612 lines
109 KiB
Plaintext
612 lines
109 KiB
Plaintext
14x12 (14x12.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 0.1200 0.0648 0.003 0.177 0.147 2.090 0.020 0.654 31.891 0.06 24281. 0.5124
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0.47 0.0351 0.0634 0.1193 0.0660 0.003 0.180 0.146 2.132 0.020 0.649 31.066 0.06 24305. 0.4975
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0.93 0.0703 0.1234 0.1183 0.0674 0.003 0.184 0.145 2.174 0.021 0.644 30.222 0.06 24332. 0.4821
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1.40 0.1054 0.1799 0.1173 0.0687 0.003 0.187 0.144 2.218 0.021 0.639 29.366 0.06 24362. 0.4664
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1.86 0.1406 0.2329 0.1161 0.0701 0.003 0.191 0.142 2.262 0.022 0.632 28.504 0.06 24396. 0.4504
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2.33 0.1757 0.2823 0.1147 0.0714 0.003 0.195 0.140 2.304 0.022 0.625 27.642 0.06 24433. 0.4341
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2.80 0.2108 0.3282 0.1131 0.0727 0.003 0.198 0.138 2.345 0.022 0.616 26.786 0.06 24475. 0.4178
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3.26 0.2460 0.3708 0.1113 0.0738 0.003 0.201 0.136 2.382 0.023 0.606 25.940 0.06 24520. 0.4013
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3.73 0.2811 0.4102 0.1092 0.0748 0.003 0.204 0.134 2.415 0.023 0.595 25.106 0.06 24570. 0.3847
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4.19 0.3163 0.4464 0.1068 0.0757 0.003 0.206 0.131 2.442 0.023 0.582 24.288 0.06 24625. 0.3681
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4.66 0.3514 0.4797 0.1041 0.0763 0.003 0.208 0.127 2.462 0.024 0.567 23.486 0.06 24683. 0.3515
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5.12 0.3865 0.5100 0.1011 0.0767 0.003 0.209 0.124 2.474 0.024 0.551 22.700 0.06 24747. 0.3348
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5.59 0.4217 0.5375 0.0978 0.0767 0.003 0.209 0.120 2.476 0.024 0.532 21.930 0.06 24814. 0.3180
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6.06 0.4568 0.5622 0.0940 0.0764 0.003 0.208 0.115 2.466 0.024 0.512 21.173 0.06 24886. 0.3011
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6.52 0.4920 0.5841 0.0899 0.0757 0.003 0.207 0.110 2.444 0.023 0.490 20.427 0.06 24963. 0.2841
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6.99 0.5271 0.6032 0.0854 0.0746 0.003 0.204 0.105 2.408 0.023 0.465 19.689 0.06 25044. 0.2668
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7.45 0.5622 0.6193 0.0805 0.0731 0.003 0.199 0.099 2.358 0.023 0.438 18.953 0.06 25129. 0.2494
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7.92 0.5974 0.6324 0.0753 0.0711 0.003 0.194 0.092 2.294 0.022 0.410 18.215 0.06 25219. 0.2317
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8.39 0.6325 0.6422 0.0697 0.0687 0.003 0.187 0.085 2.217 0.021 0.380 17.468 0.06 25313. 0.2139
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8.85 0.6677 0.6481 0.0640 0.0659 0.003 0.180 0.078 2.128 0.020 0.348 16.702 0.06 25411. 0.1959
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9.32 0.7028 0.6497 0.0580 0.0628 0.003 0.171 0.071 2.026 0.019 0.316 15.906 0.06 25514. 0.1777
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9.78 0.7379 0.6462 0.0519 0.0593 0.003 0.162 0.064 1.914 0.018 0.283 15.066 0.06 25620. 0.1592
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10.25 0.7731 0.6363 0.0457 0.0555 0.002 0.151 0.056 1.792 0.017 0.249 14.162 0.06 25731. 0.1404
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10.71 0.8082 0.6186 0.0393 0.0514 0.002 0.140 0.048 1.659 0.016 0.214 13.168 0.06 25846. 0.1211
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11.18 0.8433 0.5904 0.0329 0.0470 0.002 0.128 0.040 1.517 0.014 0.179 12.046 0.06 25965. 0.1013
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11.65 0.8785 0.5481 0.0264 0.0423 0.002 0.115 0.032 1.365 0.013 0.144 10.735 0.06 26088. 0.0809
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12.11 0.9136 0.4854 0.0198 0.0373 0.002 0.102 0.024 1.204 0.012 0.108 9.141 0.06 26215. 0.0597
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12.58 0.9488 0.3916 0.0132 0.0321 0.001 0.087 0.016 1.035 0.010 0.072 7.101 0.06 26345. 0.0379
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13.04 0.9839 0.2461 0.0067 0.0266 0.001 0.073 0.008 0.858 0.008 0.036 4.304 0.06 26480. 0.0163
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13.51 1.0190 0.0050 0.0001 0.0209 0.001 0.057 0.000 0.675 0.006 0.001 0.085 0.06 26618. 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 0.1206 0.0583 0.020 0.636 0.590 15.051 0.072 2.626 17.792 0.11 48562. 0.5729
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0.94 0.0354 0.0711 0.1198 0.0596 0.021 0.651 0.587 15.396 0.074 2.609 17.282 0.11 48610. 0.5548
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1.88 0.0708 0.1380 0.1189 0.0610 0.021 0.666 0.582 15.756 0.075 2.590 16.763 0.11 48664. 0.5361
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2.82 0.1062 0.2005 0.1179 0.0625 0.022 0.681 0.577 16.124 0.077 2.568 16.240 0.11 48725. 0.5172
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3.76 0.1416 0.2588 0.1167 0.0639 0.022 0.697 0.572 16.494 0.079 2.542 15.717 0.11 48793. 0.4980
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4.69 0.1771 0.3128 0.1153 0.0653 0.023 0.712 0.565 16.857 0.080 2.512 15.198 0.11 48869. 0.4787
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5.63 0.2125 0.3627 0.1138 0.0666 0.023 0.727 0.557 17.206 0.082 2.478 14.686 0.11 48953. 0.4594
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6.57 0.2479 0.4087 0.1119 0.0679 0.024 0.741 0.548 17.530 0.084 2.438 14.184 0.11 49046. 0.4402
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7.51 0.2833 0.4509 0.1099 0.0690 0.024 0.753 0.538 17.819 0.085 2.393 13.694 0.11 49147. 0.4210
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8.45 0.3187 0.4897 0.1075 0.0700 0.024 0.763 0.526 18.062 0.086 2.341 13.218 0.11 49257. 0.4019
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9.39 0.3541 0.5250 0.1048 0.0707 0.024 0.771 0.513 18.247 0.087 2.283 12.756 0.11 49376. 0.3830
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10.33 0.3895 0.5572 0.1018 0.0711 0.025 0.776 0.498 18.364 0.088 2.216 12.307 0.11 49504. 0.3641
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11.27 0.4249 0.5864 0.0984 0.0713 0.025 0.778 0.482 18.401 0.088 2.142 11.873 0.11 49641. 0.3454
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12.21 0.4603 0.6128 0.0946 0.0711 0.025 0.775 0.463 18.346 0.088 2.060 11.451 0.11 49787. 0.3266
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13.14 0.4957 0.6363 0.0904 0.0704 0.024 0.769 0.443 18.186 0.087 1.969 11.041 0.11 49943. 0.3079
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14.08 0.5312 0.6570 0.0858 0.0694 0.024 0.757 0.420 17.913 0.086 1.869 10.641 0.11 50107. 0.2891
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15.02 0.5666 0.6750 0.0808 0.0679 0.023 0.740 0.396 17.520 0.084 1.761 10.249 0.11 50280. 0.2703
