390 lines
69 KiB
Plaintext
390 lines
69 KiB
Plaintext
21x10.5PN (21x105PN.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 0.0867 0.0331 0.011 0.685 0.537 8.110 0.077 2.390 30.047 0.08 47153. 0.6154
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0.45 0.0225 0.0574 0.0853 0.0334 0.011 0.692 0.528 8.192 0.078 2.350 29.255 0.08 47181. 0.5942
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0.90 0.0450 0.1117 0.0837 0.0337 0.011 0.699 0.519 8.267 0.079 2.308 28.464 0.08 47212. 0.5729
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1.34 0.0675 0.1629 0.0821 0.0340 0.011 0.704 0.509 8.335 0.080 2.262 27.677 0.08 47246. 0.5515
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1.79 0.0900 0.2111 0.0803 0.0342 0.011 0.709 0.498 8.392 0.080 2.213 26.894 0.08 47282. 0.5301
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2.24 0.1125 0.2563 0.0784 0.0344 0.011 0.713 0.486 8.438 0.081 2.161 26.118 0.08 47320. 0.5087
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2.69 0.1351 0.2985 0.0764 0.0346 0.011 0.716 0.473 8.469 0.081 2.105 25.349 0.08 47361. 0.4873
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3.13 0.1576 0.3377 0.0742 0.0346 0.011 0.717 0.460 8.485 0.081 2.046 24.587 0.08 47406. 0.4659
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3.58 0.1801 0.3741 0.0719 0.0346 0.011 0.717 0.446 8.481 0.081 1.982 23.832 0.08 47452. 0.4445
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4.03 0.2026 0.4077 0.0695 0.0345 0.011 0.715 0.430 8.458 0.081 1.915 23.084 0.08 47502. 0.4232
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4.48 0.2251 0.4385 0.0669 0.0343 0.011 0.711 0.414 8.412 0.080 1.843 22.343 0.08 47555. 0.4019
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4.92 0.2476 0.4664 0.0641 0.0340 0.011 0.705 0.397 8.342 0.080 1.768 21.607 0.08 47611. 0.3806
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5.37 0.2701 0.4916 0.0612 0.0337 0.011 0.697 0.380 8.248 0.079 1.688 20.876 0.08 47670. 0.3594
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5.82 0.2926 0.5140 0.0583 0.0332 0.011 0.687 0.361 8.129 0.078 1.606 20.146 0.08 47732. 0.3382
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6.27 0.3151 0.5334 0.0551 0.0326 0.011 0.675 0.342 7.984 0.076 1.520 19.415 0.08 47798. 0.3171
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6.71 0.3376 0.5499 0.0519 0.0319 0.010 0.660 0.322 7.814 0.075 1.432 18.681 0.08 47866. 0.2961
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7.16 0.3602 0.5632 0.0486 0.0311 0.010 0.644 0.301 7.618 0.073 1.340 17.938 0.08 47938. 0.2751
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7.61 0.3827 0.5732 0.0452 0.0302 0.010 0.625 0.280 7.396 0.071 1.246 17.183 0.08 48013. 0.2541
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8.06 0.4052 0.5796 0.0417 0.0292 0.010 0.604 0.259 7.146 0.068 1.150 16.408 0.08 48091. 0.2331
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8.51 0.4277 0.5819 0.0381 0.0280 0.009 0.581 0.236 6.870 0.066 1.052 15.608 0.08 48173. 0.2120
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8.95 0.4502 0.5797 0.0345 0.0268 0.009 0.555 0.214 6.566 0.063 0.951 14.771 0.08 48258. 0.1909
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9.40 0.4727 0.5722 0.0308 0.0254 0.008 0.527 0.191 6.235 0.060 0.849 13.886 0.08 48347. 0.1695
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9.85 0.4952 0.5584 0.0270 0.0240 0.008 0.497 0.168 5.876 0.056 0.745 12.934 0.08 48439. 0.1479
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10.30 0.5177 0.5368 0.0232 0.0224 0.007 0.464 0.144 5.489 0.052 0.640 11.894 0.08 48534. 0.1261
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10.74 0.5402 0.5054 0.0194 0.0207 0.007 0.429 0.120 5.075 0.048 0.534 10.731 0.08 48633. 0.1039
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11.19 0.5627 0.4610 0.0155 0.0189 0.006 0.392 0.096 4.634 0.044 0.427 9.398 0.08 48735. 0.0814
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11.64 0.5852 0.3990 0.0116 0.0170 0.006 0.352 0.072 4.167 0.040 0.320 7.821 0.08 48841. 0.0586
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12.09 0.6078 0.3117 0.0077 0.0150 0.005 0.311 0.048 3.675 0.035 0.212 5.883 0.08 48950. 0.0359
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12.53 0.6303 0.1858 0.0038 0.0129 0.004 0.267 0.024 3.160 0.030 0.105 3.382 0.08 49062. 0.0145
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12.98 0.6528 -0.0044 -0.0001 0.0107 0.004 0.222 0.000 2.622 0.025 -0.002 -0.077 0.09 49175. 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 0.0871 0.0300 0.079 2.482 2.160 58.724 0.280 9.609 16.685 0.17 94303. 0.6852
