575 lines
102 KiB
Plaintext
575 lines
102 KiB
Plaintext
16x6 (16x6.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 0.0762 0.0316 0.003 0.168 0.159 1.990 0.019 0.707 36.248 0.06 30524. 0.5301
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0.28 0.0182 0.0429 0.0745 0.0317 0.003 0.169 0.156 1.994 0.019 0.693 35.410 0.06 30539. 0.5124
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0.55 0.0365 0.0837 0.0729 0.0317 0.003 0.169 0.152 1.997 0.019 0.677 34.565 0.06 30555. 0.4945
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0.83 0.0547 0.1225 0.0711 0.0317 0.003 0.169 0.148 1.997 0.019 0.660 33.713 0.06 30572. 0.4764
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1.11 0.0729 0.1592 0.0692 0.0317 0.003 0.169 0.145 1.996 0.019 0.643 32.856 0.06 30590. 0.4582
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1.38 0.0912 0.1937 0.0673 0.0317 0.003 0.168 0.141 1.993 0.019 0.625 31.992 0.06 30609. 0.4399
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1.66 0.1094 0.2262 0.0653 0.0316 0.003 0.168 0.136 1.987 0.019 0.606 31.122 0.06 30628. 0.4214
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1.93 0.1276 0.2564 0.0632 0.0314 0.003 0.167 0.132 1.979 0.019 0.587 30.244 0.06 30649. 0.4029
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2.21 0.1459 0.2845 0.0610 0.0313 0.003 0.166 0.127 1.968 0.019 0.566 29.359 0.06 30671. 0.3842
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2.49 0.1641 0.3103 0.0587 0.0311 0.003 0.165 0.123 1.954 0.019 0.545 28.464 0.06 30694. 0.3655
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2.76 0.1823 0.3338 0.0564 0.0308 0.003 0.164 0.118 1.937 0.018 0.524 27.559 0.06 30718. 0.3468
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3.04 0.2006 0.3550 0.0539 0.0305 0.003 0.162 0.113 1.918 0.018 0.501 26.642 0.06 30743. 0.3279
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3.32 0.2188 0.3737 0.0514 0.0301 0.003 0.160 0.107 1.895 0.018 0.478 25.711 0.06 30770. 0.3090
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3.59 0.2371 0.3899 0.0489 0.0297 0.003 0.158 0.102 1.869 0.018 0.454 24.763 0.06 30798. 0.2901
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3.87 0.2553 0.4035 0.0462 0.0292 0.002 0.155 0.097 1.840 0.018 0.429 23.795 0.06 30826. 0.2711
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4.14 0.2735 0.4143 0.0435 0.0287 0.002 0.153 0.091 1.807 0.017 0.404 22.803 0.06 30857. 0.2520
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4.42 0.2918 0.4222 0.0407 0.0281 0.002 0.150 0.085 1.770 0.017 0.378 21.784 0.06 30888. 0.2329
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4.70 0.3100 0.4269 0.0379 0.0275 0.002 0.146 0.079 1.730 0.017 0.352 20.731 0.06 30921. 0.2138
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4.97 0.3282 0.4281 0.0350 0.0268 0.002 0.143 0.073 1.686 0.016 0.325 19.638 0.06 30955. 0.1946
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5.25 0.3465 0.4257 0.0320 0.0260 0.002 0.138 0.067 1.638 0.016 0.297 18.497 0.06 30990. 0.1753
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5.53 0.3647 0.4190 0.0290 0.0252 0.002 0.134 0.061 1.586 0.015 0.269 17.298 0.06 31026. 0.1560
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5.80 0.3829 0.4077 0.0259 0.0243 0.002 0.129 0.054 1.530 0.015 0.241 16.028 0.06 31064. 0.1367
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6.08 0.4012 0.3910 0.0228 0.0234 0.002 0.124 0.048 1.470 0.014 0.212 14.673 0.06 31104. 0.1174
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6.35 0.4194 0.3681 0.0196 0.0223 0.002 0.119 0.041 1.406 0.013 0.182 13.212 0.06 31145. 0.0980
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6.63 0.4376 0.3378 0.0164 0.0213 0.002 0.113 0.034 1.337 0.013 0.152 11.620 0.06 31187. 0.0789
