20x10 (20x10.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 0.0773 0.0298 0.008 0.483 0.394 5.718 0.055 1.753 31.261 0.08 31293. 0.5758 0.45 0.0235 0.0594 0.0761 0.0302 0.008 0.490 0.388 5.798 0.055 1.727 30.376 0.08 31311. 0.5553 0.89 0.0471 0.1153 0.0749 0.0306 0.008 0.496 0.382 5.872 0.056 1.698 29.496 0.08 31331. 0.5347 1.34 0.0706 0.1678 0.0735 0.0309 0.008 0.502 0.375 5.940 0.057 1.667 28.623 0.08 31352. 0.5141 1.78 0.0941 0.2170 0.0720 0.0312 0.008 0.507 0.367 5.999 0.057 1.633 27.759 0.08 31375. 0.4935 2.23 0.1177 0.2629 0.0704 0.0315 0.008 0.511 0.359 6.049 0.058 1.596 26.907 0.08 31401. 0.4729 2.67 0.1412 0.3056 0.0686 0.0317 0.008 0.514 0.350 6.087 0.058 1.556 26.066 0.08 31428. 0.4523 3.12 0.1647 0.3452 0.0667 0.0318 0.008 0.517 0.340 6.112 0.058 1.513 25.237 0.08 31457. 0.4318 3.57 0.1883 0.3817 0.0646 0.0319 0.008 0.517 0.330 6.122 0.058 1.466 24.420 0.08 31488. 0.4113 4.01 0.2118 0.4153 0.0625 0.0319 0.008 0.517 0.318 6.117 0.058 1.417 23.616 0.08 31522. 0.3910 4.46 0.2353 0.4459 0.0601 0.0317 0.008 0.515 0.307 6.094 0.058 1.364 22.822 0.08 31558. 0.3708 4.90 0.2589 0.4736 0.0577 0.0315 0.008 0.512 0.294 6.055 0.058 1.308 22.037 0.08 31596. 0.3507 5.35 0.2824 0.4984 0.0551 0.0312 0.008 0.507 0.281 5.997 0.057 1.250 21.259 0.08 31636. 0.3307 5.79 0.3059 0.5203 0.0524 0.0308 0.008 0.500 0.267 5.921 0.057 1.190 20.486 0.08 31678. 0.3108 6.24 0.3295 0.5393 0.0497 0.0303 0.008 0.492 0.253 5.826 0.056 1.126 19.714 0.08 31723. 0.2910 6.69 0.3530 0.5551 0.0468 0.0297 0.008 0.483 0.239 5.712 0.055 1.061 18.940 0.08 31770. 0.2714 7.13 0.3765 0.5678 0.0438 0.0290 0.007 0.471 0.223 5.578 0.053 0.993 18.161 0.08 31820. 0.2518 7.58 0.4000 0.5770 0.0407 0.0282 0.007 0.458 0.208 5.424 0.052 0.924 17.371 0.08 31872. 0.2323 8.02 0.4236 0.5825 0.0376 0.0273 0.007 0.444 0.192 5.250 0.050 0.853 16.563 0.08 31926. 0.2128 8.47 0.4471 0.5840 0.0344 0.0263 0.007 0.427 0.175 5.056 0.048 0.780 15.731 0.08 31983. 0.1933 8.91 0.4706 0.5809 0.0311 0.0252 0.006 0.409 0.159 4.841 0.046 0.706 14.865 0.08 32042. 0.1737 9.36 0.4942 0.5724 0.0278 0.0240 0.006 0.389 0.142 4.605 0.044 0.630 13.951 0.08 32104. 0.1540 9.81 0.5177 0.5576 0.0244 0.0226 0.006 0.368 0.124 4.349 0.042 0.553 12.972 0.08 32168. 0.1342 10.25 0.5412 0.5351 0.0210 0.0212 0.005 0.344 0.107 4.071 0.039 0.475 11.907 0.08 32235. 0.1142 10.70 0.5648 0.5027 0.0175 0.0197 0.005 0.319 0.089 3.773 0.036 0.397 10.721 0.08 32304. 0.0939 11.14 0.5883 0.4576 0.0140 0.0180 0.005 0.292 0.071 3.455 0.033 0.317 9.367 0.08 32376. 0.0734 11.59 0.6118 0.3950 0.0105 0.0162 0.004 0.264 0.053 3.118 0.030 0.238 7.775 0.08 32450. 0.0527 12.03 0.6354 0.3076 0.0070 0.0144 0.004 0.233 0.036 2.761 0.026 0.158 5.831 0.08 32526. 0.0322 12.48 0.6589 0.1828 0.0034 0.0124 0.003 0.202 0.018 2.387 0.023 0.078 3.341 0.08 32605. 0.0130 12.92 0.6824 -0.0045 -0.0001 0.0104 0.003 0.169 0.000 1.994 0.019 -0.002 -0.080 0.08 32684. 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 0.0265 0.055 1.722 1.584 40.755 0.195 7.047 17.632 0.16 62585. 0.6511 0.90 0.0236 0.0671 0.0765 0.0270 0.056 1.752 1.561 41.450 0.198 6.943 17.082 0.16 62621. 0.6261 1.79 0.0473 0.1299 0.0753 0.0274 0.056 1.780 1.535 42.107 0.201 6.829 16.539 0.16 62661. 0.6012 2.69 0.0709 0.1886 0.0739 0.0278 0.057 1.805 1.507 42.714 0.204 6.704 16.005 0.16 62704. 0.5765 3.58 0.0946 0.2432 0.0724 0.0282 0.058 1.828 1.477 43.256 0.207 6.568 15.483 0.16 62751. 0.5520 4.48 0.1182 0.2940 0.0708 0.0285 0.059 1.848 1.443 43.720 0.209 6.419 14.972 0.16 62802. 0.5277 5.37 0.1419 0.3410 0.0690 0.0287 0.059 1.863 1.407 44.091 0.211 6.258 14.473 0.16 62857. 0.5037 6.27 0.1655 0.3845 0.0671 0.0289 0.059 1.874 1.368 44.354 0.212 6.084 13.987 0.16 62916. 0.4799 7.17 0.1892 0.4245 0.0650 0.0290 0.060 1.881 1.326 44.498 0.212 5.897 13.514 0.16 62979. 0.4565 8.06 0.2128 0.4613 0.0628 0.0290 0.060 1.881 1.281 44.512 0.213 5.697 13.052 0.16 63046. 0.4334 8.96 0.2365 0.4949 0.0605 0.0289 0.060 1.876 1.233 44.388 0.212 5.486 12.602 0.16 63118. 0.4106 9.85 0.2601 0.5254 0.0580 0.0287 0.059 1.864 1.183 44.118 0.211 5.262 12.162 0.16 63195. 