427 lines
76 KiB
Plaintext
427 lines
76 KiB
Plaintext
20x8W (20x8W.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 0.0804 0.0307 0.008 0.498 0.410 5.895 0.056 1.824 31.542 0.08 47584. 0.5925
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0.37 0.0195 0.0498 0.0787 0.0308 0.008 0.500 0.401 5.917 0.057 1.786 30.771 0.08 47609. 0.5720
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0.74 0.0390 0.0971 0.0770 0.0309 0.008 0.502 0.392 5.933 0.057 1.746 29.999 0.08 47636. 0.5514
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1.11 0.0585 0.1419 0.0751 0.0309 0.008 0.502 0.383 5.943 0.057 1.703 29.229 0.08 47665. 0.5307
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1.48 0.0779 0.1842 0.0732 0.0310 0.008 0.503 0.373 5.945 0.057 1.659 28.460 0.08 47695. 0.5100
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1.85 0.0974 0.2240 0.0711 0.0309 0.008 0.502 0.363 5.940 0.057 1.613 27.693 0.08 47727. 0.4893
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2.21 0.1169 0.2614 0.0690 0.0309 0.008 0.501 0.352 5.925 0.057 1.565 26.927 0.08 47761. 0.4685
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2.58 0.1364 0.2963 0.0668 0.0307 0.008 0.499 0.340 5.902 0.056 1.514 26.162 0.08 47797. 0.4478
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2.95 0.1559 0.3287 0.0645 0.0306 0.008 0.496 0.329 5.869 0.056 1.462 25.398 0.08 47835. 0.4272
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3.32 0.1754 0.3587 0.0621 0.0303 0.008 0.492 0.316 5.827 0.056 1.407 24.632 0.08 47874. 0.4065
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3.69 0.1949 0.3861 0.0596 0.0301 0.008 0.488 0.304 5.773 0.055 1.351 23.865 0.08 47916. 0.3859
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4.06 0.2144 0.4110 0.0570 0.0297 0.008 0.483 0.291 5.709 0.055 1.293 23.095 0.08 47959. 0.3653
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4.43 0.2338 0.4334 0.0544 0.0293 0.008 0.476 0.277 5.633 0.054 1.233 22.320 0.08 48005. 0.3448
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4.80 0.2533 0.4530 0.0516 0.0289 0.007 0.469 0.263 5.545 0.053 1.171 21.537 0.08 48053. 0.3242
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5.17 0.2728 0.4699 0.0488 0.0284 0.007 0.460 0.249 5.445 0.052 1.108 20.744 0.08 48103. 0.3037
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5.54 0.2923 0.4839 0.0460 0.0278 0.007 0.451 0.234 5.331 0.051 1.042 19.939 0.08 48155. 0.2832
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5.91 0.3118 0.4949 0.0430 0.0271 0.007 0.440 0.219 5.204 0.050 0.976 19.116 0.08 48209. 0.2627
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6.27 0.3313 0.5026 0.0400 0.0264 0.007 0.428 0.204 5.064 0.048 0.907 18.271 0.08 48266. 0.2421
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6.64 0.3508 0.5067 0.0369 0.0256 0.007 0.415 0.188 4.909 0.047 0.838 17.398 0.08 48325. 0.2215
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7.01 0.3703 0.5069 0.0338 0.0247 0.006 0.401 0.172 4.740 0.045 0.766 16.489 0.08 48387. 0.2008
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7.38 0.3897 0.5027 0.0306 0.0237 0.006 0.385 0.156 4.555 0.044 0.694 15.535 0.08 48450. 0.1800
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7.75 0.4092 0.4934 0.0274 0.0227 0.006 0.368 0.139 4.356 0.042 0.620 14.522 0.08 48516. 0.1591
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8.12 0.4287 0.4783 0.0241 0.0216 0.006 0.350 0.123 4.141 0.040 0.546 13.436 0.08 48585. 0.1381
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8.49 0.4482 0.4560 0.0207 0.0204 0.005 0.331 0.106 3.911 0.037 0.470 12.253 0.08 48656. 0.1168
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8.86 0.4677 0.4250 0.0173 0.0191 0.005 0.310 0.088 3.665 0.035 0.393 10.945 0.08 48730. 0.0955
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9.23 0.4872 0.3831 0.0139 0.0177 0.005 0.288 0.071 3.404 0.033 0.316 9.471 0.08 48806. 0.0741
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9.60 0.5067 0.3270 0.0105 0.0163 0.004 0.264 0.054 3.127 0.030 0.238 7.773 0.08 48884. 0.0528
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9.96 0.5261 0.2517 0.0071 0.0148 0.004 0.240 0.036 2.835 0.027 0.160 5.762 0.08 48964. 0.0321
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10.33 0.5456 0.1496 0.0036 0.0132 0.003 0.214 0.018 2.529 0.024 0.082 3.302 0.08 49047. 0.0131
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10.70 0.5651 0.0064 0.0001 0.0115 0.003 0.186 0.001 2.205 0.021 0.003 0.136 0.08 49126. 0.0001
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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 0.0808 0.0275 0.057 1.784 1.648 42.221 0.202 7.332 17.709 0.16 95166. 0.6671
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0.75 0.0197 0.0565 0.0791 0.0276 0.057 1.793 1.614 42.435 0.203 7.179 17.251 0.16 95218. 0.6430
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1.49 0.0395 0.1100 0.0773 0.0277 0.057 1.800 1.578 42.601 0.203 7.017 16.796 0.16 95272. 0.6189
