649 lines
115 KiB
Plaintext
649 lines
115 KiB
Plaintext
13x14 (13x14.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 0.1329 0.0843 0.002 0.156 0.119 1.843 0.018 0.530 29.317 0.05 21484. 0.4585
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0.53 0.0431 0.0663 0.1324 0.0860 0.003 0.159 0.119 1.878 0.018 0.528 28.655 0.05 21510. 0.4473
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1.06 0.0861 0.1294 0.1319 0.0878 0.003 0.162 0.118 1.918 0.018 0.526 27.953 0.05 21540. 0.4354
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1.58 0.1292 0.1890 0.1313 0.0897 0.003 0.166 0.118 1.961 0.019 0.523 27.218 0.05 21575. 0.4231
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2.11 0.1723 0.2450 0.1306 0.0918 0.003 0.170 0.117 2.007 0.019 0.521 26.457 0.05 21615. 0.4102
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2.64 0.2153 0.2972 0.1298 0.0941 0.003 0.174 0.116 2.056 0.020 0.518 25.676 0.05 21660. 0.3969
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3.17 0.2584 0.3457 0.1289 0.0964 0.003 0.178 0.116 2.106 0.020 0.514 24.885 0.05 21711. 0.3832
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3.70 0.3015 0.3904 0.1278 0.0987 0.003 0.182 0.114 2.156 0.021 0.509 24.089 0.05 21767. 0.3693
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4.22 0.3445 0.4315 0.1264 0.1009 0.003 0.186 0.113 2.205 0.021 0.504 23.297 0.05 21829. 0.3552
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4.75 0.3876 0.4691 0.1247 0.1030 0.003 0.190 0.112 2.251 0.021 0.497 22.514 0.05 21897. 0.3410
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5.28 0.4306 0.5034 0.1226 0.1049 0.003 0.194 0.110 2.292 0.022 0.489 21.745 0.05 21971. 0.3266
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5.81 0.4737 0.5346 0.1201 0.1064 0.003 0.197 0.108 2.326 0.022 0.479 20.992 0.05 22051. 0.3121
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6.34 0.5168 0.5628 0.1171 0.1075 0.003 0.199 0.105 2.350 0.022 0.467 20.258 0.05 22137. 0.2974
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6.87 0.5598 0.5882 0.1136 0.1081 0.003 0.200 0.102 2.362 0.023 0.453 19.542 0.05 22229. 0.2825
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7.39 0.6029 0.6108 0.1094 0.1080 0.003 0.200 0.098 2.361 0.023 0.436 18.844 0.05 22328. 0.2674
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7.92 0.6460 0.6306 0.1046 0.1072 0.003 0.198 0.094 2.342 0.022 0.417 18.160 0.05 22432. 0.2520
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8.45 0.6890 0.6478 0.0992 0.1055 0.003 0.195 0.089 2.305 0.022 0.395 17.488 0.05 22543. 0.2362
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8.98 0.7321 0.6621 0.0931 0.1030 0.003 0.190 0.083 2.250 0.021 0.371 16.824 0.05 22659. 0.2202
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9.51 0.7752 0.6734 0.0866 0.0997 0.003 0.184 0.078 2.178 0.021 0.345 16.159 0.05 22780. 0.2040
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10.03 0.8182 0.6812 0.0796 0.0957 0.003 0.177 0.071 2.090 0.020 0.317 15.485 0.05 22908. 0.1874
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10.56 0.8613 0.6849 0.0724 0.0910 0.003 0.168 0.065 1.988 0.019 0.288 14.791 0.05 23040. 0.1707
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11.09 0.9044 0.6837 0.0648 0.0858 0.003 0.158 0.058 1.874 0.018 0.258 14.064 0.05 23178. 0.1536
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11.62 0.9474 0.6766 0.0571 0.0800 0.002 0.148 0.051 1.748 0.017 0.228 13.284 0.05 23321. 0.1362
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12.15 0.9905 0.6617 0.0492 0.0737 0.002 0.136 0.044 1.610 0.015 0.196 12.427 0.05 23469. 0.1183
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12.67 1.0335 0.6366 0.0412 0.0669 0.002 0.124 0.037 1.462 0.014 0.164 11.457 0.05 23623. 0.0998
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13.20 1.0766 0.5970 0.0331 0.0597 0.002 0.110 0.030 1.304 0.012 0.132 10.315 0.05 23781. 0.0805
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13.73 1.1197 0.5362 0.0249 0.0520 0.002 0.096 0.022 1.136 0.011 0.099 8.907 0.05 23944. 0.0603
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14.26 1.1627 0.4413 0.0167 0.0439 0.001 0.081 0.015 0.959 0.009 0.066 7.059 0.05 24111. 0.0391
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14.79 1.2058 0.2867 0.0084 0.0354 0.001 0.065 0.008 0.774 0.007 0.034 4.422 0.06 24284. 0.0174
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15.31 1.2489 0.0109 0.0002 0.0266 0.001 0.049 0.000 0.582 0.006 0.001 0.162 0.06 24460. 0.0001
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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 0.1335 0.0767 0.018 0.567 0.479 13.405 0.064 2.128 16.190 0.10 42967. 0.5075
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1.07 0.0435 0.0738 0.1330 0.0784 0.018 0.579 0.477 13.699 0.065 2.121 15.791 0.10 43020. 0.4941
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2.13 0.0869 0.1436 0.1326 0.0802 0.019 0.593 0.475 14.024 0.067 2.114 15.368 0.10 43082. 0.4800
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3.20 0.1304 0.2092 0.1320 0.0823 0.019 0.608 0.473 14.380 0.069 2.105 14.927 0.10 43153. 0.4653
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4.26 0.1738 0.2704 0.1314 0.0844 0.020 0.624 0.471 14.762 0.070 2.095 14.471 0.10 43233. 0.4500
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5.33 0.2173 0.3272 0.1307 0.0868 0.020 0.641 0.468 15.166 0.072 2.083 14.007 0.10 43325. 0.4343
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6.39 0.2607 0.3795 0.1298 0.0891 0.021 0.659 0.465 15.583 0.074 2.069 13.538 0.10 43427. 0.4184
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7.46 0.3042 0.4274 0.1287 0.0915 0.021 0.676 0.461 16.004 0.076 2.051 13.070 0.10 43541. 0.4022
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8.53 0.3476 0.4712 0.1273 0.0939 0.022 0.694 0.456 16.416 0.078 2.030 12.607 0.10 43667. 0.3859
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9.59 0.3911 0.5110 0.1256 0.0961 0.023 0.710 0.450 16.804 0.080 2.003 12.153 0.10 43805. 0.3695
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10.66 0.4345 0.5471 0.1235 0.0981 0.023 0.725 0.443 17.152 0.082 1.970 11.710 0.10 43955. 0.3531
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11.72 0.4780 0.5797 0.1210 0.0998 0.023 0.737 0.434 17.443 0.083 1.930 11.280 0.10 44118. 0.3367
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12.79 0.5214 0.6092 0.1180 0.1010 0.024 0.746 0.423 17.657 0.084 1.881 10.866 0.10 44293. 0.3202
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13.85 0.5649 0.6356 0.1144 0.1017 0.024 0.751 0.410 17.774 0.085 1.824 10.465 0.10 44481. 0.3037
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14.92 0.6083 0.6593 0.1102 0.1017 0.024 0.751 0.395 17.772 0.085 1.757 10.079 0.10 44681. 0.2870
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15.99 0.6518 0.6802 0.1053 0.1009 0.024 0.745 0.377 17.633 0.084 1.678 9.706 0.10 44893. 0.2702
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17.05 0.6952 0.6986 0.0997 0.0992 0.023 0.733 0.357 17.343 0.083 1.589 9.346 0.11 45118. 0.2531
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18.12 0.7387 0.7144 0.0935 0.0967 0.023 0.714 0.335 16.902 0.081 1.491 8.995 0.11 45354. 0.2360
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19.18 0.7822 0.7275 0.0868 0.0934 0.022 0.690 0.311 16.320 0.078 1.385 8.651 0.11 45601. 0.2187
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20.25 0.8256 0.7376 0.0798 0.0893 0.021 0.660 0.286 15.610 0.075 1.272 8.309 0.11 45860. 0.2013
