427 lines
76 KiB
Plaintext
427 lines
76 KiB
Plaintext
19x11 (19x11.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 0.0966 0.0400 0.008 0.502 0.401 5.942 0.057 1.785 30.625 0.08 39484. 0.5991
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0.46 0.0255 0.0600 0.0953 0.0405 0.008 0.509 0.396 6.022 0.058 1.760 29.799 0.08 39511. 0.5789
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0.92 0.0511 0.1167 0.0938 0.0410 0.008 0.515 0.390 6.099 0.058 1.733 28.974 0.08 39542. 0.5585
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1.38 0.0766 0.1702 0.0922 0.0415 0.008 0.522 0.383 6.170 0.059 1.703 28.152 0.08 39575. 0.5380
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1.84 0.1022 0.2203 0.0905 0.0420 0.008 0.527 0.376 6.234 0.060 1.671 27.337 0.08 39611. 0.5175
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2.30 0.1277 0.2672 0.0886 0.0423 0.008 0.532 0.368 6.290 0.060 1.637 26.529 0.08 39650. 0.4970
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2.76 0.1532 0.3110 0.0865 0.0426 0.008 0.536 0.359 6.336 0.061 1.599 25.731 0.08 39692. 0.4764
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3.22 0.1788 0.3518 0.0843 0.0429 0.009 0.538 0.350 6.370 0.061 1.558 24.943 0.08 39737. 0.4559
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3.68 0.2043 0.3895 0.0820 0.0430 0.009 0.540 0.340 6.389 0.061 1.514 24.165 0.08 39785. 0.4354
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4.14 0.2299 0.4243 0.0794 0.0430 0.009 0.540 0.330 6.392 0.061 1.467 23.398 0.08 39837. 0.4149
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4.60 0.2554 0.4561 0.0766 0.0429 0.009 0.539 0.318 6.377 0.061 1.416 22.641 0.08 39892. 0.3945
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5.06 0.2810 0.4852 0.0737 0.0427 0.009 0.536 0.306 6.342 0.061 1.362 21.893 0.08 39951. 0.3741
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5.51 0.3065 0.5114 0.0706 0.0423 0.008 0.531 0.293 6.284 0.060 1.304 21.152 0.08 40013. 0.3536
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5.97 0.3320 0.5348 0.0672 0.0418 0.008 0.524 0.279 6.204 0.059 1.242 20.418 0.08 40079. 0.3332
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6.43 0.3576 0.5553 0.0638 0.0411 0.008 0.516 0.265 6.101 0.058 1.178 19.686 0.08 40148. 0.3128
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6.89 0.3831 0.5728 0.0601 0.0402 0.008 0.505 0.250 5.974 0.057 1.110 18.954 0.08 40220. 0.2925
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7.35 0.4087 0.5872 0.0563 0.0392 0.008 0.492 0.234 5.825 0.056 1.041 18.217 0.08 40297. 0.2721
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7.81 0.4342 0.5984 0.0524 0.0380 0.008 0.478 0.218 5.652 0.054 0.968 17.471 0.08 40377. 0.2518
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8.27 0.4597 0.6059 0.0484 0.0367 0.007 0.461 0.201 5.457 0.052 0.894 16.709 0.08 40460. 0.2314
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8.73 0.4853 0.6095 0.0443 0.0353 0.007 0.443 0.184 5.239 0.050 0.818 15.923 0.08 40547. 0.2109
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9.19 0.5108 0.6086 0.0401 0.0336 0.007 0.422 0.166 4.998 0.048 0.740 15.104 0.08 40638. 0.1903
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9.65 0.5364 0.6024 0.0358 0.0319 0.006 0.400 0.149 4.735 0.045 0.661 14.238 0.08 40733. 0.1695
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10.11 0.5619 0.5898 0.0314 0.0299 0.006 0.376 0.131 4.449 0.042 0.581 13.307 0.08 40831. 0.1485
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10.57 0.5875 0.5694 0.0270 0.0279 0.006 0.350 0.112 4.141 0.040 0.499 12.288 0.08 40933. 0.1271
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11.03 0.6130 0.5388 0.0225 0.0256 0.005 0.322 0.094 3.810 0.036 0.416 11.144 0.08 41038. 0.1053
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11.49 0.6385 0.4948 0.0180 0.0233 0.005 0.292 0.075 3.458 0.033 0.333 9.824 0.08 41148. 0.0830
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11.95 0.6641 0.4319 0.0135 0.0208 0.004 0.261 0.056 3.085 0.029 0.249 8.246 0.08 41261. 0.0603
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12.41 0.6896 0.3414 0.0090 0.0181 0.004 0.228 0.037 2.693 0.026 0.166 6.275 0.08 41377. 0.0374
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12.87 0.7152 0.2071 0.0044 0.0154 0.003 0.193 0.018 2.282 0.022 0.082 3.671 0.08 41497. 0.0154
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13.33 0.7407 -0.0032 -0.0001 0.0125 0.002 0.157 0.000 1.853 0.018 -0.001 -0.054 0.08 41618. 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 0.0971 0.0362 0.058 1.818 1.612 43.015 0.205 7.172 17.002 0.15 78966. 0.6667
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0.93 0.0260 0.0675 0.0957 0.0368 0.059 1.848 1.590 43.717 0.209 7.072 16.497 0.15 79023. 0.6424
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1.87 0.0519 0.1310 0.0942 0.0373 0.060 1.876 1.565 44.390 0.212 6.963 15.996 0.15 79084. 0.6181
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2.80 0.0779 0.1904 0.0926 0.0379 0.060 1.903 1.539 45.022 0.215 6.844 15.501 0.15 79152. 0.5938
