353 lines
63 KiB
Plaintext
353 lines
63 KiB
Plaintext
20x18(F1-GT) (20x18(F1-GT).dat)
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v2022-0915
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Simulation Date: 10/10/2023
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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 0.1075 0.0483 0.012 0.784 0.548 9.276 0.089 2.439 26.811 0.08 38467. 0.5825
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0.64 0.0337 0.0728 0.1069 0.0495 0.013 0.803 0.545 9.501 0.091 2.425 26.025 0.08 38502. 0.5637
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1.28 0.0674 0.1412 0.1062 0.0507 0.013 0.823 0.541 9.734 0.093 2.408 25.230 0.08 38541. 0.5447
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1.92 0.1011 0.2051 0.1053 0.0519 0.013 0.843 0.537 9.971 0.095 2.389 24.434 0.08 38585. 0.5254
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2.55 0.1348 0.2647 0.1043 0.0532 0.014 0.863 0.532 10.206 0.097 2.366 23.643 0.08 38634. 0.5059
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3.19 0.1685 0.3199 0.1031 0.0543 0.014 0.882 0.526 10.433 0.100 2.339 22.863 0.08 38689. 0.4864
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3.83 0.2022 0.3711 0.1017 0.0554 0.014 0.900 0.519 10.644 0.102 2.307 22.100 0.08 38750. 0.4669
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4.47 0.2359 0.4184 0.1000 0.0564 0.015 0.915 0.510 10.829 0.103 2.268 21.358 0.08 38817. 0.4475
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5.11 0.2697 0.4621 0.0980 0.0572 0.015 0.928 0.500 10.978 0.105 2.222 20.641 0.08 38890. 0.4280
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5.75 0.3034 0.5025 0.0956 0.0577 0.015 0.937 0.487 11.081 0.106 2.168 19.951 0.08 38969. 0.4086
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6.38 0.3371 0.5398 0.0928 0.0580 0.015 0.941 0.473 11.128 0.106 2.105 19.288 0.08 39055. 0.3893
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7.02 0.3708 0.5742 0.0896 0.0579 0.015 0.939 0.457 11.115 0.106 2.033 18.652 0.08 39147. 0.3700
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7.66 0.4045 0.6059 0.0861 0.0575 0.015 0.933 0.439 11.038 0.105 1.953 18.041 0.08 39246. 0.3507
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8.30 0.4382 0.6349 0.0822 0.0567 0.015 0.921 0.419 10.897 0.104 1.865 17.452 0.08 39352. 0.3315
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8.94 0.4719 0.6614 0.0781 0.0557 0.014 0.904 0.398 10.694 0.102 1.770 16.881 0.08 39463. 0.3124
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9.58 0.5056 0.6853 0.0736 0.0543 0.014 0.882 0.375 10.430 0.100 1.670 16.324 0.08 39582. 0.2934
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10.21 0.5393 0.7065 0.0690 0.0526 0.014 0.854 0.352 10.107 0.097 1.564 15.778 0.08 39706. 0.2745
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10.85 0.5730 0.7250 0.0641 0.0506 0.013 0.822 0.327 9.725 0.093 1.453 15.238 0.08 39837. 0.2555
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11.49 0.6067 0.7404 0.0590 0.0484 0.012 0.785 0.301 9.288 0.089 1.339 14.698 0.08 39974. 0.2366
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12.13 0.6404 0.7526 0.0538 0.0458 0.012 0.743 0.274 8.795 0.084 1.221 14.153 0.08 40118. 0.2175
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12.77 0.6741 0.7608 0.0485 0.0429 0.011 0.697 0.247 8.247 0.079 1.099 13.593 0.08 40267. 0.1983
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13.41 0.7078 0.7645 0.0430 0.0398 0.010 0.646 0.219 7.647 0.073 0.975 13.008 0.08 40423. 0.1787
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14.04 0.7415 0.7623 0.0374 0.0364 0.009 0.591 0.191 6.994 0.067 0.849 12.381 0.08 40585. 0.1587
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14.68 0.7752 0.7523 0.0318 0.0328 0.008 0.532 0.162 6.289 0.060 0.721 11.688 0.08 40753. 0.1380
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15.32 0.8090 0.7313 0.0261 0.0288 0.007 0.468 0.133 5.535 0.053 0.591 10.888 0.08 40927. 0.1164
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15.96 0.8427 0.6934 0.0203 0.0246 0.006 0.400 0.103 4.731 0.045 0.460 9.911 0.08 41107. 0.0935
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16.60 0.8764 0.6270 0.0145 0.0202 0.005 0.328 0.074 3.881 0.037 0.328 8.616 0.08 41292. 0.0686
