649 lines
115 KiB
Plaintext
649 lines
115 KiB
Plaintext
13.5x14 (135x14.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 0.1174 0.0703 0.003 0.160 0.124 1.892 0.018 0.553 29.790 0.05 21353. 0.4564
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0.53 0.0414 0.0675 0.1170 0.0718 0.003 0.163 0.124 1.932 0.018 0.551 29.070 0.05 21378. 0.4446
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1.06 0.0828 0.1314 0.1165 0.0734 0.003 0.167 0.123 1.976 0.019 0.549 28.313 0.05 21407. 0.4322
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1.59 0.1242 0.1916 0.1160 0.0752 0.003 0.171 0.123 2.023 0.019 0.546 27.526 0.05 21440. 0.4192
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2.12 0.1656 0.2480 0.1154 0.0771 0.003 0.175 0.122 2.074 0.020 0.543 26.716 0.05 21477. 0.4058
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2.65 0.2070 0.3004 0.1147 0.0790 0.003 0.180 0.121 2.126 0.020 0.540 25.890 0.05 21519. 0.3920
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3.18 0.2484 0.3489 0.1138 0.0810 0.003 0.184 0.120 2.180 0.021 0.536 25.058 0.05 21567. 0.3780
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3.71 0.2898 0.3935 0.1127 0.0830 0.003 0.189 0.119 2.233 0.021 0.531 24.227 0.05 21619. 0.3637
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4.23 0.3312 0.4344 0.1113 0.0849 0.003 0.193 0.118 2.284 0.022 0.524 23.403 0.05 21677. 0.3492
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4.76 0.3726 0.4718 0.1097 0.0867 0.003 0.197 0.116 2.332 0.022 0.517 22.592 0.05 21741. 0.3346
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5.29 0.4140 0.5058 0.1078 0.0882 0.003 0.201 0.114 2.373 0.023 0.507 21.800 0.05 21811. 0.3200
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5.82 0.4554 0.5367 0.1054 0.0894 0.003 0.203 0.112 2.406 0.023 0.496 21.027 0.05 21886. 0.3052
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6.35 0.4968 0.5646 0.1026 0.0903 0.003 0.205 0.109 2.429 0.023 0.483 20.276 0.05 21967. 0.2904
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6.88 0.5382 0.5896 0.0993 0.0906 0.003 0.206 0.105 2.439 0.023 0.468 19.545 0.05 22054. 0.2754
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7.41 0.5796 0.6118 0.0955 0.0905 0.003 0.206 0.101 2.434 0.023 0.450 18.834 0.05 22146. 0.2602
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7.94 0.6210 0.6313 0.0911 0.0896 0.003 0.204 0.096 2.412 0.023 0.429 18.139 0.05 22245. 0.2449
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8.47 0.6625 0.6481 0.0862 0.0882 0.003 0.201 0.091 2.372 0.023 0.406 17.456 0.05 22349. 0.2292
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9.00 0.7039 0.6619 0.0809 0.0860 0.003 0.196 0.086 2.314 0.022 0.381 16.780 0.05 22458. 0.2134
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9.53 0.7453 0.6726 0.0751 0.0832 0.003 0.189 0.080 2.240 0.021 0.354 16.104 0.06 22573. 0.1974
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10.06 0.7867 0.6798 0.0690 0.0799 0.003 0.182 0.073 2.150 0.021 0.325 15.418 0.06 22693. 0.1812
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10.59 0.8281 0.6828 0.0627 0.0760 0.003 0.173 0.066 2.046 0.020 0.295 14.712 0.06 22818. 0.1647
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11.12 0.8695 0.6809 0.0562 0.0717 0.003 0.163 0.059 1.930 0.018 0.264 13.972 0.06 22948. 0.1481
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11.64 0.9109 0.6729 0.0494 0.0669 0.002 0.152 0.052 1.801 0.017 0.233 13.181 0.06 23083. 0.1311
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12.17 0.9523 0.6571 0.0426 0.0617 0.002 0.140 0.045 1.661 0.016 0.201 12.313 0.06 23223. 0.1136
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12.70 0.9937 0.6311 0.0356 0.0561 0.002 0.128 0.038 1.510 0.014 0.168 11.332 0.06 23368. 0.0957
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13.23 1.0351 0.5907 0.0286 0.0501 0.002 0.114 0.030 1.348 0.013 0.135 10.182 0.06 23517. 0.0770
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13.76 1.0765 0.5291 0.0215 0.0438 0.002 0.100 0.023 1.177 0.011 0.101 8.769 0.06 23671. 0.0575
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14.29 1.1179 0.4339 0.0144 0.0371 0.001 0.084 0.015 0.997 0.010 0.068 6.926 0.06 23830. 0.0371
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14.82 1.1593 0.2804 0.0073 0.0301 0.001 0.068 0.008 0.809 0.008 0.034 4.316 0.06 23994. 0.0165
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15.35 1.2007 0.0106 0.0002 0.0228 0.001 0.052 0.000 0.613 0.006 0.001 0.157 0.06 24161. 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 0.1179 0.0635 0.018 0.577 0.499 13.661 0.065 2.220 16.568 0.11 42706. 0.5087
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1.07 0.0417 0.0755 0.1175 0.0650 0.019 0.591 0.497 13.992 0.067 2.213 16.126 0.11 42756. 0.4944
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2.13 0.0835 0.1466 0.1171 0.0667 0.019 0.607 0.496 14.355 0.069 2.205 15.663 0.11 42814. 0.4793
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3.20 0.1252 0.2132 0.1166 0.0685 0.020 0.623 0.494 14.747 0.070 2.196 15.184 0.11 42881. 0.4637
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4.27 0.1670 0.2750 0.1160 0.0704 0.020 0.641 0.491 15.164 0.072 2.185 14.693 0.11 42956. 0.4476
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5.34 0.2087 0.3322 0.1153 0.0725 0.021 0.659 0.488 15.601 0.074 2.172 14.196 0.11 43042. 0.4312
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6.40 0.2505 0.3846 0.1145 0.0745 0.022 0.678 0.485 16.047 0.077 2.156 13.698 0.11 43138. 0.4145
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7.47 0.2922 0.4326 0.1134 0.0766 0.022 0.697 0.480 16.493 0.079 2.136 13.204 0.11 43245. 0.3977
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8.54 0.3340 0.4762 0.1121 0.0786 0.023 0.715 0.475 16.925 0.081 2.111 12.718 0.11 43363. 0.3808
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9.61 0.3757 0.5157 0.1105 0.0805 0.023 0.732 0.468 17.327 0.083 2.081 12.244 0.11 43492. 0.3640
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10.67 0.4175 0.5515 0.1085 0.0821 0.024 0.747 0.459 17.682 0.084 2.043 11.784 0.11 43633. 0.3472
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11.74 0.4592 0.5838 0.1061 0.0835 0.024 0.759 0.449 17.971 0.086 1.999 11.340 0.11 43786. 0.3304
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12.81 0.5010 0.6128 0.1033 0.0844 0.024 0.768 0.437 18.175 0.087 1.945 10.913 0.11 43951. 0.3137
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13.88 0.5427 0.6389 0.0999 0.0849 0.025 0.772 0.423 18.275 0.087 1.882 10.502 0.11 44127. 0.2969
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14.94 0.5845 0.6622 0.0961 0.0848 0.024 0.771 0.407 18.253 0.087 1.809 10.107 0.11 44315. 0.2802
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16.01 0.6262 0.6828 0.0916 0.0840 0.024 0.765 0.388 18.091 0.086 1.726 9.727 0.11 44515. 0.2633
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17.08 0.6680 0.7007 0.0866 0.0826 0.024 0.751 0.367 17.780 0.085 1.632 9.359 0.11 44726. 0.2464
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18.15 0.7097 0.7161 0.0812 0.0805 0.023 0.732 0.344 17.323 0.083 1.529 9.001 0.11 44948. 0.2294
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19.21 0.7515 0.7286 0.0753 0.0777 0.022 0.707 0.319 16.726 0.080 1.419 8.649 0.11 45180. 0.2123
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20.28 0.7932 0.7380 0.0692 0.0743 0.021 0.676 0.293 16.002 0.076 1.303 8.300 0.11 45424. 0.1952
