353 lines
63 KiB
Plaintext
353 lines
63 KiB
Plaintext
25x12.5E (25x125E.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 0.0831 0.0289 0.023 1.432 1.034 16.940 0.162 4.601 27.694 0.10 58210. 0.6610
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0.53 0.0223 0.0622 0.0817 0.0292 0.023 1.447 1.017 17.118 0.163 4.523 26.942 0.10 58244. 0.6376
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1.05 0.0445 0.1210 0.0802 0.0295 0.023 1.460 0.998 17.279 0.165 4.439 26.195 0.10 58281. 0.6142
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1.58 0.0668 0.1764 0.0785 0.0297 0.023 1.473 0.978 17.422 0.166 4.349 25.456 0.10 58321. 0.5908
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2.11 0.0890 0.2285 0.0768 0.0299 0.024 1.483 0.956 17.541 0.168 4.253 24.726 0.10 58364. 0.5675
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2.64 0.1113 0.2773 0.0750 0.0301 0.024 1.490 0.933 17.634 0.168 4.151 24.006 0.10 58410. 0.5443
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3.16 0.1336 0.3229 0.0730 0.0302 0.024 1.496 0.909 17.696 0.169 4.043 23.296 0.10 58459. 0.5213
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3.69 0.1558 0.3655 0.0709 0.0302 0.024 1.498 0.883 17.722 0.169 3.927 22.596 0.10 58511. 0.4983
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4.22 0.1781 0.4049 0.0687 0.0302 0.024 1.497 0.855 17.709 0.169 3.805 21.907 0.10 58566. 0.4755
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4.74 0.2004 0.4414 0.0664 0.0301 0.024 1.492 0.826 17.654 0.169 3.675 21.228 0.10 58625. 0.4529
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5.27 0.2226 0.4750 0.0639 0.0299 0.024 1.483 0.795 17.550 0.168 3.538 20.557 0.10 58688. 0.4303
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5.80 0.2449 0.5056 0.0613 0.0297 0.023 1.470 0.763 17.395 0.166 3.394 19.894 0.10 58754. 0.4078
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6.32 0.2671 0.5334 0.0585 0.0293 0.023 1.452 0.729 17.183 0.164 3.242 19.237 0.10 58824. 0.3854
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6.85 0.2894 0.5582 0.0557 0.0289 0.023 1.429 0.693 16.912 0.161 3.082 18.584 0.10 58898. 0.3631
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7.38 0.3117 0.5800 0.0527 0.0283 0.022 1.401 0.656 16.581 0.158 2.916 17.932 0.10 58975. 0.3408
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7.91 0.3339 0.5988 0.0495 0.0276 0.022 1.369 0.617 16.191 0.155 2.743 17.277 0.10 59057. 0.3185
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8.43 0.3562 0.6142 0.0463 0.0269 0.021 1.331 0.577 15.742 0.150 2.565 16.616 0.10 59142. 0.2961
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8.96 0.3784 0.6262 0.0430 0.0260 0.020 1.288 0.535 15.234 0.145 2.382 15.942 0.10 59231. 0.2738
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9.49 0.4007 0.6342 0.0396 0.0250 0.020 1.240 0.493 14.667 0.140 2.194 15.251 0.10 59324. 0.2514
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10.01 0.4230 0.6380 0.0361 0.0240 0.019 1.187 0.450 14.042 0.134 2.001 14.534 0.10 59421. 0.2288
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10.54 0.4452 0.6368 0.0326 0.0228 0.018 1.129 0.406 13.360 0.128 1.806 13.782 0.10 59522. 0.2061
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11.07 0.4675 0.6299 0.0290 0.0215 0.017 1.067 0.361 12.622 0.121 1.607 12.982 0.10 59627. 0.1831
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11.59 0.4898 0.6160 0.0254 0.0202 0.016 1.000 0.316 11.830 0.113 1.406 12.120 0.10 59736. 0.1599
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12.12 0.5120 0.5937 0.0217 0.0187 0.015 0.928 0.271 10.985 0.105 1.203 11.171 0.10 59849. 0.1364
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12.65 0.5343 0.5604 0.0181 0.0172 0.014 0.853 0.225 10.090 0.096 1.000 10.106 0.10 59966. 0.1125
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13.18 0.5565 0.5128 0.0144 0.0156 0.012 0.773 0.179 9.148 0.087 0.797 8.879 0.10 60087. 0.0882
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13.70 0.5788 0.4457 0.0107 0.0139 0.011 0.690 0.134 8.164 0.078 0.594 7.419 0.10 60212. 0.0636
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14.23 0.6011 0.3504 0.0071 0.0122 0.010 0.604 0.088 7.142 0.068 0.393 5.616 0.10 60342. 0.0392
