686 lines
122 KiB
Plaintext
686 lines
122 KiB
Plaintext
13x4.5EP (13x45EP.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 0.0680 0.0272 0.001 0.050 0.061 0.594 0.006 0.271 46.533 0.05 16698. 0.5205
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0.20 0.0165 0.0404 0.0666 0.0272 0.001 0.050 0.060 0.595 0.006 0.265 45.510 0.05 16706. 0.5037
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0.40 0.0330 0.0789 0.0651 0.0272 0.001 0.050 0.058 0.595 0.006 0.259 44.470 0.05 16713. 0.4866
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0.61 0.0495 0.1155 0.0635 0.0272 0.001 0.050 0.057 0.594 0.006 0.253 43.414 0.05 16721. 0.4693
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0.81 0.0660 0.1502 0.0619 0.0272 0.001 0.050 0.055 0.594 0.006 0.247 42.343 0.05 16730. 0.4517
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1.01 0.0825 0.1829 0.0601 0.0271 0.001 0.050 0.054 0.593 0.006 0.240 41.255 0.05 16738. 0.4340
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1.21 0.0990 0.2136 0.0584 0.0270 0.001 0.050 0.052 0.591 0.006 0.233 40.149 0.05 16748. 0.4160
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1.42 0.1155 0.2422 0.0565 0.0269 0.001 0.050 0.051 0.588 0.006 0.225 39.023 0.05 16758. 0.3979
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1.62 0.1320 0.2687 0.0546 0.0268 0.001 0.049 0.049 0.586 0.006 0.217 37.876 0.05 16768. 0.3795
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1.82 0.1485 0.2930 0.0526 0.0266 0.001 0.049 0.047 0.582 0.006 0.209 36.706 0.05 16779. 0.3609
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2.02 0.1650 0.3149 0.0505 0.0264 0.001 0.049 0.045 0.578 0.006 0.201 35.510 0.05 16790. 0.3422
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2.23 0.1815 0.3344 0.0483 0.0262 0.001 0.048 0.043 0.573 0.005 0.193 34.284 0.05 16802. 0.3232
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2.43 0.1979 0.3515 0.0461 0.0259 0.001 0.048 0.041 0.567 0.005 0.184 33.026 0.05 16814. 0.3040
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2.63 0.2144 0.3658 0.0437 0.0256 0.001 0.047 0.039 0.560 0.005 0.174 31.730 0.05 16827. 0.2846
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2.83 0.2309 0.3773 0.0413 0.0253 0.001 0.047 0.037 0.553 0.005 0.165 30.392 0.05 16840. 0.2651
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3.03 0.2474 0.3859 0.0389 0.0249 0.001 0.046 0.035 0.545 0.005 0.155 29.010 0.05 16854. 0.2454
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3.24 0.2639 0.3913 0.0364 0.0245 0.001 0.045 0.033 0.536 0.005 0.145 27.576 0.05 16869. 0.2256
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3.44 0.2804 0.3933 0.0338 0.0241 0.001 0.044 0.030 0.526 0.005 0.135 26.085 0.05 16884. 0.2056
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3.64 0.2969 0.3916 0.0311 0.0236 0.001 0.044 0.028 0.516 0.005 0.124 24.531 0.05 16900. 0.1857
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3.84 0.3134 0.3859 0.0284 0.0231 0.001 0.043 0.025 0.505 0.005 0.113 22.906 0.05 16916. 0.1657
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4.05 0.3299 0.3760 0.0257 0.0226 0.001 0.042 0.023 0.493 0.005 0.102 21.200 0.05 16933. 0.1458
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4.25 0.3464 0.3614 0.0229 0.0220 0.001 0.041 0.021 0.480 0.005 0.091 19.404 0.05 16951. 0.1260
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4.45 0.3629 0.3415 0.0201 0.0214 0.001 0.039 0.018 0.467 0.004 0.080 17.506 0.05 16969. 0.1065
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4.65 0.3794 0.3160 0.0172 0.0207 0.001 0.038 0.015 0.452 0.004 0.069 15.494 0.05 16988. 0.0873
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4.85 0.3959 0.2842 0.0144 0.0200 0.001 0.037 0.013 0.437 0.004 0.057 13.353 0.05 17007. 0.0687
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5.06 0.4124 0.2453 0.0115 0.0193 0.001 0.036 0.010 0.422 0.004 0.046 11.065 0.05 17027. 0.0509
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5.26 0.4289 0.1986 0.0086 0.0186 0.001 0.034 0.008 0.405 0.004 0.034 8.614 0.05 17048. 0.0342
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5.46 0.4454 0.1431 0.0057 0.0178 0.001 0.033 0.005 0.388 0.004 0.023 5.976 0.05 17069. 0.0194
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5.66 0.4619 0.0777 0.0029 0.0170 0.000 0.031 0.003 0.371 0.004 0.011 3.128 0.05 17091. 0.0072
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5.87 0.4784 0.0006 0.0000 0.0161 0.000 0.030 0.000 0.353 0.003 0.000 0.024 0.05 17114. 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 0.0682 0.0239 0.006 0.177 0.245 4.184 0.020 1.088 26.517 0.10 33397. 0.5943
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0.41 0.0166 0.0463 0.0668 0.0240 0.006 0.177 0.239 4.192 0.020 1.065 25.912 0.10 33411. 0.5746
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0.81 0.0332 0.0903 0.0653 0.0240 0.006 0.177 0.234 4.196 0.020 1.041 25.302 0.10 33426. 0.5547
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1.22 0.0498 0.1322 0.0637 0.0240 0.006 0.177 0.228 4.196 0.020 1.016 24.687 0.10 33443. 0.5346
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1.63 0.0664 0.1719 0.0621 0.0240 0.006 0.177 0.222 4.193 0.020 0.990 24.069 0.10 33460. 0.5144
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2.04 0.0830 0.2093 0.0603 0.0239 0.006 0.177 0.216 4.185 0.020 0.962 23.445 0.10 33477. 0.4941
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2.44 0.0996 0.2444 0.0585 0.0239 0.006 0.176 0.210 4.172 0.020 0.934 22.817 0.10 33496. 0.4736
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2.85 0.1162 0.2772 0.0567 0.0238 0.006 0.176 0.203 4.154 0.020 0.904 22.183 0.10 33516. 0.4530
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3.26 0.1328 0.3076 0.0547 0.0236 0.006 0.175 0.196 4.131 0.020 0.873 21.541 0.10 33537. 0.4323
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3.66 0.1494 0.3357 0.0527 0.0235 0.005 0.173 0.189 4.101 0.020 0.840 20.892 0.10 33558. 0.4115
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4.07 0.1660 0.3612 0.0506 0.0233 0.005 0.172 0.181 4.066 0.019 0.807 20.234 0.10 33581. 0.3905
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4.48 0.1826 0.3842 0.0484 0.0230 0.005 0.170 0.174 4.024 0.019 0.772 19.564 0.10 33605. 0.3693
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4.89 0.1992 0.4045 0.0462 0.0227 0.005 0.168 0.165 3.975 0.019 0.736 18.881 0.10 33630. 0.3480
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5.29 0.2158 0.4220 0.0438 0.0224 0.005 0.166 0.157 3.918 0.019 0.699 18.182 0.10 33656. 0.3265
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5.70 0.2324 0.4365 0.0414 0.0221 0.005 0.163 0.148 3.855 0.018 0.660 17.465 0.10 33683. 0.3049
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6.11 0.2491 0.4479 0.0389 0.0216 0.005 0.160 0.140 3.785 0.018 0.621 16.727 0.10 33711. 0.2831
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6.52 0.2657 0.4560 0.0364 0.0212 0.005 0.157 0.130 3.707 0.018 0.580 15.963 0.10 33741. 0.2613
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6.92 0.2823 0.4604 0.0338 0.0207 0.005 0.153 0.121 3.622 0.017 0.539 15.171 0.10 33772. 0.2393
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7.33 0.2989 0.4610 0.0311 0.0202 0.005 0.149 0.112 3.530 0.017 0.497 14.345 0.10 33803. 0.2172
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7.74 0.3155 0.4572 0.0284 0.0196 0.005 0.145 0.102 3.431 0.016 0.453 13.480 0.10 33836. 0.1950
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8.14 0.3321 0.4487 0.0257 0.0190 0.004 0.140 0.092 3.324 0.016 0.410 12.567 0.10 33871. 0.1728
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8.55 0.3487 0.4349 0.0229 0.0184 0.004 0.136 0.082 3.209 0.015 0.365 11.601 0.10 33906. 0.1506