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3.74 0.1038 0.2459 0.0909 0.0384 0.061 1.927 1.509 45.599 0.218 6.714 15.014 0.15 79225. 0.5697
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4.67 0.1298 0.2975 0.0889 0.0388 0.062 1.949 1.478 46.106 0.220 6.573 14.536 0.15 79305. 0.5457
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5.60 0.1557 0.3455 0.0869 0.0391 0.062 1.966 1.443 46.528 0.222 6.419 14.068 0.15 79391. 0.5219
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6.54 0.1817 0.3900 0.0846 0.0394 0.063 1.980 1.406 46.849 0.224 6.253 13.609 0.15 79483. 0.4983
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7.47 0.2076 0.4310 0.0822 0.0396 0.063 1.988 1.365 47.050 0.225 6.073 13.161 0.15 79583. 0.4749
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8.40 0.2336 0.4688 0.0796 0.0396 0.063 1.991 1.322 47.114 0.225 5.879 12.724 0.15 79689. 0.4518
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9.34 0.2595 0.5034 0.0767 0.0396 0.063 1.987 1.275 47.023 0.225 5.671 12.297 0.15 79802. 0.4288
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10.27 0.2855 0.5350 0.0737 0.0393 0.063 1.976 1.225 46.760 0.223 5.448 11.880 0.15 79922. 0.4060
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11.21 0.3114 0.5635 0.0705 0.0390 0.062 1.957 1.171 46.311 0.221 5.210 11.471 0.15 80050. 0.3834
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12.14 0.3374 0.5892 0.0671 0.0384 0.061 1.930 1.115 45.666 0.218 4.958 11.071 0.15 80185. 0.3610
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13.07 0.3633 0.6119 0.0635 0.0377 0.060 1.894 1.055 44.823 0.214 4.693 10.677 0.15 80327. 0.3387
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14.01 0.3893 0.6317 0.0598 0.0368 0.059 1.850 0.993 43.780 0.209 4.417 10.288 0.15 80476. 0.3166
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14.94 0.4152 0.6485 0.0559 0.0358 0.057 1.798 0.929 42.540 0.203 4.131 9.901 0.15 80633. 0.2947
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15.87 0.4412 0.6622 0.0519 0.0346 0.055 1.737 0.862 41.101 0.196 3.835 9.515 0.15 80798. 0.2728
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16.81 0.4671 0.6724 0.0478 0.0332 0.053 1.668 0.794 39.464 0.188 3.531 9.124 0.15 80970. 0.2511
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17.74 0.4931 0.6788 0.0436 0.0317 0.050 1.590 0.724 37.628 0.180 3.220 8.727 0.15 81149. 0.2293
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18.68 0.5190 0.6808 0.0393 0.0299 0.048 1.504 0.653 35.592 0.170 2.902 8.316 0.15 81336. 0.2074
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19.61 0.5450 0.6778 0.0349 0.0281 0.045 1.410 0.580 33.358 0.159 2.579 7.884 0.15 81531. 0.1854
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20.54 0.5709 0.6684 0.0305 0.0260 0.041 1.307 0.506 30.926 0.148 2.251 7.421 0.15 81733. 0.1630
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21.48 0.5969 0.6509 0.0260 0.0238 0.038 1.196 0.431 28.298 0.135 1.918 6.912 0.15 81942. 0.1402
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22.41 0.6228 0.6223 0.0214 0.0214 0.034 1.077 0.356 25.476 0.122 1.582 6.334 0.15 82160. 0.1167
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23.35 0.6488 0.5781 0.0168 0.0189 0.030 0.949 0.280 22.466 0.107 1.244 5.649 0.15 82385. 0.0923
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24.28 0.6747 0.5098 0.0123 0.0162 0.026 0.815 0.204 19.276 0.092 0.905 4.789 0.15 82617. 0.0667
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25.21 0.7007 0.4012 0.0077 0.0134 0.021 0.673 0.127 15.916 0.076 0.567 3.630 0.15 82857. 0.0400
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26.15 0.7266 0.2163 0.0031 0.0104 0.017 0.524 0.052 12.401 0.059 0.229 1.887 0.15 83103. 0.0132
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27.08 0.7526
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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 0.0975 0.0347 0.187 3.925 3.644 139.315 0.443 16.211 11.865 0.23 118446. 0.6995
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1.39 0.0257 0.0701 0.0962 0.0353 0.190 3.994 3.595 141.746 0.451 15.990 11.503 0.23 118530. 0.6736
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2.78 0.0515 0.1358 0.0947 0.0359 0.193 4.060 3.541 144.089 0.459 15.748 11.145 0.23 118622. 0.6476
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4.17 0.0772 0.1972 0.0931 0.0365 0.196 4.122 3.481 146.296 0.466 15.484 10.793 0.23 118722. 0.6219
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5.56 0.1030 0.2545 0.0914 0.0370 0.199 4.179 3.416 148.324 0.472 15.196 10.447 0.23 118831. 0.5963
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6.95 0.1287 0.3079 0.0895 0.0374 0.201 4.230 3.346 150.122 0.478 14.882 10.109 0.23 118950. 0.5710
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8.34 0.1544 0.3574 0.0875 0.0378 0.203 4.272 3.269 151.639 0.483 14.541 9.778 0.23 119077. 0.5460
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9.73 0.1802 0.4032 0.0852 0.0381 0.205 4.306 3.186 152.818 0.486 14.171 9.456 0.23 119214. 0.5213
