612 lines
109 KiB
Plaintext
612 lines
109 KiB
Plaintext
14x14N (14x14N.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 0.1153 0.0674 0.003 0.184 0.141 2.176 0.021 0.628 29.428 0.06 23573. 0.4634
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0.53 0.0402 0.0671 0.1149 0.0688 0.003 0.188 0.141 2.221 0.021 0.625 28.723 0.06 23598. 0.4514
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1.07 0.0804 0.1308 0.1144 0.0703 0.003 0.192 0.140 2.270 0.022 0.623 27.979 0.06 23626. 0.4388
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1.60 0.1207 0.1908 0.1138 0.0720 0.003 0.196 0.139 2.322 0.022 0.620 27.204 0.06 23659. 0.4256
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2.13 0.1609 0.2469 0.1131 0.0737 0.003 0.201 0.138 2.378 0.023 0.616 26.408 0.06 23697. 0.4119
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2.67 0.2011 0.2992 0.1123 0.0755 0.003 0.206 0.137 2.436 0.023 0.612 25.597 0.06 23740. 0.3978
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3.20 0.2413 0.3476 0.1113 0.0773 0.003 0.211 0.136 2.495 0.024 0.606 24.781 0.06 23787. 0.3834
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3.73 0.2816 0.3922 0.1102 0.0791 0.003 0.216 0.135 2.552 0.024 0.600 23.967 0.06 23841. 0.3689
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4.27 0.3218 0.4332 0.1087 0.0808 0.003 0.220 0.133 2.607 0.025 0.592 23.163 0.06 23899. 0.3542
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4.80 0.3620 0.4707 0.1070 0.0823 0.004 0.225 0.131 2.657 0.025 0.583 22.371 0.06 23964. 0.3394
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5.33 0.4022 0.5049 0.1050 0.0837 0.004 0.228 0.129 2.700 0.026 0.572 21.598 0.06 24034. 0.3246
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5.87 0.4425 0.5360 0.1027 0.0847 0.004 0.231 0.126 2.735 0.026 0.559 20.843 0.06 24110. 0.3097
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6.40 0.4827 0.5641 0.0999 0.0855 0.004 0.233 0.122 2.759 0.026 0.544 20.108 0.06 24192. 0.2947
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6.93 0.5229 0.5893 0.0967 0.0858 0.004 0.234 0.118 2.769 0.026 0.527 19.390 0.06 24280. 0.2796
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7.47 0.5631 0.6117 0.0930 0.0857 0.004 0.234 0.114 2.764 0.026 0.507 18.689 0.06 24374. 0.2644
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8.00 0.6033 0.6313 0.0889 0.0850 0.004 0.232 0.109 2.742 0.026 0.484 18.001 0.06 24473. 0.2489
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8.53 0.6436 0.6480 0.0842 0.0836 0.004 0.228 0.103 2.699 0.026 0.459 17.323 0.06 24579. 0.2331
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9.07 0.6838 0.6617 0.0790 0.0817 0.004 0.223 0.097 2.636 0.025 0.430 16.650 0.06 24689. 0.2171
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9.60 0.7240 0.6723 0.0735 0.0791 0.003 0.216 0.090 2.554 0.024 0.400 15.976 0.06 24806. 0.2008
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10.13 0.7642 0.6792 0.0676 0.0760 0.003 0.207 0.083 2.453 0.023 0.368 15.292 0.06 24927. 0.1843
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10.67 0.8045 0.6820 0.0614 0.0724 0.003 0.197 0.075 2.336 0.022 0.334 14.587 0.06 25054. 0.1676
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11.20 0.8447 0.6799 0.0550 0.0683 0.003 0.186 0.067 2.204 0.021 0.299 13.848 0.06 25187. 0.1505
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11.73 0.8849 0.6716 0.0484 0.0637 0.003 0.174 0.059 2.057 0.020 0.263 13.058 0.06 25324. 0.1332
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12.27 0.9251 0.6555 0.0417 0.0588 0.003 0.160 0.051 1.898 0.018 0.227 12.191 0.06 25466. 0.1154
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12.80 0.9654 0.6290 0.0349 0.0535 0.002 0.146 0.043 1.726 0.016 0.190 11.211 0.06 25614. 0.0971
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13.33 1.0056 0.5882 0.0280 0.0478 0.002 0.130 0.034 1.543 0.015 0.152 10.064 0.06 25766. 0.0780
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13.86 1.0458 0.5261 0.0210 0.0418 0.002 0.114 0.026 1.348 0.013 0.114 8.655 0.06 25924. 0.0582
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14.40 1.0860 0.4306 0.0140 0.0354 0.002 0.097 0.017 1.143 0.011 0.076 6.821 0.06 26086. 0.0375
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14.93 1.1263 0.2771 0.0071 0.0288 0.001 0.078 0.009 0.928 0.009 0.039 4.233 0.06 26252. 0.0165
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15.46 1.1665 0.0088 0.0002 0.0219 0.001 0.060 0.000 0.706 0.007 0.001 0.130 0.06 26423. 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 0.1158 0.0609 0.021 0.664 0.567 15.721 0.075 2.522 16.356 0.11 47146. 0.5162
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1.08 0.0406 0.0751 0.1154 0.0623 0.022 0.680 0.565 16.090 0.077 2.513 15.924 0.11 47195. 0.5016
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2.15 0.0811 0.1459 0.1149 0.0639 0.022 0.697 0.563 16.496 0.079 2.503 15.471 0.11 47254. 0.4864
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3.23 0.1217 0.2122 0.1144 0.0656 0.023 0.716 0.560 16.933 0.081 2.491 15.000 0.11 47320. 0.4705
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4.30 0.1622 0.2738 0.1137 0.0674 0.023 0.735 0.557 17.397 0.083 2.477 14.519 0.11 47397. 0.4541
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5.38 0.2028 0.3308 0.1129 0.0692 0.024 0.756 0.553 17.879 0.085 2.460 14.031 0.11 47483. 0.4374
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6.45 0.2434 0.3831 0.1120 0.0711 0.025 0.776 0.548 18.369 0.088 2.440 13.544 0.11 47580. 0.4204
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7.53 0.2839 0.4311 0.1109 0.0730 0.025 0.797 0.543 18.853 0.090 2.415 13.061 0.11 47688. 0.4033
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8.60 0.3245 0.4748 0.1095 0.0748 0.026 0.816 0.536 19.316 0.092 2.384 12.586 0.11 47807. 0.3862
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9.68 0.3651 0.5145 0.1078 0.0765 0.026 0.834 0.528 19.744 0.094 2.347 12.124 0.11 47938. 0.3692
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10.75 0.4056 0.5505 0.1058 0.0779 0.027 0.850 0.518 20.118 0.096 2.304 11.676 0.11 48080. 0.3522
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11.83 0.4462 0.5831 0.1034 0.0791 0.027 0.863 0.506 20.421 0.098 2.252 11.243 0.11 48235. 0.3353
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12.91 0.4867 0.6125 0.1006 0.0799 0.028 0.872 0.493 20.637 0.099 2.191 10.826 0.11 48401. 0.3184
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13.98 0.5273 0.6389 0.0973 0.0803 0.028 0.877 0.477 20.745 0.099 2.120 10.423 0.11 48580. 0.3016
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15.06 0.5679 0.6623 0.0936 0.0803 0.028 0.876 0.458 20.726 0.099 2.039 10.034 0.11 48770. 0.2848
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16.13 0.6084 0.6830 0.0894 0.0796 0.028 0.869 0.438 20.559 0.098 1.947 9.657 0.11 48972. 0.2678
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17.21 0.6490 0.7010 0.0846 0.0783 0.027 0.855 0.414 20.229 0.097 1.843 9.292 0.11 49186. 0.2507
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18.28 0.6895 0.7162 0.0794 0.0764 0.026 0.834 0.389 19.729 0.094 1.729 8.935 0.11 49411. 0.2335
