0.5960 21.50 0.1489 0.3939 0.0729 0.0276 2.262 15.843 15.541 1686.988 1.790 69.128 4.179 0.61 242292. 0.5702 24.58 0.1701 0.4369 0.0707 0.0275 2.258 15.815 15.057 1684.035 1.787 66.973 4.055 0.61 242512. 0.5447 27.65 0.1914 0.4770 0.0683 0.0274 2.248 15.744 14.544 1676.414 1.779 64.694 3.935 0.61 242745. 0.5195 30.72 0.2126 0.5141 0.0657 0.0272 2.231 15.625 14.003 1663.727 1.765 62.288 3.818 0.61 242991. 0.4945 33.79 0.2339 0.5485 0.0630 0.0269 2.207 15.454 13.434 1645.575 1.746 59.753 3.703 0.61 243251. 0.4698 36.86 0.2552 0.5802 0.0602 0.0265 2.175 15.228 12.835 1621.530 1.720 57.088 3.590 0.61 243524. 0.4452 39.94 0.2764 0.6091 0.0573 0.0260 2.134 14.943 12.206 1591.189 1.688 54.292 3.479 0.61 243812. 0.4208 43.01 0.2977 0.6354 0.0542 0.0254 2.084 14.598 11.550 1554.391 1.649 51.373 3.370 0.61 244113. 0.3965 46.08 0.3190 0.6590 0.0510 0.0247 2.026 14.192 10.868 1511.121 1.603 48.340 3.262 0.61 244429. 0.3723 49.15 0.3402 0.6797 0.0477 0.0239 1.960 13.724 10.163 1461.387 1.551 45.206 3.154 0.61 244759. 0.3481 52.22 0.3615 0.6974 0.0443 0.0230 1.884 13.197 9.438 1405.204 1.491 41.979 3.046 0.61 245104. 0.3240 55.30 0.3828 0.7120 0.0408 0.0219 1.800 12.609 8.693 1342.591 1.425 38.668 2.937 0.61 245463. 0.2998 58.37 0.4040 0.7229 0.0372 0.0208 1.708 11.961 7.933 1273.587 1.351 35.284 2.825 0.61 245837. 0.2754 61.44 0.4253 0.7297 0.0336 0.0196 1.607 11.253 7.157 1198.253 1.271 31.835 2.709 0.61 246225. 0.2509 64.51 0.4466 0.7317 0.0299 0.0182 1.497 10.487 6.369 1116.682 1.185 28.331 2.587 0.61 246629. 0.2260 67.58 0.4678 0.7277 0.0261 0.0168 1.380 9.664 5.572 1029.018 1.092 24.785 2.456 0.61 247047. 0.2007 70.66 0.4891 0.7160 0.0224 0.0153 1.254 8.785 4.768 935.456 0.993 21.207 2.312 0.61 247481. 0.1747 73.73 0.5104 0.6941 0.0186 0.0137 1.121 7.854 3.959 836.263 0.887 17.611 2.147 0.61 247930. 0.1479 76.80 0.5316 0.6574 0.0148 0.0120 0.981 6.873 3.150 731.789 0.776 14.012 1.952 0.61 248394. 0.1200 79.87 0.5529 0.5981 0.0110 0.0102 0.835 5.846 2.344 622.488 0.660 10.427 1.708 0.61 248874. 0.0905 82.94 0.5741 0.5009 0.0073 0.0083 0.682 4.779 1.546 508.922 0.540 6.874 1.377 0.62 249369. 0.0593 86.02 0.5954 0.3313 0.0036 0.0064 0.525 3.679 0.759 391.753 0.416 3.375 0.879 0.62 249878. 0.0265 89.09 0.6167 -0.0124 -0.0001 0.0044 0.363 2.541 -0.019 270.519 0.287 -0.084 -0.032 0.62 250378. 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 0.0866 0.0267 3.006 18.948 22.782 2241.830 2.141 101.333 4.609 0.67 267851. 0.7616 3.41 0.0212 0.0670 0.0852 0.0270 3.041 19.164 22.402 2267.382 2.165 99.645 4.481 0.67 268006. 