538 lines
95 KiB
Plaintext
538 lines
95 KiB
Plaintext
17x8E (17x8E.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 0.0808 0.0307 0.003 0.218 0.213 2.579 0.025 0.946 37.402 0.07 26796. 0.5971
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0.34 0.0211 0.0543 0.0794 0.0309 0.003 0.220 0.209 2.597 0.025 0.929 36.488 0.07 26811. 0.5773
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0.68 0.0423 0.1058 0.0779 0.0311 0.004 0.221 0.205 2.613 0.025 0.912 35.573 0.07 26827. 0.5575
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1.02 0.0634 0.1547 0.0763 0.0313 0.004 0.222 0.201 2.626 0.025 0.893 34.659 0.07 26844. 0.5375
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1.36 0.0846 0.2008 0.0746 0.0314 0.004 0.223 0.196 2.636 0.025 0.873 33.747 0.07 26863. 0.5174
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1.70 0.1057 0.2442 0.0727 0.0315 0.004 0.223 0.191 2.643 0.025 0.851 32.838 0.07 26883. 0.4972
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2.04 0.1268 0.2850 0.0708 0.0315 0.004 0.224 0.186 2.646 0.025 0.828 31.931 0.07 26904. 0.4770
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2.38 0.1480 0.3231 0.0687 0.0315 0.004 0.223 0.181 2.644 0.025 0.804 31.027 0.07 26926. 0.4567
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2.71 0.1691 0.3585 0.0666 0.0314 0.004 0.223 0.175 2.637 0.025 0.779 30.125 0.07 26950. 0.4364
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3.05 0.1902 0.3912 0.0643 0.0313 0.004 0.222 0.169 2.625 0.025 0.752 29.223 0.07 26975. 0.4160
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3.39 0.2114 0.4213 0.0619 0.0310 0.003 0.220 0.163 2.607 0.025 0.724 28.321 0.07 27002. 0.3955
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3.73 0.2325 0.4486 0.0593 0.0308 0.003 0.218 0.156 2.583 0.025 0.694 27.415 0.07 27030. 0.3749
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4.07 0.2537 0.4730 0.0567 0.0304 0.003 0.216 0.149 2.552 0.024 0.663 26.502 0.07 27060. 0.3542
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4.41 0.2748 0.4946 0.0539 0.0299 0.003 0.212 0.142 2.514 0.024 0.631 25.579 0.07 27091. 0.3334
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4.75 0.2959 0.5131 0.0510 0.0294 0.003 0.209 0.134 2.469 0.024 0.597 24.641 0.07 27124. 0.3124
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5.09 0.3171 0.5284 0.0480 0.0288 0.003 0.204 0.126 2.417 0.023 0.561 23.684 0.07 27158. 0.2913
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5.43 0.3382 0.5403 0.0449 0.0281 0.003 0.199 0.118 2.358 0.023 0.525 22.702 0.07 27194. 0.2700
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5.77 0.3593 0.5484 0.0417 0.0273 0.003 0.194 0.110 2.293 0.022 0.488 21.686 0.07 27232. 0.2485
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6.11 0.3805 0.5523 0.0384 0.0264 0.003 0.188 0.101 2.221 0.021 0.449 20.628 0.07 27271. 0.2269
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6.45 0.4016 0.5516 0.0350 0.0255 0.003 0.181 0.092 2.142 0.020 0.410 19.519 0.07 27312. 0.2051
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6.79 0.4228 0.5457 0.0316 0.0245 0.003 0.174 0.083 2.056 0.020 0.370 18.345 0.07 27354. 0.1831
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7.13 0.4439 0.5339 0.0281 0.0234 0.003 0.166 0.074 1.965 0.019 0.329 17.091 0.07 27398. 0.1610
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7.46 0.4650 0.5150 0.0246 0.0222 0.003 0.158 0.065 1.867 0.018 0.288 15.738 0.07 27444. 0.1387
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7.80 0.4862 0.4879 0.0211 0.0210 0.002 0.149 0.055 1.763 0.017 0.247 14.260 0.07 27492. 0.1162
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8.14 0.5073 0.4507 0.0175 0.0197 0.002 0.140 0.046 1.653 0.016 0.205 12.624 0.07 27541. 0.0938
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8.48 0.5285 0.4012 0.0139 0.0183 0.002 0.130 0.037 1.539 0.015 0.163 10.788 0.07 27592. 0.0714
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8.82 0.5496 0.3362 0.0103 0.0169 0.002 0.120 0.027 1.419 0.014 0.121 8.692 0.07 27644. 0.0496
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9.16 0.5707 0.2511 0.0068 0.0154 0.002 0.109 0.018 1.294 0.012 0.079 6.253 0.07 27699. 0.0289
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9.50 0.5919 0.1396 0.0033 0.0139 0.002 0.099 0.009 1.166 0.011 0.038 3.351 0.07 27755. 0.0108
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9.84 0.6130 -0.0088 -0.0002 0.0123 0.001 0.087 0.000 1.035 0.010 -0.002 -0.204 0.07 27812. 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 0.0811 0.0280 0.025 0.796 0.854 18.838 0.090 3.798 20.558 0.13 53592. 0.6576
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0.68 0.0212 0.0598 0.0797 0.0283 0.025 0.803 0.839 19.004 0.091 3.731 20.021 0.13 53622. 0.6348
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1.36 0.0424 0.1163 0.0782 0.0285 0.026 0.809 0.823 19.153 0.091 3.660 19.487 0.13 53654. 0.6119
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2.04 0.0636 0.1697 0.0766 0.0287 0.026 0.815 0.806 19.280 0.092 3.584 18.958 0.13 53689. 0.5891
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2.72 0.0848 0.2201 0.0749 0.0289 0.026 0.819 0.788 19.382 0.093 3.504 18.433 0.13 53726. 0.5663
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3.40 0.1060 0.2673 0.0730 0.0290 0.026 0.822 0.768 19.454 0.093 3.418 17.915 0.13 53765. 0.5436
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4.08 0.1272 0.3116 0.0711 0.0290 0.026 0.824 0.748 19.493 0.093 3.327 17.402 0.13 53808. 0.5210
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4.77 0.1484 0.3530 0.0690 0.0290 0.026 0.824 0.726 19.496 0.093 3.230 16.895 0.13 53853. 0.4984
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5.45 0.1696 0.3914 0.0668 0.0290 0.026 0.822 0.703 19.457 0.093 3.128 16.393 0.13 53901. 0.4759
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6.13 0.1909 0.4270 0.0645 0.0288 0.026 0.819 0.679 19.374 0.093 3.020 15.897 0.13 53951. 0.4535
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6.81 0.2121 0.4598 0.0621 0.0286 0.026 0.813 0.654 19.242 0.092 2.907 15.405 0.13 54005. 0.4311
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7.49 0.2333 0.4897 0.0596 0.0284 0.026 0.805 0.627 19.058 0.091 2.788 14.916 0.13 54062. 0.4088
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8.17 0.2545 0.5167 0.0569 0.0280 0.025 0.795 0.599 18.818 0.090 2.663 14.428 0.13 54121. 0.3864
