612 lines
109 KiB
Plaintext
612 lines
109 KiB
Plaintext
12x10 (12x10.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 0.1237 0.0701 0.001 0.088 0.082 1.047 0.010 0.363 35.411 0.05 18526. 0.4950
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0.39 0.0341 0.0586 0.1227 0.0713 0.001 0.090 0.081 1.065 0.010 0.361 34.533 0.05 18544. 0.4808
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0.77 0.0681 0.1141 0.1216 0.0726 0.001 0.092 0.080 1.084 0.010 0.357 33.637 0.05 18565. 0.4663
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1.16 0.1022 0.1666 0.1204 0.0738 0.001 0.093 0.080 1.102 0.011 0.354 32.732 0.05 18587. 0.4514
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1.55 0.1362 0.2159 0.1190 0.0750 0.002 0.095 0.079 1.120 0.011 0.350 31.821 0.05 18612. 0.4362
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1.93 0.1703 0.2622 0.1173 0.0762 0.002 0.096 0.078 1.138 0.011 0.345 30.910 0.05 18640. 0.4209
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2.32 0.2043 0.3054 0.1155 0.0773 0.002 0.098 0.076 1.154 0.011 0.340 30.004 0.05 18671. 0.4054
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2.71 0.2384 0.3457 0.1135 0.0782 0.002 0.099 0.075 1.168 0.011 0.333 29.106 0.05 18705. 0.3897
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3.10 0.2724 0.3830 0.1111 0.0791 0.002 0.100 0.073 1.180 0.011 0.327 28.218 0.05 18741. 0.3739
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3.48 0.3065 0.4175 0.1085 0.0797 0.002 0.101 0.072 1.190 0.011 0.319 27.342 0.05 18781. 0.3580
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3.87 0.3406 0.4492 0.1056 0.0801 0.002 0.101 0.070 1.196 0.011 0.310 26.478 0.05 18824. 0.3420
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4.26 0.3746 0.4782 0.1024 0.0802 0.002 0.101 0.068 1.198 0.011 0.301 25.626 0.05 18870. 0.3259
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4.64 0.4087 0.5046 0.0988 0.0800 0.002 0.101 0.065 1.195 0.011 0.290 24.784 0.05 18919. 0.3097
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5.03 0.4427 0.5282 0.0949 0.0795 0.002 0.100 0.063 1.187 0.011 0.279 23.949 0.05 18971. 0.2932
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5.42 0.4768 0.5491 0.0906 0.0786 0.002 0.099 0.060 1.174 0.011 0.266 23.119 0.05 19026. 0.2766
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5.80 0.5108 0.5672 0.0859 0.0774 0.002 0.098 0.057 1.155 0.011 0.253 22.288 0.05 19085. 0.2597
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6.19 0.5449 0.5823 0.0809 0.0757 0.002 0.096 0.053 1.130 0.011 0.238 21.452 0.05 19146. 0.2425
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6.58 0.5789 0.5943 0.0756 0.0736 0.001 0.093 0.050 1.099 0.010 0.222 20.604 0.05 19211. 0.2252
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6.97 0.6130 0.6027 0.0700 0.0712 0.001 0.090 0.046 1.063 0.010 0.206 19.736 0.05 19278. 0.2076
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7.35 0.6470 0.6072 0.0642 0.0684 0.001 0.086 0.042 1.022 0.010 0.189 18.836 0.05 19349. 0.1898
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7.74 0.6811 0.6071 0.0583 0.0654 0.001 0.082 0.039 0.976 0.009 0.171 17.893 0.05 19422. 0.1717
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8.13 0.7152 0.6018 0.0522 0.0620 0.001 0.078 0.034 0.926 0.009 0.153 16.890 0.05 19499. 0.1533
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8.51 0.7492 0.5899 0.0459 0.0583 0.001 0.074 0.030 0.871 0.008 0.135 15.805 0.05 19578. 0.1346
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8.90 0.7833 0.5701 0.0395 0.0543 0.001 0.069 0.026 0.811 0.008 0.116 14.610 0.05 19661. 0.1155
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9.29 0.8173 0.5400 0.0331 0.0501 0.001 0.063 0.022 0.748 0.007 0.097 13.261 0.05 19746. 0.0959
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9.67 0.8514 0.4962 0.0266 0.0456 0.001 0.058 0.018 0.681 0.007 0.078 11.699 0.05 19834. 0.0758
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10.06 0.8854 0.4336 0.0200 0.0408 0.001 0.052 0.013 0.610 0.006 0.059 9.829 0.05 19925. 0.0552
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10.45 0.9195 0.3435 0.0134 0.0358 0.001 0.045 0.009 0.535 0.005 0.039 7.498 0.05 20019. 0.0345
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10.84 0.9535 0.2110 0.0068 0.0306 0.001 0.039 0.004 0.457 0.004 0.020 4.442 0.05 20115. 0.0145
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11.22 0.9876 0.0074 0.0002 0.0252 0.001 0.032 0.000 0.376 0.004 0.001 0.151 0.05 20214. 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 0.1243 0.0622 0.010 0.314 0.328 7.432 0.035 1.461 20.045 0.10 37053. 0.5618
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0.78 0.0344 0.0667 0.1233 0.0635 0.010 0.321 0.326 7.588 0.036 1.450 19.488 0.10 37089. 0.5441
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1.56 0.0687 0.1296 0.1223 0.0649 0.010 0.327 0.323 7.747 0.037 1.438 18.923 0.10 37130. 0.5260
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2.34 0.1031 0.1886 0.1211 0.0662 0.011 0.334 0.320 7.907 0.038 1.423 18.355 0.10 37175. 0.5077
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3.12 0.1375 0.2437 0.1197 0.0675 0.011 0.341 0.316 8.064 0.039 1.407 17.789 0.10 37227. 0.4892
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3.91 0.1719 0.2950 0.1181 0.0688 0.011 0.347 0.312 8.216 0.039 1.388 17.228 0.10 37283. 0.4706
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4.69 0.2062 0.3427 0.1163 0.0700 0.011 0.353 0.307 8.359 0.040 1.367 16.674 0.10 37345. 0.4520
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5.47 0.2406 0.3867 0.1142 0.0711 0.011 0.359 0.302 8.487 0.041 1.343 16.131 0.10 37414. 0.4333
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6.25 0.2750 0.4274 0.1119 0.0720 0.012 0.363 0.296 8.598 0.041 1.315 15.599 0.10 37488. 0.4147
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7.03 0.3094 0.4648 0.1092 0.0727 0.012 0.367 0.289 8.685 0.041 1.284 15.079 0.10 37569. 0.3962
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7.81 0.3437 0.4991 0.1063 0.0732 0.012 0.370 0.281 8.745 0.042 1.250 14.573 0.10 37656. 0.3777
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8.59 0.3781 0.5304 0.1030 0.0734 0.012 0.371 0.272 8.774 0.042 1.211 14.079 0.10 37749. 0.3593
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9.38 0.4125 0.5589 0.0994 0.0734 0.012 0.370 0.263 8.765 0.042 1.169 13.598 0.10 37849. 0.3408
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10.16 0.4469 0.5845 0.0954 0.0730 0.012 0.368 0.252 8.714 0.042 1.122 13.127 0.10 37955. 0.3224
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10.94 0.4812 0.6073 0.0910 0.0721 0.012 0.364 0.241 8.618 0.041 1.070 12.666 0.10 38067. 0.3038
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11.72 0.5156 0.6274 0.0863 0.0709 0.011 0.358 0.228 8.472 0.040 1.015 12.213 0.10 38186. 0.2852
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12.50 0.5500 0.6447 0.0812 0.0693 0.011 0.350 0.215 8.275 0.040 0.955 11.764 0.10 38311. 0.2665
