575 lines
102 KiB
Plaintext
575 lines
102 KiB
Plaintext
15x10 (15x10.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 0.1096 0.0521 0.003 0.200 0.177 2.372 0.023 0.787 33.818 0.06 26765. 0.5563
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0.40 0.0283 0.0580 0.1083 0.0528 0.003 0.203 0.175 2.406 0.023 0.777 32.940 0.06 26787. 0.5386
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0.80 0.0566 0.1129 0.1068 0.0535 0.003 0.206 0.172 2.438 0.023 0.767 32.059 0.06 26810. 0.5206
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1.21 0.0849 0.1647 0.1052 0.0542 0.003 0.209 0.170 2.469 0.024 0.755 31.178 0.06 26837. 0.5025
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1.61 0.1131 0.2135 0.1034 0.0548 0.003 0.211 0.167 2.497 0.024 0.742 30.301 0.06 26865. 0.4842
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2.01 0.1414 0.2592 0.1015 0.0554 0.003 0.213 0.164 2.523 0.024 0.728 29.430 0.06 26896. 0.4658
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2.41 0.1697 0.3019 0.0993 0.0558 0.003 0.215 0.160 2.544 0.024 0.713 28.566 0.06 26930. 0.4473
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2.81 0.1980 0.3417 0.0970 0.0562 0.003 0.216 0.156 2.560 0.024 0.696 27.712 0.06 26966. 0.4288
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3.21 0.2263 0.3786 0.0944 0.0564 0.003 0.217 0.152 2.572 0.025 0.678 26.867 0.06 27006. 0.4102
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3.62 0.2546 0.4127 0.0916 0.0565 0.003 0.218 0.148 2.576 0.025 0.658 26.033 0.06 27048. 0.3916
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4.02 0.2828 0.4440 0.0887 0.0565 0.003 0.218 0.143 2.574 0.025 0.636 25.208 0.06 27093. 0.3729
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4.42 0.3111 0.4726 0.0854 0.0562 0.003 0.217 0.138 2.563 0.024 0.613 24.391 0.06 27141. 0.3542
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4.82 0.3394 0.4984 0.0820 0.0558 0.003 0.215 0.132 2.544 0.024 0.588 23.581 0.06 27191. 0.3355
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5.22 0.3677 0.5215 0.0783 0.0552 0.003 0.213 0.126 2.515 0.024 0.562 22.775 0.06 27245. 0.3166
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5.62 0.3960 0.5417 0.0743 0.0543 0.003 0.209 0.120 2.476 0.024 0.533 21.970 0.06 27302. 0.2976
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6.03 0.4243 0.5591 0.0702 0.0533 0.003 0.205 0.113 2.427 0.023 0.504 21.162 0.06 27362. 0.2786
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6.43 0.4525 0.5734 0.0659 0.0520 0.003 0.200 0.106 2.369 0.023 0.473 20.346 0.06 27424. 0.2594
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6.83 0.4808 0.5844 0.0614 0.0505 0.003 0.194 0.099 2.301 0.022 0.440 19.517 0.06 27490. 0.2402
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7.23 0.5091 0.5918 0.0567 0.0488 0.003 0.188 0.091 2.223 0.021 0.407 18.667 0.06 27559. 0.2209
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7.63 0.5374 0.5952 0.0519 0.0469 0.003 0.181 0.084 2.137 0.020 0.373 17.787 0.06 27630. 0.2014
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8.04 0.5657 0.5941 0.0470 0.0448 0.003 0.173 0.076 2.041 0.019 0.338 16.866 0.06 27705. 0.1818
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8.44 0.5940 0.5877 0.0421 0.0425 0.003 0.164 0.068 1.937 0.018 0.302 15.889 0.06 27783. 0.1619
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8.84 0.6222 0.5748 0.0370 0.0400 0.002 0.154 0.060 1.824 0.017 0.265 14.835 0.06 27863. 0.1417
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9.24 0.6505 0.5541 0.0318 0.0373 0.002 0.144 0.051 1.702 0.016 0.228 13.679 0.06 27947. 0.1212
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9.64 0.6788 0.5233 0.0266 0.0345 0.002 0.133 0.043 1.571 0.015 0.191 12.380 0.06 28033. 0.1003
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10.04 0.7071 0.4792 0.0213 0.0314 0.002 0.121 0.034 1.433 0.014 0.153 10.884 0.06 28123. 0.0789
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10.45 0.7354 0.4169 0.0160 0.0282 0.002 0.109 0.026 1.286 0.012 0.115 9.103 0.06 28215. 0.0572
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10.85 0.7637 0.3280 0.0107 0.0248 0.002 0.096 0.017 1.132 0.011 0.077 6.898 0.06 28311. 0.0354
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11.25 0.7919 0.1986 0.0053 0.0213 0.001 0.082 0.009 0.970 0.009 0.038 4.027 0.06 28409. 0.0146
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11.65 0.8202 0.0015 0.0000 0.0176 0.001 0.068 0.000 0.802 0.008 0.000 0.030 0.06 28510. 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 0.1101 0.0466 0.023 0.718 0.711 16.978 0.081 3.161 18.985 0.12 53529. 0.6261
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0.81 0.0285 0.0654 0.1088 0.0474 0.023 0.730 0.702 17.270 0.082 3.123 18.440 0.12 53573. 0.6044
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1.62 0.0569 0.1269 0.1073 0.0482 0.024 0.742 0.693 17.555 0.084 3.081 17.898 0.12 53621. 0.5827
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2.43 0.0854 0.1847 0.1057 0.0489 0.024 0.753 0.682 17.827 0.085 3.035 17.360 0.12 53674. 0.5609
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3.24 0.1139 0.2387 0.1039 0.0496 0.024 0.764 0.671 18.080 0.086 2.984 16.828 0.12 53731. 0.5391
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4.04 0.1424 0.2891 0.1020 0.0502 0.025 0.774 0.658 18.308 0.087 2.927 16.305 0.12 53794. 0.5174
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4.85 0.1708 0.3360 0.0998 0.0508 0.025 0.782 0.644 18.505 0.088 2.866 15.792 0.12 53862. 0.4958
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5.66 0.1993 0.3795 0.0975 0.0512 0.025 0.789 0.629 18.664 0.089 2.798 15.288 0.12 53936. 0.4743
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6.47 0.2278 0.4197 0.0949 0.0515 0.025 0.794 0.613 18.779 0.090 2.725 14.796 0.12 54015. 0.4530
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7.28 0.2562 0.4568 0.0921 0.0517 0.025 0.796 0.595 18.841 0.090 2.645 14.314 0.12 54100. 0.4318
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8.09 0.2847 0.4909 0.0891 0.0517 0.025 0.796 0.575 18.845 0.090 2.558 13.844 0.12 54191. 0.4107
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8.90 0.3132 0.5220 0.0859 0.0515 0.025 0.794 0.554 18.782 0.090 2.465 13.383 0.12 54288. 0.3897
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9.71 0.3417 0.5503 0.0824 0.0511 0.025 0.788 0.532 18.646 0.089 2.365 12.932 0.12 54391. 0.3689
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10.51 0.3701 0.5757 0.0786 0.0506 0.025 0.779 0.508 18.432 0.088 2.258 12.490 0.12 54499. 0.3481
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11.32 0.3986 0.5984 0.0747 0.0497 0.024 0.766 0.482 18.134 0.087 2.144 12.053 0.12 54614. 0.3273
