538 lines
95 KiB
Plaintext
538 lines
95 KiB
Plaintext
16x8 (16x8.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 0.0946 0.0408 0.003 0.217 0.197 2.570 0.025 0.878 34.852 0.06 30478. 0.5680
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0.35 0.0228 0.0516 0.0929 0.0411 0.003 0.219 0.194 2.589 0.025 0.863 34.000 0.06 30498. 0.5493
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0.69 0.0457 0.1006 0.0912 0.0414 0.003 0.220 0.190 2.605 0.025 0.847 33.146 0.06 30519. 0.5304
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1.04 0.0685 0.1470 0.0893 0.0416 0.004 0.221 0.186 2.619 0.025 0.829 32.292 0.06 30542. 0.5114
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1.38 0.0914 0.1908 0.0873 0.0418 0.004 0.222 0.182 2.630 0.025 0.811 31.439 0.06 30567. 0.4923
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1.73 0.1142 0.2320 0.0852 0.0419 0.004 0.223 0.178 2.637 0.025 0.791 30.587 0.06 30593. 0.4731
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2.08 0.1370 0.2707 0.0829 0.0420 0.004 0.223 0.173 2.641 0.025 0.770 29.738 0.06 30621. 0.4538
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2.42 0.1599 0.3068 0.0805 0.0419 0.004 0.223 0.168 2.639 0.025 0.748 28.890 0.06 30651. 0.4344
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2.77 0.1827 0.3403 0.0779 0.0418 0.004 0.223 0.163 2.633 0.025 0.724 28.044 0.06 30683. 0.4149
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3.11 0.2055 0.3713 0.0753 0.0417 0.004 0.222 0.157 2.621 0.025 0.699 27.199 0.06 30717. 0.3954
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3.46 0.2284 0.3998 0.0724 0.0414 0.003 0.220 0.151 2.603 0.025 0.673 26.353 0.06 30752. 0.3759
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3.81 0.2512 0.4256 0.0694 0.0410 0.003 0.218 0.145 2.579 0.025 0.645 25.506 0.06 30790. 0.3562
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4.15 0.2741 0.4488 0.0663 0.0405 0.003 0.215 0.139 2.548 0.024 0.616 24.655 0.06 30829. 0.3365
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4.50 0.2969 0.4693 0.0631 0.0399 0.003 0.212 0.132 2.511 0.024 0.586 23.797 0.06 30871. 0.3168
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4.84 0.3197 0.4870 0.0597 0.0392 0.003 0.209 0.125 2.467 0.024 0.555 22.931 0.06 30915. 0.2970
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5.19 0.3426 0.5018 0.0563 0.0384 0.003 0.204 0.117 2.417 0.023 0.523 22.051 0.06 30960. 0.2772
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5.54 0.3654 0.5134 0.0527 0.0375 0.003 0.199 0.110 2.359 0.023 0.489 21.153 0.06 31008. 0.2573
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5.88 0.3882 0.5217 0.0490 0.0365 0.003 0.194 0.102 2.295 0.022 0.455 20.231 0.06 31058. 0.2374
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6.23 0.4111 0.5264 0.0452 0.0353 0.003 0.188 0.094 2.223 0.021 0.420 19.278 0.06 31110. 0.2173
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6.57 0.4339 0.5271 0.0414 0.0341 0.003 0.181 0.086 2.145 0.020 0.385 18.286 0.06 31165. 0.1972
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6.92 0.4568 0.5231 0.0375 0.0327 0.003 0.174 0.078 2.059 0.020 0.348 17.243 0.06 31221. 0.1769
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7.27 0.4796 0.5140 0.0335 0.0312 0.003 0.166 0.070 1.966 0.019 0.311 16.134 0.06 31280. 0.1565
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7.61 0.5024 0.4986 0.0294 0.0297 0.003 0.158 0.061 1.866 0.018 0.273 14.941 0.06 31340. 0.1358
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7.96 0.5253 0.4758 0.0253 0.0279 0.002 0.149 0.053 1.758 0.017 0.235 13.638 0.06 31404. 0.1150
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8.30 0.5481 0.4439 0.0212 0.0261 0.002 0.139 0.044 1.644 0.016 0.197 12.192 0.06 31469. 0.0940
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8.65 0.5710 0.4002 0.0170 0.0242 0.002 0.129 0.035 1.522 0.015 0.157 10.553 0.06 31536. 0.0728
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9.00 0.5938 0.3413 0.0127 0.0221 0.002 0.118 0.027 1.393 0.013 0.118 8.653 0.06 31606. 0.0517
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9.34 0.6166 0.2616 0.0085 0.0200 0.002 0.106 0.018 1.257 0.012 0.079 6.388 0.06 31678. 0.0312
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9.69 0.6395 0.1526 0.0042 0.0177 0.001 0.094 0.009 1.115 0.011 0.039 3.593 0.06 31752. 0.0124
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10.03 0.6623 -0.0006 0.0000 0.0154 0.001 0.082 0.000 0.967 0.009 0.000 -0.015 0.06 31827. 0.0000
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PROP RPM = 2000
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V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
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(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
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0.00 0.0000 0.0000 0.0950 0.0363 0.024 0.772 0.794 18.256 0.087 3.531 19.721 0.13 60955. 0.6444
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0.71 0.0233 0.0594 0.0933 0.0366 0.025 0.779 0.780 18.431 0.088 3.469 19.191 0.13 60996. 0.6215
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1.41 0.0466 0.1156 0.0916 0.0369 0.025 0.786 0.765 18.589 0.089 3.402 18.665 0.13 61039. 0.5986
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2.12 0.0699 0.1686 0.0897 0.0372 0.025 0.791 0.749 18.724 0.089 3.331 18.142 0.13 61087. 0.5758
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2.83 0.0933 0.2184 0.0876 0.0374 0.025 0.796 0.732 18.834 0.090 3.255 17.626 0.13 61137. 0.5530
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3.53 0.1166 0.2650 0.0854 0.0376 0.025 0.799 0.714 18.913 0.090 3.174 17.115 0.13 61191. 0.5302
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4.24 0.1399 0.3087 0.0831 0.0377 0.025 0.801 0.694 18.958 0.091 3.088 16.610 0.13 61249. 0.5075
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4.95 0.1632 0.3493 0.0806 0.0377 0.025 0.801 0.674 18.964 0.091 2.996 16.112 0.13 61311. 0.4850
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5.65 0.1865 0.3870 0.0780 0.0376 0.025 0.800 0.652 18.927 0.090 2.899 15.620 0.13 61377. 0.4625
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6.36 0.2098 0.4218 0.0753 0.0374 0.025 0.796 0.629 18.842 0.090 2.796 15.133 0.13 61446. 0.4400
