501 lines
89 KiB
Plaintext
501 lines
89 KiB
Plaintext
18.1x10 (181x10.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 0.1008 0.0423 0.007 0.417 0.345 4.929 0.047 1.533 31.710 0.07 39306. 0.6035
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0.43 0.0248 0.0576 0.0992 0.0427 0.007 0.421 0.339 4.981 0.048 1.508 30.880 0.07 39335. 0.5830
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0.85 0.0497 0.1121 0.0974 0.0431 0.007 0.425 0.333 5.029 0.048 1.482 30.051 0.07 39365. 0.5624
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1.28 0.0745 0.1636 0.0956 0.0435 0.007 0.429 0.327 5.072 0.048 1.454 29.226 0.07 39399. 0.5416
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1.70 0.0993 0.2120 0.0935 0.0438 0.007 0.432 0.320 5.109 0.049 1.423 28.405 0.07 39434. 0.5208
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2.13 0.1241 0.2574 0.0914 0.0441 0.007 0.434 0.313 5.137 0.049 1.390 27.591 0.07 39473. 0.5000
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2.55 0.1490 0.2998 0.0890 0.0442 0.007 0.436 0.305 5.157 0.049 1.355 26.784 0.07 39514. 0.4792
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2.98 0.1738 0.3393 0.0865 0.0443 0.007 0.437 0.296 5.167 0.049 1.317 25.983 0.07 39559. 0.4583
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3.40 0.1986 0.3760 0.0839 0.0443 0.007 0.437 0.287 5.165 0.049 1.276 25.191 0.07 39606. 0.4374
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3.83 0.2235 0.4098 0.0810 0.0442 0.007 0.435 0.277 5.149 0.049 1.232 24.405 0.07 39656. 0.4165
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4.26 0.2483 0.4408 0.0780 0.0439 0.007 0.433 0.267 5.119 0.049 1.186 23.626 0.07 39710. 0.3955
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4.68 0.2731 0.4690 0.0747 0.0435 0.007 0.429 0.256 5.073 0.048 1.137 22.851 0.07 39766. 0.3745
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5.11 0.2980 0.4943 0.0713 0.0430 0.007 0.424 0.244 5.011 0.048 1.085 22.080 0.07 39826. 0.3535
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5.53 0.3228 0.5168 0.0678 0.0423 0.007 0.417 0.232 4.933 0.047 1.031 21.309 0.07 39889. 0.3326
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5.96 0.3476 0.5364 0.0640 0.0415 0.006 0.409 0.219 4.838 0.046 0.974 20.536 0.07 39955. 0.3116
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6.38 0.3724 0.5529 0.0602 0.0405 0.006 0.399 0.206 4.726 0.045 0.916 19.757 0.07 40024. 0.2906
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6.81 0.3973 0.5662 0.0562 0.0394 0.006 0.389 0.192 4.598 0.044 0.855 18.966 0.07 40097. 0.2696
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7.23 0.4221 0.5759 0.0521 0.0382 0.006 0.376 0.178 4.452 0.043 0.793 18.158 0.07 40173. 0.2485
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7.66 0.4469 0.5819 0.0479 0.0368 0.006 0.363 0.164 4.290 0.041 0.729 17.326 0.07 40252. 0.2274
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8.09 0.4718 0.5835 0.0436 0.0353 0.006 0.348 0.149 4.112 0.039 0.664 16.460 0.07 40335. 0.2061
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8.51 0.4966 0.5802 0.0392 0.0336 0.005 0.331 0.134 3.916 0.037 0.597 15.548 0.07 40421. 0.1847
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8.94 0.5214 0.5710 0.0348 0.0318 0.005 0.313 0.119 3.702 0.035 0.529 14.575 0.07 40510. 0.1630
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9.36 0.5462 0.5548 0.0303 0.0298 0.005 0.293 0.103 3.472 0.033 0.460 13.518 0.07 40603. 0.1410
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9.79 0.5711 0.5298 0.0257 0.0277 0.004 0.273 0.088 3.225 0.031 0.390 12.347 0.07 40699. 0.1186
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10.21 0.5959 0.4934 0.0210 0.0254 0.004 0.250 0.072 2.961 0.028 0.320 11.018 0.07 40799. 0.0958
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10.64 0.6207 0.4416 0.0164 0.0230 0.004 0.227 0.056 2.680 0.026 0.249 9.467 0.07 40902. 0.0726
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11.07 0.6456 0.3682 0.0117 0.0205 0.003 0.202 0.040 2.384 0.023 0.177 7.591 0.07 41008. 0.0492
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11.49 0.6704 0.2628 0.0070 0.0178 0.003 0.175 0.024 2.073 0.020 0.106 5.218 0.07 41118. 0.0261
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11.92 0.6952 0.1064 0.0023 0.0150 0.002 0.148 0.008 1.748 0.017 0.035 2.036 0.07 41230. 0.0058
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12.34 0.7200
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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 0.1012 0.0382 0.048 1.507 1.385 35.659 0.170 6.160 17.617 0.14 78612. 0.6721
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0.84 0.0245 0.0632 0.0997 0.0387 0.048 1.526 1.363 36.110 0.172 6.065 17.126 0.14 78667. 0.6483
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1.68 0.0491 0.1227 0.0980 0.0392 0.049 1.544 1.340 36.532 0.174 5.961 16.640 0.14 78728. 0.6245
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2.52 0.0736 0.1788 0.0961 0.0396 0.050 1.560 1.315 36.914 0.176 5.850 16.160 0.14 78794. 0.6008
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3.36 0.0981 0.2314 0.0942 0.0399 0.050 1.574 1.288 37.248 0.178 5.730 15.686 0.14 78864. 0.5771
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4.21 0.1227 0.2806 0.0920 0.0402 0.050 1.586 1.259 37.523 0.179 5.600 15.219 0.14 78940. 0.5536
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5.05 0.1472 0.3266 0.0897 0.0405 0.051 1.594 1.228 37.730 0.180 5.461 14.761 0.14 79022. 0.5302
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5.89 0.1717 0.3694 0.0873 0.0406 0.051 1.600 1.194 37.856 0.181 5.312 14.310 0.14 79109. 0.5070
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6.73 0.1963 0.4091 0.0847 0.0406 0.051 1.601 1.158 37.890 0.181 5.153 13.868 0.14 79202. 0.4839
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7.57 0.2208 0.4458 0.0819 0.0406 0.051 1.598 1.120 37.821 0.181 4.982 13.433 0.14 79301. 0.4609
