760 lines
135 KiB
Plaintext
760 lines
135 KiB
Plaintext
12x7E-3 (12x7E-3.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 0.1413 0.0706 0.001 0.089 0.093 1.054 0.010 0.415 40.203 0.05 15441. 0.6007
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0.28 0.0247 0.0484 0.1389 0.0708 0.001 0.089 0.092 1.057 0.010 0.408 39.371 0.05 15455. 0.5831
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0.56 0.0494 0.0948 0.1362 0.0710 0.001 0.090 0.090 1.060 0.010 0.400 38.533 0.05 15470. 0.5653
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0.84 0.0741 0.1391 0.1334 0.0711 0.001 0.090 0.088 1.061 0.010 0.392 37.691 0.05 15485. 0.5472
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1.12 0.0987 0.1813 0.1304 0.0711 0.001 0.090 0.086 1.061 0.010 0.383 36.845 0.05 15502. 0.5289
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1.40 0.1234 0.2213 0.1272 0.0710 0.001 0.090 0.084 1.060 0.010 0.374 35.996 0.05 15520. 0.5104
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1.68 0.1481 0.2593 0.1239 0.0708 0.001 0.089 0.082 1.057 0.010 0.364 35.141 0.05 15539. 0.4916
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1.96 0.1728 0.2951 0.1203 0.0704 0.001 0.089 0.080 1.052 0.010 0.354 34.282 0.05 15559. 0.4726
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2.24 0.1975 0.3288 0.1165 0.0700 0.001 0.088 0.077 1.045 0.010 0.343 33.416 0.05 15579. 0.4534
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2.52 0.2222 0.3602 0.1125 0.0694 0.001 0.088 0.074 1.037 0.010 0.331 32.543 0.05 15602. 0.4340
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2.81 0.2469 0.3894 0.1084 0.0687 0.001 0.087 0.072 1.026 0.010 0.318 31.659 0.05 15625. 0.4142
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3.09 0.2716 0.4162 0.1040 0.0678 0.001 0.086 0.069 1.013 0.010 0.306 30.763 0.05 15649. 0.3943
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3.37 0.2962 0.4405 0.0994 0.0668 0.001 0.084 0.066 0.998 0.010 0.292 29.850 0.05 15674. 0.3740
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3.65 0.3209 0.4623 0.0946 0.0656 0.001 0.083 0.062 0.980 0.009 0.278 28.917 0.05 15701. 0.3534
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3.93 0.3456 0.4814 0.0896 0.0643 0.001 0.081 0.059 0.960 0.009 0.263 27.958 0.05 15729. 0.3326
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4.21 0.3703 0.4975 0.0844 0.0628 0.001 0.079 0.056 0.938 0.009 0.248 26.967 0.05 15758. 0.3114
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4.49 0.3950 0.5104 0.0791 0.0612 0.001 0.077 0.052 0.914 0.009 0.232 25.939 0.05 15788. 0.2900
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4.77 0.4197 0.5199 0.0736 0.0594 0.001 0.075 0.049 0.887 0.008 0.216 24.865 0.05 15819. 0.2682
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5.05 0.4444 0.5254 0.0680 0.0575 0.001 0.073 0.045 0.859 0.008 0.200 23.735 0.05 15851. 0.2460
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5.33 0.4691 0.5267 0.0623 0.0554 0.001 0.070 0.041 0.828 0.008 0.183 22.539 0.05 15885. 0.2236
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5.61 0.4937 0.5230 0.0564 0.0532 0.001 0.067 0.037 0.795 0.008 0.166 21.262 0.05 15920. 0.2007
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5.89 0.5184 0.5136 0.0504 0.0509 0.001 0.064 0.033 0.760 0.007 0.148 19.887 0.05 15956. 0.1775
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6.17 0.5431 0.4975 0.0443 0.0484 0.001 0.061 0.029 0.722 0.007 0.130 18.389 0.05 15993. 0.1539
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6.45 0.5678 0.4735 0.0381 0.0457 0.001 0.058 0.025 0.683 0.007 0.112 16.739 0.05 16032. 0.1299
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6.73 0.5925 0.4398 0.0319 0.0429 0.001 0.054 0.021 0.641 0.006 0.094 14.899 0.05 16072. 0.1057
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7.01 0.6172 0.3940 0.0255 0.0400 0.001 0.050 0.017 0.597 0.006 0.075 12.815 0.05 16113. 0.0814
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7.29 0.6419 0.3330 0.0192 0.0369 0.001 0.047 0.013 0.551 0.005 0.056 10.415 0.05 16155. 0.0573
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7.57 0.6665 0.2522 0.0128 0.0337 0.001 0.043 0.008 0.504 0.005 0.038 7.594 0.05 16199. 0.0341
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7.85 0.6912 0.1446 0.0064 0.0304 0.001 0.038 0.004 0.454 0.004 0.019 4.201 0.05 16244. 0.0133
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8.14 0.7159 -0.0003 0.0000 0.0270 0.001 0.034 0.000 0.404 0.004 0.000 -0.008 0.05 16290. 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 0.1419 0.0645 0.010 0.325 0.375 7.701 0.037 1.669 22.095 0.10 30881. 0.6617
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0.57 0.0253 0.0544 0.1394 0.0648 0.010 0.327 0.368 7.739 0.037 1.639 21.596 0.10 30910. 0.6410
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1.15 0.0505 0.1062 0.1367 0.0650 0.010 0.328 0.361 7.769 0.037 1.607 21.097 0.10 30940. 0.6201
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1.72 0.0758 0.1556 0.1338 0.0652 0.010 0.329 0.354 7.789 0.037 1.574 20.600 0.10 30973. 0.5991
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2.30 0.1011 0.2025 0.1308 0.0653 0.010 0.330 0.346 7.798 0.037 1.537 20.104 0.10 31007. 0.5779
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2.87 0.1263 0.2469 0.1275 0.0653 0.010 0.329 0.337 7.795 0.037 1.499 19.610 0.10 31044. 0.5567
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3.45 0.1516 0.2888 0.1240 0.0651 0.010 0.329 0.328 7.778 0.037 1.458 19.118 0.10 31083. 0.5352
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4.02 0.1769 0.3283 0.1203 0.0648 0.010 0.327 0.318 7.746 0.037 1.415 18.627 0.10 31124. 0.5137
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4.59 0.2022 0.3653 0.1164 0.0644 0.010 0.325 0.308 7.697 0.037 1.369 18.138 0.10 31167. 0.4920
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5.17 0.2274 0.3999 0.1123 0.0639 0.010 0.322 0.297 7.631 0.036 1.321 17.649 0.10 31212. 0.4702
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5.74 0.2527 0.4320 0.1080 0.0632 0.010 0.319 0.285 7.546 0.036 1.270 17.159 0.10 31260. 0.4483
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6.32 0.2780 0.4616 0.1034 0.0623 0.010 0.314 0.273 7.441 0.036 1.216 16.668 0.10 31311. 0.4262
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6.89 0.3032 0.4886 0.0987 0.0612 0.010 0.309 0.261 7.316 0.035 1.160 16.172 0.10 31363. 0.4039
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7.47 0.3285 0.5129 0.0937 0.0600 0.010 0.303 0.248 7.170 0.034 1.102 15.670 0.10 31418. 0.3814
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8.04 0.3538 0.5344 0.0886 0.0586 0.009 0.296 0.234 7.003 0.033 1.041 15.160 0.10 31476. 0.3586
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8.61 0.3790 0.5528 0.0832 0.0571 0.009 0.288 0.220 6.817 0.033 0.979 14.637 0.10 31536. 0.3357
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9.19 0.4043 0.5680 0.0777 0.0553 0.009 0.279 0.205 6.610 0.032 0.914 14.099 0.10 31598. 0.3125
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9.76 0.4296 0.5795 0.0721 0.0534 0.009 0.270 0.191 6.383 0.030 0.848 13.540 0.10 31663. 0.2890
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10.34 0.4549 0.5871 0.0663 0.0514 0.008 0.259 0.175 6.136 0.029 0.780 12.955 0.10 31731. 0.2652
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10.91 0.4801 0.5902 0.0604 0.0491 0.008 0.248 0.160 5.868 0.028 0.710 12.337 0.10 31801. 0.2410
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11.49 0.5054 0.5880 0.0543 0.0467 0.007 0.236 0.144 5.580 0.027 0.639 11.677 0.10 31873. 0.2164
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12.06 0.5307 0.5796 0.0482 0.0441 0.007 0.223 0.127 5.271 0.025 0.567 10.962 0.10 31949. 0.1913
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12.63 0.5559 0.5636 0.0419 0.0414 0.007 0.209 0.111 4.942 0.024 0.493 10.176 0.10 32026. 0.1657
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13.21 0.5812 0.5383 0.0356 0.0384 0.006 0.194 0.094 4.592 0.022 0.419 9.295 0.10 32107. 0.1394
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13.78 0.6065 0.5009 0.0292 0.0354 0.006 0.178 0.077 4.223 0.020 0.343 8.290 0.10 32190. 0.1126
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14.36 0.6317 0.4476 0.0227 0.0321 0.005 0.162 0.060 3.836 0.018 0.267 7.110 0.10 32276. 0.0853
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14.93 0.6570 0.3722 0.0163 0.0287 0.005 0.145 0.043 3.430 0.016 0.191 5.686 0.10 32364. 0.0577
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15.51 0.6823 0.2651 0.0098 0.0252 0.004 0.127 0.026 3.007 0.014 0.115 3.900 0.10 32455. 0.0307
