390 lines
69 KiB
Plaintext
390 lines
69 KiB
Plaintext
21.5x10.5PN (215x105PN.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 0.0848 0.0319 0.012 0.746 0.580 8.822 0.084 2.579 29.811 0.09 49137. 0.6190
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0.45 0.0220 0.0571 0.0834 0.0322 0.012 0.753 0.570 8.907 0.085 2.535 29.027 0.09 49166. 0.5976
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0.90 0.0440 0.1111 0.0819 0.0324 0.012 0.759 0.559 8.985 0.086 2.489 28.245 0.09 49197. 0.5761
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1.35 0.0661 0.1621 0.0802 0.0327 0.012 0.765 0.548 9.053 0.086 2.438 27.467 0.09 49231. 0.5545
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1.80 0.0881 0.2101 0.0785 0.0329 0.012 0.770 0.536 9.111 0.087 2.385 26.693 0.09 49267. 0.5329
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2.24 0.1101 0.2550 0.0766 0.0331 0.012 0.774 0.523 9.155 0.087 2.328 25.925 0.09 49306. 0.5114
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2.69 0.1321 0.2971 0.0746 0.0332 0.012 0.776 0.510 9.185 0.088 2.267 25.164 0.09 49348. 0.4898
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3.14 0.1542 0.3362 0.0724 0.0332 0.012 0.777 0.495 9.197 0.088 2.202 24.410 0.09 49392. 0.4683
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3.59 0.1762 0.3725 0.0701 0.0332 0.012 0.777 0.479 9.190 0.088 2.132 23.663 0.09 49439. 0.4467
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4.04 0.1982 0.4059 0.0677 0.0331 0.012 0.774 0.463 9.160 0.087 2.059 22.922 0.09 49489. 0.4252
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4.49 0.2202 0.4365 0.0652 0.0329 0.012 0.770 0.445 9.107 0.087 1.982 22.188 0.09 49543. 0.4038
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4.94 0.2423 0.4644 0.0625 0.0326 0.012 0.763 0.427 9.029 0.086 1.900 21.458 0.09 49599. 0.3824
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5.39 0.2643 0.4895 0.0597 0.0322 0.012 0.754 0.408 8.925 0.085 1.815 20.732 0.09 49658. 0.3610
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5.83 0.2863 0.5117 0.0568 0.0318 0.012 0.743 0.388 8.795 0.084 1.726 20.007 0.09 49720. 0.3398
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6.28 0.3083 0.5311 0.0537 0.0312 0.012 0.730 0.367 8.638 0.082 1.633 19.281 0.09 49785. 0.3186
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6.73 0.3303 0.5475 0.0506 0.0305 0.011 0.715 0.346 8.454 0.081 1.538 18.550 0.09 49854. 0.2974
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7.18 0.3524 0.5607 0.0474 0.0298 0.011 0.697 0.324 8.242 0.079 1.440 17.812 0.09 49926. 0.2763
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7.63 0.3744 0.5706 0.0440 0.0289 0.011 0.676 0.301 8.001 0.076 1.339 17.060 0.09 50001. 0.2552
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8.08 0.3964 0.5769 0.0406 0.0279 0.010 0.654 0.278 7.733 0.074 1.235 16.289 0.09 50079. 0.2341
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8.53 0.4184 0.5791 0.0372 0.0268 0.010 0.628 0.254 7.435 0.071 1.129 15.492 0.09 50161. 0.2129
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8.98 0.4405 0.5768 0.0336 0.0257 0.010 0.601 0.230 7.107 0.068 1.022 14.659 0.09 50246. 0.1916
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9.42 0.4625 0.5692 0.0300 0.0244 0.009 0.571 0.205 6.750 0.064 0.912 13.777 0.09 50335. 0.1701
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9.87 0.4845 0.5553 0.0263 0.0230 0.009 0.538 0.180 6.363 0.061 0.801 12.829 0.09 50427. 0.1484
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10.32 0.5065 0.5337 0.0226 0.0215 0.008 0.503 0.155 5.947 0.057 0.688 11.793 0.09 50522. 0.1264
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10.77 0.5286 0.5022 0.0189 0.0199 0.007 0.465 0.129 5.501 0.053 0.574 10.636 0.09 50621. 0.1042
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11.22 0.5506 0.4579 0.0151 0.0181 0.007 0.425 0.103 5.025 0.048 0.459 9.310 0.09 50723. 0.0815
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11.67 0.5726 0.3961 0.0113 0.0163 0.006 0.382 0.077 4.522 0.043 0.343 7.743 0.09 50829. 0.0587
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12.12 0.5946 0.3091 0.0075 0.0144 0.005 0.337 0.051 3.992 0.038 0.228 5.819 0.09 50938. 0.0359
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12.57 0.6166 0.1840 0.0037 0.0124 0.005 0.290 0.025 3.437 0.033 0.113 3.339 0.09 51050. 0.0145
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13.02 0.6387 -0.0048 -0.0001 0.0103 0.004 0.241 -0.001 2.856 0.027 -0.002 -0.084 0.09 51163. 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 0.0853 0.0288 0.086 2.701 2.332 63.916 0.305 10.372 16.547 0.17 98272. 0.6889