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8.41 0.2454 0.4796 0.0789 0.0404 0.050 1.591 1.079 37.636 0.180 4.801 13.007 0.14 79406. 0.4381
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9.25 0.2699 0.5106 0.0757 0.0400 0.050 1.577 1.036 37.326 0.178 4.608 12.589 0.14 79517. 0.4154
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10.09 0.2944 0.5388 0.0724 0.0396 0.049 1.559 0.990 36.886 0.176 4.405 12.177 0.14 79634. 0.3928
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10.93 0.3190 0.5642 0.0689 0.0389 0.049 1.535 0.942 36.313 0.173 4.191 11.770 0.14 79757. 0.3704
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11.78 0.3435 0.5868 0.0652 0.0382 0.048 1.505 0.892 35.605 0.170 3.969 11.368 0.14 79887. 0.3481
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12.62 0.3680 0.6066 0.0614 0.0373 0.047 1.469 0.841 34.762 0.166 3.739 10.968 0.14 80023. 0.3260
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13.46 0.3926 0.6235 0.0575 0.0362 0.045 1.428 0.787 33.783 0.161 3.501 10.568 0.14 80165. 0.3040
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14.30 0.4171 0.6372 0.0535 0.0350 0.044 1.380 0.732 32.666 0.156 3.256 10.166 0.14 80314. 0.2820
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15.14 0.4416 0.6476 0.0494 0.0337 0.042 1.327 0.676 31.409 0.150 3.006 9.758 0.15 80469. 0.2600
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15.98 0.4662 0.6543 0.0452 0.0322 0.040 1.268 0.618 30.013 0.143 2.749 9.339 0.15 80631. 0.2380
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16.82 0.4907 0.6568 0.0409 0.0305 0.038 1.203 0.559 28.474 0.136 2.487 8.906 0.15 80800. 0.2159
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17.66 0.5152 0.6543 0.0365 0.0287 0.036 1.132 0.499 26.794 0.128 2.220 8.450 0.15 80975. 0.1935
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18.50 0.5398 0.6458 0.0320 0.0268 0.033 1.055 0.438 24.971 0.119 1.949 7.961 0.15 81157. 0.1709
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19.35 0.5643 0.6297 0.0275 0.0247 0.031 0.972 0.377 23.006 0.110 1.675 7.425 0.15 81345. 0.1477
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20.19 0.5889 0.6036 0.0230 0.0224 0.028 0.883 0.314 20.901 0.100 1.398 6.820 0.15 81540. 0.1239
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21.03 0.6134 0.5635 0.0184 0.0200 0.025 0.788 0.251 18.658 0.089 1.118 6.113 0.15 81742. 0.0994
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21.87 0.6379 0.5030 0.0138 0.0175 0.022 0.688 0.188 16.282 0.078 0.838 5.247 0.15 81950. 0.0738
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22.71 0.6625 0.4102 0.0091 0.0148 0.018 0.582 0.125 13.779 0.066 0.557 4.120 0.15 82165. 0.0473
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23.55 0.6870 0.2609 0.0045 0.0120 0.015 0.472 0.062 11.158 0.053 0.276 2.527 0.15 82385. 0.0204
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24.39 0.7115 -0.0049 -0.0001 0.0090 0.011 0.355 -0.001 8.408 0.040 -0.004 -0.046 0.15 82603. 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 0.1017 0.0367 0.155 3.252 3.130 115.425 0.367 13.923 12.300 0.22 117914. 0.7055
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1.28 0.0249 0.0669 0.1001 0.0372 0.157 3.297 3.081 117.034 0.373 13.706 11.942 0.22 117999. 0.6796
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2.56 0.0497 0.1299 0.0984 0.0377 0.159 3.340 3.028 118.538 0.377 13.470 11.588 0.22 118092. 0.6537
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3.84 0.0746 0.1890 0.0965 0.0381 0.161 3.378 2.971 119.906 0.382 13.216 11.239 0.22 118192. 0.6280
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5.12 0.0995 0.2444 0.0945 0.0385 0.162 3.412 2.909 121.105 0.385 12.941 10.897 0.22 118300. 0.6025
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6.39 0.1243 0.2960 0.0924 0.0388 0.164 3.440 2.843 122.099 0.389 12.645 10.561 0.22 118416. 0.5772
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7.67 0.1492 0.3442 0.0900 0.0390 0.165 3.461 2.771 122.850 0.391 12.327 10.232 0.22 118541. 0.5522
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8.95 0.1741 0.3889 0.0875 0.0392 0.165 3.474 2.694 123.318 0.393 11.985 9.910 0.22 118674. 0.5274
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10.23 0.1990 0.4304 0.0849 0.0392 0.166 3.478 2.612 123.460 0.393 11.618 9.596 0.22 118816. 0.5028
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11.51 0.2238 0.4687 0.0820 0.0392 0.165 3.472 2.524 123.234 0.392 11.226 9.289 0.22 118968. 0.4784
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12.79 0.2487 0.5040 0.0789 0.0390 0.164 3.454 2.430 122.599 0.390 10.808 8.990 0.22 119129. 0.4543
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14.07 0.2736 0.5363 0.0757 0.0386 0.163 3.424 2.330 121.522 0.387 10.364 8.697 0.22 119299. 0.4304
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15.35 0.2984 0.5658 0.0723 0.0381 0.161 3.380 2.225 119.984 0.382 9.896 8.410 0.22 119479. 0.4067
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16.62 0.3233 0.5925 0.0687 0.0375 0.158 3.324 2.114 117.975 0.376 9.405 8.129 0.22 119668. 0.3832
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17.90 0.3482 0.6163 0.0650 0.0367 0.155 3.254 1.999 115.489 0.368 8.894 7.853 0.22 119867. 0.3600
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19.18 0.3730 0.6374 0.0611 0.0357 0.151 3.170 1.880 112.522 0.358 8.364 7.579 0.22 120076. 0.3369
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20.46 0.3979 0.6555 0.0571 0.0347 0.146 3.073 1.757 109.069 0.347 7.816 7.308 0.22 120295. 0.3140
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21.74 0.4228 0.6706 0.0530 0.0334 0.141 2.962 1.631 105.125 0.335 7.254 7.036 0.22 120523. 0.2913
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23.02 0.4477 0.6824 0.0488 0.0320 0.135 2.837 1.501 100.685 0.320 6.677 6.762 0.22 120762. 0.2686