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14.76 0.6233 0.2121 0.0035 0.0104 0.008 0.515 0.044 6.089 0.058 0.196 3.279 0.10 60475. 0.0161
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15.28 0.6456 0.0025 0.0000 0.0085 0.007 0.423 0.000 5.007 0.048 0.002 0.037 0.10 60610. 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 0.0835 0.0271 0.171 5.375 4.158 127.179 0.607 18.497 14.831 0.20 116418. 0.7098
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1.06 0.0224 0.0669 0.0821 0.0275 0.173 5.440 4.088 128.716 0.615 18.184 14.406 0.20 116487. 0.6836
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2.12 0.0447 0.1298 0.0806 0.0278 0.175 5.499 4.012 130.128 0.621 17.847 13.986 0.20 116561. 0.6575
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3.18 0.0671 0.1890 0.0790 0.0280 0.176 5.552 3.931 131.383 0.627 17.487 13.573 0.20 116641. 0.6316
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4.23 0.0894 0.2444 0.0772 0.0283 0.178 5.598 3.845 132.451 0.632 17.102 13.167 0.20 116727. 0.6060
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5.29 0.1118 0.2963 0.0754 0.0284 0.179 5.633 3.753 133.299 0.636 16.691 12.768 0.20 116819. 0.5805
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6.35 0.1341 0.3447 0.0734 0.0286 0.180 5.658 3.654 133.892 0.639 16.253 12.378 0.20 116918. 0.5554
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7.41 0.1565 0.3897 0.0713 0.0286 0.180 5.671 3.549 134.197 0.641 15.788 11.997 0.20 117023. 0.5305
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8.47 0.1789 0.4315 0.0691 0.0286 0.180 5.671 3.438 134.178 0.641 15.294 11.623 0.20 117135. 0.5059
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9.53 0.2012 0.4702 0.0667 0.0285 0.179 5.655 3.321 133.800 0.639 14.771 11.257 0.20 117254. 0.4815
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10.59 0.2236 0.5058 0.0642 0.0284 0.178 5.622 3.197 133.027 0.635 14.219 10.899 0.20 117380. 0.4574
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11.64 0.2459 0.5385 0.0616 0.0281 0.177 5.571 3.066 131.821 0.629 13.636 10.548 0.20 117514. 0.4335
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12.70 0.2683 0.5682 0.0588 0.0278 0.175 5.500 2.928 130.142 0.621 13.022 10.203 0.20 117655. 0.4097
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13.76 0.2906 0.5950 0.0559 0.0273 0.172 5.408 2.783 127.970 0.611 12.378 9.863 0.20 117803. 0.3862
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14.82 0.3130 0.6190 0.0529 0.0267 0.168 5.295 2.632 125.296 0.598 11.707 9.527 0.20 117960. 0.3628
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15.88 0.3354 0.6400 0.0497 0.0260 0.164 5.161 2.475 122.121 0.583 11.010 9.193 0.20 118124. 0.3395
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16.94 0.3577 0.6578 0.0465 0.0253 0.159 5.006 2.313 118.442 0.566 10.290 8.859 0.20 118295. 0.3163
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18.00 0.3801 0.6724 0.0431 0.0244 0.153 4.829 2.147 114.261 0.546 9.550 8.523 0.20 118475. 0.2931
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19.05 0.4024 0.6834 0.0397 0.0234 0.147 4.631 1.976 109.579 0.523 8.791 8.181 0.20 118662. 0.2699
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20.11 0.4248 0.6903 0.0362 0.0223 0.140 4.412 1.802 104.401 0.498 8.016 7.829 0.20 118858. 0.2467
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21.17 0.4471 0.6928 0.0326 0.0211 0.132 4.173 1.625 98.733 0.471 7.227 7.464 0.20 119061. 0.2233
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22.23 0.4695 0.6898 0.0290 0.0197 0.124 3.913 1.445 92.583 0.442 6.426 7.078 0.20 119273. 0.1997
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23.29 0.4919 0.6802 0.0254 0.0183 0.115 3.633 1.263 85.965 0.410 5.617 6.663 0.20 119492. 0.1757
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24.35 0.5142 0.6624 0.0217 0.0168 0.106 3.334 1.080 78.895 0.377 4.802 6.206 0.20 119720. 0.1513
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25.41 0.5366 0.6337 0.0180 0.0152 0.096 3.017 0.896 71.395 0.341 3.984 5.690 0.20 119956. 0.1264
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26.46 0.5589 0.5899 0.0143 0.0135 0.085 2.683 0.712 63.495 0.303 3.166 5.085 0.20 120200. 0.1007
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27.52 0.5813 0.5242 0.0106 0.0118 0.074 2.334 0.529 55.231 0.264 2.353 4.345 0.20 120453. 0.0742
