353 lines
63 KiB
Plaintext
353 lines
63 KiB
Plaintext
26x15E (26x15E.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 0.0898 0.0325 0.031 1.957 1.307 23.155 0.221 5.816 25.611 0.10 61813. 0.6609
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0.62 0.0250 0.0672 0.0885 0.0330 0.032 1.987 1.289 23.504 0.224 5.733 24.873 0.10 61854. 0.6373
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1.23 0.0501 0.1305 0.0871 0.0334 0.032 2.015 1.269 23.838 0.228 5.643 24.141 0.10 61899. 0.6137
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1.85 0.0751 0.1899 0.0856 0.0339 0.032 2.041 1.247 24.150 0.231 5.546 23.417 0.10 61947. 0.5901
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2.47 0.1002 0.2454 0.0840 0.0343 0.033 2.065 1.223 24.433 0.233 5.440 22.704 0.10 62000. 0.5666
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3.08 0.1252 0.2973 0.0822 0.0346 0.033 2.086 1.197 24.680 0.236 5.325 22.002 0.10 62057. 0.5433
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3.70 0.1502 0.3456 0.0803 0.0349 0.033 2.103 1.169 24.883 0.238 5.201 21.314 0.10 62119. 0.5201
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4.32 0.1753 0.3905 0.0782 0.0351 0.034 2.116 1.139 25.034 0.239 5.067 20.641 0.10 62185. 0.4972
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4.93 0.2003 0.4320 0.0760 0.0352 0.034 2.124 1.107 25.126 0.240 4.924 19.982 0.10 62256. 0.4744
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5.55 0.2253 0.4703 0.0736 0.0353 0.034 2.126 1.072 25.150 0.240 4.769 19.338 0.10 62332. 0.4519
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6.16 0.2504 0.5056 0.0711 0.0352 0.034 2.121 1.035 25.097 0.240 4.604 18.708 0.10 62413. 0.4296
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6.78 0.2754 0.5378 0.0684 0.0350 0.033 2.110 0.996 24.960 0.238 4.429 18.092 0.10 62499. 0.4074
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7.40 0.3005 0.5671 0.0655 0.0347 0.033 2.090 0.954 24.732 0.236 4.242 17.488 0.10 62591. 0.3854
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8.01 0.3255 0.5935 0.0624 0.0342 0.033 2.063 0.909 24.404 0.233 4.043 16.894 0.10 62687. 0.3635
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8.63 0.3505 0.6170 0.0592 0.0336 0.032 2.026 0.862 23.969 0.229 3.833 16.308 0.10 62789. 0.3416
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9.25 0.3756 0.6375 0.0558 0.0329 0.031 1.980 0.812 23.423 0.224 3.612 15.726 0.10 62897. 0.3198
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9.86 0.4006 0.6549 0.0522 0.0319 0.031 1.924 0.760 22.769 0.217 3.382 15.145 0.10 63009. 0.2980
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10.48 0.4256 0.6689 0.0485 0.0309 0.030 1.860 0.706 22.009 0.210 3.142 14.560 0.10 63127. 0.2762
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11.10 0.4507 0.6793 0.0447 0.0297 0.028 1.787 0.651 21.145 0.202 2.896 13.965 0.10 63251. 0.2543
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11.71 0.4757 0.6856 0.0408 0.0283 0.027 1.706 0.594 20.181 0.193 2.643 13.352 0.10 63380. 0.2323
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12.33 0.5008 0.6872 0.0368 0.0268 0.026 1.616 0.536 19.120 0.183 2.384 12.714 0.10 63514. 0.2100
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12.95 0.5258 0.6832 0.0327 0.0252 0.024 1.518 0.477 17.964 0.172 2.121 12.037 0.10 63654. 0.1876
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13.56 0.5508 0.6723 0.0286 0.0234 0.022 1.413 0.417 16.717 0.160 1.854 11.308 0.10 63799. 0.1648
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14.18 0.5759 0.6529 0.0245 0.0216 0.021 1.300 0.356 15.384 0.147 1.585 10.504 0.10 63949. 0.1415
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14.79 0.6009 0.6223 0.0203 0.0196 0.019 1.181 0.295 13.969 0.133 1.314 9.594 0.11 64106. 0.1177
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15.41 0.6259 0.5763 0.0161 0.0175 0.017 1.055 0.235 12.481 0.119 1.044 8.530 0.11 64267. 0.0933
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16.03 0.6510 0.5084 0.0120 0.0153 0.015 0.923 0.174 10.926 0.104 0.775 7.236 0.11 64434. 0.0682
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16.64 0.6760 0.4070 0.0079 0.0131 0.012 0.787 0.115 9.314 0.089 0.510 5.578 0.11 64607. 0.0426
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17.26 0.7011 0.2504 0.0038 0.0107 0.010 0.647 0.056 7.656 0.073 0.248 3.309 0.11 64785. 0.0176
