427 lines
76 KiB
Plaintext
427 lines
76 KiB
Plaintext
20x10W (20x10W.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 0.0942 0.0376 0.010 0.610 0.481 7.213 0.069 2.138 30.217 0.08 47529. 0.6145
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0.44 0.0231 0.0563 0.0926 0.0379 0.010 0.615 0.472 7.276 0.069 2.100 29.425 0.08 47560. 0.5931
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0.87 0.0461 0.1096 0.0908 0.0382 0.010 0.620 0.463 7.332 0.070 2.059 28.638 0.08 47594. 0.5716
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1.31 0.0692 0.1599 0.0889 0.0384 0.010 0.624 0.453 7.378 0.070 2.016 27.856 0.08 47630. 0.5501
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1.75 0.0922 0.2073 0.0868 0.0386 0.010 0.627 0.443 7.414 0.071 1.969 27.082 0.08 47669. 0.5287
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2.18 0.1153 0.2518 0.0846 0.0387 0.010 0.629 0.432 7.439 0.071 1.920 26.315 0.08 47710. 0.5072
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2.62 0.1383 0.2935 0.0823 0.0388 0.010 0.630 0.420 7.450 0.071 1.867 25.556 0.08 47754. 0.4858
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3.06 0.1614 0.3323 0.0799 0.0388 0.010 0.629 0.407 7.446 0.071 1.811 24.805 0.08 47801. 0.4644
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3.49 0.1844 0.3684 0.0773 0.0387 0.010 0.628 0.394 7.426 0.071 1.752 24.061 0.08 47850. 0.4431
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3.93 0.2075 0.4018 0.0745 0.0385 0.010 0.625 0.380 7.389 0.071 1.690 23.323 0.08 47903. 0.4218
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4.37 0.2305 0.4324 0.0716 0.0382 0.010 0.620 0.365 7.334 0.070 1.625 22.592 0.08 47959. 0.4006
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4.80 0.2536 0.4603 0.0686 0.0378 0.010 0.614 0.350 7.260 0.069 1.557 21.865 0.08 48017. 0.3795
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5.24 0.2766 0.4855 0.0655 0.0373 0.010 0.606 0.334 7.167 0.068 1.486 21.140 0.08 48079. 0.3585
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5.68 0.2997 0.5080 0.0623 0.0367 0.009 0.596 0.317 7.053 0.067 1.412 20.416 0.08 48144. 0.3375
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6.11 0.3227 0.5276 0.0589 0.0360 0.009 0.585 0.300 6.919 0.066 1.336 19.690 0.08 48212. 0.3166
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6.55 0.3458 0.5443 0.0555 0.0352 0.009 0.572 0.283 6.765 0.065 1.258 18.959 0.08 48283. 0.2958
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6.99 0.3688 0.5579 0.0519 0.0343 0.009 0.557 0.265 6.589 0.063 1.177 18.218 0.08 48358. 0.2749
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7.42 0.3919 0.5682 0.0483 0.0333 0.009 0.540 0.246 6.391 0.061 1.094 17.463 0.08 48436. 0.2541
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7.86 0.4149 0.5749 0.0445 0.0321 0.008 0.522 0.227 6.171 0.059 1.010 16.687 0.08 48517. 0.2333
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8.30 0.4380 0.5776 0.0407 0.0309 0.008 0.501 0.208 5.929 0.057 0.924 15.884 0.08 48602. 0.2124
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8.73 0.4610 0.5759 0.0368 0.0295 0.008 0.479 0.188 5.664 0.054 0.836 15.044 0.08 48690. 0.1913
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9.17 0.4841 0.5688 0.0329 0.0280 0.007 0.454 0.168 5.376 0.051 0.746 14.153 0.08 48781. 0.1701
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9.60 0.5071 0.5556 0.0289 0.0264 0.007 0.428 0.147 5.065 0.048 0.655 13.194 0.08 48876. 0.1486
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10.04 0.5302 0.5346 0.0248 0.0246 0.006 0.400 0.127 4.730 0.045 0.563 12.144 0.08 48974. 0.1268
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10.48 0.5532 0.5038 0.0207 0.0228 0.006 0.370 0.106 4.373 0.042 0.470 10.968 0.08 49076. 0.1046
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10.91 0.5763 0.4603 0.0166 0.0208 0.005 0.337 0.085 3.993 0.038 0.377 9.619 0.08 49181. 0.0821
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11.35 0.5993 0.3991 0.0124 0.0187 0.005 0.303 0.063 3.590 0.034 0.282 8.020 0.08 49290. 0.0593
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11.79 0.6224 0.3126 0.0083 0.0165 0.004 0.268 0.042 3.166 0.030 0.188 6.050 0.08 49402. 0.0365
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12.22 0.6454 0.1875 0.0041 0.0142 0.004 0.230 0.021 2.722 0.026 0.093 3.499 0.08 49517. 0.0149
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12.66 0.6685 -0.0031 -0.0001 0.0117 0.003 0.191 0.000 2.255 0.022 -0.001 -0.056 0.08 49629. 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 0.0947 0.0341 0.070 2.216 1.932 52.435 0.250 8.593 16.711 0.16 95057. 0.6814
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0.88 0.0231 0.0624 0.0930 0.0345 0.071 2.240 1.898 52.995 0.253 8.441 16.243 0.16 95119. 0.6565
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1.75 0.0463 0.1213 0.0913 0.0348 0.072 2.261 1.861 53.495 0.255 8.278 15.780 0.16 95187. 0.6316
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2.63 0.0694 0.1767 0.0893 0.0351 0.072 2.279 1.822 53.924 0.257 8.104 15.325 0.16 95259. 0.6069
