464 lines
82 KiB
Plaintext
464 lines
82 KiB
Plaintext
15.75x13-3 (1575x13-3.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 0.1702 0.0947 0.007 0.466 0.334 5.509 0.053 1.484 27.473 0.06 27875. 0.5913
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0.51 0.0343 0.0600 0.1687 0.0963 0.008 0.474 0.331 5.602 0.053 1.472 26.785 0.06 27909. 0.5740
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1.02 0.0686 0.1170 0.1671 0.0979 0.008 0.481 0.328 5.695 0.054 1.457 26.089 0.06 27946. 0.5563
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1.53 0.1028 0.1707 0.1652 0.0995 0.008 0.489 0.324 5.787 0.055 1.441 25.389 0.06 27986. 0.5383
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2.05 0.1371 0.2214 0.1631 0.1010 0.008 0.497 0.320 5.875 0.056 1.422 24.689 0.06 28031. 0.5201
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2.56 0.1714 0.2689 0.1607 0.1024 0.008 0.503 0.315 5.957 0.057 1.402 23.992 0.06 28079. 0.5017
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3.07 0.2057 0.3134 0.1580 0.1037 0.008 0.510 0.310 6.031 0.058 1.378 23.301 0.06 28132. 0.4832
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3.58 0.2400 0.3549 0.1550 0.1048 0.008 0.515 0.304 6.093 0.058 1.351 22.617 0.06 28189. 0.4645
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4.09 0.2743 0.3935 0.1515 0.1056 0.008 0.519 0.297 6.142 0.059 1.322 21.943 0.06 28250. 0.4456
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4.60 0.3085 0.4293 0.1477 0.1062 0.008 0.522 0.290 6.174 0.059 1.288 21.279 0.06 28316. 0.4267
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5.11 0.3428 0.4623 0.1435 0.1064 0.008 0.523 0.281 6.186 0.059 1.251 20.626 0.06 28387. 0.4076
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5.62 0.3771 0.4927 0.1388 0.1062 0.008 0.522 0.272 6.176 0.059 1.210 19.984 0.06 28462. 0.3884
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6.14 0.4114 0.5205 0.1336 0.1056 0.008 0.519 0.262 6.139 0.059 1.165 19.352 0.06 28541. 0.3690
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6.65 0.4457 0.5458 0.1279 0.1045 0.008 0.513 0.251 6.075 0.058 1.116 18.729 0.06 28625. 0.3495
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7.16 0.4799 0.5684 0.1218 0.1029 0.008 0.506 0.239 5.982 0.057 1.062 18.112 0.06 28714. 0.3298
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7.67 0.5142 0.5883 0.1153 0.1008 0.008 0.495 0.226 5.860 0.056 1.006 17.498 0.06 28807. 0.3100
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8.18 0.5485 0.6055 0.1084 0.0982 0.008 0.483 0.213 5.711 0.055 0.945 16.882 0.06 28905. 0.2900
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8.69 0.5828 0.6196 0.1012 0.0952 0.007 0.468 0.198 5.535 0.053 0.883 16.260 0.06 29007. 0.2698
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9.20 0.6171 0.6304 0.0937 0.0917 0.007 0.451 0.184 5.334 0.051 0.817 15.624 0.06 29114. 0.2495
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9.71 0.6514 0.6374 0.0860 0.0878 0.007 0.432 0.169 5.108 0.049 0.750 14.967 0.06 29225. 0.2289
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10.23 0.6856 0.6402 0.0780 0.0835 0.007 0.411 0.153 4.858 0.046 0.680 14.280 0.06 29340. 0.2081
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10.74 0.7199 0.6378 0.0698 0.0788 0.006 0.387 0.137 4.583 0.044 0.609 13.550 0.06 29460. 0.1868
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11.25 0.7542 0.6293 0.0615 0.0737 0.006 0.362 0.121 4.286 0.041 0.536 12.760 0.06 29584. 0.1651
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11.76 0.7885 0.6128 0.0530 0.0682 0.005 0.335 0.104 3.965 0.038 0.462 11.887 0.06 29712. 0.1428
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12.27 0.8228 0.5861 0.0444 0.0623 0.005 0.306 0.087 3.621 0.035 0.387 10.894 0.06 29845. 0.1197
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12.78 0.8571 0.5452 0.0356 0.0560 0.004 0.275 0.070 3.255 0.031 0.311 9.729 0.06 29982. 0.0958
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13.29 0.8913 0.4839 0.0268 0.0493 0.004 0.242 0.052 2.867 0.027 0.233 8.303 0.06 30123. 0.0709
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13.81 0.9256 0.3912 0.0179 0.0423 0.003 0.208 0.035 2.459 0.023 0.156 6.464 0.07 30268. 0.0451
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14.32 0.9599 0.2459 0.0089 0.0349 0.003 0.172 0.018 2.031 0.019 0.078 3.918 0.07 30417. 0.0193
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14.83 0.9942 0.0012 0.0000 0.0273 0.002 0.134 0.000 1.585 0.015 0.000 0.019 0.07 30570. 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 0.1710 0.0867 0.054 1.704 1.341 40.323 0.193 5.966 15.088 0.12 55750. 0.6511
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1.03 0.0345 0.0663 0.1696 0.0884 0.055 1.737 1.330 41.104 0.196 5.916 14.677 0.12 55817. 0.6306
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2.06 0.0691 0.1288 0.1680 0.0900 0.056 1.770 1.317 41.891 0.200 5.860 14.263 0.12 55892. 0.6099
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3.09 0.1036 0.1876 0.1661 0.0917 0.057 1.803 1.303 42.669 0.204 5.795 13.850 0.13 55974. 0.5890
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4.12 0.1381 0.2427 0.1640 0.0933 0.058 1.835 1.286 43.422 0.207 5.722 13.438 0.13 56064. 0.5679
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5.15 0.1726 0.2942 0.1617 0.0949 0.059 1.865 1.268 44.131 0.211 5.640 13.031 0.13 56162. 0.5467
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6.18 0.2072 0.3422 0.1590 0.0962 0.060 1.892 1.247 44.774 0.214 5.546 12.630 0.13 56268. 0.5254