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0.90 0.0221 0.0636 0.0839 0.0292 0.087 2.733 2.292 64.661 0.309 10.197 16.080 0.17 98330. 0.6639
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1.80 0.0442 0.1235 0.0823 0.0295 0.088 2.762 2.250 65.349 0.312 10.009 15.618 0.17 98393. 0.6388
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2.70 0.0664 0.1798 0.0807 0.0298 0.088 2.788 2.205 65.965 0.315 9.808 15.162 0.17 98461. 0.6139
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3.61 0.0885 0.2326 0.0789 0.0300 0.089 2.810 2.157 66.492 0.317 9.593 14.712 0.17 98534. 0.5891
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4.51 0.1106 0.2820 0.0770 0.0302 0.090 2.828 2.105 66.915 0.319 9.363 14.269 0.17 98613. 0.5645
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5.41 0.1327 0.3280 0.0750 0.0303 0.090 2.841 2.050 67.215 0.321 9.118 13.833 0.17 98696. 0.5400
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6.31 0.1548 0.3709 0.0728 0.0304 0.090 2.847 1.991 67.372 0.322 8.857 13.405 0.17 98786. 0.5158
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7.21 0.1770 0.4106 0.0705 0.0304 0.090 2.847 1.929 67.367 0.322 8.578 12.985 0.17 98881. 0.4917
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8.11 0.1991 0.4472 0.0681 0.0303 0.090 2.839 1.862 67.182 0.321 8.283 12.572 0.17 98982. 0.4678
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9.02 0.2212 0.4809 0.0655 0.0302 0.090 2.823 1.792 66.801 0.319 7.971 12.167 0.17 99089. 0.4441
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9.92 0.2433 0.5117 0.0628 0.0299 0.089 2.798 1.718 66.212 0.316 7.642 11.769 0.17 99202. 0.4206
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10.82 0.2654 0.5396 0.0600 0.0295 0.088 2.764 1.641 65.409 0.312 7.298 11.377 0.17 99321. 0.3973
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11.72 0.2876 0.5647 0.0571 0.0291 0.086 2.721 1.560 64.384 0.307 6.939 10.990 0.17 99447. 0.3743
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12.62 0.3097 0.5869 0.0540 0.0285 0.085 2.668 1.476 63.135 0.301 6.567 10.607 0.17 99578. 0.3514
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13.52 0.3318 0.6062 0.0508 0.0278 0.083 2.606 1.390 61.654 0.294 6.183 10.226 0.17 99717. 0.3287
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14.42 0.3539 0.6225 0.0476 0.0271 0.080 2.533 1.301 59.939 0.286 5.787 9.845 0.17 99862. 0.3062
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15.33 0.3760 0.6357 0.0442 0.0262 0.078 2.450 1.210 57.985 0.277 5.380 9.462 0.17 100013. 0.2837
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16.23 0.3982 0.6455 0.0408 0.0252 0.075 2.358 1.116 55.786 0.266 4.964 9.073 0.17 100171. 0.2613
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17.13 0.4203 0.6515 0.0373 0.0241 0.072 2.254 1.020 53.340 0.255 4.538 8.676 0.17 100336. 0.2389
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18.03 0.4424 0.6533 0.0338 0.0229 0.068 2.140 0.923 50.642 0.242 4.104 8.264 0.17 100508. 0.2165
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18.93 0.4645 0.6501 0.0301 0.0215 0.064 2.015 0.824 47.691 0.228 3.663 7.832 0.17 100686. 0.1938
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19.83 0.4866 0.6408 0.0264 0.0201 0.060 1.880 0.723 44.485 0.212 3.215 7.370 0.17 100871. 0.1708
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20.74 0.5088 0.6240 0.0227 0.0185 0.055 1.734 0.621 41.024 0.196 2.762 6.864 0.17 101064. 0.1475
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21.64 0.5309 0.5972 0.0189 0.0168 0.050 1.577 0.518 37.311 0.178 2.304 6.296 0.17 101263. 0.1235
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22.54 0.5530 0.5566 0.0152 0.0151 0.045 1.409 0.414 33.350 0.159 1.842 5.633 0.17 101469. 0.0988
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23.44 0.5751 0.4958 0.0113 0.0132 0.039 1.232 0.310 29.149 0.139 1.379 4.825 0.17 101682. 0.0732
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24.34 0.5972 0.4032 0.0075 0.0112 0.033 1.045 0.206 24.721 0.118 0.916 3.778 0.17 101902. 0.0467
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25.24 0.6194 0.2554 0.0037 0.0091 0.027 0.849 0.102 20.080 0.096 0.454 2.308 0.17 102128. 0.0201
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26.14 0.6415 -0.0053 -0.0001 0.0069 0.020 0.643 -0.002 15.204 0.073 -0.007 -0.046 0.17 102350. 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 0.0858 0.0277 0.278 5.844 5.279 207.417 0.660 23.479 11.543 0.26 147402. 0.7231
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1.36 0.0222 0.0666 0.0844 0.0281 0.282 5.918 5.190 210.037 0.669 23.085 11.208 0.26 147490. 0.6962
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2.71 0.0443 0.1292 0.0828 0.0284 0.285 5.986 5.095 212.464 0.676 22.662 10.877 0.26 147586. 0.6694
