686 lines
122 KiB
Plaintext
686 lines
122 KiB
Plaintext
13x13N (13x13N.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 0.1044 0.0613 0.002 0.115 0.095 1.365 0.013 0.423 31.560 0.05 17055. 0.4391
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0.48 0.0393 0.0654 0.1041 0.0625 0.002 0.118 0.095 1.393 0.013 0.421 30.849 0.05 17072. 0.4285
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0.97 0.0786 0.1276 0.1037 0.0639 0.002 0.120 0.094 1.423 0.014 0.420 30.093 0.05 17091. 0.4174
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1.45 0.1178 0.1863 0.1034 0.0654 0.002 0.123 0.094 1.456 0.014 0.418 29.301 0.05 17114. 0.4056
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1.93 0.1571 0.2415 0.1029 0.0670 0.002 0.126 0.094 1.492 0.014 0.417 28.478 0.05 17139. 0.3934
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2.42 0.1964 0.2929 0.1024 0.0686 0.002 0.129 0.093 1.530 0.015 0.414 27.633 0.05 17168. 0.3807
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2.90 0.2357 0.3405 0.1017 0.0704 0.002 0.133 0.093 1.569 0.015 0.412 26.773 0.05 17201. 0.3677
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3.38 0.2749 0.3844 0.1009 0.0722 0.002 0.136 0.092 1.608 0.015 0.409 25.906 0.05 17237. 0.3544
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3.87 0.3142 0.4246 0.0999 0.0739 0.002 0.139 0.091 1.647 0.016 0.405 25.041 0.05 17276. 0.3409
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4.35 0.3535 0.4613 0.0987 0.0756 0.002 0.142 0.090 1.685 0.016 0.400 24.183 0.05 17320. 0.3271
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4.84 0.3928 0.4947 0.0971 0.0771 0.002 0.145 0.088 1.719 0.016 0.393 23.337 0.05 17368. 0.3132
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5.32 0.4320 0.5248 0.0953 0.0784 0.002 0.148 0.087 1.747 0.017 0.386 22.508 0.05 17420. 0.2991
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5.80 0.4713 0.5519 0.0929 0.0794 0.002 0.149 0.085 1.768 0.017 0.376 21.698 0.05 17476. 0.2848
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6.29 0.5106 0.5761 0.0901 0.0799 0.002 0.150 0.082 1.780 0.017 0.365 20.906 0.05 17536. 0.2703
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6.77 0.5499 0.5975 0.0868 0.0799 0.002 0.150 0.079 1.780 0.017 0.351 20.134 0.05 17600. 0.2554
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7.25 0.5891 0.6161 0.0829 0.0793 0.002 0.149 0.075 1.766 0.017 0.336 19.378 0.05 17668. 0.2402
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7.74 0.6284 0.6320 0.0785 0.0780 0.002 0.147 0.071 1.739 0.017 0.318 18.633 0.05 17740. 0.2248
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8.22 0.6677 0.6448 0.0736 0.0762 0.002 0.144 0.067 1.699 0.016 0.298 17.894 0.05 17817. 0.2091
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8.70 0.7070 0.6544 0.0684 0.0739 0.002 0.139 0.062 1.647 0.016 0.277 17.150 0.05 17897. 0.1932
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9.19 0.7462 0.6602 0.0629 0.0711 0.002 0.134 0.057 1.584 0.015 0.255 16.392 0.05 17981. 0.1770
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9.67 0.7855 0.6616 0.0571 0.0678 0.002 0.128 0.052 1.511 0.014 0.231 15.607 0.05 18068. 0.1606
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10.15 0.8248 0.6579 0.0512 0.0641 0.002 0.121 0.047 1.429 0.014 0.207 14.780 0.05 18159. 0.1440
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10.64 0.8641 0.6478 0.0450 0.0601 0.002 0.113 0.041 1.339 0.013 0.182 13.892 0.05 18254. 0.1270
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11.12 0.9034 0.6297 0.0388 0.0557 0.002 0.105 0.035 1.240 0.012 0.157 12.915 0.05 18352. 0.1095
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11.60 0.9426 0.6009 0.0324 0.0509 0.002 0.096 0.030 1.134 0.011 0.131 11.813 0.05 18454. 0.0916
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12.09 0.9819 0.5578 0.0260 0.0458 0.001 0.086 0.024 1.021 0.010 0.105 10.526 0.05 18559. 0.0731
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12.57 1.0212 0.4940 0.0195 0.0404 0.001 0.076 0.018 0.900 0.009 0.079 8.963 0.05 18668. 0.0540
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13.05 1.0605 0.3986 0.0131 0.0347 0.001 0.065 0.012 0.774 0.007 0.053 6.964 0.05 18780. 0.0343
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13.54 1.0997 0.2513 0.0066 0.0288 0.001 0.054 0.006 0.642 0.006 0.027 4.235 0.05 18895. 0.0148
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14.02 1.1390 0.0087 0.0002 0.0227 0.001 0.043 0.000 0.506 0.005 0.001 0.142 0.05 19012. 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 0.1048 0.0544 0.013 0.410 0.382 9.703 0.046 1.698 17.845 0.10 34110. 0.4976
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1.00 0.0404 0.0759 0.1046 0.0557 0.013 0.420 0.381 9.933 0.047 1.693 17.385 0.10 34145. 0.4842
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1.99 0.0808 0.1475 0.1043 0.0572 0.014 0.431 0.380 10.189 0.049 1.688 16.898 0.10 34185. 0.4699
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2.99 0.1213 0.2145 0.1039 0.0587 0.014 0.442 0.378 10.469 0.050 1.683 16.390 0.10 34232. 0.4550
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3.98 0.1617 0.2769 0.1035 0.0604 0.014 0.455 0.377 10.772 0.051 1.676 15.865 0.10 34285. 0.4396
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4.98 0.2021 0.3344 0.1030 0.0622 0.015 0.469 0.375 11.094 0.053 1.668 15.329 0.10 34345. 0.4236
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5.97 0.2425 0.3871 0.1023 0.0641 0.015 0.483 0.373 11.428 0.055 1.657 14.788 0.10 34413. 0.4074
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6.97 0.2830 0.4351 0.1015 0.0660 0.016 0.497 0.370 11.768 0.056 1.644 14.247 0.10 34489. 0.3910
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7.96 0.3234 0.4786 0.1005 0.0679 0.016 0.511 0.366 12.103 0.058 1.627 13.712 0.10 34572. 0.3744
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8.96 0.3638 0.5179 0.0992 0.0697 0.017 0.525 0.361 12.422 0.059 1.606 13.188 0.10 34665. 0.3577
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9.95 0.4042 0.5531 0.0976 0.0713 0.017 0.537 0.355 12.711 0.061 1.580 12.676 0.10 34765. 0.3410
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10.95 0.4447 0.5846 0.0955 0.0727 0.017 0.547 0.348 12.952 0.062 1.547 12.181 0.10 34874. 0.3243
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11.94 0.4851 0.6127 0.0930 0.0737 0.018 0.555 0.339 13.128 0.063 1.507 11.703 0.10 34992. 0.3074
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12.94 0.5255 0.6377 0.0900 0.0741 0.018 0.559 0.328 13.216 0.063 1.457 11.242 0.10 35119. 0.2904
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13.93 0.5659 0.6597 0.0863 0.0741 0.018 0.558 0.314 13.200 0.063 1.398 10.800 0.10 35255. 0.2733
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14.93 0.6063 0.6789 0.0821 0.0733 0.018 0.552 0.299 13.069 0.062 1.330 10.374 0.11 35399. 0.2560
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15.92 0.6468 0.6954 0.0774 0.0719 0.017 0.542 0.282 12.824 0.061 1.253 9.961 0.11 35551. 0.2386
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16.92 0.6872 0.7090 0.0722 0.0700 0.017 0.527 0.263 12.469 0.060 1.169 9.558 0.11 35712. 0.2212
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17.91 0.7276 0.7194 0.0666 0.0674 0.016 0.508 0.243 12.015 0.057 1.079 9.160 0.11 35880. 0.2037
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18.91 0.7680 0.7262 0.0608 0.0643 0.015 0.485 0.221 11.468 0.055 0.985 8.760 0.11 36057. 0.1861
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19.91 0.8085 0.7288 0.0548 0.0608 0.015 0.458 0.200 10.835 0.052 0.887 8.352 0.11 36242. 0.1684
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20.90 0.8489 0.7263 0.0486 0.0568 0.014 0.428 0.177 10.122 0.048 0.787 7.927 0.11 36434. 0.1505
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21.90 0.8893 0.7173 0.0422 0.0524 0.013 0.394 0.154 9.334 0.045 0.684 7.473 0.11 36633. 0.1323
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22.89 0.9297 0.6997 0.0358 0.0475 0.011 0.358 0.130 8.472 0.040 0.579 6.973 0.11 36841. 0.1136
