427 lines
76 KiB
Plaintext
427 lines
76 KiB
Plaintext
20.5x13.5EPN (205x135EPN.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 0.0963 0.0388 0.011 0.713 0.542 8.435 0.081 2.411 29.144 0.08 39187. 0.6141
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0.54 0.0279 0.0673 0.0952 0.0395 0.012 0.725 0.536 8.579 0.082 2.383 28.322 0.08 39216. 0.5933
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1.08 0.0558 0.1306 0.0939 0.0401 0.012 0.737 0.529 8.721 0.083 2.352 27.500 0.08 39248. 0.5724
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1.63 0.0837 0.1901 0.0926 0.0408 0.012 0.749 0.521 8.857 0.085 2.318 26.682 0.08 39283. 0.5513
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2.17 0.1116 0.2457 0.0911 0.0414 0.012 0.760 0.513 8.986 0.086 2.280 25.871 0.08 39322. 0.5301
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2.71 0.1395 0.2977 0.0894 0.0419 0.012 0.770 0.503 9.105 0.087 2.238 25.070 0.08 39364. 0.5090
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3.25 0.1674 0.3460 0.0876 0.0424 0.012 0.778 0.493 9.209 0.088 2.193 24.281 0.08 39410. 0.4880
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3.79 0.1953 0.3908 0.0856 0.0428 0.012 0.786 0.482 9.296 0.089 2.143 23.507 0.08 39460. 0.4670
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4.33 0.2232 0.4322 0.0834 0.0431 0.013 0.791 0.470 9.361 0.089 2.088 22.749 0.08 39514. 0.4462
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4.88 0.2511 0.4703 0.0811 0.0433 0.013 0.795 0.456 9.402 0.090 2.029 22.007 0.08 39571. 0.4255
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5.42 0.2790 0.5054 0.0785 0.0433 0.013 0.796 0.442 9.415 0.090 1.965 21.283 0.08 39633. 0.4049
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5.96 0.3069 0.5374 0.0757 0.0432 0.013 0.794 0.426 9.396 0.090 1.896 20.574 0.08 39699. 0.3845
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6.50 0.3348 0.5665 0.0727 0.0430 0.013 0.790 0.409 9.341 0.089 1.821 19.881 0.08 39769. 0.3641
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7.04 0.3627 0.5927 0.0696 0.0426 0.012 0.782 0.391 9.247 0.088 1.741 19.201 0.08 39844. 0.3439
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7.58 0.3906 0.6161 0.0661 0.0419 0.012 0.770 0.372 9.112 0.087 1.656 18.531 0.08 39923. 0.3236
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8.13 0.4185 0.6365 0.0625 0.0411 0.012 0.755 0.352 8.931 0.085 1.565 17.868 0.08 40006. 0.3034
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8.67 0.4464 0.6538 0.0587 0.0401 0.012 0.736 0.330 8.703 0.083 1.469 17.207 0.08 40094. 0.2830
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9.21 0.4743 0.6678 0.0546 0.0388 0.011 0.712 0.307 8.429 0.080 1.367 16.542 0.08 40185. 0.2625
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9.75 0.5023 0.6782 0.0504 0.0373 0.011 0.685 0.284 8.110 0.077 1.262 15.866 0.08 40282. 0.2419
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10.29 0.5302 0.6845 0.0461 0.0357 0.010 0.655 0.259 7.749 0.074 1.153 15.171 0.08 40382. 0.2211
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10.83 0.5581 0.6860 0.0416 0.0338 0.010 0.621 0.234 7.349 0.070 1.041 14.445 0.08 40487. 0.2000
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11.38 0.5860 0.6819 0.0370 0.0318 0.009 0.584 0.208 6.911 0.066 0.927 13.675 0.08 40596. 0.1787
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11.92 0.6139 0.6709 0.0324 0.0296 0.009 0.544 0.182 6.437 0.061 0.811 12.841 0.08 40710. 0.1569
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12.46 0.6418 0.6511 0.0277 0.0273 0.008 0.501 0.156 5.930 0.057 0.693 11.921 0.08 40827. 0.1347
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13.00 0.6697 0.6199 0.0230 0.0248 0.007 0.456 0.129 5.393 0.051 0.575 10.877 0.08 40949. 0.1120
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13.54 0.6976 0.5732 0.0183 0.0222 0.006 0.408 0.103 4.827 0.046 0.457 9.655 0.08 41076. 0.0886
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14.08 0.7255 0.5044 0.0136 0.0195 0.006 0.358 0.076 4.237 0.040 0.339 8.170 0.08 41206. 0.0646
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14.63 0.7534 0.4025 0.0089 0.0167 0.005 0.307 0.050 3.627 0.035 0.223 6.278 0.08 41341. 0.0403
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15.17 0.7813 0.2468 0.0044 0.0138 0.004 0.254 0.025 3.001 0.029 0.109 3.712 0.08 41480. 0.0166
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15.71 0.8092 -0.0056 -0.0001 0.0109 0.003 0.200 0.000 2.364 0.023 -0.002 -0.082 0.08 41623. 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 0.0967 0.0363 0.085 2.664 2.176 63.033 0.301 9.679 15.658 0.16 78373. 0.6611
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1.09 0.0280 0.0724 0.0955 0.0370 0.086 2.715 2.151 64.252 0.307 9.568 15.185 0.16 78431. 0.6374
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2.17 0.0560 0.1402 0.0943 0.0377 0.088 2.766 2.123 65.456 0.313 9.445 14.713 0.16 78495. 0.6137
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3.26 0.0840 0.2037 0.0930 0.0383 0.089 2.816 2.093 66.625 0.318 9.308 14.247 0.16 78566. 0.5899