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16.08 0.7076 0.1091 0.0033 0.0215 0.003 0.109 0.009 2.569 0.012 0.039 1.548 0.10 32548. 0.0071
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16.66 0.7328
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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 0.1423 0.0618 0.033 0.702 0.846 24.929 0.079 3.765 15.401 0.14 46321. 0.6928
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0.86 0.0252 0.0568 0.1398 0.0622 0.034 0.706 0.832 25.072 0.080 3.699 15.043 0.14 46364. 0.6707
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1.72 0.0505 0.1108 0.1371 0.0625 0.034 0.710 0.816 25.188 0.080 3.628 14.686 0.14 46410. 0.6485
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2.58 0.0757 0.1622 0.1343 0.0627 0.034 0.712 0.798 25.271 0.080 3.552 14.331 0.14 46458. 0.6262
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3.44 0.1010 0.2110 0.1312 0.0628 0.034 0.713 0.780 25.317 0.081 3.471 13.979 0.14 46510. 0.6038
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4.30 0.1262 0.2571 0.1279 0.0628 0.034 0.713 0.761 25.320 0.081 3.384 13.630 0.14 46565. 0.5813
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5.16 0.1515 0.3007 0.1245 0.0627 0.034 0.712 0.740 25.277 0.080 3.293 13.283 0.14 46623. 0.5588
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6.02 0.1767 0.3418 0.1208 0.0625 0.034 0.709 0.718 25.182 0.080 3.195 12.939 0.14 46685. 0.5363
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6.89 0.2020 0.3803 0.1169 0.0621 0.034 0.705 0.695 25.031 0.080 3.092 12.598 0.14 46749. 0.5136
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7.75 0.2272 0.4163 0.1128 0.0616 0.033 0.699 0.671 24.818 0.079 2.984 12.259 0.14 46818. 0.4909
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8.61 0.2525 0.4498 0.1085 0.0609 0.033 0.691 0.645 24.542 0.078 2.869 11.921 0.14 46890. 0.4681
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9.47 0.2777 0.4808 0.1039 0.0600 0.032 0.682 0.618 24.197 0.077 2.749 11.584 0.14 46965. 0.4453
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10.33 0.3030 0.5092 0.0991 0.0590 0.032 0.670 0.590 23.781 0.076 2.623 11.246 0.14 47044. 0.4222
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11.19 0.3282 0.5350 0.0942 0.0578 0.031 0.656 0.560 23.294 0.074 2.491 10.906 0.14 47126. 0.3991
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12.05 0.3535 0.5580 0.0890 0.0564 0.030 0.641 0.529 22.736 0.072 2.355 10.562 0.14 47213. 0.3758
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12.91 0.3787 0.5780 0.0837 0.0548 0.030 0.623 0.498 22.107 0.070 2.214 10.213 0.14 47302. 0.3523
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13.77 0.4039 0.5950 0.0782 0.0531 0.029 0.603 0.465 21.408 0.068 2.069 9.856 0.14 47396. 0.3287
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14.63 0.4292 0.6085 0.0726 0.0512 0.028 0.581 0.432 20.637 0.066 1.920 9.487 0.14 47493. 0.3048
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15.49 0.4544 0.6183 0.0668 0.0491 0.027 0.558 0.397 19.795 0.063 1.767 9.103 0.14 47594. 0.2806
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16.35 0.4797 0.6237 0.0609 0.0468 0.025 0.532 0.362 18.880 0.060 1.611 8.700 0.14 47699. 0.2560
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17.21 0.5049 0.6242 0.0549 0.0444 0.024 0.504 0.326 17.893 0.057 1.451 8.271 0.14 47808. 0.2310
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18.07 0.5302 0.6187 0.0487 0.0418 0.023 0.474 0.290 16.833 0.054 1.289 7.808 0.14 47921. 0.2055
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18.94 0.5554 0.6059 0.0425 0.0389 0.021 0.442 0.253 15.701 0.050 1.124 7.299 0.15 48037. 0.1794
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19.80 0.5807 0.5840 0.0362 0.0360 0.019 0.408 0.215 14.499 0.046 0.957 6.729 0.15 48158. 0.1526
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20.66 0.6059 0.5500 0.0298 0.0328 0.018 0.373 0.177 13.227 0.042 0.788 6.074 0.15 48282. 0.1250
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21.52 0.6312 0.4998 0.0233 0.0295 0.016 0.335 0.139 11.888 0.038 0.618 5.298 0.15 48410. 0.0965
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22.38 0.6564 0.4263 0.0169 0.0260 0.014 0.295 0.100 10.486 0.033 0.447 4.346 0.15 48543. 0.0674
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23.24 0.6817 0.3177 0.0104 0.0224 0.012 0.254 0.062 9.024 0.029 0.276 3.119 0.15 48679. 0.0380
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24.10 0.7069 0.1517 0.0040 0.0186 0.010 0.212 0.024 7.508 0.024 0.106 1.436 0.15 48818. 0.0108
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24.96 0.7322
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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 0.1427 0.0603 0.077 1.219 1.509 57.672 0.138 6.712 11.868 0.19 61760. 0.7128
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1.14 0.0250 0.0577 0.1402 0.0607 0.078 1.226 1.483 58.030 0.139 6.595 11.590 0.19 61817. 0.6901
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2.27 0.0499 0.1126 0.1376 0.0610 0.078 1.232 1.455 58.324 0.139 6.471 11.313 0.19 61877. 0.6672
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3.41 0.0749 0.1648 0.1348 0.0613 0.079 1.237 1.425 58.542 0.140 6.337 11.039 0.19 61941. 0.6443
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4.54 0.0999 0.2143 0.1317 0.0614 0.079 1.240 1.393 58.672 0.140 6.195 10.767 0.19 62009. 0.6213
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5.68 0.1249 0.2612 0.1285 0.0614 0.079 1.240 1.359 58.705 0.140 6.044 10.498 0.19 62082. 0.5984
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6.81 0.1498 0.3055 0.1251 0.0614 0.079 1.239 1.323 58.629 0.140 5.883 10.233 0.19 62158. 0.5754
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7.95 0.1748 0.3473 0.1215 0.0611 0.078 1.235 1.284 58.432 0.139 5.713 9.969 0.19 62239. 0.5524
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9.08 0.1998 0.3865 0.1176 0.0608 0.078 1.228 1.244 58.104 0.139 5.532 9.709 0.19 62324. 0.5294
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10.22 0.2247 0.4233 0.1136 0.0603 0.077 1.218 1.201 57.635 0.138 5.342 9.451 0.19 62414. 0.5064
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11.35 0.2497 0.4576 0.1093 0.0597 0.076 1.205 1.156 57.014 0.136 5.141 9.195 0.19 62508. 0.4834
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12.49 0.2747 0.4894 0.1048 0.0588 0.075 1.188 1.108 56.233 0.134 4.930 8.940 0.19 62607. 0.4602
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13.62 0.2997 0.5187 0.1001 0.0579 0.074 1.168 1.059 55.286 0.132 4.710 8.686 0.19 62711. 0.4371
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14.76 0.3246 0.5455 0.0952 0.0567 0.073 1.145 1.007 54.169 0.129 4.479 8.432 0.19 62819. 0.4138
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15.89 0.3496 0.5696 0.0902 0.0553 0.071 1.117 0.953 52.884 0.126 4.241 8.177 0.19 62932. 0.3904
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17.03 0.3746 0.5910 0.0849 0.0538 0.069 1.087 0.898 51.433 0.123 3.994 7.918 0.19 63050. 0.3669
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18.16 0.3996 0.6095 0.0795 0.0521 0.067 1.053 0.841 49.813 0.119 3.739 7.655 0.19 63172. 0.3432
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19.30 0.4245 0.6248 0.0740 0.0503 0.064 1.015 0.782 48.024 0.115 3.478 7.385 0.19 63300. 0.3193
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20.43 0.4495 0.6366 0.0683 0.0482 0.062 0.973 0.722 46.064 0.110 3.210 7.107 0.19 63432. 0.2952
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21.57 0.4745 0.6444 0.0624 0.0460 0.059 0.928 0.660 43.932 0.105 2.936 6.816 0.19 63570. 0.2708
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22.70 0.4994 0.6477 0.0565 0.0436 0.056 0.880 0.597 41.627 0.099 2.657 6.508 0.19 63712. 0.2459
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23.84 0.5244 0.6456 0.0504 0.0410 0.052 0.827 0.533 39.149 0.093 2.372 6.178 0.19 63859. 0.2206
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24.97 0.5494 0.6370 0.0443 0.0382 0.049 0.771 0.468 36.499 0.087 2.083 5.819 0.19 64012. 0.1947
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26.11 0.5744 0.6201 0.0381 0.0352 0.045 0.712 0.402 33.679 0.080 1.789 5.418 0.19 64169. 0.1680
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27.24 0.5993 0.5925 0.0317 0.0321 0.041 0.649 0.336 30.692 0.073 1.493 4.961 0.19 64332. 0.1405
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28.38 0.6243 0.5501 0.0254 0.0288 0.037 0.582 0.269 27.544 0.066 1.194 4.422 0.19 64500. 0.1120
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29.51 0.6493 0.4867 0.0190 0.0254 0.033 0.512 0.201 24.242 0.058 0.894 3.762 0.19 64673. 0.0825