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8.85 0.2757 0.5409 0.0541 0.0276 0.025 0.783 0.569 18.518 0.088 2.532 13.941 0.13 54184. 0.3641
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9.53 0.2969 0.5620 0.0512 0.0270 0.024 0.767 0.538 18.157 0.087 2.395 13.451 0.14 54250. 0.3417
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10.21 0.3181 0.5800 0.0481 0.0264 0.024 0.750 0.507 17.736 0.085 2.253 12.956 0.14 54319. 0.3192
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10.89 0.3393 0.5947 0.0450 0.0257 0.023 0.729 0.474 17.256 0.082 2.107 12.453 0.14 54392. 0.2967
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11.57 0.3605 0.6057 0.0418 0.0249 0.022 0.706 0.440 16.715 0.080 1.957 11.939 0.14 54467. 0.2741
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12.25 0.3817 0.6128 0.0385 0.0240 0.022 0.681 0.405 16.116 0.077 1.803 11.407 0.14 54546. 0.2514
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12.93 0.4029 0.6155 0.0352 0.0230 0.021 0.653 0.370 15.459 0.074 1.645 10.854 0.14 54628. 0.2285
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13.62 0.4241 0.6131 0.0317 0.0219 0.020 0.623 0.334 14.743 0.070 1.485 10.271 0.14 54714. 0.2054
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14.30 0.4453 0.6048 0.0282 0.0208 0.019 0.590 0.297 13.971 0.067 1.322 9.649 0.14 54802. 0.1821
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14.98 0.4665 0.5894 0.0247 0.0196 0.018 0.555 0.260 13.144 0.063 1.157 8.978 0.14 54895. 0.1585
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15.66 0.4877 0.5656 0.0212 0.0183 0.016 0.518 0.223 12.262 0.059 0.991 8.239 0.14 54990. 0.1346
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16.34 0.5089 0.5309 0.0176 0.0169 0.015 0.479 0.185 11.330 0.054 0.824 7.412 0.14 55089. 0.1104
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17.02 0.5301 0.4823 0.0140 0.0154 0.014 0.437 0.147 10.350 0.049 0.656 6.464 0.14 55192. 0.0859
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17.70 0.5513 0.4150 0.0105 0.0139 0.013 0.394 0.110 9.325 0.045 0.489 5.349 0.14 55298. 0.0614
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18.38 0.5726 0.3218 0.0069 0.0123 0.011 0.349 0.073 8.261 0.039 0.324 3.994 0.14 55407. 0.0373
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19.06 0.5938 0.1906 0.0034 0.0107 0.010 0.303 0.036 7.163 0.034 0.160 2.281 0.14 55520. 0.0150
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19.74 0.6150 -0.0008 0.0000 0.0090 0.008 0.255 0.000 6.033 0.029 -0.001 -0.009 0.14 55634. 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 0.0814 0.0269 0.082 1.720 1.928 61.056 0.194 8.577 14.325 0.20 80386. 0.6886
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1.02 0.0212 0.0625 0.0800 0.0272 0.083 1.737 1.895 61.651 0.196 8.427 13.939 0.20 80431. 0.6642
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2.05 0.0425 0.1216 0.0785 0.0274 0.083 1.752 1.859 62.185 0.198 8.267 13.557 0.20 80480. 0.6398
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3.07 0.0637 0.1773 0.0769 0.0276 0.084 1.765 1.820 62.645 0.199 8.096 13.179 0.20 80532. 0.6155
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4.09 0.0850 0.2297 0.0751 0.0278 0.085 1.776 1.779 63.019 0.201 7.914 12.806 0.20 80588. 0.5913
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5.11 0.1062 0.2789 0.0733 0.0279 0.085 1.783 1.736 63.292 0.201 7.720 12.438 0.20 80648. 0.5673
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6.14 0.1274 0.3249 0.0714 0.0280 0.085 1.788 1.689 63.452 0.202 7.514 12.076 0.20 80711. 0.5434
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7.16 0.1487 0.3679 0.0693 0.0280 0.085 1.789 1.640 63.484 0.202 7.296 11.720 0.20 80779. 0.5196
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8.18 0.1699 0.4078 0.0671 0.0280 0.085 1.786 1.589 63.375 0.202 7.066 11.369 0.20 80851. 0.4960
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9.21 0.1912 0.4448 0.0648 0.0278 0.085 1.778 1.534 63.112 0.201 6.822 11.023 0.20 80927. 0.4726
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10.23 0.2124 0.4790 0.0623 0.0276 0.084 1.766 1.476 62.682 0.200 6.566 10.682 0.20 81008. 0.4493
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11.25 0.2336 0.5102 0.0598 0.0274 0.083 1.749 1.416 62.070 0.198 6.297 10.345 0.20 81093. 0.4261
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12.27 0.2549 0.5386 0.0571 0.0270 0.082 1.726 1.352 61.263 0.195 6.014 10.010 0.20 81183. 0.4029
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13.30 0.2761 0.5641 0.0543 0.0266 0.081 1.697 1.285 60.247 0.192 5.718 9.678 0.20 81278. 0.3798
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14.32 0.2974 0.5867 0.0514 0.0260 0.079 1.663 1.216 59.021 0.188 5.409 9.346 0.20 81377. 0.3568
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15.34 0.3186 0.6061 0.0483 0.0254 0.077 1.622 1.144 57.583 0.183 5.089 9.012 0.20 81481. 0.3337
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16.36 0.3398 0.6224 0.0452 0.0247 0.075 1.576 1.070 55.935 0.178 4.759 8.675 0.20 81590. 0.3106
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17.39 0.3611 0.6352 0.0420 0.0239 0.073 1.524 0.993 54.078 0.172 4.419 8.333 0.20 81704. 0.2875
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18.41 0.3823 0.6441 0.0387 0.0229 0.070 1.465 0.915 52.013 0.166 4.071 7.981 0.20 81822. 0.2643
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19.43 0.4036 0.6488 0.0353 0.0219 0.067 1.401 0.835 49.741 0.158 3.715 7.616 0.20 81946. 0.2409
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20.46 0.4248 0.6486 0.0318 0.0208 0.063 1.332 0.754 47.264 0.150 3.352 7.233 0.20 82075. 0.2174
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21.48 0.4460 0.6427 0.0283 0.0197 0.060 1.256 0.671 44.587 0.142 2.985 6.826 0.20 82208. 0.1936
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22.50 0.4673 0.6300 0.0248 0.0184 0.056 1.175 0.587 41.712 0.133 2.612 6.386 0.20 82347. 0.1694
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23.52 0.4885 0.6086 0.0212 0.0170 0.052 1.089 0.503 38.648 0.123 2.237 5.902 0.20 82491. 0.1449
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24.55 0.5098 0.5764 0.0177 0.0156 0.047 0.997 0.418 35.402 0.113 1.859 5.356 0.20 82640. 0.1199