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17.24 0.9101 0.5049 0.0086 0.0155 0.004 0.252 0.044 2.986 0.029 0.196 6.681 0.08 41482. 0.0411
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17.87 0.9438 0.2446 0.0028 0.0106 0.003 0.173 0.014 2.041 0.019 0.062 3.121 0.08 41669. 0.0109
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18.51 0.9775
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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 0.1078 0.0455 0.094 2.952 2.200 69.859 0.334 9.784 14.282 0.16 76933. 0.6214
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1.26 0.0334 0.0767 0.1073 0.0467 0.096 3.031 2.188 71.711 0.342 9.730 13.836 0.16 77001. 0.6004
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2.53 0.0667 0.1484 0.1066 0.0479 0.099 3.112 2.173 73.636 0.352 9.667 13.387 0.16 77078. 0.5790
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3.79 0.1001 0.2151 0.1057 0.0492 0.101 3.195 2.157 75.602 0.361 9.593 12.939 0.16 77165. 0.5575
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5.06 0.1335 0.2770 0.1048 0.0505 0.104 3.278 2.137 77.571 0.370 9.506 12.496 0.16 77263. 0.5359
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6.32 0.1668 0.3341 0.1036 0.0517 0.107 3.359 2.114 79.493 0.380 9.401 12.060 0.16 77371. 0.5144
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7.58 0.2002 0.3868 0.1023 0.0529 0.109 3.436 2.086 81.306 0.388 9.276 11.634 0.16 77491. 0.4929
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8.85 0.2336 0.4352 0.1006 0.0540 0.111 3.505 2.052 82.936 0.396 9.127 11.222 0.16 77622. 0.4716
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10.11 0.2669 0.4798 0.0986 0.0549 0.113 3.563 2.012 84.303 0.403 8.949 10.824 0.16 77766. 0.4504
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11.38 0.3003 0.5208 0.0963 0.0555 0.114 3.606 1.964 85.323 0.407 8.738 10.443 0.16 77922. 0.4294
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12.64 0.3337 0.5584 0.0936 0.0559 0.115 3.631 1.909 85.925 0.410 8.492 10.078 0.16 78091. 0.4086
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13.90 0.3670 0.5931 0.0905 0.0560 0.115 3.637 1.846 86.056 0.411 8.212 9.730 0.16 78273. 0.3879
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15.17 0.4004 0.6249 0.0871 0.0558 0.115 3.621 1.776 85.692 0.409 7.898 9.398 0.16 78467. 0.3674
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16.43 0.4338 0.6540 0.0833 0.0552 0.114 3.585 1.698 84.823 0.405 7.553 9.080 0.16 78674. 0.3471
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17.69 0.4671 0.6807 0.0792 0.0543 0.112 3.527 1.614 83.454 0.398 7.181 8.775 0.16 78894. 0.3271
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18.96 0.5005 0.7048 0.0748 0.0531 0.109 3.448 1.525 81.591 0.390 6.785 8.480 0.16 79126. 0.3073
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20.22 0.5339 0.7264 0.0702 0.0516 0.106 3.349 1.432 79.244 0.378 6.368 8.194 0.16 79371. 0.2876
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21.49 0.5672 0.7455 0.0654 0.0497 0.102 3.230 1.334 76.424 0.365 5.932 7.914 0.16 79628. 0.2681
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22.75 0.6006 0.7619 0.0604 0.0476 0.098 3.091 1.232 73.139 0.349 5.479 7.639 0.16 79897. 0.2488
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24.01 0.6340 0.7754 0.0553 0.0452 0.093 2.933 1.127 69.398 0.331 5.013 7.366 0.16 80179. 0.2294
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25.28 0.6673 0.7857 0.0500 0.0424 0.087 2.756 1.019 65.208 0.311 4.534 7.090 0.16 80473. 0.2100
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26.54 0.7007 0.7922 0.0446 0.0394 0.081 2.560 0.909 60.575 0.289 4.044 6.808 0.16 80779. 0.1905
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27.81 0.7341 0.7940 0.0391 0.0361 0.074 2.346 0.797 55.505 0.265 3.545 6.513 0.16 81097. 0.1706
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29.07 0.7674 0.7896 0.0335 0.0326 0.067 2.113 0.683 50.006 0.239 3.039 6.196 0.16 81428. 0.1502
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30.33 0.8008 0.7767 0.0278 0.0287 0.059 1.863 0.568 44.087 0.211 2.525 5.841 0.16 81769. 0.1291
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31.60 0.8342 0.7508 0.0221 0.0246 0.051 1.596 0.451 37.760 0.180 2.007 5.420 0.16 82123. 0.1068
