575 lines
102 KiB
Plaintext
575 lines
102 KiB
Plaintext
16x12E (16x12E.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 0.1022 0.0466 0.004 0.248 0.213 2.931 0.028 0.949 33.020 0.06 23756. 0.5593
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0.48 0.0316 0.0675 0.1013 0.0474 0.004 0.252 0.212 2.985 0.028 0.941 32.147 0.06 23776. 0.5422
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0.96 0.0632 0.1312 0.1003 0.0483 0.004 0.257 0.209 3.040 0.029 0.932 31.258 0.06 23798. 0.5247
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1.44 0.0948 0.1912 0.0992 0.0492 0.004 0.262 0.207 3.095 0.030 0.922 30.359 0.06 23823. 0.5068
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1.92 0.1264 0.2473 0.0980 0.0501 0.004 0.266 0.205 3.150 0.030 0.910 29.457 0.06 23851. 0.4886
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2.39 0.1580 0.2997 0.0965 0.0509 0.004 0.271 0.202 3.203 0.031 0.897 28.556 0.06 23882. 0.4702
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2.87 0.1896 0.3483 0.0950 0.0517 0.004 0.275 0.198 3.252 0.031 0.882 27.661 0.06 23916. 0.4518
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3.35 0.2212 0.3934 0.0932 0.0524 0.004 0.279 0.195 3.297 0.031 0.866 26.777 0.06 23953. 0.4332
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3.83 0.2528 0.4350 0.0912 0.0530 0.004 0.282 0.190 3.334 0.032 0.847 25.907 0.06 23993. 0.4146
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4.31 0.2844 0.4733 0.0890 0.0535 0.005 0.284 0.186 3.364 0.032 0.826 25.053 0.06 24037. 0.3960
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4.79 0.3160 0.5083 0.0865 0.0538 0.005 0.286 0.181 3.382 0.032 0.803 24.218 0.06 24085. 0.3774
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5.27 0.3476 0.5403 0.0837 0.0539 0.005 0.286 0.175 3.389 0.032 0.778 23.401 0.06 24135. 0.3589
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5.75 0.3792 0.5693 0.0807 0.0537 0.005 0.286 0.169 3.382 0.032 0.750 22.603 0.06 24190. 0.3403
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6.22 0.4108 0.5954 0.0774 0.0534 0.005 0.284 0.162 3.358 0.032 0.719 21.820 0.06 24247. 0.3216
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6.70 0.4424 0.6186 0.0737 0.0527 0.004 0.280 0.154 3.318 0.032 0.685 21.051 0.06 24309. 0.3029
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7.18 0.4740 0.6388 0.0698 0.0518 0.004 0.275 0.146 3.258 0.031 0.648 20.291 0.06 24374. 0.2841
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7.66 0.5056 0.6559 0.0656 0.0505 0.004 0.269 0.137 3.180 0.030 0.609 19.532 0.06 24442. 0.2651
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8.14 0.5372 0.6696 0.0610 0.0490 0.004 0.260 0.127 3.080 0.029 0.567 18.767 0.06 24515. 0.2457
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8.62 0.5688 0.6795 0.0562 0.0471 0.004 0.250 0.117 2.962 0.028 0.522 17.984 0.06 24590. 0.2260
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9.10 0.6004 0.6848 0.0512 0.0449 0.004 0.239 0.107 2.824 0.027 0.476 17.171 0.06 24669. 0.2059
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9.58 0.6320 0.6847 0.0460 0.0424 0.004 0.226 0.096 2.671 0.026 0.427 16.311 0.06 24752. 0.1854
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10.05 0.6636 0.6781 0.0406 0.0398 0.003 0.211 0.085 2.502 0.024 0.377 15.383 0.06 24837. 0.1643
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10.53 0.6952 0.6631 0.0352 0.0369 0.003 0.196 0.073 2.319 0.022 0.327 14.361 0.07 24927. 0.1427
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11.01 0.7268 0.6376 0.0296 0.0338 0.003 0.180 0.062 2.124 0.020 0.275 13.207 0.07 25019. 0.1205
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11.49 0.7584 0.5977 0.0240 0.0305 0.003 0.162 0.050 1.918 0.018 0.223 11.866 0.07 25115. 0.0975
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11.97 0.7900 0.5381 0.0184 0.0270 0.002 0.144 0.038 1.702 0.016 0.171 10.255 0.07 25215. 0.0738
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12.45 0.8216 0.4497 0.0128 0.0235 0.002 0.125 0.027 1.477 0.014 0.119 8.240 0.07 25317. 0.0495
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12.93 0.8532 0.3167 0.0074 0.0198 0.002 0.105 0.015 1.246 0.012 0.068 5.588 0.07 25423. 0.0254
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13.41 0.8848 0.1087 0.0020 0.0161 0.001 0.085 0.004 1.011 0.010 0.018 1.850 0.07 25532. 0.0044
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13.88 0.9164
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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 0.1025 0.0430 0.029 0.916 0.856 21.667 0.103 3.808 17.923 0.13 47511. 0.6082
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0.94 0.0311 0.0719 0.1016 0.0439 0.030 0.934 0.849 22.112 0.106 3.777 17.419 0.13 47550. 0.5886
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1.88 0.0622 0.1396 0.1007 0.0448 0.030 0.954 0.841 22.568 0.108 3.742 16.907 0.13 47594. 0.5687
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2.83 0.0933 0.2031 0.0996 0.0458 0.031 0.973 0.832 23.030 0.110 3.702 16.393 0.13 47643. 0.5485
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3.77 0.1243 0.2623 0.0984 0.0467 0.031 0.993 0.822 23.489 0.112 3.658 15.879 0.13 47698. 0.5281
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4.71 0.1554 0.3173 0.0971 0.0475 0.032 1.012 0.811 23.935 0.114 3.608 15.369 0.13 47758. 0.5076
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5.65 0.1865 0.3683 0.0956 0.0484 0.033 1.029 0.798 24.358 0.116 3.551 14.865 0.13 47825. 0.4871
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6.59 0.2176 0.4154 0.0938 0.0492 0.033 1.046 0.784 24.746 0.118 3.487 14.370 0.13 47897. 0.4666
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7.54 0.2487 0.4587 0.0919 0.0498 0.034 1.060 0.768 25.085 0.120 3.416 13.885 0.13 47976. 0.4462
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8.48 0.2798 0.4985 0.0898 0.0504 0.034 1.072 0.750 25.360 0.121 3.336 13.413 0.13 48061. 0.4260
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9.42 0.3109 0.5349 0.0874 0.0508 0.034 1.080 0.730 25.559 0.122 3.247 12.954 0.13 48153. 0.4059
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10.36 0.3419 0.5682 0.0847 0.0510 0.034 1.085 0.708 25.665 0.123 3.148 12.509 0.13 48252. 0.3859
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11.30 0.3730 0.5985 0.0818 0.0510 0.034 1.085 0.683 25.664 0.123 3.040 12.077 0.13 48357. 0.3661
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12.25 0.4041 0.6259 0.0786 0.0507 0.034 1.079 0.657 25.542 0.122 2.920 11.659 0.13 48470. 0.3464
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13.19 0.4352 0.6505 0.0751 0.0502 0.034 1.069 0.627 25.286 0.121 2.790 11.252 0.13 48589. 0.3268