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21.31 0.8691 0.7441 0.0724 0.0846 0.020 0.625 0.260 14.781 0.071 1.154 7.963 0.11 46129. 0.1838
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22.38 0.9125 0.7465 0.0648 0.0792 0.019 0.585 0.232 13.844 0.066 1.033 7.609 0.11 46410. 0.1661
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23.45 0.9560 0.7438 0.0570 0.0732 0.017 0.541 0.204 12.804 0.061 0.909 7.236 0.11 46701. 0.1482
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24.51 0.9994 0.7342 0.0490 0.0667 0.016 0.493 0.176 11.668 0.056 0.782 6.833 0.11 47002. 0.1298
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25.58 1.0429 0.7154 0.0410 0.0597 0.014 0.441 0.147 10.440 0.050 0.653 6.380 0.11 47313. 0.1108
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26.64 1.0863 0.6831 0.0328 0.0522 0.012 0.386 0.118 9.124 0.044 0.523 5.848 0.11 47634. 0.0909
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27.71 1.1298 0.6292 0.0246 0.0442 0.010 0.326 0.088 7.726 0.037 0.392 5.180 0.11 47965. 0.0697
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28.77 1.1732 0.5378 0.0164 0.0358 0.008 0.264 0.059 6.250 0.030 0.261 4.264 0.11 48306. 0.0468
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29.84 1.2167 0.3702 0.0082 0.0269 0.006 0.199 0.029 4.706 0.022 0.131 2.830 0.11 48656. 0.0220
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30.91 1.2601 0.0040 0.0001 0.0177 0.004 0.131 0.000 3.101 0.015 0.001 0.030 0.11 49014. 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 0.1338 0.0736 0.058 1.223 1.079 43.404 0.138 4.799 11.275 0.15 64451. 0.5306
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1.60 0.0436 0.0773 0.1333 0.0753 0.060 1.251 1.075 44.406 0.141 4.784 10.985 0.15 64530. 0.5162
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3.21 0.0872 0.1503 0.1329 0.0772 0.061 1.282 1.072 45.519 0.145 4.767 10.680 0.15 64623. 0.5010
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4.81 0.1309 0.2187 0.1324 0.0792 0.063 1.317 1.068 46.738 0.149 4.749 10.361 0.15 64730. 0.4851
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6.42 0.1745 0.2823 0.1318 0.0814 0.064 1.354 1.063 48.050 0.153 4.727 10.033 0.15 64851. 0.4687
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8.02 0.2181 0.3411 0.1311 0.0838 0.066 1.393 1.057 49.436 0.157 4.702 9.699 0.15 64989. 0.4518
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9.63 0.2617 0.3952 0.1302 0.0862 0.068 1.433 1.050 50.872 0.162 4.671 9.362 0.15 65144. 0.4347
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11.23 0.3053 0.4445 0.1291 0.0887 0.070 1.474 1.041 52.322 0.167 4.632 9.027 0.15 65315. 0.4174
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12.84 0.3489 0.4894 0.1278 0.0911 0.072 1.514 1.031 53.745 0.171 4.584 8.697 0.16 65505. 0.4000
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14.44 0.3926 0.5302 0.1261 0.0934 0.074 1.552 1.017 55.090 0.175 4.524 8.374 0.16 65714. 0.3827
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16.05 0.4362 0.5670 0.1240 0.0954 0.076 1.586 1.000 56.301 0.179 4.450 8.060 0.16 65941. 0.3653
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17.65 0.4798 0.6003 0.1215 0.0971 0.077 1.615 0.980 57.316 0.182 4.360 7.757 0.16 66187. 0.3480
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19.26 0.5234 0.6302 0.1185 0.0984 0.078 1.636 0.956 58.070 0.185 4.251 7.466 0.16 66451. 0.3307
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20.86 0.5670 0.6571 0.1149 0.0991 0.078 1.648 0.927 58.493 0.186 4.122 7.186 0.16 66735. 0.3134
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22.47 0.6107 0.6812 0.1106 0.0992 0.078 1.649 0.892 58.512 0.186 3.969 6.917 0.16 67038. 0.2961
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24.07 0.6543 0.7027 0.1057 0.0984 0.078 1.636 0.852 58.057 0.185 3.791 6.659 0.16 67358. 0.2786
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25.67 0.6979 0.7217 0.1001 0.0968 0.077 1.608 0.807 57.086 0.182 3.589 6.412 0.16 67697. 0.2610
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27.28 0.7415 0.7382 0.0938 0.0942 0.075 1.566 0.757 55.597 0.177 3.366 6.173 0.16 68054. 0.2433
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28.88 0.7851 0.7523 0.0871 0.0909 0.072 1.511 0.702 53.624 0.171 3.124 5.941 0.16 68427. 0.2256
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30.49 0.8287 0.7636 0.0800 0.0868 0.069 1.443 0.645 51.207 0.163 2.869 5.713 0.16 68818. 0.2079
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32.09 0.8724 0.7717 0.0725 0.0820 0.065 1.363 0.585 48.382 0.154 2.602 5.485 0.16 69225. 0.1901
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33.70 0.9160 0.7761 0.0649 0.0766 0.061 1.273 0.523 45.179 0.144 2.328 5.254 0.16 69649. 0.1722
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35.30 0.9596 0.7759 0.0570 0.0705 0.056 1.173 0.460 41.621 0.132 2.046 5.014 0.16 70088. 0.1541
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36.91 1.0032 0.7696 0.0491 0.0639 0.051 1.063 0.396 37.725 0.120 1.760 4.757 0.16 70542. 0.1356
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38.51 1.0468 0.7549 0.0410 0.0568 0.045 0.944 0.330 33.506 0.107 1.469 4.472 0.16 71013. 0.1164
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40.12 1.0904 0.7277 0.0328 0.0491 0.039 0.817 0.264 28.981 0.092 1.176 4.138 0.16 71498. 0.0964
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41.72 1.1341 0.6798 0.0246 0.0410 0.032 0.681 0.198 24.167 0.077 0.881 3.717 0.16 71998. 0.0749
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43.33 1.1777 0.5942 0.0163 0.0323 0.026 0.538 0.132 19.086 0.061 0.586 3.128 0.16 72512. 0.0514
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44.93 1.2213 0.4251 0.0081 0.0233 0.018 0.388 0.065 13.765 0.044 0.291 2.158 0.17 73041. 0.0250
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46.53 1.2649 -0.0006 0.0000 0.0140 0.011 0.232 0.000 8.234 0.026 0.000 -0.003 0.17 73581. 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 0.1340 0.0719 0.135 2.124 1.921 100.507 0.240 8.545 8.669 0.21 85933. 0.5444
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2.14 0.0437 0.0793 0.1336 0.0736 0.138 2.174 1.915 102.898 0.246 8.519 8.442 0.21 86040. 0.5294
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4.29 0.0874 0.1542 0.1331 0.0755 0.142 2.230 1.909 105.557 0.252 8.491 8.202 0.21 86163. 0.5135
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6.43 0.1311 0.2242 0.1326 0.0776 0.145 2.292 1.902 108.470 0.259 8.459 7.953 0.21 86306. 0.4969
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8.58 0.1748 0.2893 0.1321 0.0798 0.150 2.358 1.894 111.612 0.266 8.423 7.695 0.21 86469. 0.4798
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10.72 0.2185 0.3493 0.1314 0.0822 0.154 2.429 1.884 114.937 0.274 8.379 7.434 0.21 86653. 0.4623
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12.86 0.2622 0.4044 0.1305 0.0847 0.159 2.502 1.872 118.386 0.283 8.325 7.171 0.21 86859. 0.4445
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15.01 0.3059 0.4546 0.1295 0.0871 0.163 2.575 1.857 121.875 0.291 8.258 6.909 0.21 87089. 0.4266
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17.15 0.3497 0.5002 0.1282 0.0896 0.168 2.648 1.838 125.304 0.299 8.174 6.652 0.21 87343. 0.4086
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19.29 0.3934 0.5414 0.1265 0.0919 0.172 2.716 1.814 128.554 0.307 8.069 6.401 0.21 87622. 0.3906