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11.12 0.2059 0.4455 0.0828 0.0383 0.206 4.328 3.096 153.603 0.489 13.772 9.143 0.23 119362. 0.4968
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12.50 0.2317 0.4845 0.0802 0.0384 0.206 4.337 3.000 153.934 0.490 13.342 8.838 0.23 119519. 0.4727
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13.89 0.2574 0.5203 0.0775 0.0383 0.206 4.332 2.895 153.748 0.489 12.879 8.542 0.23 119687. 0.4489
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15.28 0.2831 0.5530 0.0745 0.0381 0.205 4.310 2.784 152.989 0.487 12.383 8.254 0.23 119865. 0.4253
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16.67 0.3089 0.5828 0.0713 0.0378 0.203 4.271 2.665 151.605 0.483 11.855 7.974 0.23 120054. 0.4020
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18.06 0.3346 0.6097 0.0679 0.0373 0.201 4.214 2.539 149.565 0.476 11.294 7.700 0.23 120254. 0.3789
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19.45 0.3604 0.6339 0.0644 0.0366 0.197 4.137 2.407 146.854 0.467 10.705 7.433 0.23 120464. 0.3561
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20.84 0.3861 0.6552 0.0607 0.0358 0.192 4.042 2.268 143.469 0.457 10.090 7.172 0.23 120686. 0.3336
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22.23 0.4118 0.6738 0.0568 0.0347 0.187 3.928 2.125 139.409 0.444 9.452 6.913 0.23 120918. 0.3112
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23.62 0.4376 0.6894 0.0529 0.0336 0.181 3.794 1.977 134.675 0.429 8.793 6.657 0.23 121161. 0.2891
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25.01 0.4633 0.7019 0.0488 0.0322 0.173 3.642 1.824 129.265 0.411 8.115 6.402 0.23 121416. 0.2670
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26.40 0.4891 0.7110 0.0446 0.0307 0.165 3.470 1.668 123.177 0.392 7.421 6.143 0.23 121681. 0.2451
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27.79 0.5148 0.7163 0.0404 0.0290 0.156 3.280 1.509 116.410 0.371 6.712 5.880 0.23 121957. 0.2231
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29.18 0.5405 0.7171 0.0360 0.0272 0.146 3.070 1.347 108.964 0.347 5.990 5.606 0.23 122245. 0.2009
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30.57 0.5663 0.7124 0.0316 0.0251 0.135 2.841 1.182 100.839 0.321 5.257 5.316 0.23 122544. 0.1785
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31.96 0.5920 0.7007 0.0272 0.0229 0.123 2.593 1.015 92.042 0.293 4.515 5.002 0.23 122854. 0.1556
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33.35 0.6178 0.6796 0.0226 0.0206 0.111 2.327 0.846 82.581 0.263 3.765 4.649 0.23 123175. 0.1321
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34.73 0.6435 0.6447 0.0181 0.0181 0.097 2.042 0.677 72.473 0.231 3.009 4.234 0.23 123508. 0.1075
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36.12 0.6692 0.5887 0.0135 0.0154 0.083 1.740 0.506 61.742 0.197 2.251 3.718 0.23 123851. 0.0817
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37.51 0.6950 0.4965 0.0090 0.0126 0.068 1.421 0.336 50.424 0.161 1.493 3.019 0.23 124205. 0.0540
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38.90 0.7207 0.3328 0.0044 0.0096 0.052 1.086 0.166 38.561 0.123 0.738 1.952 0.23 124570. 0.0245
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40.29 0.7465 -0.0103 -0.0001 0.0065 0.035 0.736 -0.003 26.121 0.083 -0.015 -0.059 0.23 124928. 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 0.0980 0.0340 0.434 6.839 6.515 323.640 0.773 28.980 9.131 0.30 157922. 0.7198
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1.86 0.0259 0.0722 0.0967 0.0347 0.442 6.964 6.427 329.589 0.787 28.588 8.845 0.30 158035. 0.6925
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3.73 0.0518 0.1398 0.0953 0.0353 0.450 7.086 6.331 335.325 0.801 28.158 8.563 0.30 158158. 0.6654
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5.59 0.0776 0.2030 0.0937 0.0358 0.457 7.200 6.225 340.737 0.813 27.688 8.286 0.30 158293. 0.6384
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7.45 0.1035 0.2618 0.0919 0.0364 0.464 7.305 6.109 345.714 0.825 27.173 8.015 0.30 158440. 0.6118
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9.31 0.1294 0.3164 0.0900 0.0368 0.470 7.399 5.983 350.135 0.836 26.612 7.750 0.30 158599. 0.5854
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11.18 0.1553 0.3671 0.0880 0.0372 0.475 7.478 5.846 353.871 0.845 26.002 7.493 0.30 158770. 0.5595
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13.04 0.1812 0.4140 0.0857 0.0375 0.478 7.539 5.697 356.788 0.852 25.340 7.242 0.30 158955. 0.5338
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14.90 0.2071 0.4572 0.0833 0.0377 0.481 7.580 5.536 358.744 0.856 24.624 6.999 0.30 159153. 0.5086
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16.76 0.2329 0.4971 0.0807 0.0378 0.482 7.598 5.362 359.590 0.858 23.850 6.763 0.30 159365. 0.4837
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18.63 0.2588 0.5336 0.0779 0.0378 0.482 7.590 5.175 359.179 0.857 23.019 6.535 0.30 159591. 0.4591
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20.49 0.2847 0.5671 0.0749 0.0376 0.479 7.551 4.974 357.369 0.853 22.126 6.314 0.30 159832. 0.4349
