427 lines
76 KiB
Plaintext
427 lines
76 KiB
Plaintext
21x13WE (21x13WE.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 0.1000 0.0396 0.013 0.820 0.620 9.706 0.093 2.756 28.959 0.08 44125. 0.6370
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0.53 0.0264 0.0649 0.0986 0.0402 0.013 0.832 0.611 9.848 0.094 2.719 28.159 0.08 44157. 0.6152
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1.05 0.0529 0.1261 0.0972 0.0407 0.013 0.844 0.602 9.983 0.095 2.679 27.361 0.08 44193. 0.5933
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1.58 0.0793 0.1837 0.0956 0.0413 0.014 0.855 0.592 10.111 0.097 2.634 26.570 0.08 44232. 0.5713
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2.10 0.1057 0.2377 0.0938 0.0417 0.014 0.864 0.581 10.226 0.098 2.586 25.788 0.08 44274. 0.5494
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2.63 0.1322 0.2882 0.0919 0.0421 0.014 0.873 0.570 10.327 0.099 2.534 25.017 0.08 44319. 0.5276
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3.15 0.1586 0.3354 0.0898 0.0425 0.014 0.880 0.557 10.411 0.099 2.477 24.259 0.08 44368. 0.5058
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3.68 0.1850 0.3793 0.0876 0.0427 0.014 0.885 0.543 10.473 0.100 2.415 23.514 0.08 44421. 0.4841
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4.20 0.2114 0.4200 0.0852 0.0429 0.014 0.888 0.528 10.511 0.100 2.349 22.784 0.08 44478. 0.4626
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4.73 0.2379 0.4577 0.0826 0.0429 0.014 0.889 0.512 10.522 0.100 2.277 22.068 0.08 44538. 0.4412
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5.26 0.2643 0.4923 0.0798 0.0428 0.014 0.888 0.495 10.501 0.100 2.200 21.366 0.08 44603. 0.4199
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5.78 0.2907 0.5241 0.0768 0.0426 0.014 0.883 0.476 10.445 0.100 2.118 20.678 0.08 44672. 0.3987
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6.31 0.3172 0.5531 0.0737 0.0422 0.014 0.875 0.456 10.352 0.099 2.030 20.001 0.08 44745. 0.3776
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6.83 0.3436 0.5792 0.0703 0.0417 0.014 0.863 0.435 10.216 0.098 1.937 19.334 0.08 44822. 0.3565
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7.36 0.3700 0.6024 0.0667 0.0409 0.013 0.848 0.413 10.036 0.096 1.838 18.674 0.08 44903. 0.3354
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7.88 0.3965 0.6227 0.0629 0.0400 0.013 0.829 0.390 9.810 0.094 1.733 18.016 0.08 44989. 0.3142
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8.41 0.4229 0.6399 0.0589 0.0389 0.013 0.806 0.365 9.539 0.091 1.624 17.357 0.08 45079. 0.2930
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8.94 0.4493 0.6538 0.0548 0.0376 0.012 0.780 0.339 9.225 0.088 1.510 16.691 0.08 45173. 0.2717
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9.46 0.4758 0.6640 0.0505 0.0362 0.012 0.750 0.313 8.869 0.085 1.392 16.010 0.08 45272. 0.2503
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9.99 0.5022 0.6701 0.0461 0.0346 0.011 0.716 0.286 8.472 0.081 1.272 15.306 0.08 45374. 0.2287
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10.51 0.5286 0.6714 0.0416 0.0328 0.011 0.679 0.258 8.036 0.077 1.148 14.569 0.08 45481. 0.2068
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11.04 0.5550 0.6670 0.0371 0.0309 0.010 0.639 0.230 7.563 0.072 1.022 13.785 0.08 45592. 0.1847
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11.56 0.5815 0.6558 0.0325 0.0288 0.009 0.596 0.201 7.053 0.067 0.895 12.936 0.08 45708. 0.1621
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12.09 0.6079 0.6359 0.0278 0.0266 0.009 0.550 0.172 6.509 0.062 0.766 11.998 0.08 45828. 0.1391
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12.61 0.6343 0.6048 0.0231 0.0242 0.008 0.501 0.143 5.932 0.057 0.636 10.936 0.08 45952. 0.1156
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13.14 0.6608 0.5585 0.0184 0.0217 0.007 0.450 0.114 5.327 0.051 0.506 9.696 0.09 46080. 0.0914
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13.67 0.6872 0.4910 0.0137 0.0192 0.006 0.397 0.085 4.695 0.045 0.377 8.196 0.09 46213. 0.0667
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14.19 0.7136 0.3917 0.0090 0.0165 0.005 0.341 0.056 4.040 0.039 0.249 6.296 0.09 46350. 0.0417
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14.72 0.7401 0.2417 0.0045 0.0137 0.005 0.285 0.028 3.367 0.032 0.124 3.746 0.09 46491. 0.0175
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15.24 0.7665 0.0020 0.0000 0.0109 0.004 0.227 0.000 2.681 0.026 0.001 0.030 0.09 46635. 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 0.1004 0.0371 0.098 3.076 2.489 72.795 0.348 11.069 15.506 0.17 88249. 0.6834
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1.06 0.0266 0.0697 0.0990 0.0377 0.099 3.128 2.455 74.007 0.353 10.921 15.048 0.17 88314. 0.6588
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2.11 0.0531 0.1351 0.0976 0.0383 0.101 3.177 2.419 75.174 0.359 10.759 14.594 0.17 88385. 0.6342
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3.17 0.0797 0.1965 0.0960 0.0389 0.102 3.223 2.379 76.273 0.364 10.582 14.147 0.17 88463. 0.6097
