26x13E (26x13E.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 0.0824 0.0283 0.027 1.707 1.199 20.195 0.193 5.335 26.938 0.10 61851. 0.6658 0.55 0.0223 0.0630 0.0810 0.0286 0.027 1.726 1.179 20.415 0.195 5.245 26.199 0.10 61887. 0.6421 1.10 0.0446 0.1225 0.0795 0.0289 0.028 1.743 1.158 20.618 0.197 5.149 25.466 0.10 61926. 0.6183 1.65 0.0669 0.1786 0.0779 0.0292 0.028 1.758 1.134 20.797 0.199 5.046 24.740 0.10 61968. 0.5947 2.20 0.0892 0.2312 0.0762 0.0294 0.028 1.771 1.110 20.948 0.200 4.935 24.024 0.10 62013. 0.5711 2.74 0.1114 0.2805 0.0744 0.0295 0.028 1.781 1.083 21.067 0.201 4.818 23.319 0.10 62061. 0.5477 3.29 0.1337 0.3266 0.0724 0.0297 0.028 1.787 1.055 21.148 0.202 4.692 22.624 0.10 62113. 0.5244 3.84 0.1560 0.3695 0.0704 0.0297 0.028 1.791 1.025 21.186 0.202 4.558 21.940 0.10 62169. 0.5012 4.39 0.1783 0.4093 0.0682 0.0297 0.028 1.790 0.993 21.177 0.202 4.417 21.267 0.10 62228. 0.4783 4.94 0.2006 0.4461 0.0659 0.0296 0.028 1.785 0.959 21.114 0.202 4.266 20.604 0.10 62290. 0.4554 5.49 0.2229 0.4800 0.0634 0.0294 0.028 1.774 0.923 20.994 0.200 4.108 19.951 0.10 62357. 0.4327 6.04 0.2452 0.5109 0.0608 0.0292 0.028 1.759 0.886 20.811 0.199 3.940 19.306 0.10 62427. 0.4101 6.59 0.2675 0.5389 0.0581 0.0288 0.028 1.738 0.846 20.558 0.196 3.764 18.668 0.10 62502. 0.3875 7.13 0.2897 0.5640 0.0552 0.0284 0.027 1.710 0.804 20.233 0.193 3.578 18.034 0.10 62580. 0.3650 7.68 0.3120 0.5861 0.0523 0.0278 0.027 1.677 0.761 19.836 0.189 3.385 17.402 0.10 62662. 0.3426 8.23 0.3343 0.6051 0.0492 0.0272 0.026 1.637 0.716 19.366 0.185 3.184 16.768 0.10 62749. 0.3202 8.78 0.3566 0.6208 0.0460 0.0264 0.025 1.591 0.669 18.823 0.180 2.977 16.128 0.10 62839. 0.2978 9.33 0.3789 0.6330 0.0427 0.0255 0.024 1.539 0.621 18.208 0.174 2.764 15.477 0.10 62934. 0.2753 9.88 0.4012 0.6413 0.0393 0.0246 0.023 1.481 0.572 17.522 0.167 2.545 14.810 0.10 63033. 0.2528 10.43 0.4235 0.6453 0.0358 0.0235 0.022 1.417 0.522 16.765 0.160 2.321 14.118 0.10 63136. 0.2302 10.98 0.4458 0.6444 0.0323 0.0224 0.021 1.347 0.471 15.939 0.152 2.093 13.392 0.10 63244. 0.2073 11.52 0.4681 0.6376 0.0287 0.0211 0.020 1.272 0.419 15.044 0.144 1.862 12.621 0.10 63355. 0.1843 12.07 0.4903 0.6239 0.0251 0.0198 0.019 1.190 0.366 14.082 0.134 1.628 11.789 0.10 63471. 0.1610 12.62 0.5126 0.6016 0.0215 0.0183 0.018 1.104 0.313 13.056 0.125 1.392 10.872 0.10 63591. 0.1373 13.17 0.5349 0.5682 0.0178 0.0168 0.016 1.012 0.260 11.970 0.114 1.155 9.841 0.10 63716. 0.1132 13.72 0.5572 0.5202 0.0142 0.0152 0.015 0.915 0.206 10.827 0.103 0.918 8.650 0.10 63845. 0.0887 14.27 0.5795 0.4520 0.0105 0.0135 0.013 0.814 0.153 9.632 0.092 0.683 7.227 0.10 63979. 0.0639 14.82 0.6018 0.3545 0.0069 0.0118 0.011 0.709 0.101 8.391 0.080 0.449 5.458 0.11 64116. 0.0391 15.37 0.6241 0.2117 0.0034 0.0100 0.010 0.601 0.049 7.112 0.068 0.219 3.143 0.11 64258. 0.0157 15.91 0.6464 -0.0080 -0.0001 0.0081 0.008 0.490 -0.001 5.798 0.055 -0.006 -0.114 0.11 64402. 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 0.0828 0.0266 0.204 6.422 4.823 151.952 0.726 21.454 14.397 0.21 123698. 0.7136 1.10 0.0223 0.0674 0.0814 0.0270 0.206 6.502 4.743 153.855 0.735 21.095 13.981 0.21 123771. 0.6871 2.20 0.0447 0.1309 0.0799 0.0273 0.209 6.576 4.656 155.610 0.743 20.709 13.571 0.21 123849. 0.6608 3.30 0.0670 0.1905 0.0783 0.0276 0.211 6.643 4.563 157.178 0.750 20.295 13.167 0.21 123933. 0.6347 4.40 0.0893 0.2463 0.0766 0.0278 0.213 6.699 4.463 158.521 0.757 19.853 12.771 0.21 124024. 