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4.07 0.0665 0.1880 0.0812 0.0287 0.288 6.047 4.993 214.643 0.683 22.208 10.551 0.26 147688. 0.6428
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5.42 0.0887 0.2431 0.0794 0.0290 0.290 6.100 4.884 216.523 0.689 21.723 10.230 0.26 147798. 0.6164
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6.78 0.1108 0.2946 0.0775 0.0292 0.292 6.143 4.767 218.043 0.694 21.204 9.916 0.26 147916. 0.5903
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8.13 0.1330 0.3425 0.0755 0.0293 0.294 6.174 4.642 219.141 0.698 20.649 9.609 0.26 148043. 0.5645
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9.49 0.1552 0.3871 0.0733 0.0294 0.295 6.191 4.509 219.749 0.699 20.058 9.308 0.26 148177. 0.5389
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10.84 0.1773 0.4284 0.0710 0.0294 0.295 6.193 4.368 219.802 0.700 19.428 9.013 0.26 148321. 0.5136
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12.20 0.1995 0.4665 0.0686 0.0293 0.294 6.177 4.218 219.233 0.698 18.760 8.726 0.26 148473. 0.4886
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13.55 0.2217 0.5017 0.0660 0.0292 0.292 6.142 4.059 217.989 0.694 18.052 8.445 0.26 148634. 0.4639
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14.91 0.2438 0.5339 0.0633 0.0289 0.290 6.086 3.891 216.029 0.688 17.308 8.170 0.26 148804. 0.4394
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16.26 0.2660 0.5632 0.0604 0.0285 0.286 6.010 3.716 213.327 0.679 16.528 7.900 0.26 148984. 0.4152
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17.62 0.2882 0.5897 0.0574 0.0281 0.281 5.913 3.533 209.860 0.668 15.715 7.636 0.26 149173. 0.3914
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18.97 0.3103 0.6135 0.0544 0.0275 0.276 5.793 3.344 205.611 0.654 14.872 7.376 0.26 149372. 0.3677
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20.33 0.3325 0.6343 0.0512 0.0268 0.269 5.651 3.148 200.562 0.638 14.001 7.118 0.26 149580. 0.3444
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21.68 0.3547 0.6523 0.0479 0.0260 0.261 5.485 2.946 194.698 0.620 13.104 6.863 0.26 149798. 0.3212
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23.04 0.3768 0.6673 0.0445 0.0251 0.252 5.297 2.739 188.000 0.598 12.182 6.608 0.26 150027. 0.2982
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24.39 0.3990 0.6791 0.0411 0.0241 0.242 5.084 2.527 180.455 0.574 11.238 6.350 0.26 150265. 0.2752
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25.75 0.4212 0.6873 0.0376 0.0230 0.231 4.847 2.310 172.046 0.548 10.274 6.089 0.26 150513. 0.2523
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27.10 0.4433 0.6916 0.0340 0.0218 0.218 4.586 2.089 162.764 0.518 9.290 5.820 0.26 150772. 0.2294
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28.46 0.4655 0.6912 0.0303 0.0204 0.205 4.299 1.864 152.597 0.486 8.290 5.540 0.26 151041. 0.2062
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29.81 0.4877 0.6851 0.0266 0.0189 0.190 3.988 1.636 141.543 0.451 7.276 5.242 0.26 151320. 0.1828
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31.17 0.5098 0.6717 0.0228 0.0173 0.174 3.651 1.405 129.601 0.413 6.248 4.916 0.26 151609. 0.1589
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32.52 0.5320 0.6487 0.0190 0.0156 0.157 3.290 1.171 116.780 0.372 5.211 4.550 0.26 151909. 0.1343
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33.88 0.5542 0.6120 0.0152 0.0138 0.138 2.905 0.937 103.098 0.328 4.166 4.120 0.26 152220. 0.1087
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35.23 0.5763 0.5543 0.0114 0.0118 0.119 2.496 0.701 88.583 0.282 3.118 3.589 0.26 152540. 0.0819
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36.59 0.5985 0.4619 0.0076 0.0098 0.098 2.065 0.465 73.278 0.233 2.069 2.879 0.26 152871. 0.0536
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37.94 0.6207 0.3038 0.0037 0.0077 0.077 1.612 0.230 57.233 0.182 1.025 1.827 0.26 153212. 0.0239
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39.30 0.6428 -0.0096 -0.0001 0.0054 0.054 1.136 -0.005 40.310 0.128 -0.022 -0.056 0.26 153540. 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 0.0865 0.0273 0.648 10.214 9.459 483.364 1.154 42.074 8.876 0.34 196527. 0.7443
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1.81 0.0222 0.0683 0.0851 0.0276 0.657 10.349 9.301 489.752 1.169 41.372 8.614 0.34 196645. 0.7163
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3.62 0.0444 0.1326 0.0835 0.0280 0.665 10.474 9.132 495.674 1.183 40.617 8.356 0.34 196772. 0.6885
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5.43 0.0666 0.1928 0.0818 0.0283 0.672 10.586 8.950 501.000 1.196 39.808 8.102 0.34 196910. 0.6609