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8.96 0.3653 0.4151 0.0201 0.0177 0.004 0.130 0.072 3.088 0.015 0.320 10.569 0.10 33943. 0.1285
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9.37 0.3819 0.3884 0.0172 0.0169 0.004 0.125 0.062 2.959 0.014 0.274 9.460 0.10 33981. 0.1065
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9.77 0.3985 0.3539 0.0143 0.0161 0.004 0.119 0.051 2.823 0.013 0.229 8.260 0.10 34020. 0.0849
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10.18 0.4151 0.3102 0.0115 0.0153 0.004 0.113 0.041 2.680 0.013 0.183 6.950 0.10 34061. 0.0638
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10.59 0.4317 0.2556 0.0086 0.0145 0.003 0.107 0.031 2.530 0.012 0.137 5.507 0.10 34103. 0.0437
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10.99 0.4483 0.1882 0.0057 0.0136 0.003 0.100 0.020 2.375 0.011 0.091 3.904 0.10 34146. 0.0253
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11.40 0.4649 0.1050 0.0029 0.0127 0.003 0.094 0.010 2.214 0.011 0.046 2.101 0.10 34191. 0.0096
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11.81 0.4815 0.0017 0.0000 0.0117 0.003 0.087 0.000 2.048 0.010 0.001 0.034 0.10 34235. 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 0.0684 0.0225 0.018 0.374 0.552 13.289 0.042 2.455 18.840 0.15 50095. 0.6343
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0.63 0.0171 0.0507 0.0670 0.0226 0.018 0.375 0.540 13.319 0.042 2.402 18.391 0.15 50117. 0.6124
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1.26 0.0342 0.0989 0.0654 0.0226 0.018 0.376 0.527 13.337 0.042 2.346 17.940 0.15 50141. 0.5904
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1.89 0.0513 0.1446 0.0638 0.0226 0.018 0.376 0.514 13.341 0.042 2.288 17.487 0.15 50166. 0.5683
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2.52 0.0684 0.1878 0.0621 0.0226 0.018 0.376 0.501 13.329 0.042 2.226 17.033 0.15 50192. 0.5460
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3.14 0.0855 0.2285 0.0603 0.0225 0.018 0.375 0.486 13.302 0.042 2.162 16.577 0.15 50220. 0.5237
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3.77 0.1026 0.2666 0.0584 0.0225 0.018 0.373 0.471 13.256 0.042 2.096 16.120 0.15 50249. 0.5013
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4.40 0.1197 0.3022 0.0565 0.0224 0.018 0.372 0.455 13.191 0.042 2.026 15.660 0.15 50280. 0.4789
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5.03 0.1367 0.3352 0.0544 0.0222 0.018 0.369 0.439 13.106 0.042 1.953 15.197 0.15 50312. 0.4563
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5.66 0.1538 0.3655 0.0523 0.0220 0.017 0.366 0.422 12.998 0.041 1.878 14.730 0.15 50346. 0.4336
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6.29 0.1709 0.3931 0.0501 0.0218 0.017 0.362 0.404 12.866 0.041 1.799 14.259 0.15 50382. 0.4109
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6.92 0.1880 0.4179 0.0479 0.0215 0.017 0.358 0.386 12.709 0.040 1.717 13.780 0.15 50419. 0.3880
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7.55 0.2051 0.4398 0.0455 0.0212 0.017 0.353 0.367 12.526 0.040 1.633 13.294 0.15 50459. 0.3650
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8.18 0.2222 0.4586 0.0431 0.0209 0.017 0.347 0.347 12.316 0.039 1.546 12.797 0.15 50499. 0.3418
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8.80 0.2393 0.4743 0.0406 0.0205 0.016 0.340 0.327 12.080 0.038 1.456 12.288 0.15 50542. 0.3185
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9.43 0.2564 0.4865 0.0380 0.0200 0.016 0.333 0.306 11.816 0.038 1.363 11.765 0.15 50586. 0.2951
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10.06 0.2735 0.4951 0.0354 0.0195 0.015 0.325 0.285 11.524 0.037 1.268 11.224 0.15 50633. 0.2716
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10.69 0.2906 0.4997 0.0327 0.0190 0.015 0.316 0.263 11.205 0.036 1.172 10.661 0.15 50681. 0.2479
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11.32 0.3077 0.4999 0.0299 0.0184 0.015 0.306 0.241 10.857 0.035 1.073 10.073 0.15 50731. 0.2241
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11.95 0.3248 0.4952 0.0271 0.0178 0.014 0.295 0.218 10.482 0.033 0.972 9.454 0.15 50783. 0.2002
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12.58 0.3419 0.4850 0.0242 0.0171 0.014 0.284 0.195 10.078 0.032 0.869 8.797 0.16 50837. 0.1762
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13.21 0.3590 0.4686 0.0213 0.0163 0.013 0.272 0.172 9.645 0.031 0.766 8.094 0.16 50893. 0.1521
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13.83 0.3761 0.4448 0.0184 0.0156 0.012 0.259 0.149 9.185 0.029 0.661 7.334 0.16 50951. 0.1281
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14.46 0.3932 0.4125 0.0155 0.0147 0.012 0.245 0.125 8.697 0.028 0.555 6.505 0.16 51011. 0.1041
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15.09 0.4102 0.3699 0.0125 0.0139 0.011 0.231 0.101 8.182 0.026 0.449 5.590 0.16 51074. 0.0804
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15.72 0.4273 0.3147 0.0095 0.0130 0.010 0.215 0.077 7.643 0.024 0.342 4.566 0.16 51138. 0.0574
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16.35 0.4444 0.2441 0.0066 0.0120 0.009 0.199 0.053 7.080 0.023 0.236 3.405 0.16 51204. 0.0356
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16.98 0.4615 0.1538 0.0037 0.0110 0.009 0.183 0.030 6.496 0.021 0.132 2.066 0.16 51272. 0.0161
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17.61 0.4786 0.0372 0.0008 0.0100 0.008 0.166 0.006 5.891 0.019 0.028 0.482 0.16 51341. 0.0017
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18.24 0.4957
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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 0.0687 0.0217 0.041 0.642 0.984 30.370 0.073 4.379 14.702 0.21 66792. 0.6610
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0.82 0.0167 0.0516 0.0672 0.0218 0.041 0.643 0.964 30.445 0.073 4.286 14.356 0.21 66821. 0.6386
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1.64 0.0334 0.1007 0.0657 0.0218 0.041 0.644 0.942 30.491 0.073 4.189 14.009 0.21 66852. 0.6160
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2.46 0.0502 0.1474 0.0641 0.0218 0.041 0.645 0.919 30.506 0.073 4.087 13.663 0.21 66885. 0.5934
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3.28 0.0669 0.1915 0.0624 0.0218 0.041 0.644 0.895 30.486 0.073 3.981 13.316 0.21 66919. 0.5708
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4.10 0.0836 0.2331 0.0607 0.0218 0.041 0.643 0.870 30.428 0.073 3.870 12.969 0.21 66955. 0.5481
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4.92 0.1003 0.2723 0.0589 0.0217 0.041 0.641 0.844 30.329 0.072 3.754 12.621 0.21 66993. 0.5254
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5.74 0.1170 0.3089 0.0570 0.0216 0.040 0.638 0.817 30.185 0.072 3.633 12.273 0.21 67033. 0.5026
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6.56 0.1338 0.3430 0.0550 0.0214 0.040 0.634 0.789 29.994 0.072 3.507 11.924 0.21 67075. 0.4798
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7.38 0.1505 0.3745 0.0529 0.0213 0.040 0.629 0.759 29.751 0.071 3.377 11.573 0.21 67119. 0.4569
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8.20 0.1672 0.4034 0.0508 0.0211 0.039 0.622 0.729 29.453 0.070 3.241 11.220 0.21 67165. 0.4340
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9.02 0.1839 0.4297 0.0486 0.0208 0.039 0.615 0.697 29.098 0.069 3.100 10.863 0.21 67213. 0.4109
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9.84 0.2006 0.4531 0.0463 0.0205 0.038 0.606 0.664 28.682 0.068 2.954 10.502 0.21 67264. 0.3878
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10.66 0.2174 0.4737 0.0440 0.0202 0.038 0.596 0.630 28.204 0.067 2.803 10.135 0.21 67316. 0.3646
