538 lines
95 KiB
Plaintext
538 lines
95 KiB
Plaintext
14x12E (14x12E.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 0.1062 0.0541 0.002 0.147 0.130 1.745 0.017 0.578 33.800 0.06 18232. 0.5108
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0.46 0.0347 0.0665 0.1056 0.0551 0.002 0.150 0.129 1.777 0.017 0.575 32.998 0.06 18248. 0.4973
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0.92 0.0694 0.1297 0.1049 0.0561 0.002 0.153 0.128 1.811 0.017 0.571 32.166 0.06 18268. 0.4832
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1.38 0.1041 0.1894 0.1041 0.0572 0.002 0.156 0.128 1.847 0.018 0.567 31.310 0.06 18289. 0.4686
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1.84 0.1388 0.2455 0.1033 0.0584 0.003 0.159 0.126 1.884 0.018 0.562 30.436 0.06 18313. 0.4536
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2.30 0.1735 0.2980 0.1023 0.0595 0.003 0.162 0.125 1.922 0.018 0.557 29.551 0.06 18340. 0.4382
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2.76 0.2082 0.3468 0.1011 0.0607 0.003 0.166 0.124 1.959 0.019 0.551 28.661 0.06 18370. 0.4226
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3.22 0.2429 0.3921 0.0998 0.0618 0.003 0.169 0.122 1.995 0.019 0.543 27.773 0.06 18403. 0.4068
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3.68 0.2776 0.4339 0.0982 0.0628 0.003 0.171 0.120 2.028 0.019 0.535 26.893 0.06 18439. 0.3908
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4.14 0.3123 0.4724 0.0964 0.0638 0.003 0.174 0.118 2.058 0.020 0.525 26.024 0.06 18478. 0.3748
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4.60 0.3470 0.5076 0.0944 0.0645 0.003 0.176 0.116 2.082 0.020 0.514 25.171 0.06 18521. 0.3586
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5.06 0.3817 0.5399 0.0920 0.0651 0.003 0.178 0.113 2.100 0.020 0.501 24.337 0.06 18567. 0.3424
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5.52 0.4164 0.5692 0.0894 0.0654 0.003 0.178 0.109 2.110 0.020 0.487 23.522 0.06 18616. 0.3261
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5.98 0.4511 0.5958 0.0864 0.0654 0.003 0.178 0.106 2.110 0.020 0.470 22.726 0.06 18669. 0.3097
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6.44 0.4858 0.6197 0.0830 0.0651 0.003 0.177 0.102 2.099 0.020 0.452 21.949 0.06 18726. 0.2932
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6.90 0.5205 0.6409 0.0792 0.0643 0.003 0.175 0.097 2.076 0.020 0.431 21.188 0.06 18785. 0.2765
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7.36 0.5552 0.6594 0.0751 0.0632 0.003 0.172 0.092 2.040 0.019 0.409 20.436 0.06 18848. 0.2596
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7.82 0.5899 0.6750 0.0705 0.0616 0.003 0.168 0.086 1.989 0.019 0.384 19.687 0.06 18915. 0.2424
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8.28 0.6246 0.6872 0.0656 0.0596 0.003 0.163 0.080 1.924 0.018 0.357 18.931 0.06 18984. 0.2248
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8.74 0.6593 0.6956 0.0603 0.0572 0.002 0.156 0.074 1.845 0.018 0.328 18.154 0.06 19057. 0.2068
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9.20 0.6940 0.6994 0.0548 0.0544 0.002 0.148 0.067 1.754 0.017 0.298 17.340 0.06 19133. 0.1882
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9.66 0.7287 0.6975 0.0490 0.0512 0.002 0.140 0.060 1.652 0.016 0.267 16.469 0.06 19213. 0.1691
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10.12 0.7634 0.6884 0.0430 0.0477 0.002 0.130 0.053 1.541 0.015 0.234 15.516 0.06 19295. 0.1493
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10.58 0.7981 0.6702 0.0370 0.0440 0.002 0.120 0.045 1.420 0.014 0.201 14.448 0.06 19380. 0.1288
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11.04 0.8328 0.6399 0.0308 0.0400 0.002 0.109 0.038 1.292 0.012 0.168 13.220 0.06 19469. 0.1075
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11.50 0.8675 0.5931 0.0245 0.0359 0.002 0.098 0.030 1.158 0.011 0.134 11.763 0.06 19560. 0.0854
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11.96 0.9022 0.5229 0.0183 0.0315 0.001 0.086 0.022 1.018 0.010 0.100 9.971 0.06 19655. 0.0625
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12.42 0.9369 0.4176 0.0121 0.0270 0.001 0.074 0.015 0.873 0.008 0.066 7.670 0.06 19753. 0.0391
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12.88 0.9716 0.2563 0.0059 0.0225 0.001 0.061 0.007 0.725 0.007 0.032 4.540 0.06 19853. 0.0162
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13.34 1.0063 -0.0034 -0.0001 0.0178 0.001 0.049 0.000 0.575 0.005 0.000 -0.057 0.06 19956. 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 0.1066 0.0499 0.017 0.544 0.522 12.873 0.061 2.321 18.384 0.11 36463. 0.5566
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0.93 0.0349 0.0727 0.1060 0.0509 0.018 0.555 0.519 13.141 0.063 2.308 17.909 0.11 36497. 0.5407
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1.85 0.0698 0.1413 0.1053 0.0520 0.018 0.567 0.516 13.426 0.064 2.293 17.418 0.11 36535. 0.5242
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2.78 0.1047 0.2059 0.1045 0.0532 0.018 0.580 0.512 13.727 0.066 2.277 16.914 0.11 36579. 0.5072
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3.70 0.1396 0.2662 0.1037 0.0544 0.019 0.593 0.508 14.039 0.067 2.258 16.403 0.11 36627. 0.4898
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4.63 0.1745 0.3223 0.1027 0.0556 0.019 0.607 0.503 14.356 0.069 2.237 15.887 0.11 36682. 0.4721
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5.55 0.2094 0.3741 0.1015 0.0568 0.020 0.620 0.497 14.672 0.070 2.212 15.371 0.11 36742. 0.4543
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6.48 0.2443 0.4220 0.1002 0.0580 0.020 0.633 0.491 14.979 0.072 2.183 14.858 0.11 36809. 0.4362
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7.40 0.2792 0.4658 0.0987 0.0591 0.020 0.645 0.483 15.267 0.073 2.149 14.354 0.11 36881. 0.4182
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8.33 0.3141 0.5060 0.0969 0.0601 0.021 0.656 0.474 15.526 0.074 2.110 13.859 0.11 36961. 0.4001
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9.25 0.3490 0.5427 0.0948 0.0610 0.021 0.665 0.464 15.745 0.075 2.065 13.376 0.11 37047. 0.3820
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10.18 0.3839 0.5760 0.0925 0.0616 0.021 0.672 0.453 15.910 0.076 2.014 12.908 0.11 37140. 0.3640
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11.10 0.4188 0.6063 0.0898 0.0620 0.021 0.677 0.440 16.010 0.076 1.955 12.454 0.11 37240. 0.3461