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0.90 0.0226 0.0639 0.0857 0.0303 0.080 2.512 2.125 59.442 0.284 9.451 16.212 0.17 94361. 0.6603
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1.80 0.0452 0.1241 0.0842 0.0307 0.081 2.540 2.086 60.109 0.287 9.280 15.744 0.17 94423. 0.6354
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2.70 0.0678 0.1807 0.0825 0.0310 0.081 2.566 2.045 60.712 0.290 9.098 15.281 0.17 94491. 0.6106
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3.60 0.0904 0.2338 0.0807 0.0312 0.082 2.588 2.001 61.235 0.292 8.902 14.824 0.17 94563. 0.5860
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4.50 0.1131 0.2834 0.0788 0.0315 0.083 2.606 1.954 61.662 0.294 8.692 14.375 0.17 94641. 0.5615
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5.40 0.1357 0.3296 0.0768 0.0316 0.083 2.619 1.904 61.976 0.296 8.468 13.933 0.17 94724. 0.5372
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6.30 0.1583 0.3726 0.0746 0.0317 0.083 2.627 1.850 62.157 0.297 8.229 13.499 0.17 94813. 0.5130
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7.19 0.1809 0.4124 0.0723 0.0317 0.083 2.628 1.792 62.187 0.297 7.973 13.074 0.17 94907. 0.4891
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8.09 0.2035 0.4491 0.0698 0.0316 0.083 2.622 1.731 62.046 0.296 7.701 12.656 0.17 95008. 0.4653
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8.99 0.2261 0.4828 0.0672 0.0315 0.083 2.608 1.667 61.721 0.295 7.413 12.247 0.17 95114. 0.4417
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9.89 0.2487 0.5137 0.0645 0.0312 0.082 2.586 1.598 61.200 0.292 7.109 11.845 0.17 95227. 0.4184
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10.79 0.2713 0.5417 0.0616 0.0308 0.081 2.556 1.526 60.475 0.289 6.790 11.449 0.17 95346. 0.3952
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11.69 0.2939 0.5668 0.0586 0.0304 0.080 2.516 1.452 59.542 0.284 6.457 11.058 0.17 95471. 0.3723
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12.59 0.3166 0.5891 0.0554 0.0298 0.078 2.468 1.374 58.396 0.279 6.112 10.672 0.17 95603. 0.3495
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13.49 0.3392 0.6084 0.0522 0.0291 0.076 2.410 1.294 57.033 0.272 5.754 10.288 0.17 95741. 0.3270
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14.39 0.3618 0.6248 0.0488 0.0283 0.074 2.343 1.211 55.449 0.265 5.386 9.905 0.17 95886. 0.3045
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15.29 0.3844 0.6380 0.0454 0.0274 0.072 2.267 1.126 53.641 0.256 5.008 9.520 0.17 96037. 0.2822
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16.19 0.4070 0.6479 0.0419 0.0263 0.069 2.181 1.039 51.605 0.246 4.620 9.129 0.17 96195. 0.2600
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17.09 0.4296 0.6540 0.0383 0.0252 0.066 2.085 0.950 49.337 0.236 4.224 8.730 0.17 96360. 0.2377
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17.99 0.4522 0.6558 0.0346 0.0239 0.063 1.979 0.859 46.835 0.224 3.820 8.317 0.17 96532. 0.2154
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18.89 0.4748 0.6527 0.0309 0.0225 0.059 1.864 0.766 44.097 0.211 3.409 7.883 0.17 96710. 0.1928
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19.78 0.4974 0.6435 0.0271 0.0210 0.055 1.738 0.673 41.121 0.196 2.992 7.420 0.17 96896. 0.1700
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20.68 0.5201 0.6268 0.0233 0.0193 0.051 1.602 0.578 37.909 0.181 2.570 6.912 0.17 97088. 0.1468
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21.58 0.5427 0.6001 0.0194 0.0176 0.046 1.456 0.482 34.462 0.165 2.143 6.342 0.17 97287. 0.1230
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22.48 0.5653 0.5595 0.0155 0.0157 0.041 1.301 0.385 30.786 0.147 1.714 5.677 0.17 97493. 0.0985
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23.38 0.5879 0.4987 0.0116 0.0137 0.036 1.136 0.288 26.889 0.128 1.283 4.865 0.17 97706. 0.0730
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24.28 0.6105 0.4059 0.0077 0.0116 0.031 0.963 0.192 22.781 0.109 0.852 3.813 0.17 97926. 0.0466
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25.18 0.6331 0.2576 0.0038 0.0094 0.025 0.781 0.095 18.478 0.088 0.423 2.333 0.17 98152. 0.0201
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26.08 0.6557 -0.0048 -0.0001 0.0071 0.019 0.590 -0.001 13.962 0.067 -0.006 -0.042 0.17 98377. 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 0.0876 0.0288 0.255 5.366 4.889 190.461 0.606 21.746 11.643 0.25 141450. 0.7193
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1.35 0.0227 0.0670 0.0862 0.0292 0.259 5.437 4.809 192.984 0.614 21.390 11.302 0.25 141537. 0.6925
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2.70 0.0453 0.1300 0.0847 0.0295 0.262 5.503 4.723 195.338 0.622 21.006 10.966 0.25 141631. 0.6659