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6.91 0.4559 0.2987 0.0132 0.0201 0.002 0.107 0.027 1.264 0.012 0.122 9.865 0.06 31230. 0.0600
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7.18 0.4741 0.2488 0.0099 0.0189 0.002 0.100 0.021 1.187 0.011 0.092 7.901 0.06 31275. 0.0417
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7.46 0.4923 0.1854 0.0066 0.0176 0.001 0.093 0.014 1.106 0.011 0.061 5.670 0.06 31322. 0.0244
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7.74 0.5106 0.1046 0.0033 0.0162 0.001 0.086 0.007 1.021 0.010 0.031 3.086 0.06 31369. 0.0094
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8.01 0.5288 0.0004 0.0000 0.0148 0.001 0.079 0.000 0.931 0.009 0.000 0.011 0.06 31416. 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 0.0765 0.0274 0.019 0.583 0.639 13.798 0.066 2.844 21.017 0.13 61048. 0.6163
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0.56 0.0184 0.0500 0.0749 0.0275 0.019 0.585 0.626 13.844 0.066 2.784 20.507 0.13 61078. 0.5950
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1.11 0.0367 0.0975 0.0732 0.0276 0.019 0.586 0.612 13.876 0.066 2.721 19.996 0.13 61110. 0.5735
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1.67 0.0551 0.1426 0.0714 0.0276 0.019 0.587 0.597 13.893 0.066 2.655 19.486 0.13 61144. 0.5521
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2.22 0.0734 0.1851 0.0696 0.0276 0.019 0.587 0.581 13.893 0.066 2.586 18.977 0.13 61180. 0.5306
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2.78 0.0918 0.2252 0.0676 0.0276 0.019 0.586 0.565 13.875 0.066 2.513 18.470 0.13 61218. 0.5091
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3.34 0.1101 0.2628 0.0656 0.0275 0.019 0.585 0.548 13.838 0.066 2.438 17.963 0.13 61258. 0.4876
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3.89 0.1285 0.2980 0.0635 0.0274 0.018 0.582 0.530 13.778 0.066 2.359 17.456 0.13 61300. 0.4662
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4.45 0.1468 0.3307 0.0613 0.0272 0.018 0.579 0.512 13.697 0.065 2.277 16.950 0.13 61344. 0.4447
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5.01 0.1652 0.3609 0.0590 0.0270 0.018 0.574 0.493 13.591 0.065 2.192 16.444 0.13 61391. 0.4233
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5.56 0.1836 0.3886 0.0566 0.0267 0.018 0.569 0.473 13.461 0.064 2.104 15.937 0.13 61439. 0.4019
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6.12 0.2019 0.4138 0.0542 0.0264 0.018 0.562 0.453 13.305 0.064 2.013 15.427 0.13 61490. 0.3806
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6.67 0.2203 0.4364 0.0516 0.0261 0.018 0.555 0.431 13.122 0.063 1.919 14.914 0.13 61544. 0.3593
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7.23 0.2386 0.4564 0.0491 0.0256 0.017 0.546 0.410 12.910 0.062 1.823 14.397 0.13 61600. 0.3380
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7.79 0.2570 0.4736 0.0464 0.0252 0.017 0.535 0.388 12.670 0.060 1.724 13.873 0.13 61658. 0.3167
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8.34 0.2753 0.4880 0.0437 0.0246 0.017 0.524 0.365 12.398 0.059 1.622 13.341 0.13 61719. 0.2954
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8.90 0.2937 0.4993 0.0408 0.0240 0.016 0.511 0.341 12.095 0.058 1.518 12.797 0.13 61782. 0.2742
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9.46 0.3120 0.5073 0.0380 0.0234 0.016 0.497 0.317 11.760 0.056 1.411 12.239 0.13 61848. 0.2528
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10.01 0.3304 0.5119 0.0351 0.0226 0.015 0.481 0.293 11.391 0.054 1.303 11.661 0.13 61917. 0.2314
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10.57 0.3488 0.5124 0.0321 0.0218 0.015 0.464 0.268 10.987 0.052 1.192 11.060 0.13 61989. 0.2099