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2.24 0.0592 0.1606 0.0755 0.0278 0.057 1.805 1.539 42.711 0.204 6.846 16.345 0.16 95331. 0.5949
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2.99 0.0789 0.2083 0.0735 0.0278 0.057 1.807 1.499 42.759 0.204 6.667 15.899 0.16 95392. 0.5711
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3.74 0.0986 0.2532 0.0714 0.0278 0.057 1.806 1.457 42.741 0.204 6.479 15.458 0.16 95457. 0.5473
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4.48 0.1184 0.2952 0.0693 0.0278 0.057 1.802 1.412 42.651 0.204 6.283 15.021 0.16 95526. 0.5237
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5.23 0.1381 0.3345 0.0670 0.0277 0.057 1.795 1.366 42.484 0.203 6.078 14.588 0.16 95599. 0.5003
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5.98 0.1578 0.3711 0.0646 0.0275 0.057 1.785 1.319 42.235 0.202 5.865 14.160 0.16 95676. 0.4770
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6.72 0.1775 0.4049 0.0622 0.0273 0.056 1.771 1.269 41.900 0.200 5.644 13.735 0.16 95756. 0.4539
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7.47 0.1973 0.4361 0.0597 0.0270 0.056 1.753 1.217 41.475 0.198 5.415 13.312 0.16 95841. 0.4309
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8.22 0.2170 0.4645 0.0571 0.0267 0.055 1.731 1.164 40.954 0.196 5.178 12.892 0.16 95930. 0.4081
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8.97 0.2367 0.4903 0.0544 0.0263 0.054 1.705 1.109 40.333 0.193 4.934 12.473 0.16 96023. 0.3854
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9.71 0.2564 0.5133 0.0516 0.0258 0.053 1.674 1.053 39.608 0.189 4.682 12.054 0.16 96120. 0.3628
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10.46 0.2762 0.5335 0.0488 0.0252 0.052 1.639 0.995 38.775 0.185 4.424 11.634 0.16 96222. 0.3404
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11.21 0.2959 0.5508 0.0458 0.0246 0.051 1.599 0.935 37.829 0.181 4.159 11.210 0.16 96329. 0.3180
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11.95 0.3156 0.5650 0.0428 0.0239 0.049 1.554 0.874 36.767 0.176 3.887 10.780 0.16 96440. 0.2957
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12.70 0.3353 0.5759 0.0398 0.0232 0.048 1.504 0.811 35.584 0.170 3.609 10.343 0.16 96556. 0.2733
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13.45 0.3551 0.5833 0.0367 0.0223 0.046 1.449 0.748 34.277 0.164 3.326 9.893 0.16 96677. 0.2510
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14.20 0.3748 0.5867 0.0335 0.0214 0.044 1.388 0.683 32.843 0.157 3.036 9.427 0.16 96802. 0.2285
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14.94 0.3945 0.5856 0.0302 0.0204 0.042 1.322 0.616 31.279 0.149 2.742 8.939 0.16 96932. 0.2059
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15.69 0.4142 0.5793 0.0269 0.0193 0.040 1.250 0.549 29.582 0.141 2.443 8.421 0.16 97068. 0.1831
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16.44 0.4340 0.5666 0.0236 0.0181 0.037 1.173 0.481 27.752 0.133 2.140 7.862 0.16 97208. 0.1600
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17.19 0.4537 0.5459 0.0202 0.0168 0.035 1.090 0.412 25.786 0.123 1.832 7.246 0.16 97353. 0.1365
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17.93 0.4734 0.5152 0.0168 0.0154 0.032 1.001 0.342 23.685 0.113 1.522 6.553 0.16 97503. 0.1125
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18.68 0.4931 0.4707 0.0133 0.0140 0.029 0.907 0.272 21.450 0.102 1.209 5.748 0.16 97658. 0.0879
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19.43 0.5129 0.4070 0.0099 0.0124 0.026 0.806 0.201 19.082 0.091 0.894 4.779 0.16 97819. 0.0629
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20.17 0.5326 0.3145 0.0064 0.0108 0.022 0.701 0.130 16.585 0.079 0.578 3.556 0.16 97983. 0.0376
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20.92 0.5523 0.1755 0.0029 0.0091 0.019 0.590 0.059 13.957 0.067 0.262 1.913 0.16 98151. 0.0136
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21.67 0.5720
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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 0.0813 0.0263 0.183 3.836 3.731 136.170 0.433 16.595 12.427 0.24 142745. 0.7042
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1.12 0.0197 0.0592 0.0796 0.0264 0.184 3.858 3.653 136.938 0.436 16.250 12.101 0.24 142822. 0.6785
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2.23 0.0393 0.1153 0.0778 0.0265 0.184 3.875 3.571 137.542 0.438 15.886 11.777 0.24 142904. 0.6530
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3.35 0.0590 0.1683 0.0759 0.0266 0.185 3.887 3.485 137.957 0.439 15.502 11.458 0.24 142991. 0.6276
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4.47 0.0786 0.2182 0.0740 0.0266 0.185 3.893 3.395 138.164 0.440 15.099 11.144 0.24 143084. 0.6024
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5.58 0.0983 0.2652 0.0719 0.0266 0.185 3.892 3.300 138.143 0.440 14.677 10.834 0.24 143181. 0.5774
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6.70 0.1179 0.3093 0.0697 0.0266 0.185 3.885 3.200 137.877 0.439 14.236 10.528 0.24 143284. 0.5526