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28.58 0.6036 0.4243 0.0070 0.0100 0.063 1.971 0.348 46.647 0.223 1.549 3.386 0.20 120714. 0.0469
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29.64 0.6260 0.2657 0.0034 0.0081 0.051 1.597 0.170 37.794 0.180 0.758 2.045 0.20 120982. 0.0198
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30.70 0.6483 -0.0095 -0.0001 0.0061 0.038 1.212 -0.004 28.678 0.137 -0.020 -0.070 0.20 121252. 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 0.0841 0.0265 0.563 11.819 9.422 419.498 1.335 41.908 10.187 0.30 174620. 0.7339
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1.59 0.0224 0.0689 0.0827 0.0269 0.570 11.971 9.263 424.876 1.352 41.203 9.889 0.30 174723. 0.7064
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3.18 0.0447 0.1336 0.0812 0.0272 0.576 12.110 9.093 429.829 1.368 40.445 9.595 0.30 174835. 0.6791
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4.77 0.0671 0.1944 0.0795 0.0274 0.582 12.235 8.910 434.249 1.382 39.633 9.307 0.30 174956. 0.6520
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6.35 0.0895 0.2514 0.0778 0.0277 0.587 12.341 8.715 438.026 1.394 38.764 9.024 0.30 175085. 0.6253
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7.94 0.1118 0.3046 0.0759 0.0279 0.591 12.426 8.506 441.048 1.404 37.836 8.748 0.30 175224. 0.5988
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9.53 0.1342 0.3542 0.0739 0.0280 0.594 12.487 8.284 443.197 1.411 36.847 8.478 0.30 175372. 0.5727
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11.12 0.1566 0.4004 0.0718 0.0281 0.596 12.519 8.047 444.354 1.414 35.795 8.214 0.30 175530. 0.5469
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12.71 0.1789 0.4433 0.0696 0.0281 0.596 12.521 7.796 444.397 1.415 34.679 7.957 0.30 175698. 0.5215
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14.30 0.2013 0.4830 0.0672 0.0280 0.594 12.487 7.531 443.206 1.411 33.496 7.707 0.30 175878. 0.4964
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15.88 0.2236 0.5196 0.0647 0.0279 0.591 12.415 7.250 440.654 1.403 32.246 7.462 0.30 176067. 0.4716
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17.47 0.2460 0.5533 0.0621 0.0276 0.585 12.301 6.953 436.607 1.390 30.927 7.223 0.30 176268. 0.4470
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19.06 0.2684 0.5840 0.0593 0.0272 0.578 12.141 6.640 430.931 1.372 29.537 6.989 0.30 176480. 0.4227
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20.65 0.2907 0.6119 0.0563 0.0268 0.568 11.933 6.313 423.548 1.348 28.078 6.760 0.30 176703. 0.3986
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22.24 0.3131 0.6370 0.0533 0.0262 0.556 11.676 5.971 414.429 1.319 26.557 6.535 0.30 176938. 0.3748
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23.83 0.3355 0.6593 0.0501 0.0255 0.541 11.370 5.616 403.565 1.285 24.979 6.312 0.30 177185. 0.3510
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25.41 0.3578 0.6785 0.0469 0.0247 0.524 11.015 5.249 390.951 1.244 23.348 6.090 0.30 177443. 0.3275
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27.00 0.3802 0.6946 0.0435 0.0238 0.505 10.610 4.872 376.589 1.199 21.670 5.868 0.30 177712. 0.3040
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28.59 0.4026 0.7073 0.0400 0.0228 0.483 10.156 4.485 360.482 1.147 19.950 5.643 0.30 177994. 0.2805
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30.18 0.4249 0.7163 0.0365 0.0217 0.459 9.654 4.090 342.642 1.091 18.193 5.414 0.30 178287. 0.2570
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31.77 0.4473 0.7210 0.0329 0.0204 0.433 9.103 3.688 323.089 1.028 16.404 5.177 0.30 178593. 0.2334
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33.36 0.4697 0.7207 0.0293 0.0191 0.405 8.504 3.280 301.854 0.961 14.589 4.928 0.30 178911. 0.2095
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34.94 0.4920 0.7142 0.0256 0.0176 0.374 7.860 2.868 278.980 0.888 12.755 4.662 0.30 179240. 0.1853
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36.53 0.5144 0.6998 0.0219 0.0161 0.341 7.171 2.452 254.526 0.810 10.907 4.370 0.30 179582. 0.1606
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38.12 0.5367 0.6750 0.0182 0.0144 0.307 6.440 2.035 228.570 0.728 9.053 4.039 0.30 179937. 0.1352
