18x7WP (18x7WP.dat) v2024-0915 Simulation Date: 11/12/2024 AIRFOIL AERO DATA GENERATED USING: POLARS ====== 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 0.0773 0.0306 0.005 0.293 0.259 3.472 0.033 1.150 33.783 0.07 38475. 0.5600 0.32 0.0189 0.0466 0.0757 0.0307 0.005 0.294 0.253 3.482 0.033 1.126 32.978 0.07 38495. 0.5409 0.64 0.0378 0.0910 0.0740 0.0308 0.005 0.295 0.247 3.489 0.033 1.101 32.170 0.07 38516. 0.5216 0.97 0.0568 0.1330 0.0722 0.0308 0.005 0.295 0.241 3.492 0.033 1.074 31.359 0.07 38538. 0.5023 1.29 0.0757 0.1727 0.0703 0.0308 0.005 0.295 0.235 3.492 0.033 1.046 30.547 0.07 38561. 0.4829 1.61 0.0946 0.2102 0.0683 0.0308 0.005 0.295 0.229 3.487 0.033 1.017 29.732 0.07 38586. 0.4634 1.93 0.1135 0.2453 0.0663 0.0307 0.005 0.294 0.222 3.478 0.033 0.986 28.915 0.07 38612. 0.4438 2.26 0.1324 0.2780 0.0641 0.0305 0.005 0.293 0.215 3.464 0.033 0.954 28.096 0.07 38639. 0.4242 2.58 0.1513 0.3085 0.0619 0.0304 0.005 0.291 0.207 3.445 0.033 0.921 27.274 0.07 38668. 0.4046 2.90 0.1703 0.3365 0.0596 0.0302 0.005 0.289 0.199 3.420 0.033 0.887 26.447 0.07 38698. 0.3850 3.22 0.1892 0.3621 0.0572 0.0299 0.005 0.287 0.191 3.390 0.032 0.851 25.615 0.07 38730. 0.3653 3.55 0.2081 0.3853 0.0548 0.0296 0.004 0.283 0.183 3.353 0.032 0.815 24.775 0.07 38764. 0.3457 3.87 0.2270 0.4059 0.0522 0.0292 0.004 0.280 0.175 3.311 0.032 0.777 23.927 0.07 38799. 0.3260 4.19 0.2459 0.4239 0.0496 0.0288 0.004 0.276 0.166 3.262 0.031 0.738 23.067 0.07 38835. 0.3063 4.51 0.2649 0.4392 0.0469 0.0283 0.004 0.271 0.157 3.207 0.031 0.698 22.193 0.07 38874. 0.2866 4.84 0.2838 0.4517 0.0441 0.0277 0.004 0.266 0.148 3.144 0.030 0.657 21.301 0.07 38913. 0.2668 5.16 0.3027 0.4611 0.0413 0.0271 0.004 0.260 0.138 3.075 0.029 0.615 20.387 0.07 38955. 0.2471 5.48 0.3216 0.4673 0.0384 0.0264 0.004 0.253 0.129 2.998 0.029 0.572 19.445 0.07 38998. 0.2273 5.80 0.3405 0.4700 0.0355 0.0257 0.004 0.246 0.119 2.914 0.028 0.528 18.470 0.07 39044. 0.2074 6.13 0.3595 0.4688 0.0325 0.0249 0.004 0.238 0.109 2.821 0.027 0.483 17.453 0.07 39091. 0.1875 6.45 0.3784 0.4633 0.0294 0.0240 0.004 0.230 0.098 2.721 0.026 0.437 16.385 0.07 39139. 0.1675 6.77 0.3973 0.4528 0.0263 0.0230 0.004 0.221 0.088 2.613 0.025 0.391 15.252 0.07 39190. 0.1474 7.09 0.4162 0.4366 0.0231 0.0220 0.003 0.211 0.077 2.496 0.024 0.344 14.038 0.07 39242. 0.1272 7.42 0.4351 0.4137 0.0199 0.0209 0.003 0.200 0.067 2.371 0.023 0.296 12.723 0.07 39297. 0.1070 7.74 0.4540 0.3826 0.0166 0.0197 0.003 0.189 0.056 2.238 0.021 0.248 11.277 0.07 39353. 0.0867 8.06 0.4730 0.3416 0.0134 0.0185 0.003 0.177 0.045 2.097 0.020 0.199 9.664 0.07 39411. 0.0666 8.38 0.4919 0.2878 0.0100 0.0172 0.003 0.165 0.034 1.947 0.019 0.150 7.831 0.07 39471. 0.0468 8.71 0.5108 0.2177 0.0067 0.0158 0.002 0.151 0.022 1.789 0.017 0.100 5.702 0.07 39532. 0.0279 9.03 0.5297 0.1253 0.0034 0.0143 0.002 0.137 0.011 1.622 0.015 0.050 3.165 0.07 39596. 0.0110 9.35 0.5486 0.0013 0.0000 0.0128 0.002 0.122 0.000 1.448 0.014 0.000 0.031 0.07 39659. 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 0.0777 0.0270 0.033 1.035 1.040 24.479 0.117 4.624 19.263 0.14 76949. 0.6402 0.66 0.0193 0.0543 0.0760 0.0271 0.033 1.039 1.017 24.582 0.117 4.525 18.772 0.14 76990. 0.6172 1.32 0.0387 0.1057 0.0743 0.0272 0.033 1.042 0.994 24.659 0.118 4.421 18.283 0.14 77032. 0.5942 1.98 0.0580 0.1543 0.0724 0.0272 0.033 1.044 0.969 24.706 0.118 4.312 17.798 0.14 77078. 0.5712 2.64 0.0774 0.2002 0.0705 0.0273 0.033 1.045 0.944 24.720 0.118 4.197 17.315 0.14 77126. 0.5483 3.30 0.0967 0.2433 0.0685 0.0272 0.033 1.044 0.917 24.697 0.118 4.077 16.835 0.14 77176. 0.5254 3.96 0.1160 0.2837 0.0664 0.0272 0.033 1.041 0.888 24.634 0.118 3.952 16.359 0.14 77230. 0.5026 4.62 0.1354 0.3214 0.0642 0.0270 0.033 1.037 0.859 24.528 0.117 3.821 15.885 0.14 77287. 0.4800 5.27 0.1547 0.3564 0.0619 0.0269 0.033 1.030 0.828 24.378 0.116 3.685 15.414 0.14 77346. 0.4574 5.93 0.1741 0.3888 0.0595 0.0267 0.032 1.022 0.797 24.179 0.115 3.544 14.945 0.14 77409. 0.4349 6.59 0.1934 0.4185 0.0571 0.0264 0.032 1.011 0.764 23.931 0.114 3.398 14.477 0.14 77475. 0.4125 7.25 0.2127 0.4454 0.0545 0.0260 0.032 0.999 0.730 23.630 0.113 3.246 14.010 0.14 77544. 0.3902 7.91 0.2321 0.4697 0.0519 0.0257 0.031 0.984 0.695 23.274 0.111 3.091 13.541 0.14 77616. 0.3679 8.57 0.2514 0.4911 0.0492 0.0252 0.031 0.966 0.659 22.860 0.109 2.930 13.070 0.14 77692. 0.3458 9.23 0.2708 0.5097 0.0465 0.0247 0.030 0.946 0.622 22.387 0.107 2.765 12.595 0.14 77771. 0.3237 9.89 0.2901 0.5252 0.0436 0.0241 0.029 0.923 0.584 21.851 0.104 2.596 12.114 0.14 77854. 0.3017 10.55 0.3094 0.5376 0.0407 0.0234 0.028 0.898 0.545 21.251 0.101 2.423 11.625 0.14 77940. 0.2797 11.21 0.3288 0.5465 0.0377 0.0227 0.028 0.870 0.505 20.585 0.098 2.245 11.123 0.14 78031. 0.2576 11.87 0.3481 0.5517 0.0347 0.0219 0.027 0.839 0.464 19.851 0.095 2.064 10.605 0.14 78124. 