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13.28 0.5844 0.6589 0.0758 0.0672 0.011 0.339 0.200 8.030 0.038 0.891 11.317 0.10 38442. 0.2477
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14.06 0.6187 0.6700 0.0702 0.0648 0.010 0.327 0.185 7.740 0.037 0.825 10.867 0.10 38580. 0.2288
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14.84 0.6531 0.6774 0.0643 0.0620 0.010 0.313 0.170 7.405 0.035 0.756 10.410 0.10 38723. 0.2098
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15.62 0.6875 0.6807 0.0583 0.0588 0.009 0.297 0.154 7.029 0.034 0.685 9.938 0.10 38873. 0.1907
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16.41 0.7219 0.6792 0.0521 0.0554 0.009 0.279 0.138 6.614 0.032 0.612 9.443 0.10 39029. 0.1713
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17.19 0.7562 0.6717 0.0458 0.0516 0.008 0.260 0.121 6.159 0.029 0.538 8.914 0.10 39190. 0.1517
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17.97 0.7906 0.6566 0.0394 0.0474 0.008 0.239 0.104 5.667 0.027 0.463 8.335 0.10 39358. 0.1315
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18.75 0.8250 0.6313 0.0329 0.0430 0.007 0.217 0.087 5.138 0.025 0.387 7.680 0.10 39531. 0.1108
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19.53 0.8594 0.5918 0.0264 0.0383 0.006 0.193 0.070 4.574 0.022 0.310 6.911 0.10 39710. 0.0892
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20.31 0.8937 0.5311 0.0198 0.0333 0.005 0.168 0.052 3.976 0.019 0.233 5.965 0.10 39895. 0.0667
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21.09 0.9281 0.4366 0.0132 0.0280 0.004 0.141 0.035 3.346 0.016 0.155 4.721 0.10 40086. 0.0431
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21.87 0.9625 0.2818 0.0066 0.0225 0.004 0.114 0.017 2.687 0.013 0.077 2.938 0.10 40282. 0.0190
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22.66 0.9969 0.0023 0.0000 0.0168 0.003 0.085 0.000 2.002 0.010 0.000 0.023 0.10 40483. 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 0.1246 0.0590 0.032 0.670 0.741 23.780 0.076 3.296 14.134 0.14 55578. 0.5949
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1.18 0.0345 0.0707 0.1237 0.0603 0.033 0.685 0.736 24.318 0.077 3.272 13.719 0.14 55633. 0.5753
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2.35 0.0690 0.1372 0.1226 0.0617 0.033 0.701 0.729 24.871 0.079 3.244 13.301 0.14 55694. 0.5554
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3.53 0.1035 0.1993 0.1214 0.0631 0.034 0.716 0.722 25.427 0.081 3.212 12.882 0.14 55763. 0.5353
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4.70 0.1380 0.2571 0.1201 0.0644 0.035 0.732 0.714 25.978 0.083 3.176 12.466 0.14 55840. 0.5151
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5.88 0.1725 0.3108 0.1185 0.0658 0.036 0.747 0.705 26.511 0.084 3.134 12.055 0.14 55926. 0.4948
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7.06 0.2070 0.3605 0.1167 0.0670 0.036 0.761 0.694 27.011 0.086 3.086 11.651 0.14 56020. 0.4746
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8.23 0.2415 0.4063 0.1146 0.0681 0.037 0.774 0.682 27.466 0.087 3.032 11.256 0.14 56123. 0.4544
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9.41 0.2760 0.4485 0.1123 0.0691 0.037 0.785 0.668 27.860 0.089 2.970 10.872 0.14 56235. 0.4344
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10.59 0.3105 0.4872 0.1097 0.0699 0.038 0.794 0.652 28.176 0.090 2.901 10.499 0.14 56357. 0.4146
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11.76 0.3450 0.5227 0.1067 0.0704 0.038 0.800 0.635 28.400 0.090 2.823 10.136 0.14 56488. 0.3949
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12.94 0.3795 0.5550 0.1034 0.0707 0.038 0.803 0.615 28.514 0.091 2.736 9.785 0.14 56629. 0.3753
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14.11 0.4140 0.5844 0.0998 0.0707 0.038 0.803 0.594 28.502 0.091 2.640 9.445 0.14 56779. 0.3558
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15.29 0.4485 0.6110 0.0958 0.0703 0.038 0.799 0.570 28.346 0.090 2.534 9.115 0.14 56940. 0.3364
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16.47 0.4830 0.6348 0.0914 0.0695 0.038 0.790 0.543 28.032 0.089 2.417 8.793 0.14 57109. 0.3170
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17.64 0.5175 0.6558 0.0866 0.0683 0.037 0.776 0.515 27.548 0.088 2.291 8.479 0.14 57289. 0.2975
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18.82 0.5520 0.6742 0.0815 0.0667 0.036 0.758 0.484 26.890 0.086 2.155 8.172 0.14 57478. 0.2781
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19.99 0.5865 0.6897 0.0760 0.0647 0.035 0.734 0.452 26.065 0.083 2.011 7.868 0.15 57676. 0.2587
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21.17 0.6210 0.7022 0.0703 0.0622 0.034 0.707 0.418 25.080 0.080 1.861 7.566 0.15 57883. 0.2393
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22.35 0.6555 0.7114 0.0645 0.0594 0.032 0.675 0.383 23.944 0.076 1.705 7.261 0.15 58100. 0.2198
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23.52 0.6900 0.7168 0.0584 0.0562 0.030 0.638 0.347 22.661 0.072 1.545 6.950 0.15 58326. 0.2003
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24.70 0.7245 0.7177 0.0522 0.0527 0.028 0.598 0.310 21.239 0.068 1.380 6.628 0.15 58561. 0.1805
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25.88 0.7590 0.7130 0.0459 0.0488 0.026 0.554 0.273 19.679 0.063 1.213 6.286 0.15 58805. 0.1605
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27.05 0.7935 0.7013 0.0394 0.0446 0.024 0.507 0.235 17.987 0.057 1.043 5.914 0.15 59058. 0.1400
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28.23 0.8280 0.6800 0.0329 0.0401 0.022 0.455 0.196 16.167 0.051 0.871 5.495 0.15 59320. 0.1189
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29.40 0.8625 0.6447 0.0264 0.0353 0.019 0.401 0.157 14.221 0.045 0.698 5.002 0.15 59590. 0.0969
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30.58 0.8970 0.5882 0.0198 0.0302 0.016 0.343 0.118 12.157 0.039 0.523 4.387 0.15 59869. 0.0736
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31.76 0.9315 0.4953 0.0132 0.0248 0.013 0.281 0.078 9.982 0.032 0.348 3.558 0.15 60157. 0.0487
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32.93 0.9660 0.3325 0.0066 0.0191 0.010 0.217 0.039 7.704 0.025 0.174 2.303 0.15 60453. 0.0223
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34.11 1.0005 0.0029 0.0000 0.0132 0.007 0.150 0.000 5.335 0.017 0.001 0.019 0.15 60756. 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 0.1249 0.0572 0.073 1.155 1.320 54.654 0.130 5.872 10.956 0.19 74104. 0.6155
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1.57 0.0346 0.0732 0.1240 0.0586 0.075 1.182 1.311 55.953 0.134 5.830 10.625 0.19 74176. 0.5948
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3.14 0.0692 0.1418 0.1229 0.0599 0.077 1.211 1.300 57.287 0.137 5.781 10.291 0.19 74259. 0.5737
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4.72 0.1037 0.2059 0.1217 0.0614 0.079 1.239 1.287 58.635 0.140 5.726 9.957 0.19 74351. 0.5524