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7.24 0.0888 0.2492 0.0801 0.0285 0.678 10.684 8.755 505.601 1.207 38.941 7.854 0.34 197058. 0.6336
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9.05 0.1110 0.3019 0.0782 0.0287 0.683 10.763 8.546 509.334 1.216 38.013 7.610 0.34 197216. 0.6066
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10.86 0.1332 0.3509 0.0761 0.0289 0.687 10.820 8.323 512.049 1.222 37.022 7.373 0.34 197385. 0.5800
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12.67 0.1554 0.3965 0.0739 0.0290 0.689 10.852 8.085 513.583 1.226 35.964 7.141 0.34 197565. 0.5536
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14.48 0.1776 0.4388 0.0716 0.0290 0.689 10.856 7.832 513.773 1.227 34.837 6.914 0.34 197757. 0.5276
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16.29 0.1998 0.4779 0.0692 0.0289 0.687 10.829 7.563 512.464 1.223 33.640 6.694 0.34 197961. 0.5019
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18.10 0.2220 0.5140 0.0666 0.0287 0.683 10.766 7.278 509.521 1.216 32.372 6.479 0.34 198177. 0.4766
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19.91 0.2442 0.5471 0.0638 0.0285 0.677 10.668 6.978 504.847 1.205 31.037 6.269 0.34 198405. 0.4515
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21.72 0.2664 0.5773 0.0609 0.0281 0.668 10.531 6.663 498.373 1.190 29.639 6.064 0.34 198646. 0.4268
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23.52 0.2886 0.6048 0.0579 0.0276 0.657 10.355 6.336 490.049 1.170 28.181 5.864 0.34 198899. 0.4025
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25.33 0.3108 0.6295 0.0548 0.0271 0.643 10.139 5.996 479.830 1.146 26.669 5.668 0.34 199165. 0.3784
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27.14 0.3330 0.6514 0.0516 0.0264 0.627 9.882 5.644 467.673 1.116 25.106 5.474 0.34 199444. 0.3546
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28.95 0.3552 0.6706 0.0483 0.0256 0.608 9.583 5.282 453.536 1.083 23.496 5.283 0.34 199736. 0.3311
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30.76 0.3774 0.6868 0.0449 0.0247 0.587 9.242 4.911 437.380 1.044 21.842 5.092 0.34 200041. 0.3077
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32.57 0.3996 0.6999 0.0414 0.0236 0.562 8.857 4.530 419.166 1.001 20.148 4.902 0.34 200360. 0.2844
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34.38 0.4218 0.7097 0.0379 0.0225 0.535 8.428 4.141 398.860 0.952 18.417 4.709 0.34 200693. 0.2612
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36.19 0.4440 0.7158 0.0342 0.0212 0.505 7.954 3.744 376.431 0.899 16.653 4.511 0.34 201038. 0.2380
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38.00 0.4662 0.7174 0.0305 0.0199 0.472 7.435 3.340 351.860 0.840 14.858 4.306 0.35 201398. 0.2146
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39.81 0.4884 0.7136 0.0268 0.0183 0.436 6.870 2.931 325.134 0.776 13.037 4.089 0.35 201772. 0.1909
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41.62 0.5106 0.7030 0.0230 0.0167 0.397 6.260 2.516 296.255 0.707 11.193 3.853 0.35 202159. 0.1666
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43.43 0.5328 0.6830 0.0192 0.0150 0.356 5.605 2.098 265.245 0.633 9.331 3.587 0.35 202560. 0.1417
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45.24 0.5550 0.6495 0.0153 0.0131 0.311 4.905 1.676 232.145 0.554 7.456 3.275 0.35 202975. 0.1156
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47.05 0.5772 0.5951 0.0115 0.0111 0.264 4.163 1.253 197.029 0.470 5.574 2.885 0.35 203404. 0.0881
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48.86 0.5994 0.5042 0.0076 0.0090 0.215 3.381 0.830 159.998 0.382 3.693 2.354 0.35 203847. 0.0585
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50.67 0.6216 0.3403 0.0037 0.0068 0.163 2.561 0.409 121.177 0.289 1.820 1.532 0.35 204302. 0.0267
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52.48 0.6438 -0.0197 -0.0001 0.0045 0.107 1.691 -0.015 80.026 0.191 -0.067 -0.086 0.35 204728. 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 0.0874 0.0272 1.261 15.890 14.931 939.976 1.795 66.412 7.205 0.43 245642. 0.7591
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2.26 0.0222 0.0693 0.0859 0.0275 1.278 16.106 14.684 952.752 1.820 65.314 6.990 0.43 245790. 0.7304
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4.53 0.0444 0.1345 0.0844 0.0279 1.294 16.306 14.418 964.595 1.842 64.132 6.780 0.43 245951. 0.7019
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6.79 0.0666 0.1956 0.0827 0.0282 1.308 16.486 14.133 975.248 1.863 62.863 6.573 0.43 246123. 0.6738
|
|
9.05 0.0888 0.2528 0.0809 0.0284 1.320 16.642 13.827 984.455 1.880 61.502 6.371 0.43 246309. 0.6459
