464 lines
82 KiB
Plaintext
464 lines
82 KiB
Plaintext
20x13E (20x13E.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 0.0954 0.0384 0.010 0.623 0.486 7.376 0.070 2.163 29.899 0.08 36651. 0.6117
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0.52 0.0276 0.0665 0.0942 0.0391 0.010 0.634 0.481 7.500 0.072 2.138 29.061 0.08 36677. 0.5910
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1.04 0.0552 0.1292 0.0930 0.0397 0.010 0.644 0.474 7.622 0.073 2.110 28.223 0.08 36707. 0.5702
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1.57 0.0827 0.1881 0.0916 0.0403 0.010 0.654 0.467 7.739 0.074 2.079 27.389 0.08 36739. 0.5493
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2.09 0.1103 0.2433 0.0901 0.0409 0.011 0.663 0.460 7.849 0.075 2.045 26.562 0.08 36775. 0.5283
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2.61 0.1379 0.2947 0.0885 0.0414 0.011 0.672 0.451 7.949 0.076 2.007 25.745 0.08 36814. 0.5074
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3.13 0.1655 0.3426 0.0867 0.0419 0.011 0.679 0.442 8.038 0.077 1.966 24.941 0.08 36856. 0.4865
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3.66 0.1930 0.3871 0.0847 0.0422 0.011 0.686 0.432 8.110 0.077 1.921 24.152 0.08 36901. 0.4656
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4.18 0.2206 0.4282 0.0825 0.0425 0.011 0.690 0.421 8.165 0.078 1.872 23.378 0.08 36951. 0.4449
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4.70 0.2482 0.4662 0.0802 0.0427 0.011 0.693 0.409 8.197 0.078 1.818 22.621 0.08 37003. 0.4243
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5.22 0.2758 0.5010 0.0776 0.0427 0.011 0.694 0.396 8.205 0.078 1.761 21.881 0.08 37060. 0.4039
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5.75 0.3033 0.5329 0.0749 0.0426 0.011 0.692 0.382 8.185 0.078 1.698 21.156 0.08 37120. 0.3835
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6.27 0.3309 0.5618 0.0719 0.0424 0.011 0.688 0.367 8.135 0.078 1.631 20.447 0.08 37185. 0.3633
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6.79 0.3585 0.5879 0.0687 0.0419 0.011 0.680 0.351 8.051 0.077 1.559 19.750 0.08 37253. 0.3431
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7.31 0.3861 0.6110 0.0654 0.0413 0.011 0.670 0.333 7.930 0.076 1.482 19.062 0.08 37325. 0.3229
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7.83 0.4136 0.6312 0.0618 0.0405 0.010 0.657 0.315 7.771 0.074 1.401 18.380 0.08 37401. 0.3026
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8.36 0.4412 0.6484 0.0579 0.0394 0.010 0.640 0.295 7.571 0.072 1.314 17.698 0.08 37481. 0.2822
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8.88 0.4688 0.6622 0.0539 0.0382 0.010 0.620 0.275 7.332 0.070 1.223 17.012 0.08 37566. 0.2617
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9.40 0.4964 0.6723 0.0498 0.0367 0.009 0.596 0.254 7.056 0.067 1.129 16.313 0.08 37654. 0.2411
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9.92 0.5240 0.6783 0.0455 0.0351 0.009 0.570 0.232 6.745 0.064 1.031 15.591 0.08 37746. 0.2203
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10.45 0.5515 0.6794 0.0411 0.0333 0.009 0.541 0.209 6.400 0.061 0.931 14.836 0.08 37841. 0.1992
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10.97 0.5791 0.6748 0.0366 0.0314 0.008 0.509 0.186 6.024 0.058 0.829 14.034 0.08 37941. 0.1778
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11.49 0.6067 0.6632 0.0320 0.0293 0.008 0.475 0.163 5.617 0.054 0.725 13.166 0.08 38045. 0.1560
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12.01 0.6343 0.6428 0.0273 0.0270 0.007 0.438 0.139 5.181 0.049 0.620 12.206 0.08 38153. 0.1337
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12.53 0.6618 0.6109 0.0227 0.0246 0.006 0.399 0.116 4.720 0.045 0.515 11.117 0.08 38264. 0.1109
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13.06 0.6894 0.5635 0.0180 0.0221 0.006 0.358 0.092 4.235 0.040 0.409 9.844 0.08 38380. 0.0876
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13.58 0.7170 0.4942 0.0134 0.0194 0.005 0.315 0.068 3.728 0.036 0.304 8.302 0.08 38499. 0.0636
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14.10 0.7446 0.3923 0.0088 0.0167 0.004 0.271 0.045 3.205 0.031 0.199 6.346 0.08 38622. 0.0394
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14.62 0.7721 0.2382 0.0043 0.0139 0.004 0.225 0.022 2.667 0.025 0.097 3.716 0.08 38749. 0.0161
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15.15 0.7997 -0.0079 -0.0001 0.0110 0.003 0.179 -0.001 2.121 0.020 -0.002 -0.119 0.08 38880. 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 0.0957 0.0358 0.074 2.325 1.952 55.012 0.263 8.683 16.095 0.16 73300. 0.6598
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1.05 0.0277 0.0717 0.0946 0.0365 0.075 2.369 1.930 56.063 0.268 8.582 15.610 0.16 73354. 0.6362
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2.10 0.0553 0.1390 0.0934 0.0372 0.077 2.413 1.904 57.100 0.273 8.471 15.128 0.16 73413. 0.6125
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3.14 0.0830 0.2020 0.0920 0.0378 0.078 2.455 1.877 58.103 0.277 8.348 14.651 0.16 73478. 0.5888
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4.19 0.1107 0.2607 0.0905 0.0384 0.079 2.496 1.846 59.052 0.282 8.212 14.180 0.16 73550. 0.5653
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5.24 0.1384 0.3152 0.0889 0.0390 0.080 2.533 1.812 59.928 0.286 8.062 13.718 0.16 73628. 0.5418
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6.29 0.1660 0.3658 0.0870 0.0395 0.081 2.565 1.775 60.704 0.290 7.897 13.266 0.16 73712. 0.5186