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4.06 0.0680 0.1891 0.0830 0.0298 0.265 5.564 4.630 197.471 0.629 20.595 10.635 0.25 141733. 0.6394
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5.41 0.0906 0.2444 0.0812 0.0301 0.267 5.616 4.531 199.331 0.634 20.153 10.310 0.25 141842. 0.6132
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6.76 0.1133 0.2960 0.0793 0.0304 0.269 5.659 4.424 200.864 0.639 19.679 9.991 0.25 141959. 0.5872
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8.11 0.1360 0.3441 0.0773 0.0305 0.271 5.691 4.310 202.007 0.643 19.173 9.678 0.25 142084. 0.5614
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9.46 0.1586 0.3888 0.0751 0.0306 0.272 5.711 4.189 202.696 0.645 18.631 9.373 0.25 142218. 0.5360
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10.81 0.1813 0.4302 0.0728 0.0307 0.272 5.716 4.059 202.866 0.646 18.053 9.074 0.25 142361. 0.5108
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12.17 0.2039 0.4685 0.0703 0.0306 0.271 5.704 3.920 202.452 0.644 17.438 8.783 0.25 142512. 0.4859
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13.52 0.2266 0.5037 0.0677 0.0304 0.270 5.674 3.774 201.401 0.641 16.785 8.498 0.25 142673. 0.4613
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14.87 0.2493 0.5359 0.0649 0.0302 0.268 5.626 3.619 199.673 0.636 16.096 8.220 0.25 142843. 0.4369
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16.22 0.2719 0.5652 0.0620 0.0298 0.265 5.557 3.456 197.243 0.628 15.374 7.948 0.25 143022. 0.4129
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17.57 0.2946 0.5918 0.0589 0.0293 0.260 5.468 3.287 194.090 0.618 14.620 7.681 0.25 143211. 0.3891
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18.93 0.3172 0.6155 0.0558 0.0287 0.255 5.359 3.111 190.200 0.605 13.837 7.419 0.25 143409. 0.3656
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20.28 0.3399 0.6364 0.0525 0.0280 0.249 5.228 2.929 185.558 0.591 13.028 7.159 0.25 143617. 0.3423
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21.63 0.3626 0.6545 0.0491 0.0272 0.242 5.076 2.741 180.149 0.573 12.193 6.902 0.25 143835. 0.3193
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22.98 0.3852 0.6695 0.0457 0.0263 0.233 4.901 2.549 173.959 0.554 11.336 6.645 0.25 144063. 0.2964
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24.33 0.4079 0.6813 0.0421 0.0252 0.224 4.704 2.351 166.976 0.532 10.457 6.386 0.25 144302. 0.2736
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25.69 0.4305 0.6895 0.0385 0.0241 0.213 4.485 2.149 159.187 0.507 9.560 6.124 0.25 144550. 0.2508
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27.04 0.4532 0.6939 0.0348 0.0228 0.202 4.243 1.943 150.582 0.479 8.645 5.854 0.25 144808. 0.2280
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28.39 0.4759 0.6935 0.0311 0.0213 0.189 3.977 1.734 141.154 0.449 7.714 5.572 0.25 145077. 0.2050
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29.74 0.4985 0.6875 0.0273 0.0198 0.176 3.688 1.522 130.900 0.417 6.769 5.273 0.25 145356. 0.1818
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31.09 0.5212 0.6743 0.0234 0.0181 0.161 3.376 1.307 119.821 0.381 5.813 4.947 0.25 145646. 0.1580
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32.44 0.5438 0.6514 0.0195 0.0163 0.145 3.041 1.090 107.925 0.344 4.847 4.580 0.25 145946. 0.1336
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33.80 0.5665 0.6147 0.0156 0.0144 0.128 2.683 0.871 95.231 0.303 3.875 4.149 0.25 146256. 0.1082
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35.15 0.5891 0.5571 0.0117 0.0124 0.110 2.304 0.652 81.767 0.260 2.899 3.616 0.25 146577. 0.0816
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36.50 0.6118 0.4647 0.0078 0.0102 0.091 1.904 0.433 67.572 0.215 1.924 2.904 0.25 146909. 0.0534
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37.85 0.6345 0.3062 0.0038 0.0080 0.071 1.485 0.214 52.698 0.168 0.954 1.845 0.25 147249. 0.0239
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39.20 0.6571 -0.0087 -0.0001 0.0056 0.050 1.043 -0.004 37.036 0.118 -0.018 -0.050 0.26 147582. 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 0.0883 0.0283 0.595 9.372 8.757 443.541 1.059 38.951 8.955 0.33 188591. 0.7404
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1.81 0.0227 0.0688 0.0869 0.0287 0.603 9.502 8.614 449.693 1.074 38.317 8.689 0.33 188708. 0.7125
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3.61 0.0454 0.1334 0.0853 0.0290 0.611 9.624 8.461 455.436 1.087 37.633 8.426 0.33 188834. 0.6848
