464 lines
82 KiB
Plaintext
464 lines
82 KiB
Plaintext
20x10E (20x10E.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 0.0824 0.0303 0.008 0.491 0.420 5.814 0.056 1.869 32.782 0.08 36690. 0.6235
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0.42 0.0222 0.0588 0.0810 0.0306 0.008 0.496 0.413 5.869 0.056 1.838 31.929 0.08 36711. 0.6021
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0.84 0.0444 0.1145 0.0795 0.0308 0.008 0.500 0.406 5.919 0.057 1.804 31.079 0.08 36734. 0.5807
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1.26 0.0666 0.1671 0.0779 0.0311 0.008 0.504 0.397 5.962 0.057 1.768 30.235 0.08 36759. 0.5592
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1.68 0.0887 0.2166 0.0762 0.0312 0.008 0.507 0.389 5.998 0.057 1.729 29.397 0.08 36786. 0.5377
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2.10 0.1109 0.2631 0.0744 0.0314 0.008 0.509 0.380 6.026 0.058 1.688 28.566 0.08 36814. 0.5163
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2.52 0.1331 0.3066 0.0725 0.0315 0.008 0.511 0.370 6.043 0.058 1.644 27.743 0.08 36845. 0.4949
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2.94 0.1553 0.3472 0.0704 0.0315 0.008 0.511 0.359 6.049 0.058 1.598 26.928 0.08 36877. 0.4735
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3.36 0.1775 0.3849 0.0683 0.0315 0.008 0.511 0.348 6.043 0.058 1.548 26.121 0.08 36912. 0.4521
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3.78 0.1997 0.4198 0.0659 0.0314 0.008 0.509 0.336 6.023 0.058 1.496 25.322 0.08 36949. 0.4308
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4.20 0.2218 0.4518 0.0635 0.0312 0.008 0.506 0.324 5.988 0.057 1.440 24.528 0.08 36988. 0.4095
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4.62 0.2440 0.4810 0.0609 0.0309 0.008 0.502 0.311 5.936 0.057 1.382 23.738 0.08 37030. 0.3882
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5.04 0.2662 0.5073 0.0582 0.0305 0.008 0.496 0.297 5.866 0.056 1.320 22.951 0.08 37074. 0.3668
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5.46 0.2884 0.5307 0.0554 0.0301 0.008 0.488 0.282 5.778 0.055 1.256 22.162 0.08 37120. 0.3455
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5.88 0.3106 0.5511 0.0524 0.0295 0.008 0.479 0.267 5.671 0.054 1.188 21.369 0.08 37168. 0.3241
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6.30 0.3328 0.5683 0.0493 0.0289 0.007 0.469 0.251 5.545 0.053 1.118 20.568 0.08 37219. 0.3026
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6.72 0.3550 0.5821 0.0461 0.0281 0.007 0.456 0.235 5.401 0.052 1.046 19.752 0.08 37272. 0.2810
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7.14 0.3771 0.5923 0.0428 0.0273 0.007 0.443 0.218 5.238 0.050 0.972 18.915 0.08 37328. 0.2594
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7.56 0.3993 0.5985 0.0395 0.0263 0.007 0.427 0.201 5.058 0.048 0.895 18.050 0.08 37386. 0.2376
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7.98 0.4215 0.6002 0.0360 0.0253 0.007 0.411 0.184 4.859 0.046 0.817 17.149 0.08 37447. 0.2156
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8.40 0.4437 0.5968 0.0325 0.0242 0.006 0.392 0.166 4.643 0.044 0.738 16.199 0.08 37510. 0.1935
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8.82 0.4659 0.5874 0.0290 0.0230 0.006 0.373 0.148 4.410 0.042 0.657 15.186 0.08 37576. 0.1712
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9.24 0.4881 0.5711 0.0253 0.0217 0.006 0.352 0.129 4.160 0.040 0.575 14.093 0.08 37644. 0.1486
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9.66 0.5102 0.5462 0.0217 0.0203 0.005 0.329 0.111 3.894 0.037 0.492 12.893 0.08 37715. 0.1258
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10.08 0.5324 0.5108 0.0180 0.0188 0.005 0.305 0.092 3.613 0.034 0.409 11.555 0.08 37788. 0.1028
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10.50 0.5546 0.4619 0.0144 0.0173 0.004 0.280 0.073 3.317 0.032 0.326 10.032 0.08 37864. 0.0797
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10.92 0.5768 0.3954 0.0107 0.0157 0.004 0.254 0.055 3.008 0.029 0.244 8.255 0.08 37943. 0.0567
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11.34 0.5990 0.3047 0.0071 0.0140 0.004 0.227 0.036 2.688 0.026 0.161 6.126 0.08 38024. 0.0342
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11.76 0.6212 0.1797 0.0036 0.0123 0.003 0.199 0.018 2.358 0.023 0.081 3.485 0.08 38107. 0.0138
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12.18 0.6434 0.0031 0.0001 0.0105 0.003 0.171 0.000 2.020 0.019 0.001 0.059 0.08 38192. 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 0.0828 0.0280 0.058 1.817 1.688 42.995 0.205 7.507 17.805 0.16 73378. 0.6786
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0.84 0.0223 0.0641 0.0814 0.0283 0.058 1.838 1.659 43.480 0.208 7.381 17.310 0.16 73421. 0.6542
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1.69 0.0446 0.1246 0.0799 0.0286 0.059 1.856 1.629 43.926 0.210 7.246 16.820 0.16 73468. 0.6298
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2.53 0.0669 0.1815 0.0783 0.0289 0.059 1.873 1.596 44.320 0.212 7.100 16.337 0.16 73518. 0.6056
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3.38 0.0892 0.2349 0.0766 0.0291 0.060 1.887 1.561 44.655 0.213 6.945 15.860 0.16 73571. 0.5814
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4.22 0.1115 0.2849 0.0747 0.0292 0.060 1.898 1.524 44.918 0.214 6.779 15.390 0.16 73629. 0.5574
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5.07 0.1338 0.3317 0.0728 0.0294 0.060 1.906 1.484 45.100 0.215 6.603 14.929 0.16 73691. 0.5336