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7.06 0.2331 0.4538 0.0723 0.0372 0.025 0.791 0.604 18.706 0.089 2.688 14.652 0.13 61520. 0.4177
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7.77 0.2564 0.4829 0.0693 0.0368 0.025 0.782 0.579 18.515 0.088 2.574 14.176 0.13 61597. 0.3955
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8.48 0.2798 0.5093 0.0661 0.0363 0.024 0.772 0.552 18.267 0.087 2.455 13.702 0.13 61679. 0.3733
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9.18 0.3031 0.5327 0.0627 0.0357 0.024 0.759 0.524 17.962 0.086 2.331 13.231 0.13 61765. 0.3512
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9.89 0.3264 0.5533 0.0593 0.0350 0.024 0.744 0.495 17.597 0.084 2.202 12.761 0.13 61855. 0.3293
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10.60 0.3497 0.5709 0.0557 0.0341 0.023 0.726 0.465 17.173 0.082 2.069 12.288 0.13 61950. 0.3074
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11.30 0.3730 0.5853 0.0520 0.0332 0.022 0.705 0.435 16.687 0.080 1.933 11.811 0.13 62049. 0.2855
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12.01 0.3963 0.5963 0.0482 0.0321 0.022 0.682 0.403 16.140 0.077 1.793 11.325 0.13 62153. 0.2637
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12.72 0.4196 0.6036 0.0444 0.0309 0.021 0.656 0.371 15.530 0.074 1.649 10.827 0.13 62261. 0.2418
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13.42 0.4430 0.6068 0.0404 0.0295 0.020 0.628 0.338 14.856 0.071 1.502 10.312 0.13 62373. 0.2198
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14.13 0.4663 0.6052 0.0364 0.0280 0.019 0.597 0.304 14.117 0.067 1.353 9.771 0.13 62490. 0.1976
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14.84 0.4896 0.5981 0.0323 0.0264 0.018 0.563 0.270 13.314 0.064 1.201 9.196 0.13 62612. 0.1752
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15.54 0.5129 0.5842 0.0282 0.0247 0.017 0.526 0.235 12.445 0.059 1.046 8.573 0.13 62738. 0.1525
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16.25 0.5362 0.5617 0.0240 0.0229 0.015 0.486 0.200 11.510 0.055 0.890 7.885 0.13 62869. 0.1293
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16.96 0.5595 0.5279 0.0197 0.0209 0.014 0.444 0.165 10.511 0.050 0.732 7.102 0.13 63004. 0.1057
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17.66 0.5828 0.4787 0.0154 0.0188 0.013 0.399 0.129 9.448 0.045 0.573 6.183 0.13 63144. 0.0814
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18.37 0.6062 0.4074 0.0111 0.0165 0.011 0.352 0.093 8.323 0.040 0.413 5.059 0.13 63289. 0.0565
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19.07 0.6295 0.3018 0.0068 0.0142 0.010 0.302 0.057 7.139 0.034 0.253 3.610 0.13 63438. 0.0316
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19.78 0.6528 0.1391 0.0025 0.0117 0.008 0.249 0.021 5.898 0.028 0.093 1.603 0.13 63591. 0.0085
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20.49 0.6761
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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 0.0954 0.0344 0.078 1.649 1.793 58.520 0.186 7.977 13.899 0.19 91430. 0.6826
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1.05 0.0232 0.0625 0.0938 0.0348 0.079 1.666 1.762 59.142 0.188 7.838 13.515 0.19 91491. 0.6579
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2.11 0.0464 0.1214 0.0920 0.0351 0.080 1.682 1.729 59.705 0.190 7.690 13.134 0.19 91557. 0.6333
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3.16 0.0696 0.1769 0.0901 0.0354 0.081 1.696 1.693 60.195 0.192 7.531 12.758 0.19 91627. 0.6088
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4.22 0.0928 0.2291 0.0880 0.0357 0.081 1.707 1.655 60.598 0.193 7.361 12.388 0.19 91703. 0.5844
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5.27 0.1160 0.2779 0.0859 0.0358 0.082 1.716 1.614 60.899 0.194 7.180 12.023 0.19 91784. 0.5602
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6.33 0.1392 0.3235 0.0836 0.0360 0.082 1.721 1.571 61.085 0.194 6.987 11.664 0.19 91870. 0.5361
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7.38 0.1624 0.3660 0.0811 0.0360 0.082 1.723 1.525 61.140 0.195 6.782 11.312 0.19 91962. 0.5123
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8.44 0.1856 0.4055 0.0785 0.0359 0.082 1.720 1.476 61.050 0.194 6.565 10.966 0.19 92060. 0.4886
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9.49 0.2088 0.4421 0.0758 0.0358 0.082 1.713 1.424 60.800 0.194 6.335 10.625 0.19 92163. 0.4650
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10.54 0.2320 0.4757 0.0729 0.0355 0.081 1.701 1.370 60.375 0.192 6.093 10.291 0.19 92273. 0.4417
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11.60 0.2552 0.5065 0.0698 0.0352 0.080 1.684 1.312 59.765 0.190 5.838 9.961 0.19 92388. 0.4185
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12.65 0.2784 0.5345 0.0666 0.0347 0.079 1.661 1.253 58.961 0.188 5.571 9.635 0.19 92510. 0.3955
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13.71 0.3016 0.5597 0.0633 0.0341 0.078 1.633 1.190 57.960 0.184 5.294 9.314 0.19 92638. 0.3726
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14.76 0.3248 0.5821 0.0599 0.0334 0.076 1.599 1.126 56.757 0.181 5.006 8.994 0.19 92773. 0.3499
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15.82 0.3480 0.6016 0.0563 0.0326 0.074 1.559 1.059 55.349 0.176 4.709 8.676 0.19 92914. 0.3274
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16.87 0.3712 0.6181 0.0527 0.0316 0.072 1.514 0.990 53.732 0.171 4.403 8.357 0.19 93061. 0.3049
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17.93 0.3944 0.6314 0.0489 0.0306 0.070 1.462 0.919 51.902 0.165 4.090 8.035 0.19 93215. 0.2825
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18.98 0.4176 0.6413 0.0451 0.0293 0.067 1.405 0.847 49.856 0.159 3.768 7.707 0.19 93376. 0.2602
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20.03 0.4408 0.6474 0.0411 0.0280 0.064 1.341 0.773 47.591 0.151 3.440 7.371 0.19 93543. 0.2377
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21.09 0.4640 0.6491 0.0371 0.0265 0.060 1.271 0.698 45.103 0.144 3.105 7.021 0.19 93717. 0.2151
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22.14 0.4872 0.6457 0.0331 0.0250 0.057 1.194 0.622 42.391 0.135 2.765 6.652 0.19 93898. 0.1923
