427 lines
76 KiB
Plaintext
427 lines
76 KiB
Plaintext
22x10 (22x10.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 0.0731 0.0266 0.011 0.694 0.545 8.211 0.078 2.426 30.131 0.09 37865. 0.5935
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0.46 0.0219 0.0586 0.0718 0.0269 0.011 0.702 0.536 8.305 0.079 2.385 29.285 0.09 37885. 0.5720
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0.91 0.0439 0.1139 0.0705 0.0271 0.011 0.709 0.526 8.392 0.080 2.341 28.445 0.09 37907. 0.5504
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1.37 0.0658 0.1659 0.0691 0.0274 0.011 0.716 0.516 8.468 0.081 2.293 27.613 0.09 37931. 0.5288
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1.83 0.0877 0.2146 0.0675 0.0276 0.011 0.721 0.504 8.532 0.081 2.241 26.790 0.09 37956. 0.5072
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2.28 0.1096 0.2601 0.0658 0.0277 0.012 0.725 0.491 8.582 0.082 2.186 25.977 0.09 37984. 0.4857
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2.74 0.1316 0.3025 0.0641 0.0279 0.012 0.728 0.478 8.616 0.082 2.127 25.174 0.09 38013. 0.4643
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3.20 0.1535 0.3418 0.0622 0.0279 0.012 0.730 0.464 8.633 0.082 2.064 24.382 0.09 38045. 0.4430
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3.65 0.1754 0.3781 0.0602 0.0279 0.012 0.729 0.449 8.631 0.082 1.998 23.601 0.09 38079. 0.4218
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4.11 0.1973 0.4115 0.0580 0.0278 0.012 0.728 0.433 8.609 0.082 1.927 22.829 0.09 38115. 0.4008
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4.57 0.2193 0.4419 0.0558 0.0277 0.011 0.724 0.417 8.566 0.082 1.853 22.065 0.09 38153. 0.3799
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5.02 0.2412 0.4694 0.0535 0.0275 0.011 0.718 0.399 8.500 0.081 1.776 21.308 0.09 38193. 0.3591
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5.48 0.2631 0.4940 0.0511 0.0272 0.011 0.711 0.381 8.412 0.080 1.696 20.557 0.09 38236. 0.3385
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5.94 0.2850 0.5157 0.0486 0.0268 0.011 0.701 0.362 8.299 0.079 1.612 19.809 0.09 38281. 0.3181
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6.40 0.3070 0.5344 0.0459 0.0264 0.011 0.690 0.343 8.162 0.078 1.526 19.061 0.09 38329. 0.2977
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6.85 0.3289 0.5501 0.0433 0.0259 0.011 0.676 0.323 7.999 0.076 1.436 18.311 0.09 38379. 0.2775
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7.31 0.3508 0.5625 0.0405 0.0253 0.010 0.660 0.302 7.811 0.075 1.345 17.554 0.09 38431. 0.2574
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7.77 0.3728 0.5715 0.0377 0.0246 0.010 0.642 0.281 7.595 0.073 1.250 16.787 0.09 38486. 0.2374
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8.22 0.3947 0.5768 0.0347 0.0238 0.010 0.621 0.259 7.352 0.070 1.154 16.002 0.09 38543. 0.2174
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8.68 0.4166 0.5781 0.0318 0.0229 0.009 0.598 0.237 7.081 0.068 1.055 15.193 0.09 38603. 0.1974
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9.14 0.4385 0.5748 0.0287 0.0219 0.009 0.573 0.215 6.782 0.065 0.954 14.351 0.09 38666. 0.1773
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9.59 0.4605 0.5662 0.0257 0.0209 0.009 0.545 0.192 6.454 0.062 0.852 13.463 0.09 38731. 0.1572
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10.05 0.4824 0.5513 0.0225 0.0197 0.008 0.515 0.168 6.097 0.058 0.748 12.513 0.09 38799. 0.1369
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10.51 0.5043 0.5287 0.0194 0.0185 0.008 0.483 0.145 5.711 0.055 0.643 11.479 0.09 38869. 0.1164
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10.96 0.5262 0.4965 0.0162 0.0171 0.007 0.448 0.121 5.297 0.051 0.537 10.329 0.09 38942. 0.0957
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11.42 0.5482 0.4515 0.0129 0.0157 0.007 0.410 0.097 4.855 0.046 0.429 9.019 0.09 39017. 0.0747
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11.88 0.5701 0.3895 0.0097 0.0142 0.006 0.371 0.072 4.384 0.042 0.322 7.480 0.09 39096. 0.0536
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12.33 0.5920 0.3030 0.0064 0.0126 0.005 0.329 0.048 3.888 0.037 0.214 5.604 0.09 39176. 0.0328
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12.79 0.6139 0.1797 0.0032 0.0109 0.005 0.284 0.024 3.365 0.032 0.106 3.205 0.09 39259. 0.0132
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13.25 0.6359 -0.0050 -0.0001 0.0091 0.004 0.238 -0.001 2.815 0.027 -0.002 -0.087 0.09 39342. 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 0.0735 0.0238 0.079 2.487 2.194 58.848 0.281 9.758 16.909 0.17 75728. 0.6680
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0.93 0.0224 0.0669 0.0722 0.0241 0.080 2.523 2.156 59.696 0.285 9.592 16.384 0.17 75770. 0.6417
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1.86 0.0447 0.1296 0.0709 0.0244 0.081 2.556 2.116 60.478 0.289 9.411 15.868 0.17 75814. 0.6156
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2.80 0.0671 0.1882 0.0694 0.0247 0.082 2.585 2.072 61.177 0.292 9.215 15.361 0.17 75863. 0.5897
