464 lines
82 KiB
Plaintext
464 lines
82 KiB
Plaintext
19x12WE (19x12WE.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 0.1024 0.0420 0.008 0.527 0.425 6.240 0.060 1.893 30.927 0.08 36376. 0.6230
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0.48 0.0268 0.0637 0.1012 0.0426 0.008 0.535 0.420 6.330 0.060 1.869 30.100 0.08 36404. 0.6025
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0.96 0.0536 0.1238 0.0997 0.0432 0.009 0.542 0.414 6.418 0.061 1.842 29.272 0.08 36434. 0.5818
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1.45 0.0804 0.1805 0.0982 0.0437 0.009 0.549 0.408 6.500 0.062 1.814 28.449 0.08 36466. 0.5610
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1.93 0.1073 0.2338 0.0965 0.0443 0.009 0.556 0.401 6.577 0.063 1.782 27.632 0.08 36502. 0.5401
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2.41 0.1341 0.2837 0.0946 0.0447 0.009 0.562 0.393 6.644 0.063 1.748 26.824 0.08 36541. 0.5193
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2.89 0.1609 0.3303 0.0926 0.0451 0.009 0.566 0.385 6.701 0.064 1.710 26.027 0.08 36583. 0.4984
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3.38 0.1877 0.3737 0.0904 0.0454 0.009 0.570 0.375 6.745 0.064 1.670 25.244 0.08 36628. 0.4777
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3.86 0.2145 0.4141 0.0880 0.0456 0.009 0.573 0.366 6.774 0.065 1.626 24.474 0.08 36676. 0.4569
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4.34 0.2413 0.4515 0.0854 0.0457 0.009 0.573 0.355 6.785 0.065 1.578 23.718 0.08 36728. 0.4363
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4.82 0.2681 0.4860 0.0827 0.0456 0.009 0.573 0.343 6.776 0.065 1.527 22.977 0.08 36784. 0.4157
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5.31 0.2950 0.5176 0.0797 0.0454 0.009 0.570 0.331 6.746 0.064 1.472 22.248 0.08 36843. 0.3952
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5.79 0.3218 0.5465 0.0765 0.0450 0.009 0.566 0.318 6.691 0.064 1.413 21.532 0.08 36905. 0.3748
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6.27 0.3486 0.5726 0.0731 0.0445 0.009 0.559 0.304 6.611 0.063 1.350 20.824 0.08 36972. 0.3543
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6.75 0.3754 0.5958 0.0695 0.0438 0.009 0.550 0.288 6.503 0.062 1.283 20.122 0.08 37041. 0.3338
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7.24 0.4022 0.6162 0.0656 0.0428 0.009 0.538 0.273 6.366 0.061 1.213 19.422 0.08 37115. 0.3132
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7.72 0.4290 0.6334 0.0616 0.0417 0.008 0.524 0.256 6.200 0.059 1.138 18.717 0.08 37192. 0.2924
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8.20 0.4559 0.6473 0.0574 0.0404 0.008 0.507 0.238 6.003 0.057 1.060 18.002 0.08 37273. 0.2714
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8.68 0.4827 0.6575 0.0530 0.0389 0.008 0.488 0.220 5.778 0.055 0.978 17.269 0.08 37358. 0.2501
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9.17 0.5095 0.6635 0.0484 0.0372 0.007 0.467 0.201 5.525 0.053 0.895 16.509 0.08 37446. 0.2286
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9.65 0.5363 0.6646 0.0438 0.0353 0.007 0.444 0.182 5.247 0.050 0.808 15.710 0.08 37538. 0.2068
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10.13 0.5631 0.6599 0.0390 0.0333 0.007 0.418 0.162 4.945 0.047 0.720 14.856 0.08 37634. 0.1846
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10.61 0.5899 0.6481 0.0342 0.0311 0.006 0.390 0.142 4.620 0.044 0.631 13.928 0.08 37733. 0.1620
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11.10 0.6167 0.6275 0.0293 0.0288 0.006 0.361 0.122 4.273 0.041 0.540 12.899 0.08 37836. 0.1389
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11.58 0.6436 0.5955 0.0243 0.0263 0.005 0.330 0.101 3.905 0.037 0.449 11.731 0.08 37943. 0.1151
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12.06 0.6704 0.5482 0.0194 0.0237 0.005 0.297 0.080 3.519 0.034 0.358 10.368 0.08 38054. 0.0908
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12.54 0.6972 0.4797 0.0144 0.0210 0.004 0.263 0.060 3.117 0.030 0.267 8.722 0.08 38168. 0.0659
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13.03 0.7240 0.3799 0.0095 0.0182 0.004 0.228 0.040 2.700 0.026 0.176 6.652 0.08 38285. 0.0409
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13.51 0.7508 0.2313 0.0047 0.0153 0.003 0.192 0.020 2.272 0.022 0.087 3.906 0.08 38407. 0.0169
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13.99 0.7776 -0.0005 0.0000 0.0124 0.002 0.155 0.000 1.836 0.018 0.000 -0.009 0.08 38531. 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 0.1028 0.0392 0.062 1.970 1.708 46.606 0.223 7.598 16.623 0.15 72751. 0.6709
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0.97 0.0269 0.0686 0.1015 0.0399 0.064 2.002 1.687 47.380 0.226 7.502 16.146 0.15 72806. 0.6476
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1.94 0.0539 0.1332 0.1001 0.0405 0.065 2.034 1.663 48.132 0.230 7.397 15.671 0.15 72867. 0.6241
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2.91 0.0808 0.1938 0.0986 0.0411 0.066 2.064 1.637 48.849 0.233 7.282 15.201 0.15 72933. 0.6007
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3.88 0.1077 0.2505 0.0968 0.0417 0.066 2.093 1.609 49.515 0.236 7.156 14.738 0.15 73004. 0.5773
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4.85 0.1347 0.3035 0.0950 0.0422 0.067 2.118 1.578 50.112 0.239 7.019 14.282 0.15 73082. 0.5541
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5.82 0.1616 0.3528 0.0930 0.0426 0.068 2.139 1.544 50.624 0.242 6.869 13.836 0.15 73167. 0.5310
