427 lines
76 KiB
Plaintext
427 lines
76 KiB
Plaintext
21x13E (21x13E.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 0.0929 0.0362 0.012 0.750 0.576 8.876 0.085 2.561 29.419 0.08 40331. 0.6237
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0.53 0.0265 0.0660 0.0917 0.0368 0.012 0.762 0.568 9.016 0.086 2.528 28.593 0.08 40359. 0.6023
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1.05 0.0529 0.1281 0.0904 0.0373 0.012 0.773 0.560 9.151 0.087 2.492 27.770 0.08 40390. 0.5808
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1.58 0.0794 0.1865 0.0890 0.0379 0.012 0.784 0.551 9.279 0.089 2.452 26.952 0.08 40424. 0.5592
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2.10 0.1058 0.2412 0.0874 0.0383 0.013 0.794 0.542 9.398 0.090 2.409 26.142 0.08 40461. 0.5376
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2.63 0.1323 0.2923 0.0857 0.0388 0.013 0.803 0.531 9.504 0.091 2.362 25.343 0.08 40501. 0.5160
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3.16 0.1588 0.3399 0.0838 0.0391 0.013 0.811 0.519 9.594 0.092 2.311 24.557 0.08 40545. 0.4945
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3.68 0.1852 0.3841 0.0818 0.0394 0.013 0.817 0.507 9.666 0.092 2.255 23.785 0.08 40592. 0.4732
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4.21 0.2117 0.4250 0.0796 0.0396 0.013 0.821 0.493 9.716 0.093 2.194 23.029 0.08 40643. 0.4519
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4.74 0.2382 0.4627 0.0772 0.0397 0.013 0.823 0.479 9.740 0.093 2.129 22.288 0.08 40697. 0.4308
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5.26 0.2646 0.4974 0.0747 0.0397 0.013 0.823 0.463 9.735 0.093 2.058 21.562 0.08 40755. 0.4098
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5.79 0.2911 0.5291 0.0719 0.0396 0.013 0.820 0.446 9.697 0.093 1.983 20.851 0.08 40817. 0.3890
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6.31 0.3175 0.5579 0.0690 0.0393 0.013 0.814 0.428 9.625 0.092 1.902 20.153 0.08 40883. 0.3682
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6.84 0.3440 0.5838 0.0659 0.0388 0.013 0.804 0.408 9.514 0.091 1.816 19.465 0.08 40952. 0.3475
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7.37 0.3705 0.6067 0.0626 0.0382 0.013 0.791 0.388 9.362 0.089 1.725 18.786 0.08 41026. 0.3268
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7.89 0.3969 0.6267 0.0590 0.0374 0.012 0.775 0.366 9.165 0.088 1.628 18.111 0.08 41103. 0.3061
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8.42 0.4234 0.6435 0.0553 0.0364 0.012 0.754 0.343 8.924 0.085 1.526 17.435 0.08 41185. 0.2853
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8.95 0.4498 0.6570 0.0515 0.0353 0.012 0.730 0.319 8.639 0.083 1.419 16.753 0.08 41270. 0.2644
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9.47 0.4763 0.6668 0.0475 0.0339 0.011 0.703 0.294 8.314 0.079 1.309 16.058 0.08 41360. 0.2434
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10.00 0.5028 0.6724 0.0434 0.0324 0.011 0.672 0.269 7.949 0.076 1.196 15.340 0.08 41453. 0.2222
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10.52 0.5292 0.6731 0.0392 0.0308 0.010 0.638 0.243 7.545 0.072 1.080 14.590 0.08 41551. 0.2008
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11.05 0.5557 0.6682 0.0349 0.0290 0.010 0.601 0.216 7.106 0.068 0.961 13.793 0.08 41652. 0.1791
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11.58 0.5821 0.6563 0.0305 0.0271 0.009 0.560 0.189 6.631 0.063 0.841 12.931 0.08 41758. 0.1571
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12.10 0.6086 0.6357 0.0261 0.0250 0.008 0.518 0.162 6.124 0.058 0.719 11.981 0.08 41867. 0.1346
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12.63 0.6351 0.6038 0.0217 0.0228 0.007 0.472 0.134 5.586 0.053 0.597 10.906 0.08 41980. 0.1117
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13.16 0.6615 0.5568 0.0172 0.0205 0.007 0.424 0.107 5.020 0.048 0.475 9.654 0.09 42098. 0.0882
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13.68 0.6880 0.4884 0.0128 0.0181 0.006 0.374 0.080 4.429 0.042 0.354 8.143 0.09 42219. 0.0642
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14.21 0.7145 0.3885 0.0085 0.0156 0.005 0.323 0.053 3.818 0.036 0.234 6.237 0.09 42344. 0.0399
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14.73 0.7409 0.2384 0.0042 0.0130 0.004 0.270 0.026 3.190 0.030 0.115 3.690 0.09 42473. 0.0166
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15.26 0.7674 0.0007 0.0000 0.0104 0.003 0.216 0.000 2.551 0.024 0.000 0.010 0.09 42606. 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 0.0933 0.0338 0.089 2.801 2.312 66.286 0.316 10.283 15.819 0.17 80660. 0.6721
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1.06 0.0266 0.0711 0.0921 0.0344 0.090 2.852 2.282 67.475 0.322 10.152 15.343 0.17 80717. 0.6477
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2.11 0.0532 0.1378 0.0908 0.0350 0.092 2.901 2.250 68.634 0.328 10.009 14.870 0.17 80779. 0.6233
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3.17 0.0797 0.2002 0.0893 0.0356 0.094 2.947 2.215 69.740 0.333 9.851 14.403 0.17 80848. 0.5989