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5.91 0.1561 0.3752 0.0707 0.0294 0.061 1.910 1.442 45.188 0.216 6.415 14.476 0.16 73757. 0.5100
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6.76 0.1784 0.4156 0.0685 0.0294 0.061 1.909 1.397 45.173 0.216 6.215 14.030 0.16 73827. 0.4866
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7.60 0.2007 0.4530 0.0662 0.0293 0.060 1.904 1.350 45.043 0.215 6.004 13.592 0.16 73901. 0.4633
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8.45 0.2230 0.4874 0.0637 0.0292 0.060 1.893 1.300 44.786 0.214 5.781 13.162 0.16 73980. 0.4402
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9.29 0.2453 0.5188 0.0611 0.0289 0.060 1.876 1.247 44.391 0.212 5.545 12.737 0.16 74064. 0.4172
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10.14 0.2676 0.5474 0.0584 0.0285 0.059 1.853 1.191 43.845 0.209 5.296 12.318 0.16 74152. 0.3944
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10.98 0.2899 0.5730 0.0555 0.0281 0.058 1.823 1.132 43.142 0.206 5.036 11.903 0.16 74245. 0.3716
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11.83 0.3122 0.5956 0.0525 0.0275 0.057 1.787 1.071 42.280 0.202 4.764 11.490 0.16 74343. 0.3489
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12.67 0.3345 0.6152 0.0494 0.0269 0.055 1.744 1.008 41.258 0.197 4.482 11.077 0.16 74446. 0.3262
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13.51 0.3568 0.6316 0.0462 0.0261 0.054 1.694 0.942 40.078 0.191 4.190 10.660 0.16 74554. 0.3035
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14.36 0.3791 0.6445 0.0429 0.0252 0.052 1.637 0.874 38.740 0.185 3.890 10.238 0.16 74666. 0.2809
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15.20 0.4014 0.6536 0.0395 0.0242 0.050 1.574 0.805 37.244 0.178 3.582 9.806 0.16 74784. 0.2582
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16.05 0.4237 0.6585 0.0360 0.0232 0.048 1.504 0.734 35.594 0.170 3.267 9.360 0.16 74906. 0.2353
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16.89 0.4460 0.6585 0.0325 0.0220 0.045 1.428 0.662 33.789 0.161 2.946 8.892 0.16 75034. 0.2123
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17.74 0.4683 0.6529 0.0289 0.0207 0.043 1.345 0.589 31.834 0.152 2.621 8.396 0.16 75166. 0.1891
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18.58 0.4906 0.6404 0.0253 0.0194 0.040 1.257 0.515 29.733 0.142 2.292 7.861 0.16 75304. 0.1656
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19.43 0.5129 0.6193 0.0216 0.0179 0.037 1.162 0.441 27.491 0.131 1.960 7.272 0.16 75447. 0.1416
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20.27 0.5352 0.5872 0.0179 0.0163 0.034 1.061 0.366 25.115 0.120 1.627 6.608 0.16 75595. 0.1173
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21.12 0.5575 0.5403 0.0143 0.0147 0.030 0.956 0.291 22.614 0.108 1.294 5.837 0.16 75748. 0.0924
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21.96 0.5798 0.4727 0.0106 0.0130 0.027 0.845 0.217 19.999 0.095 0.963 4.910 0.16 75907. 0.0670
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22.81 0.6021 0.3745 0.0070 0.0113 0.023 0.730 0.143 17.283 0.083 0.635 3.746 0.16 76070. 0.0415
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23.65 0.6244 0.2277 0.0034 0.0094 0.019 0.612 0.070 14.483 0.069 0.312 2.196 0.16 76239. 0.0171
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24.49 0.6467 -0.0050 -0.0001 0.0076 0.016 0.490 -0.001 11.605 0.055 -0.005 -0.047 0.16 76409. 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 0.0831 0.0271 0.188 3.956 3.816 140.398 0.447 16.971 12.326 0.24 110064. 0.7064
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1.28 0.0226 0.0673 0.0817 0.0274 0.191 4.004 3.751 142.127 0.452 16.684 11.971 0.24 110130. 0.6802
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2.56 0.0451 0.1306 0.0802 0.0277 0.193 4.049 3.682 143.717 0.457 16.376 11.619 0.24 110201. 0.6541
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3.84 0.0677 0.1900 0.0786 0.0280 0.195 4.089 3.607 145.131 0.462 16.045 11.273 0.24 110277. 0.6281
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5.13 0.0902 0.2457 0.0769 0.0282 0.196 4.123 3.527 146.333 0.466 15.690 10.933 0.24 110359. 0.6024
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6.41 0.1128 0.2978 0.0750 0.0284 0.198 4.150 3.442 147.286 0.469 15.311 10.600 0.24 110447. 0.5770
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7.69 0.1353 0.3464 0.0730 0.0285 0.198 4.168 3.351 147.951 0.471 14.906 10.274 0.24 110541. 0.5518
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8.97 0.1579 0.3915 0.0709 0.0286 0.199 4.178 3.254 148.287 0.472 14.476 9.954 0.24 110641. 0.5268
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10.25 0.1805 0.4334 0.0687 0.0286 0.199 4.177 3.152 148.257 0.472 14.018 9.642 0.24 110748. 0.5022
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11.53 0.2030 0.4721 0.0663 0.0285 0.198 4.165 3.043 147.818 0.471 13.533 9.336 0.24 110862. 0.4778
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12.82 0.2256 0.5077 0.0638 0.0283 0.197 4.140 2.927 146.931 0.468 13.020 9.036 0.24 110983. 0.4536
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14.10 0.2481 0.5403 0.0611 0.0281 0.195 4.101 2.805 145.551 0.463 12.479 8.742 0.24 111111. 0.4296
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15.38 0.2707 0.5700 0.0583 0.0277 0.193 4.047 2.677 143.636 0.457 11.908 8.454 0.24 111246. 0.4058