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5.42 0.0681 0.1939 0.0837 0.0294 0.618 9.734 8.296 460.647 1.100 36.899 8.168 0.33 188970. 0.6574
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7.22 0.0908 0.2506 0.0819 0.0297 0.624 9.830 8.118 465.202 1.111 36.111 7.915 0.33 189116. 0.6302
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9.03 0.1135 0.3034 0.0800 0.0299 0.629 9.910 7.928 468.966 1.120 35.266 7.668 0.33 189273. 0.6033
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10.83 0.1362 0.3526 0.0779 0.0301 0.633 9.969 7.725 471.792 1.126 34.361 7.427 0.33 189440. 0.5767
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12.64 0.1589 0.3983 0.0757 0.0302 0.635 10.006 7.507 473.523 1.130 33.392 7.191 0.33 189620. 0.5505
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14.44 0.1815 0.4407 0.0734 0.0302 0.636 10.016 7.275 474.001 1.132 32.358 6.961 0.33 189811. 0.5246
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16.25 0.2042 0.4799 0.0709 0.0302 0.634 9.996 7.027 473.070 1.129 31.257 6.737 0.33 190014. 0.4990
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18.05 0.2269 0.5159 0.0682 0.0300 0.631 9.944 6.764 470.600 1.123 30.088 6.520 0.33 190229. 0.4738
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19.86 0.2496 0.5491 0.0654 0.0297 0.626 9.857 6.487 466.494 1.114 28.854 6.307 0.33 190456. 0.4489
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21.66 0.2723 0.5793 0.0625 0.0294 0.618 9.735 6.196 460.688 1.100 27.560 6.100 0.33 190696. 0.4243
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23.47 0.2950 0.6068 0.0594 0.0289 0.608 9.575 5.892 453.134 1.082 26.209 5.898 0.33 190949. 0.4000
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25.27 0.3177 0.6315 0.0562 0.0283 0.595 9.378 5.577 443.793 1.059 24.805 5.699 0.33 191215. 0.3761
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27.08 0.3404 0.6534 0.0529 0.0276 0.580 9.142 5.250 432.628 1.033 23.353 5.504 0.34 191493. 0.3524
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28.88 0.3631 0.6725 0.0496 0.0268 0.563 8.867 4.914 419.605 1.002 21.856 5.311 0.34 191785. 0.3290
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30.69 0.3858 0.6888 0.0461 0.0258 0.543 8.551 4.568 404.690 0.966 20.318 5.120 0.34 192090. 0.3057
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32.49 0.4085 0.7019 0.0425 0.0247 0.520 8.196 4.214 387.851 0.926 18.743 4.928 0.34 192409. 0.2826
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34.30 0.4312 0.7118 0.0388 0.0235 0.495 7.798 3.852 369.057 0.881 17.132 4.734 0.34 192741. 0.2596
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36.10 0.4539 0.7178 0.0351 0.0222 0.467 7.359 3.483 348.283 0.831 15.491 4.535 0.34 193087. 0.2365
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37.91 0.4766 0.7195 0.0313 0.0208 0.437 6.878 3.107 325.513 0.777 13.821 4.330 0.34 193447. 0.2132
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39.71 0.4993 0.7158 0.0275 0.0192 0.403 6.355 2.726 300.738 0.718 12.126 4.112 0.34 193820. 0.1897
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41.52 0.5219 0.7053 0.0236 0.0175 0.367 5.789 2.340 273.962 0.654 10.410 3.875 0.34 194207. 0.1656
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43.32 0.5446 0.6854 0.0197 0.0156 0.329 5.181 1.951 245.207 0.585 8.678 3.609 0.34 194609. 0.1408
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45.13 0.5673 0.6521 0.0157 0.0137 0.288 4.533 1.559 214.516 0.512 6.934 3.296 0.34 195024. 0.1150
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46.93 0.5900 0.5978 0.0118 0.0116 0.244 3.845 1.166 181.958 0.434 5.184 2.905 0.34 195453. 0.0876
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48.74 0.6127 0.5071 0.0078 0.0094 0.198 3.120 0.772 147.633 0.352 3.436 2.373 0.34 195896. 0.0583
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50.54 0.6354 0.3431 0.0038 0.0071 0.150 2.359 0.381 111.662 0.267 1.695 1.548 0.34 196351. 0.0267
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52.35 0.6581 -0.0173 -0.0001 0.0047 0.099 1.556 -0.012 73.626 0.176 -0.054 -0.075 0.34 196786. 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 0.0892 0.0281 1.156 14.568 13.814 861.756 1.646 61.445 7.271 0.42 235724. 0.7551
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2.26 0.0227 0.0698 0.0877 0.0285 1.172 14.776 13.591 874.062 1.669 60.453 7.053 0.42 235870. 0.7265
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4.52 0.0454 0.1354 0.0862 0.0289 1.188 14.970 13.351 885.551 1.691 59.385 6.838 0.42 236028. 0.6981
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6.77 0.0681 0.1968 0.0845 0.0292 1.202 15.146 13.092 895.979 1.711 58.234 6.628 0.42 236199. 0.6701
|
|