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30.65 0.6742 0.3913 0.0126 0.0218 0.028 0.439 0.134 20.795 0.050 0.594 2.912 0.19 64851. 0.0520
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31.78 0.6992 0.2428 0.0063 0.0180 0.023 0.364 0.066 17.215 0.041 0.294 1.743 0.20 65034. 0.0219
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32.92 0.7242 -0.0054 -0.0001 0.0141 0.018 0.285 -0.001 13.493 0.032 -0.005 -0.037 0.20 65218. 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 0.1432 0.0594 0.149 1.875 2.365 110.923 0.212 10.520 9.671 0.24 77199. 0.7272
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1.42 0.0250 0.0588 0.1407 0.0598 0.150 1.887 2.324 111.653 0.213 10.337 9.441 0.24 77269. 0.7038
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2.84 0.0500 0.1147 0.1380 0.0601 0.151 1.898 2.280 112.255 0.214 10.142 9.213 0.24 77345. 0.6803
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4.26 0.0750 0.1678 0.1352 0.0604 0.151 1.905 2.233 112.708 0.215 9.934 8.988 0.24 77425. 0.6567
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5.68 0.0999 0.2182 0.1322 0.0605 0.152 1.910 2.183 112.990 0.216 9.711 8.764 0.24 77510. 0.6332
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7.10 0.1249 0.2659 0.1289 0.0606 0.152 1.912 2.130 113.078 0.216 9.475 8.544 0.24 77601. 0.6097
|
|
8.52 0.1499 0.3109 0.1255 0.0605 0.151 1.909 2.074 112.951 0.216 9.223 8.326 0.24 77696. 0.5863
|
|
9.94 0.1749 0.3534 0.1219 0.0603 0.151 1.903 2.013 112.587 0.215 8.956 8.112 0.24 77798. 0.5628
|
|
11.36 0.1999 0.3933 0.1180 0.0600 0.150 1.893 1.950 111.964 0.214 8.673 7.899 0.24 77904. 0.5394
|
|
12.78 0.2249 0.4307 0.1140 0.0595 0.149 1.877 1.883 111.060 0.212 8.375 7.689 0.24 78017. 0.5159
|
|
14.20 0.2499 0.4656 0.1097 0.0589 0.147 1.857 1.812 109.857 0.210 8.060 7.482 0.24 78135. 0.4925
|
|
15.62 0.2748 0.4981 0.1052 0.0580 0.145 1.831 1.738 108.338 0.207 7.730 7.276 0.24 78259. 0.4690
|
|
17.04 0.2998 0.5281 0.1005 0.0571 0.143 1.800 1.660 106.489 0.203 7.384 7.071 0.24 78388. 0.4455
|
|
18.46 0.3248 0.5556 0.0956 0.0559 0.140 1.763 1.579 104.302 0.199 7.024 6.867 0.24 78524. 0.4219
|
|
19.87 0.3498 0.5804 0.0905 0.0545 0.136 1.721 1.495 101.782 0.194 6.649 6.662 0.24 78665. 0.3983
|
|
21.29 0.3748 0.6026 0.0852 0.0530 0.133 1.672 1.408 98.929 0.189 6.262 6.455 0.24 78813. 0.3745
|
|
22.71 0.3998 0.6219 0.0798 0.0513 0.128 1.618 1.318 95.742 0.183 5.864 6.245 0.24 78966. 0.3506
|
|
24.13 0.4248 0.6381 0.0742 0.0494 0.124 1.559 1.226 92.218 0.176 5.454 6.031 0.24 79126. 0.3266
|
|
25.55 0.4497 0.6509 0.0685 0.0473 0.118 1.494 1.132 88.353 0.169 5.035 5.811 0.24 79292. 0.3023
|
|
26.97 0.4747 0.6599 0.0627 0.0451 0.113 1.422 1.035 84.145 0.161 4.605 5.581 0.24 79463. 0.2777
|
|
28.39 0.4997 0.6645 0.0567 0.0426 0.107 1.345 0.937 79.591 0.152 4.167 5.339 0.24 79642. 0.2527
|
|
29.81 0.5247 0.6639 0.0506 0.0400 0.100 1.263 0.837 74.692 0.143 3.721 5.080 0.24 79826. 0.2272
|
|
31.23 0.5497 0.6569 0.0445 0.0372 0.093 1.174 0.735 69.450 0.133 3.268 4.798 0.24 80017. 0.2011
|
|
32.65 0.5747 0.6419 0.0382 0.0342 0.086 1.080 0.631 63.869 0.122 2.809 4.484 0.24 80214. 0.1742
|
|
34.07 0.5997 0.6161 0.0319 0.0311 0.078 0.980 0.527 57.955 0.111 2.344 4.125 0.24 80418. 0.1464
|
|
35.49 0.6246 0.5757 0.0255 0.0277 0.069 0.874 0.422 51.719 0.099 1.877 3.700 0.24 80628. 0.1175
|
|
36.91 0.6496 0.5138 0.0191 0.0242 0.061 0.764 0.316 45.175 0.086 1.407 3.175 0.24 80844. 0.0873
|
|
38.33 0.6746 0.4185 0.0127 0.0205 0.051 0.648 0.211 38.343 0.073 0.936 2.490 0.24 81067. 0.0559
|
|
39.75 0.6996 0.2659 0.0064 0.0167 0.042 0.528 0.105 31.245 0.060 0.467 1.526 0.24 81296. 0.0242
|
|
41.17 0.7246 -0.0006 0.0000 0.0128 0.032 0.403 0.000 23.861 0.046 -0.001 -0.004 0.24 81525. 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 0.1437 0.0588 0.255 2.674 3.417 189.805 0.302 15.201 8.167 0.29 92635. 0.7382
|
|
1.71 0.0250 0.0596 0.1412 0.0593 0.256 2.692 3.358 191.106 0.304 14.938 7.971 0.29 92720. 0.7142
|
|
3.41 0.0500 0.1163 0.1385 0.0596 0.258 2.707 3.295 192.186 0.306 14.657 7.777 0.29 92811. 0.6903
|
|
5.12 0.0750 0.1701 0.1357 0.0598 0.259 2.719 3.227 193.004 0.307 14.356 7.585 0.29 92908. 0.6663
|
|
6.82 0.1001 0.2212 0.1326 0.0600 0.260 2.726 3.155 193.523 0.308 14.035 7.395 0.29 93010. 0.6423
|
|
8.53 0.1251 0.2695 0.1294 0.0601 0.260 2.729 3.078 193.705 0.308 13.693 7.208 0.29 93119. 0.6184
|
|
10.23 0.1501 0.3151 0.1260 0.0600 0.260 2.726 2.997 193.511 0.308 13.329 7.024 0.29 93234. 0.5945
|
|
11.94 0.1751 0.3581 0.1223 0.0598 0.259 2.717 2.910 192.901 0.307 12.943 6.842 0.29 93356. 0.5707
|
|
13.64 0.2001 0.3986 0.1185 0.0595 0.257 2.702 2.818 191.836 0.305 12.535 6.663 0.29 93484. 0.5469
|
|
15.35 0.2251 0.4365 0.1144 0.0590 0.255 2.681 2.721 190.281 0.303 12.103 6.486 0.29 93620. 0.5232
|
|
17.06 0.2502 0.4719 0.1101 0.0584 0.252 2.651 2.619 188.201 0.300 11.648 6.311 0.29 93762. 0.4994
|
|
18.76 0.2752 0.5049 0.1056 0.0575 0.249 2.614 2.511 185.568 0.295 11.171 6.138 0.29 93911. 0.4757
|
|
20.47 0.3002 0.5354 0.1008 0.0565 0.245 2.569 2.399 182.354 0.290 10.670 5.967 0.29 94067. 0.4519
|
|
22.17 0.3252 0.5634 0.0959 0.0554 0.239 2.515 2.282 178.550 0.284 10.149 5.796 0.29 94230. 0.4281
|
|
23.88 0.3502 0.5888 0.0908 0.0540 0.234 2.453 2.160 174.159 0.277 9.607 5.625 0.29 94400. 0.4042
|
|
25.58 0.3752 0.6116 0.0855 0.0525 0.227 2.383 2.034 169.184 0.269 9.047 5.453 0.29 94578. 0.3803
|
|
27.29 0.4002 0.6316 0.0801 0.0507 0.219 2.305 1.904 163.620 0.260 8.471 5.279 0.29 94762. 0.3562
|
|
29.00 0.4253 0.6485 0.0745 0.0488 0.211 2.218 1.771 157.463 0.251 7.878 5.102 0.29 94954. 0.3320
|
|
30.70 0.4503 0.6621 0.0687 0.0467 0.202 2.123 1.635 150.706 0.240 7.271 4.920 0.29 95154. 0.3075
|
|
32.41 0.4753 0.6720 0.0628 0.0444 0.192 2.019 1.495 143.345 0.228 6.649 4.730 0.29 95361. 0.2828
|
|
34.11 0.5003 0.6776 0.0568 0.0420 0.182 1.907 1.352 135.376 0.215 6.016 4.531 0.29 95575. 0.2577
|
|
35.82 0.5253 0.6781 0.0508 0.0393 0.170 1.786 1.207 126.799 0.202 5.370 4.319 0.29 95797. 0.2320
|
|
37.52 0.5503 0.6724 0.0446 0.0365 0.158 1.657 1.060 117.618 0.187 4.715 4.087 0.29 96026. 0.2058
|
|
39.23 0.5754 0.6587 0.0383 0.0334 0.145 1.519 0.911 107.839 0.172 4.050 3.830 0.29 96264. 0.1787
|
|
40.93 0.6004 0.6344 0.0319 0.0302 0.131 1.373 0.760 97.475 0.155 3.379 3.535 0.29 96508. 0.1507
|
|
42.64 0.6254 0.5953 0.0255 0.0268 0.116 1.219 0.608 86.544 0.138 2.703 3.184 0.29 96761. 0.1214
|
|
44.35 0.6504 0.5343 0.0191 0.0233 0.101 1.058 0.455 75.073 0.119 2.023 2.748 0.29 97022. 0.0906
|
|
46.05 0.6754 0.4383 0.0127 0.0196 0.085 0.889 0.302 63.095 0.100 1.343 2.171 0.29 97290. 0.0583
|
|
47.76 0.7004 0.2806 0.0063 0.0157 0.068 0.714 0.150 50.650 0.081 0.666 1.340 0.29 97565. 0.0254
|
|
49.46 0.7254 -0.0069 -0.0001 0.0117 0.051 0.531 -0.003 37.686 0.060 -0.012 -0.032 0.29 97838. 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 0.1442 0.0585 0.402 3.618 4.670 299.635 0.409 20.772 7.069 0.33 108070. 0.7470
|
|
2.02 0.0254 0.0610 0.1417 0.0589 0.405 3.644 4.588 301.782 0.412 20.409 6.896 0.33 108171. 0.7223
|
|
4.04 0.0508 0.1191 0.1390 0.0593 0.407 3.665 4.501 303.561 0.414 20.019 6.725 0.33 108279. 0.6976
|
|
6.06 0.0762 0.1741 0.1361 0.0595 0.409 3.682 4.407 304.908 0.416 19.602 6.556 0.33 108393. 0.6729
|
|
8.08 0.1015 0.2262 0.1330 0.0597 0.410 3.692 4.307 305.760 0.417 19.157 6.389 0.33 108516. 0.6483
|
|
10.10 0.1269 0.2755 0.1297 0.0598 0.410 3.695 4.200 306.050 0.418 18.682 6.225 0.33 108645. 0.6238
|
|
12.12 0.1523 0.3220 0.1262 0.0597 0.410 3.691 4.086 305.713 0.417 18.176 6.063 0.33 108782. 0.5993
|
|
14.13 0.1777 0.3658 0.1225 0.0595 0.409 3.679 3.966 304.685 0.416 17.639 5.903 0.33 108928. 0.5748
|
|
16.15 0.2031 0.4069 0.1185 0.0591 0.406 3.657 3.838 302.900 0.413 17.069 5.746 0.33 109081. 0.5504
|
|
18.17 0.2285 0.4455 0.1143 0.0586 0.403 3.626 3.702 300.296 0.410 16.468 5.592 0.33 109242. 0.5261
|
|
20.19 0.2538 0.4815 0.1099 0.0580 0.398 3.584 3.560 296.818 0.405 15.833 5.439 0.33 109411. 0.5018
|
|
22.21 0.2792 0.5150 0.1053 0.0571 0.392 3.531 3.410 292.418 0.399 15.166 5.289 0.33 109589. 0.4775
|
|
24.23 0.3046 0.5459 0.1005 0.0560 0.385 3.466 3.253 287.054 0.392 14.468 5.139 0.33 109776. 0.4532
|
|
26.25 0.3300 0.5743 0.0954 0.0548 0.376 3.389 3.089 280.711 0.383 13.739 4.991 0.34 109971. 0.4289
|
|
28.27 0.3554 0.6001 0.0901 0.0534 0.367 3.301 2.919 273.399 0.373 12.983 4.842 0.34 110174. 0.4045
|
|
30.29 0.3808 0.6232 0.0847 0.0518 0.356 3.201 2.743 265.117 0.362 12.202 4.693 0.34 110386. 0.3801
|
|
32.31 0.4061 0.6433 0.0791 0.0500 0.343 3.089 2.562 255.859 0.349 11.397 4.542 0.34 110607. 0.3555
|
|
34.33 0.4315 0.6604 0.0734 0.0480 0.329 2.966 2.376 245.613 0.335 10.570 4.389 0.34 110837. 0.3308
|
|