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39.71 0.5591 0.6353 0.0144 0.0127 0.270 5.669 1.619 201.214 0.640 7.201 3.649 0.30 180304. 0.1090
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41.30 0.5815 0.5733 0.0108 0.0109 0.231 4.862 1.205 172.584 0.549 5.359 3.166 0.30 180683. 0.0816
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42.89 0.6038 0.4748 0.0071 0.0090 0.192 4.024 0.795 142.836 0.455 3.538 2.526 0.30 181074. 0.0529
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44.47 0.6262 0.3096 0.0035 0.0071 0.150 3.160 0.393 112.149 0.357 1.746 1.588 0.30 181477. 0.0234
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46.06 0.6486 -0.0039 0.0000 0.0051 0.108 2.269 -0.003 80.524 0.256 -0.015 -0.019 0.30 181880. 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 0.0849 0.0263 1.325 20.882 16.910 988.248 2.359 75.214 7.761 0.40 232813. 0.7490
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2.12 0.0224 0.0699 0.0835 0.0267 1.343 21.159 16.628 1001.335 2.391 73.959 7.532 0.40 232951. 0.7208
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4.23 0.0447 0.1356 0.0820 0.0270 1.359 21.414 16.324 1013.397 2.419 72.609 7.306 0.40 233101. 0.6928
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6.35 0.0671 0.1973 0.0803 0.0273 1.373 21.641 15.999 1024.170 2.445 71.162 7.085 0.40 233262. 0.6651
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8.47 0.0894 0.2550 0.0786 0.0276 1.386 21.836 15.650 1033.390 2.467 69.612 6.869 0.40 233435. 0.6378
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10.59 0.1118 0.3090 0.0767 0.0278 1.396 21.992 15.278 1040.784 2.485 67.955 6.658 0.40 233620. 0.6108
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12.70 0.1342 0.3593 0.0747 0.0279 1.403 22.104 14.880 1046.070 2.497 66.188 6.452 0.40 233819. 0.5842
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14.82 0.1565 0.4062 0.0726 0.0280 1.407 22.165 14.458 1048.953 2.504 64.308 6.252 0.40 234030. 0.5579
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16.94 0.1789 0.4497 0.0703 0.0280 1.407 22.169 14.009 1049.143 2.505 62.310 6.056 0.40 234256. 0.5320
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19.06 0.2012 0.4901 0.0679 0.0279 1.403 22.110 13.533 1046.345 2.498 60.193 5.866 0.40 234495. 0.5065
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21.17 0.2236 0.5273 0.0654 0.0277 1.395 21.981 13.029 1040.256 2.483 57.955 5.681 0.40 234749. 0.4813
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23.29 0.2459 0.5616 0.0627 0.0275 1.382 21.776 12.498 1030.557 2.460 55.591 5.501 0.40 235017. 0.4564
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25.41 0.2683 0.5931 0.0599 0.0271 1.364 21.488 11.938 1016.917 2.428 53.099 5.325 0.40 235300. 0.4318
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27.53 0.2907 0.6217 0.0570 0.0266 1.340 21.112 11.350 999.135 2.385 50.484 5.152 0.40 235598. 0.4074
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29.64 0.3130 0.6476 0.0539 0.0261 1.310 20.648 10.736 977.139 2.333 47.755 4.984 0.40 235912. 0.3833
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31.76 0.3354 0.6707 0.0507 0.0254 1.275 20.093 10.099 950.903 2.270 44.922 4.817 0.40 236241. 0.3593
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33.88 0.3577 0.6910 0.0474 0.0245 1.234 19.449 9.441 920.412 2.197 41.993 4.652 0.40 236585. 0.3355
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35.99 0.3801 0.7082 0.0440 0.0236 1.188 18.715 8.763 885.667 2.114 38.980 4.488 0.40 236945. 0.3118
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38.11 0.4025 0.7222 0.0405 0.0226 1.135 17.891 8.069 846.678 2.021 35.889 4.322 0.40 237321. 0.2882
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40.23 0.4248 0.7326 0.0369 0.0214 1.077 16.978 7.359 803.470 1.918 32.732 4.154 0.40 237713. 0.2645
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42.35 0.4472 0.7390 0.0333 0.0202 1.014 15.977 6.636 756.090 1.805 29.517 3.981 0.40 238120. 0.2407
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44.46 0.4695 0.7407 0.0296 0.0188 0.945 14.889 5.903 704.612 1.682 26.256 3.800 0.40 238544. 0.2167
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46.58 0.4919 0.7365 0.0259 0.0173 0.871 13.717 5.161 649.140 1.550 22.958 3.606 0.40 238984. 0.1923
