575 lines
102 KiB
Plaintext
575 lines
102 KiB
Plaintext
14x14E (14x14E.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 0.1083 0.0611 0.003 0.167 0.133 1.971 0.019 0.590 30.502 0.06 18212. 0.4654
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0.53 0.0398 0.0692 0.1079 0.0621 0.003 0.169 0.132 2.005 0.019 0.587 29.869 0.06 18232. 0.4549
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1.06 0.0797 0.1352 0.1074 0.0633 0.003 0.173 0.132 2.044 0.020 0.585 29.192 0.06 18254. 0.4437
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1.58 0.1195 0.1978 0.1070 0.0646 0.003 0.176 0.131 2.086 0.020 0.582 28.476 0.06 18279. 0.4319
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2.11 0.1593 0.2568 0.1064 0.0661 0.003 0.180 0.130 2.132 0.020 0.580 27.725 0.06 18308. 0.4195
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2.64 0.1992 0.3119 0.1058 0.0676 0.003 0.184 0.130 2.181 0.021 0.576 26.948 0.06 18341. 0.4066
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3.17 0.2390 0.3633 0.1051 0.0692 0.003 0.189 0.129 2.232 0.021 0.572 26.151 0.06 18377. 0.3932
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3.70 0.2788 0.4107 0.1042 0.0708 0.003 0.193 0.128 2.284 0.022 0.568 25.342 0.06 18418. 0.3795
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4.22 0.3187 0.4543 0.1032 0.0724 0.003 0.197 0.126 2.336 0.022 0.562 24.529 0.06 18463. 0.3654
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4.75 0.3585 0.4942 0.1019 0.0739 0.003 0.202 0.125 2.386 0.023 0.555 23.719 0.06 18512. 0.3512
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5.28 0.3983 0.5306 0.1004 0.0754 0.003 0.206 0.123 2.432 0.023 0.547 22.918 0.06 18566. 0.3367
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5.81 0.4382 0.5636 0.0985 0.0766 0.003 0.209 0.121 2.472 0.024 0.536 22.131 0.06 18624. 0.3221
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6.34 0.4780 0.5935 0.0963 0.0775 0.003 0.212 0.118 2.502 0.024 0.524 21.363 0.06 18687. 0.3074
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6.87 0.5178 0.6204 0.0936 0.0781 0.003 0.213 0.115 2.522 0.024 0.510 20.615 0.06 18754. 0.2925
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7.39 0.5577 0.6446 0.0905 0.0783 0.003 0.214 0.111 2.528 0.024 0.493 19.888 0.06 18826. 0.2775
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7.92 0.5975 0.6662 0.0869 0.0780 0.003 0.213 0.106 2.517 0.024 0.473 19.183 0.06 18903. 0.2623
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8.45 0.6373 0.6852 0.0828 0.0771 0.003 0.210 0.101 2.487 0.024 0.451 18.497 0.06 18984. 0.2469
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8.98 0.6772 0.7015 0.0782 0.0755 0.003 0.206 0.096 2.437 0.023 0.426 17.824 0.06 19070. 0.2312
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9.51 0.7170 0.7149 0.0731 0.0733 0.003 0.200 0.089 2.366 0.023 0.398 17.156 0.06 19160. 0.2151
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10.03 0.7568 0.7250 0.0675 0.0704 0.003 0.192 0.083 2.273 0.022 0.367 16.482 0.06 19254. 0.1986
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10.56 0.7967 0.7310 0.0615 0.0670 0.003 0.183 0.075 2.162 0.021 0.335 15.787 0.06 19352. 0.1815
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11.09 0.8365 0.7318 0.0551 0.0630 0.003 0.172 0.067 2.034 0.019 0.300 15.051 0.06 19454. 0.1639
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11.62 0.8763 0.7259 0.0485 0.0586 0.003 0.160 0.059 1.891 0.018 0.264 14.252 0.06 19561. 0.1456
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12.15 0.9162 0.7113 0.0417 0.0538 0.002 0.147 0.051 1.735 0.017 0.227 13.358 0.06 19671. 0.1266
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12.67 0.9560 0.6849 0.0348 0.0486 0.002 0.133 0.043 1.569 0.015 0.190 12.327 0.06 19786. 0.1067
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13.20 0.9958 0.6421 0.0278 0.0431 0.002 0.118 0.034 1.392 0.013 0.151 11.094 0.06 19904. 0.0858
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13.73 1.0357 0.5750 0.0208 0.0374 0.002 0.102 0.025 1.208 0.012 0.113 9.553 0.06 20025. 0.0639
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14.26 1.0755 0.4701 0.0138 0.0315 0.001 0.086 0.017 1.018 0.010 0.075 7.520 0.06 20151. 0.0409
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14.79 1.1153 0.3008 0.0069 0.0255 0.001 0.070 0.008 0.823 0.008 0.037 4.640 0.06 20280. 0.0178
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15.31 1.1552 0.0078 0.0001 0.0194 0.001 0.053 0.000 0.626 0.006 0.001 0.117 0.06 20413. 0.0001
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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 0.1086 0.0567 0.020 0.619 0.532 14.643 0.070 2.365 16.471 0.11 36425. 0.5034
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1.06 0.0401 0.0751 0.1082 0.0578 0.020 0.631 0.530 14.927 0.071 2.357 16.102 0.11 36463. 0.4913
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2.13 0.0802 0.1465 0.1078 0.0590 0.020 0.644 0.528 15.244 0.073 2.348 15.709 0.11 36508. 0.4784
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3.19 0.1203 0.2139 0.1074 0.0604 0.021 0.659 0.526 15.594 0.074 2.339 15.293 0.11 36559. 0.4648
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4.25 0.1605 0.2771 0.1069 0.0619 0.021 0.675 0.523 15.975 0.076 2.328 14.859 0.11 36617. 0.4505
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5.32 0.2006 0.3360 0.1063 0.0635 0.022 0.692 0.520 16.382 0.078 2.315 14.410 0.11 36683. 0.4357
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6.38 0.2407 0.3903 0.1056 0.0651 0.023 0.710 0.517 16.809 0.080 2.300 13.952 0.11 36757. 0.4205
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7.45 0.2808 0.4403 0.1047 0.0668 0.023 0.729 0.513 17.247 0.082 2.281 13.489 0.11 36840. 0.4049
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8.51 0.3209 0.4859 0.1037 0.0685 0.024 0.747 0.508 17.683 0.084 2.259 13.025 0.11 36930. 0.3890
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9.57 0.3610 0.5274 0.1024 0.0701 0.024 0.765 0.502 18.105 0.086 2.231 12.566 0.11 37030. 0.3730
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10.64 0.4011 0.5649 0.1009 0.0716 0.025 0.782 0.494 18.496 0.088 2.197 12.115 0.11 37139. 0.3569
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11.70 0.4413 0.5988 0.0990 0.0730 0.025 0.796 0.485 18.836 0.090 2.156 11.674 0.11 37257. 0.3407
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12.76 0.4814 0.6293 0.0967 0.0740 0.026 0.807 0.474 19.106 0.091 2.107 11.247 0.11 37385. 0.3244
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13.83 0.5215 0.6567 0.0941 0.0747 0.026 0.815 0.461 19.284 0.092 2.049 10.834 0.11 37521. 0.3082
