390 lines
69 KiB
Plaintext
390 lines
69 KiB
Plaintext
20x10PN (20x10PN.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 0.0897 0.0352 0.009 0.571 0.457 6.754 0.064 2.035 30.719 0.08 43830. 0.6096
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0.43 0.0229 0.0569 0.0882 0.0355 0.009 0.577 0.450 6.821 0.065 2.001 29.917 0.08 43858. 0.5887
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0.87 0.0458 0.1107 0.0866 0.0358 0.009 0.582 0.442 6.883 0.066 1.965 29.115 0.08 43887. 0.5678
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1.30 0.0687 0.1615 0.0849 0.0361 0.009 0.586 0.433 6.938 0.066 1.927 28.316 0.08 43920. 0.5467
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1.73 0.0916 0.2093 0.0831 0.0364 0.009 0.590 0.424 6.984 0.067 1.885 27.523 0.08 43954. 0.5257
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2.17 0.1145 0.2542 0.0812 0.0366 0.009 0.593 0.414 7.021 0.067 1.841 26.736 0.08 43991. 0.5046
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2.60 0.1374 0.2961 0.0791 0.0367 0.009 0.595 0.403 7.045 0.067 1.793 25.955 0.08 44031. 0.4835
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3.04 0.1603 0.3351 0.0768 0.0367 0.009 0.596 0.392 7.057 0.067 1.743 25.181 0.08 44073. 0.4624
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3.47 0.1832 0.3713 0.0745 0.0367 0.009 0.596 0.380 7.053 0.067 1.689 24.414 0.08 44119. 0.4413
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3.90 0.2061 0.4047 0.0719 0.0366 0.009 0.594 0.367 7.032 0.067 1.631 23.654 0.08 44167. 0.4203
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4.34 0.2290 0.4354 0.0692 0.0364 0.009 0.591 0.353 6.993 0.067 1.570 22.900 0.08 44217. 0.3992
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4.77 0.2519 0.4633 0.0664 0.0361 0.009 0.586 0.339 6.934 0.066 1.506 22.151 0.08 44271. 0.3782
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5.20 0.2748 0.4884 0.0634 0.0357 0.009 0.579 0.324 6.855 0.065 1.439 21.405 0.08 44328. 0.3572
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5.64 0.2977 0.5106 0.0603 0.0352 0.009 0.571 0.308 6.755 0.065 1.369 20.661 0.08 44388. 0.3362
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6.07 0.3206 0.5301 0.0571 0.0346 0.009 0.561 0.291 6.635 0.063 1.296 19.914 0.08 44450. 0.3153
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6.51 0.3435 0.5465 0.0538 0.0338 0.009 0.549 0.274 6.494 0.062 1.220 19.163 0.08 44516. 0.2945
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6.94 0.3664 0.5598 0.0504 0.0330 0.008 0.535 0.257 6.331 0.060 1.143 18.403 0.08 44585. 0.2736
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7.37 0.3893 0.5698 0.0468 0.0320 0.008 0.519 0.239 6.146 0.059 1.063 17.629 0.08 44658. 0.2528
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7.81 0.4122 0.5761 0.0432 0.0309 0.008 0.502 0.220 5.940 0.057 0.981 16.835 0.08 44733. 0.2319
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8.24 0.4351 0.5785 0.0395 0.0297 0.008 0.483 0.202 5.711 0.055 0.897 16.013 0.08 44811. 0.2110
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8.67 0.4580 0.5762 0.0358 0.0284 0.007 0.461 0.182 5.460 0.052 0.811 15.154 0.08 44893. 0.1899
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9.11 0.4809 0.5687 0.0319 0.0270 0.007 0.438 0.163 5.186 0.050 0.724 14.244 0.08 44978. 0.1686
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9.54 0.5038 0.5548 0.0280 0.0255 0.007 0.413 0.143 4.889 0.047 0.636 13.265 0.08 45066. 0.1472
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9.97 0.5267 0.5332 0.0241 0.0238 0.006 0.386 0.123 4.570 0.044 0.547 12.195 0.08 45158. 0.1254
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10.41 0.5496 0.5019 0.0201 0.0220 0.006 0.357 0.103 4.229 0.040 0.456 10.999 0.08 45253. 0.1033
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10.84 0.5725 0.4576 0.0161 0.0201 0.005 0.327 0.082 3.866 0.037 0.365 9.628 0.08 45351. 0.0809
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11.28 0.5953 0.3959 0.0121 0.0181 0.005 0.294 0.061 3.481 0.033 0.273 8.009 0.08 45452. 0.0583
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11.71 0.6182 0.3093 0.0080 0.0160 0.004 0.260 0.041 3.076 0.029 0.182 6.024 0.08 45557. 0.0357
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12.14 0.6411 0.1848 0.0040 0.0138 0.004 0.224 0.020 2.652 0.025 0.090 3.472 0.08 45664. 0.0145
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12.58 0.6640 -0.0023 0.0000 0.0115 0.003 0.187 0.000 2.209 0.021 -0.001 -0.042 0.08 45772. 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 0.0902 0.0318 0.065 2.063 1.839 48.814 0.233 8.180 17.087 0.16 87659. 0.6798
