427 lines
76 KiB
Plaintext
427 lines
76 KiB
Plaintext
20.5x20.5E(CD) (205x205E(CD).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 0.1085 0.0551 0.017 1.063 0.635 12.571 0.120 2.823 22.897 0.08 41274. 0.5170
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0.77 0.0395 0.0758 0.1081 0.0562 0.017 1.084 0.632 12.822 0.122 2.812 22.366 0.08 41317. 0.5041
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1.55 0.0789 0.1479 0.1076 0.0575 0.018 1.108 0.630 13.103 0.125 2.801 21.801 0.08 41367. 0.4904
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2.32 0.1184 0.2157 0.1072 0.0588 0.018 1.134 0.627 13.412 0.128 2.789 21.207 0.08 41424. 0.4760
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3.09 0.1578 0.2792 0.1066 0.0603 0.018 1.162 0.624 13.746 0.131 2.775 20.588 0.08 41488. 0.4610
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3.87 0.1973 0.3383 0.1060 0.0618 0.019 1.192 0.620 14.101 0.135 2.759 19.951 0.08 41562. 0.4454
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4.64 0.2367 0.3927 0.1052 0.0634 0.019 1.223 0.616 14.470 0.138 2.739 19.303 0.08 41644. 0.4294
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5.41 0.2762 0.4427 0.1043 0.0651 0.020 1.255 0.610 14.845 0.142 2.715 18.650 0.08 41735. 0.4130
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6.19 0.3157 0.4883 0.1032 0.0667 0.020 1.286 0.604 15.214 0.145 2.685 17.999 0.08 41836. 0.3964
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6.96 0.3551 0.5297 0.1018 0.0683 0.021 1.316 0.596 15.566 0.149 2.649 17.357 0.08 41947. 0.3797
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7.73 0.3946 0.5672 0.1001 0.0697 0.021 1.343 0.586 15.885 0.152 2.606 16.727 0.08 42068. 0.3629
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8.51 0.4340 0.6010 0.0981 0.0708 0.022 1.366 0.574 16.157 0.154 2.553 16.114 0.08 42199. 0.3461
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9.28 0.4735 0.6315 0.0957 0.0718 0.022 1.383 0.560 16.366 0.156 2.491 15.520 0.08 42340. 0.3292
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10.06 0.5130 0.6589 0.0929 0.0723 0.022 1.394 0.544 16.496 0.158 2.418 14.948 0.08 42492. 0.3124
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10.83 0.5524 0.6834 0.0897 0.0725 0.022 1.397 0.525 16.531 0.158 2.334 14.396 0.08 42653. 0.2956
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11.60 0.5919 0.7052 0.0860 0.0721 0.022 1.391 0.503 16.453 0.157 2.237 13.864 0.08 42825. 0.2787
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12.38 0.6313 0.7244 0.0817 0.0712 0.022 1.373 0.478 16.243 0.155 2.127 13.352 0.08 43007. 0.2617
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13.15 0.6708 0.7411 0.0769 0.0696 0.021 1.342 0.450 15.883 0.152 2.003 12.856 0.08 43199. 0.2445
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13.92 0.7102 0.7551 0.0717 0.0674 0.021 1.299 0.419 15.370 0.147 1.865 12.372 0.08 43401. 0.2271
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14.70 0.7497 0.7662 0.0659 0.0645 0.020 1.244 0.386 14.713 0.141 1.716 11.892 0.08 43612. 0.2094
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15.47 0.7892 0.7736 0.0599 0.0611 0.019 1.177 0.350 13.927 0.133 1.558 11.407 0.08 43832. 0.1914
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16.24 0.8286 0.7764 0.0535 0.0571 0.017 1.101 0.313 13.024 0.124 1.393 10.904 0.08 44062. 0.1729
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17.02 0.8681 0.7734 0.0470 0.0527 0.016 1.016 0.275 12.018 0.115 1.222 10.368 0.09 44301. 0.1540
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17.79 0.9075 0.7627 0.0402 0.0479 0.015 0.923 0.235 10.919 0.104 1.047 9.780 0.09 44549. 0.1345
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18.56 0.9470 0.7414 0.0334 0.0427 0.013 0.823 0.196 9.738 0.093 0.870 9.110 0.09 44805. 0.1142
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19.34 0.9864 0.7045 0.0266 0.0372 0.011 0.717 0.155 8.486 0.081 0.692 8.311 0.09 45070. 0.0929
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20.11 1.0259 0.6436 0.0197 0.0315 0.010 0.606 0.115 7.174 0.069 0.514 7.300 0.09 45343. 0.0703
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20.88 1.0654 0.5416 0.0130 0.0255 0.008 0.492 0.076 5.816 0.056 0.337 5.916 0.09 45625. 0.0462
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21.66 1.1048 0.3604 0.0063 0.0194 0.006 0.374 0.037 4.427 0.042 0.165 3.796 0.09 45914. 0.0207
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22.43 1.1443 -0.0084 -0.0001 0.0133 0.004 0.255 -0.001 3.023 0.029 -0.003 -0.086 0.09 46212. 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 0.1087 0.0522 0.128 4.026 2.545 95.254 0.455 11.320 12.118 0.16 82547. 0.5480
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1.55 0.0396 0.0805 0.1084 0.0533 0.130 4.112 2.536 97.308 0.465 11.281 11.822 0.16 82633. 0.5337
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3.11 0.0793 0.1568 0.1080 0.0546 0.134 4.209 2.527 99.605 0.476 11.240 11.507 0.16 82733. 0.5185
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4.66 0.1189 0.2284 0.1075 0.0560 0.137 4.316 2.516 102.136 0.488 11.193 11.175 0.16 82848. 0.5025