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7.34 0.1937 0.4125 0.0851 0.0399 0.082 2.593 1.735 61.358 0.293 7.717 12.825 0.16 73804. 0.4956
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8.39 0.2214 0.4557 0.0829 0.0403 0.083 2.614 1.691 61.863 0.295 7.520 12.395 0.16 73903. 0.4728
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9.43 0.2491 0.4954 0.0805 0.0405 0.083 2.628 1.642 62.192 0.297 7.306 11.978 0.16 74010. 0.4504
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10.48 0.2767 0.5319 0.0780 0.0406 0.084 2.634 1.590 62.320 0.298 7.073 11.573 0.16 74124. 0.4282
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11.53 0.3044 0.5652 0.0752 0.0405 0.083 2.629 1.534 62.220 0.297 6.822 11.181 0.16 74245. 0.4062
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12.58 0.3321 0.5955 0.0722 0.0403 0.083 2.615 1.473 61.866 0.295 6.552 10.799 0.16 74375. 0.3845
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13.63 0.3598 0.6230 0.0690 0.0399 0.082 2.588 1.408 61.235 0.292 6.262 10.428 0.16 74512. 0.3630
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14.68 0.3874 0.6476 0.0656 0.0393 0.081 2.548 1.338 60.304 0.288 5.953 10.066 0.16 74657. 0.3416
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15.72 0.4151 0.6694 0.0620 0.0384 0.079 2.495 1.264 59.047 0.282 5.623 9.710 0.16 74811. 0.3203
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16.77 0.4428 0.6882 0.0581 0.0374 0.077 2.428 1.186 57.455 0.274 5.274 9.360 0.16 74972. 0.2990
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17.82 0.4705 0.7040 0.0541 0.0362 0.074 2.347 1.103 55.535 0.265 4.908 9.012 0.16 75141. 0.2777
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18.87 0.4981 0.7165 0.0499 0.0347 0.071 2.253 1.018 53.301 0.254 4.528 8.662 0.16 75318. 0.2564
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19.92 0.5258 0.7253 0.0456 0.0330 0.068 2.145 0.930 50.766 0.242 4.135 8.306 0.16 75503. 0.2350
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20.97 0.5535 0.7297 0.0411 0.0312 0.064 2.026 0.839 47.942 0.229 3.733 7.939 0.16 75696. 0.2134
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22.01 0.5812 0.7290 0.0366 0.0292 0.060 1.895 0.747 44.843 0.214 3.322 7.554 0.16 75897. 0.1915
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23.06 0.6088 0.7219 0.0320 0.0270 0.056 1.753 0.653 41.483 0.198 2.905 7.141 0.16 76106. 0.1693
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24.11 0.6365 0.7068 0.0274 0.0247 0.051 1.601 0.558 37.876 0.181 2.484 6.687 0.16 76323. 0.1466
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25.16 0.6642 0.6807 0.0227 0.0222 0.046 1.439 0.463 34.041 0.163 2.060 6.172 0.16 76547. 0.1232
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26.21 0.6918 0.6393 0.0180 0.0195 0.040 1.268 0.368 29.998 0.143 1.637 5.565 0.16 76780. 0.0990
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27.25 0.7195 0.5750 0.0134 0.0168 0.035 1.089 0.273 25.774 0.123 1.216 4.812 0.16 77020. 0.0738
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28.30 0.7472 0.4735 0.0088 0.0139 0.029 0.904 0.180 21.397 0.102 0.801 3.816 0.16 77268. 0.0475
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29.35 0.7749 0.3054 0.0043 0.0110 0.023 0.714 0.088 16.903 0.081 0.393 2.373 0.16 77524. 0.0207
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30.40 0.8025 -0.0036 0.0000 0.0080 0.017 0.521 -0.001 12.326 0.059 -0.003 -0.027 0.16 77786. 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 0.0961 0.0348 0.242 5.080 4.410 180.312 0.574 19.614 11.092 0.24 109947. 0.6833
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1.57 0.0277 0.0742 0.0950 0.0355 0.247 5.183 4.359 183.968 0.586 19.389 10.747 0.24 110028. 0.6583
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3.15 0.0554 0.1436 0.0938 0.0362 0.252 5.285 4.303 187.579 0.597 19.140 10.405 0.24 110117. 0.6332
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4.72 0.0831 0.2085 0.0924 0.0369 0.256 5.384 4.241 191.083 0.608 18.864 10.067 0.24 110215. 0.6082
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6.30 0.1109 0.2688 0.0909 0.0375 0.261 5.477 4.172 194.410 0.619 18.559 9.735 0.24 110323. 0.5834
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7.87 0.1386 0.3248 0.0893 0.0381 0.265 5.564 4.097 197.486 0.629 18.223 9.409 0.24 110440. 0.5587
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9.45 0.1663 0.3766 0.0875 0.0386 0.269 5.641 4.014 200.231 0.637 17.853 9.092 0.24 110568. 0.5344
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11.02 0.1940 0.4244 0.0855 0.0391 0.272 5.707 3.922 202.558 0.645 17.447 8.783 0.24 110706. 0.5103
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12.60 0.2217 0.4685 0.0833 0.0394 0.274 5.758 3.823 204.379 0.651 17.004 8.484 0.24 110855. 0.4866
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14.17 0.2494 0.5090 0.0809 0.0397 0.276 5.793 3.714 205.601 0.654 16.521 8.194 0.24 111015. 0.4633
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15.75 0.2771 0.5462 0.0784 0.0398 0.276 5.808 3.596 206.132 0.656 15.996 7.913 0.24 111186. 0.4403
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17.32 0.3048 0.5803 0.0756 0.0397 0.276 5.801 3.469 205.882 0.655 15.429 7.642 0.24 111369. 0.4176
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18.89 0.3326 0.6113 0.0726 0.0395 0.275 5.769 3.332 204.761 0.652 14.819 7.380 0.24 111564. 0.3952