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4.23 0.1063 0.2585 0.0878 0.0361 0.095 2.991 2.176 70.771 0.338 9.678 13.944 0.17 80922. 0.5747
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5.29 0.1329 0.3127 0.0860 0.0366 0.096 3.030 2.133 71.703 0.342 9.488 13.494 0.17 81003. 0.5507
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6.34 0.1595 0.3630 0.0842 0.0370 0.097 3.064 2.087 72.509 0.346 9.282 13.053 0.17 81091. 0.5269
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7.40 0.1860 0.4095 0.0821 0.0373 0.098 3.092 2.036 73.163 0.349 9.057 12.624 0.17 81186. 0.5033
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8.46 0.2126 0.4525 0.0799 0.0376 0.099 3.112 1.982 73.637 0.352 8.814 12.205 0.17 81288. 0.4801
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9.51 0.2392 0.4921 0.0775 0.0377 0.099 3.123 1.922 73.902 0.353 8.551 11.799 0.17 81397. 0.4571
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10.57 0.2658 0.5285 0.0750 0.0377 0.099 3.124 1.859 73.929 0.353 8.267 11.403 0.17 81514. 0.4344
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11.63 0.2924 0.5617 0.0722 0.0376 0.099 3.114 1.790 73.691 0.352 7.963 11.019 0.17 81639. 0.4120
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12.69 0.3189 0.5920 0.0693 0.0373 0.098 3.092 1.717 73.160 0.349 7.638 10.645 0.17 81772. 0.3898
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13.74 0.3455 0.6194 0.0661 0.0369 0.097 3.056 1.639 72.310 0.345 7.290 10.281 0.17 81912. 0.3678
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14.80 0.3721 0.6439 0.0628 0.0363 0.095 3.005 1.556 71.113 0.340 6.921 9.924 0.17 82060. 0.3459
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15.86 0.3987 0.6655 0.0592 0.0355 0.093 2.939 1.468 69.546 0.332 6.529 9.574 0.17 82217. 0.3241
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16.91 0.4253 0.6842 0.0555 0.0345 0.091 2.857 1.375 67.608 0.323 6.118 9.227 0.17 82381. 0.3024
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17.97 0.4518 0.6998 0.0516 0.0333 0.088 2.760 1.279 65.307 0.312 5.689 8.883 0.17 82554. 0.2807
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19.03 0.4784 0.7120 0.0476 0.0320 0.084 2.648 1.179 62.655 0.299 5.244 8.535 0.17 82734. 0.2590
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20.08 0.5050 0.7204 0.0434 0.0304 0.080 2.521 1.076 59.664 0.285 4.787 8.182 0.17 82923. 0.2372
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21.14 0.5316 0.7245 0.0392 0.0287 0.076 2.381 0.971 56.345 0.269 4.319 7.816 0.17 83119. 0.2152
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22.20 0.5581 0.7233 0.0348 0.0269 0.071 2.228 0.864 52.712 0.252 3.842 7.433 0.17 83324. 0.1930
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23.26 0.5847 0.7159 0.0305 0.0249 0.065 2.061 0.755 48.779 0.233 3.359 7.021 0.17 83536. 0.1705
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24.31 0.6113 0.7002 0.0260 0.0227 0.060 1.883 0.645 44.561 0.213 2.871 6.570 0.17 83757. 0.1475
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25.37 0.6379 0.6737 0.0216 0.0204 0.054 1.694 0.535 40.078 0.191 2.381 6.058 0.17 83985. 0.1238
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26.43 0.6645 0.6320 0.0172 0.0180 0.047 1.494 0.425 35.354 0.169 1.891 5.455 0.17 84222. 0.0994
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27.48 0.6910 0.5674 0.0127 0.0155 0.041 1.285 0.316 30.417 0.145 1.405 4.709 0.17 84466. 0.0739
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28.54 0.7176 0.4661 0.0084 0.0129 0.034 1.069 0.208 25.300 0.121 0.924 3.725 0.17 84719. 0.0475
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29.60 0.7442 0.2992 0.0041 0.0102 0.027 0.847 0.102 20.042 0.096 0.453 2.306 0.17 84979. 0.0206
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30.66 0.7708 -0.0055 -0.0001 0.0075 0.020 0.620 -0.001 14.680 0.070 -0.006 -0.041 0.17 85245. 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 0.0937 0.0329 0.292 6.129 5.225 217.530 0.692 23.240 10.894 0.25 120987. 0.6958
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1.59 0.0266 0.0735 0.0925 0.0335 0.297 6.245 5.159 221.674 0.706 22.948 10.556 0.25 121072. 0.6699
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3.18 0.0532 0.1423 0.0912 0.0341 0.303 6.359 5.087 225.719 0.718 22.626 10.222 0.25 121166. 0.6441
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4.76 0.0798 0.2065 0.0898 0.0347 0.308 6.469 5.007 229.591 0.731 22.272 9.892 0.25 121269. 0.6185
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6.35 0.1064 0.2664 0.0882 0.0352 0.313 6.571 4.920 233.211 0.742 21.883 9.569 0.25 121381. 0.5930
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7.94 0.1331 0.3220 0.0865 0.0357 0.317 6.663 4.824 236.497 0.753 21.458 9.252 0.25 121503. 0.5678
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9.53 0.1597 0.3735 0.0846 0.0362 0.321 6.744 4.720 239.357 0.762 20.994 8.944 0.25 121635. 0.5429
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11.11 0.1863 0.4211 0.0826 0.0365 0.324 6.810 4.606 241.699 0.769 20.488 8.644 0.25 121778. 0.5184