0.7342 6.82 0.0425 0.1302 0.0836 0.0273 3.071 19.359 21.994 2290.363 2.187 97.829 4.356 0.67 268172. 0.7071 10.23 0.0637 0.1898 0.0819 0.0275 3.098 19.526 21.556 2310.204 2.206 95.882 4.232 0.67 268351. 0.6802 13.64 0.0850 0.2459 0.0802 0.0277 3.120 19.663 21.087 2326.352 2.222 93.796 4.111 0.67 268542. 0.6536 17.05 0.1062 0.2985 0.0783 0.0278 3.136 19.763 20.586 2338.235 2.233 91.568 3.993 0.67 268746. 0.6272 20.46 0.1275 0.3479 0.0762 0.0279 3.145 19.823 20.052 2345.268 2.240 89.192 3.878 0.67 268964. 0.6011 23.87 0.1487 0.3941 0.0741 0.0280 3.147 19.836 19.484 2346.865 2.241 86.663 3.766 0.67 269195. 0.5754 27.28 0.1700 0.4372 0.0718 0.0279 3.141 19.799 18.880 2342.453 2.237 83.979 3.656 0.67 269440. 0.5499 30.69 0.1912 0.4775 0.0693 0.0278 3.127 19.706 18.241 2331.465 2.226 81.136 3.549 0.67 269700. 0.5247 34.10 0.2125 0.5149 0.0668 0.0276 3.102 19.553 17.566 2313.353 2.209 78.133 3.444 0.67 269974. 0.4997 37.51 0.2337 0.5496 0.0641 0.0272 3.068 19.335 16.854 2287.569 2.184 74.969 3.342 0.67 270264. 0.4749 40.92 0.2549 0.5816 0.0612 0.0268 3.022 19.047 16.106 2253.518 2.152 71.639 3.242 0.67 270568. 0.4503 44.33 0.2762 0.6109 0.0582 0.0263 2.965 18.685 15.320 2210.633 2.111 68.143 3.143 0.67 270889. 0.4259 47.74 0.2974 0.6376 0.0551 0.0257 2.895 18.246 14.499 2158.673 2.061 64.490 3.046 0.68 271224. 0.4015 51.15 0.3187 0.6617 0.0519 0.0250 2.813 17.730 13.645 2097.618 2.003 60.695 2.951 0.68 271576. 0.3773 54.56 0.3399 0.6830 0.0485 0.0241 2.719 17.137 12.763 2027.482 1.936 56.769 2.855 0.68 271943. 0.3531 57.97 0.3612 0.7013 0.0451 0.0232 2.613 16.467 11.854 1948.293 1.860 52.724 2.760 0.68 272326. 0.3289 61.38 0.3824 0.7166 0.0415 0.0222 2.494 15.722 10.920 1860.084 1.776 48.574 2.663 0.68 272725. 0.3046 64.79 0.4037 0.7283 0.0379 0.0210 2.364 14.901 9.966 1762.910 1.683 44.329 2.564 0.68 273141. 0.2802 68.20 0.4249 0.7361 0.0342 0.0197 2.222 14.004 8.993 1656.859 1.582 40.002 2.462 0.68 273572. 0.2556 71.61 0.4462 0.7392 0.0304 0.0184 2.068 13.034 8.005 1542.069 1.473 35.605 2.354 0.68 274021. 0.2306 75.02 0.4674 0.7364 0.0266 0.0169 1.903 11.992 7.004 1418.737 1.355 31.152 2.239 0.68 274486. 0.2051 78.43 0.4886 0.7262 0.0228 0.0153 1.726 10.879 5.993 1287.139 1.229 26.658 2.112 0.68 274967. 0.1790 81.85 0.5099 0.7058 0.0189 0.0137 1.539 9.700 4.978 1147.650 1.096 22.140 1.967 0.68 275466. 0.1519 85.26 0.5311 0.6709 0.0151 0.0119 1.342 8.459 3.961 1000.773 0.956 17.617 1.795 0.68 275981. 0.1237 88.67 0.5524 0.6134 0.0112 0.0101 1.136 7.160 2.947 847.162 0.809 13.110 1.578 0.68 276513. 