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12.03 0.4537 0.6337 0.0867 0.0621 0.021 0.677 0.425 16.031 0.077 1.889 12.016 0.11 37347. 0.3282
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12.96 0.4886 0.6584 0.0833 0.0618 0.021 0.675 0.408 15.961 0.076 1.814 11.592 0.11 37460. 0.3103
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13.88 0.5235 0.6804 0.0795 0.0612 0.021 0.667 0.389 15.789 0.075 1.731 11.182 0.11 37581. 0.2924
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14.81 0.5584 0.6999 0.0753 0.0601 0.021 0.655 0.369 15.505 0.074 1.639 10.782 0.11 37708. 0.2743
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15.73 0.5933 0.7165 0.0707 0.0585 0.020 0.638 0.346 15.104 0.072 1.539 10.390 0.11 37842. 0.2561
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16.66 0.6282 0.7302 0.0657 0.0565 0.020 0.616 0.322 14.584 0.070 1.430 10.000 0.11 37983. 0.2377
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17.58 0.6631 0.7405 0.0603 0.0540 0.019 0.589 0.295 13.949 0.067 1.314 9.607 0.11 38131. 0.2189
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18.51 0.6980 0.7467 0.0547 0.0512 0.018 0.558 0.268 13.208 0.063 1.192 9.203 0.11 38285. 0.1997
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19.43 0.7329 0.7479 0.0489 0.0479 0.017 0.523 0.239 12.374 0.059 1.065 8.778 0.11 38445. 0.1800
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20.36 0.7678 0.7427 0.0429 0.0444 0.015 0.484 0.210 11.455 0.055 0.935 8.321 0.11 38611. 0.1599
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21.28 0.8027 0.7292 0.0368 0.0405 0.014 0.442 0.180 10.460 0.050 0.802 7.815 0.11 38784. 0.1390
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22.21 0.8376 0.7045 0.0306 0.0364 0.013 0.397 0.150 9.396 0.045 0.667 7.235 0.11 38963. 0.1174
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23.13 0.8725 0.6638 0.0244 0.0320 0.011 0.350 0.119 8.273 0.039 0.531 6.545 0.12 39148. 0.0948
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24.06 0.9074 0.5991 0.0182 0.0275 0.010 0.300 0.089 7.098 0.034 0.395 5.680 0.12 39339. 0.0710
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24.99 0.9423 0.4954 0.0120 0.0228 0.008 0.249 0.059 5.883 0.028 0.261 4.523 0.12 39536. 0.0459
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25.91 0.9772 0.3218 0.0059 0.0180 0.006 0.196 0.029 4.638 0.022 0.129 2.833 0.12 39739. 0.0202
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26.84 1.0121 0.0015 0.0000 0.0131 0.005 0.143 0.000 3.378 0.016 0.000 0.013 0.12 39948. 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 0.1068 0.0480 0.056 1.180 1.176 41.870 0.133 5.232 12.744 0.17 54694. 0.5793
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1.39 0.0350 0.0757 0.1062 0.0491 0.057 1.206 1.170 42.790 0.136 5.204 12.401 0.17 54745. 0.5622
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2.78 0.0700 0.1471 0.1055 0.0502 0.059 1.233 1.163 43.775 0.139 5.172 12.048 0.17 54803. 0.5445
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4.18 0.1050 0.2140 0.1048 0.0514 0.060 1.263 1.155 44.814 0.143 5.136 11.686 0.17 54868. 0.5263
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5.57 0.1400 0.2763 0.1039 0.0527 0.062 1.293 1.145 45.893 0.146 5.094 11.319 0.17 54942. 0.5077
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6.96 0.1750 0.3341 0.1030 0.0539 0.063 1.324 1.134 46.993 0.150 5.046 10.950 0.17 55023. 0.4888
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8.35 0.2100 0.3875 0.1018 0.0552 0.064 1.355 1.122 48.091 0.153 4.990 10.581 0.17 55114. 0.4697
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9.75 0.2450 0.4365 0.1005 0.0564 0.066 1.385 1.107 49.160 0.156 4.925 10.217 0.17 55215. 0.4506
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11.14 0.2800 0.4814 0.0990 0.0576 0.067 1.413 1.090 50.168 0.160 4.850 9.858 0.17 55324. 0.4315
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12.53 0.3150 0.5223 0.0972 0.0586 0.068 1.439 1.071 51.078 0.163 4.763 9.508 0.17 55444. 0.4124
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13.92 0.3500 0.5596 0.0951 0.0595 0.070 1.461 1.048 51.852 0.165 4.662 9.168 0.17 55574. 0.3934
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15.31 0.3850 0.5934 0.0928 0.0602 0.070 1.478 1.022 52.445 0.167 4.546 8.839 0.17 55714. 0.3745
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16.71 0.4200 0.6241 0.0901 0.0606 0.071 1.488 0.992 52.815 0.168 4.414 8.522 0.17 55865. 0.3558
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18.10 0.4551 0.6519 0.0870 0.0607 0.071 1.491 0.959 52.916 0.168 4.264 8.216 0.17 56026. 0.3371
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19.49 0.4901 0.6769 0.0835 0.0605 0.071 1.485 0.921 52.705 0.168 4.095 7.922 0.17 56197. 0.3186
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20.88 0.5251 0.6994 0.0797 0.0598 0.070 1.469 0.878 52.142 0.166 3.906 7.639 0.17 56379. 0.3000
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22.28 0.5601 0.7193 0.0755 0.0588 0.069 1.442 0.831 51.196 0.163 3.698 7.365 0.17 56571. 0.2815
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23.67 0.5951 0.7365 0.0708 0.0572 0.067 1.404 0.780 49.846 0.159 3.470 7.099 0.17 56774. 0.2628
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25.06 0.6301 0.7510 0.0658 0.0552 0.064 1.355 0.725 48.082 0.153 3.223 6.836 0.17 56986. 0.2439
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26.45 0.6651 0.7623 0.0604 0.0527 0.062 1.294 0.666 45.919 0.146 2.960 6.574 0.17 57209. 0.2248
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27.84 0.7001 0.7698 0.0548 0.0498 0.058 1.223 0.603 43.392 0.138 2.684 6.307 0.17 57441. 0.2053
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29.24 0.7351 0.7728 0.0489 0.0465 0.054 1.142 0.539 40.535 0.129 2.397 6.029 0.17 57682. 0.1855
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30.63 0.7701 0.7699 0.0429 0.0429 0.050 1.053 0.473 37.381 0.119 2.102 5.733 0.17 57933. 0.1652
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32.02 0.8051 0.7592 0.0367 0.0390 0.046 0.957 0.405 33.957 0.108 1.801 5.409 0.17 58194. 0.1442
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33.41 0.8401 0.7381 0.0305 0.0348 0.041 0.853 0.336 30.290 0.096 1.497 5.039 0.17 58464. 0.1225
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34.81 0.8751 0.7015 0.0243 0.0303 0.035 0.744 0.268 26.411 0.084 1.191 4.598 0.17 58743. 0.0997
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36.20 0.9101 0.6412 0.0181 0.0257 0.030 0.630 0.199 22.351 0.071 0.886 4.041 0.17 59031. 0.0756