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21.35 0.8350 0.7439 0.0627 0.0704 0.020 0.641 0.266 15.159 0.072 1.182 7.948 0.11 45678. 0.1781
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22.42 0.8767 0.7456 0.0561 0.0660 0.019 0.600 0.238 14.206 0.068 1.057 7.586 0.11 45942. 0.1607
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23.48 0.9185 0.7419 0.0493 0.0611 0.018 0.556 0.209 13.149 0.063 0.929 7.207 0.11 46216. 0.1432
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24.55 0.9602 0.7315 0.0424 0.0557 0.016 0.507 0.180 11.993 0.057 0.799 6.796 0.11 46501. 0.1252
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25.62 1.0020 0.7117 0.0354 0.0499 0.014 0.454 0.150 10.743 0.051 0.668 6.337 0.11 46795. 0.1067
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26.69 1.0437 0.6783 0.0284 0.0437 0.013 0.397 0.120 9.402 0.045 0.535 5.798 0.11 47098. 0.0874
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27.75 1.0855 0.6234 0.0213 0.0371 0.011 0.337 0.090 7.977 0.038 0.401 5.123 0.11 47411. 0.0668
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28.82 1.1272 0.5311 0.0142 0.0301 0.009 0.274 0.060 6.472 0.031 0.267 4.203 0.11 47734. 0.0447
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29.89 1.1690 0.3635 0.0071 0.0227 0.007 0.207 0.030 4.896 0.023 0.133 2.774 0.11 48065. 0.0209
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30.96 1.2107 0.0036 0.0000 0.0151 0.004 0.138 0.000 3.258 0.016 0.001 0.027 0.11 48404. 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 0.1181 0.0607 0.059 1.242 1.125 44.082 0.140 5.004 11.576 0.16 64059. 0.5337
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1.61 0.0419 0.0793 0.1178 0.0622 0.061 1.274 1.122 45.211 0.144 4.990 11.254 0.16 64134. 0.5181
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3.21 0.0838 0.1538 0.1174 0.0639 0.062 1.309 1.118 46.451 0.148 4.973 10.917 0.16 64221. 0.5017
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4.82 0.1257 0.2233 0.1169 0.0658 0.064 1.347 1.114 47.793 0.152 4.954 10.569 0.16 64322. 0.4848
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6.43 0.1676 0.2878 0.1164 0.0678 0.066 1.387 1.108 49.224 0.157 4.930 10.213 0.16 64436. 0.4674
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8.03 0.2095 0.3471 0.1157 0.0698 0.068 1.429 1.102 50.723 0.161 4.902 9.854 0.16 64565. 0.4496
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9.64 0.2514 0.4013 0.1148 0.0719 0.070 1.472 1.094 52.261 0.166 4.866 9.495 0.16 64710. 0.4317
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11.25 0.2933 0.4507 0.1138 0.0741 0.072 1.516 1.084 53.800 0.171 4.822 9.140 0.16 64871. 0.4136
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12.85 0.3352 0.4954 0.1125 0.0761 0.074 1.558 1.072 55.294 0.176 4.767 8.792 0.16 65049. 0.3956
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14.46 0.3770 0.5359 0.1109 0.0780 0.076 1.597 1.057 56.689 0.180 4.699 8.453 0.16 65244. 0.3777
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16.07 0.4189 0.5724 0.1089 0.0797 0.078 1.632 1.038 57.927 0.184 4.616 8.126 0.16 65457. 0.3598
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17.67 0.4608 0.6053 0.1066 0.0811 0.079 1.661 1.015 58.943 0.188 4.516 7.812 0.16 65688. 0.3421
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19.28 0.5027 0.6349 0.1037 0.0821 0.080 1.681 0.988 59.670 0.190 4.395 7.511 0.16 65936. 0.3245
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20.89 0.5446 0.6614 0.1004 0.0826 0.081 1.692 0.956 60.044 0.191 4.253 7.223 0.16 66202. 0.3070
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22.49 0.5865 0.6851 0.0965 0.0826 0.080 1.690 0.919 59.997 0.191 4.088 6.947 0.16 66486. 0.2895
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24.10 0.6284 0.7062 0.0920 0.0819 0.080 1.676 0.876 59.473 0.189 3.898 6.684 0.16 66787. 0.2720
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25.71 0.6703 0.7248 0.0870 0.0804 0.078 1.646 0.829 58.439 0.186 3.685 6.431 0.16 67106. 0.2544
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27.31 0.7122 0.7409 0.0815 0.0783 0.076 1.603 0.776 56.900 0.181 3.452 6.187 0.16 67441. 0.2369
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28.92 0.7541 0.7544 0.0756 0.0755 0.074 1.546 0.720 54.884 0.175 3.202 5.950 0.17 67793. 0.2194
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30.53 0.7960 0.7651 0.0694 0.0722 0.070 1.477 0.661 52.425 0.167 2.939 5.717 0.17 68160. 0.2020
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32.13 0.8379 0.7725 0.0629 0.0682 0.066 1.396 0.599 49.556 0.158 2.665 5.484 0.17 68544. 0.1845
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33.74 0.8798 0.7762 0.0562 0.0637 0.062 1.305 0.536 46.302 0.147 2.383 5.248 0.17 68942. 0.1669
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35.35 0.9217 0.7752 0.0494 0.0588 0.057 1.203 0.471 42.686 0.136 2.094 5.003 0.17 69356. 0.1492
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36.95 0.9636 0.7681 0.0425 0.0533 0.052 1.091 0.405 38.723 0.123 1.800 4.741 0.17 69785. 0.1311
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38.56 1.0055 0.7524 0.0355 0.0474 0.046 0.970 0.338 34.429 0.110 1.503 4.451 0.17 70229. 0.1124
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40.17 1.0473 0.7240 0.0284 0.0410 0.040 0.840 0.270 29.819 0.095 1.202 4.112 0.17 70687. 0.0929
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41.77 1.0892 0.6750 0.0213 0.0343 0.033 0.702 0.202 24.912 0.079 0.900 3.686 0.17 71160. 0.0721
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43.38 1.1311 0.5883 0.0141 0.0272 0.026 0.556 0.135 19.728 0.063 0.598 3.093 0.17 71646. 0.0493
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44.99 1.1730 0.4188 0.0070 0.0197 0.019 0.403 0.067 14.296 0.046 0.298 2.123 0.17 72146. 0.0239
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46.60 1.2149 -0.0001 0.0000 0.0119 0.012 0.244 0.000 8.649 0.028 0.000 0.000 0.17 72658. 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 0.1183 0.0592 0.137 2.153 2.003 101.875 0.243 8.910 8.919 0.21 85412. 0.5486
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2.15 0.0420 0.0815 0.1180 0.0607 0.140 2.210 1.998 104.568 0.250 8.885 8.665 0.21 85512. 0.5323
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4.29 0.0839 0.1581 0.1176 0.0624 0.144 2.272 1.991 107.528 0.257 8.857 8.400 0.21 85628. 0.5152
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6.44 0.1259 0.2294 0.1171 0.0643 0.149 2.340 1.984 110.737 0.264 8.824 8.126 0.21 85762. 0.4975
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8.59 0.1679 0.2953 0.1166 0.0663 0.153 2.412 1.975 114.164 0.273 8.784 7.846 0.21 85914. 0.4793
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10.73 0.2099 0.3559 0.1160 0.0684 0.158 2.488 1.964 117.760 0.281 8.735 7.564 0.21 86087. 0.4607
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12.88 0.2518 0.4112 0.1151 0.0705 0.163 2.566 1.950 121.456 0.290 8.674 7.283 0.21 86280. 0.4420
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15.02 0.2938 0.4614 0.1141 0.0727 0.168 2.645 1.933 125.162 0.299 8.598 7.005 0.22 86496. 0.4233
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17.17 0.3358 0.5068 0.1129 0.0748 0.173 2.721 1.911 128.769 0.307 8.502 6.733 0.22 86734. 0.4046
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19.32 0.3778 0.5478 0.1113 0.0767 0.177 2.792 1.885 132.147 0.315 8.383 6.469 0.22 86995. 0.3860