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11.48 0.2341 0.4913 0.0415 0.0198 0.037 0.585 0.595 27.662 0.066 2.648 9.761 0.21 67371. 0.3412
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12.30 0.2508 0.5057 0.0390 0.0193 0.036 0.572 0.559 27.056 0.065 2.488 9.377 0.21 67429. 0.3178
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13.12 0.2675 0.5167 0.0364 0.0189 0.035 0.558 0.523 26.386 0.063 2.324 8.982 0.21 67488. 0.2942
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13.94 0.2842 0.5241 0.0338 0.0183 0.034 0.542 0.485 25.651 0.061 2.157 8.574 0.21 67550. 0.2705
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14.76 0.3010 0.5274 0.0311 0.0178 0.033 0.525 0.446 24.850 0.059 1.986 8.149 0.21 67615. 0.2467
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15.58 0.3177 0.5262 0.0284 0.0171 0.032 0.507 0.407 23.982 0.057 1.812 7.703 0.21 67682. 0.2228
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16.40 0.3344 0.5201 0.0256 0.0165 0.031 0.487 0.367 23.046 0.055 1.634 7.232 0.21 67751. 0.1986
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17.22 0.3511 0.5081 0.0228 0.0158 0.030 0.466 0.327 22.044 0.053 1.455 6.730 0.21 67823. 0.1744
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18.04 0.3678 0.4896 0.0200 0.0150 0.028 0.443 0.286 20.975 0.050 1.273 6.189 0.21 67897. 0.1500
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18.86 0.3846 0.4631 0.0171 0.0142 0.027 0.419 0.245 19.841 0.047 1.090 5.600 0.21 67975. 0.1256
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19.68 0.4013 0.4272 0.0142 0.0133 0.025 0.394 0.203 18.643 0.045 0.905 4.951 0.21 68054. 0.1012
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20.50 0.4180 0.3798 0.0113 0.0124 0.023 0.367 0.162 17.383 0.041 0.720 4.225 0.21 68137. 0.0770
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21.32 0.4347 0.3178 0.0084 0.0115 0.022 0.340 0.120 16.067 0.038 0.536 3.400 0.21 68222. 0.0535
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22.14 0.4514 0.2373 0.0055 0.0105 0.020 0.311 0.079 14.697 0.035 0.352 2.444 0.21 68309. 0.0312
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22.96 0.4682 0.1321 0.0027 0.0095 0.018 0.281 0.038 13.280 0.032 0.171 1.312 0.21 68399. 0.0117
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23.78 0.4849 -0.0092 -0.0002 0.0084 0.016 0.249 -0.002 11.800 0.028 -0.010 -0.088 0.21 68486. 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 0.0689 0.0212 0.078 0.979 1.544 57.912 0.111 6.867 12.092 0.26 83489. 0.6808
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1.04 0.0170 0.0538 0.0674 0.0213 0.078 0.982 1.511 58.065 0.111 6.720 11.801 0.26 83526. 0.6573
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2.08 0.0339 0.1049 0.0659 0.0213 0.078 0.983 1.476 58.160 0.111 6.565 11.511 0.26 83565. 0.6337
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3.12 0.0509 0.1534 0.0643 0.0213 0.078 0.984 1.440 58.190 0.111 6.403 11.221 0.26 83606. 0.6101
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4.16 0.0678 0.1993 0.0626 0.0213 0.078 0.983 1.402 58.150 0.111 6.234 10.932 0.26 83650. 0.5864
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5.20 0.0848 0.2425 0.0608 0.0212 0.078 0.981 1.362 58.031 0.111 6.057 10.643 0.26 83696. 0.5628
|
|
6.24 0.1017 0.2831 0.0589 0.0212 0.078 0.978 1.320 57.828 0.110 5.872 10.355 0.26 83745. 0.5391
|
|
7.28 0.1187 0.3211 0.0570 0.0211 0.077 0.973 1.277 57.533 0.110 5.680 10.067 0.26 83796. 0.5154
|
|
8.32 0.1356 0.3565 0.0550 0.0209 0.077 0.966 1.232 57.138 0.109 5.479 9.778 0.26 83849. 0.4917
|
|
9.36 0.1526 0.3892 0.0529 0.0207 0.076 0.957 1.185 56.638 0.108 5.270 9.488 0.26 83905. 0.4680
|
|
10.40 0.1695 0.4192 0.0507 0.0205 0.075 0.947 1.136 56.026 0.107 5.053 9.198 0.26 83964. 0.4442
|
|
11.43 0.1865 0.4464 0.0485 0.0202 0.074 0.935 1.086 55.294 0.106 4.828 8.904 0.26 84026. 0.4204
|
|
12.47 0.2034 0.4707 0.0461 0.0199 0.073 0.920 1.033 54.437 0.104 4.595 8.608 0.26 84090. 0.3964
|
|
13.51 0.2204 0.4921 0.0437 0.0196 0.072 0.904 0.979 53.450 0.102 4.354 8.307 0.26 84157. 0.3724
|
|
14.55 0.2374 0.5104 0.0412 0.0192 0.070 0.885 0.923 52.333 0.100 4.106 8.000 0.26 84228. 0.3483
|
|
15.59 0.2543 0.5255 0.0386 0.0187 0.069 0.864 0.866 51.085 0.098 3.851 7.687 0.26 84301. 0.3241
|
|
16.63 0.2713 0.5370 0.0360 0.0182 0.067 0.840 0.807 49.703 0.095 3.589 7.364 0.26 84377. 0.2997
|
|
17.67 0.2882 0.5446 0.0333 0.0176 0.065 0.815 0.747 48.186 0.092 3.322 7.030 0.26 84456. 0.2753
|
|
18.71 0.3052 0.5481 0.0306 0.0170 0.062 0.787 0.685 46.533 0.089 3.049 6.682 0.26 84539. 0.2507
|
|
19.75 0.3221 0.5469 0.0278 0.0164 0.060 0.756 0.623 44.741 0.085 2.771 6.316 0.26 84625. 0.2259
|
|
20.79 0.3391 0.5403 0.0250 0.0157 0.057 0.724 0.560 42.810 0.082 2.489 5.928 0.26 84713. 0.2009
|
|
21.83 0.3560 0.5275 0.0221 0.0149 0.055 0.689 0.495 40.741 0.078 2.202 5.512 0.26 84806. 0.1758
|
|
22.87 0.3730 0.5075 0.0192 0.0141 0.052 0.651 0.430 38.535 0.074 1.913 5.062 0.26 84901. 0.1504
|
|
23.91 0.3899 0.4787 0.0163 0.0133 0.049 0.612 0.364 36.195 0.069 1.621 4.567 0.26 85000. 0.1249
|
|
24.95 0.4069 0.4391 0.0133 0.0123 0.045 0.570 0.299 33.724 0.064 1.328 4.015 0.26 85102. 0.0994
|
|
25.99 0.4239 0.3860 0.0104 0.0114 0.042 0.526 0.233 31.130 0.059 1.034 3.388 0.26 85208. 0.0740
|
|
27.03 0.4408 0.3154 0.0074 0.0104 0.038 0.480 0.167 28.420 0.054 0.742 2.662 0.26 85317. 0.0493
|
|
28.07 0.4578 0.2215 0.0045 0.0094 0.034 0.433 0.102 25.606 0.049 0.452 1.800 0.26 85429. 0.0260
|
|
29.11 0.4747 0.0949 0.0017 0.0083 0.030 0.384 0.037 22.694 0.043 0.165 0.743 0.26 85543. 0.0065
|
|
30.15 0.4917
|
|
|
|
|
|
|
|
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 0.0692 0.0209 0.132 1.387 2.233 98.473 0.157 9.931 10.284 0.31 100185. 0.6963
|
|
1.23 0.0167 0.0541 0.0677 0.0209 0.132 1.391 2.186 98.738 0.157 9.722 10.040 0.31 100228. 0.6726
|
|
2.46 0.0334 0.1056 0.0662 0.0210 0.133 1.393 2.136 98.905 0.157 9.502 9.796 0.31 100275. 0.6488
|
|
3.69 0.0501 0.1545 0.0646 0.0210 0.133 1.394 2.084 98.962 0.158 9.271 9.553 0.31 100324. 0.6249
|
|
4.92 0.0669 0.2008 0.0629 0.0210 0.133 1.393 2.030 98.899 0.157 9.030 9.311 0.31 100376. 0.6011
|
|
6.15 0.0836 0.2445 0.0612 0.0209 0.132 1.390 1.974 98.703 0.157 8.779 9.070 0.31 100430. 0.5773
|
|
7.38 0.1003 0.2856 0.0593 0.0208 0.132 1.386 1.915 98.363 0.157 8.516 8.829 0.31 100487. 0.5536
|
|
8.61 0.1170 0.3241 0.0574 0.0207 0.131 1.379 1.853 97.867 0.156 8.243 8.589 0.31 100547. 0.5298
|
|
9.84 0.1337 0.3601 0.0555 0.0206 0.130 1.369 1.789 97.204 0.155 7.958 8.348 0.31 100610. 0.5060
|
|
11.07 0.1504 0.3934 0.0534 0.0204 0.129 1.357 1.723 96.361 0.153 7.662 8.108 0.31 100677. 0.4822
|
|
12.30 0.1672 0.4242 0.0513 0.0202 0.128 1.343 1.653 95.327 0.152 7.354 7.867 0.31 100746. 0.4584
|
|
13.53 0.1839 0.4522 0.0490 0.0199 0.126 1.325 1.582 94.092 0.150 7.035 7.625 0.31 100818. 0.4345
|
|
14.76 0.2006 0.4775 0.0467 0.0196 0.124 1.305 1.507 92.642 0.147 6.705 7.380 0.31 100894. 0.4106
|
|
15.99 0.2173 0.5000 0.0443 0.0193 0.122 1.282 1.431 90.973 0.145 6.363 7.133 0.31 100973. 0.3866
|
|
17.22 0.2340 0.5194 0.0419 0.0189 0.119 1.255 1.352 89.080 0.142 6.012 6.881 0.31 101056. 0.3625
|
|
18.45 0.2507 0.5358 0.0394 0.0184 0.117 1.225 1.270 86.963 0.138 5.650 6.625 0.31 101142. 0.3383
|
|
19.68 0.2674 0.5488 0.0368 0.0179 0.113 1.192 1.187 84.617 0.135 5.279 6.362 0.31 101231. 0.3141
|
|
20.91 0.2842 0.5583 0.0341 0.0174 0.110 1.156 1.102 82.040 0.131 4.900 6.091 0.31 101324. 0.2897
|
|
22.14 0.3009 0.5637 0.0315 0.0168 0.106 1.116 1.015 79.229 0.126 4.513 5.809 0.31 101421. 0.2651
|
|
23.37 0.3176 0.5648 0.0287 0.0161 0.102 1.073 0.926 76.181 0.121 4.119 5.513 0.31 101521. 0.2404
|
|