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4.22 0.1062 0.2538 0.0942 0.0394 0.104 3.266 2.335 77.281 0.369 10.388 13.707 0.17 88548. 0.5853
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5.28 0.1328 0.3073 0.0923 0.0399 0.105 3.304 2.288 78.173 0.373 10.177 13.276 0.17 88639. 0.5611
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6.34 0.1593 0.3571 0.0902 0.0403 0.106 3.335 2.237 78.922 0.377 9.949 12.854 0.17 88738. 0.5371
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7.39 0.1859 0.4032 0.0880 0.0405 0.107 3.360 2.181 79.502 0.380 9.701 12.443 0.17 88845. 0.5134
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8.45 0.2124 0.4460 0.0855 0.0407 0.107 3.376 2.121 79.882 0.381 9.433 12.042 0.17 88959. 0.4900
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9.50 0.2390 0.4855 0.0829 0.0408 0.107 3.382 2.056 80.035 0.382 9.145 11.652 0.17 89081. 0.4668
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10.56 0.2655 0.5219 0.0801 0.0408 0.107 3.378 1.986 79.930 0.382 8.836 11.272 0.17 89211. 0.4439
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11.62 0.2921 0.5552 0.0771 0.0406 0.107 3.361 1.912 79.539 0.380 8.504 10.903 0.17 89350. 0.4212
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12.67 0.3186 0.5857 0.0739 0.0402 0.106 3.332 1.832 78.833 0.376 8.151 10.543 0.17 89497. 0.3988
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13.73 0.3452 0.6134 0.0705 0.0397 0.104 3.287 1.748 77.779 0.371 7.774 10.191 0.17 89653. 0.3764
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14.78 0.3717 0.6382 0.0669 0.0389 0.102 3.227 1.658 76.352 0.365 7.373 9.847 0.17 89817. 0.3542
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15.84 0.3983 0.6603 0.0630 0.0380 0.100 3.150 1.563 74.543 0.356 6.951 9.508 0.17 89990. 0.3321
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16.90 0.4248 0.6794 0.0590 0.0369 0.097 3.058 1.463 72.360 0.345 6.509 9.172 0.17 90171. 0.3100
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17.95 0.4514 0.6955 0.0549 0.0356 0.094 2.950 1.360 69.810 0.333 6.050 8.837 0.17 90361. 0.2880
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19.01 0.4779 0.7082 0.0506 0.0341 0.090 2.827 1.254 66.904 0.319 5.576 8.498 0.17 90559. 0.2659
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20.06 0.5045 0.7171 0.0462 0.0325 0.085 2.690 1.144 63.652 0.304 5.089 8.153 0.17 90767. 0.2437
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21.12 0.5310 0.7218 0.0416 0.0306 0.081 2.538 1.032 60.062 0.287 4.592 7.795 0.17 90982. 0.2213
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22.18 0.5576 0.7213 0.0370 0.0286 0.075 2.373 0.918 56.147 0.268 4.085 7.419 0.17 91207. 0.1987
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23.23 0.5841 0.7145 0.0324 0.0265 0.070 2.194 0.803 51.921 0.248 3.572 7.015 0.17 91440. 0.1756
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24.29 0.6107 0.6996 0.0277 0.0242 0.064 2.003 0.687 47.398 0.226 3.054 6.570 0.17 91681. 0.1521
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25.34 0.6372 0.6739 0.0230 0.0217 0.057 1.800 0.570 42.597 0.203 2.534 6.065 0.17 91931. 0.1279
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26.40 0.6638 0.6329 0.0183 0.0191 0.050 1.587 0.453 37.542 0.179 2.013 5.469 0.17 92190. 0.1028
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27.46 0.6903 0.5693 0.0136 0.0165 0.043 1.363 0.336 32.261 0.154 1.496 4.729 0.17 92458. 0.0766
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28.51 0.7169 0.4687 0.0089 0.0137 0.036 1.132 0.221 26.787 0.128 0.985 3.750 0.17 92734. 0.0493
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29.57 0.7434 0.3018 0.0044 0.0108 0.028 0.894 0.109 21.160 0.101 0.483 2.328 0.17 93018. 0.0214
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30.62 0.7700 -0.0065 -0.0001 0.0079 0.021 0.651 -0.002 15.410 0.074 -0.007 -0.048 0.17 93308. 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 0.1008 0.0362 0.321 6.745 5.624 239.410 0.762 25.018 10.656 0.25 132369. 0.7061
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1.59 0.0266 0.0718 0.0995 0.0368 0.327 6.864 5.550 243.634 0.776 24.686 10.332 0.25 132467. 0.6801
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3.17 0.0532 0.1392 0.0980 0.0374 0.332 6.979 5.468 247.711 0.788 24.323 10.013 0.25 132574. 0.6542
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4.76 0.0797 0.2023 0.0964 0.0380 0.337 7.088 5.379 251.561 0.801 23.925 9.698 0.25 132691. 0.6285
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6.34 0.1063 0.2611 0.0947 0.0386 0.342 7.187 5.281 255.104 0.812 23.490 9.390 0.25 132818. 0.6029
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7.93 0.1329 0.3159 0.0928 0.0390 0.346 7.276 5.175 258.254 0.822 23.017 9.088 0.25 132956. 0.5776
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9.51 0.1595 0.3668 0.0907 0.0394 0.350 7.351 5.059 260.919 0.831 22.502 8.794 0.25 133105. 0.5527
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11.10 0.1861 0.4140 0.0884 0.0397 0.353 7.410 4.933 263.005 0.837 21.944 8.508 0.25 133265. 0.5280