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7.21 0.2417 0.3868 0.1559 0.0974 0.061 1.916 1.223 45.330 0.216 5.440 12.237 0.13 56383. 0.5041
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8.24 0.2762 0.4281 0.1525 0.0984 0.061 1.934 1.196 45.774 0.219 5.320 11.852 0.13 56508. 0.4829
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9.27 0.3108 0.4664 0.1487 0.0991 0.062 1.947 1.166 46.082 0.220 5.186 11.476 0.13 56641. 0.4617
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10.30 0.3453 0.5017 0.1444 0.0994 0.062 1.954 1.132 46.229 0.221 5.037 11.110 0.13 56783. 0.4405
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11.33 0.3798 0.5341 0.1396 0.0993 0.062 1.952 1.095 46.188 0.221 4.871 10.754 0.13 56935. 0.4193
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12.36 0.4144 0.5639 0.1344 0.0987 0.062 1.941 1.054 45.936 0.219 4.688 10.407 0.13 57096. 0.3981
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13.39 0.4489 0.5911 0.1287 0.0977 0.061 1.921 1.009 45.453 0.217 4.488 10.069 0.13 57266. 0.3768
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14.42 0.4834 0.6157 0.1225 0.0962 0.060 1.890 0.961 44.731 0.214 4.272 9.739 0.13 57446. 0.3556
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15.45 0.5179 0.6377 0.1159 0.0941 0.059 1.850 0.909 43.773 0.209 4.042 9.416 0.13 57635. 0.3344
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16.48 0.5525 0.6571 0.1089 0.0915 0.057 1.800 0.854 42.584 0.203 3.798 9.096 0.13 57833. 0.3132
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17.51 0.5870 0.6738 0.1016 0.0885 0.055 1.740 0.797 41.173 0.197 3.544 8.778 0.13 58040. 0.2919
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18.54 0.6215 0.6874 0.0940 0.0850 0.053 1.671 0.737 39.546 0.189 3.280 8.458 0.13 58256. 0.2706
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19.57 0.6561 0.6977 0.0862 0.0811 0.051 1.594 0.676 37.707 0.180 3.007 8.133 0.13 58480. 0.2491
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20.60 0.6906 0.7043 0.0782 0.0767 0.048 1.507 0.613 35.661 0.170 2.727 7.798 0.13 58714. 0.2275
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21.63 0.7251 0.7062 0.0699 0.0718 0.045 1.412 0.549 33.409 0.160 2.440 7.448 0.13 58956. 0.2055
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22.66 0.7597 0.7027 0.0615 0.0665 0.042 1.308 0.483 30.954 0.148 2.147 7.074 0.13 59208. 0.1831
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23.69 0.7942 0.6920 0.0530 0.0608 0.038 1.196 0.416 28.299 0.135 1.849 6.663 0.13 59468. 0.1601
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24.72 0.8287 0.6716 0.0443 0.0547 0.034 1.075 0.348 25.447 0.121 1.547 6.197 0.13 59736. 0.1361
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25.75 0.8632 0.6373 0.0356 0.0482 0.030 0.947 0.279 22.401 0.107 1.240 5.646 0.13 60013. 0.1111
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26.78 0.8978 0.5817 0.0267 0.0412 0.026 0.810 0.209 19.170 0.092 0.931 4.954 0.13 60299. 0.0845
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27.81 0.9323 0.4897 0.0178 0.0339 0.021 0.666 0.140 15.760 0.075 0.621 4.017 0.13 60594. 0.0559
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28.84 0.9668 0.3280 0.0089 0.0262 0.016 0.515 0.070 12.185 0.058 0.310 2.594 0.13 60896. 0.0255
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29.87 1.0014 -0.0002 0.0000 0.0182 0.011 0.357 0.000 8.456 0.040 0.000 -0.001 0.13 61205. 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 0.1716 0.0835 0.176 3.692 3.028 131.047 0.417 13.467 10.479 0.19 83622. 0.6793
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1.55 0.0346 0.0692 0.1702 0.0852 0.179 3.768 3.003 133.751 0.426 13.356 10.183 0.19 83724. 0.6574
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3.10 0.0693 0.1343 0.1686 0.0869 0.183 3.845 2.975 136.482 0.434 13.231 9.885 0.19 83836. 0.6352
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4.65 0.1039 0.1954 0.1667 0.0887 0.187 3.921 2.942 139.187 0.443 13.088 9.589 0.19 83960. 0.6128
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6.20 0.1385 0.2525 0.1647 0.0903 0.190 3.995 2.906 141.811 0.451 12.925 9.294 0.19 84095. 0.5903
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7.75 0.1732 0.3058 0.1623 0.0919 0.193 4.065 2.864 144.289 0.459 12.741 9.004 0.19 84243. 0.5677
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9.30 0.2078 0.3554 0.1596 0.0933 0.197 4.129 2.817 146.549 0.466 12.530 8.719 0.19 84403. 0.5452
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10.85 0.2424 0.4013 0.1566 0.0946 0.199 4.184 2.764 148.514 0.473 12.293 8.440 0.19 84577. 0.5227
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12.40 0.2770 0.4439 0.1532 0.0956 0.201 4.229 2.703 150.101 0.478 12.024 8.169 0.19 84764. 0.5004
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13.95 0.3117 0.4832 0.1493 0.0963 0.203 4.261 2.635 151.225 0.481 11.722 7.905 0.19 84965. 0.4781
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15.49 0.3463 0.5195 0.1450 0.0967 0.204 4.277 2.560 151.798 0.483 11.386 7.648 0.19 85180. 0.4559
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17.04 0.3809 0.5530 0.1403 0.0966 0.203 4.275 2.476 151.730 0.483 11.011 7.400 0.19 85408. 0.4338
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18.59 0.4156 0.5836 0.1350 0.0961 0.202 4.253 2.383 150.936 0.480 10.598 7.160 0.19 85651. 0.4117