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24.30 0.4725 0.6905 0.0445 0.0304 0.128 2.698 1.368 95.745 0.305 6.087 6.482 0.22 121011. 0.2458
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25.58 0.4974 0.6945 0.0401 0.0287 0.121 2.544 1.233 90.299 0.287 5.485 6.194 0.22 121270. 0.2230
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26.86 0.5223 0.6936 0.0356 0.0268 0.113 2.376 1.095 84.345 0.268 4.873 5.891 0.22 121539. 0.1999
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28.13 0.5471 0.6865 0.0310 0.0247 0.104 2.194 0.956 77.883 0.248 4.251 5.566 0.22 121818. 0.1764
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29.41 0.5720 0.6716 0.0265 0.0225 0.095 1.998 0.814 70.916 0.226 3.622 5.208 0.22 122108. 0.1524
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30.69 0.5969 0.6459 0.0218 0.0202 0.085 1.788 0.672 63.450 0.202 2.987 4.800 0.22 122408. 0.1275
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31.97 0.6217 0.6045 0.0171 0.0176 0.074 1.564 0.528 55.498 0.177 2.347 4.313 0.22 122718. 0.1016
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33.25 0.6466 0.5385 0.0125 0.0150 0.063 1.326 0.383 47.077 0.150 1.706 3.694 0.22 123038. 0.0742
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34.53 0.6715 0.4298 0.0078 0.0121 0.051 1.077 0.239 38.215 0.122 1.064 2.840 0.22 123368. 0.0450
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35.81 0.6964 0.2353 0.0031 0.0092 0.039 0.815 0.096 28.938 0.092 0.425 1.499 0.22 123705. 0.0150
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37.09 0.7212
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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 0.1022 0.0359 0.359 5.663 5.595 267.987 0.640 24.886 9.469 0.29 157212. 0.7261
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1.70 0.0247 0.0684 0.1007 0.0364 0.365 5.745 5.509 271.888 0.649 24.503 9.190 0.29 157326. 0.6992
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3.39 0.0495 0.1326 0.0990 0.0369 0.370 5.822 5.415 275.544 0.658 24.088 8.914 0.29 157448. 0.6725
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5.09 0.0742 0.1929 0.0971 0.0374 0.374 5.893 5.314 278.878 0.666 23.639 8.643 0.29 157581. 0.6460
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6.79 0.0990 0.2493 0.0951 0.0378 0.378 5.955 5.205 281.813 0.673 23.154 8.378 0.29 157725. 0.6197
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8.48 0.1237 0.3019 0.0930 0.0381 0.381 6.007 5.088 284.267 0.679 22.631 8.118 0.29 157879. 0.5936
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10.18 0.1485 0.3510 0.0907 0.0384 0.384 6.046 4.961 286.147 0.683 22.068 7.864 0.29 158044. 0.5679
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11.88 0.1732 0.3966 0.0882 0.0385 0.385 6.072 4.826 287.358 0.686 21.464 7.617 0.29 158221. 0.5424
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13.57 0.1980 0.4389 0.0855 0.0386 0.386 6.081 4.680 287.801 0.687 20.816 7.375 0.29 158410. 0.5172
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15.27 0.2227 0.4780 0.0827 0.0385 0.385 6.072 4.524 287.374 0.686 20.123 7.140 0.29 158611. 0.4923
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16.97 0.2475 0.5141 0.0796 0.0383 0.384 6.043 4.358 285.980 0.683 19.383 6.912 0.29 158824. 0.4677
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18.66 0.2722 0.5473 0.0764 0.0380 0.380 5.991 4.181 283.540 0.677 18.598 6.689 0.29 159049. 0.4434
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20.36 0.2970 0.5776 0.0730 0.0375 0.375 5.917 3.995 280.003 0.668 17.769 6.471 0.29 159287. 0.4193
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22.06 0.3217 0.6052 0.0694 0.0369 0.369 5.818 3.799 275.344 0.657 16.899 6.259 0.29 159538. 0.3955
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23.75 0.3465 0.6301 0.0657 0.0361 0.361 5.696 3.596 269.548 0.643 15.993 6.050 0.29 159802. 0.3719
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25.45 0.3712 0.6522 0.0618 0.0352 0.352 5.549 3.384 262.605 0.627 15.054 5.845 0.29 160078. 0.3486
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27.15 0.3960 0.6716 0.0579 0.0341 0.341 5.378 3.166 254.502 0.608 14.084 5.643 0.29 160368. 0.3255
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28.84 0.4207 0.6881 0.0538 0.0329 0.329 5.182 2.942 245.228 0.585 13.086 5.441 0.29 160670. 0.3026
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30.54 0.4455 0.7015 0.0496 0.0315 0.315 4.961 2.712 234.768 0.560 12.062 5.239 0.29 160986. 0.2797
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32.24 0.4702 0.7115 0.0453 0.0299 0.299 4.714 2.477 223.111 0.533 11.016 5.035 0.29 161315. 0.2568
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33.93 0.4949 0.7178 0.0409 0.0282 0.282 4.443 2.237 210.247 0.502 9.948 4.825 0.29 161657. 0.2339
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35.63 0.5197 0.7195 0.0364 0.0263 0.263 4.145 1.992 196.168 0.468 8.862 4.606 0.29 162013. 0.2108
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37.33 0.5444 0.7158 0.0319 0.0242 0.243 3.822 1.744 180.873 0.432 7.759 4.374 0.29 162383. 0.1873
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39.02 0.5692 0.7050 0.0273 0.0220 0.220 3.473 1.493 164.367 0.392 6.642 4.121 0.29 162765. 0.1632
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40.72 0.5939 0.6844 0.0227 0.0197 0.197 3.099 1.240 146.665 0.350 5.514 3.834 0.29 163162. 0.1384
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42.42 0.6187 0.6496 0.0180 0.0171 0.171 2.700 0.984 127.794 0.305 4.378 3.493 0.29 163572. 0.1124
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44.11 0.6434 0.5923 0.0133 0.0144 0.145 2.278 0.728 107.796 0.257 3.238 3.063 0.29 163995. 0.0847
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45.81 0.6682 0.4952 0.0086 0.0116 0.116 1.833 0.472 86.731 0.207 2.097 2.466 0.29 164431. 0.0549