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23.20 0.5104 0.6361 0.0289 0.0232 0.053 1.112 0.544 39.453 0.126 2.420 6.254 0.19 94086. 0.1692
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24.25 0.5336 0.6184 0.0248 0.0214 0.049 1.022 0.465 36.289 0.116 2.070 5.816 0.19 94281. 0.1455
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25.31 0.5568 0.5902 0.0205 0.0194 0.044 0.927 0.386 32.902 0.105 1.716 5.320 0.19 94482. 0.1212
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26.36 0.5800 0.5472 0.0163 0.0172 0.039 0.825 0.306 29.294 0.093 1.360 4.735 0.19 94690. 0.0960
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27.42 0.6032 0.4822 0.0120 0.0150 0.034 0.718 0.225 25.470 0.081 1.002 4.012 0.19 94905. 0.0698
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28.47 0.6264 0.3819 0.0077 0.0126 0.029 0.604 0.145 21.441 0.068 0.643 3.060 0.19 95127. 0.0427
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29.53 0.6496 0.2186 0.0034 0.0101 0.023 0.485 0.064 17.215 0.055 0.285 1.689 0.19 95355. 0.0157
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30.58 0.6728
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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 0.0959 0.0335 0.181 2.851 3.203 134.932 0.322 14.247 10.767 0.25 121904. 0.7067
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1.40 0.0231 0.0642 0.0942 0.0339 0.183 2.883 3.148 136.449 0.326 14.003 10.465 0.25 121984. 0.6809
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2.80 0.0461 0.1246 0.0924 0.0342 0.185 2.912 3.089 137.827 0.329 13.741 10.166 0.25 122071. 0.6553
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4.19 0.0692 0.1816 0.0906 0.0345 0.186 2.938 3.026 139.031 0.332 13.460 9.873 0.25 122165. 0.6298
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5.59 0.0923 0.2350 0.0885 0.0348 0.188 2.959 2.959 140.030 0.334 13.160 9.584 0.25 122265. 0.6045
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6.99 0.1154 0.2851 0.0864 0.0350 0.189 2.975 2.887 140.791 0.336 12.840 9.300 0.25 122372. 0.5795
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8.39 0.1384 0.3318 0.0841 0.0351 0.189 2.985 2.810 141.280 0.337 12.500 9.022 0.25 122487. 0.5546
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9.79 0.1615 0.3754 0.0817 0.0351 0.190 2.989 2.729 141.460 0.338 12.137 8.749 0.25 122608. 0.5300
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11.19 0.1846 0.4160 0.0791 0.0351 0.189 2.986 2.642 141.297 0.337 11.753 8.482 0.25 122738. 0.5056
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12.58 0.2076 0.4535 0.0763 0.0350 0.189 2.974 2.551 140.756 0.336 11.347 8.220 0.25 122875. 0.4815
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13.98 0.2307 0.4882 0.0735 0.0347 0.187 2.954 2.455 139.803 0.334 10.918 7.964 0.25 123020. 0.4576
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15.38 0.2538 0.5200 0.0704 0.0344 0.186 2.925 2.353 138.409 0.330 10.467 7.712 0.25 123173. 0.4339
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16.78 0.2769 0.5491 0.0673 0.0339 0.183 2.886 2.247 136.557 0.326 9.996 7.464 0.25 123334. 0.4104
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18.18 0.2999 0.5754 0.0639 0.0333 0.180 2.836 2.137 134.235 0.320 9.505 7.221 0.26 123504. 0.3871
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19.58 0.3230 0.5990 0.0605 0.0326 0.176 2.777 2.023 131.433 0.314 8.996 6.980 0.26 123682. 0.3640
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20.97 0.3461 0.6198 0.0570 0.0318 0.172 2.708 1.904 128.141 0.306 8.471 6.741 0.26 123868. 0.3411
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22.37 0.3692 0.6378 0.0533 0.0309 0.167 2.628 1.783 124.351 0.297 7.930 6.502 0.26 124063. 0.3184
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23.77 0.3922 0.6527 0.0496 0.0298 0.161 2.537 1.658 120.053 0.287 7.374 6.263 0.26 124267. 0.2957
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25.17 0.4153 0.6644 0.0458 0.0286 0.155 2.435 1.530 115.239 0.275 6.805 6.022 0.26 124479. 0.2731
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26.57 0.4384 0.6726 0.0419 0.0273 0.147 2.322 1.399 109.902 0.262 6.224 5.775 0.26 124700. 0.2505
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27.97 0.4614 0.6768 0.0379 0.0258 0.140 2.198 1.266 104.032 0.248 5.632 5.520 0.26 124930. 0.2278
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29.36 0.4845 0.6762 0.0338 0.0242 0.131 2.063 1.131 97.627 0.233 5.029 5.253 0.26 125169. 0.2048
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30.76 0.5076 0.6699 0.0297 0.0225 0.122 1.916 0.993 90.681 0.216 4.417 4.967 0.26 125417. 0.1815
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32.16 0.5307 0.6563 0.0255 0.0207 0.112 1.758 0.854 83.195 0.199 3.798 4.655 0.26 125674. 0.1577
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33.56 0.5537 0.6329 0.0213 0.0187 0.101 1.588 0.713 75.172 0.179 3.171 4.302 0.26 125940. 0.1332
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34.96 0.5768 0.5958 0.0171 0.0165 0.089 1.408 0.571 66.620 0.159 2.540 3.888 0.26 126215. 0.1077
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36.36 0.5999 0.5380 0.0128 0.0143 0.077 1.216 0.428 57.550 0.137 1.905 3.376 0.26 126499. 0.0810
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37.75 0.6229 0.4463 0.0085 0.0119 0.064 1.014 0.285 47.984 0.115 1.269 2.697 0.26 126792. 0.0528
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39.15 0.6460 0.2922 0.0043 0.0094 0.051 0.802 0.142 37.943 0.091 0.633 1.702 0.26 127093. 0.0236
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40.55 0.6691 -0.0028 0.0000 0.0068 0.037 0.578 -0.001 27.370 0.065 -0.004 -0.016 0.26 127384. 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 0.0964 0.0330 0.348 4.388 5.033 259.560 0.496 22.388 8.795 0.32 152373. 0.7236
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1.75 0.0231 0.0656 0.0948 0.0334 0.352 4.439 4.947 262.600 0.502 22.006 8.545 0.32 152475. 0.6970
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3.50 0.0462 0.1273 0.0930 0.0337 0.356 4.486 4.855 265.363 0.507 21.595 8.299 0.32 152584. 0.6706
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5.25 0.0693 0.1854 0.0911 0.0340 0.359 4.527 4.756 267.783 0.511 21.156 8.056 0.32 152701. 0.6443