|
|
11.31 0.1110 0.3062 0.0790 0.0287 1.330 16.768 13.499 991.931 1.894 60.046 6.173 0.43 246507. 0.6184
|
|
13.58 0.1333 0.3559 0.0770 0.0288 1.338 16.860 13.149 997.378 1.905 58.488 5.980 0.43 246720. 0.5912
|
|
15.84 0.1555 0.4022 0.0748 0.0289 1.342 16.913 12.775 1000.475 1.911 56.824 5.792 0.43 246946. 0.5644
|
|
18.10 0.1777 0.4451 0.0724 0.0289 1.342 16.920 12.377 1000.899 1.912 55.051 5.609 0.43 247187. 0.5380
|
|
20.37 0.1999 0.4849 0.0700 0.0288 1.339 16.876 11.953 998.335 1.907 53.166 5.430 0.43 247443. 0.5119
|
|
22.63 0.2221 0.5215 0.0673 0.0287 1.331 16.778 11.504 992.519 1.896 51.169 5.257 0.43 247714. 0.4862
|
|
24.89 0.2443 0.5553 0.0646 0.0284 1.319 16.621 11.031 983.253 1.878 49.065 5.088 0.43 248000. 0.4608
|
|
27.16 0.2665 0.5862 0.0617 0.0280 1.301 16.404 10.535 970.402 1.853 46.860 4.924 0.43 248302. 0.4358
|
|
29.42 0.2887 0.6144 0.0586 0.0276 1.279 16.125 10.018 953.863 1.822 44.561 4.764 0.43 248619. 0.4111
|
|
31.68 0.3109 0.6398 0.0555 0.0270 1.252 15.781 9.482 933.546 1.783 42.174 4.607 0.43 248953. 0.3868
|
|
33.94 0.3331 0.6626 0.0522 0.0263 1.219 15.372 8.927 909.369 1.737 39.707 4.453 0.43 249302. 0.3627
|
|
36.21 0.3553 0.6826 0.0489 0.0255 1.182 14.897 8.355 881.249 1.683 37.165 4.300 0.43 249668. 0.3389
|
|
38.47 0.3776 0.6998 0.0455 0.0245 1.139 14.354 7.768 849.110 1.622 34.554 4.150 0.43 250051. 0.3154
|
|
40.73 0.3998 0.7141 0.0419 0.0235 1.090 13.741 7.167 812.867 1.552 31.879 3.999 0.43 250450. 0.2919
|
|
43.00 0.4220 0.7252 0.0383 0.0223 1.036 13.058 6.552 772.460 1.475 29.145 3.847 0.43 250866. 0.2685
|
|
45.26 0.4442 0.7327 0.0347 0.0210 0.976 12.304 5.926 727.828 1.390 26.357 3.693 0.43 251299. 0.2451
|
|
47.52 0.4664 0.7360 0.0309 0.0196 0.910 11.477 5.288 678.927 1.297 23.522 3.533 0.43 251750. 0.2215
|
|
49.78 0.4886 0.7342 0.0272 0.0181 0.839 10.578 4.641 625.736 1.195 20.643 3.364 0.43 252217. 0.1976
|
|
52.05 0.5108 0.7259 0.0233 0.0164 0.762 9.606 3.986 568.258 1.085 17.729 3.181 0.43 252702. 0.1732
|
|
54.31 0.5330 0.7087 0.0195 0.0146 0.679 8.563 3.324 506.535 0.967 14.786 2.977 0.43 253204. 0.1480
|
|
56.57 0.5552 0.6785 0.0156 0.0127 0.591 7.449 2.658 440.652 0.842 11.822 2.736 0.43 253724. 0.1216
|
|
58.84 0.5774 0.6277 0.0116 0.0107 0.497 6.267 1.989 370.750 0.708 8.848 2.434 0.43 254261. 0.0936
|
|
61.10 0.5996 0.5402 0.0077 0.0086 0.398 5.021 1.321 297.038 0.567 5.874 2.017 0.43 254815. 0.0632
|
|
63.36 0.6219 0.3754 0.0038 0.0063 0.295 3.715 0.655 219.765 0.420 2.913 1.352 0.44 255384. 0.0298
|
|
65.63 0.6441 -0.0164 -0.0001 0.0040 0.185 2.328 -0.017 137.708 0.263 -0.077 -0.057 0.44 255910. 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 0.0885 0.0273 2.189 22.994 21.776 1632.249 2.598 96.860 6.051 0.51 294745. 0.7699
|
|
2.71 0.0222 0.0698 0.0871 0.0277 2.219 23.312 21.421 1654.843 2.634 95.279 5.871 0.51 294924. 0.7409
|
|
5.42 0.0444 0.1354 0.0855 0.0280 2.247 23.607 21.037 1675.774 2.667 93.575 5.694 0.51 295117. 0.7121
|
|
8.14 0.0666 0.1969 0.0838 0.0283 2.272 23.872 20.626 1694.593 2.697 91.744 5.521 0.51 295325. 0.6836
|
|
10.85 0.0887 0.2545 0.0820 0.0286 2.294 24.101 20.184 1710.846 2.723 89.778 5.351 0.51 295548. 0.6555
|
|
13.56 0.1109 0.3083 0.0801 0.0288 2.312 24.287 19.710 1724.043 2.744 87.672 5.186 0.51 295787. 0.6277
|
|
16.27 0.1331 0.3585 0.0781 0.0290 2.325 24.422 19.204 1733.655 2.759 85.417 5.024 0.51 296043. 0.6003
|
|
18.99 0.1553 0.4051 0.0758 0.0291 2.332 24.499 18.662 1739.127 2.768 83.008 4.867 0.51 296316. 0.5733
|
|
21.70 0.1775 0.4485 0.0735 0.0291 2.333 24.510 18.084 1739.889 2.769 80.438 4.714 0.51 296605. 0.5466
|
|
24.41 0.1997 0.4886 0.0710 0.0290 2.327 24.447 17.469 1735.394 2.762 77.703 4.566 0.51 296913. 0.5203
|
|
27.12 0.2218 0.5258 0.0684 0.0288 2.313 24.303 16.818 1725.166 2.746 74.805 4.422 0.51 297239. 0.4944
|
|
29.84 0.2440 0.5600 0.0656 0.0286 2.292 24.073 16.130 1708.858 2.720 71.748 4.281 0.51 297583. 0.4689
|
|
32.55 0.2662 0.5915 0.0626 0.0282 2.261 23.754 15.410 1686.230 2.684 68.543 4.145 0.51 297945. 0.4437
|
|
35.26 0.2884 0.6202 0.0596 0.0277 2.222 23.344 14.658 1657.106 2.637 65.200 4.012 0.51 298327. 0.4188
|
|
37.97 0.3106 0.6463 0.0564 0.0271 2.174 22.840 13.878 1621.329 2.580 61.728 3.882 0.51 298727. 0.3943
|
|
40.69 0.3328 0.6698 0.0531 0.0264 2.117 22.240 13.070 1578.759 2.513 58.137 3.755 0.52 299147. 0.3702
|
|
43.40 0.3549 0.6906 0.0497 0.0256 2.051 21.543 12.238 1529.253 2.434 54.436 3.630 0.52 299587. 0.3462
|
|
46.11 0.3771 0.7087 0.0463 0.0246 1.975 20.746 11.383 1472.676 2.344 50.633 3.506 0.52 300046. 0.3225
|
|
48.82 0.3993 0.7240 0.0427 0.0236 1.889 19.847 10.507 1408.896 2.242 46.736 3.383 0.52 300525. 0.2990
|
|