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21.44 0.4371 0.5787 0.1245 0.0940 0.176 2.778 1.785 131.488 0.314 7.939 6.157 0.21 87926. 0.3727
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23.58 0.4808 0.6123 0.1220 0.0958 0.180 2.831 1.749 133.959 0.320 7.780 5.922 0.21 88255. 0.3549
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25.73 0.5245 0.6425 0.1190 0.0971 0.182 2.870 1.706 135.808 0.324 7.588 5.697 0.21 88609. 0.3372
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27.87 0.5682 0.6697 0.1154 0.0979 0.184 2.892 1.654 136.865 0.327 7.357 5.481 0.21 88989. 0.3194
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30.01 0.6119 0.6941 0.1111 0.0979 0.184 2.894 1.593 136.954 0.327 7.085 5.275 0.21 89394. 0.3017
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32.16 0.6556 0.7159 0.1061 0.0972 0.182 2.872 1.522 135.907 0.324 6.768 5.078 0.21 89823. 0.2838
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34.30 0.6993 0.7353 0.1005 0.0955 0.179 2.823 1.440 133.621 0.319 6.407 4.890 0.21 90277. 0.2659
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36.45 0.7430 0.7523 0.0942 0.0930 0.174 2.749 1.351 130.094 0.311 6.007 4.709 0.21 90754. 0.2479
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38.59 0.7867 0.7670 0.0874 0.0897 0.168 2.650 1.254 125.402 0.299 5.576 4.534 0.21 91254. 0.2300
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40.73 0.8304 0.7791 0.0803 0.0855 0.160 2.528 1.151 119.640 0.286 5.119 4.363 0.21 91777. 0.2121
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42.88 0.8741 0.7884 0.0728 0.0807 0.151 2.386 1.044 112.894 0.270 4.643 4.194 0.21 92322. 0.1942
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45.02 0.9178 0.7942 0.0651 0.0752 0.141 2.224 0.934 105.233 0.251 4.152 4.024 0.21 92889. 0.1762
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47.17 0.9615 0.7957 0.0572 0.0692 0.130 2.044 0.821 96.711 0.231 3.650 3.848 0.21 93477. 0.1580
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49.31 1.0053 0.7917 0.0492 0.0625 0.117 1.846 0.705 87.370 0.209 3.138 3.662 0.22 94085. 0.1394
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51.45 1.0490 0.7800 0.0411 0.0552 0.104 1.632 0.589 77.248 0.184 2.619 3.458 0.22 94714. 0.1202
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53.60 1.0927 0.7565 0.0329 0.0475 0.089 1.403 0.471 66.382 0.158 2.096 3.220 0.22 95364. 0.1001
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55.74 1.1364 0.7136 0.0246 0.0392 0.074 1.158 0.353 54.816 0.131 1.570 2.920 0.22 96033. 0.0786
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57.88 1.1801 0.6336 0.0164 0.0305 0.057 0.900 0.235 42.603 0.102 1.043 2.497 0.22 96721. 0.0548
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60.03 1.2238 0.4671 0.0081 0.0213 0.040 0.630 0.117 29.808 0.071 0.519 1.775 0.22 97428. 0.0275
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62.17 1.2675 -0.0006 0.0000 0.0118 0.022 0.349 0.000 16.506 0.039 0.000 -0.002 0.22 98150. 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 0.1342 0.0708 0.259 3.271 3.006 193.490 0.370 13.369 7.046 0.26 107415. 0.5535
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2.71 0.0443 0.0816 0.1338 0.0726 0.266 3.351 2.997 198.234 0.379 13.330 6.857 0.26 107550. 0.5379
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5.43 0.0885 0.1584 0.1333 0.0745 0.273 3.440 2.987 203.524 0.389 13.288 6.657 0.26 107707. 0.5214
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8.14 0.1328 0.2302 0.1329 0.0766 0.281 3.539 2.977 209.331 0.400 13.240 6.450 0.26 107888. 0.5042
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10.86 0.1771 0.2968 0.1323 0.0789 0.289 3.645 2.964 215.604 0.412 13.184 6.236 0.26 108095. 0.4864
|
|
13.57 0.2213 0.3581 0.1316 0.0814 0.298 3.757 2.949 222.253 0.424 13.117 6.018 0.26 108329. 0.4683
|
|
16.29 0.2656 0.4141 0.1308 0.0839 0.307 3.874 2.930 229.153 0.438 13.034 5.800 0.26 108593. 0.4499
|
|
19.00 0.3099 0.4650 0.1297 0.0864 0.317 3.992 2.907 236.136 0.451 12.929 5.583 0.26 108886. 0.4313
|
|
21.71 0.3541 0.5112 0.1284 0.0890 0.326 4.108 2.877 242.993 0.464 12.797 5.370 0.26 109211. 0.4127
|
|
24.43 0.3984 0.5529 0.1267 0.0913 0.335 4.217 2.840 249.477 0.476 12.630 5.163 0.26 109567. 0.3942
|
|
27.14 0.4427 0.5904 0.1247 0.0935 0.342 4.316 2.793 255.306 0.488 12.423 4.962 0.26 109956. 0.3757
|
|
29.86 0.4869 0.6242 0.1221 0.0952 0.349 4.398 2.736 260.173 0.497 12.168 4.769 0.26 110377. 0.3574
|
|
32.57 0.5312 0.6546 0.1190 0.0966 0.354 4.459 2.666 263.749 0.504 11.858 4.584 0.26 110830. 0.3392
|
|
35.28 0.5755 0.6819 0.1153 0.0973 0.356 4.491 2.582 265.684 0.507 11.485 4.408 0.26 111316. 0.3210
|
|
38.00 0.6197 0.7063 0.1108 0.0972 0.356 4.490 2.483 265.612 0.507 11.044 4.240 0.26 111834. 0.3027
|
|
40.71 0.6640 0.7282 0.1057 0.0964 0.353 4.449 2.368 263.202 0.503 10.531 4.080 0.26 112384. 0.2845
|
|
43.43 0.7083 0.7477 0.0998 0.0946 0.346 4.366 2.236 258.272 0.493 9.947 3.927 0.26 112964. 0.2661
|
|
46.14 0.7525 0.7649 0.0933 0.0918 0.336 4.241 2.091 250.851 0.479 9.302 3.781 0.26 113575. 0.2478
|
|
48.86 0.7968 0.7797 0.0864 0.0883 0.323 4.076 1.935 241.105 0.460 8.608 3.641 0.26 114215. 0.2295
|
|
51.57 0.8411 0.7921 0.0790 0.0839 0.307 3.875 1.771 229.226 0.438 7.876 3.504 0.27 114884. 0.2112
|
|
54.28 0.8853 0.8015 0.0714 0.0789 0.289 3.641 1.599 215.382 0.411 7.114 3.368 0.27 115581. 0.1930
|
|
57.00 0.9296 0.8076 0.0635 0.0731 0.268 3.376 1.423 199.706 0.381 6.330 3.232 0.27 116305. 0.1747
|
|
59.71 0.9739 0.8094 0.0555 0.0667 0.244 3.082 1.243 182.301 0.348 5.528 3.092 0.27 117057. 0.1562
|
|
62.43 1.0181 0.8055 0.0473 0.0598 0.219 2.760 1.059 163.249 0.312 4.712 2.943 0.27 117835. 0.1373
|
|
65.14 1.0624 0.7934 0.0390 0.0522 0.191 2.411 0.874 142.627 0.272 3.886 2.778 0.27 118640. 0.1177
|
|
67.85 1.1067 0.7685 0.0306 0.0441 0.162 2.037 0.686 120.513 0.230 3.053 2.583 0.27 119470. 0.0970
|
|
70.57 1.1509 0.7210 0.0222 0.0355 0.130 1.640 0.498 97.003 0.185 2.217 2.331 0.27 120325. 0.0746
|
|
73.28 1.1952 0.6269 0.0139 0.0264 0.097 1.221 0.311 72.213 0.138 1.382 1.951 0.27 121204. 0.0493
|
|
76.00 1.2395 0.4051 0.0055 0.0169 0.062 0.783 0.124 46.291 0.088 0.552 1.216 0.28 122108. 0.0194
|
|
78.71 1.2837
|
|
|
|
|
|
|
|
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 0.1343 0.0702 0.444 4.668 4.334 331.336 0.527 19.277 5.933 0.31 128896. 0.5596
|
|
3.22 0.0438 0.0816 0.1340 0.0719 0.455 4.782 4.322 339.453 0.540 19.224 5.775 0.31 129055. 0.5440
|
|
6.45 0.0876 0.1585 0.1336 0.0738 0.467 4.909 4.309 348.506 0.555 19.166 5.608 0.31 129241. 0.5275
|
|
9.67 0.1314 0.2303 0.1331 0.0759 0.481 5.050 4.295 358.453 0.570 19.102 5.434 0.31 129455. 0.5103
|
|
12.89 0.1752 0.2970 0.1326 0.0782 0.495 5.201 4.278 369.212 0.588 19.028 5.255 0.31 129700. 0.4925
|
|
16.11 0.2190 0.3584 0.1320 0.0806 0.510 5.362 4.257 380.640 0.606 18.937 5.073 0.31 129976. 0.4743
|
|
19.34 0.2628 0.4145 0.1312 0.0832 0.526 5.530 4.232 392.533 0.625 18.825 4.890 0.31 130287. 0.4559
|
|
22.56 0.3066 0.4657 0.1302 0.0857 0.543 5.700 4.200 404.615 0.644 18.683 4.709 0.31 130633. 0.4373
|
|
25.78 0.3504 0.5120 0.1289 0.0882 0.559 5.868 4.160 416.538 0.663 18.504 4.530 0.31 131015. 0.4187
|
|
29.00 0.3942 0.5538 0.1274 0.0907 0.574 6.028 4.109 427.890 0.681 18.278 4.356 0.31 131435. 0.4001
|
|
32.23 0.4380 0.5916 0.1254 0.0928 0.588 6.173 4.046 438.200 0.697 17.995 4.187 0.31 131892. 0.3816
|
|
35.45 0.4818 0.6256 0.1230 0.0947 0.599 6.296 3.967 446.951 0.711 17.645 4.026 0.31 132388. 0.3633
|
|
38.67 0.5256 0.6562 0.1200 0.0961 0.608 6.390 3.871 453.586 0.722 17.218 3.871 0.31 132922. 0.3451