0.3881 10.75 0.2838 0.5529 0.0554 0.0284 0.059 1.847 1.130 43.698 0.209 5.028 11.732 0.16 63276. 0.3659 11.64 0.3074 0.5774 0.0527 0.0281 0.058 1.822 1.075 43.122 0.206 4.783 11.310 0.16 63362. 0.3441 12.54 0.3311 0.5989 0.0499 0.0276 0.057 1.791 1.018 42.386 0.202 4.528 10.894 0.16 63452. 0.3225 13.44 0.3547 0.6174 0.0470 0.0270 0.056 1.753 0.959 41.486 0.198 4.264 10.482 0.16 63547. 0.3011 14.33 0.3784 0.6329 0.0440 0.0263 0.054 1.708 0.898 40.418 0.193 3.992 10.073 0.16 63647. 0.2800 15.23 0.4020 0.6451 0.0409 0.0255 0.053 1.656 0.835 39.180 0.187 3.713 9.663 0.16 63752. 0.2590 16.12 0.4257 0.6538 0.0378 0.0246 0.051 1.596 0.770 37.769 0.180 3.426 9.250 0.16 63862. 0.2382 17.02 0.4493 0.6588 0.0345 0.0236 0.049 1.529 0.704 36.181 0.173 3.133 8.829 0.16 63976. 0.2174 17.92 0.4730 0.6594 0.0312 0.0224 0.046 1.454 0.637 34.416 0.164 2.834 8.396 0.16 64096. 0.1966 18.81 0.4966 0.6550 0.0279 0.0211 0.044 1.372 0.569 32.471 0.155 2.529 7.943 0.16 64221. 0.1757 19.71 0.5203 0.6446 0.0245 0.0198 0.041 1.282 0.499 30.346 0.145 2.220 7.461 0.16 64350. 0.1547 20.60 0.5439 0.6265 0.0210 0.0183 0.038 1.185 0.429 28.042 0.134 1.908 6.937 0.16 64485. 0.1333 21.50 0.5676 0.5984 0.0175 0.0166 0.034 1.080 0.358 25.560 0.122 1.592 6.349 0.16 64624. 0.1114 22.39 0.5912 0.5565 0.0140 0.0149 0.031 0.968 0.286 22.904 0.109 1.273 5.669 0.16 64769. 0.0890 23.29 0.6148 0.4945 0.0105 0.0131 0.027 0.849 0.214 20.080 0.096 0.954 4.843 0.16 64919. 0.0658 24.19 0.6385 0.4009 0.0070 0.0111 0.023 0.722 0.143 17.093 0.082 0.634 3.782 0.16 65073. 0.0419 25.08 0.6621 0.2530 0.0035 0.0091 0.019 0.590 0.071 13.952 0.067 0.315 2.301 0.16 65232. 0.0180 25.98 0.6858 -0.0066 -0.0001 0.0069 0.014 0.449 -0.001 10.626 0.051 -0.006 -0.058 0.16 65389. 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 0.0781 0.0253 0.176 3.692 3.583 131.049 0.417 15.938 12.402 0.24 93875. 0.6887 1.35 0.0237 0.0708 0.0769 0.0257 0.179 3.761 3.531 133.497 0.425 15.706 11.997 0.24 93930. 0.6614 2.69 0.0474 0.1370 0.0757 0.0262 0.182 3.827 3.473 135.822 0.432 15.450 11.599 0.24 93990. 0.6342 4.04 0.0711 0.1986 0.0743 0.0266 0.185 3.887 3.410 137.977 0.439 15.169 11.210 0.24 94055. 0.6074 5.39 0.0948 0.2558 0.0728 0.0270 0.188 3.942 3.341 139.915 0.445 14.862 10.831 0.24 94125. 0.5809 6.73 0.1185 0.3089 0.0712 0.0273 0.190 3.989 3.266 141.586 0.451 14.527 10.462 0.24 94202. 0.5547 8.08 0.1422 0.3580 0.0694 0.0276 0.192 4.027 3.184 142.940 0.455 14.163 10.104 0.24 94285. 0.5290 9.43 0.1659 0.4033 0.0675 0.0278 0.193 4.055 3.096 143.926 0.458 13.771 9.756 0.24 94373. 0.5036 10.78 0.1896 0.4450 0.0654 0.0279 0.194 4.071 3.001 144.502 0.460 13.348 9.419 0.24 94469. 0.4787 12.12 0.2133 0.4832 0.0632 0.0279 0.194 4.075 2.899 144.630 0.460 12.897 9.093 0.24 94570. 0.4543 13.47 0.2371 0.5182 0.0608 0.0278 0.193 4.065 2.792 144.281 0.459 12.418 8.776 0.24 94679. 0.4302 14.82 0.2608 0.5501 0.0584 0.0277 0.192 4.041 2.678 143.430 0.457 11.912 8.469 0.24 94794. 0.4066 16.16 0.2845 0.5789 0.0558 0.0274 0.190 4.002 2.559 142.056 0.452 11.381 8.169 0.24 94916. 0.3834 17.51 0.3082 0.6047 0.0530 0.0270 0.188 3.948 2.434 140.142 0.446 10.826 7.877 0.24 95046. 0.3606 18.86 0.3319 0.6276 0.0502 0.0266 0.185 3.879 2.304 137.671 0.438 10.249 7.592 0.24 95182. 0.3381 20.20 0.3556 0.6475 0.0473 0.0260 0.181 3.793 2.170 134.629 0.429 9.652 7.311 0.24 95325. 0.3160 21.55 0.3793 0.6645 0.0443 0.0253 0.176 3.691 2.031 131.004 0.417 9.036 7.033 0.24 95476. 0.2941 22.90 0.4030 0.6784 0.0412 0.0245 0.170 3.572 1.889 126.783 0.404 8.402 6.758 0.24 95634. 0.2725 24.24 0.4267 0.6889 0.0380 0.0235 0.164 3.436 1.743 121.957 0.388 7.752 6.482 0.24 95800. 0.2511 25.59 0.4504 0.6959 0.0347 0.0225 0.156 3.283 1.594 116.514 0.371 7.088 6.203 0.24 95972. 0.2297 26.94 0.4741 0.6989 0.0314 0.0213 0.148 3.112 1.441 110.449 0.352 6.410 5.918 0.24 96153. 0.2084 28.28 0.4978 0.6972 0.0280 0.0200 0.139 2.923 1.286 103.757 0.330 5.721 5.622 0.24 96340. 0.1871 29.63 0.5215 0.6897 0.0246 0.0186 0.129 2.717 1.129 96.435 0.307 5.021 5.309 0.24 96536. 0.1655 30.98 0.5452 0.6749 0.0211 0.0171 0.119 2.493 0.970 88.486 0.282 4.312 4.970 0.24 96739. 