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22.35 0.3106 0.5976 0.0716 0.0372 0.475 7.481 4.760 354.037 0.845 21.174 6.099 0.30 160086. 0.4109
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24.22 0.3365 0.6253 0.0682 0.0367 0.468 7.377 4.534 349.104 0.833 20.165 5.890 0.30 160355. 0.3873
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26.08 0.3623 0.6502 0.0646 0.0360 0.459 7.238 4.295 342.536 0.818 19.104 5.687 0.30 160639. 0.3640
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27.94 0.3882 0.6723 0.0609 0.0352 0.448 7.064 4.046 334.324 0.798 17.996 5.489 0.30 160937. 0.3409
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29.80 0.4141 0.6917 0.0570 0.0341 0.435 6.856 3.787 324.467 0.775 16.846 5.294 0.30 161250. 0.3182
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31.67 0.4400 0.7083 0.0530 0.0329 0.420 6.613 3.520 312.962 0.747 15.658 5.102 0.30 161578. 0.2956
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33.53 0.4659 0.7218 0.0488 0.0315 0.402 6.335 3.246 299.806 0.716 14.438 4.911 0.30 161920. 0.2732
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35.39 0.4918 0.7321 0.0446 0.0300 0.382 6.022 2.965 284.994 0.680 13.187 4.718 0.31 162278. 0.2509
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37.25 0.5176 0.7387 0.0403 0.0282 0.360 5.674 2.678 268.521 0.641 11.911 4.523 0.31 162650. 0.2286
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39.12 0.5435 0.7411 0.0359 0.0263 0.336 5.291 2.386 250.386 0.598 10.611 4.321 0.31 163038. 0.2061
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40.98 0.5694 0.7381 0.0314 0.0242 0.309 4.873 2.089 230.594 0.551 9.291 4.109 0.31 163441. 0.1834
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42.84 0.5953 0.7284 0.0269 0.0220 0.280 4.420 1.788 209.157 0.499 7.954 3.878 0.31 163858. 0.1602
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44.70 0.6212 0.7092 0.0223 0.0196 0.250 3.932 1.485 186.101 0.444 6.604 3.619 0.31 164291. 0.1362
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46.57 0.6470 0.6763 0.0177 0.0170 0.217 3.412 1.179 161.468 0.385 5.245 3.313 0.31 164739. 0.1111
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48.43 0.6729 0.6211 0.0131 0.0142 0.181 2.859 0.873 135.321 0.323 3.882 2.925 0.31 165201. 0.0844
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50.29 0.6988 0.5257 0.0085 0.0113 0.144 2.277 0.566 107.750 0.257 2.520 2.385 0.31 165679. 0.0554
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52.16 0.7247 0.3442 0.0039 0.0083 0.106 1.666 0.262 78.864 0.188 1.164 1.505 0.31 166169. 0.0238
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54.02 0.7506
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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 0.0987 0.0337 0.840 10.592 10.250 626.570 1.197 45.592 7.420 0.38 197392. 0.7336
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2.32 0.0258 0.0731 0.0974 0.0344 0.856 10.792 10.114 638.436 1.219 44.989 7.186 0.38 197533. 0.7057
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4.64 0.0516 0.1415 0.0960 0.0350 0.872 10.986 9.965 649.891 1.241 44.325 6.955 0.38 197687. 0.6780
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6.96 0.0774 0.2054 0.0944 0.0356 0.886 11.169 9.801 660.714 1.262 43.596 6.728 0.38 197855. 0.6505
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9.28 0.1032 0.2648 0.0927 0.0361 0.899 11.338 9.622 670.684 1.281 42.799 6.507 0.38 198038. 0.6234
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|
11.60 0.1290 0.3200 0.0908 0.0366 0.911 11.488 9.426 679.564 1.298 41.929 6.292 0.38 198236. 0.5966
|
|
13.92 0.1548 0.3712 0.0887 0.0370 0.921 11.615 9.213 687.103 1.312 40.981 6.082 0.38 198450. 0.5701
|
|
16.24 0.1806 0.4186 0.0865 0.0373 0.929 11.715 8.982 693.035 1.324 39.952 5.878 0.38 198681. 0.5441
|
|
18.56 0.2064 0.4624 0.0841 0.0375 0.935 11.784 8.731 697.080 1.331 38.838 5.681 0.38 198928. 0.5184
|
|
20.89 0.2322 0.5027 0.0815 0.0376 0.937 11.815 8.461 698.951 1.335 37.634 5.490 0.38 199192. 0.4932
|
|
23.21 0.2580 0.5398 0.0787 0.0376 0.937 11.805 8.169 698.357 1.334 36.337 5.306 0.38 199473. 0.4683
|
|
25.53 0.2837 0.5738 0.0757 0.0374 0.932 11.749 7.856 695.016 1.327 34.946 5.127 0.38 199773. 0.4438
|
|
27.85 0.3095 0.6048 0.0725 0.0371 0.924 11.642 7.522 688.686 1.315 33.460 4.954 0.38 200089. 0.4196
|
|
30.17 0.3353 0.6331 0.0690 0.0366 0.911 11.482 7.168 679.203 1.297 31.883 4.787 0.38 200424. 0.3958
|
|
32.49 0.3611 0.6586 0.0654 0.0359 0.894 11.267 6.795 666.497 1.273 30.224 4.624 0.38 200777. 0.3722
|
|
34.81 0.3869 0.6815 0.0617 0.0350 0.872 10.997 6.405 650.545 1.242 28.490 4.466 0.38 201148. 0.3490
|
|
37.13 0.4127 0.7017 0.0578 0.0340 0.847 10.673 6.000 631.345 1.206 26.690 4.311 0.38 201538. 0.3261
|
|
39.45 0.4385 0.7192 0.0538 0.0328 0.817 10.293 5.582 608.892 1.163 24.831 4.158 0.38 201946. 0.3034
|
|
41.77 0.4643 0.7339 0.0496 0.0314 0.782 9.858 5.153 583.180 1.114 22.919 4.007 0.38 202372. 0.2809
|
|