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37.59 0.9451 0.5405 0.0119 0.0208 0.024 0.511 0.131 18.147 0.058 0.584 3.280 0.17 59328. 0.0498
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38.98 0.9801 0.3619 0.0059 0.0159 0.019 0.390 0.065 13.840 0.044 0.287 2.118 0.17 59634. 0.0226
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40.37 1.0151 -0.0004 0.0000 0.0109 0.013 0.267 0.000 9.478 0.030 0.000 -0.002 0.18 59949. 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 0.1070 0.0470 0.130 2.053 2.095 97.153 0.232 9.319 9.782 0.22 72925. 0.5934
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1.86 0.0351 0.0775 0.1064 0.0481 0.133 2.100 2.084 99.363 0.237 9.270 9.513 0.22 72993. 0.5756
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3.72 0.0701 0.1506 0.1058 0.0493 0.136 2.150 2.072 101.731 0.243 9.214 9.236 0.22 73070. 0.5571
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5.58 0.1052 0.2189 0.1050 0.0505 0.140 2.202 2.057 104.231 0.249 9.151 8.952 0.22 73157. 0.5382
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7.44 0.1402 0.2825 0.1042 0.0517 0.143 2.257 2.041 106.831 0.255 9.078 8.665 0.22 73255. 0.5188
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9.30 0.1753 0.3414 0.1032 0.0530 0.147 2.314 2.022 109.486 0.261 8.994 8.377 0.22 73365. 0.4992
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11.16 0.2104 0.3956 0.1021 0.0543 0.150 2.370 2.000 112.143 0.268 8.896 8.089 0.22 73486. 0.4795
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13.01 0.2454 0.4453 0.1008 0.0555 0.154 2.424 1.974 114.734 0.274 8.782 7.805 0.22 73620. 0.4597
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14.87 0.2805 0.4908 0.0993 0.0567 0.157 2.476 1.944 117.182 0.280 8.649 7.526 0.22 73767. 0.4399
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16.73 0.3155 0.5322 0.0975 0.0578 0.160 2.523 1.910 119.401 0.285 8.494 7.254 0.22 73927. 0.4202
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18.59 0.3506 0.5698 0.0954 0.0587 0.163 2.563 1.870 121.294 0.290 8.316 6.991 0.22 74101. 0.4006
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20.45 0.3857 0.6040 0.0931 0.0594 0.165 2.594 1.823 122.761 0.293 8.110 6.736 0.22 74288. 0.3812
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22.31 0.4207 0.6349 0.0904 0.0599 0.166 2.614 1.770 123.693 0.295 7.874 6.491 0.22 74490. 0.3620
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24.17 0.4558 0.6629 0.0873 0.0600 0.166 2.620 1.710 123.982 0.296 7.607 6.256 0.22 74705. 0.3429
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26.03 0.4908 0.6882 0.0839 0.0598 0.166 2.610 1.642 123.522 0.295 7.306 6.031 0.22 74934. 0.3239
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27.89 0.5259 0.7109 0.0800 0.0592 0.164 2.583 1.567 122.219 0.292 6.969 5.815 0.23 75178. 0.3051
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29.75 0.5609 0.7311 0.0757 0.0581 0.161 2.536 1.483 119.994 0.286 6.597 5.606 0.23 75435. 0.2862
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31.61 0.5960 0.7488 0.0710 0.0565 0.157 2.468 1.392 116.794 0.279 6.190 5.404 0.23 75705. 0.2672
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33.47 0.6311 0.7638 0.0660 0.0545 0.151 2.379 1.292 112.596 0.269 5.749 5.206 0.23 75989. 0.2481
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35.32 0.6661 0.7758 0.0606 0.0520 0.144 2.270 1.187 107.435 0.256 5.278 5.010 0.23 76287. 0.2287
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37.18 0.7012 0.7843 0.0549 0.0491 0.136 2.142 1.076 101.390 0.242 4.784 4.812 0.23 76597. 0.2091
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39.04 0.7362 0.7885 0.0490 0.0458 0.127 1.998 0.960 94.546 0.226 4.271 4.607 0.23 76920. 0.1892
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40.90 0.7713 0.7872 0.0430 0.0421 0.117 1.838 0.842 86.974 0.208 3.745 4.390 0.23 77256. 0.1688
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42.76 0.8064 0.7787 0.0368 0.0381 0.106 1.664 0.721 78.744 0.188 3.208 4.154 0.23 77605. 0.1479
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44.62 0.8414 0.7602 0.0306 0.0339 0.094 1.477 0.599 69.922 0.167 2.665 3.886 0.23 77966. 0.1261
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46.48 0.8765 0.7270 0.0243 0.0293 0.081 1.280 0.476 60.578 0.145 2.119 3.568 0.23 78339. 0.1032
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48.34 0.9115 0.6704 0.0181 0.0246 0.068 1.073 0.354 50.790 0.121 1.576 3.164 0.23 78724. 0.0789
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50.20 0.9466 0.5731 0.0119 0.0197 0.055 0.859 0.233 40.650 0.097 1.038 2.604 0.23 79121. 0.0527
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52.06 0.9817 0.3931 0.0059 0.0146 0.041 0.639 0.115 30.259 0.072 0.511 1.723 0.23 79531. 0.0245
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53.92 1.0167 0.0001 0.0000 0.0096 0.026 0.417 0.000 19.733 0.047 0.000 0.000 0.23 79951. 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 0.1072 0.0464 0.251 3.165 3.280 187.251 0.358 14.590 7.945 0.28 91155. 0.6031
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2.33 0.0351 0.0788 0.1066 0.0475 0.257 3.239 3.263 191.613 0.366 14.514 7.724 0.28 91240. 0.5848
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4.65 0.0702 0.1530 0.1060 0.0487 0.263 3.318 3.244 196.291 0.375 14.429 7.496 0.28 91336. 0.5659
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6.98 0.1053 0.2223 0.1053 0.0499 0.270 3.402 3.222 201.237 0.384 14.333 7.263 0.28 91446. 0.5464
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9.31 0.1404 0.2868 0.1045 0.0512 0.277 3.489 3.197 206.387 0.394 14.221 7.026 0.28 91568. 0.5266
|
|
11.64 0.1755 0.3464 0.1035 0.0525 0.284 3.578 3.168 211.654 0.404 14.092 6.789 0.28 91705. 0.5065
|
|
13.96 0.2107 0.4012 0.1024 0.0538 0.291 3.667 3.134 216.932 0.414 13.941 6.553 0.28 91858. 0.4863
|
|
16.29 0.2458 0.4514 0.1011 0.0551 0.298 3.754 3.095 222.088 0.424 13.765 6.320 0.28 92025. 0.4660
|
|
18.62 0.2809 0.4972 0.0996 0.0563 0.304 3.837 3.048 226.970 0.433 13.559 6.092 0.28 92209. 0.4458
|
|
20.95 0.3160 0.5390 0.0978 0.0574 0.310 3.912 2.994 231.406 0.442 13.319 5.869 0.28 92410. 0.4257
|
|
23.27 0.3511 0.5769 0.0958 0.0583 0.315 3.976 2.932 235.205 0.449 13.041 5.654 0.28 92628. 0.4057
|
|
25.60 0.3862 0.6112 0.0934 0.0590 0.319 4.026 2.860 238.165 0.455 12.720 5.446 0.28 92863. 0.3860
|
|
27.93 0.4213 0.6424 0.0907 0.0595 0.322 4.058 2.777 240.072 0.459 12.352 5.247 0.28 93115. 0.3664