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20.14 0.4502 0.6117 0.1293 0.0951 0.200 4.208 2.281 149.352 0.475 10.146 6.927 0.19 85908. 0.3898
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21.69 0.4848 0.6373 0.1230 0.0936 0.197 4.140 2.171 146.946 0.468 9.656 6.701 0.19 86179. 0.3678
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23.24 0.5195 0.6603 0.1164 0.0915 0.193 4.049 2.054 143.724 0.457 9.134 6.481 0.19 86464. 0.3460
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24.79 0.5541 0.6809 0.1094 0.0890 0.187 3.936 1.930 139.709 0.445 8.584 6.265 0.19 86763. 0.3242
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26.34 0.5887 0.6989 0.1020 0.0859 0.181 3.801 1.800 134.924 0.429 8.008 6.052 0.19 87075. 0.3025
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27.89 0.6233 0.7140 0.0944 0.0824 0.174 3.645 1.666 129.390 0.412 7.410 5.840 0.19 87400. 0.2808
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29.44 0.6580 0.7261 0.0865 0.0784 0.165 3.469 1.527 123.121 0.392 6.793 5.626 0.19 87739. 0.2590
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30.99 0.6926 0.7347 0.0785 0.0740 0.156 3.272 1.385 116.127 0.370 6.159 5.408 0.19 88091. 0.2371
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32.54 0.7272 0.7392 0.0702 0.0691 0.145 3.055 1.239 108.419 0.345 5.510 5.182 0.19 88457. 0.2149
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34.09 0.7619 0.7387 0.0618 0.0637 0.134 2.817 1.090 100.001 0.318 4.848 4.943 0.19 88836. 0.1923
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35.64 0.7965 0.7316 0.0532 0.0579 0.122 2.561 0.938 90.884 0.289 4.174 4.683 0.19 89228. 0.1690
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37.19 0.8311 0.7156 0.0445 0.0516 0.109 2.284 0.785 81.079 0.258 3.490 4.389 0.19 89633. 0.1449
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38.74 0.8658 0.6864 0.0357 0.0450 0.095 1.989 0.629 70.601 0.225 2.798 4.042 0.19 90051. 0.1194
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40.29 0.9004 0.6363 0.0268 0.0379 0.080 1.676 0.472 59.474 0.189 2.101 3.603 0.19 90482. 0.0923
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41.84 0.9350 0.5489 0.0178 0.0304 0.064 1.345 0.315 47.728 0.152 1.401 2.993 0.20 90926. 0.0626
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43.39 0.9697 0.3834 0.0089 0.0226 0.047 0.998 0.157 35.405 0.113 0.700 2.016 0.20 91382. 0.0298
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44.93 1.0043 0.0009 0.0000 0.0144 0.030 0.635 0.000 22.543 0.072 0.001 0.005 0.20 91845. 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 0.1721 0.0818 0.408 6.433 5.399 304.436 0.727 24.017 8.044 0.25 111492. 0.6964
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2.07 0.0347 0.0709 0.1707 0.0836 0.417 6.571 5.356 310.969 0.742 23.823 7.812 0.25 111628. 0.6736
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4.14 0.0694 0.1375 0.1691 0.0853 0.426 6.710 5.307 317.572 0.758 23.604 7.579 0.25 111778. 0.6505
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6.21 0.1041 0.2000 0.1674 0.0871 0.435 6.849 5.250 324.127 0.774 23.353 7.347 0.25 111943. 0.6272
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8.28 0.1388 0.2583 0.1653 0.0888 0.443 6.984 5.186 330.497 0.789 23.068 7.117 0.25 112124. 0.6039
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10.35 0.1734 0.3126 0.1630 0.0904 0.451 7.111 5.113 336.526 0.803 22.742 6.891 0.25 112321. 0.5805
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12.42 0.2081 0.3630 0.1603 0.0919 0.459 7.228 5.030 342.042 0.817 22.372 6.670 0.25 112536. 0.5573
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14.49 0.2428 0.4098 0.1573 0.0932 0.465 7.329 4.935 346.857 0.828 21.951 6.453 0.25 112768. 0.5341
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16.56 0.2775 0.4531 0.1539 0.0943 0.470 7.412 4.828 350.770 0.837 21.475 6.243 0.25 113018. 0.5111
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18.62 0.3122 0.4931 0.1501 0.0950 0.474 7.471 4.708 353.576 0.844 20.940 6.039 0.25 113287. 0.4882
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20.69 0.3469 0.5300 0.1458 0.0954 0.476 7.503 4.573 355.061 0.848 20.340 5.842 0.25 113574. 0.4654
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22.76 0.3816 0.5639 0.1410 0.0954 0.476 7.502 4.423 355.009 0.848 19.674 5.651 0.25 113881. 0.4428
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24.83 0.4163 0.5952 0.1357 0.0949 0.474 7.464 4.257 353.216 0.843 18.937 5.467 0.25 114206. 0.4203
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26.90 0.4509 0.6238 0.1299 0.0939 0.469 7.386 4.076 349.521 0.834 18.130 5.289 0.25 114549. 0.3978
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28.97 0.4856 0.6500 0.1237 0.0924 0.461 7.266 3.880 343.848 0.821 17.256 5.117 0.25 114912. 0.3755
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31.04 0.5203 0.6737 0.1170 0.0903 0.451 7.104 3.670 336.210 0.803 16.323 4.951 0.25 115293. 0.3533
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33.11 0.5550 0.6950 0.1099 0.0878 0.438 6.902 3.448 326.657 0.780 15.339 4.788 0.25 115692. 0.3313
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35.18 0.5897 0.7139 0.1025 0.0847 0.423 6.661 3.217 315.247 0.753 14.309 4.629 0.25 116110. 0.3093
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37.25 0.6244 0.7300 0.0949 0.0812 0.405 6.382 2.977 302.025 0.721 13.241 4.470 0.25 116545. 0.2874
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39.32 0.6591 0.7433 0.0870 0.0771 0.385 6.065 2.729 287.026 0.685 12.138 4.312 0.26 116999. 0.2654
