649 lines
115 KiB
Plaintext
649 lines
115 KiB
Plaintext
14x13N (14x13N.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 0.1143 0.0642 0.003 0.175 0.140 2.070 0.020 0.622 30.646 0.06 23579. 0.4804
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0.50 0.0378 0.0656 0.1137 0.0655 0.003 0.179 0.139 2.113 0.020 0.619 29.876 0.06 23602. 0.4672
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1.00 0.0755 0.1277 0.1130 0.0669 0.003 0.182 0.138 2.159 0.021 0.616 29.076 0.06 23629. 0.4533
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1.50 0.1133 0.1861 0.1123 0.0684 0.003 0.187 0.137 2.207 0.021 0.611 28.254 0.06 23660. 0.4390
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2.00 0.1511 0.2408 0.1114 0.0699 0.003 0.191 0.136 2.256 0.022 0.607 27.418 0.06 23695. 0.4244
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2.50 0.1889 0.2917 0.1103 0.0714 0.003 0.195 0.135 2.306 0.022 0.601 26.575 0.06 23734. 0.4094
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3.00 0.2266 0.3390 0.1091 0.0730 0.003 0.199 0.134 2.355 0.022 0.594 25.734 0.06 23777. 0.3942
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3.51 0.2644 0.3826 0.1077 0.0744 0.003 0.203 0.132 2.401 0.023 0.586 24.899 0.06 23826. 0.3789
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4.01 0.3022 0.4229 0.1060 0.0757 0.003 0.207 0.130 2.444 0.023 0.577 24.076 0.06 23879. 0.3635
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4.51 0.3400 0.4597 0.1040 0.0769 0.003 0.210 0.127 2.482 0.024 0.566 23.268 0.06 23937. 0.3480
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5.01 0.3777 0.4935 0.1017 0.0779 0.003 0.212 0.125 2.513 0.024 0.554 22.478 0.06 24000. 0.3325
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5.51 0.4155 0.5242 0.0991 0.0786 0.003 0.214 0.121 2.536 0.024 0.540 21.706 0.06 24069. 0.3169
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6.01 0.4533 0.5520 0.0962 0.0790 0.003 0.215 0.118 2.549 0.024 0.524 20.952 0.06 24142. 0.3013
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6.51 0.4911 0.5769 0.0928 0.0790 0.003 0.215 0.114 2.549 0.024 0.505 20.214 0.06 24221. 0.2856
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7.01 0.5288 0.5990 0.0890 0.0786 0.003 0.214 0.109 2.537 0.024 0.485 19.489 0.06 24304. 0.2697
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7.51 0.5666 0.6183 0.0848 0.0777 0.003 0.212 0.104 2.509 0.024 0.462 18.776 0.06 24393. 0.2536
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8.01 0.6044 0.6347 0.0802 0.0764 0.003 0.208 0.098 2.465 0.024 0.437 18.068 0.06 24487. 0.2373
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8.51 0.6421 0.6480 0.0752 0.0745 0.003 0.203 0.092 2.403 0.023 0.409 17.362 0.06 24585. 0.2207
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9.01 0.6799 0.6580 0.0698 0.0721 0.003 0.197 0.085 2.326 0.022 0.380 16.651 0.06 24689. 0.2039
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9.51 0.7177 0.6643 0.0641 0.0692 0.003 0.189 0.078 2.234 0.021 0.349 15.926 0.06 24797. 0.1869
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10.02 0.7555 0.6663 0.0582 0.0659 0.003 0.180 0.071 2.128 0.020 0.317 15.175 0.06 24910. 0.1697
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10.52 0.7932 0.6632 0.0520 0.0623 0.003 0.170 0.064 2.009 0.019 0.283 14.385 0.06 25027. 0.1522
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11.02 0.8310 0.6539 0.0458 0.0582 0.003 0.159 0.056 1.878 0.018 0.249 13.538 0.06 25150. 0.1344
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11.52 0.8688 0.6366 0.0394 0.0538 0.002 0.147 0.048 1.736 0.017 0.215 12.608 0.06 25276. 0.1161
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12.02 0.9066 0.6089 0.0330 0.0491 0.002 0.134 0.040 1.584 0.015 0.179 11.557 0.06 25407. 0.0973
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12.52 0.9443 0.5668 0.0264 0.0440 0.002 0.120 0.032 1.420 0.014 0.144 10.328 0.06 25543. 0.0778
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13.02 0.9821 0.5039 0.0198 0.0387 0.002 0.105 0.024 1.248 0.012 0.108 8.827 0.06 25683. 0.0576
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13.52 1.0199 0.4085 0.0132 0.0330 0.001 0.090 0.016 1.065 0.010 0.072 6.891 0.06 25827. 0.0367
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14.02 1.0577 0.2583 0.0066 0.0271 0.001 0.074 0.008 0.875 0.008 0.036 4.202 0.06 25976. 0.0159
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14.52 1.0954 0.0035 0.0001 0.0210 0.001 0.057 0.000 0.678 0.006 0.000 0.055 0.06 26128. 0.0000
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PROP RPM = 2000
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V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
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(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
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0.00 0.0000 0.0000 0.1147 0.0577 0.020 0.630 0.562 14.897 0.071 2.499 17.106 0.11 47158. 0.5374
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1.01 0.0381 0.0736 0.1142 0.0591 0.020 0.645 0.559 15.252 0.073 2.487 16.630 0.11 47205. 0.5212
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2.02 0.0761 0.1428 0.1136 0.0605 0.021 0.661 0.556 15.631 0.075 2.474 16.138 0.11 47259. 0.5044
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3.03 0.1142 0.2076 0.1128 0.0621 0.021 0.677 0.553 16.031 0.077 2.458 15.635 0.11 47321. 0.4871
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4.04 0.1523 0.2677 0.1120 0.0637 0.022 0.695 0.548 16.444 0.079 2.439 15.127 0.11 47391. 0.4695
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5.05 0.1903 0.3234 0.1110 0.0653 0.023 0.713 0.543 16.863 0.081 2.417 14.617 0.11 47470. 0.4516
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6.06 0.2284 0.3747 0.1098 0.0669 0.023 0.730 0.538 17.277 0.082 2.391 14.112 0.11 47559. 0.4337
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7.07 0.2665 0.4217 0.1083 0.0685 0.024 0.747 0.531 17.675 0.084 2.360 13.615 0.11 47657. 0.4156
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8.07 0.3045 0.4648 0.1067 0.0699 0.024 0.763 0.522 18.045 0.086 2.323 13.129 0.11 47764. 0.3977
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9.08 0.3426 0.5040 0.1047 0.0712 0.025 0.776 0.513 18.374 0.088 2.280 12.656 0.11 47882. 0.3798
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10.09 0.3807 0.5397 0.1024 0.0722 0.025 0.788 0.502 18.649 0.089 2.231 12.198 0.11 48010. 0.3621
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11.10 0.4187 0.5722 0.0998 0.0730 0.025 0.797 0.489 18.856 0.090 2.174 11.755 0.11 48149. 0.3444
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12.11 0.4568 0.6014 0.0968 0.0735 0.025 0.802 0.474 18.982 0.091 2.108 11.327 0.11 48298. 0.3268
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13.12 0.4949 0.6277 0.0934 0.0736 0.025 0.803 0.457 19.012 0.091 2.035 10.913 0.11 48457. 0.3093
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14.13 0.5329 0.6512 0.0896 0.0733 0.025 0.800 0.439 18.930 0.090 1.951 10.511 0.11 48627. 0.2918
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15.14 0.5710 0.6718 0.0853 0.0725 0.025 0.791 0.418 18.723 0.089 1.858 10.121 0.11 48807. 0.2742
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16.15 0.6091 0.6897 0.0806 0.0712 0.025 0.777 0.395 18.378 0.088 1.756 9.741 0.11 48997. 0.2565
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17.16 0.6471 0.7047 0.0755 0.0693 0.024 0.756 0.370 17.894 0.085 1.644 9.368 0.11 49197. 0.2387