|
|
30.26 0.4564 0.6705 0.0877 0.0597 0.323 4.069 2.683 240.710 0.460 11.933 5.055 0.28 93385. 0.3470
|
|
32.58 0.4915 0.6960 0.0842 0.0595 0.322 4.055 2.577 239.868 0.458 11.461 4.872 0.28 93673. 0.3278
|
|
34.91 0.5266 0.7189 0.0803 0.0588 0.318 4.012 2.458 237.356 0.453 10.934 4.697 0.28 93978. 0.3087
|
|
37.24 0.5618 0.7394 0.0760 0.0578 0.312 3.939 2.327 233.017 0.445 10.349 4.529 0.28 94300. 0.2895
|
|
39.57 0.5969 0.7574 0.0713 0.0562 0.304 3.833 2.183 226.745 0.433 9.709 4.366 0.28 94639. 0.2704
|
|
41.89 0.6320 0.7728 0.0662 0.0542 0.293 3.693 2.027 218.489 0.417 9.016 4.208 0.28 94996. 0.2511
|
|
44.22 0.6671 0.7854 0.0608 0.0516 0.279 3.522 1.861 208.321 0.398 8.276 4.051 0.28 95368. 0.2316
|
|
46.55 0.7022 0.7946 0.0551 0.0487 0.263 3.320 1.686 196.395 0.375 7.500 3.894 0.28 95757. 0.2119
|
|
48.87 0.7373 0.7997 0.0492 0.0453 0.245 3.091 1.505 182.872 0.349 6.694 3.732 0.29 96163. 0.1919
|
|
51.20 0.7724 0.7997 0.0431 0.0416 0.225 2.838 1.319 167.897 0.321 5.866 3.562 0.29 96584. 0.1715
|
|
53.53 0.8075 0.7927 0.0369 0.0376 0.203 2.563 1.129 151.603 0.290 5.022 3.378 0.29 97020. 0.1504
|
|
55.86 0.8426 0.7762 0.0306 0.0332 0.180 2.267 0.937 134.124 0.256 4.169 3.170 0.29 97473. 0.1286
|
|
58.18 0.8777 0.7454 0.0243 0.0287 0.155 1.954 0.745 115.599 0.221 3.313 2.922 0.29 97940. 0.1057
|
|
60.51 0.9129 0.6917 0.0181 0.0238 0.129 1.626 0.553 96.187 0.184 2.460 2.608 0.29 98423. 0.0813
|
|
62.84 0.9480 0.5969 0.0119 0.0189 0.102 1.286 0.363 76.069 0.145 1.616 2.167 0.29 98921. 0.0547
|
|
65.17 0.9831 0.4153 0.0058 0.0137 0.074 0.937 0.178 55.453 0.106 0.791 1.454 0.29 99434. 0.0257
|
|
67.49 1.0182 -0.0086 -0.0001 0.0086 0.046 0.584 -0.002 34.571 0.066 -0.010 -0.029 0.29 99961. 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 0.1074 0.0460 0.430 4.521 4.734 320.912 0.511 21.055 6.690 0.33 109384. 0.6101
|
|
2.79 0.0351 0.0796 0.1069 0.0471 0.441 4.628 4.710 328.512 0.523 20.949 6.503 0.33 109485. 0.5915
|
|
5.59 0.0702 0.1545 0.1063 0.0483 0.451 4.743 4.683 336.672 0.536 20.830 6.309 0.33 109601. 0.5722
|
|
8.38 0.1054 0.2245 0.1056 0.0495 0.463 4.864 4.653 345.309 0.550 20.695 6.111 0.33 109733. 0.5525
|
|
11.17 0.1405 0.2896 0.1048 0.0508 0.475 4.991 4.617 354.315 0.564 20.539 5.911 0.33 109880. 0.5324
|
|
13.97 0.1756 0.3497 0.1038 0.0521 0.488 5.121 4.577 363.541 0.579 20.357 5.710 0.33 110045. 0.5120
|
|
16.76 0.2107 0.4049 0.1028 0.0535 0.500 5.252 4.529 372.799 0.593 20.144 5.510 0.33 110227. 0.4914
|
|
19.56 0.2458 0.4554 0.1015 0.0548 0.512 5.379 4.473 381.861 0.608 19.894 5.313 0.33 110429. 0.4709
|
|
22.35 0.2810 0.5016 0.1000 0.0560 0.524 5.500 4.407 390.461 0.621 19.602 5.119 0.33 110650. 0.4504
|
|
25.14 0.3161 0.5435 0.0982 0.0571 0.534 5.611 4.330 398.295 0.634 19.260 4.931 0.33 110891. 0.4300
|
|
27.94 0.3512 0.5816 0.0962 0.0581 0.543 5.706 4.241 405.032 0.645 18.862 4.749 0.34 111152. 0.4099
|
|
30.73 0.3863 0.6161 0.0939 0.0589 0.550 5.780 4.137 410.314 0.653 18.403 4.573 0.34 111434. 0.3899
|
|
33.52 0.4214 0.6474 0.0912 0.0594 0.555 5.829 4.019 413.767 0.659 17.875 4.405 0.34 111738. 0.3701
|
|
36.32 0.4566 0.6757 0.0881 0.0595 0.557 5.846 3.883 415.010 0.661 17.273 4.244 0.34 112062. 0.3505
|
|
39.11 0.4917 0.7013 0.0846 0.0593 0.555 5.827 3.731 413.673 0.658 16.594 4.090 0.34 112407. 0.3311
|
|
41.90 0.5268 0.7244 0.0808 0.0587 0.549 5.768 3.560 409.419 0.652 15.833 3.943 0.34 112774. 0.3118
|
|
44.70 0.5619 0.7451 0.0765 0.0577 0.539 5.663 3.370 401.971 0.640 14.989 3.802 0.34 113161. 0.2926
|
|
47.49 0.5970 0.7634 0.0717 0.0561 0.525 5.510 3.162 391.136 0.623 14.064 3.667 0.34 113568. 0.2733
|
|
50.29 0.6322 0.7792 0.0666 0.0541 0.505 5.308 2.937 376.826 0.600 13.062 3.535 0.34 113996. 0.2539
|
|
53.08 0.6673 0.7923 0.0612 0.0515 0.482 5.059 2.696 359.157 0.572 11.992 3.405 0.34 114444. 0.2343
|
|
55.87 0.7024 0.8022 0.0554 0.0485 0.454 4.767 2.443 338.394 0.539 10.868 3.275 0.34 114911. 0.2145
|
|
58.67 0.7375 0.8081 0.0495 0.0452 0.422 4.435 2.181 314.817 0.501 9.701 3.142 0.34 115398. 0.1945
|
|
61.46 0.7726 0.8092 0.0434 0.0414 0.387 4.067 1.911 288.676 0.459 8.502 3.003 0.34 115903. 0.1740
|
|
64.25 0.8078 0.8037 0.0371 0.0373 0.349 3.666 1.637 260.207 0.414 7.281 2.853 0.34 116428. 0.1530
|
|
67.05 0.8429 0.7891 0.0308 0.0329 0.308 3.235 1.359 229.641 0.365 6.046 2.685 0.34 116971. 0.1312
|
|
69.84 0.8780 0.7608 0.0245 0.0283 0.264 2.778 1.080 197.227 0.314 4.806 2.485 0.35 117533. 0.1082
|
|
72.63 0.9131 0.7102 0.0182 0.0234 0.219 2.300 0.803 163.241 0.260 3.570 2.230 0.35 118112. 0.0837
|
|
75.43 0.9482 0.6190 0.0120 0.0184 0.172 1.803 0.528 128.004 0.204 2.350 1.872 0.35 118710. 0.0570
|
|
78.22 0.9834 0.4394 0.0059 0.0132 0.123 1.294 0.260 91.887 0.146 1.155 1.281 0.35 119326. 0.0274
|
|
81.02 1.0185 -0.0022 0.0000 0.0079 0.074 0.779 -0.001 55.301 0.088 -0.003 -0.006 0.35 119959. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 7000
|
|
|
|
V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
|
|
(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
|
|
0.00 0.0000 0.0000 0.1077 0.0458 0.680 6.124 6.458 507.205 0.692 28.726 5.775 0.39 127611. 0.6151
|
|
3.26 0.0351 0.0802 0.1071 0.0469 0.696 6.271 6.427 519.371 0.709 28.587 5.613 0.39 127730. 0.5964
|
|
6.52 0.0703 0.1557 0.1066 0.0481 0.714 6.429 6.392 532.449 0.726 28.431 5.445 0.39 127866. 0.5770
|
|
9.78 0.1054 0.2262 0.1059 0.0494 0.733 6.597 6.352 546.312 0.745 28.253 5.274 0.39 128019. 0.5570
|
|
13.04 0.1406 0.2916 0.1051 0.0507 0.752 6.771 6.305 560.789 0.765 28.047 5.100 0.39 128191. 0.5367
|
|
16.30 0.1757 0.3521 0.1042 0.0520 0.772 6.951 6.251 575.643 0.785 27.806 4.926 0.39 128383. 0.5162
|
|
19.57 0.2108 0.4076 0.1031 0.0534 0.792 7.131 6.188 590.575 0.806 27.523 4.752 0.39 128596. 0.4955
|
|
22.83 0.2460 0.4584 0.1019 0.0547 0.812 7.308 6.113 605.218 0.826 27.190 4.581 0.39 128831. 0.4747
|
|
26.09 0.2811 0.5048 0.1004 0.0559 0.830 7.476 6.025 619.143 0.845 26.798 4.414 0.39 129089. 0.4540
|
|
29.35 0.3162 0.5469 0.0987 0.0571 0.847 7.629 5.922 631.862 0.862 26.339 4.251 0.39 129371. 0.4335
|
|
32.61 0.3514 0.5851 0.0967 0.0581 0.862 7.762 5.801 642.836 0.877 25.803 4.093 0.39 129676. 0.4132
|
|
35.87 0.3865 0.6198 0.0944 0.0589 0.874 7.866 5.661 651.490 0.889 25.181 3.941 0.39 130006. 0.3930
|
|
39.13 0.4217 0.6512 0.0917 0.0594 0.881 7.936 5.500 657.216 0.897 24.465 3.796 0.39 130360. 0.3731
|
|
42.39 0.4568 0.6796 0.0886 0.0596 0.884 7.962 5.317 659.398 0.900 23.648 3.657 0.39 130739. 0.3534
|
|