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17.88 0.7261 -0.0089 -0.0001 0.0084 0.008 0.504 -0.001 5.962 0.057 -0.007 -0.114 0.11 64966. 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 0.0902 0.0307 0.235 7.394 5.256 174.959 0.835 23.378 13.626 0.21 123622. 0.7050
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1.23 0.0251 0.0715 0.0890 0.0312 0.239 7.519 5.182 177.921 0.850 23.050 13.211 0.21 123705. 0.6787
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2.47 0.0502 0.1386 0.0876 0.0317 0.242 7.639 5.102 180.765 0.863 22.692 12.801 0.21 123794. 0.6525
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3.70 0.0752 0.2014 0.0861 0.0322 0.246 7.752 5.014 183.436 0.876 22.302 12.398 0.21 123892. 0.6265
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4.94 0.1003 0.2599 0.0844 0.0326 0.249 7.855 4.919 185.878 0.888 21.879 12.003 0.21 123998. 0.6008
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6.17 0.1254 0.3144 0.0827 0.0330 0.252 7.946 4.816 188.032 0.898 21.420 11.616 0.21 124113. 0.5753
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7.41 0.1505 0.3651 0.0808 0.0333 0.255 8.023 4.704 189.834 0.906 20.923 11.239 0.21 124237. 0.5501
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8.64 0.1756 0.4120 0.0787 0.0335 0.256 8.081 4.583 191.216 0.913 20.387 10.872 0.21 124370. 0.5253
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9.88 0.2006 0.4554 0.0765 0.0337 0.258 8.119 4.454 192.112 0.917 19.811 10.515 0.21 124512. 0.5008
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11.11 0.2257 0.4955 0.0741 0.0337 0.258 8.133 4.315 192.452 0.919 19.192 10.169 0.21 124665. 0.4767
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12.35 0.2508 0.5323 0.0715 0.0337 0.258 8.121 4.166 192.170 0.918 18.529 9.832 0.21 124828. 0.4529
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13.58 0.2759 0.5661 0.0688 0.0335 0.256 8.080 4.007 191.198 0.913 17.822 9.505 0.21 125000. 0.4294
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14.82 0.3009 0.5969 0.0659 0.0332 0.254 8.007 3.838 189.472 0.905 17.071 9.187 0.21 125184. 0.4062
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16.05 0.3260 0.6248 0.0628 0.0328 0.251 7.900 3.658 186.923 0.892 16.273 8.877 0.21 125378. 0.3832
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17.29 0.3511 0.6499 0.0595 0.0322 0.246 7.754 3.469 183.484 0.876 15.428 8.574 0.21 125582. 0.3604
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18.52 0.3762 0.6721 0.0561 0.0314 0.240 7.570 3.269 179.131 0.855 14.539 8.277 0.21 125798. 0.3377
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19.76 0.4013 0.6915 0.0525 0.0305 0.233 7.348 3.060 173.871 0.830 13.611 7.983 0.21 126024. 0.3151
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20.99 0.4263 0.7078 0.0488 0.0294 0.225 7.088 2.844 167.722 0.801 12.649 7.690 0.21 126261. 0.2927
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22.23 0.4514 0.7208 0.0450 0.0282 0.216 6.791 2.621 160.701 0.767 11.656 7.396 0.21 126509. 0.2702
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23.46 0.4765 0.7301 0.0411 0.0268 0.205 6.459 2.392 152.829 0.730 10.638 7.098 0.21 126767. 0.2477
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24.70 0.5016 0.7352 0.0370 0.0253 0.193 6.091 2.158 144.127 0.688 9.597 6.790 0.21 127037. 0.2251
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25.93 0.5267 0.7354 0.0330 0.0236 0.181 5.689 1.920 134.620 0.643 8.539 6.468 0.21 127317. 0.2023
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27.17 0.5517 0.7295 0.0288 0.0218 0.167 5.255 1.679 124.338 0.594 7.468 6.124 0.21 127608. 0.1791
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28.40 0.5768 0.7157 0.0247 0.0199 0.152 4.789 1.436 113.317 0.541 6.387 5.748 0.21 127910. 0.1554
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29.64 0.6019 0.6915 0.0205 0.0178 0.136 4.294 1.192 101.603 0.485 5.302 5.322 0.21 128224. 0.1311
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30.87 0.6270 0.6523 0.0163 0.0156 0.120 3.772 0.948 89.252 0.426 4.218 4.820 0.21 128548. 0.1059
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32.11 0.6521 0.5907 0.0121 0.0134 0.102 3.226 0.706 76.331 0.364 3.141 4.197 0.21 128883. 0.0796