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12.70 0.2129 0.4651 0.0804 0.0368 0.326 6.858 4.483 243.425 0.775 19.940 8.353 0.25 121931. 0.4941
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14.29 0.2395 0.5055 0.0780 0.0369 0.328 6.887 4.349 244.436 0.778 19.346 8.071 0.25 122096. 0.4703
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15.88 0.2661 0.5427 0.0754 0.0370 0.328 6.892 4.206 244.634 0.779 18.706 7.797 0.25 122272. 0.4468
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17.46 0.2927 0.5767 0.0726 0.0369 0.327 6.872 4.051 243.919 0.776 18.019 7.533 0.25 122459. 0.4236
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19.05 0.3193 0.6077 0.0697 0.0366 0.325 6.824 3.886 242.199 0.771 17.283 7.277 0.25 122659. 0.4008
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20.64 0.3459 0.6359 0.0665 0.0362 0.321 6.744 3.709 239.381 0.762 16.498 7.028 0.25 122870. 0.3782
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22.23 0.3725 0.6612 0.0631 0.0356 0.316 6.631 3.521 235.366 0.749 15.663 6.786 0.25 123093. 0.3558
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23.81 0.3992 0.6837 0.0596 0.0348 0.309 6.482 3.322 230.073 0.732 14.777 6.549 0.25 123328. 0.3335
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25.40 0.4258 0.7034 0.0558 0.0338 0.300 6.297 3.113 223.494 0.711 13.845 6.317 0.25 123576. 0.3114
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26.99 0.4524 0.7202 0.0519 0.0326 0.289 6.076 2.894 215.656 0.686 12.873 6.087 0.25 123835. 0.2893
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28.58 0.4790 0.7338 0.0478 0.0312 0.277 5.821 2.668 206.597 0.658 11.867 5.857 0.25 124107. 0.2673
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30.16 0.5056 0.7438 0.0437 0.0297 0.263 5.532 2.435 196.355 0.625 10.832 5.625 0.25 124390. 0.2453
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31.75 0.5322 0.7499 0.0394 0.0280 0.248 5.211 2.197 184.968 0.589 9.772 5.387 0.25 124685. 0.2231
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33.34 0.5588 0.7511 0.0350 0.0261 0.231 4.859 1.954 172.480 0.549 8.693 5.139 0.25 124993. 0.2007
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34.93 0.5854 0.7464 0.0306 0.0240 0.213 4.478 1.708 158.938 0.506 7.599 4.875 0.25 125312. 0.1780
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36.51 0.6120 0.7342 0.0262 0.0218 0.194 4.068 1.460 144.399 0.460 6.495 4.586 0.25 125644. 0.1549
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38.10 0.6386 0.7116 0.0217 0.0195 0.173 3.633 1.211 128.931 0.410 5.386 4.260 0.26 125988. 0.1310
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39.69 0.6653 0.6742 0.0172 0.0170 0.151 3.173 0.962 112.615 0.358 4.279 3.875 0.26 126343. 0.1062
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41.28 0.6919 0.6140 0.0128 0.0144 0.128 2.692 0.715 95.551 0.304 3.180 3.393 0.26 126711. 0.0802
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42.86 0.7185 0.5155 0.0084 0.0118 0.104 2.194 0.471 77.856 0.248 2.094 2.743 0.26 127091. 0.0526
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44.45 0.7451 0.3433 0.0042 0.0090 0.080 1.681 0.232 59.669 0.190 1.031 1.762 0.26 127482. 0.0237
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46.04 0.7717 -0.0026 0.0000 0.0062 0.055 1.158 -0.001 41.109 0.131 -0.005 -0.013 0.26 127881. 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 0.0942 0.0325 0.683 10.761 9.341 509.259 1.216 41.550 8.320 0.33 161309. 0.7105
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2.12 0.0266 0.0748 0.0930 0.0331 0.696 10.974 9.226 519.324 1.240 41.036 8.058 0.33 161423. 0.6838
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4.24 0.0532 0.1448 0.0917 0.0337 0.710 11.182 9.098 529.164 1.263 40.468 7.798 0.33 161549. 0.6572
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6.35 0.0799 0.2101 0.0903 0.0343 0.722 11.381 8.957 538.595 1.286 39.843 7.543 0.33 161686. 0.6308
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8.47 0.1065 0.2708 0.0888 0.0349 0.734 11.568 8.803 547.432 1.307 39.155 7.294 0.33 161836. 0.6046
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10.59 0.1331 0.3272 0.0871 0.0354 0.745 11.737 8.633 555.469 1.326 38.401 7.050 0.33 161999. 0.5788
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12.71 0.1597 0.3794 0.0852 0.0359 0.754 11.886 8.448 562.492 1.343 37.577 6.812 0.33 162175. 0.5532
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14.82 0.1863 0.4277 0.0832 0.0362 0.762 12.008 8.246 568.271 1.357 36.679 6.582 0.33 162366. 0.5281
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16.94 0.2130 0.4722 0.0809 0.0365 0.768 12.099 8.027 572.571 1.367 35.703 6.358 0.33 162571. 0.5033
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19.06 0.2396 0.5132 0.0785 0.0367 0.771 12.153 7.789 575.153 1.373 34.646 6.142 0.33 162791. 0.4790
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21.18 0.2662 0.5509 0.0760 0.0367 0.772 12.166 7.533 575.774 1.375 33.505 5.934 0.33 163026. 0.4550
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23.29 0.2928 0.5854 0.0732 0.0366 0.770 12.133 7.257 574.201 1.371 32.278 5.732 0.33 163277. 0.4315