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6.22 0.1585 0.2951 0.1070 0.0575 0.141 4.432 2.505 104.879 0.501 11.140 10.831 0.16 82979. 0.4859
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7.77 0.1982 0.3569 0.1064 0.0591 0.145 4.556 2.490 107.801 0.515 11.077 10.478 0.16 83126. 0.4687
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9.32 0.2378 0.4136 0.1057 0.0608 0.149 4.685 2.473 110.848 0.529 11.000 10.120 0.16 83292. 0.4511
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10.88 0.2774 0.4654 0.1048 0.0625 0.153 4.816 2.452 113.951 0.544 10.906 9.760 0.16 83476. 0.4332
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12.43 0.3171 0.5124 0.1036 0.0641 0.157 4.946 2.426 117.023 0.559 10.790 9.402 0.17 83679. 0.4151
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13.98 0.3567 0.5549 0.1023 0.0657 0.161 5.070 2.394 119.960 0.573 10.648 9.051 0.17 83903. 0.3969
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15.54 0.3963 0.5932 0.1006 0.0672 0.164 5.183 2.355 122.646 0.586 10.474 8.708 0.17 84146. 0.3788
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17.09 0.4360 0.6276 0.0986 0.0685 0.168 5.281 2.307 124.953 0.597 10.264 8.376 0.17 84410. 0.3607
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18.65 0.4756 0.6585 0.0962 0.0695 0.170 5.357 2.251 126.752 0.605 10.014 8.056 0.17 84695. 0.3426
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20.20 0.5153 0.6863 0.0934 0.0701 0.172 5.406 2.185 127.909 0.611 9.720 7.749 0.17 85001. 0.3247
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21.75 0.5549 0.7110 0.0901 0.0703 0.172 5.422 2.109 128.290 0.613 9.380 7.456 0.17 85327. 0.3069
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23.31 0.5945 0.7331 0.0863 0.0700 0.171 5.399 2.021 127.749 0.610 8.989 7.175 0.17 85673. 0.2891
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24.86 0.6342 0.7528 0.0821 0.0691 0.169 5.330 1.921 126.120 0.602 8.542 6.907 0.17 86040. 0.2713
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26.42 0.6738 0.7701 0.0772 0.0676 0.165 5.209 1.807 123.261 0.589 8.038 6.650 0.17 86427. 0.2534
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27.97 0.7134 0.7850 0.0719 0.0653 0.160 5.035 1.682 119.140 0.569 7.480 6.402 0.17 86834. 0.2353
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29.52 0.7531 0.7974 0.0661 0.0624 0.153 4.811 1.546 113.834 0.544 6.877 6.161 0.17 87260. 0.2171
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31.08 0.7927 0.8066 0.0599 0.0589 0.144 4.541 1.403 107.452 0.513 6.238 5.920 0.17 87705. 0.1987
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32.63 0.8323 0.8120 0.0535 0.0549 0.134 4.230 1.253 100.098 0.478 5.572 5.676 0.17 88169. 0.1801
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34.19 0.8720 0.8124 0.0469 0.0504 0.123 3.883 1.098 91.871 0.439 4.884 5.421 0.17 88650. 0.1610
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35.74 0.9116 0.8063 0.0402 0.0454 0.111 3.502 0.940 82.857 0.396 4.182 5.147 0.17 89149. 0.1415
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37.29 0.9512 0.7910 0.0333 0.0401 0.098 3.091 0.780 73.145 0.349 3.471 4.839 0.17 89666. 0.1212
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38.85 0.9909 0.7619 0.0265 0.0344 0.084 2.655 0.620 62.828 0.300 2.757 4.474 0.17 90200. 0.0998
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40.40 1.0305 0.7104 0.0196 0.0285 0.070 2.198 0.460 52.005 0.248 2.046 4.011 0.17 90751. 0.0771
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41.95 1.0701 0.6179 0.0129 0.0224 0.055 1.724 0.302 40.792 0.195 1.344 3.359 0.17 91319. 0.0523
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43.51 1.1098 0.4367 0.0063 0.0161 0.039 1.239 0.148 29.315 0.140 0.658 2.289 0.17 91903. 0.0250
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45.06 1.1494 -0.0054 0.0000 0.0097 0.024 0.749 -0.001 17.712 0.085 -0.005 -0.027 0.17 92502. 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 0.1090 0.0511 0.422 8.858 5.737 314.396 1.001 25.520 8.277 0.25 123819. 0.5620
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2.33 0.0397 0.0826 0.1086 0.0522 0.431 9.055 5.719 321.385 1.023 25.437 8.071 0.25 123949. 0.5471
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4.67 0.0794 0.1607 0.1082 0.0535 0.441 9.275 5.699 329.217 1.048 25.348 7.851 0.25 124099. 0.5313
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7.00 0.1191 0.2340 0.1078 0.0549 0.453 9.519 5.677 337.861 1.075 25.250 7.621 0.25 124271. 0.5147
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9.34 0.1588 0.3022 0.1073 0.0564 0.466 9.783 5.651 347.249 1.105 25.136 7.381 0.25 124468. 0.4974
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11.67 0.1985 0.3652 0.1067 0.0580 0.479 10.066 5.621 357.266 1.137 25.001 7.136 0.25 124690. 0.4795
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14.01 0.2382 0.4229 0.1060 0.0597 0.493 10.361 5.583 367.736 1.171 24.835 6.887 0.25 124939. 0.4613
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16.34 0.2779 0.4755 0.1052 0.0615 0.507 10.662 5.537 378.427 1.205 24.630 6.637 0.25 125216. 0.4427