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14.89 0.5616 0.6813 0.0909 0.0749 0.026 0.818 0.445 19.347 0.092 1.980 10.436 0.11 37667. 0.2918
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15.95 0.6017 0.7033 0.0873 0.0747 0.026 0.815 0.427 19.275 0.092 1.901 10.055 0.11 37823. 0.2755
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17.02 0.6418 0.7227 0.0831 0.0738 0.026 0.805 0.407 19.048 0.091 1.809 9.687 0.11 37987. 0.2590
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18.08 0.6819 0.7397 0.0784 0.0722 0.025 0.788 0.384 18.651 0.089 1.707 9.331 0.11 38160. 0.2423
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19.15 0.7221 0.7540 0.0731 0.0700 0.024 0.764 0.358 18.078 0.086 1.593 8.984 0.11 38342. 0.2253
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20.21 0.7622 0.7654 0.0674 0.0671 0.023 0.732 0.330 17.330 0.083 1.468 8.639 0.11 38533. 0.2080
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21.27 0.8023 0.7732 0.0613 0.0636 0.022 0.694 0.300 16.422 0.078 1.335 8.291 0.11 38732. 0.1904
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22.34 0.8424 0.7765 0.0549 0.0595 0.021 0.650 0.269 15.372 0.073 1.195 7.930 0.11 38940. 0.1723
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23.40 0.8825 0.7739 0.0482 0.0550 0.019 0.600 0.236 14.197 0.068 1.050 7.544 0.12 39156. 0.1537
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24.46 0.9226 0.7637 0.0414 0.0500 0.017 0.546 0.203 12.911 0.062 0.902 7.121 0.12 39379. 0.1344
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25.53 0.9627 0.7427 0.0344 0.0447 0.015 0.487 0.169 11.528 0.055 0.750 6.636 0.12 39611. 0.1142
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26.59 1.0029 0.7061 0.0274 0.0390 0.013 0.425 0.134 10.062 0.048 0.598 6.057 0.12 39850. 0.0931
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27.65 1.0430 0.6454 0.0204 0.0330 0.011 0.360 0.100 8.524 0.041 0.445 5.324 0.12 40096. 0.0706
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28.72 1.0831 0.5438 0.0135 0.0268 0.009 0.293 0.066 6.932 0.033 0.294 4.319 0.12 40351. 0.0465
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29.78 1.1232 0.3638 0.0066 0.0205 0.007 0.224 0.033 5.301 0.025 0.145 2.786 0.12 40612. 0.0211
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30.85 1.1633 0.0008 0.0000 0.0141 0.005 0.154 0.000 3.652 0.017 0.000 0.006 0.12 40881. 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 0.1088 0.0548 0.064 1.347 1.198 47.793 0.152 5.331 11.374 0.17 54637. 0.5219
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1.60 0.0402 0.0780 0.1084 0.0560 0.065 1.374 1.195 48.761 0.155 5.313 11.111 0.17 54695. 0.5090
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3.20 0.0805 0.1520 0.1080 0.0572 0.067 1.404 1.190 49.848 0.159 5.294 10.830 0.17 54762. 0.4952
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4.80 0.1207 0.2217 0.1076 0.0586 0.068 1.438 1.186 51.048 0.162 5.273 10.534 0.17 54839. 0.4807
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6.40 0.1609 0.2869 0.1071 0.0601 0.070 1.475 1.180 52.356 0.167 5.250 10.225 0.17 54927. 0.4656
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8.00 0.2012 0.3475 0.1066 0.0617 0.072 1.515 1.174 53.756 0.171 5.222 9.906 0.17 55026. 0.4498
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9.60 0.2414 0.4033 0.1059 0.0634 0.074 1.556 1.167 55.226 0.176 5.189 9.581 0.17 55138. 0.4337
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11.20 0.2817 0.4544 0.1050 0.0651 0.076 1.598 1.157 56.735 0.181 5.148 9.252 0.17 55262. 0.4172
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12.80 0.3219 0.5009 0.1040 0.0668 0.078 1.641 1.146 58.245 0.185 5.098 8.925 0.17 55399. 0.4004
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14.40 0.3621 0.5431 0.1028 0.0685 0.080 1.682 1.132 59.708 0.190 5.036 8.601 0.17 55549. 0.3836
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16.00 0.4024 0.5811 0.1012 0.0701 0.082 1.720 1.115 61.066 0.194 4.960 8.283 0.17 55714. 0.3666
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17.60 0.4426 0.6154 0.0993 0.0714 0.083 1.754 1.095 62.256 0.198 4.868 7.974 0.17 55892. 0.3496
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19.20 0.4828 0.6462 0.0971 0.0725 0.085 1.781 1.070 63.208 0.201 4.758 7.675 0.17 56084. 0.3327
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20.80 0.5231 0.6738 0.0944 0.0733 0.086 1.799 1.040 63.846 0.203 4.625 7.388 0.17 56290. 0.3157
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22.40 0.5633 0.6985 0.0912 0.0736 0.086 1.806 1.005 64.094 0.204 4.470 7.112 0.17 56510. 0.2988
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24.00 0.6036 0.7207 0.0875 0.0733 0.086 1.800 0.964 63.876 0.203 4.290 6.848 0.17 56744. 0.2819
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25.61 0.6438 0.7404 0.0833 0.0724 0.085 1.779 0.918 63.126 0.201 4.083 6.596 0.17 56992. 0.2649
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27.21 0.6840 0.7577 0.0786 0.0709 0.083 1.741 0.866 61.794 0.197 3.850 6.353 0.17 57254. 0.2477
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28.81 0.7243 0.7726 0.0733 0.0687 0.080 1.686 0.807 59.853 0.191 3.591 6.118 0.17 57529. 0.2304
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30.41 0.7645 0.7847 0.0675 0.0658 0.077 1.615 0.744 57.309 0.182 3.308 5.887 0.17 57816. 0.2128
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32.01 0.8047 0.7935 0.0613 0.0622 0.073 1.527 0.676 54.213 0.173 3.007 5.655 0.17 58117. 0.1949
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33.61 0.8450 0.7982 0.0549 0.0581 0.068 1.426 0.605 50.624 0.161 2.690 5.418 0.17 58430. 0.1766
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35.21 0.8852 0.7977 0.0482 0.0535 0.062 1.313 0.531 46.598 0.148 2.362 5.168 0.17 58755. 0.1578
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36.81 0.9254 0.7901 0.0413 0.0484 0.057 1.188 0.455 42.183 0.134 2.025 4.896 0.17 59093. 0.1385
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38.41 0.9657 0.7726 0.0344 0.0430 0.050 1.054 0.379 37.426 0.119 1.684 4.588 0.17 59442. 0.1183
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40.01 1.0059 0.7404 0.0273 0.0372 0.043 0.912 0.301 32.372 0.103 1.340 4.221 0.17 59802. 0.0971
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41.61 1.0462 0.6847 0.0203 0.0311 0.036 0.763 0.224 27.071 0.086 0.996 3.754 0.18 60174. 0.0745
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43.21 1.0864 0.5876 0.0134 0.0248 0.029 0.608 0.148 21.574 0.069 0.656 3.102 0.18 60558. 0.0499