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4.35 0.1120 0.2628 0.0915 0.0390 0.091 2.863 2.059 67.734 0.323 9.158 13.787 0.16 78644. 0.5662
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5.43 0.1400 0.3177 0.0898 0.0396 0.092 2.906 2.022 68.760 0.328 8.992 13.335 0.16 78729. 0.5427
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6.52 0.1680 0.3686 0.0880 0.0401 0.093 2.945 1.981 69.675 0.333 8.809 12.893 0.16 78821. 0.5193
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7.61 0.1960 0.4157 0.0860 0.0405 0.094 2.977 1.936 70.450 0.336 8.609 12.462 0.16 78921. 0.4962
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8.70 0.2240 0.4591 0.0838 0.0409 0.095 3.003 1.886 71.055 0.339 8.391 12.042 0.16 79029. 0.4734
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9.78 0.2520 0.4990 0.0814 0.0411 0.096 3.020 1.833 71.460 0.341 8.153 11.635 0.16 79145. 0.4509
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10.87 0.2800 0.5356 0.0788 0.0412 0.096 3.027 1.775 71.633 0.342 7.895 11.239 0.16 79270. 0.4286
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11.96 0.3080 0.5690 0.0761 0.0412 0.096 3.024 1.712 71.545 0.342 7.617 10.856 0.16 79402. 0.4066
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13.04 0.3360 0.5995 0.0731 0.0409 0.095 3.007 1.645 71.164 0.340 7.317 10.484 0.16 79544. 0.3849
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14.13 0.3640 0.6271 0.0699 0.0405 0.094 2.978 1.573 70.463 0.336 6.995 10.122 0.16 79694. 0.3633
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15.22 0.3919 0.6518 0.0664 0.0399 0.093 2.934 1.495 69.415 0.331 6.651 9.770 0.16 79853. 0.3419
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16.30 0.4199 0.6737 0.0628 0.0391 0.091 2.873 1.413 67.992 0.325 6.284 9.425 0.16 80020. 0.3206
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17.39 0.4479 0.6927 0.0589 0.0381 0.089 2.797 1.325 66.174 0.316 5.896 9.085 0.16 80196. 0.2994
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18.48 0.4759 0.7087 0.0548 0.0368 0.086 2.703 1.234 63.968 0.305 5.488 8.748 0.16 80381. 0.2781
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19.57 0.5039 0.7214 0.0506 0.0353 0.082 2.594 1.138 61.390 0.293 5.063 8.410 0.16 80575. 0.2568
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20.65 0.5319 0.7304 0.0462 0.0336 0.078 2.470 1.040 58.455 0.279 4.625 8.068 0.16 80777. 0.2355
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21.74 0.5599 0.7352 0.0417 0.0317 0.074 2.332 0.939 55.180 0.263 4.175 7.715 0.17 80988. 0.2139
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22.83 0.5879 0.7350 0.0371 0.0297 0.069 2.180 0.835 51.581 0.246 3.715 7.345 0.17 81208. 0.1921
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23.91 0.6159 0.7285 0.0324 0.0274 0.064 2.015 0.730 47.674 0.228 3.249 6.949 0.17 81436. 0.1700
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25.00 0.6439 0.7141 0.0277 0.0250 0.058 1.837 0.625 43.479 0.208 2.778 6.515 0.17 81673. 0.1474
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26.09 0.6719 0.6888 0.0230 0.0224 0.052 1.649 0.518 39.017 0.186 2.305 6.023 0.17 81919. 0.1241
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27.17 0.6999 0.6484 0.0183 0.0197 0.046 1.450 0.412 34.314 0.164 1.832 5.443 0.17 82173. 0.1000
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28.26 0.7279 0.5851 0.0136 0.0169 0.039 1.242 0.306 29.398 0.140 1.362 4.723 0.17 82435. 0.0748
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29.35 0.7559 0.4845 0.0090 0.0140 0.033 1.027 0.202 24.307 0.116 0.898 3.766 0.17 82707. 0.0484
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30.44 0.7839 0.3159 0.0044 0.0110 0.026 0.806 0.100 19.080 0.091 0.443 2.368 0.17 82986. 0.0214
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31.52 0.8119 0.0008 0.0000 0.0079 0.018 0.582 0.000 13.760 0.066 0.001 0.006 0.17 83273. 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 0.0970 0.0353 0.277 5.828 4.916 206.859 0.658 21.866 10.779 0.24 117556. 0.6841
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1.63 0.0280 0.0748 0.0959 0.0360 0.283 5.947 4.860 211.096 0.672 21.618 10.443 0.24 117644. 0.6590
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3.27 0.0561 0.1448 0.0947 0.0367 0.289 6.066 4.798 215.292 0.685 21.343 10.109 0.24 117741. 0.6338
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4.90 0.0841 0.2101 0.0934 0.0374 0.294 6.181 4.730 219.371 0.698 21.038 9.779 0.24 117847. 0.6087
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6.53 0.1122 0.2708 0.0919 0.0381 0.299 6.290 4.654 223.256 0.711 20.700 9.455 0.24 117964. 0.5838
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8.17 0.1402 0.3272 0.0902 0.0387 0.304 6.392 4.570 226.858 0.722 20.327 9.137 0.24 118092. 0.5591
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9.80 0.1683 0.3793 0.0884 0.0392 0.309 6.482 4.478 230.086 0.732 19.917 8.827 0.24 118231. 0.5346
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11.44 0.1963 0.4274 0.0864 0.0397 0.312 6.560 4.377 232.838 0.741 19.467 8.526 0.24 118382. 0.5105