0.0938 92.08 0.5736 0.5174 0.0074 0.0082 0.922 5.812 1.943 687.645 0.657 8.644 1.282 0.68 277062. 0.0619 95.49 0.5949 0.3461 0.0036 0.0062 0.702 4.422 0.954 523.198 0.500 4.243 0.827 0.68 277628. 0.0280 98.90 0.6161 -0.0139 -0.0001 0.0042 0.474 2.985 -0.025 353.149 0.337 -0.111 -0.032 0.69 278181. 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 0.0880 0.0273 4.090 23.433 28.019 3049.593 2.647 124.627 4.167 0.74 294603. 0.7636 3.75 0.0212 0.0666 0.0866 0.0276 4.134 23.686 27.560 3082.506 2.676 122.587 4.055 0.74 294775. 0.7370 7.49 0.0424 0.1296 0.0850 0.0278 4.173 23.914 27.066 3112.175 2.702 120.388 3.945 0.74 294959. 0.7104 11.24 0.0637 0.1890 0.0834 0.0281 4.208 24.111 26.535 3137.819 2.724 118.026 3.836 0.74 295156. 0.6839 14.98 0.0849 0.2449 0.0816 0.0283 4.236 24.271 25.965 3158.659 2.742 115.492 3.728 0.74 295368. 0.6577 18.73 0.1061 0.2975 0.0797 0.0284 4.256 24.388 25.355 3173.887 2.755 112.780 3.623 0.74 295593. 0.6316 22.48 0.1273 0.3469 0.0776 0.0285 4.268 24.455 24.704 3182.670 2.763 109.884 3.521 0.74 295834. 0.6057 26.22 0.1485 0.3932 0.0754 0.0285 4.270 24.467 24.010 3184.156 2.764 106.797 3.420 0.74 296089. 0.5801 29.97 0.1697 0.4365 0.0731 0.0284 4.261 24.416 23.273 3177.508 2.758 103.517 3.322 0.74 296360. 0.5548 33.72 0.1910 0.4769 0.0707 0.0283 4.240 24.296 22.491 3161.908 2.745 100.039 3.226 0.74 296647. 0.5296 37.46 0.2122 0.5145 0.0681 0.0281 4.206 24.101 21.664 3136.569 2.723 96.362 3.133 0.74 296950. 0.5048 41.21 0.2334 0.5494 0.0653 0.0277 4.158 23.826 20.792 3100.747 2.692 92.482 3.041 0.74 297269. 0.4801 44.95 0.2546 0.5818 0.0624 0.0273 4.095 23.464 19.874 3053.651 2.651 88.398 2.952 0.74 297605. 0.4555 48.70 0.2758 0.6115 0.0594 0.0268 4.016 23.009 18.909 2994.498 2.600 84.107 2.864 0.74 297958. 0.4311 52.45 0.2970 0.6387 0.0562 0.0262 3.920 22.459 17.900 2922.935 2.537 79.619 2.778 0.74 298328. 0.4068 56.19 0.3183 0.6632 0.0529 0.0254 3.807 21.814 16.851 2838.934 2.465 74.951 2.692 0.74 298715. 0.3826 59.94 0.3395 0.6851 0.0495 0.0245 3.678 21.073 15.764 2742.528 2.381 70.120 2.607 0.74 299119. 0.3583 63.69 0.3607 0.7041 0.0460 0.0236 3.532 20.238 14.645 2633.776 2.286 65.141 2.522 0.74 299541. 0.3341 67.43 0.3819 0.7201 0.0424 0.0225 3.370 19.308 13.495 2512.753 2.181 60.028 2.436 0.75 299981. 0.3098 71.18 0.4031 0.7327 0.0387 0.0213 3.191 18.284 12.319 2379.576 2.066 54.795 2.348 0.75 300438. 0.2853 74.92 0.4243 0.7414 0.0349 0.0200 2.996 17.169 11.119 2234.415 1.940 49.459 2.257 0.75 300913. 0.2605 78.67 0.4456 0.7454 0.0311 0.0186 2.786 15.963 9.900 2077.521 1.804 44.033 2.161 0.75 301406. 