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0.87 0.0230 0.0634 0.0887 0.0322 0.066 2.088 1.809 49.407 0.236 8.046 16.606 0.16 87714. 0.6553
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1.74 0.0460 0.1232 0.0871 0.0325 0.067 2.111 1.777 49.958 0.239 7.902 16.129 0.16 87774. 0.6307
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2.61 0.0690 0.1794 0.0854 0.0328 0.068 2.132 1.742 50.453 0.241 7.747 15.658 0.16 87839. 0.6063
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3.48 0.0920 0.2321 0.0836 0.0331 0.068 2.150 1.704 50.880 0.243 7.581 15.193 0.16 87908. 0.5819
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4.36 0.1150 0.2814 0.0816 0.0333 0.069 2.165 1.664 51.227 0.245 7.403 14.736 0.16 87983. 0.5577
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5.23 0.1380 0.3274 0.0795 0.0335 0.069 2.176 1.621 51.480 0.246 7.212 14.286 0.16 88063. 0.5337
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6.10 0.1610 0.3701 0.0773 0.0336 0.069 2.182 1.576 51.622 0.246 7.009 13.845 0.16 88148. 0.5099
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6.97 0.1840 0.4098 0.0749 0.0336 0.069 2.182 1.527 51.640 0.247 6.792 13.411 0.16 88239. 0.4862
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7.84 0.2070 0.4464 0.0723 0.0335 0.069 2.177 1.475 51.518 0.246 6.561 12.986 0.16 88336. 0.4627
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8.71 0.2300 0.4800 0.0696 0.0334 0.069 2.166 1.420 51.244 0.245 6.316 12.568 0.16 88439. 0.4394
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9.58 0.2530 0.5108 0.0668 0.0331 0.068 2.147 1.362 50.808 0.243 6.057 12.157 0.16 88547. 0.4162
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10.45 0.2760 0.5387 0.0638 0.0327 0.067 2.122 1.301 50.203 0.240 5.786 11.753 0.16 88661. 0.3933
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11.33 0.2990 0.5637 0.0607 0.0322 0.066 2.089 1.237 49.426 0.236 5.503 11.354 0.16 88782. 0.3705
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12.20 0.3220 0.5860 0.0574 0.0316 0.065 2.049 1.171 48.474 0.231 5.210 10.959 0.16 88908. 0.3480
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13.07 0.3450 0.6053 0.0541 0.0308 0.063 2.001 1.103 47.343 0.226 4.906 10.566 0.16 89041. 0.3256
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13.94 0.3680 0.6217 0.0506 0.0300 0.062 1.945 1.032 46.031 0.220 4.592 10.173 0.16 89180. 0.3033
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14.81 0.3910 0.6349 0.0471 0.0290 0.060 1.882 0.960 44.534 0.213 4.270 9.778 0.16 89326. 0.2811
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15.68 0.4140 0.6447 0.0434 0.0279 0.057 1.811 0.886 42.850 0.205 3.941 9.378 0.16 89478. 0.2590
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16.55 0.4370 0.6508 0.0397 0.0267 0.055 1.732 0.810 40.976 0.196 3.604 8.968 0.16 89636. 0.2368
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17.42 0.4600 0.6526 0.0359 0.0253 0.052 1.644 0.733 38.910 0.186 3.260 8.543 0.16 89801. 0.2146
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18.30 0.4830 0.6494 0.0321 0.0239 0.049 1.549 0.654 36.650 0.175 2.910 8.097 0.16 89972. 0.1921
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19.17 0.5060 0.6402 0.0282 0.0223 0.046 1.445 0.574 34.196 0.163 2.555 7.620 0.16 90150. 0.1694
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20.04 0.5290 0.6235 0.0242 0.0205 0.042 1.333 0.494 31.547 0.151 2.196 7.098 0.16 90335. 0.1463
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20.91 0.5520 0.5968 0.0202 0.0187 0.038 1.213 0.412 28.707 0.137 1.833 6.510 0.16 90526. 0.1226
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21.78 0.5750 0.5563 0.0162 0.0167 0.034 1.085 0.330 25.679 0.123 1.467 5.827 0.16 90724. 0.0982
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22.65 0.5980 0.4958 0.0121 0.0146 0.030 0.950 0.247 22.469 0.107 1.100 4.993 0.16 90928. 0.0729
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23.52 0.6210 0.4039 0.0081 0.0124 0.026 0.807 0.165 19.086 0.091 0.733 3.917 0.16 91139. 0.0467
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24.39 0.6440 0.2578 0.0040 0.0101 0.021 0.657 0.083 15.541 0.074 0.367 2.410 0.16 91356. 0.0203
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25.26 0.6670 0.0016 0.0000 0.0077 0.016 0.499 0.000 11.818 0.056 0.002 0.014 0.16 91569. 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 0.0907 0.0305 0.212 4.454 4.160 158.102 0.503 18.504 11.935 0.24 131484. 0.7142
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1.31 0.0231 0.0666 0.0892 0.0309 0.215 4.513 4.092 160.193 0.510 18.203 11.587 0.24 131567. 0.6877
