427 lines
76 KiB
Plaintext
427 lines
76 KiB
Plaintext
20x15(WCAR-T6) (20x15(WCAR-T6).dat)
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v2022-0915
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Simulation Date: 10/10/2023
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AIRFOIL AERO DATA GENERATED USING: POLAR DIAGRAMS
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====== PERFORMANCE DATA (versus advance ratio and MPH) ======
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DEFINITIONS:
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J=V/nD (advance ratio)
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Ct=T/(rho * n**2 * D**4) (thrust coef.)
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Cp=P/(rho * n**3 * D**5) (power coef.)
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Pe=Ct*J/Cp (efficiency)
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V (model speed in MPH)
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Mach (at prop tip)
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Reyn (at 75% of span)
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FOM (Figure of Merit)
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PROP RPM = 1000
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V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
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(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
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0.00 0.0000 0.0000 0.1035 0.0454 0.012 0.737 0.528 8.722 0.083 2.347 27.434 0.08 38073. 0.5846
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0.59 0.0309 0.0684 0.1028 0.0464 0.012 0.754 0.524 8.916 0.085 2.332 26.665 0.08 38104. 0.5664
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1.17 0.0618 0.1328 0.1020 0.0475 0.012 0.770 0.520 9.113 0.087 2.314 25.891 0.08 38139. 0.5479
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1.76 0.0927 0.1933 0.1011 0.0485 0.012 0.787 0.515 9.308 0.089 2.293 25.120 0.08 38178. 0.5291
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2.34 0.1236 0.2500 0.1000 0.0494 0.013 0.802 0.510 9.494 0.091 2.268 24.358 0.08 38221. 0.5103
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2.93 0.1545 0.3028 0.0987 0.0503 0.013 0.817 0.503 9.666 0.092 2.238 23.610 0.08 38269. 0.4913
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3.51 0.1854 0.3522 0.0971 0.0511 0.013 0.829 0.495 9.813 0.094 2.202 22.882 0.08 38322. 0.4723
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4.10 0.2163 0.3982 0.0952 0.0517 0.013 0.839 0.485 9.928 0.095 2.159 22.177 0.08 38380. 0.4533
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4.68 0.2472 0.4412 0.0930 0.0521 0.013 0.845 0.474 10.000 0.095 2.108 21.499 0.08 38443. 0.4342
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5.27 0.2781 0.4814 0.0904 0.0522 0.013 0.847 0.461 10.025 0.096 2.050 20.849 0.08 38511. 0.4152
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5.85 0.3090 0.5189 0.0874 0.0521 0.013 0.845 0.446 9.998 0.095 1.983 20.228 0.08 38585. 0.3963
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6.44 0.3399 0.5540 0.0842 0.0517 0.013 0.838 0.429 9.919 0.095 1.910 19.631 0.08 38664. 0.3774
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7.02 0.3708 0.5866 0.0807 0.0510 0.013 0.827 0.411 9.789 0.093 1.829 19.055 0.08 38748. 0.3585
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7.61 0.4017 0.6168 0.0768 0.0500 0.013 0.812 0.392 9.610 0.092 1.743 18.495 0.08 38837. 0.3397
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8.19 0.4326 0.6445 0.0728 0.0489 0.013 0.793 0.371 9.383 0.090 1.651 17.946 0.08 38932. 0.3208
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8.78 0.4635 0.6697 0.0686 0.0475 0.012 0.770 0.350 9.112 0.087 1.555 17.403 0.08 39032. 0.3019
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9.36 0.4944 0.6921 0.0641 0.0458 0.012 0.744 0.327 8.798 0.084 1.455 16.860 0.08 39137. 0.2829
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9.95 0.5253 0.7114 0.0595 0.0440 0.011 0.714 0.304 8.443 0.081 1.351 16.313 0.08 39248. 0.2637
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10.53 0.5562 0.7275 0.0548 0.0419 0.011 0.680 0.280 8.048 0.077 1.243 15.754 0.08 39364. 0.2444
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11.12 0.5871 0.7397 0.0500 0.0397 0.010 0.644 0.255 7.616 0.073 1.133 15.176 0.08 39485. 0.2247
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11.70 0.6180 0.7475 0.0450 0.0372 0.010 0.604 0.230 7.146 0.068 1.021 14.568 0.08 39611. 0.2048
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12.29 0.6489 0.7498 0.0400 0.0346 0.009 0.561 0.204 6.641 0.063 0.906 13.918 0.08 39743. 0.1843
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12.87 0.6797 0.7454 0.0348 0.0318 0.008 0.516 0.178 6.100 0.058 0.790 13.207 0.08 39879. 0.1633
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13.46 0.7106 0.7322 0.0297 0.0288 0.007 0.467 0.151 5.527 0.053 0.673 12.409 0.08 40021. 0.1416
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14.04 0.7415 0.7071 0.0244 0.0256 0.007 0.416 0.125 4.923 0.047 0.554 11.484 0.08 40168. 0.1189
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14.63 0.7724 0.6647 0.0192 0.0223 0.006 0.363 0.098 4.290 0.041 0.436 10.364 0.08 40320. 0.0952
