242 lines
43 KiB
Plaintext
242 lines
43 KiB
Plaintext
28x20-4 (28x20-4.dat)
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v2022-0915
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Simulation Date: 09/22/2022
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AIRFOIL AERO DATA GENERATED USING: POLAR DIAGRAMS
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====== PERFORMANCE DATA (versus advance ratio and MPH) ======
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DEFINITIONS:
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J=V/nD (advance ratio)
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Ct=T/(rho * n**2 * D**4) (thrust coef.)
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Cp=P/(rho * n**3 * D**5) (power coef.)
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Pe=Ct*J/Cp (efficiency)
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V (model speed in MPH)
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Mach (at prop tip)
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Reyn (at 75% of span)
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FOM (Figure of Merit)
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PROP RPM = 1000
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V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
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(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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PROP RPM = 2000
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V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
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(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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PROP RPM = 3000
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V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
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(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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PROP RPM = 4000
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V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
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(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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PROP RPM = 5000
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V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
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(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
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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
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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
|
|
|
|
|
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