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20.47 0.3603 0.6395 0.0694 0.0391 0.272 5.711 3.184 202.687 0.645 14.164 7.126 0.24 111771. 0.3731
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22.04 0.3880 0.6648 0.0660 0.0385 0.268 5.623 3.027 199.577 0.635 13.464 6.879 0.24 111989. 0.3511
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23.62 0.4157 0.6874 0.0623 0.0377 0.262 5.504 2.859 195.345 0.622 12.718 6.639 0.24 112220. 0.3293
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25.19 0.4434 0.7072 0.0584 0.0366 0.255 5.352 2.682 189.955 0.605 11.928 6.403 0.24 112463. 0.3076
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26.77 0.4711 0.7241 0.0544 0.0354 0.246 5.168 2.495 183.429 0.584 11.100 6.171 0.24 112717. 0.2860
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28.34 0.4988 0.7379 0.0502 0.0339 0.236 4.953 2.302 175.809 0.560 10.239 5.939 0.24 112984. 0.2643
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29.92 0.5265 0.7482 0.0458 0.0322 0.224 4.709 2.102 167.138 0.532 9.350 5.705 0.24 113262. 0.2427
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31.49 0.5543 0.7545 0.0413 0.0304 0.211 4.436 1.897 157.459 0.501 8.439 5.465 0.24 113553. 0.2209
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33.07 0.5820 0.7561 0.0368 0.0283 0.197 4.136 1.688 146.815 0.467 7.510 5.216 0.24 113855. 0.1988
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34.64 0.6097 0.7518 0.0322 0.0261 0.181 3.811 1.476 135.253 0.431 6.566 4.950 0.24 114169. 0.1765
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36.22 0.6374 0.7399 0.0275 0.0237 0.165 3.461 1.262 122.826 0.391 5.613 4.660 0.24 114495. 0.1536
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37.79 0.6651 0.7177 0.0228 0.0211 0.147 3.088 1.047 109.596 0.349 4.656 4.332 0.24 114833. 0.1300
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39.36 0.6928 0.6807 0.0181 0.0184 0.128 2.695 0.832 95.638 0.304 3.700 3.945 0.24 115182. 0.1055
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40.94 0.7205 0.6209 0.0135 0.0156 0.109 2.283 0.618 81.041 0.258 2.749 3.459 0.24 115543. 0.0798
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42.51 0.7482 0.5223 0.0089 0.0127 0.088 1.857 0.407 65.908 0.210 1.811 2.802 0.24 115917. 0.0525
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44.09 0.7760 0.3492 0.0044 0.0097 0.068 1.419 0.201 50.365 0.160 0.892 1.807 0.25 116301. 0.0237
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45.66 0.8037 -0.0011 0.0000 0.0067 0.046 0.973 0.000 34.528 0.110 -0.002 -0.006 0.25 116694. 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 0.0966 0.0343 0.565 8.907 7.878 421.538 1.006 35.039 8.476 0.32 146591. 0.6980
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2.10 0.0277 0.0756 0.0955 0.0350 0.577 9.095 7.789 430.403 1.028 34.645 8.208 0.32 146699. 0.6721
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4.20 0.0555 0.1463 0.0943 0.0357 0.589 9.280 7.690 439.173 1.048 34.206 7.942 0.32 146818. 0.6462
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6.30 0.0832 0.2122 0.0929 0.0364 0.600 9.460 7.581 447.694 1.069 33.720 7.680 0.32 146949. 0.6204
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8.40 0.1109 0.2735 0.0914 0.0371 0.611 9.631 7.460 455.801 1.088 33.181 7.423 0.32 147093. 0.5948
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10.50 0.1386 0.3302 0.0898 0.0377 0.621 9.790 7.326 463.313 1.106 32.586 7.172 0.32 147250. 0.5695
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12.60 0.1664 0.3828 0.0880 0.0382 0.630 9.932 7.179 470.036 1.122 31.930 6.927 0.32 147420. 0.5445
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14.70 0.1941 0.4312 0.0860 0.0387 0.638 10.053 7.017 475.762 1.136 31.210 6.689 0.32 147604. 0.5199
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16.81 0.2218 0.4759 0.0838 0.0391 0.644 10.148 6.839 480.274 1.147 30.422 6.459 0.32 147803. 0.4956
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18.91 0.2496 0.5169 0.0815 0.0393 0.648 10.214 6.646 483.351 1.154 29.562 6.237 0.32 148017. 0.4717
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21.01 0.2773 0.5546 0.0789 0.0394 0.650 10.243 6.436 484.768 1.157 28.628 6.022 0.32 148246. 0.4482
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23.11 0.3050 0.5891 0.0761 0.0394 0.649 10.234 6.209 484.304 1.156 27.618 5.815 0.32 148491. 0.4251
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25.21 0.3327 0.6206 0.0731 0.0392 0.646 10.180 5.964 481.745 1.150 26.528 5.615 0.32 148751. 0.4023
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27.31 0.3605 0.6492 0.0699 0.0388 0.640 10.077 5.701 476.888 1.138 25.359 5.422 0.32 149027. 0.3798
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29.41 0.3882 0.6750 0.0664 0.0382 0.630 9.921 5.420 469.532 1.121 24.107 5.236 0.32 149319. 0.3576
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31.51 0.4159 0.6982 0.0628 0.0374 0.616 9.709 5.120 459.470 1.097 22.773 5.054 0.32 149627. 0.3355
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33.61 0.4437 0.7186 0.0589 0.0363 0.599 9.437 4.802 446.604 1.066 21.360 4.877 0.32 149952. 0.3136
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35.71 0.4714 0.7363 0.0548 0.0351 0.578 9.107 4.469 430.987 1.029 19.878 4.703 0.32 150292. 0.2917
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37.81 0.4991 0.7510 0.0505 0.0336 0.553 8.721 4.123 412.715 0.985 18.337 4.531 0.32 150648. 0.2699
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39.91 0.5269 0.7625 0.0461 0.0319 0.526 8.281 3.765 391.887 0.936 16.746 4.357 0.32 151020. 0.2481