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18.68 0.3176 0.5232 0.1041 0.0632 0.522 10.961 5.480 389.040 1.238 24.376 6.389 0.25 125522. 0.4240
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21.01 0.3573 0.5661 0.1027 0.0648 0.535 11.248 5.409 399.221 1.271 24.061 6.146 0.25 125857. 0.4052
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23.35 0.3970 0.6048 0.1011 0.0664 0.548 11.511 5.323 408.567 1.301 23.675 5.909 0.25 126224. 0.3864
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25.68 0.4367 0.6395 0.0991 0.0677 0.559 11.739 5.217 416.643 1.326 23.207 5.680 0.25 126621. 0.3678
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28.02 0.4764 0.6706 0.0967 0.0687 0.567 11.917 5.092 422.993 1.346 22.648 5.460 0.25 127050. 0.3492
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30.35 0.5161 0.6985 0.0939 0.0694 0.573 12.035 4.943 427.158 1.360 21.989 5.249 0.25 127510. 0.3308
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32.69 0.5558 0.7234 0.0906 0.0696 0.575 12.077 4.771 428.671 1.365 21.222 5.048 0.25 128000. 0.3126
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35.02 0.5955 0.7457 0.0868 0.0693 0.573 12.031 4.573 427.025 1.359 20.339 4.857 0.25 128522. 0.2944
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37.36 0.6352 0.7656 0.0825 0.0685 0.565 11.880 4.346 421.647 1.342 19.330 4.675 0.25 129074. 0.2762
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39.69 0.6749 0.7832 0.0777 0.0669 0.553 11.609 4.089 412.042 1.312 18.188 4.501 0.25 129657. 0.2580
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42.03 0.7146 0.7987 0.0723 0.0647 0.534 11.216 3.805 398.101 1.267 16.924 4.335 0.25 130269. 0.2397
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44.36 0.7543 0.8117 0.0664 0.0617 0.510 10.708 3.498 380.071 1.210 15.557 4.174 0.25 130910. 0.2213
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46.70 0.7940 0.8220 0.0602 0.0582 0.481 10.095 3.172 358.317 1.141 14.110 4.015 0.25 131580. 0.2027
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49.03 0.8337 0.8288 0.0538 0.0541 0.447 9.387 2.832 333.192 1.061 12.599 3.856 0.25 132277. 0.1839
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51.36 0.8734 0.8312 0.0471 0.0495 0.409 8.594 2.482 305.022 0.971 11.042 3.691 0.26 133002. 0.1649
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53.70 0.9131 0.8278 0.0404 0.0445 0.368 7.723 2.125 274.111 0.873 9.452 3.516 0.26 133753. 0.1453
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56.03 0.9529 0.8160 0.0335 0.0391 0.323 6.783 1.763 240.761 0.766 7.843 3.322 0.26 134531. 0.1250
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58.37 0.9926 0.7917 0.0266 0.0333 0.275 5.784 1.400 205.292 0.653 6.229 3.094 0.26 135334. 0.1038
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60.70 1.0323 0.7464 0.0197 0.0273 0.225 4.735 1.039 168.058 0.535 4.622 2.805 0.26 136163. 0.0810
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63.04 1.0720 0.6614 0.0130 0.0210 0.174 3.647 0.683 129.459 0.412 3.039 2.393 0.26 137017. 0.0561
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65.37 1.1117 0.4851 0.0064 0.0146 0.121 2.534 0.336 89.944 0.286 1.493 1.692 0.26 137896. 0.0278
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67.71 1.1514 0.0001 0.0000 0.0081 0.067 1.409 0.000 49.996 0.159 0.000 0.000 0.26 138797. 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 0.1092 0.0505 0.989 15.585 10.221 737.539 1.761 45.461 6.285 0.33 165089. 0.5696
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3.12 0.0397 0.0837 0.1088 0.0517 1.011 15.936 10.190 754.181 1.800 45.323 6.128 0.33 165262. 0.5545
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6.23 0.0795 0.1628 0.1085 0.0530 1.036 16.331 10.156 772.865 1.845 45.176 5.960 0.33 165463. 0.5384
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9.35 0.1192 0.2371 0.1081 0.0544 1.064 16.768 10.120 793.529 1.894 45.012 5.784 0.33 165693. 0.5216
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12.46 0.1590 0.3061 0.1076 0.0559 1.094 17.243 10.077 816.023 1.948 44.823 5.601 0.33 165955. 0.5040
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15.58 0.1987 0.3697 0.1071 0.0576 1.127 17.751 10.026 840.078 2.006 44.596 5.413 0.33 166251. 0.4859
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18.70 0.2384 0.4281 0.1064 0.0593 1.160 18.284 9.963 865.288 2.066 44.317 5.223 0.33 166583. 0.4673
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21.81 0.2782 0.4811 0.1056 0.0611 1.195 18.829 9.885 891.096 2.127 43.968 5.031 0.33 166953. 0.4484
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24.93 0.3179 0.5292 0.1045 0.0628 1.229 19.372 9.787 916.795 2.189 43.533 4.842 0.33 167362. 0.4294
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28.04 0.3577 0.5724 0.1032 0.0645 1.263 19.895 9.665 941.530 2.248 42.989 4.656 0.33 167810. 0.4103
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31.16 0.3974 0.6113 0.1016 0.0661 1.293 20.377 9.514 964.327 2.302 42.318 4.475 0.33 168300. 0.3912
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34.28 0.4372 0.6462 0.0997 0.0674 1.320 20.795 9.330 984.124 2.349 41.499 4.300 0.33 168831. 0.3723