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12.13 0.4271 0.6182 0.0705 0.0487 0.024 0.750 0.455 17.753 0.085 2.023 11.622 0.12 54735. 0.3066
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12.94 0.4555 0.6351 0.0661 0.0474 0.023 0.731 0.427 17.288 0.083 1.898 11.194 0.12 54862. 0.2860
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13.75 0.4840 0.6489 0.0616 0.0459 0.022 0.708 0.397 16.742 0.080 1.767 10.765 0.12 54995. 0.2654
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14.56 0.5125 0.6594 0.0569 0.0442 0.022 0.681 0.367 16.116 0.077 1.633 10.331 0.12 55134. 0.2449
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15.37 0.5409 0.6663 0.0521 0.0423 0.021 0.651 0.336 15.411 0.074 1.495 9.889 0.12 55279. 0.2242
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16.18 0.5694 0.6689 0.0471 0.0401 0.020 0.618 0.304 14.629 0.070 1.353 9.432 0.12 55430. 0.2035
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16.99 0.5979 0.6667 0.0421 0.0378 0.018 0.582 0.272 13.769 0.066 1.209 8.953 0.12 55587. 0.1826
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17.79 0.6264 0.6585 0.0370 0.0352 0.017 0.542 0.239 12.832 0.061 1.062 8.441 0.12 55750. 0.1614
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18.60 0.6548 0.6426 0.0318 0.0324 0.016 0.500 0.205 11.820 0.056 0.913 7.880 0.12 55920. 0.1397
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19.41 0.6833 0.6168 0.0266 0.0294 0.014 0.454 0.172 10.734 0.051 0.763 7.248 0.12 56095. 0.1174
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20.22 0.7118 0.5769 0.0213 0.0263 0.013 0.405 0.137 9.575 0.046 0.611 6.508 0.12 56276. 0.0944
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21.03 0.7402 0.5164 0.0160 0.0229 0.011 0.353 0.103 8.346 0.040 0.458 5.602 0.12 56463. 0.0703
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21.84 0.7687 0.4230 0.0106 0.0193 0.009 0.298 0.069 7.050 0.034 0.306 4.419 0.12 56657. 0.0453
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22.65 0.7972 0.2718 0.0053 0.0156 0.008 0.241 0.034 5.693 0.027 0.153 2.738 0.12 56855. 0.0199
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23.46 0.8257 0.0024 0.0000 0.0117 0.006 0.181 0.000 4.277 0.020 0.001 0.024 0.12 57058. 0.0000
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PROP RPM = 3000
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V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
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(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
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0.00 0.0000 0.0000 0.1105 0.0444 0.073 1.538 1.604 54.595 0.174 7.136 13.328 0.18 80293. 0.6604
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1.22 0.0286 0.0690 0.1092 0.0452 0.075 1.567 1.585 55.617 0.177 7.051 12.928 0.18 80358. 0.6367
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2.43 0.0571 0.1337 0.1077 0.0460 0.076 1.595 1.564 56.616 0.180 6.957 12.531 0.18 80430. 0.6130
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3.65 0.0857 0.1943 0.1061 0.0468 0.077 1.622 1.541 57.573 0.183 6.853 12.138 0.18 80510. 0.5894
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4.87 0.1142 0.2508 0.1043 0.0475 0.078 1.647 1.515 58.467 0.186 6.739 11.752 0.18 80597. 0.5659
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6.09 0.1428 0.3034 0.1024 0.0482 0.079 1.670 1.487 59.279 0.189 6.612 11.374 0.18 80691. 0.5425
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7.30 0.1714 0.3523 0.1002 0.0488 0.080 1.690 1.455 59.985 0.191 6.473 11.004 0.18 80794. 0.5193
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8.52 0.1999 0.3975 0.0979 0.0492 0.081 1.706 1.421 60.563 0.193 6.321 10.643 0.18 80905. 0.4963
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9.74 0.2285 0.4393 0.0953 0.0496 0.082 1.718 1.384 60.988 0.194 6.155 10.292 0.18 81025. 0.4736
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10.95 0.2570 0.4778 0.0925 0.0498 0.082 1.725 1.343 61.235 0.195 5.975 9.950 0.18 81153. 0.4511
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12.17 0.2856 0.5131 0.0895 0.0498 0.082 1.727 1.299 61.280 0.195 5.780 9.617 0.18 81290. 0.4288
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13.39 0.3142 0.5455 0.0862 0.0497 0.082 1.721 1.252 61.098 0.194 5.569 9.294 0.18 81436. 0.4068
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14.60 0.3427 0.5749 0.0827 0.0493 0.081 1.709 1.201 60.665 0.193 5.342 8.979 0.18 81591. 0.3849
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15.82 0.3713 0.6015 0.0790 0.0487 0.080 1.689 1.146 59.960 0.191 5.099 8.672 0.18 81755. 0.3632
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17.04 0.3998 0.6253 0.0750 0.0479 0.079 1.661 1.088 58.968 0.188 4.841 8.371 0.18 81928. 0.3416
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18.26 0.4284 0.6464 0.0707 0.0469 0.077 1.625 1.027 57.686 0.184 4.569 8.076 0.18 82111. 0.3202
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19.47 0.4570 0.6646 0.0663 0.0456 0.075 1.581 0.963 56.116 0.179 4.284 7.786 0.18 82302. 0.2989
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20.69 0.4855 0.6800 0.0618 0.0441 0.073 1.529 0.897 54.262 0.173 3.989 7.497 0.18 82503. 0.2777
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21.91 0.5141 0.6922 0.0571 0.0424 0.070 1.469 0.828 52.131 0.166 3.685 7.208 0.18 82713. 0.2566
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23.12 0.5426 0.7010 0.0522 0.0404 0.067 1.401 0.758 49.724 0.158 3.372 6.915 0.18 82931. 0.2355
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24.34 0.5712 0.7059 0.0473 0.0382 0.063 1.325 0.686 47.044 0.150 3.052 6.615 0.18 83159. 0.2144
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25.56 0.5998 0.7063 0.0422 0.0358 0.059 1.242 0.613 44.094 0.140 2.726 6.303 0.18 83396. 0.1930
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26.78 0.6283 0.7010 0.0371 0.0332 0.055 1.152 0.538 40.876 0.130 2.394 5.972 0.18 83643. 0.1714
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27.99 0.6569 0.6886 0.0319 0.0304 0.050 1.053 0.463 37.392 0.119 2.058 5.612 0.18 83898. 0.1493
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29.21 0.6854 0.6666 0.0266 0.0273 0.045 0.948 0.386 33.648 0.107 1.718 5.206 0.18 84162. 0.1265
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30.43 0.7140 0.6307 0.0213 0.0241 0.040 0.835 0.309 29.649 0.094 1.375 4.729 0.18 84436. 0.1028
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31.64 0.7426 0.5737 0.0160 0.0206 0.034 0.716 0.232 25.404 0.081 1.030 4.136 0.18 84718. 0.0779
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32.86 0.7711 0.4811 0.0106 0.0170 0.028 0.590 0.154 20.927 0.067 0.685 3.339 0.18 85010. 0.0513