0.2355 12.53 0.3675 0.5527 0.0316 0.0210 0.026 0.805 0.423 19.046 0.091 1.880 10.065 0.14 78222. 0.2133 13.19 0.3868 0.5490 0.0284 0.0200 0.024 0.768 0.380 18.169 0.087 1.692 9.496 0.14 78323. 0.1909 13.85 0.4061 0.5396 0.0252 0.0190 0.023 0.728 0.337 17.220 0.082 1.501 8.890 0.14 78428. 0.1683 14.50 0.4255 0.5235 0.0220 0.0179 0.022 0.684 0.294 16.196 0.077 1.308 8.232 0.14 78537. 0.1455 15.16 0.4448 0.4990 0.0187 0.0166 0.020 0.638 0.250 15.098 0.072 1.111 7.507 0.14 78650. 0.1223 15.82 0.4642 0.4639 0.0153 0.0154 0.019 0.588 0.205 13.924 0.066 0.913 6.688 0.14 78767. 0.0988 16.48 0.4835 0.4146 0.0120 0.0140 0.017 0.536 0.160 12.676 0.061 0.713 5.737 0.14 78888. 0.0749 17.14 0.5028 0.3455 0.0086 0.0125 0.015 0.480 0.115 11.354 0.054 0.512 4.598 0.14 79012. 0.0508 17.80 0.5222 0.2476 0.0052 0.0110 0.013 0.421 0.070 9.959 0.048 0.310 3.173 0.14 79141. 0.0273 18.46 0.5415 0.1042 0.0018 0.0094 0.011 0.359 0.024 8.492 0.041 0.107 1.288 0.14 79272. 0.0065 19.12 0.5609 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 0.0781 0.0256 0.105 2.205 2.351 78.251 0.249 10.457 13.627 0.21 115421. 0.6811 0.97 0.0191 0.0567 0.0764 0.0257 0.105 2.215 2.302 78.624 0.250 10.238 13.278 0.21 115481. 0.6567 1.95 0.0381 0.1105 0.0747 0.0258 0.106 2.223 2.250 78.910 0.251 10.007 12.931 0.21 115544. 0.6323 2.92 0.0572 0.1614 0.0729 0.0258 0.106 2.228 2.195 79.096 0.252 9.764 12.588 0.21 115611. 0.6080 3.90 0.0763 0.2094 0.0710 0.0259 0.106 2.231 2.138 79.171 0.252 9.510 12.249 0.21 115682. 0.5839 4.87 0.0953 0.2546 0.0690 0.0258 0.106 2.229 2.078 79.124 0.252 9.244 11.913 0.21 115757. 0.5598 5.85 0.1144 0.2970 0.0669 0.0258 0.106 2.224 2.016 78.945 0.251 8.966 11.581 0.21 115836. 0.5360 6.82 0.1334 0.3366 0.0648 0.0257 0.105 2.215 1.951 78.625 0.250 8.676 11.252 0.21 115920. 0.5123 7.80 0.1525 0.3736 0.0625 0.0255 0.105 2.202 1.883 78.154 0.249 8.375 10.927 0.21 116007. 0.4888 8.77 0.1716 0.4079 0.0602 0.0253 0.104 2.184 1.813 77.525 0.247 8.062 10.605 0.21 116100. 0.4654 9.75 0.1906 0.4395 0.0578 0.0251 0.103 2.162 1.740 76.728 0.244 7.739 10.285 0.21 116196. 0.4422 10.72 0.2097 0.4685 0.0553 0.0247 0.102 2.134 1.665 75.755 0.241 7.404 9.966 0.21 116298. 0.4192 11.70 0.2288 0.4949 0.0527 0.0244 0.100 2.102 1.587 74.598 0.237 7.059 9.649 0.21 116404. 0.3963 12.67 0.2478 0.5185 0.0501 0.0239 0.098 2.064 1.507 73.250 0.233 6.704 9.333 0.21 116516. 0.3735 13.65 0.2669 0.5394 0.0473 0.0234 0.096 2.020 1.425 71.701 0.228 6.339 9.016 0.21 116632. 0.3509 14.62 0.2860 0.5575 0.0445 0.0228 0.094 1.971 1.341 69.944 0.223 5.965 8.696 0.22 116753. 0.3283 15.60 0.3050 0.5726 0.0417 0.0222 0.091 1.915 1.255 67.973 0.216 5.582 8.373 0.22 116880. 0.3058 16.57 0.3241 0.5845 0.0387 0.0215 0.088 1.853 1.167 65.779 0.209 5.189 8.045 0.22 117012. 0.2833 17.55 0.3431 0.5930 0.0358 0.0207 0.085 1.785 1.077 63.355 0.202 4.789 7.708 0.22 117149. 0.2607 18.52 0.3622 0.5976 0.0327 0.0198 0.081 1.710 0.985 60.696 0.193 4.381 7.360 0.22 117292. 0.2381 19.50 0.3813 0.5980 0.0296 0.0189 0.078 1.628 0.891 57.797 0.184 3.965 6.996 0.22 117440. 0.2153 20.47 0.4003 0.5933 0.0265 0.0179 0.073 1.540 0.797 54.651 0.174 3.543 6.611 0.22 117594. 0.1923 21.45 0.4194 0.5825 0.0233 0.0167 0.069 1.444 0.700 51.257 0.163 3.114 6.196 0.22 117753. 0.1690 22.42 0.4385 0.5642 0.0200 0.0156 0.064 1.341 0.603 47.610 0.152 2.680 5.740 0.22 117919. 0.1453 23.40 0.4575 0.5362 0.0167 0.0143 0.059 1.231 0.504 43.710 0.139 2.241 5.228 0.22 118089. 0.1210 24.37 0.4766 0.4952 0.0134 0.0129 0.053 1.115 0.404 39.558 0.126 1.798 4.635 0.22 118266. 0.0961 25.35 0.4956 0.4356 0.0101 0.0115 0.047 0.990 0.304 35.154 0.112 1.352 3.921 0.22 118448. 0.0705 26.32 0.5147 0.3484 0.0067 0.0100 0.041 0.859 0.203 30.504 0.097 0.903 3.019 0.22 118636. 0.0444 27.30 0.5338 0.2161 0.0034 0.0084 0.034 0.722 0.102 25.611 0.082 0.454 1.806 0.22 118829. 0.0188 28.27 0.5528 -0.0008 0.0000 0.0067 0.027 0.575 0.000 20.419 0.065 -0.001 -0.006 0.22 119011. 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 0.0786 0.0248 0.242 3.810 4.206 180.311 0.430 18.707 10.579 0.29 153890. 0.7072 1.31 0.0193 0.0593 0.0769 0.0250 0.243 3.830 4.117 181.239 0.433 18.311 10.302 0.29 153971. 0.6814 2.63 0.0385 0.1155 0.0752 0.0251 0.244 3.845 4.023 181.952 0.434 17.894 10.029 0.29 154056. 0.6557 3.94 0.0578 0.1686 0.0733 0.0251 0.245 3.855 3.925 182.420 0.435 17.456 9.758 0.29 154147. 0.6302 5.25 0.0771 0.2186 0.0714 0.0252 0.245 3.859 3.821 182.616 0.436 16.997 9.491 0.29 154243. 0.6048 6.57 0.0963 0.2657 0.0694 0.0252 0.245 3.857 3.713 182.510 0.436 16.516 9.228 0.29 154345. 0.5796 7.88 0.1156 0.3099 0.0673 0.0251 0.244 3.847 3.600 182.077 0.435 16.013 8.968 0.29 154452. 0.5547 9.20 0.1349 0.3512 0.0651 0.0250 0.243 3.831 3.482 181.295 0.433 15.488 8.712 0.29 154565. 0.5299 10.51 0.1541 0.3897 0.0628 0.0248 0.242 3.806 3.359 180.141 0.430 14.943 8.459 0.29 154684. 