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15.96 0.6020 0.6901 0.0755 0.0659 0.023 0.719 0.370 17.011 0.081 1.645 9.863 0.11 50462. 0.2514
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16.90 0.6374 0.7023 0.0699 0.0635 0.022 0.693 0.343 16.391 0.078 1.524 9.478 0.11 50653. 0.2325
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17.84 0.6728 0.7110 0.0641 0.0607 0.021 0.662 0.314 15.667 0.075 1.397 9.092 0.11 50852. 0.2135
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18.78 0.7082 0.7160 0.0581 0.0575 0.020 0.627 0.285 14.844 0.071 1.266 8.697 0.11 51060. 0.1945
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19.72 0.7436 0.7164 0.0520 0.0539 0.019 0.589 0.254 13.926 0.066 1.132 8.287 0.11 51276. 0.1752
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20.66 0.7790 0.7112 0.0457 0.0500 0.017 0.546 0.224 12.918 0.062 0.995 7.853 0.11 51501. 0.1557
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21.59 0.8144 0.6988 0.0393 0.0458 0.016 0.500 0.192 11.821 0.056 0.856 7.381 0.11 51733. 0.1357
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22.53 0.8498 0.6767 0.0328 0.0412 0.014 0.450 0.161 10.640 0.051 0.715 6.850 0.12 51974. 0.1151
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23.47 0.8853 0.6406 0.0263 0.0363 0.013 0.396 0.129 9.376 0.045 0.572 6.225 0.12 52224. 0.0936
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24.41 0.9207 0.5831 0.0197 0.0311 0.011 0.340 0.097 8.034 0.038 0.429 5.448 0.12 52481. 0.0709
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25.35 0.9561 0.4894 0.0131 0.0256 0.009 0.280 0.064 6.620 0.032 0.286 4.404 0.12 52746. 0.0468
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26.29 0.9915 0.3269 0.0066 0.0199 0.007 0.217 0.032 5.138 0.025 0.143 2.836 0.12 53019. 0.0213
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27.23 1.0269 0.0034 0.0000 0.0139 0.005 0.152 0.000 3.597 0.017 0.001 0.029 0.12 53298. 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 0.1209 0.0557 0.065 1.367 1.332 48.504 0.154 5.923 12.452 0.17 72842. 0.6023
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1.41 0.0355 0.0748 0.1201 0.0570 0.067 1.400 1.323 49.694 0.158 5.886 12.079 0.17 72914. 0.5824
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2.83 0.0711 0.1449 0.1192 0.0585 0.068 1.435 1.314 50.935 0.162 5.844 11.700 0.17 72995. 0.5621
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4.24 0.1066 0.2103 0.1182 0.0599 0.070 1.471 1.303 52.209 0.166 5.795 11.319 0.17 73087. 0.5415
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5.65 0.1421 0.2710 0.1171 0.0614 0.072 1.507 1.290 53.491 0.170 5.738 10.939 0.17 73190. 0.5207
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7.06 0.1776 0.3272 0.1157 0.0628 0.073 1.543 1.275 54.756 0.174 5.672 10.563 0.17 73304. 0.4999
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8.48 0.2132 0.3789 0.1142 0.0642 0.075 1.577 1.258 55.972 0.178 5.595 10.194 0.17 73431. 0.4792
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9.89 0.2487 0.4264 0.1124 0.0655 0.077 1.609 1.238 57.106 0.182 5.507 9.833 0.17 73571. 0.4586
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11.30 0.2842 0.4699 0.1103 0.0667 0.078 1.638 1.215 58.123 0.185 5.405 9.483 0.17 73724. 0.4381
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12.72 0.3197 0.5097 0.1079 0.0677 0.079 1.662 1.189 58.983 0.188 5.289 9.143 0.17 73890. 0.4179
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14.13 0.3553 0.5461 0.1052 0.0685 0.080 1.681 1.159 59.650 0.190 5.157 8.815 0.17 74069. 0.3978
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15.54 0.3908 0.5791 0.1022 0.0690 0.081 1.693 1.126 60.083 0.191 5.008 8.499 0.17 74262. 0.3779
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16.96 0.4263 0.6091 0.0988 0.0691 0.081 1.697 1.088 60.241 0.192 4.840 8.194 0.17 74469. 0.3582
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18.37 0.4618 0.6361 0.0950 0.0690 0.081 1.693 1.046 60.084 0.191 4.654 7.899 0.17 74690. 0.3387
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19.78 0.4974 0.6604 0.0908 0.0684 0.080 1.678 1.000 59.569 0.190 4.448 7.615 0.17 74924. 0.3191
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21.19 0.5329 0.6819 0.0861 0.0673 0.079 1.653 0.949 58.662 0.187 4.222 7.339 0.17 75172. 0.2997
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22.61 0.5684 0.7008 0.0811 0.0658 0.077 1.616 0.894 57.346 0.183 3.976 7.071 0.17 75434. 0.2802
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24.02 0.6039 0.7170 0.0758 0.0638 0.075 1.567 0.835 55.628 0.177 3.714 6.809 0.17 75708. 0.2608
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25.43 0.6395 0.7304 0.0702 0.0614 0.072 1.508 0.773 53.527 0.170 3.439 6.551 0.17 75996. 0.2414
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26.85 0.6750 0.7407 0.0643 0.0586 0.068 1.439 0.709 51.064 0.163 3.152 6.294 0.17 76297. 0.2220
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28.26 0.7105 0.7476 0.0583 0.0554 0.065 1.360 0.642 48.256 0.154 2.856 6.034 0.17 76610. 0.2026
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29.67 0.7461 0.7503 0.0521 0.0518 0.061 1.271 0.574 45.119 0.144 2.552 5.768 0.17 76937. 0.1831
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31.09 0.7816 0.7479 0.0458 0.0478 0.056 1.174 0.504 41.664 0.133 2.242 5.488 0.17 77275. 0.1633
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32.50 0.8171 0.7390 0.0393 0.0435 0.051 1.068 0.433 37.901 0.121 1.928 5.187 0.17 77627. 0.1431
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33.91 0.8526 0.7210 0.0328 0.0388 0.045 0.953 0.362 33.839 0.108 1.609 4.850 0.17 77991. 0.1223
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35.32 0.8882 0.6898 0.0263 0.0338 0.040 0.831 0.290 29.490 0.094 1.288 4.454 0.17 78367. 0.1005
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36.74 0.9237 0.6375 0.0197 0.0285 0.033 0.701 0.217 24.868 0.079 0.965 3.958 0.17 78755. 0.0773
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38.15 0.9592 0.5479 0.0131 0.0229 0.027 0.563 0.144 19.990 0.064 0.642 3.276 0.17 79155. 0.0522
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39.56 0.9947 0.3806 0.0065 0.0171 0.020 0.419 0.072 14.879 0.047 0.320 2.194 0.17 79566. 0.0247
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40.98 1.0303 0.0019 0.0000 0.0110 0.013 0.269 0.000 9.561 0.030 0.001 0.010 0.18 79987. 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 0.1211 0.0542 0.150 2.367 2.373 112.023 0.267 10.553 9.606 0.22 97122. 0.6201
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1.89 0.0356 0.0770 0.1204 0.0556 0.154 2.428 2.358 114.885 0.274 10.489 9.310 0.22 97217. 0.5992
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3.78 0.0712 0.1491 0.1195 0.0571 0.158 2.491 2.342 117.874 0.281 10.416 9.011 0.22 97326. 0.5779
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5.66 0.1068 0.2162 0.1186 0.0586 0.162 2.556 2.323 120.945 0.289 10.331 8.710 0.22 97448. 0.5563
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7.55 0.1424 0.2784 0.1174 0.0601 0.166 2.621 2.300 124.043 0.296 10.231 8.411 0.22 97586. 0.5346