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14.13 0.4663 0.6724 0.0713 0.0494 0.033 1.052 0.596 24.884 0.119 2.649 10.855 0.13 48715. 0.3072
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15.07 0.4974 0.6915 0.0672 0.0483 0.033 1.028 0.561 24.327 0.116 2.497 10.466 0.13 48848. 0.2876
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16.01 0.5284 0.7077 0.0628 0.0469 0.032 0.998 0.525 23.609 0.113 2.334 10.081 0.13 48988. 0.2678
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16.96 0.5595 0.7207 0.0582 0.0452 0.030 0.961 0.486 22.729 0.109 2.161 9.695 0.13 49135. 0.2478
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17.90 0.5906 0.7300 0.0533 0.0431 0.029 0.917 0.445 21.696 0.104 1.980 9.304 0.13 49289. 0.2276
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18.84 0.6217 0.7351 0.0482 0.0408 0.028 0.867 0.403 20.521 0.098 1.791 8.901 0.13 49449. 0.2071
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19.78 0.6528 0.7351 0.0430 0.0382 0.026 0.812 0.359 19.216 0.092 1.597 8.476 0.13 49615. 0.1863
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20.72 0.6839 0.7286 0.0377 0.0353 0.024 0.752 0.315 17.791 0.085 1.399 8.019 0.13 49789. 0.1649
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21.67 0.7150 0.7138 0.0322 0.0323 0.022 0.687 0.269 16.256 0.078 1.198 7.515 0.13 49969. 0.1430
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22.61 0.7460 0.6879 0.0268 0.0290 0.020 0.618 0.224 14.619 0.070 0.995 6.941 0.13 50155. 0.1204
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23.55 0.7771 0.6463 0.0213 0.0256 0.017 0.545 0.178 12.893 0.062 0.792 6.261 0.13 50348. 0.0969
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24.49 0.8082 0.5813 0.0158 0.0220 0.015 0.469 0.132 11.089 0.053 0.589 5.414 0.13 50547. 0.0722
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25.43 0.8393 0.4786 0.0104 0.0183 0.012 0.390 0.087 9.223 0.044 0.388 4.293 0.13 50752. 0.0465
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26.38 0.8704 0.3089 0.0052 0.0145 0.010 0.309 0.043 7.310 0.035 0.192 2.672 0.13 50964. 0.0203
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27.32 0.9015 0.0007 0.0000 0.0107 0.007 0.227 0.000 5.370 0.026 0.000 0.006 0.13 51182. 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 0.1027 0.0416 0.095 1.989 1.931 70.597 0.225 8.591 12.408 0.19 71265. 0.6324
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1.42 0.0312 0.0748 0.1019 0.0425 0.097 2.032 1.916 72.135 0.230 8.521 12.046 0.19 71324. 0.6114
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2.83 0.0623 0.1450 0.1010 0.0434 0.099 2.077 1.898 73.718 0.235 8.443 11.679 0.19 71391. 0.5901
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4.25 0.0935 0.2107 0.0999 0.0443 0.101 2.122 1.878 75.323 0.240 8.355 11.311 0.19 71465. 0.5685
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5.67 0.1246 0.2718 0.0987 0.0453 0.103 2.167 1.856 76.921 0.245 8.255 10.944 0.19 71547. 0.5468
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7.08 0.1558 0.3285 0.0974 0.0462 0.105 2.211 1.831 78.481 0.250 8.143 10.580 0.19 71638. 0.5250
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8.50 0.1870 0.3808 0.0959 0.0471 0.107 2.253 1.802 79.963 0.255 8.016 10.222 0.19 71737. 0.5033
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9.91 0.2181 0.4290 0.0942 0.0479 0.109 2.291 1.770 81.327 0.259 7.873 9.871 0.19 71846. 0.4816
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11.33 0.2493 0.4734 0.0922 0.0486 0.111 2.325 1.734 82.527 0.263 7.712 9.529 0.19 71965. 0.4602
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12.75 0.2804 0.5140 0.0901 0.0492 0.112 2.353 1.693 83.514 0.266 7.532 9.197 0.19 72094. 0.4389
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14.16 0.3116 0.5511 0.0877 0.0496 0.113 2.373 1.648 84.238 0.268 7.332 8.875 0.19 72232. 0.4179
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15.58 0.3427 0.5850 0.0850 0.0498 0.114 2.385 1.598 84.647 0.269 7.109 8.565 0.19 72381. 0.3971
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17.00 0.3739 0.6158 0.0821 0.0498 0.114 2.386 1.543 84.690 0.270 6.864 8.264 0.19 72540. 0.3765
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18.41 0.4051 0.6437 0.0789 0.0496 0.113 2.376 1.482 84.316 0.268 6.594 7.975 0.19 72709. 0.3561
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19.83 0.4362 0.6689 0.0753 0.0491 0.112 2.352 1.416 83.481 0.266 6.300 7.695 0.19 72889. 0.3358
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21.24 0.4674 0.6914 0.0715 0.0484 0.110 2.314 1.344 82.144 0.261 5.980 7.424 0.19 73079. 0.3157
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22.66 0.4985 0.7112 0.0674 0.0473 0.108 2.262 1.267 80.274 0.256 5.636 7.159 0.19 73280. 0.2955
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24.08 0.5297 0.7282 0.0630 0.0458 0.104 2.193 1.184 77.846 0.248 5.267 6.899 0.19 73491. 0.2753
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25.49 0.5609 0.7422 0.0583 0.0441 0.100 2.109 1.096 74.855 0.238 4.875 6.641 0.19 73712. 0.2550
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26.91 0.5920 0.7529 0.0534 0.0420 0.096 2.010 1.004 71.332 0.227 4.464 6.382 0.19 73943. 0.2345
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28.33 0.6232 0.7596 0.0483 0.0396 0.090 1.897 0.908 67.316 0.214 4.038 6.117 0.19 74185. 0.2137
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29.74 0.6543 0.7615 0.0430 0.0370 0.084 1.771 0.809 62.843 0.200 3.599 5.840 0.19 74436. 0.1927
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31.16 0.6855 0.7575 0.0377 0.0341 0.078 1.633 0.709 57.948 0.184 3.151 5.546 0.19 74697. 0.1712
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32.58 0.7167 0.7458 0.0323 0.0310 0.071 1.484 0.606 52.662 0.168 2.697 5.223 0.20 74968. 0.1491
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33.99 0.7478 0.7236 0.0268 0.0277 0.063 1.325 0.503 47.020 0.150 2.239 4.856 0.20 75249. 0.1263
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35.41 0.7790 0.6862 0.0213 0.0242 0.055 1.157 0.400 41.061 0.131 1.780 4.421 0.20 75539. 0.1026
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36.82 0.8101 0.6255 0.0158 0.0205 0.047 0.981 0.298 34.828 0.111 1.323 3.874 0.20 75839. 0.0775
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38.24 0.8413 0.5254 0.0104 0.0167 0.038 0.799 0.196 28.374 0.090 0.872 3.134 0.20 76149. 0.0509
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39.66 0.8725 0.3503 0.0051 0.0128 0.029 0.613 0.097 21.758 0.069 0.430 2.015 0.20 76468. 0.0230
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41.07 0.9036 0.0008 0.0000 0.0089 0.020 0.424 0.000 15.045 0.048 0.001 0.005 0.20 76795. 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 0.1030 0.0408 0.220 3.468 3.443 164.114 0.392 15.314 9.515 0.25 95018. 0.6475