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2.62 0.0461 0.1292 0.0876 0.0313 0.217 4.568 4.019 162.138 0.516 17.878 11.244 0.24 131658. 0.6613
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3.93 0.0692 0.1879 0.0859 0.0316 0.220 4.618 3.941 163.896 0.522 17.529 10.906 0.24 131755. 0.6352
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5.24 0.0922 0.2429 0.0840 0.0319 0.222 4.661 3.857 165.424 0.527 17.154 10.574 0.24 131860. 0.6092
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6.55 0.1153 0.2943 0.0821 0.0321 0.224 4.696 3.766 166.675 0.531 16.752 10.249 0.24 131973. 0.5835
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7.86 0.1383 0.3422 0.0800 0.0323 0.225 4.722 3.669 167.602 0.533 16.321 9.930 0.24 132093. 0.5581
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9.17 0.1614 0.3867 0.0777 0.0324 0.225 4.738 3.566 168.153 0.535 15.861 9.619 0.24 132222. 0.5329
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10.48 0.1845 0.4280 0.0753 0.0325 0.226 4.741 3.455 168.275 0.536 15.370 9.314 0.24 132359. 0.5079
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11.79 0.2075 0.4661 0.0727 0.0324 0.225 4.731 3.338 167.918 0.534 14.847 9.016 0.24 132505. 0.4833
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13.10 0.2306 0.5012 0.0700 0.0322 0.224 4.706 3.213 167.035 0.532 14.293 8.726 0.24 132660. 0.4589
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14.41 0.2536 0.5333 0.0672 0.0319 0.222 4.665 3.082 165.592 0.527 13.708 8.441 0.24 132823. 0.4347
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15.72 0.2767 0.5626 0.0641 0.0315 0.219 4.608 2.944 163.568 0.521 13.093 8.163 0.24 132996. 0.4109
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17.03 0.2998 0.5891 0.0610 0.0310 0.216 4.535 2.800 160.947 0.512 12.452 7.889 0.24 133177. 0.3873
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18.34 0.3228 0.6128 0.0577 0.0304 0.212 4.444 2.650 157.717 0.502 11.786 7.621 0.24 133368. 0.3639
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19.65 0.3459 0.6336 0.0544 0.0297 0.206 4.335 2.495 153.867 0.490 11.098 7.355 0.24 133568. 0.3408
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20.96 0.3689 0.6516 0.0509 0.0288 0.200 4.209 2.335 149.386 0.476 10.388 7.091 0.24 133778. 0.3179
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22.27 0.3920 0.6666 0.0473 0.0278 0.193 4.064 2.171 144.262 0.459 9.658 6.827 0.24 133997. 0.2951
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23.58 0.4150 0.6783 0.0437 0.0267 0.186 3.902 2.003 138.487 0.441 8.911 6.561 0.24 134226. 0.2725
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24.89 0.4381 0.6865 0.0399 0.0255 0.177 3.720 1.832 132.049 0.420 8.147 6.291 0.24 134465. 0.2498
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26.20 0.4612 0.6908 0.0361 0.0241 0.168 3.520 1.657 124.941 0.398 7.368 6.014 0.24 134714. 0.2271
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27.51 0.4842 0.6904 0.0322 0.0226 0.157 3.301 1.478 117.158 0.373 6.576 5.724 0.24 134972. 0.2042
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28.82 0.5073 0.6842 0.0283 0.0210 0.146 3.062 1.298 108.696 0.346 5.772 5.415 0.24 135240. 0.1810
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30.13 0.5303 0.6709 0.0243 0.0192 0.134 2.805 1.115 99.558 0.317 4.958 5.079 0.24 135518. 0.1573
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31.44 0.5534 0.6478 0.0203 0.0173 0.120 2.529 0.930 89.750 0.286 4.137 4.700 0.24 135807. 0.1330
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32.75 0.5765 0.6111 0.0162 0.0153 0.106 2.234 0.744 79.287 0.252 3.309 4.256 0.24 136105. 0.1077
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34.06 0.5995 0.5535 0.0121 0.0132 0.091 1.921 0.557 68.191 0.217 2.479 3.706 0.24 136413. 0.0812
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35.37 0.6226 0.4614 0.0081 0.0109 0.076 1.592 0.371 56.494 0.180 1.648 2.975 0.24 136731. 0.0531
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36.68 0.6456 0.3045 0.0040 0.0085 0.059 1.246 0.185 44.235 0.141 0.821 1.893 0.24 137057. 0.0239
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37.99 0.6687 -0.0046 0.0000 0.0060 0.042 0.882 -0.002 31.303 0.100 -0.008 -0.027 0.24 137370. 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 0.0913 0.0299 0.493 7.769 7.446 367.653 0.878 33.121 9.186 0.32 175304. 0.7354
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1.75 0.0231 0.0684 0.0898 0.0303 0.500 7.877 7.326 372.758 0.890 32.585 8.914 0.32 175415. 0.7078
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3.50 0.0462 0.1326 0.0882 0.0307 0.506 7.977 7.196 377.513 0.901 32.007 8.646 0.32 175536. 0.6804