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42.01 0.5546 0.7701 0.0417 0.0300 0.494 7.789 3.398 368.603 0.880 15.114 4.181 0.32 151407. 0.2261
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44.11 0.5823 0.7733 0.0371 0.0279 0.460 7.247 3.024 342.968 0.819 13.449 3.999 0.32 151811. 0.2040
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46.22 0.6100 0.7710 0.0324 0.0256 0.423 6.658 2.644 315.095 0.752 11.759 3.806 0.32 152230. 0.1815
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48.32 0.6378 0.7616 0.0277 0.0232 0.382 6.025 2.260 285.111 0.681 10.053 3.595 0.32 152665. 0.1586
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50.42 0.6655 0.7423 0.0230 0.0206 0.340 5.350 1.875 253.168 0.604 8.338 3.359 0.32 153116. 0.1349
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52.52 0.6932 0.7088 0.0183 0.0179 0.294 4.637 1.489 219.447 0.524 6.625 3.079 0.32 153583. 0.1102
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54.62 0.7210 0.6528 0.0136 0.0150 0.247 3.891 1.107 184.164 0.440 4.924 2.726 0.33 154065. 0.0841
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56.72 0.7487 0.5575 0.0089 0.0120 0.198 3.118 0.729 147.578 0.352 3.245 2.242 0.33 154563. 0.0562
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58.82 0.7764 0.3826 0.0044 0.0090 0.148 2.324 0.360 109.994 0.263 1.600 1.484 0.33 155077. 0.0261
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60.92 0.8041 0.0002 0.0000 0.0058 0.096 1.515 0.000 71.687 0.171 0.000 0.001 0.33 155601. 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 0.0971 0.0341 1.098 13.847 12.384 819.133 1.564 55.083 6.857 0.40 183231. 0.7079
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2.63 0.0277 0.0765 0.0961 0.0349 1.122 14.146 12.247 836.827 1.598 54.476 6.638 0.40 183366. 0.6816
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5.25 0.0555 0.1479 0.0949 0.0356 1.146 14.442 12.095 854.354 1.632 53.800 6.421 0.40 183515. 0.6552
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7.88 0.0832 0.2145 0.0936 0.0363 1.169 14.731 11.926 871.404 1.664 53.048 6.208 0.40 183679. 0.6289
|
|
10.51 0.1110 0.2763 0.0921 0.0370 1.190 15.005 11.739 887.648 1.695 52.213 5.998 0.40 183859. 0.6029
|
|
13.14 0.1387 0.3336 0.0905 0.0376 1.211 15.260 11.531 902.727 1.724 51.289 5.794 0.40 184055. 0.5772
|
|
15.76 0.1665 0.3866 0.0887 0.0382 1.229 15.489 11.301 916.250 1.750 50.269 5.595 0.40 184268. 0.5518
|
|
18.39 0.1942 0.4355 0.0867 0.0387 1.244 15.684 11.049 927.802 1.772 49.147 5.402 0.40 184499. 0.5268
|
|
21.02 0.2219 0.4805 0.0845 0.0390 1.256 15.839 10.773 936.951 1.789 47.916 5.215 0.40 184749. 0.5022
|
|
23.64 0.2497 0.5219 0.0821 0.0393 1.265 15.945 10.470 943.253 1.801 46.572 5.035 0.40 185017. 0.4780
|
|
26.27 0.2774 0.5599 0.0796 0.0394 1.269 15.996 10.142 946.259 1.807 45.110 4.861 0.40 185304. 0.4542
|
|
28.90 0.3052 0.5947 0.0768 0.0394 1.268 15.984 9.785 945.525 1.806 43.525 4.694 0.40 185610. 0.4308
|
|
31.53 0.3329 0.6265 0.0737 0.0392 1.261 15.901 9.401 940.627 1.796 41.815 4.533 0.40 185936. 0.4078
|
|
34.15 0.3607 0.6555 0.0705 0.0388 1.249 15.741 8.988 931.157 1.778 39.977 4.378 0.40 186282. 0.3851
|
|
36.78 0.3884 0.6818 0.0670 0.0382 1.229 15.497 8.545 916.716 1.751 38.010 4.228 0.40 186648. 0.3626
|
|
39.41 0.4161 0.7054 0.0633 0.0374 1.203 15.161 8.073 896.890 1.713 35.910 4.083 0.40 187034. 0.3403
|
|
42.04 0.4439 0.7263 0.0594 0.0363 1.169 14.732 7.573 871.472 1.664 33.685 3.941 0.40 187440. 0.3182
|
|
44.66 0.4716 0.7446 0.0553 0.0350 1.127 14.209 7.048 840.557 1.605 31.349 3.803 0.40 187866. 0.2962
|
|
47.29 0.4994 0.7601 0.0510 0.0335 1.079 13.597 6.502 804.332 1.536 28.919 3.666 0.40 188312. 0.2743
|
|
49.92 0.5271 0.7724 0.0466 0.0318 1.023 12.898 5.937 762.992 1.457 26.410 3.530 0.40 188777. 0.2523
|
|
52.54 0.5549 0.7811 0.0420 0.0299 0.961 12.116 5.358 716.735 1.369 23.834 3.391 0.40 189263. 0.2303
|
|
55.17 0.5826 0.7856 0.0374 0.0277 0.893 11.254 4.768 665.768 1.272 21.207 3.248 0.40 189768. 0.2081
|
|
57.80 0.6103 0.7849 0.0327 0.0254 0.818 10.317 4.168 610.313 1.166 18.539 3.097 0.40 190293. 0.1855
|
|
60.43 0.6381 0.7773 0.0279 0.0229 0.738 9.308 3.562 550.628 1.052 15.844 2.934 0.40 190838. 0.1625
|
|
63.05 0.6658 0.7603 0.0232 0.0203 0.653 8.233 2.954 487.015 0.930 13.137 2.751 0.41 191402. 0.1387
|
|
65.68 0.6936 0.7296 0.0184 0.0175 0.563 7.097 2.345 419.838 0.802 10.432 2.534 0.41 191986. 0.1138
|
|
68.31 0.7213 0.6767 0.0137 0.0146 0.469 5.909 1.741 349.532 0.668 7.745 2.260 0.41 192590. 0.0875
|
|
70.93 0.7491 0.5840 0.0090 0.0115 0.371 4.676 1.145 276.622 0.528 5.095 1.878 0.41 193213. 0.0590
|
|
73.56 0.7768 0.4075 0.0044 0.0084 0.271 3.410 0.562 201.724 0.385 2.499 1.263 0.41 193855. 0.0278
|
|
76.19 0.8046 -0.0070 0.0000 0.0052 0.168 2.119 -0.006 125.367 0.239 -0.026 -0.021 0.41 194510. 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 0.0979 0.0342 1.900 19.962 17.965 1417.010 2.255 79.909 5.750 0.48 219864. 0.7151
|
|
3.15 0.0277 0.0769 0.0968 0.0349 1.942 20.402 17.773 1448.265 2.305 79.055 5.566 0.48 220026. 0.6885
|
|
6.30 0.0554 0.1487 0.0957 0.0357 1.984 20.839 17.558 1479.265 2.354 78.099 5.384 0.48 220205. 0.6618
|
|
9.45 0.0832 0.2156 0.0943 0.0364 2.024 21.264 17.319 1509.458 2.402 77.034 5.204 0.48 220402. 0.6354
|
|
12.60 0.1109 0.2778 0.0929 0.0371 2.063 21.670 17.052 1538.271 2.448 75.848 5.028 0.48 220618. 0.6091
|
|
15.75 0.1386 0.3353 0.0913 0.0377 2.099 22.047 16.756 1565.061 2.491 74.532 4.856 0.48 220854. 0.5832