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9.44 0.1780 0.3358 0.1161 0.0615 0.170 2.686 2.274 127.105 0.303 10.115 8.115 0.22 97739. 0.5129
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11.33 0.2136 0.3885 0.1146 0.0630 0.174 2.748 2.244 130.055 0.310 9.981 7.825 0.22 97909. 0.4913
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13.21 0.2492 0.4369 0.1128 0.0643 0.178 2.806 2.209 132.814 0.317 9.824 7.543 0.22 98095. 0.4698
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15.10 0.2847 0.4812 0.1107 0.0655 0.181 2.859 2.168 135.294 0.323 9.644 7.269 0.22 98299. 0.4486
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16.99 0.3203 0.5217 0.1083 0.0665 0.184 2.903 2.122 137.403 0.328 9.438 7.005 0.22 98522. 0.4276
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18.88 0.3559 0.5585 0.1056 0.0673 0.186 2.938 2.069 139.049 0.332 9.204 6.750 0.22 98762. 0.4069
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20.76 0.3915 0.5921 0.1026 0.0678 0.188 2.961 2.010 140.136 0.335 8.939 6.505 0.22 99021. 0.3865
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22.65 0.4271 0.6225 0.0992 0.0681 0.189 2.970 1.943 140.566 0.336 8.642 6.269 0.22 99298. 0.3662
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24.54 0.4627 0.6500 0.0954 0.0679 0.188 2.963 1.868 140.238 0.335 8.310 6.042 0.22 99593. 0.3461
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26.43 0.4983 0.6747 0.0912 0.0673 0.186 2.938 1.785 139.052 0.332 7.942 5.824 0.22 99907. 0.3262
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28.31 0.5339 0.6968 0.0865 0.0663 0.184 2.893 1.695 136.922 0.327 7.538 5.614 0.23 100238. 0.3063
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30.20 0.5695 0.7163 0.0815 0.0648 0.179 2.827 1.596 133.810 0.319 7.099 5.410 0.23 100588. 0.2865
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32.09 0.6051 0.7332 0.0761 0.0628 0.174 2.741 1.491 129.729 0.310 6.631 5.212 0.23 100956. 0.2667
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33.98 0.6407 0.7475 0.0704 0.0604 0.167 2.635 1.380 124.724 0.298 6.138 5.018 0.23 101341. 0.2471
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35.86 0.6763 0.7588 0.0646 0.0575 0.159 2.511 1.265 118.843 0.284 5.625 4.826 0.23 101743. 0.2275
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37.75 0.7119 0.7669 0.0585 0.0543 0.150 2.369 1.146 112.130 0.268 5.096 4.634 0.23 102163. 0.2079
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39.64 0.7475 0.7713 0.0523 0.0506 0.140 2.211 1.024 104.617 0.250 4.553 4.438 0.23 102599. 0.1882
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41.53 0.7831 0.7709 0.0459 0.0466 0.129 2.036 0.899 96.333 0.230 4.000 4.234 0.23 103053. 0.1683
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43.41 0.8186 0.7644 0.0395 0.0423 0.117 1.845 0.773 87.300 0.208 3.438 4.016 0.23 103523. 0.1480
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45.30 0.8542 0.7495 0.0329 0.0375 0.104 1.639 0.645 77.542 0.185 2.870 3.774 0.23 104010. 0.1270
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47.19 0.8898 0.7221 0.0264 0.0325 0.090 1.418 0.516 67.088 0.160 2.296 3.490 0.23 104513. 0.1051
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49.08 0.9254 0.6743 0.0197 0.0271 0.075 1.183 0.387 55.969 0.134 1.720 3.134 0.23 105032. 0.0817
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50.96 0.9610 0.5891 0.0131 0.0214 0.059 0.935 0.257 44.231 0.106 1.144 2.637 0.23 105567. 0.0560
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52.85 0.9966 0.4214 0.0065 0.0155 0.043 0.675 0.128 31.928 0.076 0.569 1.819 0.23 106118. 0.0273
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54.74 1.0322 0.0005 0.0000 0.0093 0.026 0.404 0.000 19.123 0.046 0.000 0.002 0.23 106680. 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 0.1214 0.0534 0.289 3.640 3.715 215.331 0.411 16.526 7.826 0.28 121400. 0.6322
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2.38 0.0360 0.0792 0.1207 0.0548 0.296 3.737 3.694 221.042 0.422 16.429 7.579 0.28 121520. 0.6105
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4.77 0.0719 0.1532 0.1198 0.0563 0.304 3.838 3.668 227.017 0.434 16.316 7.329 0.28 121658. 0.5883
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7.15 0.1079 0.2219 0.1189 0.0578 0.313 3.942 3.639 233.164 0.445 16.184 7.078 0.28 121813. 0.5659
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9.54 0.1438 0.2855 0.1177 0.0593 0.321 4.046 3.604 239.374 0.457 16.030 6.829 0.28 121987. 0.5433
|
|
11.92 0.1798 0.3440 0.1164 0.0609 0.329 4.150 3.563 245.513 0.469 15.849 6.583 0.28 122181. 0.5208
|
|
14.30 0.2158 0.3977 0.1149 0.0623 0.337 4.250 3.516 251.431 0.480 15.638 6.342 0.28 122397. 0.4984
|
|
16.69 0.2517 0.4468 0.1131 0.0637 0.345 4.344 3.461 256.962 0.491 15.392 6.108 0.28 122634. 0.4762
|
|
19.07 0.2877 0.4918 0.1110 0.0649 0.351 4.428 3.397 261.927 0.500 15.108 5.882 0.28 122894. 0.4543
|
|
21.45 0.3237 0.5327 0.1086 0.0660 0.357 4.499 3.323 266.140 0.508 14.782 5.664 0.28 123176. 0.4327
|
|
23.84 0.3596 0.5700 0.1058 0.0668 0.361 4.554 3.240 269.407 0.515 14.409 5.454 0.28 123482. 0.4114
|
|
26.22 0.3956 0.6039 0.1027 0.0673 0.364 4.590 3.145 271.534 0.519 13.987 5.253 0.28 123811. 0.3904
|
|
28.61 0.4315 0.6346 0.0993 0.0675 0.365 4.603 3.038 272.320 0.520 13.513 5.060 0.28 124164. 0.3696
|
|
30.99 0.4675 0.6623 0.0954 0.0673 0.364 4.591 2.919 271.559 0.519 12.982 4.875 0.28 124540. 0.3491
|
|
33.37 0.5035 0.6873 0.0910 0.0667 0.361 4.548 2.786 269.046 0.514 12.394 4.697 0.28 124940. 0.3286
|
|
35.76 0.5394 0.7096 0.0863 0.0656 0.355 4.473 2.641 264.618 0.505 11.747 4.527 0.28 125363. 0.3083
|
|
38.14 0.5754 0.7294 0.0811 0.0640 0.346 4.365 2.483 258.205 0.493 11.045 4.362 0.28 125808. 0.2881
|
|
40.53 0.6114 0.7466 0.0756 0.0619 0.335 4.224 2.315 249.849 0.477 10.297 4.202 0.28 126276. 0.2680
|
|
42.91 0.6473 0.7612 0.0699 0.0594 0.321 4.051 2.138 239.641 0.458 9.510 4.047 0.28 126767. 0.2480
|
|
45.29 0.6833 0.7730 0.0638 0.0564 0.305 3.849 1.954 227.678 0.435 8.692 3.893 0.28 127279. 0.2281
|
|
47.68 0.7192 0.7816 0.0577 0.0531 0.287 3.618 1.765 214.042 0.409 7.849 3.739 0.28 127814. 0.2082
|
|
50.06 0.7552 0.7864 0.0513 0.0493 0.267 3.361 1.571 198.797 0.380 6.986 3.583 0.29 128370. 0.1882
|
|
52.44 0.7912 0.7865 0.0448 0.0451 0.244 3.077 1.373 181.998 0.348 6.106 3.421 0.29 128948. 0.1680
|
|
54.83 0.8271 0.7805 0.0383 0.0406 0.220 2.767 1.172 163.691 0.313 5.212 3.247 0.29 129546. 0.1473
|
|
57.21 0.8631 0.7657 0.0317 0.0357 0.193 2.433 0.969 143.926 0.275 4.309 3.053 0.29 130166. 0.1259
|
|
59.60 0.8990 0.7376 0.0250 0.0304 0.165 2.075 0.764 122.761 0.234 3.399 2.823 0.29 130807. 0.1034
|
|
61.98 0.9350 0.6867 0.0183 0.0249 0.134 1.695 0.559 100.270 0.192 2.485 2.527 0.29 131468. 0.0792
|
|
64.36 0.9710 0.5910 0.0115 0.0190 0.103 1.294 0.353 76.547 0.146 1.572 2.094 0.29 132150. 0.0522
|
|
66.75 1.0069 0.3832 0.0049 0.0128 0.069 0.874 0.149 51.715 0.099 0.664 1.310 0.29 132850. 0.0212
|
|
69.13 1.0429
|
|
|
|
|
|
|
|
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 0.1217 0.0529 0.494 5.190 5.363 368.430 0.586 23.855 6.602 0.33 145676. 0.6408