0.6089 5.50 0.1117 0.2985 0.0748 0.0280 0.214 6.745 4.357 159.598 0.762 19.379 12.382 0.21 124122. 0.5833 6.60 0.1340 0.3472 0.0728 0.0281 0.215 6.777 4.243 160.368 0.766 18.875 12.002 0.21 124226. 0.5580 7.70 0.1564 0.3926 0.0708 0.0282 0.216 6.795 4.123 160.788 0.768 18.338 11.630 0.21 124337. 0.5329 8.80 0.1787 0.4346 0.0686 0.0282 0.216 6.796 3.995 160.817 0.768 17.768 11.267 0.21 124456. 0.5082 9.90 0.2010 0.4735 0.0662 0.0281 0.215 6.779 3.859 160.410 0.766 17.164 10.911 0.21 124582. 0.4837 11.00 0.2234 0.5094 0.0638 0.0280 0.214 6.742 3.715 159.524 0.762 16.526 10.564 0.21 124715. 0.4595 12.10 0.2457 0.5423 0.0612 0.0277 0.212 6.682 3.564 158.113 0.755 15.851 10.223 0.21 124857. 0.4355 13.20 0.2680 0.5722 0.0584 0.0274 0.209 6.598 3.404 156.129 0.745 15.141 9.889 0.21 125006. 0.4117 14.30 0.2904 0.5993 0.0556 0.0269 0.206 6.489 3.236 153.544 0.733 14.395 9.560 0.21 125163. 0.3881 15.40 0.3127 0.6235 0.0526 0.0264 0.202 6.354 3.061 150.351 0.718 13.617 9.235 0.21 125329. 0.3647 16.50 0.3351 0.6447 0.0494 0.0257 0.197 6.193 2.880 146.547 0.700 12.809 8.913 0.21 125503. 0.3413 17.60 0.3574 0.6628 0.0462 0.0249 0.191 6.007 2.692 142.131 0.679 11.974 8.591 0.21 125685. 0.3181 18.70 0.3797 0.6777 0.0429 0.0240 0.184 5.794 2.499 137.104 0.655 11.115 8.267 0.21 125875. 0.2949 19.80 0.4021 0.6890 0.0395 0.0230 0.176 5.556 2.301 131.469 0.628 10.234 7.938 0.21 126074. 0.2717 20.90 0.4244 0.6963 0.0360 0.0220 0.168 5.292 2.098 125.230 0.598 9.334 7.600 0.21 126281. 0.2485 22.00 0.4467 0.6992 0.0325 0.0208 0.159 5.004 1.892 118.396 0.565 8.417 7.250 0.21 126496. 0.2251 23.10 0.4691 0.6967 0.0289 0.0195 0.149 4.690 1.683 110.976 0.530 7.487 6.880 0.21 126721. 0.2014 24.20 0.4914 0.6877 0.0253 0.0181 0.138 4.352 1.472 102.986 0.492 6.547 6.482 0.21 126954. 0.1775 25.30 0.5138 0.6705 0.0216 0.0166 0.127 3.991 1.259 94.447 0.451 5.599 6.045 0.21 127195. 0.1531 26.40 0.5361 0.6425 0.0179 0.0150 0.115 3.609 1.045 85.386 0.408 4.648 5.551 0.21 127446. 0.1281 27.50 0.5584 0.5994 0.0143 0.0133 0.102 3.205 0.831 75.838 0.362 3.698 4.972 0.21 127705. 0.1023 28.60 0.5808 0.5345 0.0106 0.0115 0.088 2.783 0.619 65.847 0.314 2.753 4.263 0.21 127973. 0.0757 29.70 0.6031 0.4351 0.0070 0.0097 0.074 2.344 0.409 55.465 0.265 1.818 3.341 0.21 128249. 0.0482 30.80 0.6254 0.2761 0.0035 0.0078 0.060 1.891 0.202 44.757 0.214 0.897 2.045 0.21 128534. 0.0207 31.90 0.6478 -0.0027 0.0000 0.0059 0.045 1.426 -0.001 33.735 0.161 -0.006 -0.019 0.21 128821. 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 0.0834 0.0261 0.673 14.144 10.933 502.025 1.598 48.631 9.878 0.31 185539. 0.7371 1.65 0.0224 0.0694 0.0820 0.0264 0.682 14.332 10.751 508.687 1.619 47.821 9.586 0.31 185648. 0.7094 3.30 0.0447 0.1347 0.0805 0.0267 0.690 14.505 10.556 514.844 1.639 46.951 9.299 0.31 185767. 0.6818 4.96 0.0671 0.1959 0.0789 0.0270 0.698 14.661 10.346 520.360 1.656 46.017 9.018 0.31 185894. 0.6546 6.61 0.0895 0.2533 0.0772 0.0273 0.704 14.794 10.121 525.103 1.671 45.017 8.742 0.31 186031. 0.6276 8.26 0.1118 0.3068 0.0754 0.0275 0.709 14.902 9.880 528.932 1.684 43.947 8.473 0.31 186177. 0.6010 9.91 0.1342 0.3568 0.0734 0.0276 0.713 14.980 9.624 531.704 1.692 42.806 8.210 0.31 186334. 0.5748 11.56 0.1566 0.4032 0.0713 0.0277 0.715 15.024 9.351 533.271 1.697 41.591 7.953 0.31 186502. 0.5488 13.22 0.1789 0.4463 0.0691 0.0277 0.715 15.030 9.060 533.484 1.698 40.300 7.703 0.31 186680. 0.5233 14.87 0.2013 0.4862 0.0668 0.0276 0.714 14.994 8.753 532.195 1.694 38.932 7.460 0.31 186870. 