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32.86 0.8675 0.7032 0.0164 0.0202 0.042 1.312 0.334 31.038 0.148 1.486 4.881 0.16 82487. 0.0828
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34.13 0.9009 0.6136 0.0106 0.0156 0.032 1.012 0.216 23.937 0.114 0.963 4.102 0.17 82860. 0.0560
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35.39 0.9343 0.4216 0.0048 0.0107 0.022 0.695 0.099 16.452 0.079 0.438 2.717 0.17 83235. 0.0250
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36.65 0.9676
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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 0.1081 0.0443 0.308 6.471 4.963 229.678 0.731 22.074 9.800 0.24 115397. 0.6405
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1.89 0.0333 0.0788 0.1076 0.0455 0.317 6.651 4.936 236.061 0.751 21.957 9.485 0.24 115499. 0.6183
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3.79 0.0667 0.1523 0.1069 0.0468 0.325 6.838 4.906 242.715 0.773 21.821 9.168 0.24 115614. 0.5957
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5.68 0.1000 0.2206 0.1061 0.0481 0.335 7.030 4.870 249.536 0.794 21.660 8.851 0.24 115745. 0.5730
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7.58 0.1334 0.2837 0.1052 0.0495 0.344 7.224 4.827 256.393 0.816 21.469 8.539 0.24 115891. 0.5503
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9.47 0.1667 0.3419 0.1041 0.0507 0.353 7.413 4.775 263.119 0.838 21.240 8.232 0.24 116053. 0.5277
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11.37 0.2001 0.3954 0.1027 0.0520 0.361 7.593 4.713 269.505 0.858 20.965 7.932 0.24 116232. 0.5052
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13.26 0.2334 0.4444 0.1011 0.0531 0.369 7.756 4.639 275.303 0.876 20.634 7.643 0.24 116429. 0.4830
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15.16 0.2668 0.4894 0.0992 0.0541 0.376 7.895 4.550 280.235 0.892 20.239 7.364 0.24 116645. 0.4609
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17.05 0.3001 0.5307 0.0969 0.0548 0.381 8.002 4.445 284.016 0.904 19.769 7.098 0.24 116879. 0.4390
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18.95 0.3335 0.5685 0.0942 0.0552 0.384 8.069 4.321 286.391 0.912 19.221 6.844 0.24 117132. 0.4174
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20.84 0.3668 0.6032 0.0911 0.0554 0.385 8.091 4.180 287.179 0.914 18.592 6.602 0.24 117405. 0.3960
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22.74 0.4002 0.6351 0.0876 0.0552 0.384 8.066 4.021 286.279 0.911 17.887 6.371 0.24 117696. 0.3748
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24.63 0.4335 0.6643 0.0838 0.0547 0.380 7.992 3.847 283.658 0.903 17.112 6.151 0.24 118006. 0.3540
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26.53 0.4669 0.6910 0.0797 0.0539 0.375 7.870 3.659 279.319 0.889 16.274 5.941 0.24 118336. 0.3334
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28.42 0.5002 0.7152 0.0754 0.0527 0.366 7.699 3.458 273.282 0.870 15.381 5.739 0.24 118684. 0.3131
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30.32 0.5336 0.7369 0.0707 0.0512 0.356 7.482 3.246 265.578 0.845 14.440 5.544 0.24 119051. 0.2931
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32.21 0.5669 0.7562 0.0659 0.0494 0.344 7.219 3.025 256.237 0.816 13.456 5.355 0.24 119436. 0.2733
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34.11 0.6003 0.7730 0.0609 0.0473 0.329 6.911 2.796 245.288 0.781 12.436 5.170 0.24 119840. 0.2536
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36.00 0.6336 0.7871 0.0558 0.0449 0.312 6.558 2.559 232.757 0.741 11.383 4.987 0.24 120263. 0.2340
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37.90 0.6670 0.7981 0.0505 0.0422 0.293 6.161 2.316 218.666 0.696 10.301 4.804 0.24 120704. 0.2145
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39.79 0.7003 0.8057 0.0451 0.0392 0.272 5.720 2.067 203.036 0.646 9.196 4.618 0.24 121163. 0.1948
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41.69 0.7337 0.8089 0.0395 0.0359 0.249 5.237 1.814 185.890 0.592 8.069 4.426 0.24 121640. 0.1749
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43.58 0.7670 0.8066 0.0339 0.0323 0.224 4.712 1.557 167.250 0.532 6.924 4.222 0.24 122135. 0.1545
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45.48 0.8004 0.7965 0.0282 0.0284 0.197 4.146 1.296 147.148 0.468 5.765 3.995 0.25 122647. 0.1334