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1.89 0.0312 0.0765 0.1022 0.0417 0.225 3.546 3.416 167.825 0.401 15.192 9.231 0.25 95097. 0.6256
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3.78 0.0624 0.1483 0.1013 0.0426 0.230 3.627 3.385 171.651 0.410 15.055 8.944 0.25 95186. 0.6034
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5.67 0.0936 0.2153 0.1002 0.0436 0.235 3.709 3.350 175.534 0.419 14.901 8.656 0.25 95285. 0.5810
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7.56 0.1248 0.2775 0.0991 0.0446 0.241 3.791 3.311 179.408 0.428 14.726 8.370 0.25 95395. 0.5585
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9.46 0.1560 0.3352 0.0977 0.0455 0.246 3.871 3.266 183.194 0.437 14.527 8.086 0.25 95516. 0.5359
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11.35 0.1872 0.3884 0.0962 0.0464 0.251 3.947 3.216 186.803 0.446 14.303 7.808 0.25 95649. 0.5135
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13.24 0.2184 0.4373 0.0945 0.0472 0.255 4.018 3.159 190.131 0.454 14.050 7.535 0.25 95795. 0.4911
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15.13 0.2496 0.4822 0.0926 0.0479 0.259 4.080 3.095 193.071 0.461 13.765 7.270 0.25 95954. 0.4690
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17.02 0.2808 0.5233 0.0905 0.0485 0.262 4.131 3.023 195.504 0.467 13.446 7.013 0.25 96125. 0.4472
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18.91 0.3120 0.5608 0.0881 0.0490 0.265 4.169 2.943 197.309 0.471 13.090 6.765 0.26 96311. 0.4256
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20.80 0.3432 0.5951 0.0854 0.0493 0.266 4.191 2.854 198.360 0.474 12.694 6.525 0.26 96509. 0.4043
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22.69 0.3744 0.6262 0.0825 0.0493 0.266 4.195 2.755 198.531 0.474 12.256 6.295 0.26 96722. 0.3832
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24.58 0.4056 0.6545 0.0792 0.0491 0.265 4.178 2.647 197.703 0.472 11.775 6.073 0.26 96949. 0.3624
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26.47 0.4368 0.6801 0.0757 0.0486 0.263 4.137 2.529 195.764 0.467 11.249 5.860 0.26 97189. 0.3417
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28.37 0.4680 0.7030 0.0718 0.0478 0.258 4.070 2.401 192.616 0.460 10.678 5.653 0.26 97444. 0.3212
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30.26 0.4992 0.7233 0.0677 0.0467 0.252 3.976 2.262 188.183 0.449 10.063 5.453 0.26 97712. 0.3008
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32.15 0.5304 0.7408 0.0633 0.0453 0.245 3.854 2.114 182.402 0.435 9.403 5.257 0.26 97994. 0.2803
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34.04 0.5616 0.7556 0.0585 0.0435 0.235 3.703 1.956 175.261 0.418 8.703 5.063 0.26 98290. 0.2597
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35.93 0.5928 0.7671 0.0536 0.0414 0.224 3.525 1.791 166.830 0.398 7.968 4.870 0.26 98599. 0.2390
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37.82 0.6240 0.7749 0.0485 0.0390 0.211 3.322 1.620 157.202 0.375 7.205 4.674 0.26 98921. 0.2182
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39.71 0.6552 0.7783 0.0432 0.0364 0.196 3.095 1.444 146.463 0.350 6.421 4.471 0.26 99257. 0.1970
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41.60 0.6864 0.7761 0.0378 0.0334 0.181 2.846 1.264 134.692 0.322 5.621 4.255 0.26 99606. 0.1754
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43.49 0.7176 0.7667 0.0324 0.0303 0.164 2.577 1.081 121.968 0.291 4.809 4.021 0.26 99969. 0.1533
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45.38 0.7488 0.7472 0.0269 0.0269 0.145 2.290 0.897 108.374 0.259 3.991 3.755 0.26 100344. 0.1305
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47.28 0.7800 0.7130 0.0213 0.0233 0.126 1.986 0.713 94.005 0.224 3.172 3.440 0.26 100732. 0.1065
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49.17 0.8112 0.6559 0.0159 0.0196 0.106 1.669 0.530 78.967 0.189 2.356 3.043 0.26 101133. 0.0812
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51.06 0.8424 0.5587 0.0104 0.0157 0.085 1.339 0.349 63.388 0.151 1.552 2.496 0.26 101547. 0.0541
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52.95 0.8736 0.3813 0.0051 0.0118 0.064 1.002 0.172 47.416 0.113 0.764 1.643 0.26 101974. 0.0250
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54.84 0.9049 -0.0005 0.0000 0.0077 0.042 0.659 0.000 31.207 0.075 -0.001 -0.002 0.26 102411. 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 0.1034 0.0403 0.425 5.358 5.396 316.971 0.605 24.003 7.722 0.32 118770. 0.6579
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2.36 0.0312 0.0776 0.1026 0.0412 0.435 5.483 5.355 324.325 0.619 23.817 7.488 0.32 118869. 0.6355
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4.73 0.0624 0.1504 0.1016 0.0422 0.445 5.611 5.307 331.917 0.634 23.607 7.253 0.32 118980. 0.6127
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7.09 0.0936 0.2182 0.1006 0.0432 0.455 5.741 5.254 339.632 0.649 23.369 7.016 0.32 119104. 0.5898
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9.46 0.1248 0.2812 0.0995 0.0442 0.466 5.872 5.193 347.341 0.663 23.100 6.782 0.32 119241. 0.5668
|
|
11.82 0.1561 0.3395 0.0981 0.0451 0.476 5.999 5.124 354.887 0.678 22.794 6.549 0.32 119393. 0.5437
|
|
14.19 0.1873 0.3932 0.0967 0.0460 0.486 6.121 5.047 362.092 0.692 22.447 6.321 0.32 119559. 0.5208
|
|
16.55 0.2185 0.4425 0.0950 0.0469 0.495 6.234 4.958 368.755 0.704 22.055 6.099 0.32 119742. 0.4980
|
|
18.92 0.2497 0.4878 0.0931 0.0476 0.502 6.333 4.859 374.658 0.716 21.612 5.882 0.32 119940. 0.4755
|
|
21.28 0.2809 0.5292 0.0909 0.0483 0.509 6.416 4.747 379.569 0.725 21.115 5.673 0.32 120155. 0.4533
|
|
23.65 0.3121 0.5671 0.0885 0.0487 0.514 6.479 4.622 383.244 0.732 20.560 5.470 0.32 120387. 0.4313
|
|
26.01 0.3433 0.6016 0.0859 0.0490 0.517 6.516 4.483 385.434 0.736 19.942 5.276 0.32 120636. 0.4097
|
|
28.37 0.3745 0.6330 0.0829 0.0491 0.517 6.523 4.330 385.890 0.737 19.258 5.089 0.32 120902. 0.3883
|
|
30.74 0.4058 0.6616 0.0797 0.0489 0.515 6.498 4.160 384.370 0.734 18.505 4.909 0.32 121185. 0.3672
|
|
33.10 0.4370 0.6874 0.0761 0.0484 0.510 6.435 3.975 380.654 0.727 17.681 4.737 0.32 121486. 0.3463
|
|
35.47 0.4682 0.7106 0.0723 0.0476 0.502 6.332 3.774 374.547 0.715 16.787 4.570 0.32 121805. 0.3256
|
|
37.83 0.4994 0.7313 0.0681 0.0465 0.491 6.185 3.557 365.891 0.699 15.821 4.409 0.32 122140. 0.3050
|
|
40.20 0.5306 0.7494 0.0637 0.0451 0.475 5.994 3.324 354.563 0.677 14.786 4.252 0.32 122493. 0.2843
|
|
42.56 0.5618 0.7647 0.0589 0.0433 0.457 5.757 3.077 340.534 0.650 13.686 4.098 0.32 122863. 0.2636
|
|