0.4981 16.52 0.2237 0.5231 0.0643 0.0275 0.710 14.911 8.427 529.250 1.685 37.484 7.222 0.31 187071. 0.4731 18.17 0.2460 0.5569 0.0617 0.0272 0.703 14.777 8.083 524.488 1.669 35.955 6.990 0.31 187284. 0.4485 19.83 0.2684 0.5879 0.0589 0.0269 0.694 14.587 7.721 517.743 1.648 34.342 6.764 0.31 187509. 0.4242 21.48 0.2908 0.6160 0.0560 0.0264 0.682 14.338 7.340 508.917 1.620 32.650 6.542 0.31 187746. 0.4000 23.13 0.3131 0.6412 0.0530 0.0259 0.668 14.030 6.943 497.974 1.585 30.883 6.324 0.31 187995. 0.3761 24.78 0.3355 0.6637 0.0498 0.0252 0.650 13.662 6.531 484.904 1.543 29.049 6.109 0.31 188257. 0.3523 26.43 0.3579 0.6831 0.0466 0.0244 0.630 13.233 6.105 469.701 1.495 27.153 5.895 0.31 188531. 0.3287 28.09 0.3802 0.6995 0.0432 0.0235 0.607 12.745 5.666 452.367 1.440 25.202 5.681 0.31 188817. 0.3052 29.74 0.4026 0.7125 0.0398 0.0225 0.581 12.197 5.216 432.908 1.378 23.201 5.465 0.31 189116. 0.2817 31.39 0.4250 0.7217 0.0363 0.0214 0.552 11.589 4.756 411.338 1.309 21.156 5.245 0.31 189428. 0.2581 33.04 0.4473 0.7268 0.0327 0.0201 0.520 10.923 4.288 387.682 1.234 19.075 5.017 0.31 189753. 0.2345 34.69 0.4697 0.7268 0.0291 0.0188 0.485 10.198 3.813 361.977 1.152 16.962 4.778 0.31 190090. 0.2106 36.35 0.4921 0.7207 0.0254 0.0174 0.448 9.418 3.333 334.275 1.064 14.827 4.523 0.31 190440. 0.1864 38.00 0.5144 0.7067 0.0217 0.0158 0.409 8.583 2.850 304.650 0.970 12.675 4.243 0.31 190804. 0.1616 39.65 0.5368 0.6823 0.0180 0.0142 0.366 7.697 2.364 273.197 0.870 10.516 3.925 0.31 191180. 0.1362 41.30 0.5592 0.6430 0.0143 0.0125 0.322 6.763 1.879 240.040 0.764 8.359 3.551 0.31 191570. 0.1099 42.95 0.5815 0.5812 0.0107 0.0107 0.275 5.785 1.397 205.333 0.654 6.214 3.086 0.31 191973. 0.0823 44.61 0.6039 0.4822 0.0070 0.0088 0.227 4.769 0.920 169.267 0.539 4.093 2.466 0.32 192389. 0.0534 46.26 0.6263 0.3143 0.0034 0.0069 0.177 3.721 0.451 132.064 0.420 2.007 1.550 0.32 192817. 0.0235 47.91 0.6486 -0.0103 -0.0001 0.0049 0.126 2.640 -0.010 93.698 0.298 -0.045 -0.049 0.32 193244. 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 0.0843 0.0260 1.589 25.032 19.636 1184.631 2.828 87.343 7.518 0.41 247370. 0.7519 2.20 0.0224 0.0704 0.0829 0.0263 1.610 25.375 19.313 1200.853 2.867 85.904 7.295 0.41 247516. 0.7235 4.40 0.0447 0.1366 0.0814 0.0266 1.630 25.692 18.964 1215.853 2.903 84.354 7.075 0.41 247674. 0.6953 6.61 0.0671 0.1987 0.0798 0.0269 1.649 25.976 18.590 1229.303 2.935 82.689 6.859 0.41 247845. 0.6674 8.81 0.0894 0.2567 0.0781 0.0272 1.664 26.221 18.189 1240.881 2.962 80.905 6.649 0.41 248028. 0.6399 11.01 0.1118 0.3110 0.0762 0.0274 1.677 26.419 17.760 1250.252 2.985 78.996 6.443 0.41 248224. 0.6128 13.21 0.1342 0.3616 0.0743 0.0275 1.686 26.562 17.302 1257.060 3.001 76.957 6.243 0.41 248434. 0.5860 15.41 0.1565 0.4087 0.0722 0.0276 1.691 26.645 16.813 1260.952 3.010 74.784 6.048 0.41 248658. 0.5596 17.62 0.1789 0.4524 0.0699 0.0276 1.692 26.658 16.294 1261.565 3.012 72.474 5.858 0.41 248897. 0.5336 19.82 0.2012 0.4929 0.0676 0.0276 1.688 26.594 15.743 1258.539 3.005 70.024 5.674 0.41 249151. 0.5080 22.02 0.2236 0.5304 0.0651 0.0274 1.678 26.445 15.160 1251.505 2.988 67.430 5.494 0.41 249420. 0.4828 24.22 0.2460 0.5649 0.0624 0.0272 1.663 26.203 14.543 1240.072 2.960 64.689 5.319 0.41 249704. 0.4578 26.43 0.2683 0.5965 0.0596 0.0268 1.641 25.860 13.893 1223.840 2.922 61.797 5.149 0.41 250005. 0.4331 28.63 0.2907 0.6253 0.0567 0.0264 1.613 25.411 13.210 1202.556 2.871 58.760 4.983 0.41 250321. 