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11.12 0.3671 0.5086 0.0290 0.0210 0.014 0.446 0.243 10.548 0.050 1.079 10.428 0.13 62063. 0.1883
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11.68 0.3855 0.4997 0.0259 0.0200 0.014 0.426 0.217 10.073 0.048 0.964 9.757 0.13 62140. 0.1666
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12.24 0.4038 0.4847 0.0228 0.0190 0.013 0.404 0.190 9.561 0.046 0.847 9.036 0.13 62219. 0.1446
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12.79 0.4222 0.4626 0.0196 0.0179 0.012 0.381 0.164 9.013 0.043 0.729 8.249 0.13 62302. 0.1225
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13.35 0.4405 0.4316 0.0164 0.0167 0.011 0.356 0.137 8.427 0.040 0.609 7.375 0.13 62387. 0.1001
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13.91 0.4589 0.3894 0.0132 0.0155 0.010 0.330 0.110 7.803 0.037 0.489 6.387 0.13 62476. 0.0776
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14.46 0.4773 0.3323 0.0099 0.0142 0.010 0.302 0.083 7.143 0.034 0.367 5.241 0.13 62567. 0.0552
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15.02 0.4956 0.2550 0.0066 0.0128 0.009 0.272 0.055 6.447 0.031 0.245 3.873 0.13 62660. 0.0333
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15.57 0.5140 0.1489 0.0033 0.0114 0.008 0.241 0.027 5.714 0.027 0.122 2.181 0.13 62756. 0.0133
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16.13 0.5323 -0.0023 0.0000 0.0098 0.007 0.209 0.000 4.940 0.024 -0.002 -0.032 0.13 62848. 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 0.0769 0.0257 0.059 1.231 1.445 43.690 0.139 6.427 15.000 0.19 91570. 0.6613
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0.84 0.0186 0.0541 0.0752 0.0258 0.059 1.236 1.414 43.862 0.140 6.290 14.624 0.19 91616. 0.6378
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1.69 0.0372 0.1055 0.0735 0.0259 0.059 1.239 1.382 43.987 0.140 6.147 14.249 0.19 91665. 0.6143
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2.53 0.0557 0.1541 0.0717 0.0259 0.059 1.241 1.348 44.060 0.140 5.996 13.876 0.19 91717. 0.5908
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3.38 0.0743 0.2000 0.0698 0.0259 0.059 1.242 1.312 44.073 0.140 5.837 13.506 0.19 91772. 0.5674
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4.22 0.0929 0.2432 0.0678 0.0259 0.059 1.240 1.275 44.021 0.140 5.672 13.138 0.19 91829. 0.5441
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5.07 0.1115 0.2837 0.0658 0.0258 0.059 1.237 1.236 43.898 0.140 5.499 12.773 0.19 91890. 0.5208
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5.91 0.1301 0.3216 0.0636 0.0257 0.059 1.231 1.196 43.700 0.139 5.318 12.410 0.19 91955. 0.4976
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6.76 0.1486 0.3569 0.0614 0.0256 0.058 1.223 1.153 43.422 0.138 5.131 12.049 0.19 92022. 0.4746
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7.60 0.1672 0.3895 0.0590 0.0253 0.058 1.213 1.110 43.060 0.137 4.936 11.689 0.19 92093. 0.4516
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8.44 0.1858 0.4195 0.0566 0.0251 0.057 1.200 1.064 42.609 0.136 4.735 11.331 0.19 92167. 0.4287
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9.29 0.2044 0.4469 0.0541 0.0248 0.056 1.185 1.018 42.066 0.134 4.527 10.973 0.19 92245. 0.4059
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10.13 0.2229 0.4715 0.0516 0.0244 0.056 1.167 0.969 41.426 0.132 4.312 10.614 0.19 92327. 0.3833
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10.98 0.2415 0.4935 0.0489 0.0239 0.055 1.146 0.920 40.684 0.130 4.091 10.254 0.19 92413. 0.3606
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11.82 0.2601 0.5127 0.0462 0.0234 0.053 1.122 0.869 39.838 0.127 3.864 9.891 0.19 92502. 0.3381
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12.67 0.2787 0.5289 0.0434 0.0229 0.052 1.095 0.816 38.881 0.124 3.631 9.524 0.19 92595. 0.3156