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33.34 0.6771 0.4921 0.0080 0.0110 0.084 2.659 0.467 62.922 0.300 2.077 3.366 0.21 129229. 0.0519
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34.58 0.7022 0.3251 0.0040 0.0086 0.066 2.076 0.232 49.123 0.235 1.033 2.144 0.21 129586. 0.0233
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35.81 0.7273 0.0060 0.0001 0.0061 0.047 1.479 0.003 35.006 0.167 0.013 0.038 0.21 129949. 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 0.0908 0.0301 0.776 16.312 11.906 578.983 1.843 52.956 9.327 0.31 185426. 0.7263
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1.87 0.0253 0.0740 0.0896 0.0306 0.790 16.605 11.739 589.387 1.876 52.216 9.034 0.31 185550. 0.6985
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3.74 0.0506 0.1432 0.0882 0.0311 0.804 16.887 11.557 599.389 1.908 51.407 8.746 0.31 185686. 0.6710
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5.60 0.0759 0.2079 0.0867 0.0316 0.816 17.152 11.359 608.795 1.938 50.524 8.463 0.31 185835. 0.6437
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7.47 0.1012 0.2681 0.0850 0.0321 0.828 17.395 11.143 617.409 1.965 49.563 8.186 0.31 185996. 0.6167
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9.34 0.1264 0.3241 0.0832 0.0325 0.838 17.609 10.908 625.018 1.989 48.519 7.916 0.31 186170. 0.5900
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11.21 0.1517 0.3760 0.0813 0.0328 0.847 17.789 10.654 631.394 2.010 47.388 7.653 0.31 186358. 0.5638
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13.08 0.1770 0.4241 0.0792 0.0331 0.853 17.927 10.379 636.303 2.025 46.166 7.398 0.31 186561. 0.5379
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14.94 0.2023 0.4685 0.0769 0.0332 0.858 18.017 10.083 639.502 2.036 44.849 7.151 0.31 186778. 0.5125
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16.81 0.2276 0.5094 0.0745 0.0333 0.859 18.053 9.765 640.749 2.040 43.434 6.912 0.31 187010. 0.4875
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18.68 0.2529 0.5471 0.0719 0.0332 0.858 18.026 9.424 639.803 2.037 41.917 6.681 0.31 187258. 0.4628
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20.55 0.2782 0.5816 0.0691 0.0331 0.853 17.931 9.060 636.429 2.026 40.298 6.457 0.31 187521. 0.4386
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22.42 0.3035 0.6131 0.0662 0.0327 0.845 17.761 8.672 630.395 2.007 38.574 6.240 0.31 187801. 0.4147
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24.28 0.3288 0.6418 0.0630 0.0323 0.833 17.509 8.260 621.456 1.978 36.742 6.029 0.31 188096. 0.3910
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26.15 0.3540 0.6677 0.0597 0.0317 0.817 17.169 7.824 609.381 1.940 34.802 5.824 0.31 188408. 0.3676
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28.02 0.3793 0.6907 0.0562 0.0309 0.797 16.738 7.365 594.088 1.891 32.761 5.623 0.31 188736. 0.3444
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29.89 0.4046 0.7110 0.0525 0.0299 0.772 16.217 6.886 575.605 1.832 30.630 5.426 0.31 189080. 0.3214
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31.75 0.4299 0.7283 0.0487 0.0288 0.743 15.608 6.389 553.987 1.763 28.420 5.231 0.31 189441. 0.2984
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33.62 0.4552 0.7424 0.0448 0.0275 0.710 14.912 5.877 529.296 1.685 26.142 5.036 0.31 189819. 0.2755
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35.49 0.4805 0.7530 0.0408 0.0261 0.673 14.132 5.352 501.598 1.597 23.805 4.839 0.31 190213. 0.2527
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37.36 0.5058 0.7595 0.0367 0.0245 0.632 13.269 4.815 470.967 1.499 21.419 4.638 0.31 190623. 0.2297
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39.23 0.5311 0.7613 0.0326 0.0227 0.587 12.326 4.270 437.494 1.393 18.993 4.427 0.31 191050. 0.2065
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41.09 0.5564 0.7571 0.0284 0.0208 0.538 11.306 3.718 401.287 1.277 16.538 4.203 0.31 191494. 0.1829
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42.96 0.5816 0.7452 0.0241 0.0188 0.486 10.213 3.162 362.479 1.154 14.065 3.957 0.31 191954. 0.1588
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44.83 0.6069 0.7226 0.0199 0.0167 0.431 9.051 2.604 321.237 1.023 11.583 3.677 0.32 192431. 0.1339
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46.70 0.6322 0.6845 0.0156 0.0144 0.372 7.826 2.047 277.769 0.884 9.107 3.343 0.32 192925. 0.1080