24.60 0.3343 0.5609 0.0259 0.0154 0.098 1.027 0.836 72.895 0.116 3.718 5.201 0.31 101625. 0.2155
|
|
25.83 0.3510 0.5512 0.0231 0.0147 0.093 0.977 0.745 69.372 0.110 3.312 4.868 0.31 101733. 0.1903
|
|
27.06 0.3677 0.5347 0.0202 0.0139 0.088 0.924 0.652 65.612 0.104 2.901 4.508 0.31 101845. 0.1649
|
|
28.29 0.3845 0.5101 0.0173 0.0131 0.083 0.868 0.559 61.619 0.098 2.486 4.114 0.31 101961. 0.1393
|
|
29.52 0.4012 0.4755 0.0144 0.0122 0.077 0.809 0.465 57.400 0.091 2.069 3.675 0.31 102080. 0.1135
|
|
30.75 0.4179 0.4283 0.0115 0.0112 0.071 0.746 0.371 52.964 0.084 1.650 3.178 0.31 102204. 0.0877
|
|
31.98 0.4346 0.3648 0.0086 0.0102 0.065 0.681 0.277 48.326 0.077 1.233 2.602 0.31 102332. 0.0621
|
|
33.21 0.4513 0.2794 0.0057 0.0092 0.058 0.613 0.184 43.501 0.069 0.819 1.920 0.31 102463. 0.0373
|
|
34.44 0.4680 0.1635 0.0029 0.0082 0.052 0.542 0.092 38.508 0.061 0.409 1.083 0.31 102598. 0.0149
|
|
35.67 0.4847 -0.0002 0.0000 0.0071 0.045 0.469 0.000 33.293 0.053 0.000 -0.001 0.31 102727. 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 0.0696 0.0206 0.207 1.868 3.054 154.725 0.211 13.586 8.954 0.36 116879. 0.7091
|
|
1.45 0.0169 0.0555 0.0681 0.0207 0.208 1.873 2.989 155.150 0.212 13.297 8.739 0.36 116931. 0.6846
|
|
2.90 0.0337 0.1083 0.0665 0.0207 0.208 1.877 2.921 155.415 0.212 12.993 8.525 0.36 116986. 0.6602
|
|
4.35 0.0506 0.1583 0.0649 0.0207 0.209 1.878 2.849 155.499 0.212 12.674 8.311 0.36 117044. 0.6357
|
|
5.79 0.0675 0.2057 0.0632 0.0207 0.208 1.876 2.775 155.383 0.212 12.341 8.099 0.36 117105. 0.6113
|
|
7.24 0.0844 0.2504 0.0614 0.0207 0.208 1.872 2.696 155.050 0.212 11.993 7.888 0.36 117169. 0.5869
|
|
8.69 0.1012 0.2925 0.0595 0.0206 0.207 1.865 2.615 154.479 0.211 11.630 7.677 0.36 117237. 0.5625
|
|
10.14 0.1181 0.3319 0.0576 0.0205 0.206 1.855 2.530 153.650 0.210 11.252 7.467 0.36 117308. 0.5381
|
|
11.59 0.1350 0.3687 0.0556 0.0204 0.205 1.842 2.441 152.545 0.208 10.857 7.258 0.36 117383. 0.5138
|
|
13.04 0.1519 0.4028 0.0535 0.0202 0.203 1.825 2.349 151.143 0.206 10.447 7.048 0.36 117461. 0.4895
|
|
14.48 0.1687 0.4342 0.0513 0.0199 0.200 1.804 2.253 149.427 0.204 10.021 6.839 0.36 117543. 0.4651
|
|
15.93 0.1856 0.4630 0.0490 0.0197 0.198 1.780 2.154 147.377 0.201 9.579 6.628 0.36 117629. 0.4407
|
|
17.38 0.2025 0.4889 0.0467 0.0193 0.194 1.751 2.051 144.974 0.198 9.121 6.416 0.36 117719. 0.4163
|
|
18.83 0.2194 0.5119 0.0443 0.0190 0.191 1.717 1.944 142.207 0.194 8.648 6.201 0.36 117813. 0.3918
|
|
20.28 0.2362 0.5319 0.0418 0.0186 0.187 1.679 1.835 139.074 0.190 8.160 5.983 0.36 117911. 0.3672
|
|
21.73 0.2531 0.5487 0.0392 0.0181 0.182 1.637 1.722 135.570 0.185 7.659 5.761 0.36 118013. 0.3426
|
|
23.18 0.2700 0.5622 0.0366 0.0176 0.177 1.590 1.607 131.688 0.180 7.146 5.533 0.36 118119. 0.3178
|
|
24.62 0.2869 0.5719 0.0339 0.0170 0.171 1.539 1.488 127.425 0.174 6.621 5.298 0.36 118229. 0.2929
|
|
26.07 0.3037 0.5776 0.0312 0.0164 0.165 1.482 1.368 122.775 0.167 6.085 5.054 0.36 118344. 0.2678
|
|
27.52 0.3206 0.5788 0.0284 0.0157 0.158 1.422 1.245 117.734 0.161 5.539 4.797 0.36 118463. 0.2426
|
|
28.97 0.3375 0.5747 0.0255 0.0150 0.151 1.356 1.120 112.301 0.153 4.984 4.526 0.36 118586. 0.2171
|
|
30.42 0.3543 0.5647 0.0226 0.0142 0.143 1.286 0.994 106.476 0.145 4.422 4.234 0.36 118714. 0.1913
|
|
31.87 0.3712 0.5474 0.0197 0.0134 0.134 1.211 0.866 100.263 0.137 3.853 3.919 0.36 118847. 0.1652
|
|
33.31 0.3881 0.5214 0.0168 0.0125 0.126 1.131 0.737 93.668 0.128 3.279 3.570 0.36 118984. 0.1389
|
|
34.76 0.4050 0.4845 0.0138 0.0116 0.116 1.047 0.608 86.702 0.118 2.703 3.179 0.36 119126. 0.1123
|
|
36.21 0.4218 0.4336 0.0109 0.0106 0.106 0.959 0.478 79.385 0.108 2.126 2.731 0.36 119273. 0.0856
|
|
37.66 0.4387 0.3640 0.0079 0.0096 0.096 0.866 0.349 71.740 0.098 1.551 2.205 0.36 119424. 0.0590
|
|
39.11 0.4556 0.2688 0.0050 0.0085 0.086 0.770 0.221 63.797 0.087 0.981 1.568 0.36 119580. 0.0334
|
|
40.56 0.4725 0.1360 0.0021 0.0074 0.075 0.671 0.094 55.578 0.076 0.417 0.765 0.36 119739. 0.0106
|
|
42.00 0.4893
|
|
|
|
|
|
|
|
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 0.0700 0.0205 0.308 2.425 4.013 229.503 0.274 17.850 7.931 0.41 133572. 0.7199
|
|
1.64 0.0167 0.0557 0.0685 0.0206 0.309 2.431 3.928 230.129 0.275 17.473 7.742 0.41 133631. 0.6953
|
|
3.28 0.0334 0.1086 0.0669 0.0206 0.309 2.435 3.839 230.515 0.275 17.078 7.555 0.41 133694. 0.6707
|
|
4.92 0.0502 0.1589 0.0653 0.0206 0.309 2.437 3.746 230.633 0.275 16.664 7.368 0.41 133759. 0.6462
|
|
6.56 0.0669 0.2065 0.0636 0.0206 0.309 2.435 3.649 230.456 0.275 16.231 7.182 0.41 133829. 0.6216
|
|
8.20 0.0836 0.2515 0.0619 0.0206 0.308 2.430 3.547 229.955 0.274 15.779 6.997 0.41 133902. 0.5972
|
|
9.84 0.1003 0.2939 0.0600 0.0205 0.307 2.421 3.441 229.101 0.273 15.308 6.813 0.41 133978. 0.5727
|
|
11.48 0.1170 0.3337 0.0581 0.0204 0.306 2.407 3.331 227.866 0.272 14.816 6.630 0.41 134059. 0.5483
|
|
13.12 0.1337 0.3709 0.0561 0.0202 0.303 2.390 3.216 226.221 0.270 14.304 6.448 0.41 134143. 0.5239
|
|
14.76 0.1505 0.4054 0.0540 0.0200 0.301 2.368 3.096 224.139 0.268 13.772 6.266 0.41 134232. 0.4996
|
|
16.40 0.1672 0.4374 0.0518 0.0198 0.297 2.341 2.972 221.590 0.265 13.219 6.083 0.41 134325. 0.4752
|
|
18.04 0.1839 0.4667 0.0496 0.0195 0.293 2.309 2.843 218.548 0.261 12.646 5.901 0.41 134422. 0.4508
|
|
19.68 0.2006 0.4932 0.0472 0.0192 0.288 2.271 2.710 214.984 0.257 12.052 5.717 0.41 134523. 0.4264
|
|
21.32 0.2173 0.5170 0.0448 0.0188 0.283 2.228 2.572 210.880 0.252 11.438 5.531 0.41 134629. 0.4019
|
|
22.96 0.2340 0.5378 0.0424 0.0184 0.277 2.179 2.429 206.231 0.246 10.806 5.343 0.41 134739. 0.3774
|
|
24.60 0.2508 0.5556 0.0398 0.0180 0.270 2.124 2.283 201.030 0.240 10.156 5.152 0.41 134854. 0.3527
|
|
26.24 0.2675 0.5701 0.0372 0.0175 0.262 2.063 2.134 195.269 0.233 9.490 4.956 0.41 134974. 0.3280
|
|
27.88 0.2842 0.5811 0.0345 0.0169 0.253 1.996 1.980 188.940 0.226 8.809 4.754 0.41 135098. 0.3031
|
|
29.52 0.3009 0.5882 0.0318 0.0163 0.244 1.923 1.824 182.037 0.217 8.113 4.545 0.41 135227. 0.2781
|
|
31.16 0.3176 0.5909 0.0290 0.0156 0.234 1.844 1.665 174.552 0.208 7.405 4.326 0.41 135361. 0.2529
|
|
32.80 0.3343 0.5888 0.0262 0.0149 0.223 1.759 1.503 166.484 0.199 6.685 4.095 0.41 135500. 0.2274
|
|
34.44 0.3511 0.5809 0.0233 0.0141 0.212 1.668 1.339 157.832 0.188 5.955 3.847 0.41 135644. 0.2017
|
|
36.08 0.3678 0.5662 0.0204 0.0133 0.199 1.570 1.173 148.599 0.177 5.216 3.579 0.41 135794. 0.1756
|
|
37.72 0.3845 0.5432 0.0175 0.0124 0.186 1.466 1.005 138.795 0.166 4.471 3.285 0.41 135948. 0.1492
|
|
39.36 0.4012 0.5099 0.0146 0.0115 0.172 1.357 0.837 128.437 0.153 3.722 2.955 0.41 136107. 0.1225
|
|
41.00 0.4179 0.4632 0.0116 0.0105 0.158 1.242 0.668 117.547 0.140 2.971 2.577 0.41 136272. 0.0954
|
|
42.64 0.4346 0.3989 0.0087 0.0095 0.142 1.122 0.499 106.161 0.127 2.222 2.134 0.41 136442. 0.0683
|
|
44.28 0.4514 0.3101 0.0058 0.0084 0.126 0.997 0.332 94.320 0.113 1.478 1.597 0.42 136618. 0.0417
|
|
45.92 0.4681 0.1855 0.0029 0.0073 0.110 0.867 0.167 82.067 0.098 0.742 0.922 0.42 136797. 0.0171
|
|
47.56 0.4848 0.0017 0.0000 0.0062 0.093 0.732 0.001 69.252 0.083 0.005 0.008 0.42 136969. 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 0.0704 0.0205 0.437 3.060 5.113 325.865 0.346 22.744 7.117 0.46 150264. 0.7292
|
|
1.85 0.0167 0.0563 0.0690 0.0205 0.438 3.069 5.005 326.743 0.347 22.263 6.948 0.46 150331. 0.7043
|
|
3.70 0.0335 0.1099 0.0674 0.0205 0.439 3.074 4.892 327.272 0.347 21.759 6.780 0.46 150401. 0.6794
|
|
5.55 0.0502 0.1607 0.0658 0.0206 0.439 3.075 4.773 327.410 0.347 21.230 6.612 0.46 150475. 0.6546
|
|
7.39 0.0670 0.2089 0.0640 0.0205 0.439 3.072 4.649 327.119 0.347 20.678 6.446 0.46 150554. 0.6297
|
|