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3.73 0.0894 0.2429 0.0678 0.0250 0.083 2.611 2.024 61.775 0.295 9.005 14.864 0.17 75916. 0.5641
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4.66 0.1118 0.2936 0.0661 0.0252 0.083 2.631 1.974 62.255 0.297 8.778 14.378 0.17 75972. 0.5387
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5.59 0.1342 0.3407 0.0643 0.0253 0.084 2.646 1.919 62.602 0.299 8.536 13.904 0.17 76033. 0.5137
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6.52 0.1565 0.3843 0.0623 0.0254 0.084 2.654 1.861 62.800 0.300 8.277 13.440 0.17 76098. 0.4890
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7.45 0.1789 0.4244 0.0603 0.0254 0.084 2.656 1.799 62.837 0.300 8.003 12.988 0.17 76168. 0.4646
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8.39 0.2012 0.4612 0.0581 0.0253 0.084 2.650 1.734 62.700 0.299 7.714 12.545 0.17 76242. 0.4406
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9.32 0.2236 0.4948 0.0558 0.0252 0.084 2.636 1.666 62.381 0.298 7.410 12.113 0.17 76321. 0.4170
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10.25 0.2460 0.5252 0.0534 0.0250 0.083 2.615 1.594 61.869 0.295 7.092 11.689 0.18 76404. 0.3937
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11.18 0.2683 0.5525 0.0509 0.0247 0.082 2.584 1.520 61.155 0.292 6.761 11.273 0.18 76492. 0.3707
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12.11 0.2907 0.5768 0.0483 0.0243 0.081 2.545 1.443 60.231 0.288 6.416 10.863 0.18 76586. 0.3480
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13.04 0.3131 0.5980 0.0456 0.0239 0.079 2.497 1.362 59.089 0.282 6.060 10.458 0.18 76684. 0.3256
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13.98 0.3354 0.6161 0.0429 0.0233 0.077 2.439 1.280 57.722 0.276 5.692 10.056 0.18 76787. 0.3034
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14.91 0.3578 0.6310 0.0400 0.0227 0.075 2.372 1.195 56.124 0.268 5.314 9.655 0.18 76896. 0.2815
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15.84 0.3801 0.6425 0.0371 0.0219 0.073 2.294 1.107 54.288 0.259 4.926 9.253 0.18 77010. 0.2597
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16.77 0.4025 0.6503 0.0341 0.0211 0.070 2.206 1.018 52.210 0.249 4.529 8.845 0.18 77128. 0.2380
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17.70 0.4249 0.6541 0.0310 0.0202 0.067 2.108 0.927 49.883 0.238 4.123 8.428 0.18 77253. 0.2164
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18.63 0.4472 0.6532 0.0279 0.0191 0.063 1.999 0.834 47.306 0.226 3.710 7.996 0.18 77382. 0.1948
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19.57 0.4696 0.6469 0.0248 0.0180 0.060 1.880 0.740 44.474 0.212 3.289 7.542 0.18 77517. 0.1730
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20.50 0.4919 0.6339 0.0216 0.0167 0.056 1.749 0.644 41.387 0.198 2.863 7.054 0.18 77658. 0.1509
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21.43 0.5143 0.6123 0.0183 0.0154 0.051 1.608 0.547 38.045 0.182 2.432 6.518 0.18 77804. 0.1285
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22.36 0.5367 0.5793 0.0150 0.0139 0.046 1.456 0.449 34.451 0.164 1.997 5.910 0.18 77955. 0.1056
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23.29 0.5590 0.5302 0.0117 0.0124 0.041 1.294 0.350 30.609 0.146 1.559 5.192 0.18 78112. 0.0820
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24.22 0.5814 0.4568 0.0084 0.0107 0.036 1.121 0.252 26.525 0.127 1.119 4.302 0.18 78274. 0.0575
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25.16 0.6037 0.3440 0.0051 0.0090 0.030 0.939 0.153 22.211 0.106 0.679 3.119 0.18 78441. 0.0325
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26.09 0.6261 0.1588 0.0018 0.0071 0.024 0.747 0.054 17.672 0.084 0.241 1.389 0.18 78612. 0.0086
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27.02 0.6485
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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 0.0739 0.0228 0.255 5.353 4.968 189.988 0.605 22.096 11.860 0.26 113589. 0.7050
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1.38 0.0221 0.0694 0.0727 0.0231 0.259 5.436 4.885 192.946 0.614 21.728 11.483 0.26 113650. 0.6769
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2.76 0.0441 0.1344 0.0714 0.0234 0.262 5.513 4.795 195.689 0.623 21.328 11.114 0.26 113717. 0.6491
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4.14 0.0662 0.1951 0.0699 0.0237 0.266 5.583 4.698 198.159 0.631 20.896 10.753 0.26 113789. 0.6216
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5.52 0.0883 0.2516 0.0684 0.0240 0.269 5.643 4.593 200.297 0.638 20.429 10.401 0.26 113866. 0.5945
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6.90 0.1104 0.3041 0.0667 0.0242 0.271 5.692 4.480 202.046 0.643 19.928 10.057 0.26 113950. 0.5678
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8.28 0.1324 0.3528 0.0649 0.0244 0.273 5.729 4.359 203.355 0.647 19.391 9.724 0.26 114040. 0.5415
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9.66 0.1545 0.3979 0.0630 0.0245 0.274 5.752 4.231 204.171 0.650 18.819 9.399 0.26 114136. 0.5156
