28x20-4 (28x20-4.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 0.2104 0.1080 0.144 9.095 4.004 107.600 1.028 17.811 16.879 0.11 96606. 0.7129 0.80 0.0305 0.0582 0.2069 0.1086 0.145 9.150 3.938 108.252 1.034 17.517 16.500 0.11 96738. 0.6911 1.61 0.0611 0.1136 0.2032 0.1092 0.146 9.195 3.867 108.792 1.039 17.200 16.122 0.11 96879. 0.6692 2.41 0.0916 0.1665 0.1991 0.1096 0.146 9.229 3.791 109.195 1.043 16.861 15.745 0.11 97028. 0.6470 3.22 0.1221 0.2167 0.1948 0.1098 0.147 9.250 3.709 109.437 1.045 16.496 15.371 0.11 97187. 0.6248 4.02 0.1527 0.2643 0.1902 0.1099 0.147 9.255 3.621 109.492 1.046 16.106 15.000 0.11 97355. 0.6025 4.82 0.1832 0.3094 0.1853 0.1097 0.147 9.241 3.527 109.334 1.044 15.689 14.633 0.11 97532. 0.5801 5.63 0.2138 0.3520 0.1801 0.1093 0.146 9.208 3.427 108.939 1.040 15.245 14.270 0.11 97719. 0.5576 6.43 0.2443 0.3922 0.1745 0.1087 0.145 9.152 3.321 108.283 1.034 14.772 13.911 0.11 97916. 0.5351 7.23 0.2748 0.4300 0.1685 0.1077 0.144 9.073 3.208 107.345 1.025 14.270 13.556 0.11 98124. 0.5125 8.04 0.3054 0.4653 0.1623 0.1065 0.142 8.968 3.089 106.104 1.013 13.739 13.204 0.11 98341. 0.4898 8.84 0.3359 0.4984 0.1557 0.1049 0.140 8.836 2.963 104.542 0.998 13.180 12.856 0.11 98568. 0.4671 9.65 0.3664 0.5291 0.1487 0.1030 0.138 8.676 2.831 102.644 0.980 12.593 12.511 0.11 98805. 0.4443 10.45 0.3970 0.5574 0.1415 0.1008 0.135 8.486 2.693 100.400 0.959 11.979 12.166 0.11 99053. 0.4214 11.25 0.4275 0.5833 0.1339 0.0982 0.131 8.267 2.549 97.806 0.934 11.339 11.822 0.11 99312. 0.3984 12.06 0.4580 0.6067 0.1261 0.0952 0.127 8.018 2.400 94.860 0.906 10.676 11.476 0.11 99580. 0.3753 12.86 0.4886 0.6274 0.1180 0.0919 0.123 7.739 2.246 91.561 0.874 9.990 11.126 0.11 99859. 0.3519 13.67 0.5191 0.6452 0.1097 0.0882 0.118 7.430 2.087 87.910 0.839 9.284 10.769 0.11 100149. 0.3284 14.47 0.5497 0.6599 0.1011 0.0842 0.113 7.092 1.924 83.909 0.801 8.560 10.402 0.11 100449. 0.3046 15.27 0.5802 0.6710 0.0923 0.0799 0.107 6.725 1.758 79.563 0.760 7.819 10.021 0.11 100760. 0.2804 16.08 0.6107 0.6780 0.0834 0.0751 0.100 6.328 1.588 74.874 0.715 7.063 9.619 0.11 101081. 0.2558 16.88 0.6413 0.6800 0.0743 0.0701 0.094 5.904 1.415 69.849 0.667 6.294 9.188 0.11 101413. 0.2307 17.69 0.6718 0.6760 0.0651 0.0647 0.086 5.451 1.240 64.498 0.616 5.514 8.718 0.11 101756. 0.2049 18.49 0.7023 0.6641 0.0558 0.0590 0.079 4.972 1.063 58.830 0.562 4.727 8.193 0.11 102109. 0.1783 19.29 0.7329 0.6419 0.0465 0.0531 0.071 4.468 0.884 52.862 0.505 3.934 7.589 0.11 102473. 0.1506 20.10 0.7634 0.6049 0.0371 0.0468 0.063 3.940 0.706 46.611 0.445 3.138 6.866 0.11 102848. 0.1217 20.90 0.7939 0.5461 0.0277 0.0402 0.054 3.389 0.527 40.099 0.383 2.344 5.960 0.11 103235. 