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47.51 0.6929 0.3157 0.0039 0.0087 0.087 1.366 0.216 64.667 0.154 0.961 1.516 0.29 164878. 0.0228
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49.20 0.7177
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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 0.1029 0.0356 0.695 8.765 8.800 518.479 0.990 39.144 7.699 0.36 196505. 0.7404
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2.13 0.0248 0.0697 0.1013 0.0361 0.706 8.897 8.666 526.302 1.005 38.545 7.468 0.36 196647. 0.7127
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4.26 0.0497 0.1351 0.0996 0.0366 0.716 9.021 8.520 533.638 1.019 37.896 7.241 0.36 196802. 0.6852
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6.38 0.0745 0.1964 0.0978 0.0371 0.725 9.134 8.361 540.335 1.032 37.192 7.019 0.36 196969. 0.6579
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8.51 0.0993 0.2537 0.0958 0.0375 0.733 9.234 8.190 546.235 1.043 36.431 6.801 0.36 197149. 0.6310
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10.64 0.1241 0.3073 0.0936 0.0378 0.739 9.317 8.006 551.172 1.053 35.610 6.588 0.36 197344. 0.6043
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12.77 0.1490 0.3571 0.0913 0.0381 0.744 9.381 7.807 554.966 1.060 34.726 6.381 0.36 197552. 0.5780
|
|
14.89 0.1738 0.4034 0.0888 0.0383 0.748 9.423 7.593 557.426 1.065 33.776 6.179 0.36 197774. 0.5520
|
|
17.02 0.1986 0.4464 0.0861 0.0383 0.749 9.439 7.364 558.350 1.066 32.756 5.982 0.36 198012. 0.5263
|
|
19.15 0.2234 0.4861 0.0832 0.0383 0.748 9.425 7.119 557.538 1.065 31.663 5.791 0.36 198265. 0.5009
|
|
21.28 0.2483 0.5228 0.0802 0.0381 0.744 9.379 6.856 554.796 1.060 30.497 5.605 0.36 198533. 0.4758
|
|
23.40 0.2731 0.5566 0.0769 0.0377 0.738 9.297 6.578 549.963 1.050 29.258 5.425 0.36 198817. 0.4510
|
|
25.53 0.2979 0.5876 0.0735 0.0373 0.728 9.178 6.284 542.940 1.037 27.949 5.249 0.36 199116. 0.4266
|
|
27.66 0.3227 0.6158 0.0699 0.0366 0.716 9.022 5.975 533.676 1.019 26.577 5.078 0.36 199432. 0.4024
|
|
29.79 0.3476 0.6413 0.0661 0.0358 0.700 8.827 5.653 522.141 0.997 25.146 4.911 0.36 199763. 0.3785
|
|
31.91 0.3724 0.6641 0.0622 0.0349 0.682 8.593 5.320 508.312 0.971 23.662 4.747 0.36 200111. 0.3549
|
|
34.04 0.3972 0.6843 0.0582 0.0338 0.660 8.320 4.975 492.167 0.940 22.129 4.585 0.36 200475. 0.3315
|
|
36.17 0.4220 0.7016 0.0540 0.0325 0.635 8.007 4.621 473.680 0.905 20.553 4.425 0.36 200856. 0.3083
|
|
38.30 0.4469 0.7159 0.0498 0.0311 0.607 7.655 4.257 452.823 0.865 18.936 4.264 0.36 201253. 0.2852
|
|
40.43 0.4717 0.7271 0.0454 0.0295 0.576 7.262 3.885 429.574 0.820 17.282 4.102 0.36 201667. 0.2622
|
|
42.55 0.4965 0.7345 0.0410 0.0277 0.542 6.828 3.506 403.911 0.771 15.596 3.937 0.36 202098. 0.2390
|
|
44.68 0.5214 0.7377 0.0365 0.0258 0.504 6.353 3.120 375.821 0.718 13.879 3.766 0.36 202546. 0.2157
|
|
46.81 0.5462 0.7355 0.0319 0.0237 0.463 5.837 2.729 345.301 0.659 12.137 3.584 0.36 203010. 0.1919
|
|
48.94 0.5710 0.7265 0.0273 0.0214 0.419 5.280 2.332 312.361 0.597 10.373 3.386 0.36 203492. 0.1676
|
|
51.06 0.5958 0.7079 0.0226 0.0190 0.372 4.683 1.931 277.034 0.529 8.591 3.162 0.37 203990. 0.1425
|
|
53.19 0.6207 0.6751 0.0179 0.0164 0.321 4.046 1.528 239.374 0.457 6.796 2.895 0.37 204506. 0.1160
|
|
55.32 0.6455 0.6193 0.0131 0.0137 0.267 3.372 1.123 199.471 0.381 4.996 2.554 0.37 205038. 0.0877
|
|
57.45 0.6703 0.5212 0.0084 0.0108 0.211 2.662 0.718 157.446 0.301 3.195 2.070 0.37 205586. 0.0569
|
|
59.57 0.6951 0.3293 0.0037 0.0078 0.152 1.918 0.315 113.432 0.217 1.402 1.261 0.37 206148. 0.0229
|
|
61.70 0.7200
|
|
|
|
|
|
|
|
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 0.1038 0.0355 1.199 12.597 12.775 894.218 1.423 56.825 6.480 0.43 235791. 0.7508
|
|
2.54 0.0247 0.0699 0.1022 0.0361 1.218 12.791 12.584 907.972 1.445 55.972 6.286 0.43 235960. 0.7229
|
|
5.07 0.0493 0.1356 0.1005 0.0366 1.235 12.972 12.375 920.879 1.466 55.046 6.095 0.43 236145. 0.6951
|
|
7.61 0.0740 0.1971 0.0987 0.0370 1.251 13.139 12.150 932.676 1.484 54.042 5.908 0.43 236345. 0.6676
|
|
10.15 0.0987 0.2547 0.0967 0.0375 1.265 13.285 11.905 943.097 1.501 52.955 5.726 0.43 236560. 0.6405
|
|
12.69 0.1233 0.3085 0.0945 0.0378 1.276 13.409 11.642 951.850 1.515 51.782 5.547 0.43 236792. 0.6136
|
|
15.22 0.1480 0.3586 0.0922 0.0381 1.286 13.504 11.357 958.632 1.526 50.518 5.374 0.43 237040. 0.5871
|
|
17.76 0.1727 0.4052 0.0898 0.0382 1.292 13.567 11.052 963.113 1.533 49.158 5.205 0.43 237306. 0.5609
|
|
20.30 0.1974 0.4485 0.0871 0.0383 1.294 13.593 10.723 964.950 1.536 47.698 5.040 0.43 237589. 0.5351
|
|
22.83 0.2220 0.4886 0.0842 0.0383 1.292 13.577 10.372 963.794 1.534 46.134 4.881 0.43 237890. 0.5096
|
|
25.37 0.2467 0.5257 0.0812 0.0381 1.286 13.514 9.996 959.310 1.527 44.463 4.726 0.43 238209. 0.4844
|
|
27.91 0.2714 0.5599 0.0779 0.0378 1.276 13.400 9.597 951.217 1.514 42.686 4.576 0.43 238547. 0.4596
|
|
30.44 0.2960 0.5913 0.0745 0.0373 1.260 13.232 9.175 939.332 1.495 40.809 4.430 0.43 238904. 0.4350
|
|
32.98 0.3207 0.6200 0.0709 0.0367 1.239 13.010 8.732 923.562 1.470 38.838 4.288 0.43 239280. 0.4108
|
|
35.52 0.3454 0.6462 0.0672 0.0359 1.212 12.733 8.269 903.854 1.439 36.782 4.150 0.43 239674. 0.3868
|
|
38.06 0.3700 0.6697 0.0633 0.0350 1.180 12.399 7.790 880.170 1.401 34.649 4.014 0.43 240088. 0.3632
|
|
40.59 0.3947 0.6907 0.0592 0.0339 1.143 12.009 7.294 852.471 1.357 32.445 3.881 0.43 240521. 0.3398
|
|
43.13 0.4194 0.7089 0.0551 0.0326 1.101 11.561 6.784 820.715 1.306 30.176 3.749 0.43 240973. 0.3166
|
|
45.67 0.4441 0.7244 0.0508 0.0312 1.053 11.056 6.261 784.857 1.249 27.849 3.618 0.44 241446. 0.2935
|
|
48.20 0.4687 0.7368 0.0465 0.0296 0.999 10.493 5.726 744.854 1.185 25.468 3.487 0.44 241937. 0.2705
|
|
50.74 0.4934 0.7459 0.0421 0.0278 0.940 9.870 5.180 700.671 1.115 23.039 3.353 0.44 242449. 0.2474
|
|