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21.46 0.4197 0.5847 0.1093 0.0785 0.181 2.856 1.852 135.154 0.323 8.237 6.214 0.22 87280. 0.3675
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23.61 0.4617 0.6180 0.1070 0.0799 0.185 2.908 1.812 137.636 0.329 8.059 5.970 0.22 87589. 0.3493
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25.76 0.5037 0.6478 0.1041 0.0810 0.187 2.946 1.764 139.432 0.333 7.845 5.737 0.22 87921. 0.3312
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27.90 0.5456 0.6746 0.1008 0.0815 0.188 2.966 1.707 140.382 0.335 7.593 5.515 0.22 88277. 0.3132
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30.05 0.5876 0.6986 0.0969 0.0815 0.188 2.965 1.641 140.325 0.335 7.298 5.303 0.22 88657. 0.2953
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32.19 0.6296 0.7200 0.0924 0.0808 0.187 2.940 1.565 139.123 0.332 6.960 5.101 0.22 89061. 0.2774
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34.34 0.6716 0.7390 0.0874 0.0794 0.183 2.889 1.479 136.700 0.326 6.580 4.909 0.22 89487. 0.2595
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36.49 0.7135 0.7556 0.0818 0.0773 0.178 2.812 1.386 133.061 0.318 6.164 4.724 0.22 89935. 0.2417
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38.63 0.7555 0.7698 0.0759 0.0745 0.172 2.710 1.285 128.271 0.306 5.717 4.545 0.22 90406. 0.2240
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40.78 0.7975 0.7813 0.0696 0.0711 0.164 2.587 1.179 122.414 0.292 5.246 4.370 0.22 90897. 0.2063
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42.93 0.8394 0.7899 0.0631 0.0671 0.155 2.442 1.069 115.563 0.276 4.757 4.197 0.22 91410. 0.1887
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45.07 0.8814 0.7950 0.0565 0.0626 0.145 2.278 0.956 107.783 0.257 4.252 4.023 0.22 91944. 0.1710
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47.22 0.9234 0.7958 0.0496 0.0576 0.133 2.094 0.840 99.121 0.237 3.737 3.844 0.22 92498. 0.1531
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49.37 0.9654 0.7909 0.0426 0.0520 0.120 1.894 0.722 89.619 0.214 3.212 3.655 0.22 93072. 0.1350
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51.51 1.0073 0.7782 0.0356 0.0461 0.106 1.676 0.603 79.312 0.189 2.680 3.446 0.22 93666. 0.1163
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53.66 1.0493 0.7537 0.0285 0.0396 0.092 1.442 0.482 68.239 0.163 2.144 3.204 0.23 94279. 0.0967
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55.80 1.0913 0.7096 0.0213 0.0328 0.076 1.193 0.361 56.443 0.135 1.605 2.900 0.23 94911. 0.0757
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57.95 1.1333 0.6283 0.0142 0.0255 0.059 0.929 0.240 43.976 0.105 1.067 2.473 0.23 95562. 0.0526
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60.10 1.1752 0.4609 0.0070 0.0179 0.041 0.653 0.119 30.908 0.074 0.530 1.750 0.23 96230. 0.0263
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62.24 1.2172 -0.0006 0.0000 0.0101 0.023 0.366 0.000 17.317 0.041 0.000 -0.002 0.23 96914. 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 0.1184 0.0582 0.263 3.311 3.134 195.882 0.374 13.941 7.258 0.27 106763. 0.5585
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2.69 0.0420 0.0830 0.1181 0.0598 0.270 3.401 3.126 201.160 0.384 13.905 7.049 0.27 106888. 0.5417
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5.37 0.0841 0.1609 0.1178 0.0615 0.278 3.499 3.117 206.971 0.395 13.863 6.830 0.27 107034. 0.5241
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8.06 0.1261 0.2334 0.1174 0.0634 0.286 3.605 3.106 213.281 0.407 13.814 6.604 0.27 107201. 0.5059
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10.75 0.1681 0.3003 0.1169 0.0654 0.295 3.719 3.092 220.030 0.420 13.754 6.374 0.27 107392. 0.4872
|
|
13.43 0.2102 0.3617 0.1162 0.0675 0.305 3.839 3.076 227.125 0.434 13.681 6.142 0.27 107608. 0.4682
|
|
16.12 0.2522 0.4177 0.1154 0.0697 0.314 3.963 3.055 234.431 0.448 13.588 5.911 0.27 107851. 0.4490
|
|
18.81 0.2942 0.4685 0.1145 0.0719 0.324 4.087 3.029 241.773 0.462 13.472 5.682 0.27 108121. 0.4298
|
|
21.49 0.3362 0.5144 0.1132 0.0740 0.334 4.208 2.996 248.936 0.475 13.326 5.459 0.27 108419. 0.4107
|
|
24.18 0.3783 0.5557 0.1117 0.0760 0.343 4.322 2.955 255.663 0.488 13.144 5.242 0.27 108746. 0.3917
|
|
26.87 0.4203 0.5929 0.1097 0.0778 0.351 4.423 2.904 261.672 0.500 12.918 5.034 0.27 109103. 0.3729
|
|
29.55 0.4623 0.6264 0.1074 0.0793 0.358 4.508 2.842 266.653 0.509 12.642 4.834 0.27 109490. 0.3542
|
|
32.24 0.5044 0.6564 0.1046 0.0804 0.362 4.569 2.768 270.290 0.516 12.310 4.644 0.27 109907. 0.3358
|
|
34.93 0.5464 0.6834 0.1012 0.0809 0.365 4.602 2.679 272.258 0.520 11.917 4.463 0.27 110353. 0.3175
|
|
37.61 0.5884 0.7076 0.0973 0.0809 0.365 4.602 2.576 272.241 0.520 11.457 4.291 0.27 110829. 0.2993
|
|
40.30 0.6305 0.7293 0.0928 0.0803 0.362 4.564 2.457 269.963 0.516 10.928 4.128 0.27 111335. 0.2812
|
|
42.99 0.6725 0.7485 0.0878 0.0789 0.356 4.484 2.323 265.266 0.507 10.333 3.972 0.27 111869. 0.2631
|
|
45.67 0.7145 0.7655 0.0822 0.0768 0.346 4.364 2.176 258.160 0.493 9.679 3.823 0.27 112431. 0.2451
|
|
48.36 0.7566 0.7802 0.0763 0.0740 0.334 4.205 2.018 248.771 0.475 8.977 3.680 0.28 113021. 0.2272
|
|
51.05 0.7986 0.7923 0.0700 0.0705 0.318 4.011 1.852 237.260 0.453 8.238 3.541 0.28 113637. 0.2094
|
|
53.73 0.8406 0.8017 0.0635 0.0665 0.300 3.783 1.679 223.775 0.427 7.469 3.403 0.28 114280. 0.1917
|
|
56.42 0.8827 0.8079 0.0567 0.0620 0.280 3.524 1.501 208.440 0.398 6.677 3.266 0.28 114949. 0.1739
|
|
59.11 0.9247 0.8100 0.0498 0.0569 0.257 3.235 1.319 191.349 0.365 5.866 3.126 0.28 115644. 0.1560
|
|
61.79 0.9667 0.8069 0.0428 0.0513 0.231 2.917 1.133 172.584 0.330 5.041 2.979 0.28 116363. 0.1378
|
|
64.48 1.0087 0.7965 0.0357 0.0453 0.204 2.573 0.946 152.217 0.291 4.206 2.818 0.28 117107. 0.1191
|
|
67.17 1.0508 0.7749 0.0286 0.0387 0.175 2.203 0.756 130.322 0.249 3.363 2.632 0.28 117875. 0.0995
|
|
69.85 1.0928 0.7347 0.0214 0.0318 0.143 1.809 0.566 106.986 0.204 2.517 2.399 0.28 118668. 0.0784
|
|
72.54 1.1348 0.6581 0.0142 0.0245 0.110 1.391 0.376 82.315 0.157 1.671 2.070 0.28 119483. 0.0551
|
|
75.23 1.1769 0.4936 0.0070 0.0168 0.076 0.954 0.186 56.447 0.108 0.828 1.497 0.29 120321. 0.0281
|
|
77.91 1.2189 -0.0056 0.0000 0.0088 0.040 0.499 -0.001 29.539 0.056 -0.005 -0.016 0.29 121177. 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 0.1186 0.0577 0.449 4.722 4.520 335.173 0.533 20.103 6.116 0.32 128114. 0.5651
|
|
3.23 0.0421 0.0840 0.1183 0.0592 0.462 4.850 4.508 344.309 0.548 20.053 5.939 0.32 128264. 0.5481
|
|
6.45 0.0841 0.1628 0.1180 0.0610 0.475 4.992 4.496 354.382 0.564 19.996 5.754 0.32 128439. 0.5303
|
|
9.68 0.1262 0.2360 0.1176 0.0629 0.490 5.147 4.481 365.340 0.581 19.929 5.563 0.32 128640. 0.5118
|
|
12.90 0.1682 0.3037 0.1171 0.0649 0.506 5.312 4.462 377.084 0.600 19.848 5.367 0.32 128869. 0.4928
|
|
16.13 0.2103 0.3656 0.1165 0.0670 0.522 5.486 4.440 389.454 0.620 19.747 5.170 0.32 129128. 0.4735
|
|
19.36 0.2524 0.4221 0.1158 0.0692 0.539 5.666 4.411 402.222 0.640 19.620 4.974 0.32 129419. 0.4541
|
|
22.58 0.2944 0.4733 0.1148 0.0714 0.557 5.847 4.375 415.084 0.661 19.459 4.780 0.32 129743. 0.4346
|
|
25.81 0.3365 0.5195 0.1136 0.0736 0.574 6.025 4.329 427.664 0.681 19.255 4.591 0.32 130101. 0.4152
|
|
29.04 0.3785 0.5611 0.1121 0.0756 0.589 6.192 4.271 439.518 0.700 18.998 4.408 0.32 130494. 0.3959
|
|
32.26 0.4206 0.5985 0.1102 0.0775 0.604 6.341 4.200 450.144 0.716 18.679 4.231 0.32 130923. 0.3769
|
|
35.49 0.4627 0.6321 0.1079 0.0790 0.616 6.466 4.112 459.000 0.731 18.288 4.063 0.32 131388. 0.3581