0.0913 21.70 0.8245 0.4517 0.0183 0.0335 0.045 2.819 0.349 33.354 0.319 1.553 4.747 0.11 103632. 0.0592 22.51 0.8550 0.2932 0.0091 0.0265 0.035 2.232 0.173 26.408 0.252 0.770 2.972 0.11 104040. 0.0261 23.31 0.8855 -0.0015 0.0000 0.0194 0.026 1.630 -0.001 19.290 0.184 -0.003 -0.014 0.11 104458. 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 0.2116 0.1045 1.117 35.188 16.108 832.630 3.976 71.650 8.775 0.22 193196. 0.7433 1.61 0.0306 0.0606 0.2081 0.1052 1.124 35.424 15.844 838.217 4.002 70.474 8.573 0.22 193462. 0.7203 3.22 0.0612 0.1183 0.2044 0.1057 1.130 35.622 15.559 842.904 4.025 69.208 8.373 0.22 193745. 0.6971 4.84 0.0918 0.1733 0.2003 0.1062 1.135 35.774 15.254 846.491 4.042 67.848 8.173 0.22 194045. 0.6738 6.45 0.1224 0.2254 0.1960 0.1065 1.138 35.870 14.925 848.772 4.053 66.388 7.976 0.22 194364. 0.6504 8.06 0.1531 0.2749 0.1914 0.1066 1.139 35.902 14.573 849.534 4.056 64.823 7.781 0.22 194702. 0.6269 9.67 0.1837 0.3217 0.1865 0.1065 1.138 35.861 14.197 848.567 4.052 63.148 7.588 0.22 195059. 0.6035 11.28 0.2143 0.3660 0.1812 0.1061 1.134 35.739 13.795 845.664 4.038 61.361 7.399 0.22 195435. 0.5800 12.89 0.2449 0.4077 0.1756 0.1055 1.127 35.526 13.368 840.631 4.014 59.459 7.213 0.22 195831. 0.5566 14.51 0.2755 0.4470 0.1696 0.1045 1.117 35.216 12.914 833.284 3.979 57.441 7.029 0.22 196247. 0.5332 16.12 0.3061 0.4839 0.1633 0.1033 1.104 34.800 12.434 823.453 3.932 55.306 6.849 0.22 196684. 0.5097 17.73 0.3367 0.5185 0.1567 0.1017 1.088 34.273 11.928 810.978 3.872 53.054 6.671 0.22 197141. 0.4863 19.34 0.3673 0.5508 0.1497 0.0998 1.067 33.629 11.396 795.735 3.799 50.689 6.496 0.22 197619. 0.4628 20.95 0.3980 0.5808 0.1424 0.0976 1.043 32.864 10.840 777.639 3.713 48.215 6.322 0.22 198117. 0.4393 22.56 0.4286 0.6084 0.1348 0.0949 1.015 31.977 10.260 756.644 3.613 45.638 6.150 0.22 198636. 0.4158 24.18 0.4592 0.6337 0.1269 0.0919 0.983 30.966 9.659 732.727 3.499 42.964 5.979 0.22 199176. 0.3922 25.79 0.4898 0.6566 0.1187 0.0886 0.947 29.831 9.038 705.880 3.370 40.202 5.808 0.22 199737. 0.3685 27.40 0.5204 0.6768 0.1103 0.0848 0.907 28.573 8.399 676.105 3.228 37.359 5.635 0.22 200319. 0.3447 29.01 0.5510 0.6942 0.1017 0.0807 0.863 27.191 7.743 643.414 3.072 34.440 5.458 0.22 200923. 0.3206 30.62 0.5816 0.7085 0.0929 0.0763 0.815 25.688 7.072 607.831 2.902 31.455 5.277 0.22 201547. 0.2962 32.24 0.6122 0.7190 0.0839 0.0714 0.764 24.063 6.387 569.390 2.719 28.411 5.088 0.22 202193. 0.2714 33.85 0.6429 0.7253 0.0748 0.0663 0.708 22.320 5.691 528.143 2.522 25.315 4.888 0.23 202860. 0.2461 35.46 0.6735 0.7262 0.0655 0.0607 0.649 20.461 4.986 484.161 2.312 22.179 4.671 0.23 203548. 