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48.70 0.5143 0.7248 0.0222 0.0157 0.791 12.463 4.414 589.818 1.408 19.636 3.395 0.40 239440. 0.1674
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50.82 0.5366 0.7029 0.0184 0.0140 0.706 11.132 3.665 526.836 1.258 16.302 3.155 0.40 239913. 0.1418
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52.93 0.5590 0.6667 0.0146 0.0123 0.617 9.729 2.916 460.441 1.099 12.972 2.873 0.40 240401. 0.1151
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55.05 0.5813 0.6081 0.0109 0.0104 0.524 8.261 2.172 390.944 0.933 9.660 2.520 0.40 240907. 0.0872
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57.17 0.6037 0.5120 0.0072 0.0085 0.427 6.735 1.435 318.725 0.761 6.385 2.043 0.40 241429. 0.0574
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59.29 0.6261 0.3434 0.0036 0.0065 0.328 5.161 0.711 244.227 0.583 3.164 1.321 0.40 241966. 0.0262
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61.40 0.6484 -0.0008 0.0000 0.0045 0.224 3.537 -0.001 167.401 0.400 -0.005 -0.003 0.41 242501. 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 0.0860 0.0265 2.601 32.783 26.754 1939.283 3.704 119.000 6.257 0.50 290993. 0.7596
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2.65 0.0224 0.0705 0.0845 0.0268 2.636 33.226 26.312 1965.493 3.754 117.037 6.072 0.50 291167. 0.7310
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5.29 0.0447 0.1367 0.0830 0.0272 2.668 33.634 25.837 1989.643 3.800 114.923 5.890 0.50 291355. 0.7027
|
|
7.94 0.0671 0.1988 0.0814 0.0275 2.697 33.998 25.326 2011.206 3.841 112.652 5.712 0.50 291557. 0.6746
|
|
10.59 0.0894 0.2570 0.0796 0.0277 2.722 34.310 24.779 2029.655 3.876 110.218 5.537 0.50 291774. 0.6470
|
|
13.23 0.1118 0.3114 0.0777 0.0279 2.742 34.560 24.194 2044.434 3.905 107.614 5.368 0.50 292007. 0.6197
|
|
15.88 0.1342 0.3622 0.0757 0.0281 2.756 34.738 23.569 2054.981 3.925 104.834 5.202 0.50 292256. 0.5927
|
|
18.53 0.1565 0.4094 0.0736 0.0281 2.763 34.835 22.903 2060.713 3.936 101.872 5.041 0.50 292522. 0.5662
|
|
21.17 0.1789 0.4534 0.0713 0.0281 2.764 34.841 22.195 2061.038 3.936 98.723 4.884 0.50 292805. 0.5401
|
|
23.82 0.2012 0.4942 0.0689 0.0281 2.756 34.745 21.444 2055.375 3.925 95.383 4.732 0.50 293105. 0.5143
|
|
26.47 0.2236 0.5319 0.0664 0.0279 2.740 34.538 20.649 2043.125 3.902 91.848 4.584 0.50 293424. 0.4889
|
|
29.11 0.2460 0.5667 0.0637 0.0276 2.714 34.209 19.810 2023.646 3.865 88.113 4.440 0.50 293760. 0.4638
|
|
31.76 0.2683 0.5987 0.0608 0.0273 2.677 33.746 18.924 1996.282 3.813 84.174 4.300 0.50 294115. 0.4390
|
|
34.41 0.2907 0.6279 0.0578 0.0268 2.629 33.143 17.994 1960.616 3.745 80.037 4.163 0.50 294489. 0.4144
|
|
37.06 0.3130 0.6545 0.0547 0.0262 2.570 32.397 17.023 1916.488 3.660 75.716 4.029 0.50 294882. 0.3901
|
|
39.70 0.3354 0.6783 0.0515 0.0254 2.499 31.507 16.013 1863.843 3.560 71.228 3.897 0.50 295295. 0.3660
|
|
42.35 0.3578 0.6993 0.0481 0.0246 2.417 30.473 14.970 1802.659 3.443 66.587 3.767 0.50 295726. 0.3421
|
|
45.00 0.3801 0.7174 0.0447 0.0237 2.324 29.294 13.896 1732.933 3.310 61.809 3.637 0.50 296177. 0.3182
|
|
47.64 0.4025 0.7325 0.0411 0.0226 2.219 27.972 12.794 1654.687 3.160 56.907 3.507 0.50 296648. 0.2944
|
|
50.29 0.4248 0.7441 0.0375 0.0214 2.103 26.506 11.668 1567.975 2.995 51.898 3.375 0.50 297138. 0.2706
|
|
52.94 0.4472 0.7519 0.0338 0.0201 1.975 24.898 10.521 1472.889 2.813 46.796 3.240 0.50 297648. 0.2466
|
|
55.58 0.4696 0.7551 0.0301 0.0187 1.837 23.152 9.357 1369.575 2.616 41.618 3.099 0.50 298179. 0.2225
|
|
58.23 0.4919 0.7527 0.0263 0.0172 1.687 21.270 8.179 1258.244 2.403 36.381 2.948 0.50 298729. 0.1979
|
|
60.88 0.5143 0.7431 0.0225 0.0156 1.528 19.257 6.993 1139.186 2.176 31.105 2.784 0.50 299300. 0.1728
|
|
63.52 0.5366 0.7237 0.0186 0.0138 1.358 17.121 5.803 1012.787 1.934 25.810 2.599 0.50 299891. 0.1469
|
|
66.17 0.5590 0.6901 0.0148 0.0120 1.179 14.868 4.613 879.543 1.680 20.519 2.379 0.50 300502. 0.1199
|
|
68.82 0.5814 0.6342 0.0110 0.0101 0.992 12.511 3.430 740.084 1.413 15.258 2.102 0.50 301134. 0.0914
|
|
71.46 0.6037 0.5396 0.0073 0.0081 0.798 10.061 2.260 595.184 1.137 10.054 1.723 0.50 301787. 0.0608
|
|
74.11 0.6261 0.3670 0.0036 0.0061 0.598 7.535 1.110 445.742 0.851 4.937 1.130 0.51 302459. 0.0279
|
|