53.28 0.5181 0.7510 0.0376 0.0259 0.875 9.189 4.624 652.283 1.038 20.566 3.215 0.44 242981. 0.2241
|
|
55.82 0.5427 0.7512 0.0330 0.0238 0.804 8.448 4.059 599.679 0.954 18.055 3.070 0.44 243532. 0.2005
|
|
58.35 0.5674 0.7453 0.0283 0.0216 0.728 7.648 3.487 542.877 0.864 15.511 2.914 0.44 244104. 0.1764
|
|
60.89 0.5921 0.7309 0.0236 0.0191 0.646 6.789 2.909 481.923 0.767 12.940 2.738 0.44 244696. 0.1514
|
|
63.43 0.6167 0.7039 0.0189 0.0166 0.559 5.873 2.327 416.907 0.664 10.350 2.532 0.44 245307. 0.1252
|
|
65.96 0.6414 0.6567 0.0141 0.0138 0.467 4.902 1.742 347.971 0.554 7.749 2.271 0.44 245939. 0.0972
|
|
68.50 0.6661 0.5725 0.0094 0.0109 0.369 3.878 1.157 275.316 0.438 5.147 1.906 0.44 246590. 0.0665
|
|
71.04 0.6908 0.4071 0.0047 0.0079 0.267 2.806 0.574 199.183 0.317 2.553 1.307 0.44 247258. 0.0321
|
|
73.57 0.7154 -0.0203 -0.0001 0.0047 0.158 1.665 -0.016 118.178 0.188 -0.073 -0.063 0.44 247860. 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 0.1048 0.0357 1.912 17.215 17.558 1425.683 1.945 78.098 5.586 0.50 275066. 0.7588
|
|
2.97 0.0247 0.0705 0.1032 0.0362 1.942 17.486 17.298 1448.126 1.976 76.942 5.418 0.50 275265. 0.7305
|
|
5.93 0.0494 0.1366 0.1015 0.0367 1.970 17.740 17.015 1469.190 2.004 75.683 5.253 0.50 275482. 0.7024
|
|
8.90 0.0742 0.1986 0.0997 0.0372 1.996 17.972 16.708 1488.436 2.031 74.316 5.091 0.50 275716. 0.6746
|
|
11.86 0.0989 0.2566 0.0977 0.0377 2.019 18.177 16.375 1505.427 2.054 72.834 4.933 0.50 275969. 0.6472
|
|
14.83 0.1236 0.3108 0.0956 0.0380 2.038 18.350 16.014 1519.698 2.073 71.232 4.780 0.50 276241. 0.6201
|
|
17.80 0.1483 0.3612 0.0932 0.0383 2.053 18.483 15.626 1530.750 2.088 69.502 4.630 0.50 276533. 0.5933
|
|
20.76 0.1731 0.4082 0.0907 0.0385 2.063 18.571 15.207 1538.050 2.098 67.640 4.484 0.50 276845. 0.5669
|
|
23.73 0.1978 0.4518 0.0880 0.0385 2.067 18.608 14.757 1541.044 2.102 65.637 4.343 0.50 277177. 0.5409
|
|
26.70 0.2225 0.4923 0.0852 0.0385 2.064 18.585 14.274 1539.163 2.100 63.489 4.206 0.50 277531. 0.5152
|
|
29.66 0.2472 0.5297 0.0821 0.0383 2.054 18.497 13.758 1531.866 2.090 61.193 4.073 0.50 277906. 0.4898
|
|
32.63 0.2719 0.5642 0.0788 0.0380 2.037 18.338 13.208 1518.694 2.072 58.750 3.945 0.50 278302. 0.4648
|
|
35.59 0.2967 0.5961 0.0753 0.0375 2.011 18.104 12.627 1499.351 2.045 56.165 3.820 0.50 278721. 0.4400
|
|
38.56 0.3214 0.6252 0.0717 0.0369 1.976 17.794 12.017 1473.684 2.010 53.450 3.698 0.51 279162. 0.4156
|
|
41.53 0.3461 0.6518 0.0679 0.0361 1.933 17.407 11.380 1441.615 1.967 50.617 3.580 0.51 279625. 0.3915
|
|
44.49 0.3708 0.6758 0.0640 0.0351 1.882 16.942 10.719 1403.085 1.914 47.676 3.465 0.51 280110. 0.3677
|
|
47.46 0.3956 0.6973 0.0599 0.0340 1.821 16.398 10.035 1358.033 1.853 44.637 3.352 0.51 280618. 0.3442
|
|
50.43 0.4203 0.7162 0.0557 0.0327 1.752 15.774 9.332 1306.395 1.782 41.508 3.240 0.51 281149. 0.3208
|
|
53.39 0.4450 0.7324 0.0514 0.0312 1.674 15.070 8.610 1248.101 1.703 38.297 3.129 0.51 281703. 0.2976
|
|
56.36 0.4697 0.7456 0.0470 0.0296 1.587 14.285 7.871 1183.083 1.614 35.011 3.018 0.51 282280. 0.2745
|
|
59.32 0.4944 0.7555 0.0425 0.0278 1.490 13.418 7.117 1111.284 1.516 31.658 2.905 0.51 282879. 0.2512
|
|
62.29 0.5192 0.7616 0.0379 0.0258 1.385 12.469 6.350 1032.663 1.409 28.245 2.789 0.51 283503. 0.2278
|
|
65.26 0.5439 0.7631 0.0332 0.0237 1.270 11.437 5.571 947.209 1.292 24.778 2.667 0.51 284149. 0.2041
|
|
68.22 0.5686 0.7586 0.0285 0.0214 1.147 10.323 4.781 854.948 1.166 21.265 2.536 0.51 284819. 0.1798
|
|
71.19 0.5933 0.7457 0.0238 0.0189 1.014 9.128 3.983 755.961 1.031 17.715 2.390 0.51 285513. 0.1546
|
|
74.15 0.6181 0.7206 0.0190 0.0163 0.872 7.853 3.178 650.394 0.887 14.138 2.217 0.51 286229. 0.1281
|
|
77.12 0.6428 0.6752 0.0141 0.0135 0.722 6.502 2.371 538.482 0.735 10.546 1.997 0.51 286969. 0.0997
|
|
80.09 0.6675 0.5918 0.0093 0.0105 0.564 5.078 1.563 420.560 0.574 6.951 1.686 0.51 287732. 0.0683
|
|
83.05 0.6922 0.4212 0.0045 0.0074 0.398 3.586 0.758 297.015 0.405 3.370 1.157 0.51 288514. 0.0326
|
|
86.02 0.7169
|
|
|
|
|
|
|
|
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 0.1060 0.0360 2.880 22.692 23.197 2147.798 2.564 103.181 4.899 0.57 314330. 0.7649
|
|
3.39 0.0247 0.0705 0.1044 0.0366 2.926 23.056 22.861 2182.262 2.605 101.687 4.752 0.57 314558. 0.7365
|
|
6.77 0.0494 0.1368 0.1028 0.0371 2.970 23.398 22.495 2214.609 2.643 100.056 4.607 0.57 314806. 0.7084
|
|
10.16 0.0741 0.1989 0.1009 0.0376 3.009 23.710 22.095 2244.163 2.679 98.280 4.466 0.57 315074. 0.6805
|
|
13.54 0.0988 0.2570 0.0990 0.0380 3.044 23.986 21.662 2270.255 2.710 96.350 4.328 0.57 315364. 0.6530
|
|
16.93 0.1235 0.3112 0.0968 0.0384 3.074 24.218 21.192 2292.177 2.736 94.260 4.193 0.57 315676. 0.6258
|
|
20.32 0.1482 0.3618 0.0945 0.0387 3.097 24.397 20.684 2309.177 2.756 92.001 4.063 0.58 316010. 0.5990
|
|
23.70 0.1729 0.4090 0.0920 0.0389 3.112 24.516 20.136 2320.453 2.770 89.563 3.936 0.58 316367. 0.5725
|
|
27.09 0.1976 0.4528 0.0893 0.0390 3.118 24.566 19.546 2325.163 2.775 86.939 3.813 0.58 316748. 0.5465
|
|
30.47 0.2222 0.4935 0.0864 0.0389 3.114 24.537 18.912 2322.453 2.772 84.122 3.694 0.58 317153. 0.5207
|
|
33.86 0.2469 0.5311 0.0833 0.0387 3.100 24.422 18.234 2311.502 2.759 81.106 3.578 0.58 317583. 0.4953
|
|
37.25 0.2716 0.5660 0.0800 0.0384 3.073 24.211 17.512 2291.602 2.735 77.894 3.466 0.58 318037. 0.4702
|
|
40.63 0.2963 0.5981 0.0765 0.0379 3.034 23.902 16.747 2262.301 2.700 74.492 3.358 0.58 318516. 0.4454
|
|
44.02 0.3210 0.6277 0.0728 0.0373 2.982 23.491 15.943 2223.363 2.654 70.916 3.252 0.58 319020. 0.4210
|
|
47.41 0.3457 0.6547 0.0690 0.0364 2.916 22.976 15.103 2174.672 2.596 67.180 3.150 0.58 319550. 0.3969
|
|
50.79 0.3704 0.6792 0.0650 0.0355 2.838 22.358 14.231 2116.153 2.526 63.300 3.050 0.58 320105. 0.3730
|
|
54.18 0.3951 0.7012 0.0609 0.0343 2.746 21.635 13.329 2047.720 2.444 59.289 2.952 0.58 320686. 0.3494
|
|
57.56 0.4198 0.7208 0.0566 0.0330 2.641 20.806 12.400 1969.287 2.351 55.157 2.856 0.58 321293. 0.3260