0.2202 37.07 0.7041 0.7201 0.0561 0.0549 0.587 18.491 4.274 437.537 2.089 19.011 4.431 0.23 204258. 0.1933 38.68 0.7347 0.7045 0.0467 0.0487 0.521 16.414 3.557 388.394 1.854 15.822 4.154 0.23 204990. 0.1654 40.29 0.7653 0.6750 0.0373 0.0423 0.452 14.237 2.838 336.884 1.609 12.625 3.821 0.23 205744. 0.1359 41.91 0.7959 0.6239 0.0278 0.0355 0.380 11.968 2.120 283.198 1.352 9.431 3.396 0.23 206520. 0.1044 43.52 0.8265 0.5348 0.0185 0.0285 0.305 9.617 1.406 227.569 1.087 6.256 2.803 0.23 207318. 0.0702 45.13 0.8571 0.3690 0.0092 0.0214 0.228 7.196 0.700 170.266 0.813 3.114 1.865 0.23 208138. 0.0329 46.74 0.8878 0.0030 0.0000 0.0140 0.150 4.713 0.004 111.515 0.532 0.016 0.015 0.23 208976. 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 0.2132 0.1037 3.742 78.621 36.518 2790.548 8.883 162.433 5.936 0.33 289754. 0.7571 2.42 0.0306 0.0615 0.2097 0.1045 3.768 79.170 35.924 2810.025 8.945 159.788 5.798 0.33 290154. 0.7335 4.84 0.0613 0.1201 0.2060 0.1051 3.790 79.632 35.283 2826.439 8.997 156.939 5.662 0.33 290580. 0.7099 7.26 0.0919 0.1759 0.2019 0.1055 3.807 79.989 34.594 2839.083 9.037 153.874 5.527 0.33 291033. 0.6861 9.68 0.1226 0.2288 0.1976 0.1058 3.818 80.219 33.854 2847.248 9.063 150.581 5.393 0.33 291514. 0.6623 12.10 0.1532 0.2790 0.1930 0.1059 3.822 80.302 33.059 2850.199 9.072 147.049 5.261 0.33 292023. 0.6385 14.52 0.1838 0.3266 0.1880 0.1058 3.818 80.218 32.209 2847.206 9.063 143.266 5.131 0.33 292561. 0.6146 16.94 0.2145 0.3715 0.1827 0.1055 3.805 79.946 31.301 2837.554 9.032 139.227 5.003 0.33 293128. 0.5908 19.36 0.2451 0.4140 0.1771 0.1048 3.782 79.467 30.334 2820.565 8.978 134.924 4.878 0.33 293725. 0.5670 21.78 0.2758 0.4540 0.1711 0.1039 3.749 78.764 29.306 2795.603 8.899 130.355 4.755 0.33 294352. 0.5433 24.20 0.3064 0.4916 0.1647 0.1027 3.704 77.819 28.219 2762.071 8.792 125.518 4.634 0.33 295010. 0.5196 26.62 0.3370 0.5269 0.1580 0.1011 3.647 76.618 27.072 2719.432 8.656 120.416 4.515 0.33 295698. 0.4959 29.04 0.3677 0.5599 0.1510 0.0991 3.577 75.147 25.866 2667.232 8.490 115.052 4.399 0.33 296418. 0.4722 31.46 0.3983 0.5907 0.1436 0.0968 3.494 73.399 24.604 2605.175 8.293 109.439 4.284 0.33 297168. 0.4485 33.88 0.4289 0.6193 0.1359 0.0942 3.397 71.368 23.289 2533.096 8.063 103.591 4.170 0.33 297950. 0.4248 36.30 0.4596 0.6456 0.1280 0.0911 3.287 69.052 21.925 2450.914 7.801 97.523 4.058 0.33 298763. 0.4010 38.72 0.4902 0.6696 0.1198 0.0877 3.163 66.451 20.515 2358.591 7.508 91.253 3.945 0.33 299608. 0.3772 41.14 0.5209 0.6912 0.1113 0.0839 3.026 63.565 19.064 2256.133 7.181 84.795 3.833 0.34 300483. 0.3532 43.56 0.5515 0.7100 0.1026 0.0797 2.875 60.394 17.573 2143.581 6.823 78.167 3.718 0.34 301391. 