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34.08 0.7997 0.3202 0.0053 0.0132 0.022 0.457 0.077 16.234 0.052 0.341 2.143 0.18 85310. 0.0232
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35.29 0.8282 -0.0015 0.0000 0.0092 0.015 0.319 0.000 11.336 0.036 -0.001 -0.010 0.18 85613. 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 0.1109 0.0432 0.169 2.663 2.862 126.020 0.301 12.730 10.301 0.24 107054. 0.6817
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1.63 0.0286 0.0712 0.1096 0.0441 0.172 2.715 2.828 128.505 0.307 12.581 9.983 0.24 107142. 0.6568
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3.25 0.0572 0.1378 0.1081 0.0449 0.176 2.767 2.791 130.937 0.313 12.415 9.668 0.24 107238. 0.6319
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4.88 0.0859 0.2001 0.1065 0.0457 0.179 2.816 2.750 133.270 0.318 12.231 9.358 0.24 107344. 0.6070
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6.50 0.1145 0.2582 0.1048 0.0464 0.182 2.862 2.704 135.457 0.323 12.027 9.054 0.24 107461. 0.5824
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8.13 0.1431 0.3121 0.1028 0.0471 0.184 2.904 2.654 137.446 0.328 11.803 8.757 0.24 107587. 0.5580
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9.76 0.1717 0.3621 0.1006 0.0477 0.187 2.941 2.598 139.185 0.332 11.556 8.467 0.24 107725. 0.5338
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11.38 0.2003 0.4084 0.0983 0.0482 0.189 2.971 2.537 140.615 0.336 11.286 8.184 0.24 107873. 0.5100
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13.01 0.2289 0.4511 0.0957 0.0486 0.190 2.994 2.471 141.679 0.338 10.991 7.910 0.24 108033. 0.4864
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14.63 0.2576 0.4904 0.0929 0.0488 0.191 3.007 2.399 142.318 0.340 10.669 7.645 0.24 108205. 0.4631
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16.26 0.2862 0.5266 0.0899 0.0489 0.191 3.010 2.320 142.471 0.340 10.321 7.387 0.24 108389. 0.4402
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17.89 0.3148 0.5596 0.0866 0.0487 0.191 3.002 2.236 142.077 0.339 9.944 7.137 0.24 108584. 0.4174
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19.51 0.3434 0.5898 0.0831 0.0484 0.189 2.981 2.145 141.080 0.337 9.539 6.895 0.24 108792. 0.3950
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21.14 0.3720 0.6171 0.0793 0.0478 0.187 2.946 2.047 139.427 0.333 9.105 6.659 0.24 109011. 0.3727
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22.76 0.4006 0.6417 0.0753 0.0470 0.184 2.897 1.943 137.083 0.327 8.644 6.430 0.24 109243. 0.3506
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24.39 0.4293 0.6636 0.0710 0.0460 0.180 2.832 1.834 134.038 0.320 8.158 6.206 0.24 109487. 0.3288
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26.02 0.4579 0.6827 0.0666 0.0447 0.175 2.753 1.720 130.297 0.311 7.649 5.986 0.24 109744. 0.3071
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27.64 0.4865 0.6991 0.0620 0.0432 0.169 2.660 1.601 125.872 0.300 7.121 5.769 0.24 110012. 0.2855
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29.27 0.5151 0.7125 0.0573 0.0414 0.162 2.552 1.479 120.772 0.288 6.577 5.553 0.24 110293. 0.2641
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30.89 0.5437 0.7226 0.0524 0.0394 0.154 2.430 1.353 115.005 0.275 6.017 5.335 0.24 110586. 0.2428
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32.52 0.5723 0.7291 0.0474 0.0372 0.146 2.294 1.224 108.575 0.259 5.445 5.114 0.24 110891. 0.2213
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34.15 0.6010 0.7313 0.0423 0.0348 0.136 2.145 1.093 101.488 0.242 4.862 4.885 0.24 111208. 0.1998
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35.77 0.6296 0.7282 0.0372 0.0321 0.126 1.981 0.960 93.750 0.224 4.269 4.643 0.24 111538. 0.1780
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37.40 0.6582 0.7183 0.0319 0.0293 0.114 1.804 0.825 85.368 0.204 3.668 4.382 0.24 111880. 0.1556
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39.02 0.6868 0.6993 0.0267 0.0262 0.102 1.613 0.688 76.352 0.182 3.060 4.087 0.24 112233. 0.1326
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40.65 0.7154 0.6668 0.0213 0.0229 0.089 1.410 0.550 66.717 0.159 2.448 3.742 0.24 112599. 0.1086
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42.28 0.7440 0.6132 0.0160 0.0194 0.076 1.194 0.412 56.488 0.135 1.833 3.308 0.24 112978. 0.0831
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43.90 0.7727 0.5225 0.0106 0.0157 0.061 0.966 0.274 45.693 0.109 1.217 2.715 0.25 113368. 0.0555
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45.53 0.8013 0.3567 0.0052 0.0118 0.046 0.726 0.135 34.376 0.082 0.602 1.787 0.25 113769. 0.0257
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47.15 0.8299 -0.0081 -0.0001 0.0077 0.030 0.477 -0.002 22.554 0.054 -0.009 -0.039 0.25 114173. 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 0.1113 0.0425 0.325 4.097 4.490 242.366 0.463 19.970 8.402 0.30 133813. 0.6964
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2.03 0.0286 0.0726 0.1100 0.0434 0.332 4.181 4.438 247.320 0.472 19.739 8.139 0.30 133923. 0.6707
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4.07 0.0573 0.1405 0.1086 0.0443 0.338 4.263 4.380 252.174 0.482 19.482 7.878 0.30 134044. 0.6449
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6.10 0.0859 0.2039 0.1070 0.0451 0.344 4.342 4.316 256.838 0.491 19.197 7.622 0.30 134177. 0.6194
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8.14 0.1146 0.2629 0.1052 0.0459 0.350 4.416 4.245 261.215 0.499 18.880 7.370 0.30 134322. 0.5940
|
|
10.17 0.1432 0.3177 0.1033 0.0466 0.356 4.483 4.166 265.205 0.507 18.531 7.125 0.30 134481. 0.5689
|
|
12.21 0.1719 0.3685 0.1011 0.0472 0.360 4.542 4.080 268.700 0.513 18.147 6.887 0.30 134653. 0.5441
|
|
14.24 0.2005 0.4154 0.0988 0.0477 0.364 4.591 3.985 271.589 0.519 17.725 6.655 0.30 134839. 0.5197
|
|
16.27 0.2291 0.4588 0.0962 0.0481 0.367 4.628 3.881 273.755 0.523 17.263 6.430 0.30 135040. 0.4955
|
|
18.31 0.2578 0.4987 0.0934 0.0483 0.369 4.650 3.768 275.082 0.525 16.760 6.213 0.30 135255. 0.4718
|
|
20.34 0.2864 0.5353 0.0904 0.0484 0.369 4.656 3.645 275.447 0.526 16.215 6.003 0.30 135485. 0.4483
|
|
22.38 0.3151 0.5689 0.0871 0.0482 0.368 4.644 3.513 274.733 0.525 15.625 5.799 0.30 135730. 0.4252
|
|
24.41 0.3437 0.5996 0.0836 0.0479 0.366 4.612 3.370 272.824 0.521 14.990 5.603 0.30 135990. 0.4023
|
|
26.44 0.3723 0.6274 0.0798 0.0473 0.362 4.558 3.217 269.618 0.515 14.309 5.412 0.30 136265. 0.3797
|
|
28.48 0.4010 0.6526 0.0757 0.0465 0.355 4.480 3.054 265.043 0.506 13.585 5.227 0.30 136556. 0.3573
|
|
30.51 0.4296 0.6751 0.0715 0.0455 0.347 4.380 2.883 259.079 0.495 12.822 5.047 0.30 136862. 0.3352