76.76 0.6484 -0.0126 -0.0001 0.0040 0.391 4.925 -0.024 291.345 0.556 -0.107 -0.037 0.51 303120. 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 0.0874 0.0268 4.557 47.867 39.148 3397.911 5.408 174.130 5.226 0.59 349154. 0.7674
|
|
3.18 0.0224 0.0707 0.0859 0.0272 4.619 48.524 38.511 3444.594 5.482 171.297 5.071 0.60 349364. 0.7386
|
|
6.36 0.0448 0.1373 0.0844 0.0276 4.677 49.130 37.824 3487.560 5.551 168.239 4.919 0.60 349592. 0.7101
|
|
9.55 0.0672 0.1997 0.0827 0.0279 4.728 49.669 37.084 3525.854 5.612 164.950 4.771 0.60 349837. 0.6818
|
|
12.73 0.0896 0.2581 0.0810 0.0281 4.772 50.129 36.290 3558.539 5.664 161.417 4.625 0.60 350100. 0.6540
|
|
15.91 0.1120 0.3128 0.0791 0.0283 4.807 50.497 35.439 3584.622 5.705 157.631 4.484 0.60 350382. 0.6265
|
|
19.09 0.1344 0.3638 0.0770 0.0285 4.832 50.757 34.528 3603.082 5.734 153.582 4.347 0.60 350684. 0.5995
|
|
22.28 0.1568 0.4114 0.0749 0.0285 4.845 50.895 33.557 3612.882 5.750 149.262 4.213 0.60 351005. 0.5728
|
|
25.46 0.1792 0.4557 0.0726 0.0285 4.845 50.896 32.523 3612.977 5.750 144.663 4.083 0.60 351348. 0.5465
|
|
28.64 0.2016 0.4968 0.0701 0.0285 4.831 50.746 31.425 3602.312 5.733 139.779 3.957 0.60 351711. 0.5206
|
|
31.82 0.2240 0.5349 0.0675 0.0283 4.801 50.429 30.262 3579.831 5.697 134.605 3.834 0.60 352096. 0.4950
|
|
35.01 0.2464 0.5701 0.0648 0.0280 4.753 49.930 29.032 3544.413 5.641 129.133 3.715 0.60 352503. 0.4698
|
|
38.19 0.2689 0.6026 0.0619 0.0276 4.687 49.233 27.733 3494.891 5.562 123.356 3.599 0.60 352933. 0.4449
|
|
41.37 0.2913 0.6323 0.0588 0.0271 4.600 48.325 26.367 3430.479 5.460 117.282 3.486 0.60 353385. 0.4202
|
|
44.55 0.3137 0.6594 0.0557 0.0265 4.494 47.204 24.940 3350.897 5.333 110.934 3.376 0.60 353860. 0.3957
|
|
47.74 0.3361 0.6838 0.0523 0.0257 4.366 45.868 23.457 3256.057 5.182 104.335 3.268 0.60 354358. 0.3714
|
|
50.92 0.3585 0.7055 0.0489 0.0249 4.219 44.317 21.922 3145.924 5.007 97.507 3.161 0.60 354879. 0.3473
|
|
54.10 0.3809 0.7244 0.0454 0.0239 4.051 42.550 20.340 3020.503 4.807 90.473 3.054 0.60 355423. 0.3233
|
|
57.28 0.4033 0.7403 0.0418 0.0228 3.862 40.569 18.717 2879.840 4.583 83.255 2.948 0.60 355991. 0.2993
|
|
60.47 0.4257 0.7529 0.0381 0.0215 3.653 38.374 17.058 2724.042 4.335 75.875 2.840 0.60 356583. 0.2753
|
|
63.65 0.4481 0.7618 0.0343 0.0202 3.424 35.968 15.368 2553.276 4.064 68.356 2.730 0.60 357198. 0.2512
|
|
66.83 0.4705 0.7662 0.0305 0.0187 3.175 33.356 13.652 2367.819 3.768 60.723 2.615 0.60 357838. 0.2268
|
|
70.01 0.4929 0.7651 0.0266 0.0171 2.907 30.542 11.916 2168.053 3.451 53.001 2.493 0.60 358502. 0.2020
|
|
73.20 0.5153 0.7570 0.0227 0.0154 2.621 27.533 10.166 1954.510 3.111 45.219 2.359 0.60 359190. 0.1766
|
|
76.38 0.5377 0.7392 0.0188 0.0137 2.317 24.341 8.410 1727.892 2.750 37.409 2.208 0.60 359902. 0.1503
|
|
79.56 0.5601 0.7071 0.0149 0.0118 1.997 20.977 6.656 1489.112 2.370 29.604 2.027 0.60 360639. 0.1228
|
|
82.74 0.5825 0.6520 0.0110 0.0098 1.662 17.458 4.911 1239.320 1.972 21.844 1.797 0.61 361400. 0.0935
|
|
85.93 0.6049 0.5555 0.0071 0.0077 1.314 13.804 3.186 979.938 1.560 14.171 1.475 0.61 362186. 0.0618
|
|
89.11 0.6273 0.3706 0.0033 0.0056 0.956 10.038 1.490 712.603 1.134 6.629 0.949 0.61 362995. 0.0272
|
|
92.29 0.6497
|
|
|
|
|
|
|
|
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 0.0891 0.0275 7.407 66.689 54.378 5523.079 7.535 241.875 4.466 0.69 407289. 0.7729
|
|
3.69 0.0223 0.0702 0.0877 0.0279 7.509 67.609 53.519 5599.291 7.638 238.051 4.335 0.69 407535. 0.7444
|
|
7.39 0.0446 0.1363 0.0862 0.0282 7.603 68.457 52.588 5669.478 7.734 233.913 4.207 0.69 407801. 0.7161
|
|
11.08 0.0669 0.1983 0.0846 0.0285 7.687 69.212 51.585 5732.021 7.820 229.451 4.082 0.69 408088. 0.6881
|
|
14.77 0.0892 0.2565 0.0828 0.0288 7.758 69.856 50.506 5785.346 7.892 224.649 3.960 0.69 408395. 0.6605
|
|
18.47 0.1114 0.3110 0.0809 0.0290 7.815 70.369 49.346 5827.821 7.950 219.492 3.841 0.69 408725. 0.6332
|
|
22.16 0.1337 0.3619 0.0789 0.0291 7.855 70.731 48.104 5857.805 7.991 213.966 3.725 0.69 409077. 0.6063
|
|
25.86 0.1560 0.4094 0.0767 0.0292 7.877 70.922 46.776 5873.605 8.013 208.060 3.612 0.70 409452. 0.5798
|
|
29.55 0.1783 0.4538 0.0744 0.0292 7.877 70.921 45.361 5873.536 8.013 201.764 3.503 0.70 409851. 0.5537
|
|
33.24 0.2006 0.4950 0.0719 0.0291 7.853 70.708 43.855 5855.896 7.989 195.067 3.397 0.70 410275. 0.5280
|
|