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41.39 0.6938 0.7533 0.0789 0.0726 0.362 5.711 2.474 270.274 0.645 11.005 4.152 0.26 117470. 0.2433
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43.46 0.7284 0.7596 0.0705 0.0677 0.338 5.320 2.213 251.787 0.601 9.845 3.987 0.26 117959. 0.2210
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45.53 0.7631 0.7611 0.0621 0.0622 0.311 4.894 1.947 231.584 0.553 8.661 3.814 0.26 118466. 0.1983
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47.60 0.7978 0.7566 0.0534 0.0563 0.281 4.431 1.676 209.685 0.501 7.457 3.626 0.26 118990. 0.1749
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49.67 0.8325 0.7438 0.0447 0.0500 0.250 3.933 1.402 186.117 0.444 6.235 3.416 0.26 119532. 0.1507
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51.73 0.8672 0.7185 0.0358 0.0432 0.216 3.400 1.124 160.920 0.384 5.000 3.168 0.26 120091. 0.1251
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53.80 0.9019 0.6731 0.0269 0.0360 0.180 2.835 0.844 134.149 0.320 3.754 2.854 0.26 120668. 0.0977
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55.87 0.9366 0.5905 0.0179 0.0284 0.142 2.237 0.563 105.880 0.253 2.503 2.411 0.26 121261. 0.0674
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57.94 0.9713 0.4255 0.0090 0.0205 0.102 1.611 0.281 76.218 0.182 1.252 1.675 0.26 121871. 0.0331
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60.01 1.0059 0.0026 0.0000 0.0122 0.061 0.956 0.001 45.239 0.108 0.004 0.010 0.26 122489. 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 0.1727 0.0809 0.789 9.940 8.465 587.988 1.123 37.654 6.530 0.31 139359. 0.7078
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2.59 0.0347 0.0720 0.1713 0.0827 0.806 10.159 8.399 600.971 1.148 37.359 6.339 0.31 139529. 0.6844
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5.18 0.0695 0.1396 0.1698 0.0845 0.824 10.381 8.323 614.115 1.173 37.023 6.148 0.31 139717. 0.6608
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7.77 0.1042 0.2030 0.1680 0.0863 0.841 10.602 8.237 627.182 1.198 36.639 5.957 0.31 139923. 0.6370
|
|
10.36 0.1390 0.2620 0.1660 0.0880 0.858 10.817 8.138 639.901 1.222 36.200 5.769 0.31 140150. 0.6131
|
|
12.95 0.1737 0.3170 0.1637 0.0897 0.874 11.021 8.025 651.963 1.245 35.697 5.583 0.31 140397. 0.5893
|
|
15.54 0.2084 0.3681 0.1611 0.0912 0.889 11.208 7.896 663.025 1.266 35.123 5.402 0.31 140666. 0.5655
|
|
18.13 0.2432 0.4154 0.1581 0.0925 0.902 11.372 7.750 672.709 1.285 34.470 5.225 0.31 140957. 0.5419
|
|
20.72 0.2779 0.4591 0.1547 0.0936 0.913 11.506 7.583 680.619 1.300 33.730 5.053 0.31 141271. 0.5185
|
|
23.31 0.3126 0.4995 0.1509 0.0944 0.920 11.602 7.396 686.339 1.311 32.895 4.887 0.31 141607. 0.4952
|
|
25.90 0.3474 0.5368 0.1466 0.0948 0.925 11.655 7.185 689.446 1.317 31.959 4.727 0.31 141968. 0.4720
|
|
28.50 0.3821 0.5712 0.1418 0.0949 0.925 11.656 6.951 689.508 1.317 30.916 4.572 0.31 142352. 0.4491
|
|
31.09 0.4169 0.6028 0.1365 0.0944 0.920 11.598 6.691 686.118 1.310 29.761 4.423 0.32 142759. 0.4263
|
|
33.68 0.4516 0.6318 0.1307 0.0934 0.910 11.477 6.406 678.957 1.297 28.495 4.280 0.32 143191. 0.4036
|
|
36.27 0.4863 0.6584 0.1244 0.0919 0.896 11.290 6.098 667.873 1.276 27.123 4.141 0.32 143645. 0.3810
|
|
38.86 0.5211 0.6826 0.1177 0.0898 0.876 11.037 5.768 652.885 1.247 25.658 4.007 0.32 144123. 0.3586
|
|
41.45 0.5558 0.7045 0.1106 0.0872 0.850 10.719 5.420 634.095 1.211 24.110 3.877 0.32 144624. 0.3363
|
|
44.04 0.5905 0.7240 0.1032 0.0841 0.820 10.339 5.057 611.613 1.168 22.492 3.750 0.32 145148. 0.3142
|
|
46.63 0.6253 0.7409 0.0954 0.0806 0.785 9.898 4.679 585.529 1.118 20.812 3.624 0.32 145694. 0.2921
|
|
49.22 0.6600 0.7551 0.0875 0.0765 0.745 9.397 4.289 555.910 1.062 19.077 3.499 0.32 146263. 0.2700
|
|
51.81 0.6948 0.7662 0.0793 0.0719 0.701 8.838 3.888 522.803 0.998 17.294 3.373 0.32 146853. 0.2478
|
|
54.40 0.7295 0.7737 0.0709 0.0669 0.652 8.220 3.478 486.245 0.929 15.469 3.244 0.32 147467. 0.2254
|
|
56.99 0.7642 0.7768 0.0624 0.0614 0.598 7.544 3.059 446.271 0.852 13.607 3.109 0.32 148102. 0.2026
|
|
59.58 0.7990 0.7743 0.0537 0.0554 0.540 6.811 2.633 402.921 0.770 11.713 2.964 0.32 148759. 0.1792
|
|
62.17 0.8337 0.7638 0.0449 0.0490 0.478 6.022 2.201 356.251 0.680 9.791 2.802 0.32 149438. 0.1549
|
|
64.76 0.8684 0.7416 0.0360 0.0421 0.411 5.178 1.764 306.337 0.585 7.847 2.612 0.32 150139. 0.1293
|
|
67.35 0.9032 0.6999 0.0270 0.0348 0.340 4.282 1.324 253.291 0.484 5.888 2.370 0.33 150862. 0.1016
|
|
69.94 0.9379 0.6214 0.0180 0.0271 0.265 3.335 0.881 197.270 0.377 3.920 2.027 0.33 151605. 0.0709
|
|
72.53 0.9727 0.4572 0.0090 0.0191 0.186 2.341 0.439 138.478 0.264 1.953 1.438 0.33 152369. 0.0355
|
|
75.12 1.0074 -0.0045 0.0000 0.0106 0.103 1.302 -0.002 77.043 0.147 -0.010 -0.014 0.33 153142. 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 0.1734 0.0804 1.355 14.233 12.237 1010.385 1.608 54.431 5.493 0.37 167221. 0.7159
|
|
3.13 0.0350 0.0731 0.1720 0.0823 1.386 14.557 12.144 1033.355 1.645 54.016 5.330 0.37 167426. 0.6920
|
|
6.26 0.0700 0.1418 0.1705 0.0841 1.417 14.885 12.037 1056.644 1.682 53.541 5.167 0.37 167653. 0.6679
|
|
9.39 0.1049 0.2060 0.1688 0.0860 1.448 15.212 11.915 1079.827 1.719 52.997 5.005 0.38 167903. 0.6436
|
|
12.52 0.1399 0.2659 0.1668 0.0878 1.478 15.530 11.774 1102.421 1.755 52.371 4.844 0.38 168177. 0.6193
|
|
15.65 0.1749 0.3215 0.1645 0.0895 1.507 15.832 11.613 1123.870 1.789 51.653 4.687 0.38 168477. 0.5950