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7.00 0.0924 0.2400 0.0891 0.0343 0.362 4.561 4.651 269.798 0.515 20.686 7.818 0.32 152827. 0.6183
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8.75 0.1155 0.2910 0.0869 0.0345 0.364 4.587 4.538 271.342 0.518 20.184 7.585 0.32 152961. 0.5925
|
|
10.50 0.1386 0.3387 0.0846 0.0346 0.365 4.604 4.417 272.344 0.520 19.649 7.357 0.32 153105. 0.5671
|
|
12.25 0.1617 0.3832 0.0822 0.0347 0.366 4.610 4.290 272.736 0.521 19.080 7.134 0.32 153258. 0.5418
|
|
14.00 0.1848 0.4245 0.0796 0.0346 0.365 4.606 4.154 272.447 0.520 18.477 6.916 0.32 153420. 0.5169
|
|
15.75 0.2079 0.4628 0.0768 0.0345 0.364 4.588 4.010 271.408 0.518 17.838 6.702 0.32 153592. 0.4922
|
|
17.50 0.2310 0.4982 0.0739 0.0343 0.361 4.557 3.859 269.551 0.515 17.165 6.493 0.32 153774. 0.4678
|
|
19.25 0.2541 0.5308 0.0709 0.0339 0.358 4.510 3.700 266.820 0.510 16.456 6.289 0.32 153966. 0.4436
|
|
21.00 0.2772 0.5606 0.0677 0.0335 0.353 4.449 3.533 263.179 0.503 15.715 6.089 0.32 154169. 0.4197
|
|
22.75 0.3003 0.5878 0.0643 0.0329 0.347 4.372 3.359 258.603 0.494 14.943 5.892 0.32 154381. 0.3961
|
|
24.50 0.3234 0.6122 0.0609 0.0322 0.339 4.278 3.180 253.073 0.483 14.143 5.699 0.32 154605. 0.3726
|
|
26.25 0.3465 0.6338 0.0573 0.0313 0.331 4.168 2.994 246.569 0.471 13.316 5.507 0.32 154838. 0.3494
|
|
28.00 0.3697 0.6527 0.0537 0.0304 0.321 4.041 2.802 239.074 0.457 12.465 5.316 0.32 155083. 0.3264
|
|
29.75 0.3928 0.6687 0.0499 0.0293 0.309 3.898 2.606 230.570 0.440 11.591 5.126 0.32 155338. 0.3035
|
|
31.50 0.4159 0.6815 0.0461 0.0281 0.296 3.737 2.405 221.038 0.422 10.696 4.934 0.32 155604. 0.2806
|
|
33.25 0.4390 0.6909 0.0421 0.0268 0.282 3.558 2.199 210.463 0.402 9.781 4.739 0.32 155882. 0.2577
|
|
35.00 0.4621 0.6965 0.0381 0.0253 0.267 3.361 1.990 198.830 0.380 8.849 4.538 0.32 156170. 0.2348
|
|
36.76 0.4852 0.6975 0.0340 0.0237 0.250 3.146 1.776 186.130 0.355 7.901 4.329 0.32 156470. 0.2116
|
|
38.51 0.5083 0.6930 0.0299 0.0219 0.231 2.914 1.560 172.355 0.329 6.939 4.105 0.32 156780. 0.1880
|
|
40.26 0.5314 0.6814 0.0257 0.0200 0.211 2.663 1.341 157.504 0.301 5.964 3.861 0.32 157102. 0.1640
|
|
42.01 0.5545 0.6603 0.0214 0.0180 0.190 2.393 1.119 141.584 0.270 4.978 3.586 0.32 157436. 0.1391
|
|
43.76 0.5776 0.6256 0.0172 0.0158 0.167 2.106 0.896 124.610 0.238 3.985 3.261 0.32 157781. 0.1132
|
|
45.51 0.6007 0.5699 0.0129 0.0136 0.143 1.802 0.671 106.609 0.204 2.987 2.857 0.32 158137. 0.0859
|
|
47.26 0.6238 0.4789 0.0086 0.0111 0.117 1.481 0.447 87.619 0.167 1.986 2.312 0.32 158504. 0.0566
|
|
49.01 0.6469 0.3194 0.0042 0.0086 0.091 1.144 0.222 67.688 0.129 0.987 1.487 0.32 158881. 0.0257
|
|
50.76 0.6700 -0.0090 -0.0001 0.0059 0.063 0.788 -0.004 46.643 0.089 -0.019 -0.040 0.32 159238. 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 0.0971 0.0328 0.597 6.273 7.297 445.290 0.709 32.458 7.433 0.38 182839. 0.7363
|
|
2.10 0.0231 0.0665 0.0954 0.0332 0.604 6.348 7.173 450.656 0.717 31.907 7.220 0.38 182961. 0.7091
|
|
4.20 0.0462 0.1292 0.0936 0.0335 0.611 6.417 7.040 455.536 0.725 31.315 7.010 0.38 183092. 0.6821
|
|
6.31 0.0694 0.1881 0.0917 0.0338 0.617 6.477 6.898 459.815 0.732 30.681 6.804 0.38 183234. 0.6553
|
|
8.41 0.0925 0.2434 0.0897 0.0341 0.621 6.528 6.745 463.383 0.737 30.001 6.602 0.38 183385. 0.6288
|
|
10.51 0.1156 0.2951 0.0875 0.0343 0.625 6.566 6.582 466.122 0.742 29.275 6.404 0.38 183547. 0.6026
|
|
12.61 0.1387 0.3435 0.0852 0.0344 0.627 6.592 6.408 467.912 0.745 28.502 6.211 0.38 183720. 0.5766
|
|
14.71 0.1619 0.3885 0.0828 0.0345 0.628 6.602 6.223 468.630 0.746 27.679 6.023 0.38 183904. 0.5510
|
|
16.82 0.1850 0.4305 0.0802 0.0344 0.628 6.595 6.026 468.153 0.745 26.806 5.839 0.38 184100. 0.5256
|
|
18.92 0.2081 0.4694 0.0774 0.0343 0.625 6.570 5.819 466.359 0.742 25.881 5.659 0.38 184307. 0.5006
|
|
21.02 0.2312 0.5053 0.0745 0.0341 0.621 6.524 5.599 463.130 0.737 24.905 5.484 0.38 184526. 0.4758
|
|
23.12 0.2544 0.5385 0.0714 0.0337 0.615 6.457 5.368 458.368 0.730 23.878 5.312 0.38 184758. 0.4514
|
|
25.23 0.2775 0.5689 0.0682 0.0333 0.606 6.367 5.127 452.007 0.719 22.803 5.144 0.38 185001. 0.4272
|
|
27.33 0.3006 0.5966 0.0648 0.0327 0.595 6.255 4.875 444.003 0.707 21.684 4.980 0.38 185257. 0.4032
|
|
29.43 0.3237 0.6217 0.0614 0.0320 0.582 6.118 4.614 434.324 0.691 20.523 4.818 0.38 185526. 0.3796
|
|
31.53 0.3468 0.6440 0.0578 0.0311 0.567 5.958 4.344 422.934 0.673 19.323 4.659 0.38 185807. 0.3561
|
|
33.63 0.3700 0.6637 0.0541 0.0302 0.550 5.773 4.067 409.803 0.652 18.088 4.501 0.38 186101. 0.3329
|
|
35.74 0.3931 0.6804 0.0503 0.0291 0.530 5.563 3.781 394.899 0.629 16.820 4.343 0.38 186408. 0.3097
|
|
37.84 0.4162 0.6942 0.0464 0.0278 0.507 5.328 3.489 378.191 0.602 15.521 4.185 0.38 186728. 0.2867
|
|
39.94 0.4393 0.7047 0.0424 0.0265 0.482 5.066 3.191 359.651 0.572 14.194 4.025 0.38 187062. 0.2637
|
|
42.04 0.4625 0.7114 0.0384 0.0250 0.455 4.779 2.887 339.253 0.540 12.842 3.860 0.38 187409. 0.2405
|
|
44.14 0.4856 0.7138 0.0343 0.0233 0.425 4.465 2.578 316.979 0.504 11.465 3.688 0.39 187769. 0.2172
|
|
46.25 0.5087 0.7109 0.0301 0.0215 0.393 4.125 2.264 292.818 0.466 10.068 3.506 0.39 188143. 0.1935
|
|
48.35 0.5318 0.7011 0.0259 0.0196 0.358 3.758 1.945 266.767 0.425 8.653 3.308 0.39 188530. 0.1692
|
|
50.45 0.5550 0.6820 0.0216 0.0176 0.320 3.365 1.624 238.839 0.380 7.223 3.084 0.39 188931. 0.1441
|
|
52.55 0.5781 0.6496 0.0173 0.0154 0.280 2.945 1.300 209.059 0.333 5.781 2.820 0.39 189346. 0.1179
|
|
54.66 0.6012 0.5963 0.0130 0.0131 0.238 2.500 0.974 177.476 0.282 4.331 2.489 0.39 189774. 0.0901
|
|
56.76 0.6243 0.5067 0.0086 0.0106 0.193 2.031 0.647 144.158 0.229 2.879 2.036 0.39 190215. 0.0601
|
|
58.86 0.6475 0.3441 0.0043 0.0080 0.146 1.538 0.321 109.190 0.174 1.428 1.333 0.39 190668. 0.0277
|
|
60.96 0.6706 -0.0132 -0.0001 0.0053 0.097 1.017 -0.008 72.175 0.115 -0.035 -0.049 0.39 191089. 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 0.0978 0.0327 0.947 8.527 10.013 706.190 0.963 44.537 6.431 0.44 213299. 0.7463
|
|
2.45 0.0231 0.0672 0.0962 0.0331 0.959 8.632 9.844 714.884 0.975 43.787 6.246 0.44 213442. 0.7187
|
|
4.91 0.0463 0.1305 0.0944 0.0335 0.969 8.727 9.663 722.792 0.986 42.979 6.064 0.44 213596. 0.6912
|
|
7.36 0.0694 0.1899 0.0925 0.0338 0.979 8.811 9.468 729.728 0.995 42.113 5.885 0.44 213761. 0.6641