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25.57 0.5310 0.5296 0.0141 0.0141 0.043 0.901 0.333 31.984 0.102 1.482 4.724 0.20 82794. 0.0944
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26.59 0.5522 0.4626 0.0105 0.0125 0.038 0.800 0.249 28.410 0.090 1.106 3.968 0.20 82953. 0.0685
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27.62 0.5735 0.3662 0.0070 0.0109 0.033 0.696 0.165 24.697 0.079 0.733 3.025 0.21 83118. 0.0425
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28.64 0.5947 0.2239 0.0035 0.0092 0.028 0.588 0.082 20.864 0.066 0.365 1.784 0.21 83287. 0.0177
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29.66 0.6160 0.0024 0.0000 0.0075 0.023 0.477 0.001 16.917 0.054 0.003 0.018 0.21 83458. 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 0.0818 0.0264 0.190 2.992 3.444 141.611 0.338 15.319 11.031 0.27 107179. 0.7087
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1.37 0.0213 0.0642 0.0804 0.0266 0.192 3.023 3.384 143.069 0.342 15.052 10.728 0.27 107239. 0.6832
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2.73 0.0425 0.1249 0.0789 0.0269 0.194 3.051 3.320 144.382 0.345 14.766 10.429 0.27 107304. 0.6578
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4.10 0.0638 0.1820 0.0772 0.0271 0.195 3.075 3.251 145.519 0.347 14.461 10.134 0.27 107374. 0.6325
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5.46 0.0851 0.2357 0.0755 0.0273 0.196 3.095 3.178 146.447 0.350 14.136 9.843 0.27 107449. 0.6075
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6.83 0.1064 0.2861 0.0737 0.0274 0.197 3.109 3.100 147.134 0.351 13.791 9.558 0.27 107529. 0.5826
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8.19 0.1276 0.3333 0.0717 0.0275 0.198 3.118 3.018 147.547 0.352 13.423 9.277 0.27 107614. 0.5579
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9.56 0.1489 0.3772 0.0696 0.0275 0.198 3.120 2.930 147.652 0.352 13.034 9.001 0.27 107705. 0.5334
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10.93 0.1702 0.4182 0.0674 0.0274 0.198 3.115 2.838 147.417 0.352 12.622 8.731 0.27 107801. 0.5091
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12.29 0.1914 0.4561 0.0651 0.0273 0.197 3.102 2.740 146.809 0.350 12.187 8.465 0.27 107903. 0.4850
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13.66 0.2127 0.4911 0.0626 0.0271 0.196 3.081 2.637 145.796 0.348 11.729 8.203 0.27 108011. 0.4611
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15.02 0.2340 0.5233 0.0601 0.0269 0.194 3.050 2.529 144.344 0.345 11.247 7.945 0.27 108125. 0.4374
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16.39 0.2552 0.5525 0.0574 0.0265 0.191 3.009 2.415 142.419 0.340 10.741 7.691 0.27 108245. 0.4137
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17.75 0.2765 0.5789 0.0545 0.0261 0.188 2.958 2.296 139.989 0.334 10.211 7.438 0.27 108372. 0.3901
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19.12 0.2978 0.6024 0.0516 0.0255 0.184 2.896 2.172 137.046 0.327 9.659 7.187 0.27 108505. 0.3666
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20.49 0.3191 0.6229 0.0485 0.0249 0.179 2.823 2.043 133.589 0.319 9.087 6.936 0.27 108644. 0.3432
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21.85 0.3403 0.6403 0.0454 0.0241 0.174 2.739 1.910 129.621 0.309 8.496 6.684 0.27 108789. 0.3198
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23.22 0.3616 0.6542 0.0421 0.0233 0.168 2.644 1.773 125.141 0.299 7.888 6.428 0.27 108942. 0.2963
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24.58 0.3829 0.6645 0.0388 0.0224 0.161 2.539 1.633 120.153 0.287 7.265 6.166 0.27 109100. 0.2728
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25.95 0.4041 0.6706 0.0354 0.0213 0.154 2.423 1.490 114.659 0.274 6.629 5.895 0.27 109266. 0.2491
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27.31 0.4254 0.6720 0.0319 0.0202 0.146 2.296 1.345 108.665 0.259 5.981 5.612 0.27 109438. 0.2253
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28.68 0.4467 0.6679 0.0284 0.0190 0.137 2.159 1.197 102.178 0.244 5.323 5.312 0.27 109616. 0.2012
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30.05 0.4680 0.6570 0.0249 0.0177 0.128 2.012 1.047 95.209 0.227 4.657 4.988 0.27 109802. 0.1767
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31.41 0.4892 0.6377 0.0213 0.0163 0.118 1.855 0.896 87.774 0.210 3.986 4.631 0.27 109994. 0.1517
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32.78 0.5105 0.6074 0.0177 0.0149 0.107 1.688 0.745 79.895 0.191 3.312 4.227 0.27 110193. 0.1263
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34.14 0.5318 0.5622 0.0141 0.0133 0.096 1.513 0.593 71.597 0.171 2.637 3.756 0.27 110399. 0.1001
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35.51 0.5530 0.4958 0.0105 0.0117 0.084 1.329 0.442 62.916 0.150 1.965 3.185 0.27 110612. 0.0733
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36.87 0.5743 0.3974 0.0069 0.0100 0.072 1.139 0.292 53.894 0.129 1.299 2.458 0.27 110832. 0.0460
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38.24 0.5956 0.2466 0.0034 0.0083 0.060 0.942 0.145 44.582 0.106 0.643 1.471 0.27 111059. 0.0194
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39.61 0.6168 -0.0016 0.0000 0.0065 0.047 0.739 -0.001 34.982 0.084 -0.003 -0.009 0.27 111286. 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 0.0823 0.0260 0.367 4.622 5.412 273.395 0.522 24.074 8.979 0.34 133969. 0.7231
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1.71 0.0213 0.0654 0.0809 0.0263 0.371 4.671 5.318 276.312 0.528 23.656 8.730 0.34 134045. 0.6969
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3.42 0.0426 0.1271 0.0793 0.0266 0.374 4.715 5.218 278.943 0.533 23.208 8.484 0.34 134126. 0.6708
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5.12 0.0639 0.1852 0.0777 0.0268 0.377 4.754 5.110 281.224 0.537 22.730 8.242 0.34 134214. 0.6449
|
|
6.83 0.0851 0.2398 0.0760 0.0270 0.380 4.786 4.996 283.092 0.541 22.220 8.004 0.34 134308. 0.6193
|
|
8.54 0.1064 0.2910 0.0741 0.0271 0.381 4.809 4.874 284.483 0.543 21.678 7.770 0.34 134408. 0.5938
|
|
10.25 0.1277 0.3389 0.0721 0.0272 0.383 4.823 4.744 285.329 0.545 21.101 7.541 0.34 134515. 0.5686
|
|
11.96 0.1490 0.3836 0.0700 0.0272 0.383 4.827 4.606 285.566 0.545 20.489 7.317 0.34 134628. 0.5436
|
|
13.67 0.1703 0.4252 0.0678 0.0272 0.382 4.820 4.461 285.126 0.545 19.842 7.096 0.34 134749. 0.5188