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6.79 0.1886 0.3986 0.0907 0.0429 0.068 2.157 1.508 51.031 0.244 6.706 13.399 0.15 73258. 0.5081
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7.75 0.2155 0.4411 0.0884 0.0432 0.069 2.169 1.468 51.315 0.245 6.529 12.974 0.15 73355. 0.4854
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8.72 0.2424 0.4803 0.0858 0.0433 0.069 2.175 1.425 51.455 0.246 6.337 12.559 0.15 73460. 0.4629
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9.69 0.2694 0.5165 0.0830 0.0433 0.069 2.174 1.378 51.432 0.246 6.130 12.155 0.15 73572. 0.4407
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10.66 0.2963 0.5498 0.0800 0.0431 0.069 2.165 1.328 51.227 0.245 5.908 11.761 0.15 73691. 0.4186
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11.63 0.3232 0.5802 0.0767 0.0428 0.068 2.148 1.275 50.823 0.243 5.671 11.378 0.15 73817. 0.3967
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12.60 0.3502 0.6078 0.0733 0.0422 0.067 2.122 1.218 50.205 0.240 5.417 11.002 0.15 73951. 0.3750
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13.57 0.3771 0.6327 0.0697 0.0415 0.066 2.086 1.157 49.360 0.236 5.148 10.634 0.15 74092. 0.3533
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14.54 0.4041 0.6547 0.0658 0.0406 0.065 2.040 1.093 48.274 0.230 4.862 10.271 0.15 74240. 0.3316
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15.51 0.4310 0.6738 0.0617 0.0395 0.063 1.983 1.025 46.934 0.224 4.561 9.910 0.15 74396. 0.3099
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16.48 0.4579 0.6898 0.0575 0.0381 0.061 1.916 0.954 45.339 0.216 4.246 9.549 0.15 74559. 0.2881
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17.45 0.4849 0.7024 0.0530 0.0366 0.058 1.838 0.881 43.503 0.208 3.918 9.183 0.15 74730. 0.2662
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18.42 0.5118 0.7113 0.0484 0.0349 0.056 1.751 0.805 41.436 0.198 3.580 8.809 0.15 74908. 0.2441
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19.39 0.5387 0.7157 0.0438 0.0329 0.052 1.654 0.727 39.149 0.187 3.233 8.421 0.15 75094. 0.2217
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20.36 0.5657 0.7148 0.0390 0.0308 0.049 1.549 0.647 36.651 0.175 2.879 8.010 0.15 75287. 0.1990
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21.33 0.5926 0.7075 0.0341 0.0286 0.046 1.435 0.566 33.952 0.162 2.520 7.568 0.15 75487. 0.1759
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22.29 0.6196 0.6919 0.0292 0.0261 0.042 1.313 0.485 31.063 0.148 2.156 7.079 0.15 75695. 0.1522
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23.26 0.6465 0.6652 0.0242 0.0236 0.038 1.183 0.403 27.996 0.134 1.791 6.523 0.15 75910. 0.1278
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24.23 0.6734 0.6231 0.0193 0.0208 0.033 1.047 0.320 24.767 0.118 1.425 5.865 0.15 76133. 0.1025
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25.20 0.7004 0.5582 0.0143 0.0180 0.029 0.904 0.238 21.394 0.102 1.060 5.052 0.15 76363. 0.0762
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26.17 0.7273 0.4569 0.0095 0.0151 0.024 0.756 0.157 17.898 0.085 0.699 3.982 0.15 76600. 0.0487
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27.14 0.7542 0.2918 0.0047 0.0120 0.019 0.605 0.077 14.304 0.068 0.344 2.452 0.16 76845. 0.0211
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28.11 0.7812 -0.0033 0.0000 0.0089 0.014 0.450 -0.001 10.637 0.051 -0.003 -0.026 0.16 77095. 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 0.1032 0.0381 0.205 4.306 3.858 152.818 0.486 17.159 11.450 0.23 109124. 0.6945
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1.46 0.0270 0.0709 0.1019 0.0388 0.209 4.382 3.810 155.517 0.495 16.945 11.111 0.23 109207. 0.6697
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2.91 0.0540 0.1376 0.1005 0.0394 0.212 4.456 3.757 158.147 0.503 16.710 10.774 0.23 109298. 0.6449
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4.37 0.0810 0.2000 0.0990 0.0400 0.215 4.526 3.699 160.659 0.511 16.452 10.442 0.23 109397. 0.6202
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5.83 0.1079 0.2584 0.0973 0.0406 0.219 4.592 3.635 162.999 0.519 16.169 10.115 0.23 109505. 0.5956
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7.28 0.1349 0.3127 0.0954 0.0412 0.221 4.652 3.566 165.110 0.526 15.860 9.795 0.23 109622. 0.5712
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8.74 0.1619 0.3633 0.0934 0.0416 0.224 4.703 3.490 166.931 0.531 15.522 9.482 0.23 109749. 0.5470
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10.20 0.1889 0.4102 0.0912 0.0420 0.226 4.744 3.407 168.395 0.536 15.155 9.177 0.23 109886. 0.5231
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11.65 0.2159 0.4536 0.0888 0.0422 0.227 4.774 3.317 169.437 0.539 14.755 8.880 0.23 110033. 0.4995
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13.11 0.2429 0.4938 0.0862 0.0424 0.228 4.789 3.220 169.988 0.541 14.323 8.592 0.23 110191. 0.4761
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14.56 0.2698 0.5308 0.0833 0.0424 0.228 4.789 3.115 169.980 0.541 13.857 8.313 0.23 110359. 0.4531
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16.02 0.2968 0.5648 0.0803 0.0422 0.227 4.771 3.002 169.348 0.539 13.355 8.041 0.23 110538. 0.4303
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17.48 0.3238 0.5960 0.0771 0.0419 0.225 4.734 2.882 168.033 0.535 12.817 7.778 0.23 110728. 0.4078
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18.93 0.3508 0.6244 0.0736 0.0414 0.223 4.676 2.753 165.979 0.528 12.243 7.522 0.23 110929. 0.3854