51.54 0.4215 0.7362 0.0391 0.0224 1.794 18.846 9.611 1337.793 2.129 42.752 3.259 0.52 301024. 0.2755
|
|
54.25 0.4437 0.7451 0.0354 0.0211 1.689 17.739 8.698 1259.266 2.004 38.689 3.133 0.52 301544. 0.2519
|
|
56.96 0.4659 0.7500 0.0316 0.0196 1.573 16.527 7.769 1173.238 1.867 34.555 3.003 0.52 302084. 0.2282
|
|
59.67 0.4880 0.7501 0.0277 0.0180 1.448 15.209 6.825 1079.669 1.718 30.358 2.867 0.52 302644. 0.2042
|
|
62.39 0.5102 0.7441 0.0239 0.0164 1.312 13.785 5.869 978.564 1.557 26.107 2.721 0.52 303225. 0.1797
|
|
65.10 0.5324 0.7297 0.0199 0.0145 1.167 12.256 4.904 869.993 1.385 21.813 2.557 0.52 303827. 0.1544
|
|
67.81 0.5546 0.7030 0.0160 0.0126 1.011 10.623 3.932 754.102 1.200 17.488 2.365 0.52 304450. 0.1278
|
|
70.52 0.5768 0.6566 0.0120 0.0106 0.846 8.891 2.955 631.136 1.004 13.145 2.124 0.52 305093. 0.0996
|
|
73.24 0.5990 0.5747 0.0080 0.0084 0.672 7.064 1.979 501.457 0.798 8.802 1.790 0.52 305756. 0.0687
|
|
75.95 0.6211 0.4158 0.0041 0.0061 0.490 5.149 1.006 365.508 0.582 4.476 1.249 0.52 306438. 0.0342
|
|
78.66 0.6433 0.0205 0.0001 0.0037 0.298 3.126 0.029 221.910 0.353 0.129 0.060 0.52 307088. 0.0003
|
|
|
|
|
|
|
|
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 0.0899 0.0276 3.521 31.704 30.109 2625.674 3.582 133.924 5.201 0.60 343831. 0.7782
|
|
3.17 0.0222 0.0702 0.0885 0.0280 3.571 32.151 29.624 2662.658 3.632 131.768 5.046 0.60 344041. 0.7489
|
|
6.34 0.0445 0.1361 0.0869 0.0284 3.617 32.564 29.101 2696.872 3.679 129.439 4.894 0.60 344269. 0.7199
|
|
9.52 0.0667 0.1979 0.0852 0.0287 3.658 32.935 28.537 2727.578 3.721 126.932 4.745 0.60 344514. 0.6912
|
|
12.69 0.0889 0.2558 0.0834 0.0290 3.693 33.254 27.931 2754.033 3.757 124.236 4.600 0.60 344776. 0.6629
|
|
15.86 0.1112 0.3099 0.0815 0.0292 3.722 33.512 27.280 2775.434 3.786 121.341 4.458 0.60 345058. 0.6349
|
|
19.03 0.1334 0.3604 0.0794 0.0294 3.743 33.699 26.583 2790.918 3.807 118.239 4.320 0.60 345359. 0.6073
|
|
22.20 0.1556 0.4074 0.0771 0.0295 3.754 33.804 25.836 2799.589 3.819 114.919 4.186 0.60 345680. 0.5801
|
|
25.37 0.1779 0.4511 0.0748 0.0295 3.756 33.815 25.039 2800.515 3.820 111.374 4.055 0.60 346021. 0.5533
|
|
28.55 0.2001 0.4916 0.0722 0.0294 3.745 33.722 24.190 2792.801 3.810 107.597 3.929 0.60 346383. 0.5268
|
|
31.72 0.2223 0.5292 0.0695 0.0292 3.722 33.515 23.289 2775.675 3.787 103.590 3.806 0.60 346767. 0.5008
|
|
34.89 0.2446 0.5638 0.0667 0.0289 3.686 33.188 22.338 2748.564 3.750 99.360 3.686 0.60 347171. 0.4750
|
|
38.06 0.2668 0.5957 0.0637 0.0285 3.636 32.735 21.340 2711.086 3.698 94.922 3.570 0.60 347598. 0.4497
|
|
41.23 0.2890 0.6250 0.0606 0.0280 3.571 32.154 20.299 2662.958 3.633 90.288 3.457 0.60 348046. 0.4247
|
|
44.40 0.3113 0.6516 0.0574 0.0274 3.492 31.442 19.216 2603.943 3.552 85.475 3.347 0.60 348517. 0.4001
|
|
47.58 0.3335 0.6756 0.0540 0.0267 3.398 30.595 18.097 2533.818 3.457 80.494 3.239 0.60 349010. 0.3757
|
|
50.75 0.3557 0.6971 0.0506 0.0258 3.289 29.611 16.942 2452.359 3.345 75.358 3.133 0.60 349526. 0.3517
|
|
53.92 0.3780 0.7160 0.0470 0.0248 3.164 28.488 15.755 2359.354 3.219 70.080 3.029 0.60 350066. 0.3278
|
|
57.09 0.4002 0.7320 0.0434 0.0237 3.023 27.223 14.539 2254.590 3.076 64.669 2.925 0.60 350628. 0.3041
|
|
60.26 0.4225 0.7452 0.0397 0.0225 2.867 25.814 13.295 2137.883 2.916 59.136 2.821 0.60 351214. 0.2804
|
|
63.43 0.4447 0.7550 0.0359 0.0212 2.694 24.259 12.026 2009.067 2.741 53.492 2.715 0.60 351824. 0.2567
|
|
66.61 0.4669 0.7611 0.0321 0.0197 2.505 22.556 10.735 1868.021 2.548 47.748 2.606 0.60 352457. 0.2329
|
|
69.78 0.4892 0.7625 0.0281 0.0181 2.299 20.704 9.423 1714.685 2.339 41.915 2.493 0.60 353115. 0.2086
|
|
72.95 0.5114 0.7580 0.0242 0.0163 2.077 18.704 8.095 1549.071 2.113 36.007 2.370 0.61 353796. 0.1839
|
|
76.12 0.5336 0.7454 0.0202 0.0144 1.839 16.558 6.753 1371.292 1.871 30.037 2.234 0.61 354502. 0.1583
|
|
79.29 0.5559 0.7206 0.0161 0.0124 1.585 14.267 5.401 1181.598 1.612 24.022 2.073 0.61 355232. 0.1314
|
|
82.46 0.5781 0.6762 0.0121 0.0103 1.315 11.838 4.043 980.396 1.337 17.983 1.870 0.61 355986. 0.1025
|
|
85.64 0.6003 0.5951 0.0080 0.0081 1.030 9.277 2.685 768.291 1.048 11.943 1.585 0.61 356763. 0.0708
|
|
88.81 0.6226 0.4309 0.0040 0.0057 0.732 6.593 1.332 546.011 0.745 5.926 1.107 0.61 357562. 0.0348
|
|
91.98 0.6448 -0.0263 -0.0001 0.0032 0.413 3.721 -0.044 308.169 0.420 -0.197 -0.065 0.61 358257. 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 0.0917 0.0282 5.370 42.306 40.088 4004.245 4.780 178.313 4.541 0.68 392894. 0.7839
|
|
3.63 0.0223 0.0701 0.0902 0.0286 5.446 42.904 39.457 4060.830 4.847 175.505 4.407 0.68 393136. 0.7548
|
|
7.26 0.0445 0.1360 0.0886 0.0290 5.516 43.457 38.773 4113.211 4.910 172.463 4.276 0.68 393399. 0.7259