|
|
15.37 0.1916 0.4638 0.0655 0.0271 0.381 4.800 4.307 283.944 0.542 19.159 6.881 0.34 134877. 0.4943
|
|
17.08 0.2128 0.4994 0.0630 0.0269 0.378 4.766 4.146 281.958 0.539 18.439 6.669 0.34 135013. 0.4700
|
|
18.79 0.2341 0.5322 0.0604 0.0266 0.374 4.718 3.975 279.101 0.533 17.682 6.460 0.34 135156. 0.4459
|
|
20.50 0.2554 0.5621 0.0577 0.0262 0.369 4.654 3.797 275.301 0.526 16.887 6.255 0.34 135306. 0.4219
|
|
22.21 0.2767 0.5892 0.0549 0.0258 0.363 4.573 3.609 270.497 0.517 16.054 6.052 0.34 135465. 0.3980
|
|
23.92 0.2980 0.6134 0.0519 0.0252 0.355 4.474 3.414 264.671 0.505 15.186 5.851 0.34 135631. 0.3742
|
|
25.62 0.3193 0.6347 0.0488 0.0246 0.346 4.358 3.212 257.820 0.492 14.285 5.650 0.34 135805. 0.3505
|
|
27.33 0.3406 0.6529 0.0457 0.0238 0.335 4.225 3.003 249.947 0.477 13.356 5.449 0.34 135988. 0.3268
|
|
29.04 0.3618 0.6678 0.0424 0.0230 0.323 4.075 2.788 241.053 0.460 12.399 5.245 0.34 136178. 0.3032
|
|
30.75 0.3831 0.6791 0.0390 0.0220 0.310 3.907 2.567 231.142 0.441 11.419 5.038 0.34 136377. 0.2794
|
|
32.46 0.4044 0.6864 0.0356 0.0210 0.295 3.723 2.342 220.219 0.421 10.418 4.824 0.34 136584. 0.2556
|
|
34.17 0.4257 0.6891 0.0321 0.0198 0.279 3.521 2.113 208.295 0.398 9.398 4.601 0.34 136799. 0.2315
|
|
35.87 0.4470 0.6865 0.0286 0.0186 0.262 3.303 1.880 195.384 0.373 8.363 4.365 0.34 137023. 0.2072
|
|
37.58 0.4683 0.6772 0.0250 0.0173 0.243 3.068 1.645 181.509 0.347 7.316 4.110 0.34 137255. 0.1825
|
|
39.29 0.4896 0.6596 0.0214 0.0159 0.224 2.818 1.407 166.701 0.318 6.261 3.830 0.34 137496. 0.1573
|
|
41.00 0.5108 0.6312 0.0178 0.0144 0.202 2.553 1.169 151.001 0.288 5.200 3.512 0.34 137746. 0.1314
|
|
42.71 0.5321 0.5877 0.0141 0.0128 0.180 2.273 0.931 134.465 0.257 4.139 3.139 0.34 138004. 0.1048
|
|
44.42 0.5534 0.5223 0.0105 0.0112 0.157 1.981 0.693 117.163 0.224 3.082 2.683 0.34 138270. 0.0773
|
|
46.12 0.5747 0.4232 0.0070 0.0094 0.133 1.677 0.458 99.181 0.189 2.035 2.093 0.34 138545. 0.0490
|
|
47.83 0.5960 0.2663 0.0034 0.0077 0.108 1.363 0.226 80.620 0.154 1.004 1.270 0.34 138829. 0.0209
|
|
49.54 0.6173 -0.0045 0.0000 0.0059 0.082 1.039 -0.003 61.466 0.117 -0.012 -0.021 0.34 139112. 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 0.0829 0.0259 0.631 6.623 7.848 470.181 0.748 34.909 7.571 0.40 160756. 0.7342
|
|
2.05 0.0213 0.0662 0.0814 0.0262 0.637 6.696 7.713 475.320 0.756 34.306 7.360 0.40 160847. 0.7075
|
|
4.10 0.0426 0.1286 0.0799 0.0265 0.644 6.761 7.567 479.958 0.764 33.659 7.151 0.40 160946. 0.6810
|
|
6.15 0.0639 0.1873 0.0783 0.0267 0.649 6.818 7.412 483.981 0.770 32.969 6.946 0.40 161051. 0.6546
|
|
8.20 0.0852 0.2425 0.0765 0.0269 0.653 6.864 7.246 487.280 0.776 32.232 6.745 0.40 161164. 0.6285
|
|
10.25 0.1064 0.2943 0.0747 0.0270 0.657 6.899 7.070 489.739 0.779 31.447 6.548 0.40 161284. 0.6027
|
|
12.30 0.1277 0.3427 0.0727 0.0271 0.659 6.920 6.882 491.242 0.782 30.613 6.355 0.40 161413. 0.5771
|
|
14.35 0.1490 0.3879 0.0706 0.0271 0.659 6.926 6.683 491.674 0.783 29.728 6.165 0.40 161550. 0.5518
|
|
16.40 0.1703 0.4300 0.0683 0.0271 0.658 6.916 6.473 490.917 0.781 28.791 5.980 0.40 161695. 0.5267
|
|
18.45 0.1916 0.4691 0.0660 0.0270 0.656 6.887 6.250 488.858 0.778 27.801 5.799 0.40 161849. 0.5019
|
|
20.50 0.2129 0.5053 0.0635 0.0268 0.651 6.838 6.016 485.383 0.773 26.758 5.621 0.40 162012. 0.4773
|
|
22.55 0.2342 0.5386 0.0609 0.0265 0.644 6.767 5.769 480.378 0.765 25.660 5.447 0.40 162184. 0.4529
|
|
24.60 0.2555 0.5690 0.0582 0.0261 0.635 6.673 5.510 473.716 0.754 24.507 5.275 0.40 162365. 0.4287
|
|
26.65 0.2768 0.5967 0.0553 0.0257 0.624 6.555 5.238 465.291 0.741 23.299 5.106 0.40 162556. 0.4045
|
|
28.71 0.2981 0.6215 0.0523 0.0251 0.610 6.411 4.955 455.065 0.724 22.040 4.939 0.41 162756. 0.3806
|
|
30.76 0.3193 0.6434 0.0492 0.0244 0.594 6.241 4.661 443.035 0.705 20.733 4.772 0.41 162965. 0.3567
|
|
32.81 0.3406 0.6623 0.0460 0.0237 0.576 6.046 4.358 429.202 0.683 19.384 4.605 0.41 163185. 0.3328
|
|
34.86 0.3619 0.6780 0.0427 0.0228 0.555 5.826 4.046 413.570 0.658 17.996 4.437 0.41 163414. 0.3090
|
|
36.91 0.3832 0.6903 0.0393 0.0218 0.531 5.580 3.726 396.143 0.630 16.573 4.266 0.41 163652. 0.2851
|
|
38.96 0.4045 0.6986 0.0359 0.0208 0.505 5.310 3.399 376.931 0.600 15.120 4.090 0.41 163901. 0.2611
|
|
41.01 0.4258 0.7025 0.0324 0.0196 0.477 5.014 3.066 355.952 0.567 13.640 3.907 0.41 164160. 0.2369
|
|
43.06 0.4471 0.7011 0.0288 0.0184 0.447 4.694 2.729 333.232 0.530 12.137 3.714 0.41 164429. 0.2124
|
|
45.11 0.4684 0.6933 0.0252 0.0170 0.414 4.350 2.387 308.811 0.491 10.617 3.506 0.41 164707. 0.1875
|
|
47.16 0.4897 0.6773 0.0216 0.0156 0.379 3.983 2.042 282.742 0.450 9.084 3.276 0.41 164997. 0.1621
|
|
49.21 0.5109 0.6505 0.0179 0.0141 0.342 3.594 1.696 255.100 0.406 7.544 3.015 0.41 165296. 0.1359
|
|
51.26 0.5322 0.6087 0.0143 0.0125 0.303 3.183 1.350 225.982 0.360 6.003 2.709 0.41 165606. 0.1089
|
|
53.31 0.5535 0.5447 0.0106 0.0108 0.262 2.754 1.005 195.513 0.311 4.469 2.331 0.41 165926. 0.0809
|
|
55.36 0.5748 0.4454 0.0070 0.0090 0.220 2.308 0.663 163.848 0.261 2.949 1.835 0.41 166256. 0.0517
|
|
57.41 0.5961 0.2841 0.0034 0.0072 0.176 1.848 0.326 131.164 0.209 1.452 1.129 0.41 166597. 0.0223
|
|
59.46 0.6174 -0.0067 -0.0001 0.0054 0.131 1.372 -0.006 97.407 0.155 -0.025 -0.026 0.41 166934. 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 0.0836 0.0259 1.002 9.020 10.773 747.044 1.019 47.916 6.541 0.47 187539. 0.7431
|
|
2.39 0.0213 0.0667 0.0821 0.0262 1.013 9.121 10.587 755.348 1.030 47.093 6.358 0.47 187646. 0.7161
|
|
4.78 0.0426 0.1295 0.0806 0.0265 1.023 9.211 10.389 762.838 1.041 46.210 6.177 0.47 187761. 0.6892
|
|
7.18 0.0639 0.1887 0.0789 0.0267 1.032 9.289 10.177 769.335 1.050 45.267 6.000 0.47 187884. 0.6626
|
|
9.57 0.0851 0.2444 0.0772 0.0269 1.039 9.354 9.950 774.659 1.057 44.260 5.826 0.47 188016. 0.6362
|
|
11.96 0.1064 0.2965 0.0753 0.0270 1.044 9.402 9.709 778.627 1.062 43.186 5.656 0.47 188158. 0.6101
|
|
14.35 0.1277 0.3453 0.0733 0.0271 1.047 9.431 9.452 781.049 1.065 42.045 5.489 0.47 188308. 0.5842
|
|
16.74 0.1490 0.3910 0.0712 0.0271 1.048 9.439 9.180 781.737 1.066 40.833 5.326 0.47 188468. 0.5586
|
|
19.13 0.1703 0.4334 0.0690 0.0271 1.047 9.424 8.891 780.503 1.065 39.549 5.167 0.47 188638. 0.5334
|
|
21.53 0.1916 0.4729 0.0666 0.0270 1.042 9.384 8.587 777.164 1.060 38.193 5.011 0.47 188818. 0.5083
|
|