|
|
32.55 0.4583 0.6949 0.0670 0.0442 0.338 4.255 2.703 251.735 0.481 12.023 4.870 0.30 137183. 0.3132
|
|
34.58 0.4869 0.7121 0.0624 0.0427 0.326 4.108 2.517 243.032 0.464 11.194 4.697 0.30 137519. 0.2915
|
|
36.62 0.5156 0.7263 0.0576 0.0409 0.312 3.939 2.324 232.987 0.445 10.338 4.525 0.30 137871. 0.2698
|
|
38.65 0.5442 0.7375 0.0527 0.0389 0.297 3.746 2.127 221.616 0.423 9.460 4.353 0.30 138238. 0.2483
|
|
40.68 0.5728 0.7452 0.0477 0.0367 0.280 3.532 1.925 208.928 0.399 8.561 4.178 0.30 138620. 0.2267
|
|
42.72 0.6015 0.7489 0.0426 0.0342 0.261 3.295 1.719 194.934 0.372 7.644 3.999 0.30 139017. 0.2051
|
|
44.75 0.6301 0.7476 0.0374 0.0315 0.241 3.037 1.509 179.644 0.343 6.713 3.810 0.30 139430. 0.1831
|
|
46.79 0.6588 0.7398 0.0322 0.0286 0.219 2.757 1.297 163.072 0.311 5.768 3.607 0.30 139858. 0.1607
|
|
48.82 0.6874 0.7233 0.0268 0.0255 0.195 2.455 1.082 145.240 0.277 4.814 3.380 0.30 140301. 0.1375
|
|
50.86 0.7160 0.6939 0.0215 0.0222 0.169 2.133 0.866 126.178 0.241 3.851 3.113 0.31 140759. 0.1133
|
|
52.89 0.7447 0.6438 0.0161 0.0186 0.142 1.791 0.649 105.931 0.202 2.885 2.777 0.31 141233. 0.0875
|
|
54.92 0.7733 0.5565 0.0107 0.0148 0.113 1.429 0.431 84.562 0.162 1.917 2.311 0.31 141721. 0.0594
|
|
56.96 0.8020 0.3900 0.0053 0.0109 0.083 1.051 0.214 62.153 0.119 0.952 1.562 0.31 142223. 0.0283
|
|
58.99 0.8306 -0.0057 0.0000 0.0068 0.052 0.655 -0.002 38.732 0.074 -0.008 -0.022 0.31 142727. 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 0.1118 0.0422 0.557 5.850 6.495 415.264 0.661 28.891 7.094 0.36 160569. 0.7073
|
|
2.44 0.0287 0.0736 0.1106 0.0431 0.569 5.973 6.421 423.997 0.675 28.563 6.869 0.36 160701. 0.6809
|
|
4.89 0.0573 0.1424 0.1091 0.0439 0.580 6.094 6.339 432.561 0.688 28.196 6.647 0.36 160846. 0.6546
|
|
7.33 0.0860 0.2065 0.1076 0.0448 0.591 6.210 6.247 440.795 0.702 27.789 6.428 0.36 161006. 0.6285
|
|
9.77 0.1146 0.2662 0.1058 0.0456 0.601 6.319 6.146 448.534 0.714 27.336 6.215 0.36 161181. 0.6027
|
|
12.21 0.1433 0.3216 0.1039 0.0463 0.611 6.418 6.033 455.598 0.725 26.836 6.006 0.36 161372. 0.5771
|
|
14.66 0.1720 0.3729 0.1017 0.0469 0.619 6.505 5.909 461.799 0.735 26.284 5.804 0.36 161579. 0.5519
|
|
17.10 0.2006 0.4203 0.0994 0.0474 0.626 6.578 5.773 466.939 0.743 25.677 5.607 0.36 161803. 0.5270
|
|
19.54 0.2293 0.4641 0.0968 0.0478 0.631 6.632 5.623 470.816 0.749 25.013 5.417 0.36 162044. 0.5025
|
|
21.98 0.2579 0.5044 0.0940 0.0481 0.635 6.666 5.460 473.221 0.753 24.288 5.234 0.36 162303. 0.4784
|
|
24.43 0.2866 0.5415 0.0910 0.0482 0.636 6.676 5.284 473.944 0.754 23.501 5.056 0.36 162579. 0.4546
|
|
26.87 0.3153 0.5754 0.0877 0.0480 0.634 6.660 5.092 472.777 0.752 22.649 4.885 0.36 162874. 0.4312
|
|
29.31 0.3439 0.6065 0.0841 0.0477 0.630 6.614 4.886 469.518 0.747 21.732 4.720 0.36 163187. 0.4081
|
|
31.75 0.3726 0.6348 0.0803 0.0471 0.622 6.536 4.664 463.987 0.738 20.747 4.560 0.36 163518. 0.3852
|
|
34.20 0.4012 0.6604 0.0763 0.0463 0.612 6.425 4.429 456.057 0.726 19.700 4.405 0.36 163867. 0.3626
|
|
36.64 0.4299 0.6833 0.0720 0.0453 0.598 6.278 4.180 445.689 0.709 18.594 4.254 0.36 164235. 0.3402
|
|
39.08 0.4586 0.7038 0.0675 0.0440 0.581 6.098 3.920 432.900 0.689 17.437 4.107 0.36 164621. 0.3181
|
|
41.53 0.4872 0.7215 0.0628 0.0424 0.560 5.885 3.650 417.725 0.665 16.236 3.963 0.36 165025. 0.2962
|
|
43.97 0.5159 0.7365 0.0580 0.0407 0.537 5.638 3.371 400.195 0.637 14.996 3.821 0.36 165448. 0.2745
|
|
46.41 0.5446 0.7486 0.0531 0.0386 0.510 5.358 3.085 380.334 0.605 13.722 3.679 0.36 165889. 0.2528
|
|
48.85 0.5732 0.7573 0.0481 0.0364 0.480 5.045 2.792 358.163 0.570 12.419 3.536 0.36 166349. 0.2311
|
|
51.30 0.6019 0.7621 0.0429 0.0339 0.447 4.701 2.493 333.697 0.531 11.091 3.389 0.36 166826. 0.2093
|
|
53.74 0.6305 0.7623 0.0377 0.0312 0.412 4.324 2.190 306.955 0.489 9.740 3.236 0.36 167322. 0.1873
|
|
56.18 0.6592 0.7563 0.0324 0.0282 0.373 3.916 1.882 277.961 0.442 8.370 3.071 0.36 167837. 0.1648
|
|
58.62 0.6879 0.7420 0.0270 0.0251 0.331 3.476 1.571 246.753 0.393 6.986 2.887 0.37 168369. 0.1415
|
|
61.07 0.7165 0.7152 0.0216 0.0217 0.286 3.006 1.257 213.385 0.340 5.590 2.672 0.37 168920. 0.1172
|
|
63.51 0.7452 0.6683 0.0162 0.0181 0.239 2.507 0.942 177.937 0.283 4.188 2.400 0.37 169489. 0.0911
|
|
65.95 0.7738 0.5843 0.0108 0.0143 0.188 1.979 0.626 140.518 0.224 2.785 2.021 0.37 170076. 0.0625
|
|
68.39 0.8025 0.4182 0.0054 0.0103 0.136 1.427 0.311 101.274 0.161 1.385 1.395 0.37 170679. 0.0305
|
|
70.84 0.8312 -0.0041 0.0000 0.0061 0.081 0.849 -0.002 60.235 0.096 -0.008 -0.013 0.37 171282. 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 0.1124 0.0420 0.881 7.934 8.888 657.080 0.896 39.536 6.136 0.42 187322. 0.7155
|
|
2.85 0.0287 0.0743 0.1112 0.0429 0.900 8.105 8.789 671.241 0.916 39.096 5.939 0.42 187475. 0.6888
|
|
5.70 0.0574 0.1437 0.1098 0.0438 0.919 8.273 8.679 685.139 0.935 38.603 5.745 0.42 187645. 0.6621
|
|
8.56 0.0861 0.2084 0.1082 0.0447 0.937 8.434 8.555 698.514 0.953 38.054 5.555 0.42 187832. 0.6356
|
|
11.41 0.1147 0.2686 0.1065 0.0455 0.954 8.586 8.418 711.096 0.970 37.444 5.369 0.42 188036. 0.6094
|
|
14.26 0.1434 0.3244 0.1046 0.0462 0.969 8.725 8.266 722.593 0.986 36.766 5.188 0.42 188259. 0.5835
|
|
17.11 0.1721 0.3761 0.1024 0.0469 0.983 8.847 8.098 732.700 1.000 36.018 5.013 0.42 188502. 0.5580
|
|
19.97 0.2008 0.4239 0.1001 0.0474 0.994 8.948 7.912 741.096 1.011 35.194 4.842 0.42 188764. 0.5328
|
|
22.82 0.2295 0.4680 0.0975 0.0478 1.002 9.025 7.709 747.452 1.020 34.290 4.678 0.42 189046. 0.5081
|
|
25.67 0.2582 0.5086 0.0947 0.0481 1.008 9.073 7.487 751.434 1.025 33.302 4.519 0.42 189349. 0.4837
|
|
28.52 0.2869 0.5459 0.0917 0.0482 1.009 9.089 7.246 752.702 1.027 32.228 4.366 0.42 189672. 0.4597
|
|
31.38 0.3155 0.5802 0.0883 0.0480 1.007 9.067 6.984 750.918 1.024 31.065 4.218 0.42 190017. 0.4361
|
|
34.23 0.3442 0.6116 0.0848 0.0477 1.000 9.005 6.702 745.760 1.017 29.810 4.076 0.42 190383. 0.4128
|
|
37.08 0.3729 0.6402 0.0809 0.0471 0.988 8.898 6.399 736.935 1.005 28.463 3.939 0.42 190770. 0.3897
|
|
39.93 0.4016 0.6662 0.0769 0.0463 0.971 8.745 6.076 724.240 0.988 27.028 3.806 0.42 191179. 0.3670
|
|
42.78 0.4303 0.6896 0.0726 0.0453 0.949 8.544 5.736 707.608 0.965 25.513 3.677 0.42 191609. 0.3444
|
|
45.64 0.4590 0.7105 0.0680 0.0440 0.921 8.296 5.379 687.066 0.937 23.927 3.551 0.42 192061. 0.3222
|
|
48.49 0.4877 0.7288 0.0634 0.0424 0.889 8.002 5.009 662.671 0.904 22.279 3.428 0.42 192534. 0.3001
|
|
51.34 0.5163 0.7444 0.0585 0.0406 0.851 7.661 4.626 634.473 0.866 20.578 3.307 0.42 193028. 0.2783
|
|
54.19 0.5450 0.7571 0.0536 0.0385 0.808 7.275 4.233 602.513 0.822 18.830 3.187 0.42 193544. 0.2565
|
|