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13.51 0.2973 0.5420 0.0406 0.0223 0.051 1.065 0.763 37.812 0.120 3.393 9.150 0.19 92692. 0.2931
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14.36 0.3158 0.5518 0.0377 0.0216 0.049 1.032 0.708 36.625 0.117 3.149 8.767 0.19 92793. 0.2705
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15.20 0.3344 0.5579 0.0347 0.0208 0.047 0.995 0.652 35.317 0.112 2.900 8.372 0.19 92899. 0.2479
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16.05 0.3530 0.5600 0.0316 0.0199 0.045 0.955 0.595 33.885 0.108 2.646 7.962 0.19 93008. 0.2252
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16.89 0.3716 0.5575 0.0286 0.0190 0.043 0.911 0.537 32.327 0.103 2.387 7.530 0.19 93122. 0.2023
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17.73 0.3902 0.5496 0.0254 0.0180 0.041 0.863 0.478 30.638 0.098 2.124 7.070 0.19 93240. 0.1792
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18.58 0.4087 0.5353 0.0222 0.0170 0.039 0.812 0.418 28.819 0.092 1.857 6.572 0.19 93362. 0.1557
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19.42 0.4273 0.5129 0.0190 0.0158 0.036 0.757 0.357 26.866 0.086 1.587 6.024 0.19 93488. 0.1320
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20.27 0.4459 0.4804 0.0157 0.0146 0.033 0.698 0.295 24.780 0.079 1.314 5.406 0.19 93619. 0.1078
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21.11 0.4645 0.4343 0.0124 0.0133 0.030 0.636 0.233 22.562 0.072 1.038 4.692 0.19 93754. 0.0831
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21.96 0.4830 0.3693 0.0091 0.0119 0.027 0.569 0.171 20.212 0.064 0.760 3.837 0.19 93894. 0.0582
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22.80 0.5016 0.2769 0.0058 0.0104 0.024 0.500 0.108 17.733 0.056 0.482 2.770 0.19 94037. 0.0334
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23.65 0.5202 0.1413 0.0024 0.0089 0.020 0.426 0.045 15.125 0.048 0.202 1.363 0.19 94184. 0.0107
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24.49 0.5388
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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 0.0773 0.0248 0.134 2.112 2.582 99.959 0.239 11.484 11.716 0.25 122090. 0.6904
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1.12 0.0184 0.0559 0.0756 0.0249 0.135 2.121 2.528 100.384 0.240 11.243 11.420 0.25 122152. 0.6659
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2.23 0.0369 0.1090 0.0739 0.0250 0.135 2.128 2.470 100.699 0.240 10.988 11.127 0.25 122216. 0.6414
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3.35 0.0553 0.1592 0.0721 0.0251 0.135 2.132 2.410 100.888 0.241 10.722 10.837 0.25 122285. 0.6170
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4.47 0.0737 0.2067 0.0703 0.0251 0.135 2.133 2.348 100.938 0.241 10.442 10.549 0.25 122357. 0.5927
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5.59 0.0922 0.2514 0.0683 0.0250 0.135 2.131 2.282 100.835 0.241 10.149 10.264 0.25 122434. 0.5686
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6.70 0.1106 0.2933 0.0662 0.0250 0.135 2.125 2.213 100.565 0.240 9.844 9.981 0.25 122514. 0.5445
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7.82 0.1290 0.3326 0.0641 0.0249 0.134 2.116 2.141 100.117 0.239 9.525 9.701 0.25 122599. 0.5206
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8.94 0.1475 0.3693 0.0619 0.0247 0.133 2.102 2.067 99.479 0.237 9.194 9.424 0.25 122689. 0.4969
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10.06 0.1659 0.4033 0.0595 0.0245 0.132 2.084 1.990 98.642 0.235 8.850 9.149 0.25 122782. 0.4733
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11.17 0.1843 0.4347 0.0571 0.0242 0.131 2.062 1.910 97.595 0.233 8.494 8.875 0.25 122881. 0.4498