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3.51 0.0926 0.2287 0.0873 0.0353 0.073 2.293 1.780 54.269 0.259 7.918 14.878 0.16 95337. 0.5824
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4.38 0.1157 0.2775 0.0851 0.0355 0.073 2.304 1.735 54.519 0.260 7.719 14.438 0.16 95420. 0.5580
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5.26 0.1389 0.3230 0.0828 0.0356 0.073 2.310 1.688 54.660 0.261 7.508 14.007 0.16 95509. 0.5339
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6.14 0.1620 0.3655 0.0803 0.0356 0.073 2.311 1.638 54.681 0.261 7.284 13.583 0.16 95603. 0.5100
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7.01 0.1852 0.4049 0.0777 0.0355 0.073 2.306 1.584 54.569 0.261 7.047 13.168 0.16 95703. 0.4863
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7.89 0.2083 0.4414 0.0749 0.0354 0.073 2.295 1.528 54.314 0.259 6.797 12.760 0.16 95809. 0.4628
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8.77 0.2315 0.4751 0.0720 0.0351 0.072 2.278 1.469 53.908 0.257 6.534 12.359 0.16 95921. 0.4395
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9.64 0.2546 0.5059 0.0690 0.0347 0.072 2.254 1.407 53.345 0.255 6.259 11.965 0.16 96039. 0.4164
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10.52 0.2778 0.5340 0.0658 0.0343 0.071 2.224 1.343 52.619 0.251 5.974 11.577 0.16 96163. 0.3936
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11.40 0.3009 0.5593 0.0626 0.0337 0.069 2.186 1.276 51.725 0.247 5.677 11.193 0.16 96294. 0.3710
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12.27 0.3241 0.5818 0.0592 0.0330 0.068 2.141 1.208 50.660 0.242 5.371 10.812 0.16 96431. 0.3486
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13.15 0.3472 0.6015 0.0557 0.0322 0.066 2.088 1.137 49.419 0.236 5.056 10.432 0.16 96575. 0.3263
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14.03 0.3703 0.6182 0.0522 0.0312 0.064 2.028 1.064 47.997 0.229 4.731 10.052 0.16 96725. 0.3042
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14.91 0.3935 0.6318 0.0485 0.0302 0.062 1.960 0.989 46.390 0.221 4.399 9.669 0.16 96882. 0.2821
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15.78 0.4166 0.6421 0.0447 0.0290 0.060 1.885 0.912 44.595 0.213 4.059 9.280 0.16 97046. 0.2601
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16.66 0.4398 0.6487 0.0409 0.0277 0.057 1.801 0.834 42.609 0.203 3.711 8.882 0.16 97216. 0.2380
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17.54 0.4629 0.6510 0.0370 0.0263 0.054 1.709 0.755 40.428 0.193 3.358 8.469 0.16 97394. 0.2159
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18.41 0.4861 0.6485 0.0330 0.0248 0.051 1.608 0.674 38.051 0.182 2.998 8.034 0.16 97578. 0.1935
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19.29 0.5092 0.6400 0.0290 0.0231 0.048 1.499 0.592 35.476 0.169 2.633 7.568 0.16 97769. 0.1708
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20.17 0.5324 0.6240 0.0250 0.0213 0.044 1.382 0.509 32.702 0.156 2.264 7.058 0.16 97967. 0.1477
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21.04 0.5555 0.5981 0.0208 0.0194 0.040 1.257 0.425 29.732 0.142 1.890 6.483 0.16 98172. 0.1240
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21.92 0.5787 0.5585 0.0167 0.0173 0.036 1.123 0.340 26.568 0.127 1.514 5.812 0.16 98384. 0.0995
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22.80 0.6018 0.4988 0.0125 0.0151 0.031 0.981 0.255 23.215 0.111 1.136 4.991 0.16 98603. 0.0740
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23.67 0.6250 0.4074 0.0084 0.0128 0.026 0.832 0.170 19.679 0.094 0.758 3.926 0.16 98829. 0.0475
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24.55 0.6481 0.2607 0.0042 0.0104 0.021 0.675 0.085 15.969 0.076 0.379 2.423 0.16 99060. 0.0208
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25.43 0.6713 -0.0009 0.0000 0.0078 0.016 0.509 0.000 12.052 0.058 -0.001 -0.008 0.16 99276. 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 0.0952 0.0329 0.228 4.799 4.370 170.321 0.542 19.439 11.638 0.24 142580. 0.7138
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1.32 0.0232 0.0653 0.0936 0.0332 0.231 4.854 4.294 172.300 0.548 19.098 11.303 0.24 142674. 0.6871
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2.64 0.0464 0.1268 0.0918 0.0336 0.233 4.904 4.211 174.076 0.554 18.731 10.972 0.24 142776. 0.6606
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3.95 0.0696 0.1846 0.0898 0.0339 0.235 4.948 4.123 175.609 0.559 18.338 10.648 0.24 142885. 0.6343
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5.27 0.0928 0.2388 0.0878 0.0341 0.237 4.983 4.028 176.856 0.563 17.917 10.331 0.24 143003. 0.6083
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6.59 0.1160 0.2895 0.0856 0.0343 0.238 5.009 3.927 177.775 0.566 17.469 10.020 0.24 143128. 0.5826
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7.91 0.1392 0.3369 0.0832 0.0344 0.239 5.024 3.820 178.324 0.568 16.991 9.716 0.24 143261. 0.5571
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9.23 0.1624 0.3810 0.0808 0.0344 0.239 5.028 3.706 178.458 0.568 16.484 9.419 0.24 143403. 0.5320
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10.55 0.1856 0.4220 0.0781 0.0344 0.239 5.019 3.585 178.135 0.567 15.947 9.129 0.24 143554. 0.5071