44.93 0.5930 0.7769 0.0540 0.0412 0.434 5.476 2.817 323.937 0.619 12.531 3.945 0.32 123250. 0.2428
|
|
47.29 0.6242 0.7857 0.0488 0.0388 0.409 5.155 2.548 304.952 0.582 11.333 3.790 0.32 123654. 0.2218
|
|
49.66 0.6554 0.7902 0.0435 0.0361 0.381 4.797 2.271 283.748 0.542 10.101 3.630 0.32 124074. 0.2006
|
|
52.02 0.6867 0.7895 0.0381 0.0331 0.349 4.403 1.988 260.480 0.497 8.844 3.462 0.32 124511. 0.1790
|
|
54.38 0.7179 0.7819 0.0326 0.0299 0.316 3.978 1.701 235.306 0.449 7.568 3.280 0.33 124964. 0.1569
|
|
56.75 0.7491 0.7648 0.0270 0.0265 0.279 3.523 1.412 208.390 0.398 6.282 3.074 0.33 125433. 0.1340
|
|
59.11 0.7803 0.7336 0.0215 0.0229 0.241 3.041 1.123 179.918 0.344 4.995 2.831 0.33 125919. 0.1100
|
|
61.48 0.8115 0.6800 0.0160 0.0191 0.201 2.537 0.835 150.108 0.287 3.714 2.523 0.33 126421. 0.0845
|
|
63.84 0.8427 0.5865 0.0105 0.0152 0.160 2.015 0.551 119.213 0.228 2.450 2.095 0.33 126939. 0.0570
|
|
66.21 0.8739 0.4100 0.0052 0.0111 0.117 1.480 0.273 87.530 0.167 1.213 1.413 0.33 127472. 0.0271
|
|
68.57 0.9051 0.0070 0.0001 0.0070 0.074 0.936 0.003 55.371 0.106 0.013 0.023 0.33 128019. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 6000
|
|
|
|
V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
|
|
(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
|
|
0.00 0.0000 0.0000 0.1037 0.0401 0.730 7.671 7.799 544.536 0.867 34.692 6.496 0.38 142520. 0.6653
|
|
2.84 0.0312 0.0784 0.1030 0.0410 0.748 7.853 7.741 557.433 0.887 34.430 6.298 0.38 142638. 0.6426
|
|
5.68 0.0625 0.1519 0.1021 0.0420 0.765 8.040 7.674 570.765 0.908 34.134 6.098 0.38 142772. 0.6195
|
|
8.52 0.0937 0.2203 0.1011 0.0430 0.784 8.232 7.599 584.331 0.930 33.799 5.898 0.38 142920. 0.5963
|
|
11.36 0.1250 0.2838 0.0999 0.0440 0.802 8.423 7.513 597.904 0.952 33.417 5.699 0.38 143085. 0.5729
|
|
14.20 0.1562 0.3426 0.0986 0.0450 0.820 8.610 7.415 611.210 0.973 32.982 5.503 0.38 143268. 0.5495
|
|
17.04 0.1874 0.3967 0.0971 0.0459 0.837 8.789 7.304 623.935 0.993 32.489 5.310 0.38 143468. 0.5263
|
|
19.88 0.2187 0.4464 0.0955 0.0468 0.853 8.956 7.178 635.727 1.012 31.929 5.121 0.38 143687. 0.5032
|
|
22.72 0.2499 0.4919 0.0936 0.0475 0.867 9.103 7.036 646.200 1.028 31.296 4.939 0.38 143926. 0.4804
|
|
25.56 0.2812 0.5336 0.0914 0.0482 0.878 9.226 6.876 654.943 1.042 30.583 4.762 0.38 144184. 0.4579
|
|
28.40 0.3124 0.5716 0.0891 0.0487 0.887 9.319 6.696 661.527 1.053 29.785 4.591 0.38 144463. 0.4357
|
|
31.24 0.3436 0.6064 0.0864 0.0490 0.892 9.375 6.496 665.511 1.059 28.895 4.427 0.38 144762. 0.4138
|
|
34.08 0.3749 0.6380 0.0834 0.0490 0.894 9.388 6.274 666.456 1.061 27.908 4.270 0.38 145083. 0.3922
|
|
36.92 0.4061 0.6668 0.0802 0.0489 0.890 9.353 6.030 663.936 1.057 26.821 4.119 0.38 145424. 0.3710
|
|
39.76 0.4374 0.6928 0.0766 0.0484 0.882 9.263 5.762 657.558 1.047 25.630 3.975 0.38 145786. 0.3499
|
|
42.60 0.4686 0.7163 0.0728 0.0476 0.868 9.114 5.471 646.980 1.030 24.335 3.835 0.39 146169. 0.3290
|
|
45.44 0.4999 0.7373 0.0686 0.0465 0.847 8.902 5.156 631.922 1.006 22.936 3.701 0.39 146572. 0.3082
|
|
48.28 0.5311 0.7558 0.0641 0.0450 0.821 8.624 4.819 612.163 0.974 21.435 3.571 0.39 146997. 0.2874
|
|
51.12 0.5623 0.7715 0.0593 0.0432 0.788 8.278 4.460 587.651 0.935 19.839 3.443 0.39 147442. 0.2666
|
|
53.96 0.5936 0.7844 0.0543 0.0411 0.749 7.869 4.084 558.614 0.889 18.164 3.316 0.39 147907. 0.2457
|
|
56.80 0.6248 0.7939 0.0491 0.0387 0.705 7.401 3.693 525.364 0.836 16.425 3.188 0.39 148393. 0.2247
|
|
59.64 0.6561 0.7993 0.0438 0.0359 0.655 6.877 3.290 488.195 0.777 14.636 3.057 0.39 148898. 0.2034
|
|
62.48 0.6873 0.7997 0.0383 0.0329 0.600 6.302 2.880 447.380 0.712 12.809 2.920 0.39 149423. 0.1817
|
|
65.32 0.7185 0.7935 0.0328 0.0297 0.541 5.680 2.463 403.193 0.642 10.957 2.771 0.39 149968. 0.1595
|
|
68.16 0.7498 0.7781 0.0272 0.0262 0.477 5.014 2.043 355.928 0.566 9.089 2.604 0.39 150533. 0.1365
|
|
71.00 0.7810 0.7491 0.0216 0.0225 0.410 4.309 1.623 305.913 0.487 7.220 2.407 0.39 151116. 0.1124
|
|
73.84 0.8123 0.6979 0.0160 0.0187 0.340 3.572 1.205 253.533 0.404 5.360 2.156 0.39 151720. 0.0868
|
|
76.68 0.8435 0.6065 0.0105 0.0147 0.267 2.807 0.793 199.242 0.317 3.525 1.804 0.39 152342. 0.0589
|
|
79.52 0.8747 0.4284 0.0052 0.0106 0.193 2.022 0.389 143.568 0.228 1.730 1.229 0.40 152984. 0.0281
|
|
82.36 0.9060 -0.0045 0.0000 0.0064 0.117 1.226 -0.002 87.063 0.139 -0.011 -0.012 0.40 153640. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 7000
|
|
|
|
V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
|
|
(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
|
|
0.00 0.0000 0.0000 0.1042 0.0400 1.157 10.421 10.661 863.048 1.177 47.418 5.603 0.44 166267. 0.6708
|
|
3.31 0.0312 0.0789 0.1034 0.0410 1.185 10.672 10.583 883.829 1.206 47.074 5.431 0.44 166405. 0.6479
|
|
6.63 0.0625 0.1528 0.1026 0.0419 1.214 10.932 10.495 905.339 1.235 46.682 5.258 0.44 166561. 0.6247
|
|
9.94 0.0937 0.2216 0.1016 0.0430 1.243 11.196 10.395 927.261 1.265 46.237 5.085 0.44 166734. 0.6012
|
|
13.26 0.1250 0.2855 0.1005 0.0440 1.273 11.462 10.281 949.227 1.295 45.729 4.912 0.44 166927. 0.5776
|
|
16.57 0.1562 0.3445 0.0992 0.0450 1.302 11.722 10.150 970.796 1.324 45.149 4.742 0.44 167140. 0.5541
|
|
19.88 0.1875 0.3989 0.0977 0.0459 1.330 11.972 10.002 991.461 1.353 44.488 4.576 0.45 167374. 0.5307
|
|
23.20 0.2187 0.4488 0.0961 0.0468 1.355 12.203 9.833 1010.649 1.379 43.735 4.413 0.45 167630. 0.5074
|
|
26.51 0.2500 0.4945 0.0942 0.0476 1.378 12.410 9.641 1027.737 1.402 42.882 4.255 0.45 167908. 0.4845
|
|
29.83 0.2812 0.5364 0.0921 0.0483 1.397 12.582 9.424 1042.058 1.422 41.919 4.102 0.45 168210. 0.4618
|
|
33.14 0.3125 0.5746 0.0897 0.0488 1.412 12.714 9.181 1052.912 1.436 40.837 3.955 0.45 168536. 0.4395
|
|
36.45 0.3437 0.6095 0.0871 0.0491 1.421 12.794 8.909 1059.588 1.445 39.629 3.814 0.45 168885. 0.4175
|
|
39.77 0.3750 0.6413 0.0841 0.0492 1.423 12.816 8.608 1061.369 1.448 38.286 3.678 0.45 169259. 0.3958
|
|
43.08 0.4062 0.6703 0.0809 0.0490 1.418 12.770 8.274 1057.567 1.443 36.804 3.549 0.45 169658. 0.3744
|
|
46.40 0.4375 0.6965 0.0773 0.0485 1.405 12.649 7.909 1047.542 1.429 35.179 3.424 0.45 170081. 0.3532
|
|
49.71 0.4687 0.7203 0.0734 0.0478 1.382 12.446 7.511 1030.736 1.406 33.408 3.305 0.45 170528. 0.3322
|
|
53.03 0.5000 0.7416 0.0692 0.0466 1.350 12.155 7.080 1006.694 1.373 31.494 3.190 0.45 171000. 0.3113
|
|
56.34 0.5312 0.7604 0.0647 0.0452 1.308 11.773 6.618 975.060 1.330 29.438 3.079 0.45 171496. 0.2904
|
|
59.65 0.5624 0.7766 0.0599 0.0434 1.255 11.299 6.126 935.734 1.277 27.250 2.970 0.45 172015. 0.2695
|
|
62.97 0.5937 0.7900 0.0548 0.0412 1.192 10.735 5.610 889.077 1.213 24.952 2.862 0.45 172559. 0.2486
|
|
66.28 0.6249 0.8002 0.0496 0.0387 1.121 10.089 5.073 835.587 1.140 22.565 2.754 0.45 173126. 0.2275