|
|
2.84 0.0357 0.0795 0.1210 0.0543 0.507 5.329 5.333 378.317 0.602 23.721 6.394 0.33 145819. 0.6189
|
|
5.67 0.0713 0.1538 0.1202 0.0558 0.521 5.475 5.298 388.678 0.619 23.566 6.183 0.33 145982. 0.5964
|
|
8.51 0.1070 0.2228 0.1193 0.0573 0.536 5.626 5.257 399.355 0.636 23.384 5.971 0.33 146166. 0.5738
|
|
11.35 0.1427 0.2866 0.1182 0.0588 0.550 5.778 5.209 410.161 0.653 23.171 5.761 0.33 146373. 0.5510
|
|
14.19 0.1783 0.3454 0.1169 0.0604 0.564 5.929 5.153 420.873 0.670 22.920 5.553 0.33 146603. 0.5283
|
|
17.02 0.2140 0.3993 0.1154 0.0619 0.578 6.075 5.087 431.234 0.686 22.627 5.350 0.33 146858. 0.5058
|
|
19.86 0.2497 0.4487 0.1137 0.0633 0.591 6.212 5.010 440.961 0.702 22.284 5.153 0.33 147139. 0.4834
|
|
22.70 0.2853 0.4938 0.1116 0.0645 0.603 6.336 4.921 449.747 0.716 21.887 4.962 0.33 147447. 0.4614
|
|
25.53 0.3210 0.5350 0.1093 0.0656 0.613 6.442 4.818 457.272 0.728 21.430 4.779 0.33 147781. 0.4396
|
|
28.37 0.3567 0.5725 0.1066 0.0664 0.621 6.525 4.700 463.206 0.737 20.907 4.603 0.34 148144. 0.4182
|
|
31.21 0.3923 0.6066 0.1036 0.0670 0.627 6.582 4.567 467.215 0.744 20.314 4.434 0.34 148533. 0.3971
|
|
34.05 0.4280 0.6376 0.1002 0.0673 0.629 6.606 4.417 468.957 0.746 19.645 4.272 0.34 148951. 0.3763
|
|
36.88 0.4637 0.6657 0.0964 0.0671 0.628 6.594 4.248 468.081 0.745 18.897 4.117 0.34 149396. 0.3556
|
|
39.72 0.4993 0.6910 0.0922 0.0666 0.623 6.540 4.062 464.236 0.739 18.066 3.968 0.34 149869. 0.3352
|
|
42.56 0.5350 0.7138 0.0875 0.0656 0.613 6.440 3.856 457.125 0.728 17.150 3.826 0.34 150369. 0.3148
|
|
45.40 0.5707 0.7341 0.0824 0.0641 0.599 6.291 3.632 446.604 0.711 16.155 3.689 0.34 150896. 0.2946
|
|
48.23 0.6063 0.7520 0.0770 0.0621 0.580 6.096 3.393 432.715 0.689 15.091 3.556 0.34 151450. 0.2745
|
|
51.07 0.6420 0.7674 0.0713 0.0596 0.557 5.855 3.141 415.610 0.661 13.970 3.428 0.34 152030. 0.2546
|
|
53.91 0.6777 0.7802 0.0653 0.0567 0.530 5.571 2.878 395.453 0.629 12.803 3.301 0.34 152636. 0.2348
|
|
56.74 0.7134 0.7901 0.0592 0.0534 0.499 5.246 2.608 372.387 0.593 11.599 3.176 0.34 153269. 0.2150
|
|
59.58 0.7490 0.7966 0.0529 0.0497 0.465 4.882 2.330 346.528 0.552 10.364 3.050 0.34 153926. 0.1951
|
|
62.42 0.7847 0.7990 0.0464 0.0456 0.426 4.479 2.047 317.969 0.506 9.104 2.920 0.34 154610. 0.1751
|
|
65.26 0.8204 0.7959 0.0399 0.0411 0.385 4.040 1.759 286.791 0.456 7.825 2.782 0.34 155318. 0.1547
|
|
68.09 0.8560 0.7855 0.0333 0.0363 0.339 3.565 1.468 253.079 0.403 6.530 2.631 0.35 156051. 0.1336
|
|
70.93 0.8917 0.7637 0.0267 0.0311 0.291 3.056 1.175 216.926 0.345 5.225 2.456 0.35 156809. 0.1116
|
|
73.77 0.9274 0.7231 0.0200 0.0256 0.239 2.514 0.880 178.451 0.284 3.913 2.236 0.35 157591. 0.0879
|
|
76.60 0.9630 0.6462 0.0133 0.0198 0.185 1.941 0.585 137.809 0.219 2.601 1.924 0.35 158397. 0.0617
|
|
79.44 0.9987 0.4827 0.0066 0.0137 0.128 1.341 0.291 95.200 0.152 1.294 1.386 0.35 159226. 0.0313
|
|
82.28 1.0344 -0.0008 0.0000 0.0073 0.068 0.716 0.000 50.824 0.081 -0.001 -0.002 0.35 160068. 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 0.1220 0.0525 0.780 7.024 7.319 581.704 0.794 32.556 5.707 0.39 169951. 0.6471
|
|
3.31 0.0357 0.0802 0.1214 0.0540 0.801 7.216 7.280 597.587 0.815 32.382 5.526 0.39 170118. 0.6249
|
|
6.63 0.0714 0.1552 0.1206 0.0555 0.824 7.417 7.234 614.261 0.838 32.178 5.342 0.39 170308. 0.6022
|
|
9.94 0.1071 0.2247 0.1197 0.0570 0.847 7.625 7.181 631.474 0.861 31.940 5.158 0.39 170522. 0.5793
|
|
13.25 0.1428 0.2890 0.1186 0.0586 0.870 7.836 7.118 648.927 0.885 31.659 4.975 0.39 170763. 0.5563
|
|
16.56 0.1785 0.3481 0.1174 0.0602 0.893 8.045 7.043 666.260 0.909 31.327 4.795 0.39 171032. 0.5333
|
|
19.88 0.2142 0.4024 0.1159 0.0617 0.916 8.248 6.955 683.058 0.932 30.936 4.618 0.39 171330. 0.5105
|
|
23.19 0.2499 0.4521 0.1142 0.0631 0.937 8.438 6.852 698.858 0.953 30.479 4.447 0.39 171658. 0.4879
|
|
26.50 0.2856 0.4975 0.1122 0.0644 0.956 8.611 6.732 713.162 0.973 29.946 4.282 0.39 172018. 0.4656
|
|
29.81 0.3213 0.5388 0.1099 0.0655 0.973 8.760 6.594 725.448 0.990 29.330 4.123 0.39 172409. 0.4437
|
|
33.13 0.3570 0.5766 0.1073 0.0664 0.986 8.877 6.435 735.183 1.003 28.623 3.970 0.39 172832. 0.4221
|
|
36.44 0.3926 0.6109 0.1043 0.0670 0.995 8.957 6.254 741.821 1.012 27.819 3.824 0.39 173287. 0.4008
|
|
39.75 0.4283 0.6421 0.1009 0.0673 0.999 8.993 6.050 744.812 1.016 26.910 3.684 0.39 173775. 0.3798
|
|
43.06 0.4640 0.6703 0.0970 0.0672 0.997 8.979 5.821 743.586 1.014 25.892 3.551 0.39 174296. 0.3590
|
|
46.38 0.4997 0.6959 0.0928 0.0666 0.989 8.906 5.566 737.583 1.006 24.758 3.423 0.39 174849. 0.3385
|
|
49.69 0.5354 0.7189 0.0881 0.0656 0.974 8.770 5.285 726.316 0.991 23.508 3.300 0.39 175433. 0.3180
|
|
53.00 0.5711 0.7396 0.0830 0.0641 0.952 8.568 4.979 709.551 0.968 22.147 3.183 0.40 176050. 0.2977
|
|
56.31 0.6068 0.7578 0.0775 0.0621 0.922 8.300 4.652 687.352 0.938 20.691 3.070 0.40 176697. 0.2775
|
|
59.63 0.6425 0.7737 0.0718 0.0596 0.885 7.969 4.307 659.958 0.900 19.156 2.960 0.40 177375. 0.2574
|
|
62.94 0.6782 0.7871 0.0658 0.0567 0.842 7.578 3.947 627.637 0.856 17.557 2.853 0.40 178084. 0.2375
|
|
66.25 0.7139 0.7976 0.0596 0.0534 0.792 7.132 3.576 590.619 0.806 15.906 2.746 0.40 178823. 0.2177
|
|
69.57 0.7496 0.8050 0.0533 0.0496 0.736 6.630 3.195 549.091 0.749 14.213 2.640 0.40 179592. 0.1978
|
|
72.88 0.7853 0.8084 0.0468 0.0455 0.675 6.076 2.807 503.202 0.686 12.486 2.530 0.40 180391. 0.1777
|
|
76.19 0.8210 0.8067 0.0402 0.0409 0.608 5.471 2.412 453.086 0.618 10.731 2.415 0.40 181218. 0.1572
|
|
79.50 0.8567 0.7979 0.0336 0.0360 0.535 4.816 2.013 398.876 0.544 8.954 2.289 0.40 182075. 0.1361
|
|
82.82 0.8924 0.7783 0.0268 0.0308 0.457 4.114 1.610 340.724 0.465 7.163 2.144 0.40 182960. 0.1140
|
|
86.13 0.9281 0.7406 0.0201 0.0252 0.374 3.367 1.206 278.822 0.380 5.363 1.961 0.41 183874. 0.0903
|
|
89.44 0.9638 0.6673 0.0133 0.0193 0.286 2.577 0.801 213.421 0.291 3.562 1.702 0.41 184816. 0.0638
|
|
92.75 0.9995 0.5062 0.0066 0.0131 0.194 1.749 0.398 144.846 0.198 1.768 1.245 0.41 185785. 0.0329
|
|
96.07 1.0352 -0.0054 0.0000 0.0066 0.098 0.886 -0.002 73.410 0.100 -0.009 -0.013 0.41 186767. 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 0.1224 0.0524 1.161 9.150 9.587 866.041 1.034 42.645 5.021 0.44 194223. 0.6516
|
|
3.79 0.0357 0.0807 0.1217 0.0539 1.194 9.403 9.539 890.021 1.062 42.430 4.861 0.44 194413. 0.6293
|
|
7.57 0.0714 0.1560 0.1210 0.0554 1.227 9.670 9.482 915.249 1.092 42.178 4.699 0.44 194630. 0.6065
|
|
11.36 0.1071 0.2259 0.1202 0.0570 1.262 9.946 9.416 941.350 1.124 41.880 4.537 0.44 194875. 0.5834
|
|
15.15 0.1428 0.2905 0.1192 0.0586 1.298 10.226 9.336 967.871 1.155 41.528 4.375 0.44 195151. 0.5603
|
|
18.93 0.1785 0.3499 0.1180 0.0602 1.333 10.505 9.242 994.266 1.187 41.109 4.216 0.44 195458. 0.5372
|
|
22.72 0.2142 0.4044 0.1165 0.0617 1.368 10.776 9.131 1019.901 1.217 40.614 4.061 0.45 195798. 0.5143
|
|
26.51 0.2499 0.4543 0.1149 0.0632 1.400 11.031 9.000 1044.068 1.246 40.030 3.910 0.45 196173. 0.4916
|
|
30.29 0.2856 0.4998 0.1129 0.0645 1.430 11.263 8.846 1066.007 1.272 39.347 3.764 0.45 196584. 0.4692