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37.39 0.4769 0.6774 0.0973 0.0685 1.341 21.127 9.109 999.812 2.387 40.516 4.132 0.33 169403. 0.3535
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40.51 0.5166 0.7054 0.0945 0.0692 1.355 21.348 8.847 1010.270 2.412 39.351 3.972 0.33 170017. 0.3349
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43.63 0.5564 0.7304 0.0912 0.0695 1.360 21.434 8.541 1014.356 2.422 37.992 3.819 0.33 170673. 0.3164
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46.74 0.5961 0.7529 0.0875 0.0693 1.356 21.360 8.188 1010.843 2.413 36.422 3.674 0.33 171370. 0.2980
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49.86 0.6359 0.7730 0.0831 0.0684 1.339 21.096 7.784 998.343 2.383 34.623 3.536 0.34 172108. 0.2797
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52.97 0.6756 0.7909 0.0782 0.0668 1.308 20.616 7.325 975.649 2.329 32.584 3.406 0.34 172887. 0.2613
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56.09 0.7153 0.8067 0.0728 0.0646 1.264 19.915 6.817 942.476 2.250 30.322 3.281 0.34 173705. 0.2428
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59.21 0.7551 0.8203 0.0669 0.0616 1.206 19.005 6.267 899.400 2.147 27.875 3.160 0.34 174562. 0.2243
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62.32 0.7948 0.8313 0.0607 0.0580 1.136 17.903 5.684 847.276 2.023 25.280 3.043 0.34 175457. 0.2056
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65.44 0.8346 0.8391 0.0542 0.0539 1.055 16.629 5.075 786.952 1.879 22.573 2.925 0.34 176388. 0.1868
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68.55 0.8743 0.8429 0.0475 0.0493 0.964 15.197 4.447 719.204 1.717 19.780 2.805 0.34 177356. 0.1676
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71.67 0.9140 0.8413 0.0407 0.0442 0.865 13.624 3.806 644.768 1.539 16.930 2.677 0.34 178360. 0.1481
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74.79 0.9538 0.8320 0.0337 0.0387 0.757 11.926 3.158 564.376 1.347 14.045 2.538 0.34 179399. 0.1278
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77.90 0.9935 0.8110 0.0268 0.0328 0.642 10.118 2.507 478.809 1.143 11.151 2.375 0.34 180472. 0.1066
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81.02 1.0333 0.7703 0.0199 0.0266 0.522 8.218 1.860 388.928 0.928 8.272 2.169 0.35 181580. 0.0838
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84.13 1.0730 0.6911 0.0130 0.0203 0.397 6.249 1.222 295.715 0.706 5.434 1.874 0.35 182721. 0.0587
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87.25 1.1128 0.5192 0.0064 0.0137 0.269 4.232 0.599 200.279 0.478 2.666 1.357 0.35 183894. 0.0298
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90.37 1.1525 -0.0021 0.0000 0.0071 0.139 2.193 -0.001 103.799 0.248 -0.005 -0.005 0.35 185097. 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 0.1094 0.0503 1.925 24.262 16.006 1435.215 2.741 71.195 5.058 0.41 206357. 0.5737
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3.90 0.0398 0.0843 0.1091 0.0515 1.968 24.812 15.961 1467.782 2.803 70.995 4.932 0.41 206574. 0.5586
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7.79 0.0795 0.1639 0.1088 0.0528 2.017 25.432 15.914 1504.437 2.873 70.784 4.798 0.41 206824. 0.5425
|
|
11.69 0.1193 0.2387 0.1084 0.0542 2.072 26.119 15.861 1545.080 2.951 70.551 4.656 0.41 207112. 0.5256
|
|
15.59 0.1591 0.3081 0.1080 0.0558 2.131 26.869 15.800 1589.440 3.036 70.280 4.509 0.41 207439. 0.5080
|
|
19.49 0.1988 0.3722 0.1075 0.0574 2.195 27.673 15.727 1637.017 3.126 69.954 4.357 0.41 207810. 0.4898
|
|
23.38 0.2386 0.4309 0.1069 0.0592 2.262 28.518 15.636 1687.031 3.222 69.548 4.204 0.41 208225. 0.4712
|
|
27.28 0.2783 0.4843 0.1061 0.0610 2.331 29.387 15.521 1738.403 3.320 69.037 4.050 0.41 208687. 0.4522
|
|
31.18 0.3181 0.5326 0.1051 0.0628 2.400 30.255 15.376 1789.740 3.418 68.391 3.897 0.41 209198. 0.4331
|
|
35.07 0.3579 0.5761 0.1039 0.0645 2.467 31.093 15.192 1839.349 3.513 67.576 3.746 0.41 209760. 0.4139
|
|
38.97 0.3976 0.6151 0.1023 0.0661 2.528 31.870 14.964 1885.278 3.601 66.560 3.600 0.41 210372. 0.3948
|
|
42.87 0.4374 0.6501 0.1004 0.0675 2.582 32.548 14.683 1925.388 3.677 65.311 3.459 0.41 211036. 0.3757
|
|
46.77 0.4772 0.6814 0.0981 0.0687 2.625 33.090 14.343 1957.440 3.738 63.800 3.324 0.42 211753. 0.3568
|
|
50.66 0.5169 0.7095 0.0953 0.0694 2.654 33.457 13.939 1979.162 3.780 62.000 3.194 0.42 212521. 0.3381
|
|
54.56 0.5567 0.7347 0.0920 0.0697 2.666 33.610 13.464 1988.258 3.797 59.889 3.072 0.42 213342. 0.3195
|
|
58.46 0.5964 0.7573 0.0883 0.0695 2.658 33.509 12.914 1982.264 3.786 57.441 2.955 0.42 214215. 0.3010
|
|
62.36 0.6362 0.7775 0.0840 0.0687 2.626 33.106 12.281 1958.414 3.740 54.627 2.844 0.42 215139. 0.2826
|
|
66.25 0.6760 0.7957 0.0790 0.0671 2.567 32.360 11.562 1914.274 3.656 51.428 2.740 0.42 216113. 0.2641
|
|
70.15 0.7157 0.8118 0.0736 0.0649 2.480 31.260 10.763 1849.212 3.532 47.873 2.640 0.42 217138. 0.2455
|
|
74.05 0.7555 0.8259 0.0677 0.0619 2.366 29.825 9.896 1764.318 3.370 44.019 2.544 0.42 218210. 0.2269
|
|
77.94 0.7953 0.8375 0.0614 0.0583 2.228 28.083 8.977 1661.272 3.173 39.929 2.451 0.42 219330. 0.2081
|
|
81.84 0.8350 0.8461 0.0548 0.0541 2.068 26.062 8.016 1541.747 2.945 35.655 2.358 0.42 220497. 0.1893