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25.41 0.3195 0.6169 0.0702 0.0364 0.765 12.049 6.961 570.203 1.361 30.964 5.537 0.33 163543. 0.4082
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27.53 0.3461 0.6455 0.0670 0.0359 0.756 11.908 6.646 563.556 1.345 29.561 5.349 0.34 163825. 0.3853
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29.65 0.3727 0.6714 0.0636 0.0353 0.743 11.707 6.310 554.023 1.323 28.067 5.166 0.34 164123. 0.3626
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31.76 0.3993 0.6946 0.0600 0.0345 0.726 11.440 5.954 541.403 1.293 26.482 4.988 0.34 164438. 0.3401
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33.88 0.4259 0.7150 0.0563 0.0335 0.705 11.108 5.579 525.665 1.255 24.814 4.814 0.34 164768. 0.3177
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36.00 0.4526 0.7326 0.0523 0.0323 0.680 10.711 5.188 506.875 1.210 23.075 4.642 0.34 165114. 0.2954
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38.12 0.4792 0.7472 0.0482 0.0309 0.651 10.251 4.782 485.118 1.158 21.272 4.471 0.34 165477. 0.2732
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40.23 0.5058 0.7584 0.0440 0.0294 0.618 9.730 4.365 460.482 1.099 19.417 4.300 0.34 165855. 0.2510
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42.35 0.5324 0.7659 0.0397 0.0276 0.581 9.151 3.938 433.060 1.034 17.518 4.125 0.34 166250. 0.2287
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44.47 0.5590 0.7688 0.0353 0.0257 0.540 8.515 3.504 402.954 0.962 15.584 3.944 0.34 166660. 0.2063
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46.59 0.5857 0.7662 0.0309 0.0236 0.497 7.824 3.063 370.279 0.884 13.623 3.752 0.34 167087. 0.1834
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48.70 0.6123 0.7564 0.0264 0.0214 0.449 7.082 2.618 335.172 0.800 11.644 3.543 0.34 167529. 0.1602
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50.82 0.6389 0.7368 0.0219 0.0190 0.399 6.293 2.171 297.797 0.711 9.658 3.307 0.34 167988. 0.1362
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52.94 0.6655 0.7029 0.0174 0.0165 0.346 5.459 1.725 258.355 0.617 7.673 3.029 0.34 168463. 0.1111
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55.06 0.6921 0.6466 0.0129 0.0138 0.291 4.587 1.282 217.086 0.518 5.703 2.679 0.34 168953. 0.0848
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57.17 0.7188 0.5512 0.0085 0.0111 0.234 3.683 0.845 174.282 0.416 3.759 2.199 0.34 169460. 0.0565
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59.29 0.7454 0.3772 0.0042 0.0083 0.175 2.753 0.417 130.283 0.311 1.854 1.451 0.34 169982. 0.0262
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61.41 0.7720 -0.0006 0.0000 0.0054 0.114 1.804 0.000 85.363 0.204 -0.002 -0.002 0.34 170514. 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 0.0949 0.0324 1.329 16.757 14.701 991.287 1.893 65.389 6.726 0.42 201626. 0.7206
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2.65 0.0266 0.0756 0.0937 0.0330 1.356 17.097 14.522 1011.418 1.932 64.595 6.513 0.42 201769. 0.6934
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5.30 0.0533 0.1463 0.0925 0.0337 1.383 17.431 14.325 1031.117 1.969 63.717 6.301 0.42 201926. 0.6664
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7.94 0.0799 0.2122 0.0910 0.0343 1.408 17.750 14.107 1050.020 2.005 62.748 6.094 0.42 202098. 0.6395
|
|
10.59 0.1065 0.2735 0.0895 0.0349 1.432 18.050 13.867 1067.755 2.039 61.680 5.890 0.42 202285. 0.6129
|
|
13.24 0.1332 0.3304 0.0878 0.0354 1.454 18.323 13.603 1083.915 2.070 60.507 5.692 0.42 202490. 0.5866
|
|
15.89 0.1598 0.3831 0.0859 0.0358 1.473 18.562 13.314 1098.062 2.097 59.223 5.500 0.42 202711. 0.5607
|
|
18.54 0.1864 0.4317 0.0839 0.0362 1.488 18.760 12.999 1109.743 2.119 57.820 5.313 0.42 202950. 0.5352
|
|
21.18 0.2130 0.4766 0.0817 0.0365 1.500 18.907 12.656 1118.487 2.136 56.293 5.132 0.42 203207. 0.5101
|
|
23.83 0.2397 0.5180 0.0793 0.0367 1.507 18.997 12.284 1123.814 2.146 54.638 4.958 0.42 203482. 0.4855
|
|
26.48 0.2663 0.5560 0.0767 0.0367 1.509 19.022 11.882 1125.240 2.149 52.850 4.789 0.42 203777. 0.4613
|
|
29.13 0.2929 0.5908 0.0739 0.0366 1.505 18.972 11.449 1122.297 2.143 50.924 4.627 0.42 204091. 0.4374
|
|
31.78 0.3196 0.6227 0.0709 0.0364 1.495 18.840 10.985 1114.526 2.129 48.859 4.470 0.42 204425. 0.4140
|
|
34.42 0.3462 0.6518 0.0677 0.0360 1.477 18.620 10.488 1101.480 2.104 46.652 4.319 0.42 204778. 0.3908
|
|
37.07 0.3728 0.6781 0.0643 0.0353 1.452 18.302 9.960 1082.688 2.068 44.300 4.172 0.42 205152. 0.3679
|
|
39.72 0.3995 0.7017 0.0607 0.0345 1.418 17.881 9.398 1057.742 2.020 41.803 4.030 0.42 205546. 0.3452
|
|
42.37 0.4261 0.7228 0.0568 0.0335 1.377 17.354 8.807 1026.568 1.961 39.174 3.891 0.42 205959. 0.3227
|
|
45.02 0.4527 0.7410 0.0529 0.0323 1.327 16.723 8.190 989.287 1.889 36.429 3.755 0.42 206393. 0.3003
|
|
47.66 0.4794 0.7564 0.0487 0.0309 1.269 15.993 7.551 946.067 1.807 33.585 3.620 0.42 206847. 0.2779
|
|
50.31 0.5060 0.7686 0.0445 0.0293 1.203 15.165 6.892 897.083 1.713 30.656 3.485 0.42 207320. 0.2556
|
|
52.96 0.5326 0.7772 0.0401 0.0275 1.130 14.242 6.218 842.517 1.609 27.656 3.347 0.42 207814. 0.2332