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12.69 0.2126 0.4577 0.0860 0.0400 0.355 7.450 4.798 264.411 0.842 21.341 8.230 0.25 133437. 0.5037
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14.27 0.2392 0.4981 0.0834 0.0401 0.355 7.467 4.652 265.037 0.844 20.690 7.961 0.25 133621. 0.4797
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15.86 0.2658 0.5352 0.0806 0.0400 0.355 7.460 4.495 264.782 0.843 19.992 7.699 0.25 133817. 0.4561
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17.44 0.2924 0.5694 0.0776 0.0398 0.353 7.425 4.326 263.544 0.839 19.243 7.446 0.25 134026. 0.4327
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19.03 0.3190 0.6006 0.0743 0.0395 0.350 7.360 4.146 261.221 0.831 18.444 7.200 0.25 134247. 0.4096
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20.61 0.3455 0.6291 0.0709 0.0389 0.346 7.261 3.955 257.705 0.820 17.591 6.961 0.25 134481. 0.3868
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22.20 0.3721 0.6548 0.0672 0.0382 0.339 7.125 3.751 252.900 0.805 16.685 6.727 0.25 134728. 0.3641
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23.79 0.3987 0.6777 0.0634 0.0373 0.331 6.953 3.536 246.779 0.786 15.729 6.499 0.25 134988. 0.3415
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25.37 0.4253 0.6980 0.0594 0.0362 0.321 6.744 3.311 239.359 0.762 14.729 6.275 0.25 135260. 0.3190
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26.96 0.4519 0.7152 0.0552 0.0349 0.309 6.499 3.078 230.668 0.734 13.690 6.052 0.25 135546. 0.2967
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28.54 0.4784 0.7294 0.0509 0.0334 0.296 6.219 2.837 220.736 0.703 12.617 5.829 0.25 135844. 0.2743
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30.13 0.5050 0.7400 0.0464 0.0317 0.281 5.905 2.589 209.595 0.667 11.516 5.603 0.25 136156. 0.2519
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31.72 0.5316 0.7467 0.0419 0.0298 0.265 5.558 2.336 197.279 0.628 10.389 5.370 0.25 136480. 0.2293
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33.30 0.5582 0.7486 0.0373 0.0278 0.247 5.179 2.078 183.825 0.585 9.243 5.127 0.25 136817. 0.2065
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34.89 0.5848 0.7446 0.0326 0.0256 0.227 4.769 1.817 169.279 0.539 8.082 4.868 0.25 137168. 0.1834
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36.47 0.6113 0.7331 0.0279 0.0232 0.206 4.330 1.554 153.695 0.489 6.910 4.585 0.25 137531. 0.1597
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38.06 0.6379 0.7113 0.0231 0.0207 0.184 3.864 1.289 137.140 0.437 5.733 4.263 0.25 137907. 0.1352
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39.64 0.6645 0.6748 0.0184 0.0181 0.161 3.372 1.025 119.693 0.381 4.558 3.883 0.26 138296. 0.1098
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41.23 0.6911 0.6156 0.0137 0.0153 0.136 2.858 0.762 101.453 0.323 3.389 3.406 0.26 138698. 0.0831
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42.82 0.7177 0.5181 0.0090 0.0125 0.111 2.325 0.502 82.539 0.263 2.234 2.760 0.26 139113. 0.0547
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44.40 0.7443 0.3464 0.0044 0.0095 0.085 1.777 0.247 63.090 0.201 1.101 1.779 0.26 139541. 0.0247
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45.99 0.7708 -0.0029 0.0000 0.0065 0.058 1.217 -0.001 43.203 0.138 -0.006 -0.014 0.26 139975. 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 0.1014 0.0358 0.753 11.860 10.057 561.277 1.340 44.733 8.127 0.33 176484. 0.7201
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2.12 0.0266 0.0730 0.1001 0.0364 0.766 12.077 9.925 571.540 1.364 44.148 7.877 0.33 176615. 0.6934
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4.23 0.0532 0.1415 0.0986 0.0371 0.780 12.287 9.781 581.457 1.388 43.506 7.630 0.33 176758. 0.6667
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6.35 0.0798 0.2055 0.0970 0.0377 0.792 12.485 9.623 590.839 1.411 42.801 7.387 0.33 176915. 0.6403
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8.46 0.1064 0.2652 0.0953 0.0382 0.804 12.668 9.449 599.489 1.431 42.031 7.149 0.33 177084. 0.6141
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10.58 0.1329 0.3207 0.0934 0.0387 0.814 12.830 9.260 607.200 1.450 41.191 6.917 0.33 177269. 0.5882
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12.69 0.1595 0.3723 0.0913 0.0391 0.823 12.969 9.055 613.749 1.465 40.276 6.692 0.33 177467. 0.5626
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14.81 0.1861 0.4201 0.0891 0.0395 0.830 13.078 8.832 618.907 1.478 39.283 6.472 0.33 177681. 0.5374
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16.92 0.2127 0.4644 0.0866 0.0397 0.835 13.152 8.590 622.433 1.486 38.209 6.260 0.33 177911. 0.5126
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19.04 0.2393 0.5052 0.0840 0.0398 0.837 13.187 8.330 624.084 1.490 37.051 6.054 0.33 178157. 0.4882
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21.15 0.2659 0.5429 0.0812 0.0398 0.836 13.177 8.050 623.613 1.489 35.805 5.855 0.33 178419. 0.4641
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23.27 0.2925 0.5775 0.0781 0.0396 0.832 13.117 7.749 620.775 1.482 34.469 5.662 0.33 178698. 0.4404