0.1436 32.33 0.5689 0.6504 0.0176 0.0154 0.107 2.252 0.809 79.915 0.254 3.597 4.590 0.24 96949. 0.1211 33.67 0.5926 0.6121 0.0141 0.0136 0.095 1.993 0.647 70.736 0.225 2.876 4.147 0.24 97167. 0.0978 35.02 0.6163 0.5529 0.0105 0.0118 0.082 1.718 0.484 60.965 0.194 2.153 3.602 0.24 97392. 0.0735 36.37 0.6400 0.4590 0.0070 0.0098 0.068 1.426 0.321 50.628 0.161 1.430 2.879 0.24 97625. 0.0479 37.71 0.6637 0.3002 0.0035 0.0077 0.053 1.120 0.159 39.752 0.127 0.708 1.816 0.24 97864. 0.0212 39.06 0.6874 -0.0135 -0.0001 0.0054 0.038 0.793 -0.005 28.160 0.090 -0.022 -0.079 0.24 98094. 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 0.0247 0.407 6.408 6.411 303.246 0.724 28.517 9.589 0.32 125163. 0.7123 1.80 0.0238 0.0731 0.0775 0.0252 0.415 6.534 6.319 309.239 0.738 28.106 9.268 0.32 125236. 0.6835 3.60 0.0475 0.1413 0.0762 0.0256 0.422 6.655 6.217 314.945 0.752 27.653 8.953 0.32 125316. 0.6549 5.40 0.0713 0.2046 0.0748 0.0261 0.429 6.767 6.105 320.245 0.765 27.155 8.647 0.32 125403. 0.6268 7.20 0.0950 0.2634 0.0733 0.0264 0.436 6.868 5.982 325.025 0.776 26.609 8.348 0.32 125498. 0.5990 9.00 0.1188 0.3179 0.0717 0.0268 0.441 6.955 5.848 329.165 0.786 26.014 8.059 0.32 125600. 0.5718 10.80 0.1425 0.3682 0.0699 0.0271 0.446 7.027 5.703 332.540 0.794 25.366 7.778 0.32 125711. 0.5450 12.60 0.1663 0.4146 0.0680 0.0273 0.449 7.079 5.545 335.030 0.800 24.665 7.507 0.32 125830. 0.5187 14.40 0.1900 0.4573 0.0659 0.0274 0.451 7.111 5.376 336.527 0.803 23.911 7.245 0.32 125957. 0.4928 16.20 0.2138 0.4965 0.0637 0.0274 0.452 7.120 5.194 336.940 0.804 23.104 6.992 0.32 126094. 0.4675 18.00 0.2375 0.5323 0.0613 0.0274 0.451 7.104 5.001 336.196 0.803 22.247 6.748 0.32 126239. 0.4427 19.79 0.2613 0.5650 0.0588 0.0272 0.448 7.063 4.798 334.233 0.798 21.341 6.511 0.32 126393. 0.4184 21.59 0.2850 0.5946 0.0562 0.0269 0.444 6.994 4.584 331.002 0.790 20.390 6.281 0.32 126557. 0.3946 23.39 0.3088 0.6213 0.0534 0.0266 0.438 6.898 4.361 326.458 0.779 19.396 6.058 0.32 126730. 0.3712 25.19 0.3325 0.6451 0.0506 0.0261 0.430 6.774 4.128 320.561 0.765 18.362 5.841 0.32 126913. 0.3482 26.99 0.3563 0.6660 0.0476 0.0255 0.420 6.620 3.887 313.278 0.748 17.291 5.628 0.32 127105. 0.3256 28.79 0.3801 0.6840 0.0446 0.0248 0.408 6.436 3.639 304.574 0.727 16.186 5.419 0.32 127307. 0.3033 30.59 0.4038 0.6990 0.0415 0.0240 0.395 6.221 3.383 294.423 0.703 15.049 5.212 0.32 127518. 0.2813 32.39 0.4276 0.7109 0.0383 0.0230 0.379 5.976 3.121 282.795 0.675 13.883 5.006 0.32 127740. 0.2595 34.19 0.4513 0.7193 0.0350 0.0219 0.362 5.698 2.853 269.669 0.644 12.691 4.799 0.32 127971. 0.2378 35.99 0.4751 0.7239 0.0316 0.0208 0.342 5.389 2.580 255.029 0.609 11.475 4.588 0.32 128213. 0.2162 37.79 0.4988 0.7241 0.0282 0.0194 0.320 5.047 2.302 238.861 0.570 10.238 4.370 0.32 128464. 0.1945 39.59 0.5226 0.7187 0.0248 0.0180 0.297 4.673 2.019 221.161 0.528 8.982 4.141 0.32 128726. 0.1726 41.39 0.5463 0.7065 0.0212 0.0164 0.271 4.267 1.733 201.933 0.482 7.710 3.894 0.32 128997. 0.1504 43.19 0.5701 0.6848 0.0177 0.0147 0.243 3.829 1.445 181.193 0.433 6.427 3.617 0.32 129279. 0.1275 44.99 0.5938 0.6495 0.0141 0.0129 0.213 3.359 1.154 158.970 0.380 5.134 3.293 0.32 129571. 0.1038 46.79 0.6176 0.5930 0.0106 0.0110 0.181 2.859 0.863 135.310 0.323 3.836 2.891 0.32 129872. 0.0788 48.59 0.6413 0.5000 0.0070 0.0090 0.148 2.330 0.571 110.275 0.263 2.538 2.347 0.32 130184. 0.0520 50.39 0.6651 0.3339 0.0034 0.0068 0.113 1.773 0.280 83.928 0.200 1.244 1.511 0.32 130504. 0.0235 52.19 0.6888 -0.0328 -0.0002 0.0045 0.074 1.173 -0.018 55.523 0.133 -0.078 -0.143 0.32 130796. 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 0.0792 0.0244 0.786 9.903 10.098 585.850 1.119 44.915 7.818 0.40 156446. 0.7288 2.25 0.0238 0.0745 0.0781 0.0249 0.802 10.107 9.955 597.901 1.142 44.280 7.552 0.40 156538. 0.6991 4.50 0.0475 0.1439 0.0769 0.0254 0.817 10.301 9.797 609.390 1.164 43.578 7.292 0.40 156638. 0.6696 6.75 0.0713 0.2083 0.0755 0.0258 0.832 10.482 9.623 620.082 1.184 42.805 7.039 0.40 156747. 0.6407 9.00 0.0950 0.2680 0.0740 0.0262 0.845 10.646 9.433 629.747 1.203 41.956 6.794 0.40 156866. 0.6122 11.25 0.1188 0.3233 0.0724 0.0266 0.856 10.787 9.224 638.143 1.219 41.028 6.556 0.40 156994. 