44.09 0.4901 0.7455 0.0454 0.0298 0.743 9.368 4.712 554.197 1.058 20.960 3.857 0.38 202816. 0.2585
|
|
46.41 0.5159 0.7536 0.0411 0.0281 0.700 8.823 4.262 521.935 0.997 18.959 3.704 0.38 203280. 0.2362
|
|
48.73 0.5417 0.7579 0.0366 0.0262 0.652 8.222 3.804 486.391 0.929 16.921 3.547 0.38 203762. 0.2137
|
|
51.05 0.5675 0.7573 0.0322 0.0241 0.600 7.566 3.339 447.571 0.855 14.851 3.384 0.38 204262. 0.1909
|
|
53.37 0.5933 0.7505 0.0276 0.0218 0.544 6.855 2.867 405.498 0.774 12.754 3.207 0.38 204781. 0.1677
|
|
55.69 0.6191 0.7351 0.0230 0.0194 0.483 6.089 2.391 360.222 0.688 10.636 3.011 0.38 205319. 0.1438
|
|
58.01 0.6449 0.7072 0.0184 0.0168 0.418 5.271 1.911 311.820 0.596 8.502 2.780 0.38 205875. 0.1187
|
|
60.34 0.6707 0.6589 0.0138 0.0140 0.349 4.402 1.430 260.415 0.497 6.361 2.491 0.39 206450. 0.0920
|
|
62.66 0.6965 0.5734 0.0091 0.0111 0.276 3.485 0.949 206.176 0.394 4.221 2.087 0.39 207043. 0.0628
|
|
64.98 0.7223 0.4066 0.0045 0.0080 0.200 2.524 0.470 149.318 0.285 2.090 1.427 0.39 207653. 0.0302
|
|
67.30 0.7481 -0.0144 -0.0001 0.0048 0.120 1.512 -0.010 89.449 0.171 -0.043 -0.049 0.39 208236. 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 0.0995 0.0337 1.450 15.235 14.884 1081.477 1.721 66.202 6.242 0.45 236855. 0.7437
|
|
2.79 0.0258 0.0738 0.0983 0.0344 1.479 15.531 14.691 1102.527 1.755 65.344 6.044 0.45 237024. 0.7154
|
|
5.57 0.0516 0.1428 0.0968 0.0350 1.506 15.818 14.478 1122.861 1.787 64.397 5.848 0.45 237209. 0.6872
|
|
8.36 0.0774 0.2072 0.0953 0.0356 1.532 16.089 14.244 1142.085 1.818 63.356 5.657 0.45 237412. 0.6593
|
|
11.14 0.1032 0.2672 0.0936 0.0361 1.555 16.338 13.987 1159.808 1.846 62.215 5.470 0.45 237632. 0.6318
|
|
13.93 0.1290 0.3229 0.0917 0.0366 1.577 16.561 13.706 1175.611 1.871 60.966 5.288 0.45 237870. 0.6046
|
|
16.71 0.1548 0.3745 0.0896 0.0370 1.595 16.750 13.400 1189.048 1.892 59.603 5.111 0.45 238128. 0.5778
|
|
19.50 0.1806 0.4223 0.0874 0.0374 1.609 16.900 13.067 1199.651 1.909 58.120 4.940 0.45 238405. 0.5515
|
|
22.28 0.2064 0.4665 0.0850 0.0376 1.619 17.002 12.705 1206.929 1.921 56.512 4.775 0.45 238703. 0.5256
|
|
25.07 0.2322 0.5072 0.0824 0.0377 1.623 17.051 12.314 1210.379 1.926 54.772 4.614 0.45 239020. 0.5001
|
|
27.86 0.2580 0.5446 0.0795 0.0377 1.622 17.038 11.892 1209.484 1.925 52.897 4.460 0.45 239359. 0.4750
|
|
30.64 0.2838 0.5790 0.0765 0.0375 1.614 16.957 11.439 1203.758 1.916 50.882 4.310 0.45 239719. 0.4502
|
|
33.43 0.3096 0.6105 0.0733 0.0372 1.600 16.803 10.955 1192.767 1.898 48.728 4.166 0.45 240101. 0.4258
|
|
36.21 0.3354 0.6392 0.0698 0.0366 1.577 16.570 10.441 1176.222 1.872 46.441 4.026 0.45 240504. 0.4018
|
|
39.00 0.3612 0.6652 0.0662 0.0360 1.548 16.256 9.899 1153.995 1.837 44.032 3.891 0.46 240928. 0.3781
|
|
41.78 0.3871 0.6886 0.0624 0.0351 1.510 15.863 9.333 1126.048 1.792 41.513 3.759 0.46 241375. 0.3547
|
|
44.57 0.4129 0.7095 0.0585 0.0340 1.465 15.388 8.745 1092.378 1.739 38.897 3.631 0.46 241843. 0.3316
|
|
47.36 0.4387 0.7277 0.0544 0.0328 1.412 14.833 8.137 1052.979 1.676 36.194 3.505 0.46 242333. 0.3088
|
|
50.14 0.4645 0.7431 0.0502 0.0314 1.352 14.198 7.512 1007.840 1.604 33.413 3.381 0.46 242845. 0.2861
|
|
52.93 0.4903 0.7556 0.0460 0.0298 1.283 13.481 6.871 956.942 1.523 30.562 3.257 0.46 243380. 0.2636
|
|
55.71 0.5161 0.7649 0.0416 0.0281 1.207 12.682 6.216 900.271 1.433 27.650 3.132 0.46 243937. 0.2412
|
|
58.50 0.5419 0.7705 0.0371 0.0261 1.124 11.802 5.549 837.821 1.333 24.684 3.004 0.46 244516. 0.2186
|
|
61.28 0.5677 0.7714 0.0326 0.0240 1.032 10.841 4.872 769.604 1.225 21.670 2.871 0.46 245117. 0.1957
|
|
64.07 0.5935 0.7665 0.0280 0.0217 0.933 9.800 4.185 695.662 1.107 18.617 2.729 0.46 245741. 0.1724
|
|
66.85 0.6193 0.7535 0.0234 0.0192 0.826 8.679 3.492 616.078 0.981 15.532 2.571 0.46 246387. 0.1484
|
|
69.64 0.6451 0.7284 0.0187 0.0165 0.712 7.480 2.793 530.990 0.845 12.424 2.386 0.46 247055. 0.1231
|
|
72.43 0.6709 0.6837 0.0140 0.0137 0.591 6.207 2.092 440.613 0.701 9.304 2.153 0.46 247746. 0.0962
|
|
75.21 0.6967 0.6024 0.0093 0.0108 0.463 4.864 1.391 345.247 0.549 6.185 1.827 0.46 248458. 0.0665
|
|
78.00 0.7225 0.4379 0.0046 0.0076 0.329 3.455 0.692 245.272 0.390 3.080 1.281 0.46 249190. 0.0329
|
|
80.78 0.7483 -0.0080 0.0000 0.0044 0.188 1.971 -0.007 139.919 0.223 -0.031 -0.023 0.46 249885. 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 0.1005 0.0339 2.314 20.838 20.461 1725.747 2.354 91.011 5.378 0.53 276309. 0.7512
|
|
3.25 0.0258 0.0742 0.0993 0.0345 2.360 21.254 20.203 1760.216 2.401 89.862 5.206 0.53 276506. 0.7226
|
|
6.51 0.0517 0.1437 0.0979 0.0352 2.405 21.656 19.917 1793.529 2.447 88.591 5.037 0.53 276723. 0.6942
|
|
9.76 0.0775 0.2084 0.0963 0.0358 2.447 22.037 19.602 1825.036 2.490 87.188 4.872 0.53 276960. 0.6661
|
|
13.01 0.1033 0.2687 0.0946 0.0364 2.486 22.388 19.255 1854.102 2.529 85.645 4.710 0.53 277218. 0.6383
|
|
16.26 0.1291 0.3247 0.0927 0.0369 2.521 22.701 18.874 1880.030 2.565 83.951 4.553 0.53 277497. 0.6109
|
|
19.52 0.1550 0.3766 0.0907 0.0373 2.551 22.967 18.458 1902.094 2.595 82.099 4.401 0.53 277799. 0.5840
|
|