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20.39 0.3778 0.6500 0.0700 0.0407 0.219 4.596 2.615 163.141 0.519 11.634 7.272 0.23 111142. 0.3632
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21.85 0.4048 0.6730 0.0661 0.0398 0.214 4.493 2.470 159.469 0.508 10.988 7.026 0.23 111365. 0.3410
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23.30 0.4317 0.6931 0.0620 0.0386 0.208 4.365 2.317 154.916 0.493 10.306 6.784 0.23 111600. 0.3189
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24.76 0.4587 0.7103 0.0577 0.0373 0.200 4.212 2.156 149.484 0.476 9.592 6.543 0.23 111845. 0.2967
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26.22 0.4857 0.7243 0.0532 0.0357 0.192 4.035 1.990 143.209 0.456 8.850 6.302 0.23 112103. 0.2745
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27.67 0.5127 0.7347 0.0486 0.0339 0.183 3.835 1.818 136.130 0.433 8.085 6.056 0.23 112371. 0.2522
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29.13 0.5397 0.7411 0.0439 0.0320 0.172 3.614 1.641 128.279 0.408 7.300 5.803 0.23 112650. 0.2296
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30.59 0.5667 0.7426 0.0391 0.0298 0.161 3.372 1.461 119.689 0.381 6.500 5.538 0.23 112941. 0.2067
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32.04 0.5936 0.7380 0.0342 0.0275 0.148 3.110 1.279 110.394 0.351 5.687 5.253 0.23 113242. 0.1835
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33.50 0.6206 0.7256 0.0293 0.0250 0.135 2.830 1.094 100.431 0.320 4.866 4.941 0.23 113555. 0.1596
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34.96 0.6476 0.7027 0.0243 0.0224 0.120 2.531 0.908 89.843 0.286 4.040 4.585 0.23 113879. 0.1350
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36.41 0.6746 0.6647 0.0193 0.0196 0.106 2.217 0.722 78.684 0.250 3.213 4.164 0.23 114214. 0.1093
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37.87 0.7016 0.6037 0.0144 0.0167 0.090 1.888 0.537 67.017 0.213 2.390 3.636 0.23 114560. 0.0823
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39.33 0.7286 0.5044 0.0095 0.0137 0.074 1.547 0.354 54.920 0.175 1.576 2.926 0.23 114917. 0.0538
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40.78 0.7555 0.3330 0.0047 0.0106 0.057 1.197 0.174 42.481 0.135 0.776 1.862 0.23 115285. 0.0240
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42.24 0.7825 -0.0033 0.0000 0.0074 0.040 0.839 -0.001 29.782 0.095 -0.005 -0.018 0.23 115660. 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 0.1037 0.0376 0.479 7.548 6.890 357.209 0.853 30.647 8.749 0.30 145494. 0.7092
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1.94 0.0270 0.0723 0.1024 0.0383 0.488 7.687 6.805 363.763 0.868 30.269 8.485 0.30 145604. 0.6836
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3.89 0.0540 0.1402 0.1010 0.0389 0.496 7.822 6.712 370.158 0.884 29.853 8.224 0.30 145726. 0.6580
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5.83 0.0810 0.2036 0.0995 0.0396 0.505 7.951 6.609 376.272 0.898 29.396 7.967 0.30 145858. 0.6325
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7.77 0.1080 0.2629 0.0978 0.0402 0.512 8.071 6.496 381.981 0.912 28.895 7.714 0.30 146003. 0.6072
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9.72 0.1350 0.3181 0.0959 0.0407 0.519 8.181 6.373 387.144 0.924 28.346 7.466 0.30 146160. 0.5821
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11.66 0.1620 0.3694 0.0939 0.0412 0.525 8.275 6.238 391.613 0.935 27.746 7.225 0.30 146329. 0.5573
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13.61 0.1890 0.4169 0.0917 0.0416 0.530 8.351 6.091 395.232 0.944 27.093 6.990 0.30 146512. 0.5328
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15.55 0.2161 0.4610 0.0893 0.0418 0.534 8.407 5.931 397.836 0.950 26.382 6.762 0.30 146709. 0.5086
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17.49 0.2431 0.5016 0.0867 0.0420 0.535 8.437 5.758 399.260 0.953 25.611 6.541 0.30 146919. 0.4847
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19.44 0.2701 0.5392 0.0838 0.0420 0.536 8.438 5.571 399.341 0.953 24.779 6.327 0.30 147144. 0.4612
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21.38 0.2971 0.5737 0.0808 0.0418 0.534 8.408 5.370 397.920 0.950 23.884 6.121 0.30 147384. 0.4380
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23.32 0.3241 0.6053 0.0776 0.0415 0.530 8.343 5.154 394.852 0.943 22.924 5.920 0.30 147638. 0.4151
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25.27 0.3511 0.6343 0.0741 0.0410 0.523 8.241 4.923 390.005 0.931 21.899 5.726 0.30 147906. 0.3923
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27.21 0.3781 0.6605 0.0704 0.0403 0.514 8.099 4.678 383.262 0.915 20.809 5.536 0.30 148190. 0.3698
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29.16 0.4051 0.6840 0.0665 0.0394 0.502 7.914 4.419 374.507 0.894 19.654 5.352 0.30 148489. 0.3474
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31.10 0.4321 0.7048 0.0624 0.0382 0.488 7.684 4.145 363.621 0.868 18.435 5.170 0.30 148802. 0.3250
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33.04 0.4591 0.7228 0.0580 0.0369 0.470 7.409 3.857 350.606 0.837 17.157 4.990 0.30 149131. 0.3026
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34.99 0.4861 0.7378 0.0536 0.0353 0.450 7.090 3.559 335.548 0.801 15.829 4.810 0.31 149474. 0.2802
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36.93 0.5131 0.7494 0.0489 0.0335 0.427 6.731 3.251 318.534 0.760 14.459 4.629 0.31 149833. 0.2577