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13.07 0.2244 0.4717 0.0842 0.0401 0.315 6.621 4.266 235.011 0.748 18.975 8.233 0.24 118544. 0.4867
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14.70 0.2524 0.5124 0.0818 0.0403 0.317 6.663 4.145 236.499 0.753 18.439 7.950 0.24 118719. 0.4633
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16.34 0.2805 0.5498 0.0793 0.0404 0.318 6.683 4.014 237.193 0.755 17.856 7.677 0.24 118906. 0.4402
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17.97 0.3085 0.5839 0.0765 0.0404 0.318 6.677 3.873 236.987 0.754 17.226 7.412 0.25 119106. 0.4175
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19.60 0.3366 0.6150 0.0734 0.0402 0.316 6.643 3.720 235.777 0.751 16.548 7.157 0.25 119319. 0.3951
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21.24 0.3646 0.6433 0.0702 0.0398 0.313 6.578 3.556 233.464 0.743 15.819 6.909 0.25 119545. 0.3730
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22.87 0.3927 0.6687 0.0668 0.0392 0.308 6.479 3.381 229.953 0.732 15.040 6.670 0.25 119784. 0.3510
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24.50 0.4207 0.6914 0.0631 0.0384 0.302 6.343 3.195 225.144 0.717 14.210 6.436 0.25 120036. 0.3293
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26.14 0.4488 0.7113 0.0592 0.0373 0.294 6.169 2.997 218.973 0.697 13.330 6.207 0.25 120302. 0.3076
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27.77 0.4768 0.7283 0.0551 0.0360 0.284 5.958 2.789 211.456 0.673 12.405 5.982 0.25 120580. 0.2860
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29.40 0.5049 0.7423 0.0508 0.0345 0.272 5.709 2.573 202.642 0.645 11.443 5.758 0.25 120872. 0.2644
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31.04 0.5329 0.7528 0.0464 0.0328 0.258 5.426 2.349 192.586 0.613 10.449 5.533 0.25 121177. 0.2427
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32.67 0.5610 0.7595 0.0419 0.0309 0.243 5.109 2.120 181.341 0.577 9.429 5.302 0.25 121494. 0.2210
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34.31 0.5890 0.7614 0.0372 0.0288 0.227 4.760 1.886 168.961 0.538 8.389 5.063 0.25 121825. 0.1990
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35.94 0.6171 0.7576 0.0325 0.0265 0.209 4.381 1.649 155.504 0.495 7.333 4.808 0.25 122169. 0.1767
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37.57 0.6451 0.7463 0.0278 0.0240 0.189 3.973 1.409 141.033 0.449 6.266 4.531 0.25 122526. 0.1539
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39.21 0.6732 0.7248 0.0231 0.0214 0.168 3.539 1.168 125.626 0.400 5.195 4.217 0.25 122895. 0.1304
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40.84 0.7012 0.6886 0.0183 0.0186 0.147 3.081 0.927 109.369 0.348 4.125 3.846 0.25 123278. 0.1060
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42.47 0.7293 0.6295 0.0136 0.0157 0.124 2.602 0.689 92.370 0.294 3.063 3.381 0.25 123673. 0.0803
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44.11 0.7573 0.5314 0.0089 0.0127 0.100 2.106 0.453 74.754 0.238 2.015 2.748 0.25 124081. 0.0529
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45.74 0.7854 0.3567 0.0044 0.0097 0.076 1.597 0.222 56.669 0.180 0.989 1.779 0.25 124502. 0.0240
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47.37 0.8134 -0.0050 0.0000 0.0065 0.051 1.078 -0.002 38.253 0.122 -0.009 -0.024 0.25 124932. 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 0.0975 0.0348 0.649 10.229 8.784 484.108 1.156 39.072 8.230 0.33 156735. 0.6982
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2.18 0.0281 0.0761 0.0965 0.0356 0.663 10.447 8.686 494.382 1.180 38.637 7.969 0.33 156852. 0.6723
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4.36 0.0561 0.1473 0.0952 0.0363 0.677 10.662 8.577 504.569 1.205 38.152 7.710 0.33 156982. 0.6464
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6.54 0.0842 0.2137 0.0939 0.0370 0.690 10.871 8.456 514.488 1.228 37.614 7.455 0.33 157124. 0.6205
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8.72 0.1123 0.2753 0.0924 0.0377 0.703 11.071 8.322 523.950 1.251 37.018 7.205 0.33 157281. 0.5949
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10.90 0.1403 0.3325 0.0908 0.0383 0.714 11.257 8.174 532.745 1.272 36.359 6.959 0.33 157451. 0.5695
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13.08 0.1684 0.3853 0.0890 0.0389 0.725 11.424 8.011 540.645 1.291 35.633 6.721 0.33 157637. 0.5445
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15.26 0.1965 0.4340 0.0870 0.0394 0.734 11.567 7.831 547.409 1.307 34.835 6.489 0.33 157838. 0.5198
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17.43 0.2245 0.4788 0.0848 0.0398 0.741 11.681 7.635 552.787 1.320 33.960 6.265 0.33 158055. 0.4955
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19.61 0.2526 0.5200 0.0824 0.0400 0.746 11.760 7.420 556.519 1.329 33.006 6.048 0.33 158289. 0.4715
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21.79 0.2807 0.5578 0.0798 0.0402 0.749 11.798 7.187 558.344 1.333 31.969 5.839 0.33 158539. 0.4480
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23.97 0.3087 0.5924 0.0770 0.0401 0.748 11.791 6.935 558.003 1.332 30.845 5.637 0.33 158806. 0.4249