|
|
60.95 0.4445 0.7376 0.0523 0.0315 2.522 19.871 11.447 1880.750 2.245 50.916 2.761 0.58 321926. 0.3028
|
|
64.34 0.4692 0.7517 0.0478 0.0299 2.390 18.828 10.471 1782.016 2.127 46.575 2.665 0.58 322584. 0.2796
|
|
67.72 0.4939 0.7626 0.0433 0.0280 2.244 17.676 9.475 1672.998 1.997 42.143 2.569 0.58 323270. 0.2563
|
|
71.11 0.5186 0.7699 0.0386 0.0260 2.083 16.415 8.460 1553.632 1.855 37.630 2.470 0.58 323982. 0.2329
|
|
74.49 0.5433 0.7728 0.0339 0.0239 1.909 15.044 7.429 1423.904 1.700 33.044 2.366 0.58 324720. 0.2091
|
|
77.88 0.5680 0.7700 0.0292 0.0215 1.722 13.564 6.384 1283.850 1.532 28.396 2.255 0.58 325485. 0.1847
|
|
81.27 0.5927 0.7595 0.0243 0.0190 1.520 11.977 5.328 1133.585 1.353 23.698 2.132 0.58 326276. 0.1595
|
|
84.65 0.6174 0.7372 0.0195 0.0163 1.305 10.284 4.263 973.331 1.162 18.962 1.987 0.59 327094. 0.1330
|
|
88.04 0.6420 0.6958 0.0146 0.0135 1.077 8.489 3.193 803.437 0.959 14.203 1.803 0.59 327938. 0.1044
|
|
91.42 0.6667 0.6180 0.0097 0.0105 0.837 6.597 2.123 624.409 0.745 9.441 1.542 0.59 328808. 0.0728
|
|
94.81 0.6914 0.4554 0.0048 0.0073 0.586 4.615 1.055 436.839 0.521 4.693 1.096 0.59 329701. 0.0365
|
|
98.20 0.7161 -0.0274 -0.0002 0.0040 0.316 2.493 -0.033 235.947 0.282 -0.147 -0.064 0.59 330463. 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 0.1074 0.0365 4.160 29.135 29.756 3102.324 3.292 132.357 4.350 0.65 353577. 0.7693
|
|
3.81 0.0247 0.0705 0.1059 0.0371 4.228 29.612 29.337 3153.130 3.346 130.491 4.220 0.65 353835. 0.7410
|
|
7.63 0.0494 0.1368 0.1042 0.0377 4.292 30.060 28.877 3200.815 3.396 128.445 4.092 0.65 354116. 0.7128
|
|
11.44 0.0741 0.1989 0.1024 0.0382 4.351 30.469 28.375 3244.380 3.442 126.210 3.967 0.65 354419. 0.6850
|
|
15.25 0.0989 0.2571 0.1004 0.0386 4.402 30.830 27.827 3282.826 3.483 123.775 3.845 0.65 354747. 0.6575
|
|
19.06 0.1236 0.3114 0.0983 0.0390 4.446 31.133 27.232 3315.094 3.517 121.129 3.726 0.65 355100. 0.6303
|
|
22.88 0.1483 0.3621 0.0960 0.0393 4.479 31.368 26.588 3340.101 3.544 118.262 3.610 0.65 355478. 0.6035
|
|
26.69 0.1730 0.4093 0.0935 0.0395 4.501 31.524 25.891 3356.672 3.562 115.162 3.498 0.65 355882. 0.5771
|
|
30.50 0.1977 0.4533 0.0907 0.0396 4.511 31.589 25.139 3363.591 3.569 111.819 3.390 0.65 356313. 0.5510
|
|
34.31 0.2224 0.4941 0.0878 0.0395 4.505 31.551 24.331 3359.615 3.565 108.224 3.285 0.65 356772. 0.5253
|
|
38.13 0.2472 0.5320 0.0847 0.0393 4.484 31.401 23.465 3343.545 3.548 104.370 3.183 0.65 357258. 0.4999
|
|
41.94 0.2719 0.5671 0.0814 0.0390 4.445 31.126 22.540 3314.354 3.517 100.258 3.085 0.65 357772. 0.4747
|
|
45.75 0.2966 0.5996 0.0778 0.0385 4.387 30.723 21.560 3271.366 3.471 95.898 2.989 0.65 358314. 0.4500
|
|
49.56 0.3213 0.6294 0.0741 0.0378 4.310 30.186 20.528 3214.246 3.410 91.310 2.897 0.65 358884. 0.4255
|
|
53.38 0.3460 0.6568 0.0702 0.0370 4.215 29.516 19.450 3142.842 3.335 86.513 2.807 0.65 359483. 0.4013
|
|
57.19 0.3707 0.6818 0.0662 0.0360 4.100 28.710 18.329 3057.056 3.244 81.527 2.719 0.65 360111. 0.3774
|
|
61.00 0.3955 0.7044 0.0620 0.0348 3.965 27.768 17.169 2956.794 3.137 76.369 2.634 0.65 360767. 0.3538
|
|
64.82 0.4202 0.7244 0.0577 0.0334 3.811 26.690 15.974 2841.936 3.015 71.054 2.549 0.65 361452. 0.3303
|
|
68.63 0.4449 0.7420 0.0532 0.0319 3.637 25.473 14.747 2712.355 2.878 65.595 2.466 0.65 362167. 0.3070
|
|
72.44 0.4696 0.7567 0.0487 0.0302 3.444 24.116 13.491 2567.910 2.725 60.006 2.383 0.65 362911. 0.2837
|
|
76.25 0.4943 0.7685 0.0441 0.0283 3.230 22.619 12.207 2408.493 2.555 54.298 2.299 0.65 363685. 0.2604
|
|
80.07 0.5190 0.7768 0.0393 0.0263 2.996 20.980 10.900 2234.001 2.370 48.483 2.213 0.65 364488. 0.2369
|
|
83.88 0.5437 0.7808 0.0345 0.0241 2.742 19.200 9.571 2044.427 2.169 42.572 2.123 0.66 365321. 0.2130
|
|
87.69 0.5685 0.7794 0.0297 0.0216 2.467 17.278 8.224 1839.819 1.952 36.580 2.027 0.66 366184. 0.1885
|
|
91.50 0.5932 0.7705 0.0248 0.0191 2.173 15.217 6.862 1620.352 1.719 30.520 1.921 0.66 367077. 0.1631
|
|
95.32 0.6179 0.7503 0.0198 0.0163 1.859 13.020 5.488 1386.345 1.471 24.410 1.795 0.66 367999. 0.1364
|
|
99.13 0.6426 0.7113 0.0148 0.0134 1.527 10.690 4.107 1138.311 1.208 18.270 1.637 0.66 368951. 0.1075
|
|
102.94 0.6673 0.6361 0.0098 0.0103 1.176 8.236 2.725 876.991 0.931 12.123 1.410 0.66 369932. 0.0754
|
|
106.76 0.6920 0.4740 0.0049 0.0071 0.809 5.665 1.347 603.264 0.640 5.992 1.013 0.66 370938. 0.0381
|
|
110.57 0.7168 -0.0566 -0.0003 0.0036 0.410 2.871 -0.079 305.728 0.324 -0.350 -0.117 0.66 371679. 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 0.1091 0.0375 5.861 36.943 37.313 4370.785 4.174 165.969 3.872 0.72 392805. 0.7668
|
|
4.27 0.0249 0.0704 0.1076 0.0381 5.953 37.520 36.803 4439.061 4.239 163.701 3.760 0.72 393095. 0.7396
|
|
8.54 0.0498 0.1366 0.1060 0.0386 6.039 38.061 36.241 4503.101 4.300 161.199 3.650 0.72 393410. 0.7124
|
|
12.80 0.0747 0.1988 0.1041 0.0391 6.117 38.555 35.623 4561.523 4.356 158.450 3.542 0.72 393752. 0.6853
|
|
17.07 0.0996 0.2572 0.1022 0.0396 6.186 38.990 34.946 4612.926 4.405 155.440 3.436 0.72 394121. 0.6585
|
|
21.34 0.1245 0.3118 0.1000 0.0399 6.244 39.352 34.207 4655.840 4.446 152.154 3.332 0.72 394519. 0.6318
|
|
25.61 0.1494 0.3628 0.0977 0.0402 6.288 39.630 33.403 4688.702 4.477 148.578 3.231 0.72 394946. 0.6054
|
|
29.88 0.1743 0.4103 0.0951 0.0404 6.316 39.809 32.531 4709.818 4.498 144.699 3.133 0.72 395403. 0.5793
|
|
34.14 0.1992 0.4546 0.0924 0.0405 6.326 39.873 31.588 4717.426 4.505 140.502 3.037 0.72 395890. 0.5534
|
|
38.41 0.2241 0.4958 0.0894 0.0404 6.316 39.807 30.570 4709.691 4.497 135.977 2.944 0.72 396408. 0.5277
|
|
42.68 0.2490 0.5340 0.0862 0.0402 6.282 39.597 29.477 4684.824 4.474 131.116 2.854 0.72 396958. 0.5023
|
|
46.95 0.2739 0.5694 0.0828 0.0398 6.224 39.229 28.309 4641.272 4.432 125.918 2.766 0.72 397538. 0.4772
|
|
51.21 0.2988 0.6021 0.0791 0.0393 6.139 38.694 27.068 4577.989 4.372 120.399 2.682 0.72 398151. 0.4523