|
|
18.78 0.2099 0.3732 0.1619 0.0910 1.534 16.109 11.427 1143.549 1.820 50.829 4.532 0.38 168803. 0.5708
|
|
21.91 0.2448 0.4209 0.1589 0.0924 1.557 16.352 11.216 1160.783 1.847 49.887 4.382 0.38 169156. 0.5468
|
|
25.04 0.2798 0.4651 0.1555 0.0935 1.575 16.550 10.975 1174.850 1.870 48.816 4.237 0.38 169537. 0.5229
|
|
28.17 0.3148 0.5059 0.1516 0.0943 1.589 16.693 10.702 1185.005 1.886 47.604 4.096 0.38 169946. 0.4993
|
|
31.30 0.3498 0.5435 0.1473 0.0948 1.596 16.770 10.396 1190.483 1.895 46.242 3.961 0.38 170384. 0.4758
|
|
34.43 0.3847 0.5782 0.1424 0.0948 1.597 16.771 10.054 1190.511 1.895 44.720 3.830 0.38 170850. 0.4525
|
|
37.56 0.4197 0.6101 0.1371 0.0943 1.588 16.684 9.675 1184.365 1.885 43.033 3.705 0.38 171346. 0.4293
|
|
40.69 0.4547 0.6394 0.1312 0.0933 1.571 16.503 9.258 1171.487 1.864 41.181 3.585 0.38 171870. 0.4063
|
|
43.82 0.4897 0.6663 0.1248 0.0917 1.544 16.223 8.807 1151.627 1.833 39.173 3.469 0.38 172423. 0.3835
|
|
46.95 0.5247 0.6909 0.1179 0.0896 1.508 15.846 8.325 1124.833 1.790 37.028 3.357 0.38 173003. 0.3608
|
|
50.08 0.5596 0.7131 0.1107 0.0869 1.463 15.373 7.815 1091.292 1.737 34.762 3.248 0.38 173612. 0.3383
|
|
53.21 0.5946 0.7330 0.1032 0.0837 1.410 14.808 7.283 1051.200 1.673 32.393 3.142 0.38 174249. 0.3159
|
|
56.34 0.6296 0.7504 0.0953 0.0800 1.347 14.153 6.730 1004.714 1.599 29.933 3.038 0.38 174912. 0.2936
|
|
59.47 0.6646 0.7650 0.0872 0.0758 1.277 13.410 6.159 951.949 1.515 27.394 2.934 0.38 175603. 0.2713
|
|
62.60 0.6995 0.7767 0.0789 0.0711 1.198 12.580 5.572 892.988 1.421 24.785 2.830 0.38 176322. 0.2489
|
|
65.73 0.7345 0.7849 0.0704 0.0659 1.110 11.663 4.972 827.893 1.318 22.114 2.724 0.38 177067. 0.2263
|
|
68.86 0.7695 0.7887 0.0618 0.0602 1.015 10.660 4.359 756.731 1.204 19.389 2.613 0.39 177839. 0.2032
|
|
71.99 0.8045 0.7869 0.0529 0.0541 0.911 9.573 3.736 679.573 1.082 16.617 2.493 0.39 178637. 0.1796
|
|
75.12 0.8394 0.7772 0.0440 0.0475 0.800 8.403 3.104 596.523 0.949 13.806 2.360 0.39 179462. 0.1549
|
|
78.25 0.8744 0.7554 0.0349 0.0404 0.681 7.152 2.465 507.726 0.808 10.964 2.202 0.39 180314. 0.1288
|
|
81.38 0.9094 0.7128 0.0258 0.0329 0.554 5.824 1.821 413.394 0.658 8.099 1.998 0.39 181191. 0.1004
|
|
84.51 0.9444 0.6290 0.0166 0.0250 0.421 4.421 1.175 313.819 0.499 5.225 1.698 0.39 182095. 0.0685
|
|
87.64 0.9794 0.4399 0.0075 0.0167 0.281 2.950 0.529 209.388 0.333 2.351 1.145 0.39 183022. 0.0310
|
|
90.77 1.0143
|
|
|
|
|
|
|
|
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 0.1741 0.0803 2.148 19.343 16.729 1601.941 2.185 74.410 4.737 0.44 195078. 0.7218
|
|
3.63 0.0348 0.0732 0.1728 0.0822 2.198 19.789 16.607 1638.873 2.236 73.870 4.596 0.44 195315. 0.6978
|
|
7.26 0.0696 0.1419 0.1714 0.0840 2.248 20.242 16.468 1676.386 2.287 73.250 4.456 0.44 195578. 0.6736
|
|
10.89 0.1043 0.2061 0.1697 0.0859 2.298 20.694 16.308 1713.806 2.338 72.537 4.316 0.44 195868. 0.6493
|
|
14.52 0.1391 0.2660 0.1678 0.0878 2.347 21.135 16.123 1750.369 2.388 71.715 4.178 0.44 196185. 0.6250
|
|
18.16 0.1739 0.3217 0.1656 0.0895 2.394 21.555 15.910 1785.188 2.435 70.767 4.042 0.44 196532. 0.6007
|
|
21.79 0.2087 0.3734 0.1630 0.0911 2.437 21.943 15.665 1817.268 2.479 69.676 3.910 0.44 196910. 0.5765
|
|
25.42 0.2435 0.4213 0.1601 0.0925 2.475 22.284 15.383 1845.530 2.518 68.425 3.781 0.44 197318. 0.5525
|
|
29.05 0.2782 0.4656 0.1568 0.0937 2.506 22.565 15.063 1868.822 2.549 66.999 3.656 0.44 197759. 0.5286
|
|
32.68 0.3130 0.5065 0.1530 0.0946 2.529 22.772 14.699 1885.951 2.573 65.381 3.535 0.44 198233. 0.5049
|
|
36.31 0.3478 0.5442 0.1487 0.0950 2.542 22.890 14.289 1895.692 2.586 63.557 3.419 0.44 198740. 0.4815
|
|
39.94 0.3826 0.5791 0.1439 0.0951 2.544 22.903 13.830 1896.818 2.588 61.515 3.307 0.44 199280. 0.4582
|
|
43.57 0.4174 0.6112 0.1386 0.0947 2.532 22.799 13.320 1888.164 2.576 59.246 3.200 0.44 199853. 0.4351
|
|
47.20 0.4521 0.6408 0.1328 0.0937 2.506 22.565 12.759 1868.812 2.549 56.751 3.097 0.44 200460. 0.4121
|
|
50.84 0.4869 0.6680 0.1264 0.0922 2.465 22.197 12.149 1838.319 2.508 54.040 2.998 0.44 201099. 0.3893
|
|
54.47 0.5217 0.6930 0.1197 0.0901 2.409 21.695 11.497 1796.722 2.451 51.137 2.902 0.44 201771. 0.3666
|
|
58.10 0.5565 0.7157 0.1125 0.0875 2.339 21.062 10.807 1744.311 2.380 48.068 2.810 0.44 202476. 0.3442
|
|
61.73 0.5913 0.7361 0.1050 0.0843 2.255 20.302 10.084 1681.406 2.294 44.854 2.720 0.45 203212. 0.3218
|
|
65.36 0.6260 0.7542 0.0971 0.0806 2.157 19.419 9.333 1608.268 2.194 41.514 2.632 0.45 203980. 0.2996
|
|
68.99 0.6608 0.7697 0.0891 0.0765 2.045 18.415 8.557 1525.095 2.081 38.063 2.545 0.45 204779. 0.2774
|
|
72.62 0.6956 0.7825 0.0808 0.0718 1.920 17.291 7.760 1432.021 1.954 34.515 2.458 0.45 205609. 0.2551
|
|
76.25 0.7304 0.7920 0.0723 0.0666 1.782 16.049 6.943 1329.143 1.813 30.881 2.369 0.45 206471. 0.2326
|
|
79.88 0.7652 0.7976 0.0636 0.0610 1.631 14.690 6.109 1216.573 1.660 27.171 2.277 0.45 207363. 0.2097
|
|
83.52 0.8000 0.7981 0.0547 0.0549 1.468 13.215 5.260 1094.419 1.493 23.395 2.180 0.45 208286. 0.1863
|
|
87.15 0.8347 0.7916 0.0458 0.0483 1.291 11.626 4.398 962.835 1.313 19.564 2.072 0.45 209240. 0.1619
|
|
90.78 0.8695 0.7744 0.0367 0.0412 1.102 9.926 3.527 822.040 1.121 15.687 1.946 0.45 210224. 0.1362
|
|
94.41 0.9043 0.7394 0.0276 0.0337 0.902 8.118 2.648 672.349 0.917 11.778 1.786 0.46 211238. 0.1083
|
|
98.04 0.9391 0.6692 0.0184 0.0258 0.690 6.209 1.765 514.207 0.701 7.851 1.557 0.46 212282. 0.0771
|
|