0.4087 30.83 0.3130 0.6514 0.0536 0.0258 1.577 24.852 12.497 1176.127 2.808 55.588 4.820 0.41 250654. 0.3845 33.03 0.3354 0.6747 0.0505 0.0251 1.535 24.184 11.757 1144.521 2.732 52.293 4.659 0.41 251003. 0.3605 35.23 0.3578 0.6951 0.0472 0.0243 1.485 23.407 10.991 1107.726 2.645 48.886 4.500 0.42 251369. 0.3367 37.44 0.3801 0.7126 0.0438 0.0234 1.429 22.520 10.202 1065.742 2.544 45.378 4.342 0.42 251751. 0.3130 39.64 0.4025 0.7268 0.0403 0.0223 1.366 21.523 9.393 1018.581 2.432 41.780 4.183 0.42 252150. 0.2893 41.84 0.4248 0.7376 0.0368 0.0212 1.296 20.418 8.566 966.278 2.307 38.103 4.021 0.42 252566. 0.2656 44.04 0.4472 0.7443 0.0332 0.0199 1.219 19.205 7.725 908.890 2.170 34.359 3.855 0.42 252999. 0.2418 46.24 0.4696 0.7463 0.0295 0.0186 1.135 17.887 6.870 846.505 2.021 30.558 3.681 0.42 253449. 0.2177 48.45 0.4919 0.7425 0.0258 0.0171 1.045 16.466 6.006 779.253 1.860 26.715 3.496 0.42 253916. 0.1934 50.65 0.5143 0.7312 0.0220 0.0155 0.949 14.946 5.136 707.308 1.689 22.843 3.293 0.42 254401. 0.1684 52.85 0.5366 0.7099 0.0183 0.0138 0.846 13.331 4.262 630.905 1.506 18.957 3.064 0.42 254903. 0.1427 55.05 0.5590 0.6741 0.0145 0.0121 0.738 11.629 3.389 550.344 1.314 15.074 2.793 0.42 255422. 0.1160 57.25 0.5814 0.6159 0.0108 0.0102 0.625 9.847 2.521 466.006 1.113 11.213 2.454 0.42 255959. 0.0879 59.46 0.6037 0.5195 0.0071 0.0083 0.507 7.995 1.662 378.360 0.903 7.395 1.993 0.42 256513. 0.0580 61.66 0.6261 0.3485 0.0035 0.0063 0.386 6.085 0.818 287.949 0.687 3.640 1.289 0.42 257084. 0.0263 63.86 0.6484 -0.0083 -0.0001 0.0043 0.261 4.113 -0.013 194.635 0.465 -0.057 -0.030 0.42 257650. 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 0.0854 0.0261 3.124 39.375 31.100 2329.248 4.449 138.332 6.056 0.52 309186. 0.7622 2.77 0.0225 0.0713 0.0840 0.0265 3.167 39.928 30.591 2361.972 4.511 136.069 5.874 0.52 309371. 0.7333 5.54 0.0450 0.1383 0.0825 0.0268 3.208 40.439 30.042 2392.204 4.569 133.627 5.696 0.52 309571. 0.7046 8.31 0.0675 0.2010 0.0809 0.0271 3.244 40.897 29.452 2419.278 4.620 131.001 5.522 0.52 309786. 0.6763 11.07 0.0900 0.2598 0.0792 0.0274 3.275 41.290 28.817 2442.530 4.665 128.179 5.351 0.52 310018. 0.6483 13.84 0.1124 0.3147 0.0773 0.0276 3.301 41.607 28.138 2461.271 4.701 125.156 5.185 0.52 310266. 0.6207 16.61 0.1349 0.3658 0.0753 0.0278 3.319 41.835 27.411 2474.784 4.726 121.922 5.024 0.52 310532. 0.5936 19.38 0.1574 0.4134 0.0732 0.0279 3.329 41.963 26.635 2482.337 4.741 118.471 4.867 0.52 310816. 0.5668 22.15 0.1799 0.4577 0.0709 0.0279 3.330 41.977 25.809 2483.198 4.743 114.797 4.714 0.52 311118. 0.5405 24.92 0.2024 0.4987 0.0685 0.0278 3.321 41.866 24.931 2476.631 4.730 110.895 4.566 0.52 311440. 0.5145 27.68 0.2249 0.5367 0.0659 0.0276 3.301 41.617 24.002 2461.888 4.702 106.760 4.422 0.52 311780. 0.4889 30.45 0.2474 0.5717 0.0632 0.0274 3.270 41.216 23.019 2438.184 4.657 102.386 4.282 0.52 312140. 0.4636 33.22 0.2699 0.6038 0.0604 0.0270 3.225 40.650 21.980 2404.701 4.593 97.769 4.146 0.52 312521. 0.4387 35.99 0.2923 0.6332 0.0574 0.0265 3.166 39.910 20.889 2360.929 4.509 92.915 4.013 0.52 312922. 0.4139 38.76 0.3148 0.6598 0.0542 0.0259 3.093 38.993 19.749 2306.683 4.405 87.844 3.883 0.52 313343. 0.3895 41.53 0.3373 0.6837 0.0510 0.0252 3.006 37.898 18.564 2241.901 4.282 82.573 3.756 0.52 313785. 0.3652 44.29 0.3598 0.7048 0.0476 0.0243 2.905 36.625 17.338 2166.559 4.138 77.120 3.630 0.52 314247. 