0.5842 13.50 0.1426 0.3744 0.0706 0.0269 0.865 10.904 8.997 645.024 1.232 40.017 6.326 0.40 157133. 0.5567 15.75 0.1663 0.4215 0.0686 0.0271 0.872 10.990 8.750 650.145 1.242 38.921 6.104 0.40 157282. 0.5298 18.00 0.1901 0.4648 0.0666 0.0272 0.876 11.044 8.485 653.288 1.248 37.739 5.891 0.40 157442. 0.5034 20.25 0.2138 0.5046 0.0643 0.0273 0.877 11.060 8.200 654.271 1.250 36.474 5.685 0.40 157613. 0.4776 22.50 0.2376 0.5411 0.0620 0.0272 0.876 11.038 7.897 652.945 1.247 35.127 5.486 0.40 157795. 0.4523 24.75 0.2614 0.5744 0.0594 0.0270 0.871 10.974 7.577 649.188 1.240 33.704 5.294 0.40 157988. 0.4275 27.00 0.2851 0.6047 0.0568 0.0268 0.862 10.868 7.241 642.900 1.228 32.208 5.109 0.40 158193. 0.4033 29.25 0.3089 0.6320 0.0540 0.0264 0.850 10.717 6.889 633.992 1.211 30.643 4.929 0.40 158410. 0.3795 31.50 0.3326 0.6565 0.0512 0.0259 0.835 10.521 6.523 622.388 1.189 29.015 4.754 0.40 158639. 0.3562 33.75 0.3564 0.6781 0.0482 0.0253 0.815 10.278 6.144 608.017 1.161 27.328 4.583 0.40 158880. 0.3333 36.00 0.3801 0.6969 0.0451 0.0246 0.792 9.987 5.752 590.815 1.128 25.587 4.416 0.40 159132. 0.3107 38.25 0.4039 0.7129 0.0420 0.0238 0.765 9.648 5.350 570.725 1.090 23.795 4.251 0.40 159397. 0.2885 40.50 0.4277 0.7258 0.0387 0.0228 0.734 9.258 4.936 547.693 1.046 21.957 4.088 0.40 159675. 0.2665 42.75 0.4514 0.7355 0.0354 0.0217 0.700 8.819 4.514 521.676 0.996 20.076 3.924 0.40 159964. 0.2446 45.00 0.4752 0.7415 0.0320 0.0205 0.661 8.328 4.082 492.637 0.941 18.158 3.759 0.40 160266. 0.2228 47.25 0.4989 0.7433 0.0286 0.0192 0.618 7.785 3.643 460.552 0.880 16.206 3.588 0.40 160581. 0.2009 49.50 0.5227 0.7399 0.0251 0.0177 0.570 7.191 3.198 425.411 0.812 14.224 3.410 0.40 160908. 0.1789 51.75 0.5465 0.7299 0.0215 0.0161 0.519 6.546 2.747 387.223 0.740 12.218 3.217 0.40 161248. 0.1564 54.00 0.5702 0.7110 0.0180 0.0144 0.464 5.849 2.291 346.018 0.661 10.191 3.003 0.40 161600. 0.1334 56.25 0.5940 0.6790 0.0144 0.0126 0.405 5.103 1.832 301.855 0.577 8.151 2.753 0.40 161965. 0.1094 58.50 0.6177 0.6262 0.0108 0.0106 0.342 4.308 1.372 254.824 0.487 6.102 2.442 0.40 162343. 0.0839 60.75 0.6415 0.5367 0.0071 0.0085 0.275 3.466 0.911 205.049 0.392 4.052 2.015 0.40 162732. 0.0564 63.00 0.6653 0.3705 0.0035 0.0064 0.205 2.581 0.452 152.661 0.292 2.008 1.341 0.41 163133. 0.0264 65.25 0.6890 -0.0250 -0.0001 0.0040 0.129 1.625 -0.018 96.100 0.184 -0.082 -0.087 0.41 163496. 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 0.0800 0.0244 1.355 14.233 14.684 1010.341 1.608 65.314 6.592 0.48 187725. 0.7411 2.71 0.0238 0.0756 0.0789 0.0249 1.384 14.536 14.481 1031.884 1.642 64.410 6.365 0.48 187835. 0.7106 5.42 0.0477 0.1459 0.0777 0.0254 1.411 14.826 14.255 1052.444 1.675 63.408 6.144 0.48 187956. 0.6805 8.13 0.0715 0.2112 0.0763 0.0258 1.437 15.096 14.006 1071.604 1.706 62.301 5.928 0.48 188088. 0.6509 10.84 0.0953 0.2717 0.0748 0.0263 1.460 15.340 13.732 1088.944 1.733 61.081 5.720 0.48 188231. 0.6219 13.54 0.1192 0.3276 0.0732 0.0266 1.481 15.553 13.432 1104.030 1.757 59.744 5.518 0.48 188386. 0.5933 16.25 0.1430 0.3793 0.0714 0.0269 1.497 15.727 13.103 1116.418 1.777 58.284 5.324 0.48 188554. 0.5654 18.96 0.1669 0.4269 0.0694 0.0271 1.510 15.857 12.747 1125.669 1.792 56.697 5.136 0.48 188734. 0.5380 21.67 0.1907 0.4708 0.0673 0.0273 1.517 15.938 12.361 1131.391 1.801 54.982 4.956 0.48 188927. 0.5112 24.38 0.2145 0.5111 0.0651 0.0273 1.520 15.964 11.948 1133.253 1.804 53.143 4.782 0.48 189134. 0.4849 27.09 0.2384 0.5480 0.0627 0.0273 1.517 15.932 11.507 1130.990 1.800 51.184 4.615 0.48 189354. 0.4593 29.80 0.2622 0.5818 0.0601 0.0271 1.508 15.839 11.041 1124.390 1.790 49.109 4.454 0.48 189588. 0.4342 32.51 0.2860 0.6125 0.0575 0.0268 1.493 15.683 10.550 1113.270 1.772 46.927 4.298 0.48 189836. 0.4096 35.21 0.3099 0.6403 0.0547 0.0265 1.472 15.460 10.037 1097.481 1.747 44.643 4.148 0.48 190099. 0.3855 37.92 0.3337 0.6654 0.0518 0.0260 1.444 15.170 9.502 1076.887 1.714 42.265 4.002 0.48 190375. 0.3619 40.63 0.3576 0.6876 0.0487 0.0253 1.410 14.811 8.948 1051.367 1.673 39.799 3.860 0.48 190666. 