|
|
9.82 0.0926 0.2457 0.0905 0.0341 0.986 8.881 9.259 735.511 1.003 41.185 5.710 0.44 213939. 0.6372
|
|
12.27 0.1157 0.2980 0.0883 0.0343 0.992 8.935 9.036 739.954 1.009 40.193 5.539 0.44 214129. 0.6106
|
|
14.73 0.1388 0.3468 0.0860 0.0344 0.996 8.970 8.798 742.861 1.013 39.134 5.372 0.44 214331. 0.5843
|
|
17.18 0.1620 0.3923 0.0835 0.0345 0.998 8.984 8.545 744.035 1.015 38.008 5.209 0.44 214547. 0.5584
|
|
19.63 0.1851 0.4347 0.0809 0.0344 0.997 8.975 8.276 743.279 1.014 36.812 5.050 0.45 214776. 0.5328
|
|
22.09 0.2083 0.4740 0.0781 0.0343 0.993 8.940 7.991 740.396 1.010 35.545 4.895 0.45 215019. 0.5075
|
|
24.54 0.2314 0.5105 0.0751 0.0341 0.986 8.877 7.690 735.195 1.003 34.207 4.744 0.45 215275. 0.4825
|
|
27.00 0.2545 0.5441 0.0721 0.0337 0.976 8.785 7.374 727.518 0.992 32.799 4.597 0.45 215546. 0.4578
|
|
29.45 0.2777 0.5750 0.0688 0.0332 0.962 8.661 7.042 717.258 0.978 31.324 4.453 0.45 215831. 0.4334
|
|
31.90 0.3008 0.6032 0.0654 0.0326 0.945 8.505 6.697 704.345 0.961 29.788 4.313 0.45 216131. 0.4093
|
|
34.36 0.3240 0.6288 0.0619 0.0319 0.924 8.316 6.339 688.725 0.940 28.194 4.174 0.45 216445. 0.3854
|
|
36.81 0.3471 0.6517 0.0583 0.0311 0.899 8.094 5.968 670.346 0.914 26.547 4.038 0.45 216774. 0.3618
|
|
39.27 0.3702 0.6720 0.0546 0.0301 0.871 7.838 5.587 649.156 0.886 24.851 3.904 0.45 217118. 0.3384
|
|
41.72 0.3934 0.6895 0.0508 0.0290 0.838 7.548 5.195 625.106 0.853 23.110 3.770 0.45 217478. 0.3151
|
|
44.18 0.4165 0.7041 0.0468 0.0277 0.802 7.222 4.794 598.144 0.816 21.326 3.636 0.45 217852. 0.2919
|
|
46.63 0.4397 0.7155 0.0428 0.0263 0.762 6.861 4.385 568.227 0.775 19.503 3.500 0.45 218242. 0.2688
|
|
49.08 0.4628 0.7232 0.0388 0.0248 0.718 6.464 3.967 535.313 0.730 17.644 3.361 0.45 218648. 0.2455
|
|
51.54 0.4859 0.7268 0.0346 0.0231 0.670 6.030 3.542 499.373 0.681 15.753 3.217 0.45 219069. 0.2220
|
|
53.99 0.5091 0.7252 0.0304 0.0213 0.617 5.559 3.110 460.388 0.628 13.833 3.064 0.45 219506. 0.1982
|
|
56.45 0.5322 0.7171 0.0261 0.0194 0.561 5.051 2.673 418.356 0.571 11.888 2.898 0.45 219958. 0.1737
|
|
58.90 0.5554 0.6999 0.0218 0.0173 0.501 4.507 2.231 373.295 0.509 9.922 2.710 0.45 220427. 0.1485
|
|
61.36 0.5785 0.6696 0.0174 0.0151 0.436 3.927 1.785 325.249 0.444 7.940 2.489 0.45 220911. 0.1220
|
|
63.81 0.6016 0.6185 0.0131 0.0127 0.368 3.312 1.337 274.294 0.374 5.948 2.211 0.45 221412. 0.0938
|
|
66.26 0.6248 0.5307 0.0087 0.0102 0.296 2.663 0.888 220.544 0.301 3.951 1.827 0.45 221927. 0.0631
|
|
68.72 0.6479 0.3661 0.0043 0.0076 0.220 1.982 0.440 164.135 0.224 1.956 1.215 0.45 222456. 0.0296
|
|
71.17 0.6711 -0.0183 -0.0001 0.0048 0.140 1.259 -0.013 104.260 0.142 -0.060 -0.059 0.45 222937. 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 0.0988 0.0328 1.419 11.178 13.203 1057.967 1.263 58.725 5.660 0.51 243752. 0.7542
|
|
2.81 0.0232 0.0676 0.0971 0.0333 1.437 11.318 12.982 1071.219 1.279 57.745 5.497 0.51 243916. 0.7263
|
|
5.61 0.0463 0.1313 0.0953 0.0336 1.453 11.445 12.745 1083.265 1.293 56.688 5.336 0.51 244093. 0.6986
|
|
8.42 0.0695 0.1912 0.0934 0.0340 1.467 11.557 12.489 1093.827 1.306 55.553 5.179 0.51 244283. 0.6712
|
|
11.23 0.0926 0.2473 0.0914 0.0342 1.479 11.650 12.216 1102.627 1.316 54.336 5.025 0.51 244487. 0.6441
|
|
14.03 0.1158 0.2999 0.0892 0.0344 1.488 11.721 11.923 1109.384 1.324 53.034 4.875 0.51 244705. 0.6173
|
|
16.84 0.1389 0.3490 0.0869 0.0346 1.494 11.768 11.611 1113.797 1.329 51.644 4.728 0.51 244937. 0.5908
|
|
19.65 0.1621 0.3949 0.0844 0.0346 1.496 11.786 11.278 1115.570 1.332 50.164 4.585 0.51 245185. 0.5647
|
|
22.45 0.1852 0.4376 0.0817 0.0346 1.494 11.774 10.924 1114.401 1.330 48.591 4.446 0.51 245448. 0.5389
|
|
25.26 0.2084 0.4773 0.0789 0.0345 1.489 11.727 10.549 1109.999 1.325 46.923 4.311 0.51 245726. 0.5135
|
|
28.07 0.2315 0.5141 0.0760 0.0342 1.478 11.644 10.153 1102.070 1.315 45.161 4.179 0.51 246021. 0.4883
|
|
30.87 0.2547 0.5481 0.0728 0.0338 1.462 11.520 9.736 1090.374 1.302 43.306 4.050 0.51 246331. 0.4634
|
|
33.68 0.2778 0.5794 0.0696 0.0334 1.441 11.355 9.299 1074.751 1.283 41.362 3.924 0.51 246658. 0.4389
|
|
36.48 0.3010 0.6081 0.0662 0.0328 1.415 11.147 8.844 1055.094 1.259 39.336 3.802 0.51 247002. 0.4146
|
|
39.29 0.3242 0.6341 0.0626 0.0320 1.383 10.896 8.371 1031.323 1.231 37.234 3.682 0.51 247362. 0.3906
|
|
42.10 0.3473 0.6576 0.0590 0.0311 1.346 10.601 7.882 1003.359 1.198 35.061 3.563 0.51 247740. 0.3669
|
|
44.90 0.3705 0.6785 0.0552 0.0301 1.302 10.260 7.379 971.129 1.159 32.823 3.447 0.51 248134. 0.3433
|
|
47.71 0.3936 0.6966 0.0513 0.0290 1.253 9.874 6.862 934.558 1.116 30.524 3.331 0.51 248546. 0.3200
|
|
50.52 0.4168 0.7119 0.0474 0.0277 1.198 9.441 6.333 893.570 1.067 28.169 3.215 0.51 248975. 0.2967
|
|
53.32 0.4399 0.7241 0.0433 0.0263 1.137 8.960 5.792 848.098 1.012 25.762 3.098 0.51 249422. 0.2734
|
|
56.13 0.4631 0.7328 0.0392 0.0248 1.070 8.432 5.240 798.081 0.953 23.308 2.978 0.51 249886. 0.2500
|
|
58.94 0.4862 0.7375 0.0350 0.0231 0.997 7.855 4.679 743.474 0.887 20.810 2.854 0.51 250368. 0.2264
|
|
61.74 0.5094 0.7371 0.0307 0.0212 0.918 7.229 4.108 684.249 0.817 18.274 2.723 0.51 250869. 0.2024
|
|
64.55 0.5325 0.7304 0.0264 0.0193 0.832 6.555 3.531 620.404 0.741 15.704 2.581 0.51 251387. 0.1779
|
|
67.36 0.5557 0.7150 0.0220 0.0171 0.740 5.832 2.947 551.963 0.659 13.107 2.421 0.52 251923. 0.1524
|
|
70.16 0.5788 0.6867 0.0176 0.0149 0.642 5.061 2.358 478.998 0.572 10.487 2.233 0.52 252478. 0.1257
|
|
72.97 0.6020 0.6379 0.0132 0.0125 0.539 4.243 1.766 401.622 0.479 7.854 1.994 0.52 253050. 0.0972
|
|
75.78 0.6251 0.5520 0.0088 0.0099 0.429 3.381 1.172 320.009 0.382 5.214 1.662 0.52 253640. 0.0660
|
|
78.58 0.6483 0.3864 0.0043 0.0073 0.314 2.476 0.580 234.367 0.280 2.578 1.122 0.52 254246. 0.0313
|
|
81.39 0.6715 -0.0245 -0.0002 0.0044 0.192 1.513 -0.022 143.167 0.171 -0.097 -0.069 0.52 254780. 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 0.0999 0.0331 2.036 14.262 16.895 1518.592 1.611 75.151 5.046 0.57 274196. 0.7607
|
|
3.16 0.0232 0.0679 0.0982 0.0335 2.062 14.443 16.616 1537.892 1.632 73.910 4.901 0.57 274381. 0.7326
|
|
6.32 0.0463 0.1318 0.0964 0.0339 2.086 14.608 16.315 1555.426 1.650 72.571 4.758 0.57 274582. 0.7048
|
|
9.48 0.0695 0.1919 0.0945 0.0342 2.106 14.752 15.992 1570.789 1.667 71.131 4.618 0.57 274797. 0.6772