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38.87 0.5401 0.7571 0.0442 0.0315 0.402 6.332 2.935 299.643 0.715 13.055 4.443 0.31 150206. 0.2350
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40.82 0.5671 0.7602 0.0393 0.0293 0.374 5.894 2.613 278.952 0.666 11.622 4.249 0.31 150594. 0.2121
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42.76 0.5942 0.7577 0.0344 0.0270 0.344 5.421 2.286 256.542 0.612 10.168 4.042 0.31 150997. 0.1887
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44.70 0.6212 0.7477 0.0294 0.0244 0.312 4.913 1.956 232.502 0.555 8.698 3.815 0.31 151415. 0.1648
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46.65 0.6482 0.7276 0.0244 0.0218 0.278 4.373 1.623 206.939 0.494 7.220 3.558 0.31 151847. 0.1400
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48.59 0.6752 0.6929 0.0194 0.0189 0.241 3.803 1.291 179.983 0.430 5.741 3.253 0.31 152295. 0.1141
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50.54 0.7022 0.6354 0.0144 0.0160 0.204 3.207 0.960 151.788 0.362 4.269 2.868 0.31 152757. 0.0868
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52.48 0.7292 0.5386 0.0095 0.0129 0.164 2.589 0.633 122.544 0.293 2.814 2.341 0.31 153234. 0.0575
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54.42 0.7562 0.3642 0.0047 0.0097 0.124 1.954 0.311 92.473 0.221 1.384 1.526 0.31 153726. 0.0263
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56.37 0.7832 -0.0047 0.0000 0.0065 0.083 1.305 -0.003 61.761 0.147 -0.011 -0.019 0.31 154226. 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 0.1043 0.0374 0.930 11.728 10.828 693.771 1.325 48.162 7.079 0.38 181859. 0.7194
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2.43 0.0270 0.0731 0.1030 0.0381 0.948 11.949 10.696 706.844 1.350 47.577 6.864 0.38 181997. 0.6932
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4.86 0.0540 0.1417 0.1016 0.0387 0.965 12.165 10.551 719.613 1.374 46.933 6.651 0.38 182149. 0.6672
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7.29 0.0810 0.2058 0.1001 0.0394 0.981 12.371 10.392 731.836 1.398 46.224 6.441 0.38 182315. 0.6412
|
|
9.72 0.1080 0.2656 0.0984 0.0400 0.997 12.565 10.217 743.264 1.420 45.444 6.235 0.38 182496. 0.6154
|
|
12.15 0.1350 0.3213 0.0966 0.0406 1.011 12.740 10.025 753.620 1.439 44.590 6.033 0.38 182692. 0.5899
|
|
14.58 0.1620 0.3730 0.0945 0.0411 1.023 12.891 9.814 762.608 1.456 43.655 5.837 0.38 182905. 0.5647
|
|
17.01 0.1890 0.4210 0.0923 0.0415 1.032 13.015 9.585 769.916 1.470 42.634 5.647 0.38 183134. 0.5399
|
|
19.44 0.2161 0.4654 0.0899 0.0417 1.040 13.105 9.335 775.219 1.481 41.523 5.462 0.38 183380. 0.5154
|
|
21.87 0.2431 0.5064 0.0873 0.0419 1.044 13.155 9.064 778.188 1.486 40.318 5.283 0.38 183643. 0.4912
|
|
24.30 0.2701 0.5443 0.0845 0.0419 1.044 13.160 8.771 778.496 1.487 39.015 5.110 0.38 183925. 0.4674
|
|
26.73 0.2971 0.5792 0.0814 0.0418 1.040 13.115 8.456 775.827 1.482 37.611 4.944 0.38 184225. 0.4439
|
|
29.15 0.3241 0.6112 0.0782 0.0415 1.032 13.015 8.117 769.890 1.470 36.105 4.782 0.38 184543. 0.4208
|
|
31.58 0.3511 0.6405 0.0747 0.0409 1.020 12.855 7.755 760.421 1.452 34.496 4.626 0.38 184879. 0.3978
|
|
34.01 0.3781 0.6672 0.0710 0.0402 1.002 12.631 7.371 747.189 1.427 32.784 4.474 0.38 185234. 0.3751
|
|
36.44 0.4051 0.6912 0.0671 0.0393 0.979 12.340 6.963 729.963 1.394 30.970 4.326 0.38 185608. 0.3525
|
|
38.87 0.4321 0.7126 0.0629 0.0381 0.950 11.977 6.531 708.503 1.353 29.052 4.181 0.38 186000. 0.3300
|
|
41.30 0.4591 0.7312 0.0586 0.0368 0.916 11.542 6.079 682.801 1.304 27.041 4.038 0.38 186411. 0.3075
|
|
43.73 0.4861 0.7470 0.0540 0.0352 0.876 11.039 5.610 653.026 1.247 24.951 3.896 0.38 186841. 0.2850
|
|
46.16 0.5131 0.7595 0.0494 0.0333 0.831 10.470 5.125 619.346 1.183 22.795 3.753 0.38 187289. 0.2624
|
|
48.59 0.5401 0.7684 0.0446 0.0313 0.780 9.837 4.628 581.917 1.111 20.584 3.607 0.38 187756. 0.2396
|
|
51.02 0.5671 0.7728 0.0397 0.0291 0.725 9.143 4.120 540.890 1.033 18.328 3.455 0.38 188241. 0.2166
|
|
53.45 0.5941 0.7719 0.0347 0.0267 0.666 8.392 3.605 496.424 0.948 16.037 3.294 0.38 188745. 0.1932
|
|
55.88 0.6211 0.7639 0.0297 0.0242 0.602 7.585 3.085 448.698 0.857 13.722 3.118 0.38 189268. 0.1691
|
|
58.31 0.6482 0.7463 0.0247 0.0214 0.534 6.727 2.561 397.926 0.760 11.393 2.920 0.38 189809. 0.1443
|
|
60.74 0.6752 0.7146 0.0196 0.0185 0.462 5.821 2.038 344.364 0.658 9.063 2.684 0.39 190368. 0.1183
|
|
63.17 0.7022 0.6605 0.0146 0.0155 0.387 4.874 1.516 288.323 0.551 6.744 2.385 0.39 190946. 0.0907
|
|
65.60 0.7292 0.5670 0.0096 0.0124 0.309 3.891 1.001 230.183 0.440 4.451 1.972 0.39 191542. 0.0609
|
|
68.03 0.7562 0.3925 0.0048 0.0092 0.229 2.880 0.494 170.393 0.325 2.199 1.316 0.39 192157. 0.0286
|
|
70.46 0.7832 0.0003 0.0000 0.0059 0.147 1.848 0.000 109.312 0.209 0.001 0.001 0.39 192781. 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 0.1050 0.0374 1.608 16.892 15.701 1199.137 1.908 69.840 5.939 0.45 218218. 0.7268
|
|
2.92 0.0270 0.0736 0.1038 0.0381 1.639 17.218 15.515 1222.230 1.945 69.009 5.757 0.45 218384. 0.7003
|
|
5.83 0.0540 0.1426 0.1024 0.0388 1.669 17.536 15.308 1244.807 1.981 68.091 5.578 0.45 218567. 0.6740
|
|
8.75 0.0810 0.2072 0.1009 0.0395 1.698 17.840 15.081 1266.441 2.016 67.078 5.401 0.45 218766. 0.6477
|
|
11.67 0.1081 0.2673 0.0992 0.0401 1.725 18.126 14.830 1286.688 2.048 65.963 5.228 0.45 218984. 0.6217
|
|
14.58 0.1351 0.3234 0.0973 0.0407 1.750 18.384 14.554 1305.061 2.077 64.738 5.058 0.45 219220. 0.5960
|
|
17.50 0.1621 0.3754 0.0953 0.0412 1.772 18.610 14.252 1321.036 2.102 63.395 4.893 0.45 219475. 0.5705