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5.25 0.0693 0.1929 0.0865 0.0311 0.512 8.068 7.056 381.817 0.912 31.385 8.382 0.32 175667. 0.6532
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7.00 0.0924 0.2493 0.0846 0.0314 0.517 8.147 6.906 385.566 0.920 30.716 8.124 0.32 175808. 0.6263
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8.75 0.1155 0.3019 0.0827 0.0316 0.521 8.212 6.744 388.651 0.928 29.999 7.871 0.32 175958. 0.5997
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10.50 0.1386 0.3509 0.0805 0.0318 0.524 8.261 6.571 390.953 0.933 29.230 7.624 0.32 176120. 0.5734
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12.25 0.1617 0.3964 0.0783 0.0319 0.526 8.291 6.387 392.348 0.937 28.407 7.383 0.32 176293. 0.5474
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14.00 0.1848 0.4386 0.0759 0.0320 0.527 8.298 6.189 392.710 0.938 27.529 7.148 0.32 176476. 0.5217
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15.75 0.2079 0.4777 0.0733 0.0319 0.526 8.281 5.979 391.914 0.936 26.594 6.919 0.32 176672. 0.4964
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17.50 0.2310 0.5137 0.0706 0.0317 0.523 8.238 5.756 389.850 0.931 25.602 6.697 0.32 176879. 0.4713
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19.25 0.2541 0.5467 0.0677 0.0314 0.518 8.166 5.520 386.434 0.923 24.554 6.479 0.32 177097. 0.4466
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21.00 0.2772 0.5769 0.0646 0.0311 0.512 8.064 5.273 381.611 0.911 23.454 6.267 0.32 177328. 0.4222
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22.75 0.3002 0.6043 0.0615 0.0305 0.503 7.931 5.015 375.343 0.896 22.305 6.060 0.32 177572. 0.3981
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24.50 0.3233 0.6289 0.0582 0.0299 0.493 7.768 4.746 367.600 0.878 21.112 5.856 0.32 177827. 0.3743
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26.25 0.3464 0.6508 0.0548 0.0292 0.481 7.572 4.469 358.355 0.856 19.877 5.656 0.32 178095. 0.3508
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27.99 0.3695 0.6699 0.0513 0.0283 0.466 7.345 4.183 347.580 0.830 18.605 5.458 0.32 178376. 0.3275
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29.74 0.3926 0.6861 0.0477 0.0273 0.450 7.084 3.889 335.248 0.800 17.297 5.261 0.32 178670. 0.3044
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31.49 0.4157 0.6992 0.0440 0.0261 0.431 6.790 3.587 321.335 0.767 15.957 5.064 0.32 178976. 0.2814
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33.24 0.4388 0.7089 0.0402 0.0249 0.410 6.462 3.280 305.815 0.730 14.588 4.864 0.32 179295. 0.2584
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34.99 0.4619 0.7149 0.0364 0.0235 0.387 6.100 2.966 288.670 0.689 13.192 4.660 0.32 179628. 0.2354
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36.74 0.4850 0.7164 0.0324 0.0220 0.362 5.703 2.646 269.885 0.644 11.772 4.448 0.32 179974. 0.2123
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38.49 0.5081 0.7126 0.0285 0.0203 0.335 5.271 2.322 249.456 0.596 10.330 4.223 0.32 180333. 0.1888
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40.24 0.5312 0.7019 0.0244 0.0185 0.305 4.805 1.994 227.384 0.543 8.871 3.978 0.32 180705. 0.1648
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41.99 0.5543 0.6818 0.0204 0.0166 0.273 4.304 1.663 203.689 0.486 7.398 3.704 0.32 181090. 0.1401
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43.74 0.5774 0.6483 0.0163 0.0145 0.239 3.770 1.330 178.404 0.426 5.915 3.381 0.32 181489. 0.1144
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45.49 0.6005 0.5939 0.0122 0.0123 0.203 3.203 0.995 151.586 0.362 4.427 2.978 0.32 181901. 0.0872
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47.24 0.6236 0.5033 0.0081 0.0100 0.165 2.606 0.661 123.314 0.294 2.939 2.430 0.32 182326. 0.0580
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48.99 0.6467 0.3407 0.0040 0.0076 0.126 1.980 0.328 93.681 0.224 1.457 1.586 0.32 182763. 0.0266
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50.74 0.6698 -0.0131 -0.0001 0.0051 0.084 1.316 -0.008 62.270 0.149 -0.036 -0.059 0.32 183169. 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 0.0921 0.0297 0.956 12.055 11.735 713.101 1.362 52.199 7.464 0.40 219116. 0.7502
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2.19 0.0231 0.0695 0.0906 0.0301 0.970 12.227 11.547 723.323 1.381 51.362 7.241 0.40 219256. 0.7219
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4.38 0.0462 0.1347 0.0890 0.0305 0.983 12.388 11.344 732.847 1.400 50.458 7.021 0.40 219408. 0.6938
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6.57 0.0693 0.1959 0.0873 0.0309 0.994 12.534 11.125 741.471 1.416 49.484 6.805 0.40 219572. 0.6659