9.24 0.0837 0.2545 0.0623 0.0205 0.438 3.065 4.519 326.358 0.346 20.101 6.281 0.46 150636. 0.6050
|
|
11.09 0.1005 0.2974 0.0604 0.0204 0.436 3.053 4.384 325.084 0.345 19.498 6.116 0.46 150723. 0.5802
|
|
12.94 0.1172 0.3377 0.0584 0.0203 0.433 3.036 4.242 323.257 0.343 18.870 5.953 0.46 150814. 0.5556
|
|
14.79 0.1340 0.3753 0.0564 0.0201 0.430 3.013 4.095 320.835 0.340 18.217 5.790 0.46 150910. 0.5309
|
|
16.64 0.1507 0.4104 0.0543 0.0199 0.426 2.984 3.943 317.776 0.337 17.537 5.627 0.46 151010. 0.5063
|
|
18.48 0.1675 0.4429 0.0521 0.0197 0.421 2.949 3.784 314.042 0.333 16.831 5.465 0.46 151115. 0.4817
|
|
20.33 0.1842 0.4727 0.0499 0.0194 0.415 2.907 3.619 309.591 0.328 16.099 5.302 0.46 151225. 0.4571
|
|
22.18 0.2010 0.4997 0.0475 0.0191 0.408 2.859 3.449 304.382 0.323 15.340 5.139 0.46 151339. 0.4324
|
|
24.03 0.2177 0.5240 0.0451 0.0187 0.400 2.802 3.272 298.391 0.317 14.555 4.974 0.46 151459. 0.4077
|
|
25.88 0.2345 0.5454 0.0426 0.0183 0.391 2.739 3.091 291.607 0.309 13.747 4.807 0.46 151583. 0.3829
|
|
27.73 0.2512 0.5637 0.0400 0.0178 0.381 2.667 2.904 284.023 0.301 12.917 4.638 0.46 151713. 0.3581
|
|
29.58 0.2680 0.5788 0.0374 0.0173 0.370 2.589 2.713 275.627 0.292 12.066 4.464 0.46 151848. 0.3331
|
|
31.42 0.2847 0.5903 0.0347 0.0167 0.357 2.502 2.517 266.406 0.283 11.196 4.285 0.46 151989. 0.3081
|
|
33.27 0.3015 0.5980 0.0319 0.0161 0.344 2.407 2.317 256.351 0.272 10.307 4.100 0.46 152135. 0.2828
|
|
35.12 0.3182 0.6014 0.0291 0.0154 0.329 2.305 2.114 245.452 0.260 9.402 3.906 0.46 152286. 0.2573
|
|
36.97 0.3350 0.5998 0.0263 0.0147 0.313 2.195 1.907 233.707 0.248 8.482 3.701 0.46 152443. 0.2316
|
|
38.82 0.3517 0.5925 0.0234 0.0139 0.297 2.077 1.697 221.113 0.235 7.550 3.482 0.47 152606. 0.2055
|
|
40.67 0.3685 0.5783 0.0205 0.0130 0.279 1.950 1.485 207.678 0.220 6.606 3.244 0.47 152774. 0.1791
|
|
42.51 0.3852 0.5556 0.0175 0.0121 0.259 1.816 1.271 193.417 0.205 5.654 2.981 0.47 152949. 0.1523
|
|
44.36 0.4020 0.5223 0.0145 0.0112 0.239 1.675 1.056 178.351 0.189 4.698 2.686 0.47 153129. 0.1251
|
|
46.21 0.4187 0.4753 0.0116 0.0102 0.218 1.526 0.841 162.518 0.172 3.739 2.346 0.47 153315. 0.0975
|
|
48.06 0.4355 0.4096 0.0086 0.0092 0.196 1.371 0.626 145.967 0.155 2.783 1.944 0.47 153507. 0.0697
|
|
49.91 0.4522 0.3176 0.0057 0.0081 0.173 1.209 0.412 128.762 0.137 1.833 1.452 0.47 153705. 0.0422
|
|
51.76 0.4690 0.1864 0.0028 0.0070 0.149 1.042 0.201 110.963 0.118 0.894 0.822 0.47 153908. 0.0167
|
|
53.60 0.4857 -0.0134 -0.0002 0.0058 0.124 0.866 -0.012 92.221 0.098 -0.052 -0.057 0.47 154094. 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 0.0710 0.0205 0.600 3.779 6.362 447.159 0.427 28.297 6.453 0.51 166953. 0.7375
|
|
2.08 0.0170 0.0574 0.0695 0.0205 0.601 3.790 6.226 448.344 0.428 27.691 6.298 0.51 167029. 0.7121
|
|
4.16 0.0339 0.1121 0.0679 0.0205 0.602 3.795 6.083 449.026 0.429 27.055 6.144 0.51 167109. 0.6866
|
|
6.24 0.0509 0.1639 0.0662 0.0206 0.602 3.796 5.933 449.150 0.429 26.388 5.991 0.51 167193. 0.6612
|
|
8.32 0.0678 0.2130 0.0645 0.0205 0.602 3.792 5.776 448.654 0.428 25.691 5.839 0.51 167282. 0.6359
|
|
10.40 0.0848 0.2594 0.0626 0.0205 0.600 3.782 5.612 447.482 0.427 24.962 5.688 0.51 167375. 0.6106
|
|
12.48 0.1018 0.3030 0.0607 0.0204 0.598 3.766 5.441 445.575 0.425 24.201 5.538 0.51 167473. 0.5854
|
|
14.56 0.1187 0.3440 0.0587 0.0203 0.594 3.743 5.262 442.870 0.423 23.407 5.389 0.51 167577. 0.5602
|
|
16.64 0.1357 0.3823 0.0566 0.0201 0.589 3.713 5.076 439.310 0.420 22.580 5.241 0.51 167685. 0.5351
|
|
18.72 0.1527 0.4180 0.0545 0.0199 0.583 3.675 4.883 434.835 0.415 21.719 5.093 0.51 167799. 0.5100
|
|
20.80 0.1696 0.4510 0.0522 0.0196 0.576 3.629 4.682 429.388 0.410 20.825 4.946 0.51 167918. 0.4849
|
|
22.88 0.1866 0.4813 0.0499 0.0194 0.567 3.575 4.473 422.911 0.404 19.898 4.798 0.51 168042. 0.4598
|
|
24.96 0.2035 0.5087 0.0475 0.0190 0.557 3.511 4.257 415.345 0.397 18.937 4.649 0.51 168172. 0.4347
|
|
27.04 0.2205 0.5334 0.0450 0.0186 0.545 3.437 4.034 406.658 0.388 17.943 4.499 0.51 168308. 0.4095
|
|
29.12 0.2375 0.5550 0.0424 0.0182 0.532 3.354 3.804 396.839 0.379 16.920 4.348 0.52 168450. 0.3842
|
|
31.20 0.2544 0.5736 0.0398 0.0177 0.517 3.261 3.568 385.874 0.368 15.868 4.193 0.52 168597. 0.3589
|
|
33.28 0.2714 0.5888 0.0371 0.0171 0.501 3.159 3.325 373.745 0.357 14.791 4.035 0.52 168750. 0.3334
|
|
35.36 0.2884 0.6003 0.0343 0.0165 0.483 3.046 3.077 360.436 0.344 13.689 3.873 0.52 168910. 0.3078
|
|
37.44 0.3053 0.6079 0.0315 0.0158 0.464 2.924 2.825 345.932 0.330 12.564 3.703 0.52 169076. 0.2820
|
|
39.52 0.3223 0.6109 0.0286 0.0151 0.443 2.791 2.567 330.223 0.315 11.418 3.526 0.52 169248. 0.2560
|
|
41.60 0.3392 0.6087 0.0257 0.0143 0.420 2.648 2.305 313.304 0.299 10.255 3.338 0.52 169426. 0.2296
|
|
43.68 0.3562 0.6004 0.0228 0.0135 0.396 2.495 2.040 295.176 0.282 9.075 3.135 0.52 169611. 0.2029
|
|
45.76 0.3732 0.5846 0.0198 0.0126 0.370 2.332 1.772 275.851 0.263 7.883 2.914 0.52 169803. 0.1758
|
|
47.84 0.3901 0.5595 0.0168 0.0117 0.342 2.158 1.502 255.355 0.244 6.681 2.668 0.52 170001. 0.1482
|
|
49.92 0.4071 0.5226 0.0137 0.0107 0.313 1.975 1.231 233.725 0.223 5.473 2.388 0.52 170206. 0.1200
|
|
52.00 0.4241 0.4699 0.0107 0.0097 0.283 1.784 0.959 211.020 0.202 4.265 2.061 0.52 170417. 0.0915
|
|
54.08 0.4410 0.3952 0.0077 0.0086 0.251 1.583 0.688 187.320 0.179 3.062 1.667 0.52 170636. 0.0627
|
|
56.16 0.4580 0.2884 0.0047 0.0074 0.218 1.375 0.420 162.721 0.155 1.869 1.171 0.52 170860. 0.0344
|
|
58.24 0.4749 0.1308 0.0017 0.0063 0.184 1.160 0.155 137.273 0.131 0.690 0.512 0.52 171089. 0.0091
|
|
60.32 0.4919
|
|
|
|
|
|
|
|
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 0.0716 0.0205 0.801 4.588 7.766 597.123 0.518 34.544 5.899 0.57 183640. 0.7449
|
|
2.30 0.0170 0.0579 0.0701 0.0206 0.803 4.600 7.599 598.646 0.520 33.802 5.758 0.57 183724. 0.7192
|
|
4.59 0.0340 0.1131 0.0685 0.0206 0.804 4.606 7.424 599.484 0.520 33.022 5.617 0.57 183813. 0.6935
|
|
6.89 0.0511 0.1654 0.0668 0.0206 0.804 4.607 7.240 599.552 0.520 32.205 5.477 0.57 183906. 0.6678
|
|
9.18 0.0681 0.2149 0.0650 0.0206 0.803 4.601 7.048 598.777 0.520 31.351 5.339 0.57 184005. 0.6423
|
|
11.48 0.0851 0.2617 0.0631 0.0205 0.801 4.588 6.847 597.077 0.518 30.457 5.202 0.57 184108. 0.6167
|
|
13.77 0.1021 0.3059 0.0612 0.0204 0.797 4.567 6.637 594.371 0.516 29.524 5.065 0.57 184217. 0.5913
|
|
16.07 0.1191 0.3473 0.0592 0.0203 0.792 4.538 6.419 590.578 0.513 28.550 4.930 0.57 184332. 0.5659
|
|
18.37 0.1361 0.3860 0.0571 0.0201 0.785 4.500 6.191 585.617 0.508 27.536 4.795 0.57 184452. 0.5406
|
|
20.66 0.1532 0.4221 0.0549 0.0199 0.777 4.452 5.953 579.407 0.503 26.481 4.660 0.57 184578. 0.5152
|
|
22.96 0.1702 0.4555 0.0526 0.0197 0.767 4.394 5.707 571.873 0.496 25.384 4.526 0.57 184710. 0.4899
|
|
25.25 0.1872 0.4862 0.0503 0.0194 0.755 4.326 5.451 562.934 0.489 24.247 4.392 0.57 184848. 0.4646
|
|
27.55 0.2042 0.5142 0.0478 0.0190 0.741 4.245 5.186 552.512 0.480 23.067 4.257 0.57 184992. 0.4393
|
|
29.84 0.2212 0.5392 0.0453 0.0186 0.725 4.154 4.912 540.565 0.469 21.848 4.121 0.57 185143. 0.4139
|
|
32.14 0.2383 0.5613 0.0427 0.0181 0.707 4.050 4.630 527.076 0.458 20.593 3.984 0.57 185300. 0.3884
|
|
34.44 0.2553 0.5803 0.0400 0.0176 0.687 3.934 4.340 512.027 0.444 19.303 3.844 0.57 185463. 0.3629
|
|
36.73 0.2723 0.5960 0.0373 0.0170 0.664 3.807 4.042 495.393 0.430 17.980 3.701 0.57 185633. 0.3372
|
|
39.03 0.2893 0.6080 0.0345 0.0164 0.640 3.666 3.738 477.155 0.414 16.628 3.554 0.57 185810. 0.3113
|
|
41.32 0.3063 0.6160 0.0316 0.0157 0.613 3.514 3.428 457.292 0.397 15.248 3.400 0.57 185993. 0.2853
|
|
43.62 0.3234 0.6194 0.0287 0.0150 0.584 3.349 3.112 435.789 0.378 13.843 3.239 0.57 186184. 0.2589
|
|