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44.81 1.1266 0.4054 0.0066 0.0183 0.021 0.449 0.073 15.944 0.051 0.323 2.064 0.18 60952. 0.0233
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46.41 1.1669 -0.0020 0.0000 0.0118 0.014 0.289 0.000 10.247 0.033 -0.001 -0.010 0.18 61358. 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 0.1089 0.0538 0.149 2.348 2.134 111.135 0.265 9.491 8.708 0.22 72848. 0.5331
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2.14 0.0403 0.0797 0.1086 0.0549 0.152 2.397 2.127 113.448 0.271 9.460 8.503 0.22 72926. 0.5197
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4.27 0.0806 0.1552 0.1082 0.0562 0.156 2.452 2.120 116.044 0.277 9.428 8.285 0.22 73015. 0.5055
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6.41 0.1209 0.2264 0.1078 0.0576 0.159 2.513 2.112 118.918 0.284 9.392 8.054 0.22 73119. 0.4905
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8.55 0.1612 0.2928 0.1073 0.0591 0.164 2.579 2.102 122.051 0.291 9.352 7.813 0.22 73236. 0.4748
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10.69 0.2015 0.3544 0.1068 0.0607 0.168 2.650 2.092 125.409 0.299 9.304 7.565 0.22 73369. 0.4586
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12.82 0.2418 0.4111 0.1061 0.0624 0.173 2.725 2.079 128.941 0.308 9.246 7.312 0.22 73518. 0.4419
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14.96 0.2821 0.4629 0.1053 0.0642 0.178 2.801 2.063 132.575 0.316 9.175 7.057 0.22 73683. 0.4248
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17.10 0.3224 0.5099 0.1043 0.0659 0.183 2.878 2.043 136.217 0.325 9.088 6.803 0.22 73867. 0.4076
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19.23 0.3627 0.5525 0.1031 0.0677 0.187 2.953 2.019 139.752 0.334 8.980 6.552 0.22 74068. 0.3902
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21.37 0.4030 0.5909 0.1015 0.0693 0.192 3.023 1.989 143.044 0.341 8.847 6.306 0.22 74288. 0.3728
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23.51 0.4433 0.6254 0.0997 0.0707 0.196 3.084 1.952 145.939 0.348 8.684 6.068 0.22 74526. 0.3553
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25.65 0.4836 0.6563 0.0974 0.0718 0.199 3.133 1.908 148.268 0.354 8.487 5.837 0.22 74783. 0.3380
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27.78 0.5239 0.6840 0.0947 0.0725 0.201 3.166 1.855 149.850 0.358 8.253 5.616 0.23 75059. 0.3206
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29.92 0.5642 0.7089 0.0915 0.0729 0.202 3.180 1.793 150.499 0.359 7.976 5.404 0.23 75353. 0.3033
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32.06 0.6045 0.7312 0.0879 0.0726 0.201 3.170 1.721 150.034 0.358 7.655 5.203 0.23 75666. 0.2860
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34.20 0.6448 0.7510 0.0836 0.0718 0.199 3.133 1.638 148.291 0.354 7.286 5.010 0.23 75998. 0.2687
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36.33 0.6851 0.7686 0.0788 0.0703 0.195 3.067 1.544 145.148 0.347 6.869 4.826 0.23 76348. 0.2513
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38.47 0.7254 0.7838 0.0735 0.0680 0.188 2.970 1.440 140.538 0.336 6.406 4.648 0.23 76715. 0.2338
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40.61 0.7657 0.7965 0.0677 0.0651 0.180 2.842 1.327 134.479 0.321 5.901 4.474 0.23 77100. 0.2160
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42.74 0.8060 0.8061 0.0615 0.0615 0.170 2.685 1.205 127.085 0.303 5.361 4.302 0.23 77502. 0.1979
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44.88 0.8463 0.8119 0.0550 0.0574 0.159 2.504 1.078 118.496 0.283 4.795 4.126 0.23 77921. 0.1796
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47.02 0.8866 0.8127 0.0483 0.0527 0.146 2.300 0.946 108.844 0.260 4.209 3.943 0.23 78356. 0.1607
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49.16 0.9269 0.8070 0.0414 0.0476 0.132 2.076 0.811 98.246 0.235 3.608 3.745 0.23 78807. 0.1414
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51.29 0.9672 0.7921 0.0344 0.0420 0.116 1.834 0.674 86.812 0.207 2.999 3.522 0.23 79274. 0.1212
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53.43 1.0075 0.7632 0.0274 0.0361 0.100 1.577 0.536 74.654 0.178 2.385 3.258 0.23 79756. 0.1000
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55.57 1.0478 0.7117 0.0204 0.0300 0.083 1.308 0.399 61.889 0.148 1.773 2.922 0.23 80254. 0.0773
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57.70 1.0881 0.6191 0.0134 0.0236 0.065 1.028 0.262 48.649 0.116 1.168 2.447 0.24 80766. 0.0525
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59.84 1.1284 0.4378 0.0066 0.0170 0.047 0.741 0.129 35.082 0.084 0.574 1.669 0.24 81294. 0.0251
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61.98 1.1687 -0.0011 0.0000 0.0103 0.029 0.451 0.000 21.356 0.051 -0.001 -0.004 0.24 81835. 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 0.1091 0.0532 0.288 3.626 3.339 214.512 0.410 14.850 7.059 0.28 91059. 0.5406
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2.71 0.0409 0.0818 0.1087 0.0543 0.294 3.704 3.328 219.110 0.418 14.804 6.889 0.28 91158. 0.5268
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5.42 0.0817 0.1593 0.1084 0.0556 0.301 3.791 3.317 224.286 0.428 14.754 6.708 0.28 91272. 0.5120
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8.12 0.1226 0.2321 0.1080 0.0570 0.308 3.888 3.305 230.026 0.439 14.700 6.517 0.28 91403. 0.4965
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10.83 0.1634 0.3000 0.1075 0.0586 0.317 3.994 3.291 236.296 0.451 14.638 6.317 0.28 91552. 0.4803
|
|
13.54 0.2043 0.3627 0.1070 0.0602 0.326 4.108 3.274 243.027 0.464 14.564 6.111 0.28 91722. 0.4635
|
|
16.25 0.2451 0.4204 0.1063 0.0620 0.335 4.228 3.254 250.112 0.478 14.475 5.901 0.28 91912. 0.4462
|
|
18.96 0.2860 0.4729 0.1055 0.0638 0.345 4.351 3.229 257.402 0.492 14.364 5.690 0.28 92124. 0.4286
|
|
21.66 0.3268 0.5205 0.1045 0.0656 0.355 4.475 3.198 264.704 0.506 14.226 5.480 0.28 92359. 0.4108
|
|
24.37 0.3677 0.5634 0.1032 0.0674 0.364 4.594 3.160 271.779 0.519 14.054 5.273 0.28 92616. 0.3928
|
|
27.08 0.4085 0.6020 0.1017 0.0690 0.373 4.705 3.112 278.342 0.532 13.841 5.071 0.28 92898. 0.3749
|
|
29.79 0.4494 0.6365 0.0997 0.0704 0.381 4.802 3.053 284.072 0.543 13.579 4.874 0.28 93203. 0.3570
|
|
32.50 0.4902 0.6675 0.0974 0.0715 0.387 4.879 2.982 288.618 0.551 13.262 4.686 0.28 93532. 0.3391
|
|
35.20 0.5311 0.6952 0.0946 0.0723 0.391 4.929 2.896 291.604 0.557 12.882 4.505 0.28 93886. 0.3213
|
|
37.91 0.5719 0.7200 0.0913 0.0725 0.392 4.947 2.795 292.646 0.559 12.433 4.332 0.28 94263. 0.3036
|
|
40.62 0.6128 0.7422 0.0875 0.0722 0.391 4.925 2.678 291.372 0.556 11.910 4.168 0.28 94665. 0.2859
|
|
43.33 0.6536 0.7620 0.0831 0.0713 0.385 4.859 2.543 287.455 0.549 11.309 4.012 0.28 95090. 0.2681