|
|
69.60 0.6562 0.8065 0.0442 0.0359 1.040 9.367 4.521 775.735 1.058 20.108 2.643 0.45 173716. 0.2061
|
|
72.91 0.6874 0.8079 0.0387 0.0329 0.952 8.573 3.957 709.964 0.969 17.599 2.528 0.45 174329. 0.1844
|
|
76.22 0.7187 0.8031 0.0331 0.0296 0.857 7.712 3.384 638.716 0.871 15.053 2.403 0.46 174965. 0.1621
|
|
79.54 0.7499 0.7894 0.0274 0.0261 0.754 6.792 2.807 562.464 0.767 12.487 2.264 0.46 175624. 0.1391
|
|
82.85 0.7812 0.7624 0.0218 0.0223 0.646 5.817 2.229 481.746 0.657 9.916 2.099 0.46 176306. 0.1149
|
|
86.17 0.8124 0.7138 0.0162 0.0184 0.533 4.796 1.655 397.184 0.542 7.360 1.890 0.46 177010. 0.0891
|
|
89.48 0.8437 0.6252 0.0106 0.0143 0.415 3.737 1.088 309.519 0.422 4.838 1.594 0.46 177736. 0.0610
|
|
92.79 0.8749 0.4477 0.0052 0.0102 0.295 2.652 0.533 219.618 0.300 2.370 1.100 0.46 178485. 0.0295
|
|
96.11 0.9062 -0.0074 0.0000 0.0059 0.172 1.550 -0.005 128.370 0.175 -0.022 -0.018 0.46 179251. 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 0.1047 0.0400 1.730 13.628 13.991 1289.921 1.540 62.231 4.920 0.51 190011. 0.6748
|
|
3.79 0.0312 0.0791 0.1039 0.0410 1.772 13.961 13.894 1321.408 1.577 61.799 4.769 0.51 190169. 0.6519
|
|
7.57 0.0625 0.1533 0.1031 0.0420 1.816 14.306 13.783 1354.051 1.616 61.307 4.617 0.51 190347. 0.6286
|
|
11.36 0.0937 0.2223 0.1022 0.0431 1.861 14.658 13.657 1387.379 1.656 60.745 4.465 0.51 190545. 0.6051
|
|
15.14 0.1249 0.2863 0.1011 0.0441 1.905 15.012 13.512 1420.832 1.696 60.100 4.313 0.51 190765. 0.5815
|
|
18.93 0.1562 0.3455 0.0998 0.0451 1.950 15.359 13.346 1453.744 1.735 59.362 4.164 0.51 191008. 0.5578
|
|
22.71 0.1874 0.4000 0.0984 0.0461 1.992 15.693 13.156 1485.340 1.773 58.517 4.017 0.51 191275. 0.5344
|
|
26.50 0.2186 0.4501 0.0968 0.0470 2.031 16.004 12.939 1514.750 1.808 57.551 3.874 0.51 191568. 0.5111
|
|
30.29 0.2499 0.4960 0.0950 0.0478 2.067 16.281 12.692 1541.021 1.839 56.452 3.736 0.51 191886. 0.4880
|
|
34.07 0.2811 0.5380 0.0929 0.0485 2.096 16.515 12.412 1563.132 1.866 55.208 3.601 0.51 192231. 0.4653
|
|
37.86 0.3123 0.5763 0.0905 0.0490 2.119 16.693 12.096 1580.016 1.886 53.805 3.472 0.51 192603. 0.4429
|
|
41.64 0.3436 0.6113 0.0879 0.0494 2.133 16.805 11.743 1590.583 1.899 52.234 3.349 0.51 193003. 0.4208
|
|
45.43 0.3748 0.6433 0.0849 0.0495 2.137 16.838 11.350 1593.742 1.902 50.484 3.230 0.51 193431. 0.3991
|
|
49.21 0.4060 0.6724 0.0817 0.0493 2.130 16.782 10.915 1588.437 1.896 48.549 3.117 0.51 193886. 0.3776
|
|
53.00 0.4373 0.6989 0.0781 0.0488 2.110 16.627 10.437 1573.693 1.878 46.422 3.008 0.51 194370. 0.3564
|
|
56.79 0.4685 0.7229 0.0742 0.0481 2.077 16.362 9.915 1548.654 1.849 44.102 2.904 0.51 194881. 0.3353
|
|
60.57 0.4997 0.7445 0.0700 0.0470 2.028 15.981 9.350 1512.625 1.806 41.589 2.804 0.51 195420. 0.3144
|
|
64.36 0.5310 0.7637 0.0654 0.0455 1.965 15.479 8.743 1465.059 1.749 38.887 2.707 0.51 195987. 0.2935
|
|
68.14 0.5622 0.7803 0.0606 0.0436 1.885 14.853 8.096 1405.786 1.678 36.009 2.612 0.52 196581. 0.2726
|
|
71.93 0.5934 0.7942 0.0555 0.0414 1.791 14.108 7.415 1335.331 1.594 32.983 2.519 0.52 197202. 0.2515
|
|
75.71 0.6246 0.8051 0.0502 0.0389 1.682 13.254 6.708 1254.440 1.497 29.837 2.425 0.52 197850. 0.2304
|
|
79.50 0.6559 0.8122 0.0447 0.0361 1.561 12.296 5.980 1163.833 1.389 26.597 2.330 0.52 198524. 0.2090
|
|
83.29 0.6871 0.8147 0.0392 0.0330 1.427 11.243 5.235 1064.181 1.270 23.286 2.231 0.52 199225. 0.1872
|
|
87.07 0.7183 0.8111 0.0335 0.0297 1.282 10.102 4.479 956.156 1.141 19.925 2.125 0.52 199951. 0.1649
|
|
90.86 0.7496 0.7991 0.0278 0.0261 1.127 8.880 3.717 840.480 1.003 16.535 2.006 0.52 200704. 0.1418
|
|
94.64 0.7808 0.7743 0.0221 0.0223 0.963 7.586 2.954 717.969 0.857 13.139 1.866 0.52 201483. 0.1176
|
|
98.43 0.8120 0.7284 0.0164 0.0183 0.791 6.229 2.194 589.576 0.704 9.760 1.688 0.52 202287. 0.0917
|
|
102.22 0.8433 0.6433 0.0108 0.0142 0.612 4.822 1.445 456.432 0.545 6.425 1.435 0.53 203117. 0.0633
|
|
106.00 0.8745 0.4685 0.0053 0.0099 0.429 3.379 0.711 319.865 0.382 3.163 1.008 0.53 203971. 0.0312
|
|
109.79 0.9057 -0.0001 0.0000 0.0056 0.243 1.915 0.000 181.244 0.216 0.000 0.000 0.53 204846. 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 0.1052 0.0402 2.473 17.319 17.803 1844.095 1.957 79.186 4.379 0.57 213752. 0.6775
|
|
4.26 0.0312 0.0792 0.1045 0.0412 2.534 17.747 17.686 1889.674 2.005 78.666 4.245 0.57 213930. 0.6547
|
|
8.52 0.0624 0.1534 0.1038 0.0422 2.598 18.191 17.552 1937.026 2.055 78.072 4.110 0.57 214129. 0.6315
|
|
12.77 0.0937 0.2226 0.1028 0.0433 2.663 18.646 17.399 1985.467 2.107 77.390 3.975 0.57 214352. 0.6080
|
|
17.03 0.1249 0.2867 0.1018 0.0443 2.728 19.104 17.222 2034.199 2.158 76.604 3.840 0.57 214599. 0.5844
|
|
21.29 0.1561 0.3460 0.1006 0.0454 2.792 19.555 17.019 2082.247 2.209 75.700 3.707 0.57 214873. 0.5609
|
|
25.55 0.1873 0.4006 0.0992 0.0464 2.854 19.989 16.785 2128.483 2.258 74.658 3.577 0.57 215173. 0.5374
|
|
29.81 0.2186 0.4507 0.0976 0.0473 2.912 20.395 16.516 2171.630 2.304 73.463 3.450 0.57 215502. 0.5141
|
|
34.06 0.2498 0.4967 0.0958 0.0482 2.964 20.758 16.209 2210.294 2.345 72.097 3.326 0.57 215861. 0.4911
|
|
38.32 0.2810 0.5388 0.0937 0.0489 3.008 21.065 15.859 2242.980 2.380 70.542 3.207 0.57 216249. 0.4684
|
|
42.58 0.3122 0.5772 0.0914 0.0494 3.042 21.301 15.464 2268.125 2.407 68.783 3.092 0.57 216668. 0.4460
|
|
46.84 0.3435 0.6124 0.0888 0.0498 3.063 21.451 15.019 2284.126 2.424 66.806 2.982 0.57 217118. 0.4239
|
|
51.09 0.3747 0.6445 0.0858 0.0499 3.070 21.501 14.523 2289.392 2.429 64.598 2.877 0.58 217600. 0.4021
|
|
55.35 0.4059 0.6738 0.0826 0.0498 3.061 21.435 13.972 2282.375 2.422 62.148 2.777 0.58 218112. 0.3806
|
|
59.61 0.4371 0.7005 0.0790 0.0493 3.033 21.240 13.365 2261.645 2.400 59.450 2.680 0.58 218657. 0.3594
|
|
63.87 0.4684 0.7247 0.0751 0.0485 2.985 20.905 12.702 2225.954 2.362 56.500 2.588 0.58 219233. 0.3383
|
|
68.13 0.4996 0.7466 0.0708 0.0474 2.916 20.420 11.983 2174.281 2.307 53.300 2.500 0.58 219840. 0.3173
|
|
72.38 0.5308 0.7661 0.0663 0.0459 2.824 19.777 11.208 2105.834 2.234 49.855 2.414 0.58 220478. 0.2964
|
|
76.64 0.5620 0.7831 0.0614 0.0440 2.709 18.974 10.382 2020.334 2.144 46.180 2.331 0.58 221146. 0.2754
|
|
80.90 0.5933 0.7976 0.0562 0.0418 2.573 18.017 9.512 1918.514 2.036 42.310 2.249 0.58 221845. 0.2544
|
|
85.16 0.6245 0.8090 0.0509 0.0393 2.416 16.918 8.607 1801.457 1.911 38.284 2.167 0.58 222574. 0.2332
|
|
89.42 0.6557 0.8169 0.0454 0.0364 2.240 15.686 7.674 1670.205 1.772 34.133 2.084 0.58 223333. 0.2117
|
|
93.67 0.6869 0.8203 0.0397 0.0333 2.046 14.329 6.720 1525.739 1.619 29.889 1.998 0.58 224122. 0.1899
|
|
97.93 0.7182 0.8179 0.0340 0.0298 1.836 12.857 5.750 1369.039 1.453 25.578 1.905 0.59 224939. 0.1675