0.2354 82.42 0.4668 0.7437 0.0272 0.0171 2.560 14.670 8.664 1909.249 1.657 38.537 2.058 0.75 301916. 0.2097 86.16 0.4880 0.7344 0.0233 0.0155 2.320 13.294 7.416 1730.095 1.502 32.987 1.944 0.75 302446. 0.1833 89.91 0.5092 0.7149 0.0194 0.0138 2.066 11.839 6.161 1540.723 1.338 27.404 1.814 0.75 302993. 0.1558 93.66 0.5304 0.6805 0.0154 0.0120 1.800 10.312 4.904 1342.002 1.165 21.812 1.657 0.75 303559. 0.1271 97.40 0.5516 0.6229 0.0115 0.0102 1.522 8.721 3.650 1135.040 0.985 16.237 1.459 0.75 304143. 0.0965 101.15 0.5729 0.5256 0.0076 0.0082 1.235 7.078 2.408 921.210 0.800 10.709 1.185 0.75 304746. 0.0637 104.89 0.5941 0.3512 0.0037 0.0063 0.942 5.395 1.182 702.110 0.610 5.258 0.764 0.75 305367. 0.0287 108.64 0.6153 -0.0138 -0.0001 0.0043 0.640 3.664 -0.030 476.901 0.414 -0.136 -0.029 0.75 305974. 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 0.0897 0.0289 5.614 29.485 33.983 4186.114 3.331 151.157 3.682 0.81 321341. 0.7430 4.08 0.0212 0.0643 0.0883 0.0291 5.653 29.694 33.441 4215.803 3.355 148.746 3.598 0.81 321529. 0.7202 8.16 0.0424 0.1257 0.0867 0.0292 5.688 29.875 32.855 4241.425 3.375 146.140 3.513 0.81 321731. 0.6971 12.24 0.0635 0.1840 0.0851 0.0294 5.716 30.020 32.224 4262.099 3.392 143.332 3.429 0.81 321948. 0.6739 16.32 0.0847 0.2393 0.0833 0.0295 5.735 30.125 31.545 4276.937 3.403 140.313 3.345 0.81 322180. 0.6504 20.40 0.1059 0.2917 0.0813 0.0295 5.746 30.182 30.817 4285.006 3.410 137.074 3.262 0.81 322427. 0.6268 24.48 0.1271 0.3411 0.0793 0.0295 5.747 30.184 30.037 4285.322 3.410 133.606 3.179 0.81 322691. 0.6032 28.56 0.1483 0.3877 0.0771 0.0295 5.735 30.124 29.205 4276.897 3.403 129.904 3.097 0.81 322971. 0.5794 32.64 0.1694 0.4315 0.0748 0.0294 5.711 29.997 28.319 4258.739 3.389 125.962 3.016 0.81 323268. 0.5556 36.71 0.1906 0.4725 0.0723 0.0292 5.672 29.793 27.378 4229.802 3.366 121.777 2.936 0.81 323582. 0.5317 40.79 0.2118 0.5108 0.0696 0.0289 5.618 29.506 26.381 4189.069 3.334 117.344 2.856 0.81 323914. 0.5079 44.87 0.2330 0.5465 0.0669 0.0285 5.546 29.128 25.329 4135.483 3.291 112.662 2.778 0.81 324264. 0.4840 48.95 0.2541 0.5795 0.0639 0.0280 5.455 28.652 24.219 4067.906 3.237 107.727 2.700 0.81 324631. 0.4600 53.03 0.2753 0.6100 0.0609 0.0275 5.344 28.070 23.052 3985.260 3.171 102.536 2.624 0.81 325017. 0.4361 57.11 0.2965 0.6377 0.0576 0.0268 5.213 27.380 21.830 3887.285 3.093 97.100 2.547 0.81 325422. 0.4120 61.19 0.3177 0.6628 0.0543 0.0260 5.061 26.580 20.558 3773.648 3.003 91.441 2.471 0.81 325845. 