45.91 0.3404 0.6176 0.0257 0.0142 0.553 3.171 2.791 412.641 0.358 12.415 3.068 0.57 186381. 0.2323
|
|
48.21 0.3574 0.6095 0.0227 0.0133 0.520 2.980 2.466 387.852 0.337 10.969 2.884 0.57 186586. 0.2052
|
|
50.50 0.3744 0.5938 0.0197 0.0124 0.485 2.777 2.137 361.439 0.314 9.506 2.682 0.57 186798. 0.1777
|
|
52.80 0.3914 0.5686 0.0167 0.0115 0.447 2.562 1.806 333.436 0.289 8.032 2.456 0.57 187018. 0.1496
|
|
55.10 0.4084 0.5310 0.0136 0.0104 0.408 2.335 1.473 303.900 0.264 6.552 2.199 0.57 187244. 0.1209
|
|
57.39 0.4255 0.4768 0.0105 0.0094 0.366 2.097 1.140 272.912 0.237 5.072 1.895 0.57 187479. 0.0917
|
|
59.69 0.4425 0.3990 0.0075 0.0083 0.323 1.849 0.809 240.585 0.209 3.598 1.525 0.57 187720. 0.0621
|
|
61.98 0.4595 0.2860 0.0044 0.0071 0.278 1.591 0.480 207.050 0.180 2.137 1.052 0.57 187969. 0.0331
|
|
64.28 0.4765 0.1154 0.0014 0.0059 0.231 1.324 0.156 172.349 0.150 0.692 0.409 0.57 188221. 0.0073
|
|
66.57 0.4935
|
|
|
|
|
|
|
|
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 0.0723 0.0207 1.046 5.494 9.336 780.021 0.621 41.526 5.429 0.62 200324. 0.7516
|
|
2.50 0.0170 0.0580 0.0708 0.0207 1.049 5.507 9.136 781.897 0.622 40.637 5.300 0.62 200416. 0.7258
|
|
4.99 0.0339 0.1132 0.0692 0.0207 1.050 5.514 8.926 782.866 0.623 39.703 5.171 0.62 200513. 0.7001
|
|
7.49 0.0509 0.1656 0.0675 0.0207 1.050 5.514 8.706 782.826 0.623 38.725 5.044 0.62 200615. 0.6744
|
|
9.99 0.0679 0.2153 0.0657 0.0207 1.048 5.506 8.476 781.672 0.622 37.701 4.918 0.62 200723. 0.6488
|
|
12.48 0.0848 0.2623 0.0638 0.0206 1.045 5.489 8.235 779.302 0.620 36.631 4.793 0.62 200836. 0.6233
|
|
14.98 0.1018 0.3066 0.0619 0.0205 1.040 5.463 7.984 775.610 0.617 35.513 4.669 0.62 200955. 0.5978
|
|
17.47 0.1188 0.3482 0.0598 0.0204 1.033 5.427 7.722 770.490 0.613 34.347 4.546 0.62 201080. 0.5724
|
|
19.97 0.1357 0.3873 0.0577 0.0202 1.024 5.380 7.449 763.838 0.608 33.132 4.423 0.62 201211. 0.5470
|
|
22.47 0.1527 0.4237 0.0555 0.0200 1.013 5.322 7.165 755.553 0.601 31.869 4.301 0.62 201348. 0.5217
|
|
24.96 0.1696 0.4574 0.0532 0.0197 1.000 5.251 6.870 745.530 0.593 30.556 4.179 0.62 201492. 0.4963
|
|
27.46 0.1866 0.4885 0.0509 0.0194 0.984 5.168 6.563 733.670 0.584 29.194 4.058 0.62 201643. 0.4710
|
|
29.96 0.2036 0.5168 0.0484 0.0191 0.965 5.070 6.246 719.868 0.573 27.782 3.935 0.62 201800. 0.4456
|
|
32.45 0.2205 0.5424 0.0459 0.0186 0.944 4.959 5.918 704.069 0.560 26.322 3.812 0.62 201963. 0.4202
|
|
34.95 0.2375 0.5650 0.0432 0.0182 0.920 4.834 5.580 686.250 0.546 24.818 3.688 0.62 202134. 0.3947
|
|
37.45 0.2545 0.5846 0.0405 0.0176 0.894 4.694 5.232 666.387 0.530 23.273 3.561 0.62 202312. 0.3691
|
|
39.94 0.2714 0.6010 0.0378 0.0171 0.864 4.539 4.876 644.451 0.513 21.690 3.432 0.62 202497. 0.3434
|
|
42.44 0.2884 0.6137 0.0350 0.0164 0.832 4.370 4.512 620.414 0.494 20.070 3.299 0.62 202689. 0.3175
|
|
44.94 0.3054 0.6226 0.0321 0.0157 0.797 4.186 4.140 594.251 0.473 18.417 3.160 0.62 202888. 0.2914
|
|
47.43 0.3223 0.6269 0.0292 0.0150 0.759 3.986 3.762 565.944 0.450 16.734 3.015 0.62 203096. 0.2650
|
|
49.93 0.3393 0.6262 0.0262 0.0142 0.718 3.772 3.377 535.483 0.426 15.023 2.861 0.62 203310. 0.2382
|
|
52.42 0.3563 0.6193 0.0232 0.0133 0.674 3.542 2.988 502.874 0.400 13.289 2.695 0.62 203533. 0.2111
|
|
54.92 0.3732 0.6050 0.0201 0.0124 0.628 3.297 2.594 468.138 0.373 11.536 2.513 0.62 203763. 0.1834
|
|
57.42 0.3902 0.5814 0.0170 0.0114 0.578 3.038 2.196 431.320 0.343 9.769 2.310 0.62 204001. 0.1551
|
|
59.91 0.4072 0.5455 0.0139 0.0104 0.526 2.765 1.797 392.490 0.312 7.994 2.077 0.62 204247. 0.1262
|
|
62.41 0.4241 0.4932 0.0108 0.0093 0.472 2.478 1.398 351.753 0.280 6.218 1.803 0.62 204502. 0.0966
|
|
64.91 0.4411 0.4174 0.0078 0.0082 0.415 2.178 1.000 309.254 0.246 4.449 1.467 0.62 204764. 0.0665
|
|
67.40 0.4580 0.3062 0.0047 0.0070 0.356 1.868 0.606 265.167 0.211 2.695 1.036 0.62 205034. 0.0366
|
|
69.90 0.4750 0.1367 0.0017 0.0058 0.294 1.547 0.216 219.571 0.175 0.960 0.446 0.62 205308. 0.0094
|
|
72.40 0.4920
|
|
|
|
|
|
|
|
PROP RPM = 13000
|
|
|
|
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 0.0732 0.0208 1.342 6.507 11.083 1000.832 0.735 49.297 5.023 0.67 217005. 0.7577
|
|
2.68 0.0168 0.0577 0.0716 0.0209 1.345 6.522 10.848 1003.055 0.737 48.251 4.905 0.67 217104. 0.7320
|
|
5.37 0.0337 0.1127 0.0700 0.0209 1.347 6.528 10.601 1004.113 0.738 47.152 4.788 0.67 217209. 0.7064
|
|
8.05 0.0505 0.1649 0.0683 0.0209 1.346 6.527 10.342 1003.874 0.737 46.001 4.673 0.67 217319. 0.6809
|
|
10.73 0.0673 0.2145 0.0665 0.0209 1.344 6.516 10.071 1002.212 0.736 44.797 4.558 0.67 217435. 0.6554
|
|
13.42 0.0842 0.2614 0.0646 0.0208 1.340 6.495 9.788 998.996 0.734 43.538 4.444 0.67 217557. 0.6300
|
|
16.10 0.1010 0.3057 0.0627 0.0207 1.333 6.463 9.493 994.096 0.730 42.223 4.331 0.67 217686. 0.6046
|
|
18.78 0.1178 0.3474 0.0606 0.0206 1.324 6.420 9.184 987.376 0.725 40.852 4.219 0.67 217821. 0.5794
|
|
21.47 0.1347 0.3866 0.0585 0.0204 1.312 6.363 8.863 978.707 0.719 39.425 4.108 0.67 217962. 0.5541
|
|
24.15 0.1515 0.4232 0.0563 0.0202 1.298 6.293 8.530 967.961 0.711 37.939 3.997 0.67 218110. 0.5289
|
|
26.83 0.1683 0.4572 0.0540 0.0199 1.281 6.209 8.183 955.010 0.702 36.397 3.886 0.67 218264. 0.5037
|
|
29.52 0.1852 0.4886 0.0517 0.0196 1.260 6.110 7.823 939.729 0.690 34.796 3.776 0.67 218426. 0.4785
|
|
32.20 0.2020 0.5174 0.0492 0.0192 1.236 5.994 7.450 921.986 0.677 33.137 3.665 0.67 218595. 0.4533
|
|
34.88 0.2188 0.5434 0.0466 0.0188 1.209 5.863 7.064 901.704 0.662 31.422 3.553 0.67 218771. 0.4279
|
|
37.57 0.2357 0.5667 0.0440 0.0183 1.179 5.714 6.667 878.853 0.646 29.655 3.441 0.67 218954. 0.4026
|
|
40.25 0.2525 0.5870 0.0413 0.0178 1.144 5.549 6.259 853.405 0.627 27.839 3.326 0.67 219145. 0.3771
|
|
42.93 0.2693 0.6041 0.0386 0.0172 1.107 5.366 5.840 825.325 0.606 25.977 3.210 0.67 219343. 0.3515
|
|
45.62 0.2861 0.6178 0.0357 0.0166 1.066 5.166 5.412 794.579 0.584 24.073 3.089 0.67 219549. 0.3257
|
|
48.30 0.3030 0.6278 0.0328 0.0159 1.021 4.949 4.975 761.134 0.559 22.129 2.965 0.67 219763. 0.2996
|
|
50.98 0.3198 0.6335 0.0299 0.0151 0.972 4.714 4.530 724.967 0.533 20.149 2.834 0.67 219985. 0.2733
|
|
53.67 0.3366 0.6342 0.0269 0.0143 0.920 4.461 4.078 686.064 0.504 18.137 2.696 0.67 220215. 0.2467
|
|
56.35 0.3535 0.6292 0.0239 0.0134 0.864 4.190 3.619 644.432 0.473 16.097 2.547 0.67 220453. 0.2196
|
|
59.03 0.3703 0.6171 0.0208 0.0125 0.805 3.902 3.155 600.092 0.441 14.033 2.385 0.67 220699. 0.1919
|
|
61.72 0.3871 0.5962 0.0177 0.0115 0.742 3.596 2.687 553.097 0.406 11.952 2.203 0.67 220954. 0.1637
|
|
64.40 0.4040 0.5637 0.0146 0.0105 0.675 3.274 2.217 503.531 0.370 9.859 1.997 0.67 221217. 0.1347
|
|
67.08 0.4208 0.5157 0.0115 0.0094 0.606 2.936 1.746 451.522 0.332 7.764 1.753 0.67 221489. 0.1050
|
|
69.77 0.4376 0.4455 0.0084 0.0083 0.533 2.583 1.276 397.247 0.292 5.675 1.457 0.67 221769. 0.0746
|
|
72.45 0.4545 0.3421 0.0053 0.0071 0.457 2.217 0.810 340.931 0.250 3.601 1.077 0.67 222057. 0.0439
|
|
75.13 0.4713 0.1842 0.0023 0.0059 0.379 1.838 0.349 282.747 0.208 1.551 0.559 0.68 222352. 0.0150
|
|
77.82 0.4881
|
|
|
|
|
|
|
|
PROP RPM = 14000
|
|
|
|
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 0.0741 0.0211 1.697 7.641 13.023 1265.627 0.863 57.928 4.667 0.72 233681. 0.7632
|
|
2.86 0.0167 0.0572 0.0726 0.0211 1.701 7.656 12.750 1268.147 0.865 56.711 4.560 0.72 233787. 0.7378
|
|
5.73 0.0334 0.1118 0.0710 0.0212 1.702 7.663 12.462 1269.196 0.866 55.433 4.454 0.72 233900. 0.7124
|
|
8.59 0.0500 0.1637 0.0692 0.0212 1.701 7.659 12.162 1268.614 0.865 54.095 4.348 0.72 234018. 0.6871
|
|
11.45 0.0667 0.2130 0.0674 0.0211 1.698 7.645 11.847 1266.247 0.864 52.695 4.244 0.72 234143. 0.6618
|
|