|
|
18.90 0.1663 0.3886 0.0895 0.0383 2.131 22.386 16.429 1589.138 2.529 73.075 4.689 0.48 221110. 0.5576
|
|
22.05 0.1941 0.4377 0.0875 0.0388 2.159 22.677 16.068 1609.769 2.562 71.469 4.527 0.48 221387. 0.5324
|
|
25.20 0.2218 0.4829 0.0854 0.0392 2.181 22.908 15.671 1626.188 2.588 69.703 4.371 0.48 221687. 0.5076
|
|
28.35 0.2495 0.5246 0.0830 0.0395 2.196 23.069 15.236 1637.608 2.606 67.771 4.220 0.48 222008. 0.4833
|
|
31.50 0.2772 0.5628 0.0804 0.0396 2.204 23.148 14.763 1643.240 2.615 65.666 4.075 0.48 222353. 0.4593
|
|
34.65 0.3050 0.5979 0.0776 0.0396 2.202 23.135 14.249 1642.301 2.614 63.380 3.935 0.48 222721. 0.4358
|
|
37.80 0.3327 0.6300 0.0746 0.0394 2.191 23.019 13.694 1634.035 2.601 60.909 3.801 0.48 223113. 0.4127
|
|
40.96 0.3604 0.6593 0.0713 0.0390 2.169 22.789 13.096 1617.728 2.575 58.251 3.672 0.48 223528. 0.3898
|
|
44.11 0.3881 0.6859 0.0679 0.0384 2.136 22.436 12.456 1592.680 2.535 55.403 3.547 0.48 223967. 0.3673
|
|
47.26 0.4159 0.7099 0.0641 0.0376 2.090 21.950 11.771 1558.159 2.480 52.360 3.427 0.48 224431. 0.3449
|
|
50.41 0.4436 0.7313 0.0602 0.0365 2.030 21.325 11.046 1513.771 2.409 49.130 3.310 0.48 224918. 0.3227
|
|
53.56 0.4713 0.7502 0.0560 0.0352 1.957 20.562 10.283 1459.664 2.323 45.738 3.195 0.48 225429. 0.3006
|
|
56.71 0.4990 0.7663 0.0517 0.0337 1.872 19.668 9.489 1396.158 2.222 42.205 3.083 0.48 225964. 0.2786
|
|
59.86 0.5267 0.7795 0.0472 0.0319 1.775 18.646 8.668 1323.598 2.107 38.555 2.970 0.48 226523. 0.2566
|
|
63.01 0.5545 0.7892 0.0426 0.0300 1.666 17.501 7.825 1242.331 1.977 34.806 2.857 0.48 227105. 0.2345
|
|
66.16 0.5822 0.7948 0.0379 0.0278 1.546 16.238 6.965 1152.717 1.835 30.979 2.740 0.48 227711. 0.2122
|
|
69.31 0.6099 0.7955 0.0332 0.0254 1.415 14.864 6.091 1055.152 1.679 27.092 2.618 0.48 228340. 0.1896
|
|
72.46 0.6376 0.7898 0.0284 0.0229 1.274 13.384 5.208 950.087 1.512 23.165 2.486 0.49 228994. 0.1665
|
|
75.61 0.6654 0.7751 0.0235 0.0202 1.124 11.806 4.321 838.057 1.334 19.218 2.338 0.49 229670. 0.1426
|
|
78.76 0.6931 0.7471 0.0187 0.0174 0.965 10.138 3.433 719.702 1.145 15.272 2.164 0.49 230370. 0.1176
|
|
81.91 0.7208 0.6977 0.0139 0.0144 0.799 8.393 2.552 595.795 0.948 11.352 1.943 0.49 231094. 0.0911
|
|
85.06 0.7485 0.6091 0.0092 0.0113 0.627 6.582 1.683 467.266 0.744 7.484 1.633 0.49 231841. 0.0622
|
|
88.21 0.7763 0.4349 0.0045 0.0081 0.450 4.722 0.831 335.213 0.534 3.697 1.125 0.49 232611. 0.0301
|
|
91.36 0.8040 0.0023 0.0000 0.0048 0.269 2.826 0.003 200.584 0.319 0.011 0.006 0.49 233395. 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 0.0987 0.0344 3.036 27.338 24.670 2264.120 3.089 109.732 4.942 0.56 256490. 0.7202
|
|
3.67 0.0277 0.0771 0.0977 0.0351 3.105 27.953 24.416 2315.037 3.158 108.603 4.784 0.56 256679. 0.6935
|
|
7.35 0.0554 0.1491 0.0966 0.0359 3.172 28.564 24.131 2365.609 3.227 107.335 4.627 0.56 256888. 0.6668
|
|
11.02 0.0831 0.2161 0.0953 0.0367 3.238 29.160 23.812 2414.944 3.294 105.916 4.472 0.56 257118. 0.6403
|
|
14.70 0.1109 0.2784 0.0939 0.0374 3.302 29.729 23.456 2462.098 3.359 104.331 4.321 0.56 257370. 0.6140
|
|
18.37 0.1386 0.3361 0.0923 0.0380 3.361 30.259 23.059 2506.014 3.419 102.565 4.173 0.56 257646. 0.5880
|
|
22.05 0.1663 0.3895 0.0905 0.0386 3.414 30.737 22.618 2545.563 3.473 100.603 4.030 0.56 257945. 0.5623
|
|
25.72 0.1940 0.4388 0.0886 0.0392 3.459 31.147 22.130 2579.541 3.519 98.433 3.891 0.56 258269. 0.5370
|
|
29.40 0.2217 0.4842 0.0864 0.0396 3.496 31.475 21.592 2606.691 3.556 96.041 3.757 0.56 258619. 0.5122
|
|
33.07 0.2494 0.5260 0.0841 0.0399 3.521 31.705 21.002 2625.733 3.582 93.417 3.628 0.56 258995. 0.4878
|
|
36.75 0.2772 0.5644 0.0815 0.0400 3.534 31.821 20.357 2635.372 3.595 90.549 3.504 0.56 259398. 0.4638
|
|
40.42 0.3049 0.5997 0.0787 0.0400 3.533 31.809 19.656 2634.333 3.594 87.429 3.384 0.56 259828. 0.4402
|
|
44.09 0.3326 0.6320 0.0756 0.0398 3.515 31.652 18.896 2621.384 3.576 84.051 3.270 0.56 260286. 0.4170
|
|
47.77 0.3603 0.6616 0.0724 0.0394 3.480 31.338 18.078 2595.363 3.541 80.410 3.159 0.56 260771. 0.3941
|
|
51.44 0.3880 0.6885 0.0688 0.0388 3.426 30.852 17.199 2555.140 3.486 76.502 3.053 0.56 261285. 0.3715
|
|
55.12 0.4157 0.7129 0.0651 0.0379 3.352 30.181 16.260 2499.533 3.410 72.322 2.950 0.56 261826. 0.3490
|
|
58.79 0.4435 0.7348 0.0611 0.0369 3.256 29.315 15.261 2427.857 3.312 67.881 2.851 0.56 262395. 0.3268
|
|
62.47 0.4712 0.7542 0.0569 0.0355 3.138 28.258 14.211 2340.315 3.193 63.209 2.754 0.56 262992. 0.3046
|
|
66.14 0.4989 0.7710 0.0525 0.0340 3.000 27.016 13.116 2237.425 3.052 58.339 2.659 0.56 263617. 0.2825
|
|
69.82 0.5266 0.7848 0.0480 0.0322 2.843 25.595 11.983 2119.753 2.892 53.303 2.564 0.56 264269. 0.2604
|
|
73.49 0.5543 0.7954 0.0433 0.0302 2.666 24.003 10.820 1987.864 2.712 48.127 2.469 0.56 264949. 0.2382
|
|
77.16 0.5820 0.8021 0.0385 0.0280 2.471 22.246 9.631 1842.345 2.513 42.839 2.371 0.56 265656. 0.2159
|
|
80.84 0.6098 0.8041 0.0337 0.0256 2.258 20.332 8.423 1683.842 2.297 37.465 2.269 0.57 266391. 0.1932
|
|
84.51 0.6375 0.7998 0.0288 0.0230 2.029 18.270 7.202 1513.094 2.064 32.033 2.159 0.57 267153. 0.1700
|
|
88.19 0.6652 0.7870 0.0239 0.0202 1.785 16.071 5.974 1330.969 1.816 26.570 2.036 0.57 267943. 0.1460
|
|
91.86 0.6929 0.7614 0.0190 0.0173 1.527 13.747 4.746 1138.519 1.553 21.108 1.891 0.57 268759. 0.1208
|
|
95.54 0.7206 0.7147 0.0141 0.0142 1.257 11.314 3.525 937.009 1.278 15.680 1.706 0.57 269604. 0.0940
|
|
99.21 0.7483 0.6289 0.0093 0.0111 0.976 8.790 2.321 727.969 0.993 10.323 1.446 0.57 270475. 0.0646