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47.37 0.8337 0.7747 0.0225 0.0242 0.168 3.539 1.033 125.622 0.400 4.596 3.730 0.25 123176. 0.1112
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49.27 0.8671 0.7329 0.0167 0.0198 0.138 2.894 0.769 102.723 0.327 3.419 3.394 0.25 123722. 0.0873
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51.16 0.9004 0.6520 0.0110 0.0151 0.105 2.212 0.503 78.504 0.250 2.238 2.907 0.25 124282. 0.0605
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53.06 0.9338 0.4724 0.0052 0.0102 0.071 1.492 0.237 52.949 0.169 1.055 2.031 0.25 124845. 0.0290
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54.95 0.9671
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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 0.1085 0.0437 0.721 11.358 8.850 537.531 1.283 39.366 7.468 0.32 153857. 0.6518
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2.52 0.0333 0.0799 0.1079 0.0450 0.741 11.683 8.806 552.917 1.320 39.169 7.224 0.32 153993. 0.6289
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5.05 0.0666 0.1544 0.1073 0.0463 0.763 12.023 8.754 568.999 1.358 38.938 6.978 0.32 154147. 0.6057
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7.57 0.1000 0.2235 0.1066 0.0476 0.785 12.373 8.693 585.534 1.398 38.665 6.734 0.32 154320. 0.5825
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10.10 0.1333 0.2874 0.1057 0.0490 0.808 12.725 8.619 602.215 1.438 38.339 6.492 0.32 154514. 0.5592
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12.62 0.1666 0.3461 0.1046 0.0503 0.830 13.072 8.531 618.646 1.477 37.946 6.255 0.32 154730. 0.5360
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15.15 0.1999 0.3999 0.1033 0.0516 0.851 13.404 8.424 634.332 1.514 37.472 6.024 0.32 154968. 0.5129
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17.67 0.2332 0.4493 0.1017 0.0528 0.870 13.707 8.296 648.677 1.549 36.899 5.800 0.32 155231. 0.4901
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20.19 0.2666 0.4945 0.0998 0.0538 0.886 13.968 8.141 661.011 1.578 36.209 5.586 0.32 155518. 0.4676
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22.72 0.2999 0.5359 0.0975 0.0546 0.899 14.171 7.956 670.638 1.601 35.388 5.381 0.32 155830. 0.4453
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25.24 0.3332 0.5738 0.0949 0.0551 0.908 14.304 7.739 676.934 1.616 34.423 5.185 0.32 156167. 0.4232
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27.77 0.3665 0.6086 0.0918 0.0553 0.911 14.357 7.489 679.440 1.622 33.313 5.000 0.32 156530. 0.4014
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30.29 0.3998 0.6405 0.0884 0.0552 0.909 14.324 7.209 677.901 1.618 32.065 4.823 0.32 156918. 0.3799
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32.81 0.4331 0.6697 0.0846 0.0547 0.901 14.204 6.900 672.218 1.605 30.690 4.655 0.32 157332. 0.3588
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35.34 0.4665 0.6964 0.0805 0.0539 0.888 13.997 6.565 662.391 1.581 29.201 4.495 0.32 157771. 0.3379
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37.86 0.4998 0.7207 0.0761 0.0528 0.870 13.702 6.208 648.463 1.548 27.612 4.342 0.32 158235. 0.3174
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40.39 0.5331 0.7426 0.0715 0.0513 0.846 13.323 5.830 630.501 1.505 25.934 4.194 0.32 158723. 0.2971
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42.91 0.5664 0.7622 0.0666 0.0495 0.816 12.860 5.436 608.576 1.453 24.179 4.051 0.32 159237. 0.2771
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45.44 0.5997 0.7792 0.0616 0.0474 0.781 12.314 5.026 582.756 1.391 22.357 3.912 0.32 159775. 0.2573
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47.96 0.6331 0.7937 0.0564 0.0450 0.742 11.687 4.604 553.102 1.320 20.477 3.775 0.32 160338. 0.2376
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50.48 0.6664 0.8054 0.0511 0.0423 0.697 10.981 4.169 519.668 1.241 18.545 3.639 0.32 160925. 0.2180
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53.01 0.6997 0.8137 0.0457 0.0393 0.647 10.196 3.725 482.504 1.152 16.569 3.502 0.33 161537. 0.1983
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55.53 0.7330 0.8181 0.0401 0.0359 0.592 9.333 3.272 441.660 1.054 14.555 3.361 0.33 162172. 0.1783