14.31 0.0834 0.2598 0.0656 0.0210 1.692 7.619 11.518 1261.931 0.861 51.232 4.140 0.72 234274. 0.6366
|
|
17.18 0.1001 0.3040 0.0636 0.0209 1.684 7.580 11.175 1255.506 0.856 49.705 4.037 0.72 234411. 0.6115
|
|
20.04 0.1167 0.3457 0.0616 0.0208 1.672 7.527 10.817 1246.810 0.850 48.112 3.935 0.72 234556. 0.5864
|
|
22.90 0.1334 0.3849 0.0595 0.0206 1.657 7.460 10.444 1235.682 0.843 46.454 3.834 0.72 234707. 0.5614
|
|
25.77 0.1501 0.4216 0.0573 0.0204 1.639 7.377 10.056 1221.963 0.833 44.730 3.733 0.72 234865. 0.5363
|
|
28.63 0.1668 0.4558 0.0550 0.0201 1.617 7.278 9.654 1205.502 0.822 42.939 3.632 0.72 235030. 0.5113
|
|
31.49 0.1834 0.4876 0.0526 0.0198 1.591 7.161 9.236 1186.142 0.809 41.081 3.532 0.72 235203. 0.4863
|
|
34.35 0.2001 0.5167 0.0501 0.0194 1.561 7.026 8.803 1163.726 0.794 39.156 3.431 0.72 235382. 0.4613
|
|
37.22 0.2168 0.5433 0.0476 0.0190 1.526 6.871 8.355 1138.144 0.776 37.165 3.330 0.72 235570. 0.4361
|
|
40.08 0.2335 0.5671 0.0449 0.0185 1.488 6.698 7.894 1109.358 0.757 35.113 3.228 0.72 235765. 0.4109
|
|
42.94 0.2501 0.5881 0.0422 0.0180 1.445 6.504 7.420 1077.337 0.735 33.005 3.124 0.72 235968. 0.3856
|
|
45.80 0.2668 0.6061 0.0395 0.0174 1.397 6.291 6.934 1042.044 0.711 30.843 3.018 0.72 236179. 0.3601
|
|
48.67 0.2835 0.6208 0.0366 0.0167 1.346 6.058 6.437 1003.437 0.684 28.631 2.910 0.72 236398. 0.3345
|
|
51.53 0.3002 0.6319 0.0338 0.0160 1.289 5.805 5.929 961.484 0.656 26.373 2.797 0.72 236626. 0.3086
|
|
54.39 0.3168 0.6389 0.0308 0.0153 1.229 5.531 5.412 916.163 0.625 24.073 2.679 0.72 236861. 0.2824
|
|
57.26 0.3335 0.6413 0.0278 0.0145 1.163 5.237 4.886 867.464 0.592 21.734 2.555 0.72 237105. 0.2559
|
|
60.12 0.3502 0.6381 0.0248 0.0136 1.093 4.923 4.353 815.404 0.556 19.361 2.421 0.72 237358. 0.2289
|
|
62.98 0.3669 0.6283 0.0217 0.0127 1.019 4.588 3.813 760.023 0.518 16.960 2.276 0.72 237619. 0.2013
|
|
65.84 0.3835 0.6101 0.0186 0.0117 0.941 4.235 3.268 701.399 0.478 14.537 2.113 0.72 237890. 0.1731
|
|
68.71 0.4002 0.5810 0.0155 0.0107 0.858 3.862 2.720 639.654 0.436 12.100 1.929 0.72 238169. 0.1442
|
|
71.57 0.4169 0.5373 0.0124 0.0096 0.771 3.471 2.171 574.962 0.392 9.656 1.713 0.73 238457. 0.1143
|
|
74.43 0.4336 0.4731 0.0092 0.0085 0.681 3.064 1.622 507.564 0.346 7.216 1.450 0.73 238754. 0.0837
|
|
77.30 0.4502 0.3783 0.0061 0.0073 0.587 2.643 1.077 437.762 0.299 4.792 1.116 0.73 239060. 0.0525
|
|
80.16 0.4669 0.2344 0.0031 0.0061 0.491 2.209 0.538 365.856 0.250 2.393 0.667 0.73 239373. 0.0222
|
|
83.02 0.4836 -0.0025 0.0000 0.0048 0.390 1.754 -0.004 290.542 0.198 -0.020 -0.007 0.73 239663. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 15000
|
|
|
|
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 0.0753 0.0215 2.123 8.923 15.177 1583.464 1.008 67.508 4.347 0.77 250351. 0.7674
|
|
3.07 0.0167 0.0571 0.0737 0.0215 2.127 8.936 14.859 1585.765 1.010 66.092 4.250 0.77 250466. 0.7423
|
|
6.13 0.0333 0.1116 0.0720 0.0215 2.127 8.939 14.524 1586.298 1.010 64.604 4.153 0.77 250588. 0.7171
|
|
9.20 0.0500 0.1636 0.0703 0.0215 2.125 8.930 14.174 1584.853 1.009 63.046 4.056 0.77 250716. 0.6920
|
|
12.26 0.0667 0.2130 0.0685 0.0214 2.120 8.910 13.807 1581.217 1.007 61.415 3.961 0.77 250850. 0.6669
|
|
15.33 0.0833 0.2598 0.0666 0.0214 2.112 8.876 13.424 1575.179 1.003 59.711 3.866 0.77 250992. 0.6417
|
|
18.40 0.1000 0.3041 0.0646 0.0212 2.101 8.827 13.024 1566.522 0.997 57.932 3.771 0.77 251140. 0.6167
|
|
21.46 0.1167 0.3460 0.0625 0.0211 2.085 8.762 12.607 1555.024 0.990 56.077 3.677 0.77 251296. 0.5916
|
|
24.53 0.1334 0.3854 0.0604 0.0209 2.066 8.680 12.173 1540.483 0.981 54.145 3.584 0.77 251459. 0.5666
|
|
27.60 0.1500 0.4224 0.0581 0.0206 2.042 8.580 11.721 1522.695 0.969 52.135 3.491 0.77 251629. 0.5416
|
|
30.66 0.1667 0.4569 0.0558 0.0204 2.014 8.461 11.252 1501.472 0.956 50.048 3.399 0.77 251807. 0.5166
|
|
33.73 0.1834 0.4889 0.0534 0.0200 1.980 8.321 10.765 1476.633 0.940 47.882 3.307 0.77 251993. 0.4916
|
|
36.79 0.2000 0.5184 0.0509 0.0196 1.942 8.159 10.260 1447.989 0.922 45.638 3.214 0.77 252186. 0.4665
|
|
39.86 0.2167 0.5453 0.0483 0.0192 1.898 7.976 9.739 1415.418 0.901 43.317 3.121 0.77 252388. 0.4413
|
|
42.93 0.2334 0.5695 0.0456 0.0187 1.849 7.770 9.201 1378.887 0.878 40.925 3.026 0.77 252598. 0.4160
|
|
45.99 0.2500 0.5909 0.0429 0.0181 1.795 7.542 8.648 1338.378 0.852 38.466 2.931 0.77 252816. 0.3905
|
|
49.06 0.2667 0.6093 0.0401 0.0175 1.735 7.291 8.081 1293.868 0.824 35.945 2.833 0.77 253043. 0.3649
|
|
52.12 0.2834 0.6243 0.0372 0.0169 1.670 7.017 7.501 1245.336 0.793 33.365 2.732 0.77 253278. 0.3390
|
|
55.19 0.3000 0.6357 0.0343 0.0162 1.600 6.721 6.909 1192.772 0.759 30.731 2.627 0.77 253522. 0.3129
|
|
58.26 0.3167 0.6429 0.0313 0.0154 1.524 6.402 6.305 1136.185 0.723 28.047 2.517 0.77 253775. 0.2864
|
|
61.32 0.3334 0.6453 0.0282 0.0146 1.442 6.061 5.692 1075.606 0.685 25.317 2.400 0.77 254037. 0.2595
|
|
64.39 0.3500 0.6419 0.0251 0.0137 1.356 5.697 5.069 1011.102 0.644 22.549 2.274 0.78 254308. 0.2320
|
|
67.46 0.3667 0.6316 0.0220 0.0128 1.264 5.312 4.439 942.780 0.600 19.746 2.136 0.78 254588. 0.2039
|
|
70.52 0.3834 0.6125 0.0189 0.0118 1.168 4.907 3.803 870.795 0.554 16.917 1.981 0.78 254878. 0.1751
|
|
73.59 0.4001 0.5820 0.0157 0.0108 1.067 4.482 3.163 795.365 0.506 14.070 1.804 0.78 255177. 0.1454
|
|
76.65 0.4167 0.5362 0.0125 0.0097 0.961 4.039 2.522 716.776 0.456 11.216 1.596 0.78 255486. 0.1148
|
|
79.72 0.4334 0.4692 0.0093 0.0086 0.852 3.580 1.881 635.397 0.405 8.365 1.342 0.78 255804. 0.0834
|
|
82.79 0.4501 0.3711 0.0062 0.0075 0.740 3.109 1.244 551.676 0.351 5.532 1.022 0.78 256132. 0.0517
|
|
85.85 0.4667 0.2245 0.0030 0.0063 0.625 2.626 0.613 466.037 0.297 2.726 0.597 0.78 256467. 0.0212
|
|
88.92 0.4834 -0.0110 -0.0001 0.0051 0.504 2.120 -0.023 376.205 0.239 -0.104 -0.028 0.78 256772. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 16000
|
|
|
|
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 0.0766 0.0222 2.666 10.502 17.571 1987.934 1.186 78.157 4.009 0.82 267014. 0.7615
|
|
3.27 0.0167 0.0563 0.0750 0.0222 2.664 10.494 17.204 1986.418 1.186 76.522 3.928 0.82 267138. 0.7383
|
|
6.54 0.0333 0.1102 0.0733 0.0222 2.659 10.475 16.818 1982.951 1.183 74.804 3.847 0.82 267269. 0.7148
|
|
9.80 0.0500 0.1618 0.0715 0.0221 2.652 10.445 16.413 1977.296 1.180 73.005 3.765 0.82 267407. 0.6911
|
|
13.07 0.0666 0.2110 0.0697 0.0220 2.641 10.403 15.990 1969.217 1.175 71.122 3.683 0.82 267551. 0.6673
|
|
16.34 0.0833 0.2579 0.0678 0.0219 2.626 10.346 15.547 1958.455 1.169 69.153 3.601 0.82 267704. 0.6433
|
|
19.61 0.0999 0.3024 0.0658 0.0217 2.608 10.273 15.085 1944.755 1.161 67.097 3.518 0.82 267863. 0.6191
|
|
22.87 0.1166 0.3445 0.0637 0.0215 2.585 10.184 14.603 1927.854 1.151 64.952 3.436 0.82 268030. 0.5949
|
|
26.14 0.1332 0.3842 0.0615 0.0213 2.558 10.077 14.100 1907.552 1.138 62.718 3.353 0.82 268205. 0.5705
|
|
29.41 0.1499 0.4215 0.0592 0.0210 2.526 9.951 13.578 1883.762 1.124 60.394 3.269 0.82 268388. 0.5458
|
|
32.68 0.1665 0.4563 0.0568 0.0207 2.489 9.806 13.035 1856.251 1.108 57.980 3.185 0.82 268579. 0.5211
|
|
35.95 0.1832 0.4885 0.0544 0.0204 2.447 9.639 12.472 1824.728 1.089 55.474 3.100 0.82 268778. 0.4961
|
|
39.21 0.1999 0.5182 0.0518 0.0200 2.399 9.450 11.888 1788.913 1.068 52.878 3.014 0.82 268985. 0.4709
|
|
42.48 0.2165 0.5451 0.0492 0.0195 2.345 9.237 11.284 1748.643 1.044 50.192 2.927 0.82 269201. 0.4455
|
|
45.75 0.2332 0.5692 0.0465 0.0190 2.285 9.001 10.662 1703.886 1.017 47.423 2.838 0.82 269426. 0.4199
|
|
49.02 0.2498 0.5904 0.0437 0.0185 2.219 8.740 10.022 1654.523 0.987 44.576 2.747 0.82 269660. 0.3941
|
|
52.28 0.2665 0.6083 0.0408 0.0179 2.146 8.455 9.365 1600.582 0.955 41.657 2.654 0.82 269902. 0.3680
|
|