|
|
102.89 0.7761 0.4550 0.0046 0.0078 0.688 6.197 1.141 513.206 0.700 5.077 1.009 0.57 271373. 0.0316
|
|
106.56 0.8038 -0.0048 0.0000 0.0045 0.395 3.553 -0.007 294.226 0.401 -0.029 -0.010 0.57 272285. 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 0.0998 0.0348 4.582 36.099 32.559 3416.778 4.078 144.823 4.322 0.63 293106. 0.7236
|
|
4.20 0.0277 0.0770 0.0988 0.0355 4.687 36.926 32.241 3495.053 4.172 143.408 4.184 0.63 293322. 0.6970
|
|
8.39 0.0554 0.1489 0.0977 0.0363 4.791 37.749 31.882 3572.958 4.265 141.811 4.047 0.63 293561. 0.6705
|
|
12.59 0.0831 0.2159 0.0965 0.0371 4.894 38.554 31.478 3649.100 4.356 140.014 3.913 0.63 293824. 0.6440
|
|
16.78 0.1108 0.2782 0.0951 0.0379 4.991 39.324 31.025 3722.023 4.443 137.997 3.781 0.64 294112. 0.6178
|
|
20.98 0.1385 0.3359 0.0935 0.0385 5.083 40.043 30.517 3790.089 4.524 135.738 3.652 0.64 294427. 0.5919
|
|
25.18 0.1662 0.3893 0.0918 0.0392 5.165 40.693 29.950 3851.533 4.597 133.218 3.527 0.64 294769. 0.5663
|
|
29.37 0.1939 0.4386 0.0898 0.0397 5.236 41.252 29.321 3904.491 4.661 130.418 3.406 0.64 295141. 0.5411
|
|
33.57 0.2216 0.4841 0.0877 0.0401 5.293 41.701 28.624 3947.013 4.711 127.319 3.289 0.64 295541. 0.5163
|
|
37.77 0.2493 0.5260 0.0854 0.0405 5.333 42.019 27.857 3977.114 4.747 123.906 3.177 0.64 295972. 0.4919
|
|
41.96 0.2770 0.5646 0.0828 0.0406 5.354 42.185 27.015 3992.797 4.766 120.165 3.069 0.64 296433. 0.4680
|
|
46.16 0.3046 0.6000 0.0800 0.0406 5.353 42.178 26.098 3992.098 4.765 116.083 2.965 0.64 296925. 0.4444
|
|
50.35 0.3323 0.6326 0.0769 0.0404 5.328 41.977 25.102 3973.130 4.743 111.652 2.866 0.64 297449. 0.4212
|
|
54.55 0.3600 0.6624 0.0736 0.0400 5.276 41.565 24.026 3934.104 4.696 106.866 2.770 0.64 298005. 0.3983
|
|
58.75 0.3877 0.6897 0.0701 0.0394 5.194 40.923 22.869 3873.308 4.623 101.720 2.678 0.64 298592. 0.3757
|
|
62.94 0.4154 0.7145 0.0663 0.0385 5.081 40.031 21.629 3788.947 4.523 96.206 2.589 0.64 299211. 0.3533
|
|
67.14 0.4431 0.7368 0.0622 0.0374 4.935 38.879 20.310 3679.889 4.393 90.337 2.503 0.64 299862. 0.3310
|
|
71.34 0.4708 0.7567 0.0580 0.0361 4.756 37.469 18.919 3546.383 4.233 84.152 2.420 0.64 300545. 0.3088
|
|
75.53 0.4985 0.7741 0.0535 0.0345 4.545 35.808 17.468 3389.226 4.046 77.697 2.338 0.64 301259. 0.2866
|
|
79.73 0.5262 0.7886 0.0489 0.0326 4.304 33.907 15.965 3209.286 3.831 71.012 2.256 0.64 302005. 0.2645
|
|
83.92 0.5539 0.8001 0.0442 0.0306 4.033 31.775 14.419 3007.444 3.590 64.135 2.175 0.64 302782. 0.2423
|
|
88.12 0.5816 0.8078 0.0393 0.0283 3.734 29.420 12.838 2784.610 3.324 57.103 2.091 0.65 303590. 0.2198
|
|
92.32 0.6093 0.8110 0.0344 0.0259 3.409 26.855 11.230 2541.780 3.034 49.952 2.004 0.65 304430. 0.1970
|
|
96.51 0.6370 0.8083 0.0294 0.0232 3.058 24.090 9.604 2280.086 2.722 42.717 1.910 0.65 305300. 0.1737
|
|
100.71 0.6647 0.7974 0.0244 0.0204 2.683 21.140 7.967 2000.870 2.388 35.437 1.806 0.65 306202. 0.1496
|
|
104.91 0.6924 0.7740 0.0194 0.0173 2.287 18.022 6.330 1705.747 2.036 28.154 1.683 0.65 307135. 0.1242
|
|
109.10 0.7201 0.7303 0.0144 0.0142 1.873 14.756 4.701 1396.672 1.667 20.912 1.527 0.65 308099. 0.0971
|
|
113.30 0.7478 0.6477 0.0095 0.0109 1.443 11.368 3.094 1076.013 1.284 13.761 1.304 0.65 309093. 0.0673
|
|
117.49 0.7755 0.4754 0.0047 0.0076 1.001 7.888 1.519 746.581 0.891 6.757 0.923 0.65 310118. 0.0334
|
|
121.69 0.8032 -0.0082 0.0000 0.0042 0.551 4.339 -0.014 410.695 0.490 -0.062 -0.015 0.66 311159. 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 0.1010 0.0355 6.669 46.704 41.704 4973.071 5.277 185.501 3.804 0.71 329710. 0.7207
|
|
4.71 0.0277 0.0762 0.1001 0.0363 6.817 47.742 41.325 5083.616 5.394 183.815 3.687 0.71 329953. 0.6954
|
|
9.43 0.0553 0.1476 0.0990 0.0371 6.965 48.780 40.895 5194.104 5.511 181.900 3.571 0.71 330221. 0.6700
|
|
14.14 0.0830 0.2143 0.0978 0.0379 7.111 49.799 40.407 5302.612 5.626 179.729 3.456 0.71 330516. 0.6446
|
|
18.86 0.1106 0.2764 0.0965 0.0386 7.251 50.780 39.855 5407.037 5.737 177.274 3.343 0.71 330841. 0.6192
|
|
23.57 0.1383 0.3341 0.0950 0.0393 7.382 51.700 39.233 5505.048 5.841 174.507 3.232 0.71 331195. 0.5940
|
|
28.29 0.1660 0.3875 0.0933 0.0400 7.502 52.536 38.534 5594.082 5.936 171.399 3.124 0.71 331580. 0.5690
|
|
33.00 0.1936 0.4369 0.0914 0.0405 7.605 53.262 37.752 5671.350 6.017 167.923 3.019 0.72 331998. 0.5443
|
|
37.72 0.2213 0.4824 0.0893 0.0410 7.689 53.850 36.883 5733.944 6.084 164.055 2.918 0.72 332449. 0.5198
|
|
42.43 0.2489 0.5245 0.0870 0.0413 7.750 54.271 35.920 5778.859 6.132 159.774 2.819 0.72 332934. 0.4957
|
|
47.15 0.2766 0.5632 0.0844 0.0415 7.782 54.498 34.860 5803.025 6.157 155.059 2.725 0.72 333454. 0.4720
|
|
51.86 0.3043 0.5988 0.0816 0.0415 7.782 54.502 33.699 5803.404 6.158 149.895 2.634 0.72 334008. 0.4486
|
|
56.58 0.3319 0.6316 0.0785 0.0413 7.747 54.255 32.435 5777.053 6.130 144.269 2.547 0.72 334598. 0.4255
|
|
61.29 0.3596 0.6617 0.0752 0.0409 7.672 53.730 31.064 5721.236 6.070 138.174 2.463 0.72 335224. 0.4027
|
|
66.01 0.3872 0.6893 0.0716 0.0402 7.555 52.906 29.587 5633.425 5.977 131.604 2.382 0.72 335885. 0.3802
|
|
70.72 0.4149 0.7145 0.0678 0.0394 7.390 51.756 28.001 5511.037 5.847 124.549 2.305 0.72 336582. 0.3578
|
|
75.44 0.4426 0.7373 0.0637 0.0382 7.177 50.265 26.309 5352.261 5.679 117.022 2.230 0.72 337315. 0.3355
|
|
80.15 0.4702 0.7578 0.0594 0.0368 6.916 48.435 24.522 5157.350 5.472 109.072 2.157 0.72 338084. 0.3133
|
|
84.87 0.4979 0.7758 0.0548 0.0352 6.608 46.276 22.653 4927.462 5.228 100.759 2.085 0.72 338887. 0.2912