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26.15 0.3368 0.6240 0.0740 0.0399 0.745 11.733 6.662 555.243 1.326 29.634 5.442 0.33 159091. 0.4021
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28.33 0.3648 0.6526 0.0707 0.0395 0.737 11.618 6.370 549.824 1.313 28.333 5.255 0.33 159393. 0.3796
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30.51 0.3929 0.6786 0.0673 0.0389 0.726 11.443 6.057 541.515 1.293 26.941 5.073 0.33 159712. 0.3574
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32.69 0.4210 0.7018 0.0636 0.0381 0.711 11.201 5.723 530.076 1.265 25.456 4.897 0.33 160049. 0.3353
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34.87 0.4490 0.7223 0.0596 0.0371 0.691 10.890 5.369 515.343 1.230 23.881 4.725 0.33 160404. 0.3134
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37.05 0.4771 0.7401 0.0555 0.0358 0.667 10.509 4.997 497.348 1.187 22.226 4.557 0.33 160776. 0.2916
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39.23 0.5052 0.7550 0.0512 0.0342 0.639 10.063 4.609 476.206 1.137 20.503 4.390 0.33 161165. 0.2698
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41.41 0.5332 0.7667 0.0467 0.0325 0.606 9.552 4.209 452.043 1.079 18.723 4.223 0.33 161572. 0.2480
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43.59 0.5613 0.7746 0.0422 0.0306 0.570 8.980 3.798 424.987 1.015 16.895 4.054 0.33 161996. 0.2261
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45.77 0.5894 0.7782 0.0375 0.0284 0.530 8.350 3.379 395.165 0.943 15.031 3.879 0.33 162438. 0.2041
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47.94 0.6174 0.7763 0.0328 0.0261 0.486 7.664 2.954 362.716 0.866 13.138 3.694 0.33 162897. 0.1817
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50.12 0.6455 0.7675 0.0280 0.0236 0.440 6.927 2.524 327.797 0.783 11.227 3.493 0.33 163373. 0.1588
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52.30 0.6736 0.7489 0.0232 0.0209 0.390 6.140 2.093 290.590 0.694 9.308 3.266 0.33 163866. 0.1352
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54.48 0.7016 0.7163 0.0185 0.0181 0.337 5.310 1.662 251.310 0.600 7.391 2.999 0.33 164377. 0.1106
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56.66 0.7297 0.6612 0.0137 0.0151 0.282 4.442 1.234 210.218 0.502 5.487 2.662 0.33 164905. 0.0846
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58.84 0.7578 0.5665 0.0090 0.0121 0.225 3.542 0.812 167.623 0.400 3.610 2.196 0.33 165450. 0.0566
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61.02 0.7858 0.3905 0.0044 0.0089 0.166 2.618 0.399 123.887 0.296 1.773 1.460 0.34 166012. 0.0264
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63.20 0.8139 -0.0045 0.0000 0.0057 0.106 1.677 -0.003 79.342 0.189 -0.013 -0.016 0.34 166585. 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 0.0982 0.0347 1.263 15.919 13.813 941.701 1.799 61.441 6.653 0.41 195910. 0.7078
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2.75 0.0283 0.0775 0.0971 0.0354 1.291 16.269 13.662 962.381 1.838 60.767 6.439 0.41 196057. 0.6812
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5.49 0.0566 0.1500 0.0959 0.0362 1.318 16.615 13.492 982.903 1.877 60.013 6.226 0.41 196221. 0.6546
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8.24 0.0849 0.2174 0.0945 0.0369 1.345 16.954 13.304 1002.901 1.915 59.174 6.017 0.41 196401. 0.6281
|
|
10.99 0.1132 0.2799 0.0931 0.0376 1.371 17.276 13.094 1021.986 1.952 58.242 5.811 0.41 196599. 0.6019
|
|
13.74 0.1415 0.3379 0.0914 0.0383 1.394 17.576 12.861 1039.726 1.986 57.207 5.611 0.41 196815. 0.5759
|
|
16.48 0.1698 0.3913 0.0896 0.0389 1.416 17.845 12.604 1055.654 2.016 56.064 5.416 0.41 197050. 0.5503
|
|
19.23 0.1981 0.4406 0.0876 0.0394 1.434 18.076 12.321 1069.276 2.042 54.804 5.226 0.41 197305. 0.5251
|
|
21.98 0.2264 0.4859 0.0854 0.0398 1.448 18.258 12.010 1080.076 2.063 53.421 5.044 0.41 197581. 0.5003
|
|
24.72 0.2547 0.5276 0.0829 0.0400 1.458 18.384 11.670 1087.523 2.077 51.908 4.867 0.41 197877. 0.4759
|
|
27.47 0.2830 0.5657 0.0803 0.0402 1.463 18.444 11.300 1091.083 2.084 50.261 4.697 0.41 198195. 0.4520
|
|
30.22 0.3113 0.6006 0.0775 0.0401 1.462 18.430 10.898 1090.223 2.082 48.474 4.534 0.41 198534. 0.4284
|
|
32.97 0.3396 0.6325 0.0744 0.0399 1.454 18.332 10.464 1084.428 2.071 46.544 4.377 0.41 198896. 0.4052
|
|
35.71 0.3679 0.6615 0.0711 0.0395 1.439 18.142 9.998 1073.213 2.050 44.469 4.225 0.41 199279. 0.3824
|
|
38.46 0.3962 0.6878 0.0675 0.0389 1.416 17.853 9.498 1056.103 2.017 42.246 4.079 0.41 199685. 0.3598
|
|
41.21 0.4245 0.7113 0.0637 0.0380 1.385 17.456 8.964 1032.608 1.972 39.873 3.938 0.41 200113. 0.3374
|
|
43.95 0.4528 0.7322 0.0597 0.0369 1.344 16.946 8.398 1002.427 1.914 37.355 3.800 0.41 200563. 0.3152
|
|
46.70 0.4811 0.7504 0.0555 0.0356 1.295 16.324 7.803 965.648 1.844 34.709 3.665 0.41 201035. 0.2931
|
|
49.45 0.5094 0.7657 0.0511 0.0340 1.237 15.595 7.184 922.507 1.762 31.955 3.532 0.41 201530. 0.2710
|
|
52.20 0.5377 0.7778 0.0465 0.0322 1.171 14.762 6.545 873.259 1.668 29.111 3.399 0.41 202047. 0.2489
|
|