0.3388 43.34 0.3814 0.7070 0.0456 0.0246 1.369 14.380 8.375 1020.812 1.625 37.252 3.721 0.48 190972. 0.3159 46.05 0.4052 0.7237 0.0424 0.0238 1.321 13.877 7.786 985.118 1.568 34.631 3.585 0.48 191292. 0.2935 48.76 0.4291 0.7374 0.0391 0.0228 1.266 13.301 7.181 944.198 1.503 31.942 3.450 0.48 191627. 0.2712 51.47 0.4529 0.7479 0.0358 0.0216 1.204 12.650 6.562 897.971 1.429 29.190 3.315 0.48 191977. 0.2491 54.18 0.4767 0.7549 0.0323 0.0204 1.135 11.923 5.931 846.375 1.347 26.382 3.178 0.48 192342. 0.2271 56.88 0.5006 0.7578 0.0288 0.0190 1.059 11.120 5.289 789.370 1.256 23.524 3.039 0.48 192722. 0.2050 59.59 0.5244 0.7557 0.0253 0.0175 0.975 10.240 4.636 726.937 1.157 20.622 2.893 0.48 193117. 0.1827 62.30 0.5483 0.7472 0.0217 0.0159 0.884 9.285 3.975 659.094 1.049 17.683 2.736 0.48 193528. 0.1600 65.01 0.5721 0.7299 0.0180 0.0141 0.786 8.254 3.308 585.898 0.932 14.715 2.561 0.48 193953. 0.1367 67.72 0.5959 0.6995 0.0144 0.0122 0.681 7.149 2.636 507.456 0.808 11.726 2.356 0.48 194394. 0.1122 70.43 0.6198 0.6480 0.0107 0.0102 0.569 5.972 1.962 423.933 0.675 8.725 2.099 0.49 194850. 0.0862 73.14 0.6436 0.5577 0.0070 0.0081 0.450 4.727 1.287 335.559 0.534 5.723 1.739 0.49 195320. 0.0579 75.85 0.6674 0.3816 0.0033 0.0058 0.325 3.417 0.614 242.552 0.386 2.730 1.148 0.49 195803. 0.0264 78.55 0.6913 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 0.0245 2.162 19.471 20.222 1612.541 2.200 89.947 5.688 0.56 218997. 0.7504 3.15 0.0238 0.0759 0.0799 0.0250 2.210 19.898 19.952 1647.917 2.248 88.747 5.492 0.56 219125. 0.7197 6.31 0.0476 0.1466 0.0787 0.0255 2.255 20.306 19.652 1681.736 2.294 87.410 5.300 0.56 219266. 0.6893 9.46 0.0714 0.2122 0.0773 0.0260 2.298 20.688 19.318 1713.307 2.337 85.928 5.114 0.56 219420. 0.6595 12.62 0.0952 0.2729 0.0758 0.0264 2.336 21.033 18.950 1741.945 2.376 84.289 4.934 0.56 219587. 0.6302 15.77 0.1190 0.3291 0.0742 0.0268 2.370 21.335 18.544 1766.938 2.410 82.485 4.760 0.56 219768. 0.6014 18.93 0.1428 0.3811 0.0724 0.0271 2.397 21.584 18.100 1787.553 2.439 80.510 4.593 0.56 219964. 0.5733 22.08 0.1665 0.4290 0.0705 0.0274 2.418 21.771 17.616 1803.074 2.460 78.357 4.431 0.56 220174. 0.5457 25.23 0.1903 0.4731 0.0684 0.0275 2.431 21.890 17.092 1812.851 2.473 76.026 4.276 0.56 220400. 0.5187 28.39 0.2141 0.5137 0.0662 0.0276 2.436 21.932 16.528 1816.339 2.478 73.519 4.127 0.56 220641. 0.4923 31.54 0.2379 0.5510 0.0637 0.0275 2.431 21.893 15.927 1813.105 2.473 70.842 3.984 0.56 220898. 0.4665 34.70 0.2617 0.5851 0.0612 0.0274 2.418 21.768 15.289 1802.801 2.459 68.004 3.846 0.56 221171. 0.4412 37.85 0.2855 0.6163 0.0585 0.0271 2.394 21.555 14.616 1785.142 2.435 65.013 3.714 0.56 221461. 0.4165 41.01 0.3093 0.6446 0.0557 0.0267 2.360 21.250 13.912 1759.889 2.401 61.880 3.585 0.56 221766. 0.3924 44.16 0.3331 0.6701 0.0527 0.0262 2.316 20.851 13.178 1726.834 2.356 58.615 3.461 0.56 222089. 0.3686 47.31 0.3569 0.6929 0.0497 0.0256 2.261 20.355 12.416 1685.786 2.300 55.226 3.341 0.56 222428. 0.3453 50.47 0.3807 0.7131 0.0465 0.0248 2.195 19.761 11.629 1636.574 2.233 51.724 3.223 0.56 222784. 0.3224 53.62 0.4045 0.7305 0.0433 0.0240 2.118 19.066 10.818 1579.044 2.154 48.116 3.107 0.56 223157. 0.2998 56.78 0.4283 0.7450 0.0400 0.0230 2.029 18.270 9.985 1513.052 2.064 44.413 2.993 0.56 223547. 0.2775 59.93 0.4521 0.7566 0.0366 0.0218 1.929 17.369 9.133 1438.478 1.962 40.623 2.880 0.56 223955. 0.2553 63.09 0.4758 0.7648 0.0331 0.0206 1.817 16.364 8.263 1355.217 1.849 36.753 2.765 0.56 224380. 0.2332 66.24 0.4996 0.7692 0.0295 0.0192 1.694 15.253 7.377 1263.202 1.723 32.812 2.649 0.56 224822. 0.2111 69.39 0.5234 0.7688 0.0259 0.0176 1.559 14.036 6.477 1162.406 1.586 28.809 2.527 0.56 225282. 0.1887 72.55 0.5472 0.7625 0.0223 0.0160 1.412 12.713 5.565 1052.849 1.436 24.753 2.397 0.56 225760. 0.1659 75.70 0.5710 0.7479 0.0186 0.0142 1.253 11.285 4.644 934.621 1.275 20.655 2.254 0.56 226255. 0.1425 78.86 0.5948 0.7211 0.0149 0.0123 1.083 9.755 3.715 807.889 1.102 16.526 2.086 0.57 226768. 0.1180 82.01 0.6186 0.6745 0.0111 0.0102 0.902 8.125 2.783 672.916 0.918 12.379 1.876 0.57 227298. 0.0918 85.17 0.6424 0.5911 0.0074 0.0080 0.711 6.400 1.850 530.068 0.723 8.229 1.583 0.57 227845. 