0.3411 47.06 0.3823 0.7230 0.0442 0.0233 2.790 35.173 16.076 2080.663 3.974 71.505 3.504 0.52 314731. 0.3171 49.83 0.4048 0.7381 0.0406 0.0223 2.661 33.543 14.781 1984.247 3.790 65.745 3.379 0.52 315236. 0.2931 52.60 0.4273 0.7497 0.0370 0.0211 2.518 31.736 13.457 1877.380 3.586 59.857 3.251 0.52 315762. 0.2692 55.37 0.4498 0.7574 0.0333 0.0198 2.360 29.755 12.109 1760.190 3.362 53.860 3.120 0.52 316309. 0.2450 58.14 0.4722 0.7604 0.0295 0.0183 2.190 27.603 10.741 1632.866 3.119 47.774 2.983 0.52 316878. 0.2207 60.90 0.4947 0.7576 0.0257 0.0168 2.006 25.284 9.357 1495.682 2.857 41.620 2.838 0.52 317469. 0.1959 63.67 0.5172 0.7474 0.0219 0.0151 1.809 22.804 7.963 1349.011 2.576 35.421 2.677 0.52 318081. 0.1705 66.44 0.5397 0.7268 0.0180 0.0134 1.600 20.173 6.565 1193.351 2.279 29.202 2.495 0.52 318715. 0.1443 69.21 0.5622 0.6910 0.0142 0.0115 1.380 17.401 5.169 1029.343 1.966 22.991 2.278 0.52 319372. 0.1169 71.98 0.5847 0.6309 0.0104 0.0096 1.150 14.501 3.781 857.800 1.638 16.819 1.999 0.52 320050. 0.0877 74.75 0.6072 0.5270 0.0066 0.0076 0.912 11.490 2.410 679.717 1.298 10.720 1.608 0.53 320751. 0.0563 77.51 0.6297 0.3304 0.0029 0.0056 0.665 8.389 1.064 496.229 0.948 4.731 0.972 0.53 321471. 0.0226 80.28 0.6521 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 0.0869 0.0266 5.487 57.638 45.573 4091.532 6.512 202.707 5.052 0.62 370980. 0.7697 3.29 0.0223 0.0708 0.0855 0.0269 5.564 58.453 44.847 4149.428 6.604 199.480 4.902 0.62 371202. 0.7409 6.59 0.0446 0.1374 0.0840 0.0273 5.636 59.207 44.063 4202.917 6.689 195.993 4.755 0.62 371441. 0.7124 9.88 0.0669 0.1998 0.0824 0.0276 5.700 59.882 43.218 4250.831 6.765 192.235 4.611 0.62 371699. 0.6842 13.18 0.0892 0.2583 0.0807 0.0279 5.756 60.462 42.310 4292.018 6.831 188.194 4.471 0.62 371976. 0.6564 16.47 0.1115 0.3131 0.0788 0.0281 5.800 60.930 41.335 4325.265 6.884 183.857 4.335 0.62 372273. 0.6289 19.77 0.1338 0.3642 0.0769 0.0282 5.833 61.269 40.290 4349.328 6.922 179.212 4.202 0.62 372591. 0.6019 23.06 0.1561 0.4118 0.0747 0.0283 5.851 61.461 39.175 4362.932 6.944 174.249 4.073 0.62 372930. 0.5753 26.36 0.1784 0.4562 0.0725 0.0283 5.853 61.487 37.985 4364.803 6.947 168.959 3.947 0.62 373290. 0.5490 29.65 0.2007 0.4974 0.0700 0.0283 5.838 61.330 36.721 4353.665 6.929 163.336 3.826 0.62 373673. 0.5232 32.95 0.2230 0.5356 0.0675 0.0281 5.804 60.972 35.380 4328.238 6.889 157.371 3.708 0.62 374079. 0.4977 36.24 0.2453 0.5709 0.0648 0.0278 5.749 60.394 33.961 4287.186 6.823 151.058 3.593 0.62 374508. 0.4725 39.54 0.2677 0.6035 0.0619 0.0275 5.671 59.575 32.461 4229.084 6.731 144.388 3.481 0.62 374960. 0.4476 42.83 0.2900 0.6334 0.0589 0.0270 5.569 58.503 30.883 4152.933 6.610 137.368 3.373 0.62 375437. 0.4230 46.13 0.3123 0.6607 0.0558 0.0264 5.442 57.170 29.232 4058.343 6.459 130.022 3.267 0.62 375937. 0.3986 49.42 0.3346 0.6854 0.0525 0.0256 5.291 55.576 27.513 3945.209 6.279 122.378 3.163 0.62 376462. 0.3744 52.72 0.3569 0.7074 0.0491 0.0248 5.114 53.721 25.734 3813.495 6.069 114.464 3.061 0.62 377012. 0.3504 56.01 0.3792 0.7267 0.0456 0.0238 4.912 51.604 23.899 3663.214 5.830 106.305 2.959 0.62 377586. 0.3265 59.31 0.4015 0.7430 0.0420 0.0227 4.686 49.226 22.016 3494.426 5.562 97.926 2.858 0.62 378184. 0.3026 62.60 0.4238 0.7561 0.0383 0.0215 4.435 46.590 20.089 3307.257 5.264 89.355 2.755 0.62 378808. 0.2787 65.90 0.4461 0.7656 0.0346 0.0201 4.160 43.697 18.124 3101.913 4.937 80.617 2.650 0.63 379457. 0.2546 69.19 0.4684 0.7709 0.0308 0.0187 3.860 40.553 16.129 2878.714 4.582 71.742 2.541 0.63 380131. 