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58.06 0.7663 0.8173 0.0345 0.0323 0.533 8.393 2.812 397.195 0.948 12.509 3.211 0.33 162831. 0.1580
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60.58 0.7997 0.8094 0.0288 0.0284 0.468 7.378 2.346 349.180 0.834 10.436 3.048 0.33 163513. 0.1370
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63.10 0.8330 0.7906 0.0230 0.0242 0.399 6.291 1.876 297.710 0.711 8.344 2.858 0.33 164218. 0.1148
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65.63 0.8663 0.7535 0.0172 0.0198 0.326 5.133 1.403 242.905 0.580 6.239 2.619 0.33 164945. 0.0910
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68.15 0.8996 0.6800 0.0114 0.0150 0.248 3.907 0.928 184.893 0.441 4.127 2.276 0.33 165690. 0.0643
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70.68 0.9329 0.5135 0.0055 0.0101 0.166 2.613 0.452 123.659 0.295 2.010 1.657 0.33 166441. 0.0327
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73.20 0.9663
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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 0.1089 0.0435 1.401 17.660 13.879 1044.677 1.995 61.736 6.026 0.40 192312. 0.6586
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3.18 0.0336 0.0813 0.1084 0.0448 1.442 18.181 13.814 1075.503 2.054 61.446 5.826 0.40 192483. 0.6353
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6.36 0.0672 0.1569 0.1078 0.0462 1.486 18.727 13.738 1107.825 2.116 61.105 5.624 0.40 192677. 0.6116
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9.55 0.1008 0.2270 0.1071 0.0475 1.530 19.291 13.646 1141.166 2.179 60.698 5.424 0.40 192896. 0.5878
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12.73 0.1344 0.2916 0.1062 0.0489 1.576 19.861 13.536 1174.914 2.244 60.207 5.225 0.40 193141. 0.5640
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15.91 0.1680 0.3509 0.1051 0.0503 1.620 20.425 13.402 1208.261 2.308 59.612 5.031 0.40 193414. 0.5403
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19.09 0.2016 0.4052 0.1039 0.0517 1.663 20.965 13.239 1240.197 2.369 58.887 4.842 0.40 193716. 0.5169
|
|
22.27 0.2352 0.4549 0.1023 0.0529 1.702 21.460 13.040 1269.498 2.425 58.004 4.659 0.40 194049. 0.4936
|
|
25.46 0.2688 0.5004 0.1004 0.0539 1.736 21.887 12.799 1294.771 2.473 56.932 4.484 0.40 194413. 0.4706
|
|
28.64 0.3024 0.5419 0.0981 0.0548 1.763 22.222 12.510 1314.578 2.511 55.645 4.316 0.40 194809. 0.4479
|
|
31.82 0.3360 0.5799 0.0955 0.0553 1.780 22.443 12.168 1327.625 2.536 54.125 4.157 0.40 195237. 0.4254
|
|
35.00 0.3696 0.6147 0.0924 0.0555 1.788 22.533 11.774 1332.968 2.546 52.369 4.006 0.40 195697. 0.4033
|
|
38.18 0.4032 0.6467 0.0889 0.0554 1.784 22.484 11.328 1330.088 2.540 50.389 3.863 0.40 196190. 0.3815
|
|
41.36 0.4368 0.6759 0.0850 0.0549 1.769 22.293 10.837 1318.787 2.519 48.203 3.727 0.40 196716. 0.3600
|
|
44.55 0.4704 0.7026 0.0808 0.0541 1.742 21.960 10.304 1299.063 2.481 45.834 3.598 0.40 197273. 0.3388
|
|
47.73 0.5040 0.7269 0.0764 0.0530 1.704 21.486 9.735 1271.012 2.427 43.302 3.474 0.40 197862. 0.3180
|
|
50.91 0.5376 0.7488 0.0717 0.0514 1.656 20.873 9.134 1234.769 2.358 40.628 3.355 0.40 198483. 0.2975
|
|
54.09 0.5712 0.7684 0.0667 0.0496 1.596 20.124 8.505 1190.479 2.274 37.830 3.240 0.40 199136. 0.2772
|
|
57.27 0.6048 0.7856 0.0616 0.0474 1.526 19.242 7.852 1138.280 2.174 34.924 3.129 0.40 199820. 0.2572
|
|
60.46 0.6384 0.8001 0.0563 0.0449 1.446 18.228 7.177 1078.298 2.059 31.924 3.019 0.40 200534. 0.2373
|
|
63.64 0.6720 0.8119 0.0509 0.0421 1.355 17.084 6.484 1010.645 1.930 28.842 2.910 0.41 201280. 0.2174
|
|
66.82 0.7056 0.8204 0.0453 0.0390 1.254 15.813 5.776 935.424 1.787 25.690 2.801 0.41 202057. 0.1975
|
|
70.00 0.7392 0.8249 0.0396 0.0355 1.144 14.415 5.053 852.741 1.629 22.477 2.688 0.41 202863. 0.1773
|
|
73.18 0.7728 0.8241 0.0339 0.0318 1.023 12.893 4.320 762.719 1.457 19.213 2.569 0.41 203700. 0.1566
|
|
76.37 0.8064 0.8160 0.0281 0.0277 0.892 11.250 3.576 665.512 1.271 15.908 2.438 0.41 204566. 0.1352
|
|
79.55 0.8400 0.7965 0.0222 0.0234 0.753 9.489 2.827 561.324 1.072 12.573 2.284 0.41 205461. 0.1127
|
|
82.73 0.8736 0.7569 0.0163 0.0188 0.604 7.614 2.072 450.409 0.860 9.218 2.087 0.41 206382. 0.0881
|
|
85.91 0.9072 0.6751 0.0103 0.0139 0.447 5.630 1.316 333.018 0.636 5.854 1.792 0.41 207326. 0.0603
|
|