36.94 0.2229 0.5334 0.0693 0.0290 7.803 70.262 42.258 5818.999 7.938 187.963 3.294 0.70 410723. 0.5026
|
|
40.63 0.2452 0.5689 0.0665 0.0287 7.726 69.563 40.567 5761.074 7.859 180.442 3.194 0.70 411197. 0.4774
|
|
44.32 0.2675 0.6017 0.0636 0.0283 7.617 68.587 38.780 5680.245 7.749 172.494 3.097 0.70 411697. 0.4526
|
|
48.02 0.2898 0.6319 0.0605 0.0277 7.476 67.318 36.899 5575.128 7.606 164.126 3.002 0.70 412223. 0.4280
|
|
51.71 0.3120 0.6596 0.0573 0.0271 7.302 65.749 34.929 5445.205 7.428 155.366 2.910 0.70 412775. 0.4036
|
|
55.41 0.3343 0.6847 0.0539 0.0263 7.094 63.879 32.880 5290.329 7.217 146.249 2.819 0.70 413353. 0.3794
|
|
59.10 0.3566 0.7072 0.0504 0.0254 6.853 61.707 30.757 5110.469 6.972 136.805 2.730 0.70 413959. 0.3553
|
|
62.79 0.3789 0.7271 0.0468 0.0244 6.579 59.234 28.567 4905.654 6.692 127.066 2.641 0.70 414590. 0.3313
|
|
66.49 0.4012 0.7441 0.0431 0.0233 6.271 56.461 26.318 4675.983 6.379 117.063 2.553 0.70 415250. 0.3074
|
|
70.18 0.4235 0.7580 0.0394 0.0220 5.929 53.390 24.017 4421.627 6.032 106.825 2.464 0.70 415936. 0.2834
|
|
73.87 0.4458 0.7683 0.0355 0.0206 5.556 50.024 21.670 4142.869 5.652 96.387 2.372 0.70 416649. 0.2592
|
|
77.57 0.4681 0.7746 0.0316 0.0191 5.150 46.368 19.285 3840.142 5.239 85.780 2.278 0.70 417390. 0.2348
|
|
81.26 0.4904 0.7757 0.0277 0.0175 4.712 42.431 16.871 3514.064 4.794 75.040 2.178 0.70 418158. 0.2099
|
|
84.96 0.5126 0.7703 0.0237 0.0157 4.245 38.222 14.435 3165.516 4.318 64.208 2.068 0.70 418955. 0.1844
|
|
88.65 0.5349 0.7559 0.0197 0.0139 3.749 33.757 11.989 2795.681 3.814 53.325 1.945 0.70 419779. 0.1581
|
|
92.34 0.5572 0.7281 0.0156 0.0120 3.227 29.053 9.541 2406.112 3.282 42.440 1.799 0.70 420632. 0.1304
|
|
96.04 0.5795 0.6789 0.0116 0.0099 2.680 24.135 7.106 1998.809 2.727 31.606 1.612 0.71 421512. 0.1009
|
|
99.73 0.6018 0.5906 0.0077 0.0078 2.114 19.033 4.694 1576.263 2.150 20.881 1.351 0.71 422421. 0.0687
|
|
103.42 0.6241 0.4184 0.0038 0.0057 1.531 13.782 2.322 1141.432 1.557 10.329 0.923 0.71 423357. 0.0330
|
|
107.12 0.6464 -0.0055 0.0000 0.0034 0.930 8.373 -0.018 693.411 0.946 -0.079 -0.012 0.71 424277. 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 0.0914 0.0293 11.775 92.769 72.855 8780.555 10.481 324.061 3.763 0.79 465385. 0.7539
|
|
4.21 0.0222 0.0677 0.0901 0.0296 11.892 93.690 71.750 8867.750 10.585 319.142 3.670 0.79 465668. 0.7296
|
|
8.42 0.0445 0.1320 0.0885 0.0298 11.998 94.524 70.548 8946.656 10.679 313.796 3.577 0.79 465975. 0.7051
|
|
12.63 0.0667 0.1929 0.0869 0.0300 12.090 95.248 69.246 9015.203 10.761 308.005 3.484 0.79 466304. 0.6804
|
|
16.84 0.0889 0.2505 0.0851 0.0302 12.165 95.841 67.839 9071.260 10.828 301.747 3.392 0.79 466658. 0.6557
|
|
21.05 0.1112 0.3047 0.0832 0.0304 12.220 96.278 66.322 9112.627 10.877 295.002 3.301 0.79 467037. 0.6310
|
|
25.27 0.1334 0.3557 0.0812 0.0305 12.253 96.534 64.692 9136.907 10.906 287.749 3.211 0.79 467442. 0.6062
|
|
29.48 0.1556 0.4036 0.0790 0.0305 12.259 96.584 62.944 9141.641 10.912 279.973 3.123 0.79 467874. 0.5815
|
|
33.69 0.1779 0.4484 0.0767 0.0304 12.236 96.401 61.074 9124.267 10.891 271.658 3.036 0.79 468332. 0.5569
|
|
37.90 0.2001 0.4902 0.0742 0.0303 12.179 95.956 59.081 9082.146 10.841 262.793 2.951 0.79 468819. 0.5323
|
|
42.11 0.2223 0.5292 0.0715 0.0300 12.086 95.221 56.962 9012.578 10.758 253.367 2.867 0.80 469334. 0.5078
|
|
46.32 0.2446 0.5654 0.0687 0.0297 11.952 94.165 54.714 8912.692 10.639 243.368 2.784 0.80 469878. 0.4834
|
|
50.53 0.2668 0.5989 0.0657 0.0293 11.773 92.756 52.334 8779.346 10.480 232.782 2.704 0.80 470451. 0.4591
|
|
54.74 0.2890 0.6299 0.0625 0.0287 11.546 90.967 49.823 8609.931 10.277 221.614 2.625 0.80 471054. 0.4348
|
|
58.95 0.3113 0.6583 0.0592 0.0280 11.269 88.782 47.190 8403.185 10.031 209.901 2.547 0.80 471687. 0.4107
|
|
63.16 0.3335 0.6841 0.0558 0.0272 10.942 86.204 44.444 8159.155 9.739 197.687 2.471 0.80 472349. 0.3866
|
|
67.37 0.3557 0.7074 0.0522 0.0263 10.564 83.229 41.596 7877.540 9.403 185.017 2.395 0.80 473042. 0.3625
|
|
71.58 0.3780 0.7280 0.0485 0.0252 10.136 79.854 38.654 7558.098 9.022 171.933 2.320 0.80 473765. 0.3385
|
|
75.80 0.4002 0.7457 0.0447 0.0240 9.657 76.083 35.629 7201.252 8.596 158.477 2.244 0.80 474518. 0.3144
|
|
80.01 0.4224 0.7602 0.0408 0.0227 9.129 71.924 32.530 6807.601 8.126 144.692 2.167 0.80 475302. 0.2901
|
|