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11.04 0.1766 0.4395 0.0609 0.0245 0.274 5.760 4.094 204.452 0.651 18.212 9.083 0.26 114238. 0.4902
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12.42 0.1986 0.4777 0.0588 0.0245 0.274 5.752 3.950 204.157 0.650 17.571 8.776 0.26 114347. 0.4652
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13.79 0.2207 0.5127 0.0565 0.0243 0.273 5.726 3.799 203.251 0.647 16.898 8.478 0.26 114463. 0.4407
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15.17 0.2428 0.5446 0.0542 0.0242 0.270 5.683 3.641 201.701 0.642 16.193 8.187 0.26 114586. 0.4166
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16.55 0.2649 0.5735 0.0517 0.0239 0.268 5.620 3.475 199.476 0.635 15.458 7.902 0.26 114716. 0.3929
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17.93 0.2869 0.5994 0.0492 0.0235 0.264 5.538 3.304 196.548 0.626 14.695 7.624 0.26 114853. 0.3696
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19.31 0.3090 0.6224 0.0465 0.0231 0.259 5.435 3.126 192.890 0.614 13.905 7.351 0.26 114997. 0.3466
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20.69 0.3311 0.6424 0.0438 0.0226 0.253 5.310 2.943 188.477 0.600 13.090 7.082 0.26 115149. 0.3240
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22.07 0.3532 0.6595 0.0410 0.0220 0.246 5.164 2.754 183.287 0.583 12.250 6.815 0.26 115308. 0.3017
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23.45 0.3752 0.6734 0.0381 0.0212 0.238 4.995 2.560 177.297 0.564 11.389 6.550 0.26 115475. 0.2795
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24.83 0.3973 0.6841 0.0352 0.0204 0.229 4.803 2.362 170.490 0.543 10.506 6.284 0.26 115650. 0.2576
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26.21 0.4194 0.6911 0.0321 0.0195 0.218 4.588 2.159 162.849 0.518 9.605 6.014 0.26 115832. 0.2357
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27.59 0.4414 0.6941 0.0291 0.0185 0.207 4.349 1.953 154.359 0.491 8.687 5.738 0.26 116022. 0.2139
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28.97 0.4635 0.6923 0.0259 0.0174 0.194 4.086 1.743 145.012 0.462 7.752 5.451 0.26 116220. 0.1920
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30.35 0.4856 0.6849 0.0228 0.0161 0.181 3.798 1.530 134.800 0.429 6.805 5.147 0.26 116426. 0.1698
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31.73 0.5077 0.6701 0.0196 0.0148 0.166 3.486 1.314 123.723 0.394 5.845 4.817 0.27 116639. 0.1473
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33.11 0.5297 0.6456 0.0163 0.0134 0.150 3.150 1.096 111.788 0.356 4.876 4.448 0.27 116861. 0.1242
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34.49 0.5518 0.6073 0.0131 0.0119 0.133 2.789 0.877 99.005 0.315 3.900 4.017 0.27 117090. 0.1003
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35.87 0.5739 0.5483 0.0098 0.0102 0.115 2.406 0.656 85.398 0.272 2.920 3.487 0.27 117328. 0.0754
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37.25 0.5959 0.4547 0.0065 0.0085 0.095 2.000 0.436 70.996 0.226 1.939 2.785 0.27 117573. 0.0490
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38.63 0.6180 0.2967 0.0032 0.0067 0.075 1.573 0.216 55.830 0.178 0.959 1.752 0.27 117825. 0.0217
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40.01 0.6401 -0.0157 -0.0001 0.0047 0.053 1.116 -0.008 39.594 0.126 -0.035 -0.090 0.27 118062. 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 0.0746 0.0223 0.592 9.327 8.905 441.403 1.054 39.611 9.151 0.35 151446. 0.7283
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1.85 0.0223 0.0720 0.0733 0.0227 0.602 9.482 8.757 448.713 1.071 38.952 8.852 0.35 151528. 0.6987
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3.71 0.0445 0.1392 0.0720 0.0230 0.611 9.625 8.596 455.498 1.087 38.236 8.560 0.35 151618. 0.6694
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5.56 0.0668 0.2018 0.0705 0.0233 0.619 9.754 8.422 461.614 1.102 37.461 8.275 0.35 151715. 0.6405
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7.42 0.0890 0.2601 0.0689 0.0236 0.626 9.866 8.234 466.918 1.115 36.623 7.998 0.35 151820. 0.6121
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9.27 0.1113 0.3141 0.0672 0.0238 0.632 9.958 8.031 471.267 1.125 35.720 7.729 0.35 151933. 0.5842
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11.13 0.1335 0.3642 0.0654 0.0240 0.636 10.027 7.813 474.528 1.133 34.753 7.468 0.35 152054. 0.5568
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12.98 0.1558 0.4105 0.0635 0.0241 0.639 10.070 7.581 476.578 1.138 33.721 7.215 0.35 152184. 0.5298
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14.83 0.1780 0.4532 0.0614 0.0241 0.640 10.086 7.335 477.307 1.139 32.625 6.970 0.35 152323. 0.5035
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16.69 0.2003 0.4925 0.0592 0.0241 0.639 10.071 7.074 476.616 1.138 31.467 6.732 0.35 152470. 0.4776
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18.54 0.2225 0.5285 0.0569 0.0240 0.636 10.025 6.801 474.415 1.133 30.249 6.502 0.35 152627. 0.4522