0.3290 45.98 0.5821 0.7260 0.0937 0.0751 2.710 56.940 16.049 2021.007 6.433 71.386 3.602 0.34 302330. 0.3046 48.40 0.6128 0.7386 0.0846 0.0702 2.533 53.208 14.494 1888.533 6.011 64.470 3.481 0.34 303301. 0.2797 50.82 0.6434 0.7472 0.0754 0.0649 2.342 49.201 12.913 1746.335 5.559 57.439 3.354 0.34 304305. 0.2544 53.24 0.6741 0.7509 0.0660 0.0593 2.138 44.928 11.311 1594.655 5.076 50.312 3.217 0.34 305340. 0.2284 55.66 0.7047 0.7481 0.0566 0.0533 1.923 40.397 9.693 1433.819 4.564 43.114 3.066 0.34 306408. 0.2015 58.07 0.7353 0.7366 0.0471 0.0470 1.695 35.619 8.064 1264.249 4.024 35.869 2.893 0.34 307508. 0.1734 60.49 0.7660 0.7120 0.0375 0.0404 1.457 30.611 6.431 1086.479 3.458 28.603 2.685 0.34 308641. 0.1437 62.91 0.7966 0.6662 0.0280 0.0335 1.208 25.390 4.799 901.175 2.869 21.348 2.416 0.34 309807. 0.1117 65.33 0.8273 0.5821 0.0185 0.0264 0.951 19.980 3.178 709.145 2.257 14.134 2.032 0.34 311006. 0.0765 67.75 0.8579 0.4145 0.0092 0.0190 0.686 14.407 1.573 511.340 1.628 6.997 1.395 0.34 312238. 0.0369 70.17 0.8885 -0.0042 -0.0001 0.0115 0.414 8.690 -0.009 308.446 0.982 -0.041 -0.014 0.34 313494. 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 0.2154 0.1043 8.918 140.521 65.592 6650.104 15.876 291.753 4.474 0.44 386258. 0.7647 3.22 0.0306 0.0618 0.2119 0.1050 8.981 141.519 64.537 6697.353 15.989 287.061 4.371 0.44 386794. 0.7411 6.45 0.0612 0.1207 0.2082 0.1057 9.035 142.362 63.400 6737.234 16.084 282.002 4.268 0.44 387365. 0.7173 9.67 0.0919 0.1767 0.2042 0.1061 9.076 143.012 62.175 6767.989 16.157 276.552 4.167 0.44 387972. 0.6935 12.90 0.1225 0.2299 0.1998 0.1064 9.103 143.433 60.857 6787.931 16.205 270.691 4.066 0.44 388616. 0.6696 16.12 0.1531 0.2804 0.1952 0.1066 9.113 143.588 59.441 6795.265 16.222 264.396 3.968 0.44 389298. 0.6456 19.35 0.1837 0.3282 0.1902 0.1065 9.103 143.439 57.924 6788.207 16.206 257.648 3.870 0.44 390018. 0.6217 22.57 0.2143 0.3735 0.1849 0.1061 9.072 142.949 56.302 6765.006 16.150 250.433 3.775 0.44 390778. 0.5978 25.79 0.2450 0.4163 0.1792 0.1054 9.017 142.083 54.573 6724.033 16.052 242.742 3.681 0.44 391577. 0.5740 29.02 0.2756 0.4566 0.1732 0.1045 8.936 140.809 52.735 6663.738 15.909 234.567 3.589 0.44 392417. 0.5502 32.24 0.3062 0.4947 0.1668 0.1032 8.828 139.096 50.789 6582.694 15.715 225.908 3.500 0.44 393297. 0.5264 35.47 0.3368 0.5304 0.1600 0.1016 8.689 136.917 48.733 6479.565 15.469 216.764 3.411 0.44 394218. 0.5026 38.69 0.3674 0.5639 0.1529 0.0996 8.520 134.248 46.571 6353.270 15.167 207.147 3.325 0.44 395180. 0.4789 41.92 0.3980 0.5953 0.1455 0.0973 8.318 131.075 44.307 6203.081 14.809 197.076 3.240 0.44 396184. 0.4552 45.14 0.4287 0.6245 0.1377 0.0945 8.084 127.388 41.946 6028.589 14.392 186.577 3.156 0.45 397229. 