45.65 0.4919 0.7054 0.0852 0.0594 0.882 7.938 5.109 657.435 0.897 22.723 3.524 0.39 131143. 0.3339
|
|
48.91 0.5271 0.7286 0.0813 0.0588 0.873 7.858 4.875 650.780 0.888 21.685 3.398 0.39 131570. 0.3144
|
|
52.17 0.5622 0.7495 0.0770 0.0577 0.857 7.715 4.616 638.983 0.872 20.534 3.277 0.39 132023. 0.2951
|
|
55.43 0.5973 0.7681 0.0722 0.0562 0.834 7.507 4.332 621.727 0.848 19.269 3.160 0.40 132499. 0.2757
|
|
58.70 0.6325 0.7842 0.0671 0.0541 0.803 7.231 4.024 598.865 0.817 17.898 3.048 0.40 132999. 0.2562
|
|
61.96 0.6676 0.7977 0.0616 0.0515 0.765 6.889 3.694 570.574 0.778 16.433 2.937 0.40 133522. 0.2366
|
|
65.22 0.7028 0.8081 0.0558 0.0485 0.721 6.487 3.348 537.281 0.733 14.892 2.826 0.40 134068. 0.2168
|
|
68.48 0.7379 0.8148 0.0498 0.0451 0.670 6.030 2.989 499.428 0.681 13.293 2.714 0.40 134636. 0.1967
|
|
71.74 0.7730 0.8168 0.0437 0.0413 0.613 5.523 2.619 457.419 0.624 11.650 2.597 0.40 135227. 0.1762
|
|
75.00 0.8082 0.8125 0.0374 0.0372 0.552 4.970 2.243 411.633 0.562 9.975 2.471 0.40 135839. 0.1551
|
|
78.26 0.8433 0.7994 0.0310 0.0327 0.486 4.376 1.862 362.443 0.494 8.282 2.330 0.40 136474. 0.1333
|
|
81.52 0.8784 0.7731 0.0247 0.0280 0.416 3.746 1.480 310.253 0.423 6.581 2.163 0.40 137129. 0.1103
|
|
84.78 0.9136 0.7250 0.0183 0.0231 0.343 3.085 1.099 255.511 0.349 4.887 1.951 0.40 137807. 0.0857
|
|
88.04 0.9487 0.6364 0.0120 0.0180 0.267 2.400 0.723 198.740 0.271 3.214 1.649 0.41 138505. 0.0587
|
|
91.30 0.9839 0.4576 0.0059 0.0127 0.188 1.697 0.354 140.546 0.192 1.576 1.143 0.41 139224. 0.0285
|
|
94.57 1.0190 -0.0058 0.0000 0.0074 0.109 0.985 -0.003 81.598 0.111 -0.011 -0.014 0.41 139962. 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 0.1079 0.0457 1.013 7.983 8.457 755.633 0.902 37.618 5.077 0.44 145838. 0.6188
|
|
3.73 0.0351 0.0806 0.1074 0.0468 1.038 8.177 8.418 773.924 0.924 37.445 4.934 0.44 145974. 0.6000
|
|
7.45 0.0703 0.1564 0.1069 0.0480 1.064 8.385 8.375 793.616 0.947 37.250 4.786 0.44 146128. 0.5805
|
|
11.18 0.1054 0.2272 0.1062 0.0493 1.092 8.606 8.324 814.526 0.972 37.026 4.635 0.44 146303. 0.5605
|
|
14.91 0.1405 0.2929 0.1055 0.0506 1.122 8.837 8.266 836.397 0.998 36.767 4.483 0.44 146500. 0.5401
|
|
18.63 0.1757 0.3536 0.1046 0.0520 1.152 9.074 8.198 858.880 1.025 36.463 4.329 0.44 146719. 0.5195
|
|
22.36 0.2108 0.4094 0.1036 0.0533 1.182 9.314 8.117 881.524 1.052 36.105 4.176 0.45 146963. 0.4987
|
|
26.09 0.2459 0.4604 0.1024 0.0547 1.212 9.549 8.022 903.780 1.079 35.681 4.026 0.45 147231. 0.4779
|
|
29.81 0.2811 0.5069 0.1009 0.0560 1.240 9.773 7.909 924.994 1.104 35.180 3.878 0.45 147526. 0.4571
|
|
33.54 0.3162 0.5491 0.0993 0.0572 1.266 9.978 7.777 944.427 1.127 34.590 3.735 0.45 147848. 0.4365
|
|
37.26 0.3514 0.5875 0.0973 0.0582 1.289 10.156 7.621 961.263 1.147 33.899 3.596 0.45 148197. 0.4161
|
|
40.99 0.3865 0.6222 0.0950 0.0590 1.307 10.297 7.440 974.620 1.163 33.095 3.463 0.45 148574. 0.3959
|
|
44.72 0.4216 0.6538 0.0923 0.0595 1.319 10.392 7.232 983.577 1.174 32.166 3.335 0.45 148979. 0.3759
|
|
48.44 0.4568 0.6823 0.0892 0.0597 1.324 10.430 6.993 987.196 1.178 31.103 3.213 0.45 149412. 0.3561
|
|
52.17 0.4919 0.7082 0.0858 0.0596 1.320 10.402 6.721 984.558 1.175 29.896 3.096 0.45 149874. 0.3365
|
|
55.90 0.5270 0.7316 0.0819 0.0590 1.307 10.299 6.417 974.828 1.164 28.541 2.985 0.45 150363. 0.3170
|
|
59.62 0.5622 0.7527 0.0776 0.0579 1.284 10.114 6.078 957.316 1.143 27.033 2.880 0.45 150880. 0.2975
|
|
63.35 0.5973 0.7715 0.0728 0.0564 1.249 9.842 5.705 931.531 1.112 25.376 2.778 0.45 151424. 0.2781
|
|
67.08 0.6324 0.7879 0.0676 0.0543 1.203 9.480 5.301 897.241 1.071 23.577 2.679 0.45 151996. 0.2586
|
|
70.80 0.6676 0.8018 0.0621 0.0517 1.146 9.030 4.868 854.700 1.020 21.652 2.583 0.45 152594. 0.2389
|
|
74.53 0.7027 0.8128 0.0563 0.0487 1.079 8.500 4.412 804.541 0.960 19.627 2.488 0.46 153218. 0.2190
|
|
78.26 0.7378 0.8202 0.0503 0.0452 1.002 7.897 3.940 747.435 0.892 17.523 2.391 0.46 153868. 0.1989
|
|
81.98 0.7730 0.8230 0.0441 0.0414 0.917 7.227 3.453 683.993 0.816 15.360 2.290 0.46 154543. 0.1784
|
|
85.71 0.8081 0.8199 0.0377 0.0372 0.824 6.495 2.958 614.786 0.734 13.155 2.182 0.46 155243. 0.1573
|
|
89.44 0.8433 0.8083 0.0313 0.0327 0.725 5.709 2.456 540.383 0.645 10.925 2.062 0.46 155968. 0.1354
|
|
93.16 0.8784 0.7839 0.0249 0.0279 0.619 4.875 1.952 461.397 0.551 8.685 1.919 0.46 156718. 0.1124
|
|
96.89 0.9135 0.7384 0.0185 0.0229 0.508 3.999 1.451 378.513 0.452 6.452 1.738 0.46 157492. 0.0877
|
|
100.62 0.9487 0.6530 0.0122 0.0177 0.392 3.091 0.955 292.527 0.349 4.247 1.480 0.46 158290. 0.0606
|
|
104.34 0.9838 0.4766 0.0060 0.0124 0.274 2.159 0.469 204.367 0.244 2.088 1.042 0.47 159112. 0.0299
|
|
108.07 1.0189 -0.0012 0.0000 0.0070 0.154 1.216 -0.001 115.060 0.137 -0.003 -0.002 0.47 159955. 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 0.1083 0.0457 1.443 10.107 10.735 1076.249 1.142 47.748 4.524 0.50 164063. 0.6212
|
|
4.19 0.0351 0.0808 0.1078 0.0469 1.478 10.354 10.688 1102.480 1.170 47.540 4.397 0.50 164215. 0.6025
|
|
8.38 0.0703 0.1568 0.1072 0.0481 1.516 10.620 10.635 1130.771 1.200 47.306 4.266 0.50 164389. 0.5831
|
|
12.58 0.1054 0.2278 0.1066 0.0493 1.557 10.902 10.575 1160.867 1.232 47.037 4.132 0.50 164586. 0.5631
|
|
16.77 0.1405 0.2937 0.1059 0.0507 1.599 11.198 10.504 1192.410 1.265 46.724 3.996 0.50 164807. 0.5428
|
|
20.96 0.1757 0.3546 0.1051 0.0521 1.643 11.504 10.421 1224.902 1.300 46.355 3.859 0.50 165053. 0.5221
|
|
25.15 0.2108 0.4105 0.1041 0.0535 1.687 11.812 10.323 1257.702 1.334 45.918 3.723 0.50 165327. 0.5013
|
|
29.34 0.2459 0.4616 0.1029 0.0548 1.730 12.115 10.206 1290.015 1.369 45.398 3.589 0.50 165630. 0.4805
|
|
33.54 0.2811 0.5083 0.1015 0.0561 1.771 12.405 10.067 1320.900 1.402 44.780 3.457 0.50 165961. 0.4597
|
|
37.73 0.3162 0.5506 0.0999 0.0573 1.809 12.672 9.903 1349.282 1.432 44.049 3.329 0.50 166323. 0.4391
|
|
41.92 0.3513 0.5891 0.0979 0.0584 1.843 12.903 9.710 1373.971 1.458 43.188 3.205 0.50 166716. 0.4186
|
|
46.11 0.3865 0.6239 0.0956 0.0592 1.869 13.089 9.484 1393.687 1.479 42.183 3.086 0.50 167140. 0.3984
|
|
50.30 0.4216 0.6555 0.0930 0.0598 1.887 13.214 9.221 1407.085 1.493 41.017 2.973 0.50 167596. 0.3783
|
|
54.50 0.4567 0.6842 0.0900 0.0600 1.895 13.268 8.920 1412.798 1.499 39.678 2.864 0.51 168084. 0.3585
|
|
58.69 0.4919 0.7102 0.0865 0.0599 1.890 13.237 8.578 1409.487 1.496 38.155 2.760 0.51 168603. 0.3388
|
|
62.88 0.5270 0.7338 0.0826 0.0593 1.872 13.110 8.192 1395.929 1.481 36.439 2.662 0.51 169154. 0.3193
|
|