|
|
38.71 0.5047 0.6623 0.1051 0.0801 0.624 6.558 4.005 465.524 0.741 17.815 3.902 0.33 131889. 0.3394
|
|
41.94 0.5468 0.6894 0.1018 0.0807 0.629 6.609 3.879 469.144 0.747 17.252 3.750 0.33 132426. 0.3210
|
|
45.17 0.5888 0.7138 0.0979 0.0807 0.629 6.611 3.730 469.303 0.747 16.591 3.605 0.33 132998. 0.3026
|
|
48.39 0.6309 0.7357 0.0934 0.0801 0.624 6.558 3.559 465.512 0.741 15.830 3.468 0.33 133605. 0.2843
|
|
51.62 0.6730 0.7552 0.0883 0.0787 0.613 6.445 3.366 457.486 0.728 14.972 3.337 0.33 134247. 0.2661
|
|
54.84 0.7150 0.7725 0.0828 0.0766 0.597 6.272 3.154 445.233 0.709 14.028 3.213 0.33 134923. 0.2480
|
|
58.07 0.7571 0.7876 0.0768 0.0738 0.575 6.043 2.926 428.968 0.683 13.014 3.094 0.33 135632. 0.2300
|
|
61.30 0.7991 0.8003 0.0705 0.0704 0.548 5.761 2.685 408.974 0.651 11.944 2.978 0.33 136373. 0.2121
|
|
64.52 0.8412 0.8103 0.0639 0.0663 0.517 5.431 2.435 385.510 0.614 10.830 2.865 0.33 137146. 0.1943
|
|
67.75 0.8832 0.8174 0.0571 0.0617 0.481 5.054 2.177 358.790 0.571 9.683 2.752 0.33 137950. 0.1765
|
|
70.98 0.9253 0.8206 0.0502 0.0566 0.441 4.634 1.913 328.983 0.524 8.509 2.637 0.33 138784. 0.1585
|
|
74.20 0.9674 0.8190 0.0431 0.0510 0.397 4.173 1.644 296.230 0.471 7.314 2.518 0.34 139649. 0.1403
|
|
77.43 1.0094 0.8105 0.0360 0.0448 0.350 3.672 1.372 260.657 0.415 6.103 2.388 0.34 140543. 0.1216
|
|
80.65 1.0515 0.7915 0.0288 0.0383 0.298 3.133 1.098 222.396 0.354 4.882 2.239 0.34 141466. 0.1019
|
|
83.88 1.0935 0.7548 0.0216 0.0312 0.244 2.558 0.822 181.598 0.289 3.655 2.053 0.34 142418. 0.0809
|
|
87.11 1.1356 0.6830 0.0143 0.0238 0.186 1.950 0.546 138.451 0.220 2.428 1.789 0.34 143398. 0.0574
|
|
90.33 1.1777 0.5232 0.0071 0.0160 0.125 1.313 0.271 93.199 0.148 1.208 1.321 0.34 144405. 0.0299
|
|
93.56 1.2197 -0.0002 0.0000 0.0079 0.062 0.650 0.000 46.113 0.073 0.000 0.000 0.34 145432. 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 0.1188 0.0573 0.710 6.389 6.161 529.152 0.722 27.402 5.281 0.37 149463. 0.5697
|
|
3.77 0.0421 0.0847 0.1185 0.0589 0.729 6.565 6.146 543.669 0.742 27.338 5.128 0.37 149639. 0.5525
|
|
7.53 0.0842 0.1641 0.1182 0.0606 0.751 6.758 6.130 559.705 0.764 27.265 4.967 0.37 149843. 0.5345
|
|
11.30 0.1263 0.2379 0.1178 0.0625 0.774 6.969 6.111 577.185 0.787 27.180 4.802 0.38 150077. 0.5159
|
|
15.07 0.1684 0.3060 0.1174 0.0646 0.799 7.196 6.087 595.960 0.813 27.076 4.633 0.38 150344. 0.4968
|
|
18.83 0.2105 0.3684 0.1168 0.0667 0.826 7.435 6.058 615.784 0.840 26.947 4.462 0.38 150647. 0.4774
|
|
22.60 0.2525 0.4253 0.1161 0.0689 0.853 7.683 6.021 636.297 0.868 26.783 4.292 0.38 150986. 0.4578
|
|
26.37 0.2946 0.4767 0.1152 0.0712 0.881 7.933 5.974 657.019 0.896 26.573 4.124 0.38 151365. 0.4381
|
|
30.13 0.3367 0.5232 0.1140 0.0734 0.908 8.179 5.914 677.348 0.924 26.306 3.960 0.38 151783. 0.4186
|
|
33.90 0.3788 0.5649 0.1126 0.0755 0.934 8.411 5.838 696.567 0.950 25.967 3.801 0.38 152242. 0.3992
|
|
37.67 0.4209 0.6025 0.1107 0.0773 0.957 8.620 5.742 713.862 0.974 25.542 3.649 0.38 152743. 0.3800
|
|
41.43 0.4630 0.6362 0.1084 0.0789 0.977 8.795 5.625 728.353 0.994 25.018 3.503 0.38 153286. 0.3611
|
|
45.20 0.5051 0.6666 0.1057 0.0801 0.991 8.925 5.482 739.122 1.008 24.382 3.364 0.38 153871. 0.3423
|
|
48.97 0.5472 0.6938 0.1024 0.0807 0.999 8.998 5.311 745.240 1.017 23.621 3.232 0.38 154498. 0.3237
|
|
52.73 0.5893 0.7183 0.0985 0.0808 1.000 9.005 5.109 745.799 1.017 22.726 3.107 0.38 155167. 0.3053
|
|
56.50 0.6314 0.7404 0.0940 0.0802 0.992 8.935 4.877 740.001 1.009 21.691 2.989 0.38 155877. 0.2869
|
|
60.27 0.6735 0.7601 0.0890 0.0788 0.975 8.783 4.614 727.375 0.992 20.521 2.877 0.38 156628. 0.2686
|
|
64.03 0.7155 0.7777 0.0834 0.0767 0.949 8.548 4.324 707.918 0.966 19.232 2.770 0.38 157418. 0.2504
|
|
67.80 0.7576 0.7931 0.0774 0.0739 0.915 8.235 4.012 681.973 0.930 17.845 2.668 0.39 158246. 0.2323
|
|
71.57 0.7997 0.8063 0.0710 0.0704 0.872 7.848 3.683 649.993 0.887 16.381 2.570 0.39 159112. 0.2143
|
|
75.33 0.8418 0.8169 0.0644 0.0664 0.821 7.395 3.340 612.401 0.835 14.855 2.474 0.39 160015. 0.1965
|
|
79.10 0.8839 0.8247 0.0576 0.0617 0.764 6.877 2.986 569.541 0.777 13.282 2.378 0.39 160955. 0.1786
|
|
82.87 0.9260 0.8288 0.0506 0.0565 0.700 6.299 2.624 521.689 0.712 11.672 2.282 0.39 161930. 0.1606
|
|
86.63 0.9681 0.8284 0.0435 0.0508 0.629 5.664 2.256 469.072 0.640 10.033 2.181 0.39 162940. 0.1424
|
|
90.40 1.0102 0.8215 0.0363 0.0446 0.552 4.973 1.882 411.895 0.562 8.373 2.073 0.39 163985. 0.1236
|
|
94.17 1.0523 0.8047 0.0290 0.0380 0.470 4.231 1.506 350.368 0.478 6.697 1.949 0.40 165064. 0.1040
|
|
97.93 1.0944 0.7708 0.0217 0.0309 0.382 3.438 1.127 284.737 0.388 5.013 1.795 0.40 166176. 0.0828
|
|
101.70 1.1365 0.7029 0.0144 0.0233 0.289 2.600 0.748 215.307 0.294 3.329 1.577 0.40 167320. 0.0593
|
|
105.47 1.1785 0.5470 0.0072 0.0154 0.191 1.720 0.372 142.473 0.194 1.653 1.183 0.40 168497. 0.0313
|
|
109.23 1.2206 -0.0039 0.0000 0.0072 0.089 0.805 -0.001 66.670 0.091 -0.005 -0.008 0.40 169695. 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 0.1190 0.0572 1.056 8.322 8.058 787.665 0.940 35.844 4.640 0.43 170812. 0.5725
|
|
4.31 0.0421 0.0851 0.1187 0.0587 1.085 8.551 8.041 809.319 0.966 35.766 4.506 0.43 171012. 0.5554
|
|
8.61 0.0842 0.1649 0.1184 0.0605 1.117 8.804 8.021 833.291 0.995 35.678 4.366 0.43 171245. 0.5374
|
|
12.92 0.1263 0.2391 0.1181 0.0624 1.153 9.081 7.998 859.481 1.026 35.575 4.221 0.43 171513. 0.5188
|
|
17.23 0.1685 0.3076 0.1176 0.0644 1.190 9.379 7.970 887.685 1.060 35.450 4.072 0.43 171818. 0.4997
|
|
21.53 0.2106 0.3703 0.1171 0.0666 1.230 9.694 7.934 917.547 1.095 35.293 3.922 0.43 172164. 0.4802
|
|
25.84 0.2527 0.4274 0.1165 0.0689 1.272 10.022 7.889 948.540 1.132 35.092 3.772 0.43 172552. 0.4606
|
|
30.15 0.2948 0.4791 0.1156 0.0711 1.314 10.353 7.831 979.950 1.170 34.833 3.625 0.43 172984. 0.4409
|
|
34.46 0.3369 0.5257 0.1145 0.0734 1.356 10.680 7.756 1010.871 1.207 34.499 3.480 0.43 173462. 0.4213
|
|
38.76 0.3790 0.5676 0.1131 0.0755 1.395 10.990 7.660 1040.217 1.242 34.073 3.340 0.43 173987. 0.4018
|
|
43.07 0.4211 0.6053 0.1113 0.0774 1.431 11.270 7.539 1066.745 1.273 33.535 3.206 0.43 174560. 0.3826
|
|
47.38 0.4632 0.6391 0.1091 0.0791 1.461 11.507 7.389 1089.105 1.300 32.866 3.077 0.43 175181. 0.3636
|
|
51.68 0.5054 0.6696 0.1064 0.0803 1.483 11.684 7.205 1105.883 1.320 32.047 2.955 0.43 175851. 0.3448
|
|
55.99 0.5475 0.6969 0.1031 0.0810 1.496 11.787 6.984 1115.653 1.332 31.064 2.839 0.43 176569. 0.3261
|
|
60.30 0.5896 0.7216 0.0992 0.0811 1.498 11.802 6.722 1117.023 1.333 29.902 2.730 0.44 177334. 0.3076
|
|
64.60 0.6317 0.7438 0.0948 0.0805 1.487 11.714 6.419 1108.768 1.323 28.553 2.626 0.44 178147. 0.2892
|
|
68.91 0.6738 0.7637 0.0897 0.0791 1.462 11.518 6.076 1090.142 1.301 27.025 2.528 0.44 179006. 0.2708
|
|
73.22 0.7159 0.7815 0.0841 0.0770 1.423 11.211 5.696 1061.121 1.267 25.336 2.435 0.44 179910. 0.2526
|
|
77.53 0.7580 0.7973 0.0780 0.0742 1.371 10.800 5.287 1022.211 1.220 23.516 2.346 0.44 180858. 0.2344
|
|
81.83 0.8001 0.8109 0.0717 0.0707 1.306 10.292 4.854 974.105 1.163 21.591 2.260 0.44 181850. 0.2164
|
|
86.14 0.8423 0.8220 0.0650 0.0666 1.230 9.693 4.403 917.450 1.095 19.584 2.177 0.44 182883. 0.1985
|
|
90.45 0.8844 0.8304 0.0581 0.0619 1.144 9.010 3.938 852.777 1.018 17.514 2.094 0.45 183958. 0.1806
|
|
94.75 0.9265 0.8354 0.0511 0.0567 1.047 8.246 3.461 780.508 0.932 15.394 2.011 0.45 185074. 0.1626
|
|
99.06 0.9686 0.8361 0.0439 0.0509 0.940 7.406 2.975 700.986 0.837 13.234 1.925 0.45 186230. 0.1443