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11.86 0.2088 0.4600 0.0754 0.0342 0.238 4.996 3.458 177.319 0.564 15.381 8.845 0.24 143714. 0.4826
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13.18 0.2320 0.4951 0.0724 0.0339 0.236 4.958 3.324 175.982 0.560 14.787 8.568 0.24 143883. 0.4583
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14.50 0.2552 0.5274 0.0694 0.0336 0.233 4.905 3.185 174.100 0.554 14.165 8.297 0.24 144061. 0.4344
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15.82 0.2784 0.5569 0.0662 0.0331 0.230 4.836 3.039 171.657 0.546 13.518 8.030 0.24 144248. 0.4107
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17.14 0.3016 0.5836 0.0629 0.0325 0.226 4.751 2.888 168.633 0.537 12.847 7.769 0.24 144445. 0.3873
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18.45 0.3248 0.6076 0.0595 0.0318 0.221 4.649 2.732 165.012 0.525 12.153 7.510 0.24 144652. 0.3642
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19.77 0.3480 0.6288 0.0560 0.0310 0.216 4.530 2.572 160.779 0.512 11.438 7.255 0.24 144869. 0.3413
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21.09 0.3712 0.6472 0.0524 0.0301 0.209 4.393 2.406 155.919 0.496 10.704 7.000 0.24 145095. 0.3186
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22.41 0.3944 0.6627 0.0487 0.0290 0.202 4.238 2.237 150.417 0.479 9.950 6.745 0.24 145332. 0.2960
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23.73 0.4176 0.6749 0.0450 0.0278 0.193 4.064 2.064 144.261 0.459 9.179 6.489 0.24 145578. 0.2735
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25.05 0.4408 0.6837 0.0411 0.0265 0.184 3.872 1.887 137.437 0.437 8.393 6.227 0.24 145835. 0.2510
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26.36 0.4640 0.6886 0.0372 0.0251 0.174 3.661 1.707 129.937 0.414 7.591 5.958 0.24 146102. 0.2283
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27.68 0.4872 0.6888 0.0332 0.0235 0.163 3.430 1.524 121.752 0.388 6.777 5.676 0.24 146380. 0.2055
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29.00 0.5104 0.6834 0.0292 0.0218 0.151 3.180 1.338 112.879 0.359 5.950 5.375 0.24 146668. 0.1824
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30.32 0.5336 0.6708 0.0251 0.0199 0.139 2.911 1.150 103.317 0.329 5.114 5.047 0.24 146966. 0.1588
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31.64 0.5568 0.6487 0.0209 0.0180 0.125 2.622 0.960 93.068 0.296 4.269 4.677 0.24 147275. 0.1344
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32.95 0.5800 0.6129 0.0167 0.0158 0.110 2.314 0.768 82.145 0.261 3.418 4.242 0.24 147595. 0.1091
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34.27 0.6032 0.5563 0.0126 0.0136 0.095 1.988 0.576 70.564 0.225 2.562 3.703 0.24 147925. 0.0825
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35.59 0.6264 0.4651 0.0084 0.0113 0.078 1.644 0.383 58.349 0.186 1.706 2.981 0.24 148264. 0.0542
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36.91 0.6496 0.3081 0.0042 0.0088 0.061 1.283 0.191 45.528 0.145 0.850 1.904 0.24 148612. 0.0244
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38.23 0.6728 -0.0077 -0.0001 0.0062 0.043 0.899 -0.003 31.913 0.102 -0.014 -0.046 0.24 148922. 0.0000
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PROP RPM = 4000
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V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
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(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
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0.00 0.0000 0.0000 0.0959 0.0323 0.532 8.385 7.824 396.816 0.947 34.799 8.943 0.32 190097. 0.7338
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1.76 0.0232 0.0670 0.0942 0.0327 0.539 8.487 7.687 401.654 0.959 34.191 8.680 0.32 190224. 0.7061
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3.52 0.0465 0.1300 0.0924 0.0330 0.544 8.579 7.540 406.007 0.969 33.537 8.423 0.32 190360. 0.6786
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5.28 0.0697 0.1892 0.0905 0.0333 0.550 8.659 7.382 409.771 0.978 32.836 8.171 0.32 190506. 0.6514
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7.04 0.0929 0.2446 0.0884 0.0336 0.554 8.724 7.213 412.847 0.986 32.086 7.925 0.32 190663. 0.6245
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8.80 0.1162 0.2965 0.0862 0.0338 0.557 8.772 7.033 415.133 0.991 31.285 7.685 0.32 190831. 0.5979
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10.56 0.1394 0.3449 0.0839 0.0339 0.559 8.801 6.842 416.525 0.994 30.432 7.450 0.32 191010. 0.5717
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12.32 0.1626 0.3901 0.0814 0.0339 0.559 8.810 6.638 416.917 0.995 29.525 7.221 0.32 191200. 0.5458
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14.08 0.1859 0.4320 0.0787 0.0339 0.558 8.795 6.422 416.207 0.994 28.565 6.999 0.32 191402. 0.5203
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15.84 0.2091 0.4709 0.0759 0.0337 0.556 8.754 6.194 414.304 0.989 27.552 6.781 0.32 191616. 0.4952