9.03 0.0908 0.2542 0.0827 0.0295 1.214 15.300 12.814 905.099 1.729 56.999 6.422 0.42 236382. 0.6423
|
|
11.29 0.1135 0.3078 0.0808 0.0298 1.224 15.428 12.516 912.644 1.743 55.673 6.220 0.42 236579. 0.6149
|
|
13.55 0.1362 0.3577 0.0787 0.0300 1.231 15.524 12.197 918.322 1.754 54.251 6.024 0.42 236790. 0.5878
|
|
15.80 0.1589 0.4041 0.0765 0.0301 1.236 15.583 11.855 921.823 1.761 52.729 5.833 0.42 237015. 0.5611
|
|
18.06 0.1816 0.4471 0.0741 0.0301 1.238 15.600 11.489 922.830 1.762 51.103 5.647 0.42 237255. 0.5348
|
|
20.32 0.2043 0.4869 0.0716 0.0301 1.235 15.570 11.099 921.037 1.759 49.370 5.466 0.42 237509. 0.5088
|
|
22.58 0.2270 0.5236 0.0690 0.0299 1.229 15.488 10.686 916.179 1.750 47.530 5.290 0.42 237779. 0.4832
|
|
24.83 0.2498 0.5573 0.0661 0.0296 1.218 15.350 10.249 908.063 1.734 45.587 5.119 0.42 238064. 0.4579
|
|
27.09 0.2725 0.5882 0.0632 0.0293 1.202 15.156 9.790 896.560 1.712 43.546 4.953 0.42 238365. 0.4330
|
|
29.35 0.2952 0.6164 0.0601 0.0288 1.182 14.903 9.311 881.575 1.684 41.416 4.791 0.42 238682. 0.4084
|
|
31.61 0.3179 0.6418 0.0569 0.0282 1.157 14.589 8.813 863.027 1.648 39.202 4.632 0.42 239015. 0.3842
|
|
33.86 0.3406 0.6645 0.0536 0.0274 1.128 14.214 8.298 840.850 1.606 36.911 4.476 0.42 239365. 0.3603
|
|
36.12 0.3633 0.6846 0.0501 0.0266 1.093 13.777 7.767 814.970 1.556 34.549 4.323 0.42 239730. 0.3366
|
|
38.38 0.3860 0.7018 0.0466 0.0256 1.053 13.275 7.222 785.322 1.500 32.122 4.171 0.42 240113. 0.3132
|
|
40.64 0.4087 0.7160 0.0430 0.0245 1.008 12.709 6.662 751.841 1.436 29.635 4.019 0.42 240512. 0.2899
|
|
42.89 0.4314 0.7271 0.0393 0.0233 0.958 12.078 6.091 714.468 1.365 27.092 3.867 0.42 240928. 0.2666
|
|
45.15 0.4541 0.7346 0.0355 0.0220 0.903 11.379 5.508 673.154 1.286 24.500 3.711 0.42 241361. 0.2434
|
|
47.41 0.4768 0.7380 0.0317 0.0205 0.842 10.614 4.915 627.864 1.199 21.862 3.551 0.42 241811. 0.2199
|
|
49.67 0.4995 0.7362 0.0278 0.0189 0.776 9.781 4.313 578.582 1.105 19.185 3.381 0.42 242279. 0.1962
|
|
51.92 0.5222 0.7280 0.0239 0.0171 0.704 8.880 3.704 525.315 1.003 16.475 3.198 0.42 242764. 0.1720
|
|
54.18 0.5449 0.7109 0.0199 0.0153 0.628 7.913 3.089 468.107 0.894 13.739 2.993 0.42 243266. 0.1470
|
|
56.44 0.5676 0.6808 0.0159 0.0133 0.546 6.881 2.469 407.042 0.777 10.983 2.752 0.42 243786. 0.1208
|
|
58.70 0.5903 0.6301 0.0119 0.0112 0.459 5.786 1.848 342.260 0.654 8.219 2.449 0.42 244323. 0.0930
|
|
60.95 0.6130 0.5426 0.0079 0.0089 0.367 4.631 1.227 273.961 0.523 5.456 2.031 0.42 244877. 0.0628
|
|
63.21 0.6357 0.3777 0.0039 0.0066 0.271 3.421 0.608 202.389 0.387 2.705 1.363 0.42 245447. 0.0297
|
|
65.47 0.6584 -0.0151 -0.0001 0.0041 0.170 2.139 -0.015 126.561 0.242 -0.065 -0.053 0.43 245985. 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 0.0902 0.0282 2.004 21.055 20.131 1494.661 2.379 89.541 6.109 0.50 282845. 0.7658
|
|
2.72 0.0228 0.0705 0.0888 0.0286 2.034 21.363 19.809 1516.499 2.414 88.111 5.925 0.50 283022. 0.7368
|
|
5.43 0.0455 0.1368 0.0872 0.0290 2.061 21.650 19.462 1536.871 2.446 86.566 5.744 0.50 283213. 0.7080
|
|
8.15 0.0683 0.1988 0.0855 0.0294 2.086 21.910 19.088 1555.346 2.475 84.902 5.566 0.50 283419. 0.6795
|
|
10.86 0.0910 0.2568 0.0837 0.0297 2.107 22.138 18.685 1571.489 2.501 83.111 5.393 0.50 283641. 0.6514
|
|
13.58 0.1138 0.3109 0.0818 0.0299 2.125 22.326 18.252 1584.823 2.522 81.187 5.224 0.50 283879. 0.6236
|
|
16.29 0.1366 0.3614 0.0797 0.0301 2.139 22.467 17.788 1594.835 2.538 79.122 5.059 0.50 284134. 0.5962
|
|
19.01 0.1593 0.4082 0.0775 0.0302 2.147 22.553 17.291 1600.978 2.548 76.909 4.899 0.50 284406. 0.5691
|
|
21.72 0.1821 0.4517 0.0751 0.0303 2.149 22.577 16.759 1602.686 2.551 74.542 4.743 0.50 284696. 0.5425
|
|
24.44 0.2048 0.4920 0.0726 0.0302 2.145 22.531 16.191 1599.422 2.546 72.017 4.591 0.50 285004. 0.5162
|
|
27.16 0.2276 0.5291 0.0699 0.0300 2.133 22.408 15.588 1590.711 2.532 69.334 4.445 0.50 285330. 0.4903
|
|
29.87 0.2504 0.5634 0.0670 0.0298 2.114 22.204 14.950 1576.213 2.509 66.498 4.302 0.50 285675. 0.4648
|
|
32.59 0.2731 0.5948 0.0640 0.0294 2.086 21.915 14.280 1555.698 2.476 63.519 4.164 0.50 286038. 0.4396
|
|
35.30 0.2959 0.6235 0.0609 0.0289 2.050 21.539 13.581 1529.001 2.433 60.407 4.029 0.50 286421. 0.4148
|
|
38.02 0.3186 0.6495 0.0576 0.0283 2.006 21.074 12.853 1495.987 2.381 57.171 3.897 0.50 286824. 0.3904
|
|
40.73 0.3414 0.6729 0.0542 0.0275 1.953 20.518 12.100 1456.534 2.318 53.822 3.768 0.50 287246. 0.3662
|
|
43.45 0.3641 0.6936 0.0508 0.0266 1.892 19.870 11.324 1410.519 2.245 50.368 3.641 0.50 287687. 0.3424
|
|
46.17 0.3869 0.7116 0.0472 0.0257 1.821 19.128 10.526 1357.828 2.161 46.818 3.516 0.50 288149. 0.3187
|
|
48.88 0.4097 0.7267 0.0435 0.0245 1.741 18.290 9.708 1298.347 2.066 43.179 3.391 0.50 288631. 0.2952