54.94 0.5660 0.7863 0.0419 0.0301 1.097 13.831 5.889 818.159 1.563 26.193 3.265 0.41 202586. 0.2267
|
|
57.69 0.5944 0.7904 0.0371 0.0279 1.016 12.805 5.219 757.469 1.447 23.216 3.125 0.41 203147. 0.2044
|
|
60.44 0.6227 0.7891 0.0323 0.0255 0.927 11.689 4.541 691.480 1.321 20.196 2.978 0.41 203729. 0.1817
|
|
63.18 0.6510 0.7806 0.0274 0.0228 0.832 10.490 3.856 620.518 1.185 17.149 2.818 0.42 204334. 0.1584
|
|
65.93 0.6793 0.7621 0.0225 0.0201 0.731 9.212 3.168 544.969 1.041 14.092 2.637 0.42 204961. 0.1343
|
|
68.68 0.7076 0.7285 0.0176 0.0171 0.624 7.866 2.482 465.294 0.889 11.041 2.420 0.42 205609. 0.1091
|
|
71.43 0.7359 0.6700 0.0128 0.0141 0.512 6.458 1.802 382.048 0.730 8.016 2.140 0.42 206279. 0.0822
|
|
74.17 0.7642 0.5646 0.0081 0.0109 0.397 5.002 1.133 295.893 0.565 5.038 1.736 0.42 206971. 0.0529
|
|
76.92 0.7925 0.3529 0.0034 0.0076 0.278 3.509 0.479 207.603 0.396 2.131 1.047 0.42 207684. 0.0207
|
|
79.67 0.8208
|
|
|
|
|
|
|
|
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 0.0989 0.0348 2.187 22.974 20.047 1630.882 2.596 89.169 5.575 0.49 235077. 0.7145
|
|
3.27 0.0281 0.0773 0.0979 0.0355 2.236 23.485 19.835 1667.138 2.653 88.228 5.397 0.49 235252. 0.6879
|
|
6.53 0.0561 0.1495 0.0967 0.0363 2.284 23.993 19.599 1703.173 2.711 87.176 5.219 0.49 235447. 0.6614
|
|
9.80 0.0842 0.2168 0.0954 0.0370 2.331 24.488 19.335 1738.355 2.767 86.001 5.045 0.49 235661. 0.6349
|
|
13.07 0.1122 0.2792 0.0940 0.0378 2.376 24.962 19.041 1772.009 2.820 84.693 4.874 0.49 235896. 0.6087
|
|
16.34 0.1403 0.3371 0.0924 0.0384 2.418 25.405 18.714 1803.392 2.870 83.239 4.707 0.49 236152. 0.5828
|
|
19.60 0.1683 0.3905 0.0906 0.0390 2.456 25.803 18.352 1831.699 2.915 81.627 4.544 0.49 236432. 0.5572
|
|
22.87 0.1964 0.4398 0.0886 0.0396 2.489 26.147 17.952 1856.077 2.954 79.849 4.387 0.49 236734. 0.5320
|
|
26.14 0.2244 0.4852 0.0864 0.0400 2.515 26.422 17.512 1875.636 2.985 77.893 4.235 0.49 237061. 0.5072
|
|
29.41 0.2525 0.5270 0.0841 0.0403 2.534 26.617 17.030 1889.459 3.007 75.750 4.088 0.49 237412. 0.4829
|
|
32.67 0.2805 0.5653 0.0815 0.0404 2.543 26.718 16.505 1896.625 3.019 73.413 3.947 0.49 237789. 0.4590
|
|
35.94 0.3086 0.6005 0.0786 0.0404 2.543 26.712 15.934 1896.216 3.018 70.874 3.811 0.49 238191. 0.4355
|
|
39.21 0.3366 0.6327 0.0756 0.0402 2.531 26.587 15.317 1887.342 3.004 68.128 3.681 0.49 238619. 0.4123
|
|
42.47 0.3647 0.6620 0.0723 0.0398 2.507 26.331 14.652 1869.158 2.975 65.171 3.555 0.49 239072. 0.3895
|
|
45.74 0.3927 0.6887 0.0688 0.0392 2.469 25.932 13.939 1840.855 2.930 62.002 3.434 0.49 239552. 0.3670
|
|
49.01 0.4208 0.7128 0.0650 0.0384 2.416 25.379 13.178 1801.592 2.867 58.615 3.318 0.49 240059. 0.3447
|
|
52.28 0.4488 0.7343 0.0610 0.0373 2.348 24.663 12.368 1750.749 2.786 55.014 3.204 0.49 240591. 0.3225
|
|
55.54 0.4769 0.7533 0.0568 0.0360 2.264 23.784 11.516 1688.378 2.687 51.224 3.094 0.49 241150. 0.3005
|
|
58.81 0.5049 0.7696 0.0525 0.0344 2.166 22.749 10.628 1614.860 2.570 47.272 2.985 0.49 241735. 0.2785
|
|
62.08 0.5330 0.7829 0.0479 0.0326 2.053 21.562 9.709 1530.633 2.436 43.184 2.877 0.49 242346. 0.2566
|
|
65.34 0.5610 0.7929 0.0433 0.0306 1.926 20.231 8.764 1436.132 2.286 38.983 2.768 0.50 242983. 0.2345
|
|
68.61 0.5891 0.7990 0.0385 0.0284 1.786 18.761 7.800 1331.808 2.120 34.693 2.656 0.50 243646. 0.2123
|
|
71.88 0.6171 0.8002 0.0337 0.0260 1.634 17.160 6.820 1218.145 1.939 30.335 2.539 0.50 244335. 0.1898
|
|
75.15 0.6452 0.7951 0.0288 0.0233 1.469 15.435 5.830 1095.695 1.744 25.932 2.413 0.50 245049. 0.1668
|
|
78.41 0.6732 0.7812 0.0239 0.0206 1.294 13.595 4.835 965.099 1.536 21.507 2.272 0.50 245789. 0.1430
|
|
81.68 0.7013 0.7542 0.0190 0.0176 1.109 11.652 3.841 827.126 1.316 17.085 2.106 0.50 246555. 0.1182
|
|
84.95 0.7293 0.7061 0.0141 0.0145 0.916 9.617 2.854 682.701 1.087 12.694 1.896 0.50 247346. 0.0917
|
|
88.22 0.7574 0.6188 0.0093 0.0114 0.715 7.507 1.880 532.931 0.848 8.362 1.600 0.50 248163. 0.0628
|
|
91.48 0.7854 0.4448 0.0046 0.0081 0.508 5.341 0.927 379.125 0.603 4.123 1.109 0.50 249005. 0.0306
|
|
94.75 0.8135 0.0004 0.0000 0.0047 0.298 3.133 0.001 222.437 0.354 0.002 0.001 0.50 249863. 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 0.0999 0.0350 3.499 31.505 27.542 2609.198 3.559 122.507 4.788 0.57 274234. 0.7192
|
|
3.81 0.0280 0.0774 0.0989 0.0358 3.578 32.219 27.264 2668.336 3.640 121.268 4.634 0.57 274440. 0.6926
|
|
7.62 0.0561 0.1497 0.0977 0.0366 3.657 32.930 26.950 2727.204 3.720 119.876 4.482 0.57 274667. 0.6660
|
|
11.43 0.0841 0.2171 0.0965 0.0374 3.734 33.625 26.600 2784.757 3.799 118.315 4.332 0.57 274917. 0.6396
|
|
15.24 0.1122 0.2797 0.0950 0.0381 3.808 34.291 26.207 2839.906 3.874 116.569 4.186 0.57 275191. 0.6133
|
|
19.05 0.1402 0.3376 0.0934 0.0388 3.877 34.913 25.769 2891.416 3.944 114.621 4.042 0.57 275491. 0.5873
|
|
22.86 0.1682 0.3912 0.0917 0.0394 3.940 35.475 25.282 2937.971 4.008 112.454 3.903 0.57 275817. 0.5617
|
|
26.67 0.1963 0.4406 0.0897 0.0400 3.994 35.960 24.742 2978.164 4.063 110.054 3.768 0.57 276171. 0.5365
|
|
30.48 0.2243 0.4862 0.0876 0.0404 4.037 36.351 24.147 3010.533 4.107 107.405 3.638 0.57 276553. 0.5117