67.07 0.5621 0.7550 0.0783 0.0583 1.839 12.877 7.762 1371.113 1.455 34.527 2.568 0.51 169736. 0.2998
|
|
71.26 0.5973 0.7741 0.0735 0.0567 1.789 12.531 7.289 1334.317 1.416 32.421 2.478 0.51 170349. 0.2804
|
|
75.46 0.6324 0.7908 0.0683 0.0546 1.723 12.070 6.774 1285.190 1.364 30.131 2.391 0.51 170992. 0.2608
|
|
79.65 0.6675 0.8051 0.0628 0.0520 1.642 11.496 6.223 1224.076 1.299 27.679 2.306 0.51 171665. 0.2411
|
|
83.84 0.7027 0.8166 0.0569 0.0490 1.545 10.818 5.642 1151.881 1.222 25.096 2.222 0.51 172367. 0.2212
|
|
88.03 0.7378 0.8246 0.0508 0.0455 1.434 10.045 5.038 1069.573 1.135 22.411 2.137 0.51 173099. 0.2010
|
|
92.22 0.7729 0.8283 0.0445 0.0416 1.312 9.185 4.417 978.034 1.038 19.648 2.049 0.51 173859. 0.1805
|
|
96.42 0.8081 0.8261 0.0382 0.0373 1.178 8.247 3.784 878.095 0.932 16.831 1.954 0.52 174647. 0.1593
|
|
100.61 0.8432 0.8159 0.0317 0.0328 1.033 7.237 3.143 770.581 0.818 13.979 1.850 0.52 175463. 0.1374
|
|
104.80 0.8783 0.7933 0.0252 0.0279 0.880 6.164 2.499 656.382 0.696 11.114 1.727 0.52 176306. 0.1144
|
|
108.99 0.9135 0.7500 0.0187 0.0228 0.719 5.038 1.857 536.497 0.569 8.258 1.570 0.52 177177. 0.0896
|
|
113.19 0.9486 0.6675 0.0123 0.0175 0.553 3.870 1.222 412.088 0.437 5.436 1.345 0.52 178075. 0.0623
|
|
117.38 0.9837 0.4931 0.0061 0.0121 0.382 2.672 0.601 284.512 0.302 2.674 0.958 0.52 178999. 0.0311
|
|
121.57 1.0189 -0.0005 0.0000 0.0066 0.208 1.458 0.000 155.273 0.165 -0.001 -0.001 0.53 179948. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 10000
|
|
|
|
V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
|
|
(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
|
|
0.00 0.0000 0.0000 0.1086 0.0459 1.984 12.508 13.294 1479.816 1.413 59.134 4.075 0.56 182286. 0.6227
|
|
4.66 0.0351 0.0809 0.1082 0.0470 2.033 12.814 13.240 1516.060 1.448 58.893 3.961 0.56 182455. 0.6041
|
|
9.32 0.0703 0.1570 0.1077 0.0482 2.086 13.145 13.179 1555.234 1.485 58.621 3.844 0.56 182648. 0.5848
|
|
13.97 0.1054 0.2281 0.1071 0.0495 2.142 13.498 13.109 1596.995 1.525 58.309 3.723 0.56 182866. 0.5650
|
|
18.63 0.1405 0.2941 0.1064 0.0508 2.200 13.869 13.027 1640.863 1.567 57.944 3.601 0.56 183112. 0.5447
|
|
23.29 0.1757 0.3551 0.1056 0.0522 2.261 14.252 12.930 1686.164 1.610 57.511 3.478 0.56 183386. 0.5242
|
|
27.95 0.2108 0.4111 0.1047 0.0537 2.323 14.639 12.814 1732.013 1.654 56.995 3.356 0.56 183690. 0.5034
|
|
32.60 0.2459 0.4623 0.1035 0.0551 2.383 15.022 12.675 1777.306 1.697 56.378 3.235 0.56 184026. 0.4827
|
|
37.26 0.2811 0.5090 0.1022 0.0564 2.442 15.389 12.509 1820.731 1.739 55.640 3.116 0.56 184394. 0.4619
|
|
41.92 0.3162 0.5515 0.1006 0.0577 2.495 15.728 12.311 1860.778 1.777 54.760 3.001 0.56 184797. 0.4413
|
|
46.58 0.3513 0.5900 0.0986 0.0587 2.542 16.024 12.077 1895.773 1.810 53.719 2.889 0.56 185233. 0.4209
|
|
51.23 0.3864 0.6249 0.0964 0.0596 2.580 16.261 11.802 1923.910 1.837 52.496 2.782 0.56 185705. 0.4006
|
|
55.89 0.4216 0.6566 0.0938 0.0602 2.606 16.425 11.482 1943.296 1.856 51.071 2.680 0.56 186211. 0.3806
|
|
60.55 0.4567 0.6854 0.0908 0.0605 2.618 16.499 11.113 1952.000 1.864 49.429 2.582 0.56 186753. 0.3608
|
|
65.21 0.4918 0.7115 0.0873 0.0604 2.612 16.466 10.691 1948.138 1.860 47.554 2.489 0.56 187331. 0.3411
|
|
69.86 0.5270 0.7353 0.0834 0.0598 2.588 16.313 10.215 1929.980 1.843 45.435 2.401 0.56 187943. 0.3216
|
|
74.52 0.5621 0.7567 0.0791 0.0588 2.543 16.026 9.683 1896.091 1.811 43.069 2.316 0.56 188590. 0.3021
|
|
79.18 0.5972 0.7760 0.0743 0.0572 2.475 15.598 9.096 1845.446 1.762 40.458 2.236 0.57 189272. 0.2826
|
|
83.84 0.6324 0.7931 0.0691 0.0551 2.384 15.024 8.456 1777.536 1.697 37.614 2.158 0.57 189987. 0.2630
|
|
88.49 0.6675 0.8077 0.0635 0.0525 2.270 14.308 7.770 1692.810 1.617 34.563 2.082 0.57 190735. 0.2432
|
|
93.15 0.7026 0.8196 0.0576 0.0493 2.136 13.460 7.047 1592.517 1.521 31.345 2.007 0.57 191516. 0.2233
|
|
97.81 0.7378 0.8283 0.0514 0.0458 1.982 12.492 6.294 1478.008 1.411 27.997 1.932 0.57 192329. 0.2031
|
|
102.47 0.7729 0.8327 0.0451 0.0418 1.811 11.415 5.519 1350.520 1.290 24.550 1.854 0.57 193174. 0.1825
|
|
107.13 0.8080 0.8316 0.0386 0.0375 1.624 10.237 4.728 1211.214 1.157 21.032 1.771 0.57 194050. 0.1614
|
|
111.78 0.8432 0.8225 0.0321 0.0329 1.423 8.970 3.927 1061.253 1.013 17.469 1.678 0.57 194957. 0.1394
|
|
116.44 0.8783 0.8015 0.0255 0.0279 1.209 7.623 3.122 901.879 0.861 13.888 1.570 0.58 195894. 0.1163
|
|
121.10 0.9134 0.7604 0.0189 0.0228 0.985 6.208 2.319 734.501 0.701 10.317 1.432 0.58 196862. 0.0914
|
|
125.76 0.9486 0.6804 0.0125 0.0174 0.752 4.740 1.526 560.759 0.535 6.787 1.234 0.58 197859. 0.0639
|
|
130.41 0.9837 0.5076 0.0061 0.0119 0.513 3.234 0.749 382.568 0.365 3.331 0.888 0.58 198887. 0.0322
|
|
135.07 1.0188 -0.0047 0.0000 0.0063 0.271 1.708 -0.004 202.061 0.193 -0.016 -0.008 0.58 199941. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 11000
|
|
|
|
V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
|
|
(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
|
|
0.00 0.0000 0.0000 0.1090 0.0460 2.653 15.199 16.141 1978.063 1.717 71.794 3.701 0.61 200507. 0.6232
|
|
5.12 0.0351 0.0808 0.1086 0.0472 2.718 15.572 16.080 2026.628 1.759 71.525 3.599 0.61 200693. 0.6048
|
|
10.24 0.0702 0.1569 0.1081 0.0484 2.788 15.977 16.012 2079.249 1.805 71.221 3.493 0.61 200905. 0.5858
|
|
15.37 0.1054 0.2280 0.1076 0.0497 2.864 16.409 15.933 2135.495 1.854 70.870 3.384 0.61 201145. 0.5661
|
|
20.49 0.1405 0.2940 0.1069 0.0511 2.943 16.864 15.840 2194.744 1.905 70.458 3.274 0.61 201414. 0.5461
|
|
25.61 0.1756 0.3551 0.1062 0.0525 3.025 17.336 15.730 2256.106 1.959 69.968 3.162 0.61 201715. 0.5257
|
|
30.73 0.2107 0.4111 0.1053 0.0540 3.109 17.814 15.598 2318.399 2.013 69.378 3.052 0.61 202049. 0.5051
|
|
35.85 0.2459 0.4624 0.1042 0.0554 3.192 18.289 15.438 2380.144 2.066 68.667 2.942 0.61 202419. 0.4845
|
|
40.98 0.2810 0.5092 0.1029 0.0568 3.271 18.745 15.245 2439.555 2.118 67.809 2.834 0.61 202824. 0.4638
|
|
46.10 0.3161 0.5517 0.1014 0.0581 3.345 19.168 15.013 2494.577 2.166 66.780 2.730 0.61 203266. 0.4433
|
|
51.22 0.3512 0.5903 0.0995 0.0592 3.410 19.539 14.737 2542.909 2.208 65.552 2.629 0.61 203746. 0.4229
|
|
56.34 0.3863 0.6253 0.0973 0.0601 3.463 19.840 14.411 2582.073 2.242 64.100 2.531 0.62 204265. 0.4028
|
|
61.46 0.4215 0.6571 0.0947 0.0607 3.499 20.051 14.029 2609.469 2.265 62.401 2.438 0.62 204822. 0.3828
|
|
66.59 0.4566 0.6859 0.0917 0.0610 3.517 20.151 13.586 2622.448 2.277 60.431 2.350 0.62 205419. 0.3630
|
|