|
|
34.08 0.3213 0.5414 0.1106 0.0657 1.455 11.462 8.668 1084.915 1.295 38.554 3.624 0.45 197031. 0.4471
|
|
37.87 0.3570 0.5792 0.1080 0.0666 1.475 11.622 8.462 1099.973 1.313 37.640 3.489 0.45 197515. 0.4254
|
|
41.65 0.3927 0.6137 0.1050 0.0672 1.489 11.731 8.228 1110.351 1.325 36.597 3.361 0.45 198036. 0.4041
|
|
45.44 0.4284 0.6451 0.1016 0.0675 1.496 11.783 7.962 1115.207 1.331 35.415 3.238 0.45 198595. 0.3830
|
|
49.23 0.4641 0.6735 0.0978 0.0674 1.493 11.766 7.664 1113.686 1.329 34.087 3.121 0.45 199190. 0.3621
|
|
53.01 0.4998 0.6993 0.0936 0.0669 1.482 11.674 7.330 1104.931 1.319 32.606 3.009 0.45 199823. 0.3415
|
|
56.80 0.5355 0.7226 0.0889 0.0659 1.459 11.497 6.963 1088.206 1.299 30.969 2.902 0.45 200492. 0.3209
|
|
60.59 0.5712 0.7435 0.0837 0.0643 1.426 11.232 6.562 1063.139 1.269 29.186 2.799 0.45 201197. 0.3005
|
|
64.37 0.6069 0.7621 0.0783 0.0623 1.381 10.880 6.132 1029.819 1.229 27.274 2.701 0.45 201938. 0.2803
|
|
68.16 0.6426 0.7784 0.0725 0.0598 1.326 10.445 5.678 988.609 1.180 25.257 2.605 0.45 202714. 0.2602
|
|
71.94 0.6783 0.7923 0.0664 0.0569 1.260 9.930 5.206 939.912 1.122 23.155 2.512 0.45 203525. 0.2402
|
|
75.73 0.7140 0.8035 0.0602 0.0535 1.186 9.341 4.717 884.085 1.055 20.982 2.420 0.46 204370. 0.2203
|
|
79.52 0.7497 0.8116 0.0538 0.0497 1.102 8.678 4.216 821.410 0.980 18.754 2.328 0.46 205250. 0.2004
|
|
83.30 0.7854 0.8160 0.0473 0.0455 1.009 7.946 3.705 752.117 0.898 16.479 2.234 0.46 206163. 0.1802
|
|
87.09 0.8211 0.8155 0.0407 0.0409 0.907 7.146 3.185 676.406 0.807 14.167 2.136 0.46 207110. 0.1598
|
|
90.88 0.8568 0.8082 0.0339 0.0360 0.797 6.281 2.659 594.482 0.710 11.827 2.029 0.46 208089. 0.1386
|
|
94.66 0.8925 0.7908 0.0272 0.0307 0.679 5.352 2.128 506.572 0.605 9.466 1.905 0.46 209102. 0.1165
|
|
98.45 0.9283 0.7559 0.0204 0.0250 0.554 4.363 1.595 412.968 0.493 7.093 1.751 0.46 210147. 0.0927
|
|
102.24 0.9640 0.6866 0.0135 0.0190 0.421 3.318 1.061 314.049 0.375 4.718 1.532 0.46 211224. 0.0661
|
|
106.02 0.9997 0.5302 0.0068 0.0127 0.282 2.222 0.529 210.310 0.251 2.353 1.141 0.47 212331. 0.0348
|
|
109.81 1.0354 0.0036 0.0000 0.0062 0.137 1.080 0.002 102.221 0.122 0.007 0.007 0.47 213453. 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 0.1227 0.0524 1.653 11.579 12.172 1232.947 1.308 54.142 4.478 0.50 218493. 0.6548
|
|
4.26 0.0357 0.0810 0.1222 0.0539 1.700 11.904 12.115 1267.516 1.345 53.887 4.335 0.50 218707. 0.6324
|
|
8.52 0.0714 0.1566 0.1215 0.0554 1.749 12.246 12.048 1303.976 1.384 53.588 4.191 0.50 218950. 0.6096
|
|
12.79 0.1072 0.2268 0.1207 0.0570 1.799 12.601 11.968 1341.793 1.424 53.232 4.045 0.50 219226. 0.5866
|
|
17.05 0.1429 0.2916 0.1197 0.0587 1.851 12.963 11.872 1380.320 1.465 52.808 3.901 0.50 219535. 0.5634
|
|
21.31 0.1786 0.3512 0.1186 0.0603 1.903 13.324 11.758 1418.759 1.505 52.300 3.759 0.50 219880. 0.5402
|
|
25.57 0.2143 0.4059 0.1172 0.0619 1.953 13.676 11.622 1456.183 1.545 51.695 3.620 0.50 220264. 0.5172
|
|
29.84 0.2501 0.4559 0.1156 0.0634 2.000 14.008 11.461 1491.554 1.583 50.978 3.485 0.50 220686. 0.4945
|
|
34.10 0.2858 0.5015 0.1137 0.0648 2.043 14.310 11.271 1523.751 1.617 50.133 3.355 0.50 221148. 0.4721
|
|
38.36 0.3215 0.5432 0.1114 0.0659 2.081 14.572 11.049 1551.595 1.646 49.146 3.230 0.50 221652. 0.4500
|
|
42.62 0.3572 0.5811 0.1088 0.0669 2.111 14.781 10.792 1573.880 1.670 48.003 3.110 0.50 222197. 0.4282
|
|
46.88 0.3929 0.6157 0.1059 0.0676 2.131 14.927 10.498 1589.389 1.686 46.693 2.996 0.50 222785. 0.4068
|
|
51.15 0.4287 0.6472 0.1025 0.0679 2.141 14.997 10.163 1596.900 1.694 45.204 2.887 0.50 223414. 0.3857
|
|
55.41 0.4644 0.6759 0.0987 0.0678 2.139 14.981 9.785 1595.165 1.693 43.526 2.782 0.51 224086. 0.3648
|
|
59.67 0.5001 0.7019 0.0944 0.0673 2.123 14.866 9.364 1582.947 1.680 41.649 2.683 0.51 224798. 0.3441
|
|
63.93 0.5358 0.7254 0.0897 0.0663 2.091 14.643 8.896 1559.178 1.654 39.571 2.588 0.51 225553. 0.3235
|
|
68.20 0.5715 0.7465 0.0846 0.0647 2.043 14.306 8.386 1523.299 1.616 37.302 2.497 0.51 226347. 0.3031
|
|
72.46 0.6073 0.7655 0.0790 0.0627 1.979 13.856 7.839 1475.434 1.565 34.867 2.410 0.51 227183. 0.2828
|
|
76.72 0.6430 0.7822 0.0732 0.0602 1.899 13.299 7.261 1416.099 1.503 32.295 2.326 0.51 228057. 0.2626
|
|
80.98 0.6787 0.7965 0.0671 0.0572 1.805 12.640 6.657 1345.897 1.428 29.611 2.243 0.51 228971. 0.2426
|
|
85.24 0.7144 0.8082 0.0608 0.0538 1.697 11.883 6.033 1265.344 1.343 26.837 2.163 0.51 229924. 0.2226
|
|
89.51 0.7502 0.8170 0.0544 0.0499 1.576 11.034 5.393 1174.857 1.247 23.989 2.082 0.51 230915. 0.2027
|
|
93.77 0.7859 0.8222 0.0478 0.0457 1.441 10.094 4.739 1074.770 1.140 21.081 2.000 0.52 231944. 0.1825
|
|
98.03 0.8216 0.8228 0.0411 0.0410 1.295 9.066 4.075 965.377 1.024 18.124 1.914 0.52 233011. 0.1620
|
|
102.29 0.8573 0.8169 0.0343 0.0360 1.136 7.954 3.401 846.970 0.899 15.130 1.822 0.52 234114. 0.1408
|
|
106.56 0.8930 0.8012 0.0274 0.0306 0.965 6.761 2.722 719.883 0.764 12.108 1.715 0.52 235255. 0.1186
|
|
110.82 0.9288 0.7686 0.0206 0.0248 0.784 5.490 2.039 584.534 0.620 9.069 1.582 0.52 236432. 0.0947
|
|
115.08 0.9645 0.7024 0.0137 0.0188 0.592 4.146 1.355 441.474 0.468 6.028 1.392 0.52 237644. 0.0679
|
|
119.34 1.0002 0.5489 0.0068 0.0124 0.391 2.737 0.674 291.428 0.309 2.998 1.049 0.52 238892. 0.0361
|
|
123.60 1.0359 -0.0027 0.0000 0.0057 0.181 1.268 -0.001 135.045 0.143 -0.007 -0.005 0.53 240152. 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 0.1232 0.0525 2.273 14.324 15.078 1694.709 1.618 67.067 4.035 0.56 242760. 0.6568
|
|
4.74 0.0357 0.0812 0.1226 0.0540 2.337 14.730 15.013 1742.724 1.664 66.777 3.907 0.56 242997. 0.6345
|
|
9.47 0.0715 0.1569 0.1220 0.0556 2.405 15.159 14.936 1793.527 1.713 66.435 3.777 0.56 243267. 0.6118
|
|
14.21 0.1072 0.2272 0.1212 0.0572 2.476 15.606 14.844 1846.393 1.763 66.026 3.646 0.56 243572. 0.5888
|
|
18.95 0.1429 0.2921 0.1203 0.0589 2.548 16.063 14.733 1900.416 1.815 65.534 3.516 0.56 243915. 0.5657
|
|
23.69 0.1787 0.3518 0.1193 0.0606 2.621 16.520 14.600 1954.482 1.866 64.941 3.388 0.56 244299. 0.5426
|
|
28.42 0.2144 0.4066 0.1179 0.0622 2.692 16.966 14.440 2007.277 1.917 64.227 3.263 0.56 244724. 0.5196
|
|
33.16 0.2501 0.4567 0.1164 0.0637 2.759 17.389 14.248 2057.331 1.965 63.374 3.141 0.56 245194. 0.4969
|
|
37.90 0.2859 0.5024 0.1145 0.0652 2.820 17.775 14.020 2103.042 2.008 62.360 3.024 0.56 245708. 0.4745
|
|
42.64 0.3216 0.5441 0.1123 0.0664 2.873 18.111 13.752 2142.729 2.046 61.168 2.911 0.56 246268. 0.4524
|
|
47.37 0.3573 0.5822 0.1098 0.0674 2.916 18.381 13.440 2174.676 2.077 59.781 2.803 0.56 246875. 0.4307
|
|
52.11 0.3931 0.6169 0.1068 0.0681 2.946 18.571 13.080 2197.152 2.098 58.181 2.700 0.56 247528. 0.4093
|
|
56.85 0.4288 0.6485 0.1035 0.0684 2.962 18.666 12.670 2208.432 2.109 56.354 2.602 0.56 248229. 0.3882
|
|
61.59 0.4645 0.6773 0.0997 0.0684 2.959 18.652 12.205 2206.773 2.107 54.288 2.509 0.56 248976. 0.3673
|
|
66.32 0.5003 0.7035 0.0954 0.0679 2.937 18.514 11.684 2190.450 2.092 51.970 2.419 0.56 249770. 0.3466
|
|
71.06 0.5360 0.7272 0.0907 0.0669 2.894 18.240 11.106 2157.958 2.061 49.397 2.334 0.56 250609. 0.3260