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20.40 0.2448 0.5613 0.0545 0.0238 0.631 9.945 6.514 470.624 1.124 28.973 6.278 0.35 152793. 0.4273
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22.25 0.2670 0.5911 0.0520 0.0235 0.624 9.829 6.215 465.166 1.111 27.643 6.060 0.35 152969. 0.4029
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24.10 0.2893 0.6179 0.0494 0.0231 0.614 9.677 5.904 457.970 1.093 26.261 5.847 0.35 153155. 0.3789
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25.96 0.3115 0.6418 0.0467 0.0227 0.602 9.487 5.582 448.973 1.072 24.829 5.639 0.35 153350. 0.3554
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27.81 0.3338 0.6627 0.0440 0.0221 0.588 9.258 5.250 438.112 1.046 23.352 5.435 0.35 153556. 0.3321
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29.67 0.3560 0.6807 0.0411 0.0215 0.570 8.987 4.908 425.330 1.015 21.831 5.234 0.35 153771. 0.3093
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31.52 0.3783 0.6956 0.0382 0.0207 0.551 8.676 4.557 410.576 0.980 20.269 5.034 0.35 153997. 0.2866
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33.38 0.4005 0.7074 0.0351 0.0199 0.528 8.321 4.197 393.802 0.940 18.670 4.835 0.35 154233. 0.2642
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35.23 0.4228 0.7156 0.0321 0.0189 0.503 7.923 3.830 374.969 0.895 17.037 4.633 0.35 154480. 0.2418
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37.08 0.4450 0.7198 0.0289 0.0179 0.475 7.481 3.456 354.043 0.845 15.373 4.428 0.35 154737. 0.2195
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38.94 0.4673 0.7194 0.0257 0.0167 0.444 6.994 3.076 331.000 0.790 13.680 4.215 0.35 155005. 0.1971
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40.79 0.4895 0.7133 0.0225 0.0155 0.410 6.462 2.690 305.827 0.730 11.963 3.989 0.35 155283. 0.1745
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42.65 0.5118 0.6999 0.0192 0.0141 0.374 5.885 2.299 278.524 0.665 10.226 3.744 0.35 155573. 0.1514
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44.50 0.5340 0.6765 0.0159 0.0126 0.334 5.264 1.904 249.108 0.595 8.471 3.468 0.35 155873. 0.1276
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46.35 0.5563 0.6385 0.0126 0.0110 0.292 4.598 1.507 217.614 0.520 6.705 3.142 0.35 156183. 0.1029
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48.21 0.5785 0.5773 0.0093 0.0093 0.247 3.890 1.109 184.100 0.440 4.932 2.732 0.35 156504. 0.0767
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50.06 0.6008 0.4755 0.0059 0.0075 0.199 3.141 0.710 148.644 0.355 3.158 2.166 0.36 156836. 0.0487
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51.92 0.6230 0.2894 0.0026 0.0056 0.149 2.352 0.312 111.312 0.266 1.388 1.271 0.36 157176. 0.0189
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53.77 0.6453
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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 0.0754 0.0222 1.149 14.482 14.063 856.704 1.636 62.554 7.446 0.44 189296. 0.7447
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2.30 0.0221 0.0727 0.0741 0.0225 1.169 14.730 13.835 871.363 1.664 61.536 7.201 0.44 189399. 0.7144
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4.61 0.0442 0.1407 0.0728 0.0229 1.187 14.960 13.586 884.993 1.690 60.429 6.963 0.44 189511. 0.6845
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6.91 0.0664 0.2040 0.0713 0.0232 1.203 15.169 13.315 897.309 1.714 59.227 6.731 0.44 189632. 0.6550
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9.22 0.0885 0.2628 0.0698 0.0235 1.218 15.350 13.023 908.029 1.734 57.926 6.505 0.44 189763. 0.6261
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11.52 0.1106 0.3175 0.0681 0.0237 1.230 15.499 12.708 916.875 1.751 56.525 6.286 0.44 189903. 0.5977
|
|
13.82 0.1327 0.3682 0.0663 0.0239 1.239 15.613 12.370 923.579 1.764 55.020 6.075 0.44 190054. 0.5698
|
|
16.13 0.1548 0.4150 0.0643 0.0240 1.244 15.686 12.008 927.896 1.772 53.413 5.870 0.44 190215. 0.5425
|
|
18.43 0.1770 0.4583 0.0623 0.0240 1.247 15.715 11.624 929.608 1.775 51.705 5.672 0.44 190388. 0.5158
|
|
20.74 0.1991 0.4982 0.0601 0.0240 1.245 15.696 11.218 928.522 1.773 49.899 5.480 0.44 190571. 0.4895
|
|
23.04 0.2212 0.5348 0.0578 0.0239 1.240 15.628 10.791 924.462 1.766 47.998 5.294 0.44 190766. 0.4639
|
|
25.34 0.2433 0.5683 0.0554 0.0237 1.230 15.506 10.343 917.267 1.752 46.006 5.114 0.44 190972. 0.4387
|
|
27.65 0.2654 0.5987 0.0529 0.0235 1.216 15.329 9.876 906.791 1.732 43.926 4.940 0.44 191190. 0.4140
|
|
29.95 0.2875 0.6263 0.0503 0.0231 1.197 15.094 9.390 892.896 1.705 41.765 4.770 0.44 191421. 0.3898
|
|
32.26 0.3097 0.6510 0.0476 0.0226 1.174 14.799 8.886 875.453 1.672 39.525 4.604 0.44 191663. 0.3660
|
|
34.56 0.3318 0.6730 0.0448 0.0221 1.146 14.442 8.366 854.344 1.632 37.212 4.442 0.44 191918. 0.3426
|
|
36.87 0.3539 0.6920 0.0420 0.0215 1.112 14.022 7.831 829.458 1.584 34.831 4.282 0.44 192185. 0.3196
|
|
39.17 0.3760 0.7082 0.0390 0.0207 1.074 13.535 7.281 800.691 1.529 32.385 4.124 0.44 192465. 0.2968
|
|
41.47 0.3981 0.7214 0.0360 0.0199 1.030 12.982 6.718 767.953 1.467 29.880 3.968 0.44 192757. 0.2743
|
|