57.05 0.5737 0.7667 0.0485 0.0363 0.760 6.844 3.831 566.822 0.773 17.042 3.066 0.42 194081. 0.2347
|
|
59.90 0.6024 0.7726 0.0433 0.0337 0.707 6.368 3.421 527.426 0.720 15.217 2.942 0.42 194640. 0.2129
|
|
62.75 0.6311 0.7739 0.0380 0.0310 0.650 5.848 3.004 484.356 0.661 13.363 2.813 0.42 195220. 0.1907
|
|
65.60 0.6598 0.7694 0.0327 0.0280 0.587 5.284 2.581 437.652 0.597 11.482 2.675 0.43 195821. 0.1681
|
|
68.45 0.6885 0.7569 0.0272 0.0248 0.519 4.677 2.154 387.372 0.528 9.581 2.522 0.43 196444. 0.1448
|
|
71.31 0.7171 0.7323 0.0218 0.0213 0.447 4.028 1.723 333.607 0.455 7.664 2.343 0.43 197087. 0.1203
|
|
74.16 0.7458 0.6880 0.0163 0.0177 0.371 3.338 1.290 276.483 0.377 5.738 2.116 0.43 197752. 0.0940
|
|
77.01 0.7745 0.6067 0.0108 0.0138 0.290 2.610 0.856 216.181 0.295 3.809 1.797 0.43 198438. 0.0650
|
|
79.86 0.8032 0.4406 0.0054 0.0098 0.205 1.847 0.424 152.937 0.209 1.887 1.258 0.43 199143. 0.0321
|
|
82.72 0.8319 -0.0120 -0.0001 0.0055 0.116 1.047 -0.006 86.746 0.118 -0.028 -0.033 0.43 199842. 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 0.1131 0.0421 1.316 10.366 11.681 981.139 1.171 51.957 5.400 0.48 214069. 0.7220
|
|
3.26 0.0287 0.0747 0.1119 0.0430 1.345 10.594 11.555 1002.751 1.197 51.394 5.226 0.48 214245. 0.6949
|
|
6.52 0.0574 0.1445 0.1105 0.0439 1.373 10.819 11.413 1023.982 1.222 50.763 5.055 0.48 214439. 0.6680
|
|
9.78 0.0861 0.2095 0.1090 0.0448 1.401 11.035 11.254 1044.431 1.247 50.056 4.887 0.48 214652. 0.6413
|
|
13.04 0.1148 0.2700 0.1073 0.0456 1.426 11.238 11.076 1063.684 1.270 49.268 4.723 0.48 214886. 0.6149
|
|
16.30 0.1434 0.3261 0.1054 0.0463 1.450 11.424 10.879 1081.300 1.291 48.391 4.563 0.48 215142. 0.5888
|
|
19.56 0.1721 0.3780 0.1032 0.0470 1.471 11.588 10.661 1096.807 1.309 47.420 4.409 0.48 215419. 0.5631
|
|
22.82 0.2008 0.4261 0.1009 0.0476 1.488 11.725 10.420 1109.718 1.325 46.348 4.259 0.48 215719. 0.5378
|
|
26.08 0.2295 0.4704 0.0984 0.0480 1.501 11.828 10.155 1119.532 1.336 45.170 4.114 0.48 216042. 0.5129
|
|
29.34 0.2582 0.5112 0.0955 0.0483 1.510 11.894 9.865 1125.742 1.344 43.881 3.975 0.48 216389. 0.4884
|
|
32.60 0.2869 0.5489 0.0925 0.0483 1.512 11.916 9.549 1127.832 1.346 42.476 3.840 0.48 216759. 0.4642
|
|
35.86 0.3156 0.5834 0.0892 0.0482 1.509 11.889 9.207 1125.294 1.343 40.952 3.711 0.48 217154. 0.4405
|
|
39.12 0.3443 0.6151 0.0856 0.0479 1.499 11.808 8.837 1117.639 1.334 39.307 3.586 0.48 217573. 0.4170
|
|
42.38 0.3729 0.6440 0.0817 0.0473 1.481 11.669 8.440 1104.426 1.318 37.540 3.466 0.48 218017. 0.3939
|
|
45.64 0.4016 0.6703 0.0776 0.0465 1.455 11.467 8.016 1085.340 1.296 35.656 3.350 0.48 218485. 0.3710
|
|
48.90 0.4303 0.6940 0.0733 0.0454 1.422 11.202 7.568 1060.278 1.266 33.664 3.238 0.48 218977. 0.3484
|
|
52.16 0.4590 0.7153 0.0688 0.0441 1.380 10.875 7.099 1029.279 1.229 31.577 3.128 0.48 219494. 0.3261
|
|
55.42 0.4877 0.7341 0.0640 0.0425 1.331 10.485 6.612 992.430 1.185 29.409 3.022 0.48 220035. 0.3039
|
|
58.68 0.5164 0.7503 0.0592 0.0407 1.274 10.035 6.108 949.812 1.134 27.168 2.917 0.48 220601. 0.2820
|
|
61.94 0.5451 0.7638 0.0541 0.0386 1.209 9.524 5.590 901.488 1.076 24.866 2.813 0.48 221191. 0.2601
|
|
65.20 0.5738 0.7741 0.0490 0.0363 1.137 8.954 5.061 847.507 1.012 22.509 2.708 0.48 221805. 0.2383
|
|
68.46 0.6024 0.7809 0.0438 0.0338 1.057 8.324 4.520 787.909 0.940 20.105 2.602 0.48 222444. 0.2164
|
|
71.72 0.6311 0.7834 0.0385 0.0310 0.969 7.636 3.970 722.740 0.863 17.660 2.492 0.49 223108. 0.1942
|
|
74.98 0.6598 0.7803 0.0331 0.0279 0.874 6.889 3.413 652.060 0.778 15.180 2.374 0.49 223795. 0.1716
|
|
78.24 0.6885 0.7695 0.0276 0.0247 0.772 6.085 2.849 575.960 0.688 12.672 2.244 0.49 224507. 0.1481
|
|
81.50 0.7172 0.7472 0.0221 0.0212 0.663 5.225 2.280 494.573 0.590 10.144 2.091 0.49 225243. 0.1235
|
|
84.76 0.7459 0.7058 0.0166 0.0175 0.547 4.312 1.709 408.092 0.487 7.602 1.900 0.49 226003. 0.0971
|
|
88.02 0.7746 0.6282 0.0110 0.0136 0.425 3.347 1.137 316.790 0.378 5.057 1.628 0.49 226787. 0.0679
|
|
91.28 0.8033 0.4652 0.0055 0.0095 0.296 2.335 0.567 221.027 0.264 2.520 1.163 0.49 227593. 0.0342
|
|
94.54 0.8319 -0.0031 0.0000 0.0052 0.162 1.276 -0.002 120.786 0.144 -0.009 -0.007 0.49 228391. 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 0.1139 0.0422 1.880 13.167 14.887 1402.009 1.488 66.219 4.816 0.54 240811. 0.7269
|
|
3.67 0.0287 0.0750 0.1127 0.0432 1.922 13.463 14.731 1433.575 1.521 65.525 4.661 0.54 241009. 0.6998
|
|
7.34 0.0574 0.1450 0.1114 0.0441 1.964 13.755 14.556 1464.615 1.554 64.744 4.508 0.54 241227. 0.6727
|
|
11.01 0.0861 0.2103 0.1099 0.0450 2.004 14.036 14.358 1494.544 1.586 63.865 4.357 0.54 241468. 0.6459
|
|
14.68 0.1148 0.2710 0.1082 0.0458 2.042 14.301 14.137 1522.749 1.616 62.882 4.211 0.54 241732. 0.6193
|
|
18.35 0.1435 0.3272 0.1063 0.0466 2.077 14.543 13.890 1548.580 1.643 61.784 4.068 0.54 242019. 0.5931
|
|
22.02 0.1722 0.3794 0.1042 0.0473 2.107 14.757 13.616 1571.346 1.667 60.564 3.930 0.54 242332. 0.5673
|
|
25.69 0.2009 0.4275 0.1019 0.0479 2.133 14.935 13.313 1590.335 1.687 59.214 3.797 0.54 242671. 0.5419
|
|
29.36 0.2296 0.4720 0.0993 0.0483 2.152 15.071 12.978 1604.816 1.703 57.726 3.668 0.54 243035. 0.5169
|
|
33.02 0.2583 0.5131 0.0965 0.0486 2.164 15.158 12.611 1614.052 1.713 56.095 3.544 0.54 243426. 0.4923
|
|
36.69 0.2870 0.5509 0.0934 0.0487 2.169 15.189 12.211 1617.296 1.716 54.314 3.425 0.54 243844. 0.4681
|
|
40.36 0.3157 0.5857 0.0901 0.0486 2.164 15.156 11.776 1613.813 1.712 52.379 3.310 0.54 244290. 0.4443
|
|
44.03 0.3444 0.6175 0.0865 0.0483 2.150 15.053 11.305 1602.898 1.701 50.287 3.199 0.54 244763. 0.4208
|
|
47.70 0.3731 0.6467 0.0826 0.0477 2.124 14.875 10.799 1583.912 1.681 48.036 3.093 0.54 245263. 0.3975
|
|
51.37 0.4018 0.6733 0.0785 0.0469 2.087 14.617 10.259 1556.398 1.651 45.633 2.990 0.54 245791. 0.3746
|
|
55.04 0.4305 0.6975 0.0741 0.0458 2.039 14.277 9.688 1520.200 1.613 43.091 2.890 0.54 246346. 0.3519
|
|
58.71 0.4592 0.7191 0.0695 0.0444 1.979 13.856 9.089 1475.380 1.565 40.426 2.794 0.54 246929. 0.3295
|
|
62.38 0.4880 0.7384 0.0648 0.0428 1.907 13.355 8.465 1422.066 1.509 37.654 2.700 0.54 247540. 0.3073
|
|
66.05 0.5167 0.7551 0.0599 0.0410 1.824 12.776 7.821 1360.382 1.443 34.790 2.608 0.54 248177. 0.2853
|
|
69.72 0.5454 0.7691 0.0548 0.0388 1.730 12.119 7.159 1290.422 1.369 31.844 2.516 0.54 248843. 0.2634
|
|
73.39 0.5741 0.7802 0.0496 0.0365 1.626 11.385 6.481 1212.262 1.286 28.828 2.425 0.54 249535. 0.2415
|
|
77.06 0.6028 0.7878 0.0443 0.0339 1.510 10.574 5.789 1125.963 1.195 25.751 2.332 0.55 250256. 0.2195
|
|
80.73 0.6315 0.7913 0.0389 0.0311 1.383 9.688 5.085 1031.592 1.095 22.620 2.236 0.55 251003. 0.1972
|
|
84.40 0.6602 0.7894 0.0335 0.0280 1.246 8.727 4.371 929.237 0.986 19.443 2.134 0.55 251778. 0.1745