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6.29 0.1383 0.2654 0.1204 0.0628 0.080 1.267 1.273 59.969 0.143 5.661 9.627 0.19 74454. 0.5311
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7.86 0.1729 0.3205 0.1188 0.0641 0.082 1.295 1.256 61.263 0.146 5.588 9.301 0.19 74568. 0.5097
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9.43 0.2075 0.3714 0.1170 0.0654 0.084 1.320 1.237 62.482 0.149 5.503 8.982 0.19 74694. 0.4885
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11.00 0.2421 0.4182 0.1150 0.0665 0.085 1.344 1.216 63.593 0.152 5.407 8.670 0.19 74832. 0.4674
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12.58 0.2767 0.4613 0.1126 0.0676 0.087 1.364 1.191 64.559 0.154 5.298 8.368 0.19 74982. 0.4465
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14.15 0.3112 0.5008 0.1100 0.0684 0.088 1.381 1.163 65.342 0.156 5.174 8.075 0.19 75145. 0.4259
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15.72 0.3458 0.5370 0.1071 0.0690 0.088 1.393 1.132 65.902 0.157 5.036 7.792 0.19 75321. 0.4054
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17.29 0.3804 0.5700 0.1038 0.0693 0.089 1.399 1.097 66.200 0.158 4.881 7.519 0.19 75509. 0.3851
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18.86 0.4150 0.5999 0.1001 0.0693 0.089 1.399 1.059 66.196 0.158 4.710 7.255 0.19 75711. 0.3650
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20.44 0.4496 0.6271 0.0961 0.0689 0.088 1.391 1.016 65.847 0.157 4.520 7.000 0.19 75925. 0.3450
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22.01 0.4842 0.6514 0.0917 0.0681 0.087 1.376 0.969 65.117 0.155 4.312 6.752 0.19 76153. 0.3251
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23.58 0.5187 0.6731 0.0869 0.0669 0.086 1.352 0.919 63.977 0.153 4.086 6.512 0.19 76393. 0.3052
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25.15 0.5533 0.6922 0.0817 0.0653 0.084 1.319 0.864 62.421 0.149 3.843 6.278 0.19 76646. 0.2853
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26.72 0.5879 0.7086 0.0763 0.0633 0.081 1.278 0.806 60.461 0.144 3.586 6.048 0.19 76911. 0.2655
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28.29 0.6225 0.7220 0.0705 0.0608 0.078 1.228 0.746 58.114 0.139 3.317 5.821 0.19 77189. 0.2458
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29.87 0.6571 0.7324 0.0646 0.0580 0.074 1.171 0.683 55.400 0.132 3.039 5.594 0.19 77480. 0.2261
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31.44 0.6917 0.7392 0.0585 0.0548 0.070 1.106 0.619 52.332 0.125 2.752 5.363 0.19 77782. 0.2063
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33.01 0.7262 0.7418 0.0523 0.0512 0.066 1.034 0.553 48.923 0.117 2.459 5.126 0.20 78097. 0.1864
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34.58 0.7608 0.7392 0.0459 0.0473 0.061 0.955 0.486 45.182 0.108 2.160 4.876 0.20 78424. 0.1661
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36.15 0.7954 0.7299 0.0395 0.0430 0.055 0.869 0.417 41.117 0.098 1.857 4.605 0.20 78762. 0.1455
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37.73 0.8300 0.7115 0.0330 0.0384 0.049 0.776 0.348 36.739 0.088 1.550 4.302 0.20 79113. 0.1242
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39.30 0.8646 0.6798 0.0264 0.0335 0.043 0.677 0.279 32.058 0.077 1.240 3.946 0.20 79475. 0.1019
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40.87 0.8991 0.6268 0.0198 0.0283 0.036 0.572 0.209 27.088 0.065 0.929 3.498 0.20 79849. 0.0782
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42.44 0.9337 0.5365 0.0131 0.0229 0.029 0.462 0.139 21.846 0.052 0.618 2.884 0.20 80235. 0.0525
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44.01 0.9683 0.3697 0.0065 0.0171 0.022 0.346 0.069 16.357 0.039 0.307 1.916 0.20 80631. 0.0246
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45.59 1.0029 -0.0011 0.0000 0.0111 0.014 0.225 0.000 10.646 0.025 -0.001 -0.006 0.20 81035. 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 0.1251 0.0561 0.140 1.769 2.067 104.658 0.200 9.194 8.959 0.24 92628. 0.6298
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1.97 0.0346 0.0749 0.1242 0.0575 0.144 1.813 2.053 107.230 0.205 9.130 8.682 0.24 92719. 0.6082
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3.94 0.0693 0.1450 0.1232 0.0589 0.147 1.857 2.036 109.875 0.210 9.055 8.404 0.24 92822. 0.5863
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5.90 0.1039 0.2103 0.1221 0.0603 0.151 1.903 2.017 112.550 0.215 8.969 8.126 0.24 92937. 0.5643
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7.87 0.1385 0.2709 0.1207 0.0617 0.154 1.947 1.994 115.204 0.220 8.870 7.852 0.24 93066. 0.5422
|
|
9.84 0.1732 0.3270 0.1192 0.0631 0.158 1.991 1.969 117.779 0.225 8.756 7.581 0.24 93209. 0.5201
|
|
11.81 0.2078 0.3787 0.1174 0.0644 0.161 2.032 1.939 120.213 0.230 8.626 7.317 0.24 93367. 0.4982
|
|
13.77 0.2424 0.4263 0.1153 0.0656 0.164 2.070 1.906 122.435 0.234 8.476 7.059 0.24 93540. 0.4765
|
|
15.74 0.2771 0.4700 0.1130 0.0666 0.167 2.102 1.867 124.372 0.238 8.306 6.810 0.24 93728. 0.4550
|
|
17.71 0.3117 0.5100 0.1104 0.0675 0.169 2.129 1.824 125.950 0.241 8.114 6.569 0.24 93932. 0.4338
|
|
19.68 0.3463 0.5466 0.1075 0.0681 0.170 2.148 1.775 127.091 0.243 7.897 6.336 0.24 94152. 0.4128
|
|
21.65 0.3810 0.5800 0.1042 0.0684 0.171 2.159 1.721 127.716 0.244 7.656 6.112 0.24 94389. 0.3921
|
|
23.61 0.4156 0.6104 0.1005 0.0684 0.171 2.159 1.661 127.743 0.244 7.387 5.897 0.24 94642. 0.3716
|
|
25.58 0.4502 0.6379 0.0965 0.0681 0.170 2.148 1.594 127.092 0.243 7.090 5.688 0.24 94911. 0.3512
|
|
27.55 0.4849 0.6627 0.0920 0.0673 0.169 2.125 1.521 125.686 0.240 6.764 5.488 0.24 95196. 0.3309
|
|
29.52 0.5195 0.6849 0.0872 0.0662 0.166 2.087 1.441 123.470 0.236 6.409 5.293 0.24 95497. 0.3107
|
|
31.48 0.5541 0.7045 0.0820 0.0645 0.162 2.036 1.355 120.431 0.230 6.028 5.104 0.24 95814. 0.2905
|
|
33.45 0.5887 0.7215 0.0765 0.0625 0.156 1.971 1.265 116.591 0.223 5.625 4.920 0.24 96147. 0.2705
|
|
35.42 0.6234 0.7357 0.0708 0.0600 0.150 1.893 1.170 111.985 0.214 5.203 4.738 0.24 96495. 0.2506
|
|
37.39 0.6580 0.7469 0.0649 0.0571 0.143 1.803 1.072 106.649 0.204 4.766 4.557 0.24 96859. 0.2307
|
|
39.35 0.6926 0.7548 0.0587 0.0539 0.135 1.701 0.970 100.610 0.192 4.316 4.375 0.24 97238. 0.2107
|
|
41.32 0.7273 0.7587 0.0525 0.0503 0.126 1.587 0.867 93.891 0.179 3.856 4.188 0.24 97633. 0.1907
|
|
43.29 0.7619 0.7577 0.0461 0.0464 0.116 1.462 0.762 86.512 0.165 3.387 3.993 0.24 98042. 0.1704
|
|
45.26 0.7965 0.7504 0.0396 0.0421 0.105 1.327 0.655 78.489 0.150 2.911 3.782 0.25 98467. 0.1496
|
|
47.23 0.8312 0.7345 0.0331 0.0374 0.094 1.181 0.546 69.841 0.133 2.430 3.548 0.25 98906. 0.1282
|
|
49.19 0.8658 0.7056 0.0265 0.0325 0.081 1.024 0.437 60.589 0.116 1.944 3.272 0.25 99360. 0.1058
|
|
51.16 0.9004 0.6561 0.0198 0.0272 0.068 0.858 0.327 50.761 0.097 1.456 2.925 0.25 99829. 0.0818
|
|
53.13 0.9351 0.5690 0.0132 0.0216 0.054 0.683 0.218 40.394 0.077 0.968 2.443 0.25 100312. 0.0557
|
|