0.3878 65.27 0.3389 0.6852 0.0508 0.0251 4.887 25.669 19.240 3644.392 2.900 85.577 2.394 0.81 326287. 0.3636 69.35 0.3600 0.7045 0.0472 0.0241 4.693 24.649 17.880 3499.472 2.785 79.529 2.317 0.81 326747. 0.3392 73.43 0.3812 0.7207 0.0435 0.0230 4.478 23.518 16.482 3338.968 2.657 73.313 2.239 0.81 327227. 0.3147 77.51 0.4024 0.7333 0.0397 0.0218 4.242 22.281 15.051 3163.290 2.517 66.947 2.158 0.81 327725. 0.2898 81.59 0.4236 0.7416 0.0359 0.0205 3.987 20.939 13.590 2972.860 2.366 60.450 2.073 0.81 328243. 0.2646 85.67 0.4448 0.7448 0.0320 0.0191 3.712 19.499 12.105 2768.301 2.203 53.841 1.983 0.81 328780. 0.2389 89.75 0.4659 0.7415 0.0280 0.0176 3.420 17.964 10.598 2550.479 2.030 47.139 1.885 0.82 329337. 0.2124 93.83 0.4871 0.7297 0.0240 0.0160 3.112 16.344 9.076 2320.474 1.847 40.368 1.774 0.82 329913. 0.1850 97.91 0.5083 0.7061 0.0199 0.0143 2.789 14.648 7.543 2079.582 1.655 33.551 1.645 0.82 330510. 0.1564 101.98 0.5295 0.6658 0.0159 0.0126 2.453 12.886 6.006 1829.434 1.456 26.717 1.489 0.82 331126. 0.1263 106.06 0.5506 0.6001 0.0118 0.0108 2.108 11.072 4.473 1571.963 1.251 19.897 1.291 0.82 331762. 0.0945 110.14 0.5718 0.4936 0.0078 0.0090 1.756 9.223 2.951 1309.421 1.042 13.127 1.022 0.82 332418. 0.0608 114.22 0.5930 0.3152 0.0038 0.0072 1.400 7.356 1.449 1044.292 0.831 6.446 0.629 0.82 333092. 0.0262 118.30 0.6142 -0.0111 -0.0001 0.0053 1.040 5.462 -0.036 775.427 0.617 -0.162 -0.021 0.82 333757. 0.0000 PROP RPM = 13000 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 0.0328 8.116 39.350 40.694 6052.293 4.446 181.008 3.050 0.87 348064. 0.6735 4.43 0.0212 0.0582 0.0901 0.0328 8.120 39.370 40.069 6055.391 4.448 178.227 3.001 0.87 348269. 0.6577 8.85 0.0424 0.1146 0.0886 0.0328 8.116 39.348 39.390 6051.999 4.446 175.207 2.952 0.87 348490. 0.6414 13.28 0.0636 0.1690 0.0869 0.0327 8.102 39.279 38.656 6041.329 4.438 171.941 2.902 0.87 348727. 0.6246 17.71 0.0849 0.2214 0.0852 0.0326 8.076 39.157 37.863 6022.560 4.424 168.415 2.852 0.87 348980. 0.6074 22.13 0.1061 0.2717 0.0832 0.0325 8.039 38.977 37.010 5994.795 4.404 164.618 2.800 0.87 349251. 0.5897 26.56 0.1273 0.3200 0.0812 0.0323 7.989 38.731 36.093 5957.106 4.376 160.540 2.748 0.87 349540. 0.5715 30.99 0.1485 0.3662 0.0790 0.0320 7.923 38.416 35.111 5908.516 4.340 156.172 2.695 0.88 349846. 0.5529 35.42 0.1697 0.4102 0.0766 0.0317 7.842 38.022 34.062 5848.037 4.296 151.507 2.642 0.88 350171. 0.5337 39.84 0.1909 0.4520 0.0741 0.0313 7.744 37.545 32.945 5774.680 4.242 146.538 2.588 0.88 350515. 0.5141 44.27 0.2122 0.4915 0.0714 0.0308 7.627 36.978 31.759 5687.482 4.178 141.263 2.533 0.88 350878. 