22.77 0.1808 0.4247 0.0885 0.0377 2.574 23.178 18.003 1919.532 2.619 80.080 4.254 0.53 278124. 0.5574
|
|
26.02 0.2066 0.4691 0.0860 0.0379 2.590 23.323 17.510 1931.551 2.635 77.884 4.112 0.53 278472. 0.5313
|
|
29.28 0.2324 0.5101 0.0834 0.0380 2.598 23.392 16.975 1937.325 2.643 75.505 3.974 0.53 278845. 0.5057
|
|
32.53 0.2583 0.5478 0.0806 0.0380 2.596 23.377 16.398 1936.029 2.641 72.936 3.842 0.53 279242. 0.4804
|
|
35.78 0.2841 0.5825 0.0775 0.0378 2.584 23.266 15.776 1926.865 2.629 70.173 3.714 0.53 279664. 0.4555
|
|
39.03 0.3099 0.6144 0.0743 0.0375 2.560 23.052 15.111 1909.140 2.604 67.215 3.590 0.53 280110. 0.4310
|
|
42.29 0.3358 0.6434 0.0708 0.0369 2.524 22.729 14.404 1882.377 2.568 64.070 3.471 0.53 280582. 0.4068
|
|
45.54 0.3616 0.6699 0.0671 0.0362 2.476 22.294 13.659 1846.364 2.519 60.755 3.355 0.53 281080. 0.3830
|
|
48.79 0.3874 0.6938 0.0633 0.0353 2.415 21.747 12.879 1801.054 2.457 57.286 3.243 0.53 281602. 0.3595
|
|
52.05 0.4132 0.7152 0.0593 0.0343 2.342 21.088 12.069 1746.439 2.382 53.681 3.134 0.53 282151. 0.3363
|
|
55.30 0.4391 0.7340 0.0552 0.0330 2.256 20.316 11.231 1682.521 2.295 49.954 3.028 0.53 282725. 0.3133
|
|
58.55 0.4649 0.7501 0.0509 0.0316 2.158 19.432 10.368 1609.284 2.195 46.119 2.922 0.53 283324. 0.2906
|
|
61.80 0.4907 0.7634 0.0466 0.0300 2.047 18.434 9.484 1526.703 2.083 42.186 2.818 0.53 283950. 0.2680
|
|
65.06 0.5165 0.7737 0.0422 0.0282 1.924 17.324 8.581 1434.756 1.957 38.167 2.713 0.53 284601. 0.2454
|
|
68.31 0.5424 0.7803 0.0376 0.0262 1.788 16.101 7.660 1333.435 1.819 34.071 2.606 0.54 285278. 0.2227
|
|
71.56 0.5682 0.7825 0.0330 0.0240 1.640 14.764 6.724 1222.761 1.668 29.910 2.494 0.54 285982. 0.1997
|
|
74.82 0.5940 0.7792 0.0284 0.0216 1.479 13.316 5.776 1102.802 1.504 25.692 2.376 0.54 286711. 0.1763
|
|
78.07 0.6198 0.7681 0.0237 0.0191 1.306 11.757 4.818 973.692 1.328 21.429 2.244 0.54 287467. 0.1521
|
|
81.32 0.6457 0.7454 0.0189 0.0164 1.121 10.090 3.852 835.659 1.140 17.134 2.091 0.54 288248. 0.1267
|
|
84.57 0.6715 0.7035 0.0142 0.0135 0.924 8.320 2.883 689.050 0.940 12.822 1.898 0.54 289056. 0.0995
|
|
87.83 0.6973 0.6253 0.0094 0.0105 0.717 6.452 1.913 534.357 0.729 8.510 1.624 0.54 289888. 0.0694
|
|
91.08 0.7232 0.4612 0.0047 0.0073 0.499 4.494 0.948 372.202 0.508 4.216 1.155 0.54 290744. 0.0347
|
|
94.33 0.7490 -0.0209 -0.0001 0.0039 0.269 2.424 -0.022 200.763 0.274 -0.100 -0.051 0.54 291535. 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 0.1017 0.0342 3.490 27.495 27.040 2602.397 3.106 120.273 4.713 0.60 315750. 0.7568
|
|
3.75 0.0260 0.0749 0.1005 0.0349 3.562 28.063 26.708 2656.138 3.171 118.798 4.561 0.60 315978. 0.7279
|
|
7.49 0.0521 0.1449 0.0991 0.0356 3.632 28.612 26.339 2708.083 3.233 117.157 4.412 0.60 316228. 0.6992
|
|
11.24 0.0781 0.2102 0.0976 0.0362 3.697 29.131 25.930 2757.216 3.291 115.337 4.266 0.60 316502. 0.6708
|
|
14.99 0.1041 0.2709 0.0959 0.0368 3.758 29.609 25.478 2802.500 3.345 113.325 4.123 0.60 316801. 0.6428
|
|
18.73 0.1301 0.3273 0.0940 0.0374 3.812 30.035 24.979 2842.839 3.393 111.108 3.985 0.60 317124. 0.6151
|
|
22.48 0.1562 0.3796 0.0919 0.0378 3.858 30.397 24.432 2877.085 3.434 108.672 3.852 0.60 317474. 0.5879
|
|
26.23 0.1822 0.4280 0.0897 0.0382 3.894 30.682 23.832 2904.033 3.466 106.007 3.722 0.60 317851. 0.5612
|
|
29.97 0.2082 0.4727 0.0872 0.0384 3.919 30.876 23.179 2922.437 3.488 103.100 3.597 0.60 318256. 0.5349
|
|
33.72 0.2343 0.5140 0.0845 0.0385 3.931 30.967 22.469 2931.015 3.499 99.941 3.477 0.60 318689. 0.5090
|
|
37.47 0.2603 0.5520 0.0816 0.0385 3.927 30.940 21.700 2928.477 3.496 96.522 3.361 0.60 319150. 0.4835
|
|
41.21 0.2863 0.5871 0.0785 0.0383 3.907 30.783 20.872 2913.596 3.478 92.837 3.249 0.61 319640. 0.4584
|
|
44.96 0.3124 0.6192 0.0752 0.0379 3.869 30.484 19.983 2885.299 3.444 88.886 3.141 0.61 320159. 0.4337
|
|
48.71 0.3384 0.6486 0.0716 0.0374 3.812 30.036 19.038 2842.880 3.393 84.681 3.037 0.61 320707. 0.4093
|
|
52.45 0.3644 0.6754 0.0679 0.0366 3.736 29.435 18.040 2786.043 3.326 80.244 2.937 0.61 321284. 0.3852
|
|
56.20 0.3904 0.6996 0.0639 0.0357 3.641 28.682 16.996 2714.731 3.240 75.598 2.840 0.61 321891. 0.3615
|
|
59.95 0.4165 0.7214 0.0599 0.0346 3.525 27.776 15.910 2628.958 3.138 70.768 2.745 0.61 322528. 0.3381
|
|
63.69 0.4425 0.7406 0.0556 0.0332 3.391 26.717 14.787 2528.735 3.018 65.773 2.652 0.61 323194. 0.3150
|
|
67.44 0.4685 0.7572 0.0513 0.0317 3.237 25.505 13.631 2414.054 2.882 60.631 2.561 0.61 323890. 0.2920
|
|
71.19 0.4946 0.7710 0.0468 0.0300 3.064 24.140 12.445 2284.877 2.727 55.358 2.471 0.61 324616. 0.2692
|
|
74.93 0.5206 0.7817 0.0423 0.0281 2.871 22.622 11.234 2141.183 2.556 49.967 2.380 0.61 325372. 0.2463
|
|
78.68 0.5466 0.7889 0.0376 0.0261 2.659 20.951 9.999 1982.962 2.367 44.474 2.287 0.61 326158. 0.2233
|
|
82.43 0.5726 0.7916 0.0329 0.0238 2.428 19.126 8.744 1810.261 2.161 38.891 2.191 0.61 326974. 0.2001
|
|
86.17 0.5987 0.7887 0.0281 0.0213 2.177 17.150 7.471 1623.200 1.938 33.233 2.088 0.61 327821. 0.1762
|
|
89.92 0.6247 0.7778 0.0233 0.0187 1.907 15.024 6.186 1422.008 1.697 27.515 1.973 0.61 328697. 0.1516