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48.57 0.6575 0.6214 0.0114 0.0121 0.312 6.546 1.495 232.330 0.740 6.650 2.919 0.32 193436. 0.0805
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50.43 0.6828 0.5145 0.0072 0.0096 0.248 5.219 0.950 185.227 0.590 4.227 2.327 0.32 193963. 0.0512
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52.30 0.7081 0.3167 0.0032 0.0071 0.183 3.855 0.417 136.818 0.436 1.853 1.381 0.32 194506. 0.0201
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54.17 0.7334
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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 0.0917 0.0300 1.833 28.883 21.361 1366.862 3.263 95.012 7.088 0.41 247219. 0.7393
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2.47 0.0251 0.0744 0.0904 0.0305 1.867 29.415 21.069 1392.052 3.323 93.716 6.865 0.41 247384. 0.7111
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4.95 0.0502 0.1441 0.0891 0.0310 1.899 29.927 20.750 1416.303 3.381 92.298 6.645 0.41 247565. 0.6832
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7.42 0.0754 0.2092 0.0876 0.0315 1.930 30.410 20.402 1439.156 3.436 90.748 6.430 0.41 247761. 0.6554
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9.89 0.1005 0.2698 0.0859 0.0320 1.958 30.854 20.022 1460.139 3.486 89.060 6.220 0.41 247975. 0.6281
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12.37 0.1256 0.3261 0.0842 0.0324 1.983 31.247 19.610 1478.747 3.530 87.224 6.015 0.41 248206. 0.6011
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14.84 0.1507 0.3784 0.0822 0.0328 2.004 31.578 19.162 1494.438 3.568 85.232 5.816 0.41 248455. 0.5745
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17.32 0.1758 0.4268 0.0802 0.0330 2.020 31.837 18.678 1506.657 3.597 83.078 5.623 0.41 248723. 0.5484
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19.79 0.2009 0.4716 0.0779 0.0332 2.031 32.009 18.155 1514.824 3.616 80.754 5.436 0.41 249010. 0.5227
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22.26 0.2261 0.5129 0.0755 0.0333 2.036 32.084 17.593 1518.363 3.625 78.254 5.255 0.41 249318. 0.4975
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24.74 0.2512 0.5510 0.0729 0.0332 2.034 32.049 16.990 1516.698 3.621 75.573 5.081 0.41 249645. 0.4726
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27.21 0.2763 0.5860 0.0702 0.0331 2.024 31.892 16.346 1509.270 3.603 72.708 4.912 0.41 249993. 0.4482
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29.68 0.3014 0.6181 0.0672 0.0328 2.006 31.601 15.660 1495.527 3.570 69.656 4.749 0.41 250362. 0.4242
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32.16 0.3265 0.6473 0.0641 0.0323 1.978 31.165 14.931 1474.894 3.521 66.411 4.592 0.41 250752. 0.4004
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34.63 0.3517 0.6739 0.0608 0.0317 1.940 30.572 14.157 1446.800 3.454 62.972 4.438 0.42 251164. 0.3769
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37.11 0.3768 0.6977 0.0573 0.0309 1.892 29.815 13.343 1410.993 3.368 59.350 4.289 0.42 251597. 0.3536
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39.58 0.4019 0.7189 0.0536 0.0300 1.834 28.896 12.492 1367.512 3.265 55.564 4.143 0.42 252052. 0.3305
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42.05 0.4270 0.7373 0.0498 0.0289 1.765 27.818 11.608 1316.479 3.143 51.634 3.999 0.42 252528. 0.3075
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44.53 0.4521 0.7528 0.0459 0.0276 1.687 26.583 10.696 1258.036 3.003 47.578 3.856 0.42 253026. 0.2846
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47.00 0.4772 0.7650 0.0419 0.0261 1.599 25.195 9.760 1192.336 2.846 43.414 3.713 0.42 253546. 0.2618
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49.47 0.5024 0.7736 0.0378 0.0245 1.501 23.657 8.804 1119.551 2.673 39.160 3.567 0.42 254087. 0.2388
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51.95 0.5275 0.7779 0.0336 0.0228 1.395 21.973 7.831 1039.886 2.483 34.832 3.416 0.42 254650. 0.2157
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54.42 0.5526 0.7768 0.0294 0.0209 1.279 20.150 6.845 953.590 2.277 30.448 3.256 0.42 255235. 0.1922
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56.90 0.5777 0.7689 0.0251 0.0189 1.155 18.193 5.851 860.974 2.055 26.027 3.083 0.42 255841. 0.1683