|
|
8.75 0.0924 0.2531 0.0854 0.0312 1.004 12.661 10.890 748.994 1.430 48.437 6.594 0.40 219749. 0.6384
|
|
10.94 0.1156 0.3065 0.0834 0.0315 1.013 12.766 10.637 755.193 1.442 47.311 6.388 0.40 219938. 0.6113
|
|
13.13 0.1387 0.3562 0.0813 0.0317 1.019 12.845 10.365 759.837 1.451 46.105 6.187 0.40 220141. 0.5844
|
|
15.32 0.1618 0.4024 0.0790 0.0318 1.023 12.893 10.075 762.677 1.457 44.813 5.992 0.40 220357. 0.5580
|
|
17.51 0.1849 0.4453 0.0766 0.0318 1.024 12.906 9.765 763.464 1.458 43.433 5.801 0.40 220588. 0.5318
|
|
19.70 0.2080 0.4849 0.0740 0.0317 1.022 12.880 9.434 761.949 1.455 41.963 5.616 0.40 220833. 0.5061
|
|
21.89 0.2311 0.5215 0.0713 0.0316 1.016 12.812 9.083 757.911 1.448 40.401 5.436 0.40 221093. 0.4806
|
|
24.07 0.2542 0.5552 0.0683 0.0313 1.007 12.698 8.712 751.184 1.435 38.752 5.260 0.40 221367. 0.4555
|
|
26.26 0.2773 0.5860 0.0653 0.0309 0.995 12.537 8.323 741.654 1.416 37.019 5.090 0.40 221657. 0.4308
|
|
28.45 0.3004 0.6141 0.0621 0.0304 0.978 12.328 7.916 729.249 1.393 35.210 4.923 0.40 221962. 0.4064
|
|
30.64 0.3235 0.6394 0.0588 0.0297 0.957 12.068 7.493 713.907 1.363 33.329 4.761 0.40 222282. 0.3823
|
|
32.83 0.3467 0.6621 0.0553 0.0290 0.933 11.758 7.055 695.575 1.328 31.383 4.601 0.40 222618. 0.3585
|
|
35.02 0.3698 0.6821 0.0518 0.0281 0.904 11.397 6.604 674.197 1.288 29.376 4.443 0.40 222970. 0.3350
|
|
37.20 0.3929 0.6992 0.0482 0.0271 0.871 10.983 6.141 649.720 1.241 27.314 4.287 0.40 223338. 0.3117
|
|
39.39 0.4160 0.7134 0.0444 0.0259 0.834 10.516 5.666 622.094 1.188 25.201 4.131 0.40 223722. 0.2885
|
|
41.58 0.4391 0.7244 0.0406 0.0246 0.793 9.995 5.180 591.272 1.129 23.041 3.974 0.40 224122. 0.2653
|
|
43.77 0.4622 0.7317 0.0368 0.0232 0.747 9.419 4.685 557.211 1.064 20.838 3.813 0.40 224538. 0.2422
|
|
45.96 0.4853 0.7349 0.0328 0.0217 0.697 8.788 4.181 519.889 0.993 18.598 3.648 0.40 224971. 0.2188
|
|
48.15 0.5084 0.7330 0.0288 0.0200 0.643 8.102 3.670 479.291 0.915 16.323 3.473 0.40 225421. 0.1952
|
|
50.34 0.5315 0.7246 0.0247 0.0181 0.584 7.361 3.152 435.425 0.832 14.021 3.284 0.40 225887. 0.1710
|
|
52.52 0.5547 0.7072 0.0206 0.0162 0.521 6.564 2.630 388.326 0.742 11.696 3.071 0.40 226370. 0.1461
|
|
54.71 0.5778 0.6768 0.0165 0.0141 0.453 5.715 2.103 338.063 0.646 9.355 2.822 0.40 226869. 0.1201
|
|
56.90 0.6009 0.6258 0.0124 0.0119 0.382 4.814 1.575 284.748 0.544 7.006 2.509 0.40 227385. 0.0924
|
|
59.09 0.6240 0.5383 0.0082 0.0095 0.306 3.863 1.047 228.541 0.436 4.657 2.078 0.40 227917. 0.0624
|
|
61.28 0.6471 0.3744 0.0041 0.0071 0.227 2.867 0.521 169.628 0.324 2.318 1.394 0.40 228463. 0.0295
|
|
63.47 0.6702 -0.0117 -0.0001 0.0045 0.144 1.809 -0.010 107.021 0.204 -0.044 -0.042 0.41 228963. 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 0.0930 0.0298 1.655 17.387 17.080 1234.235 1.964 75.971 6.277 0.48 262919. 0.7610
|
|
2.65 0.0234 0.0708 0.0916 0.0302 1.680 17.644 16.806 1252.520 1.993 74.755 6.086 0.48 263090. 0.7320
|
|
5.31 0.0467 0.1372 0.0899 0.0306 1.702 17.884 16.510 1269.540 2.021 73.438 5.899 0.48 263275. 0.7032
|
|
7.96 0.0701 0.1995 0.0882 0.0310 1.723 18.101 16.191 1284.924 2.045 72.017 5.715 0.48 263475. 0.6747
|
|
10.61 0.0934 0.2576 0.0863 0.0313 1.741 18.289 15.846 1298.307 2.066 70.485 5.536 0.48 263690. 0.6465
|
|
13.27 0.1168 0.3119 0.0843 0.0316 1.756 18.444 15.476 1309.283 2.084 68.837 5.361 0.48 263922. 0.6188
|
|
15.92 0.1401 0.3623 0.0821 0.0318 1.767 18.559 15.078 1317.432 2.097 67.066 5.191 0.48 264169. 0.5914
|
|
18.58 0.1635 0.4093 0.0798 0.0319 1.773 18.627 14.651 1322.307 2.105 65.168 5.026 0.48 264434. 0.5644
|
|
21.23 0.1868 0.4528 0.0773 0.0319 1.775 18.644 14.195 1323.451 2.106 63.138 4.865 0.48 264716. 0.5377
|
|
23.88 0.2102 0.4930 0.0747 0.0318 1.771 18.601 13.708 1320.422 2.102 60.971 4.709 0.48 265016. 0.5115
|
|
26.54 0.2335 0.5301 0.0719 0.0317 1.761 18.494 13.190 1312.821 2.089 58.669 4.557 0.48 265333. 0.4856
|
|
29.19 0.2569 0.5643 0.0689 0.0314 1.744 18.318 12.643 1300.350 2.070 56.234 4.410 0.48 265669. 0.4600
|
|
31.84 0.2802 0.5957 0.0657 0.0309 1.720 18.071 12.068 1282.818 2.042 53.676 4.267 0.48 266024. 0.4349
|
|
34.50 0.3036 0.6242 0.0625 0.0304 1.690 17.751 11.467 1260.094 2.006 51.004 4.127 0.48 266397. 0.4100
|
|
37.15 0.3269 0.6501 0.0591 0.0297 1.652 17.356 10.842 1232.074 1.961 48.226 3.991 0.48 266789. 0.3856
|
|
39.81 0.3503 0.6732 0.0555 0.0289 1.607 16.886 10.196 1198.661 1.908 45.351 3.858 0.48 267200. 0.3614
|
|
42.46 0.3736 0.6937 0.0519 0.0280 1.555 16.338 9.529 1159.761 1.846 42.386 3.727 0.48 267631. 0.3375
|
|
45.11 0.3970 0.7114 0.0482 0.0269 1.496 15.711 8.844 1115.276 1.775 39.340 3.597 0.48 268081. 0.3138