0.4941 48.70 0.2334 0.5288 0.0686 0.0303 7.490 36.315 30.504 5585.433 4.103 135.680 2.477 0.88 351261. 0.4736 53.12 0.2546 0.5637 0.0656 0.0296 7.332 35.547 29.178 5467.362 4.016 129.785 2.421 0.88 351663. 0.4526 57.55 0.2758 0.5963 0.0625 0.0289 7.150 34.667 27.782 5331.903 3.917 123.573 2.363 0.88 352085. 0.4312 61.98 0.2970 0.6263 0.0592 0.0281 6.945 33.671 26.317 5178.778 3.804 117.058 2.305 0.88 352527. 0.4093 66.40 0.3182 0.6531 0.0558 0.0272 6.721 32.586 24.790 5011.896 3.682 110.264 2.243 0.88 352989. 0.3867 70.83 0.3394 0.6766 0.0522 0.0262 6.477 31.404 23.205 4830.094 3.548 103.215 2.179 0.88 353472. 0.3634 75.26 0.3607 0.6966 0.0485 0.0251 6.214 30.126 21.568 4633.547 3.404 95.936 2.111 0.88 353974. 0.3394 79.68 0.3819 0.7121 0.0447 0.0240 5.933 28.765 19.884 4424.279 3.250 88.446 2.039 0.88 354498. 0.3147 84.11 0.4031 0.7221 0.0408 0.0228 5.640 27.346 18.158 4205.954 3.090 80.766 1.958 0.88 355041. 0.2888 88.54 0.4243 0.7265 0.0369 0.0215 5.328 25.833 16.395 3973.193 2.919 72.924 1.872 0.88 355606. 0.2623 92.97 0.4455 0.7243 0.0328 0.0202 4.997 24.229 14.600 3726.552 2.737 64.942 1.777 0.88 356191. 0.2351 97.39 0.4667 0.7137 0.0287 0.0188 4.650 22.546 12.780 3467.689 2.547 56.847 1.672 0.88 356798. 0.2069 101.82 0.4879 0.6925 0.0246 0.0173 4.290 20.798 10.941 3198.839 2.350 48.667 1.551 0.88 357425. 0.1776 106.25 0.5092 0.6571 0.0204 0.0158 3.919 19.002 9.090 2922.543 2.147 40.433 1.411 0.89 358074. 0.1472 110.67 0.5304 0.6028 0.0163 0.0143 3.542 17.173 7.235 2641.225 1.940 32.183 1.243 0.89 358744. 0.1157 115.10 0.5516 0.5228 0.0121 0.0128 3.162 15.330 5.385 2357.818 1.732 23.955 1.036 0.89 359436. 0.0832 119.53 0.5728 0.4066 0.0080 0.0113 2.783 13.494 3.551 2075.488 1.525 15.795 0.776 0.89 360149. 0.0506 123.95 0.5940 0.2391 0.0039 0.0097 2.410 11.685 1.743 1797.229 1.320 7.754 0.440 0.89 360883. 0.0201 128.38 0.6152 -0.0074 -0.0001 0.0082 2.036 9.872 -0.044 1518.293 1.115 -0.197 -0.013 0.89 361616. 0.0000 PROP RPM = 14000 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 0.0923 0.0391 12.074 54.358 47.612 9003.641 6.141 211.777 2.398 0.94 374807. 0.5729 4.81 0.0214 0.0500 0.0911 0.0390 12.051 54.255 46.949 8986.597 6.130 208.830 2.370 0.94 375027. 0.5621 9.62 0.0428 0.0987 0.0896 0.0389 12.009 54.065 46.220 8955.062 6.108 205.589 2.341 0.94 375265. 0.5509 14.43 0.0642 0.1463 0.0881 0.0387 11.946 53.780 45.422 8907.918 6.076 202.038 2.313 0.94 375520. 0.5396 19.24 0.0856 0.1927 0.0864 0.0384 11.860 53.395 44.550 8844.088 6.032 198.159 2.285 0.94 375795. 