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12.29 0.2028 0.4635 0.0547 0.0239 0.129 2.035 1.827 96.329 0.230 8.127 8.603 0.25 122984. 0.4264
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13.41 0.2212 0.4897 0.0521 0.0235 0.127 2.004 1.742 94.833 0.226 7.748 8.331 0.25 123091. 0.4032
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14.52 0.2397 0.5132 0.0495 0.0231 0.125 1.967 1.654 93.098 0.222 7.358 8.060 0.25 123204. 0.3801
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15.64 0.2581 0.5340 0.0468 0.0226 0.122 1.925 1.564 91.112 0.218 6.958 7.787 0.25 123322. 0.3571
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16.76 0.2765 0.5519 0.0440 0.0221 0.119 1.878 1.472 88.867 0.212 6.547 7.512 0.25 123445. 0.3342
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17.88 0.2950 0.5669 0.0412 0.0214 0.116 1.825 1.377 86.354 0.206 6.126 7.233 0.25 123573. 0.3113
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18.99 0.3134 0.5787 0.0383 0.0208 0.112 1.766 1.280 83.562 0.199 5.695 6.950 0.26 123706. 0.2884
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20.11 0.3318 0.5870 0.0354 0.0200 0.108 1.701 1.182 80.483 0.192 5.255 6.658 0.26 123844. 0.2654
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21.23 0.3503 0.5916 0.0323 0.0191 0.103 1.629 1.081 77.110 0.184 4.807 6.357 0.26 123988. 0.2423
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22.35 0.3687 0.5918 0.0293 0.0182 0.098 1.552 0.978 73.435 0.175 4.350 6.041 0.26 124138. 0.2191
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23.46 0.3871 0.5869 0.0261 0.0172 0.093 1.468 0.874 69.453 0.166 3.886 5.706 0.26 124293. 0.1956
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24.58 0.4056 0.5760 0.0230 0.0162 0.087 1.377 0.768 65.158 0.156 3.415 5.345 0.26 124454. 0.1718
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25.70 0.4240 0.5575 0.0198 0.0150 0.081 1.279 0.661 60.547 0.145 2.938 4.948 0.26 124620. 0.1475
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26.81 0.4424 0.5292 0.0165 0.0138 0.075 1.175 0.552 55.618 0.133 2.456 4.502 0.26 124792. 0.1227
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27.93 0.4609 0.4879 0.0132 0.0125 0.068 1.064 0.443 50.373 0.120 1.968 3.985 0.26 124970. 0.0972
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29.05 0.4793 0.4282 0.0099 0.0111 0.060 0.947 0.332 44.813 0.107 1.478 3.363 0.26 125154. 0.0711
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30.17 0.4977 0.3410 0.0066 0.0097 0.052 0.823 0.221 38.945 0.093 0.985 2.579 0.26 125343. 0.0445
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31.28 0.5162 0.2094 0.0033 0.0081 0.044 0.692 0.110 32.772 0.078 0.491 1.527 0.26 125536. 0.0186
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32.40 0.5346 -0.0067 -0.0001 0.0065 0.035 0.553 -0.003 26.182 0.063 -0.012 -0.047 0.26 125708. 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 0.0777 0.0243 0.256 3.233 4.059 191.243 0.365 18.056 9.627 0.32 152608. 0.7113
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1.40 0.0184 0.0574 0.0761 0.0244 0.258 3.247 3.974 192.095 0.367 17.676 9.383 0.32 152685. 0.6860
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2.79 0.0369 0.1119 0.0744 0.0245 0.258 3.258 3.884 192.728 0.368 17.277 9.141 0.32 152766. 0.6607
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4.19 0.0553 0.1635 0.0726 0.0246 0.259 3.264 3.790 193.114 0.369 16.859 8.902 0.32 152852. 0.6356
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5.59 0.0737 0.2122 0.0707 0.0246 0.259 3.266 3.692 193.224 0.369 16.420 8.665 0.32 152943. 0.6106
|
|
6.98 0.0922 0.2581 0.0687 0.0245 0.259 3.263 3.588 193.030 0.369 15.961 8.431 0.32 153039. 0.5857
|
|
8.38 0.1106 0.3012 0.0667 0.0245 0.258 3.254 3.480 192.507 0.368 15.481 8.200 0.32 153140. 0.5610