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23.89 0.9701 0.6702 0.0292 0.0423 0.010 0.319 0.106 7.543 0.036 0.473 6.400 0.11 37055. 0.0942
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24.88 1.0106 0.6228 0.0226 0.0367 0.009 0.277 0.082 6.549 0.031 0.367 5.710 0.11 37277. 0.0740
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25.88 1.0510 0.5467 0.0160 0.0308 0.007 0.232 0.058 5.495 0.026 0.260 4.819 0.11 37505. 0.0526
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26.87 1.0914 0.4189 0.0095 0.0246 0.006 0.185 0.034 4.388 0.021 0.153 3.556 0.11 37741. 0.0298
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27.87 1.1318 0.1825 0.0029 0.0182 0.004 0.137 0.011 3.236 0.015 0.047 1.494 0.11 37982. 0.0070
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28.86 1.1723
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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 0.1051 0.0516 0.042 0.875 0.861 31.056 0.099 3.828 12.571 0.15 51165. 0.5264
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1.47 0.0398 0.0789 0.1048 0.0529 0.043 0.897 0.859 31.826 0.101 3.819 12.237 0.15 51216. 0.5118
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2.94 0.0796 0.1532 0.1045 0.0543 0.044 0.921 0.856 32.682 0.104 3.809 11.884 0.15 51276. 0.4964
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4.41 0.1194 0.2227 0.1042 0.0559 0.045 0.947 0.854 33.621 0.107 3.797 11.517 0.15 51344. 0.4803
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5.88 0.1592 0.2872 0.1038 0.0576 0.046 0.976 0.851 34.635 0.110 3.783 11.139 0.15 51422. 0.4637
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7.35 0.1990 0.3466 0.1034 0.0594 0.048 1.006 0.847 35.714 0.114 3.766 10.753 0.16 51510. 0.4466
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8.82 0.2389 0.4008 0.1028 0.0612 0.049 1.038 0.842 36.840 0.117 3.745 10.365 0.16 51610. 0.4292
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10.29 0.2787 0.4502 0.1020 0.0631 0.051 1.070 0.836 37.989 0.121 3.717 9.978 0.16 51720. 0.4117
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11.76 0.3185 0.4948 0.1011 0.0650 0.052 1.102 0.828 39.131 0.125 3.682 9.596 0.16 51842. 0.3941
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13.23 0.3583 0.5350 0.0999 0.0669 0.054 1.133 0.818 40.230 0.128 3.638 9.222 0.16 51977. 0.3765
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14.70 0.3981 0.5710 0.0983 0.0686 0.055 1.162 0.805 41.239 0.131 3.583 8.859 0.16 52124. 0.3589
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16.17 0.4379 0.6032 0.0964 0.0700 0.056 1.186 0.790 42.108 0.134 3.513 8.508 0.16 52283. 0.3413
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17.64 0.4777 0.6320 0.0941 0.0711 0.057 1.205 0.771 42.774 0.136 3.428 8.171 0.16 52455. 0.3237
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19.11 0.5175 0.6576 0.0912 0.0718 0.058 1.216 0.747 43.171 0.137 3.322 7.848 0.16 52640. 0.3061
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20.58 0.5573 0.6803 0.0877 0.0719 0.058 1.218 0.719 43.235 0.138 3.197 7.539 0.16 52837. 0.2885
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22.05 0.5971 0.7004 0.0837 0.0714 0.058 1.209 0.686 42.928 0.137 3.050 7.244 0.16 53047. 0.2707
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23.52 0.6370 0.7179 0.0791 0.0702 0.057 1.190 0.648 42.240 0.134 2.884 6.961 0.16 53270. 0.2530
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24.99 0.6768 0.7329 0.0741 0.0685 0.055 1.160 0.607 41.186 0.131 2.701 6.688 0.16 53504. 0.2353
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26.46 0.7166 0.7451 0.0688 0.0661 0.053 1.121 0.563 39.790 0.127 2.506 6.422 0.16 53750. 0.2176
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27.93 0.7564 0.7543 0.0631 0.0633 0.051 1.073 0.517 38.077 0.121 2.300 6.159 0.16 54008. 0.1999
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29.40 0.7962 0.7601 0.0572 0.0600 0.048 1.016 0.469 36.069 0.115 2.086 5.896 0.16 54277. 0.1822
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30.88 0.8360 0.7617 0.0512 0.0562 0.045 0.952 0.419 33.784 0.108 1.864 5.627 0.16 54558. 0.1644
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32.35 0.8758 0.7583 0.0450 0.0519 0.042 0.880 0.368 31.237 0.099 1.638 5.347 0.16 54849. 0.1465
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33.82 0.9156 0.7481 0.0386 0.0473 0.038 0.801 0.316 28.440 0.091 1.408 5.047 0.16 55151. 0.1281
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35.29 0.9554 0.7289 0.0322 0.0422 0.034 0.716 0.264 25.406 0.081 1.174 4.712 0.16 55464. 0.1093
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36.76 0.9952 0.6962 0.0258 0.0368 0.030 0.624 0.211 22.147 0.070 0.938 4.321 0.16 55788. 0.0896
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38.23 1.0351 0.6422 0.0193 0.0311 0.025 0.526 0.158 18.679 0.059 0.702 3.832 0.16 56121. 0.0687
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39.70 1.0749 0.5504 0.0128 0.0250 0.020 0.423 0.105 15.020 0.048 0.466 3.163 0.16 56465. 0.0462
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41.17 1.1147 0.3806 0.0064 0.0186 0.015 0.315 0.052 11.194 0.036 0.231 2.109 0.16 56818. 0.0217
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42.64 1.1545 -0.0004 0.0000 0.0120 0.010 0.203 0.000 7.218 0.023 0.000 -0.002 0.16 57174. 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 0.1052 0.0501 0.096 1.509 1.532 71.397 0.170 6.816 9.735 0.21 68220. 0.5440
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1.97 0.0399 0.0816 0.1050 0.0514 0.098 1.548 1.529 73.236 0.175 6.801 9.470 0.21 68288. 0.5285
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3.93 0.0798 0.1583 0.1047 0.0528 0.101 1.591 1.525 75.280 0.180 6.784 9.189 0.21 68368. 0.5122
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5.90 0.1197 0.2300 0.1044 0.0544 0.104 1.638 1.521 77.524 0.185 6.764 8.897 0.21 68459. 0.4952
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7.86 0.1596 0.2963 0.1041 0.0561 0.107 1.689 1.515 79.953 0.191 6.741 8.597 0.21 68563. 0.4777
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9.83 0.1996 0.3572 0.1036 0.0579 0.111 1.744 1.509 82.541 0.197 6.711 8.291 0.21 68682. 0.4597
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11.79 0.2395 0.4127 0.1030 0.0598 0.114 1.801 1.501 85.246 0.204 6.674 7.984 0.21 68814. 0.4414
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13.76 0.2794 0.4631 0.1023 0.0617 0.118 1.860 1.490 88.013 0.210 6.627 7.678 0.21 68962. 0.4230
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15.72 0.3193 0.5085 0.1014 0.0637 0.122 1.918 1.476 90.769 0.217 6.567 7.377 0.21 69126. 0.4046
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17.69 0.3592 0.5492 0.1002 0.0655 0.125 1.974 1.459 93.426 0.223 6.490 7.083 0.21 69306. 0.3862
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19.65 0.3991 0.5857 0.0987 0.0672 0.129 2.026 1.437 95.875 0.229 6.392 6.798 0.21 69503. 0.3678
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21.62 0.4390 0.6183 0.0968 0.0687 0.131 2.071 1.409 97.991 0.234 6.269 6.524 0.21 69716. 0.3496
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23.58 0.4789 0.6473 0.0944 0.0699 0.134 2.105 1.375 99.625 0.238 6.117 6.261 0.21 69947. 0.3314
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25.55 0.5188 0.6731 0.0915 0.0706 0.135 2.126 1.333 100.615 0.240 5.930 6.010 0.21 70194. 0.3132
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27.51 0.5588 0.6961 0.0881 0.0707 0.135 2.130 1.283 100.809 0.241 5.705 5.771 0.21 70459. 0.2950
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29.48 0.5987 0.7164 0.0840 0.0702 0.134 2.115 1.224 100.112 0.239 5.442 5.543 0.21 70740. 0.2768
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31.45 0.6386 0.7343 0.0794 0.0691 0.132 2.081 1.157 98.501 0.235 5.145 5.327 0.21 71038. 0.2586
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33.41 0.6785 0.7498 0.0744 0.0673 0.129 2.029 1.084 96.008 0.229 4.819 5.119 0.21 71352. 0.2405