|
|
89.58 0.5255 0.7911 0.0502 0.0333 6.254 43.801 20.714 4663.906 4.949 92.137 2.014 0.72 339726. 0.2690
|
|
94.30 0.5532 0.8035 0.0453 0.0312 5.858 41.022 18.717 4367.995 4.635 83.255 1.944 0.72 340600. 0.2467
|
|
99.01 0.5809 0.8123 0.0404 0.0289 5.419 37.951 16.673 4041.095 4.288 74.161 1.871 0.73 341509. 0.2242
|
|
103.73 0.6085 0.8168 0.0353 0.0263 4.941 34.605 14.591 3684.726 3.910 64.903 1.796 0.73 342453. 0.2013
|
|
108.44 0.6362 0.8155 0.0302 0.0236 4.426 30.998 12.484 3300.667 3.502 55.527 1.715 0.73 343431. 0.1778
|
|
113.16 0.6638 0.8063 0.0251 0.0207 3.877 27.151 10.360 2891.042 3.067 46.083 1.625 0.73 344444. 0.1535
|
|
117.87 0.6915 0.7850 0.0199 0.0176 3.297 23.088 8.234 2458.477 2.609 36.626 1.519 0.73 345492. 0.1279
|
|
122.59 0.7192 0.7434 0.0148 0.0143 2.690 18.841 6.118 2006.232 2.129 27.214 1.383 0.73 346574. 0.1004
|
|
127.30 0.7468 0.6627 0.0098 0.0110 2.063 14.447 4.027 1538.345 1.632 17.913 1.187 0.73 347691. 0.0699
|
|
132.02 0.7745 0.4898 0.0048 0.0076 1.421 9.952 1.977 1059.687 1.124 8.795 0.846 0.74 348842. 0.0349
|
|
136.73 0.8022 -0.0093 0.0000 0.0041 0.770 5.395 -0.020 574.443 0.610 -0.087 -0.016 0.74 350009. 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 0.1023 0.0382 9.835 61.987 52.163 7333.817 7.003 232.023 3.226 0.79 366299. 0.6836
|
|
5.23 0.0276 0.0720 0.1015 0.0389 10.016 63.128 51.737 7468.777 7.132 230.124 3.142 0.79 366567. 0.6630
|
|
10.46 0.0552 0.1401 0.1005 0.0396 10.195 64.258 51.247 7602.425 7.260 227.946 3.057 0.79 366864. 0.6421
|
|
15.68 0.0828 0.2044 0.0994 0.0403 10.369 65.354 50.686 7732.166 7.384 225.453 2.973 0.79 367191. 0.6210
|
|
20.91 0.1104 0.2649 0.0982 0.0409 10.534 66.395 50.046 7855.268 7.501 222.607 2.890 0.79 367551. 0.5998
|
|
26.14 0.1380 0.3217 0.0967 0.0415 10.686 67.353 49.318 7968.700 7.610 219.367 2.807 0.79 367944. 0.5784
|
|
31.37 0.1656 0.3748 0.0951 0.0420 10.821 68.203 48.493 8069.221 7.706 215.696 2.726 0.79 368371. 0.5569
|
|
36.59 0.1932 0.4245 0.0933 0.0425 10.934 68.914 47.562 8153.358 7.786 211.554 2.646 0.79 368835. 0.5353
|
|
41.82 0.2208 0.4707 0.0912 0.0428 11.020 69.457 46.517 8217.535 7.847 206.908 2.568 0.80 369336. 0.5138
|
|
47.05 0.2484 0.5138 0.0889 0.0430 11.074 69.799 45.352 8258.004 7.886 201.725 2.491 0.80 369875. 0.4921
|
|
52.28 0.2760 0.5537 0.0864 0.0431 11.092 69.909 44.060 8271.010 7.898 195.979 2.416 0.80 370453. 0.4705
|
|
57.50 0.3036 0.5907 0.0836 0.0430 11.067 69.755 42.636 8252.813 7.881 189.647 2.343 0.80 371070. 0.4489
|
|
62.73 0.3312 0.6249 0.0806 0.0427 10.996 69.306 41.077 8199.690 7.830 182.711 2.272 0.80 371726. 0.4273
|
|
67.96 0.3588 0.6563 0.0772 0.0422 10.873 68.531 39.380 8108.003 7.743 175.162 2.203 0.80 372421. 0.4056
|
|
73.19 0.3864 0.6852 0.0736 0.0415 10.694 67.399 37.543 7974.149 7.615 166.993 2.135 0.80 373156. 0.3839
|
|
78.41 0.4140 0.7115 0.0697 0.0406 10.452 65.879 35.565 7794.271 7.443 158.192 2.070 0.80 373931. 0.3621
|
|
83.64 0.4416 0.7353 0.0656 0.0394 10.145 63.943 33.447 7565.170 7.224 148.770 2.005 0.80 374745. 0.3402
|
|
88.87 0.4692 0.7567 0.0612 0.0379 9.772 61.589 31.202 7286.676 6.958 138.788 1.942 0.80 375598. 0.3183
|
|
94.10 0.4968 0.7755 0.0566 0.0362 9.334 58.830 28.849 6960.241 6.647 128.320 1.880 0.80 376491. 0.2962
|
|
99.32 0.5244 0.7916 0.0518 0.0343 8.834 55.679 26.402 6587.455 6.291 117.438 1.818 0.80 377422. 0.2740
|
|
104.55 0.5520 0.8045 0.0468 0.0321 8.274 52.150 23.877 6169.923 5.892 106.205 1.755 0.81 378392. 0.2516
|
|
109.78 0.5796 0.8138 0.0417 0.0297 7.657 48.262 21.287 5709.939 5.453 94.684 1.691 0.81 379400. 0.2289
|
|
115.01 0.6072 0.8183 0.0366 0.0271 6.987 44.040 18.645 5210.417 4.976 82.935 1.623 0.81 380447. 0.2056
|
|
120.23 0.6348 0.8165 0.0313 0.0243 6.269 39.513 15.966 4674.799 4.464 71.017 1.549 0.81 381531. 0.1816
|
|
125.46 0.6624 0.8055 0.0260 0.0214 5.508 34.717 13.263 4107.486 3.922 58.992 1.465 0.81 382654. 0.1565
|
|
130.69 0.6900 0.7803 0.0207 0.0183 4.712 29.699 10.551 3513.726 3.355 46.929 1.362 0.81 383815. 0.1298
|
|
135.92 0.7176 0.7313 0.0154 0.0151 3.889 24.511 7.847 2899.953 2.769 34.904 1.227 0.81 385014. 0.1009
|
|
141.14 0.7452 0.6382 0.0101 0.0118 3.049 19.217 5.170 2273.609 2.171 22.997 1.031 0.82 386251. 0.0688
|
|
146.37 0.7728 0.4500 0.0050 0.0086 2.204 13.889 2.541 1643.245 1.569 11.302 0.701 0.82 387525. 0.0328
|
|
151.60 0.8004 -0.0073 0.0000 0.0053 1.363 8.588 -0.025 1016.038 0.970 -0.110 -0.011 0.82 388821. 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 0.1034 0.0449 15.375 88.095 63.801 11464.945 9.953 283.785 2.524 0.87 402879. 0.5915
|
|
5.75 0.0276 0.0624 0.1027 0.0455 15.580 89.272 63.354 11618.145 10.086 281.797 2.473 0.87 403172. 0.5776
|
|
11.51 0.0552 0.1222 0.1018 0.0460 15.776 90.395 62.834 11764.287 10.213 279.487 2.423 0.87 403497. 0.5634
|
|
17.26 0.0829 0.1795 0.1009 0.0466 15.957 91.431 62.231 11899.058 10.330 276.805 2.372 0.87 403855. 0.5490
|
|
23.02 0.1105 0.2343 0.0997 0.0470 16.116 92.345 61.532 12018.014 10.433 273.696 2.322 0.87 404250. 0.5344
|
|
28.77 0.1381 0.2867 0.0984 0.0474 16.249 93.102 60.725 12116.560 10.519 270.106 2.273 0.87 404681. 0.5197
|
|
34.53 0.1657 0.3368 0.0969 0.0477 16.347 93.667 59.797 12190.116 10.582 265.979 2.225 0.87 405152. 0.5048
|
|
40.28 0.1933 0.3845 0.0952 0.0479 16.406 94.007 58.737 12234.314 10.621 261.260 2.178 0.87 405664. 0.4896
|
|
46.03 0.2210 0.4301 0.0932 0.0479 16.421 94.089 57.532 12245.022 10.630 255.902 2.131 0.87 406216. 0.4742
|
|