0.5054 11.82 0.1734 0.4254 0.0604 0.0246 0.239 3.774 3.232 178.593 0.426 14.376 8.209 0.29 154809. 0.4811 13.14 0.1927 0.4585 0.0579 0.0243 0.237 3.732 3.100 176.632 0.422 13.790 7.961 0.29 154940. 0.4570 14.45 0.2119 0.4888 0.0554 0.0240 0.234 3.682 2.964 174.235 0.416 13.184 7.716 0.29 155078. 0.4331 15.76 0.2312 0.5164 0.0528 0.0236 0.230 3.621 2.824 171.382 0.409 12.559 7.473 0.29 155222. 0.4093 17.08 0.2505 0.5413 0.0500 0.0232 0.225 3.551 2.679 168.053 0.401 11.916 7.230 0.29 155373. 0.3858 18.39 0.2697 0.5634 0.0473 0.0226 0.220 3.470 2.530 164.228 0.392 11.255 6.988 0.29 155531. 0.3624 19.70 0.2890 0.5827 0.0444 0.0220 0.214 3.379 2.378 159.889 0.382 10.577 6.745 0.29 155696. 0.3391 21.02 0.3083 0.5990 0.0415 0.0214 0.208 3.276 2.222 155.014 0.370 9.882 6.500 0.29 155868. 0.3158 22.33 0.3275 0.6121 0.0385 0.0206 0.201 3.161 2.062 149.588 0.357 9.171 6.252 0.29 156047. 0.2926 23.64 0.3468 0.6217 0.0355 0.0198 0.193 3.034 1.899 143.594 0.343 8.446 5.998 0.29 156234. 0.2694 24.96 0.3661 0.6275 0.0324 0.0189 0.184 2.895 1.733 137.016 0.327 7.706 5.735 0.29 156428. 0.2461 26.27 0.3853 0.6290 0.0292 0.0179 0.174 2.744 1.563 129.841 0.310 6.953 5.461 0.29 156629. 0.2226 27.59 0.4046 0.6252 0.0260 0.0168 0.164 2.579 1.391 122.058 0.291 6.188 5.170 0.29 156838. 0.1988 28.90 0.4239 0.6152 0.0227 0.0157 0.152 2.402 1.217 113.657 0.271 5.412 4.856 0.29 157055. 0.1746 30.21 0.4431 0.5971 0.0194 0.0144 0.140 2.211 1.040 104.633 0.250 4.626 4.508 0.29 157279. 0.1499 31.53 0.4624 0.5685 0.0161 0.0131 0.127 2.007 0.861 94.984 0.227 3.832 4.113 0.29 157512. 0.1245 32.84 0.4817 0.5251 0.0127 0.0117 0.114 1.790 0.681 84.712 0.202 3.030 3.647 0.29 157752. 0.0981 34.15 0.5009 0.4598 0.0093 0.0102 0.099 1.560 0.500 73.824 0.176 2.223 3.071 0.29 157999. 0.0708 35.47 0.5202 0.3594 0.0059 0.0086 0.084 1.317 0.318 62.330 0.149 1.413 2.312 0.29 158255. 0.0425 36.78 0.5395 0.1967 0.0025 0.0069 0.067 1.061 0.135 50.234 0.120 0.601 1.220 0.29 158515. 0.0146 38.09 0.5587 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 0.0792 0.0245 0.466 5.868 6.623 347.147 0.663 29.458 8.653 0.36 192354. 0.7259 1.64 0.0193 0.0606 0.0775 0.0246 0.468 5.900 6.483 348.997 0.667 28.837 8.426 0.36 192455. 0.6993 3.28 0.0385 0.1180 0.0758 0.0247 0.470 5.924 6.336 350.420 0.669 28.183 8.201 0.36 192563. 0.6729 4.92 0.0578 0.1722 0.0739 0.0248 0.471 5.940 6.181 351.359 0.671 27.495 7.980 0.36 192676. 0.6467 6.56 0.0770 0.2233 0.0720 0.0248 0.472 5.946 6.019 351.756 0.672 26.774 7.762 0.36 192797. 0.6207 8.20 0.0963 0.2714 0.0699 0.0248 0.471 5.943 5.849 351.557 0.671 26.018 7.547 0.36 192924. 0.5950 9.84 0.1155 0.3166 0.0678 0.0247 0.470 5.929 5.672 350.711 0.670 25.228 7.335 0.36 193058. 0.5695 11.48 0.1348 0.3588 0.0656 0.0246 0.468 5.903 5.486 349.172 0.667 24.404 7.127 0.36 193200. 0.5442 13.13 0.1540 0.3983 0.0633 0.0245 0.465 5.864 5.294 346.895 0.663 23.547 6.922 0.36 193349. 0.5191 14.77 0.1733 0.4350 0.0609 0.0243 0.461 5.812 5.094 343.839 0.657 22.657 6.719 0.36 193505. 0.4944 16.41 0.1925 0.4689 0.0584 0.0240 0.456 5.747 4.887 339.962 0.649 21.736 6.520 0.36 193670. 0.4698 18.05 0.2118 0.5002 0.0559 0.0237 0.450 5.667 4.673 335.223 0.640 20.784 6.322 0.36 193842. 0.4455 19.69 0.2310 0.5288 0.0532 0.0233 0.442 5.571 4.452 329.581 0.629 19.802 6.127 0.36 194023. 0.4214 21.33 0.2503 0.5547 0.0505 0.0228 0.433 5.460 4.225 322.996 0.617 18.792 5.933 0.36 194212. 0.3975 22.97 0.2695 0.5779 0.0477 0.0223 0.423 5.332 3.991 315.430 0.602 17.753 5.739 0.36 194409. 0.3738 24.61 0.2888 0.5983 0.0449 0.0216 0.411 5.187 3.752 306.843 0.586 16.687 5.545 0.36 194615. 0.3501 26.25 0.3080 0.6158 0.0419 0.0210 0.399 5.024 3.506 297.198 0.568 15.595 5.351 0.36 194830. 0.3266 27.89 0.3273 0.6302 0.0389 0.0202 0.384 4.842 3.255 286.461 0.547 14.478 5.154 0.36 195054. 0.3031 29.53 0.3465 0.6413 0.0359 0.0194 0.368 4.642 2.999 274.598 0.524 13.338 4.953 0.36 195287. 0.2796 31.17 0.3658 0.6487 0.0327 0.0185 0.351 4.422 2.737 261.580 0.500 12.176 4.747 0.36 195530. 0.2560 32.81 0.3850 0.6518 0.0295 0.0175 0.332 4.182 2.471 247.380 0.472 10.993 4.531 0.36 195781. 0.2322 34.45 0.4043 0.6500 0.0263 0.0164 0.311 3.921 2.201 231.974 0.443 9.790 4.304 0.36 196043. 0.2081 36.09 0.4235 0.6422 0.0230 0.0152 0.289 3.640 1.927 215.346 0.411 8.570 4.058 0.36 196313. 0.1836 37.74 0.4428 0.6265 0.0197 0.0139 0.265 3.338 1.649 197.485 0.377 7.335 3.787 0.36 196594. 0.1585 39.38 0.4620 0.6005 0.0164 0.0126 0.239 3.015 1.368 178.385 0.341 6.086 3.479 0.36 196883. 0.1326 41.02 0.4813 0.5598 0.0130 0.0112 0.212 2.672 1.085 158.050 0.302 4.826 3.113 0.36 197183. 0.1057 42.66 0.5005 0.4970 0.0096 0.0096 0.183 2.307 0.800 136.493 0.261 3.557 2.657 0.36 197492. 0.0775 44.30 0.5198 0.3975 0.0061 0.0080 0.153 1.923 0.513 113.737 0.217 2.283 2.047 0.36 197811. 0.0478 45.94 0.5390 0.2302 0.0027 0.0063 0.120 1.518 0.226 89.790 0.171 1.006 1.143 0.36 198137. 