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19.36 0.7301 0.7286 0.0737 0.0738 0.026 0.806 0.361 19.067 0.091 1.605 8.584 0.11 49647. 0.2161
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20.43 0.7707 0.7378 0.0677 0.0707 0.024 0.771 0.331 18.253 0.087 1.474 8.236 0.11 49894. 0.1987
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21.51 0.8112 0.7434 0.0614 0.0670 0.023 0.731 0.301 17.301 0.083 1.338 7.884 0.11 50152. 0.1812
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22.59 0.8518 0.7448 0.0549 0.0628 0.022 0.685 0.269 16.220 0.077 1.196 7.522 0.12 50421. 0.1635
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23.66 0.8924 0.7408 0.0483 0.0582 0.020 0.635 0.236 15.019 0.072 1.052 7.142 0.12 50700. 0.1456
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24.74 0.9329 0.7300 0.0415 0.0531 0.018 0.579 0.203 13.704 0.065 0.905 6.732 0.12 50989. 0.1272
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25.81 0.9735 0.7098 0.0347 0.0476 0.016 0.519 0.170 12.280 0.059 0.755 6.273 0.12 51289. 0.1083
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26.89 1.0140 0.6759 0.0278 0.0416 0.014 0.454 0.136 10.753 0.051 0.605 5.734 0.12 51598. 0.0886
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27.96 1.0546 0.6204 0.0208 0.0354 0.012 0.386 0.102 9.129 0.044 0.453 5.061 0.12 51917. 0.0677
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29.04 1.0952 0.5276 0.0138 0.0287 0.010 0.313 0.068 7.416 0.035 0.301 4.144 0.12 52246. 0.0452
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30.11 1.1357 0.3601 0.0069 0.0218 0.008 0.238 0.034 5.622 0.027 0.150 2.727 0.12 52584. 0.0210
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31.19 1.1763 0.0032 0.0000 0.0146 0.005 0.159 0.000 3.759 0.018 0.001 0.023 0.12 52930. 0.0000
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PROP RPM = 3000
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V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
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(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
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0.00 0.0000 0.0000 0.1160 0.0582 0.068 1.430 1.278 50.745 0.162 5.685 11.425 0.17 70718. 0.5414
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1.62 0.0407 0.0789 0.1156 0.0597 0.070 1.465 1.274 52.006 0.166 5.666 11.110 0.17 70793. 0.5256
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3.24 0.0814 0.1530 0.1152 0.0613 0.072 1.504 1.269 53.392 0.170 5.645 10.780 0.17 70880. 0.5090
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4.86 0.1221 0.2223 0.1147 0.0630 0.074 1.547 1.263 54.893 0.175 5.619 10.439 0.17 70981. 0.4918
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6.48 0.1628 0.2865 0.1140 0.0648 0.076 1.591 1.257 56.487 0.180 5.589 10.090 0.17 71096. 0.4740
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8.10 0.2035 0.3456 0.1133 0.0667 0.078 1.638 1.248 58.147 0.185 5.553 9.738 0.17 71226. 0.4560
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9.71 0.2442 0.3997 0.1124 0.0687 0.080 1.686 1.238 59.836 0.190 5.508 9.386 0.17 71372. 0.4378
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11.33 0.2849 0.4491 0.1113 0.0706 0.082 1.733 1.226 61.510 0.196 5.453 9.039 0.17 71535. 0.4195
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12.95 0.3257 0.4940 0.1099 0.0724 0.085 1.778 1.211 63.119 0.201 5.385 8.700 0.17 71715. 0.4012
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14.57 0.3664 0.5347 0.1082 0.0741 0.087 1.820 1.192 64.607 0.206 5.303 8.370 0.17 71912. 0.3830
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16.19 0.4071 0.5715 0.1062 0.0756 0.088 1.857 1.170 65.917 0.210 5.205 8.051 0.17 72128. 0.3650
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17.81 0.4478 0.6047 0.1038 0.0769 0.090 1.887 1.144 66.987 0.213 5.088 7.745 0.17 72361. 0.3472
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19.43 0.4885 0.6346 0.1010 0.0778 0.091 1.909 1.113 67.757 0.216 4.951 7.451 0.17 72613. 0.3295
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21.05 0.5292 0.6615 0.0978 0.0782 0.091 1.920 1.077 68.160 0.217 4.792 7.169 0.17 72882. 0.3118
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22.67 0.5699 0.6854 0.0940 0.0782 0.091 1.919 1.036 68.129 0.217 4.608 6.898 0.17 73170. 0.2943
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24.29 0.6106 0.7066 0.0898 0.0776 0.091 1.904 0.989 67.590 0.215 4.399 6.637 0.17 73475. 0.2766
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25.90 0.6513 0.7252 0.0850 0.0763 0.089 1.873 0.936 66.488 0.212 4.164 6.386 0.17 73797. 0.2589
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27.52 0.6920 0.7412 0.0797 0.0744 0.087 1.826 0.878 64.805 0.206 3.904 6.142 0.17 74137. 0.2412
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29.14 0.7327 0.7545 0.0739 0.0718 0.084 1.763 0.815 62.562 0.199 3.623 5.906 0.17 74494. 0.2234
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30.76 0.7734 0.7650 0.0679 0.0686 0.080 1.685 0.748 59.797 0.190 3.326 5.672 0.17 74867. 0.2056
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32.38 0.8141 0.7722 0.0616 0.0649 0.076 1.593 0.678 56.551 0.180 3.017 5.440 0.17 75257. 0.1878
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34.00 0.8548 0.7756 0.0550 0.0607 0.071 1.489 0.606 52.858 0.168 2.697 5.203 0.17 75662. 0.1698
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35.62 0.8955 0.7742 0.0484 0.0559 0.065 1.373 0.533 48.745 0.155 2.370 4.958 0.17 76083. 0.1517
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37.24 0.9362 0.7667 0.0416 0.0508 0.059 1.246 0.458 44.233 0.141 2.037 4.696 0.17 76520. 0.1332
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38.86 0.9770 0.7505 0.0347 0.0451 0.053 1.108 0.382 39.341 0.125 1.700 4.406 0.17 76972. 0.1142
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40.48 1.0177 0.7216 0.0277 0.0391 0.046 0.960 0.306 34.088 0.109 1.359 4.067 0.18 77439. 0.0942
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42.09 1.0584 0.6719 0.0208 0.0327 0.038 0.803 0.229 28.495 0.091 1.017 3.641 0.18 77921. 0.0730
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43.71 1.0991 0.5845 0.0138 0.0259 0.030 0.636 0.152 22.589 0.072 0.676 3.050 0.18 78417. 0.0498
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45.33 1.1398 0.4146 0.0068 0.0188 0.022 0.462 0.075 16.404 0.052 0.336 2.086 0.18 78927. 0.0240
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46.95 1.1805 -0.0015 0.0000 0.0115 0.013 0.281 0.000 9.977 0.032 -0.001 -0.007 0.18 79448. 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 0.1162 0.0568 0.157 2.479 2.276 117.301 0.280 10.124 8.801 0.22 94290. 0.5565
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2.16 0.0408 0.0811 0.1158 0.0582 0.161 2.542 2.269 120.309 0.287 10.091 8.553 0.22 94390. 0.5399
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4.33 0.0816 0.1573 0.1154 0.0599 0.166 2.612 2.260 123.624 0.295 10.054 8.293 0.22 94507. 0.5226