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35.38 0.7184 0.7626 0.0690 0.0650 0.124 1.959 1.005 92.691 0.221 4.470 4.917 0.21 71682. 0.2225
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37.34 0.7583 0.7727 0.0633 0.0621 0.119 1.872 0.922 88.607 0.212 4.101 4.720 0.21 72027. 0.2046
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39.31 0.7982 0.7795 0.0574 0.0588 0.112 1.771 0.836 83.809 0.200 3.718 4.524 0.21 72388. 0.1867
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41.27 0.8381 0.7825 0.0513 0.0549 0.105 1.655 0.747 78.338 0.187 3.323 4.325 0.21 72764. 0.1687
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43.24 0.8780 0.7808 0.0450 0.0507 0.097 1.526 0.656 72.230 0.172 2.918 4.119 0.21 73154. 0.1506
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45.20 0.9180 0.7730 0.0387 0.0459 0.088 1.384 0.563 65.515 0.156 2.506 3.901 0.21 73559. 0.1322
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47.17 0.9579 0.7566 0.0322 0.0408 0.078 1.230 0.470 58.220 0.139 2.089 3.659 0.22 73978. 0.1132
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49.13 0.9978 0.7274 0.0258 0.0353 0.068 1.065 0.375 50.379 0.120 1.669 3.377 0.22 74411. 0.0934
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51.10 1.0377 0.6776 0.0192 0.0295 0.056 0.888 0.280 42.028 0.100 1.247 3.025 0.22 74858. 0.0723
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53.06 1.0776 0.5897 0.0127 0.0233 0.045 0.702 0.186 33.214 0.079 0.826 2.535 0.22 75319. 0.0493
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55.03 1.1175 0.4185 0.0063 0.0168 0.032 0.507 0.092 23.994 0.057 0.408 1.735 0.22 75791. 0.0237
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56.99 1.1574 -0.0081 -0.0001 0.0101 0.019 0.304 -0.001 14.403 0.034 -0.005 -0.033 0.22 76264. 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 0.1054 0.0491 0.183 2.312 2.398 136.757 0.261 10.665 7.952 0.26 85274. 0.5558
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2.46 0.0400 0.0834 0.1051 0.0504 0.188 2.373 2.392 140.357 0.268 10.642 7.731 0.26 85360. 0.5398
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4.92 0.0799 0.1617 0.1049 0.0518 0.194 2.440 2.387 144.365 0.276 10.617 7.499 0.26 85459. 0.5229
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7.38 0.1199 0.2347 0.1046 0.0534 0.200 2.515 2.380 148.771 0.284 10.588 7.257 0.26 85574. 0.5054
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9.84 0.1598 0.3022 0.1043 0.0551 0.206 2.596 2.372 153.548 0.293 10.553 7.008 0.26 85704. 0.4872
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12.30 0.1998 0.3642 0.1038 0.0570 0.213 2.682 2.363 158.645 0.303 10.509 6.755 0.26 85852. 0.4687
|
|
14.76 0.2397 0.4205 0.1033 0.0589 0.220 2.772 2.350 163.984 0.313 10.454 6.501 0.26 86018. 0.4498
|
|
17.22 0.2797 0.4716 0.1026 0.0608 0.227 2.865 2.334 169.456 0.324 10.383 6.248 0.26 86204. 0.4309
|
|
19.68 0.3197 0.5175 0.1017 0.0628 0.235 2.957 2.314 174.920 0.334 10.291 5.999 0.26 86409. 0.4119
|
|
22.14 0.3596 0.5586 0.1005 0.0647 0.242 3.046 2.287 180.199 0.344 10.173 5.757 0.26 86634. 0.3930
|
|
24.59 0.3996 0.5954 0.0990 0.0665 0.248 3.129 2.253 185.081 0.353 10.023 5.522 0.26 86880. 0.3742
|
|
27.05 0.4395 0.6282 0.0972 0.0680 0.254 3.200 2.211 189.317 0.362 9.834 5.297 0.26 87148. 0.3555
|
|
29.51 0.4795 0.6574 0.0948 0.0692 0.258 3.256 2.158 192.613 0.368 9.597 5.081 0.26 87436. 0.3369
|
|
31.97 0.5194 0.6834 0.0919 0.0699 0.261 3.290 2.092 194.647 0.372 9.306 4.875 0.26 87747. 0.3183
|
|
34.43 0.5594 0.7065 0.0885 0.0701 0.262 3.298 2.013 195.116 0.373 8.956 4.680 0.26 88078. 0.2998
|
|
36.89 0.5993 0.7271 0.0844 0.0696 0.260 3.277 1.921 193.826 0.370 8.545 4.496 0.26 88430. 0.2812
|
|
39.35 0.6393 0.7452 0.0798 0.0685 0.256 3.224 1.817 190.730 0.364 8.080 4.320 0.26 88804. 0.2628
|
|
41.81 0.6793 0.7611 0.0748 0.0667 0.249 3.142 1.702 185.889 0.355 7.569 4.152 0.26 89197. 0.2445
|
|
44.27 0.7192 0.7744 0.0694 0.0644 0.241 3.033 1.578 179.410 0.343 7.021 3.990 0.26 89610. 0.2263
|
|
46.73 0.7592 0.7851 0.0637 0.0615 0.230 2.898 1.448 171.409 0.327 6.442 3.832 0.27 90043. 0.2082
|
|
49.19 0.7991 0.7928 0.0577 0.0582 0.217 2.738 1.313 161.987 0.309 5.840 3.677 0.27 90495. 0.1901
|
|
51.65 0.8391 0.7969 0.0516 0.0543 0.203 2.556 1.174 151.226 0.289 5.220 3.520 0.27 90965. 0.1721
|
|
54.11 0.8790 0.7967 0.0453 0.0500 0.187 2.353 1.031 139.195 0.266 4.585 3.359 0.27 91454. 0.1539
|
|
56.57 0.9190 0.7907 0.0389 0.0452 0.169 2.129 0.885 125.952 0.241 3.938 3.188 0.27 91962. 0.1354
|
|
59.03 0.9590 0.7767 0.0324 0.0401 0.150 1.886 0.738 111.556 0.213 3.284 3.001 0.27 92487. 0.1164
|
|
61.49 0.9989 0.7507 0.0259 0.0345 0.129 1.624 0.590 96.068 0.183 2.624 2.785 0.27 93030. 0.0965
|
|
63.95 1.0389 0.7048 0.0194 0.0286 0.107 1.345 0.441 79.564 0.152 1.962 2.514 0.27 93589. 0.0754
|
|
66.40 1.0788 0.6217 0.0129 0.0223 0.083 1.050 0.293 62.137 0.119 1.301 2.135 0.27 94166. 0.0521
|
|
68.86 1.1188 0.4533 0.0064 0.0158 0.059 0.742 0.145 43.904 0.084 0.646 1.501 0.27 94758. 0.0258
|
|
71.32 1.1587 -0.0013 0.0000 0.0089 0.033 0.421 0.000 24.919 0.048 -0.001 -0.004 0.27 95348. 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 0.1055 0.0485 0.313 3.286 3.457 233.293 0.371 15.376 6.721 0.31 102328. 0.5640
|
|
2.96 0.0400 0.0847 0.1053 0.0498 0.321 3.374 3.450 239.525 0.381 15.345 6.533 0.31 102431. 0.5477
|
|
5.91 0.0800 0.1642 0.1051 0.0512 0.331 3.472 3.442 246.473 0.392 15.311 6.335 0.31 102551. 0.5305
|
|
8.87 0.1201 0.2382 0.1048 0.0528 0.341 3.580 3.433 254.123 0.404 15.272 6.128 0.31 102688. 0.5125
|
|
11.82 0.1601 0.3067 0.1045 0.0545 0.352 3.697 3.423 262.431 0.418 15.225 5.916 0.31 102845. 0.4940
|
|
14.78 0.2001 0.3693 0.1041 0.0564 0.364 3.822 3.410 271.313 0.432 15.166 5.700 0.31 103023. 0.4751
|
|
17.74 0.2401 0.4263 0.1035 0.0583 0.376 3.953 3.393 280.635 0.447 15.090 5.483 0.31 103223. 0.4558
|
|
20.69 0.2801 0.4779 0.1029 0.0603 0.389 4.088 3.370 290.211 0.462 14.992 5.268 0.31 103446. 0.4365
|
|
23.65 0.3202 0.5242 0.1020 0.0623 0.402 4.223 3.342 299.794 0.477 14.864 5.056 0.31 103692. 0.4172
|
|
26.60 0.3602 0.5656 0.1009 0.0642 0.414 4.354 3.305 309.075 0.492 14.699 4.849 0.31 103964. 0.3979
|
|
29.56 0.4002 0.6026 0.0994 0.0660 0.426 4.475 3.257 317.684 0.506 14.486 4.650 0.31 104260. 0.3788
|
|
32.52 0.4402 0.6355 0.0975 0.0676 0.436 4.581 3.196 325.180 0.518 14.217 4.458 0.31 104582. 0.3598
|
|
35.47 0.4802 0.6649 0.0952 0.0688 0.444 4.663 3.120 331.047 0.527 13.880 4.275 0.31 104929. 0.3409
|
|
38.43 0.5203 0.6910 0.0924 0.0696 0.449 4.715 3.027 334.715 0.533 13.463 4.101 0.31 105302. 0.3221
|
|
41.38 0.5603 0.7142 0.0889 0.0697 0.450 4.728 2.913 335.652 0.534 12.958 3.937 0.31 105701. 0.3033
|
|
44.34 0.6003 0.7349 0.0848 0.0693 0.447 4.698 2.780 333.510 0.531 12.365 3.781 0.31 106126. 0.2845
|
|
47.30 0.6403 0.7533 0.0802 0.0682 0.440 4.623 2.629 328.200 0.522 11.693 3.633 0.32 106575. 0.2659
|
|
50.25 0.6803 0.7694 0.0752 0.0665 0.429 4.505 2.463 319.825 0.509 10.954 3.493 0.32 107049. 0.2474
|
|
53.21 0.7204 0.7832 0.0697 0.0641 0.414 4.347 2.284 308.573 0.491 10.160 3.357 0.32 107546. 0.2290
|
|
56.16 0.7604 0.7944 0.0640 0.0612 0.395 4.151 2.096 294.644 0.469 9.322 3.226 0.32 108067. 0.2108
|
|
59.12 0.8004 0.8027 0.0580 0.0578 0.373 3.919 1.900 278.213 0.443 8.450 3.097 0.32 108611. 0.1927
|
|
62.08 0.8404 0.8077 0.0518 0.0539 0.348 3.655 1.698 259.425 0.413 7.551 2.968 0.32 109177. 0.1745
|
|
65.03 0.8804 0.8085 0.0455 0.0495 0.320 3.358 1.491 238.400 0.379 6.630 2.836 0.32 109766. 0.1563
|
|
67.99 0.9205 0.8039 0.0391 0.0447 0.289 3.032 1.280 215.242 0.343 5.693 2.697 0.32 110376. 0.1377
|
|
70.95 0.9605 0.7917 0.0325 0.0395 0.255 2.677 1.067 190.051 0.302 4.744 2.545 0.32 111008. 0.1186
|
|
73.90 1.0005 0.7679 0.0260 0.0339 0.219 2.295 0.851 162.937 0.259 3.787 2.370 0.32 111662. 0.0987
|
|
76.86 1.0405 0.7249 0.0194 0.0279 0.180 1.888 0.636 134.034 0.213 2.828 2.152 0.33 112336. 0.0774
|
|
79.81 1.0805 0.6450 0.0128 0.0215 0.139 1.458 0.421 103.509 0.165 1.871 1.843 0.33 113030. 0.0540
|
|