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15.21 0.8033 0.5956 0.0140 0.0189 0.005 0.307 0.071 3.631 0.035 0.318 8.929 0.08 40476. 0.0700
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15.80 0.8342 0.4805 0.0088 0.0154 0.004 0.249 0.045 2.949 0.028 0.201 6.937 0.08 40637. 0.0432
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16.39 0.8651 0.2740 0.0037 0.0117 0.003 0.190 0.019 2.243 0.021 0.084 3.814 0.08 40798. 0.0154
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16.97 0.8960
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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 0.1038 0.0419 0.086 2.722 2.117 64.415 0.308 9.418 14.908 0.16 76145. 0.6364
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1.16 0.0306 0.0735 0.1032 0.0430 0.089 2.792 2.104 66.055 0.315 9.360 14.449 0.16 76207. 0.6149
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2.32 0.0613 0.1424 0.1024 0.0441 0.091 2.862 2.089 67.730 0.323 9.292 13.989 0.16 76276. 0.5932
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3.48 0.0919 0.2066 0.1015 0.0452 0.093 2.933 2.071 69.405 0.331 9.211 13.533 0.16 76353. 0.5714
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4.64 0.1226 0.2663 0.1005 0.0462 0.095 3.002 2.049 71.036 0.339 9.115 13.084 0.16 76438. 0.5495
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5.80 0.1532 0.3217 0.0992 0.0472 0.097 3.067 2.023 72.569 0.346 8.998 12.644 0.16 76533. 0.5276
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6.96 0.1838 0.3730 0.0976 0.0481 0.099 3.125 1.992 73.936 0.353 8.859 12.218 0.16 76638. 0.5059
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8.12 0.2145 0.4205 0.0958 0.0489 0.101 3.172 1.954 75.065 0.358 8.691 11.807 0.16 76752. 0.4842
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9.28 0.2451 0.4645 0.0936 0.0494 0.102 3.207 1.909 75.887 0.362 8.493 11.413 0.16 76876. 0.4627
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10.45 0.2758 0.5054 0.0911 0.0497 0.102 3.227 1.858 76.349 0.365 8.264 11.037 0.16 77011. 0.4414
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11.61 0.3064 0.5433 0.0882 0.0497 0.102 3.230 1.799 76.418 0.365 8.003 10.679 0.16 77156. 0.4202
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12.77 0.3370 0.5786 0.0850 0.0495 0.102 3.215 1.734 76.080 0.363 7.713 10.337 0.16 77312. 0.3994
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13.93 0.3677 0.6112 0.0815 0.0490 0.101 3.184 1.663 75.335 0.360 7.396 10.011 0.16 77478. 0.3787
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15.09 0.3983 0.6413 0.0778 0.0483 0.099 3.135 1.586 74.190 0.354 7.055 9.696 0.16 77654. 0.3583
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16.25 0.4289 0.6690 0.0738 0.0473 0.097 3.071 1.505 72.659 0.347 6.692 9.392 0.16 77841. 0.3380
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17.41 0.4596 0.6942 0.0696 0.0461 0.095 2.990 1.419 70.753 0.338 6.311 9.096 0.16 78038. 0.3179
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18.57 0.4902 0.7168 0.0652 0.0446 0.092 2.894 1.329 68.487 0.327 5.914 8.805 0.16 78245. 0.2978
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19.73 0.5209 0.7366 0.0606 0.0429 0.088 2.784 1.237 65.870 0.315 5.501 8.517 0.16 78463. 0.2779
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20.89 0.5515 0.7536 0.0560 0.0410 0.084 2.659 1.141 62.911 0.300 5.077 8.229 0.16 78691. 0.2579
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22.05 0.5821 0.7673 0.0512 0.0388 0.080 2.520 1.043 59.620 0.285 4.641 7.937 0.16 78930. 0.2379
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23.21 0.6128 0.7773 0.0462 0.0365 0.075 2.367 0.943 56.002 0.267 4.195 7.639 0.16 79179. 0.2176
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24.37 0.6434 0.7829 0.0412 0.0339 0.070 2.200 0.841 52.066 0.249 3.742 7.328 0.16 79438. 0.1972
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25.53 0.6741 0.7832 0.0362 0.0311 0.064 2.021 0.738 47.819 0.228 3.281 6.997 0.16 79707. 0.1763
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26.69 0.7047 0.7765 0.0310 0.0282 0.058 1.829 0.633 43.272 0.207 2.816 6.636 0.16 79986. 0.1549
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27.85 0.7353 0.7605 0.0259 0.0250 0.052 1.625 0.528 38.442 0.184 2.348 6.228 0.16 80276. 0.1327
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29.01 0.7660 0.7308 0.0207 0.0217 0.045 1.409 0.422 33.349 0.159 1.879 5.745 0.16 80575. 0.1096
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30.17 0.7966 0.6796 0.0156 0.0182 0.038 1.184 0.317 28.015 0.134 1.411 5.138 0.16 80884. 0.0849
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31.34 0.8273 0.5906 0.0104 0.0146 0.030 0.949 0.213 22.461 0.107 0.947 4.299 0.16 81201. 0.0582
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32.50 0.8579 0.4227 0.0054 0.0109 0.022 0.705 0.109 16.692 0.080 0.486 2.967 0.16 81522. 0.0288
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33.66 0.8885 0.0206 0.0002 0.0069 0.014 0.445 0.003 10.523 0.050 0.014 0.140 0.16 81787. 0.0002
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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 0.1041 0.0405 0.282 5.917 4.778 210.028 0.669 21.253 10.318 0.24 114215. 0.6617