55.55 0.2831 0.6227 0.0379 0.0172 2.068 8.146 8.694 1542.108 0.920 38.670 2.557 0.83 270154. 0.3416
|
|
58.82 0.2998 0.6332 0.0349 0.0165 1.984 7.814 8.008 1479.162 0.883 35.619 2.456 0.83 270415. 0.3149
|
|
62.09 0.3164 0.6391 0.0319 0.0158 1.893 7.458 7.309 1411.846 0.843 32.510 2.348 0.83 270685. 0.2876
|
|
65.36 0.3331 0.6397 0.0288 0.0150 1.797 7.080 6.598 1340.320 0.800 29.348 2.233 0.83 270965. 0.2599
|
|
68.62 0.3498 0.6341 0.0256 0.0141 1.696 6.681 5.877 1264.726 0.755 26.140 2.108 0.83 271254. 0.2315
|
|
71.89 0.3664 0.6207 0.0224 0.0132 1.590 6.261 5.147 1185.294 0.707 22.892 1.969 0.83 271553. 0.2024
|
|
75.16 0.3831 0.5978 0.0192 0.0123 1.478 5.823 4.409 1102.314 0.658 19.612 1.814 0.83 271862. 0.1726
|
|
78.43 0.3997 0.5628 0.0160 0.0114 1.363 5.368 3.667 1016.154 0.606 16.311 1.637 0.83 272181. 0.1420
|
|
81.70 0.4164 0.5120 0.0127 0.0104 1.243 4.898 2.923 927.265 0.553 13.000 1.430 0.83 272510. 0.1107
|
|
84.96 0.4330 0.4402 0.0095 0.0093 1.121 4.417 2.179 836.189 0.499 9.691 1.182 0.83 272850. 0.0790
|
|
88.23 0.4497 0.3396 0.0063 0.0083 0.997 3.928 1.439 743.543 0.444 6.402 0.878 0.83 273199. 0.0477
|
|
91.50 0.4663 0.1979 0.0031 0.0073 0.871 3.433 0.707 649.874 0.388 3.144 0.493 0.83 273556. 0.0188
|
|
94.77 0.4830 -0.0109 -0.0001 0.0062 0.740 2.914 -0.032 551.596 0.329 -0.142 -0.026 0.83 273884. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 17000
|
|
|
|
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 0.0781 0.0239 3.439 12.749 20.224 2564.169 1.440 89.955 3.577 0.87 283668. 0.7289
|
|
3.53 0.0169 0.0544 0.0764 0.0238 3.421 12.683 19.797 2551.000 1.433 88.056 3.520 0.87 283803. 0.7096
|
|
7.05 0.0338 0.1070 0.0747 0.0236 3.400 12.607 19.348 2535.553 1.424 86.058 3.461 0.87 283947. 0.6898
|
|
10.58 0.0508 0.1578 0.0729 0.0235 3.376 12.517 18.876 2517.615 1.414 83.962 3.401 0.87 284097. 0.6695
|
|
14.11 0.0677 0.2066 0.0710 0.0233 3.348 12.415 18.382 2496.939 1.403 81.765 3.339 0.87 284256. 0.6487
|
|
17.64 0.0846 0.2533 0.0690 0.0230 3.317 12.297 17.866 2473.260 1.389 79.466 3.276 0.87 284422. 0.6275
|
|
21.16 0.1015 0.2981 0.0669 0.0228 3.281 12.163 17.325 2446.305 1.374 77.063 3.212 0.87 284597. 0.6058
|
|
24.69 0.1184 0.3407 0.0647 0.0225 3.240 12.011 16.761 2415.780 1.357 74.553 3.147 0.87 284780. 0.5838
|
|
28.22 0.1354 0.3811 0.0624 0.0222 3.193 11.840 16.173 2381.393 1.338 71.938 3.080 0.87 284971. 0.5613
|
|
31.75 0.1523 0.4192 0.0601 0.0218 3.142 11.650 15.561 2343.197 1.316 69.214 3.012 0.87 285171. 0.5384
|
|
35.27 0.1692 0.4548 0.0576 0.0214 3.087 11.444 14.924 2301.807 1.293 66.383 2.941 0.87 285380. 0.5148
|
|
38.80 0.1861 0.4876 0.0551 0.0210 3.026 11.220 14.263 2256.755 1.268 63.443 2.867 0.87 285598. 0.4906
|
|
42.33 0.2031 0.5176 0.0524 0.0206 2.961 10.978 13.578 2208.032 1.240 60.395 2.789 0.88 285825. 0.4657
|
|
45.86 0.2200 0.5444 0.0497 0.0201 2.891 10.717 12.869 2155.611 1.211 57.241 2.708 0.88 286062. 0.4401
|
|
49.38 0.2369 0.5676 0.0469 0.0196 2.816 10.441 12.138 2099.953 1.180 53.989 2.622 0.88 286308. 0.4139
|
|
52.91 0.2538 0.5868 0.0440 0.0190 2.738 10.150 11.386 2041.500 1.147 50.644 2.530 0.88 286563. 0.3868
|
|
56.44 0.2707 0.6022 0.0410 0.0184 2.653 9.835 10.615 1978.205 1.111 47.214 2.434 0.88 286829. 0.3593
|
|
59.97 0.2877 0.6133 0.0379 0.0178 2.562 9.497 9.826 1910.215 1.073 43.705 2.333 0.88 287104. 0.3314
|
|
63.49 0.3046 0.6197 0.0348 0.0171 2.464 9.137 9.020 1837.753 1.032 40.122 2.226 0.88 287390. 0.3030
|
|
67.02 0.3215 0.6205 0.0317 0.0164 2.362 8.756 8.199 1761.083 0.989 36.471 2.112 0.88 287685. 0.2740
|
|
70.55 0.3384 0.6148 0.0284 0.0157 2.254 8.356 7.365 1680.587 0.944 32.760 1.988 0.88 287991. 0.2444
|
|
74.08 0.3553 0.6014 0.0252 0.0149 2.141 7.938 6.519 1596.667 0.897 28.996 1.852 0.88 288308. 0.2142
|
|
77.60 0.3723 0.5788 0.0219 0.0141 2.025 7.506 5.663 1509.671 0.848 25.188 1.701 0.88 288635. 0.1834
|
|
81.13 0.3892 0.5452 0.0185 0.0132 1.904 7.061 4.799 1420.119 0.798 21.348 1.533 0.88 288973. 0.1522
|
|
84.66 0.4061 0.4982 0.0152 0.0124 1.782 6.606 3.932 1328.594 0.746 17.488 1.342 0.88 289322. 0.1206
|
|
88.19 0.4230 0.4346 0.0118 0.0115 1.657 6.144 3.063 1235.781 0.694 13.623 1.124 0.88 289682. 0.0891
|
|
91.71 0.4399 0.3506 0.0085 0.0106 1.532 5.680 2.197 1142.458 0.642 9.771 0.872 0.88 290053. 0.0586
|
|
95.24 0.4569 0.2414 0.0052 0.0098 1.407 5.217 1.338 1049.395 0.589 5.949 0.578 0.88 290434. 0.0303
|
|
98.77 0.4738 0.1000 0.0019 0.0089 1.283 4.756 0.487 956.576 0.537 2.167 0.231 0.88 290823. 0.0073
|
|
102.30 0.4907
|
|
|
|
|
|
|
|
PROP RPM = 18000
|
|
|
|
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 0.0795 0.0270 4.611 16.145 23.079 3438.309 1.824 102.657 3.045 0.92 300319. 0.6627
|
|
3.78 0.0171 0.0499 0.0778 0.0267 4.565 15.983 22.598 3403.847 1.806 100.515 3.011 0.92 300465. 0.6486
|
|
7.56 0.0342 0.0986 0.0761 0.0264 4.514 15.807 22.089 3366.292 1.786 98.254 2.976 0.92 300620. 0.6338
|
|
11.33 0.0514 0.1461 0.0742 0.0261 4.460 15.616 21.555 3325.513 1.764 95.875 2.940 0.92 300783. 0.6184
|
|
15.11 0.0685 0.1923 0.0723 0.0257 4.400 15.408 20.993 3281.281 1.741 93.376 2.902 0.92 300954. 0.6024
|
|
18.89 0.0856 0.2370 0.0703 0.0254 4.336 15.183 20.403 3233.370 1.715 90.754 2.862 0.92 301134. 0.5858
|
|
22.67 0.1027 0.2803 0.0681 0.0250 4.266 14.939 19.786 3181.526 1.688 88.007 2.821 0.93 301323. 0.5685
|
|
26.45 0.1198 0.3220 0.0659 0.0245 4.191 14.676 19.140 3125.522 1.658 85.133 2.778 0.93 301521. 0.5506
|
|
30.23 0.1369 0.3621 0.0636 0.0241 4.110 14.393 18.465 3065.121 1.626 82.132 2.732 0.93 301728. 0.5320
|
|
34.00 0.1541 0.4003 0.0612 0.0235 4.023 14.087 17.762 3000.068 1.592 79.003 2.685 0.93 301945. 0.5128
|
|
37.78 0.1712 0.4365 0.0587 0.0230 3.931 13.763 17.029 2931.041 1.555 75.747 2.635 0.93 302171. 0.4928
|
|
41.56 0.1883 0.4700 0.0560 0.0224 3.836 13.431 16.268 2860.261 1.517 72.361 2.580 0.93 302408. 0.4715
|
|
45.34 0.2054 0.5007 0.0533 0.0219 3.737 13.087 15.478 2786.984 1.479 68.847 2.519 0.93 302654. 0.4491
|
|
49.12 0.2225 0.5280 0.0505 0.0213 3.637 12.734 14.660 2711.935 1.439 65.209 2.452 0.93 302910. 0.4254
|
|
52.90 0.2396 0.5511 0.0476 0.0207 3.536 12.382 13.816 2636.848 1.399 61.454 2.377 0.93 303177. 0.4003
|
|
56.67 0.2568 0.5686 0.0446 0.0201 3.441 12.050 12.948 2566.095 1.361 57.591 2.289 0.93 303454. 0.3731
|
|
60.45 0.2739 0.5796 0.0415 0.0196 3.353 11.741 12.056 2500.458 1.327 53.625 2.187 0.93 303741. 0.3441
|
|
64.23 0.2910 0.5855 0.0384 0.0191 3.260 11.414 11.144 2430.810 1.290 49.568 2.079 0.93 304039. 0.3145
|
|
68.01 0.3081 0.5858 0.0352 0.0185 3.162 11.070 10.213 2357.576 1.251 45.427 1.965 0.93 304348. 0.2845
|
|
71.79 0.3252 0.5797 0.0319 0.0179 3.059 10.712 9.265 2281.233 1.210 41.211 1.842 0.93 304668. 0.2541
|
|
75.56 0.3423 0.5664 0.0286 0.0173 2.953 10.341 8.302 2202.294 1.168 36.927 1.710 0.93 304999. 0.2232
|
|
79.34 0.3595 0.5449 0.0252 0.0166 2.845 9.962 7.326 2121.433 1.125 32.588 1.566 0.93 305342. 0.1921
|
|
83.12 0.3766 0.5139 0.0218 0.0160 2.735 9.577 6.341 2039.443 1.082 28.206 1.410 0.93 305696. 0.1609
|
|
86.90 0.3937 0.4724 0.0184 0.0154 2.624 9.188 5.349 1956.727 1.038 23.794 1.240 0.93 306061. 0.1300
|
|
90.68 0.4108 0.4190 0.0150 0.0147 2.513 8.800 4.355 1873.995 0.994 19.370 1.054 0.93 306439. 0.0997
|
|
94.46 0.4279 0.3524 0.0116 0.0141 2.403 8.415 3.362 1791.983 0.951 14.954 0.851 0.93 306828. 0.0707
|
|
98.23 0.4450 0.2712 0.0082 0.0134 2.295 8.036 2.376 1711.422 0.908 10.568 0.630 0.93 307230. 0.0440
|
|
102.01 0.4622 0.1741 0.0048 0.0128 2.190 7.667 1.402 1632.723 0.866 6.234 0.389 0.93 307643. 0.0209
|
|
105.79 0.4793 0.0592 0.0015 0.0122 2.084 7.296 0.438 1553.775 0.824 1.946 0.128 0.94 308066. 0.0038
|
|
109.57 0.4964
|
|
|
|
|
|
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