84.22 0.4447 0.7710 0.0369 0.0213 8.553 67.387 29.366 6378.177 7.613 130.619 2.088 0.80 476117. 0.2656
|
|
88.43 0.4669 0.7774 0.0328 0.0197 7.931 62.487 26.147 5914.384 7.060 116.304 2.005 0.80 476962. 0.2407
|
|
92.64 0.4891 0.7781 0.0287 0.0181 7.266 57.244 22.885 5418.113 6.467 101.794 1.916 0.80 477839. 0.2151
|
|
96.85 0.5114 0.7713 0.0246 0.0163 6.560 51.682 19.591 4891.687 5.839 87.141 1.817 0.80 478747. 0.1887
|
|
101.06 0.5336 0.7540 0.0204 0.0145 5.818 45.834 16.277 4338.137 5.178 72.402 1.702 0.80 479687. 0.1612
|
|
105.27 0.5558 0.7212 0.0163 0.0125 5.044 39.739 12.959 3761.227 4.490 57.640 1.563 0.81 480658. 0.1320
|
|
109.48 0.5781 0.6637 0.0121 0.0106 4.245 33.445 9.651 3165.529 3.779 42.928 1.383 0.81 481661. 0.1008
|
|
113.69 0.6003 0.5636 0.0080 0.0085 3.428 27.008 6.373 2556.336 3.051 28.346 1.131 0.81 482696. 0.0670
|
|
117.90 0.6225 0.3798 0.0039 0.0065 2.601 20.492 3.142 1939.602 2.315 13.977 0.735 0.81 483761. 0.0306
|
|
122.11 0.6448 -0.0084 -0.0001 0.0044 1.762 13.885 -0.045 1314.186 1.569 -0.201 -0.016 0.81 484812. 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 0.0939 0.0360 20.598 144.253 94.703 15360.098 16.298 421.240 2.797 0.89 523441. 0.6387
|
|
4.81 0.0226 0.0581 0.0926 0.0360 20.613 144.355 93.354 15370.967 16.309 415.241 2.755 0.89 523766. 0.6247
|
|
9.62 0.0452 0.1144 0.0911 0.0360 20.600 144.263 91.872 15361.253 16.299 408.647 2.713 0.89 524119. 0.6103
|
|
14.43 0.0677 0.1689 0.0895 0.0359 20.557 143.964 90.251 15329.422 16.265 401.434 2.670 0.89 524499. 0.5954
|
|
19.24 0.0903 0.2217 0.0878 0.0358 20.482 143.439 88.482 15273.471 16.206 393.569 2.628 0.89 524908. 0.5801
|
|
24.05 0.1129 0.2725 0.0858 0.0356 20.372 142.667 86.560 15191.229 16.118 385.018 2.584 0.89 525346. 0.5644
|
|
28.86 0.1355 0.3215 0.0838 0.0353 20.223 141.628 84.477 15080.614 16.001 375.753 2.541 0.89 525816. 0.5481
|
|
33.67 0.1580 0.3685 0.0815 0.0350 20.034 140.301 82.227 14939.300 15.851 365.747 2.496 0.89 526316. 0.5313
|
|
38.48 0.1806 0.4136 0.0791 0.0346 19.800 138.664 79.806 14765.026 15.666 354.976 2.452 0.89 526850. 0.5140
|
|
43.29 0.2032 0.4566 0.0766 0.0341 19.519 136.696 77.208 14555.491 15.444 343.423 2.406 0.89 527415. 0.4962
|
|
48.10 0.2258 0.4976 0.0738 0.0335 19.188 134.375 74.432 14308.293 15.182 331.075 2.359 0.89 528014. 0.4778
|
|
52.91 0.2483 0.5364 0.0709 0.0328 18.802 131.674 71.474 14020.771 14.876 317.917 2.312 0.90 528647. 0.4588
|
|
57.73 0.2709 0.5729 0.0678 0.0320 18.358 128.565 68.330 13689.729 14.525 303.932 2.264 0.90 529314. 0.4392
|
|
62.54 0.2935 0.6072 0.0645 0.0312 17.852 125.022 65.002 13312.404 14.125 289.128 2.215 0.90 530016. 0.4191
|
|
67.35 0.3161 0.6390 0.0610 0.0302 17.283 121.036 61.502 12887.999 13.675 273.560 2.164 0.90 530752. 0.3984
|
|
72.16 0.3387 0.6684 0.0574 0.0291 16.651 116.607 57.845 12416.382 13.174 257.294 2.113 0.90 531522. 0.3772
|
|
76.97 0.3612 0.6946 0.0536 0.0279 15.968 111.823 54.044 11907.018 12.634 240.387 2.059 0.90 532327. 0.3552
|
|
81.78 0.3838 0.7166 0.0497 0.0266 15.249 106.788 50.111 11370.902 12.065 222.895 1.999 0.90 533167. 0.3321
|
|
86.59 0.4064 0.7335 0.0457 0.0253 14.499 101.537 46.060 10811.671 11.472 204.875 1.932 0.90 534042. 0.3078
|
|
91.40 0.4290 0.7436 0.0416 0.0240 13.733 96.172 41.902 10240.503 10.866 186.381 1.856 0.90 534952. 0.2820
|
|
96.21 0.4515 0.7467 0.0373 0.0226 12.936 90.593 37.654 9646.435 10.235 167.484 1.770 0.90 535898. 0.2550
|
|
101.02 0.4741 0.7424 0.0331 0.0211 12.094 84.696 33.333 9018.437 9.569 148.263 1.676 0.90 536879. 0.2272
|
|
105.83 0.4967 0.7286 0.0287 0.0196 11.214 78.536 28.955 8362.598 8.873 128.790 1.570 0.90 537896. 0.1983
|
|
110.64 0.5193 0.7023 0.0243 0.0180 10.308 72.191 24.538 7686.910 8.156 109.143 1.448 0.90 538948. 0.1683
|
|
115.45 0.5418 0.6594 0.0199 0.0164 9.384 65.719 20.102 6997.802 7.425 89.412 1.303 0.91 540037. 0.1371
|
|
120.26 0.5644 0.5944 0.0155 0.0148 8.453 59.198 15.669 6303.462 6.688 69.698 1.128 0.91 541162. 0.1048
|
|
125.07 0.5870 0.4992 0.0112 0.0131 7.527 52.710 11.267 5612.578 5.955 50.114 0.910 0.91 542323. 0.0717
|
|
129.88 0.6096 0.3623 0.0069 0.0115 6.617 46.337 6.922 4933.983 5.235 30.787 0.636 0.91 543521. 0.0393
|
|
134.69 0.6322 0.1668 0.0026 0.0100 5.732 40.141 2.663 4274.202 4.535 11.843 0.283 0.91 544753. 0.0108
|
|
139.50 0.6547
|
|
|
|
|
|
|