|
|
85.74 0.8748 0.8510 0.0480 0.0494 1.887 23.790 7.025 1407.293 2.688 31.245 2.264 0.43 221709. 0.1701
|
|
89.64 0.9145 0.8508 0.0411 0.0442 1.689 21.289 6.012 1259.373 2.405 26.741 2.165 0.43 222965. 0.1505
|
|
93.53 0.9543 0.8435 0.0341 0.0386 1.474 18.586 4.987 1099.458 2.100 22.181 2.057 0.43 224265. 0.1302
|
|
97.43 0.9941 0.8253 0.0271 0.0326 1.246 15.706 3.958 929.110 1.774 17.604 1.932 0.43 225608. 0.1090
|
|
101.33 1.0338 0.7882 0.0201 0.0263 1.006 12.680 2.934 750.070 1.433 13.051 1.774 0.43 226994. 0.0861
|
|
105.22 1.0736 0.7138 0.0132 0.0198 0.757 9.540 1.925 564.320 1.078 8.564 1.547 0.43 228422. 0.0609
|
|
109.12 1.1134 0.5460 0.0064 0.0131 0.502 6.324 0.941 374.112 0.715 4.187 1.141 0.44 229890. 0.0314
|
|
113.02 1.1531 -0.0098 -0.0001 0.0064 0.244 3.074 -0.008 181.826 0.347 -0.035 -0.020 0.44 231394. 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 0.1097 0.0504 3.329 34.974 23.107 2482.675 3.951 102.782 4.222 0.49 247622. 0.5752
|
|
4.67 0.0397 0.0844 0.1094 0.0515 3.405 35.766 23.049 2538.900 4.041 102.522 4.118 0.49 247882. 0.5604
|
|
9.35 0.0795 0.1642 0.1091 0.0528 3.490 36.660 22.988 2602.369 4.142 102.251 4.007 0.49 248182. 0.5445
|
|
14.02 0.1192 0.2391 0.1088 0.0543 3.584 37.654 22.921 2672.960 4.254 101.953 3.889 0.49 248526. 0.5278
|
|
18.70 0.1590 0.3088 0.1084 0.0558 3.688 38.743 22.844 2750.271 4.377 101.608 3.767 0.49 248919. 0.5104
|
|
23.37 0.1987 0.3732 0.1080 0.0575 3.800 39.915 22.749 2833.482 4.510 101.188 3.642 0.49 249363. 0.4923
|
|
28.05 0.2385 0.4321 0.1074 0.0593 3.918 41.153 22.631 2921.297 4.649 100.661 3.514 0.49 249860. 0.4738
|
|
32.72 0.2782 0.4856 0.1067 0.0611 4.039 42.429 22.479 3011.877 4.794 99.987 3.385 0.49 250414. 0.4550
|
|
37.40 0.3180 0.5341 0.1058 0.0630 4.161 43.710 22.285 3102.813 4.938 99.122 3.258 0.50 251027. 0.4359
|
|
42.07 0.3577 0.5777 0.1046 0.0648 4.279 44.954 22.036 3191.136 5.079 98.017 3.132 0.50 251700. 0.4168
|
|
46.75 0.3975 0.6169 0.1031 0.0664 4.390 46.112 21.723 3273.389 5.210 96.622 3.010 0.50 252434. 0.3977
|
|
51.42 0.4372 0.6520 0.1013 0.0679 4.487 47.132 21.333 3345.747 5.325 94.887 2.892 0.50 253230. 0.3786
|
|
56.10 0.4770 0.6834 0.0990 0.0691 4.565 47.955 20.856 3404.182 5.418 92.767 2.779 0.50 254089. 0.3597
|
|
60.77 0.5167 0.7116 0.0963 0.0699 4.619 48.524 20.284 3444.605 5.482 90.224 2.671 0.50 255012. 0.3410
|
|
65.45 0.5565 0.7369 0.0931 0.0703 4.644 48.782 19.609 3462.895 5.511 87.220 2.568 0.50 255996. 0.3224
|
|
70.12 0.5962 0.7597 0.0894 0.0701 4.633 48.666 18.822 3454.682 5.498 83.718 2.471 0.50 257043. 0.3039
|
|
74.80 0.6360 0.7801 0.0850 0.0693 4.580 48.108 17.913 3415.081 5.435 79.676 2.379 0.50 258152. 0.2854
|
|
79.47 0.6757 0.7985 0.0801 0.0678 4.479 47.047 16.876 3339.715 5.315 75.064 2.292 0.50 259321. 0.2669
|
|
84.15 0.7155 0.8150 0.0746 0.0655 4.328 45.463 15.720 3227.278 5.136 69.921 2.209 0.51 260551. 0.2483
|
|
88.82 0.7552 0.8295 0.0687 0.0625 4.130 43.382 14.463 3079.560 4.901 64.331 2.130 0.51 261838. 0.2296
|
|
93.50 0.7949 0.8416 0.0623 0.0589 3.888 40.845 13.126 2899.474 4.615 58.385 2.053 0.51 263182. 0.2109
|
|
98.17 0.8347 0.8510 0.0557 0.0546 3.607 37.894 11.727 2689.969 4.281 52.163 1.977 0.51 264581. 0.1919
|
|
102.85 0.8744 0.8569 0.0488 0.0498 3.291 34.567 10.282 2453.789 3.905 45.734 1.901 0.51 266035. 0.1727
|
|
107.52 0.9142 0.8581 0.0418 0.0445 2.942 30.900 8.804 2193.527 3.491 39.161 1.820 0.51 267543. 0.1531
|
|
112.20 0.9539 0.8526 0.0347 0.0388 2.564 26.932 7.307 1911.795 3.043 32.500 1.733 0.51 269102. 0.1328
|
|
116.87 0.9937 0.8369 0.0275 0.0327 2.161 22.699 5.803 1611.366 2.565 25.810 1.633 0.52 270713. 0.1115
|
|
121.55 1.0334 0.8033 0.0204 0.0263 1.737 18.248 4.305 1295.344 2.062 19.151 1.508 0.52 272376. 0.0887
|
|
126.22 1.0732 0.7341 0.0134 0.0196 1.297 13.626 2.829 967.264 1.539 12.584 1.327 0.52 274088. 0.0633
|
|
130.89 1.1129 0.5727 0.0066 0.0128 0.846 8.891 1.389 631.171 1.005 6.178 0.998 0.52 275849. 0.0333
|
|
135.57 1.1527 -0.0006 0.0000 0.0059 0.391 4.104 -0.001 291.353 0.464 -0.003 -0.001 0.52 277652. 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 0.1100 0.0506 5.313 47.841 31.540 3962.078 5.405 140.288 3.611 0.57 288884. 0.5748
|
|
5.45 0.0397 0.0842 0.1098 0.0518 5.433 48.915 31.470 4051.065 5.526 139.978 3.523 0.57 289186. 0.5603
|
|
10.90 0.0795 0.1640 0.1095 0.0531 5.568 50.132 31.399 4151.884 5.664 139.661 3.430 0.57 289536. 0.5448
|
|
16.36 0.1192 0.2389 0.1092 0.0545 5.719 51.492 31.321 4264.459 5.818 139.317 3.331 0.58 289937. 0.5285
|
|
21.81 0.1589 0.3086 0.1089 0.0561 5.885 52.987 31.232 4388.258 5.986 138.919 3.228 0.58 290394. 0.5114
|
|
27.26 0.1987 0.3730 0.1086 0.0578 6.064 54.603 31.122 4522.105 6.169 138.431 3.122 0.58 290911. 0.4936
|
|
32.71 0.2384 0.4321 0.1081 0.0596 6.255 56.317 30.982 4664.045 6.363 137.808 3.013 0.58 291490. 0.4754
|
|
38.16 0.2781 0.4858 0.1074 0.0615 6.452 58.094 30.799 4811.227 6.563 136.996 2.904 0.58 292136. 0.4568
|
|
43.62 0.3179 0.5344 0.1066 0.0634 6.651 59.888 30.560 4959.835 6.766 135.931 2.795 0.58 292849. 0.4379
|
|
49.07 0.3576 0.5781 0.1055 0.0653 6.846 61.642 30.249 5105.086 6.964 134.546 2.687 0.58 293633. 0.4190