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1.75 0.0308 0.0765 0.1035 0.0416 0.289 6.079 4.750 215.767 0.687 21.127 9.985 0.24 114307. 0.6384
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3.50 0.0615 0.1479 0.1028 0.0428 0.297 6.245 4.716 221.653 0.706 20.978 9.651 0.24 114411. 0.6149
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5.24 0.0923 0.2143 0.1019 0.0439 0.305 6.412 4.676 227.570 0.724 20.800 9.320 0.24 114528. 0.5913
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6.99 0.1231 0.2758 0.1009 0.0450 0.313 6.575 4.628 233.370 0.743 20.587 8.996 0.24 114657. 0.5678
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8.74 0.1538 0.3326 0.0996 0.0461 0.320 6.730 4.570 238.864 0.760 20.329 8.679 0.24 114800. 0.5443
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10.49 0.1846 0.3850 0.0981 0.0470 0.327 6.870 4.500 243.825 0.776 20.018 8.372 0.24 114958. 0.5211
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12.24 0.2154 0.4333 0.0962 0.0478 0.333 6.987 4.416 248.000 0.789 19.643 8.077 0.24 115130. 0.4980
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13.99 0.2461 0.4779 0.0940 0.0484 0.337 7.076 4.316 251.147 0.799 19.197 7.795 0.24 115318. 0.4751
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15.73 0.2769 0.5191 0.0915 0.0488 0.339 7.130 4.199 253.079 0.806 18.679 7.526 0.24 115521. 0.4525
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17.48 0.3077 0.5573 0.0886 0.0489 0.340 7.147 4.067 253.674 0.807 18.089 7.271 0.24 115741. 0.4302
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19.23 0.3385 0.5926 0.0854 0.0488 0.339 7.125 3.919 252.875 0.805 17.431 7.029 0.24 115976. 0.4082
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20.98 0.3692 0.6252 0.0819 0.0483 0.336 7.062 3.757 250.672 0.798 16.712 6.798 0.24 116227. 0.3866
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22.73 0.4000 0.6553 0.0781 0.0477 0.331 6.961 3.583 247.084 0.786 15.937 6.577 0.24 116493. 0.3653
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24.47 0.4308 0.6829 0.0740 0.0467 0.325 6.822 3.398 242.145 0.771 15.114 6.365 0.24 116776. 0.3442
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26.22 0.4615 0.7080 0.0698 0.0455 0.316 6.646 3.203 235.895 0.751 14.247 6.159 0.24 117074. 0.3234
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27.97 0.4923 0.7306 0.0654 0.0440 0.306 6.434 3.000 228.372 0.727 13.342 5.958 0.24 117388. 0.3027
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29.72 0.5231 0.7505 0.0608 0.0424 0.294 6.187 2.789 219.607 0.699 12.405 5.760 0.24 117717. 0.2822
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31.47 0.5538 0.7676 0.0560 0.0404 0.281 5.906 2.572 209.631 0.667 11.439 5.564 0.24 118062. 0.2618
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33.22 0.5846 0.7817 0.0512 0.0383 0.266 5.592 2.349 198.466 0.632 10.448 5.368 0.24 118423. 0.2414
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34.96 0.6154 0.7923 0.0462 0.0359 0.250 5.244 2.121 186.134 0.592 9.435 5.169 0.24 118799. 0.2209
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36.71 0.6461 0.7989 0.0412 0.0333 0.232 4.865 1.890 172.660 0.550 8.405 4.964 0.24 119191. 0.2002
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38.46 0.6769 0.8004 0.0361 0.0305 0.212 4.454 1.654 158.073 0.503 7.359 4.747 0.24 119598. 0.1791
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40.21 0.7077 0.7956 0.0309 0.0275 0.191 4.012 1.417 142.412 0.453 6.303 4.513 0.24 120021. 0.1576
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41.96 0.7384 0.7818 0.0257 0.0243 0.169 3.542 1.178 125.732 0.400 5.241 4.251 0.24 120458. 0.1354
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43.71 0.7692 0.7551 0.0205 0.0209 0.145 3.046 0.939 108.107 0.344 4.178 3.941 0.25 120910. 0.1121
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45.45 0.8000 0.7073 0.0153 0.0173 0.120 2.525 0.701 89.617 0.285 3.119 3.549 0.25 121377. 0.0872
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47.20 0.8307 0.6204 0.0101 0.0136 0.094 1.982 0.465 70.333 0.224 2.068 2.998 0.25 121855. 0.0600
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48.95 0.8615 0.4456 0.0050 0.0097 0.067 1.416 0.230 50.263 0.160 1.023 2.076 0.25 122339. 0.0292
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50.70 0.8923 -0.0576 -0.0004 0.0054 0.038 0.793 -0.016 28.135 0.090 -0.071 -0.259 0.25 122624. 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 0.1045 0.0398 0.656 10.338 8.523 489.237 1.168 37.910 7.902 0.32 152282. 0.6768
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2.35 0.0310 0.0785 0.1039 0.0410 0.675 10.634 8.475 503.264 1.201 37.695 7.638 0.32 152406. 0.6523
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4.69 0.0619 0.1517 0.1032 0.0421 0.694 10.939 8.417 517.702 1.236 37.440 7.375 0.32 152545. 0.6277
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7.04 0.0929 0.2195 0.1023 0.0433 0.714 11.247 8.348 532.274 1.271 37.134 7.114 0.32 152701. 0.6030
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9.38 0.1239 0.2821 0.1013 0.0445 0.733 11.551 8.265 546.625 1.305 36.764 6.858 0.32 152875. 0.5785
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11.73 0.1548 0.3398 0.1001 0.0456 0.751 11.839 8.164 560.297 1.338 36.314 6.609 0.32 153067. 0.5540