|
|
41.89 0.5694 0.6838 0.1164 0.0969 0.614 6.445 3.755 457.514 0.728 16.704 3.723 0.31 133494. 0.3269
|
|
45.12 0.6132 0.7085 0.1121 0.0971 0.614 6.454 3.618 458.117 0.729 16.093 3.582 0.31 134104. 0.3087
|
|
48.34 0.6570 0.7307 0.1072 0.0964 0.610 6.407 3.458 454.809 0.724 15.380 3.448 0.31 134751. 0.2905
|
|
51.56 0.7008 0.7506 0.1015 0.0947 0.600 6.300 3.274 447.219 0.712 14.564 3.321 0.32 135434. 0.2723
|
|
54.78 0.7446 0.7684 0.0952 0.0922 0.584 6.133 3.071 435.334 0.693 13.658 3.199 0.32 136153. 0.2540
|
|
58.01 0.7884 0.7839 0.0884 0.0889 0.562 5.908 2.850 419.400 0.667 12.679 3.083 0.32 136907. 0.2358
|
|
61.23 0.8322 0.7972 0.0811 0.0847 0.536 5.631 2.617 399.744 0.636 11.642 2.970 0.32 137695. 0.2177
|
|
64.45 0.8760 0.8079 0.0736 0.0798 0.505 5.306 2.374 376.659 0.599 10.561 2.859 0.32 138516. 0.1996
|
|
67.68 0.9198 0.8155 0.0658 0.0742 0.470 4.936 2.123 350.383 0.558 9.445 2.749 0.32 139370. 0.1815
|
|
70.90 0.9636 0.8195 0.0579 0.0680 0.431 4.523 1.867 321.099 0.511 8.303 2.637 0.32 140255. 0.1632
|
|
74.12 1.0074 0.8187 0.0498 0.0612 0.387 4.071 1.605 288.954 0.460 7.140 2.520 0.32 141172. 0.1446
|
|
77.34 1.0512 0.8111 0.0415 0.0538 0.341 3.579 1.340 254.077 0.404 5.960 2.392 0.33 142119. 0.1255
|
|
80.57 1.0950 0.7932 0.0332 0.0459 0.290 3.051 1.072 216.599 0.345 4.770 2.246 0.33 143097. 0.1054
|
|
83.79 1.1388 0.7578 0.0249 0.0374 0.237 2.489 0.804 176.672 0.281 3.574 2.063 0.33 144105. 0.0838
|
|
87.01 1.1826 0.6876 0.0166 0.0285 0.180 1.894 0.534 134.482 0.214 2.377 1.803 0.33 145141. 0.0597
|
|
90.23 1.2264 0.5300 0.0083 0.0191 0.121 1.272 0.267 90.266 0.144 1.186 1.340 0.33 146206. 0.0314
|
|
93.46 1.2702 0.0061 0.0000 0.0094 0.059 0.624 0.001 44.269 0.070 0.006 0.015 0.33 147291. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 7000
|
|
|
|
V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
|
|
(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
|
|
0.00 0.0000 0.0000 0.1345 0.0698 0.702 6.319 5.907 523.324 0.714 26.274 5.120 0.36 150375. 0.5638
|
|
3.76 0.0438 0.0822 0.1342 0.0715 0.719 6.475 5.891 536.231 0.732 26.205 4.983 0.36 150562. 0.5480
|
|
7.53 0.0877 0.1597 0.1338 0.0735 0.738 6.649 5.875 550.651 0.751 26.131 4.839 0.36 150778. 0.5314
|
|
11.29 0.1315 0.2321 0.1334 0.0756 0.760 6.841 5.856 566.525 0.773 26.048 4.689 0.36 151028. 0.5141
|
|
15.05 0.1754 0.2992 0.1329 0.0779 0.783 7.048 5.835 583.727 0.796 25.952 4.534 0.36 151314. 0.4962
|
|
18.82 0.2192 0.3610 0.1323 0.0803 0.807 7.269 5.808 602.038 0.821 25.836 4.376 0.36 151637. 0.4779
|
|
22.58 0.2631 0.4175 0.1315 0.0829 0.833 7.500 5.776 621.133 0.847 25.691 4.218 0.36 151999. 0.4593
|
|
26.35 0.3069 0.4690 0.1306 0.0855 0.859 7.735 5.734 640.576 0.874 25.506 4.060 0.36 152403. 0.4406
|
|
30.11 0.3508 0.5155 0.1294 0.0880 0.885 7.967 5.681 659.811 0.900 25.270 3.905 0.36 152850. 0.4218
|
|
33.87 0.3946 0.5576 0.1278 0.0905 0.909 8.189 5.614 678.173 0.925 24.971 3.755 0.36 153341. 0.4031
|
|
37.64 0.4385 0.5955 0.1259 0.0927 0.932 8.391 5.529 694.900 0.948 24.593 3.609 0.36 153875. 0.3845
|
|
41.40 0.4823 0.6296 0.1235 0.0946 0.951 8.563 5.424 709.152 0.967 24.124 3.469 0.36 154455. 0.3661
|
|
45.16 0.5261 0.6603 0.1206 0.0961 0.966 8.694 5.294 720.027 0.982 23.549 3.335 0.36 155079. 0.3477
|
|
48.93 0.5700 0.6880 0.1170 0.0969 0.974 8.773 5.138 726.566 0.991 22.854 3.208 0.37 155748. 0.3294
|
|
52.69 0.6138 0.7129 0.1128 0.0971 0.976 8.788 4.952 727.765 0.993 22.026 3.086 0.37 156461. 0.3112
|
|
56.46 0.6577 0.7353 0.1078 0.0964 0.969 8.726 4.733 722.677 0.986 21.054 2.971 0.37 157217. 0.2929
|
|
60.22 0.7015 0.7554 0.1021 0.0948 0.953 8.581 4.483 710.691 0.970 19.942 2.861 0.37 158017. 0.2745
|
|
63.98 0.7454 0.7734 0.0958 0.0923 0.928 8.353 4.205 691.776 0.944 18.705 2.757 0.37 158858. 0.2562
|
|
67.75 0.7892 0.7893 0.0889 0.0889 0.894 8.046 3.904 666.327 0.909 17.365 2.657 0.37 159739. 0.2379
|
|
71.51 0.8331 0.8029 0.0816 0.0847 0.851 7.666 3.585 634.866 0.866 15.946 2.561 0.37 160661. 0.2197
|
|
75.27 0.8769 0.8142 0.0741 0.0798 0.802 7.219 3.252 597.869 0.816 14.465 2.467 0.37 161621. 0.2016
|
|
79.04 0.9208 0.8225 0.0662 0.0741 0.745 6.710 2.908 555.718 0.758 12.937 2.374 0.37 162619. 0.1834
|
|
82.80 0.9646 0.8274 0.0582 0.0679 0.682 6.142 2.556 508.710 0.694 11.371 2.279 0.38 163654. 0.1651
|
|
86.56 1.0084 0.8277 0.0501 0.0610 0.613 5.519 2.198 457.079 0.624 9.776 2.181 0.38 164726. 0.1465
|
|
90.33 1.0523 0.8216 0.0418 0.0535 0.538 4.842 1.835 401.037 0.547 8.160 2.075 0.38 165834. 0.1273
|
|
94.09 1.0961 0.8057 0.0334 0.0455 0.457 4.115 1.468 340.793 0.465 6.528 1.953 0.38 166977. 0.1072
|
|
97.86 1.1400 0.7730 0.0250 0.0369 0.371 3.340 1.099 276.591 0.377 4.888 1.802 0.38 168155. 0.0856
|
|
101.62 1.1838 0.7064 0.0166 0.0278 0.280 2.520 0.730 208.735 0.285 3.246 1.586 0.38 169366. 0.0614
|
|
105.38 1.2277 0.5519 0.0083 0.0184 0.185 1.662 0.362 137.609 0.188 1.612 1.195 0.39 170611. 0.0326
|
|
109.15 1.2715 -0.0048 0.0000 0.0085 0.085 0.768 -0.001 63.597 0.087 -0.006 -0.010 0.39 171877. 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 0.1347 0.0696 1.045 8.232 7.726 779.124 0.930 34.366 4.498 0.41 171853. 0.5665
|
|
4.30 0.0439 0.0826 0.1344 0.0714 1.071 8.435 7.707 798.392 0.953 34.280 4.378 0.41 172066. 0.5507
|
|
8.61 0.0877 0.1605 0.1340 0.0733 1.100 8.663 7.686 819.958 0.979 34.189 4.252 0.41 172314. 0.5341
|
|
12.91 0.1316 0.2332 0.1336 0.0754 1.131 8.914 7.664 843.748 1.007 34.089 4.120 0.41 172599. 0.5168
|
|
17.22 0.1755 0.3007 0.1332 0.0777 1.166 9.187 7.638 869.584 1.038 33.972 3.984 0.41 172925. 0.4989
|
|
21.52 0.2194 0.3628 0.1326 0.0802 1.203 9.479 7.606 897.153 1.071 33.830 3.845 0.41 173294. 0.4805
|
|
25.82 0.2632 0.4195 0.1319 0.0828 1.242 9.783 7.565 925.977 1.105 33.651 3.706 0.41 173709. 0.4619
|
|
30.13 0.3071 0.4712 0.1310 0.0854 1.281 10.094 7.514 955.406 1.140 33.422 3.567 0.41 174171. 0.4431
|
|
34.43 0.3510 0.5179 0.1299 0.0880 1.320 10.403 7.448 984.604 1.175 33.128 3.431 0.41 174682. 0.4243
|
|
38.74 0.3949 0.5601 0.1284 0.0905 1.358 10.698 7.363 1012.564 1.209 32.750 3.298 0.41 175243. 0.4055
|
|
43.04 0.4387 0.5981 0.1265 0.0928 1.392 10.968 7.255 1038.127 1.239 32.270 3.170 0.41 175854. 0.3869
|
|
47.34 0.4826 0.6323 0.1241 0.0947 1.421 11.199 7.120 1060.007 1.265 31.670 3.047 0.42 176517. 0.3684
|
|
51.65 0.5265 0.6632 0.1212 0.0962 1.444 11.377 6.954 1076.829 1.285 30.930 2.929 0.42 177232. 0.3500
|
|
55.95 0.5703 0.6910 0.1177 0.0972 1.458 11.486 6.751 1087.129 1.298 30.031 2.817 0.42 177997. 0.3316
|
|
60.26 0.6142 0.7160 0.1135 0.0974 1.461 11.510 6.510 1089.373 1.300 28.955 2.710 0.42 178814. 0.3133
|
|
64.56 0.6581 0.7385 0.1085 0.0967 1.451 11.433 6.225 1082.110 1.292 27.689 2.609 0.42 179680. 0.2950
|
|
68.86 0.7020 0.7588 0.1028 0.0951 1.427 11.246 5.898 1064.396 1.271 26.235 2.513 0.42 180595. 0.2766
|
|
73.17 0.7458 0.7770 0.0965 0.0926 1.390 10.947 5.534 1036.160 1.237 24.615 2.422 0.42 181558. 0.2582
|
|
77.47 0.7897 0.7932 0.0896 0.0892 1.338 10.544 5.139 997.993 1.191 22.858 2.336 0.42 182567. 0.2399
|
|
81.78 0.8336 0.8073 0.0823 0.0850 1.275 10.044 4.720 950.686 1.135 20.994 2.252 0.43 183622. 0.2217
|
|
86.08 0.8774 0.8190 0.0747 0.0800 1.200 9.456 4.282 894.967 1.068 19.048 2.170 0.43 184720. 0.2035
|
|
90.38 0.9213 0.8280 0.0668 0.0743 1.115 8.784 3.830 831.415 0.992 17.037 2.090 0.43 185863. 0.1853
|
|
94.69 0.9652 0.8337 0.0587 0.0680 1.020 8.035 3.367 760.485 0.908 14.977 2.008 0.43 187048. 0.1670
|
|