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6.49 0.1224 0.2283 0.1149 0.0616 0.171 2.688 2.251 127.217 0.304 10.011 8.025 0.22 94641. 0.5046
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8.65 0.1631 0.2939 0.1143 0.0634 0.176 2.769 2.239 131.042 0.313 9.960 7.750 0.22 94795. 0.4861
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10.81 0.2039 0.3543 0.1136 0.0654 0.181 2.853 2.225 135.032 0.322 9.897 7.474 0.22 94969. 0.4673
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12.98 0.2447 0.4095 0.1127 0.0673 0.187 2.939 2.208 139.100 0.332 9.820 7.198 0.22 95164. 0.4483
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15.14 0.2855 0.4597 0.1116 0.0693 0.192 3.025 2.186 143.142 0.342 9.724 6.927 0.22 95382. 0.4292
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17.30 0.3263 0.5053 0.1102 0.0712 0.197 3.107 2.160 147.035 0.351 9.606 6.662 0.22 95622. 0.4103
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19.46 0.3671 0.5465 0.1086 0.0729 0.202 3.183 2.127 150.647 0.360 9.462 6.405 0.22 95886. 0.3915
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21.63 0.4078 0.5838 0.1066 0.0745 0.206 3.251 2.088 153.836 0.367 9.288 6.157 0.22 96174. 0.3729
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23.79 0.4486 0.6174 0.1042 0.0757 0.210 3.306 2.042 156.457 0.374 9.082 5.919 0.22 96487. 0.3545
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25.95 0.4894 0.6476 0.1015 0.0767 0.212 3.346 1.987 158.360 0.378 8.839 5.692 0.22 96823. 0.3363
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28.12 0.5302 0.6747 0.0982 0.0772 0.214 3.368 1.924 159.386 0.381 8.556 5.474 0.23 97184. 0.3182
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30.28 0.5710 0.6990 0.0945 0.0772 0.214 3.368 1.850 159.370 0.380 8.230 5.266 0.23 97569. 0.3002
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32.44 0.6118 0.7205 0.0902 0.0766 0.212 3.342 1.766 158.136 0.378 7.856 5.066 0.23 97977. 0.2822
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34.60 0.6525 0.7395 0.0853 0.0753 0.209 3.287 1.672 155.551 0.371 7.436 4.875 0.23 98409. 0.2642
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36.77 0.6933 0.7560 0.0800 0.0734 0.203 3.203 1.567 151.567 0.362 6.971 4.690 0.23 98864. 0.2461
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38.93 0.7341 0.7700 0.0743 0.0708 0.196 3.090 1.455 146.234 0.349 6.470 4.512 0.23 99341. 0.2281
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41.09 0.7749 0.7813 0.0682 0.0676 0.187 2.951 1.335 139.643 0.333 5.939 4.337 0.23 99840. 0.2100
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43.26 0.8157 0.7896 0.0618 0.0639 0.177 2.787 1.211 131.891 0.315 5.386 4.164 0.23 100362. 0.1920
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45.42 0.8565 0.7944 0.0553 0.0596 0.165 2.600 1.082 123.055 0.294 4.815 3.990 0.23 100904. 0.1740
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47.58 0.8972 0.7948 0.0486 0.0548 0.152 2.392 0.951 113.201 0.270 4.230 3.811 0.23 101468. 0.1557
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49.74 0.9380 0.7896 0.0417 0.0496 0.137 2.163 0.817 102.377 0.244 3.635 3.621 0.23 102052. 0.1372
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51.91 0.9788 0.7764 0.0348 0.0439 0.122 1.915 0.682 90.631 0.216 3.033 3.412 0.23 102657. 0.1181
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54.07 1.0196 0.7514 0.0278 0.0378 0.105 1.648 0.545 78.007 0.186 2.425 3.170 0.23 103282. 0.0981
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56.23 1.0604 0.7065 0.0208 0.0313 0.087 1.364 0.408 64.558 0.154 1.815 2.866 0.23 103926. 0.0767
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58.39 1.1012 0.6245 0.0138 0.0244 0.068 1.064 0.271 50.351 0.120 1.205 2.439 0.24 104590. 0.0532
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60.56 1.1419 0.4566 0.0069 0.0172 0.048 0.749 0.134 35.467 0.085 0.598 1.720 0.24 105273. 0.0264
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62.72 1.1827 -0.0016 0.0000 0.0097 0.027 0.423 0.000 19.998 0.048 -0.001 -0.006 0.24 105968. 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 0.1164 0.0559 0.303 3.813 3.561 225.588 0.431 15.841 7.161 0.28 117861. 0.5664
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2.73 0.0412 0.0833 0.1160 0.0574 0.311 3.914 3.550 231.546 0.442 15.793 6.955 0.28 117987. 0.5493
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5.46 0.0824 0.1614 0.1156 0.0590 0.319 4.025 3.538 238.130 0.455 15.737 6.739 0.28 118135. 0.5313
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8.20 0.1236 0.2341 0.1151 0.0608 0.329 4.146 3.524 245.281 0.468 15.673 6.516 0.28 118305. 0.5126
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10.93 0.1648 0.3012 0.1146 0.0627 0.339 4.275 3.506 252.909 0.483 15.595 6.288 0.28 118500. 0.4934
|
|
13.66 0.2061 0.3628 0.1138 0.0647 0.350 4.410 3.484 260.880 0.498 15.499 6.058 0.28 118721. 0.4740
|
|
16.39 0.2473 0.4189 0.1130 0.0667 0.361 4.548 3.458 269.019 0.514 15.379 5.830 0.28 118969. 0.4543
|
|
19.12 0.2885 0.4698 0.1119 0.0687 0.372 4.684 3.424 277.109 0.529 15.231 5.605 0.28 119246. 0.4347
|
|
21.85 0.3297 0.5160 0.1105 0.0706 0.382 4.816 3.383 284.901 0.544 15.046 5.385 0.28 119552. 0.4151
|
|
24.59 0.3709 0.5576 0.1089 0.0724 0.392 4.938 3.332 292.121 0.558 14.820 5.173 0.28 119888. 0.3958
|
|
27.32 0.4121 0.5951 0.1068 0.0740 0.400 5.046 3.270 298.479 0.570 14.545 4.969 0.28 120255. 0.3766
|
|
30.05 0.4533 0.6289 0.1044 0.0753 0.407 5.133 3.196 303.674 0.580 14.217 4.774 0.28 120653. 0.3577
|
|
32.78 0.4945 0.6593 0.1016 0.0762 0.412 5.196 3.109 307.398 0.587 13.830 4.588 0.28 121082. 0.3390
|
|
35.51 0.5357 0.6866 0.0983 0.0767 0.415 5.229 3.007 309.327 0.591 13.377 4.410 0.28 121542. 0.3205
|
|
38.24 0.5769 0.7109 0.0944 0.0766 0.415 5.225 2.890 309.115 0.590 12.853 4.240 0.28 122032. 0.3021
|
|
40.98 0.6182 0.7326 0.0900 0.0760 0.411 5.180 2.755 306.413 0.585 12.254 4.078 0.28 122553. 0.2837
|
|
43.71 0.6594 0.7517 0.0850 0.0746 0.404 5.088 2.603 300.960 0.575 11.578 3.923 0.28 123103. 0.2652
|
|
46.44 0.7006 0.7683 0.0796 0.0726 0.393 4.948 2.435 292.692 0.559 10.832 3.774 0.28 123682. 0.2468
|
|
49.17 0.7418 0.7826 0.0737 0.0698 0.378 4.762 2.255 281.724 0.538 10.030 3.630 0.29 124291. 0.2285
|
|
51.90 0.7830 0.7942 0.0674 0.0665 0.360 4.535 2.064 268.245 0.512 9.181 3.490 0.29 124927. 0.2102
|
|
54.64 0.8242 0.8028 0.0610 0.0626 0.339 4.267 1.866 252.444 0.482 8.298 3.352 0.29 125591. 0.1919
|
|
57.37 0.8654 0.8081 0.0543 0.0581 0.314 3.964 1.661 234.475 0.448 7.388 3.213 0.29 126282. 0.1736
|
|
60.10 0.9066 0.8089 0.0474 0.0532 0.288 3.625 1.452 214.459 0.410 6.457 3.070 0.29 127000. 0.1550
|
|
62.83 0.9478 0.8041 0.0405 0.0477 0.258 3.254 1.239 192.498 0.368 5.511 2.919 0.29 127745. 0.1362
|
|
65.56 0.9891 0.7911 0.0334 0.0418 0.226 2.851 1.024 168.682 0.322 4.553 2.752 0.29 128515. 0.1167
|
|
68.29 1.0303 0.7655 0.0264 0.0355 0.192 2.419 0.807 143.107 0.273 3.588 2.557 0.29 129311. 0.0962
|
|
71.03 1.0715 0.7178 0.0192 0.0287 0.155 1.959 0.589 115.887 0.221 2.620 2.305 0.29 130132. 0.0742
|
|
73.76 1.1127 0.6256 0.0121 0.0216 0.117 1.473 0.372 87.165 0.166 1.654 1.935 0.29 130977. 0.0494
|
|