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7.82 0.1376 0.3505 0.0675 0.0265 0.184 3.870 3.097 137.349 0.437 13.775 10.227 0.24 143393. 0.5280
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8.93 0.1572 0.3889 0.0651 0.0263 0.183 3.847 2.989 136.541 0.435 13.297 9.930 0.24 143507. 0.5037
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10.05 0.1769 0.4246 0.0627 0.0261 0.182 3.816 2.878 135.439 0.431 12.799 9.637 0.24 143628. 0.4796
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11.17 0.1965 0.4576 0.0602 0.0259 0.180 3.776 2.762 134.027 0.427 12.285 9.347 0.24 143754. 0.4557
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12.28 0.2162 0.4879 0.0576 0.0255 0.177 3.727 2.642 132.289 0.421 11.753 9.059 0.24 143887. 0.4320
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13.40 0.2359 0.5155 0.0549 0.0251 0.175 3.669 2.519 130.209 0.414 11.204 8.774 0.24 144026. 0.4085
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14.52 0.2555 0.5404 0.0521 0.0246 0.171 3.600 2.392 127.772 0.407 10.639 8.491 0.24 144172. 0.3852
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15.63 0.2752 0.5625 0.0493 0.0241 0.168 3.521 2.261 124.963 0.398 10.058 8.207 0.24 144324. 0.3621
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16.75 0.2948 0.5819 0.0464 0.0235 0.163 3.431 2.127 121.768 0.388 9.462 7.924 0.24 144483. 0.3391
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17.87 0.3145 0.5983 0.0434 0.0228 0.158 3.329 1.990 118.173 0.376 8.852 7.638 0.24 144649. 0.3161
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18.98 0.3341 0.6116 0.0403 0.0220 0.153 3.217 1.850 114.165 0.363 8.227 7.349 0.24 144822. 0.2932
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20.10 0.3538 0.6216 0.0372 0.0212 0.147 3.092 1.706 109.731 0.349 7.590 7.053 0.24 145002. 0.2703
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21.22 0.3734 0.6278 0.0340 0.0202 0.141 2.954 1.560 104.860 0.334 6.940 6.749 0.24 145189. 0.2473
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22.33 0.3931 0.6298 0.0308 0.0192 0.133 2.805 1.412 99.542 0.317 6.279 6.432 0.24 145384. 0.2242
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23.45 0.4127 0.6269 0.0275 0.0181 0.126 2.642 1.261 93.770 0.298 5.607 6.097 0.24 145585. 0.2008
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24.57 0.4324 0.6179 0.0241 0.0169 0.117 2.466 1.107 87.537 0.279 4.925 5.737 0.24 145794. 0.1771
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25.68 0.4520 0.6015 0.0207 0.0156 0.108 2.278 0.952 80.840 0.257 4.235 5.342 0.24 146011. 0.1529
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26.80 0.4717 0.5752 0.0173 0.0142 0.099 2.076 0.795 73.676 0.235 3.537 4.896 0.24 146235. 0.1281
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27.92 0.4914 0.5355 0.0139 0.0127 0.089 1.861 0.637 66.050 0.210 2.834 4.375 0.24 146466. 0.1025
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29.03 0.5110 0.4761 0.0104 0.0112 0.078 1.633 0.478 57.966 0.185 2.126 3.740 0.24 146705. 0.0759
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30.15 0.5307 0.3861 0.0069 0.0095 0.066 1.393 0.318 49.434 0.157 1.416 2.921 0.24 146950. 0.0483
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31.27 0.5503 0.2434 0.0035 0.0078 0.054 1.140 0.158 40.458 0.129 0.704 1.775 0.24 147200. 0.0207
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32.38 0.5700 -0.0130 -0.0001 0.0059 0.041 0.867 -0.006 30.756 0.098 -0.028 -0.092 0.24 147396. 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 0.0819 0.0257 0.424 6.676 6.683 315.918 0.754 29.726 9.595 0.32 190318. 0.7277
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1.50 0.0198 0.0613 0.0802 0.0259 0.426 6.716 6.544 317.811 0.759 29.106 9.339 0.32 190422. 0.7009
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2.99 0.0395 0.1193 0.0784 0.0260 0.428 6.747 6.396 319.300 0.762 28.451 9.086 0.32 190533. 0.6742
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4.49 0.0593 0.1740 0.0765 0.0261 0.430 6.769 6.241 320.332 0.765 27.761 8.837 0.32 190650. 0.6477
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5.99 0.0791 0.2256 0.0745 0.0261 0.430 6.780 6.078 320.854 0.766 27.037 8.593 0.32 190774. 0.6215
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7.49 0.0988 0.2741 0.0724 0.0261 0.430 6.779 5.908 320.820 0.766 26.277 8.352 0.32 190906. 0.5956
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8.98 0.1186 0.3197 0.0702 0.0261 0.429 6.766 5.729 320.186 0.764 25.482 8.115 0.32 191045. 0.5699
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10.48 0.1384 0.3622 0.0679 0.0259 0.428 6.739 5.543 318.910 0.761 24.653 7.883 0.32 191191. 0.5445
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11.98 0.1581 0.4020 0.0656 0.0258 0.425 6.697 5.349 316.953 0.757 23.791 7.654 0.32 191346. 0.5193
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13.48 0.1779 0.4389 0.0631 0.0256 0.421 6.641 5.147 314.274 0.750 22.895 7.429 0.32 191508. 0.4945