0.2303 72.49 0.4907 0.7709 0.0269 0.0171 3.538 37.163 14.109 2638.113 4.199 62.758 2.426 0.63 380830. 0.2056 75.78 0.5130 0.7642 0.0230 0.0155 3.193 33.538 12.073 2380.733 3.789 53.699 2.300 0.63 381555. 0.1804 79.08 0.5353 0.7482 0.0191 0.0137 2.826 29.687 10.027 2107.408 3.354 44.601 2.158 0.63 382306. 0.1542 82.37 0.5576 0.7187 0.0152 0.0118 2.440 25.627 7.982 1819.213 2.895 35.503 1.990 0.63 383083. 0.1269 85.67 0.5799 0.6675 0.0113 0.0099 2.035 21.377 5.947 1517.517 2.415 26.451 1.777 0.63 383885. 0.0978 88.96 0.6022 0.5779 0.0075 0.0078 1.615 16.961 3.933 1204.015 1.916 17.494 1.482 0.63 384713. 0.0663 92.26 0.6245 0.4067 0.0037 0.0057 1.181 12.406 1.952 880.693 1.402 8.684 1.005 0.63 385566. 0.0317 95.55 0.6468 0.0003 0.0000 0.0036 0.733 7.705 0.001 546.968 0.871 0.004 0.001 0.63 386409. 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 0.0889 0.0273 8.964 80.710 63.427 6684.254 9.119 282.123 4.304 0.72 432744. 0.7736 3.84 0.0223 0.0703 0.0875 0.0277 9.088 81.827 62.447 6776.778 9.245 277.766 4.180 0.72 433004. 0.7454 7.68 0.0446 0.1366 0.0860 0.0281 9.203 82.863 61.385 6862.537 9.362 273.039 4.057 0.72 433286. 0.7174 11.52 0.0668 0.1988 0.0844 0.0284 9.306 83.793 60.236 6939.565 9.467 267.930 3.937 0.72 433589. 0.6896 15.36 0.0891 0.2571 0.0827 0.0286 9.395 84.594 58.997 7005.895 9.557 262.417 3.820 0.72 433914. 0.6621 19.20 0.1114 0.3118 0.0808 0.0289 9.467 85.240 57.663 7059.467 9.630 256.485 3.705 0.72 434263. 0.6349 23.03 0.1337 0.3629 0.0788 0.0290 9.519 85.707 56.231 7098.119 9.683 250.115 3.593 0.72 434636. 0.6081 26.87 0.1559 0.4105 0.0767 0.0291 9.548 85.967 54.697 7119.645 9.713 243.292 3.485 0.72 435033. 0.5816 30.71 0.1782 0.4550 0.0744 0.0291 9.551 85.993 53.059 7121.813 9.715 236.005 3.379 0.72 435456. 0.5555 34.55 0.2005 0.4964 0.0719 0.0290 9.525 85.759 51.314 7102.439 9.689 228.243 3.277 0.72 435906. 0.5298 38.39 0.2228 0.5348 0.0693 0.0289 9.467 85.240 49.459 7059.415 9.630 219.995 3.178 0.72 436381. 0.5044 42.23 0.2450 0.5705 0.0666 0.0286 9.375 84.409 47.494 6990.595 9.536 211.253 3.082 0.72 436884. 0.4793 46.07 0.2673 0.6035 0.0636 0.0282 9.245 83.238 45.414 6893.667 9.404 202.003 2.988 0.72 437415. 0.4544 49.91 0.2896 0.6339 0.0606 0.0277 9.075 81.708 43.222 6766.885 9.231 192.252 2.897 0.72 437973. 0.4298 53.75 0.3119 0.6617 0.0574 0.0270 8.864 79.808 40.925 6609.575 9.017 182.033 2.808 0.73 438558. 0.4055 57.59 0.3341 0.6871 0.0540 0.0263 8.611 77.538 38.531 6421.560 8.760 171.386 2.722 0.73 439173. 0.3812 61.43 0.3564 0.7099 0.0505 0.0254 8.318 74.897 36.049 6202.833 8.462 160.348 2.636 0.73 439815. 0.3572 65.27 0.3787 0.7300 0.0469 0.0243 7.984 71.886 33.489 5953.449 8.122 148.957 2.551 0.73 440486. 0.3332 69.10 0.4010 0.7473 0.0432 0.0232 7.608 68.506 30.857 5673.533 7.740 137.250 2.467 0.73 441185. 0.3092 72.94 0.4232 0.7616 0.0395 0.0219 7.192 64.760 28.162 5363.327 7.317 125.263 2.382 0.73 441914. 0.2852 76.78 0.4455 0.7724 0.0356 0.0205 6.736 60.654 25.412 5023.224 6.853 113.033 2.295 0.73 442671. 0.2610 80.62 0.4678 0.7791 0.0317 0.0190 6.241 56.193 22.617 4653.836 6.349 100.600 2.204 0.73 443457. 0.2366 84.46 0.4901 0.7808 0.0277 0.0174 5.707 51.390 19.786 4256.040 5.806 88.007 2.109 0.73 444273. 0.2117 88.30 0.5123 0.7759 0.0237 0.0157 5.137 46.258 16.929 3831.026 5.226 75.299 2.004 0.73 445119. 0.1861 92.14 0.5346 0.7619 0.0197 0.0138 4.533 40.817 14.058 3380.403 4.611 62.528 1.886 0.73 445994. 