76.49 1.1539 0.4162 0.0051 0.0142 0.077 0.966 0.156 57.121 0.109 0.695 1.241 0.30 131846. 0.0206
|
|
79.22 1.1951
|
|
|
|
|
|
|
|
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 0.1165 0.0554 0.518 5.439 5.136 386.082 0.614 22.846 6.034 0.33 141431. 0.5731
|
|
3.25 0.0409 0.0835 0.1162 0.0569 0.531 5.583 5.121 396.307 0.631 22.780 5.861 0.33 141581. 0.5559
|
|
6.50 0.0817 0.1619 0.1158 0.0585 0.547 5.742 5.105 407.617 0.649 22.706 5.680 0.33 141757. 0.5379
|
|
9.75 0.1226 0.2348 0.1154 0.0602 0.563 5.916 5.085 419.924 0.668 22.619 5.493 0.33 141959. 0.5191
|
|
13.00 0.1635 0.3022 0.1148 0.0621 0.581 6.101 5.062 433.082 0.689 22.514 5.301 0.33 142189. 0.4999
|
|
16.25 0.2043 0.3640 0.1142 0.0641 0.599 6.295 5.033 446.870 0.711 22.385 5.108 0.33 142451. 0.4803
|
|
19.50 0.2452 0.4203 0.1134 0.0661 0.618 6.494 4.996 460.996 0.734 22.224 4.916 0.33 142744. 0.4605
|
|
22.76 0.2861 0.4715 0.1123 0.0682 0.637 6.693 4.951 475.096 0.756 22.022 4.727 0.33 143072. 0.4408
|
|
26.01 0.3269 0.5178 0.1111 0.0701 0.655 6.885 4.894 488.747 0.778 21.770 4.542 0.33 143433. 0.4211
|
|
29.26 0.3678 0.5597 0.1095 0.0719 0.672 7.064 4.824 501.480 0.798 21.459 4.364 0.34 143831. 0.4017
|
|
32.51 0.4087 0.5974 0.1075 0.0736 0.688 7.224 4.739 512.798 0.816 21.081 4.192 0.34 144265. 0.3825
|
|
35.76 0.4495 0.6314 0.1052 0.0749 0.700 7.356 4.637 522.185 0.831 20.626 4.028 0.34 144735. 0.3635
|
|
39.01 0.4904 0.6620 0.1025 0.0759 0.710 7.454 4.516 529.109 0.842 20.087 3.871 0.34 145242. 0.3448
|
|
42.26 0.5313 0.6895 0.0992 0.0765 0.715 7.509 4.374 533.021 0.848 19.455 3.722 0.34 145785. 0.3262
|
|
45.51 0.5721 0.7142 0.0955 0.0765 0.715 7.513 4.209 533.334 0.849 18.722 3.580 0.34 146365. 0.3078
|
|
48.76 0.6130 0.7362 0.0912 0.0759 0.710 7.458 4.020 529.446 0.843 17.881 3.444 0.34 146980. 0.2894
|
|
52.01 0.6539 0.7557 0.0864 0.0747 0.699 7.338 3.806 520.875 0.829 16.930 3.314 0.34 147631. 0.2710
|
|
55.26 0.6947 0.7729 0.0810 0.0728 0.680 7.148 3.569 507.449 0.808 15.877 3.190 0.34 148316. 0.2526
|
|
58.51 0.7356 0.7878 0.0752 0.0702 0.656 6.893 3.313 489.322 0.779 14.738 3.071 0.34 149035. 0.2343
|
|
61.76 0.7765 0.8003 0.0690 0.0670 0.626 6.576 3.042 466.808 0.743 13.531 2.956 0.34 149787. 0.2161
|
|
65.01 0.8173 0.8102 0.0626 0.0632 0.590 6.202 2.759 440.231 0.701 12.272 2.842 0.34 150573. 0.1979
|
|
68.27 0.8582 0.8169 0.0560 0.0588 0.550 5.774 2.467 409.866 0.652 10.971 2.730 0.35 151390. 0.1797
|
|
71.52 0.8991 0.8198 0.0492 0.0539 0.504 5.296 2.167 375.929 0.598 9.640 2.615 0.35 152239. 0.1613
|
|
74.77 0.9399 0.8178 0.0423 0.0486 0.454 4.770 1.863 338.597 0.539 8.285 2.495 0.35 153119. 0.1427
|
|
78.02 0.9808 0.8088 0.0353 0.0428 0.400 4.198 1.554 298.027 0.474 6.912 2.365 0.35 154030. 0.1236
|
|
81.27 1.0217 0.7894 0.0282 0.0365 0.341 3.583 1.243 254.378 0.405 5.527 2.216 0.35 154970. 0.1035
|
|
84.52 1.0625 0.7520 0.0211 0.0298 0.279 2.928 0.930 207.837 0.331 4.137 2.030 0.35 155941. 0.0820
|
|
87.77 1.1034 0.6795 0.0140 0.0228 0.213 2.235 0.618 158.635 0.252 2.747 1.766 0.35 156941. 0.0582
|
|
91.02 1.1443 0.5193 0.0070 0.0154 0.144 1.508 0.307 107.068 0.170 1.366 1.301 0.35 157968. 0.0302
|
|
94.27 1.1851 0.0011 0.0000 0.0077 0.072 0.753 0.000 53.439 0.085 0.001 0.003 0.36 159011. 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 0.1167 0.0551 0.818 7.361 7.002 609.654 0.832 31.144 5.209 0.39 165000. 0.5777
|
|
3.80 0.0409 0.0842 0.1164 0.0565 0.839 7.558 6.983 625.917 0.854 31.060 5.060 0.39 165176. 0.5604
|
|
7.59 0.0818 0.1632 0.1160 0.0582 0.864 7.775 6.962 643.949 0.878 30.965 4.903 0.39 165380. 0.5422
|
|
11.39 0.1227 0.2367 0.1156 0.0599 0.890 8.013 6.937 663.619 0.905 30.855 4.741 0.39 165616. 0.5234
|
|
15.18 0.1636 0.3045 0.1151 0.0619 0.918 8.268 6.907 684.704 0.934 30.722 4.575 0.39 165885. 0.5040
|
|
18.98 0.2045 0.3668 0.1145 0.0639 0.948 8.535 6.870 706.863 0.964 30.557 4.408 0.39 166190. 0.4842
|
|
22.77 0.2454 0.4235 0.1137 0.0659 0.978 8.810 6.823 729.631 0.995 30.349 4.241 0.39 166533. 0.4643
|
|
26.57 0.2863 0.4749 0.1128 0.0680 1.009 9.085 6.764 752.423 1.026 30.086 4.077 0.39 166915. 0.4444
|
|
30.37 0.3272 0.5215 0.1115 0.0700 1.039 9.352 6.690 774.554 1.057 29.755 3.917 0.39 167337. 0.4246
|
|
34.16 0.3681 0.5635 0.1100 0.0718 1.066 9.602 6.597 795.261 1.085 29.344 3.763 0.39 167802. 0.4050
|
|
37.96 0.4090 0.6014 0.1081 0.0735 1.091 9.825 6.484 813.730 1.110 28.839 3.614 0.39 168308. 0.3857
|
|
41.75 0.4499 0.6355 0.1058 0.0749 1.112 10.011 6.347 829.115 1.131 28.230 3.472 0.39 168858. 0.3666
|
|
45.55 0.4908 0.6663 0.1031 0.0759 1.127 10.149 6.183 840.553 1.147 27.504 3.337 0.39 169450. 0.3477
|
|
49.34 0.5317 0.6939 0.0999 0.0765 1.136 10.229 5.991 847.148 1.156 26.649 3.208 0.39 170086. 0.3291
|
|
53.14 0.5726 0.7187 0.0961 0.0766 1.137 10.239 5.768 847.955 1.157 25.655 3.085 0.40 170763. 0.3105
|
|
56.94 0.6135 0.7409 0.0919 0.0761 1.129 10.167 5.510 841.996 1.149 24.510 2.968 0.40 171483. 0.2920
|
|
60.73 0.6544 0.7607 0.0870 0.0748 1.111 10.004 5.219 828.487 1.130 23.213 2.857 0.40 172243. 0.2735
|
|
64.53 0.6953 0.7782 0.0816 0.0729 1.082 9.746 4.895 807.138 1.101 21.774 2.751 0.40 173044. 0.2551
|
|
68.32 0.7362 0.7934 0.0758 0.0703 1.044 9.396 4.545 778.188 1.062 20.216 2.649 0.40 173885. 0.2367
|
|
72.12 0.7771 0.8064 0.0696 0.0670 0.995 8.961 4.173 742.140 1.012 18.562 2.551 0.40 174764. 0.2184
|
|
75.91 0.8180 0.8168 0.0631 0.0632 0.938 8.446 3.785 699.518 0.954 16.836 2.454 0.40 175682. 0.2001
|
|
79.71 0.8589 0.8242 0.0564 0.0588 0.873 7.858 3.384 650.766 0.888 15.053 2.359 0.40 176637. 0.1819
|
|
83.51 0.8998 0.8281 0.0496 0.0539 0.800 7.199 2.973 596.235 0.813 13.226 2.262 0.40 177630. 0.1635
|
|
87.30 0.9407 0.8273 0.0426 0.0484 0.719 6.475 2.555 536.212 0.731 11.366 2.162 0.41 178658. 0.1448
|
|
91.10 0.9816 0.8199 0.0355 0.0425 0.632 5.687 2.132 470.948 0.642 9.482 2.053 0.41 179722. 0.1256
|
|
94.89 1.0225 0.8025 0.0284 0.0362 0.537 4.838 1.704 400.702 0.547 7.581 1.929 0.41 180822. 0.1056
|
|
98.69 1.0634 0.7680 0.0213 0.0294 0.437 3.934 1.275 325.776 0.444 5.671 1.775 0.41 181956. 0.0840
|
|
102.48 1.1043 0.6992 0.0141 0.0223 0.331 2.977 0.846 246.544 0.336 3.763 1.556 0.41 183124. 0.0600
|
|
106.28 1.1452 0.5424 0.0070 0.0148 0.219 1.974 0.420 163.489 0.223 1.866 1.164 0.41 184325. 0.0316
|
|
110.08 1.1861 -0.0056 0.0000 0.0070 0.103 0.931 -0.002 77.085 0.105 -0.009 -0.012 0.42 185541. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 8000
|
|
|
|
V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
|
|
(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
|
|
0.00 0.0000 0.0000 0.1169 0.0549 1.217 9.590 9.160 907.701 1.083 40.745 4.577 0.44 188568. 0.5806
|
|
4.34 0.0409 0.0846 0.1166 0.0564 1.250 9.847 9.137 931.984 1.112 40.642 4.447 0.44 188768. 0.5634
|
|
8.68 0.0818 0.1640 0.1163 0.0580 1.286 10.132 9.112 958.975 1.145 40.528 4.310 0.44 189002. 0.5452
|
|
13.02 0.1228 0.2379 0.1159 0.0598 1.326 10.444 9.082 988.502 1.180 40.396 4.167 0.44 189271. 0.5263
|
|
17.36 0.1637 0.3061 0.1155 0.0617 1.368 10.779 9.046 1020.253 1.218 40.236 4.021 0.44 189579. 0.5069
|
|
21.70 0.2046 0.3686 0.1149 0.0638 1.413 11.133 9.001 1053.734 1.258 40.036 3.874 0.45 189927. 0.4872