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18.17 0.6852 0.7168 0.0700 0.0669 0.023 0.730 0.343 17.275 0.082 1.525 8.999 0.11 49407. 0.2208
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19.18 0.7233 0.7256 0.0642 0.0640 0.022 0.699 0.315 16.531 0.079 1.399 8.631 0.11 49626. 0.2029
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20.19 0.7613 0.7307 0.0583 0.0607 0.021 0.662 0.285 15.671 0.075 1.269 8.257 0.11 49855. 0.1848
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21.20 0.7994 0.7313 0.0521 0.0569 0.020 0.621 0.255 14.701 0.070 1.135 7.870 0.11 50094. 0.1666
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22.21 0.8375 0.7265 0.0458 0.0528 0.018 0.576 0.224 13.628 0.065 0.997 7.463 0.11 50342. 0.1481
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23.21 0.8755 0.7146 0.0394 0.0482 0.017 0.526 0.193 12.456 0.059 0.858 7.022 0.12 50599. 0.1292
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24.22 0.9136 0.6931 0.0329 0.0433 0.015 0.473 0.161 11.190 0.053 0.716 6.527 0.12 50865. 0.1098
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25.23 0.9517 0.6578 0.0263 0.0381 0.013 0.416 0.129 9.833 0.047 0.573 5.946 0.12 51140. 0.0895
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26.24 0.9897 0.6008 0.0197 0.0325 0.011 0.355 0.097 8.391 0.040 0.430 5.223 0.12 51424. 0.0680
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27.25 1.0278 0.5072 0.0131 0.0266 0.009 0.290 0.064 6.870 0.033 0.286 4.245 0.12 51716. 0.0451
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28.26 1.0659 0.3419 0.0066 0.0204 0.007 0.223 0.032 5.277 0.025 0.143 2.759 0.12 52017. 0.0207
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29.27 1.1039 0.0034 0.0000 0.0140 0.005 0.153 0.000 3.623 0.017 0.001 0.027 0.12 52326. 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 0.1150 0.0551 0.064 1.352 1.267 47.989 0.153 5.636 11.975 0.17 70736. 0.5649
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1.52 0.0382 0.0774 0.1145 0.0565 0.066 1.386 1.261 49.204 0.157 5.610 11.627 0.17 70807. 0.5473
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3.04 0.0764 0.1501 0.1139 0.0580 0.068 1.423 1.255 50.508 0.161 5.581 11.267 0.17 70888. 0.5289
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4.56 0.1146 0.2178 0.1132 0.0595 0.070 1.462 1.247 51.884 0.165 5.546 10.900 0.17 70982. 0.5101
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6.08 0.1528 0.2805 0.1123 0.0612 0.071 1.502 1.238 53.310 0.170 5.505 10.531 0.17 71088. 0.4910
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7.59 0.1910 0.3383 0.1113 0.0628 0.073 1.543 1.227 54.757 0.174 5.457 10.162 0.17 71207. 0.4717
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9.11 0.2291 0.3914 0.1102 0.0645 0.075 1.583 1.214 56.192 0.179 5.398 9.797 0.17 71340. 0.4523
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10.63 0.2673 0.4400 0.1087 0.0661 0.077 1.622 1.198 57.576 0.183 5.329 9.439 0.17 71488. 0.4330
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12.15 0.3055 0.4842 0.1071 0.0676 0.079 1.659 1.180 58.868 0.187 5.248 9.090 0.17 71650. 0.4138
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13.67 0.3437 0.5245 0.1051 0.0689 0.080 1.691 1.158 60.023 0.191 5.152 8.752 0.17 71828. 0.3948
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15.19 0.3819 0.5611 0.1028 0.0700 0.082 1.718 1.133 60.995 0.194 5.040 8.427 0.17 72021. 0.3760
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16.71 0.4201 0.5943 0.1002 0.0708 0.083 1.739 1.104 61.737 0.197 4.912 8.113 0.17 72231. 0.3573
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18.23 0.4583 0.6242 0.0972 0.0714 0.083 1.752 1.071 62.201 0.198 4.765 7.811 0.17 72455. 0.3388
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19.75 0.4965 0.6511 0.0938 0.0715 0.084 1.756 1.034 62.336 0.198 4.598 7.521 0.17 72696. 0.3205
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21.26 0.5347 0.6751 0.0900 0.0713 0.083 1.749 0.991 62.091 0.198 4.410 7.242 0.17 72952. 0.3022
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22.78 0.5729 0.6964 0.0857 0.0705 0.082 1.730 0.944 61.414 0.195 4.199 6.972 0.17 73224. 0.2839
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24.30 0.6110 0.7150 0.0809 0.0692 0.081 1.698 0.892 60.265 0.192 3.966 6.711 0.17 73510. 0.2656
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25.82 0.6492 0.7309 0.0758 0.0673 0.079 1.652 0.835 58.635 0.187 3.713 6.457 0.17 73812. 0.2472
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27.34 0.6874 0.7441 0.0702 0.0649 0.076 1.593 0.774 56.542 0.180 3.442 6.208 0.17 74129. 0.2289
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28.86 0.7256 0.7543 0.0644 0.0620 0.072 1.522 0.710 54.015 0.172 3.158 5.962 0.17 74460. 0.2106
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30.38 0.7638 0.7611 0.0584 0.0586 0.069 1.439 0.644 51.084 0.163 2.863 5.715 0.17 74806. 0.1922
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31.90 0.8020 0.7640 0.0522 0.0548 0.064 1.346 0.575 47.772 0.152 2.559 5.463 0.17 75165. 0.1737
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33.42 0.8402 0.7619 0.0459 0.0506 0.059 1.242 0.506 44.099 0.140 2.249 5.200 0.17 75539. 0.1550
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34.94 0.8784 0.7533 0.0394 0.0460 0.054 1.129 0.435 40.080 0.128 1.933 4.919 0.17 75927. 0.1359
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36.45 0.9166 0.7360 0.0329 0.0410 0.048 1.007 0.363 35.730 0.114 1.614 4.605 0.17 76329. 0.1163
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37.97 0.9548 0.7056 0.0263 0.0356 0.042 0.875 0.290 31.063 0.099 1.291 4.239 0.17 76744. 0.0957
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39.49 0.9929 0.6544 0.0197 0.0299 0.035 0.735 0.217 26.097 0.083 0.967 3.780 0.17 77172. 0.0739
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41.01 1.0311 0.5656 0.0131 0.0239 0.028 0.588 0.145 20.854 0.066 0.643 3.146 0.18 77614. 0.0501
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42.53 1.0693 0.3972 0.0065 0.0176 0.021 0.433 0.072 15.362 0.049 0.321 2.130 0.18 78068. 0.0240
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44.05 1.1075 0.0039 0.0000 0.0111 0.013 0.272 0.000 9.653 0.031 0.002 0.020 0.18 78532. 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 0.1152 0.0536 0.149 2.341 2.257 110.796 0.265 10.037 9.238 0.22 94313. 0.5816
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2.03 0.0383 0.0798 0.1147 0.0551 0.152 2.403 2.247 113.706 0.271 9.993 8.962 0.22 94408. 0.5630
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4.06 0.0766 0.1545 0.1141 0.0566 0.157 2.469 2.235 116.836 0.279 9.943 8.678 0.22 94517. 0.5438
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6.09 0.1149 0.2240 0.1134 0.0582 0.161 2.539 2.222 120.145 0.287 9.883 8.388 0.22 94642. 0.5241
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8.12 0.1531 0.2883 0.1126 0.0598 0.166 2.611 2.206 123.580 0.295 9.813 8.097 0.22 94784. 0.5040
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10.15 0.1914 0.3474 0.1117 0.0615 0.170 2.685 2.187 127.073 0.303 9.728 7.806 0.22 94943. 0.4839
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12.18 0.2297 0.4016 0.1105 0.0632 0.175 2.758 2.164 130.543 0.312 9.627 7.520 0.22 95121. 0.4636
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14.21 0.2680 0.4510 0.1091 0.0648 0.180 2.829 2.137 133.899 0.320 9.505 7.239 0.22 95319. 0.4435
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16.24 0.3063 0.4960 0.1074 0.0663 0.184 2.896 2.105 137.037 0.327 9.362 6.966 0.22 95537. 0.4236