0.0632 88.32 0.6662 0.4252 0.0037 0.0058 0.509 4.585 0.919 379.715 0.518 4.089 1.098 0.57 228407. 0.0309 91.47 0.6900 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 0.0821 0.0248 3.265 25.724 26.780 2434.785 2.906 119.117 4.989 0.63 250260. 0.7574 3.61 0.0238 0.0763 0.0810 0.0253 3.339 26.307 26.438 2489.917 2.972 117.598 4.816 0.63 250407. 0.7265 7.22 0.0477 0.1472 0.0798 0.0259 3.410 26.865 26.055 2542.737 3.035 115.894 4.648 0.63 250569. 0.6960 10.83 0.0715 0.2130 0.0785 0.0264 3.476 27.387 25.628 2592.149 3.094 113.994 4.484 0.63 250746. 0.6660 14.45 0.0953 0.2740 0.0771 0.0268 3.536 27.861 25.153 2637.061 3.148 111.882 4.326 0.63 250938. 0.6366 18.06 0.1192 0.3304 0.0755 0.0272 3.589 28.276 24.628 2676.345 3.195 109.546 4.174 0.64 251146. 0.6077 21.67 0.1430 0.3825 0.0737 0.0276 3.633 28.620 24.050 2708.848 3.233 106.977 4.027 0.64 251371. 0.5794 25.28 0.1668 0.4307 0.0718 0.0278 3.666 28.880 23.418 2733.431 3.263 104.164 3.886 0.64 251613. 0.5517 28.89 0.1907 0.4750 0.0697 0.0280 3.687 29.045 22.731 2749.072 3.281 101.108 3.750 0.64 251873. 0.5246 32.50 0.2145 0.5159 0.0674 0.0280 3.694 29.107 21.990 2754.914 3.288 97.810 3.620 0.64 252150. 0.4981 36.11 0.2384 0.5534 0.0650 0.0280 3.688 29.057 21.196 2750.276 3.283 94.279 3.496 0.64 252446. 0.4721 39.73 0.2622 0.5879 0.0624 0.0278 3.667 28.892 20.352 2734.634 3.264 90.527 3.376 0.64 252760. 0.4468 43.34 0.2860 0.6194 0.0596 0.0275 3.631 28.606 19.462 2707.560 3.232 86.566 3.260 0.64 253093. 0.4220 46.95 0.3099 0.6481 0.0568 0.0271 3.579 28.196 18.527 2668.703 3.186 82.410 3.149 0.64 253445. 0.3976 50.56 0.3337 0.6741 0.0538 0.0266 3.510 27.657 17.552 2617.758 3.125 78.072 3.041 0.64 253815. 0.3738 54.17 0.3575 0.6974 0.0507 0.0260 3.426 26.989 16.539 2554.458 3.049 73.566 2.937 0.64 254205. 0.3504 57.78 0.3814 0.7181 0.0475 0.0252 3.324 26.187 15.491 2478.554 2.959 68.905 2.835 0.64 254614. 0.3273 61.39 0.4052 0.7362 0.0442 0.0243 3.205 25.249 14.411 2389.824 2.853 64.101 2.735 0.64 255043. 0.3046 65.01 0.4290 0.7515 0.0408 0.0233 3.068 24.174 13.302 2288.063 2.731 59.166 2.637 0.64 255492. 0.2821 68.62 0.4529 0.7638 0.0373 0.0221 2.914 22.959 12.165 2173.098 2.594 54.112 2.539 0.64 255960. 0.2598 72.23 0.4767 0.7730 0.0337 0.0208 2.742 21.604 11.005 2044.767 2.441 48.949 2.441 0.64 256448. 0.2376 75.84 0.5005 0.7784 0.0301 0.0194 2.552 20.106 9.822 1902.977 2.272 43.690 2.341 0.64 256956. 0.2153 79.45 0.5244 0.7793 0.0264 0.0178 2.344 18.465 8.621 1747.686 2.086 38.345 2.237 0.64 257484. 0.1927 83.06 0.5482 0.7744 0.0227 0.0161 2.117 16.682 7.403 1578.928 1.885 32.928 2.127 0.64 258032. 0.1698 86.68 0.5721 0.7615 0.0189 0.0142 1.873 14.758 6.172 1396.844 1.667 27.453 2.004 0.65 258601. 0.1461 90.29 0.5959 0.7367 0.0151 0.0122 1.611 12.696 4.931 1201.693 1.434 21.934 1.861 0.65 259189. 0.1213 93.90 0.6197 0.6922 0.0113 0.0101 1.333 10.501 3.685 993.889 1.186 16.389 1.682 0.65 259797. 0.0947 97.51 0.6436 0.6105 0.0075 0.0079 1.038 8.178 2.437 773.999 0.924 10.839 1.428 0.65 260425. 0.0654 101.12 0.6674 0.4417 0.0037 0.0055 0.728 5.733 1.192 542.589 0.648 5.301 0.996 0.65 261069. 0.0319 104.73 0.6912 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 0.0255 4.787 33.522 34.437 3569.455 3.787 153.176 4.376 0.71 281512. 0.7534 4.08 0.0239 0.0757 0.0824 0.0261 4.890 34.249 34.025 3646.808 3.869 151.343 4.232 0.71 281679. 0.7242 8.16 0.0479 0.1464 0.0813 0.0266 4.990 34.945 33.558 3721.000 3.948 149.267 4.091 0.71 281862. 0.6952 12.24 0.0718 0.2121 0.0800 0.0271 5.083 35.598 33.033 3790.487 4.022 146.930 3.953 0.71 282062. 0.6665 16.32 0.0958 0.2732 0.0786 0.0275 5.168 36.192 32.444 3853.706 4.089 144.312 3.819 0.71 282280. 0.6381 20.40 0.1197 0.3299 0.0770 0.0279 5.242 36.711 31.789 3909.029 4.148 141.395 3.688 0.71 282517. 0.6101 24.48 0.1436 0.3824 0.0752 0.0283 5.303 37.141 31.062 3954.774 4.196 138.164 3.562 0.71 282772. 0.5825 28.56 0.1676 0.4309 0.0733 0.0285 5.350 37.465 30.262 3989.248 4.233 134.607 3.441 0.72 283048. 0.5553 32.64 0.1915 0.4756 0.0712 0.0287 5.379 37.668 29.388 4010.865 4.256 130.719 3.323 0.72 283343. 