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16.66 0.2932 0.5967 0.0554 0.0272 0.189 3.977 2.542 141.163 0.449 11.308 8.169 0.24 111389. 0.3821
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17.94 0.3158 0.6204 0.0523 0.0266 0.185 3.892 2.402 138.125 0.440 10.683 7.887 0.24 111539. 0.3586
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19.22 0.3384 0.6411 0.0492 0.0259 0.180 3.790 2.256 134.521 0.428 10.035 7.607 0.24 111696. 0.3352
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20.51 0.3609 0.6586 0.0459 0.0251 0.175 3.673 2.105 130.352 0.415 9.364 7.326 0.24 111861. 0.3118
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21.79 0.3835 0.6726 0.0425 0.0242 0.168 3.539 1.950 125.618 0.400 8.675 7.042 0.24 112033. 0.2885
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23.07 0.4060 0.6829 0.0390 0.0232 0.161 3.390 1.791 120.324 0.383 7.968 6.753 0.24 112213. 0.2651
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24.35 0.4286 0.6891 0.0355 0.0221 0.154 3.225 1.629 114.473 0.364 7.246 6.455 0.24 112400. 0.2417
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25.63 0.4511 0.6904 0.0319 0.0208 0.145 3.045 1.464 108.074 0.344 6.511 6.143 0.24 112596. 0.2181
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26.91 0.4737 0.6859 0.0282 0.0195 0.136 2.849 1.296 101.138 0.322 5.766 5.813 0.24 112799. 0.1942
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28.20 0.4963 0.6744 0.0246 0.0181 0.126 2.639 1.127 93.680 0.298 5.012 5.456 0.24 113010. 0.1699
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29.48 0.5188 0.6540 0.0208 0.0165 0.115 2.415 0.956 85.720 0.273 4.254 5.060 0.24 113229. 0.1452
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30.76 0.5414 0.6215 0.0171 0.0149 0.104 2.177 0.785 77.286 0.246 3.493 4.609 0.24 113456. 0.1198
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32.04 0.5639 0.5724 0.0134 0.0132 0.092 1.927 0.615 68.412 0.218 2.734 4.075 0.24 113690. 0.0937
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33.32 0.5865 0.4986 0.0097 0.0114 0.079 1.666 0.445 59.140 0.188 1.979 3.413 0.24 113933. 0.0668
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34.60 0.6090 0.3855 0.0060 0.0096 0.066 1.395 0.277 49.524 0.158 1.234 2.541 0.24 114184. 0.0393
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35.89 0.6316 0.2032 0.0025 0.0076 0.053 1.116 0.113 39.621 0.126 0.502 1.292 0.24 114442. 0.0127
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37.17 0.6542
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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 0.0837 0.0267 0.439 6.923 6.825 327.652 0.782 30.357 9.448 0.32 146747. 0.7241
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1.69 0.0223 0.0680 0.0823 0.0270 0.445 7.012 6.711 331.826 0.792 29.852 9.174 0.32 146834. 0.6972
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3.38 0.0447 0.1321 0.0808 0.0273 0.450 7.093 6.589 335.675 0.801 29.309 8.904 0.32 146927. 0.6705
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5.07 0.0670 0.1922 0.0792 0.0276 0.455 7.166 6.458 339.112 0.810 28.726 8.638 0.32 147028. 0.6440
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6.77 0.0893 0.2485 0.0774 0.0278 0.459 7.228 6.318 342.055 0.817 28.102 8.378 0.32 147136. 0.6178
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8.46 0.1116 0.3012 0.0756 0.0280 0.462 7.278 6.168 344.414 0.822 27.436 8.123 0.32 147252. 0.5919
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10.15 0.1340 0.3503 0.0736 0.0282 0.464 7.313 6.008 346.099 0.826 26.724 7.874 0.32 147376. 0.5662
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11.84 0.1563 0.3961 0.0716 0.0282 0.465 7.333 5.838 347.017 0.828 25.967 7.630 0.32 147508. 0.5409
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13.53 0.1786 0.4386 0.0693 0.0282 0.465 7.334 5.657 347.074 0.829 25.162 7.393 0.32 147649. 0.5159
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15.22 0.2010 0.4779 0.0670 0.0282 0.464 7.315 5.465 346.177 0.826 24.310 7.161 0.32 147799. 0.4911
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16.92 0.2233 0.5142 0.0645 0.0280 0.462 7.274 5.263 344.230 0.822 23.408 6.934 0.32 147958. 0.4667
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18.61 0.2456 0.5475 0.0619 0.0278 0.457 7.208 5.048 341.131 0.814 22.455 6.712 0.32 148126. 0.4425
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20.30 0.2679 0.5780 0.0591 0.0274 0.452 7.116 4.823 336.777 0.804 21.451 6.495 0.32 148304. 0.4185
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21.99 0.2903 0.6056 0.0562 0.0269 0.444 6.996 4.586 331.104 0.790 20.397 6.282 0.32 148491. 0.3946
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23.68 0.3126 0.6303 0.0532 0.0264 0.435 6.848 4.338 324.093 0.774 19.296 6.071 0.32 148687. 0.3710
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25.37 0.3349 0.6522 0.0500 0.0257 0.423 6.672 4.081 315.738 0.754 18.154 5.863 0.32 148894. 0.3475
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27.07 0.3573 0.6710 0.0468 0.0249 0.410 6.467 3.816 306.036 0.731 16.973 5.655 0.32 149110. 0.3241
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28.76 0.3796 0.6867 0.0434 0.0240 0.396 6.233 3.543 294.992 0.704 15.757 5.447 0.32 149336. 0.3008
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30.45 0.4019 0.6989 0.0400 0.0230 0.379 5.972 3.262 282.608 0.675 14.510 5.236 0.32 149572. 0.2774
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32.14 0.4242 0.7072 0.0365 0.0219 0.361 5.682 2.976 268.897 0.642 13.236 5.019 0.32 149818. 0.2540