98.99 1.0091 0.8350 0.0505 0.0610 0.915 7.211 2.895 682.534 0.815 12.878 1.924 0.43 188275. 0.1483
|
|
103.30 1.0529 0.8303 0.0421 0.0534 0.802 6.317 2.417 597.881 0.714 10.750 1.833 0.43 189542. 0.1291
|
|
107.60 1.0968 0.8162 0.0337 0.0453 0.680 5.355 1.934 506.844 0.605 8.601 1.730 0.44 190850. 0.1090
|
|
111.90 1.1407 0.7861 0.0252 0.0366 0.550 4.330 1.448 409.793 0.489 6.439 1.602 0.44 192198. 0.0874
|
|
116.21 1.1846 0.7231 0.0168 0.0275 0.412 3.246 0.961 307.187 0.367 4.276 1.419 0.44 193585. 0.0631
|
|
120.51 1.2284 0.5728 0.0083 0.0178 0.268 2.109 0.477 199.613 0.238 2.122 1.084 0.44 195008. 0.0339
|
|
124.82 1.2723 -0.0072 0.0000 0.0078 0.118 0.926 -0.003 87.636 0.105 -0.011 -0.013 0.44 196456. 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 0.1349 0.0696 1.487 10.414 9.793 1108.908 1.177 43.559 4.006 0.46 193330. 0.5680
|
|
4.84 0.0439 0.0828 0.1346 0.0713 1.524 10.672 9.770 1136.314 1.206 43.457 3.900 0.46 193569. 0.5523
|
|
9.69 0.0878 0.1609 0.1343 0.0733 1.565 10.960 9.746 1167.053 1.238 43.350 3.788 0.46 193847. 0.5358
|
|
14.53 0.1317 0.2339 0.1339 0.0754 1.611 11.279 9.720 1201.041 1.274 43.233 3.671 0.46 194168. 0.5185
|
|
19.38 0.1756 0.3016 0.1335 0.0777 1.660 11.627 9.689 1238.048 1.314 43.097 3.550 0.46 194535. 0.5007
|
|
24.22 0.2195 0.3639 0.1330 0.0802 1.713 11.999 9.652 1277.646 1.356 42.931 3.426 0.46 194950. 0.4823
|
|
29.07 0.2634 0.4208 0.1323 0.0828 1.769 12.389 9.605 1319.172 1.400 42.721 3.302 0.46 195416. 0.4637
|
|
33.91 0.3073 0.4726 0.1315 0.0855 1.826 12.788 9.543 1361.703 1.445 42.449 3.179 0.46 195936. 0.4450
|
|
38.76 0.3512 0.5195 0.1304 0.0881 1.883 13.186 9.464 1404.044 1.490 42.096 3.057 0.47 196511. 0.4262
|
|
43.60 0.3951 0.5617 0.1290 0.0907 1.937 13.568 9.361 1444.739 1.533 41.638 2.939 0.47 197142. 0.4074
|
|
48.44 0.4389 0.5999 0.1271 0.0930 1.988 13.919 9.229 1482.096 1.573 41.051 2.824 0.47 197831. 0.3888
|
|
53.29 0.4828 0.6342 0.1248 0.0951 2.031 14.221 9.063 1514.243 1.607 40.310 2.715 0.47 198577. 0.3703
|
|
58.13 0.5267 0.6651 0.1220 0.0966 2.064 14.455 8.856 1539.161 1.633 39.391 2.610 0.47 199382. 0.3519
|
|
62.98 0.5706 0.6930 0.1185 0.0976 2.085 14.601 8.603 1554.714 1.650 38.267 2.510 0.47 200244. 0.3336
|
|
67.82 0.6145 0.7181 0.1143 0.0978 2.090 14.638 8.299 1558.665 1.654 36.916 2.415 0.47 201164. 0.3153
|
|
72.67 0.6584 0.7408 0.1094 0.0972 2.077 14.546 7.941 1548.888 1.643 35.320 2.325 0.47 202140. 0.2969
|
|
77.51 0.7023 0.7612 0.1037 0.0957 2.044 14.312 7.527 1523.976 1.617 33.480 2.240 0.47 203171. 0.2785
|
|
82.36 0.7462 0.7797 0.0973 0.0931 1.990 13.935 7.065 1483.790 1.574 31.424 2.160 0.48 204256. 0.2601
|
|
87.20 0.7901 0.7962 0.0904 0.0897 1.917 13.422 6.563 1429.170 1.516 29.190 2.083 0.48 205393. 0.2418
|
|
92.05 0.8340 0.8106 0.0831 0.0855 1.825 12.784 6.029 1361.269 1.444 26.817 2.009 0.48 206581. 0.2235
|
|
96.89 0.8779 0.8228 0.0754 0.0804 1.718 12.032 5.471 1281.150 1.359 24.337 1.937 0.48 207820. 0.2053
|
|
101.73 0.9218 0.8323 0.0674 0.0747 1.595 11.173 4.895 1189.663 1.262 21.773 1.866 0.48 209107. 0.1871
|
|
106.58 0.9657 0.8387 0.0593 0.0683 1.458 10.213 4.304 1087.468 1.154 19.143 1.795 0.48 210442. 0.1687
|
|
111.42 1.0096 0.8410 0.0510 0.0612 1.308 9.157 3.701 975.089 1.035 16.463 1.722 0.49 211824. 0.1501
|
|
116.27 1.0535 0.8375 0.0426 0.0535 1.144 8.011 3.090 852.985 0.905 13.744 1.643 0.49 213252. 0.1309
|
|
121.11 1.0974 0.8251 0.0341 0.0453 0.968 6.777 2.472 721.619 0.766 10.997 1.554 0.49 214725. 0.1107
|
|
125.96 1.1413 0.7973 0.0255 0.0365 0.780 5.461 1.851 581.523 0.617 8.234 1.444 0.49 216243. 0.0890
|
|
130.80 1.1852 0.7377 0.0169 0.0272 0.581 4.070 1.229 433.360 0.460 5.468 1.287 0.49 217804. 0.0646
|
|
135.65 1.2291 0.5917 0.0084 0.0175 0.373 2.611 0.610 277.984 0.295 2.712 0.995 0.50 219407. 0.0352
|
|
140.49 1.2729 -0.0101 -0.0001 0.0073 0.156 1.091 -0.004 116.188 0.123 -0.019 -0.016 0.50 221035. 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 0.1351 0.0697 2.043 12.877 12.109 1523.484 1.455 53.862 3.605 0.51 214804. 0.5685
|
|
5.42 0.0442 0.0834 0.1348 0.0714 2.094 13.196 12.083 1561.268 1.491 53.744 3.510 0.51 215072. 0.5529
|
|
10.84 0.0884 0.1621 0.1345 0.0734 2.151 13.556 12.055 1603.777 1.531 53.621 3.409 0.51 215384. 0.5364
|
|
16.27 0.1326 0.2356 0.1342 0.0756 2.214 13.954 12.025 1650.925 1.577 53.488 3.304 0.51 215743. 0.5191
|
|
21.69 0.1769 0.3038 0.1338 0.0779 2.283 14.389 11.991 1702.430 1.626 53.334 3.195 0.51 216154. 0.5012
|
|
27.11 0.2211 0.3665 0.1333 0.0804 2.357 14.857 11.948 1757.715 1.678 53.146 3.083 0.51 216620. 0.4829
|
|
32.53 0.2653 0.4237 0.1327 0.0831 2.435 15.348 11.894 1815.874 1.734 52.905 2.971 0.52 217143. 0.4643
|
|
37.96 0.3095 0.4757 0.1319 0.0858 2.515 15.853 11.823 1875.608 1.791 52.589 2.859 0.52 217727. 0.4455
|
|
43.38 0.3537 0.5228 0.1309 0.0886 2.595 16.357 11.729 1935.223 1.848 52.172 2.749 0.52 218374. 0.4266
|
|
48.80 0.3979 0.5652 0.1295 0.0912 2.672 16.842 11.606 1992.622 1.903 51.624 2.642 0.52 219084. 0.4078
|
|
54.22 0.4422 0.6034 0.1277 0.0936 2.743 17.288 11.446 2045.360 1.953 50.913 2.538 0.52 219859. 0.3891
|
|
59.64 0.4864 0.6377 0.1255 0.0957 2.804 17.671 11.242 2090.719 1.996 50.006 2.439 0.52 220699. 0.3705
|
|
65.07 0.5306 0.6687 0.1226 0.0973 2.851 17.968 10.987 2125.772 2.030 48.869 2.344 0.52 221606. 0.3521
|
|
70.49 0.5748 0.6966 0.1191 0.0983 2.880 18.151 10.672 2147.421 2.051 47.471 2.254 0.52 222577. 0.3337
|
|
75.91 0.6190 0.7218 0.1148 0.0985 2.886 18.193 10.292 2152.441 2.055 45.780 2.169 0.52 223614. 0.3153
|
|
81.33 0.6632 0.7445 0.1098 0.0978 2.867 18.069 9.841 2137.805 2.041 43.774 2.088 0.53 224713. 0.2968
|
|
86.76 0.7075 0.7651 0.1040 0.0962 2.818 17.763 9.321 2101.603 2.007 41.458 2.012 0.53 225875. 0.2783
|
|
92.18 0.7517 0.7837 0.0975 0.0935 2.741 17.274 8.738 2043.765 1.952 38.868 1.939 0.53 227097. 0.2598
|
|
97.60 0.7959 0.8003 0.0904 0.0899 2.636 16.613 8.106 1965.566 1.877 36.054 1.870 0.53 228379. 0.2413
|
|
103.02 0.8401 0.8149 0.0830 0.0855 2.506 15.794 7.434 1868.672 1.784 33.065 1.804 0.53 229717. 0.2229
|
|
108.44 0.8843 0.8273 0.0751 0.0803 2.353 14.830 6.731 1754.581 1.676 29.941 1.740 0.53 231112. 0.2046
|
|
113.87 0.9285 0.8370 0.0670 0.0743 2.178 13.731 6.006 1624.485 1.551 26.713 1.677 0.54 232562. 0.1862
|
|
119.29 0.9728 0.8436 0.0587 0.0677 1.984 12.503 5.261 1479.301 1.413 23.403 1.613 0.54 234065. 0.1677
|
|
124.71 1.0170 0.8461 0.0502 0.0604 1.770 11.155 4.503 1319.764 1.260 20.029 1.548 0.54 235621. 0.1488
|
|
130.13 1.0612 0.8426 0.0417 0.0525 1.538 9.691 3.733 1146.524 1.095 16.605 1.477 0.54 237229. 0.1293
|
|
135.55 1.1054 0.8297 0.0330 0.0439 1.288 8.116 2.956 960.249 0.917 13.147 1.396 0.54 238887. 0.1088
|
|
140.98 1.1496 0.8000 0.0243 0.0349 1.021 6.438 2.174 761.716 0.727 9.670 1.294 0.55 240596. 0.0865
|
|
146.40 1.1938 0.7339 0.0155 0.0253 0.740 4.665 1.391 551.913 0.527 6.189 1.143 0.55 242353. 0.0611
|
|
151.82 1.2381 0.5569 0.0068 0.0152 0.445 2.807 0.613 332.114 0.317 2.725 0.837 0.55 244157. 0.0297
|
|
157.24 1.2823
|
|
|
|
|
|
|
|
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 0.1354 0.0700 2.728 15.633 14.677 2034.485 1.766 65.283 3.272 0.57 236277. 0.5680
|
|
5.93 0.0439 0.0828 0.1351 0.0717 2.795 16.015 14.647 2084.224 1.809 65.150 3.188 0.57 236569. 0.5528
|
|
11.85 0.0879 0.1609 0.1348 0.0736 2.870 16.446 14.617 2140.287 1.858 65.017 3.098 0.57 236908. 0.5366
|
|
17.78 0.1318 0.2340 0.1345 0.0757 2.954 16.925 14.585 2202.621 1.912 64.874 3.003 0.57 237300. 0.5197
|
|
23.70 0.1757 0.3019 0.1342 0.0781 3.045 17.449 14.548 2270.916 1.971 64.710 2.906 0.57 237746. 0.5022