|
|
55.61 0.5593 0.7814 0.0357 0.0255 1.049 13.229 5.531 782.571 1.495 24.600 3.205 0.42 208328. 0.2106
|
|
58.26 0.5859 0.7804 0.0312 0.0234 0.962 12.129 4.834 717.475 1.370 21.501 3.056 0.42 208862. 0.1877
|
|
60.90 0.6125 0.7726 0.0267 0.0211 0.868 10.946 4.131 647.502 1.237 18.374 2.894 0.42 209416. 0.1643
|
|
63.55 0.6391 0.7553 0.0221 0.0187 0.768 9.686 3.425 572.983 1.094 15.234 2.711 0.43 209990. 0.1402
|
|
66.20 0.6658 0.7242 0.0176 0.0161 0.663 8.356 2.720 494.320 0.944 12.097 2.495 0.43 210584. 0.1150
|
|
68.85 0.6924 0.6710 0.0130 0.0134 0.553 6.965 2.019 411.999 0.787 8.982 2.223 0.43 211198. 0.0883
|
|
71.50 0.7190 0.5782 0.0086 0.0107 0.438 5.521 1.328 326.608 0.624 5.909 1.845 0.43 211832. 0.0594
|
|
74.14 0.7457 0.4023 0.0042 0.0078 0.320 4.037 0.652 238.836 0.456 2.899 1.238 0.43 212485. 0.0279
|
|
76.79 0.7723 -0.0080 -0.0001 0.0049 0.200 2.522 -0.008 149.195 0.285 -0.035 -0.024 0.43 213148. 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 0.0957 0.0325 2.305 24.208 21.356 1718.472 2.735 94.992 5.637 0.50 241935. 0.7278
|
|
3.17 0.0266 0.0760 0.0946 0.0331 2.352 24.710 21.104 1754.122 2.792 93.871 5.457 0.50 242106. 0.7005
|
|
6.35 0.0532 0.1470 0.0933 0.0338 2.399 25.202 20.824 1789.040 2.847 92.627 5.280 0.50 242295. 0.6732
|
|
9.52 0.0798 0.2132 0.0919 0.0344 2.444 25.675 20.515 1822.591 2.901 91.250 5.105 0.50 242502. 0.6461
|
|
12.70 0.1064 0.2747 0.0904 0.0350 2.486 26.119 20.173 1854.110 2.951 89.729 4.935 0.50 242727. 0.6193
|
|
15.87 0.1330 0.3319 0.0887 0.0356 2.525 26.524 19.796 1882.875 2.997 88.054 4.769 0.50 242972. 0.5928
|
|
19.05 0.1596 0.3848 0.0869 0.0360 2.559 26.880 19.383 1908.114 3.037 86.214 4.607 0.50 243238. 0.5668
|
|
22.22 0.1863 0.4337 0.0848 0.0364 2.587 27.174 18.930 1929.020 3.070 84.202 4.451 0.50 243525. 0.5411
|
|
25.40 0.2129 0.4788 0.0826 0.0367 2.608 27.396 18.437 1944.755 3.095 82.007 4.300 0.50 243834. 0.5159
|
|
28.57 0.2395 0.5204 0.0802 0.0369 2.621 27.533 17.901 1954.473 3.111 79.623 4.154 0.50 244165. 0.4911
|
|
31.75 0.2661 0.5586 0.0776 0.0370 2.625 27.573 17.321 1957.327 3.115 77.042 4.014 0.50 244519. 0.4667
|
|
34.92 0.2927 0.5938 0.0748 0.0369 2.618 27.505 16.695 1952.481 3.107 74.260 3.878 0.50 244896. 0.4428
|
|
38.10 0.3193 0.6260 0.0718 0.0366 2.600 27.317 16.023 1939.126 3.086 71.272 3.748 0.50 245297. 0.4192
|
|
41.27 0.3459 0.6554 0.0686 0.0362 2.570 26.998 15.305 1916.482 3.050 68.075 3.622 0.50 245722. 0.3959
|
|
44.45 0.3725 0.6821 0.0652 0.0356 2.526 26.536 14.538 1883.724 2.998 64.665 3.501 0.50 246170. 0.3729
|
|
47.62 0.3991 0.7062 0.0615 0.0348 2.468 25.922 13.723 1840.114 2.929 61.041 3.383 0.50 246642. 0.3501
|
|
50.80 0.4257 0.7277 0.0577 0.0337 2.394 25.152 12.864 1785.487 2.842 57.220 3.268 0.50 247139. 0.3275
|
|
53.97 0.4523 0.7466 0.0536 0.0325 2.307 24.230 11.967 1720.049 2.738 53.227 3.156 0.50 247659. 0.3050
|
|
57.15 0.4789 0.7627 0.0495 0.0311 2.205 23.160 11.036 1644.087 2.617 49.087 3.045 0.51 248204. 0.2826
|
|
60.32 0.5056 0.7758 0.0452 0.0294 2.089 21.946 10.076 1557.913 2.479 44.820 2.934 0.51 248772. 0.2602
|
|
63.50 0.5322 0.7854 0.0408 0.0276 1.960 20.593 9.094 1461.848 2.327 40.448 2.821 0.51 249364. 0.2377
|
|
66.67 0.5588 0.7909 0.0363 0.0256 1.819 19.106 8.092 1356.245 2.159 35.991 2.706 0.51 249981. 0.2151
|
|
69.85 0.5854 0.7915 0.0317 0.0235 1.665 17.489 7.075 1241.510 1.976 31.470 2.585 0.51 250621. 0.1921
|
|
73.02 0.6120 0.7855 0.0271 0.0211 1.499 15.751 6.049 1118.126 1.780 26.905 2.454 0.51 251285. 0.1686
|
|
76.20 0.6386 0.7705 0.0225 0.0186 1.323 13.899 5.018 986.675 1.570 22.319 2.307 0.51 251973. 0.1444
|
|
79.37 0.6652 0.7423 0.0179 0.0160 1.137 11.944 3.988 847.868 1.349 17.738 2.133 0.51 252685. 0.1190
|
|
82.55 0.6918 0.6926 0.0133 0.0133 0.942 9.897 2.965 702.568 1.118 13.186 1.914 0.51 253420. 0.0921
|
|
85.72 0.7184 0.6038 0.0088 0.0104 0.740 7.774 1.955 551.819 0.878 8.695 1.607 0.51 254180. 0.0628
|
|
88.90 0.7450 0.4301 0.0043 0.0075 0.532 5.590 0.966 396.849 0.632 4.295 1.104 0.51 254963. 0.0303
|
|
92.07 0.7716 0.0011 0.0000 0.0045 0.320 3.361 0.001 238.583 0.380 0.006 0.003 0.51 255757. 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 0.0967 0.0328 3.692 33.243 29.379 2753.142 3.756 130.677 4.840 0.58 282234. 0.7330
|
|
3.70 0.0266 0.0761 0.0956 0.0334 3.770 33.947 29.044 2811.413 3.835 129.190 4.686 0.58 282434. 0.7056
|
|
7.40 0.0532 0.1472 0.0944 0.0341 3.847 34.637 28.672 2868.569 3.913 127.533 4.534 0.58 282655. 0.6783
|
|
11.11 0.0798 0.2135 0.0930 0.0348 3.921 35.301 28.258 2923.555 3.988 125.692 4.384 0.58 282896. 0.6512
|
|
14.81 0.1064 0.2751 0.0915 0.0354 3.990 35.925 27.799 2975.283 4.059 123.652 4.238 0.58 283160. 0.6243
|
|
18.51 0.1330 0.3324 0.0899 0.0360 4.053 36.496 27.292 3022.562 4.123 121.397 4.096 0.58 283446. 0.5978
|
|
22.21 0.1596 0.3854 0.0880 0.0365 4.109 36.998 26.734 3064.122 4.180 118.913 3.957 0.58 283757. 0.5717
|
|
25.92 0.1862 0.4344 0.0860 0.0369 4.155 37.415 26.121 3098.639 4.227 116.187 3.824 0.58 284093. 0.5460
|
|
29.62 0.2128 0.4797 0.0838 0.0372 4.190 37.730 25.451 3124.743 4.263 113.205 3.694 0.58 284454. 0.5207