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18.27 0.3446 0.5369 0.1055 0.0677 0.188 2.955 2.067 139.852 0.334 9.192 6.703 0.22 95775. 0.4038
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20.30 0.3829 0.5740 0.1032 0.0689 0.191 3.005 2.022 142.231 0.340 8.995 6.449 0.22 96034. 0.3844
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22.33 0.4211 0.6076 0.1006 0.0697 0.193 3.044 1.971 144.059 0.344 8.767 6.205 0.22 96314. 0.3651
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24.36 0.4594 0.6379 0.0976 0.0703 0.195 3.069 1.912 145.221 0.347 8.505 5.972 0.22 96615. 0.3461
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26.39 0.4977 0.6651 0.0942 0.0705 0.195 3.076 1.845 145.594 0.348 8.207 5.748 0.22 96937. 0.3273
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28.42 0.5360 0.6895 0.0903 0.0702 0.195 3.065 1.770 145.052 0.346 7.871 5.533 0.23 97281. 0.3085
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30.45 0.5743 0.7112 0.0860 0.0695 0.192 3.032 1.685 143.468 0.343 7.495 5.327 0.23 97644. 0.2898
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32.48 0.6126 0.7303 0.0812 0.0681 0.189 2.974 1.591 140.750 0.336 7.078 5.128 0.23 98028. 0.2711
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34.51 0.6509 0.7468 0.0760 0.0663 0.184 2.892 1.489 136.873 0.327 6.625 4.936 0.23 98433. 0.2524
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36.55 0.6891 0.7607 0.0705 0.0638 0.177 2.787 1.381 131.880 0.315 6.141 4.748 0.23 98857. 0.2338
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38.58 0.7274 0.7718 0.0646 0.0609 0.169 2.659 1.266 125.839 0.300 5.632 4.564 0.23 99301. 0.2152
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40.61 0.7657 0.7798 0.0586 0.0575 0.159 2.511 1.148 118.819 0.284 5.104 4.380 0.23 99764. 0.1967
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42.64 0.8040 0.7840 0.0523 0.0537 0.149 2.343 1.025 110.876 0.265 4.561 4.195 0.23 100246. 0.1780
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44.67 0.8423 0.7838 0.0460 0.0494 0.137 2.156 0.901 102.055 0.244 4.006 4.003 0.23 100747. 0.1592
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46.70 0.8806 0.7775 0.0395 0.0447 0.124 1.952 0.774 92.394 0.221 3.441 3.798 0.23 101266. 0.1400
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48.73 0.9189 0.7631 0.0329 0.0397 0.110 1.731 0.645 81.927 0.196 2.870 3.572 0.23 101804. 0.1203
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50.76 0.9571 0.7363 0.0263 0.0342 0.095 1.494 0.516 70.692 0.169 2.294 3.309 0.23 102360. 0.0996
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52.79 0.9954 0.6892 0.0197 0.0284 0.079 1.241 0.386 58.729 0.140 1.715 2.978 0.23 102934. 0.0775
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54.82 1.0337 0.6045 0.0130 0.0223 0.062 0.974 0.256 46.095 0.110 1.137 2.515 0.23 103525. 0.0533
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56.85 1.0720 0.4346 0.0064 0.0159 0.044 0.694 0.126 32.856 0.078 0.562 1.744 0.23 104133. 0.0260
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58.88 1.1103 -0.0098 -0.0001 0.0092 0.026 0.403 -0.002 19.092 0.046 -0.007 -0.038 0.24 104754. 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 0.1154 0.0528 0.286 3.599 3.532 212.903 0.407 15.711 7.525 0.28 117890. 0.5927
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2.54 0.0383 0.0813 0.1149 0.0542 0.293 3.696 3.517 218.631 0.418 15.646 7.297 0.28 118008. 0.5736
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5.08 0.0766 0.1573 0.1144 0.0557 0.301 3.800 3.500 224.802 0.429 15.570 7.063 0.28 118145. 0.5538
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7.62 0.1150 0.2280 0.1137 0.0573 0.310 3.911 3.480 231.337 0.442 15.480 6.824 0.28 118301. 0.5335
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10.16 0.1533 0.2932 0.1129 0.0590 0.319 4.026 3.456 238.134 0.455 15.373 6.583 0.28 118478. 0.5129
|
|
12.70 0.1916 0.3532 0.1120 0.0607 0.329 4.143 3.427 245.060 0.468 15.245 6.344 0.28 118678. 0.4922
|
|
15.24 0.2299 0.4081 0.1108 0.0625 0.338 4.259 3.393 251.955 0.481 15.090 6.107 0.28 118900. 0.4715
|
|
17.78 0.2682 0.4581 0.1095 0.0641 0.347 4.372 3.351 258.635 0.494 14.905 5.876 0.28 119148. 0.4508
|
|
20.32 0.3066 0.5035 0.1079 0.0657 0.355 4.478 3.301 264.900 0.506 14.684 5.652 0.28 119420. 0.4304
|
|
22.86 0.3449 0.5448 0.1059 0.0671 0.363 4.573 3.242 270.535 0.517 14.422 5.436 0.28 119719. 0.4103
|
|
25.40 0.3832 0.5822 0.1037 0.0682 0.369 4.654 3.174 275.316 0.526 14.116 5.228 0.28 120043. 0.3904
|
|
27.94 0.4215 0.6161 0.1011 0.0692 0.374 4.717 3.094 279.017 0.533 13.762 5.029 0.28 120394. 0.3708
|
|
30.48 0.4598 0.6466 0.0981 0.0698 0.377 4.757 3.002 281.405 0.537 13.354 4.839 0.28 120771. 0.3514
|
|
33.02 0.4982 0.6742 0.0947 0.0700 0.378 4.771 2.898 282.239 0.539 12.890 4.657 0.28 121175. 0.3323
|
|
35.56 0.5365 0.6988 0.0908 0.0697 0.377 4.755 2.780 281.266 0.537 12.364 4.483 0.28 121604. 0.3132
|
|
38.10 0.5748 0.7208 0.0865 0.0690 0.373 4.703 2.647 278.237 0.531 11.775 4.315 0.28 122060. 0.2943
|
|
40.64 0.6131 0.7403 0.0817 0.0677 0.366 4.614 2.501 272.964 0.521 11.122 4.155 0.28 122541. 0.2754
|
|
43.18 0.6514 0.7573 0.0765 0.0658 0.356 4.486 2.341 265.399 0.507 10.411 4.000 0.28 123047. 0.2565
|
|
45.72 0.6897 0.7718 0.0709 0.0634 0.343 4.321 2.170 255.619 0.488 9.652 3.850 0.28 123579. 0.2377
|
|
48.26 0.7281 0.7836 0.0650 0.0604 0.327 4.121 1.990 243.760 0.466 8.853 3.704 0.29 124134. 0.2190
|
|
50.80 0.7664 0.7925 0.0589 0.0570 0.308 3.887 1.804 229.953 0.439 8.024 3.558 0.29 124714. 0.2003
|
|
53.34 0.8047 0.7979 0.0527 0.0531 0.287 3.623 1.612 214.311 0.409 7.171 3.412 0.29 125318. 0.1816
|
|
55.88 0.8430 0.7991 0.0463 0.0488 0.264 3.329 1.416 196.923 0.376 6.299 3.262 0.29 125945. 0.1627
|
|
58.42 0.8813 0.7948 0.0398 0.0441 0.239 3.007 1.217 177.862 0.340 5.412 3.103 0.29 126596. 0.1435
|
|
60.96 0.9197 0.7828 0.0332 0.0390 0.211 2.657 1.015 157.196 0.300 4.515 2.929 0.29 127269. 0.1237
|
|
63.50 0.9580 0.7592 0.0265 0.0335 0.181 2.282 0.812 134.998 0.258 3.610 2.727 0.29 127965. 0.1030
|
|
66.04 0.9963 0.7163 0.0198 0.0276 0.149 1.882 0.607 111.352 0.213 2.702 2.474 0.29 128684. 0.0808
|
|
68.58 1.0346 0.6367 0.0132 0.0214 0.116 1.460 0.403 86.368 0.165 1.794 2.118 0.29 129424. 0.0564
|
|
71.12 1.0729 0.4705 0.0065 0.0149 0.081 1.017 0.200 60.182 0.115 0.891 1.509 0.29 130186. 0.0283
|
|
73.66 1.1113 -0.0025 0.0000 0.0082 0.044 0.557 -0.001 32.949 0.063 -0.002 -0.008 0.29 130961. 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 0.1156 0.0522 0.488 5.130 5.096 364.155 0.580 22.666 6.347 0.33 141466. 0.6005
|
|
3.05 0.0384 0.0823 0.1152 0.0537 0.502 5.270 5.076 374.122 0.595 22.576 6.153 0.33 141607. 0.5810
|
|
6.10 0.0767 0.1593 0.1146 0.0552 0.516 5.422 5.052 384.881 0.613 22.472 5.954 0.33 141771. 0.5609
|
|
9.15 0.1151 0.2308 0.1140 0.0568 0.531 5.583 5.025 396.299 0.631 22.349 5.751 0.33 141959. 0.5403
|
|
12.20 0.1534 0.2967 0.1132 0.0586 0.547 5.750 4.991 408.199 0.650 22.201 5.546 0.33 142171. 0.5193
|
|
15.26 0.1918 0.3573 0.1123 0.0603 0.564 5.922 4.951 420.350 0.669 22.022 5.342 0.33 142411. 0.4982
|
|
18.31 0.2301 0.4127 0.1112 0.0620 0.580 6.092 4.902 432.473 0.688 21.806 5.142 0.33 142679. 0.4771
|
|
21.36 0.2685 0.4631 0.1099 0.0637 0.596 6.258 4.844 444.245 0.707 21.545 4.946 0.33 142976. 0.4562
|
|
24.41 0.3069 0.5089 0.1083 0.0653 0.611 6.414 4.774 455.310 0.725 21.233 4.755 0.33 143304. 0.4355
|
|
27.46 0.3452 0.5504 0.1064 0.0667 0.624 6.555 4.690 465.288 0.741 20.862 4.572 0.34 143662. 0.4150