|
|
20.41 0.1891 0.4236 0.0931 0.0416 1.789 18.793 13.922 1334.062 2.123 61.927 4.733 0.45 219751. 0.5454
|
|
23.33 0.2161 0.4683 0.0907 0.0419 1.802 18.927 13.563 1343.568 2.138 60.326 4.579 0.45 220047. 0.5207
|
|
26.25 0.2431 0.5096 0.0881 0.0420 1.809 19.003 13.172 1348.966 2.147 58.587 4.429 0.45 220364. 0.4964
|
|
29.16 0.2701 0.5477 0.0853 0.0421 1.810 19.013 12.748 1349.683 2.148 56.705 4.284 0.45 220703. 0.4724
|
|
32.08 0.2972 0.5829 0.0822 0.0419 1.804 18.949 12.292 1345.162 2.141 54.674 4.145 0.45 221063. 0.4488
|
|
35.00 0.3242 0.6152 0.0789 0.0416 1.790 18.805 11.802 1334.884 2.125 52.493 4.010 0.45 221446. 0.4254
|
|
37.91 0.3512 0.6448 0.0754 0.0411 1.768 18.572 11.277 1318.386 2.098 50.161 3.880 0.46 221850. 0.4024
|
|
40.83 0.3782 0.6718 0.0717 0.0404 1.737 18.246 10.719 1295.255 2.061 47.677 3.754 0.46 222277. 0.3795
|
|
43.74 0.4052 0.6963 0.0677 0.0394 1.697 17.821 10.127 1265.087 2.013 45.043 3.631 0.46 222726. 0.3568
|
|
46.66 0.4322 0.7181 0.0635 0.0382 1.646 17.291 9.500 1227.466 1.954 42.258 3.511 0.46 223198. 0.3342
|
|
49.58 0.4592 0.7373 0.0591 0.0368 1.586 16.656 8.843 1182.355 1.882 39.336 3.392 0.46 223692. 0.3116
|
|
52.49 0.4863 0.7537 0.0546 0.0352 1.515 15.919 8.160 1130.046 1.799 36.297 3.275 0.46 224209. 0.2889
|
|
55.41 0.5133 0.7671 0.0499 0.0334 1.436 15.085 7.455 1070.837 1.704 33.160 3.158 0.46 224748. 0.2663
|
|
58.33 0.5403 0.7768 0.0450 0.0313 1.348 14.157 6.732 1004.998 1.600 29.942 3.038 0.46 225309. 0.2434
|
|
61.24 0.5673 0.7824 0.0401 0.0291 1.251 13.140 5.993 932.797 1.485 26.658 2.914 0.46 225892. 0.2203
|
|
64.16 0.5943 0.7828 0.0351 0.0266 1.146 12.038 5.243 854.512 1.360 23.323 2.783 0.46 226497. 0.1968
|
|
67.08 0.6213 0.7765 0.0300 0.0240 1.033 10.854 4.486 770.461 1.226 19.952 2.641 0.46 227125. 0.1727
|
|
69.99 0.6483 0.7608 0.0249 0.0212 0.913 9.594 3.723 681.021 1.084 16.560 2.480 0.46 227774. 0.1478
|
|
72.91 0.6754 0.7315 0.0198 0.0183 0.787 8.264 2.960 586.647 0.934 13.166 2.289 0.46 228446. 0.1216
|
|
75.82 0.7024 0.6800 0.0147 0.0152 0.654 6.873 2.201 487.893 0.777 9.788 2.046 0.46 229140. 0.0937
|
|
78.74 0.7294 0.5889 0.0097 0.0120 0.517 5.430 1.450 385.433 0.613 6.448 1.706 0.46 229856. 0.0634
|
|
81.66 0.7564 0.4131 0.0048 0.0087 0.376 3.945 0.712 280.072 0.446 3.169 1.154 0.47 230594. 0.0301
|
|
84.57 0.7834 -0.0073 0.0000 0.0054 0.231 2.429 -0.007 172.401 0.274 -0.033 -0.020 0.47 231342. 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 0.1059 0.0376 2.566 23.108 21.551 1913.775 2.611 95.860 5.108 0.53 254569. 0.7323
|
|
3.40 0.0270 0.0739 0.1047 0.0383 2.617 23.562 21.301 1951.358 2.662 94.749 4.951 0.53 254764. 0.7057
|
|
6.81 0.0540 0.1431 0.1033 0.0390 2.666 24.006 21.024 1988.128 2.712 93.516 4.796 0.53 254977. 0.6792
|
|
10.21 0.0811 0.2079 0.1018 0.0397 2.713 24.432 20.718 2023.399 2.760 92.154 4.644 0.53 255210. 0.6528
|
|
13.61 0.1081 0.2683 0.1001 0.0404 2.758 24.831 20.380 2056.440 2.805 90.650 4.495 0.53 255465. 0.6267
|
|
17.02 0.1351 0.3244 0.0983 0.0409 2.798 25.193 20.007 2086.460 2.846 88.993 4.349 0.53 255741. 0.6008
|
|
20.42 0.1621 0.3767 0.0963 0.0415 2.833 25.509 19.598 2112.604 2.882 87.172 4.208 0.53 256040. 0.5753
|
|
23.82 0.1891 0.4251 0.0941 0.0419 2.862 25.767 19.150 2133.971 2.911 85.178 4.070 0.53 256362. 0.5501
|
|
27.23 0.2162 0.4699 0.0917 0.0422 2.883 25.956 18.660 2149.627 2.932 82.999 3.937 0.53 256708. 0.5252
|
|
30.63 0.2432 0.5114 0.0891 0.0424 2.895 26.065 18.127 2158.627 2.945 80.628 3.809 0.53 257079. 0.5008
|
|
34.03 0.2702 0.5498 0.0862 0.0424 2.897 26.082 17.549 2160.027 2.947 78.056 3.685 0.53 257475. 0.4767
|
|
37.44 0.2972 0.5851 0.0832 0.0422 2.887 25.996 16.924 2152.925 2.937 75.278 3.565 0.53 257897. 0.4530
|
|
40.84 0.3242 0.6177 0.0799 0.0419 2.865 25.797 16.252 2136.471 2.915 72.290 3.450 0.53 258344. 0.4296
|
|
44.24 0.3513 0.6476 0.0763 0.0414 2.829 25.476 15.533 2109.916 2.878 69.091 3.339 0.53 258818. 0.4064
|
|
47.64 0.3783 0.6750 0.0726 0.0407 2.779 25.026 14.766 2072.590 2.827 65.681 3.231 0.53 259317. 0.3835
|
|
51.05 0.4053 0.6998 0.0686 0.0397 2.714 24.437 13.953 2023.847 2.761 62.061 3.127 0.53 259842. 0.3607
|
|
54.45 0.4323 0.7221 0.0643 0.0385 2.632 23.703 13.091 1963.008 2.678 58.230 3.025 0.53 260394. 0.3380
|
|
57.85 0.4594 0.7418 0.0599 0.0371 2.535 22.821 12.187 1889.992 2.578 54.207 2.925 0.53 260972. 0.3153
|
|
61.26 0.4864 0.7588 0.0553 0.0354 2.421 21.798 11.246 1805.262 2.463 50.022 2.826 0.53 261575. 0.2926
|
|
64.66 0.5134 0.7728 0.0505 0.0335 2.292 20.639 10.274 1709.303 2.332 45.699 2.726 0.53 262205. 0.2699
|
|
68.06 0.5404 0.7834 0.0456 0.0314 2.149 19.350 9.276 1602.556 2.186 41.262 2.626 0.54 262860. 0.2470
|
|
71.47 0.5674 0.7900 0.0406 0.0291 1.992 17.936 8.258 1485.452 2.026 36.732 2.522 0.54 263542. 0.2238
|
|
74.87 0.5945 0.7916 0.0355 0.0267 1.822 16.403 7.223 1358.452 1.853 32.129 2.412 0.54 264249. 0.2002
|
|
78.27 0.6215 0.7867 0.0304 0.0240 1.639 14.756 6.177 1222.068 1.667 27.476 2.293 0.54 264982. 0.1760
|
|
81.68 0.6485 0.7728 0.0252 0.0211 1.444 13.003 5.124 1076.916 1.469 22.793 2.158 0.54 265740. 0.1509
|
|
85.08 0.6755 0.7455 0.0200 0.0181 1.239 11.154 4.071 923.738 1.260 18.106 1.999 0.54 266525. 0.1245
|
|
88.48 0.7025 0.6964 0.0148 0.0150 1.024 9.218 3.022 763.445 1.041 13.440 1.795 0.54 267335. 0.0964
|
|
91.89 0.7296 0.6072 0.0098 0.0117 0.801 7.210 1.984 597.143 0.815 8.827 1.507 0.54 268171. 0.0656
|
|
95.29 0.7566 0.4297 0.0047 0.0084 0.571 5.146 0.966 426.151 0.581 4.298 1.029 0.54 269032. 0.0312
|