82.77 1.1206 0.4770 0.0063 0.0149 0.096 1.008 0.207 71.566 0.114 0.923 1.315 0.33 113742. 0.0270
|
|
85.73 1.1606 -0.0163 -0.0001 0.0080 0.051 0.539 -0.004 38.265 0.061 -0.016 -0.043 0.33 114445. 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 0.1056 0.0481 0.493 4.436 4.711 367.365 0.501 20.955 5.817 0.36 119382. 0.5699
|
|
3.45 0.0400 0.0854 0.1054 0.0494 0.506 4.555 4.702 377.244 0.515 20.916 5.654 0.36 119502. 0.5534
|
|
6.89 0.0800 0.1657 0.1052 0.0508 0.521 4.688 4.693 388.275 0.530 20.873 5.482 0.36 119641. 0.5360
|
|
10.34 0.1200 0.2404 0.1050 0.0524 0.537 4.835 4.681 400.440 0.546 20.823 5.303 0.36 119801. 0.5178
|
|
13.79 0.1600 0.3094 0.1047 0.0541 0.555 4.995 4.668 413.677 0.564 20.764 5.118 0.36 119984. 0.4991
|
|
17.24 0.2000 0.3726 0.1043 0.0560 0.574 5.166 4.651 427.858 0.584 20.689 4.931 0.36 120191. 0.4800
|
|
20.68 0.2400 0.4300 0.1038 0.0579 0.594 5.346 4.630 442.780 0.604 20.592 4.742 0.36 120424. 0.4606
|
|
24.13 0.2800 0.4819 0.1032 0.0600 0.614 5.532 4.601 458.148 0.625 20.466 4.555 0.36 120684. 0.4410
|
|
27.58 0.3200 0.5285 0.1023 0.0620 0.635 5.718 4.564 473.572 0.646 20.300 4.371 0.36 120972. 0.4215
|
|
31.03 0.3600 0.5701 0.1012 0.0639 0.655 5.899 4.515 488.562 0.666 20.083 4.192 0.36 121288. 0.4020
|
|
34.47 0.4000 0.6073 0.0998 0.0658 0.674 6.068 4.452 502.523 0.686 19.803 4.018 0.36 121633. 0.3827
|
|
37.92 0.4400 0.6404 0.0980 0.0674 0.690 6.215 4.372 514.747 0.702 19.446 3.852 0.36 122008. 0.3635
|
|
41.37 0.4800 0.6698 0.0957 0.0686 0.703 6.332 4.270 524.405 0.715 18.994 3.693 0.37 122413. 0.3445
|
|
44.81 0.5200 0.6960 0.0929 0.0694 0.712 6.407 4.144 530.578 0.724 18.434 3.543 0.37 122848. 0.3255
|
|
48.26 0.5600 0.7194 0.0895 0.0697 0.714 6.428 3.991 532.396 0.726 17.753 3.400 0.37 123313. 0.3066
|
|
51.71 0.6001 0.7403 0.0854 0.0693 0.710 6.391 3.811 529.284 0.722 16.951 3.266 0.37 123808. 0.2877
|
|
55.16 0.6401 0.7589 0.0808 0.0682 0.699 6.292 3.606 521.076 0.711 16.038 3.139 0.37 124332. 0.2690
|
|
58.60 0.6801 0.7753 0.0758 0.0665 0.681 6.133 3.379 507.923 0.693 15.031 3.018 0.37 124884. 0.2504
|
|
62.05 0.7201 0.7894 0.0703 0.0641 0.657 5.918 3.136 490.124 0.669 13.949 2.902 0.37 125465. 0.2320
|
|
65.50 0.7601 0.8011 0.0645 0.0612 0.628 5.651 2.879 468.000 0.638 12.805 2.790 0.37 126072. 0.2137
|
|
68.95 0.8001 0.8101 0.0585 0.0578 0.593 5.335 2.611 441.833 0.603 11.613 2.680 0.37 126706. 0.1955
|
|
72.39 0.8401 0.8159 0.0523 0.0539 0.552 4.973 2.334 411.859 0.562 10.384 2.571 0.37 127367. 0.1773
|
|
75.84 0.8801 0.8178 0.0460 0.0495 0.507 4.567 2.051 378.271 0.516 9.125 2.460 0.37 128053. 0.1590
|
|
79.29 0.9201 0.8146 0.0395 0.0447 0.458 4.120 1.763 341.238 0.466 7.843 2.344 0.38 128765. 0.1405
|
|
82.73 0.9601 0.8043 0.0330 0.0394 0.404 3.634 1.471 300.921 0.411 6.544 2.217 0.38 129502. 0.1214
|
|
86.18 1.0001 0.7832 0.0264 0.0337 0.345 3.109 1.177 257.496 0.351 5.234 2.073 0.38 130264. 0.1015
|
|
89.63 1.0401 0.7439 0.0198 0.0276 0.283 2.550 0.881 211.176 0.288 3.921 1.893 0.38 131049. 0.0802
|
|
93.08 1.0801 0.6694 0.0132 0.0212 0.218 1.959 0.587 162.230 0.221 2.610 1.640 0.38 131858. 0.0567
|
|
96.52 1.1201 0.5094 0.0066 0.0145 0.149 1.340 0.295 110.988 0.151 1.310 1.204 0.38 132689. 0.0295
|
|
99.97 1.1601 0.0189 0.0001 0.0075 0.077 0.695 0.005 57.571 0.079 0.024 0.043 0.38 133511. 0.0001
|
|
|
|
|
|
|
|
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 0.1058 0.0478 0.732 5.764 6.161 545.595 0.651 27.406 5.122 0.41 136435. 0.5739
|
|
3.95 0.0401 0.0861 0.1056 0.0491 0.751 5.920 6.151 560.329 0.669 27.358 4.979 0.41 136572. 0.5573
|
|
7.89 0.0801 0.1670 0.1054 0.0506 0.774 6.094 6.139 576.811 0.689 27.306 4.827 0.41 136731. 0.5398
|
|
11.84 0.1202 0.2423 0.1052 0.0522 0.798 6.287 6.126 595.024 0.710 27.246 4.669 0.41 136915. 0.5216
|
|
15.78 0.1603 0.3118 0.1049 0.0539 0.825 6.496 6.110 614.887 0.734 27.175 4.507 0.41 137124. 0.5028
|
|
19.73 0.2003 0.3755 0.1045 0.0558 0.853 6.722 6.089 636.220 0.759 27.085 4.341 0.41 137362. 0.4835
|
|
23.67 0.2404 0.4333 0.1041 0.0577 0.883 6.960 6.063 658.726 0.786 26.968 4.175 0.41 137628. 0.4640
|
|
27.62 0.2804 0.4854 0.1035 0.0598 0.915 7.205 6.028 681.971 0.814 26.813 4.009 0.41 137926. 0.4443
|
|
31.57 0.3205 0.5323 0.1027 0.0618 0.946 7.452 5.982 705.372 0.842 26.607 3.846 0.41 138255. 0.4246
|
|
35.51 0.3606 0.5741 0.1016 0.0638 0.977 7.693 5.921 728.185 0.869 26.335 3.688 0.42 138617. 0.4050
|
|
39.46 0.4006 0.6114 0.1003 0.0657 1.005 7.919 5.841 749.505 0.895 25.980 3.535 0.42 139013. 0.3856
|
|
43.40 0.4407 0.6446 0.0985 0.0673 1.030 8.117 5.738 768.250 0.917 25.523 3.388 0.42 139442. 0.3663
|
|
47.35 0.4808 0.6741 0.0963 0.0687 1.050 8.274 5.608 783.154 0.935 24.942 3.248 0.42 139906. 0.3471
|
|
51.29 0.5208 0.7004 0.0935 0.0695 1.063 8.376 5.444 792.808 0.946 24.216 3.115 0.42 140405. 0.3280
|
|
55.24 0.5609 0.7239 0.0900 0.0698 1.067 8.409 5.245 795.877 0.950 23.330 2.989 0.42 140938. 0.3090
|
|
59.19 0.6010 0.7449 0.0860 0.0694 1.061 8.362 5.010 791.462 0.945 22.282 2.871 0.42 141506. 0.2900
|
|
63.13 0.6410 0.7637 0.0814 0.0683 1.045 8.234 4.741 779.296 0.930 21.087 2.759 0.42 142106. 0.2712
|
|
67.08 0.6811 0.7803 0.0763 0.0666 1.019 8.025 4.444 759.599 0.907 19.766 2.653 0.42 142739. 0.2525
|
|
71.02 0.7212 0.7947 0.0708 0.0642 0.983 7.742 4.124 732.823 0.875 18.343 2.552 0.42 143405. 0.2339
|
|
74.97 0.7612 0.8068 0.0650 0.0613 0.938 7.390 3.786 699.456 0.835 16.838 2.455 0.42 144101. 0.2156
|
|
78.91 0.8013 0.8162 0.0589 0.0579 0.885 6.972 3.433 659.932 0.788 15.269 2.359 0.43 144828. 0.1973
|
|
82.86 0.8413 0.8226 0.0527 0.0539 0.824 6.494 3.069 614.611 0.734 13.650 2.265 0.43 145585. 0.1791
|
|
86.81 0.8814 0.8253 0.0463 0.0494 0.756 5.957 2.696 563.790 0.673 11.990 2.169 0.43 146372. 0.1607
|
|
90.75 0.9215 0.8231 0.0398 0.0445 0.681 5.364 2.316 507.722 0.606 10.301 2.069 0.43 147188. 0.1421
|
|
94.70 0.9615 0.8140 0.0331 0.0392 0.599 4.719 1.931 446.656 0.533 8.588 1.961 0.43 148033. 0.1230
|
|
98.64 1.0016 0.7945 0.0265 0.0334 0.511 4.024 1.543 380.861 0.455 6.862 1.837 0.43 148906. 0.1030
|
|
102.59 1.0417 0.7572 0.0198 0.0272 0.417 3.282 1.153 310.662 0.371 5.129 1.684 0.43 149806. 0.0816
|
|
106.53 1.0817 0.6849 0.0131 0.0207 0.317 2.498 0.765 236.474 0.282 3.401 1.467 0.44 150733. 0.0579
|
|
110.48 1.1218 0.5247 0.0065 0.0139 0.213 1.678 0.379 158.802 0.190 1.687 1.083 0.44 151685. 0.0301
|
|
114.42 1.1619 -0.0072 0.0000 0.0068 0.104 0.821 -0.002 77.708 0.093 -0.011 -0.014 0.44 152616. 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 0.1059 0.0477 1.039 7.278 7.809 774.953 0.822 34.733 4.570 0.46 153488. 0.5764
|
|
4.44 0.0401 0.0865 0.1057 0.0490 1.067 7.474 7.796 795.871 0.844 34.676 4.443 0.46 153642. 0.5599
|
|
8.88 0.0802 0.1678 0.1056 0.0504 1.099 7.694 7.782 819.314 0.869 34.616 4.308 0.46 153821. 0.5425
|
|
13.33 0.1203 0.2435 0.1054 0.0520 1.134 7.938 7.767 845.277 0.897 34.549 4.168 0.46 154027. 0.5243
|
|
17.77 0.1604 0.3134 0.1051 0.0538 1.172 8.205 7.749 873.663 0.927 34.467 4.023 0.46 154263. 0.5055
|
|
22.21 0.2005 0.3774 0.1048 0.0557 1.213 8.492 7.726 904.237 0.959 34.365 3.875 0.47 154530. 0.4862
|
|
26.65 0.2406 0.4355 0.1044 0.0577 1.256 8.796 7.695 936.593 0.994 34.229 3.727 0.47 154830. 0.4666
|
|
31.10 0.2807 0.4879 0.1038 0.0597 1.301 9.111 7.655 970.124 1.029 34.048 3.579 0.47 155165. 0.4469
|
|
35.54 0.3208 0.5349 0.1031 0.0618 1.346 9.429 7.600 1004.003 1.065 33.803 3.433 0.47 155536. 0.4272
|
|
39.98 0.3608 0.5769 0.1021 0.0639 1.391 9.740 7.526 1037.160 1.100 33.477 3.291 0.47 155943. 0.4076
|
|
44.42 0.4009 0.6143 0.1008 0.0658 1.433 10.033 7.429 1068.281 1.133 33.046 3.154 0.47 156389. 0.3881
|
|
48.86 0.4410 0.6476 0.0991 0.0675 1.469 10.291 7.303 1095.795 1.163 32.484 3.023 0.47 156873. 0.3687
|
|
53.31 0.4811 0.6772 0.0969 0.0688 1.499 10.498 7.141 1117.849 1.186 31.765 2.898 0.47 157396. 0.3495
|
|
57.75 0.5212 0.7035 0.0941 0.0697 1.519 10.635 6.938 1132.389 1.202 30.859 2.779 0.47 157958. 0.3304
|
|
62.19 0.5613 0.7271 0.0907 0.0700 1.525 10.682 6.688 1137.443 1.207 29.747 2.667 0.47 158559. 0.3113
|