|
|
55.48 0.3237 0.6323 0.0753 0.0386 6.027 37.988 25.761 4494.433 4.292 114.584 2.600 0.72 398795. 0.4278
|
|
59.75 0.3486 0.6601 0.0713 0.0377 5.888 37.109 24.393 4390.375 4.192 108.498 2.520 0.72 399472. 0.4035
|
|
64.02 0.3735 0.6854 0.0672 0.0366 5.720 36.055 22.969 4265.693 4.073 102.168 2.442 0.72 400180. 0.3795
|
|
68.29 0.3984 0.7084 0.0628 0.0353 5.525 34.826 21.496 4120.278 3.935 95.615 2.366 0.72 400922. 0.3557
|
|
72.55 0.4233 0.7289 0.0584 0.0339 5.302 33.420 19.978 3953.997 3.776 88.860 2.292 0.72 401696. 0.3321
|
|
76.82 0.4482 0.7469 0.0538 0.0323 5.051 31.837 18.417 3766.678 3.597 81.921 2.218 0.73 402502. 0.3085
|
|
81.09 0.4731 0.7622 0.0492 0.0305 4.772 30.074 16.819 3558.150 3.398 74.813 2.144 0.73 403342. 0.2851
|
|
85.36 0.4980 0.7745 0.0444 0.0286 4.463 28.131 15.187 3328.248 3.178 67.551 2.070 0.73 404215. 0.2615
|
|
89.63 0.5229 0.7833 0.0395 0.0264 4.126 26.006 13.523 3076.862 2.938 60.152 1.994 0.73 405121. 0.2377
|
|
93.89 0.5478 0.7878 0.0346 0.0241 3.760 23.700 11.832 2803.976 2.678 52.629 1.914 0.73 406061. 0.2134
|
|
98.16 0.5727 0.7868 0.0296 0.0215 3.366 21.213 10.117 2509.739 2.397 45.002 1.828 0.73 407034. 0.1885
|
|
102.43 0.5976 0.7780 0.0245 0.0188 2.943 18.549 8.383 2194.514 2.096 37.287 1.733 0.73 408040. 0.1626
|
|
106.70 0.6225 0.7572 0.0194 0.0159 2.493 15.712 6.634 1858.940 1.775 29.509 1.619 0.73 409080. 0.1352
|
|
110.96 0.6474 0.7155 0.0143 0.0129 2.017 12.712 4.877 1504.025 1.436 21.692 1.471 0.73 410152. 0.1053
|
|
115.23 0.6723 0.6316 0.0091 0.0097 1.517 9.561 3.118 1131.195 1.080 13.868 1.250 0.73 411257. 0.0716
|
|
119.50 0.6972 0.4367 0.0040 0.0064 0.995 6.272 1.364 742.076 0.709 6.067 0.834 0.74 412387. 0.0316
|
|
123.77 0.7221
|
|
|
|
|
|
|
|
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 0.1110 0.0402 8.365 47.929 45.948 6237.632 5.415 204.375 3.341 0.79 432008. 0.7342
|
|
4.69 0.0249 0.0670 0.1096 0.0407 8.464 48.500 45.355 6311.947 5.480 201.738 3.259 0.79 432326. 0.7115
|
|
9.38 0.0498 0.1307 0.1080 0.0411 8.555 49.019 44.696 6379.527 5.538 198.806 3.178 0.79 432674. 0.6887
|
|
14.08 0.0747 0.1911 0.1062 0.0415 8.635 49.475 43.967 6438.764 5.590 195.563 3.097 0.79 433051. 0.6657
|
|
18.77 0.0995 0.2483 0.1043 0.0418 8.701 49.853 43.163 6488.040 5.632 191.989 3.017 0.79 433459. 0.6427
|
|
23.46 0.1244 0.3022 0.1022 0.0421 8.751 50.142 42.280 6525.640 5.665 188.063 2.939 0.79 433899. 0.6195
|
|
28.15 0.1493 0.3531 0.0998 0.0422 8.783 50.328 41.315 6549.786 5.686 183.768 2.861 0.79 434371. 0.5962
|
|
32.84 0.1742 0.4009 0.0973 0.0423 8.795 50.395 40.263 6558.578 5.694 179.088 2.784 0.79 434877. 0.5728
|
|
37.53 0.1991 0.4457 0.0945 0.0422 8.784 50.329 39.120 6549.958 5.686 174.004 2.709 0.79 435416. 0.5493
|
|
42.23 0.2240 0.4877 0.0915 0.0420 8.746 50.112 37.883 6521.763 5.662 168.503 2.635 0.79 435989. 0.5257
|
|
46.92 0.2488 0.5269 0.0883 0.0417 8.679 49.729 36.550 6471.822 5.618 162.575 2.562 0.79 436597. 0.5020
|
|
51.61 0.2737 0.5633 0.0849 0.0412 8.580 49.163 35.121 6398.157 5.554 156.220 2.490 0.79 437239. 0.4783
|
|
56.30 0.2986 0.5971 0.0812 0.0406 8.448 48.404 33.601 6299.390 5.469 149.456 2.419 0.79 437916. 0.4546
|
|
60.99 0.3235 0.6284 0.0773 0.0398 8.280 47.446 31.995 6174.730 5.360 142.313 2.350 0.79 438628. 0.4310
|
|
65.68 0.3484 0.6572 0.0732 0.0388 8.078 46.286 30.311 6023.749 5.229 134.824 2.282 0.79 439376. 0.4073
|
|
70.38 0.3733 0.6836 0.0690 0.0377 7.840 44.921 28.557 5846.122 5.075 127.023 2.216 0.80 440159. 0.3838
|
|
75.07 0.3981 0.7075 0.0646 0.0364 7.565 43.349 26.739 5641.523 4.898 118.937 2.150 0.80 440977. 0.3604
|
|
79.76 0.4230 0.7289 0.0601 0.0349 7.254 41.566 24.864 5409.546 4.696 110.593 2.085 0.80 441831. 0.3370
|
|
84.45 0.4479 0.7479 0.0554 0.0332 6.906 39.570 22.935 5149.737 4.471 102.014 2.020 0.80 442721. 0.3136
|
|
89.14 0.4728 0.7641 0.0506 0.0313 6.520 37.359 20.958 4861.978 4.221 93.220 1.955 0.80 443647. 0.2902
|
|
93.83 0.4977 0.7772 0.0458 0.0293 6.096 34.931 18.937 4545.979 3.946 84.230 1.889 0.80 444609. 0.2665
|
|
98.53 0.5226 0.7869 0.0408 0.0271 5.634 32.284 16.875 4201.587 3.647 75.062 1.822 0.80 445607. 0.2426
|
|
103.22 0.5475 0.7922 0.0357 0.0247 5.135 29.422 14.779 3829.063 3.324 65.736 1.751 0.80 446642. 0.2182
|
|
107.91 0.5723 0.7916 0.0306 0.0221 4.599 26.349 12.651 3429.139 2.977 56.272 1.673 0.80 447713. 0.1929
|
|
112.60 0.5972 0.7827 0.0254 0.0194 4.027 23.075 10.497 3003.014 2.607 46.692 1.585 0.80 448821. 0.1665
|
|
117.29 0.6221 0.7606 0.0201 0.0165 3.423 19.613 8.324 2552.433 2.216 37.023 1.479 0.81 449965. 0.1383
|
|
121.98 0.6470 0.7158 0.0148 0.0134 2.789 15.980 6.137 2079.747 1.805 27.297 1.338 0.81 451145. 0.1075
|
|
126.68 0.6719 0.6259 0.0095 0.0102 2.130 12.202 3.946 1588.001 1.379 17.551 1.127 0.81 452360. 0.0726
|
|
131.37 0.6968 0.4250 0.0042 0.0070 1.449 8.303 1.758 1080.557 0.938 7.821 0.738 0.81 453603. 0.0317
|
|
136.06 0.7216
|
|
|
|
|
|
|
|
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 0.1130 0.0465 12.564 65.992 55.633 9369.118 7.456 247.458 2.693 0.86 471183. 0.6512
|
|
5.09 0.0247 0.0590 0.1116 0.0468 12.647 66.424 54.982 9430.548 7.505 244.559 2.644 0.86 471527. 0.6357
|
|
10.18 0.0495 0.1158 0.1101 0.0471 12.710 66.757 54.249 9477.806 7.542 241.300 2.596 0.86 471903. 0.6199
|
|
15.26 0.0742 0.1705 0.1085 0.0472 12.752 66.977 53.430 9509.025 7.567 237.656 2.549 0.86 472312. 0.6039
|
|
20.35 0.0990 0.2232 0.1066 0.0473 12.770 67.073 52.518 9522.633 7.578 233.600 2.501 0.86 472755. 0.5877
|
|
25.44 0.1237 0.2738 0.1046 0.0472 12.763 67.035 51.508 9517.167 7.574 229.108 2.455 0.86 473234. 0.5711
|
|
30.53 0.1484 0.3223 0.1023 0.0471 12.728 66.851 50.395 9491.043 7.553 224.156 2.408 0.86 473747. 0.5542
|
|
35.62 0.1732 0.3688 0.0998 0.0469 12.663 66.511 49.173 9442.801 7.514 218.721 2.362 0.86 474298. 0.5369
|
|