0.4314 48.36 0.4593 0.6516 0.1297 0.0914 7.818 123.183 39.496 5829.583 13.917 175.679 3.073 0.45 398316. 0.4076 51.59 0.4899 0.6764 0.1214 0.0879 7.518 118.458 36.963 5605.992 13.383 164.411 2.991 0.45 399444. 0.3838 54.81 0.5205 0.6988 0.1128 0.0840 7.185 113.214 34.353 5357.829 12.791 152.802 2.908 0.45 400614. 0.3598 58.04 0.5511 0.7188 0.1040 0.0797 6.819 107.453 31.673 5085.197 12.140 140.882 2.825 0.45 401826. 0.3356 61.26 0.5818 0.7360 0.0950 0.0751 6.421 101.179 28.931 4788.268 11.431 128.684 2.740 0.45 403079. 0.3111 64.49 0.6124 0.7501 0.0858 0.0701 5.991 94.398 26.133 4467.340 10.665 116.238 2.653 0.45 404375. 0.2863 67.71 0.6430 0.7605 0.0765 0.0647 5.529 87.118 23.287 4122.830 9.843 103.580 2.562 0.45 405714. 0.2609 70.93 0.6736 0.7663 0.0670 0.0589 5.036 79.352 20.402 3755.327 8.965 90.748 2.464 0.45 407094. 0.2349 74.16 0.7042 0.7661 0.0574 0.0528 4.513 71.117 17.487 3365.605 8.035 77.781 2.357 0.45 408518. 0.2080 77.38 0.7349 0.7578 0.0478 0.0463 3.962 62.434 14.551 2954.685 7.054 64.724 2.234 0.45 409985. 0.1798 80.61 0.7655 0.7371 0.0381 0.0396 3.385 53.331 11.607 2523.860 6.025 51.628 2.086 0.45 411495. 0.1500 83.83 0.7961 0.6962 0.0285 0.0325 2.782 43.840 8.666 2074.740 4.953 38.545 1.894 0.46 413048. 0.1177 87.05 0.8267 0.6175 0.0188 0.0252 2.158 34.005 5.741 1609.287 3.842 25.534 1.618 0.46 414646. 0.0818 90.28 0.8573 0.4522 0.0093 0.0177 1.515 23.874 2.846 1129.818 2.697 12.659 1.143 0.46 416287. 0.0407 93.50 0.8879 -0.0029 0.0000 0.0100 0.855 13.479 -0.010 637.907 1.523 -0.044 -0.007 0.46 417959. 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 0.2183 0.1058 17.676 222.823 103.891 13181.282 25.174 462.107 3.575 0.55 482682. 0.7691 4.03 0.0306 0.0616 0.2149 0.1066 17.803 224.419 102.249 13275.710 25.355 454.804 3.493 0.55 483357. 0.7456 8.05 0.0612 0.1204 0.2111 0.1072 17.910 225.765 100.476 13355.335 25.507 446.915 3.412 0.55 484076. 0.7219 12.08 0.0917 0.1764 0.2071 0.1077 17.992 226.803 98.562 13416.727 25.624 438.405 3.332 0.55 484839. 0.6982 16.10 0.1223 0.2296 0.2028 0.1080 18.045 227.474 96.501 13456.413 25.700 429.238 3.253 0.55 485649. 0.6744 20.13 0.1529 0.2801 0.1981 0.1082 18.065 227.717 94.284 13470.791 25.727 419.376 3.175 0.55 486507. 0.6506 24.15 0.1835 0.3280 0.1931 0.1080 18.045 227.471 91.904 13456.264 25.700 408.789 3.098 0.55 487412. 0.6268 28.18 0.2141 0.3734 0.1878 0.1077 17.982 226.678 89.356 13409.330 25.610 397.454 3.022 0.55 488367. 0.6030 32.20 0.2446 0.4163 0.1821 0.1070 17.871 225.280 86.635 13326.662 25.452 385.353 2.949 0.55 489371. 0.5793 36.23 0.2752 0.4568 0.1760 0.1060 17.708 223.227 83.740 13205.190 25.220 372.477 2.876 0.55 490426. 