|
|
12.64 0.0927 0.2482 0.0925 0.0345 2.124 14.872 15.644 1583.573 1.680 69.585 4.481 0.57 275027. 0.6499
|
|
15.80 0.1158 0.3010 0.0903 0.0347 2.137 14.964 15.272 1593.364 1.691 67.928 4.347 0.57 275274. 0.6230
|
|
18.95 0.1390 0.3504 0.0879 0.0349 2.145 15.024 14.874 1599.736 1.697 66.158 4.217 0.57 275537. 0.5964
|
|
22.11 0.1622 0.3965 0.0854 0.0349 2.149 15.047 14.449 1602.257 1.700 64.271 4.090 0.57 275817. 0.5702
|
|
25.27 0.1853 0.4395 0.0827 0.0349 2.146 15.031 13.998 1600.493 1.698 62.264 3.967 0.57 276114. 0.5443
|
|
28.43 0.2085 0.4795 0.0799 0.0348 2.138 14.970 13.520 1594.015 1.691 60.135 3.847 0.57 276429. 0.5187
|
|
31.59 0.2317 0.5166 0.0769 0.0345 2.122 14.861 13.014 1582.411 1.679 57.884 3.730 0.57 276762. 0.4935
|
|
34.75 0.2548 0.5509 0.0738 0.0341 2.099 14.701 12.480 1565.330 1.661 55.513 3.616 0.57 277112. 0.4685
|
|
37.91 0.2780 0.5826 0.0705 0.0336 2.069 14.487 11.921 1542.535 1.637 53.027 3.505 0.57 277482. 0.4439
|
|
41.07 0.3012 0.6116 0.0670 0.0330 2.030 14.217 11.339 1513.872 1.606 50.434 3.397 0.57 277870. 0.4195
|
|
44.23 0.3243 0.6381 0.0634 0.0322 1.984 13.892 10.734 1479.237 1.570 47.743 3.291 0.57 278277. 0.3954
|
|
47.39 0.3475 0.6621 0.0598 0.0314 1.929 13.510 10.108 1438.517 1.526 44.960 3.187 0.57 278703. 0.3716
|
|
50.55 0.3707 0.6835 0.0559 0.0303 1.866 13.069 9.463 1391.610 1.477 42.093 3.084 0.58 279148. 0.3480
|
|
53.70 0.3938 0.7022 0.0520 0.0292 1.795 12.570 8.801 1338.410 1.420 39.148 2.983 0.58 279612. 0.3245
|
|
56.86 0.4170 0.7182 0.0480 0.0279 1.715 12.010 8.123 1278.811 1.357 36.129 2.881 0.58 280096. 0.3011
|
|
60.02 0.4402 0.7311 0.0439 0.0264 1.626 11.389 7.429 1212.717 1.287 33.044 2.779 0.58 280600. 0.2777
|
|
63.18 0.4633 0.7407 0.0397 0.0249 1.529 10.707 6.722 1140.041 1.210 29.897 2.674 0.58 281124. 0.2543
|
|
66.34 0.4865 0.7464 0.0355 0.0231 1.422 9.962 6.001 1060.719 1.125 26.695 2.566 0.58 281668. 0.2306
|
|
69.50 0.5097 0.7472 0.0312 0.0212 1.307 9.154 5.270 974.710 1.034 23.442 2.452 0.58 282232. 0.2065
|
|
72.66 0.5328 0.7419 0.0268 0.0192 1.183 8.283 4.529 882.009 0.936 20.145 2.329 0.58 282816. 0.1818
|
|
75.82 0.5560 0.7281 0.0223 0.0171 1.050 7.350 3.780 782.659 0.830 16.812 2.190 0.58 283421. 0.1562
|
|
78.98 0.5792 0.7017 0.0179 0.0148 0.908 6.356 3.024 676.755 0.718 13.451 2.027 0.58 284045. 0.1293
|
|
82.14 0.6023 0.6551 0.0134 0.0123 0.757 5.301 2.264 564.467 0.599 10.071 1.819 0.58 284690. 0.1004
|
|
85.29 0.6255 0.5713 0.0089 0.0097 0.598 4.189 1.502 446.049 0.473 6.683 1.528 0.58 285355. 0.0687
|
|
88.45 0.6487 0.4052 0.0044 0.0070 0.432 3.022 0.741 321.803 0.341 3.297 1.045 0.58 286037. 0.0330
|
|
91.61 0.6718 -0.0328 -0.0002 0.0041 0.253 1.774 -0.034 188.912 0.200 -0.151 -0.082 0.58 286613. 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 0.1012 0.0335 2.829 17.828 21.128 2109.240 2.014 93.978 4.543 0.63 304629. 0.7659
|
|
3.51 0.0232 0.0679 0.0995 0.0340 2.865 18.058 20.784 2136.416 2.040 92.448 4.413 0.63 304837. 0.7377
|
|
7.02 0.0464 0.1319 0.0977 0.0343 2.898 18.266 20.412 2161.076 2.064 90.794 4.284 0.63 305060. 0.7098
|
|
10.54 0.0695 0.1921 0.0958 0.0347 2.927 18.448 20.012 2182.653 2.084 89.012 4.159 0.63 305301. 0.6822
|
|
14.05 0.0927 0.2485 0.0938 0.0350 2.951 18.600 19.581 2200.579 2.101 87.096 4.036 0.63 305558. 0.6549
|
|
17.56 0.1159 0.3015 0.0915 0.0352 2.969 18.716 19.119 2214.274 2.114 85.041 3.916 0.64 305834. 0.6280
|
|
21.07 0.1391 0.3510 0.0892 0.0353 2.981 18.790 18.624 2223.132 2.123 82.841 3.800 0.64 306128. 0.6014
|
|
24.58 0.1622 0.3973 0.0866 0.0354 2.986 18.819 18.096 2226.551 2.126 80.493 3.686 0.64 306441. 0.5751
|
|
28.10 0.1854 0.4405 0.0840 0.0353 2.982 18.797 17.534 2223.926 2.124 77.993 3.576 0.64 306773. 0.5492
|
|
31.61 0.2086 0.4807 0.0811 0.0352 2.970 18.719 16.938 2214.668 2.115 75.339 3.469 0.64 307125. 0.5236
|
|
35.12 0.2318 0.5180 0.0781 0.0349 2.948 18.580 16.306 2198.196 2.099 72.530 3.365 0.64 307496. 0.4983
|
|
38.63 0.2550 0.5526 0.0749 0.0346 2.915 18.375 15.640 2174.029 2.076 69.569 3.263 0.64 307888. 0.4733
|
|
42.14 0.2781 0.5846 0.0715 0.0340 2.872 18.103 14.942 2141.828 2.045 66.462 3.164 0.64 308300. 0.4486
|
|
45.65 0.3013 0.6140 0.0681 0.0334 2.818 17.761 14.213 2101.393 2.007 63.220 3.068 0.64 308733. 0.4241
|
|
49.17 0.3245 0.6409 0.0644 0.0326 2.753 17.349 13.456 2052.572 1.960 59.853 2.973 0.64 309187. 0.4000
|
|
52.68 0.3477 0.6653 0.0607 0.0317 2.676 16.864 12.673 1995.226 1.905 56.370 2.881 0.64 309662. 0.3761
|
|
56.19 0.3709 0.6872 0.0568 0.0307 2.587 16.306 11.866 1929.218 1.842 52.781 2.790 0.64 310159. 0.3524
|
|
59.70 0.3940 0.7065 0.0528 0.0295 2.487 15.674 11.037 1854.405 1.771 49.092 2.700 0.64 310677. 0.3289
|
|
63.21 0.4172 0.7232 0.0488 0.0281 2.374 14.966 10.187 1770.645 1.691 45.311 2.609 0.64 311216. 0.3054
|
|
66.73 0.4404 0.7368 0.0446 0.0267 2.250 14.181 9.318 1677.807 1.602 41.445 2.519 0.64 311778. 0.2820
|
|
70.24 0.4636 0.7473 0.0404 0.0250 2.113 13.319 8.431 1575.771 1.505 37.501 2.427 0.64 312361. 0.2584
|
|
73.75 0.4867 0.7539 0.0360 0.0233 1.964 12.378 7.528 1464.449 1.398 33.486 2.332 0.64 312967. 0.2346
|
|
77.26 0.5099 0.7558 0.0317 0.0214 1.802 11.358 6.611 1343.786 1.283 29.407 2.232 0.64 313595. 0.2104
|
|
80.77 0.5331 0.7518 0.0272 0.0193 1.628 10.259 5.682 1213.777 1.159 25.273 2.123 0.64 314246. 0.1856
|
|
84.29 0.5563 0.7396 0.0227 0.0171 1.441 9.082 4.742 1074.477 1.026 21.091 2.002 0.64 314918. 0.1598
|
|
87.80 0.5795 0.7152 0.0182 0.0147 1.242 7.827 3.793 926.024 0.884 16.873 1.858 0.65 315614. 0.1327
|
|
91.31 0.6026 0.6707 0.0136 0.0122 1.031 6.497 2.840 768.655 0.734 12.631 1.676 0.65 316331. 0.1035
|
|
94.82 0.6258 0.5891 0.0090 0.0096 0.808 5.094 1.883 602.728 0.576 8.377 1.417 0.65 317071. 0.0713
|
|
98.33 0.6490 0.4231 0.0044 0.0068 0.575 3.623 0.928 428.667 0.409 4.126 0.981 0.65 317829. 0.0347
|
|
101.84 0.6722 -0.0443 -0.0003 0.0038 0.324 2.039 -0.053 241.238 0.230 -0.235 -0.099 0.65 318424. 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 0.1027 0.0341 3.834 21.971 25.947 2859.326 2.482 115.414 4.116 0.70 335049. 0.7689
|
|
3.86 0.0232 0.0678 0.1010 0.0346 3.883 22.250 25.533 2895.618 2.514 113.571 3.999 0.70 335278. 0.7411
|
|
7.73 0.0464 0.1316 0.0993 0.0350 3.927 22.503 25.084 2928.620 2.542 111.573 3.885 0.70 335526. 0.7135