|
66.63 0.6014 0.7482 0.0867 0.0697 1.518 10.628 6.391 1131.669 1.201 28.426 2.561 0.47 159198. 0.2923
|
|
71.08 0.6415 0.7672 0.0821 0.0686 1.495 10.468 6.050 1114.635 1.183 26.912 2.462 0.47 159875. 0.2733
|
|
75.52 0.6816 0.7840 0.0770 0.0669 1.457 10.205 5.673 1086.641 1.153 25.235 2.368 0.47 160588. 0.2546
|
|
79.96 0.7217 0.7987 0.0714 0.0645 1.406 9.845 5.266 1048.338 1.112 23.424 2.278 0.48 161338. 0.2360
|
|
84.40 0.7618 0.8112 0.0656 0.0616 1.342 9.396 4.835 1000.440 1.061 21.508 2.192 0.48 162123. 0.2176
|
|
88.85 0.8019 0.8211 0.0595 0.0581 1.265 8.862 4.386 943.586 1.001 19.507 2.108 0.48 162942. 0.1993
|
|
93.29 0.8420 0.8281 0.0532 0.0541 1.178 8.248 3.921 878.304 0.932 17.440 2.025 0.48 163796. 0.1810
|
|
97.73 0.8821 0.8315 0.0467 0.0496 1.080 7.560 3.444 805.027 0.854 15.321 1.941 0.48 164682. 0.1626
|
|
102.17 0.9222 0.8302 0.0401 0.0446 0.971 6.801 2.959 724.129 0.768 13.162 1.853 0.48 165602. 0.1439
|
|
106.61 0.9623 0.8224 0.0335 0.0392 0.853 5.973 2.467 635.971 0.675 10.974 1.760 0.49 166554. 0.1247
|
|
111.06 1.0024 0.8045 0.0267 0.0333 0.725 5.080 1.971 540.942 0.574 8.766 1.652 0.49 167537. 0.1047
|
|
115.50 1.0425 0.7695 0.0200 0.0271 0.589 4.128 1.473 439.517 0.466 6.550 1.520 0.49 168552. 0.0832
|
|
119.94 1.0825 0.7001 0.0132 0.0205 0.446 3.121 0.976 332.296 0.353 4.339 1.332 0.49 169596. 0.0594
|
|
124.38 1.1226 0.5425 0.0065 0.0135 0.295 2.066 0.483 220.019 0.233 2.146 0.995 0.49 170668. 0.0312
|
|
128.83 1.1627 -0.0161 -0.0001 0.0063 0.138 0.964 -0.006 102.657 0.109 -0.029 -0.029 0.49 171709. 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 0.1061 0.0477 1.425 8.983 9.654 1062.852 1.015 42.941 4.120 0.52 170540. 0.5778
|
|
4.94 0.0401 0.0867 0.1059 0.0490 1.464 9.225 9.640 1091.415 1.042 42.877 4.006 0.52 170711. 0.5614
|
|
9.88 0.0802 0.1683 0.1057 0.0504 1.507 9.496 9.625 1123.494 1.073 42.811 3.886 0.52 170910. 0.5441
|
|
14.82 0.1204 0.2442 0.1056 0.0520 1.554 9.797 9.608 1159.108 1.107 42.737 3.760 0.52 171139. 0.5260
|
|
19.76 0.1605 0.3144 0.1053 0.0538 1.607 10.127 9.588 1198.154 1.144 42.648 3.630 0.52 171401. 0.5073
|
|
24.69 0.2006 0.3786 0.1051 0.0557 1.663 10.484 9.563 1240.344 1.184 42.536 3.497 0.52 171698. 0.4881
|
|
29.63 0.2407 0.4369 0.1047 0.0577 1.723 10.862 9.529 1285.153 1.227 42.387 3.363 0.52 172032. 0.4686
|
|
34.57 0.2808 0.4895 0.1042 0.0598 1.786 11.256 9.484 1331.775 1.272 42.184 3.230 0.52 172404. 0.4490
|
|
39.51 0.3209 0.5367 0.1035 0.0619 1.849 11.656 9.421 1379.080 1.317 41.906 3.099 0.52 172815. 0.4293
|
|
44.45 0.3611 0.5788 0.1026 0.0640 1.912 12.049 9.336 1425.593 1.361 41.528 2.970 0.52 173269. 0.4097
|
|
49.39 0.4012 0.6163 0.1013 0.0660 1.971 12.420 9.223 1469.476 1.403 41.022 2.847 0.52 173764. 0.3902
|
|
54.33 0.4413 0.6497 0.0997 0.0677 2.023 12.750 9.073 1508.515 1.441 40.355 2.728 0.52 174302. 0.3709
|
|
59.27 0.4814 0.6794 0.0975 0.0691 2.065 13.017 8.878 1540.103 1.471 39.491 2.615 0.52 174884. 0.3517
|
|
64.20 0.5215 0.7058 0.0948 0.0701 2.094 13.197 8.632 1561.331 1.491 38.394 2.508 0.52 175509. 0.3325
|
|
69.14 0.5617 0.7295 0.0915 0.0704 2.105 13.265 8.327 1569.393 1.499 37.037 2.406 0.52 176177. 0.3134
|
|
74.08 0.6018 0.7507 0.0875 0.0701 2.095 13.205 7.962 1562.332 1.492 35.414 2.311 0.53 176888. 0.2944
|
|
79.02 0.6419 0.7698 0.0829 0.0691 2.064 13.012 7.542 1539.474 1.470 33.547 2.222 0.53 177642. 0.2754
|
|
83.96 0.6820 0.7868 0.0777 0.0674 2.013 12.689 7.075 1501.206 1.434 31.471 2.138 0.53 178436. 0.2567
|
|
88.90 0.7221 0.8018 0.0722 0.0650 1.942 12.243 6.570 1448.433 1.383 29.224 2.057 0.53 179270. 0.2380
|
|
93.84 0.7622 0.8146 0.0663 0.0620 1.854 11.682 6.034 1382.167 1.320 26.841 1.980 0.53 180144. 0.2196
|
|
98.78 0.8024 0.8250 0.0601 0.0585 1.748 11.016 5.474 1303.317 1.245 24.350 1.905 0.53 181056. 0.2012
|
|
103.72 0.8425 0.8326 0.0538 0.0544 1.626 10.250 4.895 1212.638 1.158 21.775 1.831 0.53 182005. 0.1829
|
|
108.65 0.8826 0.8367 0.0473 0.0499 1.490 9.388 4.301 1110.747 1.061 19.133 1.756 0.54 182992. 0.1644
|
|
113.59 0.9227 0.8363 0.0406 0.0448 1.339 8.437 3.696 998.171 0.953 16.439 1.679 0.54 184015. 0.1457
|
|
118.53 0.9628 0.8297 0.0339 0.0393 1.174 7.399 3.082 875.418 0.836 13.707 1.597 0.54 185074. 0.1265
|
|
123.47 1.0030 0.8134 0.0270 0.0333 0.996 6.280 2.462 743.034 0.710 10.949 1.503 0.54 186168. 0.1064
|
|
128.41 1.0431 0.7805 0.0202 0.0270 0.807 5.086 1.839 601.681 0.575 8.180 1.386 0.54 187297. 0.0849
|
|
133.35 1.0832 0.7140 0.0134 0.0203 0.606 3.822 1.218 452.200 0.432 5.416 1.221 0.55 188459. 0.0608
|
|
138.29 1.1233 0.5592 0.0066 0.0133 0.396 2.499 0.601 295.634 0.282 2.674 0.922 0.55 189651. 0.0323
|
|
143.23 1.1634 -0.0238 -0.0001 0.0059 0.177 1.114 -0.011 131.778 0.126 -0.049 -0.038 0.55 190798. 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 0.1062 0.0478 1.901 10.890 11.699 1417.288 1.230 52.037 3.744 0.57 187591. 0.5780
|
|
5.44 0.0401 0.0868 0.1061 0.0491 1.951 11.181 11.683 1455.066 1.263 51.966 3.642 0.57 187779. 0.5618
|
|
10.87 0.0803 0.1684 0.1059 0.0505 2.008 11.507 11.667 1497.592 1.300 51.895 3.534 0.57 187998. 0.5448
|
|
16.31 0.1204 0.2445 0.1058 0.0521 2.072 11.871 11.650 1544.928 1.341 51.817 3.420 0.57 188251. 0.5269
|
|
21.74 0.1606 0.3148 0.1056 0.0539 2.142 12.271 11.629 1596.984 1.386 51.725 3.303 0.57 188539. 0.5084
|
|
27.18 0.2007 0.3792 0.1054 0.0558 2.217 12.705 11.603 1653.433 1.435 51.609 3.183 0.57 188865. 0.4893
|
|
32.61 0.2408 0.4378 0.1050 0.0578 2.298 13.167 11.567 1713.634 1.488 51.452 3.062 0.57 189232. 0.4700
|
|
38.05 0.2810 0.4906 0.1046 0.0599 2.382 13.651 11.519 1776.557 1.542 51.235 2.941 0.57 189641. 0.4505
|
|
43.49 0.3211 0.5379 0.1040 0.0621 2.468 14.144 11.450 1840.727 1.598 50.931 2.821 0.57 190094. 0.4309
|
|
48.92 0.3613 0.5801 0.1031 0.0642 2.554 14.631 11.356 1904.168 1.653 50.510 2.705 0.57 190593. 0.4114
|
|
54.36 0.4014 0.6177 0.1019 0.0662 2.634 15.094 11.226 1964.384 1.705 49.935 2.592 0.57 191138. 0.3920
|
|
59.79 0.4415 0.6511 0.1004 0.0681 2.707 15.509 11.054 2018.344 1.752 49.166 2.484 0.57 191730. 0.3728
|
|
65.23 0.4817 0.6809 0.0983 0.0695 2.766 15.848 10.827 2062.468 1.790 48.157 2.381 0.57 192370. 0.3536
|
|
70.66 0.5218 0.7074 0.0957 0.0706 2.806 16.080 10.535 2092.742 1.817 46.861 2.283 0.58 193059. 0.3345
|
|
76.10 0.5620 0.7311 0.0924 0.0710 2.823 16.177 10.171 2105.265 1.828 45.243 2.191 0.58 193795. 0.3155
|
|
81.54 0.6021 0.7525 0.0884 0.0707 2.812 16.115 9.734 2097.251 1.821 43.295 2.105 0.58 194578. 0.2964
|
|
86.97 0.6423 0.7717 0.0838 0.0697 2.773 15.888 9.227 2067.671 1.795 41.040 2.024 0.58 195408. 0.2775
|
|
92.41 0.6824 0.7890 0.0786 0.0680 2.705 15.498 8.660 2016.991 1.751 38.522 1.948 0.58 196283. 0.2587
|
|
97.84 0.7225 0.8042 0.0731 0.0656 2.610 14.956 8.046 1946.438 1.690 35.788 1.875 0.58 197202. 0.2400
|
|
103.28 0.7627 0.8174 0.0671 0.0626 2.491 14.272 7.393 1857.413 1.612 32.882 1.805 0.58 198165. 0.2215
|
|
108.71 0.8028 0.8282 0.0609 0.0591 2.348 13.456 6.709 1751.182 1.520 29.841 1.738 0.59 199170. 0.2031
|
|
114.15 0.8430 0.8363 0.0545 0.0549 2.184 12.515 6.001 1628.798 1.414 26.692 1.671 0.59 200216. 0.1848
|
|
119.59 0.8831 0.8410 0.0479 0.0503 2.000 11.458 5.274 1491.116 1.294 23.459 1.604 0.59 201303. 0.1663
|
|
125.02 0.9232 0.8415 0.0412 0.0451 1.795 10.288 4.532 1338.868 1.162 20.159 1.535 0.59 202430. 0.1475
|
|
130.46 0.9634 0.8360 0.0343 0.0395 1.573 9.011 3.779 1172.745 1.018 16.811 1.462 0.59 203596. 0.1283
|
|
135.89 1.0035 0.8212 0.0274 0.0335 1.332 7.634 3.019 993.492 0.862 13.429 1.378 0.60 204802. 0.1081
|
|
141.33 1.0437 0.7903 0.0205 0.0270 1.076 6.163 2.255 802.007 0.696 10.032 1.276 0.60 206045. 0.0865
|
|
146.76 1.0838 0.7266 0.0136 0.0202 0.804 4.606 1.492 599.437 0.520 6.638 1.129 0.60 207324. 0.0623
|
|
152.20 1.1239 0.5748 0.0067 0.0131 0.519 2.975 0.735 387.208 0.336 3.271 0.861 0.60 208636. 0.0333
|
|
157.64 1.1641 -0.0336 -0.0002 0.0056 0.221 1.266 -0.018 164.783 0.143 -0.079 -0.049 0.60 209887. 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 0.1064 0.0480 2.479 13.019 13.945 1848.370 1.471 62.025 3.422 0.62 204641. 0.5767