40.71 0.1979 0.4132 0.0971 0.0465 12.566 66.004 47.838 9370.834 7.457 212.784 2.315 0.86 474885. 0.5192
|
|
45.79 0.2226 0.4555 0.0942 0.0460 12.435 65.315 46.386 9273.109 7.379 206.324 2.269 0.86 475510. 0.5009
|
|
50.88 0.2474 0.4956 0.0910 0.0454 12.267 64.431 44.813 9147.501 7.279 199.328 2.222 0.86 476172. 0.4822
|
|
55.97 0.2721 0.5337 0.0875 0.0446 12.059 63.337 43.119 8992.246 7.156 191.793 2.175 0.86 476871. 0.4630
|
|
61.06 0.2969 0.5695 0.0839 0.0437 11.809 62.028 41.308 8806.320 7.008 183.740 2.128 0.87 477609. 0.4433
|
|
66.15 0.3216 0.6032 0.0800 0.0426 11.519 60.501 39.390 8589.540 6.835 175.205 2.080 0.87 478384. 0.4232
|
|
71.23 0.3463 0.6346 0.0759 0.0414 11.187 58.757 37.372 8342.009 6.638 166.231 2.032 0.87 479197. 0.4027
|
|
76.32 0.3711 0.6637 0.0716 0.0400 10.814 56.798 35.266 8063.795 6.417 156.861 1.984 0.87 480049. 0.3819
|
|
81.41 0.3958 0.6905 0.0672 0.0385 10.399 54.620 33.078 7754.667 6.171 147.130 1.935 0.87 480938. 0.3607
|
|
86.50 0.4205 0.7149 0.0626 0.0368 9.942 52.221 30.816 7414.060 5.900 137.069 1.885 0.87 481866. 0.3393
|
|
91.59 0.4453 0.7368 0.0578 0.0350 9.442 49.595 28.486 7041.223 5.603 126.706 1.835 0.87 482832. 0.3175
|
|
96.67 0.4700 0.7560 0.0530 0.0329 8.898 46.737 26.094 6635.470 5.280 116.068 1.784 0.87 483836. 0.2954
|
|
101.76 0.4948 0.7715 0.0480 0.0308 8.317 43.684 23.645 6202.011 4.935 105.174 1.729 0.87 484879. 0.2726
|
|
106.85 0.5195 0.7822 0.0429 0.0285 7.702 40.454 21.144 5743.441 4.570 94.050 1.670 0.87 485961. 0.2489
|
|
111.94 0.5442 0.7856 0.0378 0.0262 7.065 37.108 18.595 5268.427 4.192 82.710 1.601 0.87 487082. 0.2238
|
|
117.03 0.5690 0.7816 0.0325 0.0237 6.390 33.565 16.005 4765.312 3.792 71.189 1.523 0.88 488241. 0.1976
|
|
122.12 0.5937 0.7668 0.0272 0.0210 5.682 29.842 13.380 4236.823 3.372 59.515 1.432 0.88 489440. 0.1699
|
|
127.20 0.6185 0.7360 0.0218 0.0183 4.944 25.968 10.728 3686.727 2.934 47.719 1.320 0.88 490677. 0.1401
|
|
132.29 0.6432 0.6794 0.0164 0.0155 4.183 21.973 8.057 3119.633 2.483 35.838 1.171 0.88 491953. 0.1078
|
|
137.38 0.6679 0.5782 0.0109 0.0126 3.407 17.896 5.378 2540.787 2.022 23.921 0.960 0.88 493267. 0.0722
|
|
142.47 0.6927 0.3914 0.0055 0.0097 2.623 13.776 2.702 1955.837 1.556 12.019 0.627 0.88 494614. 0.0334
|
|
147.56 0.7174 -0.0012 0.0000 0.0067 1.812 9.519 -0.006 1351.426 1.075 -0.025 -0.002 0.88 495854. 0.0000
|
|
|
|
|
|
|
|
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 0.1127 0.0541 18.567 90.017 65.127 13845.045 10.170 289.684 2.134 0.93 510451. 0.5582
|
|
5.55 0.0249 0.0511 0.1116 0.0544 18.685 90.592 64.481 13933.547 10.235 286.812 2.099 0.93 510816. 0.5464
|
|
11.10 0.0498 0.1005 0.1103 0.0547 18.780 91.054 63.750 14004.590 10.287 283.558 2.065 0.93 511216. 0.5344
|
|
16.65 0.0747 0.1482 0.1089 0.0549 18.847 91.375 62.923 14053.917 10.323 279.882 2.031 0.93 511652. 0.5222
|
|
22.20 0.0996 0.1944 0.1072 0.0550 18.878 91.526 61.992 14077.122 10.341 275.740 1.997 0.93 512126. 0.5098
|
|
27.75 0.1245 0.2390 0.1054 0.0549 18.868 91.476 60.945 14069.541 10.335 271.086 1.965 0.93 512640. 0.4972
|
|
33.30 0.1495 0.2822 0.1034 0.0548 18.809 91.195 59.774 14026.207 10.303 265.873 1.933 0.93 513193. 0.4845
|
|
38.85 0.1744 0.3240 0.1011 0.0544 18.697 90.648 58.465 13942.079 10.241 260.054 1.902 0.93 513788. 0.4715
|
|
44.40 0.1993 0.3644 0.0986 0.0539 18.523 89.805 57.011 13812.452 10.146 253.585 1.872 0.94 514426. 0.4582
|
|
49.95 0.2242 0.4036 0.0958 0.0532 18.283 88.642 55.401 13633.617 10.015 246.425 1.843 0.94 515106. 0.4447
|
|
55.50 0.2491 0.4416 0.0928 0.0523 17.974 87.143 53.631 13403.116 9.845 238.549 1.815 0.94 515829. 0.4309
|
|
61.05 0.2740 0.4784 0.0894 0.0512 17.594 85.302 51.697 13119.871 9.637 229.947 1.787 0.94 516595. 0.4166
|
|
66.60 0.2989 0.5139 0.0858 0.0499 17.144 83.121 49.604 12784.386 9.391 220.639 1.760 0.94 517404. 0.4018
|
|
72.15 0.3238 0.5481 0.0819 0.0484 16.627 80.615 47.363 12399.035 9.108 210.671 1.733 0.94 518256. 0.3865
|
|
77.70 0.3487 0.5808 0.0778 0.0467 16.049 77.809 44.988 11967.471 8.791 200.105 1.705 0.94 519151. 0.3707
|
|
83.25 0.3736 0.6120 0.0735 0.0449 15.412 74.723 42.490 11492.802 8.442 188.996 1.677 0.94 520089. 0.3544
|
|
88.81 0.3985 0.6416 0.0690 0.0429 14.721 71.371 39.882 10977.202 8.063 177.396 1.648 0.94 521068. 0.3374
|
|
94.36 0.4235 0.6692 0.0643 0.0407 13.976 67.760 37.173 10421.854 7.655 165.345 1.618 0.94 522090. 0.3198
|
|
99.91 0.4484 0.6948 0.0595 0.0384 13.179 63.898 34.372 9827.823 7.219 152.885 1.586 0.94 523155. 0.3015
|
|
105.46 0.4733 0.7180 0.0545 0.0359 12.332 59.791 31.487 9196.235 6.755 140.056 1.553 0.94 524261. 0.2825
|
|
111.01 0.4982 0.7384 0.0494 0.0333 11.436 55.445 28.529 8527.756 6.264 126.896 1.517 0.95 525410. 0.2627
|
|
116.56 0.5231 0.7529 0.0441 0.0307 10.527 51.038 25.500 7849.983 5.766 113.425 1.473 0.95 526601. 0.2412
|
|
122.11 0.5480 0.7527 0.0387 0.0282 9.689 46.976 22.397 7225.210 5.307 99.624 1.406 0.95 527834. 0.2157
|
|
127.66 0.5729 0.7350 0.0333 0.0259 8.907 43.182 19.231 6641.682 4.879 85.541 1.313 0.95 529110. 0.1867
|
|
133.21 0.5978 0.7019 0.0277 0.0236 8.109 39.314 16.023 6046.766 4.442 71.268 1.202 0.95 530428. 0.1560
|
|
138.76 0.6227 0.6477 0.0221 0.0213 7.304 35.410 12.784 5446.323 4.001 56.864 1.065 0.95 531788. 0.1234
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|
144.31 0.6476 0.5643 0.0165 0.0189 6.500 31.515 9.533 4847.248 3.561 42.402 0.892 0.95 533190. 0.0893
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|
149.86 0.6726 0.4403 0.0109 0.0166 5.708 27.672 6.289 4256.085 3.126 27.973 0.670 0.95 534632. 0.0545
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|
155.41 0.6975 0.2584 0.0053 0.0144 4.931 23.905 3.075 3676.752 2.701 13.678 0.379 0.96 536112. 0.0216
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|
160.96 0.7224 -0.0161 -0.0003 0.0120 4.123 19.988 -0.154 3074.188 2.258 -0.686 -0.023 0.96 537533. 0.0000
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