23.92 0.2129 0.5095 0.0641 0.0268 1.035 9.316 8.265 771.537 1.053 36.763 4.859 0.47 189009. 0.4835
|
|
26.31 0.2342 0.5432 0.0615 0.0265 1.024 9.218 7.927 763.439 1.041 35.258 4.709 0.47 189210. 0.4590
|
|
28.70 0.2554 0.5741 0.0587 0.0261 1.009 9.088 7.571 752.666 1.027 33.676 4.563 0.47 189422. 0.4346
|
|
31.09 0.2767 0.6022 0.0558 0.0257 0.991 8.924 7.198 739.044 1.008 32.019 4.418 0.47 189644. 0.4103
|
|
33.49 0.2980 0.6276 0.0528 0.0251 0.969 8.724 6.810 722.508 0.986 30.290 4.275 0.47 189878. 0.3862
|
|
35.88 0.3193 0.6501 0.0497 0.0244 0.943 8.489 6.406 703.051 0.959 28.496 4.133 0.47 190123. 0.3621
|
|
38.27 0.3406 0.6696 0.0465 0.0236 0.913 8.219 5.990 680.676 0.929 26.643 3.991 0.47 190379. 0.3382
|
|
40.66 0.3619 0.6861 0.0431 0.0228 0.879 7.914 5.561 655.387 0.894 24.736 3.849 0.47 190647. 0.3142
|
|
43.05 0.3832 0.6991 0.0397 0.0218 0.841 7.573 5.122 627.193 0.856 22.781 3.704 0.47 190925. 0.2902
|
|
45.44 0.4045 0.7083 0.0362 0.0207 0.799 7.198 4.673 596.109 0.813 20.784 3.555 0.47 191216. 0.2660
|
|
47.84 0.4257 0.7132 0.0327 0.0195 0.754 6.788 4.215 562.163 0.767 18.749 3.401 0.47 191518. 0.2417
|
|
50.23 0.4470 0.7130 0.0291 0.0182 0.705 6.344 3.751 525.398 0.717 16.684 3.238 0.48 191832. 0.2171
|
|
52.62 0.4683 0.7065 0.0255 0.0169 0.652 5.867 3.281 485.876 0.663 14.593 3.063 0.48 192157. 0.1920
|
|
55.01 0.4896 0.6921 0.0218 0.0154 0.595 5.357 2.807 443.687 0.605 12.486 2.870 0.48 192495. 0.1664
|
|
57.40 0.5109 0.6669 0.0181 0.0139 0.535 4.817 2.331 398.950 0.544 10.368 2.650 0.48 192844. 0.1401
|
|
59.80 0.5322 0.6268 0.0144 0.0122 0.472 4.248 1.855 351.824 0.480 8.250 2.391 0.48 193206. 0.1127
|
|
62.19 0.5535 0.5643 0.0107 0.0105 0.406 3.653 1.380 302.511 0.413 6.140 2.070 0.48 193579. 0.0842
|
|
64.58 0.5747 0.4653 0.0071 0.0087 0.337 3.034 0.911 251.263 0.343 4.050 1.644 0.48 193964. 0.0543
|
|
66.97 0.5960 0.3006 0.0035 0.0069 0.266 2.395 0.448 198.374 0.271 1.992 1.024 0.48 194361. 0.0237
|
|
69.36 0.6173 -0.0088 -0.0001 0.0050 0.193 1.735 -0.009 143.707 0.196 -0.041 -0.029 0.48 194754. 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 0.0844 0.0261 1.503 11.843 14.211 1120.906 1.338 63.212 5.751 0.54 214317. 0.7504
|
|
2.73 0.0213 0.0670 0.0830 0.0264 1.520 11.976 13.969 1133.510 1.353 62.135 5.590 0.54 214439. 0.7232
|
|
5.46 0.0426 0.1301 0.0814 0.0266 1.535 12.096 13.709 1144.875 1.367 60.978 5.431 0.54 214572. 0.6961
|
|
8.20 0.0638 0.1896 0.0798 0.0269 1.549 12.200 13.431 1154.723 1.378 59.741 5.276 0.54 214713. 0.6693
|
|
10.93 0.0851 0.2455 0.0780 0.0270 1.559 12.285 13.134 1162.781 1.388 58.420 5.123 0.54 214865. 0.6427
|
|
13.66 0.1064 0.2979 0.0761 0.0272 1.567 12.348 12.817 1168.770 1.395 57.010 4.974 0.54 215026. 0.6164
|
|
16.39 0.1277 0.3470 0.0741 0.0273 1.572 12.387 12.480 1172.405 1.399 55.510 4.828 0.54 215199. 0.5904
|
|
19.13 0.1490 0.3929 0.0720 0.0273 1.574 12.397 12.122 1173.396 1.401 53.917 4.686 0.54 215383. 0.5647
|
|
21.86 0.1702 0.4357 0.0697 0.0272 1.571 12.377 11.742 1171.459 1.398 52.228 4.546 0.54 215577. 0.5393
|
|
24.59 0.1915 0.4755 0.0674 0.0271 1.564 12.322 11.341 1166.316 1.392 50.443 4.410 0.54 215784. 0.5141
|
|
27.32 0.2128 0.5124 0.0648 0.0269 1.552 12.231 10.917 1157.694 1.382 48.560 4.277 0.54 216002. 0.4892
|
|
30.06 0.2341 0.5464 0.0622 0.0266 1.536 12.101 10.471 1145.313 1.367 46.577 4.147 0.54 216232. 0.4645
|
|
32.79 0.2553 0.5777 0.0594 0.0263 1.514 11.927 10.003 1128.871 1.347 44.493 4.019 0.54 216475. 0.4400
|
|
35.52 0.2766 0.6063 0.0565 0.0258 1.486 11.707 9.512 1108.094 1.323 42.307 3.893 0.54 216730. 0.4157
|
|
38.25 0.2979 0.6321 0.0534 0.0252 1.452 11.441 8.999 1082.881 1.293 40.027 3.769 0.54 216998. 0.3914
|
|
40.99 0.3192 0.6552 0.0503 0.0245 1.412 11.128 8.467 1053.220 1.257 37.660 3.646 0.54 217278. 0.3673
|
|
43.72 0.3405 0.6753 0.0470 0.0237 1.367 10.767 7.917 1019.116 1.216 35.214 3.523 0.54 217571. 0.3432
|
|
46.45 0.3617 0.6924 0.0437 0.0228 1.315 10.360 7.351 980.575 1.170 32.696 3.400 0.54 217877. 0.3191
|
|
49.18 0.3830 0.7062 0.0402 0.0218 1.257 9.906 6.770 937.612 1.119 30.114 3.275 0.54 218196. 0.2950
|
|
51.92 0.4043 0.7163 0.0367 0.0207 1.194 9.406 6.177 890.250 1.063 27.475 3.147 0.54 218528. 0.2708
|
|
54.65 0.4256 0.7222 0.0331 0.0195 1.124 8.859 5.573 838.531 1.001 24.787 3.014 0.54 218873. 0.2463
|
|
57.38 0.4469 0.7231 0.0295 0.0182 1.049 8.268 4.959 782.521 0.934 22.057 2.874 0.54 219232. 0.2216
|
|
60.11 0.4681 0.7178 0.0258 0.0168 0.969 7.631 4.338 722.315 0.862 19.295 2.724 0.54 219604. 0.1964
|
|
62.85 0.4894 0.7048 0.0220 0.0153 0.882 6.952 3.711 658.050 0.785 16.508 2.558 0.54 219990. 0.1706
|
|
65.58 0.5107 0.6812 0.0183 0.0137 0.791 6.233 3.082 589.909 0.704 13.708 2.370 0.54 220389. 0.1440
|
|
68.31 0.5320 0.6428 0.0146 0.0121 0.695 5.474 2.452 518.131 0.618 10.907 2.146 0.55 220802. 0.1164
|
|
71.04 0.5532 0.5818 0.0108 0.0103 0.594 4.681 1.825 443.027 0.529 8.116 1.868 0.55 221229. 0.0874
|
|
73.78 0.5745 0.4836 0.0071 0.0085 0.489 3.856 1.203 364.984 0.436 5.352 1.495 0.55 221669. 0.0568
|
|
76.51 0.5958 0.3161 0.0035 0.0066 0.381 3.005 0.591 284.451 0.340 2.629 0.942 0.55 222122. 0.0251
|
|
79.24 0.6171 -0.0107 -0.0001 0.0047 0.270 2.125 -0.014 201.161 0.240 -0.061 -0.031 0.55 222569. 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 0.0854 0.0263 2.161 15.133 18.199 1611.322 1.710 80.951 5.123 0.61 241088. 0.7565
|
|
3.07 0.0213 0.0671 0.0840 0.0266 2.185 15.304 17.892 1629.591 1.729 79.584 4.980 0.61 241227. 0.7292
|
|
6.14 0.0425 0.1303 0.0824 0.0269 2.207 15.459 17.562 1646.046 1.747 78.117 4.839 0.61 241376. 0.7020
|
|
9.22 0.0638 0.1899 0.0808 0.0271 2.226 15.592 17.209 1660.281 1.762 76.545 4.701 0.61 241536. 0.6751
|
|
12.29 0.0851 0.2460 0.0790 0.0273 2.242 15.702 16.831 1671.907 1.774 74.864 4.566 0.61 241707. 0.6485
|
|
15.36 0.1063 0.2986 0.0771 0.0275 2.254 15.782 16.428 1680.509 1.783 73.070 4.434 0.61 241890. 0.6221
|
|
18.43 0.1276 0.3478 0.0751 0.0275 2.261 15.831 15.998 1685.676 1.789 71.159 4.305 0.61 242085. 0.5960
|
|
21.50 0.1489 0.3939 0.0729 0.0276 2.262 15.843 15.541 1686.988 1.790 69.128 4.179 0.61 242292. 0.5702
|
|
24.58 0.1701 0.4369 0.0707 0.0275 2.258 15.815 15.057 1684.035 1.787 66.973 4.055 0.61 242512. 0.5447
|
|
27.65 0.1914 0.4770 0.0683 0.0274 2.248 15.744 14.544 1676.414 1.779 64.694 3.935 0.61 242745. 0.5195
|
|