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59.37 0.6028 0.7515 0.0208 0.0167 1.022 16.110 4.854 762.423 1.820 21.589 2.887 0.42 256470. 0.1436
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61.84 0.6279 0.7203 0.0166 0.0144 0.883 13.913 3.857 658.418 1.572 17.155 2.657 0.42 257121. 0.1178
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64.32 0.6531 0.6671 0.0123 0.0120 0.737 11.612 2.867 549.551 1.312 12.751 2.366 0.42 257793. 0.0904
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66.79 0.6782 0.5747 0.0081 0.0096 0.585 9.224 1.889 436.541 1.042 8.402 1.963 0.42 258487. 0.0609
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69.26 0.7033 0.4001 0.0040 0.0070 0.429 6.767 0.930 320.237 0.765 4.138 1.318 0.42 259203. 0.0287
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71.74 0.7284 -0.0048 0.0000 0.0044 0.270 4.249 -0.007 201.074 0.480 -0.030 -0.015 0.42 259924. 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 0.0928 0.0301 3.602 45.412 33.779 2686.381 5.131 150.249 5.703 0.52 308997. 0.7481
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3.09 0.0251 0.0748 0.0915 0.0307 3.670 46.269 33.330 2737.086 5.227 148.252 5.523 0.52 309204. 0.7196
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6.18 0.0502 0.1449 0.0902 0.0313 3.736 47.095 32.837 2785.945 5.321 146.059 5.346 0.52 309430. 0.6914
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9.27 0.0753 0.2103 0.0887 0.0318 3.798 47.874 32.297 2832.023 5.409 143.657 5.173 0.52 309677. 0.6634
|
|
12.36 0.1004 0.2712 0.0871 0.0323 3.855 48.590 31.707 2874.371 5.490 141.033 5.003 0.52 309945. 0.6358
|
|
15.46 0.1255 0.3278 0.0853 0.0327 3.905 49.225 31.064 2911.965 5.561 138.173 4.839 0.52 310234. 0.6086
|
|
18.55 0.1507 0.3804 0.0834 0.0330 3.948 49.762 30.365 2943.730 5.622 135.064 4.679 0.52 310547. 0.5818
|
|
21.64 0.1758 0.4291 0.0813 0.0333 3.981 50.181 29.607 2968.530 5.669 131.693 4.524 0.52 310883. 0.5555
|
|
24.73 0.2009 0.4742 0.0791 0.0335 4.003 50.464 28.788 2985.218 5.701 128.049 4.374 0.52 311243. 0.5296
|
|
27.82 0.2260 0.5158 0.0766 0.0336 4.013 50.589 27.906 2992.621 5.715 124.124 4.229 0.52 311628. 0.5042
|
|
30.91 0.2511 0.5542 0.0740 0.0335 4.009 50.538 26.958 2989.592 5.710 119.908 4.090 0.52 312039. 0.4792
|
|
34.00 0.2762 0.5896 0.0713 0.0334 3.990 50.291 25.943 2975.002 5.682 115.396 3.955 0.52 312475. 0.4547
|
|
37.09 0.3013 0.6221 0.0683 0.0331 3.953 49.830 24.861 2947.756 5.630 110.582 3.825 0.52 312938. 0.4304
|
|
40.18 0.3264 0.6518 0.0651 0.0326 3.898 49.137 23.710 2906.715 5.551 105.460 3.700 0.52 313427. 0.4066
|
|
43.28 0.3515 0.6788 0.0618 0.0320 3.823 48.190 22.488 2850.727 5.444 100.025 3.578 0.52 313942. 0.3829
|
|
46.37 0.3766 0.7032 0.0582 0.0312 3.727 46.982 21.199 2779.236 5.308 94.293 3.460 0.52 314485. 0.3595
|
|
49.46 0.4017 0.7251 0.0545 0.0302 3.610 45.512 19.851 2692.299 5.142 88.296 3.344 0.52 315054. 0.3363
|
|
52.55 0.4269 0.7443 0.0507 0.0291 3.473 43.785 18.450 2590.156 4.947 82.065 3.231 0.52 315650. 0.3132
|
|
55.64 0.4520 0.7607 0.0467 0.0277 3.316 41.806 17.003 2473.093 4.723 75.631 3.118 0.52 316273. 0.2902
|
|
58.73 0.4771 0.7740 0.0426 0.0263 3.140 39.580 15.517 2341.418 4.472 69.021 3.006 0.52 316923. 0.2672
|
|
61.82 0.5022 0.7838 0.0384 0.0246 2.944 37.113 13.998 2195.478 4.193 62.263 2.892 0.52 317600. 0.2442
|
|
64.91 0.5273 0.7895 0.0342 0.0228 2.730 34.412 12.452 2035.684 3.888 55.385 2.774 0.52 318304. 0.2209
|
|
68.00 0.5524 0.7902 0.0299 0.0209 2.498 31.485 10.885 1862.535 3.557 48.415 2.651 0.52 319036. 0.1974
|
|
71.10 0.5775 0.7844 0.0256 0.0188 2.248 28.343 9.304 1676.657 3.202 41.383 2.517 0.52 319794. 0.1732
|
|
74.19 0.6026 0.7697 0.0212 0.0166 1.983 24.999 7.716 1478.826 2.824 34.321 2.367 0.53 320580. 0.1484
|
|
77.28 0.6277 0.7416 0.0168 0.0143 1.703 21.469 6.130 1270.013 2.426 27.265 2.189 0.53 321393. 0.1223
|
|
80.37 0.6528 0.6921 0.0125 0.0118 1.410 17.774 4.553 1051.415 2.008 20.254 1.964 0.53 322233. 0.0946
|
|
83.46 0.6779 0.6032 0.0082 0.0093 1.106 13.938 2.997 824.496 1.575 13.330 1.649 0.53 323101. 0.0644
|
|
86.55 0.7031 0.4282 0.0040 0.0066 0.793 9.990 1.470 590.982 1.129 6.540 1.128 0.53 323995. 0.0309
|
|
89.64 0.7282 -0.0115 -0.0001 0.0039 0.471 5.943 -0.023 351.578 0.671 -0.101 -0.029 0.53 324892. 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 0.0942 0.0306 6.319 66.383 49.390 4712.308 7.500 219.688 4.754 0.62 370754. 0.7540