|
|
88.07 0.6889 0.7802 0.0279 0.0247 1.098 7.692 3.649 819.026 0.869 16.230 2.021 0.55 252580. 0.1510
|
|
91.74 0.7176 0.7598 0.0223 0.0211 0.940 6.585 2.920 701.155 0.744 12.990 1.889 0.55 253409. 0.1263
|
|
95.41 0.7463 0.7207 0.0167 0.0173 0.772 5.409 2.188 575.903 0.611 9.732 1.723 0.55 254265. 0.0997
|
|
99.07 0.7750 0.6458 0.0111 0.0134 0.595 4.167 1.455 443.667 0.471 6.470 1.487 0.55 255148. 0.0702
|
|
102.74 0.8037 0.4844 0.0055 0.0092 0.409 2.864 0.723 304.971 0.324 3.216 1.075 0.55 256056. 0.0358
|
|
106.41 0.8324 -0.0088 -0.0001 0.0048 0.214 1.500 -0.007 159.686 0.169 -0.029 -0.019 0.55 256949. 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 0.1148 0.0425 2.596 16.362 18.524 1935.827 1.849 82.395 4.340 0.59 267547. 0.7307
|
|
4.08 0.0287 0.0751 0.1137 0.0435 2.656 16.739 18.338 1980.410 1.891 81.568 4.200 0.60 267766. 0.7035
|
|
8.16 0.0574 0.1453 0.1124 0.0444 2.715 17.110 18.127 2024.304 1.933 80.631 4.062 0.60 268009. 0.6765
|
|
12.24 0.0861 0.2106 0.1109 0.0454 2.771 17.468 17.890 2066.677 1.974 79.573 3.926 0.60 268276. 0.6496
|
|
16.31 0.1149 0.2714 0.1092 0.0462 2.825 17.806 17.622 2106.657 2.012 78.382 3.794 0.60 268570. 0.6230
|
|
20.39 0.1436 0.3277 0.1074 0.0470 2.874 18.116 17.322 2143.310 2.047 77.047 3.666 0.60 268890. 0.5968
|
|
24.47 0.1723 0.3799 0.1053 0.0477 2.918 18.389 16.987 2175.663 2.078 75.557 3.541 0.60 269239. 0.5709
|
|
28.55 0.2010 0.4282 0.1030 0.0483 2.954 18.618 16.615 2202.698 2.103 73.902 3.421 0.60 269616. 0.5455
|
|
32.63 0.2297 0.4728 0.1004 0.0488 2.982 18.793 16.203 2223.391 2.123 72.073 3.305 0.60 270022. 0.5205
|
|
36.71 0.2584 0.5140 0.0976 0.0491 2.999 18.905 15.751 2236.697 2.136 70.061 3.194 0.60 270458. 0.4959
|
|
40.79 0.2871 0.5520 0.0946 0.0492 3.006 18.946 15.256 2241.580 2.141 67.859 3.087 0.60 270924. 0.4717
|
|
44.87 0.3159 0.5869 0.0912 0.0491 3.000 18.908 14.717 2237.011 2.136 65.462 2.984 0.60 271420. 0.4478
|
|
48.94 0.3446 0.6190 0.0876 0.0488 2.980 18.781 14.133 2222.007 2.122 62.865 2.885 0.60 271947. 0.4243
|
|
53.02 0.3733 0.6485 0.0837 0.0482 2.944 18.558 13.505 2195.685 2.097 60.069 2.790 0.60 272505. 0.4010
|
|
57.10 0.4020 0.6754 0.0795 0.0473 2.893 18.235 12.832 2157.401 2.060 57.078 2.698 0.60 273093. 0.3780
|
|
61.18 0.4307 0.6998 0.0751 0.0462 2.825 17.808 12.120 2106.932 2.012 53.910 2.609 0.60 273712. 0.3553
|
|
65.26 0.4594 0.7219 0.0705 0.0449 2.742 17.279 11.373 2044.367 1.952 50.586 2.523 0.60 274361. 0.3329
|
|
69.34 0.4881 0.7416 0.0657 0.0432 2.642 16.650 10.595 1969.892 1.881 47.127 2.440 0.60 275041. 0.3106
|
|
73.42 0.5169 0.7588 0.0607 0.0413 2.526 15.921 9.791 1883.694 1.799 43.549 2.357 0.60 275751. 0.2886
|
|
77.50 0.5456 0.7734 0.0556 0.0392 2.395 15.095 8.963 1785.918 1.705 39.868 2.276 0.60 276492. 0.2666
|
|
81.57 0.5743 0.7851 0.0503 0.0368 2.248 14.172 8.115 1676.669 1.601 36.097 2.195 0.60 277263. 0.2446
|
|
85.65 0.6030 0.7935 0.0449 0.0341 2.087 13.152 7.250 1556.042 1.486 32.248 2.113 0.61 278065. 0.2226
|
|
89.73 0.6317 0.7980 0.0395 0.0313 1.910 12.037 6.369 1424.132 1.360 28.330 2.029 0.61 278897. 0.2003
|
|
93.81 0.6604 0.7973 0.0339 0.0281 1.718 10.828 5.475 1281.061 1.223 24.354 1.939 0.61 279759. 0.1774
|
|
97.89 0.6891 0.7894 0.0283 0.0247 1.511 9.526 4.571 1127.010 1.076 20.331 1.840 0.61 280651. 0.1538
|
|
101.97 0.7179 0.7709 0.0227 0.0211 1.290 8.133 3.658 962.248 0.919 16.273 1.724 0.61 281574. 0.1290
|
|
106.05 0.7466 0.7342 0.0170 0.0173 1.056 6.653 2.741 787.168 0.752 12.191 1.579 0.61 282526. 0.1023
|
|
110.13 0.7753 0.6622 0.0113 0.0132 0.808 5.091 1.821 602.324 0.575 8.102 1.372 0.61 283508. 0.0724
|
|
114.20 0.8040 0.5029 0.0056 0.0090 0.548 3.452 0.904 408.454 0.390 4.023 1.004 0.61 284518. 0.0374
|
|
118.28 0.8327 -0.0127 -0.0001 0.0045 0.275 1.735 -0.011 205.237 0.196 -0.049 -0.024 0.62 285504. 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 0.1158 0.0429 3.490 19.998 22.610 2602.606 2.259 100.568 3.940 0.65 294275. 0.7329
|
|
4.52 0.0289 0.0755 0.1147 0.0439 3.572 20.468 22.394 2663.804 2.312 99.607 3.813 0.65 294517. 0.7058
|
|
9.03 0.0578 0.1460 0.1134 0.0449 3.653 20.933 22.147 2724.246 2.365 98.509 3.687 0.65 294786. 0.6788
|
|
13.55 0.0867 0.2117 0.1120 0.0459 3.732 21.382 21.866 2782.757 2.416 97.261 3.564 0.65 295082. 0.6519
|
|
18.06 0.1156 0.2727 0.1104 0.0468 3.806 21.807 21.548 2838.080 2.464 95.845 3.444 0.65 295408. 0.6253
|
|
22.58 0.1445 0.3293 0.1085 0.0476 3.874 22.198 21.189 2888.891 2.508 94.248 3.327 0.66 295764. 0.5990
|
|
27.09 0.1734 0.3817 0.1065 0.0484 3.934 22.543 20.786 2933.768 2.547 92.455 3.214 0.66 296152. 0.5731
|
|
31.61 0.2023 0.4302 0.1042 0.0490 3.985 22.831 20.336 2971.257 2.579 90.452 3.104 0.66 296571. 0.5476
|
|
36.12 0.2312 0.4750 0.1016 0.0495 4.023 23.051 19.836 2999.878 2.604 88.229 2.999 0.66 297024. 0.5225
|
|
40.64 0.2601 0.5163 0.0988 0.0498 4.047 23.191 19.284 3018.178 2.620 85.774 2.898 0.66 297510. 0.4978
|
|
45.16 0.2890 0.5544 0.0957 0.0499 4.056 23.241 18.678 3024.702 2.626 83.078 2.801 0.66 298029. 0.4735
|
|
49.67 0.3179 0.5896 0.0923 0.0498 4.047 23.190 18.016 3018.040 2.620 80.134 2.708 0.66 298583. 0.4495
|
|
54.19 0.3468 0.6219 0.0886 0.0494 4.019 23.027 17.297 2996.849 2.602 76.938 2.618 0.66 299170. 0.4259
|
|
58.70 0.3757 0.6515 0.0846 0.0488 3.969 22.744 16.522 2959.928 2.570 73.490 2.532 0.66 299792. 0.4026
|
|
63.22 0.4046 0.6787 0.0804 0.0479 3.898 22.333 15.692 2906.424 2.523 69.797 2.449 0.66 300448. 0.3795
|
|
67.73 0.4335 0.7034 0.0759 0.0468 3.803 21.792 14.812 2836.065 2.462 65.882 2.369 0.66 301138. 0.3566
|
|
72.25 0.4624 0.7258 0.0711 0.0453 3.686 21.123 13.887 2749.004 2.386 61.771 2.291 0.66 301862. 0.3340
|
|
76.76 0.4913 0.7457 0.0662 0.0436 3.548 20.328 12.925 2645.526 2.297 57.490 2.216 0.66 302620. 0.3116
|
|
81.28 0.5202 0.7633 0.0611 0.0416 3.387 19.409 11.929 2525.898 2.193 53.061 2.142 0.66 303411. 0.2894
|
|
85.80 0.5491 0.7783 0.0559 0.0394 3.205 18.367 10.904 2390.332 2.075 48.503 2.069 0.66 304237. 0.2673
|
|
90.31 0.5780 0.7904 0.0505 0.0369 3.003 17.204 9.854 2238.993 1.944 43.832 1.996 0.67 305096. 0.2451
|
|
94.83 0.6069 0.7992 0.0450 0.0342 2.779 15.921 8.782 2072.010 1.799 39.063 1.922 0.67 305989. 0.2229
|
|
99.34 0.6358 0.8040 0.0394 0.0312 2.534 14.519 7.691 1889.520 1.640 34.209 1.846 0.67 306916. 0.2003
|
|
103.86 0.6647 0.8036 0.0337 0.0279 2.269 12.999 6.583 1691.705 1.469 29.282 1.765 0.67 307876. 0.1771
|
|
108.37 0.6936 0.7959 0.0280 0.0244 1.983 11.363 5.462 1478.826 1.284 24.295 1.675 0.67 308870. 0.1532
|
|
112.89 0.7225 0.7770 0.0222 0.0206 1.678 9.615 4.331 1251.277 1.086 19.264 1.570 0.67 309897. 0.1278
|
|
117.40 0.7514 0.7385 0.0164 0.0166 1.354 7.758 3.194 1009.636 0.876 14.206 1.435 0.67 310957. 0.1003