43.78 0.4203 0.7312 0.0329 0.0189 0.981 12.360 6.142 731.163 1.396 27.320 3.810 0.44 193063. 0.2518
|
|
46.08 0.4424 0.7374 0.0298 0.0179 0.926 11.668 5.555 690.253 1.318 24.710 3.650 0.44 193381. 0.2295
|
|
48.39 0.4645 0.7394 0.0266 0.0167 0.865 10.906 4.958 645.175 1.232 22.055 3.486 0.44 193713. 0.2070
|
|
50.69 0.4866 0.7362 0.0233 0.0154 0.799 10.073 4.353 595.900 1.138 19.360 3.313 0.44 194057. 0.1843
|
|
52.99 0.5087 0.7264 0.0200 0.0140 0.727 9.169 3.739 542.424 1.036 16.632 3.127 0.44 194415. 0.1613
|
|
55.30 0.5309 0.7076 0.0167 0.0125 0.650 8.195 3.120 484.773 0.926 13.876 2.919 0.44 194786. 0.1375
|
|
57.60 0.5530 0.6757 0.0134 0.0109 0.567 7.151 2.496 423.011 0.808 11.100 2.676 0.44 195170. 0.1127
|
|
59.91 0.5751 0.6231 0.0100 0.0092 0.479 6.039 1.869 357.244 0.682 8.312 2.373 0.44 195568. 0.0865
|
|
62.21 0.5972 0.5338 0.0067 0.0074 0.386 4.862 1.241 287.622 0.549 5.521 1.957 0.44 195978. 0.0582
|
|
64.51 0.6193 0.3680 0.0033 0.0055 0.287 3.623 0.615 214.296 0.409 2.734 1.301 0.44 196400. 0.0272
|
|
66.82 0.6415 -0.0314 -0.0002 0.0035 0.180 2.272 -0.032 134.399 0.257 -0.141 -0.107 0.45 196760. 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 0.0764 0.0222 1.992 20.929 20.522 1485.718 2.365 91.281 6.265 0.52 227139. 0.7570
|
|
2.76 0.0221 0.0734 0.0751 0.0226 2.028 21.299 20.195 1511.962 2.406 89.828 6.058 0.52 227263. 0.7261
|
|
5.53 0.0442 0.1420 0.0738 0.0230 2.060 21.643 19.838 1536.380 2.445 88.241 5.857 0.52 227397. 0.6957
|
|
8.29 0.0664 0.2058 0.0724 0.0233 2.090 21.954 19.450 1558.462 2.480 86.515 5.661 0.52 227543. 0.6659
|
|
11.06 0.0885 0.2652 0.0708 0.0236 2.116 22.225 19.030 1577.714 2.511 84.644 5.471 0.52 227701. 0.6365
|
|
13.82 0.1106 0.3204 0.0691 0.0239 2.137 22.450 18.575 1593.634 2.536 82.622 5.287 0.52 227870. 0.6077
|
|
16.59 0.1327 0.3715 0.0673 0.0240 2.153 22.620 18.086 1605.734 2.556 80.448 5.109 0.52 228052. 0.5795
|
|
19.35 0.1548 0.4188 0.0654 0.0242 2.164 22.731 17.563 1613.585 2.568 78.121 4.937 0.52 228246. 0.5518
|
|
22.12 0.1769 0.4626 0.0633 0.0242 2.168 22.776 17.006 1616.798 2.573 75.644 4.771 0.52 228454. 0.5247
|
|
24.88 0.1991 0.5029 0.0611 0.0242 2.166 22.751 16.417 1615.029 2.570 73.022 4.611 0.52 228675. 0.4982
|
|
27.65 0.2212 0.5400 0.0588 0.0241 2.156 22.652 15.795 1607.971 2.559 70.258 4.455 0.52 228909. 0.4723
|
|
30.41 0.2433 0.5740 0.0563 0.0239 2.139 22.474 15.144 1595.344 2.539 67.359 4.305 0.53 229158. 0.4469
|
|
33.18 0.2654 0.6050 0.0538 0.0236 2.115 22.214 14.463 1576.892 2.510 64.331 4.160 0.53 229420. 0.4220
|
|
35.94 0.2875 0.6332 0.0512 0.0232 2.082 21.868 13.755 1552.378 2.471 61.180 4.019 0.53 229697. 0.3975
|
|
38.70 0.3096 0.6586 0.0484 0.0228 2.040 21.435 13.020 1521.579 2.422 57.915 3.881 0.53 229989. 0.3735
|
|
41.47 0.3318 0.6812 0.0456 0.0222 1.990 20.909 12.262 1484.289 2.362 54.540 3.747 0.53 230295. 0.3499
|
|
44.23 0.3539 0.7011 0.0427 0.0216 1.931 20.290 11.480 1440.316 2.292 51.064 3.615 0.53 230616. 0.3267
|
|
47.00 0.3760 0.7181 0.0397 0.0208 1.863 19.574 10.677 1389.484 2.211 47.492 3.485 0.53 230953. 0.3038
|
|
49.76 0.3981 0.7323 0.0367 0.0199 1.786 18.759 9.854 1331.631 2.119 43.833 3.357 0.53 231305. 0.2810
|
|
52.53 0.4202 0.7433 0.0335 0.0190 1.699 17.843 9.013 1266.618 2.016 40.092 3.228 0.53 231672. 0.2584
|
|
55.29 0.4423 0.7508 0.0303 0.0179 1.602 16.825 8.156 1194.328 1.901 36.277 3.097 0.53 232054. 0.2359
|
|
58.06 0.4645 0.7543 0.0271 0.0167 1.495 15.702 7.283 1114.672 1.774 32.395 2.963 0.53 232452. 0.2133
|
|
60.82 0.4866 0.7529 0.0238 0.0154 1.378 14.476 6.397 1027.600 1.635 28.453 2.824 0.53 232866. 0.1905
|
|
63.59 0.5087 0.7452 0.0205 0.0140 1.251 13.145 5.500 933.105 1.485 24.462 2.673 0.53 233296. 0.1672
|
|
66.35 0.5308 0.7290 0.0171 0.0124 1.115 11.710 4.593 831.231 1.323 20.429 2.506 0.53 233741. 0.1432
|
|
69.12 0.5529 0.7003 0.0137 0.0108 0.968 10.172 3.679 722.089 1.149 16.365 2.311 0.53 234203. 0.1182
|
|
71.88 0.5750 0.6514 0.0103 0.0091 0.812 8.535 2.761 605.867 0.964 12.283 2.067 0.53 234680. 0.0916
|
|
74.65 0.5972 0.5663 0.0069 0.0072 0.647 6.802 1.842 482.831 0.768 8.195 1.731 0.53 235172. 0.0627
|
|
77.41 0.6193 0.4029 0.0034 0.0053 0.474 4.976 0.925 353.251 0.562 4.113 1.187 0.53 235678. 0.0304
|
|
80.17 0.6414 -0.0137 -0.0001 0.0032 0.285 2.997 -0.018 212.753 0.339 -0.081 -0.039 0.53 236123. 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 0.0776 0.0225 3.202 28.832 28.390 2387.829 3.257 126.279 5.393 0.61 264970. 0.7664
|
|
3.23 0.0222 0.0739 0.0764 0.0229 3.261 29.358 27.951 2431.393 3.317 124.325 5.214 0.61 265116. 0.7352
|
|
6.46 0.0443 0.1428 0.0751 0.0233 3.315 29.848 27.469 2471.954 3.372 122.181 5.040 0.61 265274. 0.7045
|
|
9.69 0.0665 0.2070 0.0737 0.0236 3.364 30.291 26.943 2508.657 3.422 119.840 4.871 0.61 265446. 0.6744
|
|
12.92 0.0886 0.2667 0.0721 0.0240 3.407 30.678 26.370 2540.669 3.466 117.294 4.708 0.61 265630. 0.6448
|
|
16.16 0.1108 0.3222 0.0704 0.0242 3.443 30.997 25.750 2567.159 3.502 114.534 4.549 0.61 265830. 0.6157
|
|
19.39 0.1329 0.3737 0.0686 0.0244 3.470 31.241 25.080 2587.321 3.530 111.557 4.397 0.61 266043. 0.5873