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14.07 0.1858 0.3929 0.0986 0.0466 0.768 12.102 8.041 572.732 1.367 35.766 6.368 0.32 153279. 0.5298
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16.42 0.2168 0.4418 0.0967 0.0475 0.782 12.326 7.892 583.307 1.393 35.103 6.137 0.32 153512. 0.5058
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18.77 0.2477 0.4867 0.0946 0.0481 0.793 12.497 7.714 591.421 1.412 34.311 5.916 0.32 153765. 0.4820
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21.11 0.2787 0.5281 0.0920 0.0485 0.800 12.607 7.506 596.600 1.424 33.385 5.706 0.32 154039. 0.4587
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23.46 0.3096 0.5664 0.0891 0.0487 0.803 12.647 7.268 598.536 1.429 32.328 5.508 0.32 154335. 0.4356
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25.80 0.3406 0.6018 0.0858 0.0486 0.801 12.616 7.002 597.072 1.425 31.147 5.319 0.32 154652. 0.4130
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28.15 0.3716 0.6344 0.0823 0.0482 0.794 12.513 6.711 592.171 1.414 29.852 5.141 0.32 154990. 0.3907
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30.50 0.4025 0.6644 0.0784 0.0475 0.783 12.338 6.398 583.872 1.394 28.457 4.970 0.32 155350. 0.3688
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32.84 0.4335 0.6920 0.0743 0.0466 0.767 12.092 6.064 572.251 1.366 26.971 4.806 0.32 155732. 0.3472
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35.19 0.4645 0.7170 0.0700 0.0454 0.747 11.778 5.712 557.397 1.331 25.407 4.648 0.32 156134. 0.3259
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37.53 0.4954 0.7395 0.0655 0.0439 0.723 11.398 5.345 539.396 1.288 23.775 4.495 0.32 156557. 0.3049
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39.88 0.5264 0.7595 0.0609 0.0422 0.695 10.953 4.965 518.325 1.237 22.083 4.344 0.32 157002. 0.2840
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42.22 0.5574 0.7767 0.0560 0.0402 0.663 10.444 4.572 494.251 1.180 20.338 4.196 0.32 157468. 0.2632
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44.57 0.5883 0.7910 0.0511 0.0380 0.627 9.873 4.170 467.229 1.115 18.549 4.048 0.32 157955. 0.2425
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46.92 0.6193 0.8019 0.0461 0.0356 0.586 9.241 3.759 437.312 1.044 16.721 3.899 0.32 158463. 0.2218
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49.26 0.6503 0.8089 0.0410 0.0329 0.543 8.549 3.341 404.558 0.966 14.861 3.746 0.32 158991. 0.2009
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51.61 0.6812 0.8111 0.0358 0.0300 0.495 7.798 2.917 369.041 0.881 12.975 3.585 0.32 159540. 0.1796
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53.95 0.7122 0.8070 0.0305 0.0269 0.444 6.991 2.489 330.862 0.790 11.070 3.412 0.33 160110. 0.1579
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56.30 0.7432 0.7942 0.0252 0.0236 0.389 6.131 2.059 290.165 0.693 9.157 3.218 0.33 160701. 0.1355
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58.65 0.7741 0.7684 0.0200 0.0201 0.331 5.222 1.628 247.132 0.590 7.243 2.989 0.33 161311. 0.1119
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60.99 0.8051 0.7206 0.0147 0.0164 0.271 4.268 1.200 201.965 0.482 5.338 2.695 0.33 161940. 0.0866
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63.34 0.8360 0.6303 0.0095 0.0126 0.208 3.272 0.775 154.829 0.370 3.447 2.270 0.33 162585. 0.0586
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65.68 0.8670 0.4353 0.0043 0.0086 0.142 2.233 0.352 105.686 0.252 1.567 1.512 0.33 163231. 0.0263
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68.03 0.8980
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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 0.1049 0.0395 1.271 16.024 13.370 947.921 1.810 59.468 6.397 0.40 190344. 0.6863
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2.92 0.0308 0.0791 0.1043 0.0407 1.309 16.495 13.299 975.788 1.864 59.155 6.182 0.40 190498. 0.6614
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5.84 0.0616 0.1527 0.1037 0.0419 1.347 16.982 13.215 1004.575 1.919 58.781 5.967 0.40 190671. 0.6364
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8.76 0.0925 0.2209 0.1029 0.0431 1.386 17.475 13.114 1033.759 1.974 58.331 5.754 0.40 190864. 0.6113
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11.68 0.1233 0.2838 0.1019 0.0443 1.425 17.964 12.991 1062.660 2.030 57.784 5.545 0.40 191080. 0.5863
|
|
14.59 0.1541 0.3417 0.1007 0.0454 1.462 18.433 12.841 1090.402 2.083 57.115 5.341 0.40 191319. 0.5615
|
|
17.51 0.1849 0.3950 0.0993 0.0465 1.496 18.864 12.656 1115.894 2.131 56.296 5.144 0.40 191582. 0.5369
|
|
20.43 0.2158 0.4439 0.0975 0.0474 1.526 19.236 12.432 1137.906 2.173 55.297 4.955 0.40 191870. 0.5126
|
|
23.35 0.2466 0.4888 0.0954 0.0481 1.549 19.529 12.162 1155.227 2.206 54.097 4.775 0.40 192184. 0.4886
|
|
26.27 0.2774 0.5302 0.0929 0.0486 1.565 19.725 11.845 1166.866 2.229 52.685 4.604 0.40 192525. 0.4649
|
|
29.19 0.3082 0.5685 0.0901 0.0488 1.572 19.815 11.480 1172.157 2.239 51.064 4.442 0.40 192892. 0.4416
|
|
32.11 0.3391 0.6037 0.0869 0.0488 1.570 19.791 11.071 1170.740 2.236 49.244 4.289 0.40 193286. 0.4187
|
|
35.03 0.3699 0.6363 0.0833 0.0484 1.559 19.651 10.621 1162.497 2.220 47.242 4.144 0.40 193706. 0.3962
|
|