36.35 0.4569 0.6741 0.0675 0.0458 0.314 2.830 2.186 234.371 0.320 9.723 4.230 0.34 111075. 0.3058
|
|
38.36 0.4823 0.6838 0.0615 0.0434 0.298 2.682 1.991 222.125 0.303 8.857 4.066 0.34 111322. 0.2805
|
|
40.38 0.5077 0.6891 0.0554 0.0408 0.280 2.522 1.793 208.871 0.285 7.973 3.893 0.34 111579. 0.2548
|
|
42.40 0.5331 0.6890 0.0491 0.0380 0.261 2.350 1.590 194.609 0.265 7.074 3.707 0.34 111844. 0.2286
|
|
44.42 0.5584 0.6821 0.0428 0.0350 0.241 2.166 1.385 179.347 0.245 6.161 3.503 0.34 112119. 0.2016
|
|
46.44 0.5838 0.6665 0.0364 0.0318 0.219 1.969 1.177 163.100 0.222 5.236 3.274 0.34 112403. 0.1737
|
|
48.46 0.6092 0.6389 0.0299 0.0285 0.196 1.762 0.967 145.891 0.199 4.303 3.007 0.34 112696. 0.1446
|
|
50.48 0.6346 0.5940 0.0233 0.0249 0.171 1.543 0.756 127.757 0.174 3.363 2.684 0.34 112999. 0.1141
|
|
52.50 0.6600 0.5223 0.0168 0.0212 0.146 1.313 0.544 108.745 0.148 2.420 2.270 0.34 113310. 0.0819
|
|
54.52 0.6854 0.4053 0.0103 0.0174 0.119 1.074 0.332 88.918 0.121 1.479 1.696 0.34 113631. 0.0478
|
|
56.54 0.7107 0.2001 0.0038 0.0133 0.092 0.825 0.122 68.335 0.093 0.541 0.807 0.34 113959. 0.0138
|
|
58.56 0.7361
|
|
|
|
|
|
|
|
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 0.1449 0.0583 0.598 4.712 6.127 445.990 0.532 27.253 6.231 0.38 123503. 0.7542
|
|
2.28 0.0250 0.0607 0.1424 0.0588 0.602 4.746 6.022 449.222 0.536 26.786 6.080 0.38 123617. 0.7296
|
|
4.55 0.0501 0.1183 0.1397 0.0591 0.606 4.775 5.909 451.917 0.539 26.284 5.931 0.38 123738. 0.7050
|
|
6.83 0.0751 0.1731 0.1369 0.0594 0.609 4.796 5.789 453.981 0.542 25.748 5.783 0.38 123868. 0.6804
|
|
9.10 0.1001 0.2250 0.1338 0.0596 0.611 4.811 5.660 455.319 0.543 25.175 5.638 0.38 124005. 0.6559
|
|
11.38 0.1252 0.2741 0.1306 0.0596 0.611 4.816 5.522 455.839 0.544 24.564 5.495 0.38 124151. 0.6314
|
|
13.66 0.1502 0.3205 0.1271 0.0596 0.611 4.812 5.376 455.445 0.544 23.914 5.354 0.38 124305. 0.6070
|
|
15.93 0.1752 0.3643 0.1235 0.0594 0.609 4.797 5.221 454.044 0.542 23.223 5.216 0.38 124468. 0.5827
|
|
18.21 0.2003 0.4054 0.1196 0.0591 0.606 4.771 5.057 451.541 0.539 22.492 5.079 0.38 124640. 0.5585
|
|
20.48 0.2253 0.4441 0.1155 0.0586 0.601 4.732 4.883 447.845 0.535 21.719 4.945 0.38 124821. 0.5343
|
|
22.76 0.2503 0.4802 0.1111 0.0579 0.594 4.679 4.700 442.875 0.529 20.904 4.813 0.38 125011. 0.5102
|
|
25.03 0.2754 0.5139 0.1066 0.0571 0.585 4.612 4.507 436.561 0.521 20.048 4.683 0.38 125211. 0.4861
|
|
27.31 0.3004 0.5452 0.1018 0.0561 0.575 4.531 4.305 428.838 0.512 19.150 4.554 0.38 125420. 0.4620
|
|
29.59 0.3255 0.5740 0.0968 0.0549 0.563 4.434 4.095 419.675 0.501 18.214 4.426 0.38 125638. 0.4379
|
|
31.86 0.3505 0.6004 0.0917 0.0535 0.549 4.322 3.876 409.085 0.488 17.242 4.298 0.38 125866. 0.4138
|
|
34.14 0.3755 0.6241 0.0863 0.0519 0.532 4.195 3.651 397.071 0.474 16.238 4.170 0.38 126103. 0.3896
|
|
36.41 0.4006 0.6451 0.0808 0.0502 0.514 4.053 3.418 383.622 0.458 15.203 4.041 0.38 126350. 0.3653
|
|
38.69 0.4256 0.6632 0.0752 0.0482 0.494 3.896 3.179 368.726 0.440 14.139 3.910 0.38 126607. 0.3409
|
|
40.97 0.4506 0.6782 0.0694 0.0461 0.473 3.723 2.934 352.366 0.421 13.049 3.776 0.38 126873. 0.3163
|
|
43.24 0.4757 0.6896 0.0634 0.0438 0.449 3.534 2.683 334.532 0.399 11.933 3.638 0.39 127150. 0.2913
|
|
45.52 0.5007 0.6969 0.0574 0.0412 0.423 3.330 2.427 315.215 0.376 10.795 3.492 0.39 127436. 0.2660
|
|
47.79 0.5257 0.6993 0.0512 0.0385 0.395 3.111 2.166 294.415 0.351 9.637 3.338 0.39 127733. 0.2402
|
|
50.07 0.5508 0.6958 0.0450 0.0356 0.365 2.875 1.902 272.140 0.325 8.460 3.170 0.39 128040. 0.2138
|
|
52.35 0.5758 0.6846 0.0386 0.0325 0.333 2.624 1.634 248.406 0.297 7.267 2.983 0.39 128357. 0.1864
|
|
54.62 0.6008 0.6630 0.0322 0.0292 0.299 2.359 1.363 223.246 0.266 6.062 2.769 0.39 128684. 0.1580
|
|
56.90 0.6259 0.6268 0.0258 0.0257 0.264 2.078 1.090 196.705 0.235 4.847 2.513 0.39 129021. 0.1283
|
|
59.17 0.6509 0.5684 0.0193 0.0221 0.226 1.784 0.816 168.846 0.202 3.628 2.191 0.39 129369. 0.0968
|
|
61.45 0.6759 0.4733 0.0128 0.0183 0.187 1.477 0.541 139.754 0.167 2.408 1.757 0.39 129727. 0.0632
|
|
63.73 0.7010 0.3100 0.0063 0.0143 0.147 1.157 0.268 109.526 0.131 1.192 1.110 0.39 130094. 0.0281
|
|
66.00 0.7260 -0.0096 -0.0001 0.0102 0.105 0.824 -0.006 77.988 0.093 -0.025 -0.033 0.39 130457. 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 0.1456 0.0583 0.851 5.962 7.794 634.790 0.674 34.669 5.569 0.43 138933. 0.7603
|
|
2.56 0.0250 0.0609 0.1431 0.0587 0.858 6.006 7.661 639.478 0.679 34.078 5.434 0.43 139061. 0.7355
|
|
5.12 0.0500 0.1189 0.1405 0.0591 0.863 6.042 7.519 643.393 0.683 33.443 5.300 0.43 139198. 0.7107
|
|
7.67 0.0750 0.1739 0.1376 0.0594 0.867 6.071 7.366 646.400 0.686 32.764 5.169 0.43 139344. 0.6859
|
|
10.23 0.1000 0.2260 0.1346 0.0596 0.869 6.089 7.203 648.364 0.688 32.038 5.039 0.43 139499. 0.6612
|
|
12.79 0.1251 0.2754 0.1313 0.0596 0.871 6.096 7.029 649.151 0.689 31.264 4.911 0.43 139663. 0.6366
|
|
15.35 0.1501 0.3220 0.1279 0.0596 0.870 6.091 6.843 648.625 0.688 30.440 4.786 0.43 139837. 0.6121
|
|
17.91 0.1751 0.3660 0.1242 0.0594 0.867 6.073 6.647 646.649 0.686 29.564 4.662 0.43 140020. 0.5877
|
|
20.46 0.2001 0.4074 0.1203 0.0591 0.862 6.039 6.438 643.089 0.682 28.637 4.541 0.43 140214. 0.5634
|
|
23.02 0.2251 0.4462 0.1162 0.0586 0.855 5.990 6.218 637.815 0.677 27.656 4.421 0.43 140417. 0.5391
|
|
25.58 0.2501 0.4826 0.1118 0.0579 0.846 5.923 5.985 630.708 0.669 26.621 4.304 0.43 140631. 0.5149
|
|
28.14 0.2751 0.5166 0.1072 0.0571 0.834 5.838 5.741 621.669 0.660 25.534 4.188 0.43 140856. 0.4907
|
|
30.69 0.3001 0.5482 0.1025 0.0561 0.819 5.734 5.484 610.606 0.648 24.395 4.074 0.43 141091. 0.4665
|
|
33.25 0.3251 0.5774 0.0975 0.0549 0.801 5.611 5.217 597.469 0.634 23.206 3.961 0.43 141336. 0.4423
|
|
35.81 0.3501 0.6041 0.0923 0.0535 0.781 5.468 4.940 582.279 0.618 21.971 3.848 0.43 141593. 0.4181
|
|
38.37 0.3752 0.6282 0.0869 0.0519 0.758 5.306 4.653 565.039 0.600 20.695 3.735 0.43 141860. 0.3939
|
|
40.93 0.4002 0.6497 0.0814 0.0501 0.732 5.125 4.357 545.735 0.579 19.380 3.621 0.43 142137. 0.3696
|
|
43.48 0.4252 0.6684 0.0757 0.0482 0.703 4.924 4.053 524.346 0.556 18.028 3.506 0.43 142426. 0.3451
|
|
46.04 0.4502 0.6839 0.0699 0.0460 0.672 4.704 3.742 500.853 0.531 16.642 3.388 0.43 142726. 0.3205
|
|
48.60 0.4752 0.6960 0.0639 0.0437 0.637 4.463 3.423 475.237 0.504 15.225 3.267 0.43 143036. 0.2955
|
|
51.16 0.5002 0.7041 0.0579 0.0411 0.600 4.203 3.098 447.488 0.475 13.778 3.140 0.43 143359. 0.2702
|
|
53.72 0.5252 0.7075 0.0517 0.0384 0.560 3.922 2.766 417.604 0.443 12.305 3.005 0.43 143692. 0.2444
|
|
56.27 0.5502 0.7051 0.0454 0.0354 0.517 3.621 2.430 385.597 0.409 10.808 2.858 0.43 144036. 0.2179
|
|
58.83 0.5752 0.6952 0.0390 0.0323 0.471 3.301 2.089 351.492 0.373 9.292 2.696 0.44 144393. 0.1905
|
|
61.39 0.6003 0.6753 0.0326 0.0290 0.423 2.961 1.744 315.332 0.335 7.759 2.509 0.44 144760. 0.1620
|
|
63.95 0.6253 0.6409 0.0261 0.0255 0.372 2.603 1.397 277.184 0.294 6.215 2.286 0.44 145139. 0.1321
|
|
66.51 0.6503 0.5847 0.0196 0.0218 0.318 2.227 1.048 237.137 0.252 4.664 2.005 0.44 145530. 0.1004
|
|
69.06 0.6753 0.4919 0.0131 0.0179 0.262 1.834 0.700 195.315 0.207 3.112 1.625 0.44 145932. 0.0664
|
|
71.62 0.7003 0.3299 0.0066 0.0140 0.204 1.426 0.352 151.855 0.161 1.565 1.051 0.44 146345. 0.0305
|
|
74.18 0.7253 0.0054 0.0001 0.0098 0.143 1.001 0.004 106.556 0.113 0.017 0.017 0.44 146754. 0.0001
|
|
|
|
|
|
|
|
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 0.1465 0.0584 1.170 7.374 9.678 872.384 0.833 43.049 5.032 0.48 154360. 0.7655
|
|
2.84 0.0250 0.0612 0.1440 0.0589 1.179 7.429 9.514 878.939 0.839 42.319 4.910 0.48 154503. 0.7405
|
|
5.69 0.0500 0.1194 0.1413 0.0592 1.186 7.475 9.338 884.417 0.845 41.534 4.789 0.48 154656. 0.7155
|
|
8.53 0.0751 0.1746 0.1384 0.0595 1.192 7.511 9.149 888.630 0.849 40.694 4.670 0.48 154818. 0.6906
|
|
11.37 0.1001 0.2270 0.1354 0.0597 1.195 7.534 8.947 891.391 0.851 39.795 4.552 0.48 154991. 0.6658
|
|
14.22 0.1251 0.2765 0.1321 0.0598 1.197 7.544 8.731 892.511 0.852 38.837 4.437 0.48 155174. 0.6411
|
|
17.06 0.1501 0.3234 0.1287 0.0597 1.196 7.538 8.502 891.804 0.852 37.815 4.324 0.48 155367. 0.6165
|
|
19.90 0.1751 0.3675 0.1250 0.0595 1.192 7.515 8.258 889.078 0.849 36.730 4.213 0.48 155572. 0.5919
|
|
22.74 0.2002 0.4092 0.1210 0.0592 1.186 7.473 7.999 884.149 0.844 35.579 4.103 0.48 155787. 0.5675
|
|
25.59 0.2252 0.4483 0.1169 0.0587 1.176 7.411 7.725 876.833 0.837 34.362 3.996 0.48 156014. 0.5431
|
|
28.43 0.2502 0.4849 0.1125 0.0581 1.163 7.328 7.437 866.970 0.828 33.078 3.891 0.48 156253. 0.5188
|
|
31.27 0.2752 0.5192 0.1079 0.0572 1.146 7.222 7.133 854.419 0.816 31.728 3.787 0.48 156503. 0.4945
|
|