55.10 0.9697 0.4014 0.0065 0.0158 0.040 0.499 0.108 29.535 0.056 0.481 1.662 0.25 100809. 0.0267
|
|
57.06 1.0043 -0.0018 0.0000 0.0098 0.024 0.308 0.000 18.231 0.035 -0.001 -0.007 0.25 101314. 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 0.1254 0.0553 0.239 2.514 2.983 178.485 0.284 13.269 7.581 0.29 111151. 0.6403
|
|
2.36 0.0347 0.0761 0.1245 0.0567 0.245 2.578 2.963 182.984 0.291 13.178 7.344 0.29 111260. 0.6181
|
|
4.73 0.0693 0.1472 0.1235 0.0582 0.252 2.643 2.939 187.617 0.299 13.073 7.105 0.29 111384. 0.5956
|
|
7.09 0.1040 0.2135 0.1224 0.0596 0.258 2.709 2.912 192.307 0.306 12.952 6.868 0.29 111522. 0.5730
|
|
9.45 0.1387 0.2749 0.1211 0.0611 0.264 2.775 2.880 196.966 0.313 12.811 6.633 0.29 111677. 0.5504
|
|
11.82 0.1733 0.3316 0.1195 0.0625 0.270 2.838 2.844 201.495 0.321 12.649 6.401 0.29 111849. 0.5279
|
|
14.18 0.2080 0.3839 0.1178 0.0638 0.276 2.899 2.802 205.780 0.328 12.463 6.176 0.29 112038. 0.5055
|
|
16.54 0.2426 0.4320 0.1158 0.0650 0.281 2.954 2.754 209.702 0.334 12.249 5.956 0.29 112246. 0.4833
|
|
18.91 0.2773 0.4761 0.1135 0.0661 0.286 3.002 2.699 213.130 0.339 12.005 5.744 0.29 112473. 0.4614
|
|
21.27 0.3120 0.5165 0.1108 0.0670 0.290 3.042 2.637 215.934 0.344 11.729 5.539 0.29 112718. 0.4398
|
|
23.63 0.3466 0.5535 0.1079 0.0676 0.292 3.071 2.567 217.977 0.347 11.419 5.342 0.29 112983. 0.4185
|
|
26.00 0.3813 0.5872 0.1046 0.0679 0.294 3.087 2.489 219.120 0.349 11.071 5.152 0.29 113267. 0.3974
|
|
28.36 0.4160 0.6179 0.1010 0.0680 0.294 3.088 2.402 219.222 0.349 10.684 4.970 0.29 113571. 0.3766
|
|
30.72 0.4506 0.6457 0.0969 0.0676 0.293 3.073 2.306 218.138 0.347 10.255 4.794 0.29 113895. 0.3559
|
|
33.09 0.4853 0.6709 0.0925 0.0669 0.289 3.039 2.200 215.738 0.343 9.785 4.625 0.29 114238. 0.3354
|
|
35.45 0.5199 0.6934 0.0876 0.0657 0.284 2.985 2.085 211.922 0.337 9.272 4.462 0.29 114600. 0.3150
|
|
37.81 0.5546 0.7134 0.0824 0.0641 0.277 2.911 1.961 206.666 0.329 8.722 4.303 0.29 114981. 0.2947
|
|
40.18 0.5893 0.7309 0.0769 0.0620 0.268 2.818 1.830 200.007 0.318 8.139 4.149 0.29 115381. 0.2745
|
|
42.54 0.6239 0.7457 0.0711 0.0595 0.257 2.705 1.693 192.008 0.306 7.529 3.998 0.29 115800. 0.2544
|
|
44.90 0.6586 0.7576 0.0652 0.0567 0.245 2.574 1.550 182.727 0.291 6.897 3.849 0.29 116238. 0.2343
|
|
47.27 0.6933 0.7664 0.0590 0.0534 0.231 2.426 1.404 172.213 0.274 6.246 3.698 0.29 116694. 0.2143
|
|
49.63 0.7279 0.7714 0.0527 0.0498 0.215 2.261 1.255 160.507 0.255 5.580 3.545 0.29 117168. 0.1942
|
|
51.99 0.7626 0.7717 0.0463 0.0458 0.198 2.080 1.102 147.640 0.235 4.902 3.386 0.29 117660. 0.1738
|
|
54.36 0.7973 0.7661 0.0398 0.0414 0.179 1.883 0.947 133.643 0.213 4.213 3.215 0.29 118171. 0.1530
|
|
56.72 0.8319 0.7522 0.0332 0.0368 0.159 1.670 0.791 118.548 0.189 3.517 3.025 0.30 118699. 0.1315
|
|
59.08 0.8666 0.7259 0.0266 0.0317 0.137 1.442 0.633 102.393 0.163 2.814 2.803 0.30 119245. 0.1090
|
|
61.45 0.9012 0.6796 0.0199 0.0264 0.114 1.201 0.474 85.226 0.136 2.108 2.523 0.30 119808. 0.0849
|
|
63.81 0.9359 0.5959 0.0132 0.0208 0.090 0.945 0.315 67.113 0.107 1.402 2.130 0.30 120389. 0.0585
|
|
66.17 0.9706 0.4293 0.0066 0.0149 0.065 0.678 0.157 48.136 0.077 0.698 1.480 0.30 120986. 0.0287
|
|
68.54 1.0052 0.0006 0.0000 0.0088 0.038 0.400 0.000 28.377 0.045 0.001 0.002 0.30 121592. 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 0.1257 0.0549 0.377 3.393 4.070 280.961 0.383 18.104 6.571 0.33 129673. 0.6482
|
|
2.76 0.0347 0.0770 0.1249 0.0563 0.386 3.480 4.043 288.193 0.393 17.984 6.363 0.33 129800. 0.6256
|
|
5.52 0.0694 0.1489 0.1239 0.0577 0.396 3.570 4.012 295.649 0.403 17.844 6.154 0.33 129944. 0.6028
|
|
8.28 0.1041 0.2159 0.1228 0.0592 0.407 3.661 3.975 303.207 0.414 17.682 5.947 0.33 130106. 0.5797
|
|
11.04 0.1388 0.2779 0.1215 0.0607 0.417 3.752 3.933 310.725 0.424 17.494 5.741 0.33 130287. 0.5567
|
|
13.80 0.1735 0.3351 0.1200 0.0621 0.427 3.840 3.884 318.041 0.434 17.277 5.539 0.33 130488. 0.5338
|
|
16.56 0.2082 0.3878 0.1182 0.0635 0.436 3.924 3.828 324.976 0.443 17.026 5.342 0.33 130709. 0.5111
|
|
19.32 0.2429 0.4363 0.1162 0.0647 0.444 4.001 3.763 331.332 0.452 16.738 5.151 0.33 130952. 0.4886
|
|
22.08 0.2776 0.4807 0.1139 0.0658 0.452 4.068 3.689 336.902 0.460 16.408 4.966 0.33 131216. 0.4664
|
|
24.84 0.3123 0.5214 0.1113 0.0667 0.458 4.123 3.605 341.471 0.466 16.034 4.788 0.33 131503. 0.4445
|
|
27.60 0.3470 0.5586 0.1084 0.0673 0.462 4.164 3.510 344.821 0.470 15.612 4.617 0.34 131813. 0.4229
|
|
30.36 0.3817 0.5926 0.1051 0.0677 0.465 4.187 3.404 346.727 0.473 15.139 4.452 0.34 132146. 0.4016
|
|
33.12 0.4164 0.6235 0.1015 0.0677 0.465 4.189 3.285 346.960 0.473 14.612 4.294 0.34 132501. 0.3806
|
|
35.88 0.4511 0.6516 0.0974 0.0674 0.463 4.169 3.154 345.291 0.471 14.028 4.143 0.34 132879. 0.3597
|
|
38.64 0.4858 0.6770 0.0929 0.0667 0.458 4.124 3.009 341.504 0.466 13.385 3.997 0.34 133280. 0.3390
|
|
41.40 0.5205 0.6999 0.0881 0.0655 0.450 4.050 2.852 335.442 0.458 12.685 3.856 0.34 133704. 0.3184
|
|
44.16 0.5551 0.7202 0.0829 0.0639 0.439 3.949 2.683 327.064 0.446 11.933 3.720 0.34 134150. 0.2980
|
|
46.92 0.5898 0.7381 0.0773 0.0618 0.424 3.821 2.503 316.428 0.432 11.135 3.588 0.34 134618. 0.2776
|
|
49.68 0.6245 0.7534 0.0715 0.0593 0.407 3.666 2.316 303.632 0.414 10.301 3.459 0.34 135108. 0.2574
|
|
52.44 0.6592 0.7660 0.0655 0.0564 0.387 3.487 2.121 288.772 0.394 9.436 3.332 0.34 135619. 0.2373
|
|
55.20 0.6939 0.7755 0.0593 0.0531 0.365 3.283 1.921 271.927 0.371 8.545 3.204 0.34 136152. 0.2172
|
|
57.96 0.7286 0.7813 0.0530 0.0494 0.339 3.057 1.716 253.158 0.345 7.634 3.075 0.34 136707. 0.1970
|
|
60.72 0.7633 0.7828 0.0466 0.0454 0.312 2.808 1.507 232.519 0.317 6.705 2.941 0.34 137282. 0.1765
|
|
63.48 0.7980 0.7785 0.0400 0.0410 0.282 2.536 1.296 210.058 0.287 5.763 2.797 0.34 137879. 0.1557
|
|
66.24 0.8327 0.7663 0.0334 0.0363 0.249 2.244 1.081 185.826 0.254 4.809 2.639 0.34 138496. 0.1342
|
|
69.00 0.8674 0.7422 0.0267 0.0312 0.214 1.931 0.865 159.885 0.218 3.847 2.454 0.35 139134. 0.1116
|
|
71.76 0.9021 0.6984 0.0200 0.0258 0.177 1.598 0.648 132.313 0.180 2.881 2.220 0.35 139793. 0.0874
|
|
74.52 0.9368 0.6176 0.0133 0.0202 0.138 1.246 0.430 103.216 0.141 1.914 1.891 0.35 140471. 0.0606
|
|
77.28 0.9715 0.4515 0.0066 0.0142 0.098 0.878 0.214 72.729 0.099 0.950 1.333 0.35 141169. 0.0301
|
|
80.04 1.0062 -0.0044 0.0000 0.0080 0.055 0.495 -0.001 40.975 0.056 -0.005 -0.013 0.35 141876. 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 0.1260 0.0546 0.559 4.407 5.330 417.090 0.498 23.708 5.796 0.38 148193. 0.6543
|
|
3.16 0.0347 0.0776 0.1252 0.0560 0.574 4.522 5.296 428.013 0.511 23.556 5.612 0.38 148339. 0.6315
|
|
6.31 0.0694 0.1501 0.1243 0.0575 0.589 4.641 5.256 439.290 0.524 23.378 5.427 0.38 148503. 0.6083
|
|
9.47 0.1041 0.2175 0.1232 0.0590 0.604 4.762 5.210 450.737 0.538 23.172 5.242 0.38 148688. 0.5851
|
|
12.62 0.1388 0.2800 0.1219 0.0604 0.620 4.883 5.156 462.140 0.552 22.932 5.060 0.38 148895. 0.5618
|
|