|
|
121.92 0.7803 0.6600 0.0105 0.0124 1.012 5.799 2.055 754.743 0.655 9.139 1.235 0.67 312050. 0.0692
|
|
126.44 0.8092 0.4737 0.0047 0.0080 0.654 3.748 0.919 487.724 0.423 4.088 0.855 0.68 313173. 0.0320
|
|
130.95 0.8381
|
|
|
|
|
|
|
|
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 0.1169 0.0439 4.635 24.343 27.162 3456.008 2.750 120.815 3.565 0.71 320994. 0.7267
|
|
4.89 0.0287 0.0741 0.1159 0.0449 4.739 24.890 26.922 3533.779 2.812 119.750 3.456 0.71 321256. 0.7014
|
|
9.79 0.0574 0.1436 0.1147 0.0459 4.842 25.432 26.647 3610.620 2.873 118.525 3.347 0.71 321546. 0.6759
|
|
14.68 0.0861 0.2086 0.1133 0.0468 4.942 25.956 26.331 3685.066 2.932 117.120 3.241 0.71 321867. 0.6505
|
|
19.57 0.1148 0.2692 0.1118 0.0477 5.036 26.452 25.970 3755.564 2.989 115.514 3.136 0.71 322219. 0.6252
|
|
24.47 0.1435 0.3255 0.1100 0.0485 5.123 26.909 25.560 3820.453 3.040 113.689 3.034 0.71 322604. 0.6001
|
|
29.36 0.1723 0.3778 0.1080 0.0492 5.200 27.315 25.096 3877.970 3.086 111.627 2.935 0.72 323023. 0.5752
|
|
34.26 0.2010 0.4263 0.1058 0.0499 5.265 27.655 24.575 3926.278 3.124 109.309 2.839 0.72 323478. 0.5505
|
|
39.15 0.2297 0.4712 0.1033 0.0503 5.315 27.917 23.993 3963.511 3.154 106.722 2.746 0.72 323967. 0.5261
|
|
44.04 0.2584 0.5128 0.1005 0.0506 5.348 28.088 23.348 3987.756 3.173 103.852 2.656 0.72 324493. 0.5020
|
|
48.94 0.2871 0.5511 0.0974 0.0508 5.360 28.154 22.637 3997.082 3.181 100.689 2.569 0.72 325056. 0.4781
|
|
53.83 0.3158 0.5864 0.0941 0.0507 5.350 28.101 21.858 3989.563 3.175 97.223 2.485 0.72 325655. 0.4545
|
|
58.72 0.3445 0.6190 0.0904 0.0503 5.315 27.916 21.009 3963.338 3.154 93.450 2.404 0.72 326291. 0.4311
|
|
63.62 0.3732 0.6489 0.0865 0.0497 5.252 27.588 20.092 3916.717 3.117 89.368 2.327 0.72 326964. 0.4080
|
|
68.51 0.4019 0.6764 0.0822 0.0489 5.161 27.106 19.107 3848.405 3.062 84.987 2.252 0.72 327674. 0.3850
|
|
73.40 0.4306 0.7015 0.0777 0.0477 5.039 26.469 18.060 3757.890 2.990 80.331 2.180 0.72 328420. 0.3624
|
|
78.30 0.4593 0.7243 0.0730 0.0463 4.888 25.676 16.958 3645.310 2.901 75.431 2.110 0.72 329203. 0.3399
|
|
83.19 0.4881 0.7448 0.0681 0.0446 4.708 24.730 15.809 3511.054 2.794 70.320 2.042 0.72 330023. 0.3177
|
|
88.09 0.5168 0.7631 0.0629 0.0426 4.500 23.635 14.619 3355.512 2.670 65.025 1.976 0.72 330878. 0.2955
|
|
92.98 0.5455 0.7789 0.0576 0.0404 4.263 22.391 13.392 3178.999 2.530 59.569 1.911 0.72 331770. 0.2735
|
|
97.87 0.5742 0.7920 0.0522 0.0379 3.999 21.002 12.134 2981.759 2.373 53.972 1.846 0.73 332698. 0.2515
|
|
102.77 0.6029 0.8020 0.0467 0.0351 3.707 19.468 10.848 2763.979 2.200 48.252 1.780 0.73 333663. 0.2294
|
|
107.66 0.6316 0.8084 0.0411 0.0321 3.387 17.791 9.538 2525.861 2.010 42.424 1.713 0.73 334663. 0.2069
|
|
112.55 0.6603 0.8100 0.0353 0.0288 3.041 15.972 8.207 2267.677 1.805 36.504 1.641 0.73 335700. 0.1840
|
|
117.45 0.6890 0.8050 0.0295 0.0253 2.668 14.016 6.859 1989.843 1.583 30.507 1.563 0.73 336772. 0.1602
|
|
122.34 0.7177 0.7899 0.0237 0.0215 2.270 11.925 5.497 1692.987 1.347 24.451 1.473 0.73 337880. 0.1351
|
|
127.23 0.7464 0.7575 0.0178 0.0175 1.848 9.706 4.126 1378.049 1.097 18.353 1.358 0.73 339024. 0.1079
|
|
132.13 0.7752 0.6908 0.0118 0.0133 1.403 7.370 2.751 1046.381 0.833 12.238 1.193 0.74 340203. 0.0774
|
|
137.02 0.8039 0.5366 0.0059 0.0089 0.938 4.929 1.378 699.796 0.557 6.130 0.893 0.74 341415. 0.0410
|
|
141.92 0.8326 0.0048 0.0000 0.0043 0.454 2.384 0.006 338.436 0.269 0.025 0.008 0.74 342598. 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 0.1181 0.0463 6.220 30.155 32.188 4638.031 3.407 143.172 3.148 0.77 347704. 0.6986
|
|
5.30 0.0287 0.0712 0.1171 0.0473 6.344 30.760 31.931 4730.989 3.475 142.030 3.061 0.77 347985. 0.6767
|
|
10.61 0.0574 0.1383 0.1160 0.0482 6.466 31.351 31.632 4821.874 3.542 140.701 2.975 0.77 348299. 0.6546
|
|
15.91 0.0861 0.2016 0.1147 0.0490 6.583 31.915 31.286 4908.774 3.606 139.158 2.891 0.77 348645. 0.6325
|
|
21.21 0.1149 0.2610 0.1133 0.0498 6.691 32.442 30.885 4989.779 3.665 137.377 2.807 0.77 349026. 0.6103
|
|
26.51 0.1436 0.3168 0.1116 0.0506 6.789 32.917 30.425 5062.846 3.719 135.330 2.726 0.77 349444. 0.5881
|
|
31.82 0.1723 0.3690 0.1097 0.0512 6.874 33.327 29.900 5125.898 3.765 132.994 2.646 0.77 349898. 0.5659
|
|
37.12 0.2010 0.4178 0.1075 0.0517 6.942 33.658 29.304 5176.808 3.803 130.345 2.568 0.78 350392. 0.5437
|
|
42.42 0.2297 0.4633 0.1050 0.0521 6.991 33.896 28.634 5213.433 3.830 127.365 2.491 0.78 350924. 0.5215
|
|
47.72 0.2584 0.5056 0.1023 0.0523 7.018 34.027 27.886 5233.609 3.844 124.036 2.417 0.78 351496. 0.4992
|
|
53.03 0.2872 0.5449 0.0992 0.0523 7.020 34.037 27.056 5235.132 3.846 120.345 2.344 0.78 352108. 0.4770
|
|
58.33 0.3159 0.5813 0.0959 0.0521 6.995 33.912 26.142 5215.808 3.831 116.281 2.273 0.78 352760. 0.4547
|
|
63.63 0.3446 0.6149 0.0922 0.0517 6.938 33.636 25.143 5173.410 3.800 111.837 2.204 0.78 353452. 0.4324
|
|
68.93 0.3733 0.6459 0.0882 0.0510 6.847 33.197 24.059 5105.870 3.751 107.014 2.137 0.78 354184. 0.4101
|
|
74.24 0.4020 0.6743 0.0840 0.0501 6.721 32.583 22.891 5011.507 3.681 101.821 2.072 0.78 354956. 0.3878
|
|
79.54 0.4307 0.7002 0.0794 0.0488 6.557 31.790 21.648 4889.533 3.592 96.288 2.008 0.78 355768. 0.3655
|
|
84.84 0.4594 0.7238 0.0746 0.0473 6.356 30.818 20.336 4739.918 3.482 90.455 1.946 0.78 356619. 0.3433
|
|
90.14 0.4882 0.7450 0.0696 0.0456 6.119 29.667 18.966 4562.885 3.352 84.359 1.885 0.78 357509. 0.3212
|
|
95.45 0.5169 0.7639 0.0643 0.0435 5.845 28.339 17.544 4358.654 3.202 78.035 1.826 0.78 358439. 0.2991
|
|
100.75 0.5456 0.7803 0.0590 0.0412 5.535 26.836 16.077 4127.526 3.032 71.512 1.767 0.79 359408. 0.2771
|
|
106.05 0.5743 0.7941 0.0534 0.0387 5.189 25.160 14.572 3869.705 2.843 64.814 1.708 0.79 360416. 0.2550
|
|
111.35 0.6030 0.8047 0.0478 0.0358 4.808 23.312 13.031 3585.473 2.634 57.963 1.648 0.79 361464. 0.2328
|
|
116.66 0.6317 0.8117 0.0420 0.0327 4.392 21.295 11.461 3275.357 2.406 50.978 1.587 0.79 362550. 0.2102
|
|
121.96 0.6604 0.8136 0.0362 0.0294 3.943 19.116 9.864 2940.096 2.160 43.876 1.522 0.79 363675. 0.1870
|
|
127.26 0.6892 0.8085 0.0302 0.0258 3.461 16.779 8.246 2580.711 1.896 36.676 1.449 0.79 364838. 0.1628
|
|
132.56 0.7179 0.7924 0.0242 0.0220 2.948 14.295 6.609 2198.651 1.615 29.397 1.363 0.79 366040. 0.1371
|
|
137.87 0.7466 0.7571 0.0182 0.0179 2.408 11.676 4.960 1795.883 1.319 22.062 1.253 0.80 367281. 0.1091
|
|
143.17 0.7753 0.6840 0.0121 0.0137 1.844 8.940 3.304 1374.998 1.010 14.695 1.090 0.80 368559. 0.0775
|
|
148.47 0.8040 0.5179 0.0060 0.0094 1.260 6.107 1.648 939.287 0.690 7.329 0.796 0.80 369873. 0.0400
|
|