89.09 0.9408 0.4721 0.0044 0.0087 0.280 3.531 0.557 208.869 0.399 2.476 1.209 0.41 208266. 0.0265
|
|
92.28 0.9744
|
|
|
|
|
|
|
|
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 0.1093 0.0435 2.422 25.445 20.071 1806.261 2.875 89.276 5.040 0.48 230762. 0.6625
|
|
3.82 0.0336 0.0815 0.1089 0.0449 2.495 26.208 19.985 1860.413 2.961 88.895 4.872 0.48 230966. 0.6391
|
|
7.63 0.0672 0.1574 0.1083 0.0462 2.571 27.010 19.884 1917.390 3.052 88.445 4.704 0.48 231199. 0.6154
|
|
11.45 0.1008 0.2277 0.1077 0.0477 2.650 27.842 19.763 1976.400 3.146 87.904 4.535 0.48 231461. 0.5915
|
|
15.27 0.1344 0.2924 0.1069 0.0491 2.731 28.687 19.615 2036.390 3.241 87.248 4.369 0.48 231754. 0.5677
|
|
19.08 0.1679 0.3519 0.1059 0.0505 2.811 29.526 19.435 2095.966 3.336 86.445 4.206 0.48 232081. 0.5439
|
|
22.90 0.2015 0.4063 0.1047 0.0519 2.888 30.334 19.212 2153.353 3.427 85.456 4.047 0.48 232443. 0.5204
|
|
26.72 0.2351 0.4560 0.1032 0.0532 2.959 31.081 18.939 2206.376 3.512 84.240 3.893 0.48 232842. 0.4971
|
|
30.54 0.2687 0.5015 0.1013 0.0543 3.021 31.732 18.604 2252.549 3.585 82.750 3.746 0.48 233279. 0.4740
|
|
34.35 0.3023 0.5430 0.0991 0.0552 3.070 32.249 18.198 2289.266 3.643 80.944 3.606 0.48 233754. 0.4512
|
|
38.17 0.3359 0.5810 0.0965 0.0558 3.103 32.600 17.715 2314.159 3.683 78.795 3.472 0.48 234268. 0.4287
|
|
41.99 0.3695 0.6158 0.0934 0.0561 3.119 32.759 17.153 2325.475 3.701 76.297 3.346 0.48 234820. 0.4065
|
|
45.80 0.4031 0.6478 0.0900 0.0560 3.114 32.713 16.516 2322.226 3.696 73.463 3.226 0.48 235413. 0.3846
|
|
49.62 0.4367 0.6770 0.0861 0.0555 3.090 32.457 15.810 2304.022 3.667 70.323 3.112 0.48 236043. 0.3631
|
|
53.44 0.4702 0.7038 0.0819 0.0547 3.045 31.990 15.042 2270.843 3.614 66.907 3.004 0.48 236713. 0.3419
|
|
57.25 0.5038 0.7283 0.0775 0.0536 2.981 31.314 14.219 2222.860 3.538 63.248 2.901 0.48 237420. 0.3210
|
|
61.07 0.5374 0.7504 0.0727 0.0521 2.897 30.433 13.349 2160.326 3.438 59.376 2.803 0.48 238166. 0.3004
|
|
64.89 0.5710 0.7702 0.0678 0.0502 2.794 29.350 12.437 2083.500 3.316 55.319 2.707 0.48 238950. 0.2801
|
|
68.71 0.6046 0.7876 0.0626 0.0480 2.672 28.070 11.488 1992.639 3.171 51.100 2.615 0.48 239771. 0.2600
|
|
72.52 0.6382 0.8026 0.0572 0.0455 2.532 26.596 10.508 1887.973 3.005 46.740 2.524 0.49 240629. 0.2401
|
|
76.34 0.6718 0.8149 0.0518 0.0427 2.373 24.930 9.500 1769.714 2.817 42.258 2.435 0.49 241524. 0.2202
|
|
80.16 0.7054 0.8240 0.0461 0.0395 2.197 23.075 8.469 1638.051 2.607 37.670 2.345 0.49 242456. 0.2002
|
|
83.97 0.7390 0.8294 0.0404 0.0360 2.002 21.035 7.417 1493.178 2.376 32.990 2.253 0.49 243424. 0.1800
|
|
87.79 0.7726 0.8298 0.0346 0.0322 1.791 18.811 6.348 1335.314 2.125 28.234 2.156 0.49 244428. 0.1594
|
|
91.61 0.8061 0.8233 0.0287 0.0281 1.562 16.408 5.264 1164.734 1.854 23.416 2.050 0.49 245468. 0.1380
|
|
95.42 0.8397 0.8060 0.0227 0.0237 1.317 13.831 4.171 981.794 1.563 18.551 1.927 0.49 246541. 0.1154
|
|
99.24 0.8733 0.7699 0.0167 0.0190 1.055 11.086 3.070 786.941 1.252 13.656 1.770 0.49 247647. 0.0910
|
|
103.06 0.9069 0.6940 0.0107 0.0140 0.779 8.179 1.966 580.629 0.924 8.746 1.536 0.50 248779. 0.0632
|
|
106.87 0.9405 0.5030 0.0047 0.0087 0.486 5.106 0.858 362.447 0.577 3.816 1.074 0.50 249909. 0.0292
|
|
110.69 0.9741
|
|
|
|
|
|
|
|
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 0.1099 0.0438 3.866 34.811 27.448 2883.003 3.933 122.090 4.318 0.56 269204. 0.6638
|
|
4.43 0.0334 0.0811 0.1094 0.0451 3.983 35.862 27.346 2969.998 4.052 121.633 4.176 0.56 269441. 0.6407
|
|
8.86 0.0668 0.1566 0.1090 0.0465 4.106 36.971 27.224 3061.903 4.177 121.091 4.033 0.56 269710. 0.6173
|
|
13.29 0.1002 0.2266 0.1084 0.0479 4.234 38.126 27.077 3157.542 4.307 120.437 3.889 0.56 270012. 0.5938
|
|
17.72 0.1337 0.2911 0.1077 0.0494 4.365 39.307 26.897 3255.321 4.441 119.636 3.748 0.56 270351. 0.5702
|
|
22.15 0.1671 0.3504 0.1068 0.0509 4.497 40.487 26.674 3353.065 4.574 118.645 3.608 0.56 270729. 0.5467
|
|
26.58 0.2005 0.4046 0.1056 0.0523 4.624 41.633 26.396 3447.963 4.704 117.410 3.472 0.56 271148. 0.5234
|
|
31.01 0.2339 0.4542 0.1043 0.0537 4.743 42.702 26.050 3536.519 4.824 115.872 3.341 0.56 271609. 0.5003
|
|
35.44 0.2673 0.4995 0.1025 0.0549 4.847 43.646 25.621 3614.673 4.931 113.964 3.215 0.56 272114. 0.4774
|
|