|
|
9.77 0.1290 0.3416 0.0645 0.0244 0.257 3.239 3.368 191.630 0.366 14.981 7.972 0.32 153246. 0.5365
|
|
11.17 0.1475 0.3793 0.0623 0.0242 0.255 3.218 3.251 190.377 0.364 14.461 7.745 0.32 153358. 0.5122
|
|
12.57 0.1659 0.4144 0.0599 0.0240 0.253 3.190 3.130 188.730 0.360 13.921 7.522 0.32 153475. 0.4880
|
|
13.96 0.1843 0.4469 0.0575 0.0237 0.250 3.156 3.004 186.667 0.357 13.363 7.300 0.32 153598. 0.4640
|
|
15.36 0.2028 0.4767 0.0551 0.0234 0.247 3.113 2.875 184.168 0.352 12.786 7.079 0.32 153727. 0.4402
|
|
16.76 0.2212 0.5039 0.0525 0.0230 0.243 3.063 2.741 181.214 0.346 12.191 6.860 0.32 153862. 0.4165
|
|
18.15 0.2396 0.5285 0.0499 0.0226 0.238 3.005 2.603 177.785 0.340 11.579 6.641 0.32 154003. 0.3930
|
|
19.55 0.2580 0.5504 0.0471 0.0221 0.233 2.939 2.462 173.861 0.332 10.950 6.422 0.32 154150. 0.3695
|
|
20.95 0.2765 0.5695 0.0444 0.0215 0.227 2.864 2.317 169.422 0.324 10.305 6.202 0.32 154304. 0.3462
|
|
22.34 0.2949 0.5857 0.0415 0.0209 0.221 2.780 2.168 164.449 0.314 9.644 5.980 0.32 154464. 0.3229
|
|
23.74 0.3133 0.5988 0.0386 0.0202 0.213 2.687 2.016 158.926 0.304 8.968 5.754 0.32 154631. 0.2996
|
|
25.13 0.3318 0.6086 0.0356 0.0194 0.205 2.584 1.861 152.834 0.292 8.278 5.523 0.32 154804. 0.2763
|
|
26.53 0.3502 0.6146 0.0326 0.0186 0.196 2.471 1.703 146.157 0.279 7.574 5.284 0.32 154984. 0.2529
|
|
27.93 0.3686 0.6164 0.0295 0.0177 0.186 2.348 1.542 138.882 0.265 6.857 5.035 0.32 155171. 0.2292
|
|
29.32 0.3871 0.6133 0.0264 0.0167 0.176 2.214 1.378 130.997 0.250 6.128 4.771 0.32 155365. 0.2054
|
|
30.72 0.4055 0.6042 0.0232 0.0156 0.164 2.071 1.212 122.491 0.234 5.389 4.486 0.32 155566. 0.1811
|
|
32.12 0.4239 0.5876 0.0200 0.0144 0.152 1.916 1.043 113.359 0.216 4.640 4.174 0.32 155774. 0.1563
|
|
33.51 0.4424 0.5614 0.0167 0.0132 0.139 1.751 0.873 103.597 0.198 3.882 3.821 0.32 155989. 0.1309
|
|
34.91 0.4608 0.5219 0.0134 0.0119 0.125 1.576 0.701 93.206 0.178 3.117 3.410 0.32 156212. 0.1047
|
|
36.31 0.4792 0.4634 0.0101 0.0105 0.110 1.389 0.528 82.193 0.157 2.347 2.912 0.32 156441. 0.0776
|
|
37.70 0.4977 0.3757 0.0068 0.0090 0.095 1.193 0.354 70.567 0.135 1.573 2.273 0.32 156677. 0.0496
|
|
39.10 0.5161 0.2389 0.0034 0.0074 0.078 0.986 0.179 58.337 0.111 0.797 1.394 0.32 156919. 0.0216
|
|
40.49 0.5345 0.0033 0.0000 0.0058 0.061 0.766 0.002 45.289 0.086 0.008 0.018 0.32 157135. 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 0.0783 0.0240 0.438 4.603 5.889 326.783 0.520 26.195 8.174 0.38 183122. 0.7275
|
|
1.68 0.0185 0.0586 0.0767 0.0242 0.440 4.624 5.766 328.278 0.522 25.645 7.966 0.38 183215. 0.7015
|
|
3.36 0.0369 0.1142 0.0750 0.0242 0.442 4.640 5.635 329.387 0.524 25.066 7.760 0.38 183313. 0.6756
|
|
5.04 0.0554 0.1668 0.0731 0.0243 0.443 4.650 5.499 330.059 0.525 24.458 7.556 0.38 183417. 0.6498
|
|
6.72 0.0739 0.2165 0.0712 0.0243 0.443 4.652 5.355 330.246 0.526 23.821 7.355 0.38 183526. 0.6242
|
|
8.39 0.0923 0.2634 0.0692 0.0243 0.442 4.647 5.205 329.898 0.525 23.154 7.157 0.38 183642. 0.5988
|
|
10.07 0.1108 0.3074 0.0672 0.0242 0.441 4.634 5.049 328.969 0.524 22.457 6.961 0.38 183764. 0.5736
|
|
11.75 0.1293 0.3487 0.0650 0.0241 0.439 4.612 4.885 327.416 0.521 21.731 6.768 0.38 183892. 0.5486
|
|
13.43 0.1477 0.3873 0.0627 0.0239 0.436 4.581 4.716 325.203 0.518 20.975 6.577 0.38 184027. 0.5238
|
|
15.11 0.1662 0.4232 0.0604 0.0237 0.432 4.540 4.539 322.293 0.513 20.191 6.388 0.38 184168. 0.4992
|
|
16.79 0.1847 0.4565 0.0579 0.0234 0.427 4.489 4.357 318.651 0.507 19.380 6.202 0.38 184317. 0.4747
|
|
18.47 0.2031 0.4871 0.0554 0.0231 0.421 4.427 4.169 314.242 0.500 18.542 6.017 0.38 184472. 0.4505
|
|
20.15 0.2216 0.5152 0.0529 0.0227 0.414 4.353 3.974 309.031 0.492 17.677 5.833 0.38 184635. 0.4264
|
|