|
|
102.19 0.7494 0.8074 0.0282 0.0262 1.611 11.281 4.773 1201.156 1.274 21.228 1.802 0.59 225786. 0.1444
|
|
106.45 0.7806 0.7844 0.0224 0.0223 1.372 9.610 3.792 1023.281 1.086 16.868 1.681 0.59 226662. 0.1200
|
|
110.71 0.8118 0.7410 0.0167 0.0182 1.122 7.859 2.817 836.809 0.888 12.529 1.527 0.59 227566. 0.0940
|
|
114.96 0.8431 0.6586 0.0110 0.0140 0.863 6.042 1.854 643.394 0.683 8.245 1.307 0.59 228500. 0.0652
|
|
119.22 0.8743 0.4854 0.0054 0.0097 0.597 4.179 0.911 444.992 0.472 4.053 0.929 0.59 229461. 0.0325
|
|
123.48 0.9055 -0.0026 0.0000 0.0053 0.327 2.288 -0.003 243.604 0.258 -0.012 -0.005 0.59 230445. 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 0.1059 0.0405 3.416 21.528 22.110 2547.022 2.432 98.345 3.937 0.63 237489. 0.6789
|
|
4.73 0.0312 0.0792 0.1052 0.0415 3.501 22.065 21.975 2610.590 2.493 97.744 3.818 0.63 237686. 0.6564
|
|
9.46 0.0624 0.1533 0.1045 0.0425 3.590 22.625 21.820 2676.820 2.556 97.053 3.697 0.63 237907. 0.6333
|
|
14.19 0.0936 0.2224 0.1036 0.0436 3.681 23.200 21.640 2744.776 2.621 96.256 3.576 0.63 238154. 0.6101
|
|
18.92 0.1248 0.2866 0.1026 0.0447 3.773 23.779 21.433 2813.331 2.687 95.332 3.455 0.64 238429. 0.5867
|
|
23.65 0.1561 0.3458 0.1015 0.0458 3.864 24.352 21.192 2881.122 2.751 94.262 3.336 0.64 238732. 0.5632
|
|
28.37 0.1873 0.4004 0.1001 0.0468 3.951 24.905 20.913 2946.542 2.814 93.021 3.219 0.64 239066. 0.5399
|
|
33.10 0.2185 0.4506 0.0986 0.0478 4.034 25.423 20.591 3007.785 2.872 91.588 3.105 0.64 239432. 0.5167
|
|
37.83 0.2497 0.4966 0.0968 0.0487 4.107 25.888 20.220 3062.872 2.925 89.939 2.994 0.64 239830. 0.4938
|
|
42.56 0.2809 0.5388 0.0948 0.0494 4.170 26.284 19.796 3109.672 2.970 88.054 2.887 0.64 240262. 0.4711
|
|
47.29 0.3121 0.5773 0.0925 0.0500 4.219 26.591 19.314 3145.970 3.004 85.910 2.785 0.64 240728. 0.4488
|
|
52.02 0.3433 0.6126 0.0899 0.0504 4.250 26.789 18.770 3169.498 3.027 83.489 2.686 0.64 241228. 0.4268
|
|
56.75 0.3745 0.6448 0.0870 0.0505 4.262 26.861 18.160 3177.987 3.035 80.774 2.592 0.64 241763. 0.4050
|
|
61.48 0.4058 0.6743 0.0837 0.0504 4.250 26.787 17.480 3169.251 3.026 77.753 2.502 0.64 242334. 0.3836
|
|
66.21 0.4370 0.7011 0.0801 0.0499 4.213 26.551 16.730 3141.261 3.000 74.415 2.416 0.64 242939. 0.3624
|
|
70.94 0.4682 0.7256 0.0762 0.0491 4.147 26.136 15.908 3092.248 2.953 70.757 2.333 0.64 243579. 0.3413
|
|
75.67 0.4994 0.7478 0.0719 0.0480 4.051 25.532 15.014 3020.777 2.885 66.781 2.254 0.64 244254. 0.3203
|
|
80.39 0.5306 0.7676 0.0673 0.0465 3.923 24.729 14.049 2925.733 2.794 62.491 2.178 0.64 244964. 0.2994
|
|
85.12 0.5618 0.7851 0.0623 0.0446 3.764 23.723 13.019 2806.685 2.680 57.907 2.104 0.64 245707. 0.2784
|
|
89.85 0.5930 0.8001 0.0571 0.0423 3.573 22.522 11.932 2664.615 2.545 53.074 2.031 0.65 246484. 0.2573
|
|
94.58 0.6242 0.8121 0.0517 0.0397 3.354 21.139 10.800 2501.035 2.388 48.038 1.959 0.65 247294. 0.2361
|
|
99.31 0.6555 0.8208 0.0461 0.0368 3.108 19.587 9.632 2317.418 2.213 42.843 1.885 0.65 248138. 0.2146
|
|
104.04 0.6867 0.8251 0.0404 0.0336 2.836 17.878 8.436 2115.140 2.020 37.524 1.809 0.65 249014. 0.1927
|
|
108.77 0.7179 0.8239 0.0346 0.0301 2.542 16.022 7.221 1895.588 1.810 32.118 1.728 0.65 249922. 0.1703
|
|
113.50 0.7491 0.8147 0.0287 0.0264 2.226 14.033 5.994 1660.243 1.585 26.659 1.637 0.65 250863. 0.1470
|
|
118.23 0.7803 0.7936 0.0228 0.0224 1.892 11.924 4.763 1410.783 1.347 21.184 1.531 0.65 251836. 0.1225
|
|
122.96 0.8115 0.7525 0.0169 0.0183 1.541 9.713 3.537 1149.177 1.097 15.733 1.396 0.66 252840. 0.0963
|
|
127.69 0.8427 0.6729 0.0111 0.0140 1.177 7.419 2.326 877.769 0.838 10.348 1.202 0.66 253877. 0.0672
|
|
132.41 0.8739 0.5015 0.0055 0.0095 0.804 5.066 1.141 599.336 0.572 5.077 0.864 0.66 254944. 0.0338
|
|
137.14 0.9051 -0.0065 0.0000 0.0050 0.425 2.677 -0.008 316.749 0.302 -0.034 -0.011 0.66 256036. 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 0.1065 0.0411 4.616 26.448 26.926 3442.082 2.988 119.765 3.548 0.70 261221. 0.6752
|
|
5.20 0.0312 0.0785 0.1060 0.0421 4.728 27.093 26.776 3526.022 3.061 119.098 3.444 0.70 261437. 0.6536
|
|
10.40 0.0624 0.1522 0.1053 0.0431 4.846 27.768 26.602 3613.792 3.137 118.327 3.339 0.70 261680. 0.6315
|
|
15.59 0.0936 0.2210 0.1045 0.0442 4.967 28.462 26.401 3704.193 3.216 117.430 3.233 0.70 261951. 0.6091
|
|
20.79 0.1248 0.2850 0.1035 0.0453 5.090 29.166 26.165 3795.776 3.295 116.384 3.127 0.70 262252. 0.5865
|
|
25.99 0.1559 0.3443 0.1025 0.0464 5.212 29.865 25.890 3886.755 3.374 115.160 3.021 0.70 262586. 0.5638
|
|
31.19 0.1871 0.3989 0.1012 0.0475 5.331 30.543 25.569 3975.003 3.451 113.731 2.918 0.70 262952. 0.5410
|
|
36.39 0.2183 0.4492 0.0997 0.0485 5.442 31.182 25.194 4058.094 3.523 112.065 2.816 0.70 263354. 0.5184
|
|
41.59 0.2495 0.4953 0.0980 0.0494 5.543 31.760 24.760 4133.325 3.588 110.134 2.717 0.70 263792. 0.4958
|
|
46.78 0.2807 0.5376 0.0960 0.0501 5.629 32.255 24.260 4197.779 3.644 107.908 2.621 0.70 264267. 0.4735
|
|
51.98 0.3119 0.5763 0.0937 0.0507 5.697 32.644 23.687 4248.372 3.688 105.361 2.529 0.70 264779. 0.4514
|
|
57.18 0.3431 0.6117 0.0912 0.0511 5.742 32.901 23.037 4281.896 3.717 102.467 2.440 0.70 265330. 0.4295
|
|
62.38 0.3743 0.6441 0.0883 0.0513 5.760 33.003 22.304 4295.142 3.729 99.207 2.355 0.70 265919. 0.4079
|
|
67.58 0.4055 0.6737 0.0850 0.0512 5.746 32.925 21.484 4284.971 3.720 95.563 2.274 0.70 266547. 0.3866
|
|
72.77 0.4366 0.7008 0.0814 0.0507 5.697 32.645 20.576 4248.501 3.688 91.521 2.197 0.70 267213. 0.3654
|
|
77.97 0.4678 0.7256 0.0775 0.0499 5.610 32.144 19.577 4183.279 3.632 87.078 2.123 0.71 267918. 0.3444
|
|
83.17 0.4990 0.7480 0.0732 0.0488 5.481 31.406 18.488 4087.330 3.548 82.234 2.052 0.71 268660. 0.3235
|
|
88.37 0.5302 0.7683 0.0685 0.0473 5.309 30.421 17.310 3959.129 3.437 76.997 1.983 0.71 269441. 0.3026
|
|
93.57 0.5614 0.7862 0.0635 0.0453 5.093 29.184 16.050 3798.031 3.297 71.389 1.917 0.71 270259. 0.2816
|
|
98.76 0.5926 0.8017 0.0582 0.0430 4.835 27.703 14.718 3605.303 3.130 65.464 1.852 0.71 271114. 0.2605
|
|
103.96 0.6238 0.8144 0.0527 0.0404 4.537 25.994 13.328 3383.000 2.937 59.281 1.787 0.71 272005. 0.2392
|
|
109.16 0.6550 0.8238 0.0471 0.0374 4.202 24.075 11.891 3133.134 2.720 52.893 1.721 0.71 272933. 0.2177
|
|
114.36 0.6862 0.8291 0.0412 0.0341 3.832 21.957 10.419 2857.607 2.481 46.346 1.654 0.71 273896. 0.1958
|
|
119.56 0.7173 0.8291 0.0353 0.0305 3.431 19.658 8.922 2558.326 2.221 39.684 1.582 0.72 274895. 0.1733
|
|
124.76 0.7485 0.8214 0.0293 0.0267 3.000 17.191 7.408 2237.342 1.942 32.951 1.502 0.72 275929. 0.1499
|
|
129.95 0.7797 0.8021 0.0233 0.0227 2.544 14.577 5.889 1897.076 1.647 26.193 1.408 0.72 276998. 0.1253
|
|
135.15 0.8109 0.7631 0.0173 0.0184 2.066 11.836 4.374 1540.415 1.337 19.457 1.288 0.72 278102. 0.0988