|
|
33.32 0.2394 0.5215 0.0814 0.0374 4.212 37.927 24.721 3141.041 4.285 109.958 3.570 0.58 284841. 0.4959
|
|
37.02 0.2660 0.5599 0.0788 0.0374 4.219 37.989 23.929 3146.153 4.292 106.435 3.450 0.59 285255. 0.4715
|
|
40.73 0.2926 0.5953 0.0760 0.0373 4.209 37.899 23.073 3138.713 4.282 102.630 3.334 0.59 285696. 0.4475
|
|
44.43 0.3192 0.6278 0.0729 0.0371 4.181 37.642 22.153 3117.410 4.253 98.536 3.223 0.59 286164. 0.4239
|
|
48.13 0.3458 0.6575 0.0697 0.0367 4.132 37.202 21.166 3080.979 4.203 94.148 3.116 0.59 286661. 0.4006
|
|
51.83 0.3723 0.6846 0.0662 0.0360 4.061 36.563 20.113 3028.094 4.131 89.462 3.013 0.59 287185. 0.3775
|
|
55.53 0.3989 0.7091 0.0625 0.0352 3.966 35.711 18.992 2957.534 4.035 84.475 2.913 0.59 287736. 0.3547
|
|
59.24 0.4255 0.7311 0.0586 0.0341 3.847 34.642 17.808 2868.975 3.914 79.210 2.815 0.59 288316. 0.3320
|
|
62.94 0.4521 0.7506 0.0546 0.0329 3.705 33.359 16.570 2762.735 3.769 73.702 2.720 0.59 288924. 0.3094
|
|
66.64 0.4787 0.7674 0.0503 0.0314 3.539 31.868 15.284 2639.288 3.600 67.983 2.627 0.59 289560. 0.2869
|
|
70.34 0.5053 0.7812 0.0460 0.0297 3.351 30.176 13.958 2499.142 3.409 62.086 2.533 0.59 290224. 0.2644
|
|
74.05 0.5319 0.7918 0.0415 0.0279 3.142 28.289 12.598 2342.825 3.196 56.038 2.439 0.59 290915. 0.2419
|
|
77.75 0.5585 0.7984 0.0369 0.0258 2.911 26.213 11.211 2170.916 2.962 49.869 2.342 0.59 291634. 0.2191
|
|
81.45 0.5851 0.8003 0.0323 0.0236 2.661 23.957 9.804 1984.080 2.707 43.606 2.241 0.59 292381. 0.1961
|
|
85.15 0.6117 0.7959 0.0276 0.0212 2.391 21.530 8.381 1783.105 2.432 37.280 2.132 0.59 293156. 0.1725
|
|
88.86 0.6383 0.7829 0.0229 0.0187 2.104 18.944 6.952 1568.944 2.140 30.923 2.010 0.60 293958. 0.1481
|
|
92.56 0.6649 0.7571 0.0182 0.0160 1.801 16.213 5.523 1342.760 1.832 24.568 1.866 0.60 294789. 0.1225
|
|
96.26 0.6915 0.7102 0.0135 0.0132 1.483 13.354 4.104 1105.970 1.509 18.252 1.683 0.60 295647. 0.0953
|
|
99.96 0.7181 0.6243 0.0089 0.0102 1.154 10.388 2.702 860.293 1.174 12.019 1.425 0.60 296532. 0.0654
|
|
103.67 0.7447 0.4507 0.0044 0.0072 0.815 7.338 1.329 607.757 0.829 5.911 0.992 0.60 297445. 0.0319
|
|
107.37 0.7713 -0.0059 0.0000 0.0042 0.469 4.224 -0.010 349.797 0.477 -0.043 -0.013 0.60 298369. 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 0.0980 0.0332 5.592 44.059 38.860 4170.147 4.978 172.849 4.227 0.67 322520. 0.7362
|
|
4.23 0.0266 0.0758 0.0969 0.0339 5.712 45.006 38.440 4259.800 5.085 170.980 4.093 0.67 322749. 0.7090
|
|
8.45 0.0531 0.1468 0.0957 0.0347 5.831 45.938 37.969 4347.988 5.190 168.885 3.961 0.67 323001. 0.6819
|
|
12.68 0.0797 0.2130 0.0944 0.0353 5.945 46.837 37.443 4433.070 5.292 166.546 3.831 0.67 323277. 0.6550
|
|
16.91 0.1063 0.2746 0.0929 0.0360 6.052 47.684 36.857 4513.307 5.387 163.940 3.704 0.67 323579. 0.6283
|
|
21.14 0.1329 0.3317 0.0913 0.0366 6.151 48.461 36.206 4586.823 5.475 161.046 3.580 0.67 323907. 0.6019
|
|
25.36 0.1594 0.3847 0.0895 0.0371 6.238 49.146 35.487 4651.618 5.552 157.844 3.460 0.67 324263. 0.5759
|
|
29.59 0.1860 0.4338 0.0875 0.0375 6.310 49.716 34.693 4705.602 5.617 154.314 3.344 0.67 324647. 0.5503
|
|
33.82 0.2126 0.4791 0.0853 0.0378 6.365 50.150 33.822 4746.652 5.666 150.440 3.232 0.67 325060. 0.5252
|
|
38.04 0.2391 0.5210 0.0829 0.0380 6.400 50.424 32.870 4772.614 5.697 146.205 3.124 0.67 325504. 0.5004
|
|
42.27 0.2657 0.5596 0.0803 0.0381 6.412 50.516 31.834 4781.338 5.707 141.597 3.020 0.67 325978. 0.4761
|
|
46.50 0.2923 0.5952 0.0774 0.0380 6.398 50.404 30.712 4770.738 5.695 136.605 2.920 0.67 326483. 0.4521
|
|
50.72 0.3188 0.6279 0.0744 0.0378 6.355 50.067 29.501 4738.801 5.657 131.222 2.824 0.67 327019. 0.4285
|
|
54.95 0.3454 0.6579 0.0711 0.0373 6.281 49.484 28.202 4683.592 5.591 125.441 2.731 0.67 327587. 0.4052
|
|
59.18 0.3720 0.6854 0.0676 0.0367 6.173 48.633 26.811 4603.116 5.495 119.255 2.642 0.67 328187. 0.3822
|
|
63.41 0.3986 0.7103 0.0639 0.0358 6.029 47.496 25.328 4495.474 5.366 112.660 2.555 0.67 328818. 0.3594
|
|
67.63 0.4251 0.7329 0.0599 0.0347 5.847 46.065 23.760 4360.049 5.204 105.686 2.472 0.67 329482. 0.3366
|
|
71.86 0.4517 0.7529 0.0558 0.0335 5.629 44.346 22.117 4197.312 5.010 98.377 2.390 0.67 330177. 0.3141
|
|
76.09 0.4783 0.7704 0.0515 0.0319 5.375 42.346 20.409 4008.001 4.784 90.778 2.310 0.67 330904. 0.2915
|
|
80.31 0.5048 0.7850 0.0470 0.0302 5.086 40.073 18.645 3792.906 4.527 82.933 2.230 0.67 331663. 0.2690
|
|
84.54 0.5314 0.7965 0.0424 0.0283 4.764 37.537 16.834 3552.853 4.241 74.879 2.149 0.68 332453. 0.2464
|
|
88.77 0.5580 0.8043 0.0378 0.0262 4.410 34.747 14.985 3288.747 3.926 66.655 2.067 0.68 333274. 0.2235
|
|
93.00 0.5845 0.8075 0.0330 0.0239 4.025 31.713 13.107 3001.610 3.583 58.300 1.981 0.68 334128. 0.2004
|
|
97.22 0.6111 0.8047 0.0283 0.0215 3.611 28.449 11.208 2692.656 3.214 49.854 1.888 0.68 335012. 0.1766
|
|
101.45 0.6377 0.7937 0.0234 0.0188 3.169 24.970 9.299 2363.360 2.821 41.360 1.785 0.68 335929. 0.1520
|
|
105.68 0.6643 0.7703 0.0186 0.0161 2.703 21.294 7.388 2015.510 2.406 32.863 1.663 0.68 336876. 0.1263
|
|