15.78 0.1735 0.3376 0.1204 0.0619 0.635 5.000 5.093 473.254 0.565 22.653 4.881 0.38 149124. 0.5386
|
|
18.93 0.2083 0.3906 0.1187 0.0633 0.649 5.112 5.020 483.803 0.577 22.330 4.707 0.38 149377. 0.5157
|
|
22.09 0.2430 0.4394 0.1167 0.0646 0.662 5.214 4.937 493.491 0.589 21.959 4.537 0.38 149655. 0.4930
|
|
25.24 0.2777 0.4840 0.1145 0.0657 0.673 5.304 4.841 502.001 0.599 21.532 4.374 0.38 149958. 0.4706
|
|
28.40 0.3124 0.5249 0.1119 0.0666 0.683 5.378 4.732 509.006 0.608 21.047 4.216 0.38 150286. 0.4485
|
|
31.55 0.3471 0.5624 0.1090 0.0673 0.690 5.432 4.608 514.174 0.614 20.499 4.065 0.38 150640. 0.4267
|
|
34.71 0.3818 0.5965 0.1057 0.0676 0.694 5.464 4.470 517.166 0.617 19.882 3.920 0.38 151021. 0.4053
|
|
37.86 0.4165 0.6277 0.1020 0.0677 0.694 5.469 4.315 517.633 0.618 19.194 3.781 0.38 151428. 0.3841
|
|
41.02 0.4512 0.6560 0.0980 0.0674 0.691 5.444 4.144 515.230 0.615 18.431 3.648 0.38 151860. 0.3631
|
|
44.17 0.4859 0.6816 0.0935 0.0667 0.683 5.384 3.955 509.631 0.608 17.590 3.520 0.39 152319. 0.3422
|
|
47.33 0.5206 0.7047 0.0886 0.0655 0.671 5.289 3.749 500.597 0.598 16.674 3.396 0.39 152804. 0.3215
|
|
50.49 0.5553 0.7254 0.0834 0.0638 0.654 5.157 3.527 488.060 0.583 15.687 3.278 0.39 153314. 0.3010
|
|
53.64 0.5901 0.7437 0.0778 0.0618 0.633 4.988 3.292 472.106 0.564 14.641 3.162 0.39 153850. 0.2805
|
|
56.80 0.6248 0.7594 0.0720 0.0592 0.607 4.785 3.045 452.884 0.541 13.546 3.050 0.39 154410. 0.2603
|
|
59.95 0.6595 0.7725 0.0660 0.0563 0.577 4.549 2.790 430.538 0.514 12.410 2.939 0.39 154996. 0.2401
|
|
63.11 0.6942 0.7826 0.0598 0.0530 0.543 4.281 2.527 405.186 0.484 11.241 2.829 0.39 155606. 0.2199
|
|
66.26 0.7289 0.7893 0.0534 0.0493 0.505 3.982 2.258 376.923 0.450 10.044 2.717 0.39 156240. 0.1996
|
|
69.42 0.7636 0.7918 0.0469 0.0452 0.464 3.654 1.984 345.829 0.413 8.824 2.602 0.39 156898. 0.1792
|
|
72.57 0.7983 0.7888 0.0403 0.0408 0.418 3.296 1.705 311.976 0.372 7.585 2.479 0.39 157581. 0.1583
|
|
75.73 0.8330 0.7781 0.0337 0.0360 0.369 2.910 1.423 275.443 0.329 6.331 2.344 0.39 158287. 0.1367
|
|
78.88 0.8677 0.7561 0.0269 0.0309 0.317 2.497 1.139 236.321 0.282 5.067 2.186 0.40 159017. 0.1141
|
|
82.04 0.9024 0.7150 0.0202 0.0255 0.261 2.057 0.854 194.731 0.232 3.797 1.988 0.40 159770. 0.0898
|
|
85.19 0.9371 0.6377 0.0134 0.0197 0.202 1.594 0.568 150.831 0.180 2.525 1.707 0.40 160546. 0.0629
|
|
88.35 0.9718 0.4744 0.0067 0.0137 0.141 1.108 0.283 104.828 0.125 1.259 1.225 0.40 161344. 0.0319
|
|
91.51 1.0066 0.0018 0.0000 0.0074 0.076 0.601 0.001 56.901 0.068 0.003 0.005 0.40 162151. 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 0.1264 0.0544 0.794 5.561 6.765 592.089 0.628 30.091 5.182 0.43 166712. 0.6591
|
|
3.55 0.0347 0.0781 0.1256 0.0558 0.815 5.708 6.723 607.840 0.645 29.905 5.017 0.43 166875. 0.6361
|
|
7.10 0.0695 0.1511 0.1247 0.0573 0.837 5.861 6.674 624.129 0.662 29.688 4.850 0.43 167060. 0.6127
|
|
10.66 0.1042 0.2189 0.1236 0.0589 0.859 6.017 6.617 640.688 0.680 29.435 4.685 0.43 167268. 0.5893
|
|
14.21 0.1389 0.2816 0.1224 0.0604 0.881 6.172 6.551 657.208 0.697 29.139 4.521 0.43 167501. 0.5658
|
|
17.76 0.1737 0.3395 0.1209 0.0619 0.903 6.324 6.473 673.335 0.714 28.793 4.361 0.43 167759. 0.5425
|
|
21.31 0.2084 0.3928 0.1193 0.0633 0.924 6.468 6.383 688.668 0.731 28.392 4.204 0.43 168044. 0.5194
|
|
24.87 0.2431 0.4417 0.1173 0.0646 0.942 6.600 6.279 702.771 0.746 27.928 4.052 0.43 168357. 0.4965
|
|
28.42 0.2779 0.4866 0.1151 0.0657 0.959 6.717 6.159 715.188 0.759 27.394 3.906 0.43 168698. 0.4740
|
|
31.97 0.3126 0.5277 0.1125 0.0666 0.973 6.813 6.022 725.440 0.770 26.784 3.765 0.43 169068. 0.4518
|
|
35.52 0.3473 0.5652 0.1096 0.0673 0.983 6.884 5.866 733.045 0.778 26.093 3.630 0.43 169467. 0.4299
|
|
39.07 0.3821 0.5996 0.1063 0.0678 0.989 6.926 5.691 737.510 0.783 25.315 3.500 0.43 169896. 0.4083
|
|
42.63 0.4168 0.6309 0.1027 0.0678 0.990 6.934 5.496 738.333 0.783 24.445 3.376 0.43 170355. 0.3870
|
|
46.18 0.4515 0.6594 0.0986 0.0675 0.986 6.903 5.278 735.013 0.780 23.478 3.257 0.43 170843. 0.3659
|
|
49.73 0.4863 0.6853 0.0941 0.0668 0.975 6.828 5.038 727.081 0.771 22.411 3.143 0.43 171360. 0.3450
|
|
53.28 0.5210 0.7086 0.0892 0.0656 0.958 6.707 4.777 714.189 0.758 21.247 3.034 0.43 171906. 0.3242
|
|
56.84 0.5557 0.7296 0.0840 0.0640 0.934 6.539 4.495 696.234 0.739 19.992 2.928 0.44 172481. 0.3035
|
|
60.39 0.5905 0.7482 0.0784 0.0619 0.903 6.324 4.195 673.339 0.714 18.661 2.826 0.44 173085. 0.2830
|
|
63.94 0.6252 0.7643 0.0725 0.0593 0.866 6.064 3.882 645.721 0.685 17.267 2.727 0.44 173717. 0.2627
|
|
67.49 0.6599 0.7779 0.0664 0.0564 0.823 5.762 3.557 613.586 0.651 15.820 2.629 0.44 174377. 0.2424
|
|
71.04 0.6947 0.7886 0.0602 0.0530 0.774 5.420 3.222 577.108 0.612 14.330 2.532 0.44 175064. 0.2222
|
|
74.60 0.7294 0.7959 0.0538 0.0493 0.719 5.038 2.878 536.423 0.569 12.804 2.434 0.44 175779. 0.2019
|
|
78.15 0.7641 0.7993 0.0472 0.0452 0.659 4.617 2.529 491.647 0.522 11.248 2.333 0.44 176521. 0.1814
|
|
81.70 0.7988 0.7973 0.0406 0.0407 0.594 4.159 2.174 442.885 0.470 9.668 2.226 0.44 177290. 0.1605
|
|
85.25 0.8336 0.7880 0.0339 0.0359 0.523 3.665 1.814 390.249 0.414 8.069 2.108 0.44 178085. 0.1389
|
|
88.80 0.8683 0.7677 0.0271 0.0307 0.448 3.136 1.452 333.873 0.354 6.457 1.972 0.44 178908. 0.1162
|
|
92.36 0.9030 0.7289 0.0203 0.0252 0.367 2.573 1.087 273.930 0.291 4.836 1.800 0.45 179756. 0.0918
|
|
95.91 0.9378 0.6541 0.0135 0.0194 0.282 1.978 0.722 210.649 0.224 3.214 1.556 0.45 180630. 0.0647
|
|
99.46 0.9725 0.4922 0.0067 0.0133 0.194 1.355 0.359 144.332 0.153 1.598 1.129 0.45 181529. 0.0331
|
|
103.01 1.0072 -0.0037 0.0000 0.0069 0.101 0.706 -0.001 75.223 0.080 -0.006 -0.008 0.45 182436. 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 0.1268 0.0543 1.088 6.858 8.378 811.440 0.775 37.263 4.683 0.48 185228. 0.6627
|
|
3.95 0.0347 0.0785 0.1260 0.0558 1.118 7.044 8.328 833.334 0.796 37.044 4.533 0.48 185410. 0.6396
|
|
7.90 0.0695 0.1517 0.1252 0.0573 1.148 7.235 8.270 856.019 0.817 36.787 4.382 0.48 185615. 0.6162
|
|
11.85 0.1042 0.2198 0.1241 0.0589 1.179 7.431 8.203 879.119 0.839 36.485 4.232 0.48 185846. 0.5927
|
|
15.79 0.1390 0.2828 0.1229 0.0604 1.210 7.626 8.123 902.210 0.862 36.131 4.084 0.48 186104. 0.5691
|
|
19.74 0.1737 0.3409 0.1215 0.0619 1.240 7.817 8.030 924.787 0.883 35.716 3.938 0.48 186391. 0.5457
|
|
23.69 0.2085 0.3943 0.1199 0.0634 1.269 7.998 7.921 946.292 0.904 35.231 3.796 0.48 186708. 0.5224
|
|
27.64 0.2432 0.4434 0.1179 0.0647 1.296 8.166 7.794 966.112 0.923 34.668 3.659 0.48 187056. 0.4995
|
|
31.59 0.2780 0.4884 0.1157 0.0659 1.319 8.314 7.648 983.602 0.939 34.017 3.527 0.48 187435. 0.4769
|
|
35.54 0.3127 0.5296 0.1132 0.0668 1.338 8.436 7.480 998.091 0.953 33.272 3.399 0.48 187847. 0.4546
|
|
39.49 0.3475 0.5673 0.1103 0.0676 1.353 8.527 7.290 1008.900 0.963 32.424 3.277 0.48 188291. 0.4327
|
|
43.44 0.3822 0.6018 0.1071 0.0680 1.362 8.582 7.074 1015.340 0.970 31.467 3.160 0.48 188769. 0.4110
|
|
47.38 0.4170 0.6333 0.1034 0.0681 1.363 8.593 6.833 1016.712 0.971 30.394 3.048 0.48 189279. 0.3896