51.79 0.2486 0.4734 0.0910 0.0478 16.385 93.884 56.173 12218.388 10.607 249.857 2.085 0.88 406811. 0.4585
|
|
57.54 0.2762 0.5146 0.0886 0.0475 16.295 93.365 54.651 12150.838 10.548 243.088 2.040 0.88 407450. 0.4425
|
|
63.30 0.3038 0.5537 0.0858 0.0471 16.144 92.504 52.959 12038.713 10.451 235.560 1.995 0.88 408131. 0.4260
|
|
69.05 0.3314 0.5905 0.0828 0.0465 15.930 91.275 51.090 11878.752 10.312 227.247 1.951 0.88 408857. 0.4091
|
|
74.81 0.3591 0.6252 0.0795 0.0457 15.647 89.656 49.041 11668.078 10.129 218.134 1.906 0.88 409626. 0.3917
|
|
80.56 0.3867 0.6576 0.0759 0.0446 15.292 87.622 46.810 11403.357 9.899 208.211 1.862 0.88 410439. 0.3737
|
|
86.31 0.4143 0.6876 0.0720 0.0434 14.860 85.144 44.394 11080.889 9.620 197.465 1.817 0.88 411296. 0.3552
|
|
92.07 0.4419 0.7153 0.0677 0.0419 14.345 82.197 41.795 10697.420 9.287 185.906 1.772 0.88 412197. 0.3361
|
|
97.82 0.4695 0.7404 0.0633 0.0401 13.750 78.784 39.030 10253.156 8.901 173.607 1.727 0.88 413141. 0.3165
|
|
103.58 0.4972 0.7627 0.0585 0.0382 13.081 74.950 36.120 9754.251 8.468 160.663 1.680 0.88 414127. 0.2962
|
|
109.33 0.5248 0.7811 0.0536 0.0360 12.349 70.755 33.085 9208.287 7.994 147.164 1.630 0.88 415157. 0.2750
|
|
115.09 0.5524 0.7951 0.0485 0.0337 11.557 66.221 29.945 8618.224 7.482 133.193 1.576 0.89 416228. 0.2530
|
|
120.84 0.5800 0.8030 0.0433 0.0313 10.719 61.420 26.714 7993.418 6.939 118.824 1.516 0.89 417342. 0.2299
|
|
126.59 0.6076 0.8025 0.0379 0.0287 9.847 56.423 23.410 7343.043 6.375 104.130 1.446 0.89 418497. 0.2053
|
|
132.35 0.6353 0.7928 0.0325 0.0260 8.928 51.154 20.055 6657.324 5.779 89.206 1.366 0.89 419694. 0.1795
|
|
138.10 0.6629 0.7699 0.0270 0.0233 7.972 45.678 16.668 5944.609 5.161 74.137 1.272 0.89 420932. 0.1523
|
|
143.86 0.6905 0.7276 0.0215 0.0204 6.994 40.077 13.267 5215.678 4.528 59.012 1.154 0.89 422212. 0.1233
|
|
149.61 0.7181 0.6557 0.0160 0.0175 6.010 34.434 9.877 4481.315 3.890 43.933 1.000 0.90 423534. 0.0922
|
|
155.36 0.7458 0.5369 0.0106 0.0147 5.033 28.840 6.523 3753.371 3.258 29.016 0.788 0.90 424897. 0.0591
|
|
161.12 0.7734 0.3406 0.0052 0.0119 4.083 23.393 3.237 3044.428 2.643 14.399 0.482 0.90 426300. 0.0255
|
|
166.87 0.8010 0.0056 0.0001 0.0092 3.165 18.138 0.040 2360.469 2.049 0.177 0.008 0.90 427737. 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 0.1018 0.0519 23.100 121.328 74.719 17225.434 13.708 332.352 1.967 0.95 439562. 0.4990
|
|
6.43 0.0283 0.0545 0.1012 0.0526 23.414 122.978 74.306 17459.686 13.894 330.511 1.930 0.95 439882. 0.4882
|
|
12.87 0.0566 0.1068 0.1005 0.0533 23.722 124.596 73.818 17689.385 14.077 328.345 1.893 0.95 440237. 0.4771
|
|
19.30 0.0849 0.1570 0.0998 0.0540 24.014 126.131 73.244 17907.293 14.250 325.790 1.855 0.95 440630. 0.4658
|
|
25.74 0.1132 0.2051 0.0988 0.0546 24.279 127.524 72.566 18105.150 14.408 322.775 1.818 0.95 441065. 0.4543
|
|
32.17 0.1416 0.2513 0.0977 0.0551 24.505 128.710 71.767 18273.432 14.542 319.222 1.781 0.95 441542. 0.4427
|
|
38.61 0.1699 0.2955 0.0965 0.0555 24.677 129.612 70.829 18401.621 14.644 315.045 1.746 0.95 442065. 0.4311
|
|
45.04 0.1982 0.3380 0.0950 0.0557 24.780 130.154 69.730 18478.572 14.705 310.158 1.712 0.95 442635. 0.4193
|
|
51.48 0.2265 0.3789 0.0932 0.0557 24.800 130.256 68.451 18493.035 14.716 304.471 1.679 0.95 443254. 0.4075
|
|
57.91 0.2548 0.4184 0.0912 0.0556 24.721 129.844 66.974 18434.527 14.670 297.899 1.648 0.96 443922. 0.3956
|
|
64.35 0.2831 0.4566 0.0889 0.0551 24.533 128.855 65.280 18294.047 14.558 290.365 1.619 0.96 444641. 0.3837
|
|
70.78 0.3114 0.4936 0.0863 0.0544 24.225 127.240 63.355 18064.824 14.376 281.802 1.591 0.96 445412. 0.3715
|
|
77.22 0.3397 0.5295 0.0833 0.0535 23.793 124.970 61.187 17742.467 14.119 272.159 1.564 0.96 446234. 0.3590
|
|
83.65 0.3681 0.5642 0.0800 0.0522 23.233 122.027 58.768 17324.742 13.787 261.401 1.539 0.96 447108. 0.3460
|
|
90.08 0.3964 0.5977 0.0764 0.0507 22.542 118.400 56.092 16809.695 13.377 249.496 1.514 0.96 448034. 0.3326
|
|
96.52 0.4247 0.6298 0.0724 0.0488 21.722 114.092 53.155 16198.079 12.890 236.433 1.488 0.96 449011. 0.3184
|
|
102.95 0.4530 0.6602 0.0681 0.0467 20.776 109.122 49.966 15492.526 12.329 222.247 1.463 0.96 450039. 0.3034
|
|
109.39 0.4813 0.6888 0.0634 0.0443 19.714 103.545 46.551 14700.659 11.698 207.059 1.436 0.96 451117. 0.2875
|
|
115.82 0.5096 0.7150 0.0585 0.0417 18.548 97.422 42.942 13831.415 11.007 191.007 1.408 0.96 452244. 0.2707
|
|
122.26 0.5379 0.7367 0.0533 0.0389 17.331 91.028 39.164 12923.612 10.284 174.202 1.375 0.97 453420. 0.2524
|
|
128.69 0.5662 0.7524 0.0480 0.0361 16.076 84.435 35.245 11987.564 9.539 156.768 1.334 0.97 454645. 0.2323
|
|
135.13 0.5946 0.7593 0.0425 0.0333 14.809 77.784 31.209 11043.363 8.788 138.817 1.282 0.97 455917. 0.2101
|
|
141.56 0.6229 0.7430 0.0368 0.0309 13.747 72.204 27.057 10251.056 8.158 120.348 1.197 0.97 457236. 0.1827
|
|
148.00 0.6512 0.7100 0.0311 0.0285 12.700 66.706 22.848 9470.498 7.536 101.629 1.094 0.97 458603. 0.1535
|
|
154.43 0.6795 0.6579 0.0254 0.0262 11.657 61.225 18.624 8692.390 6.917 82.842 0.972 0.97 460018. 0.1230
|
|
160.87 0.7078 0.5819 0.0196 0.0239 10.635 55.859 14.427 7930.568 6.311 64.171 0.825 0.98 461479. 0.0919
|
|
167.30 0.7361 0.4762 0.0140 0.0217 9.653 50.701 10.304 7198.215 5.728 45.832 0.649 0.98 462988. 0.0611
|
|
173.74 0.7644 0.3347 0.0086 0.0196 8.725 45.826 6.304 6506.167 5.177 28.040 0.439 0.98 464546. 0.0324
|
|
180.17 0.7927 0.1507 0.0034 0.0177 7.857 41.268 2.464 5858.929 4.662 10.961 0.191 0.98 466164. 0.0088
|
|
186.60 0.8211
|
|
|
|
|
|
|