|
|
34.29 0.2524 0.5281 0.0852 0.0407 4.068 36.629 23.493 3033.586 4.138 104.496 3.513 0.57 276963. 0.4873
|
|
38.10 0.2804 0.5666 0.0826 0.0409 4.084 36.777 22.777 3045.809 4.155 101.314 3.392 0.57 277403. 0.4633
|
|
41.91 0.3084 0.6020 0.0798 0.0409 4.084 36.776 21.998 3045.708 4.155 97.849 3.276 0.57 277873. 0.4398
|
|
45.73 0.3365 0.6344 0.0767 0.0407 4.066 36.608 21.154 3031.829 4.136 94.094 3.165 0.57 278373. 0.4166
|
|
49.54 0.3645 0.6640 0.0734 0.0403 4.027 36.258 20.244 3002.798 4.096 90.044 3.058 0.57 278904. 0.3938
|
|
53.35 0.3926 0.6910 0.0699 0.0397 3.966 35.708 19.266 2957.302 4.034 85.694 2.955 0.57 279465. 0.3712
|
|
57.16 0.4206 0.7155 0.0661 0.0388 3.881 34.944 18.220 2893.993 3.948 81.041 2.856 0.57 280056. 0.3489
|
|
60.97 0.4486 0.7375 0.0620 0.0377 3.771 33.952 17.106 2811.815 3.836 76.087 2.759 0.57 280679. 0.3267
|
|
64.78 0.4767 0.7570 0.0578 0.0364 3.635 32.732 15.932 2710.808 3.698 70.864 2.666 0.58 281331. 0.3045
|
|
68.59 0.5047 0.7739 0.0533 0.0348 3.475 31.292 14.706 2591.580 3.535 65.412 2.574 0.58 282014. 0.2825
|
|
72.40 0.5328 0.7880 0.0487 0.0329 3.292 29.641 13.437 2454.840 3.349 59.767 2.483 0.58 282728. 0.2605
|
|
76.21 0.5608 0.7988 0.0440 0.0309 3.086 27.787 12.132 2301.306 3.139 53.962 2.391 0.58 283471. 0.2384
|
|
80.02 0.5888 0.8060 0.0392 0.0286 2.859 25.740 10.798 2131.714 2.908 48.029 2.297 0.58 284245. 0.2161
|
|
83.83 0.6169 0.8084 0.0342 0.0261 2.611 23.508 9.442 1946.857 2.656 41.998 2.200 0.58 285049. 0.1935
|
|
87.64 0.6449 0.8048 0.0293 0.0235 2.344 21.102 8.071 1747.631 2.384 35.901 2.095 0.58 285882. 0.1703
|
|
91.45 0.6730 0.7929 0.0243 0.0206 2.059 18.536 6.693 1535.089 2.094 29.771 1.978 0.58 286745. 0.1464
|
|
95.26 0.7010 0.7683 0.0193 0.0176 1.757 15.824 5.315 1310.485 1.788 23.642 1.840 0.58 287639. 0.1214
|
|
99.07 0.7291 0.7230 0.0143 0.0144 1.442 12.984 3.946 1075.339 1.467 17.554 1.665 0.58 288562. 0.0946
|
|
102.88 0.7571 0.6387 0.0094 0.0112 1.115 10.040 2.596 831.473 1.134 11.547 1.416 0.59 289514. 0.0653
|
|
106.69 0.7851 0.4652 0.0046 0.0078 0.779 7.016 1.274 581.048 0.793 5.668 0.995 0.59 290496. 0.0321
|
|
110.50 0.8132 -0.0075 0.0000 0.0044 0.437 3.935 -0.011 325.899 0.445 -0.049 -0.015 0.59 291494. 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 0.1010 0.0355 5.289 41.666 36.371 3943.707 4.707 161.779 4.183 0.65 313381. 0.7221
|
|
4.35 0.0280 0.0772 0.1000 0.0363 5.411 42.628 36.024 4034.690 4.816 160.234 4.050 0.65 313615. 0.6957
|
|
8.70 0.0560 0.1494 0.0989 0.0371 5.532 43.587 35.631 4125.484 4.924 158.488 3.917 0.65 313874. 0.6693
|
|
13.05 0.0840 0.2167 0.0977 0.0379 5.652 44.527 35.189 4214.473 5.031 156.519 3.787 0.65 314160. 0.6430
|
|
17.40 0.1121 0.2792 0.0963 0.0387 5.766 45.430 34.691 4299.924 5.133 154.304 3.659 0.65 314474. 0.6169
|
|
21.75 0.1401 0.3371 0.0948 0.0394 5.874 46.275 34.132 4379.918 5.228 151.820 3.535 0.65 314817. 0.5911
|
|
26.10 0.1681 0.3906 0.0930 0.0400 5.971 47.041 33.508 4452.389 5.315 149.042 3.413 0.65 315190. 0.5656
|
|
30.45 0.1961 0.4401 0.0911 0.0406 6.055 47.704 32.813 4515.157 5.390 145.950 3.296 0.65 315595. 0.5404
|
|
34.80 0.2241 0.4857 0.0890 0.0410 6.123 48.241 32.042 4565.948 5.450 142.524 3.183 0.65 316032. 0.5157
|
|
39.16 0.2521 0.5277 0.0866 0.0414 6.172 48.626 31.193 4602.445 5.494 138.745 3.074 0.65 316502. 0.4914
|
|
43.51 0.2801 0.5663 0.0840 0.0416 6.199 48.836 30.260 4622.309 5.517 134.597 2.969 0.65 317005. 0.4675
|
|
47.86 0.3082 0.6019 0.0812 0.0416 6.200 48.846 29.241 4623.239 5.519 130.066 2.869 0.65 317543. 0.4440
|
|
52.21 0.3362 0.6345 0.0781 0.0414 6.173 48.632 28.135 4603.000 5.494 125.142 2.772 0.65 318115. 0.4209
|
|
56.56 0.3642 0.6644 0.0748 0.0410 6.114 48.172 26.938 4559.476 5.442 119.819 2.680 0.65 318722. 0.3981
|
|
60.91 0.3922 0.6918 0.0712 0.0404 6.022 47.445 25.650 4490.667 5.360 114.089 2.591 0.66 319364. 0.3755
|
|
65.26 0.4202 0.7166 0.0674 0.0395 5.893 46.430 24.269 4394.543 5.246 107.948 2.505 0.66 320041. 0.3532
|
|
69.61 0.4482 0.7391 0.0633 0.0384 5.725 45.108 22.797 4269.419 5.096 101.399 2.422 0.66 320753. 0.3310
|
|
73.96 0.4762 0.7591 0.0590 0.0370 5.519 43.479 21.242 4115.243 4.912 94.483 2.341 0.66 321499. 0.3088
|
|
78.31 0.5042 0.7766 0.0545 0.0354 5.274 41.553 19.616 3932.938 4.695 87.250 2.262 0.66 322280. 0.2868
|
|
82.66 0.5323 0.7915 0.0498 0.0335 4.993 39.341 17.930 3723.603 4.445 79.751 2.184 0.66 323096. 0.2647
|
|
87.01 0.5603 0.8032 0.0450 0.0314 4.678 36.856 16.194 3488.356 4.164 72.032 2.106 0.66 323945. 0.2425
|
|
91.36 0.5883 0.8114 0.0400 0.0290 4.329 34.108 14.418 3228.331 3.854 64.133 2.026 0.66 324829. 0.2202
|
|
95.71 0.6163 0.8151 0.0350 0.0265 3.949 31.112 12.612 2944.757 3.515 56.098 1.943 0.66 325747. 0.1975
|
|
100.06 0.6443 0.8131 0.0299 0.0237 3.539 27.882 10.784 2639.017 3.150 47.968 1.853 0.66 326699. 0.1742
|
|
104.41 0.6723 0.8030 0.0248 0.0208 3.101 24.435 8.945 2312.725 2.761 39.787 1.754 0.67 327684. 0.1502
|
|
108.77 0.7003 0.7809 0.0197 0.0177 2.639 20.791 7.105 1967.822 2.349 31.602 1.638 0.67 328704. 0.1249
|
|
113.12 0.7284 0.7386 0.0146 0.0144 2.155 16.975 5.276 1606.646 1.918 23.466 1.489 0.67 329758. 0.0979