39.87 0.3007 0.5409 0.1004 0.0558 4.932 44.412 25.096 3678.107 5.018 111.625 3.095 0.56 272663. 0.4548
|
|
44.30 0.3342 0.5788 0.0979 0.0565 4.992 44.952 24.463 3722.813 5.079 108.811 2.980 0.56 273258. 0.4325
|
|
48.73 0.3676 0.6136 0.0949 0.0569 5.023 45.228 23.720 3745.733 5.110 105.508 2.872 0.56 273898. 0.4104
|
|
53.16 0.4010 0.6456 0.0915 0.0569 5.022 45.220 22.871 3745.073 5.109 101.732 2.770 0.56 274584. 0.3886
|
|
57.59 0.4344 0.6749 0.0878 0.0565 4.989 44.919 21.924 3720.083 5.075 97.520 2.673 0.56 275314. 0.3672
|
|
62.02 0.4678 0.7018 0.0836 0.0557 4.922 44.322 20.889 3670.683 5.007 92.915 2.581 0.56 276089. 0.3461
|
|
66.45 0.5012 0.7264 0.0792 0.0546 4.824 43.434 19.776 3597.145 4.907 87.963 2.494 0.56 276909. 0.3253
|
|
70.88 0.5346 0.7488 0.0744 0.0531 4.693 42.260 18.594 3499.902 4.775 82.706 2.410 0.56 277772. 0.3048
|
|
75.31 0.5681 0.7689 0.0695 0.0513 4.532 40.805 17.352 3379.413 4.610 77.184 2.329 0.56 278679. 0.2846
|
|
79.74 0.6015 0.7868 0.0643 0.0491 4.340 39.075 16.059 3236.110 4.415 71.430 2.251 0.57 279630. 0.2646
|
|
84.17 0.6349 0.8024 0.0589 0.0466 4.117 37.074 14.720 3070.398 4.189 65.473 2.174 0.57 280623. 0.2448
|
|
88.60 0.6683 0.8154 0.0534 0.0438 3.866 34.807 13.341 2882.643 3.932 59.342 2.099 0.57 281659. 0.2249
|
|
93.03 0.7017 0.8255 0.0477 0.0406 3.585 32.278 11.928 2673.180 3.647 53.057 2.024 0.57 282738. 0.2051
|
|
97.46 0.7351 0.8320 0.0420 0.0371 3.275 29.490 10.486 2442.332 3.332 46.641 1.947 0.57 283858. 0.1850
|
|
101.89 0.7686 0.8341 0.0361 0.0333 2.937 26.449 9.018 2190.454 2.988 40.113 1.867 0.57 285019. 0.1645
|
|
106.32 0.8020 0.8300 0.0301 0.0291 2.572 23.159 7.530 1917.977 2.616 33.494 1.781 0.57 286222. 0.1434
|
|
110.75 0.8354 0.8164 0.0241 0.0247 2.180 19.627 6.026 1625.454 2.217 26.804 1.682 0.57 287463. 0.1211
|
|
115.18 0.8688 0.7866 0.0181 0.0199 1.762 15.861 4.511 1313.590 1.792 20.066 1.558 0.58 288743. 0.0971
|
|
119.61 0.9022 0.7234 0.0120 0.0149 1.318 11.871 2.990 983.146 1.341 13.301 1.380 0.58 290054. 0.0700
|
|
124.04 0.9356 0.5697 0.0059 0.0096 0.850 7.656 1.465 634.020 0.865 6.514 1.048 0.58 291374. 0.0372
|
|
128.47 0.9691
|
|
|
|
|
|
|
|
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 0.1104 0.0444 5.858 46.152 36.031 4368.221 5.214 160.267 3.741 0.63 307639. 0.6589
|
|
5.06 0.0334 0.0804 0.1101 0.0457 6.031 47.518 35.917 4497.550 5.369 159.760 3.622 0.63 307908. 0.6369
|
|
10.13 0.0668 0.1554 0.1096 0.0471 6.216 48.969 35.782 4634.930 5.533 159.156 3.502 0.63 308214. 0.6145
|
|
15.19 0.1002 0.2251 0.1091 0.0486 6.408 50.489 35.617 4778.794 5.704 158.423 3.380 0.63 308558. 0.5919
|
|
20.25 0.1337 0.2894 0.1085 0.0501 6.607 52.055 35.412 4926.945 5.881 157.513 3.260 0.64 308945. 0.5692
|
|
25.32 0.1671 0.3486 0.1077 0.0516 6.807 53.633 35.155 5076.299 6.059 156.370 3.141 0.64 309375. 0.5464
|
|
30.38 0.2005 0.4028 0.1067 0.0531 7.004 55.179 34.829 5222.698 6.234 154.921 3.025 0.64 309853. 0.5237
|
|
35.44 0.2339 0.4524 0.1055 0.0545 7.189 56.639 34.416 5360.834 6.399 153.081 2.912 0.64 310379. 0.5012
|
|
40.50 0.2673 0.4977 0.1039 0.0558 7.355 57.944 33.893 5484.383 6.546 150.756 2.803 0.64 310955. 0.4788
|
|
45.57 0.3007 0.5391 0.1019 0.0568 7.492 59.023 33.241 5586.464 6.668 147.857 2.699 0.64 311583. 0.4565
|
|
50.63 0.3342 0.5771 0.0994 0.0576 7.591 59.805 32.445 5660.527 6.757 144.315 2.600 0.64 312264. 0.4345
|
|
55.69 0.3676 0.6118 0.0965 0.0580 7.646 60.237 31.498 5701.406 6.806 140.105 2.506 0.64 312996. 0.4126
|
|
60.76 0.4010 0.6438 0.0932 0.0580 7.652 60.285 30.406 5705.915 6.811 135.244 2.417 0.64 313781. 0.3910
|
|
65.82 0.4344 0.6732 0.0894 0.0577 7.607 59.932 29.177 5672.573 6.771 129.778 2.333 0.64 314617. 0.3697
|
|
70.88 0.4678 0.7002 0.0853 0.0570 7.511 59.178 27.825 5601.142 6.686 123.766 2.253 0.64 315505. 0.3487
|
|
75.95 0.5012 0.7250 0.0808 0.0559 7.365 58.025 26.365 5492.078 6.556 117.272 2.177 0.64 316444. 0.3280
|
|
81.01 0.5347 0.7475 0.0760 0.0544 7.169 56.483 24.810 5346.117 6.381 110.355 2.105 0.64 317433. 0.3076
|
|
86.07 0.5681 0.7680 0.0710 0.0525 6.925 54.560 23.172 5164.058 6.164 103.069 2.035 0.64 318471. 0.2874
|
|
91.14 0.6015 0.7862 0.0658 0.0503 6.634 52.263 21.462 4946.637 5.905 95.461 1.968 0.65 319560. 0.2675
|
|
96.20 0.6349 0.8022 0.0603 0.0477 6.295 49.599 19.688 4694.505 5.604 87.572 1.902 0.65 320697. 0.2476
|
|