0.0177 47.58 0.5583 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 0.0799 0.0244 0.800 8.408 9.629 596.839 0.950 42.828 7.317 0.43 230812. 0.7402 1.95 0.0191 0.0610 0.0783 0.0245 0.805 8.453 9.428 600.047 0.955 41.935 7.126 0.43 230933. 0.7133 3.91 0.0382 0.1189 0.0765 0.0246 0.808 8.488 9.216 602.517 0.959 40.993 6.938 0.43 231062. 0.6866 5.86 0.0573 0.1735 0.0747 0.0247 0.810 8.511 8.994 604.146 0.962 40.004 6.752 0.43 231198. 0.6601 7.82 0.0764 0.2251 0.0727 0.0247 0.811 8.520 8.760 604.840 0.963 38.967 6.569 0.43 231341. 0.6339 9.77 0.0955 0.2737 0.0707 0.0247 0.811 8.516 8.516 604.503 0.962 37.880 6.390 0.43 231493. 0.6079 11.72 0.1146 0.3193 0.0686 0.0246 0.809 8.495 8.261 603.047 0.960 36.744 6.213 0.43 231653. 0.5821 13.68 0.1337 0.3621 0.0664 0.0245 0.805 8.458 7.994 600.393 0.956 35.559 6.039 0.43 231822. 0.5566 15.63 0.1528 0.4022 0.0641 0.0244 0.800 8.402 7.717 596.465 0.949 34.326 5.868 0.43 232000. 0.5314 17.59 0.1720 0.4395 0.0617 0.0241 0.793 8.328 7.430 591.192 0.941 33.047 5.700 0.43 232186. 0.5065 19.54 0.1911 0.4741 0.0592 0.0239 0.784 8.234 7.132 584.502 0.930 31.723 5.534 0.43 232382. 0.4818 21.49 0.2102 0.5061 0.0567 0.0235 0.773 8.119 6.824 576.327 0.917 30.354 5.371 0.43 232587. 0.4573 23.45 0.2293 0.5354 0.0540 0.0231 0.760 7.982 6.507 566.596 0.902 28.942 5.209 0.43 232802. 0.4331 25.40 0.2484 0.5622 0.0513 0.0227 0.745 7.822 6.180 555.241 0.884 27.489 5.048 0.43 233027. 0.4091 27.36 0.2675 0.5863 0.0485 0.0221 0.727 7.638 5.844 542.195 0.863 25.995 4.889 0.43 233261. 0.3853 29.31 0.2866 0.6078 0.0457 0.0215 0.707 7.429 5.500 527.393 0.839 24.463 4.730 0.43 233506. 0.3616 31.26 0.3057 0.6264 0.0427 0.0209 0.685 7.195 5.147 510.772 0.813 22.893 4.570 0.43 233762. 0.3380 33.22 0.3248 0.6421 0.0397 0.0201 0.660 6.935 4.786 492.270 0.783 21.287 4.410 0.43 234027. 0.3145 35.17 0.3439 0.6547 0.0367 0.0193 0.633 6.647 4.417 471.831 0.751 19.648 4.246 0.43 234304. 0.2909 37.13 0.3630 0.6639 0.0336 0.0183 0.603 6.331 4.041 449.403 0.715 17.976 4.079 0.43 234591. 0.2673 39.08 0.3821 0.6691 0.0304 0.0174 0.570 5.986 3.659 424.940 0.676 16.274 3.905 0.43 234890. 0.2435 41.03 0.4012 0.6696 0.0271 0.0163 0.534 5.612 3.270 398.401 0.634 14.544 3.723 0.43 235199. 0.2194 42.99 0.4203 0.6646 0.0239 0.0151 0.496 5.209 2.875 369.755 0.588 12.788 3.527 0.43 235520. 0.1949 44.94 0.4394 0.6525 0.0206 0.0138 0.455 4.775 2.475 338.981 0.540 11.010 3.312 0.43 235852. 0.1698 46.90 0.4585 0.6309 0.0172 0.0125 0.410 4.312 2.071 306.069 0.487 9.211 3.069 0.43 236196. 0.1440 48.85 0.4776 0.5959 0.0138 0.0111 0.363 3.818 1.663 271.021 0.431 7.396 2.783 0.43 236551. 0.1170 50.80 0.4967 0.5407 0.0104 0.0095 0.314 3.294 1.252 233.859 0.372 5.568 2.428 0.43 236917. 0.0885 52.76 0.5159 0.4521 0.0070 0.0079 0.261 2.742 0.839 194.617 0.310 3.731 1.955 0.43 237294. 0.0584 54.71 0.5350 0.3014 0.0035 0.0063 0.206 2.160 0.425 153.326 0.244 1.889 1.257 0.43 237681. 0.0267 56.67 0.5541 0.0033 0.0000 0.0045 0.146 1.539 0.003 109.220 0.174 0.014 0.013 0.44 238028. 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 0.0809 0.0244 1.274 11.469 13.259 949.839 1.296 58.975 6.331 0.50 269262. 0.7515 2.28 0.0191 0.0617 0.0792 0.0246 1.281 11.531 12.983 954.962 1.303 57.747 6.166 0.50 269404. 0.7243 4.57 0.0383 0.1202 0.0774 0.0247 1.286 11.578 12.691 958.876 1.308 56.452 6.003 0.50 269555. 0.6972 6.85 0.0574 0.1755 0.0756 0.0247 1.289 11.609 12.386 961.422 1.312 55.091 5.843 0.50 269715. 0.6703 9.13 0.0765 0.2276 0.0736 0.0247 1.291 11.621 12.064 962.445 1.313 53.663 5.686 0.50 269884. 0.6438 11.42 0.0957 0.2768 0.0715 0.0247 1.290 11.613 11.728 961.790 1.312 52.166 5.531 0.50 270063. 0.6174 13.70 0.1148 0.3230 0.0694 0.0247 1.286 11.583 11.376 959.313 1.309 50.601 5.379 0.50 270251. 0.5914 15.98 0.1339 0.3664 0.0672 0.0246 1.281 11.530 11.009 954.886 1.303 48.969 5.229 0.50 270449. 0.5656 18.27 0.1531 0.4070 0.0648 0.0244 1.272 11.451 10.628 948.389 1.294 47.271 5.083 0.50 270658. 0.5401 20.55 0.1722 0.4449 0.0624 0.0242 1.260 11.347 10.231 939.704 1.282 45.509 4.938 0.50 270877. 0.5149 22.83 0.1913 0.4801 0.0599 0.0239 1.245 11.214 9.821 928.721 1.267 43.683 4.796 0.50 271106. 0.4900 25.11 0.2105 0.5127 0.0573 0.0235 1.227 11.052 9.397 915.325 1.249 41.796 4.656 0.50 271347. 0.4653 27.40 0.2296 0.5427 0.0547 0.0231 1.206 10.860 8.959 899.408 1.227 39.850 4.518 0.50 271599. 0.4408 29.68 0.2488 0.5701 0.0519 0.0226 1.181 10.636 8.509 880.859 1.202 37.846 4.381 0.50 271863. 0.4166 31.96 0.2679 0.5949 0.0491 0.0221 1.153 10.379 8.046 859.572 1.173 35.786 4.245 0.50 272138. 0.3925 34.25 0.2870 0.6171 0.0462 0.0215 1.120 10.088 7.570 835.441 1.140 33.673 4.110 0.50 272425. 0.3686 36.53 0.3062 0.6365 0.0432 0.0208 1.084 9.761 7.084 808.364 1.103 31.508 3.975 0.50 272725. 0.3448 38.81 0.3253 0.6531 0.0402 0.0200 1.044 9.397 6.586 778.245 1.062 29.294 3.838 0.50 273036. 