|
|
46.04 0.6945 0.7796 0.0781 0.0696 0.376 4.744 2.390 280.660 0.536 10.632 3.863 0.28 95538. 0.2503
|
|
48.74 0.7353 0.7948 0.0726 0.0671 0.363 4.579 2.221 270.875 0.517 9.880 3.719 0.29 96010. 0.2323
|
|
51.45 0.7762 0.8074 0.0666 0.0640 0.346 4.364 2.037 258.181 0.493 9.062 3.579 0.29 96503. 0.2141
|
|
54.16 0.8170 0.8168 0.0602 0.0602 0.326 4.105 1.842 242.832 0.464 8.193 3.440 0.29 97018. 0.1957
|
|
56.87 0.8579 0.8224 0.0535 0.0558 0.302 3.805 1.637 225.113 0.430 7.283 3.299 0.29 97555. 0.1769
|
|
59.58 0.8987 0.8230 0.0466 0.0509 0.275 3.470 1.426 205.284 0.392 6.343 3.151 0.29 98112. 0.1577
|
|
62.28 0.9396 0.8165 0.0395 0.0455 0.246 3.103 1.210 183.578 0.351 5.384 2.990 0.29 98690. 0.1379
|
|
64.99 0.9804 0.8000 0.0324 0.0397 0.215 2.708 0.992 160.223 0.306 4.412 2.808 0.29 99287. 0.1172
|
|
67.70 1.0213 0.7679 0.0252 0.0336 0.182 2.290 0.773 135.449 0.259 3.437 2.587 0.29 99905. 0.0953
|
|
70.41 1.0621 0.7088 0.0181 0.0271 0.147 1.851 0.554 109.511 0.209 2.466 2.296 0.29 100542. 0.0717
|
|
73.12 1.1030 0.5968 0.0111 0.0205 0.111 1.398 0.339 82.694 0.158 1.510 1.862 0.29 101199. 0.0455
|
|
75.82 1.1438 0.3537 0.0042 0.0137 0.074 0.935 0.130 55.322 0.106 0.577 1.064 0.30 101874. 0.0161
|
|
78.53 1.1847
|
|
|
|
|
|
|
|
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 0.1092 0.0528 0.494 5.184 4.814 368.013 0.586 21.415 5.934 0.33 109270. 0.5457
|
|
3.21 0.0404 0.0815 0.1089 0.0539 0.504 5.295 4.800 375.876 0.598 21.352 5.793 0.33 109386. 0.5319
|
|
6.42 0.0807 0.1588 0.1086 0.0552 0.516 5.420 4.785 384.727 0.612 21.285 5.642 0.33 109521. 0.5172
|
|
9.63 0.1211 0.2315 0.1082 0.0566 0.529 5.558 4.769 394.549 0.628 21.212 5.482 0.33 109676. 0.5018
|
|
12.85 0.1615 0.2994 0.1078 0.0581 0.543 5.709 4.750 405.287 0.645 21.128 5.316 0.33 109852. 0.4856
|
|
16.06 0.2019 0.3621 0.1073 0.0598 0.559 5.872 4.728 416.833 0.663 21.029 5.145 0.33 110052. 0.4688
|
|
19.27 0.2422 0.4198 0.1067 0.0615 0.575 6.044 4.701 429.015 0.683 20.909 4.970 0.33 110276. 0.4516
|
|
22.48 0.2826 0.4724 0.1059 0.0633 0.592 6.221 4.667 441.593 0.703 20.760 4.794 0.33 110525. 0.4341
|
|
25.69 0.3230 0.5201 0.1049 0.0652 0.609 6.399 4.625 454.247 0.723 20.573 4.618 0.33 110801. 0.4163
|
|
28.90 0.3633 0.5632 0.1038 0.0669 0.626 6.573 4.573 466.585 0.743 20.339 4.445 0.34 111104. 0.3984
|
|
32.11 0.4037 0.6020 0.1023 0.0686 0.641 6.736 4.507 478.137 0.761 20.049 4.276 0.34 111434. 0.3805
|
|
35.32 0.4441 0.6367 0.1004 0.0701 0.655 6.880 4.427 488.366 0.777 19.691 4.112 0.34 111793. 0.3626
|
|
38.54 0.4845 0.6679 0.0982 0.0712 0.666 6.997 4.329 496.682 0.790 19.256 3.953 0.34 112179. 0.3448
|
|
41.75 0.5248 0.6958 0.0956 0.0721 0.674 7.078 4.212 502.454 0.800 18.733 3.802 0.34 112594. 0.3270
|
|
44.96 0.5652 0.7208 0.0924 0.0724 0.677 7.114 4.072 505.032 0.804 18.114 3.657 0.34 113038. 0.3093
|
|
48.17 0.6056 0.7433 0.0887 0.0723 0.676 7.097 3.910 503.774 0.802 17.390 3.520 0.34 113509. 0.2917
|
|
51.38 0.6459 0.7635 0.0845 0.0715 0.668 7.017 3.722 498.106 0.793 16.556 3.389 0.34 114008. 0.2741
|
|
54.59 0.6863 0.7814 0.0796 0.0699 0.654 6.869 3.510 487.589 0.776 15.612 3.265 0.34 114535. 0.2564
|
|
57.80 0.7267 0.7972 0.0743 0.0677 0.633 6.649 3.274 471.978 0.751 14.561 3.146 0.34 115088. 0.2386
|
|
61.02 0.7670 0.8106 0.0684 0.0647 0.605 6.358 3.015 451.320 0.718 13.413 3.030 0.34 115668. 0.2206
|
|
64.23 0.8074 0.8213 0.0622 0.0611 0.571 6.001 2.740 425.993 0.678 12.185 2.917 0.34 116273. 0.2023
|
|
67.44 0.8478 0.8286 0.0556 0.0569 0.532 5.585 2.450 396.475 0.631 10.897 2.803 0.35 116903. 0.1839
|
|
70.65 0.8882 0.8315 0.0488 0.0521 0.487 5.117 2.150 363.213 0.578 9.562 2.685 0.35 117558. 0.1650
|
|
73.86 0.9285 0.8286 0.0418 0.0469 0.438 4.601 1.843 326.611 0.520 8.196 2.559 0.35 118237. 0.1456
|
|
77.07 0.9689 0.8173 0.0347 0.0412 0.385 4.044 1.531 287.053 0.457 6.809 2.419 0.35 118940. 0.1254
|
|
80.28 1.0093 0.7933 0.0276 0.0351 0.328 3.450 1.217 244.926 0.390 5.414 2.254 0.35 119665. 0.1042
|
|
83.49 1.0496 0.7482 0.0205 0.0288 0.269 2.827 0.904 200.648 0.319 4.022 2.044 0.35 120414. 0.0815
|
|
86.71 1.0900 0.6630 0.0135 0.0222 0.207 2.179 0.595 154.687 0.246 2.646 1.744 0.35 121186. 0.0564
|
|
89.92 1.1304 0.4854 0.0066 0.0154 0.144 1.515 0.292 107.577 0.171 1.299 1.231 0.35 121979. 0.0279
|
|
93.13 1.1708 -0.0030 0.0000 0.0086 0.080 0.844 -0.001 59.916 0.095 -0.004 -0.007 0.36 122794. 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 0.1094 0.0526 0.781 7.029 6.563 582.092 0.794 29.193 5.114 0.39 127480. 0.5491
|
|
3.75 0.0404 0.0820 0.1091 0.0537 0.797 7.180 6.545 594.597 0.811 29.111 4.993 0.39 127615. 0.5353
|
|
7.50 0.0808 0.1598 0.1088 0.0550 0.816 7.350 6.526 608.695 0.830 29.026 4.863 0.39 127772. 0.5206
|
|
11.24 0.1212 0.2329 0.1084 0.0564 0.837 7.539 6.504 624.364 0.852 28.932 4.725 0.39 127953. 0.5051
|
|
14.99 0.1616 0.3011 0.1080 0.0580 0.860 7.746 6.480 641.525 0.875 28.825 4.582 0.39 128159. 0.4888
|
|
18.74 0.2019 0.3643 0.1076 0.0596 0.885 7.969 6.452 660.010 0.900 28.697 4.434 0.39 128392. 0.4720
|
|
22.49 0.2423 0.4222 0.1070 0.0614 0.911 8.205 6.417 679.553 0.927 28.541 4.283 0.39 128653. 0.4547
|
|
26.24 0.2827 0.4751 0.1062 0.0632 0.938 8.449 6.373 699.771 0.955 28.347 4.131 0.39 128944. 0.4370
|
|
29.99 0.3231 0.5231 0.1053 0.0651 0.966 8.696 6.318 720.161 0.982 28.102 3.979 0.39 129266. 0.4192
|
|
33.73 0.3635 0.5663 0.1042 0.0669 0.992 8.936 6.248 740.090 1.010 27.793 3.829 0.39 129620. 0.4012
|
|
37.48 0.4039 0.6052 0.1027 0.0685 1.018 9.162 6.162 758.805 1.035 27.407 3.683 0.39 130006. 0.3832
|
|
41.23 0.4443 0.6401 0.1009 0.0701 1.040 9.363 6.054 775.441 1.058 26.928 3.541 0.39 130424. 0.3652
|
|
44.98 0.4847 0.6713 0.0987 0.0713 1.058 9.527 5.923 789.042 1.076 26.343 3.404 0.39 130876. 0.3472
|
|
48.73 0.5250 0.6993 0.0961 0.0721 1.071 9.643 5.764 798.586 1.089 25.638 3.274 0.39 131360. 0.3294
|
|
52.47 0.5654 0.7244 0.0929 0.0725 1.077 9.696 5.575 803.020 1.095 24.799 3.149 0.39 131878. 0.3116
|
|
56.22 0.6058 0.7470 0.0893 0.0724 1.075 9.675 5.354 801.301 1.093 23.815 3.031 0.40 132429. 0.2939
|
|
59.97 0.6462 0.7673 0.0850 0.0716 1.063 9.569 5.099 792.495 1.081 22.681 2.918 0.40 133012. 0.2762
|
|
63.72 0.6866 0.7854 0.0802 0.0701 1.040 9.368 4.810 775.883 1.058 21.393 2.812 0.40 133627. 0.2584
|
|
67.47 0.7270 0.8014 0.0748 0.0678 1.007 9.069 4.487 751.057 1.025 19.957 2.710 0.40 134273. 0.2405
|
|
71.21 0.7674 0.8152 0.0689 0.0649 0.963 8.671 4.134 718.078 0.980 18.386 2.611 0.40 134950. 0.2225
|
|
74.96 0.8078 0.8263 0.0626 0.0612 0.909 8.181 3.756 677.543 0.924 16.706 2.514 0.40 135657. 0.2042
|
|