101.26 0.6683 0.8157 0.0547 0.0448 5.912 46.575 17.859 4408.279 5.262 79.437 1.838 0.65 321883. 0.2278
|
|
106.33 0.7017 0.8265 0.0490 0.0416 5.483 43.196 15.983 4088.522 4.880 71.091 1.773 0.65 323118. 0.2080
|
|
111.39 0.7352 0.8339 0.0431 0.0380 5.010 39.470 14.065 3735.786 4.459 62.560 1.708 0.65 324400. 0.1879
|
|
116.45 0.7686 0.8370 0.0371 0.0341 4.493 35.401 12.112 3350.638 4.000 53.873 1.640 0.65 325729. 0.1674
|
|
121.51 0.8020 0.8343 0.0310 0.0298 3.934 30.996 10.129 2933.752 3.502 45.056 1.566 0.66 327104. 0.1462
|
|
126.58 0.8354 0.8226 0.0249 0.0253 3.334 26.265 8.124 2485.983 2.967 36.138 1.482 0.66 328525. 0.1240
|
|
131.64 0.8688 0.7955 0.0187 0.0204 2.693 21.220 6.104 2008.418 2.397 27.148 1.378 0.66 329988. 0.0999
|
|
136.70 0.9022 0.7370 0.0125 0.0153 2.015 15.872 4.073 1502.240 1.793 18.118 1.230 0.66 331488. 0.0728
|
|
141.77 0.9357 0.5931 0.0062 0.0098 1.297 10.221 2.035 967.429 1.155 9.053 0.954 0.66 332999. 0.0399
|
|
146.83 0.9691 -0.1392 -0.0005 0.0036 0.474 3.734 -0.168 353.374 0.422 -0.749 -0.216 0.66 332629. 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 0.1109 0.0472 8.852 61.995 45.804 6601.219 7.004 203.736 3.147 0.71 346065. 0.6249
|
|
5.71 0.0335 0.0765 0.1106 0.0484 9.090 63.657 45.687 6778.265 7.192 203.217 3.057 0.71 346367. 0.6063
|
|
11.42 0.0670 0.1485 0.1103 0.0498 9.342 65.426 45.549 6966.632 7.392 202.601 2.965 0.71 346710. 0.5872
|
|
17.13 0.1005 0.2158 0.1099 0.0512 9.607 67.281 45.379 7164.175 7.601 201.847 2.873 0.71 347097. 0.5678
|
|
22.84 0.1340 0.2785 0.1094 0.0526 9.880 69.194 45.166 7367.840 7.818 200.899 2.780 0.71 347531. 0.5482
|
|
28.55 0.1675 0.3366 0.1087 0.0541 10.156 71.123 44.893 7573.264 8.035 199.685 2.689 0.72 348015. 0.5285
|
|
34.27 0.2010 0.3903 0.1078 0.0555 10.426 73.014 44.539 7774.527 8.249 198.109 2.598 0.72 348553. 0.5088
|
|
39.98 0.2345 0.4399 0.1067 0.0569 10.680 74.793 44.077 7963.960 8.450 196.056 2.510 0.72 349145. 0.4890
|
|
45.69 0.2680 0.4857 0.1053 0.0581 10.906 76.373 43.478 8132.288 8.629 193.392 2.425 0.72 349795. 0.4691
|
|
51.40 0.3015 0.5279 0.1034 0.0591 11.089 77.660 42.713 8269.316 8.774 189.986 2.343 0.72 350504. 0.4492
|
|
57.11 0.3350 0.5668 0.1011 0.0598 11.218 78.563 41.756 8365.446 8.876 185.733 2.264 0.72 351273. 0.4292
|
|
62.82 0.3685 0.6028 0.0983 0.0601 11.282 79.012 40.599 8413.268 8.927 180.582 2.189 0.72 352102. 0.4091
|
|
68.53 0.4020 0.6360 0.0950 0.0601 11.276 78.967 39.242 8408.412 8.922 174.548 2.117 0.72 352990. 0.3890
|
|
74.24 0.4356 0.6666 0.0913 0.0596 11.196 78.410 37.699 8349.167 8.859 167.687 2.048 0.72 353937. 0.3689
|
|
79.95 0.4691 0.6947 0.0871 0.0588 11.044 77.342 35.989 8235.428 8.738 160.077 1.982 0.72 354943. 0.3488
|
|
85.66 0.5026 0.7205 0.0826 0.0576 10.819 75.769 34.128 8067.923 8.560 151.803 1.919 0.72 356007. 0.3288
|
|
91.37 0.5361 0.7441 0.0778 0.0561 10.524 73.700 32.137 7847.652 8.327 142.946 1.857 0.72 357127. 0.3089
|
|
97.09 0.5696 0.7653 0.0727 0.0541 10.159 71.145 30.032 7575.581 8.038 133.582 1.798 0.73 358305. 0.2891
|
|
102.80 0.6031 0.7843 0.0674 0.0518 9.726 68.111 27.827 7252.530 7.695 123.776 1.740 0.73 359538. 0.2693
|
|
108.51 0.6366 0.8009 0.0618 0.0491 9.225 64.604 25.536 6879.083 7.299 113.586 1.684 0.73 360826. 0.2496
|
|
114.22 0.6701 0.8151 0.0561 0.0461 8.657 60.628 23.170 6455.703 6.850 103.059 1.628 0.73 362170. 0.2299
|
|
119.93 0.7036 0.8266 0.0502 0.0427 8.023 56.188 20.737 5982.931 6.348 92.239 1.572 0.73 363568. 0.2100
|
|
125.64 0.7371 0.8347 0.0442 0.0390 7.324 51.290 18.248 5461.428 5.795 81.166 1.515 0.73 365019. 0.1899
|
|
131.35 0.7706 0.8387 0.0380 0.0349 6.560 45.942 15.710 4891.984 5.191 69.877 1.457 0.74 366524. 0.1694
|
|
137.06 0.8041 0.8370 0.0318 0.0305 5.734 40.154 13.131 4275.573 4.537 58.408 1.393 0.74 368081. 0.1481
|
|
142.77 0.8376 0.8266 0.0255 0.0258 4.846 33.935 10.521 3613.447 3.834 46.797 1.321 0.74 369688. 0.1257
|
|
148.48 0.8711 0.8010 0.0191 0.0208 3.899 27.303 7.888 2907.210 3.085 35.084 1.231 0.74 371343. 0.1014
|
|
154.19 0.9046 0.7443 0.0127 0.0154 2.895 20.272 5.240 2158.610 2.290 23.307 1.101 0.74 373040. 0.0739
|
|
159.91 0.9381 0.5999 0.0062 0.0098 1.834 12.843 2.580 1367.507 1.451 11.476 0.856 0.75 374746. 0.0403
|
|
165.62 0.9716
|
|
|
|
|
|
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