|
|
117.47 0.7564 0.6579 0.0096 0.0111 1.652 13.017 3.470 1232.043 1.471 15.435 1.278 0.67 330845. 0.0681
|
|
121.82 0.7844 0.4866 0.0047 0.0076 1.136 8.953 1.702 847.432 1.012 7.572 0.911 0.67 331965. 0.0340
|
|
126.17 0.8124 -0.0094 0.0000 0.0041 0.611 4.815 -0.017 455.759 0.544 -0.076 -0.017 0.67 333103. 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 0.1023 0.0365 7.756 54.315 46.616 5783.539 6.137 207.350 3.656 0.73 352513. 0.7144
|
|
4.89 0.0280 0.0760 0.1014 0.0373 7.924 55.494 46.206 5909.061 6.270 205.525 3.547 0.73 352775. 0.6901
|
|
9.77 0.0559 0.1473 0.1003 0.0381 8.093 56.675 45.739 6034.764 6.403 203.447 3.438 0.73 353067. 0.6655
|
|
14.66 0.0839 0.2140 0.0992 0.0389 8.259 57.836 45.208 6158.437 6.534 201.085 3.330 0.73 353388. 0.6408
|
|
19.55 0.1119 0.2762 0.0978 0.0396 8.419 58.956 44.606 6277.688 6.661 198.407 3.223 0.73 353740. 0.6161
|
|
24.43 0.1399 0.3340 0.0964 0.0403 8.569 60.009 43.925 6389.839 6.780 195.379 3.118 0.73 354126. 0.5915
|
|
29.32 0.1678 0.3876 0.0947 0.0410 8.706 60.968 43.158 6491.949 6.888 191.968 3.015 0.73 354546. 0.5670
|
|
34.21 0.1958 0.4372 0.0928 0.0416 8.825 61.803 42.299 6580.862 6.983 188.145 2.915 0.73 355001. 0.5427
|
|
39.10 0.2238 0.4830 0.0907 0.0420 8.922 62.483 41.340 6653.275 7.059 183.880 2.818 0.73 355493. 0.5187
|
|
43.98 0.2517 0.5253 0.0883 0.0423 8.993 62.976 40.276 6705.728 7.115 179.149 2.724 0.73 356023. 0.4949
|
|
48.87 0.2797 0.5642 0.0858 0.0425 9.031 63.248 39.103 6734.701 7.146 173.930 2.634 0.73 356590. 0.4714
|
|
53.76 0.3077 0.6000 0.0829 0.0425 9.034 63.266 37.816 6736.655 7.148 168.204 2.546 0.74 357196. 0.4481
|
|
58.64 0.3356 0.6329 0.0799 0.0424 8.996 62.998 36.411 6708.089 7.118 161.957 2.462 0.74 357840. 0.4252
|
|
63.53 0.3636 0.6632 0.0765 0.0420 8.912 62.412 34.887 6645.654 7.051 155.179 2.381 0.74 358524. 0.4026
|
|
68.42 0.3916 0.6909 0.0729 0.0413 8.779 61.478 33.243 6546.188 6.946 147.865 2.303 0.74 359246. 0.3801
|
|
73.30 0.4196 0.7161 0.0690 0.0405 8.591 60.167 31.476 6406.594 6.798 140.005 2.228 0.74 360008. 0.3578
|
|
78.19 0.4475 0.7391 0.0649 0.0393 8.347 58.454 29.587 6224.267 6.604 131.604 2.156 0.74 360809. 0.3357
|
|
83.08 0.4755 0.7597 0.0605 0.0379 8.045 56.338 27.587 5998.926 6.365 122.708 2.086 0.74 361649. 0.3136
|
|
87.97 0.5035 0.7779 0.0559 0.0362 7.687 53.830 25.491 5731.892 6.082 113.386 2.017 0.74 362528. 0.2915
|
|
92.85 0.5314 0.7935 0.0511 0.0343 7.275 50.947 23.315 5424.819 5.756 103.704 1.949 0.74 363445. 0.2694
|
|
97.74 0.5594 0.8062 0.0462 0.0321 6.812 47.703 21.070 5079.398 5.389 93.720 1.881 0.74 364400. 0.2472
|
|
102.63 0.5874 0.8154 0.0412 0.0297 6.299 44.115 18.771 4697.416 4.984 83.492 1.812 0.74 365393. 0.2248
|
|
107.51 0.6154 0.8204 0.0360 0.0270 5.741 40.203 16.428 4280.837 4.542 73.073 1.741 0.75 366425. 0.2019
|
|
112.40 0.6433 0.8198 0.0308 0.0242 5.139 35.987 14.055 3831.943 4.066 62.518 1.664 0.75 367494. 0.1785
|
|
117.29 0.6713 0.8112 0.0256 0.0212 4.497 31.494 11.665 3353.479 3.558 51.885 1.578 0.75 368601. 0.1542
|
|
122.17 0.6993 0.7906 0.0203 0.0180 3.820 26.754 9.271 2848.815 3.023 41.236 1.476 0.75 369746. 0.1286
|
|
127.06 0.7272 0.7494 0.0151 0.0147 3.114 21.808 6.888 2322.125 2.464 30.637 1.345 0.75 370929. 0.1011
|
|
131.95 0.7552 0.6687 0.0099 0.0112 2.385 16.703 4.533 1778.538 1.887 20.163 1.156 0.75 372149. 0.0704
|
|
136.83 0.7832 0.4945 0.0049 0.0077 1.642 11.497 2.225 1224.182 1.299 9.897 0.824 0.75 373406. 0.0352
|
|
141.72 0.8112 -0.0095 0.0000 0.0042 0.891 6.240 -0.022 664.490 0.705 -0.099 -0.015 0.76 374683. 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 0.1036 0.0402 11.712 73.820 58.332 8733.794 8.340 259.461 3.029 0.81 391626. 0.6622
|
|
5.42 0.0279 0.0703 0.1028 0.0409 11.910 75.070 57.876 8881.627 8.481 257.431 2.956 0.81 391916. 0.6436
|
|
10.85 0.0559 0.1370 0.1019 0.0416 12.106 76.302 57.351 9027.481 8.621 255.095 2.881 0.81 392239. 0.6246
|
|
16.27 0.0838 0.2002 0.1008 0.0422 12.295 77.493 56.747 9168.316 8.755 252.412 2.807 0.81 392595. 0.6053
|
|
21.69 0.1117 0.2600 0.0996 0.0428 12.473 78.613 56.055 9300.877 8.882 249.335 2.734 0.81 392986. 0.5858
|
|
27.12 0.1397 0.3163 0.0982 0.0434 12.635 79.634 55.265 9421.640 8.997 245.818 2.661 0.81 393414. 0.5661
|
|
32.54 0.1676 0.3692 0.0966 0.0439 12.776 80.523 54.365 9526.827 9.097 241.815 2.588 0.81 393881. 0.5462
|
|
37.96 0.1955 0.4189 0.0948 0.0442 12.891 81.247 53.346 9612.527 9.179 237.282 2.517 0.81 394388. 0.5262
|
|
43.38 0.2235 0.4654 0.0927 0.0445 12.974 81.773 52.198 9674.770 9.239 232.178 2.447 0.82 394935. 0.5061
|
|
48.81 0.2514 0.5089 0.0905 0.0447 13.021 82.067 50.914 9709.508 9.272 226.467 2.378 0.82 395524. 0.4858
|
|
54.23 0.2794 0.5494 0.0879 0.0447 13.025 82.094 49.487 9712.673 9.275 220.117 2.311 0.82 396156. 0.4653
|
|
59.65 0.3073 0.5871 0.0851 0.0446 12.981 81.819 47.910 9680.172 9.244 213.102 2.245 0.82 396831. 0.4447
|
|
65.08 0.3352 0.6219 0.0820 0.0442 12.884 81.208 46.179 9607.893 9.175 205.402 2.180 0.82 397549. 0.4240
|
|
70.50 0.3632 0.6541 0.0787 0.0437 12.729 80.226 44.290 9491.736 9.064 197.003 2.116 0.82 398310. 0.4032