71.71 0.4917 0.7122 0.0883 0.0610 3.511 20.120 13.078 2618.419 2.273 58.173 2.265 0.62 206054. 0.3434
|
|
76.83 0.5268 0.7361 0.0844 0.0604 3.480 19.940 12.503 2595.001 2.253 55.613 2.185 0.62 206728. 0.3239
|
|
81.95 0.5620 0.7577 0.0801 0.0594 3.420 19.595 11.858 2550.211 2.214 52.745 2.109 0.62 207440. 0.3044
|
|
87.07 0.5971 0.7772 0.0752 0.0578 3.329 19.076 11.145 2482.633 2.155 49.573 2.036 0.62 208190. 0.2849
|
|
92.20 0.6322 0.7946 0.0700 0.0557 3.207 18.376 10.366 2391.541 2.076 46.108 1.966 0.62 208977. 0.2653
|
|
97.32 0.6673 0.8097 0.0643 0.0530 3.054 17.500 9.529 2277.495 1.977 42.386 1.898 0.62 209801. 0.2455
|
|
102.44 0.7024 0.8221 0.0584 0.0499 2.873 16.460 8.645 2142.170 1.860 38.455 1.831 0.63 210660. 0.2256
|
|
107.56 0.7376 0.8313 0.0521 0.0463 2.665 15.271 7.724 1987.403 1.725 34.358 1.763 0.63 211555. 0.2054
|
|
112.68 0.7727 0.8365 0.0457 0.0422 2.434 13.945 6.775 1814.881 1.576 30.137 1.693 0.63 212484. 0.1847
|
|
117.81 0.8078 0.8363 0.0392 0.0379 2.181 12.495 5.806 1626.186 1.412 25.824 1.619 0.63 213447. 0.1635
|
|
122.93 0.8429 0.8285 0.0326 0.0331 1.908 10.933 4.823 1422.902 1.235 21.453 1.537 0.63 214445. 0.1415
|
|
128.05 0.8780 0.8091 0.0259 0.0281 1.618 9.272 3.835 1206.729 1.048 17.057 1.441 0.63 215476. 0.1183
|
|
133.17 0.9132 0.7701 0.0192 0.0228 1.314 7.527 2.849 979.590 0.850 12.672 1.319 0.64 216540. 0.0933
|
|
138.29 0.9483 0.6928 0.0126 0.0173 0.997 5.715 1.874 743.728 0.646 8.334 1.143 0.64 217637. 0.0656
|
|
143.41 0.9834 0.5222 0.0062 0.0117 0.673 3.856 0.919 501.782 0.436 4.087 0.831 0.64 218766. 0.0334
|
|
148.54 1.0185 -0.0069 0.0000 0.0060 0.344 1.972 -0.006 256.688 0.223 -0.027 -0.011 0.64 219925. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 12000
|
|
|
|
V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
|
|
(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
|
|
0.00 0.0000 0.0000 0.1093 0.0464 3.473 18.243 19.277 2589.979 2.061 85.745 3.376 0.67 218727. 0.6212
|
|
5.58 0.0351 0.0804 0.1090 0.0476 3.557 18.684 19.212 2652.695 2.111 85.454 3.285 0.67 218929. 0.6035
|
|
11.17 0.0702 0.1562 0.1086 0.0488 3.649 19.165 19.138 2720.870 2.165 85.126 3.190 0.67 219159. 0.5850
|
|
16.75 0.1053 0.2272 0.1081 0.0501 3.747 19.680 19.053 2794.006 2.223 84.747 3.093 0.67 219420. 0.5658
|
|
22.34 0.1404 0.2932 0.1075 0.0515 3.851 20.224 18.952 2871.354 2.285 84.299 2.994 0.67 219714. 0.5462
|
|
27.92 0.1755 0.3542 0.1068 0.0529 3.958 20.791 18.831 2951.806 2.349 83.761 2.894 0.67 220041. 0.5263
|
|
33.51 0.2106 0.4104 0.1060 0.0544 4.068 21.369 18.684 3033.867 2.414 83.109 2.793 0.67 220406. 0.5061
|
|
39.09 0.2457 0.4617 0.1050 0.0559 4.178 21.945 18.506 3115.624 2.479 82.314 2.694 0.67 220808. 0.4857
|
|
44.68 0.2808 0.5086 0.1037 0.0573 4.284 22.502 18.288 3194.744 2.542 81.345 2.596 0.67 221249. 0.4654
|
|
50.26 0.3159 0.5512 0.1022 0.0586 4.383 23.022 18.024 3268.490 2.601 80.171 2.501 0.67 221731. 0.4451
|
|
55.85 0.3510 0.5898 0.1004 0.0598 4.471 23.482 17.706 3333.776 2.653 78.758 2.409 0.67 222255. 0.4249
|
|
61.43 0.3862 0.6249 0.0983 0.0607 4.542 23.858 17.328 3387.226 2.695 77.074 2.320 0.67 222820. 0.4048
|
|
67.02 0.4213 0.6568 0.0958 0.0614 4.593 24.126 16.881 3425.285 2.726 75.089 2.235 0.67 223428. 0.3849
|
|
72.60 0.4564 0.6858 0.0928 0.0618 4.619 24.260 16.361 3444.342 2.741 72.773 2.154 0.67 224079. 0.3652
|
|
78.19 0.4915 0.7121 0.0894 0.0617 4.614 24.236 15.761 3440.896 2.738 70.105 2.078 0.67 224772. 0.3457
|
|
83.77 0.5266 0.7362 0.0855 0.0612 4.575 24.031 15.078 3411.737 2.715 67.067 2.005 0.68 225507. 0.3262
|
|
89.36 0.5617 0.7581 0.0812 0.0601 4.498 23.625 14.310 3354.184 2.669 63.651 1.935 0.68 226284. 0.3068
|
|
94.94 0.5968 0.7778 0.0763 0.0586 4.380 23.006 13.458 3266.306 2.599 59.860 1.869 0.68 227102. 0.2873
|
|
100.53 0.6319 0.7955 0.0710 0.0564 4.220 22.167 12.525 3147.108 2.504 55.710 1.805 0.68 227961. 0.2677
|
|
106.11 0.6670 0.8110 0.0653 0.0537 4.019 21.111 11.520 2997.248 2.385 51.241 1.743 0.68 228860. 0.2480
|
|
111.70 0.7021 0.8239 0.0593 0.0505 3.780 19.855 10.457 2818.917 2.243 46.511 1.682 0.68 229797. 0.2280
|
|
117.28 0.7372 0.8337 0.0530 0.0469 3.506 18.416 9.347 2614.558 2.081 41.575 1.622 0.68 230773. 0.2078
|
|
122.87 0.7723 0.8397 0.0465 0.0428 3.200 16.809 8.202 2386.428 1.899 36.482 1.559 0.69 231787. 0.1871
|
|
128.45 0.8074 0.8405 0.0399 0.0383 2.865 15.049 7.031 2136.635 1.700 31.273 1.493 0.69 232838. 0.1659
|
|
134.04 0.8425 0.8340 0.0331 0.0335 2.504 13.152 5.843 1867.290 1.486 25.989 1.419 0.69 233926. 0.1438
|
|
139.62 0.8776 0.8162 0.0264 0.0283 2.120 11.133 4.647 1580.668 1.258 20.670 1.333 0.69 235050. 0.1205
|
|
145.21 0.9127 0.7793 0.0196 0.0229 1.716 9.011 3.453 1279.370 1.018 15.360 1.224 0.69 236210. 0.0953
|
|
150.79 0.9478 0.7047 0.0129 0.0173 1.296 6.808 2.272 966.489 0.769 10.104 1.066 0.70 237406. 0.0673
|
|
156.38 0.9829 0.5363 0.0063 0.0116 0.866 4.548 1.114 645.759 0.514 4.954 0.782 0.70 238637. 0.0346
|
|
161.96 1.0180 -0.0079 0.0000 0.0058 0.431 2.264 -0.008 321.447 0.256 -0.035 -0.011 0.70 239900. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 13000
|
|
|
|
V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
|
|
(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
|
|
0.00 0.0000 0.0000 0.1097 0.0475 4.515 21.890 22.704 3366.857 2.473 100.985 3.059 0.72 236943. 0.6108
|
|
6.05 0.0351 0.0790 0.1094 0.0486 4.619 22.397 22.635 3444.724 2.530 100.682 2.980 0.72 237162. 0.5943
|
|
12.09 0.0701 0.1537 0.1090 0.0498 4.733 22.948 22.559 3529.564 2.593 100.341 2.899 0.72 237411. 0.5771
|
|
18.14 0.1052 0.2238 0.1086 0.0511 4.856 23.541 22.470 3620.786 2.660 99.947 2.815 0.72 237692. 0.5592
|
|
24.18 0.1403 0.2893 0.1081 0.0524 4.985 24.170 22.365 3717.474 2.731 99.479 2.729 0.72 238009. 0.5409
|
|
30.23 0.1754 0.3500 0.1075 0.0539 5.120 24.825 22.237 3818.275 2.805 98.912 2.642 0.72 238364. 0.5221
|
|
36.27 0.2104 0.4061 0.1067 0.0553 5.259 25.495 22.081 3921.330 2.880 98.216 2.554 0.72 238757. 0.5030
|
|
42.32 0.2455 0.4577 0.1058 0.0568 5.397 26.165 21.888 4024.268 2.956 97.358 2.467 0.72 239192. 0.4837
|
|
48.36 0.2806 0.5048 0.1046 0.0582 5.531 26.814 21.650 4124.159 3.029 96.299 2.381 0.72 239669. 0.4643
|
|
54.41 0.3157 0.5478 0.1032 0.0595 5.656 27.422 21.358 4217.579 3.098 94.999 2.297 0.73 240191. 0.4449
|
|
60.45 0.3507 0.5870 0.1015 0.0607 5.767 27.962 21.002 4300.653 3.159 93.416 2.215 0.73 240757. 0.4254
|
|
66.50 0.3858 0.6226 0.0994 0.0616 5.859 28.407 20.573 4369.121 3.209 91.509 2.136 0.73 241369. 0.4060