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25.38 0.3191 0.6093 0.0749 0.0392 0.825 13.002 7.428 615.324 1.469 33.040 5.475 0.33 178993. 0.4170
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27.50 0.3457 0.6382 0.0715 0.0387 0.814 12.826 7.085 606.996 1.449 31.516 5.295 0.34 179306. 0.3938
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29.61 0.3723 0.6645 0.0678 0.0380 0.799 12.585 6.721 595.561 1.422 29.896 5.119 0.34 179636. 0.3708
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31.73 0.3988 0.6881 0.0639 0.0370 0.779 12.276 6.337 580.942 1.387 28.186 4.947 0.34 179983. 0.3480
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33.84 0.4254 0.7091 0.0598 0.0359 0.755 11.900 5.934 563.176 1.344 26.396 4.779 0.34 180347. 0.3253
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35.96 0.4520 0.7272 0.0556 0.0346 0.727 11.460 5.516 542.326 1.295 24.536 4.613 0.34 180728. 0.3027
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38.07 0.4786 0.7424 0.0513 0.0331 0.695 10.955 5.084 518.464 1.238 22.615 4.448 0.34 181127. 0.2802
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40.19 0.5052 0.7542 0.0468 0.0313 0.659 10.389 4.641 491.663 1.174 20.641 4.281 0.34 181542. 0.2577
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42.30 0.5318 0.7623 0.0422 0.0295 0.620 9.762 4.187 462.002 1.103 18.623 4.110 0.34 181976. 0.2350
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44.42 0.5584 0.7659 0.0376 0.0274 0.576 9.077 3.725 429.574 1.026 16.569 3.933 0.34 182426. 0.2121
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46.53 0.5850 0.7640 0.0328 0.0252 0.529 8.336 3.257 394.486 0.942 14.488 3.745 0.34 182893. 0.1889
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48.65 0.6116 0.7550 0.0281 0.0228 0.479 7.541 2.785 356.870 0.852 12.389 3.540 0.34 183378. 0.1651
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50.76 0.6382 0.7362 0.0233 0.0202 0.425 6.696 2.311 316.885 0.757 10.280 3.308 0.34 183880. 0.1405
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52.88 0.6647 0.7032 0.0185 0.0175 0.368 5.805 1.837 274.729 0.656 8.173 3.034 0.34 184399. 0.1149
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54.99 0.6913 0.6479 0.0138 0.0147 0.309 4.874 1.367 230.641 0.551 6.079 2.688 0.34 184936. 0.0878
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57.11 0.7179 0.5537 0.0091 0.0118 0.248 3.907 0.902 184.914 0.441 4.010 2.212 0.34 185490. 0.0587
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59.22 0.7445 0.3804 0.0045 0.0088 0.185 2.914 0.445 137.887 0.329 1.981 1.465 0.34 186060. 0.0273
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61.34 0.7711 -0.0005 0.0000 0.0057 0.120 1.897 0.000 89.780 0.214 -0.002 -0.002 0.34 186638. 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 0.1022 0.0357 1.467 18.489 15.829 1093.707 2.089 70.406 6.564 0.42 220592. 0.7297
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2.65 0.0266 0.0738 0.1008 0.0364 1.494 18.836 15.625 1114.238 2.128 69.501 6.361 0.42 220756. 0.7025
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5.29 0.0532 0.1429 0.0994 0.0370 1.521 19.171 15.401 1134.095 2.166 68.505 6.160 0.42 220936. 0.6754
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7.94 0.0798 0.2074 0.0978 0.0376 1.546 19.489 15.155 1152.900 2.202 67.412 5.962 0.42 221132. 0.6486
|
|
10.58 0.1064 0.2676 0.0961 0.0382 1.569 19.783 14.886 1170.261 2.235 66.213 5.770 0.42 221345. 0.6220
|
|
13.23 0.1330 0.3236 0.0942 0.0387 1.590 20.045 14.592 1185.763 2.265 64.903 5.581 0.42 221575. 0.5957
|
|
15.87 0.1596 0.3756 0.0921 0.0391 1.608 20.268 14.270 1198.961 2.290 63.475 5.399 0.42 221824. 0.5698
|
|
18.52 0.1862 0.4238 0.0898 0.0395 1.622 20.444 13.922 1209.391 2.310 61.923 5.221 0.42 222093. 0.5443
|
|
21.16 0.2128 0.4684 0.0874 0.0397 1.631 20.566 13.544 1216.580 2.323 60.242 5.049 0.42 222381. 0.5192
|
|
23.81 0.2394 0.5096 0.0848 0.0398 1.636 20.624 13.135 1220.037 2.330 58.426 4.883 0.42 222689. 0.4945
|
|
26.45 0.2660 0.5476 0.0819 0.0398 1.635 20.611 12.696 1219.273 2.329 56.470 4.723 0.42 223017. 0.4702
|
|
29.10 0.2926 0.5826 0.0789 0.0396 1.628 20.519 12.224 1213.797 2.318 54.371 4.568 0.42 223366. 0.4462
|
|
31.74 0.3192 0.6148 0.0756 0.0393 1.613 20.338 11.719 1203.119 2.298 52.125 4.418 0.42 223737. 0.4226
|
|
34.39 0.3458 0.6441 0.0722 0.0387 1.591 20.061 11.180 1186.721 2.266 49.727 4.273 0.42 224129. 0.3992
|
|
37.03 0.3724 0.6709 0.0685 0.0380 1.561 19.679 10.606 1164.131 2.223 47.176 4.132 0.42 224542. 0.3760
|
|
39.68 0.3990 0.6950 0.0645 0.0371 1.522 19.190 10.000 1135.187 2.168 44.481 3.996 0.42 224977. 0.3531
|
|
42.32 0.4256 0.7165 0.0604 0.0359 1.475 18.594 9.366 1099.952 2.101 41.659 3.862 0.42 225433. 0.3302
|
|
44.97 0.4522 0.7354 0.0562 0.0346 1.420 17.894 8.706 1058.551 2.022 38.724 3.730 0.42 225910. 0.3075
|
|
47.61 0.4788 0.7513 0.0518 0.0330 1.356 17.093 8.024 1011.124 1.931 35.692 3.600 0.42 226410. 0.2849
|
|
50.26 0.5054 0.7641 0.0473 0.0313 1.284 16.191 7.324 957.815 1.829 32.576 3.468 0.42 226930. 0.2622
|
|
52.90 0.5320 0.7733 0.0426 0.0293 1.205 15.193 6.607 898.783 1.717 29.389 3.334 0.42 227472. 0.2395