30.72 0.2126 0.5141 0.0657 0.0272 2.231 15.625 14.003 1663.727 1.765 62.288 3.818 0.61 242991. 0.4945
|
|
33.79 0.2339 0.5485 0.0630 0.0269 2.207 15.454 13.434 1645.575 1.746 59.753 3.703 0.61 243251. 0.4698
|
|
36.86 0.2552 0.5802 0.0602 0.0265 2.175 15.228 12.835 1621.530 1.720 57.088 3.590 0.61 243524. 0.4452
|
|
39.94 0.2764 0.6091 0.0573 0.0260 2.134 14.943 12.206 1591.189 1.688 54.292 3.479 0.61 243812. 0.4208
|
|
43.01 0.2977 0.6354 0.0542 0.0254 2.084 14.598 11.550 1554.391 1.649 51.373 3.370 0.61 244113. 0.3965
|
|
46.08 0.3190 0.6590 0.0510 0.0247 2.026 14.192 10.868 1511.121 1.603 48.340 3.262 0.61 244429. 0.3723
|
|
49.15 0.3402 0.6797 0.0477 0.0239 1.960 13.724 10.163 1461.387 1.551 45.206 3.154 0.61 244759. 0.3481
|
|
52.22 0.3615 0.6974 0.0443 0.0230 1.884 13.197 9.438 1405.204 1.491 41.979 3.046 0.61 245104. 0.3240
|
|
55.30 0.3828 0.7120 0.0408 0.0219 1.800 12.609 8.693 1342.591 1.425 38.668 2.937 0.61 245463. 0.2998
|
|
58.37 0.4040 0.7229 0.0372 0.0208 1.708 11.961 7.933 1273.587 1.351 35.284 2.825 0.61 245837. 0.2754
|
|
61.44 0.4253 0.7297 0.0336 0.0196 1.607 11.253 7.157 1198.253 1.271 31.835 2.709 0.61 246225. 0.2509
|
|
64.51 0.4466 0.7317 0.0299 0.0182 1.497 10.487 6.369 1116.682 1.185 28.331 2.587 0.61 246629. 0.2260
|
|
67.58 0.4678 0.7277 0.0261 0.0168 1.380 9.664 5.572 1029.018 1.092 24.785 2.456 0.61 247047. 0.2007
|
|
70.66 0.4891 0.7160 0.0224 0.0153 1.254 8.785 4.768 935.456 0.993 21.207 2.312 0.61 247481. 0.1747
|
|
73.73 0.5104 0.6941 0.0186 0.0137 1.121 7.854 3.959 836.263 0.887 17.611 2.147 0.61 247930. 0.1479
|
|
76.80 0.5316 0.6574 0.0148 0.0120 0.981 6.873 3.150 731.789 0.776 14.012 1.952 0.61 248394. 0.1200
|
|
79.87 0.5529 0.5981 0.0110 0.0102 0.835 5.846 2.344 622.488 0.660 10.427 1.708 0.61 248874. 0.0905
|
|
82.94 0.5741 0.5009 0.0073 0.0083 0.682 4.779 1.546 508.922 0.540 6.874 1.377 0.62 249369. 0.0593
|
|
86.02 0.5954 0.3313 0.0036 0.0064 0.525 3.679 0.759 391.753 0.416 3.375 0.879 0.62 249878. 0.0265
|
|
89.09 0.6167 -0.0124 -0.0001 0.0044 0.363 2.541 -0.019 270.519 0.287 -0.084 -0.032 0.62 250378. 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 0.0866 0.0267 3.006 18.948 22.782 2241.830 2.141 101.333 4.609 0.67 267851. 0.7616
|
|
3.41 0.0212 0.0670 0.0852 0.0270 3.041 19.164 22.402 2267.382 2.165 99.645 4.481 0.67 268006. 0.7342
|
|
6.82 0.0425 0.1302 0.0836 0.0273 3.071 19.359 21.994 2290.363 2.187 97.829 4.356 0.67 268172. 0.7071
|
|
10.23 0.0637 0.1898 0.0819 0.0275 3.098 19.526 21.556 2310.204 2.206 95.882 4.232 0.67 268351. 0.6802
|
|
13.64 0.0850 0.2459 0.0802 0.0277 3.120 19.663 21.087 2326.352 2.222 93.796 4.111 0.67 268542. 0.6536
|
|
17.05 0.1062 0.2985 0.0783 0.0278 3.136 19.763 20.586 2338.235 2.233 91.568 3.993 0.67 268746. 0.6272
|
|
20.46 0.1275 0.3479 0.0762 0.0279 3.145 19.823 20.052 2345.268 2.240 89.192 3.878 0.67 268964. 0.6011
|
|
23.87 0.1487 0.3941 0.0741 0.0280 3.147 19.836 19.484 2346.865 2.241 86.663 3.766 0.67 269195. 0.5754
|
|
27.28 0.1700 0.4372 0.0718 0.0279 3.141 19.799 18.880 2342.453 2.237 83.979 3.656 0.67 269440. 0.5499
|
|
30.69 0.1912 0.4775 0.0693 0.0278 3.127 19.706 18.241 2331.465 2.226 81.136 3.549 0.67 269700. 0.5247
|
|
34.10 0.2125 0.5149 0.0668 0.0276 3.102 19.553 17.566 2313.353 2.209 78.133 3.444 0.67 269974. 0.4997
|
|
37.51 0.2337 0.5496 0.0641 0.0272 3.068 19.335 16.854 2287.569 2.184 74.969 3.342 0.67 270264. 0.4749
|
|
40.92 0.2549 0.5816 0.0612 0.0268 3.022 19.047 16.106 2253.518 2.152 71.639 3.242 0.67 270568. 0.4503
|
|
44.33 0.2762 0.6109 0.0582 0.0263 2.965 18.685 15.320 2210.633 2.111 68.143 3.143 0.67 270889. 0.4259
|
|
47.74 0.2974 0.6376 0.0551 0.0257 2.895 18.246 14.499 2158.673 2.061 64.490 3.046 0.68 271224. 0.4015
|
|
51.15 0.3187 0.6617 0.0519 0.0250 2.813 17.730 13.645 2097.618 2.003 60.695 2.951 0.68 271576. 0.3773
|
|
54.56 0.3399 0.6830 0.0485 0.0241 2.719 17.137 12.763 2027.482 1.936 56.769 2.855 0.68 271943. 0.3531
|
|
57.97 0.3612 0.7013 0.0451 0.0232 2.613 16.467 11.854 1948.293 1.860 52.724 2.760 0.68 272326. 0.3289
|
|
61.38 0.3824 0.7166 0.0415 0.0222 2.494 15.722 10.920 1860.084 1.776 48.574 2.663 0.68 272725. 0.3046
|
|
64.79 0.4037 0.7283 0.0379 0.0210 2.364 14.901 9.966 1762.910 1.683 44.329 2.564 0.68 273141. 0.2802
|
|
68.20 0.4249 0.7361 0.0342 0.0197 2.222 14.004 8.993 1656.859 1.582 40.002 2.462 0.68 273572. 0.2556
|
|
71.61 0.4462 0.7392 0.0304 0.0184 2.068 13.034 8.005 1542.069 1.473 35.605 2.354 0.68 274021. 0.2306
|
|
75.02 0.4674 0.7364 0.0266 0.0169 1.903 11.992 7.004 1418.737 1.355 31.152 2.239 0.68 274486. 0.2051
|
|
78.43 0.4886 0.7262 0.0228 0.0153 1.726 10.879 5.993 1287.139 1.229 26.658 2.112 0.68 274967. 0.1790
|
|
81.85 0.5099 0.7058 0.0189 0.0137 1.539 9.700 4.978 1147.650 1.096 22.140 1.967 0.68 275466. 0.1519
|
|
85.26 0.5311 0.6709 0.0151 0.0119 1.342 8.459 3.961 1000.773 0.956 17.617 1.795 0.68 275981. 0.1237
|
|
88.67 0.5524 0.6134 0.0112 0.0101 1.136 7.160 2.947 847.162 0.809 13.110 1.578 0.68 276513. 0.0938
|
|
92.08 0.5736 0.5174 0.0074 0.0082 0.922 5.812 1.943 687.645 0.657 8.644 1.282 0.68 277062. 0.0619
|
|
95.49 0.5949 0.3461 0.0036 0.0062 0.702 4.422 0.954 523.198 0.500 4.243 0.827 0.68 277628. 0.0280
|
|
98.90 0.6161 -0.0139 -0.0001 0.0042 0.474 2.985 -0.025 353.149 0.337 -0.111 -0.032 0.69 278181. 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 0.0880 0.0273 4.090 23.433 28.019 3049.593 2.647 124.627 4.167 0.74 294603. 0.7636
|
|
3.75 0.0212 0.0666 0.0866 0.0276 4.134 23.686 27.560 3082.506 2.676 122.587 4.055 0.74 294775. 0.7370
|
|
7.49 0.0424 0.1296 0.0850 0.0278 4.173 23.914 27.066 3112.175 2.702 120.388 3.945 0.74 294959. 0.7104
|
|
11.24 0.0637 0.1890 0.0834 0.0281 4.208 24.111 26.535 3137.819 2.724 118.026 3.836 0.74 295156. 0.6839
|
|
14.98 0.0849 0.2449 0.0816 0.0283 4.236 24.271 25.965 3158.659 2.742 115.492 3.728 0.74 295368. 0.6577
|
|
18.73 0.1061 0.2975 0.0797 0.0284 4.256 24.388 25.355 3173.887 2.755 112.780 3.623 0.74 295593. 0.6316
|
|
22.48 0.1273 0.3469 0.0776 0.0285 4.268 24.455 24.704 3182.670 2.763 109.884 3.521 0.74 295834. 0.6057
|
|
26.22 0.1485 0.3932 0.0754 0.0285 4.270 24.467 24.010 3184.156 2.764 106.797 3.420 0.74 296089. 0.5801
|
|
29.97 0.1697 0.4365 0.0731 0.0284 4.261 24.416 23.273 3177.508 2.758 103.517 3.322 0.74 296360. 0.5548
|
|
33.72 0.1910 0.4769 0.0707 0.0283 4.240 24.296 22.491 3161.908 2.745 100.039 3.226 0.74 296647. 0.5296