|
|
54.52 0.3973 0.6174 0.1041 0.0670 7.029 63.287 29.848 5241.329 7.150 132.765 2.583 0.58 294489. 0.4000
|
|
59.97 0.4371 0.6525 0.1023 0.0685 7.191 64.747 29.343 5362.229 7.315 130.518 2.482 0.58 295417. 0.3811
|
|
65.42 0.4768 0.6841 0.1002 0.0698 7.323 65.940 28.718 5461.065 7.450 127.736 2.385 0.58 296419. 0.3623
|
|
70.87 0.5165 0.7124 0.0975 0.0707 7.417 66.785 27.959 5530.987 7.545 124.361 2.293 0.58 297494. 0.3436
|
|
76.33 0.5563 0.7378 0.0944 0.0711 7.463 67.197 27.055 5565.123 7.592 120.340 2.205 0.58 298643. 0.3251
|
|
81.78 0.5960 0.7607 0.0907 0.0710 7.451 67.090 25.994 5556.269 7.580 115.620 2.122 0.59 299865. 0.3067
|
|
87.23 0.6357 0.7814 0.0864 0.0703 7.371 66.368 24.762 5496.464 7.498 110.139 2.043 0.59 301158. 0.2882
|
|
92.68 0.6754 0.8001 0.0814 0.0688 7.213 64.943 23.349 5378.425 7.337 103.857 1.969 0.59 302523. 0.2697
|
|
98.13 0.7152 0.8169 0.0759 0.0665 6.973 62.784 21.767 5199.676 7.093 96.819 1.899 0.59 303957. 0.2511
|
|
103.59 0.7549 0.8318 0.0699 0.0634 6.655 59.925 20.041 4962.898 6.770 89.143 1.832 0.59 305459. 0.2324
|
|
109.04 0.7946 0.8445 0.0635 0.0597 6.266 56.422 18.200 4672.746 6.374 80.954 1.767 0.59 307027. 0.2136
|
|
114.49 0.8344 0.8546 0.0567 0.0554 5.812 52.332 16.269 4334.034 5.912 72.366 1.703 0.59 308660. 0.1947
|
|
119.94 0.8741 0.8614 0.0498 0.0505 5.299 47.710 14.271 3951.250 5.390 63.478 1.638 0.60 310356. 0.1754
|
|
125.39 0.9138 0.8638 0.0426 0.0451 4.732 42.607 12.225 3528.664 4.814 54.376 1.571 0.60 312115. 0.1557
|
|
130.85 0.9536 0.8600 0.0354 0.0393 4.118 37.076 10.149 3070.555 4.189 45.142 1.499 0.60 313934. 0.1354
|
|
136.30 0.9933 0.8464 0.0281 0.0330 3.462 31.170 8.062 2581.482 3.522 35.858 1.416 0.60 315813. 0.1140
|
|
141.75 1.0330 0.8159 0.0209 0.0264 2.771 24.953 5.982 2066.548 2.819 26.607 1.313 0.61 317752. 0.0910
|
|
147.20 1.0728 0.7510 0.0137 0.0196 2.054 18.494 3.929 1531.600 2.089 17.478 1.164 0.61 319748. 0.0654
|
|
152.65 1.1125 0.5946 0.0067 0.0126 1.319 11.874 1.926 983.360 1.341 8.569 0.889 0.61 321802. 0.0350
|
|
158.11 1.1522 -0.0047 0.0000 0.0055 0.575 5.180 -0.006 428.973 0.585 -0.029 -0.007 0.61 323903. 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 0.1103 0.0512 8.018 63.167 41.317 5978.731 7.137 183.779 3.134 0.66 330142. 0.5711
|
|
6.23 0.0397 0.0836 0.1101 0.0523 8.193 64.550 41.240 6109.649 7.293 183.435 3.062 0.66 330486. 0.5573
|
|
12.45 0.0794 0.1629 0.1099 0.0536 8.393 66.125 41.164 6258.696 7.471 183.097 2.983 0.66 330885. 0.5425
|
|
18.68 0.1191 0.2375 0.1097 0.0550 8.617 67.892 41.083 6425.958 7.670 182.739 2.900 0.66 331342. 0.5269
|
|
24.90 0.1588 0.3071 0.1095 0.0566 8.865 69.846 40.991 6610.882 7.891 182.329 2.812 0.66 331863. 0.5104
|
|
31.13 0.1985 0.3715 0.1092 0.0583 9.135 71.970 40.877 6811.965 8.131 181.821 2.722 0.66 332452. 0.4933
|
|
37.36 0.2382 0.4306 0.1088 0.0602 9.423 74.238 40.728 7026.549 8.387 181.157 2.629 0.66 333112. 0.4756
|
|
43.58 0.2779 0.4844 0.1082 0.0621 9.723 76.605 40.528 7250.605 8.655 180.266 2.535 0.66 333848. 0.4575
|
|
49.81 0.3176 0.5331 0.1075 0.0640 10.029 79.014 40.257 7478.585 8.927 179.064 2.442 0.66 334662. 0.4391
|
|
56.04 0.3573 0.5771 0.1065 0.0660 10.330 81.388 39.895 7703.352 9.195 177.454 2.349 0.66 335555. 0.4206
|
|
62.26 0.3970 0.6165 0.1053 0.0678 10.616 83.638 39.419 7916.278 9.449 175.334 2.259 0.66 336531. 0.4019
|
|
68.49 0.4367 0.6518 0.1036 0.0694 10.872 85.658 38.804 8107.514 9.678 172.601 2.171 0.66 337591. 0.3833
|
|
74.71 0.4764 0.6835 0.1016 0.0708 11.085 87.337 38.030 8266.395 9.867 169.155 2.087 0.66 338734. 0.3648
|
|
80.94 0.5161 0.7119 0.0990 0.0718 11.240 88.558 37.075 8381.933 10.005 164.911 2.006 0.67 339962. 0.3463
|
|
87.17 0.5558 0.7375 0.0959 0.0723 11.322 89.204 35.924 8443.068 10.078 159.791 1.930 0.67 341274. 0.3279
|
|
93.39 0.5955 0.7606 0.0923 0.0723 11.316 89.154 34.560 8438.415 10.073 153.722 1.858 0.67 342669. 0.3096
|
|
99.62 0.6353 0.7814 0.0880 0.0716 11.205 88.280 32.963 8355.641 9.974 146.618 1.789 0.67 344147. 0.2912
|
|
105.85 0.6750 0.8004 0.0831 0.0701 10.974 86.459 31.120 8183.274 9.768 138.422 1.725 0.67 345706. 0.2728
|
|
112.07 0.7147 0.8175 0.0776 0.0678 10.617 83.644 29.044 7916.854 9.450 129.186 1.664 0.67 347344. 0.2542
|
|
118.30 0.7544 0.8329 0.0715 0.0647 10.138 79.874 26.768 7560.021 9.024 119.064 1.606 0.68 349060. 0.2355
|
|
124.52 0.7941 0.8462 0.0650 0.0610 9.548 75.223 24.331 7119.780 8.499 108.224 1.550 0.68 350852. 0.2167
|
|
130.75 0.8338 0.8570 0.0581 0.0566 8.856 69.769 21.767 6603.555 7.882 96.822 1.495 0.68 352718. 0.1977
|
|
136.98 0.8735 0.8647 0.0510 0.0515 8.071 63.586 19.108 6018.340 7.184 84.991 1.440 0.68 354656. 0.1784
|
|
143.20 0.9132 0.8684 0.0437 0.0460 7.202 56.744 16.378 5370.755 6.411 72.851 1.383 0.68 356664. 0.1587
|
|
149.43 0.9529 0.8661 0.0363 0.0400 6.259 49.313 13.605 4667.449 5.571 60.513 1.322 0.69 358742. 0.1382
|
|
155.65 0.9926 0.8546 0.0289 0.0335 5.251 41.369 10.811 3915.548 4.674 48.088 1.252 0.69 360888. 0.1167
|
|
161.88 1.0323 0.8270 0.0214 0.0267 4.188 32.998 8.024 3123.206 3.728 35.690 1.165 0.69 363101. 0.0936
|
|
168.11 1.0720 0.7659 0.0141 0.0197 3.084 24.300 5.270 2299.974 2.745 23.442 1.039 0.69 365380. 0.0676