|
|
55.55 0.5586 0.7782 0.0379 0.0272 1.119 14.102 5.878 834.209 1.593 26.144 3.196 0.42 228036. 0.2165
|
|
58.19 0.5852 0.7779 0.0332 0.0249 1.025 12.920 5.138 764.308 1.460 22.856 3.049 0.42 228621. 0.1931
|
|
60.84 0.6118 0.7708 0.0283 0.0225 0.924 11.653 4.393 689.343 1.317 19.538 2.890 0.42 229228. 0.1692
|
|
63.48 0.6384 0.7544 0.0235 0.0199 0.818 10.306 3.643 609.635 1.164 16.205 2.711 0.43 229856. 0.1446
|
|
66.13 0.6650 0.7242 0.0187 0.0172 0.705 8.885 2.895 525.580 1.004 12.875 2.498 0.43 230506. 0.1187
|
|
68.77 0.6916 0.6719 0.0139 0.0143 0.587 7.398 2.151 437.664 0.836 9.565 2.229 0.43 231178. 0.0913
|
|
71.42 0.7182 0.5802 0.0091 0.0113 0.465 5.857 1.416 346.473 0.662 6.296 1.853 0.43 231871. 0.0616
|
|
74.06 0.7449 0.4049 0.0045 0.0082 0.339 4.272 0.695 252.696 0.483 3.090 1.247 0.43 232584. 0.0290
|
|
76.71 0.7715 -0.0098 -0.0001 0.0051 0.210 2.649 -0.010 156.702 0.299 -0.045 -0.029 0.43 233304. 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 0.1031 0.0358 2.545 26.733 22.999 1897.708 3.020 102.299 5.497 0.50 264691. 0.7366
|
|
3.17 0.0266 0.0740 0.1018 0.0365 2.594 27.245 22.711 1934.066 3.078 101.017 5.326 0.50 264888. 0.7092
|
|
6.34 0.0531 0.1434 0.1004 0.0372 2.641 27.741 22.392 1969.268 3.134 99.601 5.158 0.50 265104. 0.6819
|
|
9.51 0.0797 0.2082 0.0988 0.0378 2.686 28.211 22.042 2002.636 3.187 98.043 4.992 0.50 265339. 0.6549
|
|
12.68 0.1063 0.2686 0.0971 0.0384 2.727 28.646 21.657 2033.487 3.236 96.331 4.831 0.50 265595. 0.6281
|
|
15.85 0.1329 0.3248 0.0952 0.0389 2.764 29.034 21.236 2061.070 3.280 94.456 4.673 0.50 265872. 0.6017
|
|
19.03 0.1594 0.3770 0.0931 0.0394 2.796 29.366 20.775 2084.608 3.318 92.408 4.520 0.50 266171. 0.5757
|
|
22.20 0.1860 0.4254 0.0909 0.0397 2.821 29.629 20.274 2103.278 3.347 90.178 4.372 0.50 266494. 0.5500
|
|
25.37 0.2126 0.4702 0.0884 0.0400 2.838 29.812 19.730 2116.245 3.368 87.758 4.229 0.50 266840. 0.5248
|
|
28.54 0.2392 0.5117 0.0858 0.0401 2.847 29.902 19.141 2122.644 3.378 85.139 4.090 0.50 267210. 0.5000
|
|
31.71 0.2657 0.5500 0.0829 0.0401 2.845 29.887 18.506 2121.612 3.377 82.316 3.956 0.50 267604. 0.4756
|
|
34.88 0.2923 0.5852 0.0799 0.0399 2.833 29.756 17.824 2112.290 3.362 79.281 3.827 0.50 268024. 0.4515
|
|
38.05 0.3189 0.6177 0.0766 0.0396 2.808 29.496 17.093 2093.814 3.332 76.031 3.703 0.50 268468. 0.4277
|
|
41.22 0.3455 0.6474 0.0731 0.0390 2.770 29.094 16.312 2065.283 3.287 72.557 3.582 0.50 268939. 0.4043
|
|
44.39 0.3720 0.6745 0.0694 0.0383 2.717 28.538 15.481 2025.854 3.224 68.857 3.466 0.50 269435. 0.3810
|
|
47.56 0.3986 0.6991 0.0654 0.0373 2.649 27.825 14.601 1975.198 3.144 64.945 3.353 0.50 269956. 0.3580
|
|
50.73 0.4252 0.7212 0.0613 0.0361 2.566 26.954 13.679 1913.418 3.045 60.844 3.243 0.50 270504. 0.3351
|
|
53.90 0.4518 0.7406 0.0570 0.0348 2.468 25.930 12.719 1840.730 2.930 56.576 3.134 0.50 271077. 0.3123
|
|
57.08 0.4783 0.7573 0.0526 0.0332 2.357 24.756 11.727 1757.379 2.797 52.163 3.027 0.51 271676. 0.2896
|
|
60.25 0.5049 0.7710 0.0480 0.0314 2.231 23.436 10.707 1663.621 2.648 47.625 2.919 0.51 272300. 0.2669
|
|
63.42 0.5315 0.7812 0.0433 0.0295 2.092 21.972 9.663 1559.732 2.482 42.982 2.810 0.51 272950. 0.2441
|
|
66.59 0.5581 0.7875 0.0385 0.0273 1.939 20.370 8.600 1446.034 2.301 38.253 2.698 0.51 273626. 0.2210
|
|
69.76 0.5846 0.7887 0.0337 0.0250 1.774 18.636 7.522 1322.907 2.105 33.457 2.579 0.51 274328. 0.1976
|
|
72.93 0.6112 0.7835 0.0288 0.0225 1.597 16.775 6.434 1190.809 1.895 28.617 2.451 0.51 275055. 0.1737
|
|
76.10 0.6378 0.7694 0.0239 0.0198 1.408 14.796 5.340 1050.309 1.672 23.753 2.306 0.51 275808. 0.1489
|
|
79.27 0.6644 0.7421 0.0190 0.0170 1.210 12.708 4.247 902.104 1.436 18.891 2.135 0.51 276587. 0.1230
|
|
82.44 0.6909 0.6935 0.0142 0.0141 1.002 10.524 3.160 747.052 1.189 14.057 1.919 0.51 277391. 0.0953
|
|
85.61 0.7175 0.6060 0.0094 0.0111 0.786 8.258 2.087 586.193 0.933 9.282 1.615 0.51 278221. 0.0652
|
|
88.78 0.7441 0.4336 0.0046 0.0079 0.564 5.927 1.033 420.752 0.670 4.596 1.114 0.51 279076. 0.0316
|
|
91.95 0.7707 0.0027 0.0000 0.0047 0.337 3.542 0.004 251.423 0.400 0.017 0.007 0.51 279939. 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 0.1042 0.0362 4.080 36.740 31.646 3042.755 4.151 140.763 4.717 0.58 308777. 0.7415
|
|
3.70 0.0266 0.0741 0.1029 0.0369 4.160 37.458 31.262 3102.218 4.232 139.055 4.571 0.58 309007. 0.7141
|
|
7.40 0.0531 0.1435 0.1015 0.0376 4.237 38.154 30.837 3159.848 4.311 137.161 4.426 0.58 309260. 0.6868
|
|
11.09 0.0797 0.2084 0.1000 0.0382 4.311 38.814 30.366 3214.535 4.385 135.070 4.285 0.58 309535. 0.6597
|
|
14.79 0.1063 0.2689 0.0983 0.0388 4.379 39.425 29.848 3265.150 4.454 132.765 4.146 0.58 309834. 0.6329
|
|
18.49 0.1328 0.3252 0.0964 0.0394 4.439 39.973 29.279 3310.467 4.516 130.232 4.012 0.58 310158. 0.6065
|
|
22.19 0.1594 0.3775 0.0944 0.0398 4.491 40.440 28.655 3349.201 4.569 127.458 3.881 0.58 310508. 0.5804
|
|
25.89 0.1860 0.4260 0.0921 0.0402 4.533 40.812 27.974 3380.011 4.611 124.429 3.754 0.58 310885. 0.5548
|
|
29.58 0.2125 0.4710 0.0897 0.0405 4.562 41.072 27.233 3401.519 4.640 121.133 3.631 0.58 311290. 0.5295