|
|
22.62 0.1551 0.4213 0.0666 0.0245 3.487 31.399 24.362 2600.428 3.547 108.364 4.249 0.61 266272. 0.5594
|
|
25.85 0.1773 0.4654 0.0645 0.0246 3.494 31.465 23.596 2605.840 3.555 104.956 4.107 0.61 266516. 0.5321
|
|
29.08 0.1994 0.5061 0.0623 0.0245 3.491 31.430 22.783 2603.003 3.551 101.341 3.970 0.61 266776. 0.5054
|
|
32.31 0.2216 0.5436 0.0599 0.0244 3.475 31.290 21.926 2591.413 3.535 97.525 3.838 0.61 267051. 0.4793
|
|
35.54 0.2437 0.5780 0.0575 0.0242 3.447 31.039 21.025 2570.629 3.507 93.517 3.710 0.61 267343. 0.4537
|
|
38.77 0.2659 0.6095 0.0549 0.0239 3.407 30.672 20.082 2540.239 3.465 89.326 3.586 0.61 267652. 0.4286
|
|
42.01 0.2880 0.6382 0.0522 0.0236 3.352 30.185 19.101 2499.870 3.410 84.961 3.466 0.61 267977. 0.4040
|
|
45.24 0.3102 0.6641 0.0494 0.0231 3.284 29.573 18.083 2449.170 3.341 80.433 3.349 0.61 268319. 0.3798
|
|
48.47 0.3323 0.6874 0.0466 0.0225 3.202 28.832 17.030 2387.812 3.257 75.751 3.235 0.61 268679. 0.3561
|
|
51.70 0.3545 0.7079 0.0436 0.0218 3.105 27.959 15.945 2315.495 3.159 70.924 3.123 0.61 269056. 0.3326
|
|
54.93 0.3767 0.7257 0.0405 0.0210 2.993 26.950 14.830 2231.939 3.045 65.963 3.014 0.62 269451. 0.3095
|
|
58.16 0.3988 0.7407 0.0374 0.0201 2.866 25.802 13.686 2136.888 2.915 60.877 2.905 0.62 269863. 0.2866
|
|
61.39 0.4210 0.7527 0.0342 0.0191 2.722 24.513 12.517 2030.121 2.769 55.676 2.797 0.62 270294. 0.2639
|
|
64.62 0.4431 0.7613 0.0310 0.0180 2.563 23.080 11.324 1911.450 2.608 50.369 2.687 0.62 270742. 0.2412
|
|
67.85 0.4653 0.7660 0.0276 0.0168 2.388 21.502 10.110 1780.737 2.429 44.968 2.575 0.62 271209. 0.2184
|
|
71.09 0.4874 0.7660 0.0243 0.0154 2.196 19.777 8.876 1637.899 2.234 39.483 2.458 0.62 271694. 0.1953
|
|
74.32 0.5096 0.7600 0.0209 0.0140 1.989 17.906 7.627 1482.926 2.023 33.925 2.333 0.62 272197. 0.1718
|
|
77.55 0.5318 0.7458 0.0174 0.0124 1.765 15.889 6.364 1315.894 1.795 28.308 2.194 0.62 272719. 0.1476
|
|
80.78 0.5539 0.7193 0.0139 0.0107 1.525 13.729 5.092 1136.987 1.551 22.647 2.031 0.62 273260. 0.1222
|
|
84.01 0.5761 0.6729 0.0104 0.0089 1.269 11.429 3.813 946.519 1.291 16.958 1.827 0.62 273818. 0.0951
|
|
87.24 0.5982 0.5895 0.0069 0.0070 0.999 8.995 2.532 744.931 1.016 11.261 1.541 0.62 274395. 0.0654
|
|
90.47 0.6204 0.4230 0.0034 0.0050 0.714 6.432 1.252 532.660 0.727 5.571 1.067 0.62 274987. 0.0318
|
|
93.70 0.6425
|
|
|
|
|
|
|
|
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 0.0791 0.0231 4.896 38.572 37.815 3650.855 4.358 168.201 4.698 0.70 302788. 0.7705
|
|
3.73 0.0224 0.0743 0.0780 0.0235 4.985 39.273 37.250 3717.209 4.437 165.686 4.545 0.70 302956. 0.7399
|
|
7.45 0.0447 0.1436 0.0767 0.0239 5.068 39.928 36.625 3779.154 4.511 162.908 4.396 0.70 303140. 0.7095
|
|
11.18 0.0671 0.2083 0.0752 0.0242 5.143 40.521 35.939 3835.321 4.578 159.856 4.250 0.70 303339. 0.6796
|
|
14.91 0.0894 0.2685 0.0736 0.0245 5.209 41.040 35.188 3884.391 4.637 156.515 4.109 0.70 303554. 0.6501
|
|
18.63 0.1118 0.3244 0.0719 0.0248 5.263 41.469 34.370 3924.991 4.685 152.877 3.972 0.70 303786. 0.6210
|
|
22.36 0.1342 0.3763 0.0701 0.0250 5.305 41.794 33.483 3955.793 4.722 148.933 3.839 0.70 304034. 0.5925
|
|
26.09 0.1565 0.4244 0.0681 0.0251 5.331 42.003 32.528 3975.579 4.745 144.685 3.711 0.70 304301. 0.5645
|
|
29.81 0.1789 0.4689 0.0659 0.0252 5.342 42.084 31.505 3983.269 4.755 140.136 3.587 0.70 304585. 0.5371
|
|
33.54 0.2012 0.5099 0.0637 0.0251 5.334 42.028 30.417 3977.917 4.748 135.295 3.468 0.70 304888. 0.5102
|
|
37.26 0.2236 0.5478 0.0613 0.0250 5.309 41.825 29.266 3958.688 4.725 130.174 3.353 0.70 305209. 0.4838
|
|
40.99 0.2459 0.5826 0.0587 0.0248 5.263 41.467 28.054 3924.838 4.685 124.784 3.242 0.70 305550. 0.4580
|
|
44.72 0.2683 0.6145 0.0561 0.0245 5.197 40.948 26.785 3875.718 4.626 119.139 3.135 0.70 305909. 0.4327
|
|
48.44 0.2907 0.6436 0.0533 0.0241 5.110 40.262 25.462 3810.757 4.549 113.253 3.031 0.70 306289. 0.4079
|
|
52.17 0.3130 0.6700 0.0504 0.0236 5.001 39.403 24.087 3729.433 4.452 107.139 2.929 0.70 306688. 0.3835
|
|
55.90 0.3354 0.6937 0.0474 0.0229 4.870 38.365 22.665 3631.261 4.334 100.812 2.831 0.70 307107. 0.3595
|
|
59.62 0.3577 0.7148 0.0444 0.0222 4.715 37.145 21.197 3515.789 4.197 94.285 2.735 0.70 307546. 0.3358
|
|
63.35 0.3801 0.7332 0.0412 0.0214 4.536 35.738 19.688 3382.603 4.038 87.571 2.640 0.70 308006. 0.3124
|
|
67.08 0.4025 0.7487 0.0380 0.0204 4.333 34.140 18.140 3231.331 3.857 80.686 2.546 0.70 308486. 0.2892
|
|
70.80 0.4248 0.7613 0.0347 0.0193 4.106 32.347 16.556 3061.638 3.655 73.641 2.453 0.70 308987. 0.2662
|
|
74.53 0.4472 0.7706 0.0313 0.0181 3.853 30.357 14.940 2873.255 3.430 66.451 2.358 0.71 309509. 0.2431
|
|
78.26 0.4695 0.7759 0.0278 0.0168 3.575 28.167 13.294 2665.979 3.182 59.131 2.262 0.71 310053. 0.2199
|
|
81.98 0.4919 0.7766 0.0243 0.0154 3.272 25.776 11.622 2439.701 2.912 51.695 2.161 0.71 310617. 0.1965
|
|
85.71 0.5143 0.7710 0.0208 0.0139 2.943 23.185 9.928 2194.427 2.619 44.160 2.052 0.71 311203. 0.1724
|
|
89.44 0.5366 0.7569 0.0172 0.0122 2.589 20.394 8.216 1930.308 2.304 36.544 1.930 0.71 311810. 0.1476