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17.60 0.2323 0.5069 0.0730 0.0335 0.551 8.688 5.955 411.139 0.982 26.488 6.570 0.32 191842. 0.4703
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19.36 0.2556 0.5401 0.0699 0.0331 0.545 8.593 5.705 406.659 0.971 25.375 6.363 0.32 192080. 0.4459
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21.12 0.2788 0.5705 0.0667 0.0326 0.538 8.469 5.444 400.816 0.957 24.216 6.161 0.32 192332. 0.4217
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22.88 0.3020 0.5981 0.0634 0.0320 0.528 8.316 5.174 393.569 0.940 23.013 5.963 0.32 192595. 0.3979
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24.64 0.3253 0.6231 0.0600 0.0313 0.516 8.133 4.894 384.878 0.919 21.770 5.768 0.32 192872. 0.3744
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26.40 0.3485 0.6454 0.0565 0.0305 0.502 7.918 4.606 374.704 0.895 20.489 5.576 0.32 193162. 0.3511
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28.16 0.3717 0.6649 0.0528 0.0295 0.487 7.671 4.310 363.010 0.867 19.172 5.386 0.32 193465. 0.3280
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29.92 0.3950 0.6816 0.0491 0.0285 0.469 7.391 4.007 349.762 0.835 17.822 5.196 0.32 193782. 0.3051
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31.68 0.4182 0.6952 0.0453 0.0273 0.449 7.077 3.696 334.926 0.800 16.440 5.005 0.32 194112. 0.2823
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33.44 0.4414 0.7056 0.0414 0.0259 0.427 6.730 3.379 318.475 0.760 15.030 4.812 0.32 194455. 0.2595
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35.20 0.4647 0.7122 0.0375 0.0244 0.403 6.347 3.056 300.384 0.717 13.593 4.615 0.32 194813. 0.2367
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36.96 0.4879 0.7144 0.0334 0.0228 0.376 5.930 2.728 280.634 0.670 12.133 4.409 0.32 195184. 0.2136
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38.72 0.5111 0.7113 0.0294 0.0211 0.348 5.477 2.395 259.215 0.619 10.652 4.190 0.32 195569. 0.1902
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40.48 0.5344 0.7014 0.0252 0.0192 0.317 4.989 2.057 236.125 0.564 9.152 3.952 0.32 195968. 0.1663
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42.24 0.5576 0.6823 0.0210 0.0172 0.283 4.466 1.717 211.375 0.505 7.637 3.684 0.32 196382. 0.1416
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44.00 0.5809 0.6498 0.0168 0.0151 0.248 3.909 1.374 184.990 0.442 6.111 3.368 0.32 196809. 0.1158
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45.76 0.6041 0.5965 0.0126 0.0128 0.211 3.318 1.029 157.011 0.375 4.578 2.973 0.32 197250. 0.0885
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47.52 0.6273 0.5070 0.0084 0.0104 0.171 2.694 0.684 127.499 0.304 3.042 2.433 0.32 197704. 0.0590
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49.28 0.6506 0.3445 0.0042 0.0079 0.129 2.040 0.339 96.520 0.230 1.509 1.595 0.32 198168. 0.0273
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51.04 0.6738 -0.0182 -0.0001 0.0052 0.085 1.339 -0.011 63.387 0.151 -0.051 -0.081 0.32 198554. 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 0.0967 0.0321 1.034 13.029 12.332 770.763 1.472 54.853 7.257 0.40 237606. 0.7477
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2.20 0.0232 0.0680 0.0951 0.0325 1.047 13.193 12.118 780.458 1.491 53.902 7.043 0.40 237765. 0.7193
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4.40 0.0465 0.1319 0.0933 0.0329 1.058 13.341 11.888 789.187 1.507 52.879 6.833 0.40 237936. 0.6911
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6.60 0.0697 0.1919 0.0913 0.0332 1.068 13.469 11.641 796.744 1.522 51.780 6.627 0.40 238120. 0.6634
|
|
8.81 0.0930 0.2481 0.0892 0.0335 1.077 13.573 11.377 802.931 1.533 50.603 6.427 0.40 238316. 0.6359
|
|
11.01 0.1162 0.3007 0.0870 0.0336 1.083 13.651 11.094 807.546 1.542 49.346 6.231 0.40 238527. 0.6089
|
|
13.21 0.1395 0.3498 0.0847 0.0338 1.087 13.699 10.793 810.381 1.548 48.007 6.041 0.40 238751. 0.5822
|
|
15.41 0.1627 0.3956 0.0822 0.0338 1.088 13.713 10.473 811.227 1.549 46.583 5.855 0.40 238990. 0.5559
|
|
17.61 0.1860 0.4381 0.0795 0.0337 1.086 13.691 10.133 809.878 1.547 45.073 5.675 0.40 239243. 0.5300
|
|
19.81 0.2092 0.4777 0.0767 0.0336 1.081 13.628 9.775 806.154 1.540 43.479 5.500 0.40 239512. 0.5045
|
|
22.01 0.2325 0.5143 0.0737 0.0333 1.073 13.522 9.398 799.918 1.528 41.804 5.329 0.40 239795. 0.4793
|
|
24.21 0.2557 0.5481 0.0706 0.0330 1.061 13.372 9.004 791.060 1.511 40.051 5.163 0.40 240095. 0.4545
|
|
26.42 0.2789 0.5791 0.0674 0.0325 1.045 13.177 8.594 779.490 1.489 38.225 5.001 0.40 240409. 0.4301
|
|
28.62 0.3022 0.6075 0.0641 0.0319 1.026 12.934 8.168 765.125 1.461 36.331 4.842 0.40 240740. 0.4060
|
|
30.82 0.3254 0.6332 0.0606 0.0312 1.003 12.643 7.727 747.883 1.428 34.371 4.686 0.40 241087. 0.3822
|
|
33.02 0.3487 0.6562 0.0571 0.0303 0.976 12.301 7.273 727.691 1.390 32.352 4.533 0.40 241450. 0.3587
|
|
35.22 0.3719 0.6766 0.0534 0.0293 0.945 11.909 6.806 704.476 1.345 30.275 4.382 0.40 241830. 0.3354
|
|
37.42 0.3952 0.6943 0.0496 0.0283 0.909 11.464 6.328 678.168 1.295 28.145 4.232 0.40 242227. 0.3123
|
|
39.62 0.4184 0.7090 0.0458 0.0270 0.870 10.966 5.838 648.703 1.239 25.966 4.082 0.40 242640. 0.2893