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33.83 0.4466 0.7112 0.0329 0.0207 0.340 5.364 2.684 253.872 0.606 11.939 4.795 0.32 150074. 0.2305
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35.52 0.4689 0.7101 0.0293 0.0193 0.319 5.020 2.388 237.559 0.567 10.622 4.559 0.32 150340. 0.2067
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37.21 0.4912 0.7026 0.0256 0.0179 0.295 4.649 2.089 219.990 0.525 9.290 4.306 0.32 150616. 0.1826
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38.91 0.5136 0.6871 0.0219 0.0164 0.270 4.252 1.787 201.212 0.480 7.949 4.028 0.32 150903. 0.1580
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40.60 0.5359 0.6609 0.0182 0.0148 0.243 3.831 1.484 181.282 0.433 6.602 3.713 0.32 151200. 0.1327
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42.29 0.5582 0.6199 0.0145 0.0130 0.215 3.387 1.182 160.280 0.383 5.256 3.344 0.32 151507. 0.1066
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43.98 0.5805 0.5568 0.0108 0.0113 0.185 2.922 0.881 138.300 0.330 3.917 2.888 0.32 151825. 0.0795
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45.67 0.6029 0.4583 0.0071 0.0094 0.155 2.440 0.583 115.462 0.276 2.592 2.289 0.32 152153. 0.0513
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47.36 0.6252 0.2968 0.0036 0.0075 0.123 1.942 0.290 91.903 0.219 1.288 1.430 0.32 152490. 0.0226
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49.06 0.6475 0.0025 0.0000 0.0055 0.091 1.430 0.002 67.654 0.162 0.008 0.012 0.32 152830. 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 0.0843 0.0265 0.853 10.758 10.748 636.388 1.215 47.805 7.660 0.40 183425. 0.7367
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2.11 0.0223 0.0689 0.0829 0.0269 0.865 10.899 10.570 644.728 1.231 47.015 7.436 0.40 183534. 0.7093
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4.23 0.0447 0.1338 0.0814 0.0272 0.875 11.029 10.379 652.421 1.246 46.165 7.216 0.40 183651. 0.6820
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6.34 0.0670 0.1946 0.0798 0.0275 0.884 11.145 10.174 659.299 1.259 45.253 6.999 0.40 183777. 0.6550
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8.46 0.0893 0.2517 0.0781 0.0277 0.892 11.245 9.954 665.195 1.270 44.275 6.787 0.40 183913. 0.6282
|
|
10.57 0.1116 0.3050 0.0762 0.0279 0.898 11.325 9.719 669.933 1.279 43.230 6.580 0.40 184058. 0.6018
|
|
12.69 0.1340 0.3547 0.0743 0.0281 0.903 11.382 9.468 673.331 1.286 42.114 6.378 0.40 184214. 0.5758
|
|
14.80 0.1563 0.4010 0.0722 0.0281 0.905 11.414 9.201 675.205 1.290 40.925 6.181 0.40 184380. 0.5500
|
|
16.92 0.1786 0.4441 0.0699 0.0281 0.906 11.417 8.917 675.369 1.290 39.661 5.988 0.40 184556. 0.5246
|
|
19.03 0.2010 0.4839 0.0676 0.0281 0.903 11.387 8.615 673.635 1.287 38.321 5.801 0.40 184744. 0.4995
|
|
21.14 0.2233 0.5208 0.0651 0.0279 0.898 11.323 8.296 669.815 1.279 36.903 5.618 0.40 184943. 0.4747
|
|
23.26 0.2456 0.5547 0.0624 0.0277 0.890 11.220 7.960 663.705 1.268 35.404 5.440 0.40 185154. 0.4502
|
|
25.37 0.2679 0.5857 0.0597 0.0273 0.879 11.074 7.604 655.100 1.251 33.824 5.265 0.40 185376. 0.4260
|
|
27.49 0.2903 0.6139 0.0567 0.0268 0.863 10.884 7.231 643.870 1.230 32.165 5.094 0.40 185610. 0.4019
|
|
29.60 0.3126 0.6393 0.0537 0.0262 0.845 10.649 6.842 629.970 1.203 30.432 4.926 0.40 185856. 0.3780
|
|
31.72 0.3349 0.6618 0.0505 0.0256 0.823 10.369 6.437 613.388 1.171 28.632 4.760 0.40 186115. 0.3543
|
|
33.83 0.3573 0.6815 0.0472 0.0248 0.797 10.043 6.019 594.119 1.135 26.771 4.595 0.40 186385. 0.3307
|
|
35.95 0.3796 0.6980 0.0438 0.0238 0.767 9.672 5.588 572.166 1.093 24.855 4.430 0.40 186668. 0.3072
|
|
38.06 0.4019 0.7113 0.0404 0.0228 0.734 9.256 5.146 547.539 1.046 22.889 4.263 0.40 186963. 0.2837
|
|
40.17 0.4242 0.7208 0.0368 0.0217 0.698 8.795 4.694 520.257 0.994 20.881 4.093 0.40 187271. 0.2602
|
|
42.29 0.4466 0.7262 0.0332 0.0204 0.658 8.289 4.234 490.350 0.937 18.835 3.917 0.40 187591. 0.2365
|
|
44.40 0.4689 0.7265 0.0296 0.0191 0.614 7.740 3.768 457.866 0.874 16.758 3.732 0.40 187924. 0.2125
|
|
46.52 0.4912 0.7208 0.0259 0.0176 0.567 7.148 3.295 422.871 0.808 14.658 3.535 0.40 188270. 0.1882
|
|
48.63 0.5136 0.7074 0.0221 0.0161 0.517 6.516 2.820 385.454 0.736 12.541 3.318 0.40 188628. 0.1634
|
|
50.75 0.5359 0.6835 0.0184 0.0144 0.464 5.845 2.342 345.737 0.660 10.417 3.072 0.40 188999. 0.1379
|
|
52.86 0.5582 0.6449 0.0146 0.0127 0.407 5.137 1.864 303.873 0.580 8.293 2.783 0.40 189383. 0.1115
|
|
54.98 0.5805 0.5841 0.0109 0.0108 0.349 4.396 1.390 260.055 0.497 6.181 2.424 0.40 189781. 0.0838
|
|
57.09 0.6029 0.4867 0.0072 0.0089 0.288 3.626 0.920 214.524 0.410 4.091 1.945 0.40 190191. 0.0547
|
|
59.20 0.6252 0.3216 0.0036 0.0070 0.225 2.832 0.458 167.557 0.320 2.036 1.239 0.40 190613. 0.0246
|
|
61.32 0.6475 0.0035 0.0000 0.0050 0.160 2.015 0.003 119.187 0.228 0.015 0.013 0.41 191036. 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 0.0851 0.0266 1.477 15.517 15.627 1101.501 1.753 69.510 6.435 0.48 220097. 0.7463
|
|
2.54 0.0223 0.0695 0.0837 0.0269 1.497 15.724 15.371 1116.232 1.777 68.372 6.246 0.48 220228. 0.7184
|
|
5.08 0.0447 0.1349 0.0822 0.0272 1.515 15.916 15.096 1129.822 1.798 67.146 6.060 0.48 220369. 0.6908
|
|
7.62 0.0670 0.1963 0.0806 0.0275 1.531 16.087 14.799 1141.972 1.818 65.828 5.878 0.48 220521. 0.6634
|
|
10.15 0.0894 0.2537 0.0789 0.0278 1.545 16.234 14.482 1152.385 1.834 64.414 5.700 0.48 220684. 0.6364
|
|