109.90 0.6908 0.7264 0.0138 0.0132 2.214 17.447 5.489 1651.328 1.971 24.415 1.508 0.68 337856. 0.0987
|
|
114.13 0.7174 0.6439 0.0091 0.0101 1.708 13.455 3.613 1273.547 1.520 16.072 1.287 0.68 338866. 0.0683
|
|
118.36 0.7440 0.4717 0.0045 0.0071 1.187 9.355 1.775 885.458 1.057 7.894 0.909 0.68 339908. 0.0338
|
|
122.58 0.7705 -0.0091 0.0000 0.0039 0.656 5.171 -0.018 489.411 0.584 -0.081 -0.017 0.69 340961. 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 0.0994 0.0345 8.271 57.920 49.906 6167.338 6.544 221.984 3.670 0.75 362790. 0.7245
|
|
4.75 0.0265 0.0742 0.0984 0.0352 8.432 59.051 49.405 6287.823 6.672 219.754 3.564 0.75 363047. 0.6999
|
|
9.49 0.0530 0.1439 0.0973 0.0359 8.591 60.165 48.839 6406.394 6.797 217.237 3.458 0.75 363330. 0.6752
|
|
14.24 0.0796 0.2093 0.0960 0.0365 8.745 61.240 48.202 6520.849 6.919 214.404 3.353 0.75 363641. 0.6504
|
|
18.99 0.1061 0.2705 0.0946 0.0371 8.889 62.254 47.488 6628.875 7.033 211.225 3.249 0.75 363980. 0.6256
|
|
23.74 0.1326 0.3275 0.0930 0.0377 9.022 63.185 46.689 6727.926 7.139 207.671 3.148 0.75 364350. 0.6009
|
|
28.48 0.1591 0.3806 0.0912 0.0381 9.139 64.005 45.799 6815.248 7.231 203.712 3.048 0.75 364750. 0.5763
|
|
33.23 0.1857 0.4299 0.0893 0.0386 9.237 64.687 44.811 6887.920 7.308 199.321 2.951 0.75 365183. 0.5519
|
|
37.98 0.2122 0.4756 0.0871 0.0389 9.311 65.203 43.722 6942.865 7.367 194.474 2.856 0.75 365649. 0.5277
|
|
42.73 0.2387 0.5178 0.0847 0.0391 9.356 65.523 42.524 6976.937 7.403 189.149 2.765 0.75 366148. 0.5037
|
|
47.47 0.2652 0.5568 0.0821 0.0391 9.370 65.617 41.216 6986.916 7.413 183.328 2.676 0.75 366683. 0.4800
|
|
52.22 0.2918 0.5928 0.0793 0.0390 9.346 65.454 39.792 6969.611 7.395 176.996 2.590 0.75 367252. 0.4564
|
|
56.97 0.3183 0.6260 0.0762 0.0387 9.282 65.006 38.252 6921.899 7.344 170.144 2.507 0.75 367856. 0.4332
|
|
61.71 0.3448 0.6564 0.0729 0.0383 9.174 64.244 36.592 6840.712 7.258 162.763 2.426 0.75 368495. 0.4101
|
|
66.46 0.3713 0.6843 0.0693 0.0376 9.016 63.138 34.812 6722.931 7.133 154.845 2.349 0.75 369171. 0.3872
|
|
71.21 0.3979 0.7098 0.0656 0.0367 8.804 61.659 32.910 6565.447 6.966 146.385 2.274 0.76 369882. 0.3644
|
|
75.96 0.4244 0.7328 0.0615 0.0356 8.538 59.794 30.894 6366.934 6.756 137.414 2.201 0.76 370629. 0.3418
|
|
80.70 0.4509 0.7536 0.0573 0.0343 8.218 57.550 28.775 6127.940 6.502 127.993 2.130 0.76 371411. 0.3192
|
|
85.45 0.4774 0.7718 0.0529 0.0327 7.844 54.936 26.569 5849.586 6.207 118.180 2.060 0.76 372228. 0.2967
|
|
90.20 0.5040 0.7873 0.0484 0.0310 7.420 51.964 24.288 5533.115 5.871 108.031 1.991 0.76 373082. 0.2742
|
|
94.95 0.5305 0.7997 0.0437 0.0290 6.946 48.646 21.942 5179.893 5.496 97.597 1.921 0.76 373970. 0.2515
|
|
99.69 0.5570 0.8086 0.0389 0.0268 6.425 44.998 19.544 4791.430 5.084 86.930 1.850 0.76 374893. 0.2285
|
|
104.44 0.5835 0.8129 0.0341 0.0245 5.860 41.036 17.104 4369.500 4.636 76.078 1.775 0.76 375852. 0.2052
|
|
109.19 0.6101 0.8113 0.0292 0.0219 5.252 36.779 14.635 3916.270 4.155 65.095 1.695 0.76 376845. 0.1812
|
|
113.94 0.6366 0.8014 0.0242 0.0192 4.606 32.254 12.148 3434.428 3.644 54.036 1.604 0.76 377874. 0.1562
|
|
118.68 0.6631 0.7786 0.0192 0.0164 3.926 27.492 9.659 2927.358 3.106 42.961 1.497 0.77 378938. 0.1300
|
|
123.43 0.6896 0.7345 0.0143 0.0134 3.217 22.532 7.180 2399.267 2.546 31.936 1.357 0.77 380037. 0.1016
|
|
128.18 0.7162 0.6496 0.0094 0.0104 2.488 17.424 4.729 1855.272 1.969 21.033 1.156 0.77 381171. 0.0702
|
|
132.92 0.7427 0.4719 0.0046 0.0073 1.745 12.222 2.323 1301.428 1.381 10.335 0.810 0.77 382340. 0.0345
|
|
137.67 0.7692 -0.0092 0.0000 0.0042 0.995 6.971 -0.025 742.266 0.788 -0.111 -0.015 0.77 383521. 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 0.1010 0.0389 12.775 80.520 62.588 9526.521 9.097 278.392 2.980 0.83 403038. 0.6587
|
|
5.27 0.0265 0.0673 0.1001 0.0394 12.953 81.643 62.025 9659.327 9.224 275.885 2.912 0.83 403323. 0.6409
|
|
10.54 0.0530 0.1314 0.0990 0.0399 13.123 82.714 61.381 9786.096 9.345 273.025 2.845 0.83 403637. 0.6228
|
|
15.80 0.0795 0.1924 0.0979 0.0404 13.281 83.710 60.650 9903.824 9.457 269.771 2.778 0.83 403981. 0.6044
|
|
21.07 0.1060 0.2504 0.0965 0.0408 13.423 84.601 59.820 10009.327 9.558 266.081 2.711 0.83 404358. 0.5858
|
|
26.34 0.1324 0.3053 0.0950 0.0412 13.544 85.363 58.883 10099.455 9.644 261.912 2.644 0.83 404769. 0.5670
|
|
31.61 0.1589 0.3573 0.0933 0.0415 13.639 85.967 57.829 10170.890 9.712 257.223 2.579 0.83 405215. 0.5480
|
|
36.87 0.1854 0.4064 0.0914 0.0417 13.706 86.384 56.649 10220.273 9.760 251.976 2.514 0.83 405696. 0.5287
|
|
42.14 0.2119 0.4526 0.0893 0.0418 13.738 86.586 55.336 10244.176 9.782 246.137 2.450 0.83 406215. 0.5092
|
|
47.41 0.2384 0.4961 0.0869 0.0418 13.731 86.544 53.883 10239.119 9.778 239.673 2.387 0.84 406772. 0.4896
|
|
52.68 0.2649 0.5368 0.0844 0.0416 13.681 86.226 52.284 10201.573 9.742 232.558 2.325 0.84 407367. 0.4696
|
|
57.94 0.2914 0.5749 0.0815 0.0413 13.582 85.604 50.533 10127.982 9.672 224.771 2.263 0.84 408001. 0.4495
|
|
63.21 0.3179 0.6103 0.0785 0.0409 13.430 84.648 48.628 10014.825 9.563 216.297 2.202 0.84 408675. 0.4291
|
|
68.48 0.3444 0.6432 0.0751 0.0402 13.221 83.328 46.566 9858.633 9.414 207.124 2.142 0.84 409388. 0.4085