|
|
37.46 0.2122 0.5145 0.0681 0.0281 4.206 24.101 21.664 3136.569 2.723 96.362 3.133 0.74 296950. 0.5048
|
|
41.21 0.2334 0.5494 0.0653 0.0277 4.158 23.826 20.792 3100.747 2.692 92.482 3.041 0.74 297269. 0.4801
|
|
44.95 0.2546 0.5818 0.0624 0.0273 4.095 23.464 19.874 3053.651 2.651 88.398 2.952 0.74 297605. 0.4555
|
|
48.70 0.2758 0.6115 0.0594 0.0268 4.016 23.009 18.909 2994.498 2.600 84.107 2.864 0.74 297958. 0.4311
|
|
52.45 0.2970 0.6387 0.0562 0.0262 3.920 22.459 17.900 2922.935 2.537 79.619 2.778 0.74 298328. 0.4068
|
|
56.19 0.3183 0.6632 0.0529 0.0254 3.807 21.814 16.851 2838.934 2.465 74.951 2.692 0.74 298715. 0.3826
|
|
59.94 0.3395 0.6851 0.0495 0.0245 3.678 21.073 15.764 2742.528 2.381 70.120 2.607 0.74 299119. 0.3583
|
|
63.69 0.3607 0.7041 0.0460 0.0236 3.532 20.238 14.645 2633.776 2.286 65.141 2.522 0.74 299541. 0.3341
|
|
67.43 0.3819 0.7201 0.0424 0.0225 3.370 19.308 13.495 2512.753 2.181 60.028 2.436 0.75 299981. 0.3098
|
|
71.18 0.4031 0.7327 0.0387 0.0213 3.191 18.284 12.319 2379.576 2.066 54.795 2.348 0.75 300438. 0.2853
|
|
74.92 0.4243 0.7414 0.0349 0.0200 2.996 17.169 11.119 2234.415 1.940 49.459 2.257 0.75 300913. 0.2605
|
|
78.67 0.4456 0.7454 0.0311 0.0186 2.786 15.963 9.900 2077.521 1.804 44.033 2.161 0.75 301406. 0.2354
|
|
82.42 0.4668 0.7437 0.0272 0.0171 2.560 14.670 8.664 1909.249 1.657 38.537 2.058 0.75 301916. 0.2097
|
|
86.16 0.4880 0.7344 0.0233 0.0155 2.320 13.294 7.416 1730.095 1.502 32.987 1.944 0.75 302446. 0.1833
|
|
89.91 0.5092 0.7149 0.0194 0.0138 2.066 11.839 6.161 1540.723 1.338 27.404 1.814 0.75 302993. 0.1558
|
|
93.66 0.5304 0.6805 0.0154 0.0120 1.800 10.312 4.904 1342.002 1.165 21.812 1.657 0.75 303559. 0.1271
|
|
97.40 0.5516 0.6229 0.0115 0.0102 1.522 8.721 3.650 1135.040 0.985 16.237 1.459 0.75 304143. 0.0965
|
|
101.15 0.5729 0.5256 0.0076 0.0082 1.235 7.078 2.408 921.210 0.800 10.709 1.185 0.75 304746. 0.0637
|
|
104.89 0.5941 0.3512 0.0037 0.0063 0.942 5.395 1.182 702.110 0.610 5.258 0.764 0.75 305367. 0.0287
|
|
108.64 0.6153 -0.0138 -0.0001 0.0043 0.640 3.664 -0.030 476.901 0.414 -0.136 -0.029 0.75 305974. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 12000
|
|
|
|
V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
|
|
(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
|
|
0.00 0.0000 0.0000 0.0897 0.0289 5.614 29.485 33.983 4186.114 3.331 151.157 3.682 0.81 321341. 0.7430
|
|
4.08 0.0212 0.0643 0.0883 0.0291 5.653 29.694 33.441 4215.803 3.355 148.746 3.598 0.81 321529. 0.7202
|
|
8.16 0.0424 0.1257 0.0867 0.0292 5.688 29.875 32.855 4241.425 3.375 146.140 3.513 0.81 321731. 0.6971
|
|
12.24 0.0635 0.1840 0.0851 0.0294 5.716 30.020 32.224 4262.099 3.392 143.332 3.429 0.81 321948. 0.6739
|
|
16.32 0.0847 0.2393 0.0833 0.0295 5.735 30.125 31.545 4276.937 3.403 140.313 3.345 0.81 322180. 0.6504
|
|
20.40 0.1059 0.2917 0.0813 0.0295 5.746 30.182 30.817 4285.006 3.410 137.074 3.262 0.81 322427. 0.6268
|
|
24.48 0.1271 0.3411 0.0793 0.0295 5.747 30.184 30.037 4285.322 3.410 133.606 3.179 0.81 322691. 0.6032
|
|
28.56 0.1483 0.3877 0.0771 0.0295 5.735 30.124 29.205 4276.897 3.403 129.904 3.097 0.81 322971. 0.5794
|
|
32.64 0.1694 0.4315 0.0748 0.0294 5.711 29.997 28.319 4258.739 3.389 125.962 3.016 0.81 323268. 0.5556
|
|
36.71 0.1906 0.4725 0.0723 0.0292 5.672 29.793 27.378 4229.802 3.366 121.777 2.936 0.81 323582. 0.5317
|
|
40.79 0.2118 0.5108 0.0696 0.0289 5.618 29.506 26.381 4189.069 3.334 117.344 2.856 0.81 323914. 0.5079
|
|
44.87 0.2330 0.5465 0.0669 0.0285 5.546 29.128 25.329 4135.483 3.291 112.662 2.778 0.81 324264. 0.4840
|
|
48.95 0.2541 0.5795 0.0639 0.0280 5.455 28.652 24.219 4067.906 3.237 107.727 2.700 0.81 324631. 0.4600
|
|
53.03 0.2753 0.6100 0.0609 0.0275 5.344 28.070 23.052 3985.260 3.171 102.536 2.624 0.81 325017. 0.4361
|
|
57.11 0.2965 0.6377 0.0576 0.0268 5.213 27.380 21.830 3887.285 3.093 97.100 2.547 0.81 325422. 0.4120
|
|
61.19 0.3177 0.6628 0.0543 0.0260 5.061 26.580 20.558 3773.648 3.003 91.441 2.471 0.81 325845. 0.3878
|
|
65.27 0.3389 0.6852 0.0508 0.0251 4.887 25.669 19.240 3644.392 2.900 85.577 2.394 0.81 326287. 0.3636
|
|
69.35 0.3600 0.7045 0.0472 0.0241 4.693 24.649 17.880 3499.472 2.785 79.529 2.317 0.81 326747. 0.3392
|
|
73.43 0.3812 0.7207 0.0435 0.0230 4.478 23.518 16.482 3338.968 2.657 73.313 2.239 0.81 327227. 0.3147
|
|
77.51 0.4024 0.7333 0.0397 0.0218 4.242 22.281 15.051 3163.290 2.517 66.947 2.158 0.81 327725. 0.2898
|
|
81.59 0.4236 0.7416 0.0359 0.0205 3.987 20.939 13.590 2972.860 2.366 60.450 2.073 0.81 328243. 0.2646
|
|
85.67 0.4448 0.7448 0.0320 0.0191 3.712 19.499 12.105 2768.301 2.203 53.841 1.983 0.81 328780. 0.2389
|
|
89.75 0.4659 0.7415 0.0280 0.0176 3.420 17.964 10.598 2550.479 2.030 47.139 1.885 0.82 329337. 0.2124
|
|
93.83 0.4871 0.7297 0.0240 0.0160 3.112 16.344 9.076 2320.474 1.847 40.368 1.774 0.82 329913. 0.1850
|
|
97.91 0.5083 0.7061 0.0199 0.0143 2.789 14.648 7.543 2079.582 1.655 33.551 1.645 0.82 330510. 0.1564
|
|
101.98 0.5295 0.6658 0.0159 0.0126 2.453 12.886 6.006 1829.434 1.456 26.717 1.489 0.82 331126. 0.1263
|
|
106.06 0.5506 0.6001 0.0118 0.0108 2.108 11.072 4.473 1571.963 1.251 19.897 1.291 0.82 331762. 0.0945
|
|
110.14 0.5718 0.4936 0.0078 0.0090 1.756 9.223 2.951 1309.421 1.042 13.127 1.022 0.82 332418. 0.0608
|
|
114.22 0.5930 0.3152 0.0038 0.0072 1.400 7.356 1.449 1044.292 0.831 6.446 0.629 0.82 333092. 0.0262
|
|
118.30 0.6142 -0.0111 -0.0001 0.0053 1.040 5.462 -0.036 775.427 0.617 -0.162 -0.021 0.82 333757. 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 0.0915 0.0328 8.116 39.350 40.694 6052.293 4.446 181.008 3.050 0.87 348064. 0.6735
|
|
4.43 0.0212 0.0582 0.0901 0.0328 8.120 39.370 40.069 6055.391 4.448 178.227 3.001 0.87 348269. 0.6577
|
|
8.85 0.0424 0.1146 0.0886 0.0328 8.116 39.348 39.390 6051.999 4.446 175.207 2.952 0.87 348490. 0.6414
|
|
13.28 0.0636 0.1690 0.0869 0.0327 8.102 39.279 38.656 6041.329 4.438 171.941 2.902 0.87 348727. 0.6246
|
|
17.71 0.0849 0.2214 0.0852 0.0326 8.076 39.157 37.863 6022.560 4.424 168.415 2.852 0.87 348980. 0.6074
|
|
22.13 0.1061 0.2717 0.0832 0.0325 8.039 38.977 37.010 5994.795 4.404 164.618 2.800 0.87 349251. 0.5897
|
|
26.56 0.1273 0.3200 0.0812 0.0323 7.989 38.731 36.093 5957.106 4.376 160.540 2.748 0.87 349540. 0.5715
|
|
30.99 0.1485 0.3662 0.0790 0.0320 7.923 38.416 35.111 5908.516 4.340 156.172 2.695 0.88 349846. 0.5529