|
98.69 0.7836 -0.0223 -0.0001 0.0049 0.337 3.035 -0.028 251.328 0.343 -0.127 -0.051 0.54 269902. 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 0.1070 0.0379 3.867 30.466 28.429 2883.590 3.442 126.450 4.472 0.60 290911. 0.7363
|
|
3.88 0.0270 0.0738 0.1058 0.0387 3.944 31.075 28.110 2941.198 3.511 125.035 4.335 0.60 291133. 0.7098
|
|
7.77 0.0540 0.1430 0.1044 0.0394 4.020 31.671 27.757 2997.635 3.578 123.461 4.200 0.60 291377. 0.6833
|
|
11.65 0.0809 0.2077 0.1029 0.0401 4.093 32.244 27.364 3051.834 3.643 121.715 4.067 0.60 291643. 0.6570
|
|
15.53 0.1079 0.2680 0.1013 0.0408 4.161 32.781 26.929 3102.676 3.704 119.780 3.937 0.60 291934. 0.6309
|
|
19.41 0.1349 0.3242 0.0995 0.0414 4.223 33.270 26.448 3148.943 3.759 117.642 3.810 0.60 292249. 0.6050
|
|
23.30 0.1619 0.3765 0.0975 0.0419 4.277 33.696 25.919 3189.330 3.807 115.286 3.686 0.60 292591. 0.5795
|
|
27.18 0.1888 0.4249 0.0953 0.0424 4.321 34.046 25.337 3222.451 3.847 112.698 3.566 0.60 292960. 0.5544
|
|
31.06 0.2158 0.4699 0.0929 0.0427 4.354 34.304 24.700 3246.884 3.876 109.864 3.450 0.60 293356. 0.5296
|
|
34.95 0.2428 0.5115 0.0903 0.0429 4.373 34.455 24.004 3261.175 3.893 106.771 3.339 0.60 293780. 0.5051
|
|
38.83 0.2698 0.5500 0.0875 0.0429 4.377 34.484 23.249 3263.887 3.896 103.411 3.231 0.61 294233. 0.4811
|
|
42.71 0.2967 0.5855 0.0844 0.0428 4.363 34.376 22.431 3253.637 3.884 99.774 3.127 0.61 294715. 0.4574
|
|
46.60 0.3237 0.6183 0.0811 0.0424 4.330 34.117 21.550 3229.134 3.854 95.856 3.027 0.61 295226. 0.4340
|
|
50.48 0.3507 0.6485 0.0775 0.0419 4.277 33.695 20.606 3189.218 3.807 91.654 2.931 0.61 295767. 0.4108
|
|
54.36 0.3777 0.6762 0.0737 0.0412 4.201 33.100 19.597 3132.882 3.740 87.170 2.837 0.61 296337. 0.3879
|
|
58.24 0.4046 0.7014 0.0697 0.0402 4.102 32.321 18.526 3059.157 3.652 82.404 2.747 0.61 296937. 0.3651
|
|
62.13 0.4316 0.7241 0.0654 0.0390 3.979 31.347 17.391 2967.012 3.542 77.356 2.659 0.61 297567. 0.3424
|
|
66.01 0.4586 0.7443 0.0609 0.0375 3.830 30.177 16.198 2856.245 3.409 72.047 2.572 0.61 298227. 0.3197
|
|
69.89 0.4856 0.7620 0.0563 0.0359 3.658 28.817 14.954 2727.542 3.256 66.518 2.487 0.61 298916. 0.2970
|
|
73.78 0.5125 0.7767 0.0514 0.0339 3.462 27.276 13.669 2581.647 3.082 60.802 2.402 0.61 299634. 0.2742
|
|
77.66 0.5395 0.7883 0.0465 0.0318 3.244 25.560 12.349 2419.242 2.888 54.931 2.315 0.61 300382. 0.2513
|
|
81.54 0.5665 0.7959 0.0414 0.0295 3.005 23.677 11.001 2240.988 2.675 48.932 2.227 0.61 301159. 0.2281
|
|
85.42 0.5935 0.7989 0.0362 0.0269 2.746 21.633 9.630 2047.580 2.444 42.834 2.133 0.61 301966. 0.2044
|
|
89.31 0.6204 0.7956 0.0310 0.0242 2.467 19.438 8.243 1839.808 2.196 36.663 2.032 0.61 302802. 0.1802
|
|
93.19 0.6474 0.7838 0.0258 0.0213 2.171 17.101 6.846 1618.604 1.932 30.451 1.918 0.62 303667. 0.1550
|
|
97.07 0.6744 0.7591 0.0205 0.0182 1.857 14.634 5.447 1385.096 1.653 24.229 1.784 0.62 304561. 0.1286
|
|
100.96 0.7014 0.7135 0.0153 0.0150 1.530 12.051 4.054 1140.667 1.362 18.034 1.612 0.62 305485. 0.1002
|
|
104.84 0.7284 0.6289 0.0101 0.0117 1.189 9.372 2.676 887.009 1.059 11.904 1.368 0.62 306438. 0.0691
|
|
108.72 0.7553 0.4567 0.0050 0.0082 0.840 6.615 1.323 626.142 0.747 5.884 0.958 0.62 307419. 0.0340
|
|
112.60 0.7823 0.0004 0.0000 0.0047 0.482 3.799 0.001 359.558 0.429 0.003 0.001 0.62 308413. 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 0.1082 0.0384 5.585 39.112 36.398 4164.679 4.419 161.898 3.964 0.68 327240. 0.7386
|
|
4.37 0.0270 0.0736 0.1070 0.0392 5.698 39.902 36.009 4248.761 4.508 160.168 3.844 0.68 327490. 0.7124
|
|
8.73 0.0539 0.1426 0.1058 0.0400 5.809 40.678 35.574 4331.412 4.596 158.235 3.725 0.68 327764. 0.6862
|
|
13.10 0.0809 0.2071 0.1043 0.0407 5.915 41.426 35.090 4411.048 4.680 156.079 3.608 0.68 328064. 0.6601
|
|
17.46 0.1078 0.2674 0.1027 0.0414 6.016 42.130 34.550 4485.978 4.760 153.680 3.493 0.68 328392. 0.6341
|
|
21.83 0.1348 0.3235 0.1009 0.0420 6.108 42.772 33.952 4554.372 4.832 151.016 3.381 0.68 328748. 0.6084
|
|
26.19 0.1617 0.3757 0.0990 0.0426 6.188 43.334 33.289 4614.247 4.896 148.069 3.272 0.68 329133. 0.5830
|
|
30.56 0.1887 0.4242 0.0968 0.0431 6.254 43.797 32.558 4663.508 4.948 144.818 3.167 0.68 329548. 0.5580
|
|
34.92 0.2157 0.4692 0.0944 0.0434 6.303 44.140 31.755 4700.049 4.987 141.246 3.064 0.68 329995. 0.5333
|
|
39.29 0.2426 0.5108 0.0918 0.0436 6.332 44.344 30.876 4721.728 5.010 137.336 2.966 0.68 330473. 0.5090
|
|
43.65 0.2696 0.5494 0.0889 0.0436 6.338 44.388 29.918 4726.430 5.015 133.075 2.871 0.68 330984. 0.4850
|
|
48.02 0.2965 0.5852 0.0858 0.0435 6.319 44.253 28.879 4712.123 5.000 128.452 2.780 0.68 331527. 0.4613
|
|
52.38 0.3235 0.6182 0.0825 0.0432 6.272 43.923 27.756 4676.906 4.962 123.461 2.692 0.68 332104. 0.4380
|
|
56.75 0.3504 0.6486 0.0789 0.0426 6.194 43.380 26.551 4619.095 4.901 118.097 2.607 0.68 332713. 0.4149
|
|
61.11 0.3774 0.6766 0.0751 0.0419 6.084 42.611 25.261 4537.205 4.814 112.362 2.525 0.68 333356. 0.3920
|
|
65.48 0.4044 0.7021 0.0710 0.0409 5.941 41.602 23.889 4429.858 4.700 106.259 2.446 0.68 334032. 0.3692
|
|
69.84 0.4313 0.7253 0.0667 0.0397 5.760 40.341 22.434 4295.561 4.558 99.786 2.369 0.68 334742. 0.3465
|
|
74.21 0.4583 0.7461 0.0621 0.0382 5.544 38.823 20.901 4133.938 4.386 92.969 2.293 0.69 335485. 0.3238
|
|
78.57 0.4852 0.7643 0.0574 0.0364 5.292 37.058 19.303 3945.964 4.187 85.860 2.219 0.69 336261. 0.3011
|
|
82.94 0.5122 0.7798 0.0525 0.0345 5.006 35.056 17.649 3732.740 3.961 78.503 2.145 0.69 337070. 0.2782
|
|