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14.97 0.1977 0.4731 0.0605 0.0253 0.417 6.568 4.939 310.835 0.742 21.967 7.207 0.32 191678. 0.4699
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16.47 0.2174 0.5046 0.0579 0.0249 0.411 6.479 4.723 306.598 0.732 21.009 6.987 0.32 191857. 0.4455
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17.97 0.2372 0.5333 0.0552 0.0245 0.404 6.371 4.501 301.525 0.720 20.019 6.770 0.32 192045. 0.4214
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19.47 0.2570 0.5594 0.0524 0.0241 0.396 6.246 4.272 295.579 0.706 19.001 6.555 0.32 192241. 0.3975
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20.96 0.2767 0.5828 0.0495 0.0235 0.387 6.101 4.036 288.721 0.689 17.954 6.341 0.32 192446. 0.3738
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22.46 0.2965 0.6034 0.0465 0.0229 0.377 5.936 3.795 280.918 0.671 16.880 6.127 0.32 192661. 0.3502
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23.96 0.3163 0.6210 0.0435 0.0221 0.365 5.750 3.547 272.135 0.650 15.779 5.913 0.32 192884. 0.3267
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25.46 0.3360 0.6357 0.0404 0.0213 0.352 5.543 3.294 262.340 0.626 14.654 5.696 0.32 193117. 0.3033
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26.95 0.3558 0.6470 0.0372 0.0205 0.337 5.314 3.036 251.503 0.600 13.505 5.476 0.32 193360. 0.2799
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28.45 0.3756 0.6547 0.0340 0.0195 0.321 5.063 2.773 239.595 0.572 12.334 5.249 0.32 193612. 0.2564
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29.95 0.3953 0.6583 0.0307 0.0184 0.304 4.788 2.505 226.595 0.541 11.141 5.014 0.32 193874. 0.2328
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31.45 0.4151 0.6570 0.0274 0.0173 0.285 4.490 2.232 212.483 0.507 9.930 4.766 0.32 194146. 0.2089
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32.94 0.4349 0.6497 0.0240 0.0160 0.265 4.168 1.956 197.243 0.471 8.702 4.499 0.32 194427. 0.1846
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34.44 0.4546 0.6349 0.0206 0.0147 0.243 3.822 1.677 180.868 0.432 7.458 4.205 0.32 194719. 0.1597
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35.94 0.4744 0.6099 0.0171 0.0133 0.219 3.452 1.394 163.355 0.390 6.201 3.871 0.32 195021. 0.1341
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37.44 0.4942 0.5706 0.0136 0.0118 0.194 3.058 1.109 144.713 0.345 4.934 3.477 0.32 195333. 0.1074
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38.93 0.5139 0.5097 0.0101 0.0102 0.168 2.640 0.823 124.957 0.298 3.660 2.986 0.32 195654. 0.0795
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40.43 0.5337 0.4134 0.0066 0.0085 0.140 2.200 0.535 104.109 0.249 2.381 2.332 0.32 195985. 0.0501
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41.93 0.5535 0.2510 0.0030 0.0067 0.110 1.736 0.247 82.174 0.196 1.100 1.365 0.32 196320. 0.0199
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43.43 0.5732
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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 0.0827 0.0255 0.821 10.346 10.543 612.017 1.169 46.894 7.813 0.40 237884. 0.7443
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1.88 0.0198 0.0626 0.0810 0.0257 0.826 10.410 10.323 615.796 1.176 45.916 7.603 0.40 238015. 0.7167
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3.76 0.0397 0.1218 0.0792 0.0258 0.830 10.460 10.091 618.766 1.182 44.883 7.397 0.40 238154. 0.6893
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5.63 0.0595 0.1776 0.0772 0.0259 0.833 10.495 9.846 620.816 1.186 43.794 7.193 0.40 238302. 0.6622
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7.51 0.0793 0.2303 0.0752 0.0259 0.834 10.512 9.589 621.846 1.188 42.650 6.994 0.40 238459. 0.6354
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9.39 0.0991 0.2798 0.0731 0.0259 0.834 10.511 9.319 621.760 1.187 41.449 6.798 0.40 238624. 0.6088
|
|
11.27 0.1190 0.3262 0.0709 0.0258 0.832 10.489 9.036 620.469 1.185 40.193 6.606 0.40 238799. 0.5826
|
|
13.14 0.1388 0.3697 0.0686 0.0257 0.829 10.445 8.741 617.890 1.180 38.882 6.417 0.40 238984. 0.5566
|
|
15.02 0.1586 0.4104 0.0662 0.0256 0.823 10.378 8.435 613.944 1.173 37.518 6.231 0.40 239178. 0.5310
|
|
16.90 0.1785 0.4482 0.0637 0.0254 0.816 10.287 8.116 608.553 1.162 36.101 6.049 0.40 239383. 0.5056
|
|
18.78 0.1983 0.4832 0.0611 0.0251 0.807 10.170 7.786 601.640 1.149 34.634 5.870 0.40 239598. 0.4806
|
|
20.65 0.2181 0.5155 0.0584 0.0247 0.795 10.027 7.445 593.128 1.133 33.117 5.693 0.40 239823. 0.4558
|
|
22.53 0.2379 0.5452 0.0556 0.0243 0.782 9.854 7.093 582.941 1.113 31.551 5.519 0.40 240059. 0.4313
|
|
24.41 0.2578 0.5721 0.0528 0.0238 0.766 9.653 6.731 571.004 1.091 29.940 5.347 0.40 240307. 0.4070
|
|
26.29 0.2776 0.5964 0.0499 0.0232 0.747 9.420 6.359 557.245 1.064 28.283 5.176 0.40 240565. 0.3829
|
|
28.16 0.2974 0.6180 0.0469 0.0226 0.726 9.155 5.976 541.594 1.034 26.582 5.005 0.40 240835. 0.3590
|
|
30.04 0.3172 0.6367 0.0438 0.0218 0.703 8.858 5.585 523.981 1.001 24.841 4.834 0.40 241116. 0.3352
|
|