|
|
75.80 0.5717 0.7486 0.0855 0.0653 2.828 17.822 10.473 2108.495 2.013 46.583 2.253 0.56 251494. 0.3056
|
|
80.54 0.6075 0.7679 0.0800 0.0633 2.739 17.261 9.792 2042.211 1.950 43.556 2.175 0.57 252424. 0.2852
|
|
85.27 0.6432 0.7849 0.0741 0.0607 2.628 16.565 9.072 1959.836 1.872 40.354 2.100 0.57 253397. 0.2651
|
|
90.01 0.6790 0.7997 0.0680 0.0577 2.497 15.740 8.320 1862.220 1.778 37.010 2.027 0.57 254414. 0.2450
|
|
94.75 0.7147 0.8120 0.0616 0.0542 2.347 14.792 7.543 1750.104 1.671 33.549 1.955 0.57 255475. 0.2250
|
|
99.49 0.7504 0.8214 0.0551 0.0503 2.178 13.727 6.743 1624.078 1.551 29.995 1.883 0.57 256577. 0.2050
|
|
104.22 0.7862 0.8274 0.0484 0.0460 1.991 12.548 5.927 1484.616 1.418 26.364 1.811 0.57 257722. 0.1848
|
|
108.96 0.8219 0.8289 0.0416 0.0413 1.786 11.260 5.097 1332.133 1.272 22.670 1.735 0.57 258908. 0.1642
|
|
113.70 0.8576 0.8243 0.0348 0.0362 1.565 9.864 4.255 1167.036 1.114 18.927 1.654 0.58 260136. 0.1430
|
|
118.44 0.8934 0.8103 0.0278 0.0307 1.327 8.366 3.406 989.789 0.945 15.148 1.561 0.58 261405. 0.1207
|
|
123.17 0.9291 0.7801 0.0208 0.0248 1.074 6.770 2.551 800.975 0.765 11.347 1.445 0.58 262714. 0.0967
|
|
127.91 0.9648 0.7170 0.0138 0.0186 0.806 5.083 1.695 601.365 0.574 7.540 1.279 0.58 264062. 0.0698
|
|
132.65 1.0006 0.5670 0.0069 0.0121 0.526 3.313 0.843 391.975 0.374 3.748 0.975 0.58 265449. 0.0375
|
|
137.39 1.0363 -0.0057 0.0000 0.0054 0.233 1.468 -0.004 173.680 0.166 -0.016 -0.010 0.58 266847. 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 0.1236 0.0527 3.038 17.405 18.309 2265.115 1.966 81.439 3.666 0.61 267024. 0.6575
|
|
5.21 0.0357 0.0811 0.1231 0.0542 3.124 17.901 18.238 2329.730 2.022 81.122 3.551 0.61 267284. 0.6355
|
|
10.43 0.0715 0.1569 0.1225 0.0558 3.216 18.429 18.153 2398.371 2.082 80.746 3.433 0.61 267580. 0.6130
|
|
15.64 0.1072 0.2272 0.1219 0.0575 3.312 18.980 18.052 2470.096 2.144 80.293 3.315 0.61 267915. 0.5903
|
|
20.85 0.1430 0.2922 0.1210 0.0592 3.411 19.545 17.928 2543.695 2.208 79.744 3.197 0.61 268292. 0.5673
|
|
26.06 0.1787 0.3520 0.1200 0.0609 3.510 20.114 17.778 2617.653 2.272 79.075 3.080 0.61 268713. 0.5443
|
|
31.28 0.2145 0.4067 0.1188 0.0626 3.608 20.671 17.595 2690.161 2.335 78.260 2.966 0.61 269180. 0.5215
|
|
36.49 0.2502 0.4568 0.1173 0.0642 3.700 21.201 17.373 2759.170 2.395 77.276 2.856 0.61 269696. 0.4989
|
|
41.70 0.2859 0.5026 0.1155 0.0657 3.785 21.687 17.108 2822.442 2.450 76.095 2.749 0.61 270262. 0.4766
|
|
46.91 0.3217 0.5444 0.1134 0.0670 3.859 22.111 16.793 2877.638 2.498 74.694 2.647 0.61 270878. 0.4546
|
|
52.13 0.3574 0.5825 0.1109 0.0680 3.919 22.455 16.423 2922.357 2.537 73.049 2.549 0.61 271546. 0.4329
|
|
57.34 0.3932 0.6173 0.1080 0.0688 3.962 22.700 15.994 2954.205 2.565 71.141 2.456 0.62 272266. 0.4116
|
|
62.55 0.4289 0.6490 0.1046 0.0692 3.984 22.827 15.501 2970.800 2.579 68.951 2.367 0.62 273038. 0.3905
|
|
67.76 0.4647 0.6779 0.1009 0.0691 3.983 22.819 14.942 2969.769 2.578 66.461 2.282 0.62 273862. 0.3697
|
|
72.98 0.5004 0.7043 0.0966 0.0686 3.954 22.658 14.312 2948.764 2.560 63.659 2.201 0.62 274736. 0.3490
|
|
78.19 0.5361 0.7282 0.0919 0.0676 3.897 22.327 13.610 2905.742 2.523 60.538 2.124 0.62 275661. 0.3285
|
|
83.40 0.5719 0.7499 0.0867 0.0661 3.808 21.819 12.841 2839.574 2.465 57.115 2.051 0.62 276636. 0.3080
|
|
88.61 0.6076 0.7695 0.0811 0.0640 3.688 21.134 12.011 2750.432 2.388 53.426 1.981 0.62 277661. 0.2877
|
|
93.83 0.6434 0.7869 0.0751 0.0614 3.539 20.280 11.132 2639.315 2.291 49.516 1.913 0.62 278734. 0.2675
|
|
99.04 0.6791 0.8021 0.0689 0.0584 3.362 19.266 10.213 2507.399 2.177 45.427 1.847 0.62 279854. 0.2474
|
|
104.25 0.7149 0.8149 0.0625 0.0548 3.159 18.101 9.261 2355.721 2.045 41.192 1.783 0.63 281022. 0.2274
|
|
109.46 0.7506 0.8250 0.0559 0.0509 2.930 16.790 8.282 2185.104 1.897 36.838 1.719 0.63 282237. 0.2073
|
|
114.68 0.7863 0.8317 0.0492 0.0465 2.677 15.339 7.281 1996.204 1.733 32.386 1.654 0.63 283498. 0.1871
|
|
119.89 0.8221 0.8342 0.0423 0.0417 2.400 13.751 6.262 1789.583 1.554 27.855 1.587 0.63 284804. 0.1665
|
|
125.10 0.8578 0.8308 0.0353 0.0365 2.100 12.031 5.230 1565.800 1.359 23.262 1.515 0.63 286156. 0.1452
|
|
130.31 0.8936 0.8184 0.0283 0.0309 1.777 10.185 4.186 1325.478 1.151 18.621 1.433 0.64 287553. 0.1228
|
|
135.53 0.9293 0.7904 0.0212 0.0249 1.434 8.217 3.136 1069.409 0.928 13.951 1.330 0.64 288993. 0.0987
|
|
140.74 0.9651 0.7304 0.0141 0.0186 1.071 6.137 2.084 798.635 0.693 9.272 1.184 0.64 290478. 0.0716
|
|
145.95 1.0008 0.5842 0.0070 0.0120 0.690 3.954 1.036 514.549 0.447 4.607 0.913 0.64 292004. 0.0389
|
|
151.16 1.0365 -0.0076 0.0000 0.0051 0.293 1.678 -0.006 218.328 0.190 -0.025 -0.012 0.64 293540. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 12000
|
|
|
|
V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
|
|
(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
|
|
0.00 0.0000 0.0000 0.1240 0.0533 3.983 20.920 21.868 2970.061 2.363 97.270 3.340 0.67 291285. 0.6545
|
|
5.69 0.0357 0.0807 0.1236 0.0548 4.095 21.511 21.793 3054.006 2.430 96.936 3.237 0.67 291567. 0.6333
|
|
11.37 0.0715 0.1562 0.1231 0.0564 4.216 22.142 21.704 3143.528 2.502 96.540 3.132 0.67 291889. 0.6115
|
|
17.06 0.1072 0.2263 0.1225 0.0581 4.341 22.803 21.596 3237.450 2.576 96.061 3.026 0.67 292253. 0.5893
|
|
22.75 0.1430 0.2912 0.1218 0.0598 4.471 23.485 21.464 3334.240 2.653 95.472 2.920 0.67 292663. 0.5670
|
|
28.44 0.1787 0.3509 0.1208 0.0615 4.602 24.173 21.301 3431.920 2.731 94.745 2.815 0.67 293121. 0.5445
|
|
34.12 0.2145 0.4058 0.1197 0.0633 4.731 24.850 21.099 3528.125 2.808 93.847 2.712 0.67 293630. 0.5222
|
|
39.81 0.2502 0.4560 0.1183 0.0649 4.855 25.499 20.851 3620.142 2.881 92.747 2.612 0.67 294192. 0.5000
|
|
45.50 0.2860 0.5018 0.1166 0.0664 4.968 26.096 20.551 3704.999 2.948 91.410 2.516 0.67 294809. 0.4780
|
|
51.19 0.3217 0.5437 0.1145 0.0678 5.068 26.621 20.190 3779.546 3.008 89.805 2.423 0.67 295482. 0.4563
|
|
56.87 0.3575 0.5819 0.1121 0.0689 5.150 27.051 19.762 3840.510 3.056 87.903 2.334 0.67 296211. 0.4349
|
|
62.56 0.3932 0.6168 0.1093 0.0697 5.209 27.361 19.262 3884.596 3.091 85.676 2.249 0.67 296997. 0.4137
|
|
68.25 0.4290 0.6487 0.1060 0.0701 5.241 27.530 18.683 3908.513 3.110 83.101 2.168 0.67 297840. 0.3928
|
|
73.93 0.4647 0.6778 0.1022 0.0701 5.242 27.533 18.021 3909.006 3.111 80.158 2.091 0.67 298740. 0.3720
|
|
79.62 0.5005 0.7043 0.0980 0.0696 5.207 27.349 17.273 3882.895 3.090 76.830 2.018 0.67 299696. 0.3515
|
|
85.31 0.5362 0.7285 0.0932 0.0686 5.133 26.959 16.437 3827.441 3.046 73.110 1.948 0.68 300708. 0.3310
|
|
91.00 0.5720 0.7504 0.0880 0.0671 5.017 26.351 15.516 3741.099 2.977 69.015 1.881 0.68 301773. 0.3106
|
|
96.68 0.6077 0.7703 0.0824 0.0650 4.860 25.526 14.521 3624.047 2.884 64.590 1.817 0.68 302893. 0.2903
|
|
102.37 0.6435 0.7881 0.0764 0.0624 4.664 24.495 13.465 3477.607 2.767 59.890 1.756 0.68 304065. 0.2701
|
|
108.06 0.6792 0.8038 0.0701 0.0592 4.430 23.268 12.358 3303.393 2.629 54.967 1.697 0.68 305290. 0.2500
|
|
113.74 0.7150 0.8171 0.0636 0.0556 4.161 21.855 11.210 3102.822 2.469 49.861 1.639 0.68 306566. 0.2299