|
|
30.51 0.3836 0.5881 0.1042 0.0680 0.635 6.674 4.592 473.784 0.754 20.426 4.396 0.34 144052. 0.3948
|
|
33.56 0.4219 0.6221 0.1016 0.0689 0.644 6.767 4.478 480.398 0.765 19.919 4.228 0.34 144474. 0.3750
|
|
36.61 0.4603 0.6529 0.0986 0.0695 0.650 6.828 4.347 484.717 0.771 19.334 4.067 0.34 144928. 0.3554
|
|
39.67 0.4987 0.6806 0.0952 0.0698 0.652 6.851 4.197 486.319 0.774 18.666 3.914 0.34 145413. 0.3360
|
|
42.72 0.5370 0.7055 0.0914 0.0695 0.650 6.829 4.026 484.760 0.772 17.910 3.767 0.34 145930. 0.3168
|
|
45.77 0.5754 0.7278 0.0870 0.0688 0.643 6.756 3.835 479.600 0.763 17.059 3.627 0.34 146478. 0.2977
|
|
48.82 0.6137 0.7475 0.0822 0.0675 0.631 6.628 3.623 470.508 0.749 16.116 3.493 0.34 147057. 0.2786
|
|
51.87 0.6521 0.7649 0.0770 0.0656 0.613 6.443 3.392 457.395 0.728 15.088 3.364 0.34 147666. 0.2596
|
|
54.92 0.6904 0.7798 0.0714 0.0632 0.591 6.204 3.145 440.393 0.701 13.988 3.239 0.34 148305. 0.2407
|
|
57.97 0.7288 0.7923 0.0655 0.0602 0.563 5.913 2.885 419.737 0.668 12.831 3.117 0.34 148973. 0.2219
|
|
61.02 0.7672 0.8018 0.0593 0.0568 0.531 5.574 2.615 395.657 0.630 11.629 2.997 0.34 149670. 0.2031
|
|
64.08 0.8055 0.8082 0.0530 0.0528 0.494 5.189 2.337 368.349 0.586 10.393 2.877 0.34 150396. 0.1843
|
|
67.13 0.8439 0.8105 0.0466 0.0485 0.453 4.761 2.052 337.968 0.538 9.129 2.754 0.35 151151. 0.1654
|
|
70.18 0.8822 0.8077 0.0400 0.0437 0.409 4.292 1.763 304.644 0.485 7.843 2.625 0.35 151933. 0.1461
|
|
73.23 0.9206 0.7976 0.0334 0.0385 0.360 3.782 1.471 268.496 0.427 6.542 2.484 0.35 152743. 0.1263
|
|
76.28 0.9590 0.7765 0.0267 0.0329 0.308 3.235 1.176 229.650 0.365 5.230 2.322 0.35 153580. 0.1055
|
|
79.33 0.9973 0.7370 0.0200 0.0270 0.252 2.652 0.879 188.257 0.300 3.912 2.119 0.35 154443. 0.0833
|
|
82.38 1.0357 0.6613 0.0132 0.0207 0.194 2.036 0.583 144.509 0.230 2.595 1.831 0.35 155334. 0.0586
|
|
85.43 1.0740 0.4977 0.0066 0.0142 0.132 1.390 0.289 98.651 0.157 1.286 1.329 0.35 156249. 0.0299
|
|
88.49 1.1124 -0.0073 0.0000 0.0073 0.068 0.718 -0.002 50.945 0.081 -0.009 -0.019 0.35 157180. 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 0.1159 0.0519 0.771 6.940 6.950 574.763 0.784 30.912 5.484 0.39 165040. 0.6060
|
|
3.56 0.0384 0.0830 0.1154 0.0534 0.792 7.132 6.924 590.682 0.806 30.797 5.317 0.39 165205. 0.5863
|
|
7.12 0.0767 0.1606 0.1149 0.0549 0.815 7.340 6.894 607.904 0.829 30.663 5.144 0.39 165396. 0.5660
|
|
10.68 0.1151 0.2326 0.1143 0.0566 0.840 7.561 6.858 626.225 0.854 30.505 4.967 0.39 165615. 0.5452
|
|
14.24 0.1535 0.2991 0.1136 0.0583 0.865 7.793 6.815 645.367 0.880 30.313 4.790 0.39 165863. 0.5241
|
|
17.81 0.1919 0.3601 0.1127 0.0601 0.892 8.029 6.763 664.963 0.907 30.081 4.613 0.39 166142. 0.5028
|
|
21.37 0.2302 0.4158 0.1117 0.0618 0.918 8.266 6.699 684.561 0.934 29.797 4.439 0.39 166455. 0.4815
|
|
24.93 0.2686 0.4665 0.1104 0.0636 0.944 8.496 6.622 703.639 0.960 29.453 4.268 0.39 166801. 0.4603
|
|
28.49 0.3070 0.5125 0.1088 0.0652 0.968 8.713 6.528 721.619 0.984 29.039 4.103 0.39 167184. 0.4394
|
|
32.05 0.3454 0.5542 0.1070 0.0667 0.990 8.910 6.417 737.880 1.007 28.543 3.945 0.39 167602. 0.4188
|
|
35.61 0.3837 0.5920 0.1048 0.0679 1.008 9.077 6.286 751.782 1.026 27.959 3.792 0.39 168058. 0.3985
|
|
39.17 0.4221 0.6263 0.1022 0.0689 1.023 9.209 6.132 762.669 1.040 27.275 3.647 0.39 168550. 0.3785
|
|
42.73 0.4605 0.6572 0.0993 0.0695 1.032 9.296 5.954 769.875 1.050 26.485 3.508 0.39 169080. 0.3588
|
|
46.29 0.4988 0.6851 0.0959 0.0698 1.036 9.330 5.751 772.715 1.054 25.580 3.376 0.39 169647. 0.3393
|
|
49.86 0.5372 0.7102 0.0920 0.0696 1.033 9.303 5.520 770.474 1.051 24.552 3.249 0.39 170251. 0.3200
|
|
53.42 0.5756 0.7327 0.0877 0.0689 1.022 9.206 5.259 762.441 1.040 23.394 3.129 0.40 170891. 0.3007
|
|
56.98 0.6140 0.7527 0.0829 0.0676 1.003 9.033 4.970 748.077 1.021 22.107 3.013 0.40 171567. 0.2816
|
|
60.54 0.6523 0.7704 0.0776 0.0657 0.975 8.781 4.654 727.225 0.992 20.702 2.903 0.40 172278. 0.2625
|
|
64.10 0.6907 0.7858 0.0719 0.0632 0.939 8.453 4.316 700.094 0.955 19.198 2.796 0.40 173025. 0.2435
|
|
67.66 0.7291 0.7987 0.0660 0.0603 0.895 8.054 3.960 667.055 0.910 17.614 2.693 0.40 173805. 0.2246
|
|
71.22 0.7675 0.8089 0.0598 0.0568 0.843 7.589 3.590 628.484 0.857 15.968 2.591 0.40 174620. 0.2057
|
|
74.78 0.8058 0.8161 0.0535 0.0528 0.784 7.060 3.209 584.695 0.798 14.273 2.489 0.40 175468. 0.1869
|
|
78.34 0.8442 0.8195 0.0470 0.0484 0.719 6.471 2.819 535.941 0.731 12.540 2.386 0.40 176349. 0.1679
|
|
81.91 0.8826 0.8179 0.0404 0.0436 0.647 5.825 2.423 482.429 0.658 10.777 2.278 0.40 177262. 0.1486
|
|
85.47 0.9209 0.8096 0.0337 0.0383 0.569 5.124 2.021 424.353 0.579 8.992 2.161 0.41 178208. 0.1288
|
|
89.03 0.9593 0.7908 0.0270 0.0327 0.485 4.370 1.617 361.916 0.494 7.191 2.026 0.41 179185. 0.1080
|
|
92.59 0.9977 0.7544 0.0202 0.0267 0.396 3.566 1.210 295.361 0.403 5.383 1.858 0.41 180194. 0.0857
|
|
96.15 1.0361 0.6831 0.0134 0.0203 0.302 2.717 0.804 224.996 0.307 3.575 1.620 0.41 181233. 0.0609
|
|
99.71 1.0744 0.5241 0.0067 0.0137 0.203 1.826 0.400 151.220 0.206 1.778 1.199 0.41 182302. 0.0318
|
|
103.27 1.1128 0.0001 0.0000 0.0067 0.100 0.899 0.000 74.454 0.102 0.000 0.000 0.41 183387. 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 0.1161 0.0518 1.147 9.038 9.097 855.422 1.021 40.461 4.823 0.44 188613. 0.6097
|
|
4.07 0.0384 0.0835 0.1157 0.0532 1.179 9.290 9.065 879.317 1.050 40.321 4.676 0.44 188801. 0.5900
|
|
8.14 0.0768 0.1615 0.1152 0.0548 1.214 9.564 9.028 905.235 1.081 40.158 4.524 0.44 189019. 0.5697
|
|
12.22 0.1152 0.2340 0.1147 0.0565 1.251 9.856 8.985 932.884 1.114 39.964 4.368 0.44 189269. 0.5488
|
|
16.29 0.1536 0.3008 0.1140 0.0582 1.290 10.162 8.932 961.856 1.148 39.729 4.212 0.44 189552. 0.5276
|
|
20.36 0.1920 0.3620 0.1132 0.0600 1.330 10.477 8.867 991.601 1.184 39.441 4.056 0.45 189872. 0.5062
|
|
24.43 0.2304 0.4180 0.1122 0.0618 1.370 10.792 8.788 1021.439 1.219 39.088 3.902 0.45 190229. 0.4848
|
|
28.51 0.2688 0.4689 0.1109 0.0636 1.409 11.100 8.690 1050.568 1.254 38.655 3.752 0.45 190625. 0.4636
|
|
32.58 0.3072 0.5151 0.1094 0.0652 1.446 11.390 8.572 1078.099 1.287 38.130 3.607 0.45 191062. 0.4426
|
|
36.65 0.3456 0.5570 0.1076 0.0668 1.479 11.654 8.430 1103.077 1.317 37.499 3.466 0.45 191541. 0.4218
|
|
40.72 0.3840 0.5949 0.1054 0.0681 1.508 11.881 8.262 1124.514 1.342 36.748 3.332 0.45 192062. 0.4014
|
|
44.80 0.4224 0.6293 0.1029 0.0691 1.531 12.059 8.064 1141.400 1.362 35.867 3.204 0.45 192626. 0.3814
|
|
48.87 0.4608 0.6603 0.1000 0.0698 1.546 12.179 7.833 1152.716 1.376 34.843 3.082 0.45 193232. 0.3616
|
|
52.94 0.4991 0.6884 0.0966 0.0700 1.552 12.228 7.569 1157.417 1.382 33.666 2.966 0.45 193881. 0.3420
|
|
57.01 0.5375 0.7137 0.0928 0.0699 1.548 12.197 7.267 1154.417 1.378 32.325 2.855 0.45 194573. 0.3226
|
|
61.08 0.5759 0.7364 0.0884 0.0691 1.532 12.072 6.927 1142.635 1.364 30.812 2.750 0.45 195306. 0.3033
|
|
65.16 0.6143 0.7566 0.0836 0.0679 1.504 11.846 6.548 1121.242 1.338 29.126 2.649 0.45 196080. 0.2841
|
|
69.23 0.6527 0.7746 0.0783 0.0660 1.462 11.516 6.134 1089.986 1.301 27.282 2.552 0.45 196894. 0.2649
|
|
73.30 0.6911 0.7904 0.0726 0.0635 1.407 11.085 5.689 1049.172 1.252 25.305 2.459 0.45 197749. 0.2459
|
|
77.37 0.7295 0.8037 0.0666 0.0605 1.340 10.559 5.221 999.365 1.193 23.222 2.369 0.46 198642. 0.2269
|
|
81.45 0.7679 0.8145 0.0604 0.0570 1.262 9.943 4.734 941.138 1.123 21.055 2.281 0.46 199575. 0.2080
|
|
85.52 0.8063 0.8224 0.0540 0.0530 1.173 9.244 4.232 874.974 1.044 18.822 2.194 0.46 200546. 0.1891