0.3211 41.10 0.3444 0.6666 0.0371 0.0192 0.999 8.995 6.077 744.991 1.016 27.032 3.700 0.50 273360. 0.2973 43.38 0.3636 0.6768 0.0339 0.0182 0.950 8.555 5.559 708.522 0.967 24.727 3.559 0.50 273697. 0.2735 45.66 0.3827 0.6831 0.0307 0.0172 0.897 8.075 5.031 668.759 0.912 22.379 3.412 0.50 274046. 0.2495 47.95 0.4018 0.6849 0.0274 0.0161 0.839 7.554 4.495 625.641 0.853 19.992 3.259 0.50 274409. 0.2252 50.23 0.4210 0.6813 0.0241 0.0149 0.777 6.993 3.950 579.116 0.790 17.570 3.094 0.50 274785. 0.2004 52.51 0.4401 0.6706 0.0207 0.0136 0.710 6.389 3.398 529.152 0.722 15.117 2.913 0.50 275174. 0.1751 54.80 0.4592 0.6506 0.0173 0.0122 0.638 5.744 2.841 475.730 0.649 12.635 2.708 0.51 275576. 0.1488 57.08 0.4784 0.6171 0.0139 0.0108 0.562 5.058 2.278 418.859 0.571 10.130 2.466 0.51 275991. 0.1213 59.36 0.4975 0.5630 0.0104 0.0092 0.481 4.330 1.710 358.573 0.489 7.608 2.164 0.51 276420. 0.0922 61.64 0.5166 0.4741 0.0070 0.0076 0.396 3.561 1.141 294.927 0.402 5.074 1.754 0.51 276862. 0.0611 63.93 0.5358 0.3174 0.0035 0.0059 0.306 2.753 0.569 227.972 0.311 2.532 1.133 0.51 277314. 0.0279 66.21 0.5549 -0.0156 -0.0001 0.0040 0.209 1.880 -0.018 155.694 0.212 -0.082 -0.054 0.51 277681. 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 0.0820 0.0246 1.918 15.109 17.561 1430.094 1.707 78.111 5.570 0.57 307702. 0.7608 2.61 0.0191 0.0621 0.0803 0.0248 1.928 15.190 17.196 1437.730 1.716 76.489 5.425 0.57 307865. 0.7333 5.22 0.0383 0.1209 0.0785 0.0249 1.936 15.251 16.812 1443.510 1.723 74.778 5.282 0.57 308039. 0.7060 7.83 0.0574 0.1766 0.0766 0.0249 1.941 15.290 16.407 1447.191 1.727 72.980 5.142 0.57 308224. 0.6790 10.44 0.0766 0.2291 0.0747 0.0250 1.943 15.304 15.983 1448.536 1.729 71.092 5.005 0.57 308418. 0.6522 13.05 0.0957 0.2787 0.0726 0.0249 1.941 15.291 15.538 1447.311 1.728 69.114 4.869 0.57 308624. 0.6257 15.66 0.1149 0.3253 0.0704 0.0249 1.935 15.249 15.073 1443.293 1.723 67.044 4.737 0.57 308840. 0.5995 18.27 0.1340 0.3691 0.0681 0.0247 1.926 15.175 14.587 1436.289 1.714 64.885 4.607 0.57 309068. 0.5735 20.89 0.1532 0.4101 0.0658 0.0246 1.912 15.067 14.082 1426.115 1.702 62.638 4.479 0.57 309308. 0.5479 23.50 0.1723 0.4484 0.0633 0.0243 1.894 14.925 13.558 1412.600 1.686 60.304 4.353 0.57 309560. 0.5225 26.11 0.1914 0.4841 0.0608 0.0240 1.871 14.745 13.014 1395.576 1.666 57.888 4.230 0.57 309824. 0.4974 28.72 0.2106 0.5172 0.0582 0.0237 1.844 14.526 12.453 1374.875 1.641 55.389 4.108 0.57 310101. 0.4726 31.33 0.2297 0.5477 0.0555 0.0233 1.811 14.267 11.873 1350.332 1.612 52.812 3.988 0.57 310390. 0.4480 33.94 0.2489 0.5757 0.0527 0.0228 1.773 13.965 11.277 1321.785 1.578 50.158 3.870 0.57 310693. 0.4236 36.55 0.2680 0.6012 0.0498 0.0222 1.729 13.619 10.663 1289.071 1.539 47.430 3.752 0.57 311009. 0.3994 39.16 0.2872 0.6240 0.0469 0.0216 1.679 13.228 10.034 1252.033 1.495 44.631 3.635 0.57 311338. 0.3753 41.77 0.3063 0.6442 0.0439 0.0209 1.623 12.789 9.389 1210.518 1.445 41.763 3.518 0.57 311681. 0.3514 44.38 0.3255 0.6616 0.0408 0.0201 1.561 12.302 8.730 1164.383 1.390 38.829 3.401 0.57 312039. 0.3275 46.99 0.3446 0.6760 0.0376 0.0192 1.493 11.764 8.056 1113.489 1.329 35.833 3.282 0.57 312410. 0.3036 49.60 0.3637 0.6872 0.0344 0.0182 1.418 11.175 7.369 1057.711 1.263 32.778 3.160 0.58 312796. 0.2796 52.21 0.3829 0.6946 0.0312 0.0172 1.337 10.533 6.670 996.935 1.190 29.666 3.034 0.58 313197. 0.2555 54.82 0.4020 0.6976 0.0278 0.0160 1.249 9.837 5.958 931.067 1.111 26.503 2.903 0.58 313612. 0.2310 57.43 0.4212 0.6954 0.0245 0.0148 1.153 9.086 5.237 860.029 1.027 23.293 2.762 0.58 314042. 0.2060 60.04 0.4403 0.6863 0.0210 0.0135 1.051 8.281 4.505 783.770 0.936 20.040 2.607 0.58 314488. 0.1804 62.66 0.4595 0.6681 0.0176 0.0121 0.942 7.420 3.766 702.267 0.838 16.750 2.432 0.58 314948. 0.1539 65.27 0.4786 0.6365 0.0141 0.0106 0.825 6.503 3.019 615.530 0.735 13.429 2.225 0.58 315424. 0.1260 67.88 0.4978 0.5843 0.0106 0.0090 0.702 5.532 2.267 523.611 0.625 10.083 1.964 0.58 315914. 0.0964 70.49 0.5169 0.4965 0.0071 0.0073 0.572 4.507 1.511 426.598 0.509 6.722 1.607 0.58 316420. 0.0644 73.10 0.5361 0.3374 0.0035 0.0056 0.435 3.429 0.753 324.566 0.387 3.351 1.053 0.58 316937. 0.0298 75.71 0.5552 -0.0226 -0.0001 0.0037 0.286 2.257 -0.032 213.603 0.255 -0.142 -0.068 0.58 317322. 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 0.0834 0.0250 2.772 19.410 22.599 2066.817 2.193 100.521 4.959 0.64 346127. 0.7685 2.94 0.0192 0.0622 0.0817 0.0251 2.786 19.512 22.132 2077.622 2.204 98.441 4.832 0.64 346313. 0.7409 5.88 0.0383 0.1212 0.0799 0.0252 2.797 19.587 21.639 2085.683 2.213 96.248 4.706 0.64 346511. 0.7136 8.82 0.0575 0.1771 0.0779 0.0253 2.804 19.634 21.120 2090.656 2.218 93.942 4.582 0.64 346720. 0.6864 11.75 0.0766 0.2298 0.0759 0.0253 2.806 19.649 20.575 2092.199 2.220 91.519 4.461 0.64 346941. 0.6596 14.69 0.0958 0.2796 0.0738 0.0253 2.803 19.628 20.004 2089.968 2.218 88.978 4.341 0.64 347174. 