|
|
103.37 1.0107 0.8305 0.0367 0.0446 0.824 6.493 2.483 614.527 0.734 11.045 1.833 0.45 187426. 0.1255
|
|
107.67 1.0528 0.8156 0.0293 0.0379 0.699 5.509 1.986 521.448 0.622 8.836 1.728 0.45 188660. 0.1058
|
|
111.98 1.0949 0.7844 0.0220 0.0306 0.566 4.460 1.487 422.120 0.504 6.614 1.598 0.45 189932. 0.0847
|
|
116.29 1.1370 0.7202 0.0146 0.0230 0.425 3.349 0.987 317.010 0.378 4.392 1.413 0.46 191242. 0.0610
|
|
120.60 1.1792 0.5686 0.0072 0.0150 0.277 2.184 0.490 206.718 0.247 2.180 1.075 0.46 192588. 0.0327
|
|
124.90 1.2213 -0.0055 0.0000 0.0067 0.123 0.971 -0.002 91.900 0.110 -0.009 -0.010 0.46 193957. 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 0.1191 0.0572 1.503 10.529 10.215 1121.124 1.190 45.437 4.133 0.48 192159. 0.5741
|
|
4.85 0.0421 0.0853 0.1189 0.0587 1.545 10.818 10.195 1151.896 1.222 45.346 4.014 0.48 192384. 0.5571
|
|
9.69 0.0843 0.1653 0.1186 0.0605 1.591 11.139 10.172 1186.041 1.258 45.244 3.890 0.48 192646. 0.5392
|
|
14.54 0.1264 0.2398 0.1183 0.0624 1.641 11.490 10.145 1223.443 1.298 45.125 3.761 0.48 192947. 0.5207
|
|
19.39 0.1685 0.3085 0.1179 0.0644 1.695 11.869 10.113 1263.840 1.341 44.981 3.629 0.48 193290. 0.5016
|
|
24.24 0.2106 0.3714 0.1175 0.0666 1.752 12.272 10.072 1306.750 1.387 44.799 3.496 0.48 193678. 0.4822
|
|
29.08 0.2528 0.4287 0.1169 0.0689 1.812 12.692 10.019 1351.443 1.434 44.564 3.363 0.48 194115. 0.4626
|
|
33.93 0.2949 0.4806 0.1161 0.0712 1.873 13.119 9.950 1396.910 1.482 44.258 3.231 0.48 194601. 0.4429
|
|
38.78 0.3370 0.5273 0.1150 0.0735 1.934 13.541 9.861 1441.853 1.530 43.860 3.102 0.48 195139. 0.4234
|
|
43.63 0.3792 0.5694 0.1137 0.0757 1.991 13.943 9.745 1484.695 1.575 43.345 2.977 0.49 195730. 0.4039
|
|
48.47 0.4213 0.6071 0.1119 0.0777 2.043 14.309 9.597 1523.629 1.617 42.689 2.857 0.49 196375. 0.3847
|
|
53.32 0.4634 0.6411 0.1098 0.0794 2.088 14.619 9.412 1556.664 1.652 41.865 2.742 0.49 197074. 0.3657
|
|
58.17 0.5056 0.6716 0.1071 0.0806 2.121 14.855 9.184 1581.721 1.678 40.850 2.634 0.49 197828. 0.3469
|
|
63.01 0.5477 0.6990 0.1039 0.0814 2.141 14.995 8.908 1596.698 1.694 39.622 2.530 0.49 198636. 0.3283
|
|
67.86 0.5898 0.7238 0.1001 0.0815 2.145 15.022 8.580 1599.548 1.697 38.163 2.433 0.49 199498. 0.3097
|
|
72.71 0.6319 0.7461 0.0956 0.0810 2.130 14.918 8.198 1588.467 1.685 36.464 2.341 0.49 200414. 0.2913
|
|
77.56 0.6741 0.7663 0.0905 0.0796 2.095 14.672 7.763 1562.334 1.658 34.530 2.254 0.49 201381. 0.2729
|
|
82.40 0.7162 0.7844 0.0849 0.0775 2.040 14.285 7.281 1521.068 1.614 32.387 2.171 0.49 202400. 0.2546
|
|
87.25 0.7583 0.8004 0.0789 0.0747 1.965 13.762 6.761 1465.389 1.555 30.071 2.093 0.50 203468. 0.2365
|
|
92.10 0.8005 0.8144 0.0724 0.0712 1.872 13.113 6.209 1396.308 1.482 27.619 2.017 0.50 204585. 0.2184
|
|
96.95 0.8426 0.8260 0.0657 0.0670 1.763 12.348 5.634 1314.779 1.395 25.059 1.944 0.50 205750. 0.2005
|
|
101.79 0.8847 0.8350 0.0588 0.0623 1.638 11.472 5.039 1221.585 1.296 22.416 1.871 0.50 206961. 0.1826
|
|
106.64 0.9268 0.8408 0.0517 0.0570 1.498 10.493 4.430 1117.345 1.186 19.706 1.798 0.50 208218. 0.1645
|
|
111.49 0.9690 0.8424 0.0444 0.0511 1.344 9.415 3.810 1002.566 1.064 16.945 1.724 0.50 209520. 0.1462
|
|
116.33 1.0111 0.8382 0.0371 0.0447 1.177 8.243 3.180 877.699 0.931 14.145 1.643 0.51 210866. 0.1274
|
|
121.18 1.0532 0.8249 0.0297 0.0379 0.997 6.980 2.544 743.209 0.789 11.318 1.553 0.51 212256. 0.1077
|
|
126.03 1.0954 0.7962 0.0222 0.0306 0.804 5.631 1.905 599.631 0.636 8.474 1.441 0.51 213688. 0.0864
|
|
130.88 1.1375 0.7354 0.0148 0.0228 0.600 4.204 1.265 447.639 0.475 5.627 1.282 0.51 215163. 0.0627
|
|
135.72 1.1796 0.5881 0.0073 0.0147 0.386 2.706 0.628 288.111 0.306 2.793 0.988 0.51 216678. 0.0340
|
|
140.57 1.2218 -0.0069 0.0000 0.0062 0.164 1.146 -0.003 121.985 0.129 -0.013 -0.011 0.52 218218. 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 0.1193 0.0573 2.066 13.022 12.632 1540.683 1.471 56.189 3.719 0.54 213505. 0.5745
|
|
5.39 0.0422 0.0854 0.1191 0.0588 2.123 13.378 12.609 1582.756 1.511 56.086 3.613 0.54 213755. 0.5577
|
|
10.78 0.0843 0.1655 0.1189 0.0606 2.185 13.773 12.584 1629.560 1.556 55.972 3.503 0.54 214045. 0.5400
|
|
16.17 0.1265 0.2401 0.1186 0.0625 2.254 14.208 12.554 1680.985 1.605 55.841 3.387 0.54 214379. 0.5217
|
|
21.55 0.1686 0.3089 0.1183 0.0645 2.329 14.679 12.518 1736.714 1.658 55.682 3.269 0.54 214760. 0.5028
|
|
26.94 0.2108 0.3720 0.1178 0.0668 2.409 15.181 12.473 1796.133 1.715 55.481 3.150 0.54 215191. 0.4835
|
|
32.33 0.2529 0.4295 0.1173 0.0691 2.492 15.707 12.414 1858.279 1.775 55.218 3.030 0.54 215676. 0.4640
|
|
37.72 0.2951 0.4815 0.1165 0.0714 2.577 16.243 12.336 1921.781 1.835 54.872 2.912 0.54 216216. 0.4445
|
|
43.11 0.3372 0.5283 0.1156 0.0738 2.662 16.776 12.233 1984.850 1.895 54.414 2.796 0.54 216814. 0.4250
|
|
48.50 0.3794 0.5704 0.1143 0.0760 2.743 17.287 12.099 2045.285 1.953 53.814 2.683 0.54 217470. 0.4056
|
|
53.89 0.4215 0.6083 0.1127 0.0781 2.817 17.754 11.924 2100.531 2.006 53.040 2.575 0.54 218187. 0.3865
|
|
59.27 0.4637 0.6423 0.1106 0.0798 2.880 18.153 11.704 2147.762 2.051 52.058 2.472 0.54 218964. 0.3675
|
|
64.66 0.5058 0.6728 0.1080 0.0812 2.929 18.460 11.429 2184.003 2.086 50.835 2.374 0.54 219803. 0.3488
|
|
70.05 0.5480 0.7004 0.1048 0.0820 2.959 18.648 11.094 2206.249 2.107 49.345 2.281 0.54 220702. 0.3302
|
|
75.44 0.5901 0.7253 0.1010 0.0822 2.966 18.693 10.693 2211.587 2.112 47.563 2.193 0.54 221662. 0.3117
|
|
80.83 0.6323 0.7478 0.0966 0.0817 2.947 18.573 10.224 2197.442 2.098 45.475 2.110 0.55 222681. 0.2933
|
|
86.22 0.6744 0.7681 0.0915 0.0804 2.900 18.275 9.687 2162.177 2.065 43.088 2.032 0.55 223758. 0.2749
|
|
91.61 0.7166 0.7864 0.0859 0.0783 2.824 17.797 9.091 2105.620 2.011 40.435 1.958 0.55 224891. 0.2566
|
|
96.99 0.7587 0.8028 0.0798 0.0754 2.721 17.148 8.444 2028.760 1.937 37.560 1.888 0.55 226080. 0.2384
|
|
102.38 0.8009 0.8171 0.0733 0.0718 2.592 16.338 7.758 1933.019 1.846 34.508 1.820 0.55 227323. 0.2204
|
|
107.77 0.8430 0.8292 0.0665 0.0676 2.440 15.381 7.041 1819.759 1.738 31.319 1.755 0.55 228619. 0.2024
|
|
113.16 0.8852 0.8387 0.0595 0.0628 2.266 14.285 6.300 1690.110 1.614 28.022 1.691 0.56 229967. 0.1844
|
|
118.55 0.9273 0.8452 0.0523 0.0574 2.072 13.058 5.539 1544.950 1.475 24.640 1.626 0.56 231366. 0.1664
|
|
123.94 0.9695 0.8477 0.0450 0.0515 1.857 11.706 4.764 1384.995 1.323 21.191 1.560 0.56 232814. 0.1480
|
|
129.33 1.0116 0.8446 0.0376 0.0450 1.624 10.235 3.977 1210.880 1.156 17.690 1.490 0.56 234312. 0.1291
|
|
134.71 1.0538 0.8330 0.0301 0.0380 1.372 8.649 3.182 1023.255 0.977 14.153 1.410 0.56 235858. 0.1093
|
|
140.10 1.0959 0.8063 0.0225 0.0306 1.103 6.955 2.382 822.866 0.786 10.594 1.313 0.57 237452. 0.0881
|
|
145.49 1.1381 0.7487 0.0149 0.0227 0.819 5.161 1.580 610.657 0.583 7.029 1.174 0.57 239092. 0.0641
|
|
150.88 1.1802 0.6049 0.0074 0.0144 0.520 3.278 0.782 387.863 0.370 3.478 0.915 0.57 240777. 0.0352
|
|
156.27 1.2224 -0.0175 -0.0001 0.0058 0.209 1.317 -0.009 155.766 0.149 -0.039 -0.026 0.57 242487. 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 0.1196 0.0575 2.761 15.818 15.312 2058.634 1.787 68.109 3.374 0.59 234849. 0.5738
|
|
5.93 0.0421 0.0852 0.1194 0.0590 2.835 16.246 15.287 2114.278 1.835 67.996 3.279 0.59 235123. 0.5573
|
|
11.85 0.0843 0.1652 0.1191 0.0608 2.919 16.723 15.259 2176.356 1.889 67.874 3.180 0.59 235442. 0.5399
|
|
17.78 0.1264 0.2398 0.1189 0.0627 3.010 17.249 15.228 2244.792 1.949 67.735 3.077 0.59 235809. 0.5219