|
|
89.59 0.8447 0.8266 0.0475 0.0485 1.075 8.466 3.718 801.256 0.956 16.538 2.105 0.46 201554. 0.1701
|
|
93.66 0.8831 0.8262 0.0408 0.0436 0.966 7.610 3.195 720.302 0.860 14.213 2.012 0.46 202599. 0.1508
|
|
97.74 0.9215 0.8193 0.0340 0.0383 0.848 6.682 2.666 632.405 0.755 11.859 1.912 0.46 203681. 0.1309
|
|
101.81 0.9599 0.8025 0.0272 0.0326 0.721 5.683 2.132 537.875 0.642 9.484 1.798 0.46 204800. 0.1100
|
|
105.88 0.9983 0.7687 0.0204 0.0265 0.586 4.618 1.596 437.078 0.522 7.098 1.656 0.47 205954. 0.0877
|
|
109.95 1.0367 0.7008 0.0135 0.0200 0.443 3.492 1.059 330.485 0.394 4.712 1.454 0.47 207143. 0.0627
|
|
114.02 1.0751 0.5452 0.0067 0.0132 0.293 2.311 0.526 218.707 0.261 2.339 1.091 0.47 208366. 0.0331
|
|
118.10 1.1135 -0.0044 0.0000 0.0062 0.137 1.082 -0.002 102.366 0.122 -0.008 -0.008 0.47 209605. 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 0.1164 0.0517 1.633 11.433 11.539 1217.446 1.292 51.325 4.299 0.50 212184. 0.6120
|
|
4.58 0.0384 0.0837 0.1160 0.0532 1.678 11.754 11.502 1251.624 1.328 51.161 4.168 0.50 212396. 0.5925
|
|
9.17 0.0768 0.1621 0.1156 0.0548 1.728 12.104 11.459 1288.812 1.367 50.971 4.033 0.50 212641. 0.5722
|
|
13.75 0.1152 0.2348 0.1150 0.0565 1.782 12.478 11.408 1328.613 1.410 50.745 3.895 0.50 212921. 0.5513
|
|
18.33 0.1536 0.3018 0.1144 0.0582 1.838 12.871 11.346 1370.464 1.454 50.469 3.755 0.50 213239. 0.5302
|
|
22.92 0.1921 0.3633 0.1136 0.0601 1.896 13.276 11.270 1413.587 1.500 50.129 3.616 0.50 213598. 0.5088
|
|
27.50 0.2305 0.4194 0.1127 0.0619 1.954 13.683 11.175 1456.995 1.546 49.707 3.479 0.50 214000. 0.4874
|
|
32.08 0.2689 0.4704 0.1115 0.0637 2.011 14.083 11.058 1499.520 1.591 49.186 3.345 0.50 214446. 0.4662
|
|
36.67 0.3073 0.5168 0.1101 0.0654 2.065 14.461 10.914 1539.852 1.634 48.547 3.215 0.50 214938. 0.4451
|
|
41.25 0.3457 0.5587 0.1083 0.0670 2.114 14.806 10.740 1576.580 1.673 47.772 3.090 0.50 215476. 0.4244
|
|
45.83 0.3841 0.5968 0.1062 0.0684 2.157 15.104 10.531 1608.240 1.706 46.843 2.970 0.50 216063. 0.4040
|
|
50.41 0.4225 0.6312 0.1037 0.0694 2.190 15.339 10.285 1633.342 1.733 45.746 2.856 0.50 216698. 0.3839
|
|
55.00 0.4609 0.6624 0.1008 0.0701 2.213 15.499 9.997 1650.393 1.751 44.465 2.747 0.51 217381. 0.3641
|
|
59.58 0.4993 0.6906 0.0975 0.0705 2.223 15.570 9.664 1657.866 1.759 42.986 2.644 0.51 218112. 0.3445
|
|
64.16 0.5378 0.7160 0.0936 0.0703 2.218 15.535 9.284 1654.184 1.755 41.294 2.546 0.51 218891. 0.3251
|
|
68.75 0.5762 0.7389 0.0893 0.0696 2.196 15.381 8.853 1637.778 1.738 39.378 2.452 0.51 219717. 0.3057
|
|
73.33 0.6146 0.7595 0.0844 0.0683 2.156 15.096 8.372 1607.428 1.706 37.239 2.362 0.51 220589. 0.2865
|
|
77.91 0.6530 0.7777 0.0791 0.0664 2.096 14.676 7.845 1562.742 1.658 34.895 2.277 0.51 221507. 0.2673
|
|
82.50 0.6914 0.7938 0.0734 0.0639 2.017 14.126 7.279 1504.149 1.596 32.376 2.195 0.51 222470. 0.2482
|
|
87.08 0.7298 0.8076 0.0674 0.0609 1.921 13.453 6.681 1432.469 1.520 29.719 2.116 0.51 223477. 0.2292
|
|
91.66 0.7682 0.8190 0.0611 0.0573 1.808 12.665 6.059 1348.542 1.431 26.951 2.038 0.51 224527. 0.2103
|
|
96.25 0.8066 0.8274 0.0546 0.0533 1.680 11.768 5.418 1253.076 1.330 24.098 1.961 0.52 225621. 0.1913
|
|
100.83 0.8450 0.8325 0.0480 0.0487 1.538 10.768 4.761 1146.634 1.217 21.178 1.883 0.52 226756. 0.1722
|
|
105.41 0.8835 0.8331 0.0413 0.0438 1.381 9.670 4.093 1029.683 1.093 18.204 1.803 0.52 227934. 0.1529
|
|
110.00 0.9219 0.8276 0.0344 0.0384 1.210 8.477 3.415 902.644 0.958 15.191 1.716 0.52 229152. 0.1329
|
|
114.58 0.9603 0.8125 0.0275 0.0326 1.027 7.193 2.732 765.965 0.813 12.150 1.618 0.52 230412. 0.1120
|
|
119.16 0.9987 0.7811 0.0206 0.0264 0.832 5.824 2.045 620.178 0.658 9.094 1.495 0.52 231711. 0.0896
|
|
123.75 1.0371 0.7167 0.0137 0.0198 0.625 4.376 1.357 465.966 0.494 6.037 1.321 0.53 233050. 0.0645
|
|
128.33 1.0755 0.5649 0.0068 0.0129 0.408 2.857 0.673 304.218 0.323 2.996 1.004 0.53 234427. 0.0345
|
|
132.91 1.1139 -0.0064 0.0000 0.0058 0.182 1.276 -0.003 135.819 0.144 -0.015 -0.011 0.53 235819. 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 0.1166 0.0518 2.243 14.140 14.280 1672.927 1.598 63.516 3.872 0.56 235753. 0.6132
|
|
5.09 0.0384 0.0838 0.1163 0.0533 2.307 14.538 14.238 1719.977 1.642 63.332 3.755 0.56 235988. 0.5938
|
|
10.19 0.0768 0.1623 0.1159 0.0549 2.375 14.972 14.190 1771.345 1.692 63.119 3.634 0.56 236260. 0.5737
|
|
15.28 0.1153 0.2351 0.1154 0.0566 2.449 15.438 14.134 1826.541 1.744 62.866 3.510 0.56 236571. 0.5530
|
|
20.38 0.1537 0.3023 0.1149 0.0584 2.528 15.931 14.064 1884.818 1.800 62.556 3.384 0.56 236924. 0.5319
|
|
25.47 0.1921 0.3639 0.1142 0.0603 2.608 16.441 13.977 1945.123 1.857 62.171 3.259 0.56 237322. 0.5107
|
|
30.56 0.2305 0.4201 0.1133 0.0622 2.690 16.956 13.869 2006.093 1.916 61.687 3.136 0.56 237768. 0.4894
|
|
35.66 0.2690 0.4713 0.1122 0.0640 2.771 17.463 13.733 2066.082 1.973 61.083 3.015 0.56 238263. 0.4682
|
|
40.75 0.3074 0.5177 0.1108 0.0658 2.847 17.946 13.564 2123.218 2.028 60.332 2.898 0.56 238809. 0.4473
|
|
45.84 0.3458 0.5597 0.1091 0.0674 2.917 18.388 13.357 2175.479 2.077 59.412 2.785 0.56 239408. 0.4266
|
|
50.94 0.3842 0.5978 0.1071 0.0688 2.978 18.770 13.107 2220.760 2.121 58.300 2.677 0.56 240060. 0.4062
|
|
56.03 0.4226 0.6323 0.1046 0.0699 3.027 19.076 12.809 2256.933 2.155 56.974 2.574 0.56 240766. 0.3861
|
|
61.13 0.4611 0.6636 0.1018 0.0707 3.060 19.287 12.458 2281.864 2.179 55.415 2.476 0.56 241526. 0.3663
|
|
66.22 0.4995 0.6919 0.0984 0.0711 3.075 19.384 12.052 2293.399 2.190 53.605 2.383 0.56 242339. 0.3468
|
|
71.31 0.5379 0.7175 0.0946 0.0709 3.070 19.350 11.584 2289.327 2.186 51.527 2.295 0.56 243206. 0.3274
|
|
76.41 0.5763 0.7406 0.0903 0.0703 3.041 19.165 11.053 2267.449 2.165 49.164 2.211 0.56 244125. 0.3081
|
|
81.50 0.6148 0.7614 0.0854 0.0690 2.985 18.815 10.458 2226.031 2.126 46.518 2.131 0.57 245095. 0.2888
|
|
86.60 0.6532 0.7799 0.0801 0.0671 2.903 18.295 9.804 2164.479 2.067 43.609 2.054 0.57 246117. 0.2696
|
|
91.69 0.6916 0.7964 0.0743 0.0646 2.794 17.609 9.100 2083.373 1.989 40.478 1.981 0.57 247188. 0.2505
|
|
96.78 0.7300 0.8106 0.0683 0.0615 2.660 16.768 8.356 1983.866 1.894 37.168 1.910 0.57 248308. 0.2315
|
|
101.88 0.7684 0.8224 0.0619 0.0579 2.504 15.782 7.580 1867.152 1.783 33.718 1.841 0.57 249477. 0.2125
|
|
106.97 0.8069 0.8315 0.0554 0.0537 2.326 14.658 6.780 1734.241 1.656 30.157 1.773 0.57 250693. 0.1935
|
|
112.06 0.8453 0.8374 0.0487 0.0491 2.127 13.405 5.960 1585.935 1.514 26.509 1.704 0.58 251957. 0.1744
|
|
117.16 0.8837 0.8390 0.0419 0.0441 1.908 12.027 5.124 1422.890 1.359 22.793 1.633 0.58 253266. 0.1550
|
|
122.25 0.9221 0.8346 0.0349 0.0386 1.671 10.529 4.277 1245.699 1.190 19.024 1.557 0.58 254622. 0.1350
|
|
127.35 0.9606 0.8213 0.0279 0.0327 1.415 8.917 3.422 1054.986 1.007 15.219 1.471 0.58 256022. 0.1140
|
|
132.44 0.9990 0.7922 0.0209 0.0264 1.142 7.197 2.561 851.492 0.813 11.393 1.364 0.58 257467. 0.0915
|
|
137.53 1.0374 0.7310 0.0139 0.0197 0.853 5.377 1.701 636.170 0.607 7.564 1.212 0.58 258956. 0.0663
|
|
142.63 1.0758 0.5833 0.0069 0.0127 0.550 3.468 0.844 410.271 0.392 3.753 0.933 0.59 260487. 0.0359
|
|
147.72 1.1142 -0.0078 0.0000 0.0054 0.235 1.479 -0.005 175.008 0.167 -0.021 -0.012 0.59 262031. 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 0.1169 0.0521 2.998 17.180 17.321 2235.895 1.941 77.045 3.514 0.61 259321. 0.6129
|
|
5.60 0.0384 0.0838 0.1166 0.0535 3.082 17.662 17.276 2298.543 1.995 76.846 3.409 0.61 259579. 0.5939
|
|
11.21 0.0769 0.1622 0.1163 0.0551 3.174 18.189 17.225 2367.217 2.055 76.617 3.300 0.61 259877. 0.5741