|
|
3.73 0.0252 0.0753 0.0930 0.0312 6.442 67.671 48.754 4803.763 7.645 216.856 4.603 0.62 371005. 0.7254
|
|
7.46 0.0505 0.1457 0.0917 0.0318 6.560 68.913 48.051 4891.931 7.786 213.732 4.455 0.62 371279. 0.6970
|
|
11.19 0.0757 0.2114 0.0902 0.0323 6.672 70.085 47.279 4975.100 7.918 210.295 4.310 0.62 371578. 0.6689
|
|
14.92 0.1010 0.2726 0.0886 0.0328 6.774 71.161 46.431 5051.523 8.040 206.524 4.169 0.62 371903. 0.6411
|
|
18.65 0.1262 0.3296 0.0868 0.0332 6.865 72.116 45.503 5119.314 8.148 202.397 4.032 0.62 372255. 0.6137
|
|
22.38 0.1515 0.3824 0.0849 0.0336 6.942 72.922 44.491 5176.509 8.239 197.894 3.898 0.62 372635. 0.5868
|
|
26.10 0.1767 0.4314 0.0828 0.0339 7.002 73.549 43.389 5221.036 8.310 192.995 3.769 0.62 373043. 0.5603
|
|
29.83 0.2020 0.4767 0.0805 0.0341 7.041 73.968 42.195 5250.782 8.357 187.684 3.645 0.62 373481. 0.5343
|
|
33.56 0.2272 0.5186 0.0780 0.0342 7.059 74.149 40.905 5263.639 8.377 181.945 3.525 0.62 373949. 0.5088
|
|
37.29 0.2524 0.5573 0.0754 0.0341 7.050 74.063 39.516 5257.498 8.368 175.767 3.409 0.62 374448. 0.4836
|
|
41.02 0.2777 0.5930 0.0725 0.0340 7.014 73.680 38.026 5230.331 8.324 169.138 3.298 0.62 374979. 0.4589
|
|
44.75 0.3029 0.6258 0.0695 0.0336 6.947 72.973 36.433 5180.155 8.244 162.053 3.190 0.62 375541. 0.4345
|
|
48.48 0.3282 0.6559 0.0663 0.0331 6.846 71.914 34.735 5104.939 8.125 154.502 3.086 0.62 376135. 0.4105
|
|
52.21 0.3534 0.6834 0.0628 0.0325 6.709 70.472 32.931 5002.618 7.962 146.476 2.986 0.62 376762. 0.3867
|
|
55.94 0.3787 0.7083 0.0592 0.0316 6.534 68.635 31.026 4872.191 7.754 138.002 2.888 0.62 377421. 0.3631
|
|
59.67 0.4039 0.7307 0.0554 0.0306 6.321 66.403 29.030 4713.783 7.502 129.126 2.793 0.62 378112. 0.3397
|
|
63.40 0.4292 0.7505 0.0514 0.0294 6.072 63.784 26.955 4527.853 7.206 119.896 2.700 0.62 378836. 0.3164
|
|
67.13 0.4544 0.7675 0.0473 0.0280 5.786 60.785 24.811 4314.932 6.867 110.358 2.608 0.63 379593. 0.2932
|
|
70.86 0.4796 0.7815 0.0431 0.0265 5.465 57.413 22.607 4075.606 6.487 100.554 2.516 0.63 380382. 0.2700
|
|
74.59 0.5049 0.7921 0.0388 0.0247 5.110 53.679 20.352 3810.515 6.065 90.527 2.423 0.63 381204. 0.2466
|
|
78.31 0.5301 0.7987 0.0344 0.0229 4.721 49.593 18.057 3520.440 5.603 80.318 2.326 0.63 382058. 0.2231
|
|
82.04 0.5554 0.8004 0.0300 0.0208 4.300 45.168 15.731 3206.315 5.103 69.970 2.225 0.63 382945. 0.1992
|
|
85.77 0.5806 0.7955 0.0255 0.0186 3.848 40.420 13.383 2869.312 4.567 59.530 2.116 0.63 383865. 0.1747
|
|
89.50 0.6059 0.7815 0.0210 0.0163 3.367 35.371 11.027 2510.894 3.996 49.046 1.992 0.63 384818. 0.1493
|
|
93.23 0.6311 0.7538 0.0165 0.0138 2.860 30.046 8.672 2132.887 3.395 38.574 1.844 0.63 385804. 0.1226
|
|
96.96 0.6564 0.7028 0.0121 0.0113 2.330 24.477 6.334 1737.560 2.765 28.173 1.653 0.63 386823. 0.0939
|
|
100.69 0.6816 0.6072 0.0077 0.0086 1.780 18.703 4.027 1327.684 2.113 17.911 1.376 0.63 387875. 0.0623
|
|
104.42 0.7068 0.4047 0.0034 0.0059 1.216 12.770 1.767 906.506 1.443 7.859 0.884 0.63 388958. 0.0265
|
|
108.15 0.7321
|
|
|
|
|
|
|
|
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 0.0960 0.0315 10.329 93.004 68.518 7702.453 10.508 304.766 4.035 0.72 432482. 0.7537
|
|
4.35 0.0252 0.0745 0.0948 0.0321 10.524 94.755 67.683 7847.410 10.705 301.056 3.912 0.72 432775. 0.7263
|
|
8.69 0.0504 0.1444 0.0936 0.0327 10.712 96.450 66.757 7987.798 10.897 296.936 3.791 0.72 433096. 0.6990
|
|
13.04 0.0756 0.2098 0.0921 0.0332 10.890 98.056 65.732 8120.837 11.078 292.376 3.671 0.72 433446. 0.6717
|
|
17.38 0.1009 0.2708 0.0905 0.0337 11.055 99.539 64.600 8243.664 11.246 287.342 3.554 0.72 433827. 0.6447
|
|
21.73 0.1261 0.3277 0.0888 0.0342 11.202 100.862 63.355 8353.184 11.395 281.802 3.440 0.72 434239. 0.6179
|
|
26.07 0.1513 0.3805 0.0869 0.0345 11.326 101.983 61.989 8446.077 11.522 275.726 3.329 0.72 434683. 0.5915
|
|
30.42 0.1765 0.4295 0.0848 0.0348 11.424 102.862 60.496 8518.848 11.621 269.085 3.221 0.72 435162. 0.5654
|
|
34.76 0.2017 0.4750 0.0825 0.0350 11.490 103.454 58.870 8567.875 11.688 261.854 3.116 0.72 435674. 0.5396
|
|
39.11 0.2269 0.5170 0.0800 0.0351 11.519 103.715 57.107 8589.468 11.718 254.011 3.016 0.72 436223. 0.5143
|
|
43.45 0.2521 0.5559 0.0774 0.0351 11.506 103.600 55.202 8579.967 11.705 245.538 2.918 0.72 436807. 0.4893
|
|