0.5286 36.73 0.2155 0.5169 0.0689 0.0287 5.389 37.737 28.441 4018.282 4.264 126.505 3.210 0.72 283659. 0.5023 40.81 0.2394 0.5548 0.0664 0.0286 5.378 37.663 27.423 4010.410 4.255 121.976 3.101 0.72 283995. 0.4765 44.89 0.2633 0.5897 0.0638 0.0285 5.346 37.438 26.337 3986.382 4.230 117.146 2.997 0.72 284353. 0.4512 48.97 0.2873 0.6216 0.0610 0.0282 5.291 37.054 25.188 3945.487 4.186 112.034 2.896 0.72 284732. 0.4263 53.05 0.3112 0.6507 0.0581 0.0278 5.213 36.506 23.979 3887.137 4.124 106.658 2.798 0.72 285132. 0.4020 57.13 0.3352 0.6771 0.0550 0.0272 5.110 35.789 22.715 3810.826 4.043 101.038 2.704 0.72 285554. 0.3780 61.21 0.3591 0.7009 0.0518 0.0265 4.983 34.899 21.401 3716.114 3.943 95.192 2.612 0.72 285997. 0.3545 65.29 0.3830 0.7221 0.0485 0.0257 4.831 33.834 20.040 3602.637 3.823 89.137 2.523 0.72 286462. 0.3314 69.37 0.4070 0.7408 0.0451 0.0248 4.653 32.589 18.636 3470.088 3.682 82.891 2.436 0.72 286950. 0.3085 73.45 0.4309 0.7567 0.0416 0.0237 4.450 31.162 17.192 3318.191 3.521 76.470 2.350 0.72 287460. 0.2859 77.53 0.4548 0.7698 0.0380 0.0225 4.220 29.552 15.712 3146.710 3.339 69.889 2.265 0.72 287992. 0.2634 81.61 0.4788 0.7797 0.0344 0.0211 3.963 27.756 14.200 2955.445 3.136 63.164 2.179 0.72 288546. 0.2409 85.69 0.5027 0.7860 0.0307 0.0196 3.680 25.772 12.659 2744.247 2.912 56.308 2.092 0.72 289124. 0.2184 89.77 0.5267 0.7879 0.0269 0.0180 3.370 23.601 11.092 2513.065 2.666 49.339 2.002 0.72 289723. 0.1956 93.85 0.5506 0.7841 0.0230 0.0162 3.033 21.243 9.504 2261.951 2.400 42.272 1.906 0.72 290346. 0.1724 97.93 0.5745 0.7723 0.0191 0.0142 2.670 18.699 7.897 1991.126 2.113 35.125 1.799 0.73 290991. 0.1483 102.01 0.5985 0.7485 0.0152 0.0122 2.281 15.975 6.277 1700.998 1.805 27.920 1.674 0.73 291659. 0.1230 106.09 0.6224 0.7045 0.0113 0.0099 1.867 13.075 4.649 1392.224 1.477 20.679 1.515 0.73 292349. 0.0958 110.18 0.6464 0.6206 0.0073 0.0076 1.429 10.009 3.019 1065.801 1.131 13.430 1.285 0.73 293061. 0.0655 114.26 0.6703 0.4378 0.0034 0.0052 0.969 6.788 1.393 722.757 0.767 6.195 0.874 0.73 293791. 0.0303 118.34 0.6942 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 0.0848 0.0281 7.237 45.617 43.260 5396.993 5.154 192.423 3.636 0.79 312751. 0.7016 4.52 0.0239 0.0700 0.0839 0.0286 7.359 46.383 42.795 5487.666 5.240 190.350 3.537 0.79 312936. 0.6788 9.03 0.0477 0.1362 0.0829 0.0290 7.473 47.098 42.261 5572.275 5.321 187.975 3.440 0.79 313138. 0.6561 13.55 0.0716 0.1987 0.0817 0.0294 7.575 47.745 41.652 5648.766 5.394 185.270 3.344 0.79 313359. 0.6333 18.07 0.0954 0.2575 0.0803 0.0298 7.664 48.306 40.963 5715.154 5.458 182.204 3.251 0.79 313601. 0.6104 22.59 0.1193 0.3128 0.0788 0.0300 7.737 48.765 40.187 5769.458 5.509 178.752 3.159 0.79 313863. 0.5876 27.10 0.1431 0.3647 0.0771 0.0303 7.791 49.105 39.319 5809.712 5.548 174.892 3.070 0.79 314147. 0.5647 31.62 0.1670 0.4134 0.0752 0.0304 7.824 49.311 38.356 5834.030 5.571 170.606 2.982 0.79 314452. 0.5418 36.14 0.1908 0.4588 0.0731 0.0304 7.832 49.367 37.294 5840.680 5.577 165.886 2.896 0.79 314780. 0.5189 40.66 0.2147 0.5012 0.0709 0.0304 7.816 49.262 36.136 5828.225 5.566 160.735 2.812 0.80 315131. 0.4960 45.17 0.2385 0.5407 0.0684 0.0302 7.772 48.985 34.884 5795.550 5.534 155.165 2.730 0.80 315505. 0.4731 49.69 0.2624 0.5772 0.0658 0.0299 7.700 48.531 33.542 5741.798 5.483 149.195 2.650 0.80 315902. 0.4502 54.21 0.2862 0.6109 0.0630 0.0295 7.599 47.893 32.115 5666.272 5.411 142.848 2.571 0.80 316322. 0.4274 58.72 0.3101 0.6419 0.0600 0.0290 7.467 47.065 30.609 5568.366 5.317 136.150 2.493 0.80 316767. 0.4047 63.24 0.3339 0.6701 0.0569 0.0284 7.305 46.044 29.030 5447.493 5.202 129.125 2.417 0.80 317235. 0.3821 67.76 0.3578 0.6957 0.0537 0.0276 7.111 44.823 27.383 5303.032 5.064 121.799 2.342 0.80 317727. 0.3596 72.28 0.3816 0.7186 0.0504 0.0267 6.885 43.397 25.674 5134.327 4.903 114.196 2.268 0.80 318243. 0.3372 76.79 0.4055 0.7389 0.0469 0.0257 6.626 41.760 23.907 4940.694 4.718 106.339 2.195 0.80 318783. 0.3148 81.31 0.4293 0.7564 0.0433 0.0246 6.332 39.907 22.088 4721.449 4.509 98.249 2.122 0.80 319348. 0.2926 85.83 0.4532 0.7710 0.0397 0.0233 6.002 37.832 20.222 4475.934 4.274 89.946 2.049 0.80 319937. 