|
|
51.60 0.4324 0.7388 0.0398 0.0233 1.652 17.355 8.871 1231.975 1.961 39.459 3.266 0.50 289133. 0.2718
|
|
54.31 0.4552 0.7474 0.0359 0.0219 1.554 16.322 8.018 1158.627 1.844 35.665 3.139 0.51 289656. 0.2483
|
|
57.03 0.4779 0.7520 0.0320 0.0204 1.446 15.189 7.150 1078.242 1.716 31.805 3.008 0.51 290199. 0.2247
|
|
59.74 0.5007 0.7517 0.0281 0.0187 1.329 13.957 6.269 990.791 1.577 27.886 2.870 0.51 290763. 0.2008
|
|
62.46 0.5235 0.7451 0.0241 0.0169 1.202 12.626 5.377 896.293 1.426 23.918 2.721 0.51 291348. 0.1763
|
|
65.17 0.5462 0.7299 0.0201 0.0150 1.066 11.197 4.477 794.823 1.265 19.912 2.555 0.51 291954. 0.1510
|
|
67.89 0.5690 0.7019 0.0160 0.0130 0.921 9.671 3.570 686.540 1.093 15.877 2.358 0.51 292580. 0.1245
|
|
70.61 0.5917 0.6531 0.0119 0.0108 0.767 8.053 2.659 571.692 0.910 11.829 2.110 0.51 293228. 0.0961
|
|
73.32 0.6145 0.5661 0.0078 0.0085 0.604 6.348 1.750 450.646 0.717 7.784 1.761 0.51 293896. 0.0651
|
|
76.04 0.6373 0.3944 0.0038 0.0061 0.434 4.562 0.845 323.838 0.515 3.757 1.183 0.51 294583. 0.0304
|
|
78.75 0.6600
|
|
|
|
|
|
|
|
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 0.0916 0.0286 3.219 28.986 27.803 2400.608 3.275 123.670 5.253 0.58 329951. 0.7740
|
|
3.16 0.0227 0.0707 0.0901 0.0290 3.267 29.417 27.368 2436.227 3.323 121.731 5.095 0.58 330158. 0.7448
|
|
6.33 0.0455 0.1370 0.0886 0.0294 3.312 29.817 26.896 2469.429 3.369 119.632 4.940 0.58 330382. 0.7158
|
|
9.49 0.0682 0.1992 0.0869 0.0297 3.352 30.181 26.386 2499.515 3.410 117.366 4.788 0.58 330623. 0.6872
|
|
12.66 0.0909 0.2574 0.0851 0.0300 3.387 30.498 25.837 2525.780 3.446 114.924 4.640 0.58 330883. 0.6590
|
|
15.82 0.1136 0.3118 0.0831 0.0303 3.416 30.760 25.247 2547.452 3.475 112.297 4.495 0.58 331162. 0.6311
|
|
18.98 0.1364 0.3624 0.0810 0.0305 3.438 30.956 24.612 2563.709 3.497 109.473 4.354 0.58 331461. 0.6036
|
|
22.15 0.1591 0.4095 0.0788 0.0306 3.451 31.076 23.931 2573.676 3.511 106.444 4.217 0.58 331779. 0.5765
|
|
25.31 0.1818 0.4532 0.0764 0.0306 3.455 31.110 23.202 2576.438 3.515 103.201 4.085 0.58 332119. 0.5497
|
|
28.48 0.2046 0.4938 0.0738 0.0306 3.448 31.045 22.423 2571.119 3.507 99.737 3.956 0.58 332479. 0.5234
|
|
31.64 0.2273 0.5313 0.0711 0.0304 3.429 30.874 21.595 2556.955 3.488 96.053 3.831 0.58 332860. 0.4974
|
|
34.80 0.2500 0.5660 0.0682 0.0301 3.397 30.590 20.718 2533.386 3.456 92.155 3.709 0.58 333263. 0.4718
|
|
37.97 0.2727 0.5978 0.0652 0.0297 3.353 30.187 19.797 2500.034 3.411 88.056 3.592 0.59 333688. 0.4465
|
|
41.13 0.2955 0.6270 0.0620 0.0292 3.294 29.663 18.834 2456.645 3.351 83.771 3.477 0.59 334136. 0.4216
|
|
44.30 0.3182 0.6536 0.0587 0.0286 3.222 29.015 17.831 2403.005 3.278 79.314 3.366 0.59 334606. 0.3971
|
|
47.46 0.3409 0.6776 0.0553 0.0278 3.137 28.242 16.794 2338.927 3.191 74.698 3.257 0.59 335098. 0.3729
|
|
50.62 0.3637 0.6990 0.0518 0.0269 3.036 27.340 15.723 2264.225 3.089 69.936 3.150 0.59 335614. 0.3490
|
|
53.79 0.3864 0.7178 0.0481 0.0259 2.922 26.307 14.622 2178.712 2.972 65.038 3.044 0.59 336153. 0.3252
|
|
56.95 0.4091 0.7338 0.0444 0.0248 2.792 25.142 13.493 2082.217 2.841 60.016 2.939 0.59 336715. 0.3017
|
|
60.12 0.4318 0.7469 0.0406 0.0235 2.648 23.842 12.338 1974.580 2.694 54.880 2.834 0.59 337300. 0.2782
|
|
63.28 0.4546 0.7567 0.0367 0.0221 2.488 22.406 11.160 1855.662 2.531 49.640 2.728 0.59 337910. 0.2546
|
|
66.44 0.4773 0.7628 0.0328 0.0205 2.314 20.833 9.961 1725.366 2.354 44.308 2.619 0.59 338543. 0.2309
|
|
69.61 0.5000 0.7642 0.0288 0.0188 2.124 19.122 8.744 1583.648 2.160 38.893 2.504 0.59 339201. 0.2069
|
|
72.77 0.5228 0.7597 0.0247 0.0170 1.918 17.273 7.511 1430.528 1.952 33.408 2.381 0.59 339882. 0.1824
|
|
75.94 0.5455 0.7471 0.0206 0.0151 1.698 15.288 6.265 1266.128 1.727 27.866 2.244 0.59 340588. 0.1570
|
|
79.10 0.5682 0.7225 0.0165 0.0130 1.463 13.170 5.010 1090.694 1.488 22.285 2.083 0.59 341318. 0.1303
|
|
82.26 0.5910 0.6782 0.0123 0.0108 1.213 10.923 3.751 904.625 1.234 16.682 1.880 0.59 342072. 0.1018
|
|
85.43 0.6137 0.5973 0.0082 0.0084 0.950 8.555 2.491 708.505 0.967 11.081 1.595 0.59 342850. 0.0703
|
|
88.59 0.6364 0.4333 0.0041 0.0060 0.675 6.074 1.237 503.046 0.686 5.503 1.116 0.59 343650. 0.0347
|
|
91.76 0.6591 -0.0216 -0.0001 0.0034 0.381 3.430 -0.034 284.099 0.388 -0.150 -0.054 0.60 344375. 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 0.0932 0.0291 4.898 38.586 36.966 3652.139 4.359 164.423 4.591 0.67 377036. 0.7799
|
|
3.62 0.0227 0.0707 0.0918 0.0295 4.971 39.166 36.399 3707.036 4.425 161.903 4.454 0.67 377274. 0.7508
|
|
7.24 0.0455 0.1370 0.0902 0.0300 5.040 39.706 35.784 3758.197 4.486 159.166 4.319 0.67 377532. 0.7218
|
|