0.6330 17.63 0.1149 0.3265 0.0716 0.0252 2.794 19.568 19.406 2083.636 2.211 86.320 4.224 0.64 347420. 0.6066 20.57 0.1341 0.3706 0.0693 0.0251 2.780 19.468 18.783 2072.922 2.199 83.545 4.110 0.64 347678. 0.5806 23.51 0.1532 0.4119 0.0669 0.0249 2.759 19.323 18.133 2057.566 2.183 80.656 3.997 0.64 347950. 0.5549 26.45 0.1724 0.4506 0.0644 0.0246 2.732 19.133 17.459 2037.322 2.162 77.656 3.887 0.64 348235. 0.5294 29.38 0.1915 0.4867 0.0618 0.0243 2.698 18.895 16.760 2011.951 2.135 74.548 3.778 0.64 348534. 0.5042 32.32 0.2107 0.5203 0.0592 0.0240 2.657 18.606 16.037 1981.219 2.102 71.334 3.671 0.64 348848. 0.4793 35.26 0.2298 0.5513 0.0564 0.0235 2.608 18.265 15.292 1944.890 2.064 68.018 3.566 0.64 349175. 0.4546 38.20 0.2490 0.5798 0.0536 0.0230 2.552 17.869 14.524 1902.734 2.019 64.603 3.462 0.64 349518. 0.4301 41.14 0.2682 0.6058 0.0507 0.0224 2.487 17.416 13.735 1854.518 1.968 61.093 3.359 0.64 349875. 0.4058 44.08 0.2873 0.6293 0.0477 0.0218 2.414 16.905 12.925 1800.018 1.910 57.490 3.257 0.65 350247. 0.3817 47.01 0.3065 0.6502 0.0446 0.0210 2.332 16.332 12.095 1739.020 1.845 53.799 3.155 0.65 350635. 0.3576 49.95 0.3256 0.6684 0.0415 0.0202 2.241 15.696 11.246 1671.315 1.773 50.022 3.052 0.65 351039. 0.3336 52.89 0.3448 0.6836 0.0383 0.0193 2.141 14.995 10.379 1596.705 1.694 46.164 2.948 0.65 351458. 0.3096 55.83 0.3639 0.6957 0.0350 0.0183 2.032 14.228 9.494 1515.012 1.607 42.230 2.842 0.65 351894. 0.2855 58.77 0.3831 0.7042 0.0317 0.0173 1.912 13.393 8.593 1426.075 1.513 38.223 2.733 0.65 352346. 0.2612 61.71 0.4022 0.7084 0.0283 0.0161 1.783 12.488 7.678 1329.754 1.411 34.150 2.619 0.65 352814. 0.2365 64.64 0.4214 0.7075 0.0249 0.0148 1.644 11.513 6.748 1225.939 1.301 30.014 2.497 0.65 353300. 0.2114 67.58 0.4405 0.7000 0.0214 0.0135 1.495 10.467 5.805 1114.556 1.183 25.823 2.363 0.65 353802. 0.1856 70.52 0.4597 0.6834 0.0179 0.0120 1.335 9.350 4.852 995.573 1.056 21.583 2.211 0.65 354321. 0.1587 73.46 0.4788 0.6539 0.0144 0.0105 1.165 8.161 3.890 869.006 0.922 17.303 2.030 0.65 354857. 0.1305 76.40 0.4980 0.6037 0.0108 0.0089 0.986 6.902 2.921 734.931 0.780 12.990 1.802 0.65 355410. 0.1004 79.34 0.5172 0.5173 0.0072 0.0072 0.796 5.574 1.946 593.477 0.630 8.657 1.487 0.65 355979. 0.0676 82.28 0.5363 0.3564 0.0036 0.0054 0.596 4.177 0.969 444.753 0.472 4.310 0.988 0.65 356562. 0.0317 85.21 0.5555 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 0.0851 0.0256 3.888 24.505 28.461 2899.274 2.769 126.596 4.453 0.71 384535. 0.7743 3.27 0.0192 0.0621 0.0833 0.0257 3.907 24.625 27.876 2913.471 2.782 123.992 4.340 0.71 384744. 0.7469 6.53 0.0383 0.1211 0.0815 0.0258 3.921 24.713 27.258 2923.854 2.792 121.244 4.228 0.71 384966. 0.7196 9.80 0.0575 0.1769 0.0795 0.0258 3.929 24.764 26.608 2929.921 2.798 118.352 4.119 0.71 385201. 0.6926 13.07 0.0766 0.2298 0.0775 0.0259 3.931 24.775 25.924 2931.169 2.799 115.312 4.012 0.71 385449. 0.6658 16.33 0.0958 0.2797 0.0753 0.0258 3.925 24.740 25.207 2927.083 2.795 112.123 3.906 0.71 385711. 0.6393 19.60 0.1150 0.3267 0.0731 0.0257 3.912 24.657 24.457 2917.201 2.786 108.783 3.803 0.71 385986. 0.6130 22.86 0.1341 0.3710 0.0708 0.0256 3.890 24.521 23.673 2901.101 2.770 105.296 3.701 0.71 386276. 0.5870 26.13 0.1533 0.4126 0.0683 0.0254 3.860 24.329 22.856 2878.427 2.749 101.663 3.602 0.71 386581. 0.5613 29.40 0.1725 0.4516 0.0658 0.0251 3.820 24.079 22.007 2848.841 2.720 97.889 3.504 0.72 386901. 0.5358 32.66 0.1916 0.4880 0.0632 0.0248 3.771 23.768 21.128 2812.019 2.685 93.977 3.408 0.72 387236. 0.5106 35.93 0.2108 0.5219 0.0604 0.0244 3.711 23.393 20.219 2767.646 2.643 89.932 3.313 0.72 387586. 0.4857 39.20 0.2299 0.5534 0.0576 0.0239 3.641 22.951 19.280 2715.398 2.593 85.758 3.220 0.72 387953. 0.4610 42.46 0.2491 0.5824 0.0547 0.0234 3.560 22.440 18.313 2654.959 2.535 81.458 3.129 0.72 388336. 0.4364 45.73 0.2683 0.6090 0.0518 0.0228 3.468 21.858 17.320 2586.021 2.469 77.038 3.038 0.72 388735. 0.4121 48.99 0.2874 0.6331 0.0487 0.0221 3.364 21.200 16.299 2508.267 2.395 72.500 2.947 0.72 389151. 0.3879 52.26 0.3066 0.6546 0.0456 0.0214 3.247 20.466 15.254 2421.405 2.312 67.850 2.857 0.72 389584. 0.3638 55.53 0.3258 0.6736 0.0424 0.0205 3.118 19.653 14.184 2325.142 2.220 63.092 2.767 0.72 390035. 0.3397 58.79 0.3449 0.6897 0.0391 0.0196 2.976 18.757 13.092 2219.211 2.119 58.231 2.676 0.72 390503. 0.3156 62.06 0.3641 0.7027 0.0358 0.0186 2.821 17.778 11.977 2103.365 2.009 53.273 2.583 0.72 390989. 0.2914 65.33 0.3832 0.7122 0.0324 0.0174 2.652 16.713 10.841 1977.378 1.888 48.223 2.487 0.72 391493. 0.2669 68.59 0.4024 0.7176 0.0290 0.0162 2.469 15.561 9.687 1841.061 1.758 43.087 2.386 0.72 392015. 0.2421 71.86 0.4216 0.7181 0.0255 0.0149 2.272 14.320 8.514 1694.274 1.618 37.872 2.279 0.72 392556. 0.2168 75.13 0.4407 0.7120 0.0219 0.0136 2.061 12.991 7.326 1536.941 1.468 32.586 2.162 0.72 393115. 