31.92 0.3371 0.6524 0.0407 0.0210 0.676 8.526 5.184 504.344 0.963 23.060 4.662 0.40 241409. 0.3114
|
|
33.80 0.3569 0.6650 0.0375 0.0201 0.647 8.158 4.775 482.622 0.922 21.241 4.488 0.40 241714. 0.2877
|
|
35.68 0.3767 0.6739 0.0342 0.0191 0.615 7.755 4.359 458.761 0.876 19.387 4.309 0.40 242032. 0.2639
|
|
37.55 0.3966 0.6789 0.0309 0.0180 0.580 7.315 3.934 432.715 0.826 17.500 4.124 0.40 242361. 0.2400
|
|
39.43 0.4164 0.6791 0.0275 0.0168 0.542 6.837 3.503 404.444 0.772 15.582 3.929 0.40 242703. 0.2157
|
|
41.31 0.4362 0.6735 0.0241 0.0156 0.501 6.321 3.066 373.921 0.714 13.637 3.719 0.40 243057. 0.1910
|
|
43.19 0.4560 0.6604 0.0206 0.0142 0.457 5.767 2.623 341.128 0.652 11.668 3.488 0.40 243424. 0.1657
|
|
45.06 0.4759 0.6371 0.0171 0.0128 0.410 5.174 2.176 306.065 0.585 9.679 3.225 0.40 243804. 0.1396
|
|
46.94 0.4957 0.5992 0.0135 0.0112 0.360 4.543 1.725 268.747 0.513 7.674 2.912 0.40 244196. 0.1122
|
|
48.82 0.5155 0.5386 0.0100 0.0095 0.307 3.875 1.272 229.207 0.438 5.657 2.517 0.40 244600. 0.0833
|
|
50.70 0.5354 0.4393 0.0064 0.0078 0.251 3.169 0.817 187.493 0.358 3.634 1.976 0.40 245016. 0.0524
|
|
52.57 0.5552 0.2630 0.0028 0.0060 0.193 2.427 0.361 143.597 0.274 1.607 1.141 0.40 245436. 0.0201
|
|
54.45 0.5750
|
|
|
|
|
|
|
|
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 0.0837 0.0255 1.420 14.917 15.365 1058.893 1.685 68.342 6.581 0.48 285439. 0.7568
|
|
2.24 0.0197 0.0629 0.0820 0.0257 1.429 15.009 15.047 1065.463 1.696 66.930 6.406 0.48 285596. 0.7290
|
|
4.48 0.0394 0.1224 0.0801 0.0258 1.436 15.082 14.712 1070.620 1.704 65.438 6.233 0.48 285764. 0.7014
|
|
6.72 0.0591 0.1786 0.0782 0.0259 1.440 15.132 14.359 1074.168 1.710 63.867 6.063 0.48 285941. 0.6740
|
|
8.96 0.0789 0.2316 0.0762 0.0259 1.443 15.157 13.987 1075.935 1.712 62.215 5.896 0.48 286129. 0.6470
|
|
11.20 0.0986 0.2815 0.0741 0.0259 1.443 15.154 13.597 1075.753 1.712 60.481 5.733 0.48 286327. 0.6202
|
|
13.44 0.1183 0.3284 0.0719 0.0259 1.440 15.122 13.190 1073.467 1.708 58.667 5.573 0.48 286537. 0.5938
|
|
15.68 0.1380 0.3724 0.0695 0.0258 1.433 15.058 12.764 1068.938 1.701 56.774 5.416 0.48 286758. 0.5677
|
|
17.92 0.1577 0.4135 0.0671 0.0256 1.424 14.961 12.321 1062.028 1.690 54.804 5.262 0.48 286990. 0.5419
|
|
20.16 0.1774 0.4518 0.0646 0.0254 1.412 14.828 11.861 1052.605 1.675 52.757 5.111 0.48 287235. 0.5164
|
|
22.40 0.1972 0.4874 0.0620 0.0251 1.395 14.658 11.384 1040.534 1.656 50.637 4.962 0.48 287491. 0.4912
|
|
24.64 0.2169 0.5204 0.0593 0.0247 1.375 14.449 10.892 1025.688 1.632 48.446 4.816 0.48 287761. 0.4663
|
|
26.88 0.2366 0.5507 0.0566 0.0243 1.352 14.199 10.383 1007.936 1.604 46.184 4.672 0.48 288042. 0.4417
|
|
29.12 0.2563 0.5784 0.0537 0.0238 1.324 13.906 9.860 987.151 1.571 43.856 4.530 0.48 288337. 0.4173
|
|
31.37 0.2760 0.6036 0.0508 0.0232 1.292 13.569 9.321 963.207 1.533 41.462 4.389 0.48 288646. 0.3932
|
|
33.61 0.2957 0.6260 0.0478 0.0226 1.255 13.185 8.769 935.984 1.490 39.005 4.249 0.48 288967. 0.3692
|
|
35.85 0.3154 0.6458 0.0447 0.0218 1.214 12.754 8.203 905.365 1.441 36.488 4.110 0.48 289302. 0.3453
|
|
38.09 0.3352 0.6628 0.0415 0.0210 1.168 12.273 7.625 871.240 1.387 33.914 3.969 0.48 289652. 0.3216
|
|
40.33 0.3549 0.6767 0.0383 0.0201 1.118 11.742 7.034 833.504 1.327 31.285 3.827 0.48 290015. 0.2978
|
|
42.57 0.3746 0.6872 0.0350 0.0191 1.062 11.158 6.431 792.066 1.261 28.605 3.683 0.48 290393. 0.2740
|
|
44.81 0.3943 0.6940 0.0317 0.0180 1.002 10.521 5.818 746.842 1.189 25.877 3.533 0.48 290785. 0.2500
|
|
47.05 0.4140 0.6964 0.0283 0.0168 0.936 9.829 5.194 697.763 1.111 23.104 3.376 0.48 291192. 0.2258
|
|
49.29 0.4337 0.6934 0.0249 0.0155 0.865 9.083 4.562 644.780 1.026 20.291 3.209 0.48 291613. 0.2011
|
|
51.53 0.4534 0.6835 0.0214 0.0142 0.788 8.281 3.921 587.860 0.936 17.442 3.026 0.48 292049. 0.1758
|
|
53.77 0.4732 0.6642 0.0178 0.0127 0.707 7.424 3.274 526.997 0.839 14.563 2.818 0.48 292501. 0.1496
|
|
56.01 0.4929 0.6316 0.0143 0.0111 0.620 6.511 2.621 462.215 0.736 11.660 2.572 0.48 292966. 0.1222
|
|
58.25 0.5126 0.5782 0.0107 0.0095 0.528 5.544 1.965 393.566 0.626 8.738 2.264 0.48 293447. 0.0931
|
|
60.49 0.5323 0.4889 0.0071 0.0077 0.431 4.524 1.305 321.133 0.511 5.806 1.844 0.48 293941. 0.0618
|
|
62.73 0.5520 0.3285 0.0035 0.0059 0.328 3.451 0.645 244.944 0.390 2.869 1.194 0.48 294443. 0.0281
|
|
64.97 0.5717
|
|
|
|
|
|
|
|
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 0.0849 0.0258 2.276 20.489 21.223 1696.900 2.315 94.400 5.673 0.56 332980. 0.7667
|
|
2.61 0.0197 0.0632 0.0832 0.0259 2.290 20.616 20.787 1707.403 2.329 92.460 5.522 0.56 333165. 0.7386
|
|
5.23 0.0394 0.1231 0.0814 0.0260 2.301 20.715 20.326 1715.594 2.340 90.410 5.374 0.56 333362. 0.7108
|
|
7.84 0.0591 0.1797 0.0794 0.0261 2.308 20.782 19.840 1721.158 2.348 88.248 5.228 0.56 333570. 0.6832
|
|
10.45 0.0788 0.2330 0.0774 0.0262 2.312 20.814 19.329 1723.812 2.352 85.975 5.086 0.56 333791. 0.6560
|
|
13.06 0.0985 0.2833 0.0752 0.0262 2.311 20.808 18.792 1723.285 2.351 83.588 4.946 0.56 334024. 0.6291
|
|