|
|
11.59 0.0696 0.1918 0.0973 0.0353 3.966 22.725 24.599 2957.536 2.567 109.415 3.772 0.70 335792. 0.6862
|
|
15.46 0.0928 0.2482 0.0953 0.0356 3.998 22.910 24.076 2981.584 2.588 107.089 3.662 0.70 336077. 0.6590
|
|
19.32 0.1159 0.3012 0.0930 0.0358 4.023 23.051 23.514 2999.932 2.604 104.589 3.555 0.70 336383. 0.6322
|
|
23.19 0.1391 0.3508 0.0907 0.0360 4.039 23.142 22.911 3011.725 2.615 101.910 3.450 0.70 336708. 0.6057
|
|
27.05 0.1623 0.3972 0.0881 0.0360 4.045 23.175 22.267 3016.107 2.618 99.045 3.349 0.70 337055. 0.5795
|
|
30.92 0.1855 0.4405 0.0854 0.0360 4.039 23.145 21.581 3012.223 2.615 95.990 3.250 0.70 337422. 0.5536
|
|
34.78 0.2087 0.4808 0.0825 0.0358 4.022 23.046 20.851 2999.242 2.604 92.744 3.153 0.70 337812. 0.5280
|
|
38.65 0.2319 0.5184 0.0794 0.0355 3.991 22.870 20.077 2976.387 2.584 89.304 3.060 0.70 338223. 0.5028
|
|
42.51 0.2551 0.5533 0.0762 0.0351 3.947 22.613 19.261 2942.983 2.555 85.673 2.968 0.70 338657. 0.4778
|
|
46.38 0.2783 0.5856 0.0728 0.0346 3.887 22.272 18.404 2898.586 2.516 81.861 2.880 0.70 339113. 0.4531
|
|
50.24 0.3015 0.6153 0.0693 0.0339 3.812 21.845 17.509 2842.930 2.468 77.880 2.793 0.70 339591. 0.4287
|
|
54.11 0.3247 0.6426 0.0656 0.0331 3.722 21.329 16.579 2775.822 2.410 73.743 2.709 0.70 340093. 0.4045
|
|
57.97 0.3478 0.6675 0.0618 0.0322 3.617 20.724 15.616 2697.088 2.341 69.461 2.626 0.70 340618. 0.3806
|
|
61.84 0.3710 0.6899 0.0579 0.0311 3.495 20.028 14.624 2606.556 2.263 65.046 2.545 0.70 341166. 0.3569
|
|
65.70 0.3942 0.7098 0.0538 0.0299 3.358 19.241 13.603 2504.047 2.174 60.507 2.464 0.70 341738. 0.3333
|
|
69.57 0.4174 0.7270 0.0497 0.0285 3.204 18.360 12.557 2389.374 2.074 55.854 2.384 0.70 342334. 0.3098
|
|
73.43 0.4406 0.7414 0.0455 0.0270 3.034 17.384 11.487 2262.366 1.964 51.095 2.303 0.70 342954. 0.2862
|
|
77.30 0.4638 0.7527 0.0411 0.0253 2.847 16.312 10.395 2122.858 1.843 46.237 2.221 0.71 343597. 0.2626
|
|
81.16 0.4870 0.7602 0.0367 0.0235 2.643 15.143 9.283 1970.732 1.711 41.291 2.137 0.71 344265. 0.2387
|
|
85.03 0.5102 0.7633 0.0323 0.0216 2.422 13.876 8.153 1805.921 1.568 36.265 2.048 0.71 344958. 0.2144
|
|
88.89 0.5334 0.7606 0.0277 0.0194 2.184 12.513 7.007 1628.423 1.414 31.168 1.952 0.71 345675. 0.1895
|
|
92.76 0.5566 0.7499 0.0231 0.0172 1.929 11.052 5.848 1438.340 1.249 26.012 1.844 0.71 346417. 0.1635
|
|
96.62 0.5797 0.7273 0.0185 0.0148 1.657 9.496 4.678 1235.900 1.073 20.809 1.717 0.71 347183. 0.1362
|
|
100.49 0.6029 0.6849 0.0139 0.0122 1.370 7.849 3.501 1021.492 0.887 15.574 1.555 0.71 347974. 0.1067
|
|
104.35 0.6261 0.6052 0.0092 0.0095 1.067 6.114 2.321 795.706 0.691 10.323 1.323 0.71 348788. 0.0739
|
|
108.22 0.6493 0.4390 0.0045 0.0067 0.750 4.297 1.141 559.268 0.486 5.074 0.925 0.71 349623. 0.0362
|
|
112.08 0.6725
|
|
|
|
|
|
|
|
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 0.1044 0.0355 5.177 27.194 31.409 3860.830 3.072 139.708 3.690 0.76 365451. 0.7584
|
|
4.22 0.0232 0.0666 0.1028 0.0359 5.232 27.478 30.920 3901.133 3.104 137.533 3.595 0.76 365703. 0.7331
|
|
8.45 0.0465 0.1296 0.1010 0.0362 5.280 27.732 30.388 3937.241 3.133 135.166 3.501 0.76 365975. 0.7077
|
|
12.67 0.0697 0.1893 0.0991 0.0365 5.321 27.950 29.811 3968.212 3.158 132.600 3.407 0.76 366268. 0.6823
|
|
16.89 0.0929 0.2455 0.0971 0.0367 5.355 28.126 29.188 3993.113 3.178 129.827 3.315 0.76 366582. 0.6569
|
|
21.12 0.1161 0.2985 0.0948 0.0369 5.379 28.251 28.516 4010.941 3.192 126.837 3.225 0.76 366918. 0.6315
|
|
25.34 0.1394 0.3483 0.0924 0.0370 5.392 28.319 27.793 4020.637 3.200 123.625 3.135 0.76 367277. 0.6062
|
|
29.56 0.1626 0.3950 0.0898 0.0370 5.392 28.323 27.019 4021.108 3.200 120.182 3.048 0.76 367658. 0.5810
|
|
33.79 0.1858 0.4387 0.0871 0.0369 5.379 28.253 26.193 4011.232 3.192 116.505 2.962 0.76 368063. 0.5559
|
|
38.01 0.2091 0.4795 0.0842 0.0367 5.351 28.103 25.312 3989.890 3.175 112.590 2.878 0.76 368492. 0.5309
|
|
42.23 0.2323 0.5175 0.0811 0.0364 5.305 27.864 24.378 3955.991 3.148 108.434 2.795 0.76 368944. 0.5061
|
|
46.46 0.2555 0.5528 0.0778 0.0359 5.241 27.530 23.391 3908.550 3.110 104.042 2.714 0.76 369421. 0.4814
|
|
50.68 0.2787 0.5855 0.0743 0.0354 5.159 27.096 22.352 3846.886 3.061 99.424 2.635 0.76 369923. 0.4569
|
|
54.90 0.3020 0.6158 0.0707 0.0347 5.056 26.558 21.267 3770.555 3.001 94.596 2.558 0.77 370449. 0.4327
|
|
59.13 0.3252 0.6435 0.0670 0.0338 4.934 25.915 20.138 3679.205 2.928 89.576 2.483 0.77 371001. 0.4086
|
|
63.35 0.3484 0.6688 0.0631 0.0329 4.791 25.163 18.969 3572.519 2.843 84.376 2.408 0.77 371578. 0.3847
|
|
67.57 0.3716 0.6918 0.0591 0.0317 4.627 24.302 17.763 3450.197 2.746 79.011 2.335 0.77 372180. 0.3609
|
|
71.80 0.3949 0.7122 0.0549 0.0305 4.441 23.328 16.523 3311.951 2.636 73.494 2.263 0.77 372808. 0.3373
|
|
76.02 0.4181 0.7301 0.0507 0.0290 4.234 22.240 15.251 3157.546 2.513 67.835 2.191 0.77 373462. 0.3137
|
|
80.24 0.4413 0.7452 0.0464 0.0275 4.005 21.038 13.949 2986.795 2.377 62.045 2.118 0.77 374141. 0.2901
|
|
84.46 0.4646 0.7571 0.0420 0.0257 3.754 19.719 12.620 2799.552 2.228 56.134 2.045 0.77 374848. 0.2664
|
|
88.69 0.4878 0.7654 0.0375 0.0239 3.481 18.283 11.266 2595.746 2.066 50.112 1.969 0.77 375580. 0.2423
|
|
92.91 0.5110 0.7692 0.0329 0.0218 3.186 16.731 9.890 2375.429 1.890 43.990 1.888 0.77 376339. 0.2178
|
|
97.13 0.5342 0.7670 0.0282 0.0197 2.868 15.065 8.494 2138.816 1.702 37.780 1.801 0.77 377125. 0.1925
|
|
101.36 0.5575 0.7565 0.0235 0.0173 2.530 13.286 7.080 1886.305 1.501 31.494 1.703 0.77 377938. 0.1661
|
|
105.58 0.5807 0.7334 0.0188 0.0149 2.170 11.400 5.654 1618.528 1.288 25.148 1.584 0.77 378777. 0.1382
|
|
109.80 0.6039 0.6890 0.0140 0.0123 1.792 9.413 4.217 1336.392 1.063 18.759 1.431 0.78 379643. 0.1078
|
|
114.03 0.6272 0.6045 0.0092 0.0096 1.396 7.333 2.776 1041.124 0.829 12.347 1.209 0.78 380535. 0.0739
|
|
118.25 0.6504 0.4273 0.0044 0.0068 0.985 5.171 1.334 734.162 0.584 5.934 0.824 0.78 381448. 0.0349
|
|
122.47 0.6736
|
|
|
|
|
|
|
|
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 0.1064 0.0389 7.210 34.958 37.569 5376.739 3.950 167.106 3.169 0.83 395829. 0.7124
|
|
4.58 0.0232 0.0623 0.1048 0.0391 7.249 35.144 37.007 5405.387 3.971 164.605 3.105 0.83 396104. 0.6928
|
|
9.15 0.0465 0.1220 0.1031 0.0393 7.279 35.289 36.391 5427.696 3.987 161.868 3.041 0.83 396401. 0.6728