|
|
16.81 0.1153 0.2351 0.1159 0.0568 3.274 18.759 17.164 2441.335 2.119 76.346 3.189 0.61 260218. 0.5537
|
|
22.42 0.1537 0.3023 0.1154 0.0587 3.379 19.363 17.089 2519.980 2.188 76.013 3.076 0.61 260606. 0.5329
|
|
28.02 0.1922 0.3640 0.1147 0.0606 3.489 19.992 16.995 2601.794 2.259 75.594 2.963 0.61 261043. 0.5119
|
|
33.63 0.2306 0.4203 0.1139 0.0625 3.601 20.631 16.876 2684.962 2.331 75.062 2.851 0.61 261532. 0.4908
|
|
39.23 0.2690 0.4714 0.1129 0.0644 3.711 21.263 16.724 2767.243 2.402 74.387 2.741 0.61 262076. 0.4698
|
|
44.84 0.3074 0.5179 0.1116 0.0663 3.817 21.869 16.532 2846.052 2.471 73.536 2.635 0.61 262676. 0.4490
|
|
50.44 0.3459 0.5600 0.1100 0.0679 3.914 22.426 16.294 2918.552 2.534 72.478 2.532 0.61 263335. 0.4284
|
|
56.04 0.3843 0.5981 0.1080 0.0694 3.999 22.912 16.003 2981.777 2.589 71.183 2.434 0.62 264052. 0.4081
|
|
61.65 0.4227 0.6327 0.1057 0.0706 4.067 23.303 15.653 3032.725 2.633 69.622 2.341 0.62 264829. 0.3882
|
|
67.25 0.4612 0.6641 0.1029 0.0714 4.115 23.577 15.237 3068.411 2.664 67.773 2.252 0.62 265666. 0.3685
|
|
72.86 0.4996 0.6925 0.0996 0.0718 4.138 23.711 14.750 3085.857 2.679 65.609 2.168 0.62 266562. 0.3490
|
|
78.46 0.5380 0.7182 0.0958 0.0717 4.133 23.682 14.189 3082.042 2.676 63.111 2.088 0.62 267517. 0.3296
|
|
84.07 0.5765 0.7415 0.0915 0.0711 4.095 23.466 13.547 3053.969 2.651 60.259 2.012 0.62 268529. 0.3104
|
|
89.67 0.6149 0.7625 0.0866 0.0698 4.022 23.046 12.826 2999.237 2.604 57.051 1.940 0.62 269598. 0.2912
|
|
95.28 0.6533 0.7814 0.0812 0.0679 3.912 22.414 12.031 2916.974 2.532 53.513 1.871 0.62 270723. 0.2720
|
|
100.88 0.6918 0.7981 0.0754 0.0654 3.766 21.576 11.173 2807.934 2.438 49.696 1.805 0.63 271903. 0.2528
|
|
106.48 0.7302 0.8128 0.0693 0.0622 3.585 20.544 10.263 2673.701 2.321 45.651 1.741 0.63 273138. 0.2338
|
|
112.09 0.7686 0.8251 0.0629 0.0586 3.374 19.332 9.314 2515.936 2.184 41.429 1.679 0.63 274425. 0.2148
|
|
117.69 0.8070 0.8348 0.0563 0.0544 3.133 17.950 8.333 2336.044 2.028 37.067 1.618 0.63 275764. 0.1958
|
|
123.30 0.8455 0.8414 0.0495 0.0497 2.863 16.406 7.328 2135.142 1.854 32.593 1.557 0.63 277156. 0.1766
|
|
128.90 0.8839 0.8439 0.0425 0.0446 2.567 14.708 6.302 1914.131 1.662 28.033 1.493 0.63 278598. 0.1571
|
|
134.51 0.9223 0.8408 0.0355 0.0390 2.245 12.861 5.262 1673.823 1.453 23.405 1.426 0.64 280090. 0.1371
|
|
140.11 0.9608 0.8290 0.0284 0.0329 1.898 10.873 4.211 1415.062 1.228 18.729 1.350 0.64 281632. 0.1161
|
|
145.72 0.9992 0.8022 0.0213 0.0265 1.527 8.751 3.153 1138.850 0.989 14.024 1.256 0.64 283222. 0.0934
|
|
151.32 1.0376 0.7442 0.0141 0.0197 1.135 6.504 2.094 846.483 0.735 9.312 1.122 0.64 284861. 0.0680
|
|
156.93 1.0761 0.6005 0.0070 0.0126 0.724 4.147 1.039 539.705 0.469 4.620 0.873 0.65 286545. 0.0373
|
|
162.53 1.1145 -0.0098 0.0000 0.0051 0.295 1.692 -0.007 220.212 0.191 -0.030 -0.014 0.65 288241. 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 0.1172 0.0526 3.934 20.664 20.665 2933.798 2.335 91.920 3.195 0.67 282886. 0.6087
|
|
6.12 0.0384 0.0832 0.1170 0.0541 4.043 21.233 20.618 3014.536 2.399 91.710 3.102 0.67 283167. 0.5904
|
|
12.23 0.0769 0.1612 0.1167 0.0556 4.162 21.859 20.565 3103.386 2.470 91.473 3.006 0.67 283491. 0.5713
|
|
18.35 0.1153 0.2337 0.1163 0.0574 4.291 22.537 20.502 3199.701 2.546 91.195 2.906 0.67 283863. 0.5515
|
|
24.46 0.1538 0.3008 0.1159 0.0592 4.429 23.260 20.425 3302.381 2.628 90.853 2.805 0.67 284284. 0.5314
|
|
30.58 0.1922 0.3625 0.1153 0.0611 4.573 24.017 20.328 3409.733 2.713 90.419 2.704 0.67 284760. 0.5110
|
|
36.69 0.2306 0.4188 0.1146 0.0631 4.720 24.789 20.202 3519.427 2.801 89.859 2.604 0.67 285293. 0.4905
|
|
42.81 0.2691 0.4701 0.1137 0.0651 4.866 25.558 20.039 3628.526 2.887 89.135 2.505 0.67 285885. 0.4700
|
|
48.92 0.3075 0.5167 0.1125 0.0669 5.007 26.298 19.830 3733.580 2.971 88.206 2.409 0.67 286539. 0.4496
|
|
55.04 0.3460 0.5590 0.1110 0.0687 5.137 26.982 19.566 3830.795 3.048 87.029 2.317 0.67 287257. 0.4295
|
|
61.15 0.3844 0.5973 0.1091 0.0702 5.252 27.584 19.237 3916.170 3.116 85.565 2.228 0.67 288040. 0.4096
|
|
67.27 0.4228 0.6321 0.1068 0.0715 5.345 28.073 18.835 3985.656 3.172 83.776 2.143 0.67 288888. 0.3899
|
|
73.38 0.4613 0.6637 0.1041 0.0724 5.411 28.422 18.352 4035.202 3.211 81.631 2.063 0.67 289801. 0.3704
|
|
79.50 0.4997 0.6923 0.1009 0.0728 5.446 28.602 17.783 4060.758 3.231 79.100 1.986 0.67 290780. 0.3511
|
|
85.62 0.5382 0.7182 0.0971 0.0728 5.442 28.584 17.121 4058.191 3.229 76.154 1.914 0.68 291823. 0.3318
|
|
91.73 0.5766 0.7417 0.0928 0.0721 5.395 28.339 16.361 4023.384 3.202 72.772 1.844 0.68 292929. 0.3127
|
|
97.85 0.6150 0.7629 0.0879 0.0709 5.301 27.843 15.501 3953.009 3.146 68.950 1.779 0.68 294097. 0.2935
|
|
103.96 0.6535 0.7821 0.0825 0.0690 5.157 27.088 14.550 3845.755 3.060 64.718 1.716 0.68 295327. 0.2743
|
|
110.08 0.6919 0.7992 0.0767 0.0664 4.965 26.079 13.520 3702.580 2.946 60.136 1.656 0.68 296616. 0.2552
|
|
116.19 0.7303 0.8143 0.0705 0.0632 4.728 24.833 12.426 3525.613 2.806 55.270 1.599 0.68 297965. 0.2362
|
|
122.31 0.7688 0.8271 0.0640 0.0595 4.448 23.364 11.281 3317.126 2.640 50.180 1.543 0.69 299372. 0.2172
|
|
128.42 0.8072 0.8374 0.0573 0.0552 4.129 21.687 10.098 3079.043 2.450 44.914 1.487 0.69 300835. 0.1981
|
|
134.54 0.8457 0.8447 0.0504 0.0504 3.772 19.813 8.882 2812.891 2.238 39.508 1.432 0.69 302355. 0.1789
|
|
140.65 0.8841 0.8482 0.0433 0.0452 3.379 17.749 7.642 2519.893 2.005 33.992 1.376 0.69 303930. 0.1594
|
|
146.77 0.9225 0.8462 0.0362 0.0395 2.952 15.504 6.382 2201.135 1.752 28.388 1.315 0.69 305559. 0.1393
|
|
152.88 0.9610 0.8359 0.0290 0.0333 2.491 13.085 5.108 1857.782 1.478 22.722 1.247 0.70 307243. 0.1181
|
|
159.00 0.9994 0.8110 0.0217 0.0267 2.000 10.504 3.825 1491.281 1.187 17.015 1.163 0.70 308979. 0.0954
|
|
165.11 1.0379 0.7555 0.0144 0.0198 1.480 7.773 2.539 1103.572 0.878 11.296 1.044 0.70 310768. 0.0697
|
|
171.23 1.0763 0.6141 0.0071 0.0125 0.935 4.912 1.258 697.344 0.555 5.595 0.818 0.70 312607. 0.0385
|
|
177.35 1.1147 -0.0179 -0.0001 0.0049 0.369 1.939 -0.014 275.324 0.219 -0.062 -0.023 0.71 314451. 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 0.1175 0.0540 5.136 24.901 24.310 3829.894 2.813 108.129 2.879 0.72 306450. 0.5949
|
|
6.65 0.0386 0.0816 0.1173 0.0554 5.272 25.561 24.261 3931.396 2.888 107.911 2.799 0.72 306754. 0.5778
|
|
13.30 0.0772 0.1583 0.1170 0.0570 5.422 26.290 24.207 4043.557 2.970 107.672 2.715 0.72 307106. 0.5599
|
|
19.95 0.1157 0.2299 0.1167 0.0587 5.586 27.084 24.145 4165.639 3.060 107.396 2.629 0.72 307509. 0.5414
|
|
26.60 0.1543 0.2963 0.1163 0.0606 5.761 27.933 24.069 4296.304 3.156 107.058 2.541 0.72 307967. 0.5225
|
|
33.25 0.1929 0.3574 0.1159 0.0625 5.945 28.825 23.972 4433.429 3.257 106.627 2.452 0.72 308484. 0.5033
|
|
39.90 0.2315 0.4136 0.1152 0.0645 6.134 29.739 23.845 4573.961 3.360 106.062 2.365 0.72 309063. 0.4839
|
|
46.54 0.2701 0.4649 0.1144 0.0665 6.322 30.649 23.677 4713.950 3.463 105.316 2.278 0.72 309706. 0.4646
|
|
53.19 0.3086 0.5117 0.1134 0.0684 6.502 31.525 23.457 4848.704 3.562 104.335 2.194 0.73 310417. 0.4454
|
|
59.84 0.3472 0.5544 0.1120 0.0701 6.669 32.334 23.171 4973.068 3.653 103.063 2.113 0.73 311199. 0.4263
|
|
66.49 0.3858 0.5934 0.1102 0.0717 6.815 33.040 22.807 5081.725 3.733 101.446 2.036 0.73 312051. 0.4074
|
|
73.14 0.4244 0.6289 0.1080 0.0729 6.932 33.610 22.355 5169.409 3.797 99.433 1.961 0.73 312975. 0.3887
|
|
79.79 0.4630 0.6613 0.1054 0.0738 7.015 34.010 21.803 5230.991 3.842 96.982 1.891 0.73 313972. 0.3700