|
|
33.28 0.2391 0.5126 0.0870 0.0406 4.576 41.203 26.430 3412.323 4.655 117.561 3.513 0.58 311723. 0.5046
|
|
36.98 0.2657 0.5511 0.0842 0.0406 4.574 41.187 25.562 3411.020 4.653 113.701 3.399 0.59 312184. 0.4802
|
|
40.68 0.2922 0.5866 0.0811 0.0404 4.554 41.008 24.628 3396.208 4.633 109.545 3.289 0.59 312675. 0.4561
|
|
44.38 0.3188 0.6193 0.0778 0.0400 4.515 40.649 23.626 3366.500 4.593 105.087 3.183 0.59 313195. 0.4323
|
|
48.07 0.3453 0.6493 0.0743 0.0395 4.453 40.093 22.553 3320.440 4.530 100.317 3.081 0.59 313745. 0.4088
|
|
51.77 0.3719 0.6768 0.0705 0.0387 4.367 39.323 21.410 3256.641 4.443 95.230 2.982 0.59 314325. 0.3855
|
|
55.47 0.3985 0.7018 0.0665 0.0378 4.257 38.331 20.199 3174.517 4.331 89.843 2.886 0.59 314935. 0.3624
|
|
59.17 0.4250 0.7244 0.0623 0.0366 4.123 37.120 18.927 3074.212 4.194 84.189 2.793 0.59 315575. 0.3395
|
|
62.87 0.4516 0.7444 0.0580 0.0352 3.964 35.694 17.603 2956.083 4.033 78.299 2.701 0.59 316244. 0.3166
|
|
66.56 0.4782 0.7618 0.0535 0.0336 3.782 34.057 16.233 2820.532 3.848 72.204 2.610 0.59 316944. 0.2939
|
|
70.26 0.5047 0.7762 0.0488 0.0317 3.578 32.215 14.823 2667.985 3.640 65.932 2.520 0.59 317673. 0.2711
|
|
73.96 0.5313 0.7874 0.0441 0.0297 3.351 30.173 13.379 2498.897 3.409 59.510 2.428 0.59 318432. 0.2482
|
|
77.66 0.5579 0.7947 0.0392 0.0275 3.103 27.938 11.908 2313.795 3.156 52.965 2.334 0.59 319221. 0.2251
|
|
81.36 0.5844 0.7972 0.0343 0.0251 2.834 25.517 10.415 2113.299 2.883 46.324 2.235 0.59 320040. 0.2016
|
|
85.05 0.6110 0.7936 0.0293 0.0226 2.545 22.920 8.907 1898.160 2.589 39.618 2.128 0.59 320889. 0.1775
|
|
88.75 0.6376 0.7814 0.0243 0.0199 2.239 20.156 7.391 1669.306 2.277 32.877 2.008 0.59 321767. 0.1526
|
|
92.45 0.6641 0.7565 0.0193 0.0170 1.915 17.241 5.876 1427.880 1.948 26.135 1.866 0.60 322676. 0.1264
|
|
96.15 0.6907 0.7106 0.0144 0.0140 1.576 14.191 4.368 1175.285 1.603 19.431 1.686 0.60 323614. 0.0985
|
|
99.85 0.7173 0.6259 0.0095 0.0109 1.225 11.027 2.879 913.235 1.246 12.806 1.430 0.60 324582. 0.0678
|
|
103.54 0.7438 0.4534 0.0047 0.0077 0.863 7.773 1.418 643.752 0.878 6.305 0.999 0.60 325579. 0.0332
|
|
107.24 0.7704 -0.0069 0.0000 0.0044 0.493 4.441 -0.012 367.803 0.502 -0.053 -0.015 0.60 326582. 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 0.1056 0.0368 6.185 48.728 41.875 4612.065 5.505 186.258 4.118 0.67 352848. 0.7446
|
|
4.22 0.0265 0.0739 0.1043 0.0375 6.308 49.697 41.388 4703.750 5.615 184.095 3.991 0.67 353111. 0.7174
|
|
8.44 0.0531 0.1431 0.1030 0.0382 6.427 50.637 40.847 4792.805 5.721 181.686 3.866 0.67 353400. 0.6903
|
|
12.67 0.0796 0.2078 0.1015 0.0389 6.541 51.532 40.246 4877.502 5.822 179.013 3.743 0.67 353714. 0.6634
|
|
16.89 0.1062 0.2682 0.0998 0.0395 6.646 52.362 39.581 4956.026 5.916 176.054 3.622 0.67 354057. 0.6368
|
|
21.11 0.1327 0.3244 0.0979 0.0401 6.741 53.106 38.846 5026.458 6.000 172.789 3.505 0.67 354428. 0.6105
|
|
25.33 0.1592 0.3767 0.0959 0.0405 6.822 53.744 38.039 5086.794 6.072 169.198 3.392 0.67 354829. 0.5845
|
|
29.56 0.1858 0.4252 0.0937 0.0409 6.886 54.252 37.155 5134.936 6.129 165.263 3.282 0.67 355261. 0.5589
|
|
33.78 0.2123 0.4702 0.0912 0.0412 6.931 54.610 36.189 5168.759 6.170 160.968 3.176 0.67 355725. 0.5338
|
|
38.00 0.2389 0.5120 0.0886 0.0413 6.955 54.793 35.139 5186.094 6.190 156.298 3.073 0.67 356221. 0.5090
|
|
42.22 0.2654 0.5506 0.0857 0.0413 6.953 54.779 34.001 5184.797 6.189 151.239 2.974 0.67 356750. 0.4846
|
|
46.44 0.2919 0.5863 0.0826 0.0411 6.923 54.546 32.774 5162.719 6.163 145.780 2.879 0.67 357312. 0.4606
|
|
50.67 0.3185 0.6192 0.0793 0.0408 6.863 54.070 31.455 5117.741 6.109 139.911 2.788 0.67 357907. 0.4369
|
|
54.89 0.3450 0.6495 0.0757 0.0402 6.769 53.330 30.041 5047.681 6.025 133.622 2.699 0.67 358537. 0.4134
|
|
59.11 0.3716 0.6774 0.0719 0.0395 6.639 52.302 28.530 4950.375 5.909 126.902 2.614 0.67 359201. 0.3901
|
|
63.33 0.3981 0.7028 0.0679 0.0385 6.470 50.976 26.928 4824.828 5.759 119.774 2.531 0.67 359899. 0.3670
|
|
67.55 0.4246 0.7259 0.0636 0.0372 6.264 49.353 25.243 4671.218 5.576 112.280 2.451 0.67 360631. 0.3441
|
|
71.78 0.4512 0.7465 0.0592 0.0358 6.021 47.439 23.485 4490.105 5.360 104.463 2.372 0.67 361397. 0.3212
|
|
76.00 0.4777 0.7646 0.0546 0.0341 5.742 45.242 21.665 4282.122 5.111 96.364 2.295 0.67 362197. 0.2984
|
|
80.22 0.5042 0.7798 0.0499 0.0323 5.428 42.768 19.789 4047.942 4.832 88.021 2.217 0.67 363031. 0.2756
|
|
84.44 0.5308 0.7919 0.0450 0.0302 5.080 40.024 17.867 3788.279 4.522 79.471 2.139 0.68 363899. 0.2526
|
|
88.67 0.5573 0.8003 0.0401 0.0279 4.699 37.020 15.906 3503.953 4.183 70.749 2.059 0.68 364800. 0.2294
|
|
92.89 0.5839 0.8042 0.0351 0.0255 4.286 33.766 13.915 3195.917 3.815 61.894 1.975 0.68 365736. 0.2058
|
|
97.11 0.6104 0.8022 0.0300 0.0228 3.842 30.273 11.903 2865.331 3.420 52.944 1.884 0.68 366705. 0.1816
|
|
101.33 0.6369 0.7919 0.0249 0.0200 3.371 26.557 9.879 2513.618 3.000 43.942 1.783 0.68 367708. 0.1566
|
|
105.55 0.6635 0.7694 0.0198 0.0171 2.873 22.637 7.854 2142.542 2.557 34.934 1.663 0.68 368745. 0.1302
|
|
109.78 0.6900 0.7265 0.0147 0.0140 2.353 18.535 5.839 1754.300 2.094 25.971 1.510 0.68 369816. 0.1019