|
|
26.04 0.2455 0.4256 0.1141 0.0659 1.459 11.498 8.944 1088.253 1.299 39.782 3.728 0.45 190319. 0.4672
|
|
30.38 0.2865 0.4772 0.1132 0.0680 1.506 11.864 8.871 1122.932 1.340 39.457 3.583 0.45 190755. 0.4473
|
|
34.72 0.3274 0.5239 0.1120 0.0700 1.551 12.221 8.778 1156.725 1.381 39.045 3.442 0.45 191239. 0.4274
|
|
39.06 0.3683 0.5661 0.1105 0.0719 1.594 12.556 8.662 1188.457 1.419 38.527 3.306 0.45 191769. 0.4078
|
|
43.40 0.4092 0.6041 0.1087 0.0736 1.632 12.857 8.518 1216.873 1.453 37.886 3.175 0.45 192349. 0.3883
|
|
47.74 0.4501 0.6383 0.1065 0.0751 1.664 13.108 8.342 1240.667 1.481 37.106 3.050 0.45 192978. 0.3692
|
|
52.08 0.4911 0.6692 0.1038 0.0762 1.688 13.297 8.132 1258.510 1.502 36.171 2.931 0.45 193656. 0.3503
|
|
56.42 0.5320 0.6970 0.1006 0.0768 1.702 13.408 7.883 1269.032 1.515 35.065 2.818 0.45 194383. 0.3316
|
|
60.76 0.5729 0.7219 0.0969 0.0769 1.704 13.426 7.593 1270.789 1.517 33.773 2.710 0.45 195158. 0.3130
|
|
65.10 0.6138 0.7443 0.0926 0.0764 1.693 13.337 7.257 1262.298 1.507 32.280 2.608 0.45 195981. 0.2944
|
|
69.44 0.6548 0.7643 0.0878 0.0752 1.666 13.126 6.876 1242.349 1.483 30.584 2.510 0.45 196852. 0.2759
|
|
73.78 0.6957 0.7820 0.0823 0.0733 1.623 12.789 6.452 1210.478 1.445 28.699 2.418 0.46 197769. 0.2574
|
|
78.13 0.7366 0.7976 0.0765 0.0706 1.565 12.330 5.992 1167.029 1.393 26.653 2.329 0.46 198731. 0.2389
|
|
82.47 0.7775 0.8110 0.0702 0.0673 1.492 11.757 5.503 1112.761 1.328 24.479 2.243 0.46 199738. 0.2206
|
|
86.81 0.8185 0.8219 0.0637 0.0635 1.406 11.077 4.993 1048.478 1.252 22.207 2.160 0.46 200788. 0.2023
|
|
91.15 0.8594 0.8300 0.0570 0.0590 1.307 10.300 4.465 974.860 1.164 19.858 2.077 0.46 201882. 0.1840
|
|
95.49 0.9003 0.8347 0.0501 0.0540 1.197 9.429 3.923 892.443 1.065 17.451 1.994 0.46 203017. 0.1655
|
|
99.83 0.9412 0.8350 0.0430 0.0485 1.075 8.470 3.372 801.666 0.957 14.999 1.908 0.46 204194. 0.1468
|
|
104.17 0.9821 0.8290 0.0359 0.0425 0.943 7.426 2.813 702.910 0.839 12.514 1.815 0.47 205412. 0.1276
|
|
108.51 1.0231 0.8136 0.0287 0.0361 0.800 6.303 2.249 596.570 0.712 10.006 1.710 0.47 206670. 0.1075
|
|
112.85 1.0640 0.7817 0.0215 0.0292 0.648 5.104 1.683 483.101 0.577 7.486 1.580 0.47 207968. 0.0859
|
|
117.19 1.1049 0.7166 0.0143 0.0220 0.487 3.836 1.117 363.073 0.433 4.966 1.395 0.47 209304. 0.0618
|
|
121.53 1.1458 0.5638 0.0071 0.0144 0.318 2.506 0.554 237.225 0.283 2.462 1.058 0.47 210678. 0.0330
|
|
125.87 1.1868 -0.0079 0.0000 0.0064 0.142 1.123 -0.003 106.257 0.127 -0.015 -0.014 0.47 212066. 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 0.1171 0.0549 1.733 12.137 11.613 1292.306 1.371 51.657 4.076 0.50 212135. 0.5822
|
|
4.88 0.0409 0.0848 0.1168 0.0564 1.779 12.461 11.587 1326.836 1.408 51.537 3.961 0.50 212360. 0.5651
|
|
9.77 0.0819 0.1644 0.1165 0.0580 1.831 12.822 11.557 1365.330 1.449 51.406 3.839 0.50 212622. 0.5470
|
|
14.65 0.1228 0.2386 0.1162 0.0598 1.888 13.219 11.523 1407.580 1.493 51.254 3.713 0.50 212925. 0.5283
|
|
19.54 0.1638 0.3070 0.1158 0.0618 1.949 13.647 11.482 1453.176 1.542 51.071 3.584 0.50 213271. 0.5090
|
|
24.42 0.2047 0.3697 0.1153 0.0638 2.013 14.101 11.430 1501.445 1.593 50.841 3.453 0.50 213662. 0.4893
|
|
29.31 0.2456 0.4269 0.1146 0.0659 2.080 14.570 11.364 1551.421 1.646 50.545 3.322 0.50 214103. 0.4694
|
|
34.19 0.2866 0.4787 0.1137 0.0681 2.148 15.043 11.278 1601.841 1.700 50.163 3.193 0.50 214594. 0.4495
|
|
39.08 0.3275 0.5255 0.1126 0.0702 2.214 15.507 11.167 1651.181 1.752 49.670 3.067 0.50 215137. 0.4296
|
|
43.96 0.3685 0.5678 0.1112 0.0722 2.277 15.944 11.026 1697.715 1.801 49.044 2.946 0.50 215735. 0.4100
|
|
48.85 0.4094 0.6058 0.1094 0.0739 2.333 16.337 10.850 1739.580 1.846 48.261 2.829 0.50 216387. 0.3906
|
|
53.73 0.4503 0.6402 0.1072 0.0754 2.380 16.668 10.634 1774.844 1.883 47.299 2.718 0.50 217095. 0.3714
|
|
58.62 0.4913 0.6711 0.1046 0.0766 2.416 16.919 10.373 1801.538 1.911 46.137 2.611 0.51 217858. 0.3525
|
|
63.50 0.5322 0.6990 0.1015 0.0773 2.438 17.070 10.062 1817.654 1.929 44.754 2.511 0.51 218677. 0.3338
|
|
68.39 0.5732 0.7241 0.0978 0.0774 2.442 17.103 9.697 1821.086 1.932 43.131 2.415 0.51 219551. 0.3152
|
|
73.27 0.6141 0.7466 0.0935 0.0769 2.427 16.995 9.273 1809.676 1.920 41.248 2.324 0.51 220478. 0.2966
|
|
78.16 0.6551 0.7668 0.0886 0.0757 2.389 16.732 8.791 1781.645 1.890 39.100 2.238 0.51 221459. 0.2781
|
|
83.04 0.6960 0.7848 0.0832 0.0738 2.328 16.306 8.252 1736.273 1.842 36.706 2.156 0.51 222492. 0.2595
|
|
87.93 0.7369 0.8007 0.0773 0.0712 2.245 15.721 7.667 1674.032 1.776 34.102 2.077 0.51 223576. 0.2411
|
|
92.81 0.7779 0.8145 0.0710 0.0678 2.140 14.989 7.044 1596.023 1.693 31.331 2.002 0.51 224711. 0.2227
|
|
97.70 0.8188 0.8259 0.0645 0.0639 2.016 14.119 6.392 1503.421 1.595 28.430 1.928 0.52 225894. 0.2043
|
|
102.58 0.8598 0.8346 0.0577 0.0594 1.874 13.122 5.717 1397.232 1.483 25.430 1.856 0.52 227126. 0.1860
|
|
107.47 0.9007 0.8401 0.0507 0.0543 1.714 12.004 5.025 1278.243 1.356 22.352 1.783 0.52 228405. 0.1675
|
|
112.35 0.9416 0.8413 0.0436 0.0488 1.538 10.773 4.320 1147.091 1.217 19.215 1.708 0.52 229730. 0.1488
|
|
117.24 0.9826 0.8367 0.0363 0.0427 1.347 9.432 3.605 1004.336 1.066 16.033 1.628 0.52 231102. 0.1295
|
|
122.12 1.0235 0.8230 0.0291 0.0362 1.141 7.988 2.882 850.546 0.902 12.821 1.537 0.53 232519. 0.1094
|
|
127.01 1.0645 0.7935 0.0217 0.0292 0.920 6.446 2.157 686.379 0.728 9.592 1.425 0.53 233980. 0.0877
|
|
131.89 1.1054 0.7318 0.0144 0.0218 0.687 4.815 1.431 512.666 0.544 6.363 1.266 0.53 235485. 0.0634
|
|
136.78 1.1463 0.5831 0.0071 0.0140 0.443 3.104 0.709 330.481 0.351 3.152 0.972 0.53 237032. 0.0343
|
|
141.66 1.1873 -0.0116 -0.0001 0.0060 0.189 1.322 -0.006 140.809 0.149 -0.026 -0.019 0.53 238591. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 10000
|
|
|
|
V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
|
|
(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
|
|
0.00 0.0000 0.0000 0.1173 0.0550 2.382 15.015 14.364 1776.432 1.696 63.890 3.667 0.56 235700. 0.5826
|
|
5.46 0.0412 0.0853 0.1171 0.0565 2.446 15.416 14.333 1823.945 1.742 63.754 3.564 0.56 235951. 0.5656
|
|
10.92 0.0824 0.1655 0.1168 0.0582 2.517 15.866 14.300 1877.116 1.793 63.608 3.455 0.56 236245. 0.5477
|
|
16.38 0.1236 0.2400 0.1165 0.0600 2.596 16.361 14.263 1935.710 1.848 63.440 3.342 0.56 236583. 0.5290
|
|
21.85 0.1648 0.3089 0.1161 0.0619 2.681 16.898 14.217 1999.218 1.909 63.238 3.226 0.56 236970. 0.5097
|
|
27.31 0.2060 0.3720 0.1157 0.0640 2.772 17.469 14.160 2066.754 1.974 62.982 3.107 0.56 237409. 0.4901
|
|
32.77 0.2472 0.4294 0.1150 0.0662 2.866 18.062 14.085 2136.992 2.041 62.649 2.989 0.56 237902. 0.4702
|
|
38.23 0.2884 0.4815 0.1142 0.0684 2.961 18.664 13.986 2208.160 2.109 62.211 2.873 0.56 238453. 0.4503
|
|
43.69 0.3296 0.5285 0.1132 0.0706 3.055 19.255 13.857 2278.063 2.175 61.637 2.759 0.56 239062. 0.4305
|
|
49.15 0.3707 0.5708 0.1118 0.0726 3.144 19.814 13.690 2344.192 2.239 60.895 2.649 0.56 239733. 0.4108
|
|
54.61 0.4119 0.6089 0.1101 0.0745 3.224 20.318 13.479 2403.815 2.295 59.954 2.543 0.56 240465. 0.3913
|
|