|
|
10.88 0.0668 0.1978 0.0870 0.0293 5.579 43.954 38.035 4160.225 4.966 169.178 4.147 0.68 393681. 0.6973
|
|
14.51 0.0890 0.2558 0.0851 0.0296 5.633 44.382 37.238 4200.687 5.014 165.636 4.021 0.68 393984. 0.6690
|
|
18.14 0.1113 0.3100 0.0832 0.0299 5.677 44.727 36.382 4233.342 5.053 161.827 3.898 0.68 394309. 0.6411
|
|
21.77 0.1335 0.3606 0.0811 0.0300 5.709 44.975 35.462 4256.831 5.081 157.735 3.779 0.68 394656. 0.6135
|
|
25.39 0.1558 0.4077 0.0788 0.0301 5.726 45.111 34.476 4269.756 5.097 153.348 3.662 0.68 395026. 0.5863
|
|
29.02 0.1780 0.4516 0.0764 0.0301 5.727 45.121 33.421 4270.666 5.098 148.656 3.549 0.68 395419. 0.5595
|
|
32.65 0.2003 0.4924 0.0738 0.0300 5.710 44.989 32.296 4258.188 5.083 143.651 3.440 0.68 395836. 0.5330
|
|
36.28 0.2225 0.5302 0.0711 0.0298 5.674 44.703 31.100 4231.131 5.051 138.332 3.334 0.68 396277. 0.5069
|
|
39.91 0.2448 0.5652 0.0682 0.0295 5.617 44.254 29.836 4188.618 5.000 132.712 3.231 0.68 396743. 0.4812
|
|
43.53 0.2670 0.5975 0.0652 0.0291 5.539 43.635 28.509 4130.067 4.930 126.807 3.131 0.69 397234. 0.4558
|
|
47.16 0.2893 0.6272 0.0620 0.0286 5.438 42.843 27.122 4055.069 4.840 120.638 3.034 0.69 397749. 0.4308
|
|
50.79 0.3115 0.6544 0.0587 0.0280 5.315 41.873 25.680 3963.283 4.731 114.224 2.939 0.69 398291. 0.4061
|
|
54.42 0.3338 0.6790 0.0553 0.0272 5.169 40.723 24.187 3854.391 4.601 107.584 2.846 0.69 398858. 0.3817
|
|
58.04 0.3560 0.7011 0.0518 0.0263 4.999 39.388 22.647 3728.073 4.450 100.733 2.755 0.69 399451. 0.3575
|
|
61.67 0.3783 0.7207 0.0482 0.0253 4.806 37.866 21.063 3584.015 4.278 93.689 2.666 0.69 400070. 0.3336
|
|
65.30 0.4005 0.7376 0.0444 0.0241 4.589 36.153 19.439 3421.898 4.085 86.465 2.577 0.69 400716. 0.3098
|
|
68.93 0.4228 0.7517 0.0406 0.0229 4.347 34.247 17.778 3241.463 3.869 79.075 2.488 0.69 401388. 0.2860
|
|
72.55 0.4450 0.7626 0.0368 0.0215 4.080 32.144 16.082 3042.458 3.632 71.534 2.398 0.69 402088. 0.2622
|
|
76.18 0.4673 0.7699 0.0328 0.0199 3.788 29.844 14.356 2824.714 3.372 63.856 2.305 0.69 402814. 0.2381
|
|
79.81 0.4895 0.7728 0.0288 0.0183 3.471 27.344 12.603 2588.134 3.089 56.056 2.209 0.69 403568. 0.2138
|
|
83.44 0.5118 0.7699 0.0247 0.0165 3.128 24.646 10.826 2332.732 2.784 48.152 2.105 0.69 404349. 0.1888
|
|
87.07 0.5341 0.7593 0.0206 0.0145 2.761 21.751 9.029 2058.700 2.457 40.163 1.989 0.69 405158. 0.1630
|
|
90.69 0.5563 0.7370 0.0165 0.0125 2.369 18.663 7.219 1766.436 2.109 32.111 1.854 0.69 405994. 0.1358
|
|
94.32 0.5786 0.6954 0.0123 0.0103 1.953 15.390 5.401 1456.616 1.739 24.024 1.682 0.69 406858. 0.1066
|
|
97.95 0.6008 0.6172 0.0082 0.0080 1.516 11.941 3.582 1130.249 1.349 15.932 1.437 0.70 407748. 0.0742
|
|
101.58 0.6231 0.4531 0.0040 0.0056 1.058 8.332 1.769 788.586 0.941 7.869 1.018 0.70 408663. 0.0369
|
|
105.20 0.6453 -0.0528 -0.0002 0.0029 0.560 4.410 -0.105 417.373 0.498 -0.468 -0.114 0.70 409342. 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 0.0938 0.0298 8.064 56.472 51.927 6013.125 6.380 230.971 3.917 0.77 441925. 0.7696
|
|
4.10 0.0223 0.0685 0.0924 0.0301 8.153 57.098 51.135 6079.819 6.451 227.449 3.815 0.77 442201. 0.7438
|
|
8.19 0.0447 0.1333 0.0908 0.0304 8.235 57.670 50.273 6140.693 6.515 223.613 3.713 0.77 442500. 0.7179
|
|
12.29 0.0670 0.1946 0.0891 0.0307 8.307 58.173 49.337 6194.258 6.572 219.451 3.613 0.77 442822. 0.6919
|
|
16.38 0.0893 0.2523 0.0873 0.0309 8.367 58.593 48.324 6238.983 6.620 214.946 3.513 0.77 443167. 0.6659
|
|
20.48 0.1117 0.3066 0.0853 0.0311 8.413 58.914 47.230 6273.204 6.656 210.080 3.415 0.77 443538. 0.6399
|
|
24.57 0.1340 0.3575 0.0832 0.0312 8.442 59.120 46.051 6295.088 6.679 204.837 3.318 0.77 443934. 0.6140
|
|
28.67 0.1563 0.4051 0.0809 0.0312 8.452 59.191 44.784 6302.650 6.687 199.199 3.223 0.77 444356. 0.5881
|
|
32.77 0.1787 0.4495 0.0784 0.0312 8.440 59.107 43.424 6293.773 6.678 193.151 3.129 0.77 444805. 0.5623
|
|
36.86 0.2010 0.4909 0.0758 0.0310 8.403 58.850 41.970 6266.395 6.649 186.684 3.038 0.77 445280. 0.5366
|
|
40.96 0.2233 0.5294 0.0730 0.0308 8.339 58.402 40.422 6218.653 6.598 179.797 2.948 0.77 445783. 0.5111
|
|
45.05 0.2456 0.5650 0.0701 0.0305 8.246 57.749 38.783 6149.107 6.524 172.506 2.861 0.77 446314. 0.4858
|
|
49.15 0.2680 0.5979 0.0669 0.0300 8.122 56.881 37.058 6056.748 6.426 164.834 2.775 0.77 446873. 0.4606
|
|
53.24 0.2903 0.6283 0.0637 0.0294 7.967 55.792 35.254 5940.813 6.303 156.808 2.692 0.77 447461. 0.4357
|
|
57.34 0.3126 0.6560 0.0603 0.0287 7.779 54.476 33.376 5800.636 6.155 148.455 2.610 0.77 448077. 0.4111
|
|
61.44 0.3350 0.6813 0.0568 0.0279 7.557 52.926 31.430 5635.596 5.980 139.801 2.530 0.77 448722. 0.3867
|
|