|
|
93.16 0.5590 0.7297 0.0136 0.0104 2.210 17.408 6.490 1647.671 1.967 28.868 1.787 0.71 312439. 0.1214
|
|
96.89 0.5813 0.6802 0.0100 0.0085 1.806 14.232 4.756 1347.065 1.608 21.156 1.602 0.71 313088. 0.0932
|
|
100.62 0.6037 0.5871 0.0063 0.0065 1.380 10.875 3.020 1029.277 1.229 13.435 1.331 0.71 313758. 0.0617
|
|
104.34 0.6261 0.3841 0.0027 0.0044 0.932 7.342 1.287 694.934 0.830 5.723 0.840 0.71 314444. 0.0254
|
|
108.07 0.6484
|
|
|
|
|
|
|
|
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 0.0810 0.0251 7.597 53.206 48.967 5665.359 6.011 217.804 3.920 0.79 340586. 0.7317
|
|
4.19 0.0223 0.0700 0.0798 0.0255 7.698 53.907 48.284 5740.088 6.090 214.769 3.815 0.79 340776. 0.7071
|
|
8.38 0.0447 0.1363 0.0786 0.0258 7.788 54.541 47.524 5807.573 6.162 211.386 3.712 0.79 340983. 0.6824
|
|
12.56 0.0670 0.1988 0.0772 0.0260 7.867 55.091 46.681 5866.123 6.224 207.637 3.609 0.79 341208. 0.6577
|
|
16.75 0.0893 0.2577 0.0757 0.0262 7.931 55.542 45.751 5914.112 6.275 203.501 3.509 0.79 341451. 0.6330
|
|
20.94 0.1117 0.3130 0.0740 0.0264 7.979 55.878 44.731 5949.876 6.313 198.962 3.410 0.79 341712. 0.6083
|
|
25.13 0.1340 0.3649 0.0721 0.0265 8.008 56.084 43.617 5971.827 6.336 194.010 3.313 0.79 341994. 0.5835
|
|
29.31 0.1563 0.4135 0.0701 0.0265 8.017 56.147 42.410 5978.569 6.343 188.642 3.218 0.79 342295. 0.5589
|
|
33.50 0.1787 0.4588 0.0680 0.0265 8.004 56.056 41.112 5968.886 6.333 182.864 3.124 0.79 342617. 0.5342
|
|
37.69 0.2010 0.5010 0.0657 0.0264 7.968 55.801 39.723 5941.707 6.304 176.688 3.032 0.79 342959. 0.5097
|
|
41.88 0.2233 0.5402 0.0633 0.0262 7.907 55.372 38.248 5896.062 6.256 170.129 2.942 0.79 343323. 0.4853
|
|
46.06 0.2457 0.5764 0.0607 0.0259 7.820 54.761 36.691 5831.032 6.187 163.203 2.854 0.79 343708. 0.4611
|
|
50.25 0.2680 0.6097 0.0580 0.0255 7.705 53.960 35.056 5745.697 6.096 155.931 2.767 0.79 344114. 0.4370
|
|
54.44 0.2903 0.6401 0.0551 0.0250 7.562 52.959 33.348 5639.142 5.983 148.330 2.682 0.79 344543. 0.4131
|
|
58.63 0.3127 0.6679 0.0522 0.0244 7.390 51.751 31.569 5510.437 5.847 140.421 2.599 0.79 344994. 0.3894
|
|
62.81 0.3350 0.6929 0.0492 0.0238 7.186 50.325 29.726 5358.637 5.686 132.223 2.516 0.79 345467. 0.3659
|
|
67.00 0.3573 0.7152 0.0460 0.0230 6.950 48.674 27.822 5182.814 5.499 123.754 2.435 0.79 345962. 0.3425
|
|
71.19 0.3797 0.7348 0.0428 0.0221 6.681 46.789 25.862 4982.079 5.286 115.033 2.354 0.79 346481. 0.3193
|
|
75.38 0.4020 0.7516 0.0394 0.0211 6.377 44.662 23.848 4755.617 5.046 106.078 2.275 0.79 347022. 0.2963
|
|
79.57 0.4243 0.7655 0.0360 0.0200 6.038 42.287 21.787 4502.702 4.778 96.907 2.195 0.79 347587. 0.2732
|
|
83.75 0.4467 0.7761 0.0325 0.0187 5.663 39.659 19.681 4222.924 4.481 87.540 2.114 0.79 348175. 0.2501
|
|
87.94 0.4690 0.7829 0.0290 0.0174 5.252 36.778 17.534 3916.174 4.155 77.993 2.031 0.79 348787. 0.2268
|
|
92.13 0.4914 0.7851 0.0254 0.0159 4.804 33.642 15.353 3582.169 3.801 68.288 1.944 0.79 349422. 0.2031
|
|
96.32 0.5137 0.7812 0.0217 0.0143 4.320 30.252 13.140 3221.243 3.418 58.446 1.850 0.80 350081. 0.1789
|
|
100.50 0.5360 0.7687 0.0180 0.0126 3.801 26.617 10.901 2834.182 3.007 48.489 1.745 0.80 350764. 0.1536
|
|
104.69 0.5584 0.7428 0.0143 0.0107 3.248 22.749 8.643 2422.302 2.570 38.444 1.618 0.80 351471. 0.1269
|
|
108.88 0.5807 0.6941 0.0105 0.0088 2.665 18.664 6.372 1987.364 2.109 28.341 1.454 0.80 352201. 0.0979
|
|
113.07 0.6030 0.6010 0.0068 0.0068 2.054 14.385 4.095 1531.709 1.625 18.213 1.213 0.80 352954. 0.0654
|
|
117.25 0.6254 0.4009 0.0030 0.0047 1.418 9.932 1.818 1057.559 1.122 8.088 0.780 0.80 353725. 0.0280
|
|
121.44 0.6477
|
|
|
|
|
|
|
|
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 0.0828 0.0312 12.921 81.439 61.787 9635.140 9.201 274.828 2.909 0.87 378370. 0.6098
|
|
4.63 0.0222 0.0579 0.0818 0.0314 13.002 81.952 61.032 9695.864 9.259 271.472 2.855 0.87 378578. 0.5949
|
|
9.26 0.0444 0.1137 0.0806 0.0315 13.060 82.313 60.178 9738.552 9.300 267.672 2.803 0.87 378806. 0.5799
|
|
13.88 0.0666 0.1675 0.0793 0.0316 13.089 82.501 59.217 9760.823 9.321 263.397 2.752 0.87 379054. 0.5648
|
|
18.51 0.0889 0.2193 0.0779 0.0316 13.089 82.500 58.142 9760.673 9.321 258.616 2.702 0.87 379322. 0.5495
|
|
23.14 0.1111 0.2691 0.0763 0.0315 13.057 82.295 56.947 9736.463 9.298 253.301 2.653 0.87 379612. 0.5339
|
|
27.77 0.1333 0.3171 0.0745 0.0313 12.990 81.876 55.628 9686.933 9.250 247.435 2.605 0.87 379923. 0.5181
|
|
32.40 0.1555 0.3632 0.0726 0.0311 12.889 81.237 54.184 9611.299 9.178 241.010 2.557 0.87 380257. 0.5020
|
|
37.03 0.1777 0.4074 0.0705 0.0307 12.752 80.375 52.615 9509.264 9.081 234.030 2.510 0.87 380614. 0.4855
|
|
41.65 0.1999 0.4496 0.0682 0.0303 12.580 79.289 50.924 9380.879 8.958 226.508 2.462 0.87 380995. 0.4686
|
|
46.28 0.2222 0.4899 0.0658 0.0298 12.373 77.983 49.115 9226.317 8.810 218.462 2.415 0.87 381398. 0.4513
|
|
50.91 0.2444 0.5281 0.0632 0.0293 12.131 76.457 47.193 9045.760 8.638 209.916 2.366 0.88 381826. 0.4336
|
|
55.54 0.2666 0.5643 0.0605 0.0286 11.854 74.711 45.165 8839.231 8.441 200.894 2.318 0.88 382277. 0.4154