101.67 0.9739 0.5121 0.0092 0.0175 0.467 4.204 0.882 348.205 0.475 3.923 1.149 0.46 213354. 0.0402
|
|
105.30 1.0086 0.0004 0.0000 0.0088 0.234 2.108 0.000 174.597 0.238 0.002 0.001 0.46 214433. 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 0.1750 0.0804 3.212 25.305 21.957 2395.102 2.859 97.665 4.158 0.50 222928. 0.7259
|
|
4.15 0.0348 0.0735 0.1738 0.0823 3.287 25.900 21.806 2451.390 2.926 96.992 4.035 0.50 223199. 0.7019
|
|
8.31 0.0696 0.1424 0.1724 0.0843 3.364 26.505 21.632 2508.689 2.995 96.217 3.911 0.50 223500. 0.6777
|
|
12.46 0.1044 0.2069 0.1708 0.0862 3.441 27.110 21.430 2565.971 3.063 95.321 3.788 0.50 223830. 0.6533
|
|
16.61 0.1392 0.2670 0.1689 0.0881 3.516 27.703 21.196 2622.065 3.130 94.281 3.667 0.50 224194. 0.6289
|
|
20.76 0.1740 0.3229 0.1667 0.0899 3.588 28.269 20.925 2675.612 3.194 93.076 3.547 0.50 224591. 0.6045
|
|
24.92 0.2088 0.3747 0.1642 0.0915 3.654 28.791 20.612 2725.081 3.253 91.682 3.431 0.50 225022. 0.5803
|
|
29.07 0.2436 0.4228 0.1614 0.0930 3.713 29.253 20.251 2768.804 3.305 90.076 3.317 0.50 225490. 0.5562
|
|
33.22 0.2784 0.4672 0.1581 0.0942 3.762 29.636 19.837 2805.006 3.348 88.235 3.208 0.50 225995. 0.5323
|
|
37.37 0.3132 0.5082 0.1543 0.0951 3.798 29.919 19.366 2831.845 3.380 86.139 3.102 0.50 226538. 0.5085
|
|
41.53 0.3480 0.5461 0.1501 0.0956 3.818 30.084 18.833 2847.444 3.399 83.768 3.000 0.50 227119. 0.4850
|
|
45.68 0.3828 0.5811 0.1453 0.0957 3.822 30.110 18.234 2849.914 3.402 81.106 2.902 0.50 227738. 0.4617
|
|
49.83 0.4177 0.6135 0.1400 0.0953 3.805 29.979 17.567 2837.477 3.387 78.139 2.808 0.50 228395. 0.4385
|
|
53.98 0.4525 0.6433 0.1341 0.0943 3.767 29.675 16.832 2808.731 3.353 74.869 2.718 0.50 229090. 0.4155
|
|
58.14 0.4873 0.6708 0.1278 0.0928 3.705 29.192 16.032 2762.977 3.298 71.311 2.632 0.51 229823. 0.3926
|
|
62.29 0.5221 0.6960 0.1209 0.0907 3.621 28.529 15.174 2700.286 3.223 67.495 2.549 0.51 230593. 0.3699
|
|
66.44 0.5569 0.7191 0.1137 0.0880 3.515 27.693 14.266 2621.097 3.129 63.455 2.469 0.51 231400. 0.3474
|
|
70.60 0.5917 0.7399 0.1061 0.0848 3.387 26.687 13.314 2525.909 3.015 59.221 2.391 0.51 232244. 0.3250
|
|
74.75 0.6265 0.7585 0.0982 0.0811 3.239 25.517 12.324 2415.141 2.883 54.818 2.315 0.51 233124. 0.3027
|
|
78.90 0.6613 0.7746 0.0901 0.0769 3.070 24.185 11.301 2289.097 2.732 50.268 2.239 0.51 234039. 0.2805
|
|
83.05 0.6961 0.7880 0.0817 0.0721 2.881 22.694 10.249 2147.991 2.564 45.587 2.164 0.51 234990. 0.2581
|
|
87.21 0.7309 0.7983 0.0731 0.0669 2.671 21.046 9.171 1991.986 2.378 40.791 2.088 0.51 235977. 0.2356
|
|
91.36 0.7657 0.8049 0.0643 0.0612 2.442 19.242 8.069 1821.229 2.174 35.892 2.010 0.51 236999. 0.2127
|
|
95.51 0.8005 0.8066 0.0554 0.0549 2.194 17.284 6.948 1635.898 1.953 30.905 1.926 0.52 238056. 0.1892
|
|
99.66 0.8353 0.8017 0.0463 0.0482 1.926 15.174 5.810 1436.225 1.714 25.842 1.835 0.52 239148. 0.1648
|
|
103.82 0.8701 0.7865 0.0371 0.0411 1.639 12.917 4.658 1222.542 1.459 20.719 1.728 0.52 240274. 0.1390
|
|
107.97 0.9049 0.7541 0.0279 0.0334 1.335 10.516 3.496 995.327 1.188 15.551 1.593 0.52 241435. 0.1110
|
|
112.12 0.9397 0.6874 0.0186 0.0254 1.013 7.979 2.329 755.253 0.902 10.357 1.398 0.52 242630. 0.0795
|
|
116.27 0.9745 0.5331 0.0092 0.0169 0.675 5.317 1.160 503.227 0.601 5.161 1.046 0.52 243857. 0.0420
|
|
120.43 1.0093 -0.0067 -0.0001 0.0080 0.321 2.531 -0.007 239.514 0.286 -0.030 -0.013 0.52 245087. 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 0.1759 0.0808 4.593 32.166 27.941 3425.033 3.634 124.280 3.700 0.56 250770. 0.7287
|
|
4.67 0.0348 0.0736 0.1748 0.0827 4.703 32.936 27.761 3507.047 3.721 123.480 3.590 0.56 251075. 0.7048
|
|
9.35 0.0696 0.1426 0.1735 0.0847 4.815 33.722 27.552 3590.746 3.810 122.552 3.480 0.56 251413. 0.6806
|
|
14.02 0.1045 0.2072 0.1719 0.0867 4.928 34.510 27.309 3674.653 3.899 121.471 3.371 0.56 251785. 0.6563
|
|
18.70 0.1393 0.2674 0.1702 0.0886 5.038 35.284 27.026 3757.052 3.986 120.210 3.263 0.56 252193. 0.6319
|
|
23.37 0.1741 0.3234 0.1681 0.0905 5.144 36.025 26.695 3835.931 4.070 118.738 3.156 0.56 252640. 0.6076
|
|
28.04 0.2089 0.3753 0.1656 0.0922 5.242 36.711 26.309 3909.035 4.148 117.024 3.053 0.56 253126. 0.5834
|
|
32.72 0.2437 0.4234 0.1628 0.0937 5.329 37.320 25.863 3973.897 4.216 115.036 2.952 0.56 253653. 0.5593
|
|
37.39 0.2786 0.4679 0.1596 0.0950 5.401 37.827 25.348 4027.893 4.274 112.746 2.854 0.56 254223. 0.5354
|
|
42.06 0.3134 0.5090 0.1559 0.0960 5.456 38.207 24.758 4068.297 4.317 110.124 2.760 0.57 254834. 0.5117
|
|
46.74 0.3482 0.5470 0.1517 0.0965 5.488 38.433 24.088 4092.338 4.342 107.145 2.670 0.57 255489. 0.4882
|
|
51.41 0.3830 0.5822 0.1469 0.0967 5.494 38.479 23.333 4097.246 4.347 103.786 2.583 0.57 256187. 0.4648
|
|
56.09 0.4178 0.6147 0.1416 0.0963 5.472 38.321 22.489 4080.416 4.329 100.032 2.500 0.57 256928. 0.4417
|
|
60.76 0.4526 0.6447 0.1357 0.0953 5.417 37.939 21.556 4039.784 4.286 95.882 2.420 0.57 257713. 0.4186
|
|
65.43 0.4875 0.6724 0.1293 0.0938 5.330 37.324 20.539 3974.330 4.217 91.356 2.344 0.57 258540. 0.3958
|
|
70.11 0.5223 0.6979 0.1224 0.0916 5.209 36.477 19.445 3884.134 4.121 86.493 2.271 0.57 259408. 0.3731
|
|
74.78 0.5571 0.7213 0.1151 0.0889 5.055 35.404 18.286 3769.865 4.000 81.338 2.200 0.57 260319. 0.3505
|
|
79.45 0.5919 0.7425 0.1075 0.0857 4.871 34.112 17.070 3632.273 3.854 75.929 2.132 0.57 261270. 0.3281
|
|
84.13 0.6267 0.7615 0.0995 0.0819 4.656 32.607 15.805 3471.995 3.684 70.300 2.065 0.57 262262. 0.3058
|
|
88.80 0.6616 0.7781 0.0913 0.0776 4.411 30.893 14.496 3289.500 3.490 64.478 1.999 0.57 263295. 0.2835