87.31 0.5391 0.7921 0.0474 0.0323 4.687 32.826 15.948 3495.287 3.709 70.939 2.070 0.69 337912. 0.2552
|
|
91.67 0.5661 0.8008 0.0422 0.0299 4.338 30.377 14.210 3234.583 3.432 63.205 1.993 0.69 338787. 0.2320
|
|
96.04 0.5931 0.8049 0.0370 0.0272 3.958 27.720 12.441 2951.648 3.132 55.336 1.912 0.69 339694. 0.2082
|
|
100.40 0.6200 0.8030 0.0317 0.0244 3.551 24.865 10.650 2647.647 2.809 47.370 1.824 0.69 340634. 0.1839
|
|
104.77 0.6470 0.7929 0.0263 0.0215 3.116 21.825 8.845 2323.944 2.466 39.344 1.726 0.69 341607. 0.1586
|
|
109.13 0.6739 0.7704 0.0209 0.0183 2.658 18.616 7.037 1982.223 2.103 31.301 1.610 0.69 342613. 0.1319
|
|
113.50 0.7009 0.7273 0.0156 0.0150 2.179 15.257 5.236 1624.592 1.724 23.288 1.462 0.69 343651. 0.1033
|
|
117.86 0.7279 0.6454 0.0103 0.0116 1.681 11.774 3.452 1253.674 1.330 15.356 1.249 0.70 344722. 0.0717
|
|
122.23 0.7548 0.4736 0.0051 0.0081 1.170 8.195 1.700 872.655 0.926 7.564 0.884 0.70 345825. 0.0356
|
|
126.59 0.7818 -0.0061 0.0000 0.0045 0.649 4.545 -0.012 483.909 0.513 -0.053 -0.011 0.70 346940. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 10000
|
|
|
|
V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
|
|
(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
|
|
0.00 0.0000 0.0000 0.1096 0.0399 7.943 50.062 45.530 5922.866 5.656 202.519 3.487 0.75 363554. 0.7266
|
|
4.84 0.0269 0.0720 0.1085 0.0406 8.088 50.975 45.075 6030.892 5.759 200.493 3.390 0.75 363831. 0.7029
|
|
9.69 0.0538 0.1399 0.1073 0.0413 8.230 51.872 44.563 6137.073 5.860 198.214 3.293 0.75 364135. 0.6790
|
|
14.53 0.0808 0.2037 0.1059 0.0420 8.367 52.736 43.987 6239.340 5.958 195.656 3.198 0.75 364469. 0.6550
|
|
19.37 0.1077 0.2635 0.1044 0.0426 8.496 53.549 43.343 6335.528 6.050 192.790 3.103 0.75 364833. 0.6309
|
|
24.22 0.1346 0.3195 0.1026 0.0432 8.614 54.291 42.623 6423.240 6.134 189.588 3.010 0.75 365228. 0.6068
|
|
29.06 0.1615 0.3718 0.1007 0.0437 8.716 54.939 41.822 6499.879 6.207 186.024 2.918 0.75 365657. 0.5828
|
|
33.90 0.1884 0.4205 0.0986 0.0442 8.801 55.469 40.933 6562.685 6.267 182.070 2.829 0.76 366119. 0.5590
|
|
38.75 0.2153 0.4657 0.0962 0.0445 8.862 55.859 39.951 6608.755 6.311 177.704 2.742 0.76 366616. 0.5352
|
|
43.59 0.2423 0.5078 0.0936 0.0447 8.898 56.081 38.872 6635.091 6.336 172.903 2.657 0.76 367148. 0.5116
|
|
48.43 0.2692 0.5468 0.0908 0.0447 8.903 56.112 37.691 6638.679 6.339 167.649 2.575 0.76 367717. 0.4882
|
|
53.28 0.2961 0.5829 0.0877 0.0445 8.873 55.924 36.405 6616.519 6.318 161.929 2.496 0.76 368322. 0.4650
|
|
58.12 0.3230 0.6162 0.0843 0.0442 8.805 55.495 35.012 6565.763 6.270 155.733 2.419 0.76 368963. 0.4420
|
|
62.96 0.3499 0.6471 0.0807 0.0436 8.695 54.803 33.511 6483.797 6.192 149.056 2.344 0.76 369641. 0.4191
|
|
67.80 0.3769 0.6754 0.0768 0.0429 8.540 53.826 31.902 6368.291 6.081 141.901 2.272 0.76 370357. 0.3963
|
|
72.65 0.4038 0.7014 0.0727 0.0418 8.337 52.548 30.187 6217.079 5.937 134.271 2.202 0.76 371109. 0.3737
|
|
77.49 0.4307 0.7251 0.0683 0.0406 8.084 50.949 28.364 6027.882 5.756 126.165 2.134 0.76 371898. 0.3510
|
|
82.33 0.4576 0.7464 0.0637 0.0390 7.778 49.022 26.442 5799.894 5.538 117.612 2.068 0.76 372724. 0.3284
|
|
87.18 0.4845 0.7653 0.0588 0.0372 7.422 46.778 24.433 5534.448 5.285 108.676 2.002 0.76 373587. 0.3057
|
|
92.02 0.5114 0.7815 0.0538 0.0352 7.018 44.232 22.351 5233.196 4.997 99.416 1.937 0.76 374486. 0.2828
|
|
96.86 0.5384 0.7947 0.0487 0.0330 6.568 41.397 20.207 4897.724 4.677 89.883 1.871 0.76 375421. 0.2598
|
|
101.71 0.5653 0.8043 0.0434 0.0305 6.074 38.286 18.014 4529.633 4.325 80.124 1.804 0.77 376392. 0.2364
|
|
106.55 0.5922 0.8093 0.0380 0.0278 5.539 34.913 15.779 4130.664 3.944 70.186 1.733 0.77 377399. 0.2125
|
|
111.39 0.6191 0.8084 0.0325 0.0249 4.966 31.297 13.515 3702.853 3.536 60.113 1.655 0.77 378443. 0.1879
|
|
116.24 0.6460 0.7990 0.0270 0.0219 4.357 27.459 11.231 3248.676 3.102 49.954 1.568 0.77 379522. 0.1623
|
|
121.08 0.6729 0.7766 0.0215 0.0187 3.716 23.423 8.939 2771.212 2.646 39.762 1.463 0.77 380638. 0.1351
|
|
125.92 0.6999 0.7326 0.0160 0.0153 3.050 19.223 6.654 2274.270 2.172 29.596 1.327 0.77 381789. 0.1057
|
|
130.77 0.7268 0.6475 0.0106 0.0119 2.364 14.897 4.389 1762.516 1.683 19.521 1.129 0.77 382977. 0.0731
|
|
135.61 0.7537 0.4693 0.0052 0.0084 1.665 10.493 2.161 1241.483 1.186 9.611 0.789 0.78 384199. 0.0358
|
|
140.45 0.7806 -0.0075 0.0000 0.0048 0.959 6.047 -0.019 715.395 0.683 -0.085 -0.012 0.78 385436. 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 0.1112 0.0441 11.697 67.023 55.872 8722.545 7.572 248.521 2.905 0.83 399847. 0.6707
|
|
5.32 0.0269 0.0663 0.1102 0.0447 11.853 67.917 55.364 8838.931 7.673 246.258 2.841 0.83 400151. 0.6528
|
|
10.64 0.0538 0.1295 0.1090 0.0453 12.003 68.773 54.786 8950.328 7.770 243.688 2.776 0.83 400485. 0.6346
|
|
15.96 0.0807 0.1898 0.1077 0.0458 12.142 69.570 54.132 9054.070 7.860 240.778 2.712 0.83 400852. 0.6162
|
|
21.28 0.1075 0.2470 0.1062 0.0463 12.267 70.287 53.392 9147.355 7.941 237.488 2.647 0.83 401252. 0.5974
|
|
26.60 0.1344 0.3013 0.1046 0.0467 12.374 70.901 52.558 9227.272 8.010 233.780 2.584 0.83 401687. 0.5784
|
|
31.93 0.1613 0.3527 0.1027 0.0470 12.459 71.389 51.623 9290.731 8.065 229.617 2.520 0.83 402159. 0.5592
|
|
37.25 0.1882 0.4013 0.1006 0.0472 12.518 71.725 50.576 9334.483 8.103 224.964 2.458 0.83 402668. 0.5397
|
|
42.57 0.2151 0.4471 0.0983 0.0473 12.546 71.884 49.413 9355.241 8.121 219.787 2.396 0.83 403216. 0.5201
|
|
47.89 0.2420 0.4901 0.0958 0.0473 12.538 71.842 48.124 9349.673 8.117 214.057 2.335 0.83 403804. 0.5002
|
|