|
|
114.00 0.7166 0.6451 0.0097 0.0108 1.813 14.280 3.846 1351.620 1.613 17.109 1.291 0.68 370921. 0.0707
|
|
118.22 0.7431 0.4740 0.0048 0.0075 1.258 9.908 1.891 937.781 1.119 8.411 0.915 0.68 372059. 0.0351
|
|
122.44 0.7696 -0.0109 -0.0001 0.0041 0.690 5.434 -0.023 514.345 0.614 -0.102 -0.020 0.69 373201. 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 0.1072 0.0381 9.129 63.934 53.807 6807.694 7.223 239.335 3.585 0.75 396898. 0.7348
|
|
4.74 0.0265 0.0724 0.1060 0.0388 9.295 65.091 53.222 6930.960 7.354 236.730 3.483 0.75 397193. 0.7100
|
|
9.48 0.0530 0.1406 0.1047 0.0395 9.455 66.217 52.565 7050.805 7.481 233.809 3.381 0.75 397518. 0.6850
|
|
14.23 0.0795 0.2046 0.1032 0.0401 9.608 67.288 51.831 7164.888 7.602 230.545 3.281 0.75 397872. 0.6600
|
|
18.97 0.1060 0.2646 0.1016 0.0407 9.750 68.283 51.013 7270.776 7.715 226.908 3.182 0.75 398258. 0.6351
|
|
23.71 0.1325 0.3207 0.0998 0.0412 9.878 69.175 50.106 7365.835 7.815 222.869 3.085 0.75 398676. 0.6102
|
|
28.45 0.1590 0.3730 0.0978 0.0417 9.987 69.940 49.101 7447.246 7.902 218.403 2.990 0.75 399128. 0.5855
|
|
33.19 0.1855 0.4217 0.0956 0.0420 10.074 70.548 47.995 7512.000 7.970 213.482 2.898 0.75 399615. 0.5610
|
|
37.93 0.2120 0.4669 0.0932 0.0423 10.134 70.970 46.782 7556.982 8.018 208.085 2.808 0.75 400138. 0.5366
|
|
42.68 0.2384 0.5090 0.0905 0.0424 10.164 71.177 45.456 7578.984 8.042 202.190 2.720 0.75 400697. 0.5125
|
|
47.42 0.2649 0.5479 0.0877 0.0424 10.158 71.137 44.015 7574.743 8.037 195.780 2.636 0.75 401293. 0.4886
|
|
52.16 0.2914 0.5839 0.0846 0.0422 10.113 70.820 42.455 7540.966 8.001 188.840 2.554 0.75 401926. 0.4649
|
|
56.90 0.3179 0.6172 0.0812 0.0418 10.023 70.195 40.773 7474.365 7.931 181.357 2.474 0.75 402598. 0.4414
|
|
61.64 0.3444 0.6479 0.0776 0.0413 9.885 69.229 38.966 7371.562 7.821 173.319 2.398 0.75 403307. 0.4182
|
|
66.39 0.3709 0.6762 0.0738 0.0405 9.694 67.891 37.030 7229.101 7.670 164.711 2.323 0.75 404055. 0.3950
|
|
71.13 0.3974 0.7021 0.0697 0.0394 9.448 66.163 34.972 7045.052 7.475 155.557 2.252 0.76 404841. 0.3720
|
|
75.87 0.4239 0.7257 0.0653 0.0382 9.145 64.044 32.804 6819.487 7.236 145.912 2.182 0.76 405666. 0.3492
|
|
80.61 0.4504 0.7469 0.0608 0.0367 8.788 61.544 30.538 6553.218 6.953 135.832 2.114 0.76 406528. 0.3264
|
|
85.35 0.4769 0.7657 0.0561 0.0350 8.378 58.670 28.186 6247.235 6.629 125.372 2.046 0.76 407428. 0.3036
|
|
90.09 0.5034 0.7818 0.0513 0.0330 7.916 55.434 25.760 5902.632 6.263 114.581 1.979 0.76 408366. 0.2807
|
|
94.84 0.5299 0.7949 0.0464 0.0309 7.403 51.846 23.270 5520.625 5.858 103.507 1.912 0.76 409342. 0.2577
|
|
99.58 0.5564 0.8043 0.0413 0.0286 6.843 47.921 20.728 5102.615 5.414 92.199 1.843 0.76 410355. 0.2344
|
|
104.32 0.5829 0.8093 0.0361 0.0260 6.236 43.673 18.144 4650.308 4.934 80.704 1.770 0.76 411406. 0.2106
|
|
109.06 0.6094 0.8084 0.0309 0.0233 5.586 39.123 15.529 4165.811 4.420 69.074 1.691 0.76 412495. 0.1862
|
|
113.80 0.6359 0.7991 0.0257 0.0204 4.897 34.295 12.896 3651.796 3.875 57.362 1.602 0.76 413621. 0.1607
|
|
118.54 0.6623 0.7771 0.0204 0.0174 4.173 29.222 10.258 3111.621 3.302 45.629 1.495 0.77 414786. 0.1338
|
|
123.29 0.6888 0.7337 0.0152 0.0143 3.419 23.943 7.631 2549.480 2.705 33.940 1.358 0.77 415988. 0.1048
|
|
128.03 0.7153 0.6498 0.0100 0.0110 2.642 18.506 5.029 1970.500 2.091 22.370 1.158 0.77 417227. 0.0725
|
|
132.77 0.7418 0.4728 0.0049 0.0077 1.852 12.967 2.473 1380.720 1.465 10.999 0.812 0.77 418504. 0.0357
|
|
137.51 0.7683 -0.0111 -0.0001 0.0044 1.051 7.358 -0.032 783.463 0.831 -0.141 -0.018 0.77 419786. 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 0.1090 0.0426 14.014 88.331 67.536 10450.542 9.980 300.402 2.931 0.83 440920. 0.6731
|
|
5.26 0.0265 0.0661 0.1079 0.0432 14.191 89.440 66.869 10581.860 10.105 297.432 2.866 0.83 441248. 0.6549
|
|
10.52 0.0529 0.1292 0.1067 0.0437 14.356 90.482 66.112 10705.080 10.223 294.068 2.801 0.83 441608. 0.6364
|
|
15.78 0.0794 0.1894 0.1053 0.0441 14.506 91.429 65.259 10817.092 10.330 290.272 2.736 0.83 442001. 0.6176
|
|
21.05 0.1058 0.2465 0.1037 0.0445 14.637 92.255 64.299 10914.832 10.423 286.002 2.672 0.83 442430. 0.5987
|
|
26.31 0.1323 0.3008 0.1020 0.0449 14.745 92.933 63.223 10995.044 10.499 281.216 2.608 0.83 442896. 0.5794
|
|
31.57 0.1587 0.3522 0.1001 0.0451 14.824 93.435 62.023 11054.511 10.556 275.879 2.545 0.83 443399. 0.5600
|
|
36.83 0.1852 0.4008 0.0979 0.0453 14.872 93.735 60.691 11089.907 10.590 269.953 2.482 0.83 443942. 0.5403
|
|
42.09 0.2117 0.4466 0.0955 0.0453 14.882 93.801 59.219 11097.765 10.598 263.406 2.420 0.83 444524. 0.5204
|
|
47.35 0.2381 0.4897 0.0929 0.0452 14.851 93.605 57.601 11074.526 10.575 256.210 2.359 0.84 445147. 0.5003
|
|
52.61 0.2646 0.5302 0.0901 0.0450 14.773 93.114 55.832 11016.530 10.520 248.339 2.299 0.84 445812. 0.4799
|
|
57.88 0.2910 0.5681 0.0870 0.0446 14.644 92.299 53.905 10920.017 10.428 239.772 2.239 0.84 446519. 0.4593
|
|
63.14 0.3175 0.6034 0.0836 0.0440 14.458 91.125 51.819 10781.165 10.295 230.491 2.180 0.84 447267. 0.4385
|
|
68.40 0.3439 0.6362 0.0800 0.0432 14.209 89.560 49.568 10595.981 10.118 220.480 2.122 0.84 448058. 0.4174