0.5279 24.05 0.1070 0.2380 0.0846 0.0380 11.751 52.903 43.601 8762.717 5.977 193.936 2.257 0.94 376089. 0.5159 28.86 0.1284 0.2820 0.0826 0.0376 11.617 52.301 42.571 8662.965 5.909 189.355 2.229 0.94 376403. 0.5034 33.67 0.1498 0.3249 0.0804 0.0371 11.458 51.584 41.457 8544.168 5.828 184.403 2.201 0.94 376738. 0.4905 38.48 0.1713 0.3665 0.0781 0.0365 11.272 50.748 40.258 8405.788 5.734 179.069 2.172 0.94 377093. 0.4771 43.29 0.1927 0.4068 0.0756 0.0358 11.060 49.791 38.971 8247.243 5.625 173.344 2.143 0.94 377469. 0.4632 48.11 0.2141 0.4457 0.0729 0.0350 10.820 48.713 37.596 8068.658 5.504 167.227 2.113 0.94 377867. 0.4486 52.92 0.2355 0.4831 0.0701 0.0342 10.554 47.512 36.133 7869.804 5.368 160.718 2.082 0.94 378287. 0.4333 57.73 0.2569 0.5188 0.0671 0.0332 10.259 46.187 34.580 7650.240 5.218 153.812 2.050 0.94 378728. 0.4173 62.54 0.2783 0.5528 0.0639 0.0322 9.936 44.732 32.938 7409.250 5.054 146.507 2.016 0.94 379191. 0.4006 67.35 0.2997 0.5848 0.0605 0.0310 9.584 43.147 31.209 7146.720 4.875 138.819 1.981 0.95 379677. 0.3830 72.16 0.3211 0.6146 0.0570 0.0298 9.206 41.444 29.402 6864.664 4.682 130.781 1.943 0.95 380184. 0.3647 76.97 0.3425 0.6405 0.0534 0.0285 8.819 39.703 27.522 6576.199 4.486 122.418 1.898 0.95 380714. 0.3447 81.78 0.3639 0.6623 0.0496 0.0273 8.421 37.910 25.576 6279.287 4.283 113.762 1.847 0.95 381266. 0.3234 86.59 0.3853 0.6792 0.0457 0.0259 8.013 36.074 23.571 5975.133 4.076 104.845 1.789 0.95 381840. 0.3007 91.40 0.4067 0.6877 0.0417 0.0247 7.624 34.323 21.512 5685.121 3.878 95.685 1.716 0.95 382437. 0.2756 96.21 0.4281 0.6835 0.0376 0.0236 7.283 32.788 19.402 5430.953 3.704 86.301 1.620 0.95 383056. 0.2471 101.02 0.4495 0.6706 0.0335 0.0224 6.931 31.205 17.256 5168.727 3.526 76.754 1.514 0.95 383698. 0.2177 105.83 0.4709 0.6476 0.0292 0.0213 6.572 29.587 15.081 4900.665 3.343 67.082 1.396 0.95 384363. 0.1876 110.64 0.4924 0.6125 0.0250 0.0201 6.208 27.948 12.888 4629.246 3.158 57.327 1.263 0.95 385051. 0.1569 115.45 0.5138 0.5630 0.0207 0.0189 5.844 26.309 10.687 4357.699 2.972 47.537 1.112 0.95 385762. 0.1259 120.26 0.5352 0.4965 0.0165 0.0178 5.485 24.692 8.491 4089.899 2.790 37.767 0.942 0.95 386496. 0.0950 125.07 0.5566 0.4101 0.0122 0.0166 5.134 23.112 6.313 3828.126 2.611 28.080 0.748 0.96 387254. 0.0651 129.88 0.5780 0.3012 0.0081 0.0155 4.794 21.581 4.169 3574.649 2.438 18.544 0.529 0.96 388036. 0.0374 134.70 0.5994 0.1667 0.0040 0.0145 4.466 20.107 2.073 3330.505 2.272 9.222 0.282 0.96 388843. 0.0141 139.51 0.6208 0.0001 0.0000 0.0134 4.128 18.584 0.002 3078.176 2.100 0.007 0.000 0.96 389685. 0.0000