15.68 0.1182 0.3305 0.0730 0.0261 2.306 20.760 18.231 1719.326 2.345 81.090 4.809 0.56 334270. 0.6025
|
|
18.29 0.1379 0.3749 0.0706 0.0260 2.295 20.668 17.644 1711.713 2.335 78.482 4.675 0.56 334529. 0.5762
|
|
20.90 0.1577 0.4164 0.0682 0.0258 2.280 20.530 17.034 1700.223 2.319 75.766 4.544 0.56 334802. 0.5502
|
|
23.51 0.1774 0.4552 0.0656 0.0256 2.259 20.342 16.400 1684.648 2.298 72.946 4.415 0.56 335088. 0.5246
|
|
26.13 0.1971 0.4913 0.0630 0.0253 2.233 20.102 15.743 1664.781 2.271 70.023 4.289 0.56 335389. 0.4993
|
|
28.74 0.2168 0.5247 0.0603 0.0249 2.200 19.807 15.063 1640.415 2.238 67.001 4.165 0.56 335704. 0.4742
|
|
31.35 0.2365 0.5557 0.0575 0.0245 2.161 19.456 14.362 1611.341 2.198 63.883 4.043 0.56 336035. 0.4495
|
|
33.96 0.2562 0.5840 0.0546 0.0239 2.115 19.046 13.640 1577.363 2.152 60.671 3.922 0.56 336380. 0.4250
|
|
36.58 0.2759 0.6098 0.0516 0.0234 2.063 18.574 12.898 1538.276 2.098 57.369 3.803 0.56 336740. 0.4007
|
|
39.19 0.2956 0.6330 0.0486 0.0227 2.003 18.038 12.136 1493.892 2.038 53.980 3.685 0.56 337116. 0.3766
|
|
41.80 0.3153 0.6536 0.0454 0.0219 1.936 17.436 11.355 1444.021 1.970 50.508 3.567 0.56 337509. 0.3526
|
|
44.42 0.3350 0.6715 0.0423 0.0211 1.862 16.765 10.557 1388.489 1.894 46.956 3.448 0.56 337917. 0.3287
|
|
47.03 0.3547 0.6864 0.0390 0.0201 1.780 16.025 9.741 1327.132 1.810 43.328 3.329 0.56 338342. 0.3048
|
|
49.64 0.3744 0.6981 0.0357 0.0191 1.689 15.212 8.909 1259.800 1.719 39.629 3.208 0.56 338783. 0.2809
|
|
52.25 0.3941 0.7061 0.0323 0.0180 1.591 14.325 8.063 1186.360 1.618 35.863 3.083 0.56 339241. 0.2568
|
|
54.87 0.4138 0.7100 0.0288 0.0168 1.484 13.363 7.202 1106.700 1.510 32.035 2.952 0.56 339716. 0.2324
|
|
57.48 0.4336 0.7086 0.0253 0.0155 1.369 12.325 6.329 1020.742 1.392 28.151 2.812 0.56 340208. 0.2076
|
|
60.09 0.4533 0.7007 0.0218 0.0141 1.245 11.210 5.444 928.432 1.267 24.217 2.660 0.56 340717. 0.1821
|
|
62.70 0.4730 0.6837 0.0182 0.0126 1.113 10.019 4.550 829.760 1.132 20.240 2.487 0.56 341243. 0.1557
|
|
65.32 0.4927 0.6538 0.0146 0.0110 0.972 8.751 3.649 724.765 0.989 16.229 2.283 0.56 341787. 0.1280
|
|
67.93 0.5124 0.6035 0.0110 0.0093 0.823 7.408 2.741 613.530 0.837 12.192 2.026 0.56 342348. 0.0984
|
|
70.54 0.5321 0.5173 0.0073 0.0075 0.665 5.991 1.830 496.189 0.677 8.140 1.673 0.56 342924. 0.0664
|
|
73.15 0.5518 0.3579 0.0037 0.0057 0.500 4.501 0.917 372.797 0.509 4.080 1.116 0.56 343510. 0.0314
|
|
75.77 0.5715
|
|
|
|
|
|
|
|
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 0.0865 0.0262 3.454 27.212 28.222 2575.572 3.074 125.530 4.970 0.63 380503. 0.7746
|
|
2.99 0.0197 0.0635 0.0847 0.0264 3.475 27.378 27.644 2591.349 3.093 122.962 4.839 0.63 380717. 0.7464
|
|
5.98 0.0395 0.1235 0.0828 0.0265 3.491 27.507 27.033 2603.519 3.108 120.245 4.710 0.63 380944. 0.7184
|
|
8.97 0.0592 0.1803 0.0809 0.0266 3.502 27.592 26.389 2611.611 3.117 117.379 4.583 0.63 381185. 0.6907
|
|
11.97 0.0790 0.2339 0.0788 0.0266 3.507 27.630 25.711 2615.177 3.122 114.361 4.459 0.63 381440. 0.6634
|
|
14.96 0.0987 0.2844 0.0766 0.0266 3.505 27.616 24.998 2613.810 3.120 111.192 4.338 0.63 381709. 0.6363
|
|
17.95 0.1185 0.3320 0.0743 0.0265 3.496 27.545 24.252 2607.121 3.112 107.872 4.219 0.64 381993. 0.6096
|
|
20.94 0.1382 0.3767 0.0719 0.0264 3.480 27.415 23.472 2594.767 3.097 104.405 4.103 0.64 382292. 0.5832
|
|
23.93 0.1579 0.4185 0.0694 0.0262 3.455 27.221 22.660 2576.424 3.075 100.793 3.989 0.64 382607. 0.5571
|
|
26.92 0.1777 0.4577 0.0669 0.0260 3.422 26.960 21.816 2551.784 3.046 97.039 3.878 0.64 382938. 0.5314
|
|
29.91 0.1974 0.4942 0.0642 0.0256 3.380 26.630 20.942 2520.527 3.009 93.149 3.768 0.64 383285. 0.5060
|
|
32.91 0.2172 0.5282 0.0614 0.0252 3.329 26.227 20.037 2482.348 2.963 89.126 3.661 0.64 383648. 0.4808
|
|
35.90 0.2369 0.5596 0.0585 0.0248 3.268 25.747 19.104 2436.943 2.909 84.973 3.556 0.64 384028. 0.4559
|
|
38.89 0.2567 0.5885 0.0556 0.0242 3.197 25.188 18.142 2384.010 2.846 80.696 3.452 0.64 384426. 0.4313
|
|
41.88 0.2764 0.6149 0.0526 0.0236 3.116 24.546 17.153 2323.250 2.773 76.297 3.349 0.64 384841. 0.4069
|
|
44.87 0.2962 0.6387 0.0495 0.0229 3.023 23.818 16.138 2254.375 2.691 71.782 3.247 0.64 385274. 0.3827
|
|
47.86 0.3159 0.6600 0.0463 0.0221 2.920 23.002 15.098 2177.104 2.599 67.156 3.145 0.64 385726. 0.3586
|
|
50.85 0.3356 0.6786 0.0430 0.0213 2.804 22.094 14.034 2091.174 2.496 62.422 3.044 0.64 386195. 0.3345
|
|
53.85 0.3554 0.6944 0.0397 0.0203 2.677 21.092 12.947 1996.337 2.383 57.587 2.942 0.64 386684. 0.3105
|
|
56.84 0.3751 0.7070 0.0363 0.0192 2.538 19.993 11.838 1892.367 2.259 52.656 2.837 0.64 387191. 0.2864
|
|
59.83 0.3949 0.7161 0.0328 0.0181 2.386 18.796 10.709 1779.068 2.124 47.635 2.730 0.64 387717. 0.2621
|
|
62.82 0.4146 0.7211 0.0293 0.0168 2.221 17.499 9.562 1656.272 1.977 42.531 2.618 0.64 388263. 0.2376
|
|
65.81 0.4344 0.7211 0.0257 0.0155 2.044 16.100 8.397 1523.855 1.819 37.351 2.499 0.64 388828. 0.2125
|
|
68.80 0.4541 0.7146 0.0221 0.0141 1.853 14.599 7.218 1381.744 1.649 32.104 2.369 0.64 389413. 0.1867