0.1908 78.39 0.4599 0.6972 0.0183 0.0121 1.836 11.572 6.123 1369.059 1.307 27.237 2.029 0.72 393693. 0.1636 81.66 0.4791 0.6694 0.0147 0.0105 1.597 10.064 4.909 1190.714 1.137 21.836 1.870 0.72 394290. 0.1351 84.92 0.4982 0.6211 0.0110 0.0088 1.344 8.470 3.686 1002.101 0.957 16.393 1.668 0.72 394905. 0.1044 88.19 0.5174 0.5359 0.0073 0.0071 1.078 6.792 2.455 803.523 0.767 10.922 1.386 0.72 395539. 0.0708 91.46 0.5365 0.3731 0.0037 0.0052 0.798 5.031 1.221 595.283 0.568 5.432 0.931 0.72 396187. 0.0335 94.72 0.5557 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 0.0871 0.0268 5.414 31.024 35.269 4037.569 3.505 156.876 3.962 0.79 422917. 0.7670 3.59 0.0192 0.0610 0.0854 0.0268 5.427 31.098 34.550 4047.168 3.513 153.677 3.872 0.79 423151. 0.7419 7.19 0.0383 0.1192 0.0835 0.0268 5.434 31.136 33.790 4052.085 3.518 150.298 3.782 0.79 423398. 0.7167 10.78 0.0575 0.1745 0.0815 0.0268 5.433 31.133 32.990 4051.711 3.517 146.738 3.693 0.79 423660. 0.6915 14.37 0.0767 0.2271 0.0794 0.0268 5.425 31.084 32.148 4045.413 3.512 142.994 3.604 0.79 423936. 0.6662 17.97 0.0958 0.2770 0.0772 0.0267 5.408 30.985 31.264 4032.505 3.501 139.063 3.517 0.79 424228. 0.6410 21.56 0.1150 0.3242 0.0749 0.0266 5.381 30.830 30.338 4012.333 3.483 134.943 3.430 0.79 424534. 0.6158 25.16 0.1342 0.3687 0.0726 0.0264 5.343 30.615 29.370 3984.300 3.459 130.637 3.343 0.79 424857. 0.5907 28.75 0.1533 0.4107 0.0701 0.0262 5.294 30.335 28.360 3947.849 3.427 126.147 3.258 0.79 425196. 0.5656 32.34 0.1725 0.4501 0.0675 0.0259 5.233 29.986 27.311 3902.501 3.388 121.480 3.174 0.79 425551. 0.5408 35.94 0.1917 0.4870 0.0648 0.0255 5.160 29.566 26.223 3847.769 3.340 116.640 3.091 0.79 425923. 0.5160 39.53 0.2108 0.5214 0.0620 0.0251 5.073 29.069 25.097 3783.173 3.284 111.634 3.009 0.79 426312. 0.4914 43.12 0.2300 0.5535 0.0591 0.0246 4.973 28.493 23.935 3708.227 3.219 106.465 2.928 0.79 426718. 0.4669 46.72 0.2492 0.5831 0.0562 0.0240 4.858 27.834 22.738 3622.442 3.145 101.140 2.847 0.79 427142. 0.4426 50.31 0.2683 0.6103 0.0531 0.0234 4.728 27.088 21.507 3525.337 3.060 95.664 2.767 0.79 427585. 0.4183 53.90 0.2875 0.6351 0.0500 0.0226 4.582 26.252 20.243 3416.463 2.966 90.042 2.687 0.79 428045. 0.3942 57.50 0.3067 0.6574 0.0468 0.0218 4.419 25.322 18.948 3295.441 2.861 84.279 2.608 0.79 428525. 0.3700 61.09 0.3258 0.6770 0.0435 0.0210 4.240 24.295 17.622 3161.842 2.745 78.382 2.528 0.79 429023. 0.3459 64.69 0.3450 0.6939 0.0402 0.0200 4.044 23.170 16.267 3015.353 2.618 72.356 2.447 0.79 429540. 0.3217 68.28 0.3642 0.7076 0.0368 0.0189 3.830 21.943 14.885 2855.745 2.479 66.207 2.364 0.79 430077. 0.2973 71.87 0.3833 0.7179 0.0333 0.0178 3.598 20.615 13.476 2682.853 2.329 59.942 2.278 0.79 430634. 0.2726 75.47 0.4025 0.7238 0.0298 0.0165 3.348 19.184 12.043 2496.675 2.167 53.569 2.188 0.79 431210. 0.2475 79.06 0.4217 0.7246 0.0262 0.0152 3.081 17.652 10.588 2297.224 1.994 47.096 2.091 0.79 431807. 0.2217 82.65 0.4408 0.7184 0.0225 0.0138 2.796 16.018 9.112 2084.688 1.810 40.531 1.983 0.79 432424. 0.1951 86.25 0.4600 0.7027 0.0188 0.0123 2.494 14.287 7.618 1859.404 1.614 33.886 1.858 0.79 433061. 0.1672 89.84 0.4791 0.6729 0.0151 0.0107 2.175 12.462 6.109 1621.846 1.408 27.173 1.708 0.79 433719. 0.1377 93.43 0.4983 0.6209 0.0113 0.0091 1.841 10.547 4.587 1372.674 1.192 20.404 1.516 0.80 434397. 0.1058 97.03 0.5175 0.5300 0.0076 0.0074 1.492 8.550 3.056 1112.717 0.966 13.595 1.246 0.80 435095. 0.0710 100.62 0.5366 0.3607 0.0038 0.0056 1.130 6.476 1.520 842.788 0.732 6.759 0.818 0.80 435808. 0.0329 104.21 0.5558 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 0.0896 0.0300 7.872 41.346 43.145 5869.999 4.671 191.909 3.334 0.86 461265. 0.7138 3.93 0.0192 0.0564 0.0878 0.0298 7.841 41.186 42.279 5847.280 4.653 188.058 3.280 0.86 461524. 0.6951 7.85 0.0384 0.1110 0.0859 0.0297 7.803 40.982 41.362 5818.392 4.630 183.979 3.224 0.86 461799. 0.6760 11.78 0.0576 0.1636 0.0839 0.0295 7.755 40.731 40.394 5782.797 4.602 179.674 3.168 0.86 462089. 0.6564 15.70 0.0768 0.2142 0.0817 0.0293 7.697 40.429 39.374 5739.917 4.568 175.137 3.111 0.86 462396. 0.6364 19.63 0.0960 0.2628 0.0795 0.0290 7.629 40.072 38.302 5689.135 4.527 170.366 3.054 0.86 462719. 0.6161 23.56 0.1152 0.3093 0.0772 0.0287 7.550 39.654 37.176 5629.819 4.480 165.359 2.995 0.86 463059. 0.5953 27.48 0.1344 0.3537 0.0747 0.0284 7.458 39.172 35.998 5561.389 4.426 160.118 2.936 0.86 463416. 0.5742 31.41 0.1535 0.3960 0.0722 0.0280 7.353 38.622 34.768 5483.330 4.363 154.649 2.876 0.86 463791. 0.5528 35.33 0.1727 0.4361 0.0695 0.0275 7.235 38.001 33.489 5395.113 4.293 148.959 2.815 0.86 464184. 0.5311 39.26 0.1919 0.4740 0.0668 0.0270 7.102 37.304 32.161 5296.177 4.215 143.053 2.754 0.86 464595. 0.5092 43.18 0.2111 0.5098 0.0639 0.0265 6.954 36.527 30.787 5185.912 4.127 136.939 2.693 0.86 465025. 0.4870 47.11 0.2303 0.5433 0.0610 0.0258 6.790 35.666 29.366 5063.645 4.030 130.621 2.630 0.86 465474. 