0.1596 95.98 0.5569 0.7345 0.0157 0.0119 3.897 35.092 11.185 2906.266 3.965 49.749 1.746 0.73 446898. 0.1317 99.82 0.5792 0.6852 0.0117 0.0099 3.234 29.116 8.324 2411.297 3.289 37.026 1.566 0.73 447833. 0.1020 103.66 0.6014 0.5961 0.0077 0.0078 2.546 22.928 5.492 1898.835 2.590 24.428 1.312 0.74 448798. 0.0694 107.50 0.6237 0.4211 0.0038 0.0056 1.841 16.576 2.705 1372.830 1.873 12.031 0.894 0.74 449791. 0.0332 111.34 0.6460 -0.0124 -0.0001 0.0034 1.116 10.045 -0.047 831.871 1.135 -0.207 -0.025 0.74 450763. 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 0.0914 0.0303 14.831 116.844 85.181 11059.220 13.201 378.886 3.494 0.83 494461. 0.7277 4.38 0.0222 0.0656 0.0901 0.0305 14.940 117.708 83.932 11141.017 13.299 373.329 3.417 0.83 494760. 0.7065 8.75 0.0444 0.1282 0.0886 0.0307 15.036 118.458 82.569 11212.013 13.383 367.268 3.340 0.83 495084. 0.6850 13.13 0.0667 0.1879 0.0870 0.0309 15.113 119.070 81.088 11269.917 13.452 360.678 3.263 0.83 495433. 0.6632 17.51 0.0889 0.2446 0.0853 0.0310 15.170 119.519 79.481 11312.432 13.503 353.533 3.187 0.83 495808. 0.6412 21.89 0.1111 0.2984 0.0834 0.0311 15.203 119.780 77.744 11337.102 13.533 345.805 3.110 0.83 496209. 0.6189 26.26 0.1333 0.3494 0.0814 0.0311 15.209 119.825 75.870 11341.336 13.538 337.470 3.034 0.83 496638. 0.5965 30.64 0.1556 0.3974 0.0792 0.0310 15.184 119.625 73.855 11322.451 13.515 328.508 2.959 0.83 497096. 0.5738 35.02 0.1778 0.4427 0.0769 0.0309 15.124 119.152 71.695 11277.624 13.462 318.900 2.883 0.83 497583. 0.5510 39.39 0.2000 0.4851 0.0744 0.0307 15.025 118.373 69.386 11203.950 13.374 308.631 2.809 0.83 498100. 0.5280 43.77 0.2222 0.5249 0.0718 0.0304 14.883 117.258 66.926 11098.419 13.248 297.688 2.735 0.83 498647. 0.5050 48.15 0.2445 0.5619 0.0690 0.0300 14.695 115.772 64.312 10957.783 13.080 286.058 2.662 0.83 499225. 0.4818 52.53 0.2667 0.5963 0.0660 0.0295 14.454 113.877 61.539 10778.405 12.866 273.725 2.590 0.83 499834. 0.4585 56.90 0.2889 0.6282 0.0629 0.0289 14.157 111.539 58.609 10557.090 12.602 260.692 2.518 0.83 500474. 0.4350 61.28 0.3111 0.6574 0.0596 0.0282 13.802 108.740 55.530 10292.196 12.285 246.998 2.447 0.83 501146. 0.4115 65.66 0.3333 0.6841 0.0561 0.0274 13.389 105.483 52.315 9983.903 11.917 232.699 2.377 0.83 501850. 0.3880 70.04 0.3556 0.7079 0.0525 0.0264 12.921 101.796 48.976 9634.946 11.501 217.846 2.306 0.83 502586. 0.3641 74.41 0.3778 0.7287 0.0488 0.0253 12.396 97.661 45.524 9243.577 11.034 202.492 2.234 0.83 503354. 0.3401 78.79 0.4000 0.7464 0.0450 0.0241 11.815 93.081 41.971 8810.094 10.516 186.687 2.161 0.83 504154. 0.3159 83.17 0.4222 0.7605 0.0411 0.0228 11.177 88.061 38.328 8334.889 9.949 170.481 2.086 0.83 504987. 0.2914 87.54 0.4445 0.7705 0.0371 0.0214 10.484 82.599 34.606 7817.956 9.332 153.928 2.008 0.83 505852. 0.2665 91.92 0.4667 0.7757 0.0331 0.0199 9.738 76.721 30.818 7261.563 8.668 137.080 1.925 0.83 506751. 0.2412 96.30 0.4889 0.7746 0.0289 0.0183 8.943 70.458 26.977 6668.836 7.960 119.993 1.835 0.83 507682. 0.2151 100.68 0.5111 0.7650 0.0248 0.0166 8.104 63.851 23.095 6043.438 7.214 102.729 1.733 0.84 508646. 0.1880 105.05 0.5333 0.7437 0.0206 0.0148 7.228 56.944 19.190 5389.726 6.434 85.355 1.615 0.84 509644. 0.1596 109.43 0.5556 0.7053 0.0164 0.0129 6.320 49.795 15.276 4713.040 5.626 67.948 1.470 0.84 510675. 0.1297 113.81 0.5778 0.6403 0.0122 0.0110 5.390 42.469 11.374 4019.671 4.798 50.592 1.283 0.84 511740. 0.0977 118.18 0.6000 0.5318 0.0081 0.0091 4.448 35.042 7.505 3316.669 3.959 33.383 1.026 0.84 512838. 