37.95 0.4007 0.6664 0.0795 0.0478 1.539 19.398 10.134 1147.480 2.192 45.076 4.006 0.40 194153. 0.3741
|
|
40.86 0.4315 0.6939 0.0754 0.0469 1.510 19.032 9.615 1125.827 2.150 42.766 3.874 0.40 194626. 0.3524
|
|
43.78 0.4624 0.7191 0.0711 0.0457 1.472 18.556 9.067 1097.708 2.096 40.329 3.746 0.40 195126. 0.3310
|
|
46.70 0.4932 0.7418 0.0666 0.0443 1.426 17.974 8.494 1063.293 2.031 37.781 3.623 0.40 195651. 0.3098
|
|
49.62 0.5240 0.7621 0.0620 0.0426 1.372 17.289 7.899 1022.737 1.953 35.137 3.503 0.40 196203. 0.2889
|
|
52.54 0.5548 0.7798 0.0572 0.0407 1.309 16.502 7.286 976.173 1.864 32.409 3.385 0.40 196782. 0.2681
|
|
55.46 0.5857 0.7947 0.0522 0.0385 1.239 15.615 6.656 923.716 1.764 29.608 3.269 0.40 197386. 0.2474
|
|
58.38 0.6165 0.8065 0.0472 0.0361 1.161 14.630 6.013 865.472 1.653 26.745 3.151 0.40 198016. 0.2267
|
|
61.30 0.6473 0.8146 0.0420 0.0334 1.075 13.550 5.357 801.554 1.531 23.829 3.032 0.40 198672. 0.2059
|
|
64.22 0.6781 0.8184 0.0368 0.0305 0.982 12.376 4.692 732.102 1.398 20.872 2.907 0.41 199353. 0.1848
|
|
67.13 0.7089 0.8166 0.0315 0.0274 0.881 11.112 4.021 657.312 1.255 17.884 2.774 0.41 200060. 0.1632
|
|
70.05 0.7398 0.8070 0.0262 0.0241 0.774 9.762 3.345 577.452 1.103 14.880 2.628 0.41 200792. 0.1410
|
|
72.97 0.7706 0.7858 0.0209 0.0205 0.661 8.332 2.669 492.878 0.941 11.873 2.456 0.41 201549. 0.1177
|
|
75.89 0.8014 0.7456 0.0157 0.0168 0.542 6.829 1.996 403.988 0.772 8.878 2.241 0.41 202329. 0.0929
|
|
78.81 0.8322 0.6686 0.0104 0.0130 0.417 5.259 1.327 311.124 0.594 5.904 1.935 0.41 203130. 0.0654
|
|
81.73 0.8631 0.5029 0.0052 0.0089 0.287 3.623 0.663 214.328 0.409 2.950 1.404 0.41 203938. 0.0335
|
|
84.65 0.8939 -0.0632 -0.0003 0.0044 0.143 1.798 -0.040 106.343 0.203 -0.178 -0.170 0.41 204302. 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 0.1054 0.0394 2.193 23.038 19.340 1635.423 2.603 86.022 5.364 0.48 228400. 0.6920
|
|
3.56 0.0314 0.0809 0.1048 0.0406 2.260 23.743 19.245 1685.467 2.683 85.600 5.179 0.48 228588. 0.6665
|
|
7.13 0.0627 0.1560 0.1042 0.0419 2.330 24.475 19.130 1737.395 2.765 85.092 4.994 0.48 228799. 0.6409
|
|
10.69 0.0941 0.2255 0.1035 0.0432 2.401 25.220 18.991 1790.267 2.849 84.474 4.812 0.48 229036. 0.6152
|
|
14.25 0.1254 0.2894 0.1025 0.0444 2.471 25.960 18.820 1842.849 2.933 83.713 4.632 0.48 229300. 0.5896
|
|
17.82 0.1568 0.3481 0.1014 0.0457 2.539 26.674 18.609 1893.509 3.014 82.771 4.457 0.48 229594. 0.5641
|
|
21.38 0.1881 0.4019 0.0999 0.0468 2.602 27.332 18.346 1940.206 3.088 81.602 4.289 0.48 229918. 0.5389
|
|
24.94 0.2195 0.4513 0.0982 0.0478 2.656 27.901 18.022 1980.615 3.152 80.161 4.127 0.48 230273. 0.5140
|
|
28.50 0.2508 0.4965 0.0960 0.0485 2.699 28.349 17.628 2012.434 3.203 78.411 3.973 0.48 230661. 0.4894
|
|
32.07 0.2822 0.5381 0.0935 0.0490 2.727 28.650 17.162 2033.794 3.237 76.338 3.827 0.48 231081. 0.4652
|
|
35.63 0.3135 0.5764 0.0906 0.0493 2.740 28.786 16.624 2043.428 3.252 73.944 3.690 0.48 231535. 0.4414
|
|
39.19 0.3449 0.6117 0.0873 0.0492 2.737 28.747 16.018 2040.656 3.248 71.246 3.560 0.48 232022. 0.4180
|
|
42.76 0.3763 0.6443 0.0836 0.0488 2.716 28.530 15.348 2025.266 3.223 68.270 3.437 0.48 232542. 0.3951
|
|
46.32 0.4076 0.6743 0.0797 0.0482 2.679 28.137 14.623 1997.367 3.179 65.045 3.321 0.48 233096. 0.3726
|
|
49.88 0.4390 0.7018 0.0754 0.0472 2.625 27.572 13.849 1957.234 3.115 61.600 3.209 0.48 233682. 0.3504
|
|
53.45 0.4703 0.7269 0.0710 0.0459 2.555 26.839 13.032 1905.201 3.032 57.965 3.102 0.48 234301. 0.3286
|
|
57.01 0.5017 0.7495 0.0663 0.0444 2.470 25.943 12.177 1841.592 2.931 54.164 2.999 0.48 234952. 0.3070
|
|
60.57 0.5330 0.7697 0.0615 0.0426 2.369 24.888 11.290 1766.698 2.812 50.218 2.899 0.48 235636. 0.2857
|
|
64.13 0.5644 0.7872 0.0565 0.0405 2.254 23.677 10.375 1680.776 2.675 46.148 2.800 0.48 236352. 0.2646
|
|
67.70 0.5957 0.8019 0.0514 0.0382 2.124 22.315 9.436 1584.044 2.521 41.971 2.702 0.48 237101. 0.2435
|
|
71.26 0.6271 0.8133 0.0462 0.0356 1.980 20.803 8.476 1476.712 2.350 37.702 2.603 0.49 237881. 0.2224
|
|
74.82 0.6584 0.8210 0.0409 0.0328 1.822 19.144 7.499 1359.009 2.163 33.357 2.503 0.49 238693. 0.2011
|
|
78.39 0.6898 0.8240 0.0355 0.0297 1.651 17.344 6.509 1231.232 1.960 28.954 2.398 0.49 239538. 0.1795
|
|
81.95 0.7212 0.8209 0.0300 0.0264 1.467 15.408 5.510 1093.790 1.741 24.510 2.285 0.49 240413. 0.1574
|
|
85.51 0.7525 0.8091 0.0246 0.0228 1.270 13.344 4.507 947.248 1.508 20.049 2.158 0.49 241320. 0.1344
|
|
89.08 0.7839 0.7836 0.0191 0.0191 1.063 11.161 3.505 792.316 1.261 15.591 2.007 0.49 242256. 0.1102
|
|
92.64 0.8152 0.7338 0.0137 0.0152 0.844 8.871 2.508 629.723 1.002 11.158 1.807 0.49 243221. 0.0840
|
|
96.20 0.8466 0.6318 0.0083 0.0111 0.617 6.480 1.519 459.965 0.732 6.757 1.498 0.49 244207. 0.0542
|
|
99.76 0.8779 0.3739 0.0029 0.0068 0.378 3.975 0.532 282.140 0.449 2.366 0.855 0.49 245169. 0.0183
|
|
103.33 0.9093
|
|
|
|
|
|
|
|
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 0.1059 0.0396 3.495 31.466 26.457 2605.979 3.555 117.679 4.605 0.56 266450. 0.6949
|
|
4.10 0.0310 0.0800 0.1054 0.0408 3.602 32.433 26.342 2686.078 3.664 117.171 4.448 0.56 266665. 0.6698
|
|
8.21 0.0619 0.1544 0.1049 0.0420 3.714 33.442 26.205 2769.582 3.778 116.560 4.292 0.56 266907. 0.6445
|
|
12.31 0.0929 0.2233 0.1042 0.0433 3.829 34.474 26.037 2855.108 3.895 115.811 4.136 0.56 267179. 0.6192