|
|
23.70 0.1686 0.3087 0.1186 0.0648 3.110 17.821 15.190 2319.243 2.013 67.567 2.971 0.59 236227. 0.5033
|
|
29.63 0.2107 0.3719 0.1182 0.0670 3.217 18.433 15.143 2398.973 2.083 67.355 2.863 0.59 236700. 0.4842
|
|
35.55 0.2528 0.4294 0.1177 0.0693 3.329 19.077 15.080 2482.771 2.155 67.075 2.755 0.59 237232. 0.4650
|
|
41.48 0.2950 0.4815 0.1171 0.0717 3.445 19.739 14.995 2568.859 2.230 66.699 2.648 0.59 237825. 0.4456
|
|
47.41 0.3371 0.5284 0.1162 0.0741 3.560 20.400 14.882 2654.863 2.305 66.195 2.542 0.59 238481. 0.4263
|
|
53.33 0.3792 0.5706 0.1150 0.0764 3.671 21.037 14.731 2737.806 2.377 65.522 2.440 0.59 239202. 0.4071
|
|
59.26 0.4214 0.6085 0.1135 0.0786 3.774 21.624 14.532 2814.188 2.443 64.640 2.342 0.59 239990. 0.3881
|
|
65.18 0.4635 0.6425 0.1115 0.0804 3.862 22.130 14.277 2880.104 2.500 63.505 2.248 0.60 240844. 0.3693
|
|
71.11 0.5057 0.6732 0.1090 0.0819 3.931 22.525 13.956 2931.411 2.545 62.076 2.159 0.60 241766. 0.3506
|
|
77.03 0.5478 0.7008 0.1059 0.0828 3.975 22.774 13.560 2963.918 2.573 60.316 2.075 0.60 242755. 0.3321
|
|
82.96 0.5899 0.7258 0.1021 0.0830 3.988 22.848 13.083 2973.570 2.581 58.194 1.996 0.60 243811. 0.3137
|
|
88.89 0.6321 0.7484 0.0978 0.0826 3.965 22.720 12.521 2956.785 2.567 55.692 1.921 0.60 244932. 0.2954
|
|
94.81 0.6742 0.7689 0.0927 0.0813 3.904 22.369 11.874 2911.211 2.527 52.815 1.850 0.60 246117. 0.2771
|
|
100.74 0.7164 0.7875 0.0871 0.0792 3.804 21.795 11.151 2836.500 2.462 49.602 1.783 0.60 247364. 0.2588
|
|
106.66 0.7585 0.8042 0.0809 0.0763 3.666 21.007 10.366 2733.949 2.373 46.108 1.720 0.61 248673. 0.2407
|
|
112.59 0.8006 0.8189 0.0744 0.0728 3.494 20.020 9.530 2605.501 2.262 42.390 1.659 0.61 250041. 0.2226
|
|
118.51 0.8428 0.8314 0.0676 0.0685 3.290 18.849 8.655 2453.068 2.130 38.497 1.600 0.61 251467. 0.2046
|
|
124.44 0.8849 0.8416 0.0605 0.0636 3.055 17.506 7.748 2278.225 1.978 34.465 1.543 0.61 252950. 0.1866
|
|
130.37 0.9270 0.8488 0.0532 0.0581 2.792 15.999 6.818 2082.204 1.808 30.325 1.485 0.61 254489. 0.1685
|
|
136.29 0.9692 0.8522 0.0458 0.0521 2.502 14.338 5.868 1865.991 1.620 26.099 1.426 0.62 256082. 0.1502
|
|
142.22 1.0113 0.8503 0.0383 0.0455 2.186 12.528 4.903 1630.459 1.415 21.807 1.364 0.62 257730. 0.1313
|
|
148.14 1.0535 0.8403 0.0307 0.0384 1.846 10.577 3.927 1376.481 1.195 17.466 1.294 0.62 259430. 0.1114
|
|
154.07 1.0956 0.8161 0.0230 0.0309 1.482 8.491 2.944 1105.063 0.959 13.094 1.208 0.62 261183. 0.0901
|
|
159.99 1.1377 0.7623 0.0153 0.0228 1.096 6.281 1.959 817.477 0.710 8.712 1.087 0.63 262986. 0.0661
|
|
165.92 1.1799 0.6253 0.0076 0.0144 0.691 3.960 0.977 515.402 0.447 4.345 0.860 0.63 264839. 0.0369
|
|
171.85 1.2220 0.0060 0.0000 0.0056 0.269 1.542 0.004 200.626 0.174 0.016 0.008 0.63 266720. 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 0.1198 0.0579 3.613 18.977 18.256 2694.200 2.144 81.203 3.073 0.64 256191. 0.5708
|
|
6.47 0.0421 0.0847 0.1196 0.0595 3.709 19.479 18.229 2765.552 2.201 81.082 2.990 0.64 256490. 0.5548
|
|
12.93 0.0843 0.1645 0.1194 0.0612 3.816 20.042 18.200 2845.394 2.264 80.954 2.901 0.64 256837. 0.5380
|
|
19.40 0.1264 0.2389 0.1192 0.0631 3.934 20.664 18.168 2933.713 2.335 80.813 2.809 0.64 257237. 0.5204
|
|
25.86 0.1686 0.3077 0.1189 0.0652 4.064 21.343 18.131 3030.177 2.411 80.645 2.714 0.64 257692. 0.5023
|
|
32.33 0.2107 0.3709 0.1186 0.0674 4.203 22.074 18.083 3133.969 2.494 80.432 2.617 0.64 258208. 0.4837
|
|
38.80 0.2529 0.4285 0.1182 0.0698 4.350 22.847 18.019 3243.646 2.581 80.147 2.520 0.64 258787. 0.4649
|
|
45.26 0.2950 0.4807 0.1176 0.0722 4.502 23.645 17.931 3357.021 2.671 79.759 2.423 0.65 259433. 0.4459
|
|
51.73 0.3372 0.5278 0.1169 0.0747 4.655 24.449 17.811 3471.073 2.762 79.225 2.327 0.65 260148. 0.4269
|
|
58.19 0.3793 0.5701 0.1158 0.0770 4.803 25.230 17.648 3581.938 2.850 78.498 2.235 0.65 260934. 0.4080
|
|
64.66 0.4215 0.6081 0.1143 0.0793 4.942 25.955 17.429 3684.968 2.932 77.523 2.145 0.65 261792. 0.3893
|
|
71.13 0.4636 0.6422 0.1125 0.0812 5.062 26.589 17.142 3774.882 3.004 76.248 2.060 0.65 262724. 0.3706
|
|
77.59 0.5058 0.6730 0.1101 0.0827 5.158 27.089 16.775 3845.999 3.061 74.617 1.978 0.65 263731. 0.3522
|
|
84.06 0.5479 0.7007 0.1071 0.0837 5.220 27.417 16.318 3892.495 3.098 72.582 1.901 0.65 264810. 0.3338
|
|
90.52 0.5901 0.7258 0.1034 0.0841 5.242 27.531 15.761 3908.750 3.110 70.104 1.829 0.65 265963. 0.3156
|
|
96.99 0.6322 0.7486 0.0991 0.0837 5.216 27.398 15.098 3889.823 3.095 67.157 1.761 0.66 267188. 0.2973
|
|
103.46 0.6744 0.7693 0.0940 0.0824 5.139 26.994 14.331 3832.423 3.050 63.746 1.696 0.66 268482. 0.2791
|
|
109.92 0.7165 0.7881 0.0884 0.0803 5.010 26.314 13.470 3735.942 2.973 59.916 1.635 0.66 269845. 0.2609
|
|
116.39 0.7587 0.8051 0.0822 0.0775 4.830 25.371 12.530 3602.040 2.866 55.733 1.578 0.66 271275. 0.2427
|
|
122.85 0.8008 0.8201 0.0756 0.0738 4.604 24.183 11.526 3433.335 2.732 51.270 1.523 0.66 272770. 0.2247
|
|
129.32 0.8430 0.8332 0.0687 0.0695 4.335 22.768 10.473 3232.438 2.572 46.585 1.470 0.67 274328. 0.2067
|
|
135.79 0.8851 0.8438 0.0615 0.0646 4.025 21.141 9.381 3001.526 2.389 41.725 1.418 0.67 275948. 0.1887
|
|
142.25 0.9273 0.8517 0.0542 0.0590 3.677 19.316 8.257 2742.304 2.182 36.729 1.366 0.67 277628. 0.1706
|
|
148.72 0.9694 0.8560 0.0466 0.0528 3.294 17.300 7.109 2456.099 1.955 31.623 1.313 0.67 279369. 0.1522
|
|
155.19 1.0116 0.8552 0.0390 0.0461 2.875 15.102 5.942 2144.073 1.706 26.431 1.257 0.68 281168. 0.1332
|
|
161.65 1.0537 0.8467 0.0312 0.0389 2.424 12.730 4.761 1807.388 1.438 21.175 1.195 0.68 283025. 0.1133
|
|
168.12 1.0959 0.8245 0.0234 0.0311 1.941 10.195 3.570 1447.376 1.152 15.878 1.119 0.68 284938. 0.0919
|
|
174.58 1.1380 0.7736 0.0156 0.0229 1.429 7.507 2.375 1065.788 0.848 10.564 1.011 0.68 286907. 0.0677
|
|
181.05 1.1802 0.6404 0.0078 0.0143 0.892 4.685 1.183 665.089 0.529 5.262 0.807 0.69 288930. 0.0381
|
|
187.52 1.2223 0.0004 0.0000 0.0053 0.333 1.747 0.000 248.007 0.197 0.001 0.000 0.69 290979. 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 0.1200 0.0591 4.682 22.701 21.463 3491.549 2.565 95.466 2.788 0.70 277532. 0.5614
|
|
7.00 0.0421 0.0834 0.1198 0.0606 4.802 23.280 21.434 3580.521 2.630 95.337 2.715 0.70 277855. 0.5464
|
|
14.01 0.0843 0.1620 0.1197 0.0623 4.935 23.929 21.404 3680.347 2.703 95.207 2.638 0.70 278231. 0.5304
|
|
21.01 0.1264 0.2356 0.1195 0.0641 5.084 24.649 21.373 3791.104 2.785 95.068 2.557 0.70 278662. 0.5138
|
|
28.02 0.1686 0.3038 0.1193 0.0662 5.247 25.438 21.337 3912.488 2.874 94.906 2.474 0.70 279155. 0.4966
|
|
35.02 0.2107 0.3667 0.1190 0.0684 5.423 26.290 21.291 4043.582 2.970 94.704 2.388 0.70 279712. 0.4790
|
|
42.03 0.2529 0.4242 0.1187 0.0708 5.609 27.195 21.230 4182.685 3.072 94.432 2.302 0.70 280338. 0.4611
|
|
49.03 0.2950 0.4764 0.1182 0.0732 5.803 28.134 21.145 4327.118 3.179 94.053 2.216 0.70 281036. 0.4430
|
|
56.04 0.3372 0.5237 0.1175 0.0757 5.999 29.083 21.025 4473.090 3.286 93.517 2.132 0.70 281809. 0.4249
|
|
63.04 0.3793 0.5664 0.1166 0.0781 6.190 30.010 20.856 4615.681 3.391 92.767 2.049 0.70 282658. 0.4068
|
|
70.05 0.4215 0.6049 0.1153 0.0803 6.368 30.876 20.624 4748.940 3.488 91.734 1.970 0.70 283587. 0.3888
|
|
77.05 0.4636 0.6396 0.1135 0.0823 6.526 31.638 20.312 4866.093 3.574 90.348 1.893 0.70 284596. 0.3709
|
|
84.06 0.5058 0.6708 0.1113 0.0839 6.651 32.247 19.906 4959.824 3.643 88.541 1.820 0.71 285686. 0.3530
|
|
91.06 0.5479 0.6991 0.1084 0.0850 6.735 32.656 19.390 5022.594 3.689 86.249 1.751 0.71 286856. 0.3351