0.0635 122.56 0.6222 0.3446 0.0040 0.0072 3.502 27.594 3.693 2611.755 3.118 16.427 0.641 0.84 513969. 0.0278 126.94 0.6445 -0.0089 -0.0001 0.0052 2.551 20.100 -0.067 1902.441 2.271 -0.299 -0.016 0.84 515090. 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 0.0932 0.0390 27.152 190.147 109.914 20247.016 21.483 488.896 2.462 0.93 556176. 0.5826 4.96 0.0224 0.0528 0.0920 0.0390 27.174 190.302 108.498 20263.432 21.500 482.601 2.429 0.93 556512. 0.5709 9.93 0.0448 0.1042 0.0906 0.0390 27.151 190.145 106.929 20246.719 21.482 475.618 2.395 0.93 556876. 0.5590 14.89 0.0672 0.1542 0.0892 0.0389 27.080 189.644 105.195 20193.422 21.426 467.907 2.363 0.93 557270. 0.5469 19.85 0.0896 0.2029 0.0876 0.0387 26.955 188.771 103.287 20100.490 21.327 459.420 2.331 0.93 557695. 0.5346 24.82 0.1120 0.2501 0.0858 0.0384 26.774 187.503 101.195 19965.385 21.184 450.115 2.299 0.93 558152. 0.5219 29.78 0.1344 0.2960 0.0838 0.0381 26.533 185.817 98.910 19785.941 20.994 439.951 2.267 0.93 558641. 0.5089 34.74 0.1568 0.3406 0.0817 0.0376 26.231 183.699 96.424 19560.422 20.754 428.895 2.236 0.93 559164. 0.4955 39.71 0.1792 0.3837 0.0795 0.0371 25.865 181.135 93.732 19287.354 20.465 416.919 2.204 0.93 559722. 0.4816 44.67 0.2016 0.4254 0.0770 0.0365 25.433 178.112 90.827 18965.475 20.123 403.999 2.172 0.93 560314. 0.4672 49.63 0.2240 0.4655 0.0744 0.0358 24.934 174.618 87.707 18593.482 19.728 390.120 2.140 0.93 560941. 0.4522 54.60 0.2464 0.5041 0.0715 0.0350 24.366 170.640 84.367 18169.803 19.279 375.264 2.106 0.93 561604. 0.4366 59.56 0.2688 0.5409 0.0685 0.0340 23.725 166.153 80.803 17692.061 18.772 359.411 2.072 0.93 562303. 0.4202 64.52 0.2912 0.5759 0.0653 0.0330 23.009 161.137 77.014 17158.020 18.205 342.560 2.036 0.93 563039. 0.4032 69.49 0.3136 0.6089 0.0619 0.0319 22.218 155.593 73.014 16567.594 17.579 324.768 1.999 0.93 563810. 0.3855 74.45 0.3360 0.6399 0.0583 0.0306 21.352 149.531 68.820 15922.142 16.894 306.113 1.960 0.93 564619. 0.3670 79.41 0.3584 0.6685 0.0546 0.0293 20.414 142.965 64.451 15223.050 16.152 286.676 1.920 0.93 565464. 0.3479 84.38 0.3808 0.6932 0.0508 0.0279 19.446 136.187 59.918 14501.239 15.386 266.517 1.874 0.93 566345. 0.3274 89.34 0.4032 0.7130 0.0468 0.0265 18.458 129.264 55.240 13764.064 14.604 245.709 1.820 0.94 567263. 0.3053 94.30 0.4256 0.7266 0.0428 0.0250 17.454 122.236 50.433 13015.795 13.810 224.326 1.757 0.94 568218. 0.2817 99.27 0.4480 0.7285 0.0386 0.0237 16.533 115.781 45.503 12328.380 13.081 202.398 1.674 0.94 569209. 0.2549 104.23 0.4704 0.7207 0.0343 0.0224 15.611 109.323 40.479 11640.765 12.351 180.049 1.577 0.94 570238. 0.2265 109.19 0.4928 0.7030 0.0300 0.0210 14.656 102.641 35.385 10929.256 11.596 157.391 1.468 0.94 571304. 0.1971 114.16 0.5152 0.6729 0.0256 0.0196 13.682 95.816 30.243 10202.553 10.825 134.521 1.345 0.94 572407. 0.1669 119.12 0.5376 0.6272 0.0213 0.0182 12.702 88.952 25.081 9471.695 10.050 111.559 1.201 0.94 573548. 0.1357 124.08 0.5600 0.5622 0.0169 0.0168 11.727 82.127 19.926 8744.888 9.279 88.633 1.034 0.94 574726. 0.1041 129.05 0.5824 0.4733 0.0126 0.0155 10.769 75.418 14.813 8030.556 8.521 65.887 0.837 0.94 575943. 0.0727 134.01 0.6048 0.3551 0.0083 0.0141 9.839 68.904 9.776 7336.946 7.785 43.484 0.604 0.95 577199. 0.0426 138.97 0.6272 0.2011 0.0041 0.0128 8.944 62.638 4.853 6669.728 7.077 21.587 0.330 0.95 578493. 0.0164 143.94 0.6496 0.0006 0.0000 0.0115 8.043 56.329 0.013 5997.897 6.364 0.057 0.001 0.95 579830. 0.0000