34.12 0.3002 0.5510 0.1031 0.0562 1.125 7.092 6.815 839.052 0.801 30.313 3.684 0.48 156764. 0.4703
|
|
36.96 0.3252 0.5805 0.0981 0.0550 1.101 6.938 6.483 820.803 0.784 28.836 3.582 0.48 157038. 0.4460
|
|
39.80 0.3503 0.6075 0.0929 0.0536 1.072 6.759 6.138 799.697 0.764 27.302 3.481 0.48 157323. 0.4217
|
|
42.65 0.3753 0.6320 0.0875 0.0520 1.040 6.557 5.781 775.738 0.741 25.716 3.380 0.48 157620. 0.3974
|
|
45.49 0.4003 0.6539 0.0819 0.0502 1.004 6.330 5.414 748.909 0.715 24.081 3.279 0.48 157929. 0.3730
|
|
48.33 0.4253 0.6730 0.0762 0.0482 0.964 6.079 5.036 719.182 0.687 22.401 3.176 0.48 158251. 0.3485
|
|
51.18 0.4503 0.6891 0.0703 0.0460 0.921 5.803 4.649 686.528 0.656 20.678 3.071 0.48 158584. 0.3238
|
|
54.02 0.4754 0.7017 0.0644 0.0436 0.873 5.502 4.253 650.923 0.622 18.915 2.963 0.48 158930. 0.2988
|
|
56.86 0.5004 0.7105 0.0582 0.0410 0.821 5.176 3.848 612.353 0.585 17.116 2.850 0.48 159288. 0.2734
|
|
59.70 0.5254 0.7147 0.0520 0.0382 0.765 4.825 3.436 570.816 0.545 15.284 2.730 0.48 159659. 0.2475
|
|
62.55 0.5504 0.7131 0.0457 0.0352 0.706 4.449 3.018 526.329 0.503 13.423 2.601 0.48 160043. 0.2209
|
|
65.39 0.5754 0.7042 0.0393 0.0321 0.642 4.048 2.594 478.925 0.457 11.537 2.456 0.48 160439. 0.1934
|
|
68.23 0.6005 0.6853 0.0328 0.0287 0.575 3.623 2.165 428.667 0.409 9.631 2.291 0.48 160848. 0.1648
|
|
71.08 0.6255 0.6521 0.0262 0.0252 0.504 3.175 1.733 375.647 0.359 7.710 2.093 0.49 161269. 0.1347
|
|
73.92 0.6505 0.5970 0.0197 0.0214 0.429 2.705 1.300 319.992 0.306 5.781 1.842 0.49 161704. 0.1027
|
|
76.76 0.6755 0.5045 0.0131 0.0175 0.351 2.213 0.866 261.873 0.250 3.850 1.499 0.49 162151. 0.0682
|
|
79.61 0.7005 0.3402 0.0066 0.0135 0.270 1.703 0.433 201.484 0.192 1.926 0.975 0.49 162610. 0.0314
|
|
82.45 0.7256 -0.0001 0.0000 0.0093 0.186 1.170 0.000 138.482 0.132 -0.001 0.000 0.49 163063. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 11000
|
|
|
|
V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
|
|
(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
|
|
0.00 0.0000 0.0000 0.1474 0.0587 1.563 8.957 11.787 1165.671 1.012 52.429 4.586 0.52 169784. 0.7699
|
|
3.13 0.0250 0.0614 0.1449 0.0591 1.575 9.025 11.588 1174.562 1.020 51.544 4.475 0.52 169942. 0.7449
|
|
6.26 0.0500 0.1197 0.1423 0.0595 1.585 9.082 11.375 1181.996 1.026 50.594 4.365 0.52 170110. 0.7198
|
|
9.38 0.0751 0.1751 0.1394 0.0598 1.593 9.126 11.146 1187.717 1.031 49.576 4.256 0.52 170289. 0.6948
|
|
12.51 0.1001 0.2276 0.1363 0.0600 1.598 9.155 10.901 1191.474 1.034 48.486 4.150 0.52 170479. 0.6699
|
|
15.64 0.1251 0.2773 0.1331 0.0600 1.600 9.167 10.639 1193.011 1.036 47.322 4.045 0.52 170681. 0.6451
|
|
18.77 0.1501 0.3243 0.1296 0.0600 1.599 9.160 10.360 1192.074 1.035 46.081 3.942 0.52 170895. 0.6204
|
|
21.89 0.1751 0.3686 0.1259 0.0598 1.594 9.132 10.064 1188.411 1.032 44.762 3.841 0.52 171120. 0.5958
|
|
25.02 0.2002 0.4104 0.1219 0.0595 1.585 9.081 9.749 1181.768 1.026 43.363 3.742 0.52 171358. 0.5713
|
|
28.15 0.2252 0.4497 0.1178 0.0590 1.572 9.005 9.416 1171.904 1.017 41.883 3.644 0.52 171608. 0.5468
|
|
31.28 0.2502 0.4866 0.1134 0.0583 1.554 8.902 9.065 1158.597 1.006 40.321 3.549 0.53 171871. 0.5224
|
|
34.40 0.2752 0.5210 0.1087 0.0574 1.531 8.772 8.695 1141.661 0.991 38.678 3.455 0.53 172147. 0.4981
|
|
37.53 0.3002 0.5531 0.1039 0.0564 1.503 8.613 8.308 1120.927 0.973 36.955 3.362 0.53 172435. 0.4738
|
|
40.66 0.3253 0.5828 0.0988 0.0552 1.470 8.424 7.904 1096.301 0.952 35.155 3.270 0.53 172737. 0.4495
|
|
43.79 0.3503 0.6102 0.0936 0.0537 1.432 8.205 7.483 1067.816 0.927 33.286 3.179 0.53 173051. 0.4252
|
|
46.91 0.3753 0.6350 0.0882 0.0521 1.389 7.956 7.049 1035.481 0.899 31.354 3.088 0.53 173379. 0.4008
|
|
50.04 0.4003 0.6573 0.0826 0.0503 1.340 7.678 6.601 999.273 0.867 29.361 2.996 0.53 173719. 0.3764
|
|
53.17 0.4253 0.6768 0.0768 0.0483 1.286 7.370 6.141 959.155 0.833 27.313 2.904 0.53 174073. 0.3518
|
|
56.30 0.4504 0.6934 0.0709 0.0460 1.227 7.031 5.668 915.089 0.794 25.213 2.810 0.53 174441. 0.3271
|
|
59.42 0.4754 0.7066 0.0648 0.0436 1.163 6.662 5.185 867.045 0.753 23.064 2.712 0.53 174822. 0.3020
|
|
62.55 0.5004 0.7160 0.0587 0.0410 1.093 6.262 4.692 815.002 0.708 20.870 2.611 0.53 175216. 0.2766
|
|
65.68 0.5254 0.7209 0.0524 0.0382 1.018 5.832 4.190 758.959 0.659 18.636 2.504 0.53 175624. 0.2506
|
|
68.81 0.5504 0.7202 0.0460 0.0352 0.937 5.371 3.679 698.939 0.607 16.365 2.388 0.53 176047. 0.2239
|
|
71.93 0.5755 0.7123 0.0395 0.0320 0.852 4.879 3.162 634.988 0.551 14.065 2.259 0.53 176483. 0.1964
|
|
75.06 0.6005 0.6945 0.0330 0.0285 0.761 4.358 2.639 567.191 0.492 11.739 2.110 0.53 176933. 0.1676
|
|
78.19 0.6255 0.6625 0.0264 0.0249 0.665 3.809 2.112 495.672 0.430 9.395 1.933 0.53 177397. 0.1374
|
|
81.32 0.6505 0.6085 0.0198 0.0212 0.564 3.232 1.583 420.604 0.365 7.041 1.707 0.53 177875. 0.1050
|
|
84.44 0.6756 0.5168 0.0132 0.0172 0.459 2.630 1.053 342.217 0.297 4.685 1.396 0.54 178367. 0.0701
|
|
87.57 0.7006 0.3509 0.0066 0.0131 0.350 2.004 0.525 260.778 0.226 2.337 0.914 0.54 178871. 0.0324
|
|
90.70 0.7256 -0.0035 0.0000 0.0088 0.236 1.351 -0.003 175.760 0.153 -0.015 -0.009 0.54 179368. 0.0000
|
|
|
|
|
|
|
|
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 0.1485 0.0590 2.041 10.722 14.130 1522.242 1.211 62.849 4.210 0.57 185204. 0.7738
|
|
3.41 0.0250 0.0614 0.1460 0.0595 2.057 10.805 13.893 1534.016 1.221 61.797 4.108 0.57 185376. 0.7487
|
|
6.82 0.0500 0.1199 0.1433 0.0598 2.070 10.874 13.639 1543.862 1.229 60.666 4.007 0.57 185560. 0.7236
|
|
10.23 0.0751 0.1753 0.1405 0.0601 2.081 10.928 13.366 1551.441 1.235 59.452 3.908 0.57 185756. 0.6985
|
|
13.65 0.1001 0.2279 0.1374 0.0603 2.087 10.963 13.074 1556.421 1.239 58.152 3.810 0.57 185964. 0.6736
|
|
17.06 0.1251 0.2777 0.1341 0.0604 2.090 10.977 12.761 1558.467 1.240 56.762 3.714 0.57 186185. 0.6487
|
|
20.47 0.1501 0.3248 0.1306 0.0604 2.088 10.969 12.428 1557.245 1.239 55.280 3.620 0.57 186419. 0.6240
|
|
23.88 0.1751 0.3693 0.1269 0.0602 2.082 10.935 12.074 1552.421 1.235 53.704 3.528 0.57 186666. 0.5993
|
|
27.29 0.2001 0.4112 0.1229 0.0598 2.070 10.873 11.697 1543.667 1.228 52.030 3.437 0.57 186926. 0.5748
|
|
30.70 0.2252 0.4507 0.1187 0.0593 2.053 10.781 11.299 1530.659 1.218 50.258 3.348 0.57 187200. 0.5503
|
|
34.11 0.2502 0.4877 0.1143 0.0586 2.029 10.658 10.879 1513.113 1.204 48.388 3.261 0.57 187487. 0.5259
|
|
37.53 0.2752 0.5224 0.1097 0.0578 1.999 10.500 10.436 1490.784 1.186 46.420 3.175 0.57 187788. 0.5016
|
|
40.94 0.3002 0.5547 0.1048 0.0567 1.963 10.308 9.972 1463.448 1.165 44.355 3.091 0.57 188104. 0.4772
|
|
44.35 0.3252 0.5846 0.0997 0.0555 1.919 10.079 9.487 1430.986 1.139 42.199 3.007 0.57 188433. 0.4529
|
|
47.76 0.3502 0.6122 0.0944 0.0540 1.869 9.815 8.983 1393.435 1.109 39.958 2.924 0.57 188777. 0.4285
|
|
51.17 0.3753 0.6374 0.0889 0.0524 1.811 9.514 8.462 1350.813 1.075 37.640 2.841 0.58 189135. 0.4042
|
|
54.58 0.4003 0.6601 0.0833 0.0505 1.747 9.178 7.925 1303.089 1.037 35.250 2.758 0.58 189507. 0.3797
|
|
57.99 0.4253 0.6800 0.0775 0.0485 1.677 8.806 7.372 1250.220 0.995 32.793 2.675 0.58 189894. 0.3551
|
|
61.41 0.4503 0.6971 0.0715 0.0462 1.599 8.397 6.806 1192.154 0.949 30.272 2.589 0.58 190295. 0.3303
|
|
64.82 0.4753 0.7108 0.0654 0.0438 1.514 7.951 6.226 1128.852 0.898 27.693 2.502 0.58 190711. 0.3052
|
|
68.23 0.5003 0.7209 0.0592 0.0411 1.422 7.468 5.634 1060.293 0.844 25.059 2.410 0.58 191142. 0.2797
|
|
71.64 0.5254 0.7265 0.0529 0.0382 1.323 6.948 5.031 986.471 0.785 22.377 2.313 0.58 191587. 0.2537
|
|
75.05 0.5504 0.7266 0.0464 0.0352 1.217 6.391 4.418 907.419 0.722 19.651 2.208 0.58 192048. 0.2270
|
|
78.46 0.5754 0.7196 0.0399 0.0319 1.104 5.798 3.797 823.200 0.655 16.888 2.092 0.58 192524. 0.1993
|
|
81.87 0.6004 0.7029 0.0333 0.0284 0.984 5.169 3.169 733.924 0.584 14.094 1.958 0.58 193015. 0.1705
|
|
85.29 0.6254 0.6722 0.0266 0.0248 0.858 4.506 2.536 639.754 0.509 11.279 1.798 0.58 193522. 0.1400
|
|
88.70 0.6504 0.6195 0.0200 0.0210 0.725 3.810 1.900 540.922 0.430 8.451 1.593 0.58 194043. 0.1074
|
|
92.11 0.6755 0.5287 0.0133 0.0170 0.587 3.083 1.264 437.730 0.348 5.620 1.309 0.58 194580. 0.0720
|
|
95.52 0.7005 0.3616 0.0066 0.0128 0.443 2.328 0.629 330.531 0.263 2.799 0.864 0.59 195130. 0.0335
|
|
98.93 0.7255 -0.0059 -0.0001 0.0085 0.293 1.539 -0.007 218.569 0.174 -0.029 -0.014 0.59 195670. 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 0.1497 0.0595 2.616 12.682 16.718 1950.599 1.433 74.362 3.887 0.62 200618. 0.7772
|
|
3.69 0.0250 0.0614 0.1472 0.0599 2.636 12.782 16.441 1965.891 1.444 73.129 3.793 0.62 200806. 0.7521
|
|
7.39 0.0500 0.1199 0.1445 0.0603 2.653 12.865 16.142 1978.678 1.453 71.801 3.700 0.62 201006. 0.7269
|
|