|
|
41.82 0.4417 0.7206 0.0419 0.0257 0.826 10.414 5.338 616.025 1.177 23.742 3.930 0.40 243071. 0.2664
|
|
44.03 0.4649 0.7286 0.0379 0.0242 0.778 9.806 4.828 580.084 1.108 21.476 3.775 0.40 243518. 0.2434
|
|
46.23 0.4882 0.7325 0.0338 0.0225 0.725 9.143 4.310 540.846 1.033 19.172 3.615 0.40 243983. 0.2202
|
|
48.43 0.5114 0.7314 0.0297 0.0208 0.668 8.423 3.785 498.288 0.952 16.834 3.445 0.40 244466. 0.1966
|
|
50.63 0.5347 0.7238 0.0255 0.0188 0.607 7.648 3.252 452.406 0.864 14.467 3.261 0.40 244965. 0.1725
|
|
52.83 0.5579 0.7073 0.0213 0.0168 0.541 6.816 2.715 403.222 0.770 12.076 3.054 0.40 245483. 0.1476
|
|
55.03 0.5811 0.6780 0.0171 0.0146 0.470 5.930 2.173 350.785 0.670 9.667 2.810 0.40 246017. 0.1216
|
|
57.23 0.6044 0.6282 0.0128 0.0123 0.396 4.990 1.629 295.180 0.564 7.247 2.504 0.40 246569. 0.0938
|
|
59.44 0.6276 0.5418 0.0085 0.0099 0.317 3.998 1.084 236.529 0.452 4.824 2.080 0.40 247137. 0.0635
|
|
61.64 0.6509 0.3785 0.0042 0.0073 0.235 2.958 0.540 174.960 0.334 2.403 1.401 0.41 247718. 0.0302
|
|
63.84 0.6741 -0.0179 -0.0001 0.0045 0.146 1.840 -0.015 108.864 0.208 -0.068 -0.064 0.41 248180. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 6000
|
|
|
|
V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
|
|
(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
|
|
0.00 0.0000 0.0000 0.0978 0.0322 1.791 18.815 17.952 1335.617 2.126 79.851 6.096 0.48 285103. 0.7578
|
|
2.67 0.0235 0.0691 0.0961 0.0326 1.814 19.059 17.642 1352.945 2.153 78.470 5.914 0.48 285296. 0.7288
|
|
5.33 0.0469 0.1340 0.0943 0.0330 1.835 19.279 17.307 1368.530 2.178 76.979 5.736 0.48 285505. 0.7001
|
|
8.00 0.0704 0.1949 0.0923 0.0333 1.853 19.468 16.946 1381.995 2.200 75.377 5.562 0.48 285728. 0.6717
|
|
10.66 0.0938 0.2520 0.0902 0.0336 1.868 19.623 16.560 1392.982 2.217 73.658 5.392 0.48 285968. 0.6437
|
|
13.33 0.1173 0.3053 0.0880 0.0338 1.879 19.738 16.146 1401.124 2.230 71.818 5.227 0.48 286225. 0.6162
|
|
15.99 0.1407 0.3552 0.0856 0.0339 1.886 19.807 15.705 1406.049 2.238 69.856 5.066 0.48 286498. 0.5890
|
|
18.66 0.1642 0.4016 0.0830 0.0339 1.887 19.826 15.235 1407.377 2.240 67.766 4.910 0.48 286790. 0.5623
|
|
21.32 0.1876 0.4448 0.0803 0.0339 1.884 19.789 14.737 1404.740 2.236 65.549 4.758 0.48 287099. 0.5359
|
|
23.99 0.2111 0.4849 0.0774 0.0337 1.875 19.691 14.210 1397.815 2.225 63.206 4.611 0.48 287426. 0.5099
|
|
26.65 0.2345 0.5220 0.0744 0.0334 1.859 19.530 13.656 1386.354 2.206 60.741 4.468 0.48 287773. 0.4844
|
|
29.32 0.2580 0.5563 0.0712 0.0330 1.837 19.302 13.076 1370.169 2.181 58.161 4.328 0.48 288138. 0.4592
|
|
31.98 0.2814 0.5879 0.0679 0.0325 1.809 19.005 12.471 1349.096 2.147 55.472 4.193 0.48 288522. 0.4344
|
|
34.65 0.3049 0.6167 0.0645 0.0319 1.774 18.637 11.844 1322.991 2.106 52.681 4.060 0.48 288926. 0.4100
|
|
37.31 0.3283 0.6430 0.0610 0.0311 1.732 18.196 11.195 1291.715 2.056 49.794 3.931 0.48 289349. 0.3859
|
|
39.98 0.3518 0.6666 0.0573 0.0303 1.683 17.681 10.525 1255.135 1.998 46.817 3.804 0.48 289793. 0.3620
|
|
42.64 0.3753 0.6876 0.0536 0.0292 1.627 17.089 9.837 1213.121 1.931 43.756 3.678 0.48 290256. 0.3384
|
|
45.31 0.3987 0.7058 0.0497 0.0281 1.563 16.419 9.131 1165.552 1.855 40.616 3.553 0.48 290740. 0.3150
|
|
47.97 0.4222 0.7211 0.0458 0.0268 1.492 15.669 8.409 1112.317 1.770 37.404 3.429 0.48 291245. 0.2917
|
|
50.64 0.4456 0.7334 0.0418 0.0254 1.413 14.838 7.672 1053.314 1.676 34.124 3.304 0.48 291770. 0.2685
|
|
53.30 0.4691 0.7421 0.0377 0.0238 1.326 13.925 6.921 988.461 1.573 30.783 3.176 0.48 292317. 0.2451
|
|
55.97 0.4925 0.7466 0.0335 0.0221 1.231 12.928 6.157 917.697 1.461 27.386 3.043 0.48 292884. 0.2215
|
|
58.63 0.5160 0.7461 0.0293 0.0203 1.128 11.847 5.382 840.985 1.338 23.939 2.903 0.48 293473. 0.1976
|
|
61.30 0.5394 0.7390 0.0250 0.0183 1.017 10.683 4.598 758.331 1.207 20.451 2.750 0.48 294082. 0.1730
|
|
63.96 0.5629 0.7227 0.0207 0.0161 0.898 9.435 3.806 669.779 1.066 16.927 2.577 0.48 294714. 0.1475
|
|
66.63 0.5863 0.6925 0.0164 0.0139 0.772 8.106 3.008 575.431 0.916 13.379 2.371 0.48 295366. 0.1206
|
|
69.29 0.6098 0.6395 0.0120 0.0115 0.638 6.698 2.207 475.454 0.757 9.815 2.105 0.48 296039. 0.0917
|
|
71.96 0.6332 0.5431 0.0077 0.0089 0.496 5.213 1.405 370.082 0.589 6.248 1.722 0.49 296731. 0.0599
|
|
74.62 0.6567 0.3455 0.0033 0.0063 0.348 3.656 0.604 259.511 0.413 2.688 1.056 0.49 297436. 0.0241
|
|
77.29 0.6801
|
|
|
|
|
|
|
|
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 0.0991 0.0325 2.872 25.861 24.760 2141.752 2.922 110.134 5.244 0.56 332585. 0.7655
|
|
3.08 0.0233 0.0688 0.0974 0.0329 2.910 26.200 24.342 2169.822 2.960 108.274 5.088 0.56 332810. 0.7365
|
|
6.17 0.0465 0.1334 0.0956 0.0333 2.944 26.505 23.890 2195.090 2.995 106.264 4.936 0.56 333052. 0.7079
|
|
9.25 0.0698 0.1941 0.0937 0.0337 2.973 26.769 23.404 2216.958 3.024 104.100 4.788 0.56 333311. 0.6796
|
|
12.33 0.0930 0.2510 0.0916 0.0339 2.997 26.985 22.881 2234.850 3.049 101.776 4.644 0.56 333590. 0.6517
|
|
15.41 0.1163 0.3043 0.0893 0.0341 3.015 27.146 22.322 2248.190 3.067 99.287 4.503 0.56 333887. 0.6242
|
|
18.50 0.1395 0.3541 0.0870 0.0343 3.026 27.245 21.724 2256.387 3.078 96.629 4.367 0.56 334205. 0.5971