|
|
29.63 0.2196 0.3644 0.1338 0.0806 3.144 18.015 14.503 2344.505 2.035 64.511 2.806 0.57 238253. 0.4842
|
|
35.55 0.2636 0.4216 0.1332 0.0833 3.248 18.612 14.446 2422.262 2.103 64.255 2.705 0.57 238822. 0.4658
|
|
41.48 0.3075 0.4736 0.1325 0.0860 3.356 19.229 14.370 2502.552 2.173 63.916 2.604 0.57 239456. 0.4473
|
|
47.40 0.3514 0.5206 0.1316 0.0888 3.464 19.849 14.267 2583.181 2.243 63.461 2.505 0.57 240158. 0.4288
|
|
53.33 0.3953 0.5630 0.1303 0.0915 3.569 20.450 14.131 2661.400 2.310 62.854 2.408 0.57 240930. 0.4102
|
|
59.25 0.4393 0.6012 0.1287 0.0940 3.666 21.007 13.952 2733.957 2.373 62.057 2.315 0.57 241772. 0.3917
|
|
65.18 0.4832 0.6357 0.1265 0.0962 3.751 21.493 13.720 2797.203 2.428 61.026 2.225 0.57 242685. 0.3734
|
|
71.10 0.5271 0.6667 0.1238 0.0979 3.818 21.877 13.427 2847.191 2.472 59.722 2.139 0.57 243671. 0.3551
|
|
77.03 0.5710 0.6948 0.1205 0.0990 3.862 22.128 13.063 2879.765 2.500 58.103 2.057 0.57 244727. 0.3369
|
|
82.95 0.6150 0.7201 0.1164 0.0994 3.876 22.211 12.619 2890.592 2.509 56.131 1.980 0.58 245854. 0.3187
|
|
88.88 0.6589 0.7431 0.1115 0.0989 3.856 22.095 12.090 2875.508 2.496 53.776 1.907 0.58 247050. 0.3005
|
|
94.80 0.7028 0.7639 0.1058 0.0974 3.797 21.758 11.474 2831.649 2.458 51.038 1.838 0.58 248314. 0.2821
|
|
100.73 0.7467 0.7828 0.0994 0.0948 3.699 21.196 10.781 2758.565 2.395 47.953 1.773 0.58 249644. 0.2637
|
|
106.66 0.7907 0.7998 0.0924 0.0914 3.564 20.422 10.023 2657.784 2.307 44.584 1.711 0.58 251038. 0.2454
|
|
112.58 0.8346 0.8149 0.0850 0.0870 3.395 19.452 9.216 2531.539 2.198 40.992 1.651 0.58 252495. 0.2271
|
|
118.51 0.8785 0.8279 0.0772 0.0819 3.194 18.302 8.369 2381.912 2.068 37.226 1.594 0.59 254012. 0.2089
|
|
124.43 0.9225 0.8386 0.0691 0.0760 2.964 16.986 7.492 2210.570 1.919 33.325 1.537 0.59 255590. 0.1907
|
|
130.36 0.9664 0.8463 0.0608 0.0694 2.707 15.512 6.591 2018.798 1.753 29.317 1.481 0.59 257225. 0.1723
|
|
136.28 1.0103 0.8502 0.0523 0.0621 2.424 13.889 5.671 1807.614 1.569 25.227 1.423 0.59 258918. 0.1536
|
|
142.21 1.0542 0.8489 0.0437 0.0543 2.116 12.124 4.737 1577.895 1.370 21.071 1.362 0.60 260667. 0.1343
|
|
148.13 1.0982 0.8396 0.0350 0.0457 1.784 10.223 3.792 1330.508 1.155 16.868 1.293 0.60 262472. 0.1141
|
|
154.06 1.1421 0.8160 0.0262 0.0367 1.430 8.194 2.841 1066.448 0.926 12.635 1.208 0.60 264330. 0.0923
|
|
159.98 1.1860 0.7627 0.0174 0.0271 1.055 6.047 1.887 786.966 0.683 8.392 1.087 0.60 266242. 0.0677
|
|
165.91 1.2299 0.6253 0.0086 0.0170 0.662 3.793 0.936 493.682 0.429 4.162 0.860 0.61 268204. 0.0377
|
|
171.83 1.2739 -0.0144 -0.0001 0.0065 0.252 1.445 -0.008 188.017 0.163 -0.035 -0.019 0.61 270192. 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 0.1356 0.0703 3.562 18.708 17.497 2656.078 2.114 77.829 2.988 0.62 257748. 0.5663
|
|
6.46 0.0439 0.0825 0.1353 0.0720 3.648 19.159 17.465 2720.101 2.165 77.684 2.912 0.62 258066. 0.5515
|
|
12.93 0.0878 0.1605 0.1351 0.0740 3.745 19.669 17.433 2792.482 2.222 77.540 2.832 0.62 258435. 0.5357
|
|
19.39 0.1318 0.2335 0.1348 0.0761 3.853 20.238 17.399 2873.229 2.286 77.391 2.747 0.62 258861. 0.5191
|
|
25.85 0.1757 0.3013 0.1345 0.0784 3.972 20.863 17.361 2962.046 2.357 77.223 2.658 0.62 259347. 0.5019
|
|
32.32 0.2196 0.3639 0.1342 0.0810 4.101 21.540 17.316 3058.175 2.434 77.019 2.568 0.62 259899. 0.4842
|
|
38.78 0.2635 0.4211 0.1337 0.0837 4.238 22.259 17.256 3160.268 2.515 76.755 2.477 0.62 260518. 0.4662
|
|
45.25 0.3075 0.4731 0.1331 0.0865 4.380 23.006 17.176 3266.279 2.599 76.399 2.385 0.62 261209. 0.4479
|
|
51.71 0.3514 0.5202 0.1323 0.0893 4.524 23.761 17.066 3373.385 2.684 75.912 2.295 0.62 261973. 0.4295
|
|
58.17 0.3953 0.5627 0.1311 0.0921 4.664 24.497 16.918 3477.967 2.768 75.249 2.206 0.62 262814. 0.4112
|
|
64.64 0.4392 0.6009 0.1295 0.0947 4.795 25.185 16.718 3575.665 2.845 74.361 2.121 0.62 263732. 0.3929
|
|
71.10 0.4832 0.6354 0.1275 0.0970 4.910 25.790 16.456 3661.533 2.914 73.196 2.038 0.62 264728. 0.3747
|
|
77.56 0.5271 0.6665 0.1249 0.0988 5.002 26.274 16.120 3730.225 2.968 71.701 1.960 0.63 265803. 0.3566
|
|
84.03 0.5710 0.6946 0.1216 0.1000 5.064 26.597 15.698 3776.118 3.005 69.826 1.886 0.63 266956. 0.3385
|
|
90.49 0.6149 0.7200 0.1176 0.1005 5.087 26.719 15.180 3793.385 3.019 67.521 1.815 0.63 268186. 0.3204
|
|
96.95 0.6589 0.7431 0.1128 0.1000 5.064 26.599 14.557 3776.394 3.005 64.748 1.748 0.63 269492. 0.3023
|
|
103.42 0.7028 0.7641 0.1071 0.0985 4.990 26.210 13.827 3721.159 2.961 61.504 1.685 0.63 270872. 0.2840
|
|
109.88 0.7467 0.7832 0.1008 0.0961 4.864 25.546 13.002 3626.906 2.886 57.831 1.626 0.63 272324. 0.2657
|
|
116.35 0.7906 0.8006 0.0937 0.0926 4.688 24.621 12.096 3495.600 2.782 53.805 1.570 0.64 273846. 0.2474
|
|
122.81 0.8346 0.8160 0.0862 0.0882 4.466 23.457 11.129 3330.244 2.650 49.500 1.516 0.64 275437. 0.2291
|
|
129.27 0.8785 0.8295 0.0784 0.0830 4.202 22.072 10.112 3133.669 2.494 44.978 1.464 0.64 277094. 0.2109
|
|
135.74 0.9224 0.8406 0.0702 0.0770 3.900 20.484 9.057 2908.143 2.314 40.287 1.413 0.64 278816. 0.1926
|
|
142.20 0.9663 0.8490 0.0618 0.0703 3.561 18.703 7.973 2655.398 2.113 35.463 1.362 0.64 280602. 0.1742
|
|
148.66 1.0103 0.8538 0.0532 0.0629 3.187 16.741 6.865 2376.813 1.891 30.534 1.310 0.65 282450. 0.1555
|
|
155.13 1.0542 0.8536 0.0445 0.0549 2.781 14.605 5.738 2073.555 1.650 25.522 1.255 0.65 284359. 0.1362
|
|
161.59 1.0981 0.8456 0.0356 0.0463 2.342 12.303 4.597 1746.765 1.390 20.448 1.194 0.65 286328. 0.1160
|
|
168.05 1.1420 0.8242 0.0267 0.0370 1.874 9.845 3.447 1397.746 1.112 15.334 1.119 0.66 288356. 0.0941
|
|
174.52 1.1859 0.7743 0.0178 0.0272 1.379 7.242 2.294 1028.141 0.818 10.204 1.012 0.66 290442. 0.0695
|
|
180.98 1.2299 0.6427 0.0089 0.0170 0.858 4.509 1.143 640.101 0.509 5.085 0.810 0.66 292583. 0.0392
|
|
187.45 1.2738 0.0006 0.0000 0.0062 0.316 1.659 0.000 235.593 0.187 0.002 0.001 0.67 294751. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 13000
|
|
|
|
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 0.1358 0.0712 4.583 22.221 20.571 3417.710 2.511 91.499 2.730 0.67 279216. 0.5610
|
|
7.00 0.0439 0.0818 0.1356 0.0729 4.691 22.742 20.536 3497.792 2.569 91.342 2.663 0.67 279560. 0.5468
|
|
14.01 0.0879 0.1591 0.1354 0.0747 4.812 23.332 20.502 3588.572 2.636 91.193 2.591 0.67 279959. 0.5316
|
|
21.01 0.1318 0.2317 0.1351 0.0769 4.949 23.992 20.468 3690.148 2.711 91.042 2.516 0.67 280420. 0.5157
|
|
28.02 0.1757 0.2993 0.1349 0.0792 5.099 24.721 20.431 3802.255 2.793 90.878 2.437 0.67 280946. 0.4992
|
|
35.02 0.2197 0.3618 0.1346 0.0817 5.262 25.513 20.387 3924.074 2.882 90.680 2.356 0.67 281542. 0.4821
|
|
42.02 0.2636 0.4190 0.1342 0.0844 5.437 26.358 20.329 4054.041 2.978 90.422 2.274 0.67 282211. 0.4646
|
|
49.03 0.3075 0.4712 0.1337 0.0873 5.618 27.240 20.249 4189.699 3.078 90.067 2.192 0.67 282958. 0.4470
|
|
56.03 0.3515 0.5184 0.1330 0.0901 5.803 28.137 20.137 4327.560 3.179 89.568 2.111 0.67 283786. 0.4291
|
|
63.03 0.3954 0.5611 0.1319 0.0930 5.985 29.018 19.980 4463.083 3.278 88.872 2.031 0.67 284695. 0.4113
|
|
70.04 0.4393 0.5996 0.1305 0.0956 6.156 29.848 19.765 4590.714 3.372 87.917 1.953 0.67 285689. 0.3934
|
|
77.04 0.4833 0.6343 0.1286 0.0980 6.308 30.584 19.477 4704.048 3.455 86.635 1.878 0.68 286768. 0.3756
|
|
84.05 0.5272 0.6656 0.1261 0.0999 6.432 31.182 19.101 4796.030 3.523 84.962 1.806 0.68 287933. 0.3577
|
|
91.05 0.5711 0.6938 0.1230 0.1012 6.516 31.593 18.622 4859.160 3.569 82.832 1.738 0.68 289183. 0.3399
|
|