|
|
51.33 0.4517 0.6619 0.0993 0.0678 1.358 8.556 6.565 1012.318 0.967 29.200 2.941 0.48 189822. 0.3685
|
|
55.28 0.4865 0.6880 0.0949 0.0671 1.343 8.465 6.268 1001.504 0.956 27.880 2.839 0.48 190398. 0.3475
|
|
59.23 0.5212 0.7116 0.0899 0.0659 1.319 8.315 5.944 983.783 0.939 26.438 2.740 0.48 191006. 0.3267
|
|
63.18 0.5560 0.7328 0.0847 0.0642 1.286 8.106 5.594 959.004 0.916 24.882 2.646 0.48 191646. 0.3060
|
|
67.13 0.5907 0.7517 0.0790 0.0621 1.244 7.838 5.222 927.338 0.886 23.229 2.554 0.48 192318. 0.2854
|
|
71.08 0.6255 0.7682 0.0731 0.0595 1.192 7.515 4.833 889.085 0.849 21.496 2.465 0.49 193021. 0.2650
|
|
75.03 0.6602 0.7822 0.0670 0.0566 1.133 7.138 4.428 844.539 0.806 19.697 2.378 0.49 193756. 0.2447
|
|
78.97 0.6950 0.7935 0.0607 0.0532 1.065 6.711 4.012 793.942 0.758 17.844 2.292 0.49 194520. 0.2244
|
|
82.92 0.7297 0.8015 0.0542 0.0494 0.989 6.233 3.585 737.485 0.704 15.945 2.205 0.49 195316. 0.2041
|
|
86.87 0.7645 0.8056 0.0477 0.0452 0.906 5.708 3.149 675.330 0.645 14.009 2.115 0.49 196141. 0.1836
|
|
90.82 0.7992 0.8046 0.0410 0.0407 0.815 5.136 2.707 607.624 0.580 12.042 2.021 0.49 196997. 0.1626
|
|
94.77 0.8340 0.7966 0.0342 0.0358 0.717 4.518 2.260 534.522 0.510 10.051 1.917 0.49 197882. 0.1409
|
|
98.72 0.8687 0.7779 0.0274 0.0306 0.612 3.856 1.808 456.212 0.436 8.042 1.798 0.49 198796. 0.1182
|
|
102.67 0.9035 0.7412 0.0205 0.0250 0.500 3.152 1.354 372.932 0.356 6.023 1.647 0.50 199740. 0.0937
|
|
106.62 0.9382 0.6692 0.0136 0.0191 0.382 2.409 0.900 285.004 0.272 4.002 1.432 0.50 200712. 0.0664
|
|
110.56 0.9730 0.5094 0.0068 0.0129 0.259 1.630 0.447 192.849 0.184 1.988 1.051 0.50 201712. 0.0344
|
|
114.51 1.0077 -0.0062 0.0000 0.0065 0.130 0.818 -0.003 96.787 0.092 -0.012 -0.012 0.50 202719. 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 0.1272 0.0544 1.450 8.306 10.170 1080.931 0.938 45.237 4.268 0.52 203742. 0.6655
|
|
4.35 0.0348 0.0787 0.1265 0.0559 1.489 8.533 10.114 1110.485 0.964 44.985 4.131 0.52 203942. 0.6424
|
|
8.69 0.0695 0.1521 0.1257 0.0574 1.530 8.769 10.047 1141.172 0.991 44.689 3.993 0.52 204167. 0.6189
|
|
13.04 0.1043 0.2204 0.1247 0.0590 1.572 9.009 9.969 1172.491 1.018 44.340 3.856 0.52 204421. 0.5953
|
|
17.38 0.1390 0.2835 0.1235 0.0606 1.614 9.250 9.876 1203.859 1.045 43.928 3.721 0.52 204705. 0.5718
|
|
21.73 0.1738 0.3418 0.1221 0.0621 1.656 9.486 9.767 1234.594 1.072 43.442 3.588 0.52 205021. 0.5483
|
|
26.07 0.2086 0.3953 0.1205 0.0636 1.695 9.712 9.638 1263.926 1.097 42.870 3.459 0.52 205369. 0.5250
|
|
30.42 0.2433 0.4445 0.1187 0.0650 1.731 9.920 9.488 1291.019 1.121 42.203 3.333 0.53 205752. 0.5021
|
|
34.76 0.2781 0.4896 0.1165 0.0662 1.763 10.104 9.314 1314.988 1.142 41.429 3.213 0.53 206169. 0.4794
|
|
39.11 0.3129 0.5309 0.1140 0.0672 1.790 10.257 9.114 1334.916 1.159 40.538 3.097 0.53 206623. 0.4571
|
|
43.45 0.3476 0.5687 0.1111 0.0679 1.810 10.372 8.885 1349.873 1.172 39.520 2.985 0.53 207113. 0.4351
|
|
47.80 0.3824 0.6033 0.1079 0.0684 1.822 10.442 8.626 1358.920 1.180 38.368 2.879 0.53 207639. 0.4135
|
|
52.14 0.4171 0.6349 0.1042 0.0685 1.825 10.459 8.335 1361.111 1.182 37.073 2.777 0.53 208201. 0.3921
|
|
56.49 0.4519 0.6637 0.1002 0.0682 1.818 10.415 8.010 1355.499 1.177 35.628 2.680 0.53 208800. 0.3709
|
|
60.83 0.4867 0.6900 0.0957 0.0675 1.799 10.306 7.650 1341.203 1.164 34.028 2.587 0.53 209434. 0.3499
|
|
65.18 0.5214 0.7138 0.0907 0.0663 1.767 10.124 7.256 1317.558 1.144 32.276 2.498 0.53 210104. 0.3290
|
|
69.52 0.5562 0.7353 0.0854 0.0646 1.722 9.869 6.831 1284.351 1.115 30.383 2.412 0.53 210810. 0.3083
|
|
73.87 0.5910 0.7545 0.0798 0.0625 1.665 9.542 6.378 1241.811 1.078 28.371 2.330 0.53 211550. 0.2877
|
|
78.22 0.6257 0.7713 0.0738 0.0599 1.596 9.146 5.904 1190.344 1.033 26.259 2.250 0.53 212325. 0.2673
|
|
82.56 0.6605 0.7858 0.0677 0.0569 1.516 8.685 5.410 1130.356 0.981 24.066 2.171 0.54 213134. 0.2469
|
|
86.91 0.6952 0.7975 0.0613 0.0534 1.424 8.162 4.902 1062.179 0.922 21.804 2.093 0.54 213976. 0.2266
|
|
91.25 0.7300 0.8061 0.0548 0.0496 1.322 7.577 4.381 986.077 0.856 19.487 2.015 0.54 214852. 0.2062
|
|
95.60 0.7648 0.8110 0.0481 0.0454 1.210 6.933 3.849 902.267 0.783 17.122 1.935 0.54 215762. 0.1856
|
|
99.94 0.7995 0.8110 0.0414 0.0408 1.087 6.231 3.309 810.948 0.704 14.720 1.851 0.54 216704. 0.1646
|
|
104.29 0.8343 0.8042 0.0345 0.0358 0.955 5.473 2.762 712.331 0.618 12.287 1.759 0.54 217678. 0.1429
|
|
108.63 0.8691 0.7870 0.0276 0.0305 0.814 4.662 2.210 606.668 0.527 9.832 1.653 0.54 218685. 0.1201
|
|
112.98 0.9038 0.7523 0.0207 0.0249 0.663 3.798 1.655 494.282 0.429 7.363 1.519 0.54 219725. 0.0956
|
|
117.32 0.9386 0.6829 0.0138 0.0189 0.504 2.886 1.100 375.608 0.326 4.891 1.328 0.55 220795. 0.0681
|
|
121.67 0.9733 0.5255 0.0068 0.0126 0.337 1.930 0.546 251.217 0.218 2.427 0.985 0.55 221896. 0.0356
|
|
126.01 1.0081 -0.0091 -0.0001 0.0061 0.163 0.934 -0.004 121.514 0.105 -0.020 -0.016 0.55 223001. 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 0.1276 0.0545 1.886 9.908 12.146 1406.730 1.119 54.024 3.916 0.57 222254. 0.6673
|
|
4.76 0.0349 0.0792 0.1270 0.0560 1.939 10.184 12.082 1445.857 1.151 53.742 3.790 0.57 222472. 0.6442
|
|
9.53 0.0699 0.1530 0.1262 0.0576 1.994 10.471 12.007 1486.594 1.183 53.409 3.664 0.57 222719. 0.6207
|
|
14.29 0.1048 0.2216 0.1252 0.0592 2.049 10.764 11.918 1528.275 1.216 53.012 3.537 0.57 222997. 0.5971
|
|
19.06 0.1397 0.2851 0.1241 0.0609 2.106 11.059 11.812 1570.113 1.249 52.541 3.412 0.57 223309. 0.5734
|
|
23.82 0.1747 0.3435 0.1228 0.0624 2.161 11.348 11.686 1611.186 1.282 51.980 3.290 0.57 223655. 0.5499
|
|
28.58 0.2096 0.3973 0.1212 0.0640 2.213 11.625 11.537 1650.444 1.313 51.316 3.171 0.57 224038. 0.5266
|
|
33.35 0.2445 0.4466 0.1194 0.0654 2.262 11.881 11.361 1686.741 1.342 50.535 3.055 0.57 224458. 0.5035
|
|
38.11 0.2795 0.4918 0.1172 0.0666 2.305 12.107 11.156 1718.875 1.368 49.623 2.944 0.57 224918. 0.4808
|
|
42.87 0.3144 0.5333 0.1147 0.0677 2.341 12.295 10.919 1745.599 1.389 48.568 2.837 0.57 225417. 0.4584
|
|
47.64 0.3493 0.5712 0.1119 0.0684 2.368 12.436 10.647 1765.649 1.405 47.357 2.735 0.57 225956. 0.4364
|
|
52.40 0.3843 0.6059 0.1086 0.0689 2.384 12.522 10.337 1777.757 1.415 45.981 2.637 0.58 226535. 0.4146
|
|
57.17 0.4192 0.6376 0.1050 0.0690 2.388 12.542 9.988 1780.645 1.417 44.428 2.544 0.58 227155. 0.3932
|
|
61.93 0.4541 0.6666 0.1009 0.0687 2.378 12.489 9.598 1773.052 1.411 42.690 2.455 0.58 227815. 0.3719
|
|
66.69 0.4891 0.6929 0.0963 0.0680 2.352 12.353 9.164 1753.804 1.396 40.762 2.370 0.58 228514. 0.3508
|
|
71.46 0.5240 0.7169 0.0913 0.0667 2.309 12.129 8.689 1722.035 1.370 38.647 2.289 0.58 229252. 0.3298
|
|
76.22 0.5590 0.7386 0.0859 0.0650 2.250 11.815 8.175 1677.493 1.335 36.361 2.210 0.58 230029. 0.3090
|
|
80.98 0.5939 0.7580 0.0802 0.0628 2.173 11.414 7.628 1620.508 1.290 33.929 2.135 0.58 230845. 0.2883
|
|
85.75 0.6288 0.7751 0.0741 0.0601 2.081 10.929 7.054 1551.640 1.235 31.375 2.062 0.58 231699. 0.2678