|
|
140.35 0.8421 0.6858 0.0114 0.0140 1.570 8.997 2.877 1170.897 1.016 12.799 1.115 0.72 279241. 0.0693
|
|
145.55 0.8733 0.5152 0.0056 0.0095 1.063 6.092 1.411 792.819 0.688 6.278 0.807 0.72 280414. 0.0352
|
|
150.75 0.9045 -0.0082 0.0000 0.0049 0.551 3.156 -0.011 410.702 0.357 -0.050 -0.012 0.73 281613. 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 0.1072 0.0429 6.251 32.835 32.254 4661.724 3.710 143.467 3.138 0.76 284948. 0.6536
|
|
5.66 0.0311 0.0758 0.1067 0.0438 6.391 33.570 32.095 4766.111 3.793 142.757 3.054 0.76 285182. 0.6346
|
|
11.33 0.0623 0.1474 0.1061 0.0448 6.538 34.339 31.909 4875.216 3.880 141.932 2.969 0.76 285446. 0.6150
|
|
16.99 0.0934 0.2147 0.1054 0.0459 6.688 35.130 31.692 4987.496 3.969 140.966 2.882 0.76 285740. 0.5950
|
|
22.65 0.1246 0.2776 0.1045 0.0469 6.841 35.930 31.436 5101.069 4.059 139.829 2.795 0.76 286068. 0.5747
|
|
28.31 0.1557 0.3362 0.1035 0.0480 6.992 36.722 31.134 5213.611 4.149 138.484 2.709 0.76 286431. 0.5542
|
|
33.98 0.1869 0.3907 0.1023 0.0490 7.137 37.489 30.777 5322.400 4.235 136.897 2.623 0.76 286830. 0.5336
|
|
39.64 0.2180 0.4411 0.1009 0.0499 7.274 38.206 30.357 5424.307 4.317 135.027 2.538 0.76 287267. 0.5129
|
|
45.30 0.2492 0.4877 0.0993 0.0507 7.397 38.852 29.864 5515.924 4.389 132.836 2.456 0.76 287744. 0.4921
|
|
50.97 0.2803 0.5307 0.0974 0.0514 7.501 39.399 29.291 5593.604 4.451 130.286 2.375 0.76 288261. 0.4714
|
|
56.63 0.3115 0.5702 0.0952 0.0520 7.582 39.821 28.629 5653.528 4.499 127.342 2.297 0.77 288820. 0.4507
|
|
62.29 0.3426 0.6065 0.0927 0.0523 7.633 40.090 27.871 5691.761 4.529 123.971 2.221 0.77 289420. 0.4300
|
|
67.95 0.3738 0.6398 0.0898 0.0525 7.650 40.178 27.011 5704.294 4.539 120.146 2.148 0.77 290062. 0.4094
|
|
73.62 0.4049 0.6704 0.0866 0.0523 7.627 40.058 26.044 5687.147 4.526 115.843 2.077 0.77 290747. 0.3887
|
|
79.28 0.4360 0.6983 0.0830 0.0518 7.559 39.701 24.966 5636.501 4.485 111.048 2.009 0.77 291473. 0.3681
|
|
84.94 0.4672 0.7237 0.0791 0.0510 7.441 39.084 23.775 5548.871 4.416 105.751 1.943 0.77 292242. 0.3475
|
|
90.61 0.4983 0.7468 0.0747 0.0499 7.270 38.185 22.472 5421.337 4.314 99.955 1.880 0.77 293052. 0.3268
|
|
96.27 0.5295 0.7676 0.0700 0.0483 7.042 36.989 21.059 5251.539 4.179 93.669 1.819 0.77 293903. 0.3061
|
|
101.93 0.5606 0.7861 0.0650 0.0463 6.756 35.487 19.541 5038.186 4.009 86.918 1.759 0.77 294795. 0.2852
|
|
107.60 0.5918 0.8023 0.0596 0.0440 6.413 33.686 17.933 4782.534 3.806 79.768 1.701 0.77 295727. 0.2641
|
|
113.26 0.6229 0.8157 0.0540 0.0413 6.017 31.606 16.252 4487.190 3.571 72.290 1.643 0.78 296698. 0.2429
|
|
118.92 0.6541 0.8259 0.0483 0.0382 5.572 29.266 14.512 4154.980 3.306 64.549 1.584 0.78 297709. 0.2213
|
|
124.58 0.6852 0.8321 0.0423 0.0348 5.081 26.686 12.726 3788.719 3.015 56.603 1.523 0.78 298759. 0.1993
|
|
130.25 0.7164 0.8328 0.0363 0.0312 4.548 23.887 10.905 3391.352 2.699 48.505 1.458 0.78 299847. 0.1766
|
|
135.91 0.7475 0.8256 0.0301 0.0273 3.978 20.893 9.062 2966.230 2.360 40.309 1.386 0.78 300974. 0.1530
|
|
141.57 0.7787 0.8063 0.0240 0.0232 3.376 17.731 7.210 2517.307 2.003 32.069 1.299 0.78 302138. 0.1279
|
|
147.24 0.8098 0.7658 0.0178 0.0188 2.748 14.435 5.361 2049.420 1.631 23.844 1.186 0.79 303340. 0.1007
|
|
152.90 0.8409 0.6842 0.0117 0.0144 2.103 11.047 3.530 1568.396 1.248 15.700 1.021 0.79 304580. 0.0703
|
|
158.56 0.8721 0.5054 0.0058 0.0099 1.450 7.615 1.733 1081.141 0.860 7.708 0.727 0.79 305856. 0.0351
|
|
164.22 0.9032 -0.0075 0.0000 0.0055 0.798 4.189 -0.014 594.746 0.473 -0.060 -0.010 0.79 307162. 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 0.1079 0.0469 8.702 42.190 38.082 6488.995 4.767 169.387 2.662 0.83 308668. 0.6024
|
|
6.13 0.0311 0.0699 0.1074 0.0478 8.869 43.002 37.919 6613.944 4.858 168.665 2.600 0.83 308920. 0.5872
|
|
12.26 0.0622 0.1364 0.1069 0.0488 9.044 43.847 37.730 6743.862 4.954 167.822 2.538 0.83 309205. 0.5716
|
|
18.39 0.0934 0.1995 0.1063 0.0497 9.222 44.709 37.506 6876.543 5.051 166.827 2.474 0.83 309523. 0.5556
|
|
24.52 0.1245 0.2590 0.1055 0.0507 9.400 45.573 37.240 7009.344 5.149 165.642 2.410 0.83 309876. 0.5393
|
|
30.65 0.1556 0.3152 0.1046 0.0516 9.574 46.416 36.921 7139.026 5.244 164.226 2.346 0.83 310268. 0.5227
|
|
36.78 0.1867 0.3680 0.1035 0.0525 9.738 47.214 36.540 7261.827 5.334 162.532 2.282 0.83 310699. 0.5059
|
|
42.91 0.2179 0.4176 0.1022 0.0533 9.888 47.941 36.086 7373.538 5.416 160.509 2.220 0.83 311172. 0.4890
|
|
49.04 0.2490 0.4640 0.1007 0.0540 10.017 48.566 35.545 7469.672 5.487 158.106 2.158 0.83 311688. 0.4719
|
|
55.17 0.2801 0.5075 0.0989 0.0546 10.119 49.059 34.909 7545.611 5.543 155.273 2.098 0.83 312248. 0.4547
|
|
61.30 0.3112 0.5482 0.0968 0.0550 10.187 49.391 34.164 7596.669 5.580 151.962 2.040 0.83 312853. 0.4372
|
|
67.43 0.3423 0.5861 0.0944 0.0551 10.216 49.533 33.303 7618.419 5.596 148.131 1.983 0.83 313503. 0.4196
|
|
73.56 0.3735 0.6214 0.0916 0.0550 10.200 49.455 32.316 7606.452 5.587 143.743 1.927 0.83 314200. 0.4017
|
|
79.69 0.4046 0.6542 0.0884 0.0547 10.133 49.130 31.197 7556.485 5.551 138.766 1.873 0.83 314942. 0.3836
|
|
85.82 0.4357 0.6845 0.0848 0.0540 10.010 48.531 29.942 7464.382 5.483 133.180 1.819 0.83 315730. 0.3651
|
|
91.95 0.4668 0.7124 0.0809 0.0530 9.825 47.634 28.546 7326.405 5.382 126.973 1.767 0.83 316563. 0.3463
|
|
98.08 0.4980 0.7379 0.0765 0.0516 9.574 46.417 27.011 7139.246 5.244 120.146 1.716 0.84 317442. 0.3271
|
|
104.21 0.5291 0.7610 0.0718 0.0499 9.253 44.863 25.339 6900.175 5.069 112.708 1.666 0.84 318365. 0.3075
|
|
110.34 0.5602 0.7815 0.0667 0.0478 8.861 42.961 23.536 6607.559 4.854 104.689 1.616 0.84 319332. 0.2874
|
|
116.47 0.5913 0.7995 0.0613 0.0453 8.399 40.719 21.620 6262.773 4.600 96.165 1.566 0.84 320343. 0.2670
|
|
122.60 0.6224 0.8142 0.0556 0.0425 7.874 38.175 19.610 5871.590 4.313 87.224 1.515 0.84 321397. 0.2460
|
|
128.73 0.6536 0.8249 0.0496 0.0393 7.292 35.354 17.524 5437.652 3.994 77.945 1.462 0.84 322492. 0.2244
|
|
134.86 0.6847 0.8306 0.0436 0.0359 6.658 32.281 15.378 4965.058 3.647 68.400 1.405 0.84 323630. 0.2020
|
|
140.99 0.7158 0.8296 0.0374 0.0322 5.976 28.974 13.187 4456.355 3.273 58.655 1.342 0.85 324808. 0.1787
|
|
147.12 0.7469 0.8189 0.0311 0.0283 5.253 25.469 10.965 3917.236 2.877 48.774 1.270 0.85 326028. 0.1542
|
|
153.25 0.7781 0.7929 0.0247 0.0243 4.499 21.810 8.729 3354.549 2.464 38.825 1.180 0.85 327289. 0.1279
|
|
159.38 0.8092 0.7411 0.0184 0.0201 3.723 18.052 6.493 2776.492 2.040 28.879 1.061 0.85 328590. 0.0991
|
|
165.52 0.8403 0.6418 0.0121 0.0159 2.940 14.255 4.276 2192.439 1.610 19.018 0.885 0.85 329932. 0.0671
|
|
171.65 0.8714 0.4441 0.0059 0.0117 2.163 10.486 2.099 1612.803 1.185 9.335 0.590 0.86 331314. 0.0314