98.05 0.6151 0.7194 0.1190 0.1018 6.552 31.765 18.027 4885.616 3.589 80.185 1.674 0.68 290517. 0.3220
|
|
105.06 0.6590 0.7426 0.1143 0.1014 6.528 31.649 17.305 4867.751 3.576 76.973 1.612 0.68 291933. 0.3039
|
|
112.06 0.7029 0.7638 0.1086 0.1000 6.437 31.208 16.454 4799.948 3.526 73.186 1.555 0.68 293431. 0.2858
|
|
119.07 0.7469 0.7832 0.1022 0.0975 6.277 30.434 15.484 4680.896 3.438 68.874 1.500 0.69 295006. 0.2675
|
|
126.07 0.7908 0.8008 0.0952 0.0940 6.052 29.343 14.417 4513.064 3.315 64.125 1.449 0.69 296658. 0.2493
|
|
133.07 0.8347 0.8166 0.0876 0.0896 5.767 27.960 13.271 4300.441 3.159 59.031 1.400 0.69 298384. 0.2311
|
|
140.08 0.8787 0.8305 0.0797 0.0843 5.427 26.311 12.066 4046.838 2.973 53.669 1.352 0.69 300183. 0.2129
|
|
147.08 0.9226 0.8421 0.0714 0.0782 5.036 24.416 10.813 3755.298 2.758 48.097 1.306 0.70 302051. 0.1946
|
|
154.08 0.9665 0.8511 0.0629 0.0714 4.597 22.289 9.523 3428.116 2.518 42.359 1.260 0.70 303988. 0.1762
|
|
161.09 1.0105 0.8567 0.0542 0.0639 4.113 19.942 8.203 3067.117 2.253 36.488 1.213 0.70 305992. 0.1574
|
|
168.09 1.0544 0.8575 0.0453 0.0557 3.586 17.385 6.860 2673.839 1.964 30.513 1.164 0.70 308063. 0.1381
|
|
175.10 1.0983 0.8510 0.0363 0.0469 3.017 14.627 5.499 2249.759 1.653 24.458 1.109 0.71 310198. 0.1178
|
|
182.10 1.1423 0.8314 0.0272 0.0374 2.409 11.681 4.125 1796.634 1.320 18.349 1.041 0.71 312397. 0.0958
|
|
189.10 1.1862 0.7841 0.0181 0.0274 1.766 8.562 2.746 1316.860 0.967 12.214 0.946 0.71 314658. 0.0710
|
|
196.11 1.2301 0.6555 0.0090 0.0170 1.091 5.291 1.368 813.794 0.598 6.085 0.762 0.72 316979. 0.0404
|
|
203.11 1.2741 -0.0036 0.0000 0.0061 0.390 1.891 -0.003 290.795 0.214 -0.011 -0.004 0.72 319326. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 14000
|
|
|
|
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 0.1360 0.0731 5.874 26.447 23.893 4380.588 2.988 106.276 2.474 0.72 300682. 0.5479
|
|
7.54 0.0439 0.0799 0.1358 0.0747 6.006 27.038 23.855 4478.414 3.055 106.107 2.416 0.72 301051. 0.5347
|
|
15.08 0.0879 0.1557 0.1356 0.0765 6.155 27.709 23.820 4589.594 3.131 105.952 2.354 0.72 301481. 0.5206
|
|
22.62 0.1318 0.2270 0.1354 0.0786 6.322 28.462 23.787 4714.323 3.216 105.804 2.289 0.72 301975. 0.5057
|
|
30.17 0.1757 0.2936 0.1352 0.0809 6.507 29.295 23.752 4852.366 3.310 105.649 2.220 0.72 302540. 0.4903
|
|
37.71 0.2196 0.3554 0.1350 0.0834 6.709 30.204 23.711 5002.814 3.412 105.467 2.150 0.72 303180. 0.4743
|
|
45.25 0.2636 0.4122 0.1347 0.0861 6.925 31.176 23.658 5163.852 3.522 105.231 2.078 0.72 303899. 0.4580
|
|
52.79 0.3075 0.4642 0.1343 0.0889 7.151 32.194 23.583 5332.500 3.637 104.899 2.006 0.72 304702. 0.4414
|
|
60.33 0.3514 0.5116 0.1337 0.0918 7.382 33.232 23.475 5504.417 3.755 104.419 1.934 0.72 305590. 0.4247
|
|
67.87 0.3954 0.5547 0.1328 0.0946 7.609 34.255 23.319 5673.860 3.870 103.725 1.864 0.72 306567. 0.4079
|
|
75.42 0.4393 0.5937 0.1315 0.0973 7.823 35.220 23.098 5833.782 3.979 102.740 1.796 0.73 307636. 0.3911
|
|
82.96 0.4832 0.6291 0.1298 0.0997 8.014 36.080 22.793 5976.087 4.076 101.382 1.730 0.73 308797. 0.3742
|
|
90.50 0.5271 0.6612 0.1274 0.1016 8.169 36.779 22.385 6091.913 4.155 99.567 1.667 0.73 310050. 0.3573
|
|
98.04 0.5711 0.6903 0.1244 0.1029 8.277 37.262 21.855 6171.898 4.210 97.211 1.606 0.73 311396. 0.3402
|
|
105.58 0.6150 0.7167 0.1206 0.1035 8.323 37.469 21.187 6206.309 4.233 94.238 1.548 0.73 312833. 0.3229
|
|
113.12 0.6589 0.7406 0.1159 0.1032 8.295 37.344 20.366 6185.530 4.219 90.586 1.493 0.73 314360. 0.3054
|
|
120.66 0.7028 0.7623 0.1104 0.1018 8.183 36.840 19.388 6102.092 4.162 86.239 1.441 0.74 315974. 0.2875
|
|
128.21 0.7468 0.7822 0.1040 0.0993 7.984 35.944 18.266 5953.595 4.061 81.249 1.392 0.74 317673. 0.2695
|
|
135.75 0.7907 0.8002 0.0969 0.0958 7.701 34.670 17.024 5742.627 3.917 75.721 1.345 0.74 319454. 0.2514
|
|
143.29 0.8346 0.8164 0.0893 0.0913 7.341 33.048 15.685 5473.965 3.734 69.766 1.300 0.74 321315. 0.2332
|
|
150.83 0.8786 0.8307 0.0813 0.0859 6.909 31.106 14.271 5152.362 3.514 63.479 1.256 0.75 323254. 0.2151
|
|
158.37 0.9225 0.8430 0.0729 0.0797 6.412 28.869 12.800 4781.768 3.262 56.933 1.214 0.75 325268. 0.1968
|
|
165.91 0.9664 0.8526 0.0642 0.0728 5.854 26.354 11.282 4365.169 2.977 50.181 1.172 0.75 327356. 0.1784
|
|
173.46 1.0103 0.8590 0.0554 0.0651 5.237 23.576 9.726 3904.983 2.664 43.262 1.130 0.76 329516. 0.1596
|
|
181.00 1.0543 0.8608 0.0463 0.0568 4.564 20.548 8.141 3403.449 2.321 36.209 1.085 0.76 331747. 0.1403
|
|
188.54 1.0982 0.8553 0.0372 0.0477 3.839 17.285 6.532 2863.010 1.953 29.053 1.035 0.76 334048. 0.1198
|
|
196.08 1.1421 0.8364 0.0279 0.0381 3.067 13.806 4.905 2286.749 1.560 21.819 0.973 0.77 336417. 0.0976
|
|
203.62 1.1861 0.7884 0.0186 0.0280 2.251 10.136 3.269 1678.919 1.145 14.541 0.883 0.77 338852. 0.0724
|
|
211.16 1.2300 0.6549 0.0093 0.0174 1.402 6.311 1.631 1045.380 0.713 7.253 0.707 0.77 341352. 0.0409
|
|
218.70 1.2739 -0.0047 0.0000 0.0065 0.526 2.369 -0.004 392.313 0.268 -0.019 -0.005 0.78 343879. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 15000
|
|
|
|
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 0.1362 0.0767 7.582 31.858 27.455 5653.752 3.599 122.118 2.203 0.77 322143. 0.5229
|
|
8.08 0.0439 0.0763 0.1360 0.0783 7.739 32.520 27.413 5771.202 3.674 121.933 2.154 0.77 322538. 0.5111
|
|
16.15 0.0878 0.1489 0.1358 0.0801 7.919 33.274 27.376 5905.078 3.759 121.768 2.103 0.77 322997. 0.4985
|
|
24.23 0.1317 0.2175 0.1356 0.0821 8.121 34.123 27.343 6055.691 3.855 121.620 2.048 0.77 323526. 0.4852
|
|
32.31 0.1756 0.2819 0.1354 0.0844 8.345 35.065 27.310 6222.852 3.962 121.476 1.991 0.77 324130. 0.4714
|
|
40.38 0.2195 0.3419 0.1353 0.0869 8.590 36.094 27.274 6405.558 4.078 121.317 1.931 0.77 324813. 0.4570
|
|
48.46 0.2634 0.3974 0.1350 0.0895 8.853 37.199 27.229 6601.669 4.203 121.114 1.871 0.77 325581. 0.4423
|
|
56.54 0.3074 0.4486 0.1347 0.0923 9.129 38.359 27.164 6807.553 4.334 120.826 1.810 0.77 326437. 0.4274
|
|
64.61 0.3513 0.4955 0.1342 0.0952 9.411 39.544 27.067 7017.723 4.468 120.394 1.749 0.78 327385. 0.4124
|
|
72.69 0.3952 0.5386 0.1335 0.0980 9.688 40.710 26.920 7224.672 4.599 119.742 1.690 0.78 328429. 0.3973
|
|
80.77 0.4391 0.5781 0.1324 0.1006 9.949 41.805 26.704 7419.084 4.723 118.780 1.633 0.78 329570. 0.3823
|
|
88.84 0.4830 0.6143 0.1309 0.1029 10.179 42.770 26.395 7590.376 4.832 117.404 1.577 0.78 330811. 0.3672
|
|
96.92 0.5269 0.6476 0.1288 0.1048 10.362 43.542 25.968 7727.265 4.919 115.506 1.524 0.78 332152. 0.3520
|
|
105.00 0.5708 0.6783 0.1260 0.1060 10.484 44.054 25.400 7818.233 4.977 112.979 1.474 0.78 333593. 0.3365
|
|
113.07 0.6147 0.7064 0.1223 0.1065 10.529 44.243 24.669 7851.698 4.999 109.726 1.425 0.79 335132. 0.3207
|
|
121.15 0.6586 0.7321 0.1178 0.1060 10.482 44.044 23.756 7816.405 4.976 105.665 1.378 0.79 336768. 0.3044
|
|
129.23 0.7025 0.7557 0.1124 0.1045 10.331 43.408 22.654 7703.559 4.904 100.767 1.334 0.79 338499. 0.2877
|
|
137.30 0.7464 0.7771 0.1060 0.1018 10.071 42.319 21.377 7510.184 4.781 95.085 1.291 0.79 340321. 0.2705
|
|
145.38 0.7903 0.7966 0.0989 0.0982 9.708 40.794 19.950 7239.547 4.609 88.739 1.250 0.79 342231. 0.2530
|
|
153.46 0.8343 0.8141 0.0913 0.0935 9.250 38.868 18.404 6897.850 4.391 81.862 1.210 0.80 344227. 0.2352
|
|
161.53 0.8782 0.8296 0.0831 0.0880 8.705 36.576 16.765 6491.083 4.132 74.570 1.171 0.80 346306. 0.2173
|
|
169.61 0.9221 0.8427 0.0747 0.0817 8.078 33.944 15.053 6023.881 3.835 66.955 1.133 0.80 348465. 0.1992
|
|
177.69 0.9660 0.8532 0.0659 0.0746 7.376 30.992 13.282 5500.079 3.501 59.079 1.095 0.81 350704. 0.1809