0.5555 40.25 0.3058 0.4951 0.1695 0.1047 17.490 220.469 80.670 13042.049 24.908 358.821 2.806 0.55 491531. 0.5318 44.28 0.3364 0.5311 0.1627 0.1030 17.211 216.963 77.425 12834.613 24.512 344.389 2.736 0.55 492687. 0.5082 48.30 0.3670 0.5650 0.1555 0.1010 16.871 212.670 74.009 12580.708 24.027 329.194 2.668 0.56 493895. 0.4845 52.33 0.3976 0.5968 0.1480 0.0986 16.466 207.568 70.429 12278.849 23.451 313.267 2.602 0.56 495154. 0.4608 56.35 0.4281 0.6265 0.1402 0.0958 15.996 201.640 66.693 11928.221 22.781 296.650 2.536 0.56 496464. 0.4371 60.38 0.4587 0.6541 0.1320 0.0926 15.460 194.882 62.812 11528.448 22.018 279.389 2.471 0.56 497826. 0.4134 64.41 0.4893 0.6796 0.1236 0.0890 14.858 187.291 58.797 11079.385 21.160 261.529 2.407 0.56 499240. 0.3896 68.43 0.5199 0.7029 0.1149 0.0850 14.189 178.868 54.658 10581.104 20.208 243.119 2.343 0.56 500705. 0.3656 72.46 0.5505 0.7238 0.1059 0.0806 13.456 169.617 50.406 10033.822 19.163 224.206 2.279 0.56 502222. 0.3414 76.48 0.5810 0.7421 0.0968 0.0758 12.656 159.543 46.052 9437.903 18.025 204.839 2.213 0.56 503791. 0.3170 80.51 0.6116 0.7574 0.0874 0.0706 11.793 148.657 41.607 8793.952 16.795 185.069 2.146 0.56 505412. 0.2922 84.53 0.6422 0.7693 0.0779 0.0651 10.866 136.974 37.084 8102.802 15.475 164.951 2.076 0.56 507085. 0.2668 88.56 0.6728 0.7769 0.0683 0.0591 9.877 124.512 32.497 7365.613 14.067 144.545 2.001 0.56 508811. 0.2408 92.58 0.7034 0.7789 0.0585 0.0529 8.829 111.298 27.858 6583.935 12.574 123.913 1.919 0.57 510590. 0.2138 96.61 0.7339 0.7733 0.0487 0.0462 7.724 97.366 23.185 5759.777 11.000 103.128 1.826 0.57 512422. 0.1856 100.63 0.7645 0.7559 0.0389 0.0393 6.565 82.759 18.495 4895.709 9.350 82.266 1.714 0.57 514307. 0.1555 104.66 0.7951 0.7193 0.0290 0.0321 5.357 67.532 13.807 3994.940 7.630 61.415 1.568 0.57 516246. 0.1229 108.68 0.8257 0.6454 0.0192 0.0246 4.105 51.751 9.143 3061.403 5.847 40.668 1.355 0.57 518240. 0.0865 112.71 0.8563 0.4830 0.0095 0.0169 2.816 35.495 4.525 2099.757 4.010 20.127 0.977 0.57 520287. 0.0439 116.73 0.8868 -0.0070 -0.0001 0.0089 1.493 18.814 -0.034 1112.977 2.126 -0.149 -0.014 0.57 522370. 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 0.2222 0.1084 31.285 328.636 152.267 23328.887 37.129 677.284 2.960 0.66 578990. 0.7710 4.82 0.0305 0.0611 0.2188 0.1092 31.509 330.997 149.920 23496.479 37.396 666.844 2.894 0.66 579806. 0.7479 9.64 0.0610 0.1195 0.2151 0.1098 31.699 332.986 147.379 23637.723 37.621 655.542 2.828 0.66 580675. 0.7246 14.46 0.0915 0.1751 0.2111 0.1103 31.845 334.519 144.632 23746.492 37.794 643.324 2.763 0.66 581598. 0.7012 19.27 0.1220 0.2280 0.2067 0.1107 31.938 335.503 141.666 23816.377 37.905 630.132 2.698 0.66 582577. 