|
|
71.79 0.4738 0.6993 0.0185 0.0125 1.649 12.995 6.025 1229.924 1.468 26.798 2.222 0.64 390017. 0.1600
|
|
74.79 0.4936 0.6711 0.0148 0.0109 1.433 11.289 4.822 1068.452 1.275 21.446 2.047 0.64 390641. 0.1319
|
|
77.78 0.5133 0.6222 0.0111 0.0091 1.204 9.482 3.611 897.470 1.071 16.060 1.825 0.64 391284. 0.1017
|
|
80.77 0.5331 0.5363 0.0073 0.0073 0.962 7.577 2.395 717.180 0.856 10.653 1.515 0.64 391945. 0.0688
|
|
83.76 0.5528 0.3714 0.0036 0.0054 0.708 5.575 1.176 527.651 0.630 5.233 1.011 0.64 392616. 0.0322
|
|
86.75 0.5726
|
|
|
|
|
|
|
|
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 0.0884 0.0269 5.045 35.333 36.507 3762.266 3.992 162.382 4.401 0.71 428000. 0.7802
|
|
3.37 0.0198 0.0634 0.0866 0.0270 5.074 35.537 35.765 3784.042 4.015 159.081 4.287 0.71 428244. 0.7521
|
|
6.75 0.0396 0.1235 0.0847 0.0271 5.097 35.693 34.978 3800.578 4.033 155.584 4.174 0.71 428503. 0.7243
|
|
10.12 0.0594 0.1803 0.0827 0.0272 5.111 35.792 34.148 3811.165 4.044 151.891 4.064 0.71 428778. 0.6967
|
|
13.49 0.0792 0.2340 0.0806 0.0273 5.116 35.829 33.273 3815.119 4.048 147.999 3.956 0.71 429069. 0.6694
|
|
16.87 0.0990 0.2847 0.0783 0.0272 5.112 35.798 32.353 3811.803 4.044 143.907 3.850 0.71 429376. 0.6424
|
|
20.24 0.1187 0.3324 0.0760 0.0272 5.097 35.693 31.388 3800.620 4.033 139.616 3.746 0.71 429699. 0.6157
|
|
23.61 0.1385 0.3773 0.0736 0.0270 5.070 35.509 30.380 3781.049 4.012 135.131 3.644 0.71 430040. 0.5893
|
|
26.99 0.1583 0.4194 0.0710 0.0268 5.032 35.242 29.329 3752.600 3.982 130.456 3.545 0.71 430399. 0.5632
|
|
30.36 0.1781 0.4589 0.0684 0.0265 4.982 34.887 28.236 3714.813 3.942 125.595 3.448 0.72 430775. 0.5375
|
|
33.74 0.1979 0.4958 0.0656 0.0262 4.918 34.440 27.103 3667.245 3.891 120.555 3.352 0.72 431170. 0.5120
|
|
37.11 0.2177 0.5301 0.0628 0.0258 4.840 33.898 25.931 3609.471 3.830 115.341 3.259 0.72 431584. 0.4868
|
|
40.48 0.2375 0.5620 0.0599 0.0253 4.749 33.255 24.721 3541.054 3.757 109.959 3.166 0.72 432016. 0.4619
|
|
43.86 0.2573 0.5914 0.0568 0.0247 4.642 32.509 23.474 3461.570 3.673 104.412 3.076 0.72 432468. 0.4372
|
|
47.23 0.2771 0.6183 0.0537 0.0241 4.520 31.655 22.192 3370.596 3.576 98.709 2.986 0.72 432940. 0.4127
|
|
50.60 0.2969 0.6428 0.0505 0.0233 4.382 30.688 20.875 3267.712 3.467 92.853 2.898 0.72 433431. 0.3884
|
|
53.98 0.3167 0.6648 0.0473 0.0225 4.228 29.606 19.526 3152.511 3.345 86.851 2.809 0.72 433944. 0.3642
|
|
57.35 0.3365 0.6841 0.0439 0.0216 4.056 28.405 18.145 3024.623 3.209 80.709 2.721 0.72 434476. 0.3400
|
|
60.72 0.3562 0.7007 0.0405 0.0206 3.867 27.082 16.734 2883.686 3.060 74.434 2.632 0.72 435030. 0.3159
|
|
64.10 0.3760 0.7142 0.0370 0.0195 3.660 25.633 15.295 2729.383 2.896 68.033 2.542 0.72 435605. 0.2916
|
|
67.47 0.3958 0.7244 0.0335 0.0183 3.435 24.055 13.830 2561.427 2.718 61.515 2.449 0.72 436202. 0.2672
|
|
70.84 0.4156 0.7305 0.0299 0.0170 3.191 22.348 12.340 2379.586 2.525 54.887 2.352 0.72 436820. 0.2424
|
|
74.22 0.4354 0.7317 0.0262 0.0156 2.928 20.508 10.827 2183.679 2.317 48.159 2.249 0.72 437460. 0.2171
|
|
77.59 0.4552 0.7266 0.0225 0.0141 2.647 18.535 9.295 1973.613 2.094 41.342 2.136 0.72 438122. 0.1911
|
|
80.97 0.4750 0.7127 0.0188 0.0125 2.346 16.429 7.745 1749.407 1.856 34.449 2.008 0.72 438806. 0.1639
|
|
84.34 0.4948 0.6859 0.0150 0.0108 2.027 14.193 6.181 1511.243 1.603 27.494 1.855 0.72 439512. 0.1353
|
|
87.71 0.5146 0.6380 0.0112 0.0090 1.689 11.828 4.607 1259.458 1.336 20.492 1.659 0.72 440239. 0.1045
|
|
91.09 0.5344 0.5512 0.0073 0.0071 1.334 9.340 3.026 994.539 1.055 13.462 1.380 0.72 440986. 0.0704
|
|
94.46 0.5542 0.3778 0.0035 0.0051 0.961 6.731 1.442 716.753 0.760 6.413 0.912 0.73 441743. 0.0321
|
|
97.83 0.5740
|
|
|
|
|
|
|
|
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 0.0908 0.0285 7.332 46.212 46.282 5467.403 5.221 205.860 3.839 0.79 475460. 0.7663
|
|
3.74 0.0197 0.0615 0.0890 0.0285 7.350 46.327 45.356 5481.029 5.234 201.745 3.753 0.79 475734. 0.7416
|
|
7.47 0.0395 0.1202 0.0870 0.0286 7.360 46.386 44.375 5488.068 5.241 197.379 3.667 0.79 476026. 0.7167
|
|
11.21 0.0592 0.1760 0.0850 0.0286 7.359 46.383 43.337 5487.638 5.240 192.762 3.582 0.79 476334. 0.6918
|
|
14.95 0.0789 0.2291 0.0828 0.0285 7.347 46.309 42.241 5478.857 5.232 187.890 3.497 0.79 476660. 0.6668
|
|
18.68 0.0986 0.2795 0.0806 0.0284 7.323 46.157 41.088 5460.872 5.215 182.760 3.413 0.79 477005. 0.6418
|
|
22.42 0.1184 0.3272 0.0782 0.0283 7.286 45.920 39.877 5432.915 5.188 177.374 3.329 0.79 477368. 0.6168
|
|
26.16 0.1381 0.3723 0.0757 0.0281 7.234 45.593 38.610 5394.247 5.151 171.738 3.247 0.79 477750. 0.5918
|
|
29.89 0.1578 0.4147 0.0731 0.0278 7.167 45.171 37.288 5344.206 5.103 165.858 3.165 0.79 478151. 0.5670
|
|
33.63 0.1776 0.4547 0.0704 0.0275 7.083 44.646 35.913 5282.123 5.044 159.741 3.084 0.79 478572. 0.5422
|
|
37.37 0.1973 0.4921 0.0676 0.0271 6.983 44.014 34.486 5207.319 4.973 153.394 3.004 0.79 479013. 0.5175
|
|
41.10 0.2170 0.5270 0.0647 0.0267 6.865 43.268 33.009 5119.120 4.888 146.824 2.925 0.80 479475. 0.4930