|
|
93.48 0.6964 0.7922 0.0828 0.0728 4.137 28.974 13.149 3085.122 3.273 58.486 1.933 0.58 264367. 0.2612
|
|
98.15 0.7312 0.8033 0.0741 0.0674 3.834 26.851 11.768 2859.099 3.034 52.343 1.867 0.58 265479. 0.2386
|
|
102.82 0.7660 0.8108 0.0652 0.0616 3.502 24.527 10.356 2611.633 2.771 46.066 1.799 0.58 266631. 0.2156
|
|
107.50 0.8008 0.8137 0.0562 0.0553 3.142 22.004 8.919 2342.997 2.486 39.672 1.727 0.58 267822. 0.1921
|
|
112.17 0.8357 0.8102 0.0470 0.0484 2.754 19.285 7.459 2053.523 2.179 33.178 1.648 0.58 269052. 0.1676
|
|
116.84 0.8705 0.7969 0.0377 0.0411 2.338 16.376 5.981 1743.689 1.850 26.604 1.556 0.58 270321. 0.1418
|
|
121.52 0.9053 0.7671 0.0283 0.0334 1.896 13.281 4.490 1414.183 1.500 19.970 1.440 0.59 271628. 0.1137
|
|
126.19 0.9401 0.7039 0.0188 0.0251 1.430 10.011 2.990 1065.984 1.131 13.301 1.272 0.59 272974. 0.0820
|
|
130.87 0.9749 0.5533 0.0094 0.0165 0.939 6.578 1.489 700.408 0.743 6.625 0.964 0.59 274355. 0.0439
|
|
135.54 1.0098 -0.0094 -0.0001 0.0075 0.426 2.984 -0.011 317.699 0.337 -0.049 -0.016 0.59 275736. 0.0000
|
|
|
|
|
|
|
|
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 0.1770 0.0814 6.344 39.985 34.701 4730.728 4.518 154.349 3.327 0.62 278604. 0.7302
|
|
5.19 0.0348 0.0735 0.1759 0.0833 6.499 40.960 34.495 4846.041 4.628 153.436 3.229 0.62 278942. 0.7065
|
|
10.39 0.0697 0.1426 0.1747 0.0854 6.657 41.958 34.256 4964.167 4.740 152.370 3.130 0.62 279316. 0.6825
|
|
15.58 0.1045 0.2071 0.1733 0.0874 6.816 42.963 33.975 5083.021 4.854 151.119 3.032 0.63 279729. 0.6583
|
|
20.78 0.1393 0.2673 0.1716 0.0894 6.974 43.953 33.643 5200.154 4.966 149.646 2.934 0.63 280182. 0.6341
|
|
25.97 0.1742 0.3233 0.1696 0.0914 7.124 44.904 33.253 5312.698 5.073 147.911 2.839 0.63 280679. 0.6099
|
|
31.17 0.2090 0.3752 0.1673 0.0932 7.265 45.789 32.795 5417.403 5.173 145.873 2.746 0.63 281219. 0.5858
|
|
36.36 0.2438 0.4233 0.1645 0.0948 7.390 46.578 32.260 5510.735 5.262 143.492 2.655 0.63 281806. 0.5619
|
|
41.56 0.2787 0.4678 0.1614 0.0961 7.495 47.239 31.638 5588.907 5.337 140.727 2.568 0.63 282439. 0.5381
|
|
46.75 0.3135 0.5090 0.1577 0.0971 7.574 47.738 30.922 5648.027 5.393 137.541 2.483 0.63 283120. 0.5145
|
|
51.95 0.3483 0.5471 0.1535 0.0977 7.623 48.044 30.104 5684.114 5.428 133.901 2.402 0.63 283850. 0.4910
|
|
57.14 0.3832 0.5823 0.1488 0.0979 7.635 48.121 29.176 5693.223 5.437 129.777 2.324 0.63 284627. 0.4678
|
|
62.34 0.4180 0.6149 0.1435 0.0975 7.606 47.938 28.136 5671.654 5.416 125.148 2.250 0.63 285453. 0.4446
|
|
67.53 0.4528 0.6451 0.1376 0.0966 7.532 47.472 26.981 5616.481 5.363 120.012 2.179 0.63 286328. 0.4217
|
|
72.73 0.4876 0.6730 0.1312 0.0950 7.411 46.709 25.718 5526.236 5.277 114.396 2.111 0.63 287249. 0.3988
|
|
77.92 0.5225 0.6988 0.1242 0.0929 7.243 45.651 24.359 5401.037 5.158 108.347 2.046 0.63 288217. 0.3761
|
|
83.12 0.5573 0.7225 0.1169 0.0901 7.029 44.305 22.914 5241.857 5.006 101.923 1.983 0.63 289232. 0.3536
|
|
88.31 0.5921 0.7441 0.1091 0.0868 6.772 42.682 21.397 5049.799 4.822 95.174 1.922 0.64 290292. 0.3312
|
|
93.51 0.6270 0.7635 0.1011 0.0830 6.472 40.789 19.817 4825.815 4.608 88.144 1.863 0.64 291397. 0.3089
|
|
98.70 0.6618 0.7807 0.0927 0.0786 6.129 38.632 18.180 4570.605 4.365 80.866 1.804 0.64 292547. 0.2866
|
|
103.90 0.6966 0.7954 0.0841 0.0737 5.746 36.215 16.495 4284.673 4.092 73.370 1.746 0.64 293741. 0.2642
|
|
109.09 0.7315 0.8072 0.0753 0.0682 5.322 33.542 14.766 3968.361 3.790 65.680 1.688 0.64 294979. 0.2416
|
|
114.29 0.7663 0.8156 0.0663 0.0623 4.857 30.614 12.998 3621.983 3.459 57.817 1.628 0.64 296261. 0.2186
|
|
119.48 0.8011 0.8196 0.0571 0.0558 4.353 27.435 11.197 3245.893 3.100 49.804 1.565 0.64 297587. 0.1951
|
|
124.68 0.8360 0.8175 0.0478 0.0488 3.809 24.009 9.366 2840.560 2.713 41.661 1.496 0.65 298956. 0.1705
|
|
129.87 0.8708 0.8060 0.0383 0.0414 3.227 20.342 7.512 2406.648 2.298 33.412 1.416 0.65 300368. 0.1446
|
|
135.07 0.9056 0.7787 0.0288 0.0334 2.608 16.441 5.639 1945.116 1.857 25.083 1.315 0.65 301822. 0.1163
|
|
140.26 0.9405 0.7188 0.0192 0.0251 1.954 12.318 3.756 1457.325 1.392 16.706 1.169 0.65 303318. 0.0844
|
|
145.46 0.9753 0.5722 0.0095 0.0163 1.267 7.989 1.870 945.144 0.903 8.316 0.897 0.65 304855. 0.0457
|
|
150.65 1.0101 -0.0129 -0.0001 0.0070 0.548 3.455 -0.018 408.779 0.390 -0.078 -0.020 0.66 306385. 0.0000
|
|
|
|
|
|
|
|
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 0.1781 0.0825 8.558 49.035 42.254 6381.618 5.540 187.948 3.003 0.69 306428. 0.7273
|
|
5.72 0.0348 0.0731 0.1772 0.0844 8.765 50.219 42.031 6535.712 5.674 186.953 2.917 0.69 306798. 0.7045
|
|
11.43 0.0697 0.1418 0.1760 0.0865 8.977 51.438 41.768 6694.302 5.811 185.783 2.830 0.69 307208. 0.6814
|
|
17.15 0.1045 0.2062 0.1747 0.0886 9.192 52.670 41.456 6854.668 5.951 184.396 2.743 0.69 307661. 0.6580
|
|
22.87 0.1394 0.2663 0.1732 0.0906 9.405 53.892 41.084 7013.611 6.089 182.743 2.657 0.69 308159. 0.6345
|
|
28.58 0.1742 0.3223 0.1713 0.0926 9.611 55.072 40.641 7167.261 6.222 180.773 2.572 0.69 308705. 0.6109
|
|
34.30 0.2091 0.3742 0.1691 0.0945 9.804 56.178 40.115 7311.199 6.347 178.432 2.489 0.69 309300. 0.5872
|
|
40.02 0.2439 0.4223 0.1665 0.0961 9.978 57.172 39.493 7440.495 6.459 175.666 2.407 0.69 309945. 0.5637
|
|
45.73 0.2788 0.4669 0.1634 0.0975 10.125 58.012 38.764 7549.860 6.554 172.422 2.329 0.69 310643. 0.5402
|
|
51.45 0.3136 0.5081 0.1598 0.0986 10.237 58.657 37.916 7633.775 6.627 168.652 2.253 0.69 311394. 0.5168
|
|