|
|
73.66 0.3704 0.6666 0.0761 0.0423 13.893 87.566 47.150 10360.042 9.893 209.721 2.064 0.84 448892. 0.3960
|
|
78.92 0.3969 0.6945 0.0719 0.0411 13.505 85.119 44.568 10070.546 9.617 198.239 2.007 0.84 449768. 0.3744
|
|
84.18 0.4233 0.7200 0.0675 0.0397 13.044 82.217 41.839 9727.233 9.289 186.101 1.951 0.84 450686. 0.3526
|
|
89.44 0.4498 0.7429 0.0629 0.0381 12.514 78.873 38.980 9331.662 8.911 173.381 1.895 0.84 451646. 0.3305
|
|
94.71 0.4762 0.7628 0.0581 0.0363 11.920 75.129 36.004 8888.682 8.488 160.146 1.837 0.84 452648. 0.3080
|
|
99.97 0.5027 0.7795 0.0531 0.0343 11.261 70.976 32.928 8397.328 8.019 146.465 1.779 0.84 453692. 0.2852
|
|
105.23 0.5292 0.7922 0.0480 0.0321 10.543 66.451 29.765 7861.947 7.508 132.396 1.717 0.84 454777. 0.2618
|
|
110.49 0.5556 0.8004 0.0428 0.0297 9.765 61.549 26.530 7281.935 6.954 118.005 1.652 0.85 455903. 0.2378
|
|
115.75 0.5821 0.8030 0.0375 0.0272 8.932 56.296 23.236 6660.533 6.360 103.355 1.582 0.85 457071. 0.2131
|
|
121.01 0.6085 0.7977 0.0321 0.0245 8.049 50.735 19.899 6002.499 5.732 88.510 1.504 0.85 458281. 0.1874
|
|
126.27 0.6350 0.7813 0.0267 0.0217 7.126 44.913 16.533 5313.683 5.074 73.540 1.411 0.85 459531. 0.1603
|
|
131.54 0.6614 0.7478 0.0212 0.0188 6.171 38.892 13.157 4601.439 4.394 58.521 1.297 0.85 460824. 0.1314
|
|
136.80 0.6879 0.6873 0.0158 0.0158 5.195 32.742 9.788 3873.786 3.699 43.537 1.146 0.85 462157. 0.1002
|
|
142.06 0.7144 0.5802 0.0104 0.0128 4.211 26.542 6.450 3140.247 2.999 28.690 0.932 0.85 463532. 0.0661
|
|
147.32 0.7408 0.3847 0.0051 0.0098 3.233 20.376 3.166 2410.713 2.302 14.082 0.596 0.86 464948. 0.0296
|
|
152.58 0.7673 -0.0094 -0.0001 0.0069 2.266 14.281 -0.052 1689.617 1.613 -0.233 -0.014 0.86 466378. 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 0.1096 0.0513 22.456 128.667 82.176 16745.152 14.537 365.517 2.226 0.92 484974. 0.5638
|
|
5.82 0.0266 0.0558 0.1087 0.0518 22.670 129.895 81.498 16904.859 14.675 362.502 2.187 0.92 485330. 0.5516
|
|
11.64 0.0532 0.1096 0.1076 0.0523 22.856 130.964 80.716 17044.090 14.796 359.023 2.148 0.92 485722. 0.5392
|
|
17.46 0.0798 0.1615 0.1064 0.0526 23.007 131.829 79.816 17156.607 14.894 355.022 2.110 0.92 486152. 0.5267
|
|
23.28 0.1064 0.2116 0.1051 0.0528 23.115 132.443 78.785 17236.508 14.963 350.434 2.073 0.92 486622. 0.5142
|
|
29.10 0.1330 0.2599 0.1035 0.0530 23.170 132.763 77.608 17278.113 14.999 345.199 2.037 0.92 487134. 0.5015
|
|
34.92 0.1596 0.3065 0.1017 0.0530 23.168 132.749 76.272 17276.355 14.998 339.259 2.002 0.92 487689. 0.4886
|
|
40.74 0.1862 0.3516 0.0997 0.0528 23.102 132.369 74.766 17226.857 14.955 332.557 1.969 0.92 488289. 0.4756
|
|
46.56 0.2128 0.3950 0.0974 0.0525 22.966 131.592 73.077 17125.803 14.867 325.045 1.935 0.92 488934. 0.4623
|
|
52.38 0.2394 0.4370 0.0949 0.0520 22.757 130.395 71.196 16969.973 14.732 316.679 1.903 0.92 489626. 0.4486
|
|
58.20 0.2661 0.4773 0.0922 0.0514 22.471 128.754 69.114 16756.457 14.547 307.421 1.871 0.92 490365. 0.4346
|
|
64.02 0.2927 0.5161 0.0891 0.0505 22.103 126.650 66.825 16482.574 14.309 297.237 1.839 0.92 491152. 0.4200
|
|
69.84 0.3193 0.5532 0.0858 0.0495 21.652 124.061 64.321 16145.667 14.016 286.101 1.807 0.92 491986. 0.4049
|
|
75.66 0.3459 0.5886 0.0821 0.0483 21.112 120.967 61.598 15742.991 13.667 273.988 1.775 0.92 492868. 0.3892
|
|
81.48 0.3725 0.6222 0.0782 0.0468 20.481 117.352 58.652 15272.529 13.258 260.884 1.742 0.92 493798. 0.3727
|
|
87.30 0.3991 0.6538 0.0740 0.0452 19.758 113.208 55.489 14733.216 12.790 246.817 1.708 0.92 494776. 0.3556
|
|
93.12 0.4257 0.6833 0.0695 0.0433 18.945 108.550 52.130 14127.051 12.264 231.874 1.674 0.92 495800. 0.3377
|
|
98.94 0.4523 0.7105 0.0648 0.0413 18.046 103.400 48.596 13456.824 11.682 216.155 1.638 0.93 496872. 0.3190
|
|
104.76 0.4789 0.7347 0.0599 0.0390 17.074 97.830 44.907 12731.880 11.053 199.747 1.600 0.93 497989. 0.2996
|
|
110.58 0.5055 0.7540 0.0548 0.0367 16.066 92.054 41.079 11980.129 10.400 182.721 1.555 0.93 499153. 0.2785
|
|
116.40 0.5321 0.7677 0.0495 0.0343 15.013 86.023 37.134 11195.266 9.719 165.173 1.504 0.93 500363. 0.2562
|
|
122.22 0.5587 0.7707 0.0441 0.0320 13.989 80.152 33.082 10431.260 9.056 147.151 1.438 0.93 501618. 0.2312
|
|
128.04 0.5853 0.7622 0.0386 0.0296 12.966 74.295 28.948 9669.008 8.394 128.761 1.358 0.93 502919. 0.2041
|
|
133.86 0.6119 0.7418 0.0330 0.0272 11.913 68.259 24.758 8883.468 7.712 110.124 1.264 0.93 504265. 0.1757
|
|
139.68 0.6385 0.7054 0.0274 0.0248 10.842 62.126 20.536 8085.251 7.019 91.343 1.152 0.94 505657. 0.1459
|
|
145.50 0.6651 0.6476 0.0217 0.0223 9.770 55.981 16.308 7285.532 6.325 72.539 1.015 0.94 507095. 0.1146
|
|
151.32 0.6917 0.5606 0.0161 0.0199 8.715 49.933 12.107 6498.426 5.641 53.854 0.845 0.94 508578. 0.0822
|
|
157.14 0.7183 0.4342 0.0106 0.0176 7.690 44.064 7.969 5734.635 4.978 35.448 0.630 0.94 510107. 0.0497
|
|
162.96 0.7449 0.2546 0.0052 0.0153 6.710 38.449 3.931 5003.875 4.344 17.486 0.356 0.94 511682. 0.0197
|
|
168.78 0.7716 0.0002 0.0000 0.0132 5.761 33.008 0.002 4295.819 3.729 0.009 0.000 0.94 513307. 0.0000
|
|
|
|
|
|
|