12.69 0.1117 0.3075 0.0770 0.0280 1.557 16.352 14.141 1160.751 1.847 62.901 5.526 0.48 220860. 0.6096
|
|
15.23 0.1340 0.3577 0.0751 0.0281 1.565 16.436 13.778 1166.750 1.857 61.284 5.356 0.48 221047. 0.5833
|
|
17.77 0.1564 0.4044 0.0729 0.0282 1.569 16.483 13.390 1170.055 1.862 59.560 5.191 0.48 221247. 0.5573
|
|
20.31 0.1787 0.4478 0.0707 0.0282 1.569 16.487 12.978 1170.337 1.863 57.727 5.030 0.48 221460. 0.5316
|
|
22.85 0.2011 0.4881 0.0683 0.0281 1.565 16.443 12.541 1167.266 1.858 55.781 4.873 0.48 221686. 0.5063
|
|
25.39 0.2234 0.5254 0.0658 0.0280 1.556 16.348 12.078 1160.513 1.847 53.721 4.720 0.48 221926. 0.4813
|
|
27.93 0.2457 0.5597 0.0631 0.0277 1.542 16.196 11.588 1149.720 1.830 51.544 4.572 0.48 222179. 0.4566
|
|
30.46 0.2681 0.5911 0.0603 0.0274 1.521 15.982 11.071 1134.524 1.806 49.246 4.426 0.48 222447. 0.4321
|
|
33.00 0.2904 0.6198 0.0574 0.0269 1.495 15.703 10.529 1114.689 1.774 46.832 4.284 0.48 222729. 0.4078
|
|
35.54 0.3128 0.6458 0.0543 0.0263 1.462 15.357 9.962 1090.130 1.735 44.309 4.145 0.48 223025. 0.3838
|
|
38.08 0.3351 0.6690 0.0511 0.0256 1.423 14.944 9.372 1060.825 1.688 41.688 4.007 0.48 223336. 0.3599
|
|
40.62 0.3574 0.6893 0.0477 0.0248 1.377 14.464 8.763 1026.766 1.634 38.977 3.871 0.48 223662. 0.3362
|
|
43.16 0.3798 0.7066 0.0443 0.0238 1.325 13.917 8.135 987.958 1.572 36.184 3.735 0.48 224002. 0.3125
|
|
45.70 0.4021 0.7207 0.0408 0.0228 1.266 13.304 7.491 944.418 1.503 33.319 3.598 0.48 224357. 0.2889
|
|
48.23 0.4245 0.7312 0.0372 0.0216 1.202 12.625 6.832 896.179 1.426 30.390 3.458 0.48 224727. 0.2652
|
|
50.77 0.4468 0.7377 0.0336 0.0203 1.131 11.880 6.161 843.296 1.342 27.406 3.314 0.48 225112. 0.2413
|
|
53.31 0.4691 0.7393 0.0299 0.0189 1.054 11.070 5.481 785.851 1.251 24.377 3.163 0.48 225512. 0.2173
|
|
55.85 0.4915 0.7350 0.0261 0.0175 0.971 10.199 4.792 723.963 1.152 21.313 3.002 0.48 225927. 0.1928
|
|
58.39 0.5138 0.7232 0.0223 0.0159 0.882 9.266 4.097 657.792 1.047 18.225 2.825 0.48 226358. 0.1678
|
|
60.93 0.5362 0.7012 0.0185 0.0142 0.788 8.277 3.400 587.553 0.935 15.125 2.625 0.48 226804. 0.1420
|
|
63.47 0.5585 0.6645 0.0147 0.0124 0.689 7.234 2.704 513.520 0.817 12.027 2.388 0.48 227266. 0.1152
|
|
66.01 0.5808 0.6053 0.0110 0.0105 0.585 6.143 2.011 436.040 0.694 8.945 2.092 0.48 227743. 0.0870
|
|
68.54 0.6032 0.5082 0.0072 0.0086 0.477 5.009 1.326 355.540 0.566 5.896 1.691 0.48 228236. 0.0571
|
|
71.08 0.6255 0.3379 0.0035 0.0066 0.365 3.839 0.651 272.520 0.434 2.898 1.084 0.49 228743. 0.0257
|
|
73.62 0.6479 -0.0096 -0.0001 0.0045 0.251 2.633 -0.012 186.891 0.297 -0.054 -0.030 0.49 229247. 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 0.0862 0.0268 2.364 21.286 21.524 1762.842 2.405 95.740 5.538 0.56 256760. 0.7538
|
|
2.96 0.0223 0.0697 0.0848 0.0271 2.396 21.574 21.177 1786.736 2.437 94.194 5.376 0.56 256913. 0.7258
|
|
5.91 0.0446 0.1352 0.0833 0.0275 2.426 21.840 20.802 1808.773 2.468 92.525 5.216 0.56 257078. 0.6980
|
|
8.87 0.0669 0.1968 0.0816 0.0278 2.452 22.078 20.398 1828.469 2.494 90.730 5.060 0.56 257256. 0.6705
|
|
11.83 0.0892 0.2544 0.0799 0.0280 2.475 22.282 19.965 1845.346 2.517 88.803 4.907 0.56 257447. 0.6433
|
|
14.78 0.1115 0.3084 0.0780 0.0282 2.493 22.446 19.500 1858.898 2.536 86.737 4.758 0.56 257652. 0.6164
|
|
17.74 0.1338 0.3588 0.0761 0.0284 2.506 22.563 19.004 1868.608 2.549 84.528 4.613 0.56 257871. 0.5899
|
|
20.70 0.1561 0.4057 0.0739 0.0285 2.513 22.627 18.474 1873.949 2.556 82.170 4.471 0.56 258105. 0.5638
|
|
23.66 0.1784 0.4494 0.0717 0.0285 2.514 22.633 17.909 1874.389 2.557 79.660 4.334 0.56 258354. 0.5381
|
|
26.61 0.2007 0.4900 0.0693 0.0284 2.507 22.572 17.310 1869.398 2.550 76.995 4.200 0.56 258618. 0.5126
|
|
29.57 0.2230 0.5276 0.0667 0.0282 2.492 22.440 16.675 1858.441 2.535 74.170 4.070 0.56 258898. 0.4876
|
|
32.53 0.2453 0.5622 0.0641 0.0280 2.469 22.229 16.003 1840.957 2.511 71.183 3.943 0.56 259194. 0.4628
|
|
35.48 0.2676 0.5941 0.0612 0.0276 2.436 21.932 15.294 1816.353 2.478 68.029 3.819 0.56 259507. 0.4382
|
|
38.44 0.2900 0.6233 0.0582 0.0271 2.393 21.544 14.549 1784.229 2.434 64.713 3.698 0.56 259836. 0.4139
|
|
41.40 0.3123 0.6497 0.0551 0.0265 2.339 21.063 13.769 1744.438 2.380 61.245 3.580 0.56 260181. 0.3897
|
|
44.35 0.3346 0.6735 0.0519 0.0258 2.276 20.490 12.958 1696.943 2.315 57.639 3.464 0.56 260544. 0.3658
|
|
47.31 0.3569 0.6945 0.0485 0.0249 2.202 19.823 12.119 1641.733 2.240 53.907 3.348 0.56 260923. 0.3420
|
|
50.27 0.3792 0.7126 0.0450 0.0240 2.117 19.064 11.255 1578.819 2.154 50.062 3.233 0.56 261320. 0.3182
|
|
53.23 0.4015 0.7275 0.0415 0.0229 2.023 18.211 10.368 1508.230 2.058 46.115 3.118 0.56 261734. 0.2945
|
|
56.18 0.4238 0.7390 0.0379 0.0217 1.918 17.267 9.460 1430.015 1.951 42.078 3.000 0.56 262165. 0.2708
|
|
59.14 0.4461 0.7466 0.0342 0.0204 1.803 16.232 8.535 1344.267 1.834 37.964 2.880 0.56 262613. 0.2468
|
|
62.10 0.4684 0.7496 0.0304 0.0190 1.678 15.107 7.596 1251.120 1.707 33.786 2.754 0.56 263079. 0.2227
|
|
65.05 0.4907 0.7470 0.0266 0.0175 1.543 13.895 6.645 1150.761 1.570 29.558 2.619 0.56 263563. 0.1981
|
|
68.01 0.5130 0.7371 0.0228 0.0158 1.399 12.599 5.687 1043.452 1.423 25.296 2.472 0.56 264064. 0.1730
|
|
70.97 0.5353 0.7173 0.0189 0.0141 1.247 11.224 4.725 929.534 1.268 21.015 2.305 0.56 264584. 0.1470
|
|
73.92 0.5576 0.6833 0.0151 0.0123 1.085 9.774 3.763 809.453 1.104 16.736 2.108 0.56 265121. 0.1200
|
|
76.88 0.5799 0.6272 0.0112 0.0104 0.917 8.256 2.805 683.770 0.933 12.477 1.861 0.56 265676. 0.0914