|
|
35.42 0.1697 0.4102 0.0766 0.0317 7.842 38.022 34.062 5848.037 4.296 151.507 2.642 0.88 350171. 0.5337
|
|
39.84 0.1909 0.4520 0.0741 0.0313 7.744 37.545 32.945 5774.680 4.242 146.538 2.588 0.88 350515. 0.5141
|
|
44.27 0.2122 0.4915 0.0714 0.0308 7.627 36.978 31.759 5687.482 4.178 141.263 2.533 0.88 350878. 0.4941
|
|
48.70 0.2334 0.5288 0.0686 0.0303 7.490 36.315 30.504 5585.433 4.103 135.680 2.477 0.88 351261. 0.4736
|
|
53.12 0.2546 0.5637 0.0656 0.0296 7.332 35.547 29.178 5467.362 4.016 129.785 2.421 0.88 351663. 0.4526
|
|
57.55 0.2758 0.5963 0.0625 0.0289 7.150 34.667 27.782 5331.903 3.917 123.573 2.363 0.88 352085. 0.4312
|
|
61.98 0.2970 0.6263 0.0592 0.0281 6.945 33.671 26.317 5178.778 3.804 117.058 2.305 0.88 352527. 0.4093
|
|
66.40 0.3182 0.6531 0.0558 0.0272 6.721 32.586 24.790 5011.896 3.682 110.264 2.243 0.88 352989. 0.3867
|
|
70.83 0.3394 0.6766 0.0522 0.0262 6.477 31.404 23.205 4830.094 3.548 103.215 2.179 0.88 353472. 0.3634
|
|
75.26 0.3607 0.6966 0.0485 0.0251 6.214 30.126 21.568 4633.547 3.404 95.936 2.111 0.88 353974. 0.3394
|
|
79.68 0.3819 0.7121 0.0447 0.0240 5.933 28.765 19.884 4424.279 3.250 88.446 2.039 0.88 354498. 0.3147
|
|
84.11 0.4031 0.7221 0.0408 0.0228 5.640 27.346 18.158 4205.954 3.090 80.766 1.958 0.88 355041. 0.2888
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88.54 0.4243 0.7265 0.0369 0.0215 5.328 25.833 16.395 3973.193 2.919 72.924 1.872 0.88 355606. 0.2623
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92.97 0.4455 0.7243 0.0328 0.0202 4.997 24.229 14.600 3726.552 2.737 64.942 1.777 0.88 356191. 0.2351
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|
97.39 0.4667 0.7137 0.0287 0.0188 4.650 22.546 12.780 3467.689 2.547 56.847 1.672 0.88 356798. 0.2069
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|
101.82 0.4879 0.6925 0.0246 0.0173 4.290 20.798 10.941 3198.839 2.350 48.667 1.551 0.88 357425. 0.1776
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|
106.25 0.5092 0.6571 0.0204 0.0158 3.919 19.002 9.090 2922.543 2.147 40.433 1.411 0.89 358074. 0.1472
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|
110.67 0.5304 0.6028 0.0163 0.0143 3.542 17.173 7.235 2641.225 1.940 32.183 1.243 0.89 358744. 0.1157
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|
115.10 0.5516 0.5228 0.0121 0.0128 3.162 15.330 5.385 2357.818 1.732 23.955 1.036 0.89 359436. 0.0832
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|
119.53 0.5728 0.4066 0.0080 0.0113 2.783 13.494 3.551 2075.488 1.525 15.795 0.776 0.89 360149. 0.0506
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|
123.95 0.5940 0.2391 0.0039 0.0097 2.410 11.685 1.743 1797.229 1.320 7.754 0.440 0.89 360883. 0.0201
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|
128.38 0.6152 -0.0074 -0.0001 0.0082 2.036 9.872 -0.044 1518.293 1.115 -0.197 -0.013 0.89 361616. 0.0000
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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 0.0923 0.0391 12.074 54.358 47.612 9003.641 6.141 211.777 2.398 0.94 374807. 0.5729
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|
4.81 0.0214 0.0500 0.0911 0.0390 12.051 54.255 46.949 8986.597 6.130 208.830 2.370 0.94 375027. 0.5621
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|
9.62 0.0428 0.0987 0.0896 0.0389 12.009 54.065 46.220 8955.062 6.108 205.589 2.341 0.94 375265. 0.5509
|
|
14.43 0.0642 0.1463 0.0881 0.0387 11.946 53.780 45.422 8907.918 6.076 202.038 2.313 0.94 375520. 0.5396
|
|
19.24 0.0856 0.1927 0.0864 0.0384 11.860 53.395 44.550 8844.088 6.032 198.159 2.285 0.94 375795. 0.5279
|
|
24.05 0.1070 0.2380 0.0846 0.0380 11.751 52.903 43.601 8762.717 5.977 193.936 2.257 0.94 376089. 0.5159
|
|
28.86 0.1284 0.2820 0.0826 0.0376 11.617 52.301 42.571 8662.965 5.909 189.355 2.229 0.94 376403. 0.5034
|
|
33.67 0.1498 0.3249 0.0804 0.0371 11.458 51.584 41.457 8544.168 5.828 184.403 2.201 0.94 376738. 0.4905
|
|
38.48 0.1713 0.3665 0.0781 0.0365 11.272 50.748 40.258 8405.788 5.734 179.069 2.172 0.94 377093. 0.4771
|
|
43.29 0.1927 0.4068 0.0756 0.0358 11.060 49.791 38.971 8247.243 5.625 173.344 2.143 0.94 377469. 0.4632
|
|
48.11 0.2141 0.4457 0.0729 0.0350 10.820 48.713 37.596 8068.658 5.504 167.227 2.113 0.94 377867. 0.4486
|
|
52.92 0.2355 0.4831 0.0701 0.0342 10.554 47.512 36.133 7869.804 5.368 160.718 2.082 0.94 378287. 0.4333
|
|
57.73 0.2569 0.5188 0.0671 0.0332 10.259 46.187 34.580 7650.240 5.218 153.812 2.050 0.94 378728. 0.4173
|
|
62.54 0.2783 0.5528 0.0639 0.0322 9.936 44.732 32.938 7409.250 5.054 146.507 2.016 0.94 379191. 0.4006
|
|
67.35 0.2997 0.5848 0.0605 0.0310 9.584 43.147 31.209 7146.720 4.875 138.819 1.981 0.95 379677. 0.3830
|
|
72.16 0.3211 0.6146 0.0570 0.0298 9.206 41.444 29.402 6864.664 4.682 130.781 1.943 0.95 380184. 0.3647
|
|
76.97 0.3425 0.6405 0.0534 0.0285 8.819 39.703 27.522 6576.199 4.486 122.418 1.898 0.95 380714. 0.3447
|
|
81.78 0.3639 0.6623 0.0496 0.0273 8.421 37.910 25.576 6279.287 4.283 113.762 1.847 0.95 381266. 0.3234
|
|
86.59 0.3853 0.6792 0.0457 0.0259 8.013 36.074 23.571 5975.133 4.076 104.845 1.789 0.95 381840. 0.3007
|
|
91.40 0.4067 0.6877 0.0417 0.0247 7.624 34.323 21.512 5685.121 3.878 95.685 1.716 0.95 382437. 0.2756
|
|
96.21 0.4281 0.6835 0.0376 0.0236 7.283 32.788 19.402 5430.953 3.704 86.301 1.620 0.95 383056. 0.2471
|
|
101.02 0.4495 0.6706 0.0335 0.0224 6.931 31.205 17.256 5168.727 3.526 76.754 1.514 0.95 383698. 0.2177
|
|
105.83 0.4709 0.6476 0.0292 0.0213 6.572 29.587 15.081 4900.665 3.343 67.082 1.396 0.95 384363. 0.1876
|
|
110.64 0.4924 0.6125 0.0250 0.0201 6.208 27.948 12.888 4629.246 3.158 57.327 1.263 0.95 385051. 0.1569
|
|
115.45 0.5138 0.5630 0.0207 0.0189 5.844 26.309 10.687 4357.699 2.972 47.537 1.112 0.95 385762. 0.1259
|
|
120.26 0.5352 0.4965 0.0165 0.0178 5.485 24.692 8.491 4089.899 2.790 37.767 0.942 0.95 386496. 0.0950
|
|
125.07 0.5566 0.4101 0.0122 0.0166 5.134 23.112 6.313 3828.126 2.611 28.080 0.748 0.96 387254. 0.0651
|
|
129.88 0.5780 0.3012 0.0081 0.0155 4.794 21.581 4.169 3574.649 2.438 18.544 0.529 0.96 388036. 0.0374
|
|
134.70 0.5994 0.1667 0.0040 0.0145 4.466 20.107 2.073 3330.505 2.272 9.222 0.282 0.96 388843. 0.0141
|
|
139.51 0.6208 0.0001 0.0000 0.0134 4.128 18.584 0.002 3078.176 2.100 0.007 0.000 0.96 389685. 0.0000
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