|
|
47.77 0.4203 0.7261 0.0444 0.0257 1.428 15.004 8.142 1065.116 1.695 36.217 3.467 0.48 268551. 0.2903
|
|
50.42 0.4437 0.7376 0.0404 0.0243 1.353 14.217 7.425 1009.199 1.606 33.026 3.337 0.48 269041. 0.2668
|
|
53.07 0.4670 0.7456 0.0365 0.0228 1.271 13.347 6.693 947.460 1.508 29.773 3.204 0.48 269550. 0.2432
|
|
55.73 0.4904 0.7493 0.0324 0.0212 1.180 12.395 5.949 879.851 1.400 26.463 3.067 0.48 270080. 0.2195
|
|
58.38 0.5138 0.7478 0.0283 0.0194 1.081 11.359 5.194 806.358 1.283 23.105 2.922 0.48 270630. 0.1954
|
|
61.03 0.5371 0.7395 0.0241 0.0175 0.975 10.241 4.430 727.004 1.157 19.705 2.764 0.48 271200. 0.1707
|
|
63.69 0.5605 0.7218 0.0199 0.0155 0.861 9.042 3.659 641.865 1.022 16.274 2.585 0.48 271791. 0.1451
|
|
66.34 0.5838 0.6900 0.0157 0.0133 0.739 7.763 2.882 551.083 0.877 12.820 2.372 0.48 272402. 0.1182
|
|
69.00 0.6072 0.6345 0.0115 0.0110 0.610 6.408 2.104 454.884 0.724 9.358 2.098 0.48 273033. 0.0893
|
|
71.65 0.6305 0.5344 0.0072 0.0085 0.474 4.981 1.326 353.579 0.563 5.899 1.701 0.49 273684. 0.0575
|
|
74.30 0.6539 0.3298 0.0030 0.0060 0.332 3.486 0.552 247.477 0.394 2.457 1.012 0.49 274349. 0.0221
|
|
76.96 0.6772
|
|
|
|
|
|
|
|
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 0.0943 0.0300 2.651 23.872 23.551 1977.067 2.697 104.754 5.403 0.56 306708. 0.7692
|
|
3.06 0.0231 0.0704 0.0928 0.0305 2.691 24.229 23.184 2006.618 2.737 103.122 5.240 0.56 306906. 0.7403
|
|
6.13 0.0462 0.1365 0.0912 0.0309 2.728 24.561 22.786 2034.139 2.775 101.354 5.081 0.56 307121. 0.7116
|
|
9.19 0.0693 0.1984 0.0895 0.0313 2.761 24.862 22.357 2059.047 2.809 99.442 4.925 0.56 307353. 0.6832
|
|
12.25 0.0924 0.2564 0.0876 0.0316 2.790 25.124 21.893 2080.759 2.839 97.380 4.772 0.56 307602. 0.6551
|
|
15.32 0.1155 0.3105 0.0856 0.0319 2.814 25.340 21.394 2098.650 2.863 95.159 4.624 0.56 307870. 0.6274
|
|
18.38 0.1386 0.3609 0.0835 0.0321 2.832 25.502 20.857 2112.056 2.881 92.772 4.479 0.56 308156. 0.6001
|
|
21.44 0.1618 0.4079 0.0812 0.0322 2.843 25.602 20.281 2120.281 2.892 90.212 4.339 0.56 308461. 0.5732
|
|
24.51 0.1849 0.4515 0.0787 0.0322 2.846 25.630 19.665 2122.617 2.896 87.471 4.202 0.56 308787. 0.5467
|
|
27.57 0.2080 0.4919 0.0761 0.0322 2.841 25.578 19.007 2118.360 2.890 84.545 4.070 0.56 309133. 0.5206
|
|
30.64 0.2311 0.5293 0.0733 0.0320 2.825 25.440 18.308 2106.874 2.874 81.433 3.941 0.56 309499. 0.4948
|
|
33.70 0.2542 0.5639 0.0703 0.0317 2.800 25.208 17.567 2087.674 2.848 78.140 3.817 0.56 309886. 0.4693
|
|
36.76 0.2773 0.5956 0.0672 0.0313 2.763 24.879 16.789 2060.440 2.811 74.675 3.696 0.56 310294. 0.4443
|
|
39.83 0.3004 0.6247 0.0639 0.0307 2.716 24.451 15.974 2024.962 2.762 71.053 3.578 0.56 310723. 0.4196
|
|
42.89 0.3235 0.6512 0.0605 0.0301 2.657 23.921 15.127 1981.084 2.703 67.284 3.463 0.56 311174. 0.3952
|
|
45.95 0.3466 0.6751 0.0570 0.0293 2.586 23.288 14.249 1928.659 2.631 63.382 3.351 0.56 311647. 0.3711
|
|
49.02 0.3697 0.6964 0.0534 0.0284 2.504 22.550 13.344 1867.544 2.548 59.355 3.241 0.56 312141. 0.3473
|
|
52.08 0.3928 0.7151 0.0497 0.0273 2.411 21.705 12.413 1797.593 2.452 55.215 3.132 0.56 312658. 0.3238
|
|
55.14 0.4159 0.7311 0.0459 0.0261 2.305 20.752 11.459 1718.666 2.345 50.969 3.024 0.56 313198. 0.3003
|
|
58.21 0.4390 0.7441 0.0420 0.0248 2.187 19.689 10.483 1630.634 2.224 46.628 2.916 0.56 313760. 0.2770
|
|
61.27 0.4622 0.7538 0.0380 0.0233 2.056 18.515 9.487 1533.387 2.092 42.199 2.806 0.56 314344. 0.2536
|
|
64.33 0.4853 0.7597 0.0339 0.0217 1.913 17.229 8.474 1426.848 1.946 37.691 2.694 0.56 314952. 0.2300
|
|
67.40 0.5084 0.7610 0.0298 0.0199 1.758 15.830 7.445 1310.981 1.788 33.114 2.576 0.56 315582. 0.2062
|
|
70.46 0.5315 0.7565 0.0256 0.0180 1.590 14.318 6.402 1185.806 1.618 28.478 2.449 0.56 316236. 0.1818
|
|
73.52 0.5546 0.7438 0.0214 0.0160 1.410 12.696 5.349 1051.421 1.434 23.793 2.308 0.56 316912. 0.1566
|
|
76.59 0.5777 0.7192 0.0172 0.0138 1.218 10.964 4.288 908.019 1.239 19.075 2.142 0.56 317612. 0.1301
|
|
79.65 0.6008 0.6754 0.0129 0.0115 1.014 9.127 3.223 755.917 1.031 14.337 1.934 0.57 318335. 0.1019
|
|
82.72 0.6239 0.5960 0.0086 0.0090 0.799 7.191 2.158 595.571 0.812 9.599 1.644 0.57 319080. 0.0708
|
|
85.78 0.6470 0.4376 0.0044 0.0065 0.573 5.162 1.097 427.524 0.583 4.879 1.164 0.57 319845. 0.0358
|
|
88.84 0.6701 0.0188 0.0001 0.0038 0.334 3.010 0.027 249.322 0.340 0.118 0.048 0.57 320553. 0.0002
|
|
|
|
|
|
|
|
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 0.0957 0.0305 4.019 31.663 31.244 2996.912 3.577 138.974 4.729 0.63 350480. 0.7755
|
|
3.51 0.0232 0.0706 0.0943 0.0309 4.080 32.147 30.767 3042.662 3.632 136.851 4.586 0.63 350709. 0.7464