10.86 0.0682 0.1993 0.0885 0.0303 5.102 40.196 35.118 3804.521 4.541 156.203 4.187 0.67 377810. 0.6932
|
|
14.48 0.0910 0.2575 0.0867 0.0306 5.156 40.623 34.398 3844.906 4.590 153.002 4.058 0.67 378110. 0.6650
|
|
18.10 0.1137 0.3119 0.0848 0.0309 5.201 40.974 33.622 3878.139 4.629 149.550 3.932 0.67 378431. 0.6371
|
|
21.71 0.1365 0.3627 0.0827 0.0311 5.234 41.236 32.786 3902.962 4.659 145.832 3.810 0.67 378775. 0.6096
|
|
25.33 0.1592 0.4100 0.0804 0.0312 5.254 41.395 31.888 3918.024 4.677 141.837 3.691 0.67 379142. 0.5825
|
|
28.95 0.1820 0.4539 0.0780 0.0313 5.259 41.436 30.924 3921.932 4.681 137.552 3.576 0.67 379533. 0.5557
|
|
32.57 0.2047 0.4947 0.0754 0.0312 5.248 41.346 29.894 3913.338 4.671 132.968 3.465 0.67 379947. 0.5293
|
|
36.19 0.2275 0.5326 0.0726 0.0310 5.218 41.110 28.796 3891.071 4.645 128.086 3.357 0.67 380387. 0.5033
|
|
39.81 0.2502 0.5675 0.0697 0.0307 5.169 40.721 27.633 3854.261 4.601 122.914 3.252 0.67 380850. 0.4776
|
|
43.43 0.2730 0.5998 0.0666 0.0303 5.099 40.173 26.409 3802.342 4.539 117.469 3.150 0.67 381340. 0.4524
|
|
47.05 0.2957 0.6294 0.0634 0.0298 5.009 39.461 25.128 3734.933 4.458 111.772 3.052 0.67 381854. 0.4274
|
|
50.67 0.3185 0.6565 0.0600 0.0291 4.897 38.582 23.795 3651.736 4.359 105.841 2.956 0.67 382394. 0.4028
|
|
54.29 0.3412 0.6810 0.0565 0.0283 4.764 37.533 22.413 3552.481 4.240 99.694 2.862 0.67 382960. 0.3785
|
|
57.90 0.3640 0.7031 0.0529 0.0274 4.609 36.312 20.987 3436.898 4.102 93.349 2.770 0.67 383552. 0.3545
|
|
61.52 0.3867 0.7226 0.0492 0.0263 4.432 34.915 19.519 3304.725 3.945 86.822 2.679 0.67 384171. 0.3307
|
|
65.14 0.4095 0.7394 0.0454 0.0251 4.232 33.341 18.014 3155.706 3.767 80.125 2.589 0.67 384816. 0.3070
|
|
68.76 0.4322 0.7534 0.0415 0.0238 4.009 31.586 16.473 2989.617 3.569 73.274 2.499 0.67 385488. 0.2834
|
|
72.38 0.4550 0.7643 0.0376 0.0224 3.763 29.649 14.901 2806.225 3.350 66.282 2.409 0.67 386187. 0.2598
|
|
76.00 0.4777 0.7715 0.0335 0.0208 3.494 27.527 13.301 2605.419 3.110 59.162 2.316 0.67 386913. 0.2360
|
|
79.62 0.5005 0.7743 0.0294 0.0190 3.201 25.221 11.675 2387.118 2.849 51.931 2.218 0.67 387667. 0.2118
|
|
83.24 0.5232 0.7715 0.0253 0.0171 2.885 22.730 10.028 2151.364 2.568 44.603 2.114 0.68 388448. 0.1871
|
|
86.86 0.5460 0.7608 0.0211 0.0151 2.546 20.056 8.363 1898.335 2.266 37.198 1.998 0.68 389257. 0.1615
|
|
90.48 0.5687 0.7386 0.0169 0.0130 2.184 17.205 6.685 1628.410 1.944 29.736 1.862 0.68 390093. 0.1345
|
|
94.09 0.5915 0.6971 0.0126 0.0107 1.800 14.181 5.001 1342.215 1.602 22.243 1.690 0.68 390957. 0.1056
|
|
97.71 0.6142 0.6191 0.0084 0.0083 1.396 10.995 3.316 1040.679 1.242 14.750 1.445 0.68 391848. 0.0735
|
|
101.33 0.6369 0.4553 0.0041 0.0058 0.972 7.659 1.638 724.954 0.865 7.286 1.025 0.68 392764. 0.0367
|
|
104.95 0.6597 -0.0439 -0.0002 0.0031 0.516 4.067 -0.081 384.983 0.460 -0.360 -0.095 0.68 393528. 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 0.0952 0.0303 7.271 50.917 47.794 5421.649 5.753 212.590 3.998 0.75 424092. 0.7724
|
|
4.09 0.0228 0.0697 0.0938 0.0307 7.365 51.577 47.085 5491.975 5.827 209.432 3.889 0.75 424363. 0.7456
|
|
8.18 0.0457 0.1355 0.0922 0.0311 7.452 52.190 46.310 5557.247 5.896 205.986 3.780 0.75 424657. 0.7187
|
|
12.26 0.0685 0.1974 0.0906 0.0314 7.531 52.742 45.467 5615.951 5.959 202.237 3.672 0.75 424974. 0.6918
|
|
16.35 0.0914 0.2556 0.0887 0.0317 7.599 53.217 44.553 5666.566 6.012 198.170 3.566 0.75 425316. 0.6651
|
|
20.44 0.1142 0.3102 0.0868 0.0319 7.654 53.601 43.562 5707.439 6.056 193.765 3.462 0.75 425682. 0.6384
|
|
24.53 0.1370 0.3612 0.0846 0.0321 7.693 53.876 42.493 5736.730 6.087 189.007 3.360 0.75 426075. 0.6119
|
|
28.61 0.1599 0.4089 0.0823 0.0322 7.714 54.024 41.339 5752.470 6.104 183.877 3.260 0.75 426493. 0.5856
|
|
32.70 0.1827 0.4533 0.0799 0.0322 7.714 54.025 40.099 5752.568 6.104 178.360 3.162 0.75 426939. 0.5594
|
|
36.79 0.2055 0.4945 0.0772 0.0321 7.691 53.859 38.769 5734.956 6.085 172.445 3.066 0.75 427412. 0.5334
|
|
40.88 0.2284 0.5328 0.0744 0.0319 7.641 53.510 37.349 5697.776 6.046 166.130 2.973 0.75 427912. 0.5077
|
|
44.96 0.2512 0.5682 0.0714 0.0316 7.563 52.964 35.843 5639.613 5.984 159.428 2.883 0.75 428441. 0.4822
|
|
49.05 0.2741 0.6009 0.0682 0.0311 7.455 52.211 34.254 5559.496 5.899 152.362 2.795 0.75 428998. 0.4570
|
|
53.14 0.2969 0.6311 0.0649 0.0305 7.318 51.246 32.589 5456.737 5.790 144.958 2.709 0.75 429584. 0.4321
|
|
57.23 0.3197 0.6586 0.0615 0.0298 7.149 50.063 30.855 5330.792 5.656 137.243 2.625 0.75 430199. 0.4075
|
|
61.31 0.3426 0.6837 0.0579 0.0290 6.948 48.658 29.056 5181.156 5.497 129.242 2.544 0.75 430844. 0.3831
|
|
65.40 0.3654 0.7064 0.0542 0.0280 6.715 47.026 27.198 5007.380 5.313 120.977 2.464 0.75 431518. 0.3590