|
|
44.84 0.2368 0.5595 0.0617 0.0261 6.728 42.403 31.483 5016.834 4.791 140.038 2.846 0.80 479957. 0.4686
|
|
48.58 0.2565 0.5897 0.0587 0.0255 6.571 41.414 29.911 4899.745 4.679 133.044 2.769 0.80 480461. 0.4443
|
|
52.31 0.2762 0.6174 0.0555 0.0248 6.393 40.293 28.293 4767.178 4.552 125.848 2.692 0.80 480987. 0.4201
|
|
56.05 0.2959 0.6427 0.0522 0.0241 6.193 39.036 26.632 4618.472 4.410 118.460 2.615 0.80 481534. 0.3960
|
|
59.79 0.3157 0.6655 0.0489 0.0232 5.972 37.637 24.929 4452.955 4.252 110.885 2.539 0.80 482104. 0.3720
|
|
63.52 0.3354 0.6859 0.0455 0.0222 5.726 36.093 23.186 4270.171 4.078 103.131 2.463 0.80 482696. 0.3479
|
|
67.26 0.3551 0.7034 0.0420 0.0212 5.458 34.401 21.404 4069.992 3.887 95.207 2.385 0.80 483311. 0.3238
|
|
71.00 0.3749 0.7179 0.0384 0.0201 5.165 32.556 19.586 3851.749 3.678 87.121 2.306 0.80 483950. 0.2995
|
|
74.73 0.3946 0.7290 0.0348 0.0188 4.848 30.557 17.734 3615.252 3.452 78.882 2.225 0.80 484612. 0.2749
|
|
78.47 0.4143 0.7359 0.0311 0.0175 4.507 28.405 15.850 3360.598 3.209 70.501 2.139 0.80 485297. 0.2499
|
|
82.21 0.4341 0.7378 0.0273 0.0161 4.141 26.100 13.937 3087.884 2.949 61.990 2.047 0.80 486007. 0.2242
|
|
85.94 0.4538 0.7329 0.0235 0.0146 3.751 23.645 11.997 2797.474 2.671 53.362 1.945 0.80 486740. 0.1977
|
|
89.68 0.4735 0.7186 0.0197 0.0130 3.339 21.046 10.034 2489.988 2.378 44.631 1.828 0.80 487498. 0.1699
|
|
93.42 0.4932 0.6904 0.0158 0.0113 2.905 18.309 8.052 2166.202 2.069 35.814 1.686 0.80 488279. 0.1403
|
|
97.15 0.5130 0.6401 0.0119 0.0095 2.450 15.444 6.054 1827.184 1.745 26.930 1.503 0.80 489084. 0.1085
|
|
100.89 0.5327 0.5507 0.0079 0.0077 1.977 12.461 4.047 1474.237 1.408 18.001 1.245 0.80 489911. 0.0735
|
|
104.63 0.5524 0.3816 0.0040 0.0058 1.486 9.369 2.033 1108.416 1.058 9.042 0.832 0.81 490751. 0.0348
|
|
108.36 0.5722
|
|
|
|
|
|
|
|
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 0.0935 0.0331 11.346 65.011 57.713 8460.778 7.345 256.706 3.094 0.87 522875. 0.6896
|
|
4.12 0.0198 0.0551 0.0917 0.0329 11.288 64.676 56.587 8417.130 7.307 251.698 3.049 0.87 523182. 0.6730
|
|
8.24 0.0396 0.1086 0.0898 0.0327 11.216 64.266 55.388 8363.785 7.261 246.365 3.004 0.87 523508. 0.6558
|
|
12.37 0.0594 0.1603 0.0877 0.0325 11.131 63.778 54.116 8300.241 7.206 240.706 2.957 0.87 523854. 0.6382
|
|
16.49 0.0792 0.2103 0.0855 0.0322 11.031 63.206 52.769 8225.866 7.141 234.718 2.910 0.87 524219. 0.6201
|
|
20.61 0.0989 0.2585 0.0832 0.0318 10.916 62.546 51.348 8139.952 7.066 228.396 2.861 0.87 524605. 0.6015
|
|
24.73 0.1187 0.3049 0.0808 0.0315 10.784 61.792 49.852 8041.854 6.981 221.744 2.812 0.87 525012. 0.5824
|
|
28.86 0.1385 0.3493 0.0783 0.0310 10.636 60.940 48.284 7930.964 6.885 214.767 2.761 0.87 525439. 0.5629
|
|
32.98 0.1583 0.3918 0.0756 0.0305 10.469 59.985 46.644 7806.682 6.777 207.475 2.710 0.87 525889. 0.5430
|
|
37.10 0.1781 0.4323 0.0728 0.0300 10.283 58.923 44.936 7668.361 6.657 199.875 2.658 0.87 526360. 0.5227
|
|
41.22 0.1979 0.4708 0.0700 0.0294 10.078 57.746 43.160 7515.248 6.524 191.977 2.605 0.87 526853. 0.5021
|
|
45.35 0.2177 0.5072 0.0670 0.0287 9.852 56.450 41.320 7346.534 6.378 183.790 2.551 0.87 527369. 0.4811
|
|
49.47 0.2375 0.5414 0.0639 0.0280 9.604 55.028 39.416 7161.485 6.217 175.325 2.496 0.88 527908. 0.4598
|
|
53.59 0.2572 0.5735 0.0607 0.0272 9.333 53.475 37.453 6959.333 6.042 166.590 2.441 0.88 528471. 0.4383
|
|
57.71 0.2770 0.6033 0.0574 0.0264 9.038 51.784 35.431 6739.293 5.851 157.597 2.385 0.88 529057. 0.4164
|
|
61.84 0.2968 0.6309 0.0541 0.0254 8.717 49.949 33.353 6500.485 5.643 148.355 2.327 0.88 529668. 0.3943
|
|
65.96 0.3166 0.6560 0.0506 0.0244 8.371 47.963 31.222 6242.015 5.419 138.877 2.269 0.88 530302. 0.3719
|
|
70.08 0.3364 0.6787 0.0471 0.0233 7.996 45.818 29.040 5962.943 5.177 129.171 2.209 0.88 530962. 0.3492
|
|
74.20 0.3562 0.6980 0.0435 0.0222 7.600 43.546 26.809 5667.187 4.920 119.247 2.146 0.88 531647. 0.3259
|
|
78.33 0.3760 0.7105 0.0398 0.0210 7.211 41.316 24.528 5377.030 4.668 109.102 2.069 0.88 532357. 0.3006
|
|
82.45 0.3958 0.7181 0.0360 0.0198 6.798 38.951 22.204 5069.174 4.401 98.762 1.987 0.88 533093. 0.2746
|
|
86.57 0.4155 0.7200 0.0322 0.0186 6.360 36.442 19.838 4742.688 4.117 88.238 1.897 0.88 533854. 0.2479
|
|
90.69 0.4353 0.7146 0.0283 0.0172 5.900 33.807 17.434 4399.739 3.819 77.545 1.797 0.88 534642. 0.2202
|
|
94.82 0.4551 0.6996 0.0243 0.0158 5.419 31.049 14.995 4040.833 3.508 66.699 1.683 0.88 535455. 0.1912
|
|
98.94 0.4749 0.6719 0.0203 0.0144 4.919 28.183 12.527 3667.843 3.184 55.719 1.549 0.88 536296. 0.1609
|
|
103.06 0.4947 0.6262 0.0163 0.0128 4.403 25.229 10.033 3283.391 2.850 44.628 1.386 0.88 537162. 0.1288
|
|
107.18 0.5145 0.5547 0.0122 0.0113 3.875 22.203 7.521 2889.547 2.508 33.454 1.181 0.88 538054. 0.0950
|
|
111.31 0.5343 0.4443 0.0081 0.0097 3.338 19.124 4.997 2488.890 2.161 22.225 0.911 0.89 538969. 0.0597
|
|
115.43 0.5541 0.2715 0.0040 0.0082 2.794 16.007 2.465 2083.151 1.808 10.962 0.537 0.89 539899. 0.0247
|
|
119.55 0.5739
|
|
|
|
|
|
|