0.2703 90.35 0.4770 0.7826 0.0359 0.0219 5.637 35.530 18.312 4203.564 4.014 81.452 1.976 0.80 320551. 0.2481 94.86 0.5009 0.7907 0.0321 0.0203 5.235 32.996 16.363 3903.852 3.728 72.784 1.901 0.80 321190. 0.2256 99.38 0.5247 0.7944 0.0282 0.0186 4.797 30.236 14.380 3577.218 3.416 63.962 1.823 0.80 321853. 0.2028 103.90 0.5486 0.7924 0.0243 0.0168 4.324 27.251 12.367 3224.081 3.079 55.007 1.740 0.81 322542. 0.1795 108.41 0.5724 0.7827 0.0203 0.0148 3.815 24.044 10.328 2844.657 2.716 45.940 1.647 0.81 323255. 0.1553 112.93 0.5963 0.7610 0.0162 0.0127 3.273 20.628 8.270 2440.486 2.330 36.786 1.537 0.81 323993. 0.1297 117.45 0.6201 0.7191 0.0122 0.0105 2.700 17.018 6.199 2013.487 1.923 27.575 1.397 0.81 324755. 0.1020 121.97 0.6440 0.6384 0.0081 0.0082 2.100 13.239 4.123 1566.316 1.496 18.338 1.194 0.81 325542. 0.0711 126.48 0.6678 0.4672 0.0040 0.0057 1.478 9.313 2.047 1101.817 1.052 9.104 0.843 0.81 326349. 0.0354 131.00 0.6917 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 0.0860 0.0341 11.704 67.060 53.056 8727.339 7.576 235.992 2.757 0.87 343990. 0.5892 4.98 0.0239 0.0589 0.0852 0.0346 11.847 67.883 52.573 8834.467 7.669 233.845 2.699 0.87 344190. 0.5742 9.96 0.0478 0.1153 0.0843 0.0349 11.972 68.600 52.009 8927.813 7.750 231.337 2.642 0.87 344411. 0.5591 14.93 0.0717 0.1694 0.0832 0.0352 12.074 69.182 51.355 9003.576 7.816 228.426 2.587 0.87 344653. 0.5439 19.91 0.0956 0.2212 0.0820 0.0354 12.147 69.601 50.599 9058.030 7.863 225.066 2.534 0.87 344918. 0.5288 24.89 0.1195 0.2708 0.0806 0.0356 12.187 69.829 49.733 9087.797 7.889 221.213 2.482 0.87 345206. 0.5136 29.87 0.1434 0.3185 0.0790 0.0356 12.190 69.846 48.748 9090.021 7.891 216.830 2.432 0.87 345518. 0.4982 34.84 0.1673 0.3642 0.0772 0.0355 12.153 69.635 47.637 9062.496 7.867 211.888 2.384 0.87 345855. 0.4828 39.82 0.1911 0.4080 0.0752 0.0352 12.074 69.183 46.396 9003.740 7.816 206.368 2.337 0.87 346218. 0.4671 44.80 0.2150 0.4500 0.0730 0.0349 11.953 68.487 45.025 8913.139 7.738 200.271 2.291 0.87 346606. 0.4511 49.78 0.2389 0.4901 0.0706 0.0344 11.789 67.548 43.527 8790.890 7.632 193.610 2.246 0.88 347020. 0.4347 54.76 0.2628 0.5283 0.0679 0.0338 11.583 66.371 41.908 8637.694 7.499 186.409 2.201 0.88 347461. 0.4180 59.73 0.2867 0.5644 0.0651 0.0331 11.338 64.963 40.175 8454.456 7.339 178.699 2.155 0.88 347927. 0.4008 64.71 0.3106 0.5985 0.0621 0.0322 11.053 63.331 38.335 8242.069 7.155 170.514 2.110 0.88 348420. 0.3832 69.69 0.3345 0.6303 0.0590 0.0313 10.730 61.480 36.396 8001.158 6.946 161.889 2.063 0.88 348939. 0.3652 74.67 0.3584 0.6599 0.0557 0.0303 10.369 59.412 34.365 7732.040 6.712 152.857 2.016 0.88 349485. 0.3467 79.65 0.3823 0.6870 0.0523 0.0291 9.970 57.127 32.251 7434.626 6.454 143.450 1.968 0.88 350057. 0.3278 84.62 0.4062 0.7115 0.0487 0.0278 9.533 54.620 30.058 7108.391 6.171 133.699 1.918 0.88 350656. 0.3085 89.60 0.4301 0.7334 0.0451 0.0264 9.055 51.886 27.795 6752.580 5.862 123.630 1.867 0.88 351282. 0.2888 94.58 0.4540 0.7523 0.0413 0.0249 8.537 48.918 25.466 6366.374 5.527 113.272 1.814 0.88 351935. 0.2686 99.56 0.4779 0.7680 0.0374 0.0233 7.978 45.712 23.079 5949.043 5.164 102.653 1.760 0.88 352615. 0.2480 104.53 0.5018 0.7800 0.0335 0.0215 7.375 42.259 20.639 5499.769 4.774 91.801 1.702 0.88 353322. 0.2269 109.51 0.5257 0.7877 0.0294 0.0196 6.730 38.559 18.153 5018.202 4.356 80.743 1.641 0.88 354056. 0.2051 114.49 0.5496 0.7841 0.0253 0.0177 6.082 34.851 15.621 4535.656 3.937 69.482 1.562 0.89 354818. 0.1811 119.47 0.5734 0.7677 0.0212 0.0158 5.416 31.036 13.053 4039.073 3.506 58.059 1.466 0.89 355606. 0.1554 124.45 0.5973 0.7351 0.0169 0.0138 4.721 27.049 10.457 3520.288 3.056 46.515 1.347 0.89 356422. 0.1278 129.42 0.6212 0.6762 0.0127 0.0117 4.003 22.937 7.843 2985.074 2.591 34.885 1.192 0.89 357265. 0.0979 134.40 0.6451 0.5721 0.0085 0.0095 3.269 18.733 5.219 2437.955 2.116 23.212 0.971 0.89 358134. 0.0651 139.38 0.6690 0.3813 0.0042 0.0074 2.527 14.481 2.593 1884.647 1.636 11.535 0.624 0.89 359026. 0.0295 144.36 0.6929 -0.0589 -0.0004 0.0047 1.625 9.310 -0.248 1211.652 1.052 -1.105 -0.093 0.89 359560. 0.0000