|
|
69.49 0.3883 0.7265 0.0504 0.0269 6.449 45.163 25.285 4809.026 5.103 112.469 2.385 0.76 432221. 0.3351
|
|
73.58 0.4111 0.7441 0.0465 0.0257 6.150 43.067 23.322 4585.751 4.866 103.737 2.307 0.76 432955. 0.3113
|
|
77.66 0.4339 0.7588 0.0425 0.0243 5.816 40.733 21.313 4337.270 4.602 94.799 2.229 0.76 433719. 0.2875
|
|
81.75 0.4568 0.7705 0.0384 0.0227 5.449 38.161 19.261 4063.365 4.311 85.672 2.150 0.76 434513. 0.2636
|
|
85.84 0.4796 0.7787 0.0342 0.0211 5.048 35.348 17.171 3763.925 3.994 76.376 2.069 0.76 435338. 0.2396
|
|
89.93 0.5024 0.7824 0.0300 0.0192 4.612 32.297 15.047 3438.995 3.649 66.929 1.985 0.76 436194. 0.2151
|
|
94.01 0.5253 0.7804 0.0257 0.0173 4.142 29.009 12.894 3088.866 3.277 57.353 1.893 0.76 437080. 0.1900
|
|
98.10 0.5481 0.7703 0.0213 0.0152 3.640 25.490 10.717 2714.146 2.880 47.671 1.791 0.76 437998. 0.1638
|
|
102.19 0.5710 0.7479 0.0170 0.0130 3.106 21.749 8.523 2315.852 2.457 37.912 1.669 0.76 438947. 0.1362
|
|
106.28 0.5938 0.7045 0.0126 0.0106 2.542 17.801 6.319 1895.511 2.011 28.109 1.512 0.76 439927. 0.1062
|
|
110.36 0.6166 0.6205 0.0082 0.0081 1.952 13.667 4.114 1455.242 1.544 18.301 1.282 0.76 440937. 0.0727
|
|
114.45 0.6395 0.4374 0.0038 0.0056 1.338 9.368 1.917 997.549 1.058 8.528 0.872 0.77 441974. 0.0337
|
|
118.54 0.6623
|
|
|
|
|
|
|
|
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 0.0976 0.0344 11.317 71.331 60.484 8439.293 8.059 269.035 3.251 0.83 471108. 0.7064
|
|
4.52 0.0227 0.0632 0.0962 0.0346 11.384 71.754 59.640 8489.312 8.107 265.279 3.186 0.83 471410. 0.6876
|
|
9.05 0.0455 0.1238 0.0947 0.0348 11.439 72.099 58.711 8530.159 8.146 261.149 3.122 0.83 471738. 0.6684
|
|
13.57 0.0682 0.1818 0.0931 0.0349 11.480 72.355 57.695 8560.442 8.175 256.628 3.057 0.83 472092. 0.6488
|
|
18.09 0.0910 0.2373 0.0913 0.0350 11.504 72.509 56.586 8578.646 8.192 251.693 2.992 0.83 472473. 0.6288
|
|
22.61 0.1137 0.2901 0.0894 0.0350 11.510 72.547 55.378 8583.113 8.196 246.321 2.926 0.83 472882. 0.6085
|
|
27.14 0.1365 0.3403 0.0872 0.0350 11.495 72.452 54.067 8571.941 8.186 240.488 2.861 0.83 473319. 0.5878
|
|
31.66 0.1592 0.3879 0.0849 0.0349 11.456 72.207 52.647 8542.991 8.158 234.172 2.795 0.83 473786. 0.5667
|
|
36.18 0.1819 0.4329 0.0825 0.0347 11.391 71.794 51.113 8494.041 8.111 227.353 2.729 0.83 474283. 0.5452
|
|
40.70 0.2047 0.4753 0.0798 0.0344 11.295 71.191 49.464 8422.771 8.043 220.014 2.664 0.83 474811. 0.5234
|
|
45.23 0.2274 0.5151 0.0770 0.0340 11.167 70.383 47.696 8327.128 7.952 212.153 2.598 0.84 475369. 0.5013
|
|
49.75 0.2502 0.5523 0.0739 0.0335 11.004 69.355 45.815 8205.477 7.836 203.785 2.532 0.84 475958. 0.4790
|
|
54.27 0.2729 0.5870 0.0707 0.0329 10.804 68.098 43.826 8056.746 7.694 194.939 2.467 0.84 476578. 0.4564
|
|
58.79 0.2956 0.6192 0.0673 0.0322 10.567 66.605 41.737 7880.165 7.525 185.648 2.402 0.84 477230. 0.4337
|
|
63.32 0.3184 0.6489 0.0638 0.0313 10.292 64.872 39.557 7675.070 7.329 175.948 2.338 0.84 477914. 0.4108
|
|
67.84 0.3411 0.6761 0.0602 0.0304 9.978 62.891 37.291 7440.740 7.105 165.873 2.273 0.84 478630. 0.3879
|
|
72.36 0.3639 0.7007 0.0564 0.0293 9.624 60.657 34.949 7176.381 6.853 155.451 2.209 0.84 479378. 0.3649
|
|
76.88 0.3866 0.7227 0.0525 0.0281 9.229 58.171 32.534 6882.344 6.572 144.711 2.144 0.84 480158. 0.3417
|
|
81.41 0.4094 0.7418 0.0485 0.0268 8.795 55.434 30.053 6558.438 6.263 133.676 2.078 0.84 480972. 0.3184
|
|
85.93 0.4321 0.7578 0.0444 0.0253 8.319 52.432 27.511 6203.279 5.924 122.371 2.012 0.84 481818. 0.2948
|
|
90.45 0.4548 0.7700 0.0402 0.0237 7.803 49.183 24.913 5818.939 5.557 110.814 1.942 0.84 482698. 0.2708
|
|
94.97 0.4776 0.7778 0.0359 0.0221 7.249 45.690 22.264 5405.631 5.162 99.029 1.868 0.84 483611. 0.2463
|
|
99.50 0.5003 0.7804 0.0316 0.0202 6.653 41.932 19.569 4961.106 4.738 87.042 1.789 0.84 484558. 0.2211
|
|
104.02 0.5231 0.7759 0.0272 0.0183 6.018 37.928 16.834 4487.292 4.285 74.877 1.702 0.84 485538. 0.1951
|
|
108.54 0.5458 0.7616 0.0227 0.0163 5.346 33.693 14.066 3986.263 3.807 62.564 1.600 0.85 486552. 0.1677
|
|
113.06 0.5686 0.7322 0.0182 0.0141 4.641 29.252 11.272 3460.905 3.305 50.138 1.477 0.85 487601. 0.1386
|
|
117.59 0.5913 0.6788 0.0137 0.0119 3.909 24.637 8.462 2914.876 2.784 37.639 1.317 0.85 488683. 0.1070
|
|
122.11 0.6140 0.5827 0.0091 0.0096 3.155 19.885 5.646 2352.639 2.247 25.115 1.089 0.85 489798. 0.0723
|
|
126.63 0.6368 0.4016 0.0046 0.0073 2.386 15.038 2.837 1779.140 1.699 12.620 0.723 0.85 490944. 0.0340
|
|
131.16 0.6595 0.0008 0.0000 0.0048 1.590 10.020 0.004 1185.507 1.132 0.017 0.001 0.85 492028. 0.0000
|
|
|
|
|
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