21.83 0.2401 0.5406 0.0502 0.0223 0.406 4.268 3.774 302.983 0.482 16.788 5.650 0.38 184805. 0.4025
|
|
23.50 0.2585 0.5634 0.0475 0.0218 0.397 4.171 3.569 296.063 0.471 15.874 5.467 0.38 184983. 0.3788
|
|
25.18 0.2770 0.5834 0.0447 0.0212 0.387 4.060 3.358 288.237 0.459 14.936 5.284 0.38 185168. 0.3551
|
|
26.86 0.2955 0.6005 0.0418 0.0206 0.375 3.937 3.142 279.472 0.445 13.976 5.099 0.38 185361. 0.3315
|
|
28.54 0.3139 0.6146 0.0389 0.0198 0.362 3.800 2.921 269.736 0.429 12.993 4.912 0.38 185562. 0.3079
|
|
30.22 0.3324 0.6254 0.0359 0.0191 0.347 3.649 2.696 258.999 0.412 11.990 4.721 0.38 185771. 0.2842
|
|
31.90 0.3509 0.6326 0.0328 0.0182 0.332 3.483 2.466 247.234 0.393 10.967 4.523 0.38 185988. 0.2605
|
|
33.58 0.3694 0.6356 0.0297 0.0172 0.314 3.302 2.231 234.416 0.373 9.926 4.318 0.38 186213. 0.2365
|
|
35.26 0.3878 0.6337 0.0265 0.0162 0.296 3.107 1.993 220.524 0.351 8.867 4.100 0.38 186447. 0.2123
|
|
36.94 0.4063 0.6260 0.0233 0.0151 0.276 2.895 1.752 205.540 0.327 7.792 3.866 0.38 186689. 0.1876
|
|
38.61 0.4248 0.6108 0.0200 0.0139 0.254 2.669 1.507 189.454 0.302 6.703 3.608 0.38 186940. 0.1624
|
|
40.29 0.4432 0.5858 0.0168 0.0127 0.231 2.427 1.259 172.260 0.274 5.602 3.316 0.38 187199. 0.1365
|
|
41.97 0.4617 0.5473 0.0134 0.0113 0.206 2.169 1.010 153.961 0.245 4.491 2.974 0.38 187467. 0.1096
|
|
43.65 0.4802 0.4889 0.0101 0.0099 0.180 1.896 0.758 134.568 0.214 3.372 2.555 0.39 187743. 0.0816
|
|
45.33 0.4986 0.3991 0.0067 0.0084 0.153 1.607 0.505 114.100 0.182 2.247 2.009 0.39 188027. 0.0524
|
|
47.01 0.5171 0.2543 0.0033 0.0068 0.124 1.304 0.252 92.569 0.147 1.120 1.234 0.39 188318. 0.0227
|
|
48.69 0.5356 -0.0114 -0.0001 0.0051 0.093 0.977 -0.008 69.379 0.110 -0.036 -0.054 0.39 188557. 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 0.0790 0.0239 0.693 6.239 8.088 516.713 0.705 35.975 7.099 0.44 213632. 0.7404
|
|
1.96 0.0185 0.0595 0.0774 0.0241 0.696 6.268 7.918 519.099 0.708 35.219 6.919 0.44 213740. 0.7139
|
|
3.92 0.0370 0.1159 0.0756 0.0241 0.698 6.289 7.739 520.859 0.711 34.425 6.740 0.44 213855. 0.6876
|
|
5.88 0.0555 0.1692 0.0738 0.0242 0.700 6.302 7.552 521.913 0.712 33.590 6.563 0.44 213977. 0.6614
|
|
7.84 0.0739 0.2197 0.0719 0.0242 0.700 6.305 7.355 522.181 0.712 32.716 6.389 0.44 214106. 0.6354
|
|
9.80 0.0924 0.2672 0.0699 0.0242 0.699 6.298 7.149 521.584 0.712 31.800 6.217 0.44 214241. 0.6096
|
|
11.76 0.1109 0.3119 0.0678 0.0241 0.697 6.279 6.934 520.045 0.709 30.843 6.048 0.44 214384. 0.5840
|
|
13.73 0.1294 0.3539 0.0656 0.0240 0.694 6.249 6.710 517.498 0.706 29.845 5.881 0.44 214535. 0.5586
|
|
15.69 0.1479 0.3931 0.0633 0.0238 0.689 6.205 6.476 513.883 0.701 28.807 5.716 0.44 214693. 0.5335
|
|
17.65 0.1664 0.4297 0.0609 0.0236 0.683 6.148 6.234 509.141 0.695 27.730 5.554 0.44 214859. 0.5085
|
|
19.61 0.1849 0.4636 0.0585 0.0233 0.675 6.076 5.984 503.215 0.686 26.615 5.393 0.45 215033. 0.4838
|
|
21.57 0.2034 0.4949 0.0559 0.0230 0.665 5.990 5.725 496.050 0.677 25.463 5.234 0.45 215215. 0.4593
|
|
23.53 0.2218 0.5237 0.0533 0.0226 0.654 5.887 5.458 487.590 0.665 24.276 5.077 0.45 215406. 0.4350
|
|
25.49 0.2403 0.5498 0.0506 0.0221 0.641 5.769 5.183 477.778 0.652 23.053 4.920 0.45 215605. 0.4108
|
|
27.45 0.2588 0.5733 0.0479 0.0216 0.626 5.634 4.900 466.558 0.636 21.797 4.764 0.45 215813. 0.3868
|
|
29.41 0.2773 0.5941 0.0451 0.0210 0.609 5.480 4.611 453.876 0.619 20.509 4.608 0.45 216030. 0.3628
|
|
31.37 0.2958 0.6121 0.0422 0.0204 0.590 5.309 4.314 439.679 0.600 19.189 4.450 0.45 216256. 0.3390
|
|
33.33 0.3143 0.6270 0.0392 0.0196 0.568 5.119 4.010 423.916 0.578 17.839 4.291 0.45 216491. 0.3151
|
|
35.29 0.3328 0.6388 0.0362 0.0188 0.545 4.909 3.701 406.539 0.555 16.460 4.129 0.45 216736. 0.2913
|
|
37.25 0.3513 0.6470 0.0331 0.0180 0.520 4.679 3.384 387.503 0.529 15.054 3.961 0.45 216990. 0.2673