|
|
86.44 0.5015 0.6908 0.1022 0.0742 7.056 34.208 21.145 5261.408 3.865 94.053 1.823 0.73 315040. 0.3513
|
|
93.09 0.5401 0.7175 0.0985 0.0741 7.048 34.170 20.371 5255.492 3.860 90.611 1.758 0.73 316179. 0.3326
|
|
99.74 0.5787 0.7416 0.0941 0.0735 6.984 33.861 19.476 5208.013 3.826 86.628 1.696 0.73 317387. 0.3137
|
|
106.39 0.6173 0.7634 0.0892 0.0721 6.859 33.253 18.458 5114.557 3.757 82.101 1.637 0.74 318663. 0.2947
|
|
113.04 0.6559 0.7831 0.0837 0.0701 6.669 32.334 17.326 4973.213 3.653 77.066 1.580 0.74 320006. 0.2757
|
|
119.69 0.6944 0.8006 0.0778 0.0675 6.417 31.110 16.096 4784.945 3.515 71.596 1.526 0.74 321415. 0.2566
|
|
126.34 0.7330 0.8160 0.0715 0.0642 6.105 29.598 14.788 4552.318 3.344 65.775 1.473 0.74 322888. 0.2375
|
|
132.98 0.7716 0.8293 0.0648 0.0603 5.737 27.815 13.417 4278.161 3.143 59.677 1.422 0.74 324423. 0.2184
|
|
139.63 0.8102 0.8401 0.0580 0.0559 5.317 25.779 11.997 3964.972 2.913 53.361 1.372 0.75 326021. 0.1992
|
|
146.28 0.8488 0.8479 0.0509 0.0510 4.848 23.503 10.537 3614.829 2.655 46.869 1.322 0.75 327680. 0.1799
|
|
152.93 0.8873 0.8518 0.0437 0.0455 4.331 20.997 9.047 3229.498 2.372 40.239 1.271 0.75 329399. 0.1602
|
|
159.58 0.9259 0.8503 0.0364 0.0396 3.769 18.274 7.531 2810.670 2.065 33.499 1.215 0.75 331177. 0.1398
|
|
166.23 0.9645 0.8399 0.0290 0.0333 3.165 15.346 5.997 2360.340 1.734 26.676 1.152 0.76 333014. 0.1183
|
|
172.88 1.0031 0.8134 0.0215 0.0265 2.523 12.231 4.451 1881.161 1.382 19.798 1.073 0.76 334908. 0.0949
|
|
179.53 1.0417 0.7518 0.0140 0.0194 1.846 8.951 2.900 1376.724 1.011 12.897 0.955 0.76 336859. 0.0682
|
|
186.18 1.0802 0.5872 0.0065 0.0120 1.142 5.538 1.351 851.835 0.626 6.010 0.719 0.76 338864. 0.0350
|
|
192.83 1.1188
|
|
|
|
|
|
|
|
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 0.1177 0.0570 6.769 30.472 28.246 5047.322 3.443 125.638 2.538 0.78 330011. 0.5654
|
|
7.16 0.0386 0.0777 0.1175 0.0584 6.935 31.224 28.195 5171.752 3.528 125.412 2.473 0.78 330339. 0.5503
|
|
14.33 0.0772 0.1510 0.1173 0.0600 7.121 32.057 28.141 5309.838 3.622 125.173 2.404 0.78 330717. 0.5345
|
|
21.49 0.1158 0.2198 0.1170 0.0617 7.323 32.969 28.081 5460.793 3.725 124.905 2.332 0.78 331150. 0.5180
|
|
28.66 0.1544 0.2839 0.1167 0.0635 7.541 33.948 28.009 5623.064 3.835 124.586 2.259 0.78 331642. 0.5011
|
|
35.82 0.1930 0.3432 0.1163 0.0654 7.770 34.980 27.918 5794.011 3.952 124.181 2.186 0.78 332197. 0.4840
|
|
42.99 0.2316 0.3980 0.1158 0.0674 8.005 36.041 27.798 5969.670 4.072 123.646 2.112 0.78 332818. 0.4667
|
|
50.15 0.2702 0.4485 0.1152 0.0694 8.240 37.097 27.636 6144.680 4.191 122.924 2.040 0.78 333509. 0.4495
|
|
57.32 0.3088 0.4950 0.1143 0.0713 8.465 38.110 27.417 6312.451 4.306 121.949 1.970 0.78 334273. 0.4323
|
|
64.48 0.3474 0.5379 0.1130 0.0730 8.671 39.035 27.124 6465.623 4.410 120.650 1.903 0.78 335113. 0.4153
|
|
71.65 0.3860 0.5775 0.1114 0.0745 8.846 39.827 26.743 6596.736 4.500 118.951 1.839 0.78 336030. 0.3985
|
|
78.81 0.4246 0.6142 0.1094 0.0756 8.983 40.443 26.256 6698.833 4.569 116.785 1.778 0.78 337025. 0.3818
|
|
85.98 0.4632 0.6481 0.1069 0.0764 9.073 40.846 25.650 6765.603 4.615 114.091 1.720 0.79 338100. 0.3650
|
|
93.14 0.5018 0.6794 0.1038 0.0767 9.107 41.001 24.914 6791.269 4.632 110.816 1.664 0.79 339252. 0.3481
|
|
100.31 0.5404 0.7081 0.1002 0.0764 9.079 40.874 24.037 6770.216 4.618 106.915 1.610 0.79 340481. 0.3309
|
|
107.47 0.5790 0.7343 0.0959 0.0756 8.980 40.430 23.011 6696.734 4.568 102.353 1.559 0.79 341786. 0.3133
|
|
114.64 0.6176 0.7580 0.0910 0.0741 8.805 39.640 21.835 6565.902 4.479 97.120 1.508 0.79 343164. 0.2954
|
|
121.80 0.6562 0.7794 0.0855 0.0720 8.550 38.491 20.517 6375.585 4.349 91.260 1.460 0.79 344614. 0.2771
|
|
128.97 0.6948 0.7985 0.0795 0.0692 8.217 36.991 19.078 6127.119 4.179 84.858 1.412 0.80 346136. 0.2585
|
|
136.13 0.7334 0.8152 0.0731 0.0658 7.810 35.160 17.540 5823.769 3.972 78.016 1.366 0.80 347726. 0.2398
|
|
143.29 0.7720 0.8296 0.0664 0.0618 7.334 33.018 15.923 5468.960 3.730 70.826 1.321 0.80 349384. 0.2209
|
|
150.46 0.8106 0.8412 0.0594 0.0572 6.793 30.584 14.244 5065.906 3.455 63.359 1.275 0.80 351110. 0.2017
|
|
157.62 0.8492 0.8497 0.0522 0.0521 6.191 27.873 12.516 4616.817 3.149 55.672 1.230 0.81 352900. 0.1823
|
|
164.79 0.8878 0.8539 0.0448 0.0466 5.531 24.899 10.748 4124.175 2.813 47.806 1.182 0.81 354755. 0.1624
|
|
171.95 0.9264 0.8520 0.0373 0.0405 4.815 21.679 8.947 3590.807 2.449 39.798 1.130 0.81 356674. 0.1417
|
|
179.12 0.9650 0.8397 0.0297 0.0341 4.051 18.237 7.122 3020.773 2.060 31.677 1.069 0.81 358656. 0.1196
|
|
186.28 1.0036 0.8081 0.0220 0.0273 3.244 14.606 5.278 2419.301 1.650 23.476 0.990 0.82 360699. 0.0953
|
|
193.45 1.0422 0.7346 0.0143 0.0202 2.405 10.825 3.424 1793.057 1.223 15.231 0.866 0.82 362803. 0.0672
|
|
200.61 1.0809 0.5447 0.0065 0.0130 1.543 6.945 1.571 1150.303 0.785 6.986 0.619 0.82 364965. 0.0325
|
|
207.78 1.1195
|
|
|
|
|
|
|
|
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 0.1178 0.0624 9.109 38.274 32.455 6792.385 4.324 144.361 2.167 0.83 353570. 0.5175
|
|
7.64 0.0384 0.0709 0.1176 0.0637 9.309 39.114 32.400 6941.501 4.419 144.115 2.117 0.83 353918. 0.5051
|
|
15.29 0.0769 0.1383 0.1174 0.0653 9.532 40.052 32.344 7107.888 4.525 143.868 2.064 0.83 354320. 0.4920
|
|
22.93 0.1153 0.2019 0.1172 0.0669 9.777 41.083 32.285 7290.840 4.641 143.606 2.009 0.83 354781. 0.4783
|
|
30.57 0.1537 0.2615 0.1170 0.0688 10.043 42.198 32.218 7488.773 4.767 143.307 1.951 0.83 355303. 0.4642
|
|
38.22 0.1922 0.3172 0.1167 0.0707 10.324 43.381 32.136 7698.683 4.901 142.941 1.893 0.83 355891. 0.4498
|
|
45.86 0.2306 0.3690 0.1163 0.0727 10.615 44.604 32.028 7915.724 5.039 142.462 1.835 0.84 356549. 0.4353
|
|
53.50 0.2690 0.4170 0.1157 0.0747 10.906 45.826 31.882 8132.723 5.177 141.810 1.778 0.84 357281. 0.4208
|
|
61.14 0.3075 0.4618 0.1150 0.0766 11.185 46.999 31.680 8340.787 5.310 140.912 1.723 0.84 358090. 0.4064
|
|
68.79 0.3459 0.5036 0.1140 0.0783 11.438 48.059 31.402 8528.964 5.430 139.678 1.670 0.84 358979. 0.3922
|
|
76.43 0.3843 0.5429 0.1126 0.0797 11.648 48.942 31.028 8685.633 5.529 138.013 1.620 0.84 359950. 0.3783
|
|
84.07 0.4228 0.5801 0.1109 0.0808 11.801 49.587 30.536 8800.048 5.602 135.822 1.574 0.84 361006. 0.3645
|
|
91.72 0.4612 0.6153 0.1086 0.0814 11.886 49.943 29.905 8863.202 5.642 133.018 1.530 0.84 362147. 0.3508
|
|
99.36 0.4996 0.6487 0.1057 0.0814 11.893 49.975 29.121 8868.898 5.646 129.530 1.489 0.84 363372. 0.3368
|
|
107.00 0.5381 0.6801 0.1023 0.0809 11.817 49.655 28.169 8812.101 5.610 125.296 1.450 0.85 364680. 0.3225
|
|
114.65 0.5765 0.7095 0.0982 0.0798 11.650 48.954 27.038 8687.718 5.531 120.267 1.412 0.85 366068. 0.3076
|
|
122.29 0.6149 0.7367 0.0934 0.0780 11.387 47.848 25.725 8491.471 5.406 114.423 1.374 0.85 367537. 0.2921
|
|
129.93 0.6534 0.7616 0.0880 0.0755 11.026 46.330 24.236 8222.140 5.234 107.803 1.337 0.85 369082. 0.2759
|
|
137.58 0.6918 0.7842 0.0820 0.0724 10.571 44.418 22.596 7882.806 5.018 100.506 1.300 0.85 370703. 0.2590
|
|
145.22 0.7302 0.8043 0.0756 0.0687 10.029 42.139 20.830 7478.344 4.761 92.652 1.263 0.86 372398. 0.2417
|
|
152.86 0.7687 0.8219 0.0688 0.0644 9.405 39.520 18.964 7013.469 4.465 84.351 1.226 0.86 374164. 0.2238
|
|
160.50 0.8071 0.8364 0.0618 0.0596 8.708 36.589 17.017 6493.332 4.134 75.693 1.189 0.86 376002. 0.2055
|
|
168.15 0.8455 0.8470 0.0545 0.0544 7.943 33.377 15.006 5923.250 3.771 66.746 1.149 0.86 377908. 0.1866
|
|
175.79 0.8840 0.8520 0.0470 0.0487 7.120 29.919 12.941 5309.648 3.380 57.563 1.105 0.87 379883. 0.1667