|
|
16.42 0.1238 0.2867 0.1034 0.0446 3.944 35.509 25.828 2940.824 4.012 114.884 3.984 0.56 267481. 0.5940
|
|
20.52 0.1548 0.3450 0.1023 0.0459 4.056 36.517 25.568 3024.261 4.126 113.725 3.835 0.56 267816. 0.5688
|
|
24.63 0.1858 0.3984 0.1010 0.0471 4.160 37.459 25.241 3102.271 4.232 112.273 3.690 0.56 268186. 0.5440
|
|
28.73 0.2167 0.4474 0.0994 0.0481 4.253 38.291 24.834 3171.172 4.326 110.463 3.552 0.56 268592. 0.5193
|
|
32.84 0.2477 0.4923 0.0974 0.0490 4.328 38.967 24.335 3227.197 4.402 108.242 3.420 0.56 269035. 0.4950
|
|
36.94 0.2786 0.5336 0.0950 0.0496 4.381 39.449 23.736 3267.118 4.457 105.579 3.295 0.56 269515. 0.4710
|
|
41.04 0.3096 0.5717 0.0922 0.0499 4.410 39.709 23.038 3288.613 4.486 102.472 3.177 0.56 270034. 0.4474
|
|
45.15 0.3405 0.6069 0.0890 0.0500 4.412 39.729 22.244 3290.316 4.489 98.939 3.066 0.56 270591. 0.4243
|
|
49.25 0.3715 0.6394 0.0855 0.0497 4.387 39.504 21.360 3271.682 4.463 95.011 2.961 0.56 271186. 0.4015
|
|
53.36 0.4025 0.6694 0.0816 0.0491 4.335 39.034 20.397 3232.756 4.410 90.727 2.862 0.56 271818. 0.3792
|
|
57.46 0.4334 0.6971 0.0775 0.0482 4.256 38.324 19.364 3173.946 4.330 86.129 2.767 0.56 272488. 0.3572
|
|
61.57 0.4644 0.7224 0.0731 0.0470 4.152 37.381 18.268 3095.810 4.223 81.256 2.676 0.56 273196. 0.3356
|
|
65.67 0.4953 0.7454 0.0685 0.0455 4.022 36.211 17.119 2998.912 4.091 76.144 2.589 0.56 273940. 0.3143
|
|
69.77 0.5263 0.7661 0.0637 0.0438 3.867 34.820 15.923 2883.773 3.934 70.824 2.504 0.56 274722. 0.2932
|
|
73.88 0.5573 0.7843 0.0588 0.0418 3.689 33.215 14.686 2750.835 3.753 65.324 2.422 0.56 275540. 0.2723
|
|
77.98 0.5882 0.7999 0.0537 0.0395 3.487 31.400 13.415 2600.501 3.548 59.669 2.340 0.56 276395. 0.2514
|
|
82.09 0.6192 0.8126 0.0485 0.0369 3.263 29.379 12.114 2433.129 3.319 53.881 2.258 0.57 277286. 0.2306
|
|
86.19 0.6501 0.8220 0.0432 0.0341 3.016 27.157 10.787 2249.087 3.068 47.982 2.175 0.57 278214. 0.2096
|
|
90.30 0.6811 0.8274 0.0378 0.0311 2.748 24.739 9.441 2048.822 2.795 41.994 2.090 0.57 279177. 0.1884
|
|
94.40 0.7121 0.8275 0.0323 0.0278 2.458 22.132 8.080 1832.926 2.500 35.941 2.000 0.57 280176. 0.1668
|
|
98.51 0.7430 0.8205 0.0269 0.0243 2.149 19.346 6.711 1602.213 2.186 29.852 1.900 0.57 281211. 0.1444
|
|
102.61 0.7740 0.8026 0.0214 0.0206 1.821 16.394 5.341 1357.743 1.852 23.757 1.784 0.57 282280. 0.1210
|
|
106.71 0.8049 0.7665 0.0159 0.0167 1.476 13.290 3.976 1100.687 1.502 17.684 1.638 0.57 283382. 0.0958
|
|
110.82 0.8359 0.6937 0.0105 0.0126 1.116 10.046 2.619 832.014 1.135 11.651 1.428 0.57 284513. 0.0678
|
|
114.92 0.8668 0.5265 0.0051 0.0084 0.740 6.662 1.271 551.727 0.753 5.654 1.045 0.58 285649. 0.0346
|
|
119.03 0.8978 -0.1556 -0.0006 0.0036 0.318 2.862 -0.156 237.017 0.323 -0.693 -0.298 0.58 285302. 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 0.1065 0.0399 5.260 41.445 34.745 3922.737 4.682 154.547 4.017 0.63 304493. 0.6948
|
|
4.71 0.0311 0.0801 0.1061 0.0411 5.424 42.734 34.616 4044.743 4.828 153.973 3.882 0.63 304738. 0.6701
|
|
9.42 0.0621 0.1546 0.1056 0.0424 5.596 44.086 34.460 4172.755 4.981 153.277 3.746 0.63 305015. 0.6451
|
|
14.12 0.0932 0.2235 0.1050 0.0438 5.773 45.482 34.266 4304.841 5.139 152.416 3.610 0.63 305325. 0.6200
|
|
18.83 0.1243 0.2870 0.1043 0.0451 5.952 46.892 34.023 4438.342 5.298 151.335 3.477 0.64 305671. 0.5950
|
|
23.54 0.1554 0.3453 0.1033 0.0465 6.128 48.278 33.715 4569.528 5.454 149.963 3.347 0.64 306055. 0.5701
|
|
28.25 0.1864 0.3987 0.1021 0.0477 6.294 49.589 33.321 4693.567 5.603 148.212 3.220 0.64 306479. 0.5453
|
|
32.95 0.2175 0.4476 0.1006 0.0489 6.443 50.762 32.822 4804.622 5.735 145.992 3.098 0.64 306945. 0.5208
|
|
37.66 0.2486 0.4924 0.0987 0.0498 6.566 51.734 32.199 4896.568 5.845 143.223 2.983 0.64 307453. 0.4965
|
|
42.37 0.2796 0.5336 0.0964 0.0505 6.657 52.446 31.442 4963.992 5.925 139.855 2.873 0.64 308006. 0.4726
|
|
47.08 0.3107 0.5716 0.0936 0.0509 6.709 52.857 30.548 5002.849 5.972 135.877 2.770 0.64 308602. 0.4491
|
|
51.78 0.3418 0.6066 0.0905 0.0510 6.719 52.939 29.520 5010.639 5.981 131.306 2.672 0.64 309243. 0.4260
|
|
56.49 0.3728 0.6391 0.0869 0.0507 6.687 52.681 28.369 4986.260 5.952 126.184 2.581 0.64 309929. 0.4032
|
|
61.20 0.4039 0.6691 0.0831 0.0501 6.611 52.083 27.105 4929.674 5.884 120.561 2.494 0.64 310658. 0.3809
|
|
65.91 0.4350 0.6968 0.0789 0.0492 6.493 51.152 25.741 4841.524 5.779 114.496 2.411 0.64 311430. 0.3590
|
|
70.61 0.4661 0.7222 0.0744 0.0480 6.333 49.897 24.291 4722.771 5.637 108.045 2.333 0.64 312246. 0.3373
|
|
75.32 0.4971 0.7454 0.0698 0.0465 6.134 48.330 22.765 4574.429 5.460 101.259 2.257 0.64 313104. 0.3160
|
|
80.03 0.5282 0.7663 0.0649 0.0447 5.897 46.460 21.174 4397.421 5.249 94.184 2.184 0.64 314005. 0.2948
|
|
84.74 0.5593 0.7848 0.0598 0.0426 5.622 44.295 19.527 4192.529 5.004 86.858 2.113 0.64 314948. 0.2739
|
|
89.45 0.5903 0.8008 0.0546 0.0403 5.311 41.843 17.832 3960.440 4.727 79.316 2.042 0.65 315934. 0.2530
|
|
94.15 0.6214 0.8140 0.0493 0.0377 4.964 39.111 16.095 3701.800 4.419 71.590 1.972 0.65 316961. 0.2321
|
|
98.86 0.6525 0.8239 0.0439 0.0348 4.583 36.104 14.323 3417.244 4.079 63.710 1.901 0.65 318029. 0.2111
|
|
103.57 0.6835 0.8300 0.0384 0.0316 4.167 32.832 12.524 3107.511 3.709 55.706 1.828 0.65 319139. 0.1898