47.80 0.2773 0.5919 0.0745 0.0349 11.447 103.067 53.152 8535.791 11.644 236.421 2.824 0.72 437428. 0.4647
|
|
52.15 0.3026 0.6250 0.0714 0.0346 11.336 102.074 50.955 8453.551 11.532 226.650 2.734 0.73 438086. 0.4404
|
|
56.49 0.3278 0.6555 0.0681 0.0341 11.171 100.581 48.609 8329.952 11.364 216.213 2.647 0.73 438782. 0.4165
|
|
60.84 0.3530 0.6834 0.0646 0.0334 10.945 98.548 46.110 8161.595 11.134 205.097 2.563 0.73 439514. 0.3927
|
|
65.18 0.3782 0.7089 0.0609 0.0325 10.657 95.953 43.465 7946.620 10.841 193.332 2.481 0.73 440285. 0.3691
|
|
69.53 0.4034 0.7320 0.0570 0.0314 10.306 92.795 40.689 7685.156 10.484 180.984 2.401 0.73 441093. 0.3457
|
|
73.87 0.4286 0.7525 0.0530 0.0302 9.894 89.086 37.797 7377.988 10.065 168.120 2.324 0.73 441939. 0.3224
|
|
78.22 0.4538 0.7704 0.0488 0.0287 9.422 84.837 34.804 7026.049 9.585 154.807 2.247 0.73 442823. 0.2991
|
|
82.56 0.4790 0.7855 0.0445 0.0271 8.891 80.059 31.723 6630.344 9.045 141.105 2.170 0.73 443744. 0.2758
|
|
86.91 0.5043 0.7973 0.0400 0.0253 8.304 74.766 28.568 6192.000 8.447 127.072 2.093 0.73 444704. 0.2524
|
|
91.25 0.5295 0.8053 0.0355 0.0234 7.660 68.975 25.353 5712.376 7.793 112.770 2.013 0.73 445700. 0.2287
|
|
95.60 0.5547 0.8086 0.0310 0.0212 6.964 62.706 22.090 5193.185 7.084 98.258 1.929 0.73 446735. 0.2046
|
|
99.94 0.5799 0.8056 0.0263 0.0190 6.218 55.985 18.795 4636.595 6.325 83.602 1.839 0.73 447808. 0.1799
|
|
104.29 0.6051 0.7937 0.0217 0.0165 5.425 48.846 15.484 4045.342 5.519 68.871 1.736 0.74 448918. 0.1542
|
|
108.64 0.6303 0.7682 0.0171 0.0140 4.590 41.331 12.172 3422.935 4.670 54.143 1.613 0.74 450067. 0.1270
|
|
112.98 0.6555 0.7193 0.0124 0.0113 3.720 33.492 8.881 2773.777 3.784 39.503 1.452 0.74 451254. 0.0977
|
|
117.33 0.6808 0.6246 0.0079 0.0086 2.821 25.397 5.631 2103.337 2.869 25.048 1.214 0.74 452479. 0.0650
|
|
121.67 0.7060 0.4172 0.0034 0.0058 1.902 17.123 2.446 1418.082 1.935 10.878 0.782 0.74 453740. 0.0276
|
|
126.02 0.7312
|
|
|
|
|
|
|
|
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 0.0982 0.0354 17.345 136.651 91.528 12933.919 15.439 407.117 3.210 0.83 494168. 0.6930
|
|
4.94 0.0251 0.0679 0.0971 0.0359 17.556 138.319 90.518 13091.826 15.627 402.625 3.136 0.83 494502. 0.6733
|
|
9.88 0.0502 0.1326 0.0959 0.0363 17.755 139.880 89.386 13239.603 15.804 397.589 3.062 0.83 494868. 0.6534
|
|
14.82 0.0752 0.1942 0.0945 0.0366 17.934 141.295 88.121 13373.520 15.963 391.961 2.989 0.83 495267. 0.6331
|
|
19.76 0.1003 0.2526 0.0930 0.0370 18.090 142.525 86.711 13489.880 16.102 385.691 2.915 0.83 495701. 0.6127
|
|
24.70 0.1254 0.3079 0.0914 0.0372 18.218 143.528 85.146 13584.826 16.216 378.731 2.843 0.83 496171. 0.5920
|
|
29.64 0.1505 0.3601 0.0895 0.0374 18.311 144.262 83.416 13654.353 16.299 371.033 2.771 0.83 496679. 0.5711
|
|
34.58 0.1756 0.4093 0.0875 0.0375 18.364 144.685 81.510 13694.343 16.346 362.555 2.700 0.83 497225. 0.5501
|
|
39.52 0.2007 0.4556 0.0852 0.0375 18.373 144.751 79.420 13700.555 16.354 353.260 2.629 0.83 497811. 0.5288
|
|
44.46 0.2257 0.4990 0.0828 0.0374 18.330 144.413 77.139 13668.607 16.316 343.113 2.560 0.83 498437. 0.5074
|
|
49.40 0.2508 0.5395 0.0801 0.0372 18.230 143.625 74.660 13594.027 16.227 332.089 2.491 0.83 499105. 0.4858
|
|
54.34 0.2759 0.5773 0.0772 0.0369 18.067 142.339 71.980 13472.317 16.081 320.167 2.423 0.83 499813. 0.4640
|
|
59.28 0.3010 0.6125 0.0741 0.0364 17.834 140.507 69.094 13298.947 15.874 307.332 2.357 0.83 500564. 0.4421
|
|
64.22 0.3261 0.6449 0.0708 0.0358 17.526 138.079 66.001 13069.116 15.600 293.572 2.291 0.83 501358. 0.4200
|
|
69.16 0.3511 0.6748 0.0673 0.0350 17.135 134.997 62.695 12777.437 15.252 278.867 2.226 0.83 502193. 0.3977
|
|
74.11 0.3762 0.7022 0.0635 0.0340 16.655 131.221 59.183 12419.956 14.825 263.245 2.161 0.83 503071. 0.3752
|
|
79.05 0.4013 0.7270 0.0595 0.0329 16.087 126.739 55.483 11995.797 14.319 246.789 2.098 0.83 503992. 0.3527
|
|
83.99 0.4264 0.7490 0.0554 0.0315 15.433 121.590 51.617 11508.447 13.737 229.592 2.034 0.83 504955. 0.3298
|
|
88.93 0.4515 0.7680 0.0511 0.0300 14.698 115.801 47.604 10960.465 13.083 211.744 1.970 0.83 505961. 0.3067
|
|
93.87 0.4766 0.7836 0.0466 0.0284 13.883 109.374 43.464 10352.186 12.357 193.329 1.904 0.83 507009. 0.2833
|
|
98.81 0.5016 0.7955 0.0421 0.0265 12.989 102.334 39.215 9685.883 11.562 174.429 1.836 0.84 508099. 0.2595