|
|
60.17 0.2888 0.5982 0.0576 0.0278 11.542 72.746 43.036 8606.689 8.219 191.422 2.268 0.88 382752. 0.3968
|
|
64.79 0.3110 0.6299 0.0547 0.0270 11.195 70.559 40.811 8347.961 7.972 181.528 2.217 0.88 383252. 0.3778
|
|
69.42 0.3332 0.6591 0.0516 0.0261 10.812 68.148 38.498 8062.667 7.699 171.238 2.166 0.88 383776. 0.3584
|
|
74.05 0.3554 0.6859 0.0484 0.0251 10.393 65.507 36.102 7750.200 7.401 160.580 2.113 0.88 384326. 0.3386
|
|
78.68 0.3777 0.7100 0.0450 0.0240 9.937 62.629 33.629 7409.710 7.076 149.580 2.058 0.88 384900. 0.3184
|
|
83.31 0.3999 0.7314 0.0416 0.0228 9.441 59.505 31.084 7040.177 6.723 138.262 2.003 0.88 385499. 0.2978
|
|
87.94 0.4221 0.7498 0.0381 0.0215 8.905 56.127 28.474 6640.446 6.341 126.652 1.945 0.88 386124. 0.2768
|
|
92.56 0.4443 0.7649 0.0346 0.0201 8.327 52.482 25.803 6209.281 5.929 114.773 1.885 0.88 386774. 0.2554
|
|
97.19 0.4665 0.7761 0.0309 0.0186 7.706 48.570 23.078 5746.416 5.487 102.650 1.822 0.88 387450. 0.2334
|
|
101.82 0.4887 0.7789 0.0272 0.0171 7.076 44.596 20.299 5276.282 5.038 90.291 1.745 0.88 388151. 0.2097
|
|
106.45 0.5110 0.7712 0.0234 0.0155 6.431 40.536 17.474 4795.902 4.580 77.724 1.653 0.88 388878. 0.1842
|
|
111.08 0.5332 0.7522 0.0196 0.0139 5.753 36.262 14.612 4290.263 4.097 64.993 1.545 0.89 389631. 0.1575
|
|
115.70 0.5554 0.7167 0.0157 0.0122 5.045 31.801 11.720 3762.391 3.593 52.132 1.413 0.89 390410. 0.1290
|
|
120.33 0.5776 0.6550 0.0118 0.0104 4.315 27.194 8.808 3217.430 3.072 39.179 1.242 0.89 391215. 0.0983
|
|
124.96 0.5998 0.5497 0.0079 0.0086 3.568 22.486 5.885 2660.337 2.540 26.178 1.003 0.89 392045. 0.0649
|
|
129.59 0.6220 0.3641 0.0040 0.0068 2.811 17.715 2.961 2095.909 2.001 13.171 0.641 0.89 392897. 0.0294
|
|
134.22 0.6442 -0.0122 -0.0001 0.0048 1.988 12.532 -0.068 1482.628 1.416 -0.301 -0.021 0.89 393641. 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 0.0815 0.0375 20.685 118.524 73.661 15425.021 13.391 327.645 2.166 0.96 416242. 0.4958
|
|
5.21 0.0227 0.0486 0.0807 0.0377 20.834 119.378 72.908 15536.224 13.487 324.295 2.129 0.96 416471. 0.4847
|
|
10.43 0.0455 0.0956 0.0798 0.0380 20.958 120.088 72.048 15628.576 13.567 320.471 2.091 0.96 416721. 0.4734
|
|
15.64 0.0682 0.1408 0.0787 0.0381 21.050 120.613 71.071 15696.927 13.627 316.124 2.054 0.96 416995. 0.4618
|
|
20.85 0.0910 0.1844 0.0775 0.0382 21.102 120.914 69.965 15736.133 13.661 311.203 2.017 0.96 417292. 0.4499
|
|
26.07 0.1137 0.2263 0.0761 0.0382 21.109 120.950 68.718 15740.835 13.665 305.660 1.980 0.96 417613. 0.4378
|
|
31.28 0.1365 0.2666 0.0745 0.0382 21.062 120.681 67.322 15705.733 13.634 299.450 1.944 0.96 417960. 0.4255
|
|
36.49 0.1592 0.3054 0.0728 0.0380 20.954 120.066 65.769 15625.716 13.565 292.541 1.909 0.96 418334. 0.4129
|
|
41.71 0.1820 0.3428 0.0709 0.0376 20.781 119.070 64.054 15496.060 13.452 284.913 1.875 0.96 418734. 0.4002
|
|
46.92 0.2047 0.3788 0.0688 0.0372 20.534 117.658 62.175 15312.399 13.293 276.553 1.842 0.96 419162. 0.3873
|
|
52.13 0.2275 0.4136 0.0666 0.0366 20.210 115.802 60.129 15070.762 13.083 267.455 1.810 0.96 419618. 0.3743
|
|
57.35 0.2502 0.4472 0.0641 0.0359 19.804 113.474 57.918 14767.855 12.820 257.621 1.779 0.96 420103. 0.3611
|
|
62.56 0.2730 0.4798 0.0615 0.0350 19.313 110.659 55.544 14401.526 12.502 247.059 1.749 0.96 420616. 0.3477
|
|
67.77 0.2957 0.5113 0.0587 0.0339 18.736 107.354 53.009 13971.424 12.129 235.785 1.721 0.96 421158. 0.3342
|
|
72.99 0.3185 0.5418 0.0557 0.0327 18.076 103.572 50.321 13479.104 11.701 223.827 1.693 0.96 421730. 0.3204
|
|
78.20 0.3412 0.5712 0.0526 0.0314 17.336 99.334 47.486 12927.612 11.223 211.217 1.666 0.97 422331. 0.3062
|
|
83.41 0.3640 0.5992 0.0493 0.0299 16.523 94.674 44.514 12321.116 10.696 197.998 1.639 0.97 422961. 0.2916
|
|
88.63 0.3867 0.6257 0.0458 0.0283 15.642 89.626 41.415 11664.183 10.126 184.215 1.610 0.97 423622. 0.2764
|
|
93.84 0.4095 0.6503 0.0423 0.0266 14.699 84.225 38.201 10961.274 9.516 169.918 1.581 0.97 424311. 0.2606
|
|
99.05 0.4322 0.6725 0.0386 0.0248 13.700 78.499 34.882 10216.130 8.869 155.157 1.549 0.97 425030. 0.2440
|
|
104.27 0.4550 0.6918 0.0348 0.0229 12.648 72.471 31.470 9431.546 8.188 139.980 1.513 0.97 425779. 0.2264
|
|
109.48 0.4777 0.7074 0.0310 0.0209 11.546 66.156 27.976 8609.717 7.474 124.436 1.474 0.97 426558. 0.2079
|
|
114.69 0.5005 0.7152 0.0270 0.0189 10.436 59.799 24.406 7782.417 6.756 108.556 1.422 0.97 427366. 0.1874
|
|
119.91 0.5232 0.6928 0.0230 0.0173 9.574 54.856 20.743 7139.107 6.198 92.267 1.318 0.97 428203. 0.1601
|
|
125.12 0.5460 0.6447 0.0188 0.0160 8.810 50.478 17.022 6569.332 5.703 75.714 1.175 0.97 429070. 0.1293
|
|
130.33 0.5687 0.5725 0.0147 0.0146 8.056 46.157 13.270 6006.995 5.215 59.024 1.002 0.98 429967. 0.0973
|
|
135.55 0.5915 0.4697 0.0105 0.0133 7.317 41.925 9.509 5456.308 4.737 42.294 0.790 0.98 430893. 0.0650
|
|
140.76 0.6142 0.3275 0.0064 0.0120 6.603 37.836 5.762 4924.069 4.275 25.630 0.531 0.98 431848. 0.0340
|
|
145.97 0.6370 0.1346 0.0023 0.0107 5.909 33.857 2.044 4406.240 3.825 9.091 0.210 0.98 432829. 0.0080
|
|
151.19 0.6597
|
|
|
|
|
|
|