|
|
7.02 0.0463 0.1369 0.0927 0.0314 4.137 32.596 30.248 3085.218 3.683 134.543 4.447 0.63 350956. 0.7175
|
|
10.53 0.0695 0.1990 0.0910 0.0318 4.189 33.003 29.686 3123.680 3.729 132.042 4.310 0.63 351223. 0.6890
|
|
14.04 0.0927 0.2571 0.0891 0.0321 4.234 33.356 29.077 3157.138 3.769 129.336 4.177 0.63 351511. 0.6609
|
|
17.55 0.1158 0.3114 0.0871 0.0324 4.271 33.647 28.421 3184.633 3.801 126.415 4.048 0.64 351819. 0.6331
|
|
21.06 0.1390 0.3621 0.0849 0.0326 4.298 33.863 27.714 3205.146 3.826 123.270 3.922 0.64 352150. 0.6057
|
|
24.57 0.1622 0.4093 0.0826 0.0327 4.315 33.995 26.954 3217.615 3.841 119.889 3.799 0.64 352502. 0.5787
|
|
28.08 0.1853 0.4531 0.0801 0.0328 4.319 34.030 26.139 3220.939 3.845 116.265 3.681 0.64 352878. 0.5521
|
|
31.59 0.2085 0.4938 0.0774 0.0327 4.310 33.957 25.268 3214.050 3.836 112.390 3.566 0.64 353276. 0.5259
|
|
35.10 0.2317 0.5315 0.0746 0.0325 4.286 33.766 24.340 3195.969 3.815 108.263 3.454 0.64 353699. 0.5000
|
|
38.61 0.2548 0.5664 0.0716 0.0322 4.246 33.449 23.357 3165.951 3.779 103.890 3.346 0.64 354145. 0.4744
|
|
42.12 0.2780 0.5985 0.0684 0.0318 4.189 33.001 22.322 3123.510 3.728 99.286 3.241 0.64 354615. 0.4493
|
|
45.63 0.3012 0.6280 0.0651 0.0312 4.115 32.418 21.238 3068.338 3.663 94.468 3.139 0.64 355110. 0.4245
|
|
49.14 0.3243 0.6550 0.0616 0.0305 4.023 31.698 20.111 3000.208 3.581 89.452 3.040 0.64 355629. 0.4000
|
|
52.65 0.3475 0.6794 0.0580 0.0297 3.914 30.839 18.942 2918.916 3.484 84.254 2.943 0.64 356174. 0.3758
|
|
56.16 0.3707 0.7013 0.0543 0.0287 3.787 29.839 17.736 2824.258 3.371 78.889 2.848 0.64 356743. 0.3519
|
|
59.67 0.3938 0.7206 0.0505 0.0276 3.642 28.696 16.495 2716.018 3.242 73.371 2.755 0.64 357338. 0.3282
|
|
63.18 0.4170 0.7372 0.0466 0.0264 3.479 27.406 15.223 2593.996 3.096 67.710 2.662 0.64 357959. 0.3047
|
|
66.69 0.4402 0.7510 0.0427 0.0250 3.296 25.969 13.921 2457.994 2.934 61.920 2.569 0.64 358606. 0.2812
|
|
70.20 0.4633 0.7616 0.0386 0.0235 3.095 24.383 12.592 2307.853 2.755 56.011 2.475 0.64 359278. 0.2577
|
|
73.71 0.4865 0.7686 0.0344 0.0218 2.874 22.646 11.240 2143.458 2.559 49.996 2.378 0.64 359977. 0.2339
|
|
77.22 0.5097 0.7711 0.0302 0.0200 2.635 20.758 9.866 1964.759 2.345 43.886 2.278 0.64 360702. 0.2099
|
|
80.73 0.5328 0.7678 0.0260 0.0180 2.376 18.720 8.475 1771.792 2.115 37.695 2.169 0.64 361453. 0.1853
|
|
84.24 0.5560 0.7567 0.0217 0.0159 2.098 16.532 7.068 1564.713 1.868 31.440 2.049 0.64 362231. 0.1598
|
|
87.75 0.5791 0.7338 0.0173 0.0137 1.802 14.198 5.651 1343.825 1.604 25.137 1.907 0.65 363035. 0.1330
|
|
91.26 0.6023 0.6915 0.0130 0.0113 1.488 11.724 4.228 1109.627 1.325 18.808 1.728 0.65 363865. 0.1043
|
|
94.77 0.6255 0.6126 0.0086 0.0088 1.157 9.116 2.805 862.839 1.030 12.477 1.475 0.65 364721. 0.0725
|
|
98.28 0.6486 0.4486 0.0043 0.0061 0.810 6.385 1.387 604.294 0.721 6.171 1.041 0.65 365599. 0.0360
|
|
101.79 0.6718 -0.0509 -0.0002 0.0033 0.432 3.407 -0.081 322.492 0.385 -0.361 -0.114 0.65 366238. 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 0.0975 0.0313 5.880 41.181 40.287 4384.948 4.653 179.195 4.167 0.71 394230. 0.7760
|
|
3.96 0.0232 0.0702 0.0961 0.0318 5.966 41.781 39.689 4448.871 4.720 176.539 4.046 0.71 394489. 0.7479
|
|
7.92 0.0464 0.1363 0.0945 0.0322 6.046 42.340 39.037 4508.394 4.784 173.636 3.927 0.71 394769. 0.7199
|
|
11.87 0.0697 0.1983 0.0928 0.0326 6.118 42.846 38.327 4562.229 4.841 170.477 3.810 0.71 395073. 0.6921
|
|
15.83 0.0929 0.2565 0.0909 0.0329 6.181 43.285 37.556 4609.051 4.890 167.048 3.696 0.71 395399. 0.6645
|
|
19.79 0.1161 0.3109 0.0889 0.0332 6.232 43.646 36.721 4647.435 4.931 163.333 3.584 0.71 395750. 0.6371
|
|
23.75 0.1393 0.3617 0.0867 0.0334 6.270 43.913 35.819 4675.861 4.961 159.321 3.474 0.71 396126. 0.6101
|
|
27.70 0.1625 0.4091 0.0844 0.0335 6.293 44.071 34.846 4692.722 4.979 154.997 3.368 0.71 396526. 0.5833
|
|
31.66 0.1858 0.4531 0.0818 0.0335 6.298 44.105 33.802 4696.350 4.983 150.350 3.265 0.72 396953. 0.5568
|
|
35.62 0.2090 0.4941 0.0791 0.0335 6.283 44.000 32.683 4685.098 4.971 145.372 3.164 0.72 397406. 0.5307
|
|
39.58 0.2322 0.5321 0.0762 0.0333 6.246 43.740 31.488 4657.456 4.942 140.060 3.067 0.72 397886. 0.5048
|
|
43.54 0.2554 0.5672 0.0732 0.0329 6.185 43.315 30.221 4612.233 4.894 134.423 2.972 0.72 398392. 0.4793
|
|
47.49 0.2786 0.5997 0.0699 0.0325 6.100 42.718 28.885 4548.646 4.826 128.480 2.880 0.72 398926. 0.4542
|
|
51.45 0.3018 0.6296 0.0665 0.0319 5.989 41.944 27.485 4466.222 4.739 122.252 2.791 0.72 399488. 0.4293
|
|
55.41 0.3251 0.6570 0.0630 0.0312 5.853 40.990 26.026 4364.638 4.631 115.763 2.705 0.72 400078. 0.4048
|
|