11.08 0.0750 0.1754 0.1417 0.0606 2.667 12.929 15.822 1988.520 1.461 70.374 3.609 0.62 201219. 0.7019
|
|
14.78 0.1000 0.2280 0.1386 0.0608 2.675 12.971 15.478 1994.987 1.465 68.845 3.519 0.62 201445. 0.6769
|
|
18.47 0.1251 0.2778 0.1353 0.0609 2.679 12.988 15.110 1997.648 1.467 67.209 3.431 0.62 201685. 0.6521
|
|
22.17 0.1501 0.3250 0.1318 0.0608 2.677 12.978 14.717 1996.071 1.466 65.463 3.344 0.62 201939. 0.6273
|
|
25.86 0.1751 0.3696 0.1280 0.0607 2.668 12.937 14.299 1989.828 1.462 63.604 3.259 0.62 202207. 0.6027
|
|
29.56 0.2001 0.4116 0.1241 0.0603 2.653 12.864 13.855 1978.495 1.453 61.629 3.176 0.62 202490. 0.5781
|
|
33.25 0.2251 0.4512 0.1199 0.0598 2.631 12.754 13.385 1961.659 1.441 59.537 3.095 0.62 202787. 0.5536
|
|
36.95 0.2501 0.4883 0.1154 0.0591 2.600 12.607 12.888 1938.952 1.424 57.327 3.015 0.62 203099. 0.5292
|
|
40.64 0.2751 0.5232 0.1107 0.0582 2.561 12.419 12.365 1910.060 1.403 55.001 2.936 0.62 203427. 0.5049
|
|
44.34 0.3001 0.5557 0.1058 0.0571 2.514 12.189 11.817 1874.705 1.377 52.561 2.859 0.62 203769. 0.4805
|
|
48.03 0.3251 0.5859 0.1007 0.0559 2.458 11.916 11.243 1832.719 1.346 50.009 2.782 0.62 204127. 0.4562
|
|
51.73 0.3501 0.6138 0.0953 0.0544 2.393 11.600 10.647 1784.161 1.311 47.358 2.707 0.62 204500. 0.4319
|
|
55.42 0.3752 0.6393 0.0898 0.0527 2.319 11.242 10.030 1729.050 1.270 44.614 2.631 0.62 204888. 0.4075
|
|
59.12 0.4002 0.6623 0.0841 0.0508 2.236 10.841 9.394 1667.357 1.225 41.785 2.555 0.62 205292. 0.3830
|
|
62.81 0.4252 0.6826 0.0783 0.0487 2.144 10.396 8.740 1599.020 1.175 38.875 2.479 0.62 205712. 0.3584
|
|
66.51 0.4502 0.7001 0.0722 0.0465 2.044 9.909 8.069 1523.985 1.119 35.889 2.401 0.63 206147. 0.3335
|
|
70.20 0.4752 0.7144 0.0661 0.0440 1.934 9.377 7.382 1442.202 1.059 32.833 2.321 0.63 206598. 0.3084
|
|
73.89 0.5002 0.7251 0.0598 0.0413 1.815 8.801 6.680 1353.637 0.994 29.713 2.238 0.63 207065. 0.2829
|
|
77.59 0.5252 0.7314 0.0534 0.0384 1.687 8.181 5.965 1258.295 0.924 26.533 2.150 0.63 207548. 0.2568
|
|
81.28 0.5502 0.7323 0.0469 0.0352 1.551 7.517 5.239 1156.212 0.849 23.302 2.055 0.63 208048. 0.2300
|
|
84.98 0.5752 0.7263 0.0403 0.0319 1.405 6.810 4.502 1047.473 0.769 20.026 1.949 0.63 208563. 0.2023
|
|
88.67 0.6003 0.7107 0.0336 0.0284 1.250 6.061 3.757 932.220 0.685 16.713 1.828 0.63 209096. 0.1733
|
|
92.37 0.6253 0.6812 0.0269 0.0247 1.087 5.271 3.007 810.665 0.595 13.374 1.682 0.63 209644. 0.1426
|
|
96.06 0.6503 0.6298 0.0202 0.0208 0.916 4.441 2.252 683.106 0.502 10.019 1.496 0.63 210209. 0.1098
|
|
99.76 0.6753 0.5402 0.0134 0.0168 0.737 3.576 1.498 549.936 0.404 6.661 1.235 0.63 210790. 0.0739
|
|
103.45 0.7003 0.3723 0.0067 0.0125 0.552 2.676 0.745 411.615 0.302 3.313 0.821 0.63 211387. 0.0346
|
|
107.15 0.7253 -0.0079 -0.0001 0.0081 0.358 1.737 -0.010 267.097 0.196 -0.044 -0.017 0.64 211970. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 14000
|
|
|
|
V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
|
|
(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
|
|
0.00 0.0000 0.0000 0.1511 0.0601 3.300 14.855 19.566 2460.510 1.678 87.027 3.607 0.67 216028. 0.7801
|
|
3.98 0.0250 0.0614 0.1486 0.0605 3.326 14.973 19.245 2480.048 1.692 85.600 3.520 0.67 216230. 0.7550
|
|
7.95 0.0500 0.1197 0.1459 0.0609 3.348 15.071 18.899 2496.388 1.703 84.061 3.434 0.67 216446. 0.7299
|
|
11.93 0.0750 0.1752 0.1430 0.0612 3.365 15.147 18.526 2508.964 1.711 82.406 3.349 0.67 216676. 0.7049
|
|
15.91 0.1000 0.2278 0.1400 0.0614 3.376 15.197 18.127 2517.221 1.717 80.629 3.266 0.67 216921. 0.6800
|
|
19.89 0.1250 0.2777 0.1367 0.0615 3.380 15.218 17.699 2520.615 1.719 78.726 3.185 0.67 217180. 0.6552
|
|
23.86 0.1500 0.3249 0.1331 0.0615 3.377 15.206 17.242 2518.597 1.718 76.692 3.105 0.67 217454. 0.6304
|
|
27.84 0.1750 0.3695 0.1294 0.0613 3.367 15.157 16.755 2510.629 1.712 74.525 3.027 0.67 217744. 0.6058
|
|
31.82 0.2000 0.4116 0.1254 0.0609 3.347 15.070 16.237 2496.168 1.703 72.222 2.950 0.67 218049. 0.5813
|
|
35.80 0.2250 0.4512 0.1211 0.0604 3.319 14.941 15.688 2474.705 1.688 69.780 2.875 0.67 218371. 0.5569
|
|
39.77 0.2500 0.4885 0.1166 0.0597 3.280 14.766 15.108 2445.769 1.668 67.199 2.802 0.67 218708. 0.5325
|
|
43.75 0.2750 0.5235 0.1119 0.0588 3.230 14.544 14.497 2408.968 1.643 64.481 2.729 0.67 219061. 0.5082
|
|
47.73 0.3000 0.5562 0.1070 0.0577 3.170 14.272 13.855 2363.945 1.612 61.627 2.658 0.67 219431. 0.4838
|
|
51.71 0.3250 0.5867 0.1018 0.0564 3.098 13.949 13.184 2310.494 1.576 58.642 2.588 0.67 219817. 0.4595
|
|
55.68 0.3500 0.6148 0.0964 0.0549 3.016 13.576 12.486 2248.686 1.534 55.539 2.519 0.67 220220. 0.4352
|
|
59.66 0.3750 0.6406 0.0908 0.0532 2.921 13.153 11.764 2178.557 1.486 52.327 2.449 0.67 220639. 0.4108
|
|
63.64 0.4000 0.6640 0.0851 0.0513 2.816 12.679 11.019 2100.068 1.432 49.014 2.380 0.67 221074. 0.3863
|
|
67.62 0.4250 0.6847 0.0792 0.0491 2.700 12.154 10.253 2013.152 1.373 45.604 2.310 0.67 221527. 0.3617
|
|
71.59 0.4500 0.7027 0.0731 0.0468 2.572 11.578 9.466 1917.743 1.308 42.106 2.239 0.67 221996. 0.3368
|
|
75.57 0.4750 0.7175 0.0669 0.0443 2.432 10.950 8.661 1813.777 1.237 38.524 2.166 0.67 222482. 0.3117
|
|
79.55 0.5000 0.7288 0.0605 0.0415 2.281 10.271 7.838 1701.220 1.160 34.865 2.090 0.67 222986. 0.2861
|
|
83.52 0.5250 0.7358 0.0540 0.0386 2.119 9.539 7.000 1580.076 1.078 31.137 2.009 0.68 223507. 0.2600
|
|
87.50 0.5500 0.7375 0.0475 0.0354 1.945 8.756 6.148 1450.394 0.989 27.347 1.923 0.68 224045. 0.2331
|
|
91.48 0.5750 0.7324 0.0408 0.0320 1.760 7.923 5.284 1312.281 0.895 23.504 1.826 0.68 224600. 0.2053
|
|
95.46 0.6000 0.7180 0.0341 0.0285 1.564 7.039 4.410 1165.922 0.795 19.617 1.716 0.68 225173. 0.1762
|
|
99.43 0.6250 0.6898 0.0272 0.0247 1.357 6.107 3.529 1011.585 0.690 15.697 1.582 0.68 225764. 0.1454
|
|
103.41 0.6500 0.6398 0.0204 0.0207 1.139 5.130 2.644 849.661 0.580 11.759 1.411 0.68 226372. 0.1122
|
|
107.39 0.6750 0.5513 0.0136 0.0166 0.913 4.109 1.757 680.679 0.464 7.817 1.171 0.68 226998. 0.0759
|
|
111.37 0.7000 0.3829 0.0067 0.0123 0.678 3.050 0.874 505.271 0.345 3.886 0.784 0.68 227640. 0.0358
|
|
115.34 0.7250 -0.0095 -0.0001 0.0079 0.432 1.945 -0.013 322.102 0.220 -0.059 -0.019 0.68 228266. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 15000
|
|
|
|
V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
|
|
(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
|
|
0.00 0.0000 0.0000 0.1526 0.0608 4.111 17.273 22.689 3065.484 1.952 100.920 3.357 0.71 231430. 0.7819
|
|
4.26 0.0250 0.0612 0.1501 0.0613 4.143 17.409 22.322 3089.471 1.967 99.287 3.277 0.71 231647. 0.7571
|
|
8.52 0.0500 0.1194 0.1475 0.0617 4.170 17.522 21.925 3109.567 1.980 97.524 3.198 0.71 231880. 0.7322
|
|
12.78 0.0750 0.1748 0.1446 0.0620 4.191 17.609 21.498 3125.064 1.989 95.624 3.120 0.71 232127. 0.7074
|
|
17.04 0.0999 0.2273 0.1415 0.0622 4.204 17.667 21.039 3135.236 1.996 93.581 3.044 0.71 232390. 0.6826
|
|
21.29 0.1249 0.2771 0.1382 0.0623 4.210 17.690 20.546 3139.371 1.999 91.391 2.969 0.71 232669. 0.6579
|
|
25.55 0.1499 0.3243 0.1346 0.0622 4.206 17.675 20.020 3136.752 1.997 89.047 2.895 0.71 232964. 0.6333
|
|
29.81 0.1749 0.3689 0.1309 0.0620 4.193 17.618 19.458 3126.669 1.990 86.547 2.823 0.72 233275. 0.6088
|
|
34.07 0.1999 0.4110 0.1268 0.0617 4.168 17.515 18.859 3108.434 1.979 83.887 2.752 0.72 233603. 0.5844
|
|
38.33 0.2249 0.4508 0.1226 0.0611 4.132 17.363 18.225 3081.395 1.962 81.065 2.683 0.72 233949. 0.5600
|
|
42.59 0.2499 0.4882 0.1181 0.0604 4.083 17.158 17.554 3044.974 1.938 78.079 2.615 0.72 234311. 0.5357
|
|
46.85 0.2748 0.5233 0.1133 0.0595 4.021 16.897 16.847 2998.682 1.909 74.933 2.548 0.72 234691. 0.5114
|
|
51.11 0.2998 0.5562 0.1083 0.0584 3.945 16.578 16.103 2942.085 1.873 71.628 2.483 0.72 235088. 0.4871
|
|
55.37 0.3248 0.5869 0.1031 0.0570 3.855 16.200 15.326 2874.914 1.830 68.169 2.418 0.72 235503. 0.4628
|
|
59.62 0.3498 0.6153 0.0976 0.0555 3.751 15.762 14.517 2797.267 1.781 64.572 2.354 0.72 235935. 0.4385
|
|
63.88 0.3748 0.6414 0.0920 0.0538 3.633 15.266 13.679 2709.191 1.725 60.846 2.290 0.72 236385. 0.4142
|
|
68.14 0.3998 0.6651 0.0862 0.0518 3.501 14.711 12.815 2610.654 1.662 57.000 2.226 0.72 236852. 0.3897
|
|
72.40 0.4248 0.6863 0.0802 0.0496 3.355 14.096 11.925 2501.581 1.593 53.043 2.162 0.72 237338. 0.3651
|
|
76.66 0.4497 0.7047 0.0741 0.0473 3.194 13.422 11.012 2381.887 1.516 48.980 2.097 0.72 237841. 0.3402
|
|
80.92 0.4747 0.7201 0.0678 0.0447 3.019 12.687 10.076 2251.500 1.433 44.820 2.030 0.72 238363. 0.3151
|
|
85.18 0.4997 0.7320 0.0613 0.0419 2.830 11.892 9.121 2110.388 1.344 40.569 1.960 0.72 238903. 0.2895
|
|
89.44 0.5247 0.7397 0.0548 0.0389 2.626 11.036 8.147 1958.569 1.247 36.236 1.887 0.72 239461. 0.2633
|
|