60.07 0.4531 0.6433 0.1080 0.0760 3.291 20.743 13.216 2454.096 2.343 58.784 2.443 0.56 241261. 0.3722
|
|
65.54 0.4943 0.6743 0.1053 0.0772 3.342 21.064 12.895 2492.157 2.380 57.357 2.347 0.56 242119. 0.3532
|
|
71.00 0.5355 0.7022 0.1022 0.0779 3.373 21.258 12.510 2515.080 2.402 55.645 2.256 0.56 243039. 0.3344
|
|
76.46 0.5767 0.7274 0.0985 0.0781 3.379 21.298 12.056 2519.837 2.406 53.623 2.170 0.56 244022. 0.3158
|
|
81.92 0.6179 0.7500 0.0941 0.0776 3.357 21.159 11.526 2503.350 2.391 51.267 2.088 0.57 245065. 0.2971
|
|
87.38 0.6591 0.7703 0.0892 0.0763 3.303 20.819 10.920 2463.130 2.352 48.572 2.011 0.57 246168. 0.2785
|
|
92.84 0.7003 0.7885 0.0837 0.0743 3.216 20.271 10.243 2398.246 2.290 45.561 1.937 0.57 247330. 0.2599
|
|
98.30 0.7415 0.8046 0.0776 0.0716 3.097 19.520 9.506 2309.457 2.205 42.284 1.867 0.57 248549. 0.2413
|
|
103.76 0.7827 0.8186 0.0712 0.0681 2.948 18.581 8.722 2198.373 2.099 38.795 1.799 0.57 249824. 0.2227
|
|
109.23 0.8239 0.8303 0.0645 0.0640 2.771 17.468 7.901 2066.683 1.974 35.141 1.734 0.57 251155. 0.2043
|
|
114.69 0.8651 0.8393 0.0576 0.0594 2.569 16.193 7.051 1915.807 1.829 31.362 1.669 0.58 252540. 0.1858
|
|
120.15 0.9063 0.8451 0.0505 0.0541 2.343 14.765 6.179 1746.858 1.668 27.484 1.604 0.58 253977. 0.1671
|
|
125.61 0.9475 0.8466 0.0432 0.0484 2.093 13.192 5.290 1560.733 1.490 23.531 1.537 0.58 255468. 0.1482
|
|
131.07 0.9887 0.8422 0.0358 0.0421 1.821 11.480 4.389 1358.226 1.297 19.522 1.466 0.58 257009. 0.1287
|
|
136.53 1.0298 0.8283 0.0284 0.0353 1.529 9.637 3.479 1140.153 1.089 15.473 1.384 0.58 258601. 0.1082
|
|
141.99 1.0710 0.7977 0.0209 0.0281 1.217 7.670 2.564 907.477 0.867 11.404 1.281 0.59 260243. 0.0860
|
|
147.46 1.1122 0.7311 0.0135 0.0205 0.887 5.591 1.649 661.428 0.632 7.335 1.131 0.59 261934. 0.0609
|
|
152.92 1.1534 0.5576 0.0060 0.0125 0.541 3.411 0.740 403.601 0.385 3.292 0.832 0.59 263670. 0.0300
|
|
158.38 1.1946
|
|
|
|
|
|
|
|
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 0.1176 0.0553 3.185 18.252 17.413 2375.350 2.062 77.454 3.325 0.61 259264. 0.5815
|
|
5.97 0.0410 0.0847 0.1173 0.0568 3.269 18.732 17.380 2437.787 2.116 77.306 3.234 0.61 259538. 0.5650
|
|
11.95 0.0819 0.1643 0.1171 0.0584 3.363 19.270 17.345 2507.864 2.177 77.150 3.137 0.61 259858. 0.5476
|
|
17.92 0.1229 0.2386 0.1168 0.0602 3.467 19.866 17.306 2585.374 2.244 76.976 3.036 0.61 260227. 0.5294
|
|
23.90 0.1639 0.3072 0.1165 0.0622 3.580 20.514 17.259 2669.770 2.318 76.768 2.932 0.61 260648. 0.5105
|
|
29.87 0.2048 0.3702 0.1161 0.0643 3.701 21.208 17.200 2760.009 2.396 76.504 2.827 0.61 261126. 0.4913
|
|
35.85 0.2458 0.4275 0.1156 0.0665 3.828 21.933 17.122 2854.454 2.478 76.157 2.721 0.61 261663. 0.4718
|
|
41.82 0.2868 0.4796 0.1149 0.0687 3.957 22.674 17.017 2950.843 2.562 75.692 2.616 0.61 262262. 0.4522
|
|
47.79 0.3277 0.5265 0.1139 0.0709 4.085 23.407 16.878 3046.290 2.645 75.072 2.513 0.61 262925. 0.4327
|
|
53.77 0.3687 0.5689 0.1127 0.0730 4.207 24.107 16.694 3137.399 2.724 74.256 2.413 0.62 263654. 0.4133
|
|
59.74 0.4097 0.6071 0.1111 0.0750 4.319 24.745 16.457 3220.424 2.796 73.202 2.318 0.62 264451. 0.3941
|
|
65.72 0.4506 0.6415 0.1091 0.0766 4.414 25.291 16.158 3291.432 2.857 71.871 2.227 0.62 265317. 0.3751
|
|
71.69 0.4916 0.6726 0.1066 0.0779 4.488 25.714 15.788 3346.432 2.905 70.227 2.140 0.62 266251. 0.3564
|
|
77.67 0.5326 0.7006 0.1036 0.0787 4.535 25.982 15.341 3381.408 2.935 68.236 2.058 0.62 267254. 0.3378
|
|
83.64 0.5735 0.7260 0.1000 0.0790 4.549 26.066 14.808 3392.270 2.945 65.865 1.980 0.62 268325. 0.3193
|
|
89.62 0.6145 0.7489 0.0957 0.0786 4.526 25.932 14.183 3374.862 2.930 63.084 1.906 0.62 269462. 0.3009
|
|
95.59 0.6555 0.7695 0.0909 0.0774 4.460 25.554 13.463 3325.668 2.887 59.883 1.836 0.62 270664. 0.2824
|
|
101.56 0.6964 0.7880 0.0854 0.0755 4.349 24.920 12.654 3243.111 2.815 56.285 1.770 0.63 271930. 0.2639
|
|
107.54 0.7374 0.8045 0.0794 0.0728 4.195 24.035 11.769 3127.955 2.715 52.347 1.707 0.63 273259. 0.2454
|
|
113.51 0.7784 0.8191 0.0731 0.0694 3.999 22.916 10.822 2982.309 2.589 48.137 1.646 0.63 274650. 0.2269
|
|
119.49 0.8193 0.8314 0.0663 0.0654 3.766 21.580 9.828 2808.501 2.438 43.714 1.587 0.63 276100. 0.2085
|
|
125.46 0.8603 0.8413 0.0594 0.0607 3.498 20.044 8.797 2608.524 2.265 39.128 1.530 0.63 277610. 0.1901
|
|
131.44 0.9013 0.8482 0.0522 0.0555 3.197 18.318 7.737 2383.952 2.070 34.413 1.472 0.64 279177. 0.1716
|
|
137.41 0.9422 0.8512 0.0449 0.0497 2.864 16.413 6.655 2136.034 1.854 29.600 1.413 0.64 280801. 0.1528
|
|
143.38 0.9832 0.8489 0.0375 0.0434 2.502 14.337 5.556 1865.842 1.620 24.711 1.351 0.64 282481. 0.1334
|
|
149.36 1.0242 0.8383 0.0300 0.0367 2.111 12.098 4.444 1574.451 1.367 19.768 1.280 0.64 284216. 0.1131
|
|
155.33 1.0651 0.8133 0.0225 0.0294 1.694 9.706 3.326 1263.104 1.097 14.793 1.194 0.65 286005. 0.0913
|
|
161.31 1.1061 0.7579 0.0149 0.0217 1.252 7.172 2.206 933.387 0.810 9.811 1.072 0.65 287847. 0.0667
|
|
167.28 1.1471 0.6175 0.0074 0.0137 0.788 4.514 1.090 587.420 0.510 4.851 0.842 0.65 289739. 0.0369
|
|
173.26 1.1880 -0.0222 -0.0001 0.0053 0.304 1.745 -0.015 227.063 0.197 -0.065 -0.029 0.65 291636. 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 0.1178 0.0559 4.182 21.967 20.763 3118.791 2.482 92.353 3.020 0.67 282826. 0.5767
|
|
6.52 0.0410 0.0839 0.1176 0.0574 4.290 22.530 20.727 3198.715 2.545 92.194 2.939 0.67 283125. 0.5608
|
|
13.03 0.0819 0.1630 0.1174 0.0590 4.410 23.164 20.691 3288.736 2.617 92.032 2.854 0.67 283473. 0.5440
|
|
19.55 0.1229 0.2368 0.1171 0.0608 4.544 23.868 20.651 3388.698 2.697 91.857 2.764 0.67 283874. 0.5265
|
|
26.06 0.1638 0.3052 0.1169 0.0627 4.691 24.639 20.605 3498.033 2.784 91.651 2.672 0.67 284333. 0.5083
|
|
32.58 0.2048 0.3681 0.1165 0.0648 4.849 25.466 20.546 3615.530 2.877 91.390 2.578 0.67 284852. 0.4897
|
|
39.09 0.2457 0.4255 0.1161 0.0670 5.014 26.337 20.468 3739.206 2.976 91.043 2.483 0.67 285436. 0.4708
|
|
45.61 0.2867 0.4776 0.1155 0.0693 5.185 27.232 20.362 3866.191 3.077 90.570 2.389 0.67 286088. 0.4518
|
|
52.12 0.3276 0.5247 0.1147 0.0716 5.354 28.123 20.216 3992.734 3.177 89.921 2.297 0.67 286809. 0.4328
|
|
58.64 0.3686 0.5673 0.1136 0.0738 5.517 28.979 20.019 4114.330 3.274 89.045 2.207 0.67 287603. 0.4139
|
|
65.15 0.4095 0.6057 0.1121 0.0758 5.667 29.766 19.759 4225.948 3.363 87.888 2.121 0.67 288471. 0.3951
|
|
71.67 0.4505 0.6404 0.1102 0.0775 5.796 30.444 19.424 4322.289 3.440 86.398 2.038 0.67 289414. 0.3765
|
|
78.18 0.4914 0.6717 0.1078 0.0789 5.898 30.977 19.003 4397.961 3.500 84.526 1.960 0.67 290433. 0.3581
|
|
84.70 0.5324 0.7000 0.1049 0.0798 5.964 31.326 18.486 4447.546 3.539 82.228 1.885 0.68 291526. 0.3397
|
|
91.21 0.5733 0.7256 0.1013 0.0801 5.988 31.453 17.865 4465.500 3.554 79.462 1.815 0.68 292694. 0.3214
|
|
97.73 0.6143 0.7486 0.0972 0.0797 5.962 31.317 17.129 4446.157 3.538 76.192 1.747 0.68 293935. 0.3031
|
|
104.24 0.6552 0.7695 0.0923 0.0786 5.880 30.883 16.277 4384.598 3.489 72.401 1.684 0.68 295247. 0.2847
|
|
110.76 0.6962 0.7883 0.0869 0.0767 5.737 30.135 15.314 4278.416 3.405 68.117 1.623 0.68 296629. 0.2663
|
|
117.27 0.7371 0.8052 0.0809 0.0740 5.536 29.079 14.255 4128.431 3.285 63.407 1.566 0.68 298079. 0.2478