|
|
79.84 0.6022 0.5331 0.0074 0.0084 0.742 6.679 1.858 553.180 0.755 8.263 1.523 0.57 266249. 0.0609
|
|
82.79 0.6245 0.3642 0.0037 0.0064 0.561 5.053 0.926 418.495 0.571 4.118 1.003 0.57 266840. 0.0283
|
|
85.75 0.6468 0.0054 0.0000 0.0042 0.375 3.377 0.009 279.713 0.382 0.040 0.014 0.57 267428. 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 0.0874 0.0271 3.577 28.185 28.520 2667.741 3.184 126.857 4.849 0.63 293412. 0.7597
|
|
3.38 0.0223 0.0697 0.0860 0.0275 3.627 28.572 28.067 2704.346 3.228 124.841 4.707 0.63 293588. 0.7316
|
|
6.76 0.0446 0.1353 0.0845 0.0278 3.672 28.929 27.577 2738.085 3.268 122.661 4.568 0.63 293778. 0.7038
|
|
10.14 0.0669 0.1969 0.0829 0.0282 3.712 29.247 27.049 2768.211 3.304 120.313 4.432 0.63 293982. 0.6762
|
|
13.51 0.0892 0.2547 0.0811 0.0284 3.747 29.519 26.481 2793.982 3.335 117.786 4.299 0.63 294202. 0.6490
|
|
16.89 0.1115 0.3088 0.0793 0.0286 3.774 29.737 25.871 2814.630 3.360 115.074 4.169 0.64 294437. 0.6221
|
|
20.27 0.1338 0.3593 0.0773 0.0288 3.794 29.893 25.218 2829.363 3.377 112.169 4.043 0.64 294689. 0.5956
|
|
23.65 0.1561 0.4064 0.0751 0.0289 3.805 29.978 24.520 2837.361 3.387 109.066 3.920 0.64 294957. 0.5694
|
|
27.03 0.1784 0.4503 0.0729 0.0289 3.806 29.982 23.776 2837.821 3.387 105.757 3.800 0.64 295243. 0.5436
|
|
30.41 0.2007 0.4911 0.0704 0.0288 3.795 29.899 22.985 2829.932 3.378 102.239 3.684 0.64 295546. 0.5182
|
|
33.79 0.2230 0.5289 0.0679 0.0286 3.772 29.719 22.147 2812.881 3.358 98.508 3.571 0.64 295867. 0.4930
|
|
37.16 0.2453 0.5639 0.0651 0.0283 3.736 29.433 21.259 2785.823 3.325 94.559 3.461 0.64 296207. 0.4682
|
|
40.54 0.2676 0.5962 0.0623 0.0279 3.685 29.032 20.320 2747.856 3.280 90.385 3.354 0.64 296565. 0.4436
|
|
43.92 0.2899 0.6257 0.0592 0.0274 3.619 28.509 19.333 2698.346 3.221 85.992 3.250 0.64 296943. 0.4192
|
|
47.30 0.3122 0.6527 0.0561 0.0268 3.536 27.861 18.299 2637.052 3.148 81.395 3.147 0.64 297339. 0.3950
|
|
50.68 0.3345 0.6770 0.0528 0.0261 3.438 27.089 17.224 2563.921 3.060 76.611 3.047 0.64 297754. 0.3710
|
|
54.06 0.3568 0.6985 0.0494 0.0252 3.324 26.191 16.110 2478.947 2.959 71.657 2.948 0.64 298189. 0.3471
|
|
57.44 0.3791 0.7173 0.0458 0.0242 3.195 25.168 14.961 2382.150 2.843 66.548 2.849 0.64 298643. 0.3233
|
|
60.82 0.4014 0.7330 0.0422 0.0231 3.049 24.021 13.782 2273.580 2.714 61.302 2.749 0.64 299117. 0.2995
|
|
64.19 0.4237 0.7454 0.0385 0.0219 2.888 22.751 12.575 2153.323 2.570 55.934 2.649 0.64 299610. 0.2756
|
|
67.57 0.4460 0.7540 0.0348 0.0206 2.711 21.358 11.345 2021.519 2.413 50.461 2.545 0.64 300124. 0.2515
|
|
70.95 0.4683 0.7582 0.0309 0.0191 2.519 19.846 10.095 1878.376 2.242 44.901 2.438 0.64 300657. 0.2272
|
|
74.33 0.4906 0.7569 0.0271 0.0175 2.312 18.217 8.829 1724.187 2.058 39.272 2.323 0.64 301210. 0.2025
|
|
77.71 0.5129 0.7484 0.0231 0.0159 2.091 16.475 7.553 1559.352 1.861 33.595 2.197 0.64 301783. 0.1771
|
|
81.09 0.5352 0.7303 0.0192 0.0141 1.857 14.627 6.271 1384.403 1.653 27.893 2.055 0.64 302377. 0.1509
|
|
84.47 0.5575 0.6982 0.0153 0.0122 1.609 12.679 4.989 1200.023 1.432 22.190 1.886 0.64 302991. 0.1236
|
|
87.84 0.5798 0.6439 0.0114 0.0102 1.351 10.640 3.713 1007.081 1.202 16.514 1.672 0.65 303626. 0.0945
|
|
91.22 0.6021 0.5509 0.0075 0.0082 1.082 8.523 2.450 806.655 0.963 10.896 1.377 0.65 304281. 0.0632
|
|
94.60 0.6244 0.3785 0.0037 0.0061 0.805 6.339 1.207 600.007 0.716 5.370 0.913 0.65 304955. 0.0294
|
|
97.98 0.6467 -0.0085 -0.0001 0.0039 0.519 4.087 -0.017 386.793 0.462 -0.075 -0.020 0.65 305622. 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 0.0889 0.0277 5.202 36.430 36.725 3879.085 4.116 163.355 4.294 0.71 330049. 0.7635
|
|
3.80 0.0223 0.0694 0.0875 0.0281 5.273 36.924 36.155 3931.738 4.172 160.819 4.171 0.71 330248. 0.7358
|
|
7.59 0.0445 0.1348 0.0860 0.0284 5.338 37.381 35.537 3980.397 4.223 158.071 4.050 0.71 330462. 0.7082
|
|
11.39 0.0668 0.1962 0.0844 0.0287 5.396 37.790 34.870 4023.937 4.270 155.101 3.930 0.71 330693. 0.6809
|
|
15.18 0.0891 0.2539 0.0827 0.0290 5.446 38.141 34.150 4061.246 4.309 151.899 3.814 0.71 330942. 0.6539
|
|
18.98 0.1114 0.3079 0.0808 0.0292 5.486 38.421 33.376 4091.128 4.341 148.454 3.700 0.71 331208. 0.6272
|
|
22.78 0.1336 0.3584 0.0788 0.0294 5.515 38.621 32.544 4112.371 4.363 144.758 3.589 0.71 331492. 0.6008
|
|
26.57 0.1559 0.4056 0.0766 0.0295 5.530 38.728 31.655 4123.744 4.375 140.800 3.482 0.71 331796. 0.5747
|
|
30.37 0.1782 0.4496 0.0743 0.0295 5.530 38.730 30.705 4124.011 4.376 136.575 3.377 0.72 332118. 0.5490
|
|
34.17 0.2004 0.4906 0.0719 0.0294 5.514 38.617 29.693 4111.994 4.363 132.076 3.275 0.72 332461. 0.5236
|
|
37.96 0.2227 0.5286 0.0693 0.0292 5.480 38.378 28.619 4086.516 4.336 127.297 3.176 0.72 332824. 0.4985
|
|
41.76 0.2450 0.5639 0.0665 0.0289 5.426 38.001 27.480 4046.354 4.293 122.233 3.080 0.72 333207. 0.4738
|
|
45.55 0.2673 0.5965 0.0636 0.0285 5.351 37.474 26.276 3990.224 4.234 116.876 2.987 0.72 333612. 0.4492
|
|
49.35 0.2895 0.6265 0.0605 0.0280 5.253 36.787 25.007 3917.130 4.156 111.231 2.896 0.72 334037. 0.4248
|
|
53.15 0.3118 0.6539 0.0573 0.0273 5.132 35.938 23.677 3826.712 4.060 105.315 2.806 0.72 334484. 0.4006
|
|
56.94 0.3341 0.6787 0.0540 0.0266 4.987 34.925 22.292 3718.889 3.946 99.153 2.719 0.72 334952. 0.3766
|
|
60.74 0.3563 0.7009 0.0505 0.0257 4.819 33.750 20.856 3593.672 3.813 92.766 2.632 0.72 335442. 0.3527
|
|
64.54 0.3786 0.7204 0.0469 0.0247 4.628 32.411 19.374 3451.104 3.662 86.175 2.546 0.72 335953. 0.3288
|
|