|
|
93.67 0.6507 0.7547 0.0184 0.0159 1.619 12.753 4.891 1207.067 1.441 21.755 1.838 0.62 329603. 0.1255
|
|
97.41 0.6768 0.7106 0.0135 0.0129 1.313 10.343 3.591 978.962 1.169 15.974 1.664 0.62 330540. 0.0974
|
|
101.16 0.7028 0.6243 0.0086 0.0097 0.990 7.803 2.292 738.510 0.882 10.195 1.408 0.62 331505. 0.0658
|
|
104.91 0.7288 0.4283 0.0038 0.0064 0.653 5.142 0.999 486.686 0.581 4.445 0.931 0.62 332495. 0.0288
|
|
108.65 0.7549
|
|
|
|
|
|
|
|
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 0.1031 0.0348 5.057 35.412 34.691 3770.723 4.001 154.304 4.173 0.68 355177. 0.7590
|
|
4.21 0.0260 0.0745 0.1019 0.0355 5.161 36.145 34.288 3848.719 4.084 152.512 4.041 0.68 355432. 0.7307
|
|
8.41 0.0520 0.1442 0.1006 0.0362 5.263 36.855 33.836 3924.338 4.164 150.504 3.911 0.68 355714. 0.7025
|
|
12.62 0.0779 0.2093 0.0991 0.0369 5.359 37.529 33.333 3996.081 4.240 148.263 3.783 0.68 356022. 0.6746
|
|
16.83 0.1039 0.2699 0.0974 0.0375 5.448 38.152 32.772 4062.455 4.310 145.772 3.659 0.68 356357. 0.6469
|
|
21.03 0.1299 0.3262 0.0956 0.0381 5.527 38.709 32.152 4121.809 4.373 143.012 3.538 0.68 356722. 0.6196
|
|
25.24 0.1559 0.3785 0.0935 0.0385 5.595 39.185 31.467 4172.438 4.427 139.966 3.421 0.68 357116. 0.5926
|
|
29.45 0.1818 0.4269 0.0913 0.0389 5.649 39.562 30.715 4212.542 4.470 136.618 3.307 0.68 357541. 0.5660
|
|
33.65 0.2078 0.4717 0.0889 0.0391 5.686 39.822 29.891 4240.235 4.499 132.954 3.197 0.68 357996. 0.5398
|
|
37.86 0.2338 0.5131 0.0862 0.0393 5.704 39.947 28.993 4253.604 4.513 128.960 3.092 0.68 358484. 0.5141
|
|
42.06 0.2598 0.5513 0.0833 0.0392 5.700 39.920 28.018 4250.737 4.510 124.625 2.990 0.68 359003. 0.4887
|
|
46.27 0.2857 0.5865 0.0802 0.0390 5.672 39.724 26.965 4229.813 4.488 119.940 2.892 0.68 359555. 0.4637
|
|
50.48 0.3117 0.6189 0.0768 0.0387 5.618 39.343 25.833 4189.268 4.445 114.907 2.797 0.68 360139. 0.4390
|
|
54.68 0.3377 0.6487 0.0732 0.0381 5.536 38.768 24.627 4128.044 4.380 109.540 2.706 0.68 360756. 0.4147
|
|
58.89 0.3637 0.6759 0.0694 0.0374 5.425 37.995 23.351 4045.702 4.293 103.866 2.618 0.68 361406. 0.3907
|
|
63.10 0.3896 0.7006 0.0654 0.0364 5.287 37.023 22.014 3942.183 4.183 97.917 2.533 0.68 362089. 0.3670
|
|
67.30 0.4156 0.7229 0.0613 0.0352 5.119 35.852 20.621 3817.536 4.051 91.724 2.450 0.68 362804. 0.3436
|
|
71.51 0.4416 0.7428 0.0570 0.0339 4.924 34.483 19.180 3671.816 3.896 85.314 2.369 0.68 363553. 0.3204
|
|
75.72 0.4676 0.7601 0.0526 0.0324 4.700 32.917 17.696 3505.029 3.719 78.710 2.290 0.69 364336. 0.2975
|
|
79.92 0.4936 0.7748 0.0481 0.0306 4.448 31.153 16.172 3317.150 3.520 71.932 2.211 0.69 365151. 0.2746
|
|
84.13 0.5195 0.7865 0.0434 0.0287 4.168 29.190 14.613 3108.147 3.298 65.000 2.133 0.69 366000. 0.2518
|
|
88.34 0.5455 0.7949 0.0387 0.0266 3.859 27.029 13.024 2878.015 3.054 57.930 2.053 0.69 366883. 0.2288
|
|
92.54 0.5715 0.7991 0.0339 0.0243 3.523 24.670 11.408 2626.826 2.787 50.741 1.970 0.69 367799. 0.2055
|
|
96.75 0.5975 0.7981 0.0290 0.0217 3.158 22.114 9.768 2354.746 2.498 43.450 1.882 0.69 368749. 0.1816
|
|
100.95 0.6234 0.7896 0.0241 0.0190 2.765 19.366 8.111 2062.095 2.188 36.077 1.784 0.69 369732. 0.1569
|
|
105.16 0.6494 0.7698 0.0191 0.0162 2.346 16.430 6.440 1749.426 1.856 28.646 1.670 0.69 370749. 0.1309
|
|
109.37 0.6754 0.7305 0.0142 0.0131 1.901 13.313 4.762 1417.599 1.504 21.181 1.524 0.69 371799. 0.1027
|
|
113.57 0.7014 0.6521 0.0092 0.0099 1.432 10.029 3.083 1067.859 1.133 13.714 1.310 0.69 372882. 0.0710
|
|
117.78 0.7273 0.4711 0.0042 0.0065 0.941 6.591 1.412 701.784 0.745 6.279 0.912 0.70 373992. 0.0335
|
|
121.99 0.7533
|
|
|
|
|
|
|
|
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 0.1047 0.0365 7.279 45.875 43.486 5427.605 5.183 193.425 3.634 0.75 394584. 0.7401
|
|
4.65 0.0258 0.0720 0.1036 0.0372 7.411 46.713 43.021 5526.649 5.278 191.356 3.531 0.75 394866. 0.7152
|
|
9.30 0.0517 0.1398 0.1023 0.0378 7.539 47.517 42.494 5621.863 5.368 189.015 3.428 0.75 395177. 0.6902
|
|
13.95 0.0775 0.2035 0.1009 0.0384 7.659 48.274 41.902 5711.355 5.454 186.378 3.328 0.75 395518. 0.6652
|
|
18.60 0.1034 0.2633 0.0993 0.0390 7.769 48.966 41.237 5793.232 5.532 183.422 3.229 0.75 395889. 0.6403
|
|
23.25 0.1292 0.3192 0.0975 0.0395 7.866 49.577 40.495 5865.493 5.601 180.122 3.131 0.75 396293. 0.6154
|
|
27.90 0.1551 0.3714 0.0955 0.0399 7.947 50.088 39.671 5926.028 5.659 176.456 3.036 0.75 396729. 0.5906
|
|
32.55 0.1809 0.4201 0.0933 0.0402 8.009 50.482 38.760 5972.584 5.703 172.402 2.943 0.75 397200. 0.5659
|
|
37.21 0.2068 0.4653 0.0909 0.0404 8.050 50.737 37.757 6002.810 5.732 167.942 2.853 0.76 397705. 0.5414
|
|
41.86 0.2326 0.5073 0.0883 0.0405 8.065 50.834 36.658 6014.210 5.743 163.057 2.765 0.76 398245. 0.5169
|
|
46.51 0.2585 0.5462 0.0854 0.0404 8.052 50.749 35.461 6004.230 5.734 157.732 2.679 0.76 398821. 0.4926
|
|
51.16 0.2843 0.5821 0.0823 0.0402 8.006 50.463 34.163 5970.375 5.701 151.957 2.595 0.76 399432. 0.4685
|
|
55.81 0.3102 0.6152 0.0789 0.0398 7.926 49.956 32.764 5910.388 5.644 145.733 2.514 0.76 400079. 0.4445
|
|