|
|
5.93 0.0402 0.0866 0.1063 0.0493 2.544 13.361 13.927 1896.922 1.510 61.949 3.330 0.62 204847. 0.5610
|
|
11.87 0.0803 0.1682 0.1061 0.0507 2.617 13.747 13.911 1951.713 1.553 61.875 3.233 0.62 205086. 0.5442
|
|
17.80 0.1205 0.2443 0.1060 0.0523 2.699 14.178 13.893 2012.874 1.602 61.796 3.131 0.62 205361. 0.5267
|
|
23.74 0.1607 0.3147 0.1058 0.0540 2.790 14.653 13.873 2080.363 1.655 61.706 3.025 0.62 205675. 0.5085
|
|
29.67 0.2009 0.3793 0.1056 0.0559 2.888 15.171 13.847 2153.836 1.714 61.591 2.916 0.62 206032. 0.4898
|
|
35.61 0.2410 0.4380 0.1054 0.0580 2.994 15.725 13.812 2232.554 1.777 61.435 2.806 0.62 206432. 0.4707
|
|
41.54 0.2812 0.4910 0.1050 0.0601 3.105 16.308 13.762 2315.273 1.842 61.213 2.696 0.62 206878. 0.4514
|
|
47.47 0.3214 0.5385 0.1045 0.0623 3.219 16.905 13.691 2400.141 1.910 60.896 2.587 0.62 207372. 0.4321
|
|
53.41 0.3615 0.5808 0.1037 0.0645 3.332 17.500 13.589 2484.608 1.977 60.444 2.481 0.62 207917. 0.4128
|
|
59.34 0.4017 0.6185 0.1026 0.0666 3.440 18.069 13.447 2565.382 2.041 59.813 2.378 0.62 208511. 0.3935
|
|
65.28 0.4419 0.6520 0.1011 0.0685 3.538 18.584 13.253 2638.402 2.100 58.951 2.278 0.62 209158. 0.3744
|
|
71.21 0.4820 0.6818 0.0991 0.0701 3.619 19.009 12.995 2698.828 2.148 57.801 2.184 0.63 209857. 0.3553
|
|
77.15 0.5222 0.7084 0.0966 0.0712 3.676 19.308 12.658 2741.209 2.181 56.304 2.094 0.63 210609. 0.3363
|
|
83.08 0.5624 0.7322 0.0933 0.0717 3.701 19.442 12.233 2760.206 2.197 54.414 2.010 0.63 211413. 0.3174
|
|
89.01 0.6026 0.7536 0.0894 0.0715 3.690 19.383 11.717 2751.917 2.190 52.118 1.931 0.63 212269. 0.2984
|
|
94.95 0.6427 0.7730 0.0848 0.0705 3.641 19.122 11.116 2714.798 2.160 49.442 1.857 0.63 213176. 0.2795
|
|
100.88 0.6829 0.7905 0.0797 0.0688 3.553 18.661 10.440 2649.375 2.108 46.438 1.787 0.63 214133. 0.2607
|
|
106.82 0.7231 0.8060 0.0740 0.0664 3.429 18.012 9.704 2557.277 2.035 43.165 1.721 0.63 215138. 0.2420
|
|
112.75 0.7632 0.8195 0.0681 0.0634 3.273 17.189 8.920 2440.408 1.942 39.677 1.658 0.64 216190. 0.2235
|
|
118.69 0.8034 0.8307 0.0618 0.0598 3.085 16.204 8.098 2300.507 1.831 36.019 1.597 0.64 217289. 0.2051
|
|
124.62 0.8436 0.8393 0.0553 0.0556 2.868 15.066 7.245 2139.013 1.702 32.226 1.536 0.64 218432. 0.1866
|
|
130.55 0.8838 0.8448 0.0486 0.0508 2.625 13.785 6.369 1957.094 1.557 28.327 1.476 0.64 219620. 0.1681
|
|
136.49 0.9239 0.8461 0.0418 0.0456 2.354 12.367 5.473 1755.744 1.397 24.345 1.414 0.65 220852. 0.1493
|
|
142.42 0.9641 0.8415 0.0348 0.0399 2.060 10.818 4.564 1535.891 1.222 20.301 1.348 0.65 222127. 0.1300
|
|
148.36 1.0043 0.8281 0.0278 0.0337 1.741 9.146 3.645 1298.523 1.033 16.213 1.273 0.65 223444. 0.1097
|
|
154.29 1.0444 0.7990 0.0208 0.0271 1.401 7.359 2.721 1044.838 0.831 12.103 1.181 0.65 224802. 0.0879
|
|
160.23 1.0846 0.7377 0.0137 0.0202 1.041 5.468 1.798 776.365 0.618 7.996 1.050 0.65 226200. 0.0636
|
|
166.16 1.1248 0.5879 0.0067 0.0129 0.664 3.487 0.881 495.056 0.394 3.918 0.807 0.66 227633. 0.0342
|
|
172.09 1.1649 -0.0574 -0.0003 0.0052 0.268 1.407 -0.034 199.703 0.159 -0.149 -0.076 0.66 228973. 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 0.1066 0.0486 3.188 15.455 16.391 2377.005 1.746 72.909 3.128 0.67 221691. 0.5716
|
|
6.47 0.0405 0.0865 0.1064 0.0498 3.270 15.852 16.373 2438.159 1.791 72.828 3.046 0.67 221915. 0.5563
|
|
12.95 0.0809 0.1680 0.1063 0.0512 3.362 16.302 16.356 2507.393 1.842 72.751 2.959 0.67 222176. 0.5401
|
|
19.42 0.1214 0.2441 0.1062 0.0528 3.466 16.807 16.339 2584.934 1.899 72.674 2.867 0.67 222477. 0.5230
|
|
25.90 0.1618 0.3147 0.1061 0.0546 3.582 17.365 16.319 2670.795 1.962 72.588 2.771 0.67 222821. 0.5053
|
|
32.37 0.2023 0.3794 0.1059 0.0565 3.707 17.975 16.295 2764.622 2.031 72.481 2.673 0.67 223210. 0.4871
|
|
38.85 0.2427 0.4384 0.1057 0.0585 3.843 18.631 16.262 2865.556 2.105 72.332 2.574 0.67 223648. 0.4685
|
|
45.32 0.2832 0.4916 0.1054 0.0607 3.986 19.324 16.213 2972.074 2.183 72.115 2.474 0.67 224137. 0.4497
|
|
51.80 0.3236 0.5394 0.1049 0.0630 4.133 20.037 16.140 3081.840 2.264 71.791 2.375 0.67 224678. 0.4307
|
|
58.27 0.3641 0.5821 0.1042 0.0652 4.280 20.751 16.033 3191.557 2.344 71.316 2.279 0.67 225274. 0.4118
|
|
64.74 0.4046 0.6201 0.1032 0.0674 4.421 21.436 15.879 3296.902 2.422 70.631 2.185 0.68 225927. 0.3929
|
|
71.22 0.4450 0.6538 0.1018 0.0693 4.549 22.057 15.663 3392.481 2.492 69.670 2.094 0.68 226636. 0.3741
|
|
77.69 0.4855 0.6839 0.0999 0.0709 4.656 22.573 15.369 3471.833 2.550 68.359 2.008 0.68 227403. 0.3553
|
|
84.17 0.5259 0.7106 0.0974 0.0721 4.731 22.936 14.978 3527.646 2.591 66.623 1.926 0.68 228228. 0.3364
|
|
90.64 0.5664 0.7346 0.0941 0.0726 4.764 23.099 14.479 3552.715 2.610 64.403 1.849 0.68 229111. 0.3175
|
|
97.12 0.6068 0.7561 0.0902 0.0724 4.750 23.027 13.868 3541.733 2.602 61.683 1.776 0.68 230051. 0.2985
|
|
103.59 0.6473 0.7756 0.0855 0.0713 4.684 22.707 13.151 3492.533 2.565 58.495 1.708 0.68 231047. 0.2795
|
|
110.07 0.6877 0.7932 0.0802 0.0696 4.567 22.143 12.343 3405.736 2.502 54.903 1.644 0.69 232098. 0.2607
|
|
116.54 0.7282 0.8089 0.0745 0.0671 4.403 21.349 11.462 3283.525 2.412 50.981 1.583 0.69 233202. 0.2419
|
|
123.01 0.7687 0.8226 0.0684 0.0639 4.195 20.341 10.521 3128.498 2.298 46.796 1.525 0.69 234357. 0.2233
|
|
129.49 0.8091 0.8340 0.0620 0.0601 3.947 19.135 9.533 2943.014 2.162 42.401 1.469 0.69 235564. 0.2047
|
|
135.96 0.8496 0.8428 0.0553 0.0558 3.660 17.743 8.508 2729.009 2.005 37.842 1.414 0.69 236819. 0.1862
|
|
142.44 0.8900 0.8485 0.0485 0.0508 3.337 16.177 7.453 2488.049 1.828 33.153 1.359 0.70 238124. 0.1674
|
|
148.91 0.9305 0.8499 0.0415 0.0454 2.979 14.443 6.376 2221.461 1.632 28.361 1.302 0.70 239476. 0.1484
|
|
155.39 0.9709 0.8453 0.0343 0.0394 2.589 12.552 5.282 1930.498 1.418 23.492 1.241 0.70 240875. 0.1287
|
|
161.86 1.0114 0.8312 0.0271 0.0330 2.168 10.510 4.175 1616.543 1.187 18.571 1.171 0.70 242320. 0.1080
|
|
168.34 1.0518 0.8000 0.0199 0.0262 1.718 8.331 3.063 1281.380 0.941 13.623 1.084 0.71 243811. 0.0856
|
|
174.81 1.0923 0.7312 0.0127 0.0189 1.244 6.030 1.951 927.402 0.681 8.678 0.954 0.71 245344. 0.0602
|
|
181.28 1.1328 0.5479 0.0055 0.0114 0.748 3.626 0.848 557.670 0.410 3.770 0.689 0.71 246913. 0.0286
|
|
187.76 1.1732
|
|
|
|
|
|
|
|
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 0.1067 0.0498 4.085 18.391 19.039 3046.160 2.078 84.683 2.835 0.72 238740. 0.5583
|
|
6.92 0.0402 0.0839 0.1066 0.0510 4.184 18.839 19.019 3120.361 2.128 84.596 2.765 0.72 238979. 0.5442
|
|
13.85 0.0804 0.1633 0.1065 0.0524 4.297 19.347 19.001 3204.526 2.186 84.518 2.689 0.72 239258. 0.5292
|
|
20.77 0.1205 0.2377 0.1064 0.0540 4.424 19.917 18.985 3298.986 2.250 84.445 2.610 0.72 239578. 0.5133
|
|
27.70 0.1607 0.3069 0.1063 0.0557 4.565 20.550 18.968 3403.840 2.322 84.369 2.528 0.72 239945. 0.4968
|
|
34.62 0.2009 0.3707 0.1062 0.0576 4.719 21.244 18.947 3518.770 2.400 84.277 2.442 0.72 240359. 0.4798
|
|
41.55 0.2411 0.4290 0.1060 0.0596 4.885 21.993 18.919 3642.870 2.485 84.151 2.356 0.72 240825. 0.4625
|
|
48.47 0.2812 0.4820 0.1058 0.0617 5.062 22.787 18.876 3774.423 2.575 83.962 2.268 0.72 241344. 0.4448
|
|
55.40 0.3214 0.5298 0.1054 0.0640 5.244 23.610 18.811 3910.684 2.667 83.670 2.182 0.73 241920. 0.4271
|
|
62.32 0.3616 0.5728 0.1049 0.0662 5.428 24.437 18.710 4047.672 2.761 83.223 2.097 0.73 242553. 0.4093
|
|
69.24 0.4018 0.6114 0.1040 0.0684 5.606 25.236 18.560 4180.058 2.851 82.556 2.014 0.73 243245. 0.3916
|
|
76.17 0.4419 0.6459 0.1028 0.0704 5.768 25.967 18.342 4301.146 2.934 81.587 1.934 0.73 243998. 0.3739
|
|
83.09 0.4821 0.6769 0.1011 0.0720 5.904 26.582 18.037 4402.945 3.003 80.228 1.858 0.73 244813. 0.3562
|
|
90.02 0.5223 0.7046 0.0988 0.0732 6.003 27.026 17.622 4476.438 3.053 78.384 1.786 0.73 245689. 0.3383
|
|
96.94 0.5625 0.7296 0.0957 0.0738 6.051 27.244 17.081 4512.595 3.078 75.976 1.717 0.73 246628. 0.3203
|
|
103.87 0.6027 0.7522 0.0920 0.0737 6.041 27.195 16.405 4504.447 3.072 72.971 1.652 0.74 247628. 0.3020
|
|
110.79 0.6428 0.7726 0.0875 0.0728 5.966 26.859 15.602 4448.786 3.034 69.396 1.591 0.74 248687. 0.2836