78.71 0.8482 0.8342 0.0560 0.0569 0.845 7.610 3.359 630.217 0.860 14.940 2.417 0.40 136393. 0.1857
|
|
82.46 0.8885 0.8379 0.0491 0.0521 0.774 6.965 2.948 576.817 0.787 13.111 2.318 0.40 137158. 0.1668
|
|
86.21 0.9289 0.8360 0.0421 0.0468 0.695 6.255 2.526 517.994 0.707 11.237 2.212 0.41 137951. 0.1474
|
|
89.96 0.9693 0.8262 0.0350 0.0410 0.609 5.486 2.099 454.367 0.620 9.335 2.095 0.41 138771. 0.1272
|
|
93.70 1.0097 0.8042 0.0278 0.0349 0.518 4.668 1.668 386.563 0.527 7.421 1.958 0.41 139619. 0.1060
|
|
97.45 1.0501 0.7617 0.0207 0.0285 0.423 3.807 1.239 315.261 0.430 5.512 1.783 0.41 140493. 0.0832
|
|
101.20 1.0905 0.6798 0.0136 0.0218 0.323 2.913 0.815 241.223 0.329 3.624 1.532 0.41 141394. 0.0580
|
|
104.95 1.1309 0.5044 0.0067 0.0149 0.222 1.996 0.400 165.321 0.226 1.777 1.096 0.41 142320. 0.0290
|
|
108.70 1.1713 -0.0051 0.0000 0.0080 0.119 1.069 -0.002 88.534 0.121 -0.009 -0.011 0.41 143272. 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 0.1096 0.0525 1.164 9.167 8.586 867.687 1.036 38.193 4.488 0.44 145688. 0.5512
|
|
4.28 0.0404 0.0823 0.1093 0.0536 1.189 9.365 8.564 886.357 1.058 38.093 4.382 0.44 145843. 0.5375
|
|
8.57 0.0808 0.1604 0.1090 0.0549 1.217 9.587 8.540 907.444 1.083 37.988 4.269 0.44 146023. 0.5229
|
|
12.85 0.1212 0.2338 0.1087 0.0563 1.248 9.836 8.515 930.926 1.111 37.874 4.149 0.44 146229. 0.5074
|
|
17.14 0.1616 0.3022 0.1083 0.0579 1.283 10.108 8.486 956.693 1.142 37.744 4.023 0.44 146465. 0.4912
|
|
21.42 0.2020 0.3656 0.1079 0.0596 1.320 10.402 8.451 984.506 1.175 37.588 3.893 0.45 146731. 0.4743
|
|
25.71 0.2424 0.4238 0.1073 0.0614 1.360 10.713 8.408 1013.977 1.210 37.397 3.761 0.45 147029. 0.4570
|
|
29.99 0.2828 0.4769 0.1066 0.0632 1.401 11.036 8.353 1044.542 1.247 37.156 3.627 0.45 147362. 0.4394
|
|
34.27 0.3232 0.5250 0.1057 0.0651 1.442 11.362 8.285 1075.447 1.284 36.850 3.494 0.45 147730. 0.4215
|
|
38.56 0.3636 0.5684 0.1046 0.0669 1.483 11.683 8.197 1105.744 1.320 36.461 3.362 0.45 148134. 0.4035
|
|
42.84 0.4040 0.6074 0.1032 0.0686 1.521 11.984 8.087 1134.289 1.354 35.972 3.234 0.45 148575. 0.3854
|
|
47.13 0.4443 0.6424 0.1015 0.0702 1.555 12.253 7.950 1159.772 1.384 35.361 3.109 0.45 149053. 0.3674
|
|
51.41 0.4847 0.6737 0.0993 0.0715 1.583 12.475 7.781 1180.737 1.409 34.609 2.989 0.45 149570. 0.3494
|
|
55.70 0.5251 0.7018 0.0967 0.0724 1.603 12.632 7.576 1195.625 1.427 33.698 2.874 0.45 150124. 0.3315
|
|
59.98 0.5655 0.7270 0.0936 0.0728 1.613 12.708 7.331 1202.824 1.436 32.610 2.765 0.45 150716. 0.3137
|
|
64.27 0.6059 0.7496 0.0899 0.0727 1.610 12.686 7.044 1200.744 1.433 31.331 2.661 0.45 151346. 0.2960
|
|
68.55 0.6463 0.7700 0.0857 0.0719 1.593 12.551 6.711 1187.947 1.418 29.851 2.562 0.45 152013. 0.2782
|
|
72.83 0.6867 0.7883 0.0808 0.0704 1.560 12.291 6.332 1163.324 1.389 28.167 2.469 0.45 152716. 0.2604
|
|
77.12 0.7271 0.8046 0.0754 0.0682 1.510 11.899 5.909 1126.236 1.344 26.284 2.380 0.46 153455. 0.2425
|
|
81.40 0.7675 0.8186 0.0695 0.0652 1.444 11.376 5.446 1076.749 1.285 24.222 2.294 0.46 154230. 0.2244
|
|
85.69 0.8079 0.8302 0.0632 0.0615 1.362 10.732 4.949 1015.746 1.212 22.014 2.210 0.46 155038. 0.2061
|
|
89.97 0.8483 0.8386 0.0565 0.0572 1.266 9.978 4.427 944.380 1.127 19.691 2.126 0.46 155880. 0.1875
|
|
94.26 0.8887 0.8431 0.0496 0.0523 1.158 9.126 3.886 863.738 1.031 17.283 2.040 0.46 156754. 0.1686
|
|
98.54 0.9291 0.8423 0.0425 0.0469 1.039 8.186 3.331 774.807 0.925 14.814 1.950 0.46 157661. 0.1491
|
|
102.82 0.9695 0.8338 0.0353 0.0411 0.910 7.169 2.767 678.528 0.810 12.307 1.850 0.46 158599. 0.1289
|
|
107.11 1.0099 0.8135 0.0281 0.0348 0.772 6.084 2.200 575.859 0.687 9.784 1.733 0.47 159568. 0.1077
|
|
111.39 1.0503 0.7734 0.0208 0.0283 0.627 4.943 1.634 467.834 0.558 7.266 1.584 0.47 160568. 0.0848
|
|
115.68 1.0907 0.6946 0.0137 0.0215 0.477 3.757 1.074 355.622 0.424 4.777 1.370 0.47 161598. 0.0595
|
|
119.96 1.1311 0.5219 0.0067 0.0146 0.323 2.542 0.526 240.559 0.287 2.341 0.992 0.47 162657. 0.0302
|
|
124.25 1.1715 -0.0066 0.0000 0.0075 0.166 1.312 -0.003 124.156 0.148 -0.015 -0.012 0.47 163745. 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 0.1098 0.0526 1.658 11.611 10.887 1236.368 1.312 48.424 3.994 0.50 163896. 0.5523
|
|
4.82 0.0404 0.0824 0.1095 0.0537 1.694 11.861 10.860 1262.924 1.340 48.306 3.900 0.50 164070. 0.5387
|
|
9.64 0.0808 0.1606 0.1092 0.0550 1.734 12.143 10.833 1292.977 1.372 48.184 3.800 0.50 164272. 0.5242
|
|
14.46 0.1212 0.2341 0.1089 0.0564 1.779 12.458 10.803 1326.517 1.407 48.051 3.694 0.50 164504. 0.5088
|
|
19.28 0.1616 0.3028 0.1086 0.0579 1.828 12.804 10.769 1363.405 1.447 47.900 3.583 0.50 164769. 0.4927
|
|
24.10 0.2020 0.3663 0.1082 0.0596 1.882 13.179 10.728 1403.321 1.489 47.719 3.468 0.50 165068. 0.4760
|
|
28.92 0.2424 0.4247 0.1077 0.0614 1.939 13.577 10.678 1445.725 1.534 47.495 3.350 0.50 165404. 0.4588
|
|
33.74 0.2828 0.4779 0.1070 0.0633 1.998 13.992 10.614 1489.827 1.581 47.210 3.231 0.50 165778. 0.4412
|
|
38.56 0.3231 0.5262 0.1062 0.0652 2.058 14.412 10.531 1534.559 1.628 46.844 3.113 0.50 166191. 0.4234
|
|
43.38 0.3635 0.5697 0.1051 0.0671 2.117 14.825 10.426 1578.558 1.675 46.375 2.996 0.50 166646. 0.4054
|
|
48.20 0.4039 0.6088 0.1038 0.0689 2.173 15.216 10.292 1620.179 1.719 45.777 2.881 0.50 167142. 0.3874
|
|
53.02 0.4443 0.6438 0.1021 0.0705 2.223 15.566 10.123 1657.515 1.759 45.026 2.770 0.50 167680. 0.3694
|
|
57.84 0.4847 0.6752 0.1000 0.0718 2.264 15.857 9.913 1688.447 1.791 44.095 2.663 0.51 168261. 0.3514
|
|
62.66 0.5251 0.7034 0.0974 0.0727 2.294 16.066 9.658 1710.702 1.815 42.959 2.561 0.51 168885. 0.3335
|
|
67.47 0.5655 0.7287 0.0943 0.0732 2.309 16.171 9.352 1721.925 1.827 41.596 2.463 0.51 169551. 0.3157
|
|
72.29 0.6059 0.7514 0.0907 0.0731 2.306 16.151 8.990 1719.788 1.825 39.987 2.371 0.51 170259. 0.2979
|
|
77.11 0.6463 0.7720 0.0864 0.0723 2.283 15.986 8.570 1702.178 1.806 38.118 2.284 0.51 171010. 0.2802
|
|
81.93 0.6867 0.7905 0.0816 0.0709 2.236 15.660 8.090 1667.455 1.769 35.985 2.201 0.51 171802. 0.2623
|
|
86.75 0.7271 0.8069 0.0762 0.0686 2.165 15.164 7.553 1614.657 1.713 33.595 2.122 0.51 172633. 0.2444
|
|
91.57 0.7675 0.8213 0.0702 0.0656 2.070 14.499 6.963 1543.835 1.638 30.973 2.046 0.51 173505. 0.2263
|
|
96.39 0.8079 0.8332 0.0638 0.0619 1.953 13.676 6.331 1456.235 1.545 28.158 1.972 0.52 174415. 0.2079
|
|
101.21 0.8483 0.8422 0.0571 0.0575 1.815 12.711 5.664 1353.515 1.436 25.195 1.898 0.52 175362. 0.1893
|
|
106.03 0.8886 0.8474 0.0501 0.0526 1.659 11.620 4.973 1237.252 1.313 22.120 1.823 0.52 176346. 0.1704
|
|
110.85 0.9290 0.8475 0.0430 0.0471 1.487 10.414 4.264 1108.881 1.177 18.965 1.744 0.52 177366. 0.1509
|
|