|
|
174.33 1.1117 0.6137 0.0069 0.0125 1.954 15.395 2.580 1457.086 1.739 11.475 0.803 0.70 367724. 0.0366
|
|
180.56 1.1514 -0.0110 0.0000 0.0052 0.814 6.411 -0.019 606.809 0.724 -0.083 -0.014 0.70 370121. 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 0.1106 0.0531 11.831 82.851 52.436 8822.012 9.360 233.237 2.696 0.74 371395. 0.5534
|
|
6.99 0.0396 0.0808 0.1105 0.0541 12.072 84.539 52.356 9001.757 9.551 232.878 2.638 0.74 371781. 0.5411
|
|
13.98 0.0792 0.1578 0.1103 0.0554 12.347 86.470 52.281 9207.416 9.769 232.547 2.575 0.74 372227. 0.5279
|
|
20.97 0.1189 0.2306 0.1102 0.0568 12.658 88.648 52.207 9439.328 10.015 232.216 2.509 0.74 372739. 0.5138
|
|
27.96 0.1585 0.2989 0.1100 0.0583 13.004 91.068 52.124 9696.947 10.289 231.848 2.438 0.74 373323. 0.4990
|
|
34.95 0.1981 0.3623 0.1098 0.0600 13.381 93.711 52.021 9978.374 10.587 231.391 2.365 0.74 373982. 0.4834
|
|
41.94 0.2377 0.4209 0.1095 0.0618 13.786 96.544 51.883 10280.067 10.907 230.775 2.289 0.74 374721. 0.4674
|
|
48.93 0.2774 0.4746 0.1091 0.0637 14.210 99.516 51.689 10596.493 11.243 229.912 2.212 0.74 375544. 0.4509
|
|
55.92 0.3170 0.5236 0.1085 0.0657 14.644 102.553 51.415 10919.876 11.586 228.693 2.136 0.74 376455. 0.4341
|
|
62.91 0.3566 0.5680 0.1077 0.0676 15.073 105.560 51.032 11240.100 11.926 226.992 2.059 0.74 377455. 0.4170
|
|
69.90 0.3962 0.6081 0.1066 0.0694 15.482 108.422 50.510 11544.791 12.249 224.669 1.984 0.74 378548. 0.3998
|
|
76.89 0.4359 0.6444 0.1051 0.0711 15.851 111.004 49.815 11819.748 12.541 221.579 1.912 0.75 379734. 0.3825
|
|
83.88 0.4755 0.6771 0.1032 0.0725 16.159 113.162 48.916 12049.601 12.785 217.579 1.841 0.75 381015. 0.3650
|
|
90.87 0.5151 0.7067 0.1008 0.0735 16.385 114.749 47.783 12218.519 12.964 212.540 1.774 0.75 382391. 0.3476
|
|
97.86 0.5547 0.7333 0.0979 0.0740 16.509 115.614 46.391 12310.651 13.062 206.348 1.709 0.75 383862. 0.3300
|
|
104.85 0.5943 0.7574 0.0943 0.0740 16.508 115.605 44.716 12309.652 13.061 198.897 1.648 0.75 385427. 0.3123
|
|
111.84 0.6340 0.7791 0.0902 0.0734 16.357 114.552 42.732 12197.610 12.942 190.072 1.589 0.75 387085. 0.2944
|
|
118.83 0.6736 0.7988 0.0853 0.0719 16.035 112.293 40.420 11957.031 12.687 179.787 1.533 0.76 388835. 0.2763
|
|
125.83 0.7132 0.8165 0.0797 0.0696 15.528 108.747 37.791 11579.423 12.286 168.095 1.480 0.76 390674. 0.2580
|
|
132.82 0.7528 0.8325 0.0736 0.0666 14.843 103.945 34.889 11068.177 11.744 155.188 1.430 0.76 392600. 0.2394
|
|
139.81 0.7925 0.8464 0.0670 0.0627 13.990 97.973 31.764 10432.212 11.069 141.288 1.381 0.76 394612. 0.2206
|
|
146.80 0.8321 0.8581 0.0601 0.0582 12.984 90.926 28.462 9681.905 10.273 126.601 1.333 0.76 396706. 0.2016
|
|
153.79 0.8717 0.8668 0.0528 0.0531 11.839 82.907 25.024 8827.973 9.367 111.306 1.286 0.77 398880. 0.1823
|
|
160.78 0.9113 0.8715 0.0453 0.0474 10.569 74.014 21.484 7881.045 8.362 95.561 1.236 0.77 401134. 0.1625
|
|
167.77 0.9509 0.8703 0.0377 0.0412 9.189 64.352 17.876 6852.188 7.270 79.513 1.183 0.77 403465. 0.1418
|
|
174.76 0.9906 0.8595 0.0300 0.0346 7.716 54.036 14.232 5753.810 6.105 63.306 1.122 0.77 405872. 0.1200
|
|
181.75 1.0302 0.8316 0.0223 0.0277 6.169 43.205 10.586 4600.477 4.881 47.088 1.044 0.78 408354. 0.0963
|
|
188.74 1.0698 0.7675 0.0147 0.0205 4.572 32.022 6.973 3409.683 3.618 31.016 0.928 0.78 410910. 0.0694
|
|
195.73 1.1094 0.6064 0.0072 0.0132 2.953 20.681 3.431 2202.115 2.337 15.262 0.707 0.78 413539. 0.0371
|
|
202.72 1.1491 -0.0005 0.0000 0.0060 1.342 9.395 -0.001 1000.385 1.061 -0.006 -0.001 0.79 416226. 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 0.1108 0.0582 17.788 112.117 64.849 13264.764 12.667 288.448 2.217 0.82 412642. 0.5062
|
|
7.76 0.0396 0.0741 0.1107 0.0592 18.106 114.120 64.764 13501.737 12.893 288.069 2.176 0.82 413070. 0.4963
|
|
15.53 0.0792 0.1450 0.1106 0.0604 18.472 116.426 64.692 13774.594 13.154 287.750 2.130 0.82 413564. 0.4857
|
|
23.29 0.1188 0.2125 0.1105 0.0618 18.887 119.042 64.628 14084.091 13.449 287.466 2.081 0.82 414132. 0.4743
|
|
31.06 0.1584 0.2763 0.1103 0.0633 19.351 121.963 64.564 14429.712 13.779 287.179 2.029 0.82 414778. 0.4622
|
|
38.82 0.1980 0.3361 0.1102 0.0649 19.859 125.170 64.486 14809.070 14.142 286.832 1.975 0.82 415508. 0.4496
|
|
46.58 0.2376 0.3919 0.1100 0.0667 20.407 128.620 64.377 15217.276 14.531 286.351 1.919 0.82 416327. 0.4364
|
|
54.35 0.2772 0.4435 0.1097 0.0686 20.982 132.247 64.216 15646.370 14.941 285.631 1.862 0.82 417239. 0.4228
|
|
62.11 0.3169 0.4912 0.1093 0.0705 21.570 135.951 63.971 16084.603 15.360 284.543 1.804 0.83 418248. 0.4090
|
|
69.87 0.3565 0.5351 0.1087 0.0724 22.149 139.603 63.608 16516.721 15.772 282.930 1.747 0.83 419356. 0.3949
|
|
77.64 0.3961 0.5755 0.1078 0.0742 22.695 143.044 63.086 16923.818 16.161 280.609 1.691 0.83 420567. 0.3807
|
|
85.40 0.4357 0.6127 0.1066 0.0758 23.178 146.087 62.360 17283.855 16.505 277.379 1.636 0.83 421882. 0.3663
|
|
93.17 0.4753 0.6471 0.1049 0.0771 23.566 148.534 61.384 17573.381 16.781 273.036 1.584 0.83 423303. 0.3519
|
|
100.93 0.5149 0.6790 0.1027 0.0779 23.829 150.189 60.114 17769.135 16.968 267.389 1.534 0.83 424830. 0.3372