53.21 0.2688 0.5305 0.0929 0.0471 12.491 71.571 46.706 9314.454 8.086 207.749 2.274 0.83 404431. 0.4800
|
|
58.53 0.2957 0.5683 0.0899 0.0468 12.399 71.047 45.154 9246.283 8.027 200.844 2.215 0.83 405098. 0.4597
|
|
63.85 0.3226 0.6036 0.0865 0.0462 12.260 70.245 43.464 9141.950 7.936 193.328 2.156 0.83 405806. 0.4390
|
|
69.17 0.3495 0.6364 0.0829 0.0455 12.067 69.144 41.636 8998.543 7.812 185.196 2.099 0.83 406554. 0.4182
|
|
74.49 0.3764 0.6667 0.0789 0.0446 11.819 67.720 39.670 8813.254 7.651 176.450 2.042 0.83 407343. 0.3971
|
|
79.81 0.4033 0.6946 0.0748 0.0434 11.511 65.954 37.567 8583.404 7.451 167.096 1.985 0.84 408173. 0.3757
|
|
85.13 0.4302 0.7200 0.0703 0.0420 11.138 63.821 35.327 8305.883 7.210 157.133 1.929 0.84 409043. 0.3541
|
|
90.46 0.4570 0.7429 0.0656 0.0403 10.700 61.309 32.957 7978.893 6.927 146.593 1.873 0.84 409953. 0.3321
|
|
95.78 0.4839 0.7631 0.0606 0.0385 10.199 58.440 30.475 7605.536 6.603 135.551 1.817 0.84 410903. 0.3098
|
|
101.10 0.5108 0.7799 0.0555 0.0364 9.642 55.249 27.896 7190.244 6.242 124.083 1.760 0.84 411893. 0.2870
|
|
106.42 0.5377 0.7930 0.0502 0.0341 9.031 51.744 25.237 6734.123 5.846 112.255 1.700 0.84 412923. 0.2637
|
|
111.74 0.5646 0.8017 0.0448 0.0315 8.366 47.936 22.511 6238.529 5.416 100.127 1.637 0.84 413992. 0.2398
|
|
117.06 0.5915 0.8049 0.0393 0.0289 7.652 43.842 19.730 5705.779 4.953 87.760 1.568 0.84 415100. 0.2151
|
|
122.38 0.6183 0.8005 0.0336 0.0260 6.893 39.495 16.908 5139.959 4.462 75.209 1.492 0.84 416247. 0.1895
|
|
127.70 0.6452 0.7852 0.0280 0.0230 6.097 34.934 14.059 4546.471 3.947 62.534 1.403 0.85 417433. 0.1624
|
|
133.02 0.6721 0.7533 0.0223 0.0199 5.272 30.206 11.196 3931.125 3.413 49.801 1.292 0.85 418659. 0.1335
|
|
138.34 0.6990 0.6948 0.0166 0.0167 4.427 25.364 8.337 3300.955 2.866 37.084 1.146 0.85 419924. 0.1022
|
|
143.66 0.7259 0.5898 0.0109 0.0135 3.572 20.470 5.500 2664.009 2.313 24.465 0.936 0.85 421228. 0.0678
|
|
148.98 0.7528 0.3951 0.0054 0.0103 2.721 15.591 2.706 2029.072 1.761 12.038 0.605 0.85 422570. 0.0307
|
|
154.31 0.7797 -0.0061 -0.0001 0.0071 1.880 10.774 -0.028 1402.097 1.217 -0.125 -0.009 0.85 423933. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 12000
|
|
|
|
V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
|
|
(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
|
|
0.00 0.0000 0.0000 0.1119 0.0520 17.895 93.992 66.912 13344.392 10.619 297.624 2.274 0.90 436161. 0.5745
|
|
5.88 0.0272 0.0576 0.1110 0.0525 18.081 94.970 66.391 13483.326 10.730 295.305 2.233 0.90 436492. 0.5620
|
|
11.76 0.0545 0.1131 0.1100 0.0530 18.249 95.849 65.788 13608.125 10.829 292.623 2.193 0.90 436857. 0.5493
|
|
17.65 0.0817 0.1665 0.1088 0.0534 18.391 96.594 65.092 13713.897 10.913 289.528 2.153 0.90 437259. 0.5364
|
|
23.53 0.1090 0.2180 0.1075 0.0537 18.501 97.171 64.291 13795.826 10.978 285.965 2.114 0.90 437700. 0.5234
|
|
29.41 0.1362 0.2676 0.1060 0.0539 18.572 97.547 63.372 13849.105 11.021 281.879 2.075 0.91 438180. 0.5102
|
|
35.29 0.1635 0.3154 0.1042 0.0540 18.599 97.688 62.323 13869.155 11.037 277.215 2.038 0.91 438703. 0.4969
|
|
41.18 0.1907 0.3613 0.1022 0.0539 18.576 97.565 61.133 13851.757 11.023 271.920 2.002 0.91 439269. 0.4834
|
|
47.06 0.2180 0.4056 0.1000 0.0537 18.497 97.153 59.790 13793.178 10.976 265.946 1.966 0.91 439878. 0.4695
|
|
52.94 0.2452 0.4482 0.0975 0.0533 18.359 96.427 58.285 13690.186 10.894 259.252 1.931 0.91 440533. 0.4553
|
|
58.82 0.2724 0.4890 0.0947 0.0527 18.156 95.362 56.608 13538.988 10.774 251.793 1.896 0.91 441234. 0.4406
|
|
64.70 0.2997 0.5282 0.0916 0.0519 17.887 93.949 54.755 13338.358 10.614 243.551 1.862 0.91 441980. 0.4255
|
|
70.59 0.3269 0.5655 0.0882 0.0510 17.549 92.173 52.722 13086.157 10.414 234.506 1.827 0.91 442772. 0.4098
|
|
76.47 0.3542 0.6009 0.0845 0.0498 17.139 90.020 50.506 12780.478 10.170 224.652 1.792 0.91 443610. 0.3934
|
|
82.35 0.3814 0.6343 0.0804 0.0484 16.655 87.477 48.109 12419.523 9.883 213.989 1.757 0.91 444495. 0.3763
|
|
88.23 0.4087 0.6656 0.0761 0.0467 16.094 84.532 45.532 12001.311 9.550 202.524 1.721 0.91 445424. 0.3586
|
|
94.11 0.4359 0.6947 0.0715 0.0449 15.453 81.164 42.774 11523.255 9.170 190.260 1.684 0.91 446400. 0.3401
|
|
100.00 0.4631 0.7213 0.0666 0.0428 14.731 77.374 39.849 10985.051 8.742 177.250 1.645 0.91 447420. 0.3208
|
|
105.88 0.4904 0.7453 0.0615 0.0405 13.933 73.181 36.781 10389.755 8.268 163.602 1.606 0.92 448485. 0.3007
|
|
111.76 0.5176 0.7647 0.0562 0.0380 13.091 68.756 33.588 9761.626 7.768 149.401 1.561 0.92 449594. 0.2793
|
|
117.64 0.5449 0.7776 0.0506 0.0355 12.220 64.183 30.289 9112.350 7.251 134.725 1.508 0.92 450747. 0.2562
|
|
123.53 0.5721 0.7806 0.0450 0.0330 11.350 59.613 26.897 8463.435 6.735 119.640 1.441 0.92 451944. 0.2309
|
|
129.41 0.5994 0.7731 0.0392 0.0304 10.460 54.938 23.434 7799.785 6.207 104.236 1.363 0.92 453184. 0.2037
|
|
135.29 0.6266 0.7537 0.0333 0.0277 9.536 50.087 19.923 7111.126 5.659 88.616 1.271 0.92 454468. 0.1752
|
|
141.17 0.6539 0.7177 0.0274 0.0250 8.593 45.133 16.383 6407.666 5.099 72.871 1.160 0.92 455795. 0.1450
|
|
147.05 0.6811 0.6584 0.0215 0.0222 7.645 40.153 12.837 5700.751 4.537 57.097 1.021 0.93 457166. 0.1130
|
|
152.94 0.7083 0.5662 0.0156 0.0195 6.706 35.221 9.310 5000.449 3.979 41.410 0.844 0.93 458580. 0.0796
|
|
158.82 0.7356 0.4266 0.0098 0.0168 5.790 30.412 5.832 4317.677 3.436 25.943 0.613 0.93 460038. 0.0457
|
|
164.70 0.7628 0.2179 0.0041 0.0143 4.911 25.795 2.437 3662.184 2.914 10.841 0.302 0.93 461539. 0.0146
|
|
170.58 0.7901
|
|
|
|
|
|
|