60.46 0.3360 0.6456 0.0753 0.0392 7.808 49.214 31.267 5822.594 5.560 139.076 2.436 0.76 400762. 0.4206
|
|
65.11 0.3619 0.6734 0.0715 0.0384 7.652 48.230 29.681 5706.129 5.449 132.020 2.359 0.76 401482. 0.3969
|
|
69.76 0.3877 0.6988 0.0675 0.0374 7.457 47.000 28.014 5560.688 5.310 124.606 2.285 0.76 402237. 0.3735
|
|
74.41 0.4136 0.7218 0.0633 0.0362 7.223 45.525 26.276 5386.148 5.143 116.873 2.213 0.76 403029. 0.3503
|
|
79.06 0.4394 0.7424 0.0589 0.0349 6.950 43.803 24.473 5182.398 4.949 108.858 2.142 0.76 403857. 0.3272
|
|
83.71 0.4653 0.7606 0.0545 0.0333 6.637 41.833 22.615 4949.312 4.726 100.590 2.072 0.76 404721. 0.3044
|
|
88.36 0.4911 0.7762 0.0499 0.0315 6.285 39.614 20.705 4686.785 4.476 92.097 2.004 0.76 405622. 0.2816
|
|
93.01 0.5170 0.7891 0.0451 0.0296 5.893 37.146 18.750 4394.776 4.197 83.401 1.935 0.76 406560. 0.2588
|
|
97.66 0.5428 0.7988 0.0403 0.0274 5.462 34.429 16.755 4073.354 3.890 74.525 1.866 0.76 407534. 0.2358
|
|
102.31 0.5687 0.8046 0.0355 0.0251 4.992 31.465 14.723 3722.710 3.555 65.490 1.794 0.77 408545. 0.2126
|
|
106.97 0.5945 0.8055 0.0305 0.0225 4.483 28.258 12.661 3343.285 3.193 56.318 1.718 0.77 409593. 0.1888
|
|
111.62 0.6204 0.7994 0.0255 0.0198 3.937 24.815 10.574 2935.853 2.804 47.034 1.634 0.77 410677. 0.1641
|
|
116.27 0.6462 0.7825 0.0204 0.0168 3.355 21.144 8.468 2501.637 2.389 37.664 1.535 0.77 411798. 0.1380
|
|
120.92 0.6720 0.7474 0.0153 0.0137 2.739 17.263 6.349 2042.439 1.950 28.241 1.410 0.77 412956. 0.1097
|
|
125.57 0.6979 0.6762 0.0102 0.0105 2.093 13.192 4.227 1560.736 1.490 18.800 1.228 0.77 414149. 0.0780
|
|
130.22 0.7237 0.5155 0.0051 0.0071 1.421 8.957 2.110 1059.673 1.012 9.384 0.903 0.77 415374. 0.0405
|
|
134.87 0.7496 -0.0135 -0.0001 0.0036 0.715 4.508 -0.027 533.366 0.509 -0.120 -0.023 0.77 416481. 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 0.1064 0.0413 10.949 62.738 53.463 8164.961 7.088 237.804 2.970 0.83 433970. 0.6706
|
|
5.12 0.0259 0.0652 0.1054 0.0418 11.097 63.582 52.953 8274.705 7.183 235.536 2.903 0.83 434279. 0.6523
|
|
10.24 0.0517 0.1273 0.1042 0.0423 11.231 64.353 52.368 8375.107 7.271 232.933 2.836 0.83 434619. 0.6338
|
|
15.36 0.0776 0.1866 0.1029 0.0428 11.350 65.032 51.700 8463.444 7.347 229.961 2.771 0.83 434994. 0.6152
|
|
20.48 0.1035 0.2430 0.1014 0.0432 11.449 65.599 50.940 8537.268 7.411 226.583 2.706 0.83 435403. 0.5965
|
|
25.60 0.1294 0.2966 0.0997 0.0435 11.525 66.037 50.082 8594.252 7.461 222.764 2.643 0.83 435848. 0.5777
|
|
30.72 0.1552 0.3476 0.0977 0.0436 11.576 66.328 49.117 8632.179 7.494 218.474 2.581 0.83 436331. 0.5586
|
|
35.84 0.1811 0.3959 0.0956 0.0437 11.598 66.457 48.040 8648.890 7.508 213.683 2.519 0.83 436851. 0.5393
|
|
40.96 0.2070 0.4415 0.0932 0.0437 11.589 66.405 46.845 8642.173 7.502 208.367 2.459 0.83 437411. 0.5197
|
|
46.08 0.2328 0.4845 0.0906 0.0435 11.546 66.155 45.526 8609.667 7.474 202.501 2.398 0.83 438009. 0.4998
|
|
51.20 0.2587 0.5250 0.0877 0.0432 11.464 65.688 44.080 8548.862 7.421 196.067 2.339 0.83 438647. 0.4795
|
|
56.32 0.2846 0.5628 0.0846 0.0428 11.341 64.983 42.502 8457.101 7.342 189.051 2.279 0.83 439325. 0.4589
|
|
61.44 0.3104 0.5982 0.0812 0.0421 11.173 64.022 40.794 8331.979 7.233 181.451 2.221 0.83 440042. 0.4380
|
|
66.56 0.3363 0.6310 0.0775 0.0413 10.959 62.791 38.958 8171.763 7.094 173.286 2.162 0.83 440799. 0.4168
|
|
71.68 0.3622 0.6613 0.0736 0.0403 10.696 61.285 37.006 7975.785 6.924 164.601 2.104 0.83 441596. 0.3954
|
|
76.80 0.3881 0.6892 0.0695 0.0392 10.385 59.504 34.948 7744.029 6.723 155.448 2.047 0.84 442433. 0.3737
|
|
81.92 0.4139 0.7146 0.0653 0.0378 10.026 57.449 32.797 7476.540 6.491 145.879 1.990 0.84 443310. 0.3519
|
|
87.04 0.4398 0.7374 0.0608 0.0363 9.619 55.118 30.562 7173.181 6.227 135.941 1.932 0.84 444226. 0.3299
|
|
92.16 0.4657 0.7577 0.0562 0.0346 9.164 52.509 28.254 6833.616 5.932 125.674 1.875 0.84 445183. 0.3078
|
|
97.28 0.4915 0.7751 0.0515 0.0327 8.661 49.628 25.880 6458.775 5.607 115.112 1.817 0.84 446179. 0.2855
|
|
102.40 0.5174 0.7893 0.0467 0.0306 8.112 46.478 23.446 6048.801 5.251 104.286 1.758 0.84 447216. 0.2629
|
|
107.52 0.5433 0.7997 0.0417 0.0283 7.514 43.054 20.958 5603.119 4.864 93.223 1.697 0.84 448292. 0.2399
|
|
112.64 0.5692 0.8050 0.0367 0.0259 6.874 39.389 18.424 5126.237 4.450 81.949 1.630 0.84 449409. 0.2161
|
|
117.76 0.5950 0.8042 0.0315 0.0233 6.188 35.457 15.848 4614.502 4.006 70.492 1.558 0.84 450566. 0.1915
|
|
122.89 0.6209 0.7946 0.0263 0.0206 5.459 31.278 13.238 4070.673 3.534 58.882 1.475 0.85 451763. 0.1657
|
|
128.01 0.6468 0.7713 0.0211 0.0177 4.691 26.879 10.601 3498.068 3.037 47.152 1.375 0.85 453000. 0.1382
|
|
133.13 0.6726 0.7250 0.0158 0.0147 3.890 22.291 7.946 2900.978 2.518 35.342 1.242 0.85 454277. 0.1081
|
|
138.25 0.6985 0.6356 0.0105 0.0116 3.064 17.556 5.283 2284.726 1.983 23.499 1.049 0.85 455592. 0.0744
|
|
143.37 0.7244 0.4520 0.0052 0.0084 2.220 12.720 2.625 1655.408 1.437 11.676 0.719 0.85 456943. 0.0360
|
|
148.49 0.7502 -0.0161 -0.0001 0.0051 1.349 7.728 -0.055 1005.749 0.873 -0.244 -0.025 0.85 458186. 0.0000
|
|
|
|
|
|
|