|
|
177.78 0.9026 -0.0063 -0.0001 0.0076 1.404 6.808 -0.019 1047.073 0.769 -0.083 -0.008 0.86 332728. 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 0.1078 0.0532 12.308 55.413 44.147 9178.418 6.261 196.364 2.182 0.89 332408. 0.5316
|
|
6.62 0.0312 0.0620 0.1075 0.0541 12.520 56.367 43.993 9336.507 6.368 195.682 2.137 0.89 332677. 0.5199
|
|
13.24 0.0624 0.1214 0.1070 0.0550 12.740 57.357 43.814 9500.390 6.480 194.883 2.092 0.89 332981. 0.5078
|
|
19.86 0.0936 0.1781 0.1065 0.0560 12.963 58.361 43.600 9666.680 6.594 193.931 2.046 0.89 333321. 0.4954
|
|
26.47 0.1248 0.2321 0.1059 0.0569 13.184 59.354 43.341 9831.186 6.706 192.783 2.000 0.89 333700. 0.4828
|
|
33.09 0.1560 0.2835 0.1051 0.0579 13.395 60.305 43.028 9988.762 6.813 191.387 1.954 0.89 334120. 0.4700
|
|
39.71 0.1872 0.3323 0.1042 0.0587 13.589 61.179 42.645 10133.444 6.912 189.685 1.909 0.89 334583. 0.4571
|
|
46.33 0.2184 0.3788 0.1030 0.0594 13.757 61.935 42.179 10258.625 6.997 187.613 1.865 0.89 335092. 0.4442
|
|
52.95 0.2496 0.4230 0.1017 0.0600 13.890 62.531 41.615 10357.489 7.065 185.105 1.822 0.89 335648. 0.4311
|
|
59.57 0.2808 0.4652 0.1000 0.0604 13.978 62.929 40.938 10423.325 7.110 182.092 1.781 0.89 336252. 0.4180
|
|
66.19 0.3120 0.5054 0.0980 0.0605 14.013 63.087 40.132 10449.443 7.127 178.509 1.742 0.89 336905. 0.4047
|
|
72.80 0.3432 0.5439 0.0957 0.0604 13.987 62.970 39.185 10430.149 7.114 174.294 1.704 0.89 337608. 0.3912
|
|
79.42 0.3744 0.5805 0.0930 0.0600 13.895 62.555 38.085 10361.400 7.067 169.400 1.667 0.89 338362. 0.3773
|
|
86.04 0.4056 0.6153 0.0900 0.0593 13.731 61.815 36.822 10238.853 6.984 163.785 1.631 0.90 339165. 0.3630
|
|
92.66 0.4368 0.6483 0.0865 0.0583 13.489 60.728 35.390 10058.776 6.861 157.417 1.596 0.90 340019. 0.3482
|
|
99.28 0.4680 0.6793 0.0825 0.0569 13.166 59.275 33.785 9818.160 6.697 150.277 1.561 0.90 340923. 0.3327
|
|
105.90 0.4992 0.7083 0.0782 0.0551 12.760 57.444 32.007 9514.900 6.490 142.366 1.526 0.90 341876. 0.3166
|
|
112.52 0.5304 0.7351 0.0734 0.0530 12.267 55.227 30.057 9147.564 6.239 133.694 1.490 0.90 342877. 0.2996
|
|
119.13 0.5616 0.7595 0.0683 0.0505 11.688 52.620 27.945 8715.729 5.945 124.300 1.454 0.90 343926. 0.2819
|
|
125.75 0.5928 0.7813 0.0628 0.0476 11.026 49.640 25.691 8222.277 5.608 114.274 1.417 0.90 345022. 0.2634
|
|
132.37 0.6240 0.7997 0.0570 0.0445 10.292 46.335 23.319 7674.802 5.235 103.722 1.378 0.91 346164. 0.2440
|
|
138.99 0.6552 0.8126 0.0509 0.0411 9.509 42.809 20.848 7090.768 4.837 92.734 1.334 0.91 347351. 0.2233
|
|
145.61 0.6864 0.8180 0.0447 0.0375 8.687 39.107 18.300 6477.620 4.418 81.398 1.281 0.91 348584. 0.2010
|
|
152.23 0.7176 0.8102 0.0383 0.0339 7.860 35.384 15.688 5860.939 3.998 69.780 1.214 0.91 349861. 0.1763
|
|
158.85 0.7488 0.7892 0.0319 0.0302 6.998 31.504 13.038 5218.210 3.559 57.994 1.133 0.91 351182. 0.1501
|
|
165.46 0.7800 0.7477 0.0253 0.0264 6.119 27.546 10.370 4562.705 3.112 46.124 1.031 0.92 352548. 0.1217
|
|
172.08 0.8112 0.6751 0.0188 0.0226 5.237 23.577 7.704 3905.280 2.664 34.269 0.895 0.92 353956. 0.0911
|
|
178.70 0.8425 0.5525 0.0124 0.0189 4.372 19.681 5.069 3259.902 2.224 22.547 0.705 0.92 355409. 0.0582
|
|
185.32 0.8737 0.3482 0.0061 0.0153 3.539 15.933 2.494 2639.026 1.800 11.091 0.429 0.92 356904. 0.0248
|
|
191.94 0.9049 0.0008 0.0000 0.0119 2.750 12.380 0.004 2050.501 1.399 0.020 0.001 0.92 358441. 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 0.1056 0.0583 16.600 69.751 49.640 12378.463 7.880 220.798 1.819 0.95 356221. 0.4700
|
|
7.18 0.0316 0.0562 0.1053 0.0592 16.864 70.859 49.495 12575.199 8.006 220.156 1.785 0.95 356509. 0.4606
|
|
14.35 0.0631 0.1101 0.1050 0.0602 17.144 72.037 49.329 12784.180 8.139 219.414 1.750 0.95 356834. 0.4508
|
|
21.53 0.0947 0.1617 0.1046 0.0612 17.436 73.263 49.132 13001.893 8.277 218.538 1.714 0.95 357198. 0.4406
|
|
28.70 0.1263 0.2110 0.1040 0.0623 17.733 74.513 48.895 13223.628 8.418 217.483 1.677 0.95 357604. 0.4301
|
|
35.88 0.1579 0.2579 0.1034 0.0633 18.028 75.750 48.605 13443.227 8.558 216.193 1.640 0.95 358055. 0.4193
|
|
43.05 0.1894 0.3025 0.1027 0.0643 18.309 76.932 48.248 13652.884 8.692 214.605 1.603 0.95 358553. 0.4083
|
|
50.23 0.2210 0.3449 0.1017 0.0652 18.564 78.004 47.807 13843.257 8.813 212.645 1.566 0.95 359100. 0.3972
|
|
57.40 0.2526 0.3852 0.1006 0.0659 18.779 78.908 47.264 14003.580 8.915 210.230 1.531 0.96 359699. 0.3860
|
|
64.58 0.2841 0.4237 0.0992 0.0665 18.938 79.575 46.599 14122.028 8.990 207.272 1.497 0.96 360351. 0.3747
|
|
71.75 0.3157 0.4605 0.0974 0.0668 19.024 79.936 45.791 14186.141 9.031 203.680 1.464 0.96 361057. 0.3633
|
|
78.93 0.3473 0.4959 0.0954 0.0668 19.021 79.922 44.821 14183.603 9.030 199.364 1.433 0.96 361819. 0.3519
|
|
86.10 0.3788 0.5301 0.0929 0.0664 18.913 79.469 43.669 14103.160 8.978 194.238 1.404 0.96 362638. 0.3403
|
|
93.28 0.4104 0.5632 0.0901 0.0656 18.688 78.525 42.317 13935.564 8.872 188.228 1.377 0.96 363512. 0.3286
|
|
100.45 0.4420 0.5953 0.0867 0.0644 18.337 77.052 40.754 13674.208 8.705 181.276 1.352 0.96 364443. 0.3165
|
|
107.63 0.4736 0.6263 0.0829 0.0627 17.856 75.030 38.971 13315.475 8.477 173.345 1.327 0.96 365430. 0.3039
|
|
114.80 0.5051 0.6562 0.0787 0.0605 17.242 72.451 36.964 12857.648 8.185 164.415 1.304 0.96 366471. 0.2907
|
|
121.98 0.5367 0.6847 0.0739 0.0579 16.500 69.331 34.736 12304.059 7.833 154.506 1.280 0.97 367567. 0.2768
|
|
129.15 0.5683 0.7114 0.0687 0.0549 15.636 65.700 32.301 11659.674 7.423 143.673 1.257 0.97 368715. 0.2619
|
|
136.33 0.5998 0.7360 0.0632 0.0515 14.662 61.609 29.684 10933.598 6.961 132.037 1.231 0.97 369916. 0.2460
|
|
143.50 0.6314 0.7578 0.0573 0.0477 13.592 57.114 26.919 10135.824 6.453 119.736 1.205 0.97 371167. 0.2292
|
|
150.68 0.6630 0.7738 0.0511 0.0438 12.476 52.422 24.029 9303.162 5.923 106.880 1.172 0.97 372469. 0.2106
|
|
157.85 0.6945 0.7804 0.0448 0.0398 11.347 47.679 21.039 8461.528 5.387 93.580 1.128 0.97 373819. 0.1897
|
|
165.03 0.7261 0.7621 0.0382 0.0364 10.366 43.556 17.953 7729.792 4.921 79.854 1.053 0.98 375218. 0.1637
|
|
172.20 0.7577 0.7221 0.0315 0.0331 9.424 39.598 14.820 7027.371 4.474 65.921 0.957 0.98 376665. 0.1350
|
|
179.38 0.7893 0.6580 0.0249 0.0298 8.492 35.684 11.683 6332.818 4.032 51.965 0.837 0.98 378160. 0.1049
|
|
186.55 0.8208 0.5621 0.0183 0.0267 7.595 31.914 8.582 5663.759 3.606 38.172 0.687 0.98 379703. 0.0738
|
|
193.73 0.8524 0.4262 0.0118 0.0237 6.745 28.340 5.565 5029.504 3.202 24.751 0.502 0.99 381294. 0.0434
|
|
200.90 0.8840 0.2408 0.0057 0.0209 5.954 25.019 2.676 4440.032 2.827 11.903 0.273 0.99 382938. 0.0164
|
|
208.08 0.9155 -0.0086 -0.0002 0.0183 5.213 21.903 -0.081 3887.141 2.475 -0.361 -0.009 0.99 384681. 0.0000
|
|
|
|
|
|
|