57.17 0.3484 0.5463 0.1557 0.0993 10.308 59.063 36.941 7686.589 6.673 164.312 2.180 0.69 312198. 0.4936
|
|
62.88 0.3833 0.5816 0.1510 0.0995 10.329 59.186 35.828 7702.625 6.687 159.363 2.110 0.69 313056. 0.4705
|
|
68.60 0.4181 0.6143 0.1457 0.0992 10.294 58.985 34.573 7676.524 6.664 153.779 2.043 0.69 313968. 0.4475
|
|
74.32 0.4530 0.6447 0.1398 0.0982 10.197 58.429 33.173 7604.139 6.601 147.555 1.979 0.69 314933. 0.4246
|
|
80.03 0.4878 0.6728 0.1333 0.0967 10.035 57.501 31.637 7483.386 6.496 140.723 1.918 0.70 315950. 0.4018
|
|
85.75 0.5227 0.6988 0.1264 0.0945 9.809 56.203 29.979 7314.462 6.350 133.345 1.859 0.70 317019. 0.3792
|
|
91.47 0.5575 0.7228 0.1189 0.0917 9.520 54.546 28.213 7098.750 6.163 125.491 1.803 0.70 318138. 0.3567
|
|
97.18 0.5924 0.7448 0.1111 0.0883 9.170 52.541 26.355 6837.872 5.936 117.225 1.748 0.70 319308. 0.3344
|
|
102.90 0.6272 0.7647 0.1029 0.0844 8.761 50.200 24.416 6533.203 5.672 108.603 1.695 0.70 320527. 0.3121
|
|
108.62 0.6621 0.7823 0.0944 0.0799 8.295 47.531 22.408 6185.807 5.370 99.669 1.643 0.70 321796. 0.2898
|
|
114.33 0.6969 0.7976 0.0857 0.0749 7.773 44.539 20.337 5796.418 5.032 90.458 1.591 0.70 323113. 0.2674
|
|
120.05 0.7317 0.8102 0.0768 0.0693 7.195 41.228 18.211 5365.553 4.658 81.001 1.539 0.71 324478. 0.2447
|
|
125.76 0.7666 0.8194 0.0676 0.0632 6.562 37.602 16.035 4893.600 4.248 71.325 1.486 0.71 325891. 0.2217
|
|
131.48 0.8014 0.8245 0.0582 0.0566 5.875 33.663 13.817 4381.064 3.803 61.456 1.430 0.71 327352. 0.1981
|
|
137.20 0.8363 0.8237 0.0487 0.0495 5.134 29.419 11.560 3828.668 3.324 51.420 1.370 0.71 328861. 0.1735
|
|
142.91 0.8711 0.8140 0.0391 0.0418 4.342 24.876 9.273 3237.478 2.811 41.246 1.299 0.71 330416. 0.1474
|
|
148.63 0.9060 0.7886 0.0293 0.0337 3.499 20.048 6.962 2609.103 2.265 30.966 1.210 0.72 332018. 0.1190
|
|
154.35 0.9408 0.7311 0.0195 0.0251 2.609 14.952 4.635 1945.886 1.689 20.617 1.080 0.72 333666. 0.0867
|
|
160.06 0.9757 0.5859 0.0097 0.0162 1.678 9.613 2.303 1251.105 1.086 10.243 0.835 0.72 335358. 0.0472
|
|
165.78 1.0105 -0.0215 -0.0001 0.0068 0.705 4.039 -0.034 525.656 0.456 -0.153 -0.030 0.72 337035. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 12000
|
|
|
|
V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
|
|
(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
|
|
0.00 0.0000 0.0000 0.1792 0.0855 11.521 60.511 50.598 8591.032 6.837 225.061 2.671 0.75 334240. 0.7079
|
|
6.26 0.0350 0.0714 0.1784 0.0874 11.782 61.885 50.366 8786.121 6.992 224.029 2.600 0.75 334644. 0.6875
|
|
12.53 0.0700 0.1389 0.1774 0.0894 12.052 63.300 50.090 8986.915 7.152 222.802 2.528 0.75 335091. 0.6666
|
|
18.79 0.1050 0.2023 0.1762 0.0915 12.324 64.729 49.759 9189.827 7.313 221.329 2.456 0.75 335586. 0.6454
|
|
25.06 0.1400 0.2619 0.1748 0.0935 12.593 66.143 49.359 9390.549 7.473 219.547 2.384 0.75 336131. 0.6240
|
|
31.32 0.1750 0.3176 0.1731 0.0954 12.852 67.505 48.874 9583.996 7.627 217.390 2.313 0.75 336728. 0.6024
|
|
37.59 0.2100 0.3696 0.1710 0.0972 13.094 68.775 48.288 9764.310 7.770 214.785 2.243 0.75 337380. 0.5807
|
|
43.85 0.2450 0.4180 0.1685 0.0988 13.310 69.907 47.585 9925.044 7.898 211.658 2.175 0.75 338089. 0.5589
|
|
50.11 0.2800 0.4631 0.1656 0.1001 13.490 70.854 46.749 10059.387 8.005 207.939 2.108 0.75 338856. 0.5369
|
|
56.38 0.3150 0.5049 0.1621 0.1011 13.625 71.564 45.765 10160.252 8.085 203.562 2.043 0.75 339683. 0.5149
|
|
62.64 0.3500 0.5438 0.1580 0.1017 13.706 71.988 44.620 10220.498 8.133 198.468 1.980 0.75 340569. 0.4928
|
|
68.91 0.3850 0.5798 0.1534 0.1018 13.722 72.076 43.302 10232.868 8.143 192.609 1.919 0.76 341514. 0.4706
|
|
75.17 0.4200 0.6132 0.1481 0.1014 13.666 71.776 41.805 10190.369 8.109 185.948 1.861 0.76 342519. 0.4482
|
|
81.43 0.4550 0.6441 0.1421 0.1004 13.527 71.050 40.126 10087.293 8.027 178.478 1.804 0.76 343583. 0.4258
|
|
87.70 0.4900 0.6728 0.1355 0.0987 13.304 69.877 38.273 9920.665 7.895 170.240 1.750 0.76 344705. 0.4033
|
|
93.96 0.5250 0.6992 0.1284 0.0964 12.995 68.255 36.266 9690.408 7.711 161.312 1.697 0.76 345883. 0.3808
|
|
100.23 0.5600 0.7236 0.1209 0.0935 12.603 66.195 34.124 9397.973 7.479 151.784 1.647 0.76 347118. 0.3584
|
|
106.49 0.5950 0.7460 0.1129 0.0900 12.130 63.710 31.866 9045.129 7.198 141.739 1.598 0.76 348408. 0.3361
|
|
112.76 0.6300 0.7663 0.1045 0.0859 11.578 60.810 29.507 8633.391 6.870 131.245 1.550 0.76 349752. 0.3137
|
|
119.02 0.6650 0.7844 0.0958 0.0812 10.948 57.504 27.059 8164.066 6.497 120.360 1.503 0.77 351150. 0.2913
|
|
125.28 0.7000 0.8002 0.0869 0.0760 10.243 53.801 24.534 7638.373 6.078 109.128 1.457 0.77 352601. 0.2688
|
|
131.55 0.7350 0.8132 0.0777 0.0702 9.464 49.709 21.939 7057.329 5.616 97.586 1.410 0.77 354106. 0.2461
|
|
137.81 0.7700 0.8228 0.0683 0.0639 8.612 45.233 19.282 6421.878 5.110 85.768 1.362 0.77 355662. 0.2228
|
|
144.08 0.8050 0.8280 0.0587 0.0571 7.688 40.383 16.570 5733.293 4.562 73.702 1.311 0.77 357271. 0.1988
|
|
150.34 0.8400 0.8267 0.0489 0.0497 6.696 35.172 13.809 4993.476 3.974 61.421 1.254 0.78 358931. 0.1736
|
|
156.61 0.8750 0.8151 0.0390 0.0418 5.639 29.619 11.007 4205.065 3.346 48.958 1.187 0.78 360643. 0.1467
|
|
162.87 0.9100 0.7849 0.0289 0.0336 4.522 23.749 8.172 3371.758 2.683 36.350 1.099 0.78 362406. 0.1171
|
|
169.13 0.9450 0.7154 0.0188 0.0249 3.351 17.599 5.315 2498.639 1.988 23.642 0.965 0.78 364218. 0.0829
|
|
175.40 0.9800 0.5360 0.0087 0.0158 2.135 11.216 2.447 1592.428 1.267 10.885 0.697 0.79 366078. 0.0406
|
|
181.66 1.0150
|
|
|
|
|
|
|