68.33 0.4009 0.7369 0.0432 0.0235 4.414 30.910 17.851 3291.270 3.492 79.401 2.460 0.72 336487. 0.3049
|
|
72.13 0.4232 0.7503 0.0394 0.0222 4.176 29.248 16.292 3114.312 3.304 72.465 2.373 0.72 337042. 0.2810
|
|
75.92 0.4454 0.7600 0.0356 0.0209 3.916 27.427 14.701 2920.446 3.099 65.390 2.283 0.72 337619. 0.2568
|
|
79.72 0.4677 0.7653 0.0317 0.0194 3.634 25.451 13.084 2710.017 2.875 58.197 2.190 0.72 338219. 0.2324
|
|
83.52 0.4900 0.7654 0.0277 0.0177 3.330 23.324 11.446 2483.501 2.635 50.911 2.090 0.72 338841. 0.2075
|
|
87.31 0.5122 0.7585 0.0237 0.0160 3.006 21.051 9.793 2241.561 2.378 43.559 1.982 0.72 339485. 0.1819
|
|
91.11 0.5345 0.7421 0.0197 0.0142 2.662 18.642 8.131 1985.064 2.106 36.169 1.858 0.72 340152. 0.1554
|
|
94.91 0.5568 0.7118 0.0157 0.0123 2.300 16.108 6.469 1715.163 1.820 28.774 1.711 0.73 340842. 0.1277
|
|
98.70 0.5790 0.6591 0.0117 0.0102 1.922 13.461 4.814 1433.328 1.521 21.412 1.523 0.73 341555. 0.0981
|
|
102.50 0.6013 0.5669 0.0077 0.0082 1.531 10.719 3.175 1141.396 1.211 14.121 1.262 0.73 342290. 0.0659
|
|
106.29 0.6236 0.3921 0.0038 0.0060 1.129 7.903 1.561 841.541 0.893 6.945 0.842 0.73 343048. 0.0309
|
|
110.09 0.6459 -0.0121 -0.0001 0.0038 0.715 5.009 -0.030 533.339 0.566 -0.132 -0.025 0.73 343794. 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 0.0908 0.0293 7.546 47.562 46.284 5627.127 5.374 205.870 3.731 0.79 366665. 0.7446
|
|
4.21 0.0222 0.0671 0.0894 0.0296 7.621 48.037 45.591 5683.297 5.427 202.787 3.638 0.79 366887. 0.7208
|
|
8.42 0.0445 0.1309 0.0879 0.0299 7.690 48.467 44.836 5734.206 5.476 199.431 3.546 0.79 367127. 0.6967
|
|
12.63 0.0667 0.1913 0.0863 0.0301 7.749 48.841 44.018 5778.498 5.518 195.791 3.455 0.79 367385. 0.6725
|
|
16.84 0.0889 0.2484 0.0846 0.0303 7.798 49.148 43.132 5814.812 5.553 191.853 3.364 0.79 367662. 0.6483
|
|
21.05 0.1111 0.3022 0.0827 0.0304 7.834 49.375 42.177 5841.702 5.578 187.602 3.275 0.79 367960. 0.6239
|
|
25.26 0.1334 0.3528 0.0807 0.0305 7.855 49.511 41.148 5857.678 5.594 183.026 3.186 0.79 368277. 0.5996
|
|
29.47 0.1556 0.4003 0.0785 0.0305 7.860 49.540 40.044 5861.143 5.597 178.114 3.099 0.79 368616. 0.5753
|
|
33.68 0.1778 0.4448 0.0762 0.0305 7.846 49.450 38.861 5850.472 5.587 172.855 3.013 0.79 368976. 0.5510
|
|
37.89 0.2000 0.4864 0.0737 0.0303 7.810 49.226 37.600 5824.008 5.562 167.243 2.928 0.79 369359. 0.5268
|
|
42.10 0.2223 0.5251 0.0711 0.0301 7.751 48.854 36.257 5780.035 5.520 161.270 2.845 0.80 369763. 0.5026
|
|
46.31 0.2445 0.5610 0.0683 0.0298 7.666 48.319 34.831 5716.763 5.459 154.930 2.764 0.80 370191. 0.4785
|
|
50.52 0.2667 0.5943 0.0653 0.0293 7.553 47.605 33.321 5632.213 5.378 148.212 2.683 0.80 370642. 0.4544
|
|
54.73 0.2889 0.6249 0.0622 0.0288 7.409 46.696 31.727 5524.713 5.276 141.120 2.605 0.80 371116. 0.4304
|
|
58.93 0.3112 0.6530 0.0589 0.0281 7.233 45.589 30.053 5393.723 5.151 133.677 2.527 0.80 371613. 0.4065
|
|
63.14 0.3334 0.6784 0.0555 0.0273 7.025 44.281 28.307 5238.908 5.003 125.910 2.451 0.80 372134. 0.3825
|
|
67.35 0.3556 0.7012 0.0520 0.0264 6.786 42.770 26.495 5060.239 4.832 117.850 2.375 0.80 372679. 0.3586
|
|
71.56 0.3779 0.7213 0.0483 0.0253 6.514 41.058 24.623 4857.632 4.639 109.523 2.299 0.80 373248. 0.3347
|
|
75.77 0.4001 0.7384 0.0445 0.0241 6.211 39.144 22.697 4631.232 4.423 100.956 2.223 0.80 373841. 0.3107
|
|
79.98 0.4223 0.7522 0.0406 0.0228 5.876 37.034 20.723 4381.558 4.184 92.176 2.145 0.80 374458. 0.2865
|
|
84.19 0.4445 0.7621 0.0367 0.0214 5.511 34.732 18.707 4109.217 3.924 83.210 2.065 0.80 375099. 0.2620
|
|
88.40 0.4668 0.7675 0.0327 0.0199 5.116 32.246 16.656 3815.072 3.643 74.088 1.980 0.80 375764. 0.2371
|
|
92.61 0.4890 0.7669 0.0286 0.0182 4.694 29.586 14.577 3500.316 3.343 64.838 1.889 0.80 376454. 0.2116
|
|
96.82 0.5112 0.7586 0.0245 0.0165 4.246 26.764 12.477 3166.499 3.024 55.496 1.787 0.80 377169. 0.1852
|
|
101.03 0.5334 0.7394 0.0203 0.0147 3.776 23.797 10.363 2815.517 2.689 46.095 1.669 0.80 377909. 0.1577
|
|
105.24 0.5557 0.7044 0.0162 0.0128 3.285 20.706 8.246 2449.770 2.339 36.679 1.527 0.81 378673. 0.1286
|
|
109.45 0.5779 0.6444 0.0120 0.0108 2.779 17.514 6.136 2072.163 1.979 27.292 1.343 0.81 379463. 0.0976
|
|
113.66 0.6001 0.5420 0.0079 0.0088 2.261 14.251 4.044 1686.065 1.610 17.987 1.088 0.81 380278. 0.0642
|
|
117.87 0.6224 0.3587 0.0039 0.0067 1.737 10.948 1.982 1295.260 1.237 8.817 0.694 0.81 381116. 0.0287
|
|
122.08 0.6446 -0.0140 -0.0001 0.0047 1.206 7.600 -0.052 899.185 0.859 -0.230 -0.026 0.81 381946. 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 0.0928 0.0341 11.689 66.974 57.261 8716.244 7.567 254.697 2.980 0.87 403258. 0.6615
|
|
4.63 0.0222 0.0595 0.0915 0.0342 11.717 67.137 56.450 8737.453 7.585 251.089 2.930 0.87 403504. 0.6459
|
|
9.27 0.0445 0.1170 0.0901 0.0342 11.732 67.225 55.562 8748.799 7.595 247.139 2.881 0.87 403769. 0.6299
|
|
13.90 0.0667 0.1724 0.0885 0.0342 11.733 67.226 54.593 8748.939 7.595 242.828 2.830 0.87 404055. 0.6135
|
|
18.53 0.0889 0.2258 0.0868 0.0342 11.716 67.131 53.538 8736.588 7.584 238.138 2.779 0.87 404363. 0.5967
|
|
23.16 0.1112 0.2770 0.0849 0.0341 11.681 66.929 52.394 8710.378 7.562 233.048 2.728 0.87 404692. 0.5794
|
|
27.80 0.1334 0.3262 0.0829 0.0339 11.625 66.610 51.156 8668.859 7.526 227.543 2.677 0.87 405045. 0.5616
|
|
32.43 0.1557 0.3731 0.0808 0.0337 11.547 66.162 49.822 8610.550 7.475 221.606 2.624 0.87 405421. 0.5435
|
|
37.06 0.1779 0.4178 0.0784 0.0334 11.444 65.573 48.387 8533.872 7.408 215.224 2.572 0.87 405821. 0.5248