153.77 0.8327 -0.0064 0.0000 0.0049 0.657 3.184 -0.010 489.735 0.360 -0.045 -0.009 0.80 371151. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 14000
|
|
|
|
V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
|
|
(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
|
|
0.00 0.0000 0.0000 0.1191 0.0514 8.622 38.816 37.674 6429.322 4.385 167.574 2.658 0.83 374403. 0.6381
|
|
5.71 0.0287 0.0650 0.1183 0.0523 8.765 39.461 37.412 6536.162 4.458 166.406 2.596 0.83 374704. 0.6212
|
|
11.43 0.0575 0.1270 0.1173 0.0531 8.901 40.074 37.102 6637.765 4.528 165.028 2.535 0.83 375038. 0.6041
|
|
17.14 0.0862 0.1860 0.1162 0.0538 9.027 40.639 36.737 6731.310 4.591 163.405 2.475 0.83 375410. 0.5869
|
|
22.85 0.1149 0.2421 0.1148 0.0545 9.138 41.139 36.309 6814.073 4.648 161.501 2.417 0.83 375819. 0.5697
|
|
28.57 0.1436 0.2955 0.1132 0.0551 9.231 41.557 35.810 6883.428 4.695 159.283 2.360 0.83 376268. 0.5524
|
|
34.28 0.1724 0.3462 0.1114 0.0555 9.303 41.880 35.233 6936.928 4.732 156.716 2.304 0.83 376758. 0.5349
|
|
39.99 0.2011 0.3943 0.1093 0.0558 9.350 42.094 34.571 6972.287 4.756 153.771 2.249 0.83 377290. 0.5173
|
|
45.71 0.2298 0.4399 0.1069 0.0559 9.370 42.184 33.818 6987.286 4.766 150.421 2.195 0.84 377865. 0.4994
|
|
51.42 0.2586 0.4829 0.1043 0.0558 9.360 42.140 32.968 6979.882 4.761 146.643 2.142 0.84 378484. 0.4812
|
|
57.13 0.2873 0.5235 0.1013 0.0556 9.318 41.948 32.019 6948.061 4.739 142.420 2.090 0.84 379146. 0.4627
|
|
62.85 0.3160 0.5616 0.0979 0.0551 9.239 41.596 30.966 6889.823 4.699 137.737 2.039 0.84 379852. 0.4438
|
|
68.56 0.3448 0.5973 0.0943 0.0544 9.123 41.073 29.808 6803.182 4.640 132.587 1.987 0.84 380601. 0.4244
|
|
74.27 0.3735 0.6305 0.0903 0.0535 8.966 40.367 28.545 6686.193 4.561 126.970 1.936 0.84 381394. 0.4047
|
|
79.99 0.4022 0.6613 0.0860 0.0523 8.767 39.468 27.180 6537.267 4.459 120.897 1.886 0.84 382230. 0.3846
|
|
85.70 0.4309 0.6896 0.0813 0.0508 8.523 38.372 25.720 6355.760 4.335 114.403 1.835 0.84 383108. 0.3641
|
|
91.41 0.4597 0.7155 0.0765 0.0491 8.236 37.080 24.177 6141.885 4.189 107.537 1.785 0.84 384029. 0.3434
|
|
97.13 0.4884 0.7390 0.0713 0.0472 7.907 35.597 22.560 5896.133 4.022 100.347 1.735 0.84 384993. 0.3224
|
|
102.84 0.5171 0.7599 0.0660 0.0449 7.535 33.922 20.880 5618.803 3.833 92.875 1.686 0.84 385999. 0.3013
|
|
108.55 0.5459 0.7782 0.0605 0.0425 7.121 32.060 19.145 5310.333 3.622 85.155 1.635 0.85 387047. 0.2799
|
|
114.26 0.5746 0.7932 0.0549 0.0398 6.669 30.022 17.360 4972.809 3.392 77.216 1.583 0.85 388136. 0.2581
|
|
119.98 0.6033 0.8042 0.0491 0.0368 6.179 27.817 15.531 4607.462 3.143 69.084 1.529 0.85 389268. 0.2357
|
|
125.69 0.6320 0.8101 0.0432 0.0337 5.653 25.451 13.664 4215.656 2.875 60.780 1.470 0.85 390441. 0.2126
|
|
131.40 0.6608 0.8098 0.0372 0.0304 5.090 22.917 11.765 3795.914 2.589 52.329 1.406 0.85 391656. 0.1886
|
|
137.12 0.6895 0.8005 0.0311 0.0268 4.493 20.227 9.837 3350.398 2.285 43.753 1.332 0.85 392912. 0.1634
|
|
142.83 0.7182 0.7770 0.0249 0.0231 3.865 17.401 7.886 2882.256 1.966 35.076 1.241 0.85 394210. 0.1363
|
|
148.54 0.7470 0.7298 0.0187 0.0192 3.212 14.461 5.918 2395.346 1.634 26.324 1.121 0.86 395548. 0.1066
|
|
154.26 0.7757 0.6381 0.0125 0.0151 2.540 11.436 3.941 1894.281 1.292 17.529 0.944 0.86 396927. 0.0733
|
|
159.97 0.8044 0.4510 0.0062 0.0111 1.857 8.359 1.963 1384.474 0.944 8.731 0.643 0.86 398344. 0.0352
|
|
165.68 0.8332 -0.0054 0.0000 0.0069 1.165 5.243 -0.014 868.414 0.592 -0.063 -0.007 0.86 399742. 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 0.1192 0.0584 12.051 50.636 43.280 8986.213 5.721 192.508 2.184 0.89 401136. 0.5622
|
|
6.14 0.0288 0.0576 0.1186 0.0593 12.237 51.420 43.034 9125.325 5.809 191.414 2.139 0.89 401452. 0.5489
|
|
12.28 0.0576 0.1127 0.1177 0.0602 12.415 52.166 42.740 9257.698 5.894 190.109 2.094 0.89 401806. 0.5355
|
|
18.42 0.0864 0.1655 0.1168 0.0610 12.576 52.845 42.390 9378.276 5.970 188.549 2.050 0.89 402198. 0.5221
|
|
24.55 0.1152 0.2161 0.1156 0.0617 12.715 53.428 41.970 9481.674 6.036 186.684 2.008 0.89 402631. 0.5088
|
|
30.69 0.1441 0.2647 0.1142 0.0622 12.823 53.882 41.471 9562.401 6.088 184.464 1.967 0.89 403108. 0.4955
|
|
36.83 0.1729 0.3114 0.1126 0.0625 12.894 54.181 40.881 9615.346 6.121 181.838 1.928 0.89 403630. 0.4823
|
|
42.97 0.2017 0.3564 0.1107 0.0627 12.922 54.298 40.188 9636.126 6.135 178.758 1.892 0.89 404199. 0.4691
|
|
49.11 0.2305 0.3997 0.1085 0.0626 12.903 54.216 39.385 9621.526 6.125 175.184 1.857 0.89 404815. 0.4558
|
|
55.25 0.2593 0.4415 0.1060 0.0622 12.833 53.922 38.462 9569.390 6.092 171.080 1.823 0.90 405479. 0.4423
|
|
61.39 0.2881 0.4818 0.1031 0.0616 12.711 53.409 37.415 9478.437 6.034 166.422 1.790 0.90 406192. 0.4284
|
|
67.52 0.3169 0.5205 0.0998 0.0608 12.536 52.674 36.239 9347.894 5.951 161.191 1.758 0.90 406953. 0.4141
|
|
73.66 0.3457 0.5575 0.0962 0.0597 12.307 51.712 34.931 9177.221 5.842 155.375 1.726 0.90 407762. 0.3991
|
|
79.80 0.3745 0.5928 0.0923 0.0583 12.023 50.521 33.493 8965.913 5.708 148.975 1.694 0.90 408618. 0.3836
|
|
85.94 0.4033 0.6261 0.0879 0.0567 11.685 49.099 31.925 8713.460 5.547 142.002 1.662 0.90 409521. 0.3673
|
|
92.08 0.4322 0.6575 0.0833 0.0548 11.292 47.449 30.238 8420.629 5.361 134.499 1.629 0.90 410471. 0.3503
|
|
98.22 0.4610 0.6868 0.0784 0.0526 10.848 45.581 28.445 8089.113 5.150 126.524 1.595 0.90 411467. 0.3328
|
|
104.36 0.4898 0.7138 0.0732 0.0502 10.354 43.505 26.560 7720.814 4.915 118.139 1.560 0.90 412509. 0.3146
|
|
110.49 0.5186 0.7385 0.0678 0.0476 9.812 41.231 24.595 7317.175 4.658 109.399 1.525 0.90 413596. 0.2958
|
|
116.63 0.5474 0.7606 0.0622 0.0447 9.225 38.762 22.560 6878.974 4.379 100.349 1.488 0.91 414729. 0.2764
|
|
122.77 0.5762 0.7793 0.0564 0.0417 8.597 36.122 20.464 6410.486 4.081 91.026 1.448 0.91 415906. 0.2562
|
|
128.91 0.6050 0.7928 0.0504 0.0385 7.940 33.364 18.313 5921.064 3.769 81.457 1.403 0.91 417128. 0.2348
|
|
135.05 0.6338 0.7972 0.0444 0.0353 7.277 30.578 16.110 5426.565 3.455 71.657 1.347 0.91 418394. 0.2114
|
|
141.19 0.6626 0.7897 0.0382 0.0320 6.608 27.767 13.861 4927.781 3.137 61.652 1.276 0.91 419705. 0.1858
|
|
147.33 0.6915 0.7693 0.0319 0.0287 5.911 24.839 11.576 4408.098 2.806 51.492 1.191 0.91 421060. 0.1585
|
|
153.47 0.7203 0.7301 0.0255 0.0252 5.193 21.822 9.265 3872.762 2.465 41.212 1.085 0.92 422460. 0.1292
|
|
159.60 0.7491 0.6614 0.0191 0.0216 4.463 18.754 6.937 3328.208 2.119 30.854 0.945 0.92 423902. 0.0974
|
|
165.74 0.7779 0.5454 0.0127 0.0181 3.730 15.672 4.602 2781.216 1.771 20.472 0.751 0.92 425389. 0.0630
|
|
171.88 0.8067 0.3479 0.0063 0.0146 3.002 12.613 2.278 2238.473 1.425 10.134 0.462 0.92 426916. 0.0273
|
|
178.02 0.8355 -0.0053 -0.0001 0.0111 2.281 9.585 -0.026 1701.107 1.083 -0.114 -0.007 0.92 428447. 0.0000
|
|
|
|
|
|
|