65.53 0.3573 0.7041 0.0531 0.0270 7.302 51.137 29.422 5445.102 5.777 130.867 2.451 0.77 449397. 0.3625
|
|
69.63 0.3796 0.7243 0.0494 0.0259 7.012 49.103 27.355 5228.563 5.548 121.675 2.373 0.77 450101. 0.3384
|
|
73.72 0.4020 0.7420 0.0456 0.0247 6.686 46.821 25.234 4985.488 5.290 112.243 2.296 0.77 450835. 0.3145
|
|
77.82 0.4243 0.7568 0.0417 0.0234 6.324 44.285 23.064 4715.493 5.003 102.590 2.218 0.78 451599. 0.2905
|
|
81.91 0.4466 0.7686 0.0377 0.0219 5.925 41.494 20.848 4418.349 4.688 92.734 2.140 0.78 452393. 0.2665
|
|
86.01 0.4690 0.7766 0.0336 0.0203 5.490 38.448 18.591 4094.012 4.344 82.694 2.060 0.78 453218. 0.2422
|
|
90.11 0.4913 0.7802 0.0294 0.0185 5.019 35.149 16.297 3742.659 3.971 72.491 1.975 0.78 454073. 0.2174
|
|
94.20 0.5136 0.7778 0.0252 0.0167 4.512 31.599 13.972 3364.734 3.570 62.145 1.883 0.78 454960. 0.1919
|
|
98.30 0.5360 0.7670 0.0210 0.0147 3.971 27.808 11.619 2961.052 3.142 51.683 1.780 0.78 455877. 0.1654
|
|
102.39 0.5583 0.7434 0.0167 0.0125 3.397 23.787 9.248 2532.884 2.687 41.134 1.656 0.78 456825. 0.1373
|
|
106.49 0.5806 0.6981 0.0124 0.0103 2.792 19.553 6.864 2082.052 2.209 30.533 1.495 0.78 457804. 0.1068
|
|
110.58 0.6029 0.6113 0.0081 0.0080 2.160 15.129 4.478 1610.987 1.709 19.919 1.261 0.78 458813. 0.0728
|
|
114.68 0.6253 0.4264 0.0038 0.0056 1.505 10.542 2.099 1122.522 1.191 9.337 0.848 0.78 459848. 0.0335
|
|
118.78 0.6476
|
|
|
|
|
|
|
|
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 0.0963 0.0348 12.941 81.563 65.829 9649.817 9.215 292.809 3.094 0.85 490913. 0.6845
|
|
4.54 0.0223 0.0605 0.0949 0.0350 12.980 81.813 64.888 9679.440 9.243 288.624 3.041 0.85 491221. 0.6678
|
|
9.07 0.0445 0.1188 0.0934 0.0350 13.005 81.965 63.856 9697.473 9.260 284.030 2.987 0.85 491554. 0.6507
|
|
13.61 0.0668 0.1750 0.0918 0.0350 13.011 82.009 62.727 9702.643 9.265 279.009 2.932 0.85 491914. 0.6332
|
|
18.15 0.0890 0.2289 0.0900 0.0350 12.999 81.933 61.497 9693.650 9.257 273.539 2.877 0.85 492300. 0.6153
|
|
22.68 0.1113 0.2806 0.0880 0.0349 12.966 81.725 60.161 9668.998 9.233 267.596 2.822 0.85 492714. 0.5968
|
|
27.22 0.1336 0.3301 0.0859 0.0348 12.910 81.369 58.713 9626.939 9.193 261.157 2.766 0.85 493157. 0.5779
|
|
31.76 0.1558 0.3773 0.0836 0.0345 12.828 80.851 57.149 9565.581 9.134 254.200 2.710 0.85 493629. 0.5586
|
|
36.29 0.1781 0.4221 0.0812 0.0342 12.717 80.151 55.464 9482.855 9.055 246.706 2.653 0.85 494131. 0.5387
|
|
40.83 0.2004 0.4646 0.0785 0.0339 12.574 79.254 53.656 9376.715 8.954 238.661 2.595 0.86 494663. 0.5184
|
|
45.37 0.2226 0.5047 0.0757 0.0334 12.398 78.144 51.723 9245.307 8.829 230.065 2.538 0.86 495225. 0.4976
|
|
49.90 0.2449 0.5424 0.0727 0.0328 12.186 76.807 49.670 9087.216 8.678 220.934 2.479 0.86 495818. 0.4764
|
|
54.44 0.2671 0.5777 0.0695 0.0321 11.937 75.238 47.504 8901.521 8.500 211.299 2.421 0.86 496442. 0.4549
|
|
58.98 0.2894 0.6106 0.0662 0.0314 11.650 73.430 45.233 8687.583 8.296 201.196 2.362 0.86 497097. 0.4331
|
|
63.51 0.3117 0.6410 0.0627 0.0305 11.325 71.377 42.864 8444.727 8.064 190.661 2.302 0.86 497784. 0.4110
|
|
68.05 0.3339 0.6690 0.0591 0.0295 10.959 69.074 40.406 8172.213 7.804 179.728 2.243 0.86 498502. 0.3887
|
|
72.59 0.3562 0.6945 0.0554 0.0284 10.553 66.512 37.866 7869.165 7.514 168.427 2.183 0.86 499253. 0.3662
|
|
77.12 0.3785 0.7171 0.0516 0.0272 10.109 63.713 35.248 7538.023 7.198 156.784 2.121 0.86 500036. 0.3433
|
|
81.66 0.4007 0.7367 0.0476 0.0259 9.623 60.655 32.560 7176.206 6.853 144.825 2.058 0.86 500852. 0.3202
|
|
86.20 0.4230 0.7530 0.0436 0.0245 9.098 57.342 29.805 6784.230 6.478 132.575 1.993 0.86 501701. 0.2966
|
|
90.73 0.4452 0.7650 0.0395 0.0230 8.536 53.801 26.990 6365.350 6.078 120.054 1.923 0.86 502583. 0.2724
|
|
95.27 0.4675 0.7713 0.0353 0.0214 7.944 50.067 24.119 5923.502 5.657 107.281 1.847 0.86 503498. 0.2473
|
|
99.81 0.4898 0.7718 0.0310 0.0197 7.309 46.070 21.198 5450.594 5.205 94.288 1.764 0.86 504446. 0.2214
|
|
104.34 0.5120 0.7644 0.0267 0.0179 6.637 41.831 18.233 4949.086 4.726 81.102 1.671 0.86 505428. 0.1946
|
|
108.88 0.5343 0.7459 0.0223 0.0160 5.929 37.372 15.232 4421.521 4.222 67.753 1.563 0.87 506444. 0.1663
|
|
113.42 0.5566 0.7109 0.0179 0.0140 5.192 32.722 12.203 3871.383 3.697 54.280 1.430 0.87 507494. 0.1362
|
|
117.95 0.5788 0.6502 0.0134 0.0119 4.429 27.917 9.156 3302.904 3.154 40.728 1.257 0.87 508577. 0.1037
|
|
122.49 0.6011 0.5463 0.0089 0.0098 3.649 23.000 6.103 2721.124 2.598 27.148 1.017 0.87 509694. 0.0685
|
|
127.03 0.6233 0.3623 0.0045 0.0077 2.858 18.015 3.057 2131.344 2.035 13.599 0.651 0.87 510841. 0.0310
|
|
131.56 0.6456 -0.0028 0.0000 0.0055 2.041 12.864 -0.016 1521.955 1.453 -0.072 -0.005 0.87 511914. 0.0000
|
|
|
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