115.67 0.9694 0.8403 0.0357 0.0412 1.300 9.107 3.543 969.768 1.029 15.759 1.657 0.52 178422. 0.1307
|
|
120.49 1.0098 0.8217 0.0284 0.0349 1.101 7.713 2.817 821.307 0.871 12.530 1.556 0.52 179512. 0.1094
|
|
125.31 1.0502 0.7840 0.0211 0.0283 0.892 6.245 2.092 665.009 0.706 9.306 1.427 0.53 180637. 0.0865
|
|
130.13 1.0906 0.7082 0.0139 0.0214 0.674 4.720 1.376 502.579 0.533 6.119 1.241 0.53 181796. 0.0610
|
|
134.95 1.1310 0.5385 0.0068 0.0143 0.451 3.155 0.674 335.978 0.356 2.999 0.910 0.53 182987. 0.0313
|
|
139.77 1.1714 -0.0067 0.0000 0.0071 0.225 1.572 -0.004 167.430 0.178 -0.018 -0.011 0.53 184211. 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 0.1100 0.0527 2.280 14.373 13.466 1700.524 1.624 59.896 3.592 0.56 182103. 0.5524
|
|
5.40 0.0407 0.0830 0.1097 0.0538 2.330 14.683 13.435 1737.183 1.659 59.761 3.508 0.56 182298. 0.5389
|
|
10.80 0.0814 0.1618 0.1095 0.0551 2.385 15.035 13.404 1778.807 1.699 59.623 3.418 0.56 182524. 0.5245
|
|
16.19 0.1222 0.2359 0.1092 0.0566 2.448 15.429 13.371 1825.407 1.743 59.474 3.322 0.56 182784. 0.5092
|
|
21.59 0.1629 0.3050 0.1089 0.0582 2.517 15.863 13.333 1876.816 1.792 59.305 3.222 0.56 183081. 0.4931
|
|
26.99 0.2036 0.3690 0.1085 0.0599 2.592 16.335 13.287 1932.608 1.846 59.100 3.118 0.56 183418. 0.4764
|
|
32.39 0.2443 0.4277 0.1081 0.0617 2.671 16.837 13.229 1992.043 1.902 58.844 3.012 0.56 183795. 0.4592
|
|
37.79 0.2850 0.4812 0.1075 0.0636 2.754 17.361 13.155 2054.014 1.961 58.513 2.905 0.56 184216. 0.4416
|
|
43.19 0.3257 0.5297 0.1067 0.0656 2.839 17.893 13.058 2117.003 2.022 58.082 2.798 0.56 184682. 0.4237
|
|
48.58 0.3665 0.5733 0.1056 0.0675 2.922 18.418 12.932 2179.061 2.081 57.520 2.692 0.56 185194. 0.4057
|
|
53.98 0.4072 0.6125 0.1043 0.0693 3.001 18.915 12.769 2237.809 2.137 56.796 2.588 0.56 185753. 0.3876
|
|
59.38 0.4479 0.6476 0.1026 0.0710 3.072 19.360 12.562 2290.482 2.187 55.876 2.488 0.56 186360. 0.3695
|
|
64.78 0.4886 0.6790 0.1005 0.0723 3.130 19.728 12.303 2333.999 2.229 54.725 2.391 0.56 187015. 0.3515
|
|
70.18 0.5293 0.7071 0.0979 0.0733 3.172 19.990 11.985 2365.057 2.258 53.310 2.299 0.56 187719. 0.3335
|
|
75.57 0.5700 0.7324 0.0948 0.0738 3.192 20.118 11.601 2380.243 2.273 51.603 2.211 0.56 188470. 0.3156
|
|
80.97 0.6108 0.7552 0.0910 0.0736 3.187 20.084 11.146 2376.198 2.269 49.577 2.128 0.57 189270. 0.2977
|
|
86.37 0.6515 0.7758 0.0867 0.0728 3.151 19.862 10.615 2349.901 2.244 47.216 2.049 0.57 190117. 0.2798
|
|
91.77 0.6922 0.7944 0.0817 0.0712 3.083 19.432 10.008 2299.056 2.195 44.516 1.974 0.57 191010. 0.2618
|
|
97.17 0.7329 0.8109 0.0762 0.0689 2.980 18.784 9.327 2222.383 2.122 41.488 1.904 0.57 191948. 0.2437
|
|
102.57 0.7736 0.8254 0.0701 0.0657 2.843 17.920 8.580 2120.146 2.025 38.165 1.836 0.57 192931. 0.2254
|
|
107.96 0.8144 0.8374 0.0635 0.0618 2.674 16.856 7.779 1994.254 1.904 34.601 1.769 0.57 193958. 0.2068
|
|
113.36 0.8551 0.8465 0.0567 0.0572 2.477 15.612 6.936 1847.078 1.764 30.851 1.703 0.58 195026. 0.1880
|
|
118.76 0.8958 0.8516 0.0495 0.0521 2.254 14.207 6.062 1680.853 1.605 26.963 1.636 0.58 196136. 0.1688
|
|
124.16 0.9365 0.8515 0.0422 0.0464 2.008 12.658 5.165 1497.613 1.430 22.975 1.564 0.58 197286. 0.1490
|
|
129.56 0.9772 0.8437 0.0348 0.0403 1.742 10.982 4.255 1299.323 1.241 18.927 1.485 0.58 198477. 0.1284
|
|
134.95 1.0179 0.8236 0.0273 0.0337 1.459 9.196 3.339 1088.015 1.039 14.854 1.392 0.58 199706. 0.1066
|
|
140.35 1.0587 0.7820 0.0198 0.0268 1.161 7.319 2.426 865.915 0.827 10.793 1.271 0.59 200973. 0.0830
|
|
145.75 1.0994 0.6955 0.0125 0.0197 0.852 5.372 1.525 635.566 0.607 6.784 1.088 0.59 202279. 0.0563
|
|
151.15 1.1401 0.4850 0.0053 0.0124 0.536 3.380 0.645 399.907 0.382 2.871 0.732 0.59 203622. 0.0246
|
|
156.55 1.1808
|
|
|
|
|
|
|
|
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 0.1102 0.0529 3.049 17.472 16.326 2273.882 1.974 72.620 3.257 0.61 200308. 0.5515
|
|
5.89 0.0404 0.0821 0.1100 0.0541 3.114 17.842 16.293 2322.008 2.016 72.473 3.183 0.61 200520. 0.5384
|
|
11.77 0.0807 0.1602 0.1098 0.0553 3.187 18.263 16.260 2376.757 2.063 72.325 3.103 0.61 200766. 0.5244
|
|
17.66 0.1211 0.2337 0.1095 0.0568 3.270 18.735 16.225 2438.192 2.117 72.169 3.018 0.61 201049. 0.5096
|
|
23.55 0.1615 0.3024 0.1093 0.0583 3.361 19.257 16.185 2506.154 2.176 71.992 2.929 0.61 201372. 0.4939
|
|
29.44 0.2018 0.3661 0.1089 0.0601 3.460 19.826 16.137 2580.156 2.240 71.779 2.837 0.61 201736. 0.4776
|
|
35.32 0.2422 0.4246 0.1085 0.0619 3.566 20.434 16.077 2659.301 2.309 71.510 2.742 0.61 202146. 0.4608
|
|
41.21 0.2826 0.4781 0.1080 0.0638 3.677 21.071 15.998 2742.217 2.381 71.158 2.646 0.61 202602. 0.4436
|
|
47.10 0.3230 0.5265 0.1073 0.0658 3.791 21.722 15.893 2826.983 2.454 70.692 2.550 0.61 203106. 0.4261
|
|
52.98 0.3633 0.5702 0.1064 0.0678 3.904 22.368 15.755 2911.089 2.527 70.077 2.455 0.61 203661. 0.4084
|
|
58.87 0.4037 0.6095 0.1051 0.0696 4.012 22.986 15.574 2991.438 2.597 69.274 2.361 0.62 204266. 0.3906
|
|
64.76 0.4441 0.6447 0.1036 0.0713 4.109 23.546 15.342 3064.393 2.660 68.239 2.271 0.62 204923. 0.3728
|
|
70.65 0.4844 0.6762 0.1016 0.0728 4.192 24.019 15.047 3125.861 2.714 66.931 2.183 0.62 205632. 0.3550
|
|
76.53 0.5248 0.7046 0.0991 0.0738 4.253 24.369 14.683 3171.434 2.753 65.309 2.100 0.62 206394. 0.3372
|
|
82.42 0.5652 0.7300 0.0961 0.0744 4.287 24.562 14.239 3196.527 2.775 63.334 2.020 0.62 207208. 0.3195
|
|
88.31 0.6055 0.7530 0.0925 0.0744 4.287 24.562 13.709 3196.599 2.775 60.976 1.945 0.62 208074. 0.3018
|
|
94.20 0.6459 0.7739 0.0883 0.0737 4.248 24.338 13.087 3167.480 2.750 58.210 1.874 0.62 208991. 0.2841
|
|
100.08 0.6863 0.7927 0.0835 0.0723 4.165 23.865 12.372 3105.885 2.696 55.029 1.807 0.63 209959. 0.2663
|
|
105.97 0.7267 0.8097 0.0781 0.0701 4.036 23.127 11.565 3009.816 2.613 51.441 1.743 0.63 210976. 0.2484
|
|
111.86 0.7670 0.8246 0.0721 0.0670 3.861 22.123 10.675 2879.157 2.499 47.481 1.682 0.63 212041. 0.2303
|
|
117.74 0.8074 0.8374 0.0656 0.0632 3.642 20.870 9.715 2716.125 2.358 43.211 1.622 0.63 213153. 0.2119
|
|
123.63 0.8478 0.8475 0.0587 0.0588 3.385 19.393 8.700 2523.836 2.191 38.699 1.564 0.63 214312. 0.1933
|
|
129.52 0.8881 0.8540 0.0516 0.0537 3.091 17.714 7.645 2305.309 2.001 34.004 1.504 0.63 215514. 0.1743
|
|
135.41 0.9285 0.8559 0.0443 0.0480 2.767 15.854 6.559 2063.303 1.791 29.175 1.442 0.64 216761. 0.1548
|
|
141.29 0.9689 0.8511 0.0368 0.0419 2.414 13.834 5.454 1800.437 1.563 24.259 1.374 0.64 218051. 0.1345
|
|
147.18 1.0092 0.8357 0.0293 0.0354 2.038 11.675 4.339 1519.392 1.319 19.299 1.295 0.64 219383. 0.1131
|
|
153.07 1.0496 0.8023 0.0218 0.0285 1.640 9.398 3.224 1223.074 1.062 14.341 1.196 0.64 220757. 0.0900