|
|
117.72 0.6830 0.7909 0.0823 0.0711 5.828 26.238 14.685 4345.942 2.964 65.320 1.533 0.74 249806. 0.2651
|
|
124.64 0.7232 0.8073 0.0767 0.0687 5.630 25.346 13.675 4198.299 2.864 60.828 1.477 0.74 250980. 0.2466
|
|
131.56 0.7634 0.8216 0.0706 0.0656 5.376 24.203 12.590 4008.851 2.734 56.003 1.425 0.74 252211. 0.2281
|
|
138.49 0.8035 0.8338 0.0642 0.0618 5.070 22.823 11.446 3780.354 2.579 50.913 1.373 0.75 253495. 0.2097
|
|
145.41 0.8437 0.8435 0.0575 0.0575 4.714 21.222 10.255 3515.168 2.398 45.614 1.323 0.75 254831. 0.1913
|
|
152.34 0.8839 0.8504 0.0506 0.0526 4.312 19.412 9.026 3215.313 2.193 40.148 1.273 0.75 256220. 0.1727
|
|
159.26 0.9241 0.8534 0.0435 0.0471 3.866 17.403 7.768 2882.617 1.966 34.551 1.222 0.75 257659. 0.1538
|
|
166.19 0.9642 0.8509 0.0364 0.0412 3.378 15.207 6.486 2518.884 1.718 28.852 1.168 0.76 259149. 0.1343
|
|
173.11 1.0044 0.8400 0.0291 0.0348 2.851 12.836 5.188 2126.140 1.450 23.078 1.107 0.76 260687. 0.1138
|
|
180.03 1.0446 0.8137 0.0218 0.0279 2.289 10.306 3.880 1707.035 1.164 17.259 1.031 0.76 262273. 0.0917
|
|
186.96 1.0848 0.7550 0.0144 0.0207 1.697 7.638 2.569 1265.145 0.863 11.428 0.921 0.76 263905. 0.0666
|
|
193.88 1.1250 0.6052 0.0071 0.0132 1.080 4.861 1.264 805.136 0.549 5.622 0.712 0.77 265578. 0.0361
|
|
200.81 1.1651 -0.0527 -0.0002 0.0053 0.438 1.973 -0.043 326.876 0.223 -0.192 -0.060 0.77 267126. 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 0.1069 0.0523 5.274 22.161 21.882 3932.895 2.504 97.333 2.524 0.77 255787. 0.5328
|
|
7.41 0.0401 0.0801 0.1067 0.0535 5.393 22.662 21.861 4021.836 2.560 97.236 2.465 0.77 256043. 0.5203
|
|
14.82 0.0803 0.1561 0.1067 0.0548 5.529 23.233 21.842 4123.055 2.625 97.152 2.403 0.77 256341. 0.5068
|
|
22.23 0.1204 0.2277 0.1066 0.0563 5.682 23.875 21.825 4237.015 2.697 97.080 2.336 0.77 256684. 0.4927
|
|
29.64 0.1605 0.2945 0.1065 0.0580 5.852 24.590 21.810 4363.926 2.778 97.011 2.267 0.77 257075. 0.4778
|
|
37.05 0.2006 0.3565 0.1064 0.0599 6.039 25.377 21.793 4503.518 2.867 96.936 2.195 0.78 257518. 0.4625
|
|
44.46 0.2408 0.4134 0.1063 0.0619 6.242 26.229 21.770 4654.836 2.963 96.834 2.121 0.78 258015. 0.4467
|
|
51.87 0.2809 0.4655 0.1061 0.0640 6.458 27.137 21.735 4815.941 3.066 96.679 2.047 0.78 258570. 0.4308
|
|
59.28 0.3210 0.5127 0.1059 0.0663 6.683 28.081 21.679 4983.529 3.173 96.429 1.973 0.78 259184. 0.4147
|
|
66.69 0.3611 0.5556 0.1054 0.0685 6.910 29.034 21.589 5152.604 3.280 96.027 1.900 0.78 259859. 0.3985
|
|
74.09 0.4013 0.5944 0.1047 0.0707 7.129 29.956 21.447 5316.237 3.384 95.397 1.830 0.78 260598. 0.3825
|
|
81.50 0.4414 0.6296 0.1037 0.0727 7.329 30.798 21.233 5465.579 3.479 94.444 1.762 0.78 261401. 0.3665
|
|
88.91 0.4815 0.6617 0.1022 0.0743 7.496 31.499 20.921 5590.099 3.559 93.056 1.697 0.78 262271. 0.3504
|
|
96.32 0.5216 0.6910 0.1000 0.0755 7.615 31.996 20.484 5678.197 3.615 91.113 1.636 0.78 263207. 0.3343
|
|
103.73 0.5618 0.7178 0.0972 0.0760 7.669 32.223 19.899 5718.504 3.641 88.512 1.578 0.79 264210. 0.3178
|
|
111.14 0.6019 0.7423 0.0935 0.0758 7.647 32.132 19.154 5702.444 3.630 85.199 1.524 0.79 265278. 0.3010
|
|
118.55 0.6420 0.7648 0.0891 0.0748 7.545 31.703 18.254 5626.315 3.582 81.194 1.472 0.79 266412. 0.2838
|
|
125.96 0.6821 0.7852 0.0841 0.0730 7.364 30.941 17.215 5491.076 3.496 76.571 1.422 0.79 267608. 0.2663
|
|
133.37 0.7223 0.8035 0.0784 0.0705 7.108 29.866 16.059 5300.307 3.374 71.430 1.374 0.79 268865. 0.2486
|
|
140.78 0.7624 0.8195 0.0723 0.0673 6.783 28.503 14.809 5058.273 3.220 65.869 1.328 0.80 270182. 0.2306
|
|
148.19 0.8025 0.8332 0.0658 0.0634 6.395 26.871 13.484 4768.779 3.036 59.975 1.282 0.80 271556. 0.2126
|
|
155.60 0.8426 0.8441 0.0591 0.0590 5.947 24.989 12.099 4434.702 2.823 53.816 1.237 0.80 272987. 0.1943
|
|
163.01 0.8828 0.8519 0.0521 0.0540 5.443 22.869 10.667 4058.541 2.584 47.445 1.192 0.80 274472. 0.1757
|
|
170.42 0.9229 0.8556 0.0449 0.0484 4.884 20.523 9.196 3642.128 2.319 40.906 1.145 0.81 276012. 0.1568
|
|
177.83 0.9630 0.8537 0.0376 0.0424 4.275 17.963 7.696 3187.819 2.029 34.233 1.095 0.81 277605. 0.1371
|
|
185.24 1.0031 0.8425 0.0301 0.0359 3.619 15.208 6.174 2698.941 1.718 27.461 1.038 0.81 279251. 0.1164
|
|
192.65 1.0433 0.8146 0.0226 0.0290 2.924 12.284 4.636 2180.067 1.388 20.621 0.965 0.82 280947. 0.0937
|
|
200.06 1.0834 0.7512 0.0151 0.0218 2.196 9.226 3.092 1637.252 1.042 13.753 0.857 0.82 282693. 0.0680
|
|
207.47 1.1235 0.5935 0.0076 0.0143 1.446 6.075 1.551 1078.077 0.686 6.899 0.653 0.82 284482. 0.0367
|
|
214.87 1.1636 0.0106 0.0001 0.0067 0.680 2.858 0.013 507.175 0.323 0.056 0.011 0.82 286203. 0.0001
|
|
|
|
|
|
|
|
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 0.1069 0.0566 6.923 27.270 24.916 5162.185 3.081 110.825 2.189 0.83 272832. 0.4932
|
|
7.91 0.0402 0.0744 0.1068 0.0577 7.064 27.826 24.889 5267.464 3.144 110.707 2.143 0.83 273106. 0.4826
|
|
15.83 0.0804 0.1453 0.1067 0.0590 7.225 28.461 24.867 5387.714 3.216 110.608 2.093 0.83 273424. 0.4712
|
|
23.74 0.1205 0.2124 0.1066 0.0605 7.407 29.180 24.849 5523.704 3.297 110.526 2.040 0.83 273790. 0.4591
|
|
31.66 0.1607 0.2754 0.1066 0.0622 7.611 29.983 24.833 5675.834 3.388 110.457 1.984 0.83 274208. 0.4464
|
|
39.57 0.2009 0.3341 0.1065 0.0640 7.837 30.872 24.818 5843.960 3.488 110.390 1.926 0.83 274681. 0.4331
|
|
47.48 0.2411 0.3885 0.1064 0.0660 8.083 31.839 24.799 6027.172 3.597 110.308 1.866 0.83 275213. 0.4195
|
|
55.40 0.2813 0.4385 0.1063 0.0682 8.346 32.876 24.772 6223.313 3.714 110.186 1.805 0.83 275805. 0.4056
|
|
63.31 0.3214 0.4842 0.1061 0.0704 8.621 33.960 24.726 6428.646 3.837 109.982 1.745 0.83 276460. 0.3915
|
|
71.23 0.3616 0.5260 0.1058 0.0727 8.900 35.061 24.649 6637.023 3.961 109.639 1.685 0.83 277180. 0.3775
|
|
79.14 0.4018 0.5642 0.1052 0.0749 9.172 36.130 24.522 6839.351 4.082 109.073 1.626 0.83 277968. 0.3635
|
|
87.06 0.4420 0.5994 0.1044 0.0770 9.419 37.102 24.319 7023.430 4.192 108.173 1.571 0.83 278826. 0.3496
|
|
94.97 0.4822 0.6320 0.1030 0.0786 9.621 37.899 24.011 7174.318 4.282 106.802 1.518 0.83 279754. 0.3357
|
|
102.88 0.5223 0.6625 0.1011 0.0797 9.757 38.436 23.563 7275.827 4.342 104.809 1.469 0.84 280753. 0.3218
|
|
110.80 0.5625 0.6913 0.0985 0.0801 9.806 38.630 22.944 7312.567 4.364 102.055 1.423 0.84 281825. 0.3077
|
|
118.71 0.6027 0.7184 0.0950 0.0797 9.754 38.424 22.135 7273.588 4.341 98.456 1.380 0.84 282967. 0.2931
|
|
126.63 0.6429 0.7438 0.0907 0.0784 9.595 37.798 21.138 7155.115 4.270 94.020 1.340 0.84 284180. 0.2781
|
|
134.54 0.6831 0.7676 0.0857 0.0763 9.334 36.770 19.970 6960.437 4.154 88.827 1.301 0.84 285460. 0.2625
|
|
142.45 0.7232 0.7893 0.0801 0.0734 8.980 35.374 18.659 6696.254 3.997 82.993 1.264 0.85 286807. 0.2464
|
|
150.37 0.7634 0.8088 0.0739 0.0698 8.542 33.648 17.229 6369.585 3.802 76.635 1.227 0.85 288216. 0.2299
|
|
158.28 0.8036 0.8257 0.0674 0.0656 8.028 31.624 15.705 5986.413 3.573 69.855 1.190 0.85 289688. 0.2128
|
|
166.20 0.8438 0.8397 0.0605 0.0608 7.444 29.325 14.105 5551.191 3.313 62.738 1.152 0.85 291220. 0.1954
|
|
174.11 0.8839 0.8499 0.0534 0.0555 6.798 26.777 12.444 5068.927 3.025 55.350 1.113 0.86 292810. 0.1773
|
|
182.03 0.9241 0.8550 0.0461 0.0498 6.093 24.004 10.734 4543.854 2.712 47.743 1.071 0.86 294459. 0.1584
|
|
189.94 0.9643 0.8520 0.0386 0.0436 5.340 21.036 8.983 3982.092 2.377 39.957 1.023 0.86 296164. 0.1384
|
|
197.85 1.0045 0.8368 0.0309 0.0371 4.541 17.888 7.202 3386.086 2.021 32.037 0.965 0.87 297925. 0.1169
|
|
205.77 1.0447 0.8004 0.0232 0.0303 3.703 14.586 5.402 2761.157 1.648 24.026 0.887 0.87 299740. 0.0931
|
|
213.68 1.0848 0.7207 0.0154 0.0232 2.839 11.185 3.592 2117.400 1.264 15.975 0.769 0.87 301607. 0.0658
|
|
221.60 1.1250 0.5368 0.0077 0.0161 1.967 7.748 1.787 1466.682 0.875 7.947 0.553 0.88 303522. 0.0333
|
|
229.51 1.1652 -0.0036 0.0000 0.0090 1.096 4.316 -0.006 816.942 0.488 -0.028 -0.004 0.88 305390. 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 0.1065 0.0620 9.105 33.757 28.012 6789.509 3.814 124.598 1.871 0.88 289890. 0.4470