|
|
119.43 0.7507 0.8278 0.0569 0.0516 3.858 20.264 10.028 2877.033 2.289 44.607 1.581 0.69 307893. 0.2098
|
|
125.12 0.7865 0.8353 0.0500 0.0471 3.523 18.503 8.820 2626.908 2.090 39.230 1.523 0.69 309270. 0.1895
|
|
130.81 0.8222 0.8388 0.0430 0.0422 3.156 16.575 7.588 2353.198 1.873 33.753 1.463 0.69 310697. 0.1689
|
|
136.49 0.8580 0.8366 0.0360 0.0369 2.758 14.486 6.339 2056.648 1.637 28.196 1.398 0.69 312173. 0.1475
|
|
142.18 0.8937 0.8257 0.0288 0.0312 2.331 12.242 5.076 1738.084 1.383 22.579 1.325 0.69 313698. 0.1251
|
|
147.87 0.9295 0.7998 0.0216 0.0251 1.876 9.851 3.804 1398.603 1.113 16.922 1.234 0.69 315271. 0.1009
|
|
153.56 0.9652 0.7427 0.0143 0.0186 1.394 7.324 2.529 1039.755 0.827 11.250 1.103 0.70 316891. 0.0735
|
|
159.24 1.0010 0.5997 0.0071 0.0119 0.890 4.675 1.257 663.672 0.528 5.591 0.859 0.70 318557. 0.0404
|
|
164.93 1.0367 -0.0089 0.0000 0.0049 0.365 1.918 -0.007 272.264 0.217 -0.033 -0.012 0.70 320229. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 13000
|
|
|
|
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 0.1245 0.0546 5.194 25.181 25.754 3872.908 2.845 114.552 3.016 0.72 315544. 0.6415
|
|
6.16 0.0357 0.0791 0.1241 0.0561 5.335 25.867 25.677 3978.549 2.922 114.213 2.927 0.72 315848. 0.6217
|
|
12.32 0.0715 0.1532 0.1237 0.0577 5.487 26.602 25.588 4091.518 3.005 113.813 2.837 0.72 316194. 0.6014
|
|
18.48 0.1072 0.2224 0.1231 0.0594 5.646 27.374 25.478 4210.321 3.093 113.327 2.745 0.72 316587. 0.5807
|
|
24.64 0.1430 0.2866 0.1225 0.0611 5.811 28.172 25.343 4332.979 3.183 112.724 2.653 0.72 317029. 0.5597
|
|
30.80 0.1787 0.3459 0.1217 0.0629 5.977 28.978 25.173 4456.897 3.274 111.969 2.562 0.72 317523. 0.5387
|
|
36.96 0.2145 0.4006 0.1206 0.0646 6.140 29.771 24.960 4578.960 3.364 111.020 2.472 0.72 318073. 0.5177
|
|
43.12 0.2502 0.4509 0.1193 0.0662 6.297 30.530 24.693 4695.616 3.449 109.835 2.385 0.72 318681. 0.4968
|
|
49.29 0.2860 0.4971 0.1178 0.0677 6.441 31.228 24.364 4803.045 3.528 108.371 2.301 0.72 319348. 0.4760
|
|
55.45 0.3217 0.5395 0.1158 0.0691 6.567 31.841 23.963 4897.246 3.597 106.586 2.219 0.73 320076. 0.4553
|
|
61.61 0.3575 0.5783 0.1135 0.0702 6.670 32.340 23.481 4974.138 3.654 104.442 2.141 0.73 320866. 0.4348
|
|
67.77 0.3932 0.6138 0.1107 0.0709 6.745 32.701 22.910 5029.593 3.695 101.903 2.066 0.73 321718. 0.4145
|
|
73.93 0.4289 0.6463 0.1075 0.0714 6.785 32.895 22.243 5059.466 3.716 98.939 1.994 0.73 322633. 0.3942
|
|
80.09 0.4647 0.6759 0.1038 0.0714 6.785 32.896 21.476 5059.625 3.717 95.523 1.925 0.73 323609. 0.3739
|
|
86.25 0.5004 0.7030 0.0996 0.0709 6.740 32.677 20.602 5025.969 3.692 91.636 1.859 0.73 324646. 0.3537
|
|
92.41 0.5362 0.7276 0.0948 0.0699 6.644 32.215 19.620 4954.783 3.640 87.270 1.796 0.73 325744. 0.3334
|
|
98.57 0.5719 0.7500 0.0896 0.0683 6.496 31.493 18.535 4843.784 3.558 82.443 1.736 0.73 326901. 0.3132
|
|
104.73 0.6077 0.7703 0.0839 0.0662 6.293 30.512 17.358 4692.867 3.447 77.208 1.678 0.74 328116. 0.2929
|
|
110.89 0.6434 0.7885 0.0778 0.0635 6.039 29.281 16.105 4503.510 3.308 71.633 1.622 0.74 329388. 0.2728
|
|
117.05 0.6792 0.8047 0.0715 0.0603 5.737 27.813 14.789 4277.714 3.142 65.780 1.568 0.74 330717. 0.2527
|
|
123.21 0.7149 0.8186 0.0649 0.0567 5.387 26.120 13.422 4017.397 2.951 59.702 1.515 0.74 332101. 0.2327
|
|
129.37 0.7507 0.8299 0.0581 0.0525 4.994 24.213 12.014 3724.100 2.736 53.438 1.463 0.74 333540. 0.2126
|
|
135.53 0.7864 0.8382 0.0511 0.0479 4.558 22.099 10.571 3399.000 2.497 47.022 1.411 0.74 335034. 0.1922
|
|
141.70 0.8221 0.8426 0.0440 0.0429 4.081 19.786 9.101 3043.140 2.235 40.480 1.356 0.75 336581. 0.1715
|
|
147.86 0.8579 0.8415 0.0368 0.0375 3.564 17.280 7.607 2657.702 1.952 33.835 1.298 0.75 338181. 0.1501
|
|
154.02 0.8936 0.8318 0.0295 0.0317 3.009 14.591 6.095 2244.147 1.648 27.111 1.232 0.75 339834. 0.1275
|
|
160.18 0.9294 0.8069 0.0221 0.0254 2.420 11.732 4.571 1804.445 1.325 20.333 1.149 0.75 341538. 0.1030
|
|
166.34 0.9651 0.7499 0.0147 0.0189 1.799 8.721 3.041 1341.315 0.985 13.527 1.028 0.76 343294. 0.0752
|
|
172.50 1.0009 0.6044 0.0073 0.0121 1.151 5.581 1.513 858.391 0.631 6.728 0.799 0.76 345099. 0.0412
|
|
178.66 1.0366 -0.0091 0.0000 0.0051 0.482 2.335 -0.009 359.189 0.264 -0.041 -0.012 0.76 346908. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 14000
|
|
|
|
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 0.1248 0.0576 6.839 30.788 29.956 5099.618 3.478 133.242 2.664 0.78 339799. 0.6112
|
|
6.63 0.0357 0.0754 0.1245 0.0591 7.013 31.573 29.881 5229.620 3.567 132.909 2.592 0.78 340124. 0.5937
|
|
13.27 0.0715 0.1464 0.1242 0.0606 7.200 32.414 29.793 5368.970 3.662 132.520 2.517 0.78 340496. 0.5758
|
|
19.90 0.1072 0.2129 0.1237 0.0623 7.397 33.300 29.687 5515.765 3.762 132.049 2.441 0.78 340916. 0.5575
|
|
26.53 0.1429 0.2751 0.1232 0.0640 7.600 34.216 29.555 5667.348 3.866 131.461 2.365 0.78 341389. 0.5390
|
|
33.16 0.1787 0.3330 0.1225 0.0657 7.805 35.138 29.387 5820.171 3.970 130.715 2.290 0.78 341919. 0.5203
|
|
39.80 0.2144 0.3867 0.1216 0.0674 8.006 36.042 29.172 5969.875 4.072 129.759 2.216 0.78 342508. 0.5017
|
|
46.43 0.2501 0.4365 0.1204 0.0690 8.196 36.897 28.898 6111.535 4.169 128.539 2.145 0.78 343160. 0.4832
|
|
53.06 0.2859 0.4828 0.1190 0.0705 8.368 37.673 28.552 6239.952 4.256 126.998 2.075 0.78 343876. 0.4648
|
|
59.69 0.3216 0.5256 0.1172 0.0717 8.515 38.337 28.121 6349.966 4.331 125.080 2.009 0.78 344658. 0.4464
|
|
66.33 0.3573 0.5654 0.1150 0.0727 8.632 38.860 27.593 6436.622 4.390 122.735 1.944 0.78 345509. 0.4281
|
|
72.96 0.3931 0.6021 0.1124 0.0733 8.710 39.213 26.959 6495.143 4.430 119.915 1.883 0.78 346426. 0.4097
|
|
79.59 0.4288 0.6361 0.1092 0.0736 8.745 39.368 26.210 6520.814 4.448 116.580 1.823 0.78 347412. 0.3912
|
|
86.22 0.4645 0.6674 0.1056 0.0735 8.729 39.296 25.337 6508.934 4.440 112.697 1.766 0.79 348465. 0.3725
|
|
92.86 0.5003 0.6961 0.1014 0.0729 8.656 38.970 24.334 6454.854 4.403 108.239 1.710 0.79 349584. 0.3535
|
|
99.49 0.5360 0.7223 0.0967 0.0718 8.521 38.363 23.200 6354.333 4.334 103.195 1.656 0.79 350768. 0.3343
|
|
106.12 0.5717 0.7461 0.0914 0.0701 8.321 37.460 21.939 6204.717 4.232 97.586 1.604 0.79 352015. 0.3148
|
|
112.75 0.6075 0.7677 0.0857 0.0678 8.054 36.260 20.565 6005.925 4.097 91.474 1.553 0.79 353326. 0.2952
|
|
119.39 0.6432 0.7871 0.0796 0.0650 7.724 34.773 19.096 5759.689 3.929 84.941 1.504 0.79 354699. 0.2754
|
|
126.02 0.6790 0.8042 0.0731 0.0617 7.333 33.014 17.550 5468.254 3.730 78.061 1.456 0.80 356132. 0.2556
|
|
132.65 0.7147 0.8190 0.0664 0.0580 6.884 30.994 15.940 5133.668 3.502 70.899 1.408 0.80 357624. 0.2356
|
|
139.28 0.7504 0.8311 0.0595 0.0537 6.380 28.724 14.278 4757.750 3.245 63.506 1.361 0.80 359176. 0.2156
|
|
145.92 0.7862 0.8401 0.0524 0.0490 5.823 26.215 12.572 4342.198 2.962 55.922 1.313 0.80 360786. 0.1952
|
|
152.55 0.8219 0.8449 0.0451 0.0439 5.215 23.476 10.832 3888.515 2.652 48.179 1.263 0.80 362453. 0.1743
|
|
159.18 0.8576 0.8438 0.0378 0.0384 4.558 20.521 9.061 3398.975 2.318 40.302 1.209 0.81 364177. 0.1525
|
|