|
|
73.75 0.3708 0.6735 0.0715 0.0394 12.949 81.612 44.345 9655.697 9.221 197.244 2.083 0.84 410140. 0.3876
|
|
79.02 0.3973 0.7012 0.0677 0.0384 12.608 79.468 41.962 9402.044 8.978 186.648 2.024 0.84 410932. 0.3664
|
|
84.28 0.4238 0.7265 0.0636 0.0371 12.197 76.877 39.427 9095.496 8.686 175.372 1.966 0.84 411764. 0.3450
|
|
89.55 0.4503 0.7491 0.0593 0.0356 11.716 73.844 36.756 8736.591 8.343 163.491 1.908 0.84 412634. 0.3233
|
|
94.82 0.4768 0.7688 0.0548 0.0340 11.171 70.408 33.966 8330.050 7.955 151.080 1.849 0.84 413544. 0.3012
|
|
100.09 0.5033 0.7852 0.0501 0.0321 10.562 66.570 31.073 7875.999 7.521 138.212 1.789 0.84 414493. 0.2787
|
|
105.35 0.5298 0.7977 0.0453 0.0301 9.893 62.356 28.092 7377.488 7.045 124.954 1.727 0.84 415481. 0.2558
|
|
110.62 0.5563 0.8056 0.0404 0.0279 9.168 57.787 25.038 6836.862 6.529 111.371 1.661 0.85 416507. 0.2322
|
|
115.89 0.5828 0.8078 0.0354 0.0255 8.388 52.870 21.927 6255.178 5.973 97.532 1.590 0.85 417572. 0.2080
|
|
121.16 0.6092 0.8023 0.0303 0.0230 7.560 47.649 18.773 5637.382 5.383 83.503 1.510 0.85 418676. 0.1829
|
|
126.42 0.6357 0.7856 0.0252 0.0204 6.691 42.170 15.592 4989.233 4.764 69.355 1.417 0.85 419818. 0.1564
|
|
131.69 0.6622 0.7521 0.0200 0.0176 5.791 36.498 12.402 4318.151 4.124 55.164 1.303 0.85 420998. 0.1282
|
|
136.96 0.6887 0.6914 0.0149 0.0148 4.871 30.700 9.222 3632.155 3.468 41.018 1.152 0.85 422218. 0.0977
|
|
142.23 0.7152 0.5841 0.0098 0.0120 3.944 24.856 6.073 2940.755 2.808 27.015 0.937 0.85 423475. 0.0645
|
|
147.50 0.7417 0.3879 0.0048 0.0092 3.023 19.050 2.981 2253.879 2.152 13.258 0.600 0.86 424771. 0.0289
|
|
152.76 0.7682 -0.0078 -0.0001 0.0064 2.116 13.336 -0.040 1577.827 1.507 -0.180 -0.012 0.86 426087. 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 0.1013 0.0468 20.489 117.396 75.994 15278.297 13.263 338.022 2.256 0.92 443321. 0.5495
|
|
5.83 0.0266 0.0566 0.1006 0.0474 20.720 118.722 75.435 15450.802 13.413 335.533 2.214 0.92 443630. 0.5374
|
|
11.66 0.0533 0.1110 0.0997 0.0478 20.931 119.933 74.784 15608.490 13.550 332.641 2.173 0.92 443971. 0.5251
|
|
17.48 0.0799 0.1635 0.0987 0.0483 21.114 120.982 74.031 15744.977 13.668 329.288 2.133 0.92 444347. 0.5127
|
|
23.31 0.1066 0.2139 0.0976 0.0486 21.260 121.819 73.158 15853.870 13.763 325.409 2.093 0.92 444760. 0.5002
|
|
29.14 0.1332 0.2625 0.0962 0.0488 21.361 122.395 72.154 15928.819 13.828 320.940 2.055 0.92 445211. 0.4876
|
|
34.97 0.1598 0.3092 0.0947 0.0489 21.408 122.664 71.002 15963.842 13.858 315.816 2.017 0.92 445702. 0.4750
|
|
40.79 0.1865 0.3543 0.0929 0.0489 21.394 122.585 69.689 15953.582 13.850 309.978 1.981 0.92 446234. 0.4621
|
|
46.62 0.2131 0.3978 0.0909 0.0487 21.314 122.123 68.204 15893.501 13.797 303.371 1.946 0.92 446808. 0.4491
|
|
52.45 0.2398 0.4397 0.0887 0.0484 21.161 121.249 66.534 15779.728 13.699 295.945 1.912 0.92 447425. 0.4359
|
|
58.28 0.2664 0.4801 0.0862 0.0479 20.932 119.938 64.671 15609.146 13.551 287.658 1.879 0.92 448087. 0.4223
|
|
64.10 0.2930 0.5189 0.0835 0.0471 20.624 118.171 62.607 15379.117 13.351 278.477 1.846 0.92 448792. 0.4082
|
|
69.93 0.3197 0.5561 0.0805 0.0463 20.232 115.927 60.336 15087.071 13.097 268.373 1.814 0.92 449542. 0.3937
|
|
75.76 0.3463 0.5916 0.0771 0.0452 19.755 113.194 57.853 14731.389 12.789 257.329 1.781 0.92 450337. 0.3786
|
|
81.59 0.3730 0.6253 0.0736 0.0439 19.192 109.965 55.158 14311.118 12.424 245.341 1.748 0.92 451176. 0.3628
|
|
87.41 0.3996 0.6569 0.0697 0.0424 18.538 106.221 52.247 13823.960 12.001 232.396 1.714 0.92 452059. 0.3462
|
|
93.24 0.4262 0.6865 0.0655 0.0407 17.795 101.962 49.133 13269.645 11.520 218.542 1.679 0.92 452987. 0.3289
|
|
99.07 0.4529 0.7137 0.0611 0.0388 16.965 97.207 45.835 12650.807 10.982 203.876 1.643 0.93 453958. 0.3109
|
|
104.90 0.4795 0.7383 0.0565 0.0367 16.056 91.999 42.378 11973.086 10.394 188.499 1.605 0.93 454973. 0.2920
|
|
110.72 0.5062 0.7581 0.0517 0.0345 15.104 86.541 38.780 11262.750 9.777 172.492 1.562 0.93 456032. 0.2717
|
|
116.55 0.5328 0.7727 0.0468 0.0322 14.102 80.804 35.062 10516.021 9.129 155.955 1.512 0.93 457133. 0.2502
|
|
122.38 0.5595 0.7786 0.0417 0.0299 13.093 75.022 31.241 9763.564 8.476 138.961 1.451 0.93 458276. 0.2267
|
|
128.21 0.5861 0.7704 0.0364 0.0277 12.129 69.495 27.332 9044.289 7.852 121.574 1.371 0.93 459463. 0.2002
|
|
134.04 0.6127 0.7504 0.0312 0.0254 11.131 63.777 23.369 8300.186 7.206 103.944 1.277 0.93 460692. 0.1725
|
|
139.86 0.6394 0.7143 0.0258 0.0231 10.115 57.959 19.374 7542.899 6.548 86.175 1.165 0.94 461963. 0.1433
|
|
145.69 0.6660 0.6566 0.0205 0.0208 9.097 52.123 15.375 6783.409 5.889 68.388 1.028 0.94 463277. 0.1126
|
|
151.52 0.6927 0.5693 0.0152 0.0185 8.094 46.378 11.404 6035.750 5.240 50.726 0.857 0.94 464633. 0.0809
|
|
157.35 0.7193 0.4416 0.0100 0.0163 7.122 40.810 7.497 5311.141 4.611 33.346 0.640 0.94 466032. 0.0490
|
|
163.17 0.7459 0.2592 0.0049 0.0142 6.195 35.495 3.690 4619.461 4.010 16.415 0.362 0.94 467474. 0.0194
|
|
169.00 0.7726 0.0001 0.0000 0.0121 5.303 30.387 0.001 3954.699 3.433 0.003 0.000 0.94 468963. 0.0000
|
|
|
|
|
|
|