93.70 0.5497 0.7423 0.0481 0.0356 2.409 10.121 7.156 1796.139 1.143 31.830 1.807 0.72 240038. 0.2364
|
|
97.96 0.5747 0.7381 0.0414 0.0322 2.177 9.147 6.151 1623.285 1.033 27.360 1.719 0.73 240633. 0.2084
|
|
102.21 0.5997 0.7246 0.0345 0.0286 1.931 8.116 5.135 1440.310 0.917 22.838 1.617 0.73 241247. 0.1792
|
|
106.47 0.6246 0.6973 0.0276 0.0248 1.673 7.030 4.109 1247.658 0.794 18.278 1.494 0.73 241880. 0.1481
|
|
110.73 0.6496 0.6481 0.0207 0.0208 1.403 5.894 3.079 1045.944 0.666 13.694 1.335 0.73 242531. 0.1145
|
|
114.99 0.6746 0.5597 0.0138 0.0166 1.121 4.711 2.046 835.984 0.532 9.103 1.110 0.73 243201. 0.0777
|
|
119.25 0.6996 0.3897 0.0068 0.0123 0.830 3.487 1.017 618.745 0.394 4.524 0.745 0.73 243889. 0.0368
|
|
123.51 0.7246 -0.0104 -0.0001 0.0078 0.526 2.212 -0.017 392.609 0.250 -0.074 -0.019 0.73 244558. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 16000
|
|
|
|
V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
|
|
(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
|
|
0.00 0.0000 0.0000 0.1543 0.0622 5.102 20.096 26.105 3804.226 2.270 116.117 3.112 0.76 246824. 0.7776
|
|
4.54 0.0250 0.0605 0.1519 0.0626 5.136 20.231 25.691 3829.772 2.286 114.273 3.043 0.76 247056. 0.7541
|
|
9.08 0.0499 0.1183 0.1492 0.0630 5.164 20.342 25.242 3850.703 2.298 112.276 2.973 0.76 247305. 0.7304
|
|
13.62 0.0749 0.1734 0.1463 0.0632 5.185 20.424 24.757 3866.171 2.307 110.119 2.904 0.76 247570. 0.7066
|
|
18.15 0.0998 0.2257 0.1433 0.0634 5.197 20.472 24.235 3875.354 2.313 107.797 2.836 0.76 247851. 0.6828
|
|
22.69 0.1248 0.2755 0.1399 0.0634 5.200 20.483 23.674 3877.415 2.314 105.301 2.769 0.76 248150. 0.6589
|
|
27.23 0.1498 0.3227 0.1364 0.0633 5.192 20.452 23.073 3871.513 2.311 102.627 2.703 0.76 248465. 0.6349
|
|
31.77 0.1747 0.3674 0.1326 0.0631 5.172 20.374 22.430 3856.801 2.302 99.770 2.638 0.76 248799. 0.6109
|
|
36.31 0.1997 0.4096 0.1285 0.0627 5.139 20.245 21.746 3832.440 2.287 96.726 2.574 0.76 249150. 0.5868
|
|
40.85 0.2247 0.4495 0.1242 0.0621 5.093 20.061 21.019 3797.593 2.267 93.494 2.510 0.76 249520. 0.5628
|
|
45.38 0.2496 0.4871 0.1197 0.0613 5.031 19.818 20.250 3751.471 2.239 90.071 2.448 0.76 249908. 0.5387
|
|
49.92 0.2746 0.5224 0.1149 0.0604 4.953 19.511 19.438 3693.406 2.204 86.460 2.387 0.76 250314. 0.5146
|
|
54.46 0.2995 0.5555 0.1099 0.0592 4.858 19.138 18.585 3622.787 2.162 82.665 2.327 0.77 250739. 0.4905
|
|
59.00 0.3245 0.5864 0.1046 0.0579 4.746 18.696 17.691 3539.192 2.112 78.690 2.267 0.77 251182. 0.4663
|
|
63.54 0.3495 0.6151 0.0991 0.0563 4.617 18.186 16.761 3442.667 2.055 74.552 2.208 0.77 251644. 0.4421
|
|
68.08 0.3744 0.6415 0.0934 0.0545 4.470 17.608 15.797 3333.249 1.989 70.264 2.150 0.77 252125. 0.4177
|
|
72.61 0.3994 0.6656 0.0875 0.0525 4.306 16.962 14.802 3210.919 1.916 65.837 2.091 0.77 252624. 0.3933
|
|
77.15 0.4243 0.6872 0.0814 0.0503 4.124 16.247 13.777 3075.624 1.836 61.279 2.032 0.77 253143. 0.3687
|
|
81.69 0.4493 0.7061 0.0752 0.0479 3.926 15.464 12.724 2927.309 1.747 56.598 1.972 0.77 253680. 0.3439
|
|
86.23 0.4743 0.7220 0.0688 0.0452 3.709 14.612 11.646 2765.974 1.651 51.803 1.910 0.77 254237. 0.3187
|
|
90.77 0.4992 0.7343 0.0623 0.0424 3.475 13.691 10.544 2591.672 1.547 46.901 1.845 0.77 254813. 0.2930
|
|
95.31 0.5242 0.7425 0.0557 0.0393 3.225 12.702 9.421 2404.549 1.435 41.903 1.777 0.77 255409. 0.2667
|
|
99.85 0.5492 0.7453 0.0489 0.0361 2.957 11.648 8.277 2204.867 1.316 36.818 1.703 0.77 256024. 0.2395
|
|
104.38 0.5741 0.7412 0.0421 0.0326 2.673 10.529 7.117 1993.035 1.190 31.657 1.620 0.77 256658. 0.2113
|
|
108.92 0.5991 0.7273 0.0351 0.0289 2.373 9.348 5.943 1769.634 1.056 26.433 1.523 0.78 257313. 0.1816
|
|
113.46 0.6240 0.6990 0.0281 0.0251 2.059 8.111 4.758 1535.465 0.916 21.162 1.405 0.78 257987. 0.1499
|
|
118.00 0.6490 0.6477 0.0211 0.0211 1.732 6.823 3.566 1291.564 0.771 15.859 1.252 0.78 258681. 0.1156
|
|
122.54 0.6740 0.5559 0.0140 0.0170 1.394 5.490 2.371 1039.226 0.620 10.546 1.035 0.78 259395. 0.0779
|
|
127.08 0.6989 0.3818 0.0070 0.0128 1.046 4.120 1.178 779.935 0.465 5.242 0.685 0.78 260128. 0.0364
|
|
131.61 0.7239 -0.0096 -0.0001 0.0084 0.686 2.704 -0.019 511.772 0.305 -0.083 -0.017 0.78 260843. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 17000
|
|
|
|
V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
|
|
(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
|
|
0.00 0.0000 0.0000 0.1562 0.0649 6.388 23.686 29.833 4763.898 2.676 132.698 2.840 0.81 262208. 0.7586
|
|
4.82 0.0249 0.0588 0.1538 0.0652 6.416 23.789 29.370 4784.611 2.688 130.638 2.784 0.81 262456. 0.7378
|
|
9.63 0.0499 0.1152 0.1512 0.0654 6.436 23.863 28.867 4799.568 2.696 128.402 2.728 0.81 262721. 0.7167
|
|
14.45 0.0748 0.1693 0.1483 0.0655 6.447 23.904 28.323 4807.861 2.701 125.981 2.672 0.81 263003. 0.6953
|
|
19.27 0.0997 0.2210 0.1452 0.0655 6.448 23.908 27.735 4808.586 2.701 123.367 2.616 0.81 263303. 0.6737
|
|
24.09 0.1247 0.2704 0.1419 0.0654 6.438 23.869 27.103 4800.828 2.697 120.552 2.561 0.81 263622. 0.6518
|
|
28.90 0.1496 0.3175 0.1384 0.0652 6.415 23.784 26.423 4783.687 2.687 117.530 2.505 0.81 263959. 0.6297
|
|
33.72 0.1746 0.3623 0.1345 0.0648 6.378 23.648 25.696 4756.277 2.672 114.295 2.450 0.81 264314. 0.6074
|
|
38.54 0.1995 0.4048 0.1305 0.0643 6.327 23.456 24.920 4717.675 2.650 110.842 2.396 0.81 264689. 0.5848
|
|
43.36 0.2244 0.4451 0.1262 0.0636 6.258 23.204 24.094 4666.960 2.622 107.170 2.342 0.81 265083. 0.5620
|
|
48.17 0.2494 0.4832 0.1216 0.0627 6.173 22.887 23.219 4603.271 2.586 103.277 2.288 0.81 265497. 0.5390
|
|
52.99 0.2743 0.5190 0.1167 0.0617 6.069 22.502 22.294 4525.854 2.542 99.165 2.234 0.81 265930. 0.5158
|
|
57.81 0.2992 0.5527 0.1116 0.0604 5.946 22.045 21.322 4434.000 2.491 94.838 2.181 0.81 266383. 0.4924
|
|
62.63 0.3242 0.5842 0.1063 0.0590 5.803 21.514 20.302 4327.180 2.431 90.302 2.128 0.81 266855. 0.4688
|
|
67.44 0.3491 0.6135 0.1007 0.0573 5.640 20.909 19.239 4205.392 2.362 85.576 2.075 0.81 267347. 0.4450
|
|
72.26 0.3741 0.6405 0.0950 0.0555 5.456 20.229 18.138 4068.624 2.285 80.676 2.022 0.81 267859. 0.4211
|
|
77.08 0.3990 0.6650 0.0890 0.0534 5.254 19.478 16.999 3917.536 2.201 75.612 1.968 0.82 268391. 0.3968
|
|
81.90 0.4239 0.6869 0.0829 0.0511 5.031 18.654 15.826 3751.802 2.107 70.395 1.913 0.82 268943. 0.3722
|
|
86.71 0.4489 0.7059 0.0766 0.0487 4.789 17.755 14.621 3571.076 2.006 65.034 1.857 0.82 269515. 0.3472
|
|
91.53 0.4738 0.7218 0.0701 0.0460 4.526 16.782 13.386 3375.321 1.896 59.539 1.799 0.82 270107. 0.3218
|
|
96.35 0.4987 0.7338 0.0635 0.0431 4.244 15.735 12.122 3164.801 1.778 53.920 1.737 0.82 270720. 0.2958
|
|
101.16 0.5237 0.7413 0.0567 0.0401 3.942 14.617 10.833 2939.880 1.651 48.187 1.671 0.82 271353. 0.2690
|
|
105.98 0.5486 0.7428 0.0499 0.0368 3.622 13.430 9.521 2701.211 1.517 42.351 1.599 0.82 272007. 0.2412
|
|
110.80 0.5735 0.7365 0.0429 0.0334 3.285 12.180 8.189 2449.725 1.376 36.425 1.516 0.82 272681. 0.2122
|
|
115.62 0.5985 0.7192 0.0358 0.0298 2.932 10.871 6.840 2186.505 1.228 30.425 1.419 0.82 273376. 0.1815
|
|
120.43 0.6234 0.6858 0.0287 0.0261 2.565 9.511 5.478 1912.903 1.075 24.365 1.299 0.82 274092. 0.1486
|
|
125.25 0.6484 0.6272 0.0215 0.0222 2.187 8.107 4.106 1630.590 0.916 18.265 1.142 0.83 274829. 0.1132
|
|
130.07 0.6733 0.5265 0.0143 0.0183 1.799 6.670 2.731 1341.506 0.754 12.148 0.923 0.83 275586. 0.0746
|
|
134.89 0.6982 0.3474 0.0071 0.0143 1.405 5.209 1.357 1047.756 0.589 6.037 0.588 0.83 276364. 0.0335
|
|
139.70 0.7232 -0.0080 -0.0001 0.0102 1.001 3.713 -0.021 746.808 0.419 -0.095 -0.013 0.83 277127. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 18000
|
|
|
|
V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
|
|
(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
|
|
0.00 0.0000 0.0000 0.1582 0.0699 8.167 28.596 33.868 6089.884 3.231 150.647 2.522 0.86 277581. 0.7178
|
|
5.11 0.0250 0.0556 0.1558 0.0700 8.175 28.624 33.357 6095.799 3.234 148.374 2.482 0.86 277845. 0.7009
|
|
10.21 0.0499 0.1093 0.1532 0.0700 8.172 28.615 32.801 6093.959 3.233 145.897 2.441 0.86 278127. 0.6837
|
|
15.32 0.0749 0.1612 0.1504 0.0699 8.158 28.566 32.196 6083.451 3.227 143.208 2.400 0.86 278428. 0.6660
|
|
20.42 0.0999 0.2113 0.1473 0.0696 8.131 28.472 31.541 6063.356 3.217 140.295 2.359 0.86 278748. 0.6479
|
|
25.53 0.1248 0.2595 0.1440 0.0693 8.090 28.328 30.834 6032.752 3.200 137.149 2.318 0.86 279087. 0.6294
|
|
30.64 0.1498 0.3058 0.1405 0.0688 8.034 28.130 30.073 5990.701 3.178 133.763 2.277 0.86 279446. 0.6105
|
|
35.74 0.1747 0.3503 0.1366 0.0682 7.961 27.875 29.255 5936.276 3.149 130.128 2.235 0.86 279825. 0.5912
|
|
40.85 0.1997 0.3928 0.1326 0.0674 7.870 27.557 28.381 5868.506 3.113 126.240 2.194 0.86 280225. 0.5714