|
|
13.73 0.0697 0.1791 0.1012 0.0394 7.299 35.388 35.721 5442.786 3.998 158.886 2.977 0.83 396720. 0.6525
|
|
18.30 0.0929 0.2337 0.0991 0.0394 7.308 35.433 34.993 5449.763 4.003 155.649 2.912 0.83 397064. 0.6318
|
|
22.88 0.1162 0.2856 0.0969 0.0394 7.305 35.419 34.205 5447.661 4.002 152.145 2.848 0.83 397431. 0.6108
|
|
27.45 0.1394 0.3350 0.0945 0.0393 7.289 35.340 33.356 5435.443 3.993 148.367 2.783 0.83 397822. 0.5895
|
|
32.03 0.1626 0.3818 0.0919 0.0391 7.258 35.188 32.443 5412.025 3.975 144.306 2.719 0.83 398239. 0.5679
|
|
36.61 0.1858 0.4260 0.0891 0.0389 7.210 34.955 31.465 5376.249 3.949 139.957 2.655 0.83 398681. 0.5461
|
|
41.18 0.2091 0.4676 0.0862 0.0385 7.143 34.634 30.422 5326.886 3.913 135.316 2.590 0.83 399149. 0.5240
|
|
45.76 0.2323 0.5068 0.0830 0.0381 7.057 34.216 29.312 5262.667 3.866 130.380 2.526 0.83 399644. 0.5016
|
|
50.33 0.2555 0.5434 0.0797 0.0375 6.950 33.695 28.137 5182.400 3.807 125.151 2.463 0.83 400164. 0.4790
|
|
54.91 0.2788 0.5775 0.0762 0.0368 6.819 33.063 26.899 5085.274 3.735 119.645 2.399 0.83 400712. 0.4563
|
|
59.48 0.3020 0.6092 0.0725 0.0360 6.666 32.319 25.602 4970.790 3.651 113.878 2.336 0.83 401286. 0.4335
|
|
64.06 0.3252 0.6384 0.0687 0.0350 6.489 31.459 24.252 4838.568 3.554 107.872 2.273 0.83 401887. 0.4106
|
|
68.64 0.3485 0.6652 0.0647 0.0339 6.287 30.481 22.852 4688.203 3.444 101.646 2.211 0.83 402515. 0.3876
|
|
73.21 0.3717 0.6896 0.0606 0.0327 6.060 29.383 21.407 4519.236 3.320 95.217 2.148 0.83 403171. 0.3645
|
|
77.79 0.3949 0.7113 0.0564 0.0313 5.809 28.163 19.919 4331.571 3.182 88.599 2.086 0.83 403855. 0.3414
|
|
82.36 0.4181 0.7301 0.0521 0.0298 5.532 26.823 18.392 4125.527 3.030 81.806 2.022 0.83 404566. 0.3180
|
|
86.94 0.4414 0.7458 0.0477 0.0282 5.231 25.361 16.828 3900.636 2.865 74.851 1.957 0.83 405306. 0.2944
|
|
91.51 0.4646 0.7578 0.0432 0.0265 4.905 23.779 15.231 3657.389 2.687 67.747 1.889 0.83 406073. 0.2703
|
|
96.09 0.4878 0.7656 0.0385 0.0246 4.553 22.073 13.603 3394.986 2.494 60.505 1.817 0.83 406870. 0.2458
|
|
100.66 0.5111 0.7681 0.0338 0.0225 4.175 20.242 11.947 3113.378 2.287 53.139 1.740 0.84 407694. 0.2206
|
|
105.24 0.5343 0.7636 0.0291 0.0204 3.773 18.292 10.266 2813.437 2.067 45.661 1.655 0.84 408548. 0.1945
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|
109.82 0.5575 0.7490 0.0243 0.0181 3.348 16.231 8.563 2496.478 1.834 38.087 1.556 0.84 409430. 0.1669
|
|
114.39 0.5808 0.7192 0.0194 0.0157 2.902 14.069 6.842 2163.949 1.590 30.435 1.434 0.84 410340. 0.1376
|
|
118.97 0.6040 0.6649 0.0145 0.0131 2.438 11.819 5.109 1817.786 1.335 22.725 1.275 0.84 411280. 0.1057
|
|
123.54 0.6272 0.5666 0.0095 0.0106 1.958 9.495 3.369 1460.372 1.073 14.983 1.046 0.84 412247. 0.0704
|
|
128.12 0.6504 0.3787 0.0046 0.0079 1.467 7.114 1.626 1094.234 0.804 7.234 0.674 0.84 413238. 0.0315
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|
132.69 0.6737
|
|
|
|
|
|
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|
PROP RPM = 14000
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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 0.1082 0.0453 10.492 47.234 44.282 7823.703 5.336 196.967 2.567 0.89 426200. 0.6265
|
|
4.98 0.0235 0.0552 0.1067 0.0454 10.501 47.274 43.665 7830.284 5.341 194.223 2.529 0.89 426497. 0.6129
|
|
9.96 0.0469 0.1088 0.1050 0.0453 10.491 47.233 42.981 7823.509 5.336 191.180 2.492 0.89 426820. 0.5991
|
|
14.93 0.0704 0.1607 0.1032 0.0452 10.464 47.108 42.228 7802.794 5.322 187.829 2.455 0.89 427168. 0.5850
|
|
19.91 0.0939 0.2111 0.1011 0.0450 10.416 46.894 41.401 7767.342 5.298 184.152 2.418 0.89 427543. 0.5705
|
|
24.89 0.1173 0.2598 0.0989 0.0447 10.348 46.586 40.498 7716.390 5.263 180.136 2.380 0.89 427946. 0.5556
|
|
29.87 0.1408 0.3068 0.0965 0.0443 10.258 46.180 39.516 7649.173 5.217 175.768 2.343 0.89 428376. 0.5402
|
|
34.85 0.1643 0.3522 0.0939 0.0438 10.145 45.672 38.453 7565.004 5.160 171.039 2.305 0.89 428834. 0.5243
|
|
39.83 0.1878 0.3959 0.0911 0.0432 10.008 45.058 37.307 7463.243 5.091 165.941 2.267 0.89 429321. 0.5079
|
|
44.80 0.2112 0.4377 0.0881 0.0425 9.848 44.334 36.077 7343.288 5.009 160.472 2.228 0.89 429836. 0.4909
|
|
49.78 0.2347 0.4777 0.0849 0.0417 9.661 43.496 34.764 7204.448 4.914 154.630 2.189 0.89 430381. 0.4732
|
|
54.76 0.2582 0.5157 0.0815 0.0408 9.449 42.539 33.368 7046.037 4.806 148.421 2.148 0.89 430955. 0.4550
|
|
59.74 0.2816 0.5517 0.0779 0.0398 9.210 41.463 31.894 6867.706 4.684 141.863 2.106 0.89 431558. 0.4362
|
|
64.72 0.3051 0.5855 0.0741 0.0386 8.944 40.265 30.346 6669.332 4.549 134.980 2.064 0.89 432191. 0.4169
|
|
69.70 0.3286 0.6173 0.0702 0.0374 8.651 38.945 28.732 6450.789 4.400 127.798 2.020 0.89 432854. 0.3971
|
|
74.67 0.3520 0.6467 0.0661 0.0360 8.330 37.502 27.055 6211.768 4.237 120.340 1.975 0.89 433546. 0.3768
|
|
79.65 0.3755 0.6738 0.0619 0.0345 7.981 35.932 25.321 5951.691 4.060 112.626 1.930 0.89 434269. 0.3561
|
|
84.63 0.3990 0.6984 0.0575 0.0328 7.604 34.232 23.533 5670.018 3.867 104.675 1.883 0.90 435022. 0.3349
|
|
89.61 0.4224 0.7199 0.0530 0.0311 7.201 32.421 21.696 5370.139 3.663 96.504 1.832 0.90 435805. 0.3130
|
|
94.59 0.4459 0.7373 0.0484 0.0293 6.778 30.514 19.813 5054.226 3.447 88.128 1.778 0.90 436619. 0.2902
|
|
99.57 0.4694 0.7494 0.0437 0.0274 6.337 28.531 17.887 4725.760 3.223 79.562 1.717 0.90 437464. 0.2663
|
|
104.54 0.4928 0.7519 0.0389 0.0255 5.902 26.571 15.920 4401.198 3.002 70.811 1.641 0.90 438340. 0.2401
|
|
109.52 0.5163 0.7467 0.0340 0.0235 5.443 24.506 13.918 4059.050 2.769 61.907 1.555 0.90 439247. 0.2128
|
|
114.50 0.5398 0.7312 0.0290 0.0214 4.963 22.344 11.886 3700.935 2.524 52.868 1.457 0.90 440185. 0.1842
|
|
119.48 0.5633 0.7012 0.0240 0.0193 4.465 20.103 9.828 3329.709 2.271 43.716 1.339 0.90 441154. 0.1539
|
|
124.46 0.5867 0.6505 0.0189 0.0171 3.954 17.801 7.750 2948.503 2.011 34.473 1.192 0.90 442155. 0.1217
|
|
129.44 0.6102 0.5688 0.0138 0.0148 3.434 15.459 5.659 2560.572 1.747 25.172 1.002 0.91 443186. 0.0875
|
|
134.41 0.6337 0.4390 0.0087 0.0126 2.910 13.099 3.564 2169.715 1.480 15.852 0.745 0.91 444248. 0.0516
|
|
139.39 0.6571 0.2294 0.0036 0.0103 2.386 10.741 1.472 1779.034 1.213 6.549 0.375 0.91 445333. 0.0167
|
|
144.37 0.6806
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