|
|
21.58 0.1628 0.4006 0.0844 0.0343 3.029 27.275 21.088 2258.848 3.081 93.798 4.234 0.56 334542. 0.5705
|
|
24.66 0.1860 0.4439 0.0817 0.0342 3.024 27.228 20.412 2254.986 3.076 90.792 4.106 0.56 334900. 0.5442
|
|
27.74 0.2093 0.4842 0.0788 0.0341 3.010 27.099 19.697 2244.286 3.062 87.612 3.981 0.56 335279. 0.5183
|
|
30.83 0.2325 0.5216 0.0758 0.0338 2.986 26.882 18.944 2226.347 3.037 84.264 3.859 0.56 335679. 0.4928
|
|
33.91 0.2558 0.5562 0.0727 0.0334 2.951 26.575 18.156 2200.857 3.002 80.757 3.742 0.56 336101. 0.4677
|
|
36.99 0.2790 0.5882 0.0694 0.0329 2.907 26.173 17.333 2167.580 2.957 77.099 3.627 0.56 336545. 0.4430
|
|
40.07 0.3023 0.6176 0.0660 0.0323 2.851 25.674 16.479 2126.282 2.901 73.300 3.515 0.56 337012. 0.4187
|
|
43.16 0.3255 0.6444 0.0624 0.0315 2.785 25.076 15.596 2076.762 2.833 69.369 3.406 0.56 337500. 0.3946
|
|
46.24 0.3488 0.6687 0.0588 0.0307 2.707 24.376 14.684 2018.809 2.754 65.313 3.299 0.56 338012. 0.3709
|
|
49.32 0.3720 0.6905 0.0550 0.0296 2.618 23.572 13.746 1952.225 2.663 61.141 3.194 0.56 338547. 0.3474
|
|
52.40 0.3953 0.7097 0.0512 0.0285 2.517 22.662 12.783 1876.823 2.560 56.860 3.089 0.56 339104. 0.3241
|
|
55.49 0.4185 0.7262 0.0472 0.0272 2.404 21.643 11.798 1792.427 2.445 52.478 2.986 0.56 339686. 0.3009
|
|
58.57 0.4418 0.7398 0.0432 0.0258 2.278 20.513 10.792 1698.879 2.318 48.003 2.881 0.56 340291. 0.2777
|
|
61.65 0.4650 0.7502 0.0391 0.0242 2.140 19.272 9.766 1596.045 2.177 43.441 2.775 0.56 340920. 0.2545
|
|
64.73 0.4883 0.7567 0.0349 0.0225 1.990 17.917 8.723 1483.821 2.024 38.801 2.666 0.56 341573. 0.2311
|
|
67.82 0.5115 0.7588 0.0307 0.0207 1.827 16.447 7.664 1362.148 1.858 34.091 2.552 0.56 342250. 0.2073
|
|
70.90 0.5348 0.7549 0.0264 0.0187 1.651 14.864 6.592 1231.018 1.679 29.321 2.429 0.56 342951. 0.1830
|
|
73.98 0.5580 0.7431 0.0220 0.0166 1.462 13.167 5.508 1090.484 1.488 24.500 2.291 0.56 343677. 0.1577
|
|
77.07 0.5813 0.7193 0.0177 0.0143 1.261 11.358 4.416 940.690 1.283 19.641 2.129 0.56 344426. 0.1313
|
|
80.15 0.6045 0.6762 0.0133 0.0119 1.049 9.441 3.318 781.875 1.067 14.757 1.925 0.57 345200. 0.1028
|
|
83.23 0.6278 0.5973 0.0089 0.0093 0.824 7.419 2.218 614.388 0.838 9.864 1.637 0.57 345996. 0.0715
|
|
86.31 0.6510 0.4377 0.0045 0.0067 0.588 5.296 1.119 438.610 0.598 4.976 1.157 0.57 346810. 0.0359
|
|
89.40 0.6743 -0.0040 0.0000 0.0038 0.335 3.015 -0.006 249.662 0.341 -0.025 -0.010 0.57 347440. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 8000
|
|
|
|
V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
|
|
(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
|
|
0.00 0.0000 0.0000 0.1007 0.0331 4.358 34.338 32.861 3250.034 3.879 146.165 4.586 0.63 380047. 0.7713
|
|
3.53 0.0233 0.0689 0.0990 0.0335 4.417 34.796 32.315 3293.440 3.931 143.738 4.450 0.63 380305. 0.7422
|
|
7.06 0.0466 0.1336 0.0972 0.0339 4.469 35.209 31.724 3332.475 3.978 141.110 4.318 0.63 380584. 0.7135
|
|
10.59 0.0699 0.1944 0.0953 0.0342 4.514 35.565 31.087 3366.210 4.018 138.274 4.189 0.63 380884. 0.6852
|
|
14.12 0.0932 0.2515 0.0932 0.0345 4.551 35.856 30.401 3393.757 4.051 135.222 4.063 0.63 381204. 0.6572
|
|
17.65 0.1165 0.3049 0.0909 0.0347 4.579 36.072 29.664 3414.211 4.075 131.946 3.941 0.64 381548. 0.6297
|
|
21.18 0.1398 0.3548 0.0885 0.0349 4.595 36.204 28.876 3426.670 4.090 128.441 3.822 0.64 381913. 0.6026
|
|
24.70 0.1631 0.4015 0.0859 0.0349 4.600 36.241 28.035 3430.230 4.095 124.701 3.707 0.64 382302. 0.5759
|
|
28.23 0.1863 0.4450 0.0832 0.0348 4.592 36.176 27.141 3423.991 4.087 120.725 3.595 0.64 382715. 0.5495
|
|
31.76 0.2096 0.4856 0.0803 0.0347 4.569 35.998 26.194 3407.159 4.067 116.513 3.487 0.64 383152. 0.5236
|
|
35.29 0.2329 0.5233 0.0772 0.0344 4.531 35.701 25.196 3379.115 4.034 112.073 3.382 0.64 383613. 0.4981
|
|
38.82 0.2562 0.5582 0.0740 0.0340 4.478 35.282 24.149 3339.406 3.986 107.417 3.280 0.64 384099. 0.4729
|
|
42.35 0.2795 0.5906 0.0707 0.0334 4.409 34.735 23.057 3287.661 3.924 102.557 3.181 0.64 384611. 0.4481
|
|
45.88 0.3028 0.6204 0.0672 0.0328 4.323 34.058 21.921 3223.563 3.848 97.506 3.084 0.64 385147. 0.4237
|
|
49.41 0.3261 0.6477 0.0636 0.0320 4.220 33.247 20.746 3146.805 3.756 92.276 2.990 0.64 385710. 0.3996
|
|
52.94 0.3494 0.6726 0.0599 0.0311 4.100 32.299 19.532 3057.094 3.649 86.879 2.898 0.64 386298. 0.3757
|
|
56.47 0.3727 0.6949 0.0560 0.0300 3.962 31.211 18.283 2954.135 3.526 81.324 2.807 0.64 386913. 0.3522
|
|
60.00 0.3960 0.7148 0.0521 0.0289 3.805 29.981 17.002 2837.652 3.387 75.623 2.718 0.64 387555. 0.3287
|
|
63.53 0.4193 0.7320 0.0481 0.0275 3.631 28.604 15.689 2707.387 3.232 69.785 2.628 0.64 388223. 0.3054
|
|
67.06 0.4426 0.7464 0.0440 0.0261 3.437 27.080 14.348 2563.098 3.059 63.820 2.539 0.64 388918. 0.2822
|
|
70.59 0.4659 0.7577 0.0398 0.0245 3.225 25.405 12.981 2404.592 2.870 57.738 2.449 0.64 389641. 0.2588
|
|
74.11 0.4892 0.7653 0.0355 0.0227 2.993 23.579 11.590 2231.716 2.664 51.551 2.355 0.64 390391. 0.2353
|
|
77.64 0.5124 0.7686 0.0312 0.0208 2.742 21.599 10.177 2044.379 2.440 45.269 2.258 0.64 391168. 0.2113
|
|