|
|
158.95 1.0900 0.7327 0.0143 0.0213 1.227 7.029 2.121 914.788 0.794 9.432 1.051 0.65 222172. 0.0642
|
|
164.84 1.1303 0.5695 0.0070 0.0139 0.802 4.598 1.040 598.367 0.519 4.624 0.788 0.65 223627. 0.0337
|
|
170.73 1.1707 -0.0074 0.0000 0.0065 0.373 2.138 -0.006 278.229 0.242 -0.027 -0.010 0.65 225121. 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 0.1104 0.0534 3.997 20.992 19.470 2980.265 2.372 86.601 2.963 0.67 218512. 0.5480
|
|
6.42 0.0403 0.0815 0.1102 0.0545 4.079 21.425 19.434 3041.736 2.421 86.444 2.898 0.67 218743. 0.5354
|
|
12.84 0.0807 0.1591 0.1100 0.0558 4.173 21.919 19.400 3111.905 2.476 86.291 2.828 0.67 219011. 0.5220
|
|
19.25 0.1210 0.2323 0.1098 0.0572 4.279 22.475 19.364 3190.921 2.539 86.133 2.753 0.67 219319. 0.5077
|
|
25.67 0.1614 0.3009 0.1096 0.0588 4.397 23.093 19.325 3278.656 2.609 85.957 2.673 0.67 219670. 0.4926
|
|
32.09 0.2017 0.3645 0.1093 0.0605 4.525 23.769 19.277 3374.565 2.685 85.744 2.591 0.67 220067. 0.4768
|
|
38.51 0.2420 0.4231 0.1090 0.0624 4.664 24.494 19.216 3477.583 2.767 85.471 2.506 0.67 220512. 0.4605
|
|
44.92 0.2824 0.4766 0.1085 0.0643 4.809 25.258 19.134 3586.025 2.854 85.107 2.420 0.67 221009. 0.4437
|
|
51.34 0.3227 0.5252 0.1079 0.0663 4.958 26.043 19.023 3697.484 2.942 84.615 2.334 0.67 221558. 0.4266
|
|
57.76 0.3631 0.5691 0.1071 0.0683 5.108 26.827 18.874 3808.761 3.031 83.950 2.248 0.67 222162. 0.4092
|
|
64.18 0.4034 0.6086 0.1059 0.0702 5.251 27.581 18.674 3915.843 3.116 83.064 2.163 0.67 222821. 0.3918
|
|
70.59 0.4437 0.6439 0.1044 0.0720 5.383 28.272 18.414 4013.928 3.194 81.904 2.081 0.67 223536. 0.3742
|
|
77.01 0.4841 0.6756 0.1026 0.0735 5.495 28.861 18.079 4097.555 3.261 80.416 2.001 0.67 224309. 0.3566
|
|
83.43 0.5244 0.7041 0.1002 0.0746 5.580 29.307 17.659 4160.766 3.311 78.549 1.925 0.68 225139. 0.3391
|
|
89.85 0.5647 0.7297 0.0972 0.0753 5.629 29.564 17.143 4197.321 3.340 76.254 1.853 0.68 226026. 0.3215
|
|
96.26 0.6051 0.7528 0.0937 0.0753 5.634 29.590 16.522 4200.982 3.343 73.490 1.784 0.68 226970. 0.3039
|
|
102.68 0.6454 0.7738 0.0896 0.0747 5.587 29.344 15.789 4166.049 3.315 70.228 1.719 0.68 227970. 0.2863
|
|
109.10 0.6858 0.7928 0.0847 0.0733 5.482 28.794 14.940 4087.987 3.253 66.455 1.658 0.68 229025. 0.2685
|
|
115.52 0.7261 0.8101 0.0793 0.0711 5.316 27.921 13.979 3963.991 3.154 62.181 1.600 0.68 230133. 0.2507
|
|
121.93 0.7664 0.8254 0.0733 0.0680 5.087 26.721 12.915 3793.735 3.019 57.444 1.544 0.69 231295. 0.2326
|
|
128.35 0.8068 0.8386 0.0667 0.0642 4.801 25.216 11.763 3580.006 2.849 52.321 1.490 0.69 232508. 0.2142
|
|
134.77 0.8471 0.8492 0.0598 0.0597 4.462 23.433 10.543 3326.941 2.647 46.894 1.437 0.69 233770. 0.1956
|
|
141.19 0.8875 0.8565 0.0526 0.0545 4.075 21.402 9.270 3038.582 2.418 41.233 1.384 0.69 235082. 0.1766
|
|
147.60 0.9278 0.8593 0.0451 0.0487 3.646 19.149 7.959 2718.611 2.163 35.403 1.328 0.69 236441. 0.1570
|
|
154.02 0.9681 0.8557 0.0376 0.0425 3.179 16.697 6.623 2370.535 1.886 29.459 1.267 0.70 237846. 0.1367
|
|
160.44 1.0085 0.8420 0.0299 0.0358 2.679 14.073 5.273 1997.946 1.590 23.454 1.197 0.70 239298. 0.1152
|
|
166.86 1.0488 0.8108 0.0222 0.0288 2.152 11.304 3.922 1604.845 1.277 17.445 1.108 0.70 240795. 0.0920
|
|
173.27 1.0892 0.7441 0.0147 0.0214 1.604 8.423 2.583 1195.881 0.952 11.488 0.980 0.71 242337. 0.0660
|
|
179.69 1.1295 0.5843 0.0072 0.0139 1.041 5.470 1.270 776.601 0.618 5.649 0.742 0.71 243923. 0.0350
|
|
186.11 1.1698 -0.0011 0.0000 0.0063 0.474 2.490 -0.001 353.578 0.281 -0.005 -0.001 0.71 245551. 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 0.1106 0.0547 5.198 25.204 22.893 3876.515 2.848 101.828 2.679 0.72 236714. 0.5371
|
|
6.95 0.0403 0.0799 0.1105 0.0557 5.300 25.698 22.856 3952.522 2.903 101.665 2.623 0.72 236963. 0.5256
|
|
13.89 0.0806 0.1560 0.1103 0.0570 5.417 26.264 22.822 4039.585 2.967 101.512 2.562 0.72 237253. 0.5131
|
|
20.84 0.1209 0.2282 0.1101 0.0584 5.549 26.904 22.788 4137.951 3.040 101.361 2.498 0.72 237586. 0.4997
|
|
27.78 0.1612 0.2959 0.1100 0.0599 5.696 27.616 22.751 4247.521 3.120 101.196 2.429 0.72 237965. 0.4857
|
|
34.73 0.2015 0.3590 0.1097 0.0616 5.857 28.397 22.706 4367.684 3.208 100.998 2.358 0.72 238394. 0.4709
|
|
41.67 0.2418 0.4173 0.1095 0.0634 6.031 29.239 22.648 4497.153 3.303 100.739 2.284 0.72 238875. 0.4556
|
|
48.62 0.2821 0.4708 0.1091 0.0654 6.214 30.128 22.569 4633.861 3.404 100.385 2.209 0.72 239412. 0.4398
|
|
55.56 0.3224 0.5196 0.1085 0.0673 6.403 31.045 22.458 4774.813 3.507 99.891 2.133 0.73 240005. 0.4237
|
|
62.51 0.3627 0.5639 0.1078 0.0693 6.592 31.962 22.303 4915.987 3.611 99.206 2.058 0.73 240657. 0.4073
|
|
69.45 0.4030 0.6039 0.1068 0.0713 6.775 32.849 22.093 5052.313 3.711 98.268 1.983 0.73 241369. 0.3907
|
|
76.40 0.4433 0.6399 0.1054 0.0730 6.943 33.664 21.810 5177.716 3.803 97.013 1.911 0.73 242143. 0.3740
|
|
83.34 0.4836 0.6723 0.1036 0.0745 7.088 34.363 21.441 5285.264 3.882 95.372 1.840 0.73 242978. 0.3571
|
|
90.29 0.5239 0.7014 0.1014 0.0757 7.198 34.897 20.971 5367.394 3.943 93.279 1.772 0.73 243875. 0.3401
|
|
97.23 0.5642 0.7277 0.0985 0.0764 7.263 35.214 20.385 5416.158 3.978 90.673 1.707 0.73 244835. 0.3230
|
|
104.18 0.6045 0.7514 0.0951 0.0765 7.273 35.262 19.672 5423.535 3.984 87.501 1.645 0.74 245856. 0.3058
|
|
111.12 0.6447 0.7728 0.0910 0.0759 7.217 34.992 18.823 5381.932 3.953 83.724 1.586 0.74 246937. 0.2885
|
|
118.07 0.6850 0.7922 0.0862 0.0745 7.087 34.362 17.834 5285.017 3.882 79.324 1.531 0.74 248079. 0.2709
|
|
125.01 0.7253 0.8098 0.0807 0.0723 6.878 33.345 16.706 5128.567 3.767 74.310 1.478 0.74 249279. 0.2531
|
|
131.96 0.7656 0.8254 0.0747 0.0693 6.586 31.933 15.451 4911.514 3.608 68.727 1.427 0.74 250536. 0.2351
|
|
138.90 0.8059 0.8391 0.0681 0.0654 6.218 30.149 14.088 4637.055 3.406 62.663 1.378 0.75 251849. 0.2168
|
|
145.85 0.8462 0.8503 0.0611 0.0608 5.781 28.026 12.639 4310.524 3.166 56.218 1.330 0.75 253215. 0.1982
|
|
152.79 0.8865 0.8584 0.0538 0.0555 5.280 25.599 11.124 3937.288 2.892 49.480 1.281 0.75 254634. 0.1791
|
|
159.74 0.9268 0.8621 0.0462 0.0497 4.724 22.901 9.560 3522.358 2.587 42.524 1.231 0.75 256105. 0.1595
|
|
166.68 0.9671 0.8595 0.0385 0.0433 4.118 19.964 7.963 3070.615 2.256 35.419 1.176 0.76 257626. 0.1391
|
|
173.63 1.0074 0.8469 0.0307 0.0365 3.470 16.822 6.346 2587.241 1.900 28.228 1.113 0.76 259197. 0.1175
|
|
180.57 1.0477 0.8164 0.0228 0.0293 2.787 13.512 4.725 2078.192 1.527 21.018 1.031 0.76 260816. 0.0940
|
|
187.52 1.0880 0.7492 0.0151 0.0219 2.079 10.082 3.116 1550.630 1.139 13.859 0.911 0.76 262484. 0.0674
|
|
194.46 1.1283 0.5856 0.0074 0.0143 1.359 6.587 1.534 1013.191 0.744 6.825 0.687 0.77 264199. 0.0357