|
|
90.51 0.6638 0.7898 0.0679 0.0570 1.973 10.364 6.457 1471.434 1.171 28.722 1.990 0.58 232590. 0.2473
|
|
95.28 0.6987 0.8018 0.0614 0.0535 1.851 9.722 5.842 1380.341 1.098 25.987 1.920 0.59 233518. 0.2269
|
|
100.04 0.7336 0.8108 0.0548 0.0496 1.715 9.007 5.212 1278.707 1.018 23.183 1.849 0.59 234483. 0.2064
|
|
104.80 0.7686 0.8160 0.0480 0.0452 1.565 8.219 4.569 1166.823 0.929 20.322 1.776 0.59 235484. 0.1856
|
|
109.57 0.8035 0.8163 0.0411 0.0405 1.401 7.360 3.915 1044.955 0.832 17.414 1.699 0.59 236522. 0.1644
|
|
114.33 0.8384 0.8097 0.0342 0.0354 1.225 6.434 3.253 913.392 0.727 14.470 1.615 0.59 237595. 0.1425
|
|
119.09 0.8734 0.7924 0.0272 0.0299 1.036 5.441 2.585 772.475 0.615 11.498 1.518 0.59 238704. 0.1193
|
|
123.86 0.9083 0.7567 0.0201 0.0241 0.835 4.386 1.913 622.650 0.495 8.510 1.394 0.59 239847. 0.0943
|
|
128.62 0.9432 0.6831 0.0130 0.0180 0.623 3.272 1.241 464.521 0.370 5.518 1.211 0.60 241026. 0.0660
|
|
133.39 0.9782 0.5065 0.0060 0.0116 0.401 2.105 0.571 298.878 0.238 2.539 0.866 0.60 242237. 0.0320
|
|
138.15 1.0131
|
|
|
|
|
|
|
|
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 0.1281 0.0547 2.408 11.677 14.307 1795.938 1.319 63.636 3.613 0.62 240764. 0.6683
|
|
5.14 0.0348 0.0788 0.1275 0.0563 2.476 12.003 14.238 1846.081 1.356 63.332 3.498 0.62 240998. 0.6455
|
|
10.27 0.0695 0.1523 0.1268 0.0579 2.546 12.343 14.157 1898.462 1.395 62.971 3.382 0.62 241263. 0.6223
|
|
15.41 0.1043 0.2207 0.1259 0.0595 2.618 12.693 14.060 1952.246 1.434 62.539 3.267 0.62 241561. 0.5989
|
|
20.54 0.1391 0.2839 0.1249 0.0612 2.691 13.045 13.944 2006.439 1.474 62.021 3.152 0.62 241896. 0.5755
|
|
25.68 0.1738 0.3422 0.1236 0.0628 2.762 13.393 13.804 2059.846 1.513 61.400 3.040 0.62 242268. 0.5522
|
|
30.82 0.2086 0.3958 0.1221 0.0644 2.831 13.726 13.637 2111.113 1.551 60.659 2.930 0.62 242679. 0.5291
|
|
35.95 0.2434 0.4451 0.1203 0.0658 2.895 14.036 13.440 2158.741 1.586 59.781 2.824 0.62 243131. 0.5062
|
|
41.09 0.2781 0.4902 0.1183 0.0671 2.952 14.311 13.208 2201.155 1.617 58.749 2.722 0.62 243625. 0.4836
|
|
46.22 0.3129 0.5316 0.1158 0.0682 2.999 14.543 12.938 2236.726 1.643 57.547 2.624 0.62 244162. 0.4614
|
|
51.36 0.3477 0.5696 0.1131 0.0690 3.036 14.719 12.626 2263.815 1.663 56.162 2.530 0.62 244741. 0.4395
|
|
56.50 0.3824 0.6044 0.1099 0.0695 3.059 14.829 12.270 2280.782 1.675 54.578 2.440 0.62 245364. 0.4180
|
|
61.63 0.4172 0.6362 0.1063 0.0697 3.066 14.863 11.867 2285.991 1.679 52.786 2.355 0.62 246031. 0.3966
|
|
66.77 0.4520 0.6653 0.1022 0.0694 3.055 14.810 11.415 2277.820 1.673 50.774 2.273 0.63 246740. 0.3755
|
|
71.90 0.4867 0.6919 0.0977 0.0687 3.024 14.660 10.912 2254.769 1.656 48.535 2.195 0.63 247493. 0.3545
|
|
77.04 0.5215 0.7161 0.0927 0.0675 2.971 14.406 10.358 2215.678 1.628 46.072 2.120 0.63 248287. 0.3337
|
|
82.18 0.5563 0.7381 0.0874 0.0658 2.897 14.045 9.758 2160.144 1.587 43.402 2.049 0.63 249123. 0.3129
|
|
87.31 0.5910 0.7579 0.0816 0.0637 2.801 13.579 9.117 2088.542 1.534 40.555 1.980 0.63 250000. 0.2923
|
|
92.45 0.6258 0.7755 0.0756 0.0610 2.684 13.014 8.444 2001.589 1.470 37.559 1.913 0.63 250918. 0.2719
|
|
97.58 0.6606 0.7908 0.0693 0.0579 2.548 12.353 7.743 1900.006 1.396 34.441 1.848 0.63 251876. 0.2515
|
|
102.72 0.6953 0.8035 0.0629 0.0544 2.393 11.602 7.020 1784.396 1.311 31.223 1.784 0.63 252874. 0.2312
|
|
107.86 0.7301 0.8133 0.0562 0.0505 2.220 10.762 6.277 1655.223 1.216 27.921 1.720 0.64 253912. 0.2107
|
|
112.99 0.7649 0.8196 0.0494 0.0461 2.029 9.836 5.519 1512.865 1.111 24.548 1.655 0.64 254988. 0.1901
|
|
118.13 0.7996 0.8214 0.0425 0.0414 1.821 8.827 4.748 1357.668 0.997 21.118 1.586 0.64 256103. 0.1690
|
|
123.26 0.8344 0.8169 0.0355 0.0363 1.596 7.737 3.966 1189.988 0.874 17.641 1.512 0.64 257257. 0.1472
|
|
128.40 0.8692 0.8028 0.0284 0.0308 1.355 6.568 3.177 1010.251 0.742 14.130 1.426 0.64 258448. 0.1243
|
|
133.53 0.9039 0.7723 0.0213 0.0250 1.098 5.325 2.382 819.003 0.602 10.595 1.319 0.64 259677. 0.0996
|
|
138.67 0.9387 0.7087 0.0142 0.0188 0.827 4.011 1.586 616.982 0.453 7.054 1.166 0.65 260943. 0.0718
|
|
143.81 0.9735 0.5587 0.0071 0.0124 0.543 2.634 0.792 405.168 0.298 3.521 0.886 0.65 262244. 0.0386
|
|
148.94 1.0082 0.0038 0.0000 0.0056 0.247 1.198 0.002 184.243 0.135 0.010 0.006 0.65 263549. 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 0.1286 0.0552 3.035 13.662 16.655 2262.927 1.544 74.081 3.338 0.67 259271. 0.6661
|
|
5.53 0.0348 0.0784 0.1280 0.0568 3.119 14.041 16.583 2325.779 1.586 73.760 3.234 0.67 259522. 0.6439
|
|
11.07 0.0696 0.1518 0.1274 0.0584 3.207 14.439 16.497 2391.639 1.631 73.378 3.129 0.67 259806. 0.6213
|
|
16.60 0.1043 0.2200 0.1266 0.0600 3.298 14.849 16.393 2459.476 1.678 72.917 3.023 0.67 260127. 0.5985
|
|
22.13 0.1391 0.2832 0.1256 0.0617 3.390 15.263 16.268 2528.058 1.724 72.359 2.919 0.67 260486. 0.5756
|
|
27.67 0.1739 0.3415 0.1244 0.0634 3.481 15.672 16.116 2595.882 1.771 71.682 2.816 0.67 260886. 0.5527
|
|
33.20 0.2087 0.3952 0.1230 0.0650 3.569 16.067 15.932 2661.230 1.815 70.866 2.715 0.67 261328. 0.5300
|
|
38.73 0.2435 0.4445 0.1213 0.0664 3.651 16.435 15.712 2722.208 1.857 69.889 2.618 0.67 261815. 0.5074
|
|
44.27 0.2782 0.4898 0.1193 0.0678 3.724 16.764 15.452 2776.802 1.894 68.730 2.524 0.67 262347. 0.4851
|
|
49.80 0.3130 0.5313 0.1169 0.0689 3.786 17.043 15.146 2822.899 1.925 67.369 2.434 0.67 262926. 0.4631
|
|
55.33 0.3478 0.5693 0.1142 0.0698 3.833 17.257 14.791 2858.355 1.950 65.789 2.347 0.67 263551. 0.4414
|
|
60.87 0.3826 0.6042 0.1110 0.0703 3.864 17.394 14.382 2881.012 1.965 63.973 2.264 0.67 264223. 0.4199
|
|
66.40 0.4174 0.6361 0.1075 0.0705 3.874 17.440 13.918 2888.696 1.970 61.907 2.185 0.67 264943. 0.3986
|
|
71.93 0.4521 0.6654 0.1034 0.0703 3.861 17.383 13.394 2879.287 1.964 59.578 2.110 0.67 265708. 0.3776
|
|
77.47 0.4869 0.6921 0.0989 0.0696 3.823 17.211 12.810 2850.829 1.945 56.979 2.038 0.67 266520. 0.3567
|
|
83.00 0.5217 0.7166 0.0939 0.0684 3.757 16.916 12.165 2801.842 1.911 54.111 1.969 0.68 267378. 0.3359
|
|
88.53 0.5565 0.7388 0.0885 0.0667 3.663 16.493 11.465 2731.792 1.863 50.995 1.904 0.68 268281. 0.3152
|
|
94.07 0.5913 0.7589 0.0827 0.0645 3.542 15.945 10.716 2641.154 1.802 47.664 1.840 0.68 269228. 0.2946
|
|
99.60 0.6260 0.7768 0.0766 0.0618 3.394 15.280 9.927 2530.858 1.726 44.156 1.779 0.68 270218. 0.2741
|
|
105.13 0.6608 0.7925 0.0703 0.0586 3.221 14.501 9.105 2401.859 1.638 40.501 1.719 0.68 271252. 0.2537
|
|
110.67 0.6956 0.8057 0.0637 0.0550 3.024 13.614 8.256 2254.947 1.538 36.724 1.661 0.68 272329. 0.2333
|
|
116.20 0.7304 0.8161 0.0570 0.0510 2.804 12.622 7.385 2090.729 1.426 32.846 1.602 0.68 273448. 0.2129
|
|
121.73 0.7652 0.8231 0.0501 0.0466 2.561 11.529 6.494 1909.693 1.303 28.884 1.542 0.69 274609. 0.1922
|
|
127.27 0.8000 0.8257 0.0431 0.0418 2.296 10.338 5.587 1712.277 1.168 24.851 1.480 0.69 275812. 0.1710
|
|
132.80 0.8347 0.8222 0.0360 0.0366 2.010 9.050 4.667 1498.941 1.022 20.761 1.412 0.69 277056. 0.1492