|
|
123.79 0.7781 0.8201 0.0744 0.0706 5.280 27.734 13.119 3937.451 3.133 58.354 1.511 0.69 299597. 0.2294
|
|
130.30 0.8190 0.8329 0.0676 0.0665 4.973 26.122 11.923 3708.645 2.951 53.033 1.458 0.69 301180. 0.2110
|
|
136.82 0.8600 0.8434 0.0606 0.0618 4.619 24.263 10.680 3444.757 2.741 47.504 1.406 0.69 302827. 0.1926
|
|
143.33 0.9009 0.8511 0.0533 0.0564 4.221 22.173 9.400 3147.952 2.505 41.813 1.354 0.69 304536. 0.1740
|
|
149.85 0.9419 0.8551 0.0459 0.0506 3.782 19.862 8.092 2819.917 2.244 35.995 1.302 0.70 306308. 0.1552
|
|
156.36 0.9828 0.8540 0.0384 0.0441 3.302 17.342 6.762 2462.101 1.959 30.079 1.246 0.70 308141. 0.1358
|
|
162.88 1.0238 0.8450 0.0307 0.0372 2.784 14.622 5.416 2075.984 1.652 24.092 1.183 0.70 310033. 0.1154
|
|
169.39 1.0647 0.8221 0.0230 0.0298 2.231 11.716 4.060 1663.354 1.324 18.059 1.107 0.70 311984. 0.0935
|
|
175.91 1.1057 0.7700 0.0153 0.0220 1.645 8.640 2.700 1226.591 0.976 12.010 0.998 0.71 313993. 0.0688
|
|
182.42 1.1466 0.6343 0.0076 0.0138 1.031 5.416 1.345 768.974 0.612 5.981 0.793 0.71 316057. 0.0386
|
|
188.94 1.1876 -0.0002 0.0000 0.0053 0.394 2.069 0.000 293.765 0.234 -0.001 0.000 0.71 318125. 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 0.1180 0.0574 5.462 26.481 24.410 4072.902 2.992 108.578 2.718 0.72 306386. 0.5629
|
|
7.06 0.0409 0.0820 0.1178 0.0588 5.595 27.128 24.372 4172.507 3.065 108.407 2.649 0.72 306709. 0.5482
|
|
14.11 0.0819 0.1594 0.1176 0.0604 5.746 27.861 24.335 4285.116 3.148 108.240 2.576 0.72 307086. 0.5325
|
|
21.17 0.1228 0.2319 0.1174 0.0622 5.915 28.677 24.296 4410.657 3.240 108.068 2.498 0.72 307520. 0.5161
|
|
28.23 0.1638 0.2993 0.1172 0.0642 6.100 29.573 24.252 4548.549 3.341 107.872 2.418 0.72 308015. 0.4991
|
|
35.28 0.2047 0.3614 0.1170 0.0662 6.299 30.541 24.197 4697.423 3.451 107.628 2.336 0.72 308576. 0.4817
|
|
42.34 0.2457 0.4183 0.1166 0.0685 6.510 31.565 24.124 4854.875 3.566 107.302 2.254 0.72 309207. 0.4639
|
|
49.40 0.2866 0.4703 0.1161 0.0708 6.728 32.621 24.021 5017.284 3.686 106.847 2.172 0.72 309911. 0.4461
|
|
56.45 0.3276 0.5175 0.1154 0.0731 6.946 33.677 23.877 5179.745 3.805 106.206 2.091 0.73 310690. 0.4282
|
|
63.51 0.3685 0.5603 0.1144 0.0753 7.156 34.695 23.676 5336.211 3.920 105.313 2.012 0.73 311548. 0.4104
|
|
70.57 0.4094 0.5993 0.1131 0.0773 7.349 35.629 23.403 5479.899 4.025 104.097 1.937 0.73 312486. 0.3927
|
|
77.62 0.4504 0.6346 0.1114 0.0790 7.515 36.434 23.041 5603.734 4.116 102.487 1.865 0.73 313507. 0.3752
|
|
84.68 0.4913 0.6668 0.1091 0.0804 7.645 37.065 22.576 5700.721 4.188 100.420 1.796 0.73 314609. 0.3577
|
|
91.74 0.5323 0.6961 0.1063 0.0813 7.730 37.476 21.995 5764.013 4.234 97.835 1.731 0.73 315794. 0.3402
|
|
98.79 0.5732 0.7226 0.1029 0.0816 7.760 37.624 21.286 5786.742 4.251 94.680 1.668 0.73 317059. 0.3226
|
|
105.85 0.6142 0.7466 0.0988 0.0813 7.727 37.462 20.438 5761.885 4.232 90.906 1.609 0.74 318404. 0.3048
|
|
112.91 0.6551 0.7682 0.0940 0.0802 7.621 36.950 19.445 5683.136 4.175 86.493 1.552 0.74 319827. 0.2868
|
|
119.96 0.6961 0.7876 0.0885 0.0782 7.439 36.066 18.316 5547.067 4.075 81.468 1.498 0.74 321326. 0.2686
|
|
127.02 0.7370 0.8050 0.0825 0.0755 7.180 34.812 17.066 5354.255 3.933 75.911 1.446 0.74 322899. 0.2503
|
|
134.08 0.7779 0.8205 0.0760 0.0720 6.850 33.210 15.720 5107.931 3.752 69.922 1.396 0.74 324544. 0.2320
|
|
141.13 0.8189 0.8339 0.0691 0.0679 6.453 31.286 14.298 4811.944 3.535 63.597 1.348 0.75 326261. 0.2136
|
|
148.19 0.8598 0.8450 0.0619 0.0630 5.994 29.061 12.817 4469.755 3.283 57.010 1.301 0.75 328046. 0.1952
|
|
155.25 0.9008 0.8533 0.0546 0.0576 5.477 26.555 11.290 4084.235 3.000 50.218 1.254 0.75 329900. 0.1766
|
|
162.30 0.9417 0.8582 0.0470 0.0516 4.905 23.782 9.726 3657.801 2.687 43.263 1.206 0.75 331821. 0.1576
|
|
169.36 0.9827 0.8580 0.0393 0.0450 4.281 20.758 8.134 3192.632 2.345 36.182 1.156 0.76 333807. 0.1381
|
|
176.42 1.0236 0.8500 0.0315 0.0380 3.609 17.497 6.521 2691.152 1.977 29.004 1.099 0.76 335858. 0.1176
|
|
183.47 1.0646 0.8276 0.0236 0.0304 2.892 14.021 4.892 2156.506 1.584 21.760 1.029 0.76 337972. 0.0954
|
|
190.53 1.1055 0.7745 0.0157 0.0225 2.136 10.357 3.256 1592.938 1.170 14.484 0.927 0.77 340148. 0.0701
|
|
197.59 1.1464 0.6334 0.0078 0.0142 1.349 6.542 1.622 1006.138 0.739 7.215 0.731 0.77 342383. 0.0390
|
|
204.64 1.1874 -0.0038 0.0000 0.0057 0.539 2.614 -0.004 402.115 0.295 -0.017 -0.004 0.77 344621. 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 0.1181 0.0606 7.194 32.385 28.349 5364.202 3.659 126.096 2.397 0.78 329944. 0.5349
|
|
7.60 0.0409 0.0780 0.1180 0.0619 7.356 33.119 28.306 5485.687 3.742 125.907 2.340 0.78 330291. 0.5219
|
|
15.19 0.0819 0.1519 0.1178 0.0635 7.541 33.952 28.267 5623.639 3.836 125.731 2.280 0.78 330696. 0.5080
|
|
22.79 0.1228 0.2214 0.1176 0.0652 7.749 34.884 28.228 5778.141 3.941 125.559 2.216 0.78 331163. 0.4934
|
|
30.39 0.1637 0.2863 0.1175 0.0672 7.977 35.914 28.187 5948.657 4.058 125.376 2.149 0.78 331695. 0.4782
|
|
37.99 0.2047 0.3465 0.1173 0.0693 8.225 37.031 28.138 6133.694 4.184 125.158 2.081 0.78 332298. 0.4626
|
|
45.58 0.2456 0.4020 0.1170 0.0715 8.489 38.219 28.073 6330.404 4.318 124.869 2.011 0.78 332975. 0.4467
|
|
53.18 0.2865 0.4528 0.1166 0.0738 8.763 39.449 27.981 6534.270 4.457 124.460 1.942 0.78 333730. 0.4306
|
|
60.78 0.3275 0.4994 0.1161 0.0761 9.037 40.684 27.848 6738.830 4.597 123.866 1.874 0.78 334566. 0.4146
|
|
68.38 0.3684 0.5421 0.1153 0.0783 9.301 41.873 27.655 6935.745 4.731 123.009 1.809 0.78 335487. 0.3986
|
|
75.97 0.4093 0.5814 0.1141 0.0803 9.542 42.958 27.383 7115.345 4.853 121.798 1.746 0.78 336494. 0.3828
|
|
83.57 0.4503 0.6176 0.1126 0.0821 9.746 43.877 27.010 7267.571 4.957 120.139 1.686 0.79 337590. 0.3672
|
|
91.17 0.4912 0.6511 0.1105 0.0834 9.901 44.573 26.516 7382.941 5.036 117.943 1.629 0.79 338775. 0.3516
|
|
98.76 0.5321 0.6820 0.1079 0.0842 9.994 44.995 25.883 7452.871 5.084 115.130 1.575 0.79 340050. 0.3359
|
|
106.36 0.5731 0.7106 0.1046 0.0843 10.017 45.095 25.096 7469.396 5.095 111.626 1.524 0.79 341413. 0.3200
|
|
113.96 0.6140 0.7367 0.1006 0.0838 9.957 44.826 24.139 7424.750 5.064 107.370 1.475 0.79 342862. 0.3037
|
|
121.56 0.6549 0.7605 0.0959 0.0826 9.806 44.145 23.006 7311.976 4.987 102.330 1.427 0.79 344395. 0.2869
|
|
129.15 0.6959 0.7820 0.0904 0.0805 9.558 43.030 21.703 7127.360 4.862 96.534 1.381 0.80 346011. 0.2697
|
|
136.75 0.7368 0.8013 0.0844 0.0776 9.215 41.488 20.250 6871.952 4.687 90.073 1.337 0.80 347707. 0.2521
|
|
144.35 0.7777 0.8184 0.0778 0.0740 8.784 39.545 18.676 6550.070 4.468 83.069 1.293 0.80 349481. 0.2342
|
|
151.95 0.8186 0.8331 0.0709 0.0696 8.270 37.230 17.005 6166.685 4.206 75.637 1.251 0.80 351332. 0.2162
|
|
159.54 0.8596 0.8454 0.0636 0.0647 7.679 34.571 15.259 5726.232 3.906 67.872 1.209 0.81 353257. 0.1979
|
|
167.14 0.9005 0.8546 0.0561 0.0591 7.017 31.589 13.454 5232.303 3.569 59.843 1.166 0.81 355254. 0.1793
|
|
174.74 0.9414 0.8599 0.0484 0.0529 6.286 28.302 11.602 4687.801 3.198 51.606 1.123 0.81 357324. 0.1603
|
|
182.34 0.9824 0.8597 0.0405 0.0463 5.493 24.729 9.713 4096.093 2.794 43.201 1.075 0.81 359464. 0.1405