0.4647 51.04 0.2495 0.5745 0.0579 0.0252 6.610 34.716 27.902 4928.767 3.922 124.108 2.568 0.86 465942. 0.4421 54.96 0.2687 0.6034 0.0548 0.0244 6.411 33.673 26.395 4780.660 3.804 117.406 2.504 0.86 466429. 0.4194 58.89 0.2879 0.6299 0.0516 0.0236 6.194 32.532 24.848 4618.710 3.675 110.522 2.440 0.86 466937. 0.3965 62.81 0.3071 0.6539 0.0483 0.0227 5.958 31.293 23.261 4442.861 3.536 103.464 2.375 0.86 467465. 0.3733 66.74 0.3263 0.6747 0.0449 0.0217 5.707 29.976 21.636 4255.876 3.387 96.237 2.306 0.86 468013. 0.3496 70.67 0.3455 0.6914 0.0415 0.0207 5.444 28.593 19.975 4059.477 3.230 88.847 2.232 0.86 468582. 0.3251 74.59 0.3647 0.7038 0.0379 0.0197 5.166 27.131 18.278 3851.941 3.065 81.303 2.152 0.86 469173. 0.3000 78.52 0.3839 0.7117 0.0344 0.0185 4.868 25.570 16.550 3630.328 2.889 73.613 2.068 0.86 469784. 0.2742 82.44 0.4031 0.7143 0.0307 0.0173 4.552 23.910 14.790 3394.580 2.701 65.788 1.976 0.86 470417. 0.2478 86.37 0.4223 0.7098 0.0270 0.0161 4.219 22.159 13.003 3145.937 2.503 57.836 1.875 0.86 471072. 0.2204 90.30 0.4414 0.6964 0.0232 0.0147 3.869 20.319 11.189 2884.749 2.296 49.769 1.759 0.87 471749. 0.1918 94.22 0.4606 0.6708 0.0194 0.0133 3.503 18.399 9.353 2612.160 2.079 41.600 1.624 0.87 472447. 0.1619 98.15 0.4798 0.6280 0.0156 0.0119 3.124 16.408 7.497 2329.565 1.854 33.345 1.460 0.87 473168. 0.1303 102.07 0.4990 0.5601 0.0117 0.0104 2.733 14.357 5.625 2038.295 1.622 25.019 1.252 0.87 473911. 0.0968 106.00 0.5182 0.4533 0.0078 0.0089 2.333 12.256 3.742 1740.065 1.385 16.644 0.975 0.87 474675. 0.0615 109.92 0.5374 0.2818 0.0038 0.0073 1.926 10.116 1.852 1436.273 1.143 8.236 0.585 0.87 475456. 0.0259 113.85 0.5566 -0.0270 -0.0003 0.0056 1.472 7.733 -0.131 1097.930 0.874 -0.583 -0.054 0.87 475971. 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 0.0916 0.0363 12.129 58.805 51.772 9044.577 6.644 230.284 2.596 0.93 499608. 0.6090 4.28 0.0193 0.0482 0.0898 0.0360 12.027 58.312 50.794 8968.737 6.588 225.933 2.569 0.93 499890. 0.5968 8.55 0.0386 0.0953 0.0880 0.0356 11.908 57.734 49.749 8879.787 6.523 221.284 2.541 0.93 500190. 0.5843 12.83 0.0579 0.1414 0.0860 0.0352 11.771 57.069 48.637 8777.538 6.448 216.337 2.513 0.93 500507. 0.5714 17.11 0.0772 0.1864 0.0839 0.0348 11.616 56.316 47.456 8661.752 6.363 211.085 2.485 0.93 500843. 0.5580 21.38 0.0965 0.2302 0.0817 0.0343 11.442 55.474 46.206 8532.181 6.267 205.523 2.456 0.93 501198. 0.5443 25.66 0.1158 0.2730 0.0794 0.0337 11.249 54.541 44.885 8388.643 6.162 199.650 2.427 0.93 501572. 0.5300 29.93 0.1351 0.3145 0.0769 0.0330 11.038 53.517 43.496 8231.177 6.046 193.469 2.397 0.93 501965. 0.5153 34.21 0.1544 0.3548 0.0744 0.0324 10.809 52.403 42.039 8059.905 5.920 186.988 2.366 0.93 502378. 0.5000 38.49 0.1737 0.3937 0.0717 0.0316 10.560 51.201 40.517 7874.935 5.785 180.218 2.334 0.93 502811. 0.4842 42.76 0.1930 0.4313 0.0689 0.0308 10.294 49.908 38.931 7676.191 5.639 173.166 2.300 0.93 503265. 0.4679 47.04 0.2123 0.4673 0.0659 0.0300 10.009 48.525 37.285 7463.438 5.482 165.842 2.266 0.93 503739. 0.4510 51.32 0.2316 0.5017 0.0629 0.0290 9.704 47.049 35.579 7236.319 5.316 158.255 2.230 0.93 504234. 0.4336 55.59 0.2509 0.5344 0.0598 0.0281 9.380 45.477 33.816 6994.566 5.138 150.415 2.193 0.93 504750. 0.4157 59.87 0.2702 0.5654 0.0566 0.0270 9.036 43.808 31.999 6737.930 4.949 142.332 2.154 0.93 505288. 0.3972 64.15 0.2895 0.5943 0.0533 0.0260 8.671 42.041 30.130 6466.163 4.750 134.017 2.113 0.93 505848. 0.3782 68.42 0.3088 0.6212 0.0499 0.0248 8.286 40.173 28.211 6178.854 4.539 125.482 2.071 0.93 506429. 0.3586 72.70 0.3281 0.6457 0.0464 0.0236 7.880 38.203 26.245 5875.890 4.316 116.736 2.026 0.93 507033. 0.3383 76.98 0.3474 0.6653 0.0429 0.0224 7.476 36.245 24.231 5574.702 4.095 107.781 1.972 0.93 507660. 0.3164 81.25 0.3667 0.6747 0.0392 0.0213 7.119 34.515 22.168 5308.562 3.899 98.605 1.894 0.93 508309. 0.2907 85.53 0.3860 0.6746 0.0355 0.0203 6.783 32.884 20.061 5057.747 3.715 89.233 1.799 0.94 508981. 0.2627 89.80 0.4053 0.6665 0.0317 0.0193 6.437 31.207 17.916 4799.852 3.526 79.692 1.693 0.94 509677. 0.2336 94.08 0.4246 0.6493 0.0278 0.0182 6.080 29.478 15.737 4533.813 3.330 69.998 1.574 0.94 510396. 0.2036 98.36 0.4439 0.6206 0.0239 0.0171 5.717 27.718 13.527 4263.219 3.132 60.169 1.439 0.94 511138. 0.1725 102.63 0.4632 0.5777 0.0200 0.0160 5.349 25.935 11.292 3988.883 2.930 50.226 1.284 0.94 511905. 0.1406 106.91 0.4825 0.5174 0.0160 0.0149 4.979 24.138 9.036 3712.590 2.727 40.192 1.104 0.94 512695. 0.1082 111.19 0.5018 0.4353 0.0120 0.0138 4.609 22.347 6.767 3437.086 2.525 30.098 0.893 0.94 513509. 0.0757 115.46 0.5211 0.3260 0.0079 0.0127 4.242 20.567 4.492 3163.389 2.324 19.979 0.644 0.94 514346. 0.0445 119.74 0.5404 0.1826 0.0039 0.0116 3.878 18.801 2.218 2891.749 2.124 9.864 0.348 0.94 515203. 0.0169 124.02 0.5597 -0.0113 -0.0002 0.0104 3.471 16.828 -0.119 2588.265 1.901 -0.529 -0.021 0.94 515973. 0.0000