|
|
98.07 0.5901 0.7246 0.1048 0.0854 6.768 32.814 18.754 5046.965 3.707 83.417 1.685 0.71 288106. 0.3172
|
|
105.07 0.6322 0.7477 0.1006 0.0850 6.740 32.679 17.988 5026.224 3.692 80.013 1.623 0.71 289433. 0.2992
|
|
112.08 0.6744 0.7688 0.0956 0.0838 6.646 32.220 17.095 4955.645 3.640 76.037 1.565 0.71 290837. 0.2812
|
|
119.08 0.7165 0.7879 0.0899 0.0818 6.482 31.429 16.084 4833.917 3.551 71.542 1.509 0.71 292316. 0.2631
|
|
126.09 0.7587 0.8052 0.0837 0.0789 6.253 30.317 14.975 4662.870 3.425 66.608 1.457 0.72 293867. 0.2450
|
|
133.09 0.8008 0.8207 0.0771 0.0752 5.962 28.906 13.786 4445.828 3.266 61.322 1.407 0.72 295488. 0.2270
|
|
140.10 0.8430 0.8342 0.0701 0.0708 5.614 27.218 12.536 4186.274 3.075 55.758 1.358 0.72 297178. 0.2090
|
|
147.10 0.8851 0.8454 0.0628 0.0658 5.213 25.273 11.235 3887.183 2.855 49.975 1.311 0.72 298935. 0.1910
|
|
154.11 0.9273 0.8540 0.0553 0.0601 4.762 23.087 9.896 3550.878 2.608 44.019 1.264 0.73 300757. 0.1728
|
|
161.11 0.9694 0.8592 0.0477 0.0538 4.263 20.670 8.526 3179.139 2.335 37.924 1.216 0.73 302644. 0.1544
|
|
168.12 1.0116 0.8595 0.0399 0.0469 3.719 18.033 7.131 2773.511 2.037 31.718 1.166 0.73 304595. 0.1354
|
|
175.12 1.0537 0.8523 0.0320 0.0395 3.132 15.186 5.717 2335.727 1.716 25.429 1.110 0.73 306607. 0.1154
|
|
182.13 1.0959 0.8317 0.0240 0.0316 2.505 12.145 4.290 1867.972 1.372 19.081 1.042 0.74 308681. 0.0938
|
|
189.13 1.1380 0.7821 0.0160 0.0232 1.842 8.928 2.856 1373.232 1.009 12.703 0.943 0.74 310815. 0.0693
|
|
196.14 1.1802 0.6486 0.0080 0.0145 1.147 5.563 1.423 855.659 0.629 6.329 0.754 0.74 313006. 0.0391
|
|
203.14 1.2223 -0.0025 0.0000 0.0054 0.429 2.081 -0.002 320.007 0.235 -0.009 -0.003 0.75 315225. 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 0.1201 0.0615 6.085 27.397 24.927 4537.896 3.095 110.875 2.491 0.75 298869. 0.5407
|
|
7.54 0.0421 0.0803 0.1200 0.0629 6.231 28.052 24.896 4646.385 3.169 110.735 2.430 0.75 299217. 0.5270
|
|
15.08 0.0843 0.1564 0.1199 0.0646 6.395 28.789 24.865 4768.491 3.253 110.600 2.365 0.75 299621. 0.5126
|
|
22.62 0.1264 0.2278 0.1197 0.0664 6.577 29.609 24.834 4904.393 3.345 110.464 2.297 0.75 300085. 0.4975
|
|
30.16 0.1685 0.2943 0.1195 0.0684 6.777 30.512 24.801 5053.826 3.447 110.313 2.226 0.75 300614. 0.4818
|
|
37.70 0.2106 0.3559 0.1193 0.0706 6.994 31.489 24.760 5215.786 3.558 110.130 2.153 0.75 301212. 0.4657
|
|
45.24 0.2528 0.4125 0.1191 0.0730 7.226 32.531 24.705 5388.252 3.675 109.886 2.080 0.75 301884. 0.4493
|
|
52.78 0.2949 0.4642 0.1187 0.0754 7.467 33.615 24.627 5567.897 3.798 109.539 2.006 0.75 302633. 0.4327
|
|
60.32 0.3370 0.5114 0.1182 0.0779 7.711 34.714 24.513 5749.870 3.922 109.035 1.934 0.75 303462. 0.4161
|
|
67.86 0.3792 0.5543 0.1174 0.0803 7.949 35.787 24.349 5927.711 4.043 108.303 1.863 0.76 304374. 0.3996
|
|
75.40 0.4213 0.5933 0.1162 0.0825 8.172 36.789 24.115 6093.578 4.156 107.262 1.795 0.76 305372. 0.3831
|
|
82.94 0.4634 0.6289 0.1147 0.0845 8.366 37.665 23.790 6238.638 4.255 105.820 1.730 0.76 306456. 0.3667
|
|
90.48 0.5056 0.6614 0.1126 0.0861 8.520 38.359 23.356 6353.585 4.334 103.889 1.667 0.76 307628. 0.3502
|
|
98.02 0.5477 0.6910 0.1099 0.0871 8.621 38.814 22.793 6429.045 4.385 101.384 1.608 0.76 308886. 0.3337
|
|
105.56 0.5898 0.7181 0.1064 0.0874 8.658 38.976 22.085 6455.902 4.404 98.233 1.552 0.76 310232. 0.3169
|
|
113.10 0.6319 0.7427 0.1023 0.0870 8.617 38.795 21.220 6425.924 4.383 94.388 1.498 0.76 311662. 0.2999
|
|
120.64 0.6741 0.7651 0.0974 0.0858 8.493 38.236 20.198 6333.301 4.320 89.842 1.447 0.77 313174. 0.2826
|
|
128.19 0.7162 0.7854 0.0917 0.0837 8.283 37.289 19.031 6176.422 4.213 84.652 1.398 0.77 314768. 0.2650
|
|
135.73 0.7583 0.8037 0.0855 0.0807 7.989 35.968 17.741 5957.592 4.064 78.914 1.351 0.77 316439. 0.2473
|
|
143.27 0.8005 0.8200 0.0788 0.0769 7.618 34.297 16.352 5680.792 3.875 72.734 1.306 0.77 318186. 0.2295
|
|
150.81 0.8426 0.8342 0.0717 0.0725 7.174 32.299 14.884 5349.958 3.649 66.203 1.262 0.78 320007. 0.2116
|
|
158.35 0.8847 0.8462 0.0644 0.0673 6.663 29.996 13.353 4968.459 3.389 59.396 1.219 0.78 321900. 0.1936
|
|
165.89 0.9269 0.8556 0.0567 0.0615 6.087 27.404 11.773 4539.111 3.096 52.368 1.176 0.78 323864. 0.1755
|
|
173.43 0.9690 0.8615 0.0489 0.0550 5.451 24.539 10.154 4064.485 2.772 45.164 1.133 0.78 325897. 0.1569
|
|
180.97 1.0111 0.8625 0.0410 0.0480 4.757 21.416 8.502 3547.234 2.420 37.816 1.087 0.79 327997. 0.1378
|
|
188.51 1.0532 0.8553 0.0329 0.0405 4.010 18.055 6.824 2990.557 2.040 30.354 1.035 0.79 330165. 0.1175
|
|
196.05 1.0954 0.8333 0.0247 0.0325 3.217 14.481 5.127 2398.657 1.636 22.806 0.970 0.79 332398. 0.0954
|
|
203.59 1.1375 0.7787 0.0165 0.0241 2.383 10.729 3.418 1777.070 1.212 15.204 0.872 0.80 334695. 0.0701
|
|
211.13 1.1796 0.6318 0.0082 0.0153 1.520 6.842 1.705 1133.206 0.773 7.585 0.683 0.80 337054. 0.0387
|
|
218.67 1.2218 -0.0028 0.0000 0.0064 0.638 2.871 -0.003 475.610 0.324 -0.014 -0.003 0.80 339444. 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 0.1202 0.0659 8.025 33.720 28.638 5984.171 3.810 127.382 2.171 0.80 320204. 0.5049
|
|
8.08 0.0421 0.0751 0.1201 0.0673 8.199 34.453 28.602 6114.367 3.893 127.222 2.122 0.80 320576. 0.4932
|
|
16.16 0.0843 0.1466 0.1200 0.0689 8.397 35.282 28.569 6261.496 3.986 127.074 2.069 0.80 321008. 0.4808
|
|
24.23 0.1264 0.2140 0.1198 0.0708 8.617 36.209 28.537 6425.934 4.091 126.932 2.014 0.80 321505. 0.4677
|
|
32.31 0.1685 0.2772 0.1197 0.0728 8.861 37.232 28.505 6607.531 4.206 126.788 1.957 0.80 322070. 0.4541
|
|
40.39 0.2106 0.3360 0.1195 0.0749 9.126 38.346 28.468 6805.254 4.332 126.624 1.897 0.81 322710. 0.4400
|
|
48.47 0.2528 0.3904 0.1193 0.0773 9.410 39.538 28.420 7016.805 4.467 126.413 1.837 0.81 323428. 0.4257
|
|
56.55 0.2949 0.4405 0.1190 0.0797 9.706 40.786 28.353 7238.115 4.608 126.115 1.777 0.81 324228. 0.4112
|
|
64.63 0.3370 0.4865 0.1186 0.0822 10.008 42.052 28.253 7462.928 4.751 125.670 1.717 0.81 325113. 0.3967
|
|
72.70 0.3791 0.5288 0.1180 0.0846 10.302 43.289 28.103 7682.483 4.891 125.001 1.659 0.81 326087. 0.3823
|
|
80.78 0.4213 0.5679 0.1171 0.0868 10.575 44.435 27.879 7885.782 5.020 124.008 1.604 0.81 327152. 0.3680
|
|
88.86 0.4634 0.6041 0.1157 0.0888 10.809 45.419 27.558 8060.384 5.131 122.579 1.551 0.81 328311. 0.3538
|
|
96.94 0.5055 0.6378 0.1138 0.0902 10.988 46.169 27.112 8193.580 5.216 120.596 1.501 0.81 329564. 0.3397
|
|
105.02 0.5476 0.6693 0.1113 0.0911 11.095 46.619 26.517 8273.362 5.267 117.947 1.454 0.82 330912. 0.3254
|
|
113.10 0.5898 0.6986 0.1081 0.0913 11.116 46.707 25.750 8288.896 5.277 114.536 1.409 0.82 332354. 0.3108
|
|
121.17 0.6319 0.7259 0.1041 0.0906 11.038 46.379 24.796 8230.844 5.240 110.291 1.366 0.82 333887. 0.2957
|
|
129.25 0.6740 0.7510 0.0993 0.0891 10.853 45.602 23.649 8092.960 5.152 105.193 1.325 0.82 335510. 0.2802
|
|
137.33 0.7162 0.7742 0.0937 0.0867 10.560 44.371 22.324 7874.344 5.013 99.297 1.286 0.82 337220. 0.2641
|
|
145.41 0.7583 0.7952 0.0875 0.0835 10.164 42.708 20.845 7579.210 4.825 92.717 1.247 0.83 339013. 0.2475
|
|
153.49 0.8004 0.8140 0.0808 0.0794 9.674 40.648 19.240 7213.724 4.592 85.580 1.210 0.83 340889. 0.2306
|
|
161.56 0.8425 0.8305 0.0736 0.0747 9.097 38.224 17.536 6783.453 4.318 78.000 1.173 0.83 342843. 0.2134
|
|
169.64 0.8847 0.8445 0.0661 0.0693 8.438 35.457 15.752 6292.409 4.006 70.066 1.135 0.83 344874. 0.1959
|
|
177.72 0.9268 0.8553 0.0584 0.0633 7.705 32.374 13.905 5745.279 3.658 61.848 1.098 0.84 346981. 0.1779
|
|