59.37 0.3483 0.6819 0.0594 0.0303 5.691 39.854 24.513 4243.631 4.503 109.035 2.620 0.72 400695. 0.3806
|
|
63.32 0.3715 0.7043 0.0556 0.0293 5.502 38.532 22.951 4102.926 4.353 102.086 2.537 0.72 401341. 0.3566
|
|
67.28 0.3947 0.7243 0.0517 0.0282 5.287 37.023 21.343 3942.248 4.183 94.934 2.456 0.72 402016. 0.3328
|
|
71.24 0.4179 0.7417 0.0477 0.0269 5.044 35.324 19.693 3761.309 3.991 87.595 2.375 0.72 402719. 0.3092
|
|
75.20 0.4412 0.7563 0.0436 0.0254 4.774 33.432 18.005 3559.836 3.777 80.084 2.294 0.72 403451. 0.2856
|
|
79.15 0.4644 0.7678 0.0394 0.0238 4.476 31.345 16.281 3337.594 3.541 72.417 2.213 0.72 404213. 0.2619
|
|
83.11 0.4876 0.7757 0.0352 0.0221 4.150 29.061 14.525 3094.427 3.283 64.607 2.129 0.72 405004. 0.2381
|
|
87.07 0.5108 0.7794 0.0308 0.0202 3.795 26.580 12.741 2830.271 3.003 56.672 2.042 0.72 405824. 0.2138
|
|
91.03 0.5340 0.7775 0.0265 0.0182 3.413 23.903 10.933 2545.213 2.701 48.630 1.948 0.72 406674. 0.1890
|
|
94.99 0.5573 0.7679 0.0220 0.0160 3.003 21.032 9.105 2239.536 2.376 40.500 1.844 0.73 407554. 0.1632
|
|
98.94 0.5805 0.7466 0.0176 0.0137 2.566 17.973 7.263 1913.790 2.031 32.305 1.721 0.73 408463. 0.1361
|
|
102.90 0.6037 0.7059 0.0131 0.0112 2.104 14.734 5.412 1568.880 1.665 24.074 1.565 0.73 409402. 0.1068
|
|
106.86 0.6269 0.6273 0.0086 0.0086 1.617 11.327 3.561 1206.113 1.280 15.839 1.339 0.73 410370. 0.0741
|
|
110.82 0.6501 0.4572 0.0042 0.0059 1.109 7.767 1.716 827.046 0.878 7.632 0.941 0.73 411362. 0.0362
|
|
114.77 0.6733
|
|
|
|
|
|
|
|
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 0.0997 0.0339 8.725 54.990 50.826 6505.989 6.213 226.074 3.543 0.79 437947. 0.7411
|
|
4.40 0.0232 0.0668 0.0983 0.0342 8.812 55.543 50.108 6571.388 6.275 222.880 3.459 0.79 438237. 0.7183
|
|
8.81 0.0465 0.1303 0.0967 0.0345 8.891 56.038 49.318 6629.908 6.331 219.367 3.374 0.79 438551. 0.6952
|
|
13.21 0.0697 0.1905 0.0950 0.0348 8.958 56.461 48.453 6680.059 6.379 215.518 3.290 0.79 438891. 0.6719
|
|
17.61 0.0930 0.2476 0.0932 0.0350 9.012 56.802 47.508 6720.329 6.417 211.316 3.206 0.79 439258. 0.6484
|
|
22.01 0.1162 0.3015 0.0912 0.0351 9.051 57.045 46.480 6749.093 6.445 206.742 3.124 0.79 439651. 0.6248
|
|
26.42 0.1395 0.3523 0.0890 0.0352 9.071 57.176 45.364 6764.592 6.460 201.778 3.042 0.79 440073. 0.6010
|
|
30.82 0.1627 0.4000 0.0866 0.0352 9.072 57.179 44.156 6764.904 6.460 196.407 2.961 0.79 440523. 0.5772
|
|
35.22 0.1860 0.4448 0.0840 0.0351 9.049 57.036 42.854 6748.019 6.444 190.614 2.880 0.79 441002. 0.5532
|
|
39.63 0.2092 0.4867 0.0813 0.0350 9.001 56.730 41.454 6711.839 6.409 184.389 2.801 0.80 441510. 0.5292
|
|
44.03 0.2325 0.5257 0.0784 0.0347 8.924 56.245 39.957 6654.418 6.355 177.728 2.723 0.80 442049. 0.5051
|
|
48.43 0.2557 0.5620 0.0752 0.0342 8.816 55.566 38.364 6574.139 6.278 170.641 2.647 0.80 442617. 0.4810
|
|
52.84 0.2790 0.5956 0.0719 0.0337 8.676 54.685 36.680 6469.924 6.178 163.152 2.571 0.80 443216. 0.4569
|
|
57.24 0.3022 0.6266 0.0685 0.0330 8.503 53.596 34.913 6341.030 6.055 155.291 2.497 0.80 443845. 0.4329
|
|
61.64 0.3255 0.6551 0.0649 0.0322 8.297 52.293 33.068 6186.877 5.908 147.088 2.424 0.80 444506. 0.4090
|
|
66.04 0.3487 0.6811 0.0611 0.0313 8.055 50.771 31.154 6006.864 5.736 138.572 2.352 0.80 445198. 0.3852
|
|
70.45 0.3720 0.7046 0.0572 0.0302 7.778 49.026 29.174 5800.374 5.539 129.768 2.281 0.80 445921. 0.3615
|
|
74.85 0.3952 0.7255 0.0532 0.0290 7.465 47.052 27.136 5566.763 5.316 120.699 2.211 0.80 446675. 0.3379
|
|
79.25 0.4185 0.7438 0.0491 0.0276 7.115 44.844 25.042 5305.525 5.066 111.387 2.141 0.80 447462. 0.3143
|
|
83.66 0.4417 0.7593 0.0449 0.0261 6.727 42.400 22.898 5016.364 4.790 101.850 2.070 0.80 448281. 0.2907
|
|
88.06 0.4650 0.7716 0.0406 0.0245 6.301 39.717 20.708 4698.966 4.487 92.108 1.999 0.80 449131. 0.2669
|
|
92.46 0.4882 0.7804 0.0362 0.0227 5.837 36.792 18.476 4352.919 4.157 82.180 1.925 0.80 450015. 0.2428
|
|
96.86 0.5114 0.7846 0.0318 0.0207 5.335 33.627 16.206 3978.473 3.799 72.084 1.848 0.80 450931. 0.2182
|
|
101.27 0.5347 0.7828 0.0273 0.0186 4.796 30.229 13.904 3576.459 3.415 61.845 1.763 0.80 451880. 0.1929
|
|
105.67 0.5579 0.7726 0.0227 0.0164 4.222 26.608 11.575 3148.082 3.006 51.486 1.668 0.81 452861. 0.1665
|
|
110.07 0.5812 0.7493 0.0181 0.0140 3.614 22.779 9.226 2695.062 2.574 41.037 1.553 0.81 453875. 0.1384
|
|
114.48 0.6044 0.7039 0.0135 0.0116 2.977 18.762 6.864 2219.774 2.120 30.532 1.403 0.81 454922. 0.1078
|
|
118.88 0.6277 0.6164 0.0088 0.0090 2.314 14.582 4.499 1725.274 1.648 20.011 1.183 0.81 456001. 0.0736
|
|
123.28 0.6509 0.4316 0.0042 0.0063 1.629 10.269 2.139 1214.956 1.160 9.515 0.799 0.81 457106. 0.0343
|
|
127.69 0.6742
|
|
|
|
|
|
|