|
|
189.93 1.0233 0.8503 0.0325 0.0391 4.642 20.900 7.794 3461.738 2.361 34.666 1.021 0.82 361673. 0.1195
|
|
197.53 1.0642 0.8237 0.0244 0.0315 3.743 16.849 5.853 2790.887 1.904 26.033 0.951 0.82 363950. 0.0964
|
|
205.13 1.1052 0.7604 0.0162 0.0236 2.805 12.627 3.899 2091.454 1.427 17.342 0.846 0.82 366293. 0.0700
|
|
212.72 1.1461 0.5983 0.0081 0.0155 1.842 8.292 1.943 1373.416 0.937 8.641 0.642 0.83 368700. 0.0375
|
|
220.32 1.1870 -0.0036 0.0000 0.0073 0.868 3.908 -0.005 647.386 0.442 -0.024 -0.004 0.83 371122. 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 0.1182 0.0661 9.659 40.587 32.559 7202.848 4.585 144.824 2.050 0.83 353498. 0.4903
|
|
8.15 0.0410 0.0717 0.1180 0.0675 9.854 41.407 32.509 7348.484 4.678 144.600 2.007 0.83 353871. 0.4795
|
|
16.30 0.0819 0.1400 0.1179 0.0690 10.078 42.345 32.464 7514.894 4.784 144.400 1.959 0.83 354305. 0.4679
|
|
24.44 0.1229 0.2046 0.1177 0.0707 10.329 43.402 32.422 7702.417 4.904 144.215 1.909 0.83 354805. 0.4556
|
|
32.59 0.1639 0.2653 0.1176 0.0726 10.608 44.576 32.381 7910.730 5.036 144.033 1.857 0.83 355376. 0.4428
|
|
40.74 0.2049 0.3219 0.1174 0.0747 10.914 45.858 32.336 8138.385 5.181 143.832 1.802 0.83 356021. 0.4295
|
|
48.89 0.2458 0.3744 0.1172 0.0770 11.241 47.232 32.280 8382.070 5.336 143.580 1.747 0.84 356746. 0.4159
|
|
57.04 0.2868 0.4228 0.1169 0.0793 11.582 48.665 32.201 8636.516 5.498 143.228 1.691 0.84 357554. 0.4022
|
|
65.18 0.3278 0.4676 0.1165 0.0817 11.927 50.114 32.084 8893.661 5.662 142.709 1.636 0.84 358448. 0.3884
|
|
73.33 0.3688 0.5090 0.1158 0.0839 12.260 51.514 31.910 9142.053 5.820 141.934 1.583 0.84 359432. 0.3748
|
|
81.48 0.4097 0.5475 0.1149 0.0860 12.562 52.783 31.654 9367.364 5.963 140.795 1.533 0.84 360509. 0.3614
|
|
89.63 0.4507 0.5837 0.1136 0.0877 12.812 53.833 31.288 9553.572 6.082 139.169 1.485 0.84 361682. 0.3482
|
|
97.78 0.4917 0.6180 0.1118 0.0889 12.988 54.575 30.785 9685.300 6.166 136.931 1.442 0.84 362951. 0.3353
|
|
105.92 0.5326 0.6506 0.1093 0.0895 13.077 54.946 30.119 9751.210 6.208 133.970 1.401 0.84 364318. 0.3222
|
|
114.07 0.5736 0.6815 0.1063 0.0894 13.064 54.894 29.269 9741.871 6.202 130.188 1.363 0.85 365781. 0.3090
|
|
122.22 0.6146 0.7106 0.1024 0.0886 12.940 54.373 28.214 9649.410 6.143 125.497 1.326 0.85 367338. 0.2952
|
|
130.37 0.6556 0.7378 0.0978 0.0869 12.696 53.346 26.944 9467.132 6.027 119.848 1.291 0.85 368986. 0.2808
|
|
138.51 0.6965 0.7629 0.0924 0.0844 12.328 51.803 25.464 9193.297 5.853 113.265 1.256 0.85 370723. 0.2657
|
|
146.66 0.7375 0.7858 0.0864 0.0811 11.843 49.764 23.798 8831.443 5.622 105.853 1.222 0.86 372548. 0.2499
|
|
154.81 0.7785 0.8065 0.0798 0.0770 11.249 47.269 21.978 8388.743 5.340 97.757 1.188 0.86 374456. 0.2335
|
|
162.96 0.8194 0.8246 0.0727 0.0723 10.557 44.361 20.035 7872.727 5.012 89.117 1.154 0.86 376446. 0.2165
|
|
171.11 0.8604 0.8400 0.0653 0.0669 9.775 41.075 17.997 7289.500 4.641 80.050 1.120 0.86 378515. 0.1991
|
|
179.25 0.9014 0.8516 0.0577 0.0610 8.915 37.458 15.882 6647.582 4.232 70.642 1.084 0.87 380663. 0.1810
|
|
187.40 0.9424 0.8582 0.0498 0.0546 7.980 33.532 13.705 5950.825 3.788 60.960 1.045 0.87 382887. 0.1621
|
|
195.55 0.9833 0.8551 0.0417 0.0479 6.998 29.403 11.475 5218.100 3.322 51.040 0.997 0.87 385187. 0.1416
|
|
203.70 1.0243 0.8390 0.0334 0.0408 5.959 25.040 9.205 4443.764 2.829 40.944 0.940 0.88 387560. 0.1195
|
|
211.85 1.0653 0.7996 0.0251 0.0334 4.879 20.502 6.906 3638.484 2.316 30.720 0.861 0.88 390006. 0.0948
|
|
219.99 1.1063 0.7134 0.0167 0.0259 3.776 15.866 4.592 2815.773 1.793 20.425 0.740 0.88 392523. 0.0664
|
|
228.14 1.1472 0.5194 0.0083 0.0183 2.670 11.218 2.279 1990.756 1.267 10.138 0.519 0.89 395109. 0.0329
|
|
236.29 1.1882 -0.0036 0.0000 0.0108 1.580 6.640 -0.009 1178.406 0.750 -0.040 -0.003 0.89 397736. 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 0.1174 0.0732 12.970 51.094 36.795 9672.041 5.773 163.664 1.725 0.89 377074. 0.4387
|
|
8.73 0.0411 0.0648 0.1172 0.0744 13.193 51.972 36.729 9838.284 5.872 163.371 1.693 0.89 377473. 0.4301
|
|
17.46 0.0823 0.1269 0.1170 0.0759 13.449 52.978 36.668 10028.743 5.985 163.101 1.658 0.89 377939. 0.4209
|
|
26.18 0.1234 0.1861 0.1168 0.0775 13.740 54.125 36.613 10245.747 6.115 162.856 1.621 0.89 378475. 0.4110
|
|
34.91 0.1646 0.2420 0.1167 0.0793 14.066 55.411 36.561 10489.308 6.260 162.625 1.581 0.89 379086. 0.4007
|
|
43.64 0.2057 0.2945 0.1165 0.0814 14.427 56.832 36.509 10758.161 6.421 162.392 1.539 0.89 379778. 0.3898
|
|
52.37 0.2469 0.3435 0.1163 0.0836 14.817 58.369 36.449 11049.094 6.594 162.127 1.496 0.89 380555. 0.3786
|
|
61.10 0.2880 0.3891 0.1161 0.0859 15.229 59.991 36.372 11356.184 6.778 161.784 1.453 0.89 381421. 0.3672
|
|
69.82 0.3292 0.4314 0.1157 0.0883 15.650 61.648 36.264 11669.944 6.965 161.300 1.409 0.89 382379. 0.3557
|
|
78.55 0.3703 0.4708 0.1152 0.0906 16.061 63.269 36.103 11976.832 7.148 160.586 1.367 0.89 383433. 0.3443
|
|
87.28 0.4115 0.5077 0.1144 0.0927 16.440 64.763 35.865 12259.593 7.317 159.529 1.327 0.90 384586. 0.3331
|
|
96.01 0.4526 0.5425 0.1133 0.0945 16.761 66.026 35.521 12498.575 7.460 157.996 1.289 0.90 385841. 0.3220
|
|
104.74 0.4938 0.5758 0.1118 0.0959 16.993 66.941 35.035 12671.902 7.563 155.838 1.254 0.90 387200. 0.3111
|
|
113.46 0.5349 0.6077 0.1097 0.0965 17.114 67.416 34.377 12761.791 7.617 152.909 1.222 0.90 388664. 0.3002
|
|
122.19 0.5760 0.6386 0.1069 0.0965 17.100 67.362 33.513 12751.553 7.611 149.064 1.192 0.90 390232. 0.2892
|
|
130.92 0.6172 0.6683 0.1034 0.0955 16.929 66.688 32.410 12623.972 7.534 144.159 1.164 0.91 391901. 0.2778
|
|
139.65 0.6583 0.6971 0.0991 0.0935 16.583 65.325 31.046 12365.943 7.380 138.091 1.139 0.91 393672. 0.2659
|
|
148.38 0.6995 0.7248 0.0939 0.0906 16.058 63.258 29.419 11974.725 7.147 130.855 1.114 0.91 395540. 0.2533
|
|
157.10 0.7406 0.7512 0.0879 0.0867 15.366 60.532 27.554 11458.563 6.839 122.558 1.091 0.91 397502. 0.2399
|
|
165.83 0.7818 0.7758 0.0813 0.0820 14.528 57.231 25.490 10833.722 6.466 113.379 1.067 0.92 399556. 0.2258
|
|
174.56 0.8229 0.7984 0.0742 0.0765 13.565 53.434 23.267 10115.064 6.037 103.490 1.043 0.92 401699. 0.2109
|
|
183.29 0.8641 0.8184 0.0667 0.0705 12.491 49.207 20.917 9314.823 5.559 93.038 1.019 0.92 403927. 0.1952
|
|
192.02 0.9052 0.8346 0.0589 0.0639 11.329 44.627 18.466 8447.815 5.042 82.135 0.991 0.92 406240. 0.1786
|
|
200.74 0.9464 0.8447 0.0508 0.0570 10.096 39.771 15.932 7528.672 4.493 70.864 0.960 0.93 408634. 0.1606
|
|
209.47 0.9875 0.8376 0.0425 0.0501 8.880 34.981 13.316 6621.893 3.952 59.231 0.912 0.93 411109. 0.1395
|
|
218.20 1.0287 0.8070 0.0340 0.0433 7.672 30.223 10.641 5721.227 3.415 47.332 0.844 0.93 413662. 0.1153
|
|
226.93 1.0698 0.7447 0.0253 0.0364 6.450 25.408 7.938 4809.682 2.871 35.310 0.749 0.94 416293. 0.0884
|
|
235.66 1.1109 0.6284 0.0167 0.0295 5.238 20.633 5.238 3905.889 2.331 23.298 0.608 0.94 419000. 0.0583
|
|
244.38 1.1521 0.4132 0.0082 0.0229 4.061 15.997 2.575 3028.129 1.807 11.453 0.386 0.95 421780. 0.0259
|
|
253.11 1.1932 -0.0047 -0.0001 0.0166 2.941 11.585 -0.021 2193.077 1.309 -0.092 -0.004 0.95 424623. 0.0000
|
|
|
|
|
|
|