|
|
185.76 1.0099 0.8601 0.0569 0.0668 6.602 27.741 11.464 4923.150 3.134 50.992 1.056 0.81 353019. 0.1620
|
|
193.84 1.0538 0.8619 0.0476 0.0583 5.761 24.208 9.607 4296.185 2.735 42.732 1.014 0.81 355411. 0.1424
|
|
201.92 1.0977 0.8552 0.0383 0.0491 4.859 20.419 7.719 3623.729 2.307 34.332 0.966 0.82 357876. 0.1216
|
|
209.99 1.1416 0.8325 0.0288 0.0395 3.905 16.408 5.805 2911.809 1.854 25.822 0.904 0.82 360414. 0.0987
|
|
218.07 1.1855 0.7749 0.0192 0.0294 2.908 12.218 3.875 2168.229 1.380 17.234 0.811 0.82 363022. 0.0723
|
|
226.15 1.2294 0.6202 0.0096 0.0190 1.882 7.907 1.935 1403.308 0.893 8.609 0.626 0.83 365699. 0.0394
|
|
234.22 1.2733 -0.0037 0.0000 0.0085 0.842 3.538 -0.005 627.938 0.400 -0.022 -0.004 0.83 368412. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 16000
|
|
|
|
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 0.1362 0.0828 9.942 39.164 31.241 7413.677 4.425 138.959 1.911 0.82 343601. 0.4841
|
|
8.62 0.0439 0.0707 0.1360 0.0844 10.129 39.900 31.192 7552.963 4.508 138.742 1.873 0.82 344021. 0.4740
|
|
17.23 0.0878 0.1384 0.1358 0.0862 10.343 40.742 31.150 7712.418 4.603 138.555 1.832 0.82 344510. 0.4633
|
|
25.85 0.1317 0.2026 0.1356 0.0882 10.584 41.693 31.114 7892.498 4.710 138.396 1.788 0.82 345073. 0.4519
|
|
34.46 0.1756 0.2632 0.1355 0.0904 10.853 42.753 31.082 8093.090 4.830 138.253 1.742 0.82 345716. 0.4400
|
|
43.08 0.2195 0.3199 0.1353 0.0929 11.148 43.915 31.050 8313.011 4.961 138.109 1.694 0.82 346443. 0.4277
|
|
51.69 0.2635 0.3728 0.1352 0.0955 11.466 45.167 31.011 8550.004 5.103 137.939 1.645 0.82 347259. 0.4151
|
|
60.31 0.3074 0.4219 0.1349 0.0983 11.801 46.486 30.958 8799.692 5.252 137.702 1.596 0.83 348170. 0.4023
|
|
68.92 0.3513 0.4673 0.1346 0.1012 12.143 47.835 30.876 9055.181 5.404 137.337 1.547 0.83 349178. 0.3894
|
|
77.54 0.3952 0.5094 0.1340 0.1040 12.480 49.163 30.747 9306.479 5.554 136.764 1.499 0.83 350287. 0.3765
|
|
86.15 0.4391 0.5485 0.1332 0.1066 12.795 50.401 30.548 9540.915 5.694 135.876 1.452 0.83 351501. 0.3637
|
|
94.77 0.4830 0.5850 0.1319 0.1089 13.066 51.472 30.249 9743.564 5.815 134.549 1.408 0.83 352821. 0.3509
|
|
103.38 0.5269 0.6193 0.1300 0.1106 13.275 52.292 29.821 9898.799 5.908 132.644 1.366 0.83 354250. 0.3381
|
|
112.00 0.5708 0.6516 0.1274 0.1116 13.399 52.781 29.232 9991.423 5.963 130.023 1.327 0.84 355786. 0.3251
|
|
120.61 0.6147 0.6819 0.1240 0.1118 13.421 52.867 28.452 10007.755 5.973 126.556 1.290 0.84 357429. 0.3117
|
|
129.23 0.6586 0.7102 0.1197 0.1110 13.323 52.484 27.459 9935.236 5.930 122.137 1.254 0.84 359176. 0.2976
|
|
137.84 0.7026 0.7366 0.1144 0.1091 13.095 51.583 26.240 9764.598 5.828 116.716 1.219 0.84 361024. 0.2829
|
|
146.46 0.7465 0.7610 0.1081 0.1061 12.732 50.155 24.809 9494.236 5.666 110.348 1.185 0.84 362971. 0.2675
|
|
155.08 0.7904 0.7834 0.1011 0.1020 12.243 48.228 23.194 9129.531 5.449 103.166 1.152 0.85 365013. 0.2515
|
|
163.69 0.8343 0.8037 0.0934 0.0970 11.638 45.847 21.430 8678.702 5.180 95.323 1.120 0.85 367147. 0.2349
|
|
172.31 0.8782 0.8218 0.0852 0.0911 10.930 43.055 19.550 8150.188 4.864 86.959 1.088 0.85 369369. 0.2180
|
|
180.92 0.9221 0.8375 0.0766 0.0844 10.125 39.887 17.578 7550.487 4.506 78.186 1.056 0.86 371677. 0.2006
|
|
189.54 0.9660 0.8502 0.0677 0.0769 9.233 36.372 15.532 6885.162 4.109 69.085 1.023 0.86 374069. 0.1827
|
|
198.15 1.0099 0.8576 0.0585 0.0689 8.270 32.580 13.423 6167.301 3.681 59.706 0.987 0.86 376542. 0.1639
|
|
206.77 1.0538 0.8569 0.0491 0.0604 7.246 28.543 11.261 5403.165 3.225 50.089 0.945 0.87 379096. 0.1437
|
|
215.38 1.0977 0.8444 0.0395 0.0513 6.159 24.264 9.056 4593.079 2.741 40.280 0.894 0.87 381729. 0.1219
|
|
224.00 1.1416 0.8101 0.0297 0.0419 5.025 19.797 6.816 3747.470 2.237 30.315 0.825 0.87 384438. 0.0976
|
|
232.61 1.1856 0.7307 0.0198 0.0322 3.862 15.215 4.550 2880.208 1.719 20.238 0.717 0.88 387222. 0.0693
|
|
241.23 1.2295 0.5425 0.0099 0.0224 2.692 10.606 2.271 2007.736 1.198 10.101 0.513 0.88 390080. 0.0350
|
|
249.84 1.2734 -0.0032 0.0000 0.0128 1.538 6.059 -0.007 1146.945 0.685 -0.033 -0.003 0.89 392987. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 17000
|
|
|
|
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 0.1355 0.0904 13.021 48.277 35.083 9709.963 5.454 156.048 1.639 0.87 365107. 0.4398
|
|
9.17 0.0440 0.0647 0.1352 0.0919 13.237 49.078 35.022 9871.141 5.545 155.779 1.609 0.87 365554. 0.4315
|
|
18.35 0.0880 0.1268 0.1350 0.0937 13.489 50.012 34.971 10058.830 5.650 155.553 1.577 0.87 366073. 0.4225
|
|
27.52 0.1320 0.1860 0.1349 0.0957 13.778 51.082 34.930 10274.201 5.771 155.367 1.542 0.87 366670. 0.4129
|
|
36.69 0.1760 0.2421 0.1347 0.0979 14.101 52.282 34.894 10515.415 5.907 155.208 1.505 0.87 367352. 0.4029
|
|
45.87 0.2200 0.2948 0.1346 0.1004 14.461 53.616 34.863 10783.790 6.058 155.069 1.466 0.88 368122. 0.3923
|
|
55.04 0.2640 0.3441 0.1345 0.1032 14.855 55.074 34.831 11077.070 6.222 154.928 1.426 0.88 368988. 0.3814
|
|
64.21 0.3080 0.3900 0.1343 0.1061 15.275 56.632 34.790 11390.307 6.398 154.748 1.385 0.88 369952. 0.3703
|
|
73.38 0.3520 0.4326 0.1341 0.1091 15.710 58.246 34.728 11715.007 6.581 154.471 1.345 0.88 371019. 0.3590
|
|
82.56 0.3960 0.4722 0.1337 0.1121 16.143 59.853 34.626 12038.155 6.762 154.016 1.305 0.88 372194. 0.3479
|
|
91.73 0.4400 0.5093 0.1330 0.1150 16.551 61.362 34.458 12341.763 6.933 153.268 1.266 0.88 373479. 0.3368
|
|
100.90 0.4840 0.5443 0.1320 0.1174 16.902 62.664 34.191 12603.631 7.080 152.080 1.230 0.88 374879. 0.3260
|
|
110.08 0.5280 0.5778 0.1304 0.1192 17.162 63.628 33.785 12797.438 7.189 150.275 1.197 0.89 376395. 0.3154
|
|
119.25 0.5720 0.6102 0.1282 0.1202 17.303 64.152 33.201 12902.836 7.248 147.679 1.167 0.89 378027. 0.3047
|
|
128.42 0.6160 0.6414 0.1251 0.1202 17.300 64.142 32.401 12900.805 7.247 144.121 1.139 0.89 379776. 0.2938
|
|
137.60 0.6600 0.6714 0.1211 0.1190 17.132 63.519 31.352 12775.640 7.176 139.452 1.113 0.89 381638. 0.2824
|
|
146.77 0.7040 0.7002 0.1160 0.1166 16.786 62.236 30.034 12517.451 7.031 133.591 1.088 0.89 383610. 0.2702
|
|
155.94 0.7480 0.7277 0.1099 0.1129 16.261 60.289 28.457 12126.024 6.811 126.575 1.064 0.90 385689. 0.2573
|
|
165.12 0.7920 0.7535 0.1029 0.1082 15.575 57.744 26.655 11614.053 6.524 118.561 1.041 0.90 387870. 0.2435
|
|
174.29 0.8360 0.7775 0.0953 0.1024 14.747 54.675 24.670 10996.838 6.177 109.733 1.018 0.90 390149. 0.2290
|
|
183.46 0.8800 0.7993 0.0870 0.0958 13.796 51.150 22.540 10287.828 5.779 100.260 0.994 0.91 392524. 0.2138
|
|
192.64 0.9240 0.8186 0.0784 0.0885 12.734 47.214 20.294 9496.099 5.334 90.269 0.969 0.91 394990. 0.1979
|
|
201.81 0.9681 0.8351 0.0693 0.0804 11.570 42.895 17.954 8627.544 4.846 79.860 0.944 0.91 397545. 0.1812
|
|
210.98 1.0121 0.8452 0.0600 0.0718 10.338 38.330 15.532 7709.398 4.331 69.084 0.914 0.92 400188. 0.1632
|
|
220.15 1.0561 0.8404 0.0503 0.0632 9.101 33.743 13.028 6786.692 3.812 57.949 0.871 0.92 402915. 0.1424
|
|
229.33 1.1001 0.8153 0.0404 0.0545 7.846 29.090 10.461 5850.848 3.287 46.529 0.811 0.93 405726. 0.1188
|
|
238.50 1.1441 0.7602 0.0303 0.0456 6.566 24.342 7.848 4895.971 2.750 34.910 0.727 0.93 408618. 0.0923
|
|
247.67 1.1881 0.6503 0.0201 0.0367 5.290 19.614 5.210 3945.032 2.216 23.172 0.599 0.93 411589. 0.0619
|
|
256.85 1.2321 0.4349 0.0099 0.0281 4.051 15.020 2.572 3020.887 1.697 11.441 0.386 0.94 414637. 0.0281
|
|
266.02 1.2761 -0.0056 -0.0001 0.0200 2.873 10.653 -0.023 2142.612 1.204 -0.101 -0.005 0.94 417752. 0.0000
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