|
|
108.69 0.5545 0.7085 0.1000 0.0783 23.936 150.864 58.512 17849.010 17.045 260.263 1.487 0.83 426464. 0.3224
|
|
116.46 0.5941 0.7359 0.0966 0.0780 23.860 150.383 56.542 17792.129 16.990 251.499 1.441 0.84 428203. 0.3072
|
|
124.22 0.6337 0.7612 0.0926 0.0771 23.570 148.561 54.167 17576.502 16.784 240.934 1.398 0.84 430046. 0.2916
|
|
131.98 0.6733 0.7845 0.0878 0.0753 23.040 145.215 51.357 17180.625 16.406 228.436 1.356 0.84 431991. 0.2754
|
|
139.75 0.7129 0.8058 0.0822 0.0728 22.254 140.265 48.122 16594.990 15.847 214.048 1.315 0.84 434037. 0.2586
|
|
147.51 0.7525 0.8250 0.0761 0.0694 21.224 133.771 44.515 15826.646 15.113 198.002 1.276 0.84 436179. 0.2413
|
|
155.28 0.7921 0.8418 0.0694 0.0653 19.968 125.858 40.599 14890.436 14.219 180.583 1.237 0.85 438417. 0.2234
|
|
163.04 0.8317 0.8554 0.0623 0.0605 18.516 116.706 36.434 13807.724 13.185 162.056 1.197 0.85 440746. 0.2048
|
|
170.80 0.8713 0.8651 0.0548 0.0552 16.887 106.433 32.073 12592.271 12.025 142.660 1.155 0.85 443164. 0.1855
|
|
178.57 0.9110 0.8690 0.0471 0.0494 15.104 95.198 27.564 11263.044 10.755 122.604 1.110 0.85 445670. 0.1652
|
|
186.33 0.9506 0.8645 0.0392 0.0431 13.191 83.142 22.952 9836.688 9.393 102.089 1.058 0.86 448261. 0.1437
|
|
194.10 0.9902 0.8467 0.0312 0.0365 11.174 70.429 18.281 8332.574 7.957 81.312 0.995 0.86 450937. 0.1206
|
|
201.86 1.0298 0.8048 0.0232 0.0297 9.092 57.304 13.594 6779.730 6.474 60.466 0.909 0.86 453695. 0.0950
|
|
209.62 1.0694 0.7152 0.0153 0.0229 6.990 44.054 8.943 5212.148 4.977 39.777 0.778 0.87 456534. 0.0660
|
|
217.39 1.1090 0.5166 0.0075 0.0161 4.916 30.983 4.381 3665.616 3.500 19.485 0.542 0.87 459454. 0.0322
|
|
225.15 1.1486 -0.0071 -0.0001 0.0095 2.917 18.385 -0.034 2175.214 2.077 -0.153 -0.007 0.87 462446. 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 0.1098 0.0659 26.838 153.779 77.725 20013.240 17.374 345.721 1.762 0.90 453948. 0.4402
|
|
8.60 0.0399 0.0653 0.1096 0.0669 27.250 156.140 77.627 20320.465 17.641 345.285 1.733 0.90 454419. 0.4327
|
|
17.20 0.0798 0.1283 0.1095 0.0681 27.731 158.894 77.551 20678.916 17.952 344.948 1.701 0.90 454965. 0.4246
|
|
25.80 0.1197 0.1885 0.1095 0.0695 28.283 162.055 77.493 21090.377 18.309 344.688 1.667 0.90 455591. 0.4159
|
|
34.41 0.1596 0.2458 0.1094 0.0710 28.906 165.627 77.444 21555.209 18.712 344.472 1.630 0.90 456305. 0.4065
|
|
43.01 0.1995 0.2999 0.1093 0.0727 29.598 169.593 77.393 22071.369 19.161 344.246 1.590 0.91 457112. 0.3966
|
|
51.61 0.2393 0.3506 0.1092 0.0746 30.352 173.913 77.323 22633.564 19.649 343.934 1.550 0.91 458018. 0.3862
|
|
60.21 0.2792 0.3979 0.1091 0.0765 31.155 178.513 77.210 23232.199 20.168 343.432 1.507 0.91 459026. 0.3755
|
|
68.81 0.3191 0.4418 0.1088 0.0786 31.986 183.275 77.023 23852.010 20.706 342.599 1.465 0.91 460143. 0.3644
|
|
77.41 0.3590 0.4826 0.1084 0.0806 32.816 188.031 76.721 24470.967 21.244 341.256 1.422 0.91 461370. 0.3531
|
|
86.01 0.3989 0.5205 0.1077 0.0825 33.596 192.503 76.249 25052.891 21.749 339.156 1.380 0.91 462712. 0.3417
|
|
94.61 0.4388 0.5560 0.1067 0.0842 34.286 196.453 75.554 25566.988 22.195 336.066 1.340 0.91 464170. 0.3303
|
|
103.22 0.4787 0.5893 0.1053 0.0856 34.830 199.570 74.575 25972.615 22.547 331.709 1.302 0.91 465746. 0.3188
|
|
111.82 0.5186 0.6210 0.1035 0.0864 35.170 201.521 73.247 26226.580 22.768 325.803 1.267 0.92 467443. 0.3073
|
|
120.42 0.5585 0.6513 0.1010 0.0866 35.253 201.995 71.510 26288.170 22.821 318.076 1.234 0.92 469259. 0.2958
|
|
129.02 0.5984 0.6807 0.0979 0.0861 35.030 200.714 69.304 26121.543 22.677 308.266 1.203 0.92 471195. 0.2840
|
|
137.62 0.6382 0.7090 0.0940 0.0846 34.457 197.436 66.572 25694.902 22.306 296.114 1.175 0.92 473248. 0.2718
|
|
146.22 0.6781 0.7363 0.0894 0.0823 33.499 191.945 63.263 24980.348 21.686 281.396 1.149 0.92 475417. 0.2590
|
|
154.82 0.7180 0.7625 0.0839 0.0790 32.156 184.252 59.390 23979.096 20.817 264.166 1.123 0.93 477699. 0.2454
|
|
163.43 0.7579 0.7871 0.0777 0.0748 30.461 174.538 55.017 22714.871 19.719 244.716 1.099 0.93 480091. 0.2310
|
|
172.03 0.7978 0.8097 0.0709 0.0699 28.455 163.045 50.226 21219.180 18.421 223.404 1.074 0.93 482588. 0.2157
|
|
180.63 0.8377 0.8288 0.0637 0.0644 26.205 150.152 45.090 19541.166 16.964 200.561 1.047 0.93 485187. 0.1992
|
|
189.23 0.8776 0.8420 0.0560 0.0584 23.776 136.234 39.676 17729.949 15.392 176.480 1.015 0.94 487886. 0.1812
|
|
197.83 0.9175 0.8469 0.0481 0.0521 21.211 121.537 34.055 15817.170 13.731 151.475 0.977 0.94 490682. 0.1615
|
|
206.43 0.9574 0.8318 0.0399 0.0459 18.704 107.169 28.263 13947.229 12.108 125.715 0.919 0.94 493573. 0.1385
|
|
215.03 0.9973 0.7927 0.0316 0.0398 16.198 92.813 22.393 12078.923 10.486 99.603 0.841 0.95 496556. 0.1128
|
|
223.63 1.0371 0.7195 0.0234 0.0337 13.706 78.533 16.536 10220.577 8.873 73.554 0.734 0.95 499630. 0.0846
|
|
232.24 1.0770 0.5916 0.0152 0.0277 11.291 64.698 10.787 8419.970 7.310 47.980 0.581 0.95 502794. 0.0541
|
|
240.84 1.1169 0.3738 0.0074 0.0222 9.017 51.665 5.249 6723.844 5.837 23.345 0.354 0.96 506048. 0.0230
|
|
249.44 1.1568 -0.0005 0.0000 0.0170 6.924 39.675 -0.005 5163.435 4.482 -0.023 0.000 0.96 509401. 0.0000
|
|
|
|
|
|
|