|
|
103.75 0.5267 0.8028 0.0374 0.0246 12.018 94.688 34.876 8962.191 10.698 155.127 1.765 0.84 509231. 0.2352
|
|
108.69 0.5518 0.8043 0.0327 0.0224 10.977 86.483 30.464 8185.607 9.771 135.505 1.688 0.84 510406. 0.2103
|
|
113.63 0.5769 0.7979 0.0279 0.0202 9.873 77.785 26.000 7362.324 8.788 115.648 1.602 0.84 511623. 0.1843
|
|
118.57 0.6020 0.7801 0.0231 0.0178 8.716 68.668 21.504 6499.392 7.758 95.649 1.501 0.84 512883. 0.1570
|
|
123.51 0.6270 0.7448 0.0182 0.0154 7.517 59.222 16.999 5605.312 6.691 75.613 1.376 0.84 514185. 0.1280
|
|
128.45 0.6521 0.6814 0.0134 0.0128 6.290 49.553 12.513 4690.138 5.598 55.656 1.210 0.84 515530. 0.0966
|
|
133.39 0.6772 0.5686 0.0087 0.0103 5.049 39.779 8.072 3765.042 4.494 35.904 0.972 0.84 516917. 0.0623
|
|
138.33 0.7023 0.3590 0.0040 0.0078 3.812 30.030 3.709 2842.322 3.393 16.499 0.592 0.85 518346. 0.0257
|
|
143.27 0.7274
|
|
|
|
|
|
|
|
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 0.0990 0.0449 31.319 219.332 116.770 23354.572 24.780 519.391 2.268 0.93 555891. 0.5530
|
|
5.59 0.0252 0.0546 0.0981 0.0453 31.580 221.158 115.730 23549.008 24.986 514.767 2.229 0.93 556260. 0.5412
|
|
11.17 0.0504 0.1073 0.0971 0.0456 31.799 222.695 114.539 23712.709 25.160 509.470 2.191 0.93 556666. 0.5292
|
|
16.76 0.0756 0.1582 0.0959 0.0459 31.966 223.864 113.180 23837.166 25.292 503.423 2.154 0.93 557111. 0.5170
|
|
22.34 0.1008 0.2074 0.0946 0.0460 32.069 224.586 111.632 23914.062 25.374 496.540 2.117 0.93 557596. 0.5049
|
|
27.93 0.1260 0.2549 0.0931 0.0461 32.098 224.787 109.878 23935.465 25.396 488.736 2.082 0.93 558123. 0.4926
|
|
33.51 0.1512 0.3009 0.0915 0.0460 32.043 224.399 107.898 23894.158 25.352 479.930 2.048 0.93 558695. 0.4801
|
|
39.10 0.1764 0.3454 0.0896 0.0458 31.895 223.364 105.676 23783.945 25.236 470.048 2.015 0.93 559312. 0.4675
|
|
44.68 0.2016 0.3885 0.0875 0.0454 31.648 221.636 103.197 23599.914 25.040 459.021 1.983 0.93 559975. 0.4547
|
|
50.27 0.2268 0.4302 0.0852 0.0449 31.297 219.179 100.448 23338.299 24.763 446.793 1.952 0.93 560685. 0.4415
|
|
55.85 0.2520 0.4705 0.0826 0.0442 30.839 215.968 97.418 22996.445 24.400 433.317 1.921 0.93 561444. 0.4280
|
|
61.44 0.2773 0.5093 0.0798 0.0434 30.270 211.986 94.101 22572.416 23.950 418.559 1.891 0.93 562251. 0.4139
|
|
67.02 0.3025 0.5465 0.0767 0.0425 29.589 207.219 90.490 22064.775 23.411 402.497 1.860 0.93 563106. 0.3993
|
|
72.61 0.3277 0.5822 0.0734 0.0413 28.794 201.651 86.581 21471.943 22.782 385.114 1.829 0.93 564011. 0.3841
|
|
78.19 0.3529 0.6160 0.0698 0.0400 27.881 195.257 82.371 20791.133 22.060 366.387 1.797 0.93 564964. 0.3681
|
|
83.78 0.3781 0.6479 0.0660 0.0385 26.848 188.022 77.865 20020.713 21.243 346.345 1.764 0.93 565966. 0.3513
|
|
89.36 0.4033 0.6777 0.0620 0.0369 25.698 179.969 73.089 19163.172 20.333 325.101 1.730 0.94 567017. 0.3338
|
|
94.95 0.4285 0.7053 0.0577 0.0351 24.437 171.136 68.074 18222.666 19.335 302.792 1.694 0.94 568116. 0.3155
|
|
100.53 0.4537 0.7298 0.0533 0.0331 23.085 161.666 62.846 17214.248 18.265 279.537 1.656 0.94 569262. 0.2963
|
|
106.12 0.4789 0.7488 0.0487 0.0311 21.702 151.980 57.429 16182.962 17.171 255.443 1.610 0.94 570457. 0.2753
|
|
111.70 0.5041 0.7612 0.0440 0.0291 20.289 142.088 51.852 15129.621 16.053 230.639 1.554 0.94 571699. 0.2526
|
|
117.29 0.5293 0.7609 0.0391 0.0272 18.962 132.791 46.130 14139.708 15.003 205.186 1.480 0.94 572989. 0.2268
|
|
122.87 0.5545 0.7478 0.0342 0.0253 17.658 123.663 40.300 13167.710 13.971 179.256 1.388 0.94 574326. 0.1989
|
|
128.46 0.5797 0.7221 0.0292 0.0234 16.318 114.280 34.403 12168.649 12.911 153.024 1.282 0.94 575711. 0.1697
|
|
134.04 0.6049 0.6801 0.0241 0.0215 14.963 104.787 28.472 11157.806 11.839 126.642 1.157 0.95 577144. 0.1394
|
|
139.63 0.6301 0.6165 0.0191 0.0195 13.616 95.352 22.546 10153.168 10.773 100.286 1.007 0.95 578624. 0.1079
|
|
145.21 0.6553 0.5251 0.0141 0.0176 12.294 86.097 16.672 9167.622 9.727 74.157 0.825 0.95 580152. 0.0760
|
|
150.80 0.6805 0.3979 0.0092 0.0158 11.017 77.151 10.900 8215.083 8.716 48.485 0.602 0.95 581729. 0.0448
|
|
156.38 0.7057 0.2249 0.0045 0.0141 9.798 68.615 5.284 7306.146 7.752 23.505 0.328 0.95 583355. 0.0170
|
|
161.97 0.7309 -0.0096 -0.0002 0.0123 8.598 60.213 -0.190 6411.512 6.803 -0.846 -0.013 0.95 585045. 0.0000
|
|
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