|
|
108.28 0.7146 0.8309 0.0328 0.0282 3.719 29.304 10.704 2773.566 3.311 47.613 1.751 0.65 320290. 0.1680
|
|
112.98 0.7457 0.8249 0.0272 0.0246 3.241 25.533 8.873 2416.716 2.885 39.468 1.665 0.65 321482. 0.1455
|
|
117.69 0.7768 0.8081 0.0216 0.0207 2.734 21.539 7.040 2038.632 2.433 31.314 1.566 0.65 322713. 0.1219
|
|
122.40 0.8078 0.7731 0.0160 0.0167 2.201 17.339 5.213 1641.140 1.959 23.187 1.441 0.66 323981. 0.0965
|
|
127.11 0.8389 0.7005 0.0104 0.0125 1.644 12.950 3.397 1225.697 1.463 15.111 1.257 0.66 325281. 0.0680
|
|
131.81 0.8700 0.5264 0.0049 0.0081 1.062 8.369 1.591 792.097 0.945 7.076 0.911 0.66 326583. 0.0337
|
|
136.52 0.9010
|
|
|
|
|
|
|
|
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 0.1071 0.0412 7.736 54.173 44.213 5768.381 6.120 196.661 3.477 0.71 342527. 0.6782
|
|
5.27 0.0309 0.0778 0.1067 0.0424 7.963 55.765 44.080 5937.897 6.300 196.067 3.367 0.71 342800. 0.6559
|
|
10.55 0.0619 0.1506 0.1063 0.0437 8.202 57.443 43.918 6116.575 6.490 195.345 3.257 0.71 343108. 0.6332
|
|
15.82 0.0928 0.2182 0.1058 0.0450 8.451 59.185 43.715 6302.006 6.687 194.445 3.146 0.71 343453. 0.6103
|
|
21.10 0.1238 0.2808 0.1052 0.0464 8.704 60.957 43.457 6490.748 6.887 193.299 3.037 0.71 343838. 0.5873
|
|
26.37 0.1547 0.3386 0.1044 0.0477 8.955 62.714 43.124 6677.853 7.085 191.818 2.929 0.71 344266. 0.5643
|
|
31.64 0.1856 0.3917 0.1034 0.0490 9.195 64.393 42.691 6856.615 7.275 189.890 2.824 0.72 344738. 0.5413
|
|
36.92 0.2166 0.4406 0.1020 0.0501 9.412 65.916 42.129 7018.768 7.447 187.389 2.722 0.72 345256. 0.5184
|
|
42.19 0.2475 0.4855 0.1003 0.0511 9.595 67.199 41.412 7155.360 7.592 184.200 2.625 0.72 345823. 0.4956
|
|
47.46 0.2785 0.5269 0.0981 0.0518 9.733 68.164 40.522 7258.117 7.701 180.242 2.532 0.72 346440. 0.4729
|
|
52.74 0.3094 0.5651 0.0955 0.0523 9.817 68.750 39.452 7320.564 7.767 175.481 2.444 0.72 347106. 0.4504
|
|
58.01 0.3403 0.6005 0.0925 0.0524 9.841 68.918 38.202 7338.423 7.786 169.924 2.361 0.72 347822. 0.4282
|
|
63.29 0.3713 0.6332 0.0891 0.0522 9.802 68.647 36.783 7309.573 7.756 163.613 2.282 0.72 348589. 0.4061
|
|
68.56 0.4022 0.6636 0.0853 0.0517 9.700 67.934 35.210 7233.603 7.675 156.612 2.208 0.72 349405. 0.3843
|
|
73.83 0.4332 0.6916 0.0811 0.0508 9.536 66.784 33.498 7111.225 7.545 148.997 2.137 0.72 350270. 0.3628
|
|
79.11 0.4641 0.7173 0.0767 0.0496 9.312 65.211 31.665 6943.715 7.368 140.845 2.068 0.72 351183. 0.3415
|
|
84.38 0.4950 0.7409 0.0720 0.0481 9.028 63.227 29.727 6732.465 7.143 132.228 2.003 0.72 352145. 0.3204
|
|
89.65 0.5260 0.7622 0.0671 0.0463 8.688 60.845 27.700 6478.790 6.874 123.210 1.939 0.72 353154. 0.2994
|
|
94.93 0.5569 0.7813 0.0620 0.0442 8.293 58.074 25.595 6183.804 6.561 113.847 1.877 0.73 354210. 0.2787
|
|
100.20 0.5878 0.7980 0.0567 0.0418 7.843 54.925 23.423 5848.485 6.205 104.187 1.817 0.73 355313. 0.2579
|
|
105.48 0.6188 0.8120 0.0513 0.0391 7.341 51.407 21.194 5473.864 5.808 94.271 1.756 0.73 356462. 0.2372
|
|
110.75 0.6497 0.8231 0.0458 0.0362 6.787 47.530 18.917 5060.995 5.370 84.141 1.695 0.73 357658. 0.2163
|
|
116.02 0.6807 0.8306 0.0402 0.0329 6.184 43.304 16.600 4611.038 4.892 73.837 1.633 0.73 358900. 0.1952
|
|
121.30 0.7116 0.8334 0.0345 0.0295 5.532 38.743 14.255 4125.414 4.377 63.404 1.567 0.73 360187. 0.1736
|
|
126.57 0.7425 0.8299 0.0288 0.0258 4.836 33.865 11.891 3605.993 3.826 52.890 1.496 0.73 361519. 0.1513
|
|
131.84 0.7735 0.8170 0.0231 0.0218 4.097 28.692 9.521 3055.178 3.242 42.349 1.413 0.74 362895. 0.1280
|
|
137.12 0.8044 0.7881 0.0173 0.0177 3.320 23.250 7.156 2475.665 2.627 31.830 1.311 0.74 364314. 0.1029
|
|
142.39 0.8354 0.7274 0.0116 0.0134 2.507 17.560 4.804 1869.818 1.984 21.366 1.165 0.74 365769. 0.0749
|
|
147.67 0.8663 0.5840 0.0060 0.0088 1.661 11.629 2.463 1238.288 1.314 10.956 0.902 0.74 367236. 0.0415
|
|
152.94 0.8972 -0.0031 0.0000 0.0038 0.723 5.060 -0.005 538.829 0.572 -0.024 -0.005 0.74 367965. 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 0.1075 0.0457 11.774 74.210 54.809 8779.859 8.384 243.792 2.831 0.79 380550. 0.6150
|
|
5.88 0.0311 0.0710 0.1072 0.0469 12.073 76.094 54.680 9002.786 8.597 243.214 2.755 0.79 380853. 0.5976
|
|
11.77 0.0621 0.1381 0.1069 0.0481 12.389 78.083 54.522 9238.139 8.822 242.514 2.677 0.79 381195. 0.5799
|
|
17.65 0.0932 0.2010 0.1065 0.0494 12.717 80.150 54.325 9482.695 9.055 241.637 2.598 0.79 381578. 0.5619
|
|
23.53 0.1242 0.2600 0.1060 0.0507 13.051 82.255 54.070 9731.763 9.293 240.504 2.520 0.79 382006. 0.5437
|
|
29.41 0.1553 0.3149 0.1054 0.0520 13.381 84.340 53.734 9978.415 9.529 239.009 2.442 0.79 382480. 0.5253
|
|
35.30 0.1864 0.3662 0.1045 0.0532 13.696 86.323 53.285 10213.027 9.753 237.011 2.366 0.79 383005. 0.5068
|
|
41.18 0.2174 0.4139 0.1033 0.0543 13.978 88.100 52.685 10423.270 9.953 234.344 2.293 0.80 383582. 0.4882
|
|
47.06 0.2485 0.4584 0.1018 0.0552 14.209 89.554 51.898 10595.320 10.118 230.842 2.222 0.80 384213. 0.4696
|
|
52.94 0.2795 0.5000 0.0998 0.0558 14.371 90.575 50.894 10716.130 10.233 226.376 2.154 0.80 384900. 0.4509
|
|
58.83 0.3106 0.5390 0.0974 0.0561 14.450 91.076 49.656 10775.403 10.290 220.872 2.090 0.80 385644. 0.4321
|
|
64.71 0.3417 0.5758 0.0945 0.0561 14.438 91.002 48.182 10766.661 10.281 214.312 2.030 0.80 386446. 0.4134
|
|