|
|
8.44 0.0403 0.0679 0.1064 0.0631 9.266 34.355 27.977 6909.725 3.881 124.440 1.836 0.88 290182. 0.4384
|
|
16.87 0.0806 0.1330 0.1062 0.0644 9.452 35.045 27.947 7048.614 3.959 124.306 1.798 0.88 290522. 0.4291
|
|
25.31 0.1209 0.1950 0.1061 0.0658 9.665 35.834 27.922 7207.204 4.048 124.196 1.757 0.88 290912. 0.4191
|
|
33.75 0.1612 0.2535 0.1061 0.0675 9.905 36.724 27.901 7386.210 4.149 124.106 1.713 0.88 291358. 0.4085
|
|
42.18 0.2016 0.3083 0.1060 0.0693 10.173 37.716 27.884 7585.793 4.261 124.027 1.667 0.88 291862. 0.3974
|
|
50.62 0.2419 0.3593 0.1059 0.0713 10.467 38.807 27.866 7805.221 4.384 123.947 1.619 0.88 292429. 0.3858
|
|
59.05 0.2822 0.4065 0.1058 0.0735 10.785 39.987 27.842 8042.518 4.518 123.841 1.570 0.88 293060. 0.3740
|
|
67.49 0.3225 0.4499 0.1057 0.0758 11.122 41.236 27.804 8293.788 4.659 123.674 1.521 0.88 293758. 0.3619
|
|
75.93 0.3628 0.4897 0.1055 0.0781 11.469 42.521 27.740 8552.343 4.804 123.388 1.471 0.88 294526. 0.3497
|
|
84.36 0.4031 0.5262 0.1050 0.0805 11.811 43.791 27.631 8807.707 4.947 122.901 1.423 0.88 295366. 0.3376
|
|
92.80 0.4434 0.5601 0.1043 0.0826 12.127 44.960 27.448 9042.899 5.080 122.088 1.377 0.89 296279. 0.3256
|
|
101.24 0.4837 0.5917 0.1032 0.0844 12.390 45.937 27.159 9239.356 5.190 120.801 1.333 0.89 297267. 0.3136
|
|
109.67 0.5240 0.6217 0.1016 0.0856 12.570 46.604 26.721 9373.532 5.265 118.854 1.293 0.89 298332. 0.3017
|
|
118.11 0.5644 0.6504 0.0992 0.0861 12.634 46.841 26.093 9421.122 5.292 116.062 1.256 0.89 299475. 0.2896
|
|
126.54 0.6047 0.6784 0.0960 0.0855 12.557 46.556 25.246 9363.837 5.260 112.296 1.223 0.89 300694. 0.2773
|
|
134.98 0.6450 0.7057 0.0919 0.0840 12.330 45.716 24.176 9194.828 5.165 107.534 1.193 0.89 301989. 0.2647
|
|
143.42 0.6853 0.7322 0.0870 0.0815 11.959 44.339 22.896 8917.903 5.009 101.841 1.164 0.90 303358. 0.2515
|
|
151.85 0.7256 0.7574 0.0815 0.0781 11.460 42.488 21.436 8545.554 4.800 95.346 1.138 0.90 304798. 0.2378
|
|
160.29 0.7659 0.7810 0.0754 0.0739 10.851 40.231 19.827 8091.562 4.545 88.191 1.111 0.90 306307. 0.2234
|
|
168.73 0.8062 0.8023 0.0688 0.0691 10.148 37.626 18.098 7567.718 4.251 80.499 1.085 0.91 307882. 0.2083
|
|
177.16 0.8465 0.8209 0.0619 0.0638 9.364 34.716 16.271 6982.472 3.922 72.375 1.057 0.91 309521. 0.1924
|
|
185.60 0.8868 0.8358 0.0546 0.0579 8.506 31.535 14.365 6342.734 3.563 63.897 1.027 0.91 311223. 0.1757
|
|
194.03 0.9271 0.8443 0.0471 0.0517 7.595 28.159 12.393 5663.619 3.181 55.126 0.993 0.91 312987. 0.1577
|
|
202.47 0.9675 0.8421 0.0394 0.0453 6.647 24.645 10.368 4956.811 2.784 46.115 0.949 0.92 314812. 0.1379
|
|
210.91 1.0078 0.8180 0.0315 0.0388 5.702 21.141 8.294 4251.990 2.388 36.890 0.885 0.92 316695. 0.1150
|
|
219.34 1.0481 0.7656 0.0236 0.0322 4.733 17.548 6.196 3529.491 1.983 27.558 0.796 0.92 318636. 0.0894
|
|
227.78 1.0884 0.6616 0.0156 0.0256 3.758 13.934 4.094 2802.587 1.574 18.210 0.663 0.93 320634. 0.0605
|
|
236.22 1.1287 0.4538 0.0077 0.0191 2.798 10.375 2.016 2086.741 1.172 8.967 0.438 0.93 322683. 0.0281
|
|
244.65 1.1690 -0.0062 -0.0001 0.0127 1.865 6.915 -0.018 1390.888 0.781 -0.079 -0.006 0.94 324725. 0.0000
|
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PROP RPM = 18000
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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 0.1050 0.0676 11.786 41.268 30.950 8788.469 4.662 137.666 1.597 0.93 306973. 0.4011
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9.00 0.0406 0.0620 0.1048 0.0686 11.954 41.858 30.898 8914.226 4.729 137.436 1.572 0.93 307284. 0.3944
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18.00 0.0812 0.1219 0.1046 0.0697 12.152 42.553 30.853 9062.056 4.808 137.233 1.544 0.93 307647. 0.3871
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27.00 0.1218 0.1792 0.1045 0.0711 12.382 43.357 30.813 9233.431 4.898 137.055 1.514 0.93 308065. 0.3792
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36.00 0.1625 0.2336 0.1044 0.0726 12.645 44.278 30.778 9429.536 5.003 136.902 1.480 0.93 308541. 0.3707
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45.00 0.2031 0.2851 0.1043 0.0743 12.942 45.318 30.748 9651.002 5.120 136.766 1.445 0.93 309081. 0.3617
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54.00 0.2437 0.3332 0.1042 0.0762 13.273 46.476 30.719 9897.584 5.251 136.637 1.408 0.93 309688. 0.3522
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63.00 0.2843 0.3781 0.1041 0.0782 13.635 47.744 30.687 10167.699 5.394 136.494 1.369 0.93 310364. 0.3423
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72.00 0.3249 0.4195 0.1039 0.0805 14.024 49.106 30.644 10457.750 5.548 136.304 1.329 0.93 311112. 0.3321
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81.00 0.3655 0.4577 0.1037 0.0828 14.429 50.525 30.578 10759.953 5.708 136.010 1.289 0.93 311934. 0.3217
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90.00 0.4061 0.4929 0.1033 0.0851 14.833 51.941 30.469 11061.340 5.868 135.526 1.249 0.94 312834. 0.3113
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99.00 0.4468 0.5254 0.1027 0.0873 15.219 53.292 30.293 11349.122 6.021 134.745 1.211 0.94 313812. 0.3008
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108.00 0.4874 0.5556 0.1018 0.0893 15.557 54.474 30.015 11600.886 6.154 133.507 1.174 0.94 314869. 0.2902
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117.00 0.5280 0.5839 0.1003 0.0907 15.809 55.356 29.589 11788.667 6.254 131.611 1.138 0.94 316008. 0.2795
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125.99 0.5686 0.6108 0.0982 0.0914 15.934 55.794 28.967 11882.004 6.304 128.845 1.106 0.94 317229. 0.2686
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134.99 0.6092 0.6366 0.0953 0.0912 15.897 55.663 28.114 11854.093 6.289 125.051 1.076 0.95 318532. 0.2574
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143.99 0.6498 0.6618 0.0916 0.0899 15.674 54.883 27.016 11687.870 6.201 120.166 1.048 0.95 319917. 0.2460
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152.99 0.6904 0.6867 0.0871 0.0875 15.255 53.418 25.678 11375.979 6.035 114.216 1.024 0.95 321381. 0.2342
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161.99 0.7310 0.7113 0.0818 0.0841 14.649 51.294 24.123 10923.538 5.795 107.298 1.002 0.95 322924. 0.2220
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170.99 0.7717 0.7356 0.0759 0.0796 13.870 48.566 22.377 10342.694 5.487 99.531 0.981 0.96 324541. 0.2095
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179.99 0.8123 0.7591 0.0694 0.0743 12.942 45.318 20.468 9650.990 5.120 91.043 0.962 0.96 326231. 0.1964
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188.99 0.8529 0.7809 0.0625 0.0682 11.890 41.634 18.425 8866.332 4.704 81.954 0.943 0.96 327992. 0.1826
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197.99 0.8935 0.8003 0.0552 0.0616 10.734 37.587 16.271 8004.521 4.247 72.374 0.922 0.97 329820. 0.1679
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206.99 0.9341 0.8135 0.0476 0.0546 9.517 33.324 14.027 7096.824 3.765 62.391 0.896 0.97 331715. 0.1515
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215.99 0.9747 0.8150 0.0397 0.0475 8.275 28.975 11.710 6170.600 3.274 52.086 0.861 0.97 333675. 0.1329
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224.99 1.0153 0.7794 0.0316 0.0411 7.169 25.101 9.312 5345.632 2.836 41.421 0.790 0.98 335698. 0.1088
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233.99 1.0560 0.7048 0.0234 0.0350 6.103 21.370 6.894 4551.044 2.414 30.665 0.687 0.98 337782. 0.0814
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242.99 1.0966 0.5769 0.0153 0.0291 5.063 17.729 4.508 3775.573 2.003 20.053 0.542 0.98 339926. 0.0519
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251.99 1.1372 0.3606 0.0074 0.0234 4.072 14.258 2.185 3036.387 1.611 9.721 0.326 0.99 342126. 0.0218
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260.99 1.1778 -0.0131 -0.0002 0.0180 3.139 10.991 -0.059 2340.611 1.242 -0.262 -0.011 0.99 344349. 0.0000
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