|
|
41.69 0.2001 0.4603 0.0759 0.0330 11.314 64.830 46.849 8437.219 7.324 208.385 2.519 0.87 406245. 0.5057
|
|
46.33 0.2224 0.5006 0.0733 0.0325 11.156 63.922 45.207 8318.979 7.222 201.081 2.465 0.87 406694. 0.4862
|
|
50.96 0.2446 0.5385 0.0704 0.0320 10.966 62.834 43.459 8177.393 7.099 193.304 2.410 0.88 407168. 0.4662
|
|
55.59 0.2668 0.5741 0.0674 0.0313 10.742 61.551 41.602 8010.435 6.954 185.044 2.356 0.88 407668. 0.4457
|
|
60.22 0.2891 0.6073 0.0642 0.0306 10.482 60.058 39.636 7816.124 6.785 176.299 2.300 0.88 408194. 0.4248
|
|
64.86 0.3113 0.6380 0.0609 0.0297 10.183 58.349 37.567 7593.681 6.592 167.099 2.244 0.88 408745. 0.4035
|
|
69.49 0.3335 0.6660 0.0574 0.0287 9.851 56.443 35.405 7345.705 6.377 157.479 2.186 0.88 409322. 0.3816
|
|
74.12 0.3558 0.6907 0.0537 0.0277 9.487 54.359 33.156 7074.390 6.141 147.476 2.126 0.88 409925. 0.3591
|
|
78.75 0.3780 0.7120 0.0500 0.0265 9.092 52.098 30.828 6780.127 5.886 137.123 2.062 0.88 410555. 0.3359
|
|
83.39 0.4003 0.7294 0.0461 0.0253 8.666 49.657 28.430 6462.504 5.610 126.456 1.995 0.88 411210. 0.3121
|
|
88.02 0.4225 0.7416 0.0421 0.0240 8.219 47.093 25.968 6128.800 5.321 115.505 1.922 0.88 411892. 0.2873
|
|
92.65 0.4447 0.7478 0.0380 0.0226 7.747 44.391 23.451 5777.241 5.015 104.308 1.841 0.88 412600. 0.2616
|
|
97.28 0.4670 0.7478 0.0339 0.0211 7.246 41.518 20.887 5403.255 4.691 92.906 1.753 0.88 413335. 0.2351
|
|
101.92 0.4892 0.7398 0.0296 0.0196 6.718 38.491 18.287 5009.331 4.349 81.339 1.656 0.88 414097. 0.2077
|
|
106.55 0.5114 0.7214 0.0254 0.0180 6.167 35.339 15.659 4599.103 3.993 69.651 1.544 0.88 414886. 0.1793
|
|
111.18 0.5337 0.6889 0.0211 0.0163 5.601 32.094 13.015 4176.796 3.626 57.890 1.413 0.89 415701. 0.1496
|
|
115.81 0.5559 0.6372 0.0168 0.0147 5.024 28.787 10.366 3746.373 3.252 46.108 1.255 0.89 416544. 0.1185
|
|
120.45 0.5781 0.5586 0.0125 0.0130 4.442 25.454 7.726 3312.681 2.876 34.366 1.058 0.89 417414. 0.0863
|
|
125.08 0.6004 0.4412 0.0083 0.0113 3.863 22.137 5.111 2880.990 2.501 22.733 0.805 0.89 418312. 0.0534
|
|
129.71 0.6226 0.2664 0.0041 0.0096 3.294 18.874 2.537 2456.315 2.132 11.284 0.468 0.89 419236. 0.0219
|
|
134.34 0.6448 0.0004 0.0000 0.0080 2.729 15.638 0.003 2035.142 1.767 0.013 0.001 0.89 420166. 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 0.0931 0.0415 18.485 97.090 68.375 13784.325 10.969 304.132 2.250 0.95 439899. 0.5458
|
|
5.22 0.0230 0.0507 0.0920 0.0416 18.516 97.252 67.525 13807.237 10.987 300.352 2.218 0.95 440169. 0.5348
|
|
10.44 0.0459 0.1001 0.0907 0.0416 18.515 97.246 66.576 13806.416 10.987 296.131 2.187 0.95 440463. 0.5236
|
|
15.65 0.0689 0.1480 0.0892 0.0415 18.477 97.048 65.521 13778.317 10.964 291.435 2.157 0.95 440782. 0.5122
|
|
20.87 0.0918 0.1946 0.0876 0.0413 18.399 96.636 64.350 13719.780 10.918 286.229 2.127 0.95 441126. 0.5007
|
|
26.09 0.1148 0.2400 0.0859 0.0411 18.276 95.990 63.057 13628.090 10.845 280.477 2.099 0.95 441498. 0.4889
|
|
31.31 0.1377 0.2842 0.0839 0.0407 18.105 95.095 61.634 13501.052 10.744 274.148 2.071 0.95 441897. 0.4769
|
|
36.52 0.1607 0.3271 0.0818 0.0402 17.885 93.939 60.076 13336.946 10.613 267.216 2.043 0.95 442324. 0.4646
|
|
41.74 0.1837 0.3689 0.0795 0.0396 17.614 92.514 58.376 13134.556 10.452 259.658 2.016 0.95 442780. 0.4519
|
|
46.96 0.2066 0.4094 0.0770 0.0389 17.290 90.812 56.532 12893.009 10.260 251.455 1.989 0.95 443266. 0.4387
|
|
52.18 0.2296 0.4487 0.0743 0.0380 16.913 88.831 54.540 12611.728 10.036 242.594 1.961 0.95 443781. 0.4250
|
|
57.39 0.2525 0.4865 0.0714 0.0370 16.482 86.568 52.397 12290.398 9.780 233.064 1.934 0.96 444327. 0.4107
|
|
62.61 0.2755 0.5229 0.0682 0.0359 15.996 84.019 50.101 11928.511 9.492 222.851 1.905 0.96 444902. 0.3956
|
|
67.83 0.2984 0.5576 0.0649 0.0347 15.457 81.185 47.655 11526.234 9.172 211.969 1.875 0.96 445509. 0.3798
|
|
73.05 0.3214 0.5905 0.0614 0.0334 14.866 78.080 45.068 11085.279 8.821 200.464 1.844 0.96 446145. 0.3632
|
|
78.26 0.3444 0.6214 0.0577 0.0320 14.225 74.716 42.354 10607.685 8.441 188.393 1.811 0.96 446812. 0.3458
|
|
83.48 0.3673 0.6488 0.0538 0.0305 13.560 71.222 39.523 10111.736 8.047 175.798 1.773 0.96 447510. 0.3270
|
|
88.70 0.3903 0.6721 0.0498 0.0289 12.874 67.620 36.585 9600.329 7.640 162.730 1.728 0.96 448237. 0.3067
|
|
93.92 0.4132 0.6903 0.0457 0.0274 12.173 63.935 33.553 9077.081 7.223 149.245 1.677 0.96 448996. 0.2849
|
|
99.13 0.4362 0.7007 0.0415 0.0258 11.482 60.310 30.438 8562.419 6.814 135.389 1.612 0.96 449784. 0.2610
|
|
104.35 0.4591 0.6941 0.0371 0.0245 10.920 57.356 27.240 8143.127 6.480 121.163 1.517 0.96 450604. 0.2323
|
|
109.57 0.4821 0.6766 0.0327 0.0233 10.359 54.407 23.987 7724.392 6.147 106.696 1.409 0.96 451454. 0.2024
|
|
114.79 0.5051 0.6472 0.0282 0.0220 9.789 51.413 20.698 7299.377 5.809 92.067 1.286 0.96 452335. 0.1717
|
|
120.00 0.5280 0.6038 0.0237 0.0207 9.217 48.412 17.392 6873.240 5.470 77.361 1.148 0.97 453247. 0.1404
|
|
125.22 0.5510 0.5438 0.0192 0.0194 8.652 45.443 14.090 6451.703 5.134 62.670 0.991 0.97 454190. 0.1091
|
|
130.44 0.5739 0.4643 0.0147 0.0182 8.101 42.549 10.814 6040.898 4.807 48.099 0.812 0.97 455165. 0.0783
|
|
135.66 0.5969 0.3628 0.0103 0.0170 7.569 39.756 7.591 5644.271 4.492 33.765 0.610 0.97 456172. 0.0493
|
|
140.87 0.6198 0.2367 0.0061 0.0159 7.060 37.080 4.448 5264.472 4.189 19.783 0.383 0.97 457214. 0.0237
|
|
146.09 0.6428 0.0826 0.0019 0.0148 6.567 34.494 1.393 4897.273 3.897 6.196 0.129 0.97 458298. 0.0045
|
|
151.31 0.6658
|
|
|
|
|
|
|