70.59 0.3727 0.6104 0.0912 0.0557 14.332 90.332 46.477 10687.366 10.206 206.729 1.972 0.80 387304. 0.3945
|
|
76.47 0.4038 0.6429 0.0874 0.0549 14.132 89.072 44.558 10538.268 10.063 198.195 1.918 0.80 388219. 0.3756
|
|
82.36 0.4348 0.6734 0.0832 0.0538 13.842 87.245 42.447 10322.138 9.857 188.806 1.865 0.80 389190. 0.3565
|
|
88.24 0.4659 0.7018 0.0788 0.0523 13.468 84.884 40.167 10042.805 9.590 178.665 1.814 0.80 390215. 0.3373
|
|
94.12 0.4970 0.7279 0.0740 0.0505 13.013 82.021 37.741 9704.081 9.267 167.873 1.764 0.80 391294. 0.3179
|
|
100.00 0.5280 0.7517 0.0690 0.0485 12.484 78.683 35.189 9309.076 8.890 156.522 1.715 0.80 392427. 0.2984
|
|
105.89 0.5591 0.7730 0.0638 0.0461 11.882 74.887 32.529 8860.045 8.461 144.691 1.665 0.81 393613. 0.2786
|
|
111.77 0.5901 0.7918 0.0584 0.0435 11.209 70.647 29.777 8358.396 7.982 132.449 1.616 0.81 394852. 0.2587
|
|
117.65 0.6212 0.8077 0.0528 0.0406 10.466 65.968 26.946 7804.842 7.453 119.854 1.566 0.81 396142. 0.2385
|
|
123.53 0.6523 0.8204 0.0472 0.0375 9.655 60.856 24.047 7200.003 6.875 106.960 1.515 0.81 397483. 0.2179
|
|
129.42 0.6833 0.8294 0.0414 0.0341 8.777 55.318 21.094 6544.820 6.250 93.824 1.462 0.81 398876. 0.1970
|
|
135.30 0.7144 0.8335 0.0355 0.0304 7.834 49.375 18.099 5841.693 5.578 80.505 1.405 0.81 400320. 0.1754
|
|
141.18 0.7454 0.8307 0.0296 0.0265 6.833 43.066 15.078 5095.175 4.866 67.066 1.342 0.82 401814. 0.1529
|
|
147.06 0.7765 0.8177 0.0236 0.0224 5.776 36.407 12.045 4307.392 4.113 53.577 1.268 0.82 403356. 0.1291
|
|
152.95 0.8076 0.7873 0.0177 0.0181 4.670 29.437 9.016 3482.714 3.326 40.102 1.174 0.82 404946. 0.1034
|
|
158.83 0.8386 0.7212 0.0118 0.0137 3.522 22.199 5.997 2626.435 2.508 26.677 1.036 0.82 406575. 0.0744
|
|
164.71 0.8697 0.5622 0.0059 0.0091 2.335 14.716 2.989 1741.099 1.663 13.294 0.779 0.82 408215. 0.0395
|
|
170.59 0.9007 -0.1024 -0.0004 0.0038 0.983 6.194 -0.221 732.809 0.700 -0.984 -0.137 0.83 408187. 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 0.1073 0.0552 18.919 108.404 66.202 14107.965 12.247 294.466 2.128 0.87 418595. 0.5081
|
|
6.49 0.0311 0.0591 0.1071 0.0564 19.331 110.766 66.091 14415.448 12.514 293.972 2.079 0.87 418924. 0.4960
|
|
12.97 0.0623 0.1154 0.1069 0.0577 19.766 113.255 65.956 14739.325 12.795 293.374 2.030 0.87 419295. 0.4836
|
|
19.46 0.0934 0.1688 0.1066 0.0590 20.216 115.834 65.786 15074.962 13.087 292.618 1.979 0.87 419711. 0.4710
|
|
25.94 0.1245 0.2194 0.1063 0.0603 20.673 118.452 65.563 15415.740 13.383 291.623 1.929 0.87 420177. 0.4582
|
|
32.43 0.1557 0.2672 0.1058 0.0616 21.124 121.036 65.259 15751.933 13.675 290.272 1.879 0.87 420694. 0.4454
|
|
38.92 0.1868 0.3122 0.1051 0.0629 21.550 123.476 64.840 16069.564 13.950 288.407 1.830 0.87 421267. 0.4323
|
|
45.40 0.2179 0.3548 0.1042 0.0640 21.926 125.631 64.259 16350.053 14.194 285.826 1.783 0.87 421897. 0.4192
|
|
51.89 0.2491 0.3952 0.1029 0.0648 22.222 127.331 63.470 16571.211 14.386 282.313 1.737 0.88 422587. 0.4060
|
|
58.37 0.2802 0.4336 0.1012 0.0654 22.409 128.399 62.428 16710.174 14.506 277.678 1.694 0.88 423340. 0.3928
|
|
64.86 0.3113 0.4706 0.0990 0.0655 22.458 128.682 61.102 16747.070 14.538 271.780 1.655 0.88 424157. 0.3795
|
|
71.35 0.3425 0.5062 0.0964 0.0652 22.352 128.075 59.475 16668.064 14.470 264.543 1.618 0.88 425038. 0.3662
|
|
77.83 0.3736 0.5408 0.0933 0.0644 22.083 126.534 57.545 16467.541 14.296 255.958 1.585 0.88 425984. 0.3527
|
|
84.32 0.4047 0.5744 0.0897 0.0632 21.655 124.078 55.325 16147.930 14.018 246.085 1.554 0.88 426995. 0.3391
|
|
90.81 0.4359 0.6070 0.0856 0.0615 21.077 120.766 52.838 15716.817 13.644 235.024 1.525 0.88 428069. 0.3252
|
|
97.29 0.4670 0.6384 0.0812 0.0594 20.364 116.685 50.113 15185.703 13.183 222.904 1.497 0.88 429205. 0.3109
|
|
103.78 0.4981 0.6684 0.0765 0.0570 19.534 111.926 47.181 14566.403 12.645 209.859 1.469 0.88 430402. 0.2961
|
|
110.26 0.5293 0.6966 0.0714 0.0543 18.599 106.572 44.069 13869.591 12.040 196.019 1.441 0.88 431659. 0.2807
|
|
116.75 0.5604 0.7229 0.0661 0.0513 17.572 100.687 40.804 13103.698 11.376 181.496 1.412 0.89 432975. 0.2647
|
|
123.24 0.5915 0.7468 0.0606 0.0480 16.460 94.316 37.408 12274.556 10.656 166.390 1.382 0.89 434349. 0.2480
|
|
129.72 0.6227 0.7680 0.0549 0.0445 15.269 87.487 33.900 11385.862 9.884 150.785 1.350 0.89 435780. 0.2307
|
|
136.21 0.6538 0.7860 0.0491 0.0408 14.000 80.218 30.297 10439.789 9.063 134.759 1.316 0.89 437267. 0.2126
|
|
142.69 0.6849 0.8002 0.0431 0.0369 12.656 72.518 26.616 9437.714 8.193 118.386 1.279 0.89 438811. 0.1936
|
|
149.18 0.7161 0.8095 0.0371 0.0328 11.240 64.406 22.874 8381.929 7.277 101.744 1.238 0.90 440411. 0.1737
|
|
155.67 0.7472 0.8101 0.0309 0.0285 9.780 56.041 19.087 7293.292 6.331 84.898 1.187 0.90 442066. 0.1521
|
|
162.15 0.7783 0.7923 0.0247 0.0243 8.330 47.732 15.264 6211.978 5.393 67.896 1.115 0.90 443774. 0.1278
|
|
168.64 0.8095 0.7473 0.0185 0.0201 6.877 39.404 11.429 5128.208 4.452 50.834 1.011 0.90 445534. 0.1003
|
|
175.12 0.8406 0.6571 0.0123 0.0158 5.399 30.937 7.597 4026.281 3.495 33.792 0.856 0.90 447338. 0.0692
|
|
181.61 0.8717 0.4669 0.0061 0.0114 3.909 22.396 3.768 2914.650 2.530 16.762 0.586 0.91 449155. 0.0334
|
|
188.10 0.9029 -0.0733 -0.0005 0.0063 2.162 12.390 -0.316 1612.503 1.400 -1.405 -0.089 0.91 449583. 0.0000
|
|
|
|
|
|
|