165.81 0.8934 0.8329 0.0303 0.0325 3.858 17.367 7.266 2876.565 1.962 32.320 1.146 0.81 365957. 0.1294
|
|
172.45 0.9291 0.8043 0.0227 0.0263 3.118 14.038 5.454 2325.161 1.586 24.260 1.064 0.81 367793. 0.1041
|
|
179.08 0.9648 0.7390 0.0151 0.0198 2.346 10.564 3.632 1749.752 1.193 16.153 0.941 0.81 369684. 0.0752
|
|
185.71 1.0006 0.5769 0.0075 0.0131 1.551 6.983 1.807 1156.668 0.789 8.038 0.709 0.82 371627. 0.0399
|
|
192.34 1.0363 -0.0082 0.0000 0.0062 0.741 3.334 -0.012 552.308 0.377 -0.052 -0.010 0.82 373581. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 15000
|
|
|
|
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 0.1251 0.0630 9.202 38.667 34.448 6862.081 4.369 153.226 2.277 0.83 364049. 0.5601
|
|
7.15 0.0359 0.0696 0.1248 0.0645 9.415 39.560 34.373 7020.693 4.470 152.893 2.221 0.83 364399. 0.5457
|
|
14.30 0.0719 0.1355 0.1245 0.0660 9.644 40.523 34.289 7191.497 4.578 152.516 2.163 0.83 364797. 0.5307
|
|
21.45 0.1078 0.1978 0.1241 0.0677 9.886 41.541 34.188 7372.099 4.693 152.068 2.103 0.83 365249. 0.5155
|
|
28.59 0.1438 0.2562 0.1237 0.0694 10.137 42.593 34.063 7558.926 4.812 151.512 2.044 0.83 365757. 0.5000
|
|
35.74 0.1797 0.3110 0.1231 0.0711 10.389 43.653 33.903 7746.964 4.932 150.800 1.985 0.83 366326. 0.4844
|
|
42.89 0.2157 0.3624 0.1223 0.0728 10.634 44.683 33.694 7929.742 5.048 149.872 1.927 0.83 366959. 0.4689
|
|
50.04 0.2516 0.4106 0.1213 0.0744 10.862 45.640 33.421 8099.584 5.156 148.659 1.872 0.84 367661. 0.4535
|
|
57.19 0.2876 0.4559 0.1200 0.0757 11.061 46.479 33.067 8248.500 5.251 147.083 1.818 0.84 368433. 0.4382
|
|
64.34 0.3235 0.4986 0.1184 0.0768 11.223 47.157 32.615 8368.786 5.328 145.070 1.768 0.84 369278. 0.4231
|
|
71.49 0.3595 0.5389 0.1163 0.0776 11.336 47.635 32.048 8453.598 5.382 142.548 1.719 0.84 370197. 0.4080
|
|
78.63 0.3954 0.5769 0.1138 0.0780 11.395 47.881 31.352 8497.263 5.410 139.453 1.674 0.84 371191. 0.3927
|
|
85.78 0.4314 0.6127 0.1108 0.0780 11.392 47.868 30.515 8495.052 5.408 135.731 1.629 0.84 372259. 0.3772
|
|
92.93 0.4673 0.6463 0.1072 0.0775 11.322 47.572 29.527 8442.493 5.375 131.338 1.586 0.84 373402. 0.3613
|
|
100.08 0.5033 0.6776 0.1030 0.0765 11.178 46.967 28.381 8335.166 5.306 126.238 1.544 0.84 374616. 0.3448
|
|
107.23 0.5392 0.7066 0.0983 0.0750 10.955 46.030 27.072 8168.812 5.200 120.414 1.503 0.85 375901. 0.3278
|
|
114.38 0.5752 0.7333 0.0930 0.0729 10.649 44.748 25.606 7941.313 5.056 113.894 1.462 0.85 377256. 0.3102
|
|
121.53 0.6111 0.7577 0.0871 0.0703 10.264 43.128 24.001 7653.915 4.873 106.754 1.422 0.85 378680. 0.2920
|
|
128.67 0.6470 0.7798 0.0809 0.0671 9.803 41.190 22.278 7309.866 4.654 99.094 1.382 0.85 380170. 0.2735
|
|
135.82 0.6830 0.7994 0.0743 0.0635 9.270 38.951 20.461 6912.618 4.401 91.008 1.343 0.85 381725. 0.2545
|
|
142.97 0.7189 0.8164 0.0674 0.0593 8.669 36.427 18.564 6464.534 4.115 82.573 1.303 0.85 383345. 0.2352
|
|
150.12 0.7549 0.8304 0.0603 0.0548 8.003 33.629 16.603 5968.078 3.799 73.849 1.262 0.86 385029. 0.2155
|
|
157.27 0.7908 0.8399 0.0530 0.0499 7.283 30.601 14.586 5430.712 3.457 64.879 1.218 0.86 386775. 0.1950
|
|
164.42 0.8268 0.8427 0.0455 0.0446 6.515 27.374 12.522 4857.921 3.093 55.700 1.169 0.86 388583. 0.1734
|
|
171.57 0.8627 0.8369 0.0378 0.0390 5.696 23.935 10.421 4247.713 2.704 46.352 1.113 0.86 390452. 0.1505
|
|
178.71 0.8987 0.8170 0.0301 0.0331 4.835 20.315 8.288 3605.289 2.295 36.867 1.043 0.87 392382. 0.1258
|
|
185.86 0.9346 0.7715 0.0223 0.0270 3.940 16.557 6.134 2938.261 1.871 27.282 0.947 0.87 394371. 0.0983
|
|
193.01 0.9706 0.6749 0.0144 0.0207 3.025 12.709 3.966 2255.472 1.436 17.641 0.798 0.87 396419. 0.0666
|
|
200.16 1.0065 0.4570 0.0065 0.0144 2.101 8.830 1.799 1567.062 0.998 8.003 0.521 0.87 398524. 0.0293
|
|
207.31 1.0425
|
|
|
|
|
|
|
|
PROP RPM = 16000
|
|
|
|
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 0.1244 0.0698 12.380 48.770 38.979 9232.091 5.510 173.380 1.915 0.89 388333. 0.5011
|
|
7.60 0.0358 0.0624 0.1241 0.0713 12.633 49.764 38.902 9420.238 5.622 173.037 1.873 0.89 388702. 0.4896
|
|
15.21 0.0717 0.1219 0.1239 0.0728 12.908 50.847 38.819 9625.239 5.745 172.667 1.829 0.89 389123. 0.4777
|
|
22.81 0.1075 0.1784 0.1236 0.0745 13.200 51.999 38.723 9843.365 5.875 172.241 1.784 0.89 389599. 0.4654
|
|
30.41 0.1434 0.2318 0.1232 0.0762 13.507 53.206 38.608 10071.818 6.011 171.729 1.739 0.89 390135. 0.4528
|
|
38.01 0.1792 0.2821 0.1227 0.0780 13.819 54.439 38.464 10305.147 6.150 171.088 1.693 0.89 390735. 0.4401
|
|
45.62 0.2151 0.3296 0.1221 0.0797 14.128 55.655 38.277 10535.436 6.288 170.256 1.648 0.89 391401. 0.4273
|
|
53.22 0.2509 0.3743 0.1213 0.0813 14.419 56.802 38.030 10752.621 6.417 169.159 1.604 0.89 392139. 0.4146
|
|
60.82 0.2867 0.4166 0.1203 0.0828 14.677 57.818 37.704 10944.887 6.532 167.708 1.563 0.89 392951. 0.4021
|
|
68.43 0.3226 0.4569 0.1189 0.0840 14.885 58.635 37.276 11099.473 6.625 165.806 1.523 0.89 393841. 0.3898
|
|
76.03 0.3584 0.4955 0.1172 0.0848 15.025 59.187 36.725 11203.986 6.687 163.352 1.487 0.89 394810. 0.3776
|
|
83.63 0.3943 0.5327 0.1150 0.0851 15.084 59.419 36.028 11247.868 6.713 160.253 1.453 0.90 395860. 0.3655
|
|
91.23 0.4301 0.5684 0.1122 0.0849 15.051 59.289 35.168 11223.325 6.698 156.426 1.421 0.90 396990. 0.3532
|
|
98.84 0.4659 0.6029 0.1089 0.0842 14.919 58.770 34.128 11125.041 6.640 151.802 1.391 0.90 398200. 0.3407
|
|
106.44 0.5018 0.6359 0.1050 0.0828 14.682 57.837 32.897 10948.519 6.534 146.325 1.363 0.90 399489. 0.3276
|
|
114.04 0.5376 0.6674 0.1004 0.0809 14.338 56.481 31.468 10691.871 6.381 139.970 1.335 0.90 400855. 0.3139
|
|
121.65 0.5735 0.6972 0.0952 0.0783 13.887 54.705 29.847 10355.676 6.181 132.761 1.307 0.90 402296. 0.2993
|
|
129.25 0.6093 0.7250 0.0895 0.0752 13.335 52.530 28.053 9943.909 5.935 124.779 1.280 0.91 403810. 0.2840
|
|
136.85 0.6452 0.7509 0.0833 0.0716 12.689 49.987 26.110 9462.479 5.648 116.138 1.252 0.91 405395. 0.2680
|
|
144.45 0.6810 0.7745 0.0767 0.0675 11.958 47.106 24.044 8917.200 5.322 106.949 1.223 0.91 407050. 0.2513
|
|
152.06 0.7168 0.7957 0.0698 0.0629 11.148 43.917 21.877 8313.347 4.962 97.310 1.194 0.91 408773. 0.2340
|
|
159.66 0.7527 0.8140 0.0626 0.0579 10.265 40.437 19.627 7654.766 4.569 87.301 1.163 0.91 410564. 0.2159
|
|
167.26 0.7885 0.8277 0.0552 0.0526 9.325 36.735 17.306 6953.808 4.150 76.977 1.129 0.92 412421. 0.1968
|
|
174.87 0.8244 0.8309 0.0476 0.0472 8.372 32.980 14.918 6243.062 3.726 66.356 1.084 0.92 414343. 0.1754
|
|
182.47 0.8602 0.8178 0.0398 0.0419 7.420 29.230 12.472 5533.202 3.302 55.474 1.022 0.92 416330. 0.1513
|
|
190.07 0.8961 0.7862 0.0319 0.0363 6.438 25.361 9.987 4800.753 2.865 44.420 0.944 0.92 418380. 0.1250
|
|
197.67 0.9319 0.7243 0.0239 0.0307 5.440 21.431 7.476 4056.781 2.421 33.252 0.836 0.93 420494. 0.0958
|
|
205.28 0.9677 0.6107 0.0158 0.0251 4.443 17.504 4.957 3313.517 1.978 22.050 0.679 0.93 422669. 0.0633
|
|
212.88 1.0036 0.4027 0.0078 0.0195 3.464 13.644 2.457 2582.770 1.541 10.928 0.431 0.93 424905. 0.0283
|
|
220.48 1.0394 0.0005 0.0000 0.0142 2.513 9.898 0.002 1873.616 1.118 0.009 0.001 0.94 427186. 0.0000
|
|
|
|
|
|
|