|
|
201.41 1.1686 -0.0003 0.0000 0.0067 0.638 3.095 0.000 475.959 0.350 -0.002 0.000 0.77 265960. 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 0.1108 0.0573 6.802 30.621 26.589 5071.952 3.460 118.269 2.378 0.78 254913. 0.5139
|
|
7.47 0.0402 0.0764 0.1107 0.0583 6.925 31.175 26.551 5163.729 3.522 118.101 2.332 0.78 255182. 0.5037
|
|
14.94 0.0805 0.1495 0.1105 0.0595 7.066 31.812 26.518 5269.263 3.594 117.951 2.283 0.78 255493. 0.4926
|
|
22.41 0.1207 0.2190 0.1104 0.0609 7.227 32.535 26.486 5388.908 3.676 117.811 2.229 0.78 255850. 0.4808
|
|
29.88 0.1610 0.2846 0.1102 0.0624 7.406 33.342 26.454 5522.593 3.767 117.665 2.173 0.78 256257. 0.4683
|
|
37.34 0.2012 0.3460 0.1101 0.0640 7.603 34.229 26.415 5669.591 3.867 117.495 2.113 0.78 256717. 0.4552
|
|
44.81 0.2414 0.4031 0.1099 0.0658 7.816 35.188 26.364 5828.346 3.975 117.269 2.052 0.78 257234. 0.4415
|
|
52.28 0.2817 0.4559 0.1096 0.0677 8.041 36.201 26.293 5996.238 4.090 116.950 1.989 0.78 257809. 0.4274
|
|
59.75 0.3219 0.5043 0.1091 0.0697 8.273 37.247 26.188 6169.429 4.208 116.486 1.925 0.78 258446. 0.4130
|
|
67.22 0.3622 0.5487 0.1085 0.0716 8.506 38.293 26.038 6342.730 4.326 115.818 1.862 0.78 259146. 0.3982
|
|
74.69 0.4024 0.5892 0.1076 0.0735 8.729 39.300 25.826 6509.582 4.440 114.872 1.799 0.78 259910. 0.3833
|
|
82.16 0.4427 0.6261 0.1064 0.0752 8.934 40.221 25.533 6662.148 4.544 113.569 1.738 0.79 260740. 0.3681
|
|
89.63 0.4829 0.6597 0.1048 0.0767 9.108 41.003 25.140 6791.569 4.632 111.823 1.679 0.79 261637. 0.3528
|
|
97.10 0.5231 0.6903 0.1026 0.0778 9.237 41.587 24.629 6888.329 4.698 109.549 1.622 0.79 262601. 0.3373
|
|
104.57 0.5634 0.7182 0.0999 0.0784 9.310 41.915 23.981 6942.634 4.736 106.670 1.567 0.79 263632. 0.3216
|
|
112.03 0.6036 0.7436 0.0966 0.0784 9.313 41.928 23.182 6944.772 4.737 103.114 1.514 0.79 264729. 0.3055
|
|
119.50 0.6439 0.7668 0.0926 0.0778 9.234 41.571 22.219 6885.661 4.697 98.831 1.464 0.79 265892. 0.2892
|
|
126.97 0.6841 0.7878 0.0879 0.0763 9.062 40.798 21.087 6757.649 4.609 93.794 1.415 0.80 267119. 0.2724
|
|
134.44 0.7243 0.8068 0.0825 0.0740 8.791 39.578 19.786 6555.521 4.471 88.007 1.369 0.80 268410. 0.2552
|
|
141.91 0.7646 0.8238 0.0764 0.0709 8.419 37.900 18.327 6277.678 4.282 81.517 1.324 0.80 269762. 0.2376
|
|
149.38 0.8048 0.8385 0.0697 0.0669 7.949 35.788 16.733 5927.752 4.043 74.429 1.280 0.80 271173. 0.2195
|
|
156.85 0.8451 0.8505 0.0626 0.0622 7.392 33.280 15.032 5512.366 3.760 66.861 1.237 0.81 272643. 0.2010
|
|
164.32 0.8853 0.8591 0.0552 0.0569 6.756 30.416 13.247 5038.074 3.436 58.922 1.193 0.81 274169. 0.1819
|
|
171.79 0.9255 0.8631 0.0475 0.0509 6.050 27.236 11.399 4511.265 3.077 50.702 1.146 0.81 275750. 0.1622
|
|
179.26 0.9658 0.8602 0.0396 0.0445 5.282 23.781 9.506 3938.955 2.687 42.284 1.095 0.81 277385. 0.1415
|
|
186.72 1.0060 0.8460 0.0316 0.0376 4.465 20.100 7.586 3329.267 2.271 33.744 1.034 0.82 279074. 0.1193
|
|
194.19 1.0463 0.8113 0.0236 0.0304 3.610 16.252 5.656 2691.909 1.836 25.157 0.953 0.82 280814. 0.0950
|
|
201.66 1.0865 0.7345 0.0156 0.0230 2.734 12.307 3.734 2038.534 1.390 16.608 0.831 0.82 282606. 0.0673
|
|
209.13 1.1268 0.5536 0.0077 0.0156 1.854 8.346 1.840 1382.347 0.943 8.185 0.604 0.83 284449. 0.0343
|
|
216.60 1.1670 -0.0016 0.0000 0.0083 0.990 4.457 -0.003 738.292 0.504 -0.012 -0.002 0.83 286341. 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 0.1109 0.0620 9.051 38.031 30.540 6749.301 4.297 135.840 2.052 0.83 273111. 0.4754
|
|
8.01 0.0403 0.0708 0.1107 0.0630 9.197 38.647 30.499 6858.546 4.366 135.659 2.017 0.83 273398. 0.4668
|
|
16.01 0.0805 0.1389 0.1106 0.0641 9.367 39.358 30.465 6984.854 4.447 135.508 1.978 0.83 273731. 0.4576
|
|
24.02 0.1208 0.2039 0.1105 0.0654 9.560 40.169 30.435 7128.727 4.538 135.377 1.936 0.83 274113. 0.4478
|
|
32.02 0.1610 0.2656 0.1104 0.0669 9.776 41.079 30.408 7290.148 4.641 135.253 1.892 0.83 274549. 0.4372
|
|
40.03 0.2013 0.3238 0.1103 0.0686 10.015 42.082 30.377 7468.261 4.754 135.115 1.845 0.83 275042. 0.4262
|
|
48.04 0.2416 0.3782 0.1101 0.0703 10.274 43.169 30.336 7661.126 4.877 134.934 1.796 0.84 275595. 0.4146
|
|
56.04 0.2818 0.4290 0.1099 0.0722 10.548 44.321 30.276 7865.462 5.007 134.667 1.746 0.84 276211. 0.4026
|
|
64.05 0.3221 0.4760 0.1096 0.0741 10.830 45.508 30.185 8076.277 5.142 134.261 1.695 0.84 276893. 0.3903
|
|
72.06 0.3623 0.5195 0.1091 0.0761 11.112 46.693 30.046 8286.507 5.275 133.645 1.645 0.84 277642. 0.3778
|
|
80.06 0.4026 0.5597 0.1083 0.0779 11.382 47.825 29.842 8487.361 5.403 132.735 1.595 0.84 278461. 0.3651
|
|
88.07 0.4429 0.5970 0.1073 0.0796 11.624 48.843 29.549 8668.059 5.518 131.434 1.546 0.84 279350. 0.3523
|
|
96.07 0.4831 0.6315 0.1058 0.0809 11.823 49.680 29.145 8816.536 5.613 129.637 1.499 0.84 280311. 0.3393
|
|
104.08 0.5234 0.6637 0.1038 0.0819 11.962 50.263 28.605 8920.123 5.679 127.234 1.454 0.84 281344. 0.3260
|
|
112.09 0.5636 0.6936 0.1013 0.0823 12.024 50.523 27.905 8966.217 5.708 124.122 1.412 0.85 282449. 0.3125
|
|
120.09 0.6039 0.7216 0.0981 0.0821 11.993 50.393 27.026 8943.105 5.693 120.210 1.371 0.85 283626. 0.2986
|
|
128.10 0.6442 0.7477 0.0942 0.0812 11.856 49.816 25.950 8840.691 5.628 115.428 1.331 0.85 284874. 0.2843
|
|
136.10 0.6844 0.7718 0.0896 0.0794 11.601 48.747 24.671 8650.947 5.507 109.737 1.294 0.85 286192. 0.2693
|
|
144.11 0.7247 0.7939 0.0842 0.0768 11.223 47.157 23.187 8368.774 5.328 103.136 1.257 0.85 287577. 0.2536
|
|
152.12 0.7649 0.8139 0.0781 0.0734 10.719 45.042 21.510 7993.413 5.089 95.676 1.221 0.86 289029. 0.2373
|
|
160.12 0.8052 0.8316 0.0714 0.0691 10.098 42.430 19.666 7530.029 4.794 87.476 1.185 0.86 290545. 0.2202
|
|
168.13 0.8455 0.8459 0.0642 0.0642 9.374 39.389 17.687 6990.227 4.450 78.673 1.148 0.86 292123. 0.2023
|
|
176.14 0.8857 0.8559 0.0566 0.0586 8.561 35.974 15.601 6384.185 4.064 69.394 1.108 0.87 293761. 0.1835
|
|
184.14 0.9260 0.8595 0.0488 0.0525 7.675 32.248 13.434 5722.927 3.643 59.755 1.065 0.87 295459. 0.1636
|
|
192.15 0.9662 0.8532 0.0407 0.0461 6.731 28.281 11.208 5018.986 3.195 49.852 1.013 0.87 297214. 0.1421
|
|
200.15 1.0065 0.8322 0.0325 0.0393 5.737 24.105 8.945 4277.885 2.723 39.787 0.948 0.87 299026. 0.1189
|
|
208.16 1.0467 0.7849 0.0242 0.0323 4.714 19.808 6.666 3515.309 2.238 29.652 0.860 0.88 300893. 0.0931
|
|
216.17 1.0870 0.6873 0.0160 0.0252 3.687 15.493 4.397 2749.428 1.750 19.556 0.725 0.88 302815. 0.0637
|
|
224.17 1.1273 0.4820 0.0078 0.0184 2.681 11.264 2.161 1999.056 1.273 9.614 0.490 0.89 304792. 0.0302
|
|
232.18 1.1675 -0.0031 0.0000 0.0118 1.721 7.233 -0.009 1283.639 0.817 -0.039 -0.003 0.89 306821. 0.0000
|
|
|
|
|
|
|