185.80 0.9689 0.8615 0.0504 0.0567 6.904 29.008 12.005 5148.062 3.277 53.396 1.058 0.84 349162. 0.1593
|
|
193.88 1.0110 0.8612 0.0422 0.0496 6.040 25.379 10.061 4503.979 2.867 44.753 1.013 0.84 351415. 0.1397
|
|
201.96 1.0532 0.8505 0.0339 0.0420 5.118 21.507 8.083 3816.864 2.430 35.955 0.961 0.85 353739. 0.1187
|
|
210.03 1.0953 0.8202 0.0255 0.0341 4.150 17.438 6.078 3094.729 1.970 27.035 0.891 0.85 356132. 0.0955
|
|
218.11 1.1374 0.7489 0.0170 0.0259 3.148 13.229 4.054 2347.698 1.495 18.031 0.783 0.85 358594. 0.0685
|
|
226.19 1.1795 0.5724 0.0085 0.0175 2.130 8.951 2.022 1588.478 1.011 8.993 0.577 0.86 361123. 0.0357
|
|
234.27 1.2217 -0.0025 0.0000 0.0091 1.114 4.681 -0.004 830.791 0.529 -0.020 -0.002 0.86 363695. 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 0.1200 0.0726 10.736 42.290 32.524 8005.537 4.778 144.669 1.843 0.86 341544. 0.4568
|
|
8.63 0.0422 0.0683 0.1199 0.0740 10.941 43.101 32.479 8159.013 4.870 144.468 1.806 0.86 341942. 0.4472
|
|
17.26 0.0844 0.1336 0.1197 0.0756 11.176 44.025 32.439 8333.977 4.974 144.287 1.765 0.86 342403. 0.4370
|
|
25.89 0.1266 0.1955 0.1196 0.0774 11.440 45.067 32.402 8531.158 5.092 144.122 1.723 0.86 342933. 0.4262
|
|
34.52 0.1688 0.2539 0.1194 0.0794 11.735 46.227 32.367 8750.707 5.223 143.967 1.678 0.86 343536. 0.4148
|
|
43.15 0.2110 0.3085 0.1193 0.0816 12.058 47.500 32.331 8991.782 5.367 143.808 1.631 0.86 344218. 0.4030
|
|
51.78 0.2532 0.3594 0.1192 0.0839 12.406 48.871 32.288 9251.176 5.521 143.619 1.583 0.86 344983. 0.3910
|
|
60.41 0.2953 0.4065 0.1189 0.0864 12.772 50.312 32.230 9524.002 5.684 143.361 1.535 0.86 345836. 0.3788
|
|
69.04 0.3375 0.4501 0.1186 0.0890 13.147 51.789 32.145 9803.679 5.851 142.981 1.487 0.86 346779. 0.3665
|
|
77.67 0.3797 0.4906 0.1181 0.0914 13.516 53.242 32.014 10078.728 6.015 142.399 1.441 0.86 347816. 0.3543
|
|
86.30 0.4219 0.5283 0.1174 0.0938 13.858 54.589 31.813 10333.698 6.167 141.504 1.396 0.86 348951. 0.3423
|
|
94.93 0.4641 0.5638 0.1163 0.0957 14.148 55.733 31.511 10550.185 6.297 140.163 1.355 0.87 350186. 0.3305
|
|
103.56 0.5063 0.5976 0.1147 0.0972 14.361 56.571 31.075 10708.769 6.391 138.224 1.316 0.87 351522. 0.3189
|
|
112.19 0.5485 0.6300 0.1124 0.0979 14.469 56.999 30.469 10789.865 6.440 135.528 1.281 0.87 352962. 0.3073
|
|
120.82 0.5907 0.6611 0.1095 0.0978 14.457 56.950 29.665 10780.520 6.434 131.948 1.248 0.87 354503. 0.2955
|
|
129.45 0.6329 0.6909 0.1057 0.0968 14.309 56.366 28.638 10670.038 6.368 127.383 1.217 0.87 356143. 0.2832
|
|
138.08 0.6751 0.7192 0.1010 0.0948 14.018 55.220 27.381 10453.167 6.239 121.791 1.188 0.88 357881. 0.2702
|
|
146.71 0.7173 0.7459 0.0956 0.0919 13.586 53.520 25.904 10131.301 6.047 115.222 1.160 0.88 359713. 0.2565
|
|
155.34 0.7595 0.7708 0.0894 0.0881 13.024 51.306 24.235 9712.135 5.797 107.798 1.132 0.88 361635. 0.2422
|
|
163.97 0.8016 0.7936 0.0827 0.0835 12.345 48.631 22.408 9205.840 5.494 99.669 1.104 0.88 363645. 0.2271
|
|
172.60 0.8438 0.8141 0.0755 0.0782 11.562 45.548 20.453 8622.107 5.146 90.974 1.076 0.89 365740. 0.2115
|
|
181.23 0.8860 0.8320 0.0679 0.0723 10.686 42.093 18.397 7968.251 4.756 81.828 1.047 0.89 367917. 0.1952
|
|
189.86 0.9282 0.8466 0.0600 0.0658 9.723 38.302 16.259 7250.481 4.327 72.318 1.017 0.89 370174. 0.1783
|
|
198.49 0.9704 0.8547 0.0518 0.0589 8.700 34.272 14.049 6487.703 3.872 62.491 0.982 0.90 372510. 0.1600
|
|
207.12 1.0126 0.8506 0.0435 0.0517 7.646 30.118 11.776 5701.397 3.403 52.378 0.937 0.90 374923. 0.1397
|
|
215.75 1.0548 0.8300 0.0349 0.0443 6.552 25.810 9.453 4885.831 2.916 42.046 0.878 0.90 377412. 0.1173
|
|
224.38 1.0970 0.7823 0.0262 0.0367 5.426 21.376 7.094 4046.458 2.415 31.556 0.795 0.91 379974. 0.0921
|
|
233.02 1.1392 0.6827 0.0174 0.0290 4.291 16.905 4.715 3200.136 1.910 20.972 0.668 0.91 382609. 0.0631
|
|
241.65 1.1814 0.4747 0.0086 0.0215 3.172 12.494 2.336 2365.115 1.412 10.393 0.448 0.92 385315. 0.0298
|
|
250.28 1.2236 -0.0034 0.0000 0.0141 2.091 8.235 -0.011 1558.886 0.930 -0.047 -0.003 0.92 388079. 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 0.1185 0.0796 14.104 52.290 36.247 10517.158 5.908 161.227 1.563 0.91 362951. 0.4091
|
|
9.23 0.0425 0.0621 0.1183 0.0808 14.326 53.115 36.183 10683.022 6.001 160.942 1.536 0.91 363376. 0.4016
|
|
18.45 0.0849 0.1219 0.1181 0.0823 14.584 54.071 36.124 10875.335 6.109 160.681 1.507 0.91 363869. 0.3936
|
|
27.68 0.1274 0.1789 0.1179 0.0839 14.879 55.166 36.071 11095.535 6.233 160.442 1.475 0.91 364435. 0.3849
|
|
36.91 0.1698 0.2330 0.1178 0.0858 15.213 56.404 36.021 11344.568 6.373 160.221 1.440 0.91 365081. 0.3757
|
|
46.13 0.2123 0.2839 0.1176 0.0879 15.586 57.785 35.973 11622.236 6.528 160.008 1.404 0.91 365810. 0.3660
|
|
55.36 0.2547 0.3316 0.1174 0.0902 15.989 59.281 35.920 11923.199 6.698 159.774 1.366 0.91 366629. 0.3560
|
|
64.59 0.2972 0.3760 0.1172 0.0926 16.424 60.895 35.859 12247.726 6.880 159.501 1.328 0.91 367541. 0.3456
|
|
73.82 0.3396 0.4171 0.1170 0.0952 16.882 62.592 35.778 12589.062 7.072 159.141 1.289 0.92 368549. 0.3351
|
|
83.04 0.3821 0.4552 0.1166 0.0979 17.347 64.316 35.661 12935.976 7.266 158.622 1.250 0.92 369656. 0.3245
|
|
92.27 0.4246 0.4906 0.1160 0.1004 17.798 65.985 35.485 13271.600 7.455 157.839 1.213 0.92 370867. 0.3140
|
|
101.50 0.4670 0.5237 0.1151 0.1027 18.202 67.484 35.218 13573.117 7.624 156.652 1.177 0.92 372184. 0.3036
|
|
110.72 0.5095 0.5550 0.1138 0.1045 18.523 68.676 34.822 13812.834 7.759 154.888 1.143 0.92 373609. 0.2933
|
|
119.95 0.5519 0.5852 0.1120 0.1056 18.721 69.410 34.252 13960.504 7.842 152.353 1.113 0.92 375144. 0.2831
|
|
129.18 0.5944 0.6146 0.1094 0.1058 18.753 69.526 33.462 13983.868 7.855 148.839 1.085 0.93 376789. 0.2729
|
|
138.40 0.6368 0.6436 0.1060 0.1049 18.588 68.918 32.416 13861.416 7.786 144.186 1.061 0.93 378544. 0.2625
|
|
147.63 0.6793 0.6721 0.1016 0.1027 18.212 67.522 31.094 13580.766 7.629 138.304 1.038 0.93 380406. 0.2517
|
|
156.86 0.7218 0.7000 0.0964 0.0994 17.626 65.350 29.500 13143.885 7.383 131.218 1.018 0.93 382372. 0.2403
|
|
166.09 0.7642 0.7271 0.0904 0.0950 16.850 62.472 27.665 12564.925 7.058 123.056 0.999 0.94 384438. 0.2283
|
|
175.31 0.8067 0.7530 0.0838 0.0897 15.908 58.980 25.626 11862.696 6.664 113.985 0.980 0.94 386599. 0.2156
|
|
184.54 0.8491 0.7772 0.0766 0.0836 14.828 54.976 23.421 11057.426 6.211 104.178 0.961 0.94 388853. 0.2021
|
|
193.77 0.8916 0.7992 0.0689 0.0769 13.630 50.535 21.083 10164.070 5.709 93.777 0.941 0.95 391195. 0.1878
|
|
202.99 0.9340 0.8183 0.0609 0.0695 12.326 45.699 18.635 9191.542 5.163 82.889 0.920 0.95 393625. 0.1725
|
|
212.22 0.9765 0.8305 0.0526 0.0619 10.965 40.655 16.092 8176.915 4.593 71.579 0.893 0.95 396138. 0.1556
|
|
221.45 1.0189 0.8236 0.0440 0.0544 9.647 35.768 13.455 7194.105 4.041 59.848 0.848 0.96 398734. 0.1352
|
|
230.67 1.0614 0.7846 0.0351 0.0475 8.414 31.195 10.733 6274.197 3.524 47.739 0.776 0.96 401409. 0.1105
|
|
239.90 1.1039 0.7101 0.0261 0.0405 7.187 26.645 7.978 5359.093 3.010 35.484 0.675 0.96 404164. 0.0829
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249.13 1.1463 0.5798 0.0171 0.0338 5.996 22.232 5.234 4471.566 2.512 23.281 0.531 0.97 406995. 0.0528
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258.36 1.1888 0.3614 0.0083 0.0275 4.868 18.049 2.554 3630.152 2.039 11.359 0.319 0.97 409902. 0.0222
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267.58 1.2312 -0.0065 -0.0001 0.0216 3.821 14.165 -0.035 2849.106 1.600 -0.156 -0.006 0.98 412885. 0.0000
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