81.17 0.5357 0.7662 0.0268 0.0187 2.471 19.467 8.746 1842.569 2.199 38.904 2.153 0.64 391973. 0.1868
|
|
84.70 0.5590 0.7560 0.0224 0.0165 2.181 17.183 7.300 1626.377 1.941 32.470 2.036 0.64 392806. 0.1614
|
|
88.23 0.5823 0.7341 0.0179 0.0142 1.872 14.749 5.842 1396.024 1.666 25.983 1.898 0.65 393667. 0.1346
|
|
91.76 0.6056 0.6931 0.0134 0.0117 1.545 12.170 4.375 1151.886 1.375 19.462 1.723 0.65 394554. 0.1057
|
|
95.29 0.6289 0.6156 0.0089 0.0091 1.200 9.451 2.906 894.508 1.068 12.927 1.474 0.65 395468. 0.0737
|
|
98.82 0.6522 0.4526 0.0044 0.0064 0.837 6.598 1.438 624.469 0.745 6.398 1.045 0.65 396400. 0.0368
|
|
102.35 0.6755
|
|
|
|
|
|
|
|
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 0.1026 0.0340 6.376 44.653 42.393 4754.657 5.045 188.562 4.044 0.71 427482. 0.7725
|
|
4.00 0.0235 0.0689 0.1010 0.0344 6.458 45.228 41.702 4815.956 5.110 185.489 3.927 0.71 427777. 0.7441
|
|
8.01 0.0470 0.1339 0.0992 0.0348 6.532 45.746 40.950 4871.097 5.168 182.146 3.813 0.71 428095. 0.7159
|
|
12.01 0.0705 0.1949 0.0972 0.0351 6.596 46.193 40.136 4918.689 5.219 178.525 3.701 0.71 428438. 0.6879
|
|
16.02 0.0940 0.2522 0.0950 0.0354 6.648 46.556 39.256 4957.354 5.260 174.613 3.592 0.71 428806. 0.6602
|
|
20.02 0.1175 0.3059 0.0928 0.0356 6.686 46.823 38.309 4985.690 5.290 170.401 3.485 0.71 429199. 0.6329
|
|
24.02 0.1409 0.3561 0.0903 0.0357 6.708 46.978 37.293 5002.278 5.308 165.880 3.381 0.71 429619. 0.6058
|
|
28.03 0.1644 0.4031 0.0877 0.0358 6.713 47.010 36.206 5005.705 5.311 161.045 3.281 0.71 430065. 0.5791
|
|
32.03 0.1879 0.4469 0.0849 0.0357 6.698 46.906 35.047 4994.561 5.299 155.891 3.183 0.72 430538. 0.5528
|
|
36.04 0.2114 0.4878 0.0819 0.0355 6.662 46.652 33.818 4967.577 5.271 150.421 3.088 0.72 431039. 0.5268
|
|
40.04 0.2349 0.5258 0.0787 0.0352 6.603 46.241 32.519 4923.788 5.224 144.645 2.996 0.72 431569. 0.5012
|
|
44.04 0.2584 0.5611 0.0754 0.0347 6.521 45.665 31.156 4862.480 5.159 138.580 2.906 0.72 432126. 0.4759
|
|
48.05 0.2819 0.5939 0.0720 0.0342 6.414 44.920 29.731 4783.084 5.075 132.242 2.819 0.72 432712. 0.4510
|
|
52.05 0.3054 0.6241 0.0684 0.0335 6.283 44.000 28.249 4685.155 4.971 125.650 2.735 0.72 433328. 0.4264
|
|
56.06 0.3289 0.6518 0.0647 0.0326 6.126 42.902 26.713 4568.265 4.847 118.819 2.652 0.72 433973. 0.4022
|
|
60.06 0.3524 0.6771 0.0608 0.0317 5.943 41.623 25.127 4432.019 4.703 111.766 2.572 0.72 434647. 0.3782
|
|
64.06 0.3758 0.6999 0.0569 0.0305 5.734 40.158 23.495 4276.003 4.537 104.504 2.492 0.72 435352. 0.3544
|
|
68.07 0.3993 0.7203 0.0528 0.0293 5.498 38.503 21.818 4099.833 4.350 97.048 2.414 0.72 436087. 0.3308
|
|
72.07 0.4228 0.7381 0.0487 0.0279 5.234 36.656 20.101 3903.124 4.141 89.411 2.336 0.72 436852. 0.3073
|
|
76.08 0.4463 0.7530 0.0444 0.0263 4.942 34.612 18.347 3685.535 3.910 81.605 2.258 0.72 437648. 0.2837
|
|
80.08 0.4698 0.7649 0.0401 0.0246 4.622 32.370 16.557 3446.796 3.657 73.645 2.179 0.72 438475. 0.2601
|
|
84.08 0.4933 0.7731 0.0357 0.0228 4.273 29.927 14.735 3186.698 3.381 65.543 2.097 0.72 439334. 0.2362
|
|
88.09 0.5168 0.7769 0.0312 0.0208 3.896 27.283 12.886 2905.130 3.082 57.316 2.012 0.72 440223. 0.2119
|
|
92.09 0.5403 0.7749 0.0267 0.0186 3.489 24.437 11.012 2602.102 2.761 48.980 1.919 0.72 441144. 0.1869
|
|
96.10 0.5638 0.7648 0.0221 0.0163 3.055 21.392 9.117 2277.835 2.417 40.553 1.815 0.73 442097. 0.1608
|
|
100.10 0.5873 0.7422 0.0174 0.0138 2.592 18.152 7.207 1932.835 2.051 32.057 1.691 0.73 443081. 0.1332
|
|
104.10 0.6107 0.6980 0.0128 0.0112 2.103 14.725 5.287 1567.950 1.664 23.516 1.529 0.73 444095. 0.1032
|
|
108.11 0.6342 0.6104 0.0081 0.0085 1.588 11.123 3.363 1184.380 1.257 14.959 1.288 0.73 445138. 0.0693
|
|
112.11 0.6577 0.4100 0.0035 0.0056 1.050 7.356 1.441 783.273 0.831 6.408 0.834 0.73 446197. 0.0294
|
|
116.12 0.6812
|
|
|
|
|
|
|
|
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 0.1050 0.0366 9.412 59.322 53.526 7018.530 6.702 238.083 3.459 0.79 474879. 0.7425
|
|
4.45 0.0235 0.0658 0.1033 0.0369 9.492 59.827 52.689 7078.218 6.759 234.362 3.376 0.79 475208. 0.7190
|
|
8.89 0.0470 0.1284 0.1015 0.0371 9.560 60.257 51.774 7129.150 6.808 230.291 3.294 0.79 475565. 0.6954
|
|
13.34 0.0704 0.1878 0.0996 0.0373 9.615 60.601 50.777 7169.766 6.847 225.858 3.212 0.79 475949. 0.6716
|
|
17.78 0.0939 0.2441 0.0975 0.0375 9.653 60.843 49.696 7198.480 6.874 221.048 3.131 0.79 476361. 0.6476
|
|
22.23 0.1174 0.2974 0.0952 0.0376 9.674 60.972 48.527 7213.699 6.889 215.847 3.051 0.79 476801. 0.6236
|
|
26.68 0.1409 0.3476 0.0927 0.0376 9.674 60.972 47.267 7213.677 6.889 210.245 2.972 0.79 477271. 0.5995
|
|
31.12 0.1643 0.3948 0.0901 0.0375 9.651 60.828 45.916 7196.667 6.872 204.234 2.894 0.79 477771. 0.5753
|
|
35.57 0.1878 0.4392 0.0872 0.0373 9.603 60.525 44.471 7160.859 6.838 197.807 2.817 0.79 478302. 0.5511
|
|
40.01 0.2113 0.4808 0.0842 0.0370 9.527 60.050 42.933 7104.583 6.784 190.967 2.741 0.80 478863. 0.5269
|
|
44.46 0.2348 0.5197 0.0810 0.0366 9.423 59.390 41.305 7026.507 6.710 183.725 2.666 0.80 479455. 0.5027
|
|
48.91 0.2582 0.5559 0.0776 0.0361 9.287 58.537 39.592 6925.640 6.613 176.105 2.593 0.80 480080. 0.4787
|
|