|
|
45.95 0.2247 0.4335 0.1282 0.0665 7.760 27.172 27.450 5786.625 3.070 122.095 2.152 0.86 280645. 0.5512
|
|
51.06 0.2496 0.4722 0.1236 0.0653 7.630 26.718 26.460 5689.846 3.019 117.694 2.109 0.86 281086. 0.5305
|
|
56.17 0.2746 0.5089 0.1187 0.0640 7.480 26.190 25.413 5577.477 2.959 113.039 2.067 0.86 281548. 0.5094
|
|
61.27 0.2996 0.5436 0.1135 0.0626 7.307 25.586 24.311 5448.901 2.891 108.134 2.024 0.86 282031. 0.4879
|
|
66.38 0.3245 0.5762 0.1081 0.0609 7.112 24.904 23.154 5303.645 2.814 102.987 1.980 0.86 282534. 0.4659
|
|
71.48 0.3495 0.6067 0.1025 0.0590 6.895 24.144 21.947 5141.787 2.728 97.619 1.936 0.86 283059. 0.4435
|
|
76.59 0.3744 0.6350 0.0967 0.0570 6.656 23.306 20.694 4963.347 2.633 92.048 1.891 0.86 283604. 0.4207
|
|
81.70 0.3994 0.6608 0.0906 0.0548 6.395 22.393 19.399 4768.895 2.530 86.287 1.845 0.86 284171. 0.3974
|
|
86.80 0.4244 0.6834 0.0844 0.0524 6.118 21.423 18.063 4562.277 2.420 80.345 1.796 0.86 284758. 0.3732
|
|
91.91 0.4493 0.7024 0.0779 0.0499 5.823 20.390 16.689 4342.375 2.304 74.233 1.743 0.87 285367. 0.3482
|
|
97.01 0.4743 0.7172 0.0714 0.0472 5.511 19.297 15.279 4109.524 2.180 67.963 1.686 0.87 285997. 0.3223
|
|
102.12 0.4993 0.7274 0.0646 0.0444 5.180 18.139 13.837 3862.833 2.049 61.547 1.625 0.87 286648. 0.2955
|
|
107.23 0.5242 0.7320 0.0578 0.0414 4.830 16.912 12.365 3601.567 1.911 54.998 1.557 0.87 287321. 0.2677
|
|
112.33 0.5492 0.7295 0.0507 0.0382 4.461 15.622 10.866 3326.939 1.765 48.331 1.481 0.87 288016. 0.2388
|
|
117.44 0.5741 0.7175 0.0436 0.0349 4.078 14.278 9.343 3040.639 1.613 41.558 1.394 0.87 288732. 0.2083
|
|
122.54 0.5991 0.6926 0.0364 0.0315 3.681 12.888 7.801 2744.651 1.456 34.700 1.289 0.87 289471. 0.1761
|
|
127.65 0.6241 0.6493 0.0292 0.0280 3.273 11.462 6.244 2440.924 1.295 27.774 1.160 0.87 290231. 0.1418
|
|
132.76 0.6490 0.5792 0.0218 0.0245 2.859 10.011 4.677 2131.890 1.131 20.804 0.995 0.87 291013. 0.1052
|
|
137.86 0.6740 0.4678 0.0145 0.0209 2.441 8.547 3.106 1820.150 0.966 13.817 0.774 0.88 291817. 0.0667
|
|
142.97 0.6990 0.2899 0.0072 0.0173 2.023 7.082 1.538 1508.219 0.800 6.840 0.462 0.88 292642. 0.0280
|
|
148.07 0.7239 -0.0089 -0.0002 0.0137 1.597 5.592 -0.036 1190.800 0.632 -0.160 -0.014 0.88 293459. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 19000
|
|
|
|
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 0.1596 0.0772 10.605 35.181 38.072 7908.379 3.975 169.342 2.184 0.90 292961. 0.6588
|
|
5.47 0.0253 0.0517 0.1573 0.0771 10.589 35.126 37.518 7896.141 3.969 166.878 2.155 0.90 293243. 0.6455
|
|
10.94 0.0507 0.1020 0.1547 0.0769 10.556 35.016 36.909 7871.429 3.956 164.172 2.127 0.90 293545. 0.6318
|
|
16.42 0.0760 0.1510 0.1519 0.0765 10.505 34.847 36.243 7833.245 3.937 161.211 2.099 0.90 293868. 0.6178
|
|
21.89 0.1014 0.1987 0.1489 0.0760 10.434 34.613 35.518 7780.689 3.911 157.982 2.070 0.90 294212. 0.6034
|
|
27.36 0.1267 0.2450 0.1456 0.0753 10.343 34.311 34.729 7712.947 3.876 154.475 2.042 0.91 294577. 0.5885
|
|
32.83 0.1521 0.2899 0.1420 0.0745 10.231 33.939 33.875 7629.311 3.834 150.678 2.014 0.91 294965. 0.5732
|
|
38.30 0.1774 0.3334 0.1381 0.0735 10.097 33.494 32.955 7529.138 3.784 146.585 1.985 0.91 295375. 0.5573
|
|
43.78 0.2028 0.3754 0.1340 0.0724 9.939 32.972 31.967 7411.823 3.725 142.191 1.956 0.91 295807. 0.5408
|
|
49.25 0.2281 0.4160 0.1296 0.0710 9.758 32.371 30.911 7276.730 3.657 137.490 1.927 0.91 296262. 0.5238
|
|
54.72 0.2534 0.4550 0.1249 0.0696 9.552 31.688 29.785 7123.285 3.580 132.484 1.897 0.91 296740. 0.5061
|
|
60.19 0.2788 0.4923 0.1199 0.0679 9.321 30.922 28.591 6950.978 3.494 127.174 1.866 0.91 297241. 0.4878
|
|
65.66 0.3041 0.5279 0.1146 0.0660 9.064 30.069 27.330 6759.297 3.397 121.564 1.834 0.91 297764. 0.4688
|
|
71.14 0.3295 0.5617 0.1090 0.0639 8.781 29.129 26.004 6547.923 3.291 115.665 1.801 0.91 298310. 0.4491
|
|
76.61 0.3548 0.5936 0.1032 0.0617 8.472 28.104 24.619 6317.510 3.175 109.504 1.768 0.91 298879. 0.4288
|
|
82.08 0.3802 0.6234 0.0972 0.0593 8.138 26.996 23.180 6068.603 3.050 103.105 1.732 0.91 299471. 0.4079
|
|
87.55 0.4055 0.6509 0.0909 0.0566 7.780 25.807 21.691 5801.241 2.916 96.483 1.696 0.91 300086. 0.3862
|
|
93.02 0.4309 0.6747 0.0845 0.0540 7.410 24.580 20.154 5525.464 2.777 89.646 1.654 0.91 300724. 0.3632
|
|
98.50 0.4562 0.6938 0.0779 0.0512 7.031 23.323 18.572 5242.818 2.635 82.608 1.607 0.91 301384. 0.3386
|
|
103.97 0.4815 0.7066 0.0710 0.0484 6.649 22.057 16.946 4958.149 2.492 75.378 1.550 0.91 302068. 0.3121
|
|
109.44 0.5069 0.7112 0.0641 0.0456 6.270 20.798 15.280 4675.292 2.350 67.967 1.482 0.92 302775. 0.2833
|
|
114.91 0.5322 0.7084 0.0569 0.0428 5.874 19.487 13.580 4380.500 2.202 60.404 1.406 0.92 303505. 0.2534
|
|
120.38 0.5576 0.6960 0.0497 0.0398 5.465 18.129 11.850 4075.359 2.048 52.708 1.319 0.92 304259. 0.2220
|
|
125.86 0.5829 0.6714 0.0423 0.0367 5.046 16.738 10.094 3762.511 1.891 44.899 1.217 0.92 305036. 0.1890
|
|
131.33 0.6083 0.6305 0.0349 0.0336 4.620 15.327 8.319 3445.393 1.732 37.001 1.095 0.92 305836. 0.1544
|
|
136.80 0.6336 0.5681 0.0274 0.0305 4.193 13.908 6.529 3126.447 1.571 29.042 0.947 0.92 306661. 0.1184
|
|
142.27 0.6589 0.4768 0.0198 0.0274 3.767 12.495 4.734 2808.727 1.412 21.057 0.764 0.92 307509. 0.0813
|
|
147.75 0.6843 0.3465 0.0123 0.0244 3.346 11.101 2.943 2495.328 1.254 13.091 0.535 0.93 308381. 0.0449
|
|
153.22 0.7096 0.1621 0.0049 0.0214 2.933 9.729 1.163 2187.011 1.099 5.175 0.241 0.93 309274. 0.0127
|
|
158.69 0.7350
|
|
|
|
|
|
|
|
PROP RPM = 20000
|
|
|
|
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 0.1592 0.0848 13.583 42.804 42.081 10128.550 4.836 187.174 1.884 0.95 308383. 0.5977
|
|
5.81 0.0256 0.0474 0.1571 0.0848 13.581 42.800 41.526 10127.377 4.835 184.707 1.860 0.95 308676. 0.5860
|
|
11.63 0.0512 0.0936 0.1548 0.0846 13.554 42.715 40.909 10107.438 4.826 181.964 1.836 0.95 308991. 0.5741
|
|
17.44 0.0767 0.1386 0.1522 0.0843 13.499 42.541 40.226 10066.105 4.806 178.924 1.813 0.95 309329. 0.5621
|
|
23.25 0.1023 0.1825 0.1493 0.0837 13.412 42.268 39.471 10001.643 4.775 175.569 1.790 0.95 309690. 0.5499
|
|
29.06 0.1279 0.2253 0.1462 0.0830 13.294 41.893 38.643 9912.966 4.733 171.882 1.768 0.95 310076. 0.5374
|
|
34.88 0.1535 0.2671 0.1428 0.0820 13.141 41.412 37.736 9799.000 4.679 167.852 1.747 0.95 310485. 0.5247
|
|
40.69 0.1790 0.3078 0.1390 0.0809 12.953 40.820 36.750 9658.943 4.612 163.465 1.726 0.95 310920. 0.5115
|
|
46.50 0.2046 0.3476 0.1350 0.0795 12.729 40.115 35.682 9492.273 4.532 158.713 1.705 0.95 311379. 0.4980
|
|
52.32 0.2302 0.3863 0.1306 0.0778 12.470 39.297 34.530 9298.639 4.440 153.590 1.684 0.95 311864. 0.4840
|
|
58.13 0.2558 0.4239 0.1260 0.0760 12.174 38.365 33.295 9078.057 4.334 148.095 1.664 0.96 312373. 0.4694
|
|
63.94 0.2813 0.4604 0.1210 0.0739 11.842 37.321 31.977 8830.938 4.216 142.233 1.642 0.96 312908. 0.4541
|
|
69.75 0.3069 0.4956 0.1157 0.0716 11.476 36.167 30.578 8557.939 4.086 136.011 1.621 0.96 313467. 0.4382
|
|
75.57 0.3325 0.5294 0.1101 0.0691 11.077 34.908 29.102 8260.155 3.944 129.447 1.598 0.96 314051. 0.4215
|
|
81.38 0.3581 0.5617 0.1043 0.0665 10.647 33.552 27.556 7939.241 3.791 122.571 1.574 0.96 314660. 0.4041
|
|
87.19 0.3836 0.5922 0.0982 0.0636 10.187 32.104 25.946 7596.555 3.627 115.410 1.549 0.96 315294. 0.3859
|
|
93.01 0.4092 0.6207 0.0918 0.0605 9.699 30.567 24.277 7232.903 3.453 107.985 1.522 0.96 315952. 0.3668
|
|
98.82 0.4348 0.6466 0.0853 0.0574 9.190 28.962 22.552 6853.183 3.272 100.310 1.493 0.96 316635. 0.3466
|
|
104.63 0.4604 0.6669 0.0786 0.0542 8.690 27.386 20.771 6480.096 3.094 92.389 1.454 0.96 317343. 0.3240
|
|
110.44 0.4860 0.6800 0.0716 0.0512 8.202 25.848 18.939 6116.290 2.920 84.239 1.404 0.96 318075. 0.2989
|
|
116.26 0.5115 0.6788 0.0645 0.0486 7.787 24.541 17.052 5807.057 2.773 75.848 1.332 0.96 318832. 0.2689
|
|
122.07 0.5371 0.6672 0.0572 0.0461 7.379 23.256 15.125 5502.886 2.627 67.278 1.247 0.97 319614. 0.2371
|
|
127.88 0.5627 0.6445 0.0498 0.0435 6.966 21.954 13.167 5194.762 2.480 58.568 1.150 0.97 320421. 0.2040
|
|
133.69 0.5883 0.6086 0.0423 0.0409 6.552 20.647 11.185 4885.464 2.333 49.752 1.038 0.97 321253. 0.1698
|
|
139.51 0.6138 0.5568 0.0348 0.0383 6.139 19.348 9.188 4578.104 2.186 40.870 0.910 0.97 322109. 0.1349
|
|
145.32 0.6394 0.4857 0.0272 0.0358 5.734 18.071 7.188 4276.091 2.042 31.970 0.762 0.97 322991. 0.0999
|
|
151.13 0.6650 0.3923 0.0197 0.0333 5.339 16.825 5.197 3981.157 1.901 23.117 0.592 0.97 323899. 0.0660
|
|
156.95 0.6906 0.2728 0.0122 0.0309 4.953 15.610 3.229 3693.735 1.764 14.361 0.396 0.97 324833. 0.0348
|
|
162.76 0.7161 0.1220 0.0049 0.0285 4.573 14.412 1.286 3410.301 1.628 5.719 0.171 0.98 325799. 0.0095
|
|
168.57 0.7417
|
|
|
|
|
|
|