0.6778 24.09 0.1525 0.2782 0.2021 0.1108 31.971 335.849 138.469 23840.955 37.944 615.910 2.634 0.66 583613. 0.6543 28.91 0.1830 0.3260 0.1971 0.1106 31.935 335.468 135.030 23813.867 37.901 600.612 2.572 0.66 584707. 0.6308 33.73 0.2135 0.3712 0.1917 0.1103 31.821 334.268 131.340 23728.744 37.765 584.199 2.511 0.66 585860. 0.6073 38.55 0.2440 0.4141 0.1859 0.1096 31.621 332.168 127.393 23579.641 37.528 566.646 2.450 0.66 587072. 0.5838 43.37 0.2746 0.4547 0.1798 0.1085 31.328 329.090 123.187 23361.111 37.180 547.936 2.392 0.66 588345. 0.5603 48.19 0.3051 0.4931 0.1733 0.1072 30.935 324.962 118.719 23068.104 36.714 528.064 2.334 0.66 589678. 0.5368 53.00 0.3356 0.5293 0.1664 0.1055 30.436 319.720 113.991 22696.012 36.122 507.032 2.278 0.67 591072. 0.5134 57.82 0.3661 0.5635 0.1591 0.1033 29.826 313.310 109.006 22240.990 35.398 484.860 2.223 0.67 592527. 0.4899 62.64 0.3966 0.5957 0.1514 0.1008 29.101 305.694 103.775 21700.342 34.537 461.592 2.169 0.67 594043. 0.4664 67.46 0.4271 0.6258 0.1435 0.0979 28.259 296.852 98.311 21072.656 33.538 437.286 2.116 0.67 595620. 0.4428 72.28 0.4576 0.6539 0.1352 0.0946 27.300 286.775 92.629 20357.322 32.400 412.013 2.064 0.67 597258. 0.4192 77.10 0.4881 0.6801 0.1266 0.0909 26.223 275.462 86.744 19554.223 31.122 385.839 2.012 0.67 598958. 0.3955 81.92 0.5186 0.7041 0.1177 0.0867 25.028 262.914 80.673 18663.516 29.704 358.834 1.961 0.67 600719. 0.3717 86.73 0.5491 0.7258 0.1086 0.0822 23.717 249.139 74.431 17685.672 28.148 331.070 1.909 0.67 602541. 0.3476 91.55 0.5796 0.7451 0.0993 0.0772 22.290 234.147 68.034 16621.396 26.454 302.616 1.857 0.67 604424. 0.3232 96.37 0.6101 0.7617 0.0897 0.0719 20.748 217.953 61.499 15471.845 24.624 273.548 1.803 0.67 606369. 0.2984 101.19 0.6406 0.7750 0.0800 0.0662 19.094 200.578 54.844 14238.460 22.661 243.945 1.747 0.68 608376. 0.2731 106.01 0.6711 0.7843 0.0702 0.0600 17.330 182.052 48.087 12923.353 20.568 213.891 1.688 0.68 610444. 0.2470 110.83 0.7016 0.7885 0.0602 0.0536 15.461 162.415 41.250 11529.331 18.349 183.481 1.623 0.68 612575. 0.2200 115.64 0.7321 0.7853 0.0501 0.0467 13.491 141.717 34.356 10060.062 16.011 152.815 1.549 0.68 614768. 0.1916 120.46 0.7626 0.7712 0.0400 0.0396 11.426 120.026 27.430 8520.310 13.560 122.009 1.460 0.68 617025. 0.1614 125.28 0.7932 0.7384 0.0299 0.0321 9.275 97.428 20.501 6916.095 11.007 91.189 1.344 0.68 619344. 0.1285 130.10 0.8237 0.6695 0.0198 0.0244 7.047 74.027 13.600 5254.944 8.364 60.493 1.174 0.68 621728. 0.0914 134.92 0.8542 0.5115 0.0099 0.0165 4.755 49.952 6.761 3545.965 5.644 30.073 0.865 0.69 624174. 0.0475 139.74 0.8847 0.0008 0.0000 0.0083 2.408 25.296 0.005 1795.690 2.858 0.022 0.001 0.69 626664. 0.0000