53.35 0.2817 0.5896 0.0741 0.0354 9.120 57.485 37.798 6801.151 6.495 168.127 2.521 0.80 480735. 0.4547
|
|
57.80 0.3052 0.6208 0.0705 0.0346 8.921 56.227 35.930 6652.278 6.352 159.817 2.450 0.80 481424. 0.4308
|
|
62.24 0.3287 0.6494 0.0667 0.0337 8.687 54.756 33.992 6478.249 6.186 151.196 2.380 0.80 482144. 0.4071
|
|
66.69 0.3521 0.6757 0.0627 0.0327 8.419 53.066 31.989 6278.283 5.995 142.286 2.311 0.80 482898. 0.3835
|
|
71.14 0.3756 0.6995 0.0587 0.0315 8.115 51.150 29.924 6051.590 5.779 133.104 2.243 0.80 483684. 0.3600
|
|
75.58 0.3991 0.7208 0.0545 0.0302 7.774 49.001 27.803 5797.349 5.536 123.669 2.175 0.80 484504. 0.3365
|
|
80.03 0.4226 0.7395 0.0503 0.0287 7.396 46.613 25.629 5514.857 5.266 113.999 2.108 0.80 485357. 0.3131
|
|
84.47 0.4460 0.7555 0.0459 0.0271 6.979 43.986 23.406 5204.063 4.970 104.110 2.040 0.80 486244. 0.2896
|
|
88.92 0.4695 0.7682 0.0415 0.0253 6.524 41.118 21.137 4864.757 4.646 94.017 1.971 0.80 487166. 0.2658
|
|
93.37 0.4930 0.7773 0.0369 0.0234 6.030 38.006 18.826 4496.561 4.294 83.739 1.899 0.80 488121. 0.2417
|
|
97.81 0.5165 0.7817 0.0323 0.0214 5.498 34.655 16.478 4100.088 3.915 73.293 1.823 0.80 489112. 0.2171
|
|
102.26 0.5399 0.7797 0.0276 0.0191 4.930 31.071 14.096 3676.074 3.510 62.700 1.739 0.80 490136. 0.1916
|
|
106.71 0.5634 0.7687 0.0229 0.0168 4.326 27.265 11.687 3225.816 3.080 51.983 1.643 0.81 491195. 0.1648
|
|
111.15 0.5869 0.7435 0.0182 0.0143 3.689 23.253 9.255 2751.078 2.627 41.166 1.526 0.81 492289. 0.1362
|
|
115.60 0.6104 0.6942 0.0134 0.0117 3.023 19.053 6.808 2254.139 2.153 30.281 1.370 0.81 493416. 0.1049
|
|
120.04 0.6338 0.5979 0.0085 0.0091 2.330 14.689 4.353 1737.837 1.660 19.362 1.136 0.81 494575. 0.0695
|
|
124.49 0.6573 0.3897 0.0037 0.0063 1.616 10.184 1.897 1204.942 1.151 8.438 0.714 0.81 495752. 0.0289
|
|
128.94 0.6808
|
|
|
|
|
|
|
|
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 0.1074 0.0433 14.857 85.126 66.259 11078.593 9.618 294.719 2.713 0.87 522241. 0.6478
|
|
4.86 0.0233 0.0568 0.1059 0.0434 14.880 85.259 65.309 11095.833 9.632 290.494 2.670 0.87 522601. 0.6330
|
|
9.71 0.0466 0.1118 0.1042 0.0434 14.879 85.254 64.258 11095.243 9.632 285.821 2.627 0.87 522991. 0.6178
|
|
14.57 0.0699 0.1651 0.1023 0.0433 14.852 85.101 63.103 11075.333 9.615 280.681 2.584 0.87 523411. 0.6023
|
|
19.43 0.0932 0.2165 0.1002 0.0432 14.798 84.790 61.837 11034.772 9.579 275.052 2.542 0.87 523863. 0.5864
|
|
24.28 0.1166 0.2660 0.0980 0.0429 14.715 84.313 60.458 10972.748 9.526 268.919 2.499 0.87 524347. 0.5701
|
|
29.14 0.1399 0.3138 0.0956 0.0426 14.601 83.664 58.963 10888.246 9.452 262.269 2.456 0.87 524864. 0.5533
|
|
33.99 0.1632 0.3596 0.0930 0.0422 14.457 82.834 57.350 10780.280 9.359 255.093 2.413 0.87 525413. 0.5361
|
|
38.85 0.1865 0.4035 0.0901 0.0417 14.279 81.816 55.617 10647.738 9.243 247.384 2.369 0.87 525997. 0.5184
|
|
43.71 0.2098 0.4454 0.0871 0.0410 14.067 80.600 53.764 10489.517 9.106 239.143 2.325 0.87 526614. 0.5001
|
|
48.56 0.2331 0.4854 0.0840 0.0403 13.819 79.180 51.795 10304.754 8.946 230.384 2.280 0.88 527265. 0.4814
|
|
53.42 0.2564 0.5232 0.0806 0.0395 13.535 77.553 49.715 10092.922 8.762 221.132 2.234 0.88 527950. 0.4622
|
|
58.28 0.2797 0.5590 0.0770 0.0386 13.214 75.714 47.531 9853.601 8.554 211.419 2.188 0.88 528671. 0.4425
|
|
63.13 0.3030 0.5926 0.0733 0.0375 12.855 73.659 45.250 9586.208 8.322 201.272 2.141 0.88 529426. 0.4225
|
|
67.99 0.3263 0.6240 0.0695 0.0363 12.458 71.383 42.877 9289.965 8.065 190.719 2.093 0.88 530216. 0.4022
|
|
72.84 0.3497 0.6531 0.0655 0.0351 12.021 68.878 40.420 8963.999 7.782 179.786 2.045 0.88 531042. 0.3815
|
|
77.70 0.3730 0.6800 0.0614 0.0337 11.543 66.139 37.882 8607.539 7.472 168.500 1.996 0.88 531903. 0.3605
|
|
82.56 0.3963 0.7044 0.0572 0.0322 11.023 63.159 35.271 8219.709 7.136 156.886 1.946 0.88 532800. 0.3391
|
|
87.41 0.4196 0.7263 0.0528 0.0305 10.459 59.930 32.591 7799.510 6.771 144.967 1.895 0.88 533733. 0.3174
|
|
92.27 0.4429 0.7455 0.0484 0.0287 9.851 56.444 29.848 7345.854 6.377 132.766 1.843 0.88 534703. 0.2954
|
|
97.13 0.4662 0.7598 0.0438 0.0269 9.219 52.821 27.044 6874.269 5.968 120.292 1.784 0.88 535709. 0.2722
|
|
101.98 0.4895 0.7663 0.0392 0.0250 8.582 49.172 24.181 6399.405 5.555 107.558 1.714 0.88 536752. 0.2473
|
|
106.84 0.5128 0.7664 0.0345 0.0231 7.906 45.303 21.269 5895.831 5.118 94.604 1.636 0.88 537832. 0.2214
|
|
111.69 0.5361 0.7577 0.0297 0.0210 7.198 41.242 18.312 5367.320 4.659 81.453 1.547 0.89 538948. 0.1943
|
|
116.55 0.5594 0.7371 0.0248 0.0188 6.458 37.004 15.317 4815.829 4.181 68.131 1.443 0.89 540102. 0.1656
|
|
121.41 0.5828 0.6989 0.0199 0.0166 5.694 32.623 12.291 4245.668 3.686 54.671 1.313 0.89 541293. 0.1351
|
|
126.26 0.6061 0.6337 0.0150 0.0143 4.911 28.137 9.243 3661.838 3.179 41.112 1.145 0.89 542520. 0.1021
|
|
131.12 0.6294 0.5252 0.0100 0.0120 4.116 23.583 6.183 3069.182 2.664 27.500 0.914 0.89 543781. 0.0667
|
|
135.98 0.6527 0.3413 0.0051 0.0097 3.316 19.001 3.122 2472.851 2.147 13.885 0.573 0.89 545070. 0.0297
|
|
140.83 0.6760 0.0007 0.0000 0.0072 2.481 14.216 0.005 1850.167 1.606 0.022 0.001 0.89 546155. 0.0000
|
|
|
|
|
|
|