|
|
138.33 0.8695 0.8095 0.0289 0.0310 1.703 7.669 3.738 1270.225 0.866 16.627 1.335 0.69 278340. 0.1262
|
|
143.86 0.9043 0.7807 0.0216 0.0251 1.377 6.199 2.802 1026.844 0.700 12.465 1.238 0.69 279665. 0.1013
|
|
149.40 0.9391 0.7193 0.0144 0.0188 1.032 4.648 1.864 769.818 0.525 8.291 1.098 0.70 281030. 0.0733
|
|
154.93 0.9739 0.5711 0.0072 0.0122 0.671 3.022 0.928 500.561 0.341 4.127 0.841 0.70 282433. 0.0396
|
|
160.46 1.0086 -0.0052 0.0000 0.0054 0.295 1.329 -0.004 220.115 0.150 -0.016 -0.007 0.70 283834. 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 0.1291 0.0564 3.808 16.002 19.189 2839.801 1.808 85.351 3.065 0.71 277775. 0.6565
|
|
5.93 0.0348 0.0773 0.1286 0.0579 3.911 16.434 19.115 2916.566 1.857 85.025 2.973 0.71 278042. 0.6355
|
|
11.86 0.0696 0.1497 0.1280 0.0595 4.019 16.888 19.027 2997.142 1.908 84.633 2.879 0.71 278345. 0.6142
|
|
17.79 0.1043 0.2172 0.1273 0.0611 4.131 17.357 18.920 3080.239 1.961 84.157 2.786 0.71 278688. 0.5926
|
|
23.72 0.1391 0.2800 0.1264 0.0628 4.243 17.830 18.789 3164.297 2.014 83.574 2.693 0.71 279071. 0.5708
|
|
29.64 0.1739 0.3381 0.1253 0.0644 4.355 18.299 18.628 3247.437 2.067 82.858 2.602 0.72 279498. 0.5491
|
|
35.57 0.2087 0.3918 0.1240 0.0660 4.462 18.750 18.431 3327.507 2.118 81.983 2.512 0.72 279971. 0.5274
|
|
41.50 0.2435 0.4413 0.1224 0.0675 4.562 19.171 18.193 3402.171 2.166 80.922 2.425 0.72 280492. 0.5058
|
|
47.43 0.2783 0.4868 0.1204 0.0688 4.652 19.547 17.906 3468.943 2.208 79.648 2.341 0.72 281062. 0.4844
|
|
53.36 0.3130 0.5287 0.1181 0.0700 4.727 19.864 17.567 3525.281 2.244 78.136 2.260 0.72 281682. 0.4632
|
|
59.29 0.3478 0.5672 0.1155 0.0708 4.786 20.108 17.168 3568.589 2.272 76.365 2.182 0.72 282353. 0.4421
|
|
65.22 0.3826 0.6025 0.1124 0.0714 4.823 20.264 16.707 3596.251 2.289 74.315 2.107 0.72 283074. 0.4212
|
|
71.15 0.4174 0.6348 0.1088 0.0715 4.835 20.317 16.180 3605.595 2.295 71.967 2.035 0.72 283846. 0.4003
|
|
77.08 0.4522 0.6645 0.1048 0.0713 4.820 20.251 15.582 3593.951 2.288 69.307 1.966 0.72 284668. 0.3796
|
|
83.01 0.4870 0.6916 0.1003 0.0706 4.772 20.053 14.911 3558.789 2.266 66.324 1.900 0.72 285540. 0.3588
|
|
88.93 0.5217 0.7163 0.0953 0.0694 4.691 19.711 14.169 3498.096 2.227 63.023 1.837 0.72 286461. 0.3381
|
|
94.86 0.5565 0.7388 0.0899 0.0677 4.574 19.220 13.360 3411.016 2.172 59.424 1.776 0.73 287430. 0.3175
|
|
100.79 0.5913 0.7592 0.0840 0.0654 4.423 18.584 12.493 3297.986 2.100 55.569 1.718 0.73 288446. 0.2969
|
|
106.72 0.6261 0.7775 0.0779 0.0627 4.238 17.807 11.578 3160.128 2.012 51.500 1.662 0.73 289510. 0.2765
|
|
112.65 0.6609 0.7936 0.0715 0.0595 4.021 16.897 10.624 2998.658 1.909 47.255 1.607 0.73 290620. 0.2561
|
|
118.58 0.6957 0.8073 0.0648 0.0559 3.774 15.860 9.637 2814.607 1.792 42.865 1.553 0.73 291775. 0.2357
|
|
124.51 0.7304 0.8183 0.0580 0.0518 3.498 14.700 8.622 2608.781 1.661 38.353 1.499 0.73 292976. 0.2152
|
|
130.44 0.7652 0.8260 0.0510 0.0473 3.194 13.421 7.585 2381.793 1.516 33.739 1.444 0.73 294221. 0.1945
|
|
136.37 0.8000 0.8295 0.0439 0.0423 2.862 12.026 6.528 2134.213 1.359 29.039 1.387 0.74 295511. 0.1733
|
|
142.29 0.8348 0.8270 0.0367 0.0370 2.503 10.519 5.456 1866.710 1.188 24.269 1.326 0.74 296845. 0.1514
|
|
148.22 0.8696 0.8154 0.0294 0.0314 2.119 8.904 4.372 1580.133 1.006 19.445 1.255 0.74 298223. 0.1283
|
|
154.15 0.9044 0.7878 0.0221 0.0253 1.711 7.188 3.279 1275.665 0.812 14.583 1.166 0.74 299643. 0.1032
|
|
160.08 0.9391 0.7272 0.0147 0.0189 1.281 5.381 2.182 954.969 0.608 9.704 1.036 0.75 301106. 0.0748
|
|
166.01 0.9739 0.5779 0.0073 0.0123 0.832 3.495 1.086 620.303 0.395 4.831 0.794 0.75 302609. 0.0405
|
|
171.94 1.0087 -0.0071 0.0000 0.0054 0.367 1.541 -0.006 273.502 0.174 -0.025 -0.009 0.75 304108. 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 0.1295 0.0586 4.808 18.940 21.904 3585.323 2.140 97.431 2.771 0.76 296276. 0.6342
|
|
6.32 0.0348 0.0746 0.1291 0.0601 4.931 19.426 21.832 3677.319 2.195 97.107 2.693 0.76 296560. 0.6152
|
|
12.65 0.0696 0.1449 0.1285 0.0617 5.061 19.937 21.744 3773.959 2.252 96.718 2.613 0.76 296881. 0.5959
|
|
18.97 0.1043 0.2107 0.1279 0.0633 5.195 20.463 21.637 3873.564 2.312 96.243 2.534 0.76 297244. 0.5763
|
|
25.29 0.1391 0.2721 0.1271 0.0650 5.329 20.994 21.505 3974.072 2.372 95.654 2.454 0.76 297651. 0.5565
|
|
31.61 0.1739 0.3294 0.1261 0.0666 5.462 21.516 21.340 4073.014 2.431 94.922 2.376 0.76 298105. 0.5368
|
|
37.94 0.2087 0.3826 0.1249 0.0681 5.589 22.016 21.136 4167.604 2.487 94.012 2.300 0.76 298608. 0.5171
|
|
44.26 0.2434 0.4320 0.1234 0.0696 5.706 22.477 20.884 4254.873 2.539 92.890 2.226 0.76 299162. 0.4975
|
|
50.58 0.2782 0.4778 0.1216 0.0708 5.809 22.883 20.576 4331.788 2.585 91.524 2.155 0.76 299769. 0.4779
|
|
56.91 0.3130 0.5202 0.1194 0.0719 5.894 23.219 20.207 4395.327 2.623 89.881 2.085 0.77 300430. 0.4583
|
|
63.23 0.3478 0.5595 0.1169 0.0726 5.958 23.468 19.769 4442.528 2.651 87.934 2.018 0.77 301145. 0.4388
|
|
69.55 0.3825 0.5958 0.1138 0.0731 5.995 23.616 19.258 4470.458 2.668 85.658 1.954 0.77 301915. 0.4193
|
|
75.87 0.4173 0.6292 0.1103 0.0732 6.003 23.646 18.667 4476.140 2.671 83.030 1.892 0.77 302740. 0.3996
|
|
82.20 0.4521 0.6599 0.1064 0.0729 5.976 23.542 17.993 4456.516 2.660 80.033 1.831 0.77 303618. 0.3798
|
|
88.52 0.4869 0.6880 0.1019 0.0721 5.912 23.289 17.233 4408.639 2.631 76.654 1.773 0.77 304550. 0.3599
|
|
94.84 0.5216 0.7138 0.0969 0.0708 5.807 22.874 16.388 4330.115 2.584 72.895 1.717 0.77 305534. 0.3398
|
|
101.17 0.5564 0.7371 0.0914 0.0690 5.659 22.292 15.463 4219.863 2.519 68.782 1.662 0.77 306569. 0.3196
|
|
107.49 0.5912 0.7583 0.0855 0.0667 5.469 21.544 14.470 4078.329 2.434 64.361 1.609 0.77 307655. 0.2993
|
|
113.81 0.6260 0.7773 0.0793 0.0639 5.239 20.638 13.418 3906.714 2.332 59.683 1.558 0.78 308792. 0.2790
|
|
120.13 0.6607 0.7940 0.0728 0.0606 4.970 19.579 12.319 3706.321 2.212 54.793 1.508 0.78 309977. 0.2587
|
|
126.46 0.6955 0.8082 0.0661 0.0569 4.664 18.374 11.180 3478.224 2.076 49.729 1.458 0.78 311211. 0.2384
|
|
132.78 0.7303 0.8198 0.0592 0.0527 4.323 17.028 10.009 3223.316 1.924 44.519 1.408 0.78 312493. 0.2179
|
|
139.10 0.7651 0.8282 0.0521 0.0481 3.946 15.544 8.810 2942.390 1.756 39.186 1.358 0.78 313823. 0.1971
|
|
145.43 0.7998 0.8322 0.0449 0.0431 3.535 13.927 7.587 2636.360 1.573 33.748 1.305 0.79 315200. 0.1758
|
|
151.75 0.8346 0.8301 0.0375 0.0377 3.093 12.184 6.345 2306.453 1.377 28.224 1.248 0.79 316624. 0.1537
|
|
158.07 0.8694 0.8183 0.0301 0.0320 2.621 10.324 5.088 1954.291 1.166 22.630 1.181 0.79 318093. 0.1302
|
|
164.39 0.9042 0.7890 0.0226 0.0259 2.122 8.357 3.819 1582.006 0.944 16.985 1.095 0.79 319609. 0.1046
|
|
170.72 0.9389 0.7239 0.0150 0.0195 1.599 6.299 2.543 1192.442 0.712 11.312 0.967 0.79 321170. 0.0754
|
|
177.04 0.9737 0.5650 0.0075 0.0129 1.058 4.169 1.267 789.238 0.471 5.635 0.728 0.80 322773. 0.0401
|
|
183.36 1.0085 -0.0067 0.0000 0.0061 0.504 1.985 -0.007 375.674 0.224 -0.031 -0.008 0.80 324374. 0.0000
|
|
|
|
|
|
|