|
|
72.54 0.4209 0.6550 0.0970 0.0623 5.925 28.728 20.063 4418.473 3.246 89.239 2.060 0.73 242027. 0.3866
|
|
78.59 0.4560 0.6844 0.0941 0.0627 5.960 28.894 19.463 4444.029 3.264 86.571 1.986 0.73 242731. 0.3673
|
|
84.63 0.4910 0.7111 0.0907 0.0626 5.956 28.875 18.767 4441.146 3.262 83.475 1.917 0.73 243482. 0.3480
|
|
90.68 0.5261 0.7355 0.0869 0.0621 5.908 28.643 17.970 4405.444 3.236 79.930 1.850 0.73 244278. 0.3287
|
|
96.72 0.5612 0.7576 0.0825 0.0611 5.811 28.173 17.069 4333.152 3.183 75.924 1.787 0.73 245119. 0.3094
|
|
102.77 0.5963 0.7777 0.0777 0.0595 5.661 27.447 16.066 4221.459 3.101 71.461 1.726 0.73 246006. 0.2900
|
|
108.81 0.6313 0.7957 0.0723 0.0574 5.456 26.454 14.964 4068.805 2.989 66.559 1.668 0.74 246936. 0.2704
|
|
114.86 0.6664 0.8116 0.0666 0.0547 5.198 25.200 13.774 3875.890 2.847 61.265 1.612 0.74 247909. 0.2507
|
|
120.90 0.7015 0.8250 0.0605 0.0514 4.889 23.702 12.511 3645.509 2.678 55.649 1.557 0.74 248924. 0.2308
|
|
126.95 0.7366 0.8355 0.0541 0.0477 4.534 21.981 11.191 3380.867 2.483 49.777 1.501 0.74 249981. 0.2105
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132.99 0.7716 0.8423 0.0475 0.0435 4.137 20.058 9.826 3084.959 2.266 43.707 1.445 0.74 251078. 0.1898
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139.04 0.8067 0.8441 0.0407 0.0389 3.702 17.949 8.429 2760.636 2.028 37.491 1.385 0.75 252216. 0.1685
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|
145.08 0.8418 0.8387 0.0339 0.0340 3.233 15.674 7.009 2410.819 1.771 31.177 1.319 0.75 253393. 0.1463
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151.13 0.8769 0.8222 0.0270 0.0288 2.734 13.256 5.578 2038.786 1.498 24.813 1.241 0.75 254610. 0.1228
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|
157.17 0.9119 0.7865 0.0200 0.0232 2.211 10.718 4.148 1648.412 1.211 18.451 1.141 0.75 255865. 0.0974
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163.22 0.9470 0.7122 0.0132 0.0176 1.669 8.091 2.731 1244.402 0.914 12.146 0.995 0.75 257159. 0.0689
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169.26 0.9821 0.5419 0.0065 0.0117 1.116 5.412 1.340 832.451 0.611 5.961 0.730 0.76 258491. 0.0354
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|
175.31 1.0172 -0.0075 0.0000 0.0059 0.562 2.724 -0.009 419.034 0.308 -0.040 -0.010 0.76 259858. 0.0000
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PROP RPM = 14000
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V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
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(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
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0.00 0.0000 0.0000 0.1101 0.0498 5.919 26.646 26.414 4413.596 3.010 117.491 2.715 0.78 255157. 0.5847
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6.50 0.0350 0.0756 0.1098 0.0509 6.045 27.213 26.345 4507.519 3.075 117.184 2.651 0.78 255391. 0.5703
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13.00 0.0701 0.1473 0.1095 0.0521 6.182 27.832 26.269 4609.947 3.144 116.843 2.585 0.78 255658. 0.5552
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|
19.50 0.1051 0.2151 0.1091 0.0533 6.330 28.497 26.180 4720.132 3.220 116.449 2.516 0.78 255961. 0.5395
|
|
26.01 0.1401 0.2788 0.1087 0.0546 6.486 29.202 26.075 4836.907 3.299 115.980 2.445 0.78 256300. 0.5233
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|
32.51 0.1751 0.3382 0.1081 0.0560 6.650 29.936 25.946 4958.538 3.382 115.407 2.373 0.78 256680. 0.5067
|
|
39.01 0.2102 0.3935 0.1075 0.0574 6.816 30.686 25.786 5082.651 3.467 114.695 2.301 0.78 257103. 0.4897
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|
45.51 0.2452 0.4447 0.1066 0.0588 6.982 31.431 25.585 5206.187 3.551 113.804 2.229 0.78 257569. 0.4726
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|
52.01 0.2802 0.4920 0.1056 0.0601 7.142 32.151 25.334 5325.434 3.632 112.687 2.158 0.78 258082. 0.4552
|
|
58.51 0.3152 0.5355 0.1043 0.0614 7.290 32.819 25.021 5436.061 3.708 111.294 2.088 0.78 258642. 0.4377
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|
65.01 0.3503 0.5755 0.1027 0.0625 7.420 33.406 24.634 5533.232 3.774 109.574 2.019 0.78 259250. 0.4201
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|
71.51 0.3853 0.6123 0.1007 0.0634 7.525 33.880 24.162 5611.729 3.828 107.473 1.953 0.78 259908. 0.4023
|
|
78.02 0.4203 0.6459 0.0983 0.0640 7.598 34.208 23.593 5666.063 3.865 104.942 1.889 0.78 260615. 0.3845
|
|
84.52 0.4554 0.6768 0.0955 0.0643 7.631 34.356 22.917 5690.630 3.882 101.936 1.827 0.79 261372. 0.3665
|
|
91.02 0.4904 0.7050 0.0922 0.0641 7.617 34.291 22.126 5679.895 3.874 98.415 1.767 0.79 262179. 0.3483
|
|
97.52 0.5254 0.7308 0.0884 0.0636 7.548 33.982 21.212 5628.636 3.839 94.352 1.709 0.79 263036. 0.3300
|
|
104.02 0.5604 0.7542 0.0841 0.0625 7.419 33.400 20.173 5532.293 3.774 89.731 1.654 0.79 263941. 0.3113
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|
110.52 0.5955 0.7755 0.0792 0.0608 7.225 32.525 19.010 5387.360 3.675 84.555 1.600 0.79 264894. 0.2925
|
|
117.02 0.6305 0.7945 0.0739 0.0586 6.962 31.344 17.725 5191.668 3.541 78.843 1.549 0.79 265895. 0.2733
|
|
123.52 0.6655 0.8112 0.0681 0.0558 6.632 29.858 16.333 4945.515 3.373 72.648 1.498 0.79 266942. 0.2537
|
|
130.03 0.7005 0.8253 0.0619 0.0525 6.239 28.086 14.850 4652.146 3.173 66.054 1.448 0.80 268034. 0.2338
|
|
136.53 0.7356 0.8364 0.0554 0.0487 5.787 26.053 13.296 4315.382 2.943 59.141 1.397 0.80 269171. 0.2136
|
|
143.03 0.7706 0.8437 0.0487 0.0445 5.282 23.781 11.686 3939.054 2.687 51.980 1.346 0.80 270351. 0.1928
|
|
149.53 0.8056 0.8459 0.0418 0.0398 4.730 21.294 10.034 3527.079 2.406 44.631 1.290 0.80 271575. 0.1713
|
|
156.03 0.8407 0.8403 0.0348 0.0348 4.136 18.618 8.353 3083.892 2.103 37.153 1.228 0.80 272841. 0.1488
|
|
162.53 0.8757 0.8226 0.0277 0.0295 3.506 15.786 6.655 2614.775 1.784 29.602 1.154 0.81 274149. 0.1248
|
|
169.03 0.9107 0.7833 0.0206 0.0240 2.851 12.835 4.954 2125.967 1.450 22.037 1.057 0.81 275498. 0.0986
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|
175.53 0.9457 0.7015 0.0136 0.0183 2.179 9.810 3.265 1624.863 1.108 14.525 0.912 0.81 276889. 0.0690
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|
182.04 0.9808 0.5186 0.0067 0.0126 1.502 6.763 1.605 1120.246 0.764 7.139 0.650 0.81 278320. 0.0345
|
|
188.54 1.0158 -0.0061 0.0000 0.0070 0.833 3.752 -0.010 621.502 0.424 -0.045 -0.007 0.82 279789. 0.0000
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