|
|
75.92 0.3911 0.6837 0.0751 0.0429 12.509 78.840 42.243 9327.684 8.907 187.898 2.054 0.82 399115. 0.3821
|
|
81.35 0.4190 0.7107 0.0711 0.0419 12.219 77.012 40.036 9111.481 8.701 178.078 1.993 0.82 399963. 0.3609
|
|
86.77 0.4470 0.7353 0.0669 0.0407 11.853 74.709 37.667 8838.914 8.441 167.542 1.933 0.82 400854. 0.3395
|
|
92.19 0.4749 0.7573 0.0625 0.0392 11.410 71.917 35.150 8508.638 8.125 156.347 1.874 0.82 401789. 0.3180
|
|
97.62 0.5028 0.7767 0.0578 0.0374 10.893 68.658 32.504 8123.032 7.757 144.580 1.815 0.82 402766. 0.2962
|
|
103.04 0.5308 0.7931 0.0529 0.0354 10.306 64.960 29.749 7685.533 7.339 132.324 1.756 0.82 403786. 0.2741
|
|
108.46 0.5587 0.8061 0.0478 0.0331 9.652 60.835 26.902 7197.539 6.873 119.659 1.695 0.83 404848. 0.2517
|
|
113.89 0.5866 0.8151 0.0426 0.0307 8.933 56.305 23.979 6661.598 6.361 106.657 1.633 0.83 405952. 0.2288
|
|
119.31 0.6146 0.8192 0.0373 0.0280 8.154 51.395 20.996 6080.623 5.807 93.389 1.566 0.83 407098. 0.2054
|
|
124.73 0.6425 0.8163 0.0319 0.0251 7.321 46.146 17.969 5459.576 5.214 79.926 1.493 0.83 408286. 0.1811
|
|
130.15 0.6705 0.8034 0.0265 0.0221 6.443 40.609 14.915 4804.535 4.588 66.342 1.408 0.83 409515. 0.1556
|
|
135.58 0.6984 0.7750 0.0211 0.0190 5.528 34.842 11.851 4122.260 3.936 52.712 1.304 0.83 410785. 0.1285
|
|
141.00 0.7263 0.7209 0.0156 0.0157 4.588 28.915 8.796 3421.029 3.267 39.124 1.166 0.83 412097. 0.0990
|
|
146.42 0.7543 0.6200 0.0103 0.0125 3.635 22.908 5.772 2710.344 2.588 25.673 0.966 0.84 413451. 0.0664
|
|
151.85 0.7822 0.4229 0.0050 0.0092 2.683 16.911 2.803 2000.794 1.911 12.466 0.635 0.84 414845. 0.0304
|
|
157.27 0.8101 -0.0223 -0.0002 0.0060 1.744 10.994 -0.093 1300.680 1.242 -0.413 -0.032 0.84 416263. 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 0.1044 0.0481 18.656 106.894 71.076 13911.521 12.077 316.145 2.317 0.89 430751. 0.5592
|
|
5.98 0.0280 0.0596 0.1037 0.0487 18.898 108.283 70.619 14092.243 12.234 314.114 2.273 0.89 431067. 0.5467
|
|
11.96 0.0560 0.1169 0.1029 0.0493 19.127 109.597 70.084 14263.241 12.382 311.736 2.229 0.89 431418. 0.5340
|
|
17.94 0.0840 0.1719 0.1020 0.0499 19.336 110.793 69.458 14418.865 12.517 308.951 2.185 0.89 431807. 0.5212
|
|
23.92 0.1120 0.2246 0.1009 0.0503 19.516 111.825 68.727 14553.291 12.634 305.696 2.142 0.90 432235. 0.5083
|
|
29.90 0.1400 0.2753 0.0997 0.0507 19.660 112.650 67.875 14660.559 12.727 301.906 2.100 0.90 432705. 0.4952
|
|
35.88 0.1680 0.3239 0.0982 0.0510 19.760 113.220 66.887 14734.825 12.792 297.513 2.059 0.90 433218. 0.4820
|
|
41.86 0.1961 0.3706 0.0965 0.0511 19.808 113.495 65.749 14770.602 12.823 292.452 2.019 0.90 433776. 0.4686
|
|
47.85 0.2241 0.4153 0.0946 0.0511 19.797 113.436 64.448 14762.962 12.816 286.663 1.980 0.90 434380. 0.4550
|
|
53.83 0.2521 0.4582 0.0925 0.0509 19.723 113.011 62.970 14707.588 12.768 280.093 1.942 0.90 435031. 0.4411
|
|
59.81 0.2801 0.4993 0.0900 0.0505 19.580 112.190 61.307 14600.715 12.675 272.693 1.904 0.90 435731. 0.4268
|
|
65.79 0.3081 0.5386 0.0873 0.0499 19.363 110.948 59.448 14439.051 12.535 264.424 1.867 0.90 436478. 0.4121
|
|
71.77 0.3361 0.5759 0.0843 0.0492 19.069 109.261 57.387 14219.515 12.344 255.256 1.831 0.90 437274. 0.3969
|
|
77.75 0.3641 0.6113 0.0809 0.0482 18.693 107.107 55.119 13939.166 12.101 245.168 1.794 0.90 438118. 0.3811
|
|
83.73 0.3921 0.6447 0.0773 0.0470 18.231 104.462 52.640 13594.984 11.802 234.145 1.756 0.90 439011. 0.3647
|
|
89.71 0.4201 0.6759 0.0733 0.0456 17.680 101.302 49.950 13183.702 11.445 222.178 1.718 0.90 439953. 0.3476
|
|
95.69 0.4481 0.7048 0.0691 0.0439 17.033 97.596 47.046 12701.419 11.026 209.263 1.680 0.90 440942. 0.3298
|
|
101.67 0.4761 0.7313 0.0645 0.0420 16.291 93.347 43.946 12148.470 10.546 195.472 1.641 0.90 441979. 0.3113
|
|
107.65 0.5041 0.7553 0.0597 0.0399 15.459 88.579 40.675 11527.879 10.008 180.922 1.600 0.91 443064. 0.2921
|
|
113.63 0.5321 0.7756 0.0547 0.0375 14.556 83.405 37.257 10854.517 9.423 165.718 1.557 0.91 444195. 0.2720
|
|
119.61 0.5601 0.7903 0.0495 0.0351 13.606 77.962 33.712 10146.178 8.808 149.952 1.507 0.91 445372. 0.2505
|
|
125.59 0.5882 0.7978 0.0441 0.0325 12.619 72.305 30.063 9410.024 8.169 133.718 1.449 0.91 446595. 0.2274
|
|
131.58 0.6162 0.7942 0.0387 0.0300 11.630 66.636 26.324 8672.206 7.528 117.091 1.377 0.91 447865. 0.2022
|
|
137.56 0.6442 0.7801 0.0331 0.0273 10.593 60.696 22.528 7899.130 6.857 100.204 1.294 0.91 449180. 0.1757
|
|
143.54 0.6722 0.7512 0.0275 0.0246 9.525 54.578 18.695 7102.904 6.166 83.157 1.194 0.91 450540. 0.1477
|
|
149.52 0.7002 0.7012 0.0218 0.0218 8.444 48.384 14.852 6296.876 5.466 66.062 1.070 0.92 451946. 0.1180
|
|
155.50 0.7282 0.6206 0.0162 0.0190 7.368 42.218 11.029 5494.398 4.770 49.055 0.910 0.92 453397. 0.0865
|
|
161.48 0.7562 0.4948 0.0107 0.0163 6.315 36.184 7.256 4709.092 4.088 32.275 0.699 0.92 454894. 0.0539
|
|
167.46 0.7842 0.3007 0.0052 0.0137 5.303 30.384 3.571 3954.305 3.433 15.885 0.410 0.92 456436. 0.0222
|
|
173.44 0.8122 0.0000 0.0000 0.0112 4.336 24.843 0.000 3233.159 2.807 0.001 0.000 0.92 458020. 0.0000
|
|
|
|
|
|
|