|
|
183.43 0.9224 0.8477 0.0393 0.0428 6.250 26.263 10.832 4660.778 2.967 48.181 1.054 0.87 381926. 0.1454
|
|
191.08 0.9608 0.8304 0.0315 0.0365 5.331 22.401 8.689 3975.386 2.531 38.649 0.991 0.87 384035. 0.1225
|
|
198.72 0.9993 0.7898 0.0237 0.0300 4.375 18.385 6.521 3262.657 2.077 29.006 0.907 0.87 386209. 0.0970
|
|
206.36 1.0377 0.7029 0.0158 0.0233 3.397 14.275 4.339 2533.332 1.613 19.301 0.777 0.88 388448. 0.0678
|
|
214.01 1.0761 0.5106 0.0078 0.0165 2.414 10.141 2.160 1799.763 1.146 9.606 0.544 0.88 390749. 0.0335
|
|
221.65 1.1146 0.0001 0.0000 0.0099 1.440 6.052 0.000 1074.045 0.684 0.001 0.000 0.88 393089. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 16000
|
|
|
|
V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
|
|
(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
|
|
0.00 0.0000 0.0000 0.1171 0.0692 12.262 48.305 36.689 9144.051 5.457 163.191 1.820 0.89 377149. 0.4620
|
|
8.18 0.0386 0.0640 0.1169 0.0705 12.494 49.219 36.622 9317.058 5.561 162.895 1.783 0.89 377522. 0.4522
|
|
16.37 0.0772 0.1251 0.1166 0.0719 12.754 50.240 36.556 9510.429 5.676 162.602 1.743 0.89 377952. 0.4418
|
|
24.55 0.1158 0.1832 0.1164 0.0736 13.042 51.374 36.490 9725.117 5.804 162.305 1.702 0.89 378444. 0.4309
|
|
32.74 0.1543 0.2380 0.1162 0.0753 13.356 52.613 36.418 9959.547 5.944 161.987 1.659 0.89 379003. 0.4195
|
|
40.92 0.1929 0.2896 0.1159 0.0772 13.692 53.938 36.335 10210.462 6.094 161.618 1.614 0.89 379633. 0.4078
|
|
49.11 0.2315 0.3378 0.1156 0.0792 14.044 55.322 36.231 10472.363 6.250 161.157 1.569 0.89 380337. 0.3959
|
|
57.29 0.2701 0.3830 0.1152 0.0812 14.399 56.720 36.094 10737.050 6.408 160.545 1.525 0.89 381119. 0.3839
|
|
65.48 0.3087 0.4252 0.1146 0.0832 14.742 58.075 35.905 10993.459 6.561 159.705 1.481 0.89 381984. 0.3720
|
|
73.66 0.3473 0.4650 0.1137 0.0849 15.057 59.314 35.644 11228.164 6.701 158.545 1.440 0.89 382934. 0.3603
|
|
81.85 0.3858 0.5026 0.1126 0.0864 15.323 60.362 35.287 11426.424 6.820 156.958 1.401 0.90 383972. 0.3487
|
|
90.03 0.4244 0.5384 0.1111 0.0876 15.520 61.138 34.809 11573.438 6.907 154.832 1.364 0.90 385101. 0.3373
|
|
98.21 0.4630 0.5728 0.1091 0.0882 15.630 61.570 34.184 11655.206 6.956 152.052 1.330 0.90 386321. 0.3260
|
|
106.40 0.5016 0.6059 0.1065 0.0882 15.632 61.580 33.385 11656.976 6.957 148.496 1.299 0.90 387632. 0.3146
|
|
114.58 0.5402 0.6379 0.1033 0.0875 15.514 61.113 32.388 11568.540 6.904 144.064 1.270 0.90 389034. 0.3029
|
|
122.77 0.5788 0.6687 0.0995 0.0861 15.261 60.118 31.174 11380.282 6.792 138.664 1.242 0.90 390525. 0.2908
|
|
130.95 0.6174 0.6983 0.0949 0.0839 14.869 58.571 29.733 11087.512 6.617 132.251 1.216 0.91 392103. 0.2780
|
|
139.14 0.6559 0.7264 0.0896 0.0809 14.339 56.484 28.072 10692.380 6.382 124.862 1.191 0.91 393765. 0.2644
|
|
147.32 0.6945 0.7527 0.0836 0.0772 13.682 53.899 26.216 10202.950 6.089 116.609 1.165 0.91 395509. 0.2501
|
|
155.51 0.7331 0.7770 0.0772 0.0728 12.913 50.869 24.198 9629.365 5.747 107.634 1.140 0.91 397333. 0.2350
|
|
163.69 0.7717 0.7990 0.0704 0.0679 12.045 47.450 22.050 8982.256 5.361 98.080 1.113 0.91 399234. 0.2191
|
|
171.88 0.8103 0.8183 0.0632 0.0626 11.090 43.685 19.799 8269.464 4.935 88.065 1.086 0.92 401212. 0.2025
|
|
180.06 0.8489 0.8328 0.0557 0.0568 10.067 39.657 17.462 7507.025 4.480 77.669 1.055 0.92 403264. 0.1848
|
|
188.25 0.8874 0.8411 0.0480 0.0507 8.985 35.396 15.056 6700.475 3.999 66.967 1.019 0.92 405389. 0.1657
|
|
196.43 0.9260 0.8289 0.0401 0.0448 7.947 31.305 12.575 5925.926 3.537 55.936 0.963 0.93 407586. 0.1431
|
|
204.61 0.9646 0.7970 0.0321 0.0388 6.882 27.109 10.052 5131.781 3.063 44.713 0.888 0.93 409854. 0.1181
|
|
212.80 1.0032 0.7340 0.0239 0.0327 5.802 22.858 7.506 4326.915 2.582 33.385 0.787 0.93 412191. 0.0903
|
|
220.98 1.0418 0.6180 0.0158 0.0267 4.729 18.628 4.960 3526.230 2.105 22.061 0.638 0.94 414598. 0.0595
|
|
229.17 1.0804 0.4061 0.0078 0.0208 3.680 14.496 2.445 2744.100 1.638 10.877 0.404 0.94 417071. 0.0265
|
|
237.35 1.1189 -0.0027 0.0000 0.0151 2.674 10.532 -0.011 1993.643 1.190 -0.050 -0.003 0.94 419600. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 17000
|
|
|
|
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 0.1147 0.0760 16.160 59.915 40.597 12050.647 6.769 180.576 1.528 0.94 400798. 0.4081
|
|
8.78 0.0389 0.0578 0.1145 0.0771 16.400 60.802 40.506 12229.116 6.869 180.168 1.502 0.94 401198. 0.4007
|
|
17.55 0.0779 0.1134 0.1142 0.0784 16.674 61.820 40.417 12433.848 6.984 179.773 1.474 0.94 401660. 0.3928
|
|
26.33 0.1168 0.1667 0.1140 0.0799 16.984 62.968 40.329 12664.745 7.114 179.381 1.444 0.94 402190. 0.3844
|
|
35.10 0.1558 0.2174 0.1137 0.0815 17.327 64.240 40.238 12920.569 7.258 178.978 1.413 0.95 402791. 0.3755
|
|
43.88 0.1947 0.2654 0.1134 0.0832 17.699 65.621 40.139 13198.319 7.414 178.538 1.379 0.95 403468. 0.3663
|
|
52.66 0.2336 0.3106 0.1131 0.0851 18.094 67.084 40.024 13492.557 7.579 178.025 1.345 0.95 404226. 0.3567
|
|
61.43 0.2726 0.3531 0.1127 0.0870 18.499 68.587 39.880 13794.958 7.749 177.385 1.311 0.95 405068. 0.3470
|
|
70.21 0.3115 0.3932 0.1122 0.0889 18.900 70.074 39.691 14093.955 7.917 176.545 1.277 0.95 405997. 0.3373
|
|
78.99 0.3505 0.4309 0.1115 0.0907 19.277 71.471 39.437 14374.987 8.075 175.415 1.244 0.95 407017. 0.3275
|
|
87.76 0.3894 0.4666 0.1105 0.0922 19.607 72.696 39.093 14621.255 8.213 173.884 1.213 0.95 408130. 0.3178
|
|
96.54 0.4283 0.5005 0.1092 0.0934 19.867 73.658 38.631 14814.769 8.322 171.829 1.183 0.95 409339. 0.3081
|
|
105.31 0.4673 0.5331 0.1075 0.0942 20.028 74.256 38.019 14935.077 8.389 169.107 1.155 0.95 410646. 0.2984
|
|
114.09 0.5062 0.5643 0.1052 0.0944 20.070 74.411 37.228 14966.368 8.407 165.588 1.128 0.96 412051. 0.2885
|
|
122.87 0.5452 0.5943 0.1024 0.0939 19.971 74.045 36.227 14892.663 8.366 161.138 1.103 0.96 413554. 0.2783
|
|
131.64 0.5841 0.6231 0.0989 0.0927 19.710 73.075 34.988 14697.613 8.256 155.628 1.080 0.96 415154. 0.2677
|
|
140.42 0.6230 0.6508 0.0947 0.0906 19.267 71.435 33.491 14367.771 8.071 148.969 1.057 0.96 416849. 0.2564
|
|
149.19 0.6620 0.6775 0.0897 0.0876 18.634 69.088 31.735 13895.722 7.806 141.156 1.036 0.96 418637. 0.2446
|
|
157.97 0.7009 0.7033 0.0840 0.0838 17.809 66.027 29.735 13279.968 7.460 132.260 1.016 0.97 420516. 0.2321
|
|
166.75 0.7398 0.7284 0.0778 0.0790 16.796 62.274 27.517 12525.076 7.036 122.394 0.996 0.97 422484. 0.2191
|
|
175.52 0.7788 0.7525 0.0710 0.0735 15.620 57.911 25.114 11647.543 6.543 111.707 0.978 0.97 424539. 0.2054
|
|
184.30 0.8177 0.7750 0.0638 0.0673 14.307 53.046 22.562 10669.054 5.993 100.356 0.959 0.98 426677. 0.1910
|
|
193.07 0.8567 0.7940 0.0562 0.0607 12.897 47.815 19.889 9616.948 5.402 88.466 0.938 0.98 428896. 0.1753
|
|
201.85 0.8956 0.8061 0.0484 0.0538 11.431 42.382 17.119 8524.274 4.788 76.145 0.911 0.98 431195. 0.1580
|
|
210.63 0.9345 0.7880 0.0402 0.0477 10.147 37.622 14.237 7566.858 4.250 63.324 0.853 0.98 433570. 0.1349
|
|
219.40 0.9735 0.7346 0.0319 0.0423 8.995 33.350 11.294 6707.593 3.768 50.236 0.764 0.99 436022. 0.1076
|
|
228.18 1.0124 0.6469 0.0236 0.0370 7.866 29.163 8.363 5865.608 3.295 37.197 0.647 0.99 438547. 0.0784
|
|
236.96 1.0514 0.5096 0.0155 0.0319 6.784 25.153 5.472 5058.925 2.842 24.338 0.491 1.00 441146. 0.0481
|
|
245.73 1.0903 0.3021 0.0075 0.0271 5.770 21.393 2.660 4302.808 2.417 11.832 0.280 1.00 443816. 0.0192
|
|
254.51 1.1292 -0.0052 -0.0001 0.0227 4.834 17.923 -0.037 3604.905 2.025 -0.166 -0.005 1.00 446560. 0.0000
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