|
|
39.22 0.3697 0.6511 0.0299 0.0170 0.492 4.429 3.063 366.768 0.500 13.622 3.787 0.45 217253. 0.2431
|
|
41.18 0.3882 0.6505 0.0267 0.0160 0.462 4.157 2.735 344.301 0.470 12.167 3.604 0.45 217527. 0.2186
|
|
43.14 0.4067 0.6441 0.0235 0.0148 0.429 3.865 2.403 320.074 0.437 10.690 3.406 0.45 217810. 0.1936
|
|
45.10 0.4252 0.6303 0.0202 0.0136 0.394 3.551 2.067 294.070 0.401 9.193 3.188 0.45 218103. 0.1681
|
|
47.06 0.4437 0.6067 0.0169 0.0123 0.357 3.215 1.727 266.280 0.363 7.680 2.941 0.45 218406. 0.1417
|
|
49.02 0.4622 0.5695 0.0135 0.0110 0.317 2.858 1.383 236.709 0.323 6.152 2.650 0.45 218719. 0.1143
|
|
50.98 0.4807 0.5120 0.0101 0.0095 0.275 2.480 1.037 205.375 0.280 4.614 2.291 0.45 219042. 0.0856
|
|
52.94 0.4992 0.4215 0.0067 0.0080 0.231 2.081 0.690 172.308 0.235 3.069 1.816 0.45 219375. 0.0553
|
|
54.90 0.5176 0.2711 0.0033 0.0064 0.184 1.661 0.342 137.530 0.188 1.519 1.126 0.45 219714. 0.0241
|
|
56.86 0.5361 -0.0224 -0.0002 0.0046 0.134 1.203 -0.020 99.658 0.136 -0.088 -0.090 0.45 219961. 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 0.0799 0.0240 1.036 8.161 10.676 772.428 0.922 47.486 6.269 0.51 244135. 0.7512
|
|
2.27 0.0187 0.0607 0.0782 0.0241 1.041 8.199 10.450 776.014 0.926 46.480 6.108 0.51 244262. 0.7241
|
|
4.53 0.0374 0.1182 0.0764 0.0242 1.044 8.226 10.212 778.623 0.929 45.421 5.949 0.51 244395. 0.6971
|
|
6.80 0.0561 0.1726 0.0745 0.0242 1.046 8.242 9.961 780.129 0.931 44.308 5.792 0.51 244537. 0.6703
|
|
9.06 0.0748 0.2239 0.0726 0.0242 1.047 8.245 9.699 780.411 0.932 43.140 5.637 0.51 244687. 0.6438
|
|
11.33 0.0935 0.2724 0.0705 0.0242 1.045 8.234 9.424 779.342 0.930 41.917 5.485 0.51 244845. 0.6175
|
|
13.59 0.1121 0.3179 0.0684 0.0241 1.042 8.207 9.136 776.805 0.927 40.638 5.335 0.51 245011. 0.5913
|
|
15.86 0.1308 0.3606 0.0661 0.0240 1.036 8.164 8.836 772.694 0.922 39.304 5.187 0.51 245186. 0.5654
|
|
18.12 0.1495 0.4006 0.0638 0.0238 1.028 8.103 8.524 766.916 0.915 37.916 5.041 0.51 245371. 0.5398
|
|
20.39 0.1682 0.4378 0.0614 0.0236 1.018 8.023 8.201 759.382 0.906 36.476 4.898 0.51 245564. 0.5144
|
|
22.66 0.1869 0.4724 0.0588 0.0233 1.006 7.924 7.865 750.004 0.895 34.984 4.756 0.51 245767. 0.4892
|
|
24.92 0.2056 0.5044 0.0562 0.0229 0.991 7.805 7.519 738.695 0.882 33.443 4.617 0.51 245979. 0.4642
|
|
27.19 0.2243 0.5337 0.0536 0.0225 0.973 7.664 7.161 725.369 0.866 31.853 4.478 0.51 246201. 0.4395
|
|
29.45 0.2430 0.5604 0.0508 0.0220 0.952 7.501 6.793 709.939 0.847 30.217 4.340 0.51 246434. 0.4149
|
|
31.72 0.2617 0.5844 0.0480 0.0215 0.928 7.315 6.415 692.318 0.826 28.535 4.203 0.51 246676. 0.3904
|
|
33.98 0.2804 0.6057 0.0451 0.0209 0.902 7.104 6.027 672.423 0.803 26.810 4.066 0.51 246929. 0.3661
|
|
36.25 0.2990 0.6241 0.0421 0.0202 0.872 6.869 5.630 650.172 0.776 25.043 3.928 0.51 247192. 0.3418
|
|
38.51 0.3177 0.6396 0.0391 0.0194 0.839 6.608 5.224 625.485 0.747 23.235 3.788 0.51 247466. 0.3175
|
|
40.78 0.3364 0.6517 0.0360 0.0186 0.802 6.321 4.809 598.289 0.714 21.389 3.646 0.51 247752. 0.2932
|
|
43.04 0.3551 0.6603 0.0328 0.0176 0.762 6.007 4.385 568.517 0.679 19.507 3.499 0.51 248048. 0.2687
|
|
45.31 0.3738 0.6646 0.0296 0.0166 0.719 5.664 3.955 536.107 0.640 17.590 3.346 0.51 248355. 0.2440
|
|
47.58 0.3925 0.6640 0.0263 0.0156 0.672 5.293 3.517 501.009 0.598 15.642 3.184 0.51 248674. 0.2189
|
|
49.84 0.4112 0.6573 0.0230 0.0144 0.621 4.894 3.072 463.185 0.553 13.665 3.008 0.51 249004. 0.1934
|
|
52.11 0.4299 0.6428 0.0196 0.0131 0.567 4.465 2.622 422.609 0.504 11.662 2.814 0.51 249346. 0.1671
|
|
54.37 0.4486 0.6176 0.0162 0.0118 0.509 4.007 2.167 379.273 0.453 9.637 2.591 0.51 249700. 0.1399
|
|
56.64 0.4673 0.5771 0.0128 0.0103 0.447 3.520 1.707 333.189 0.398 7.595 2.324 0.51 250065. 0.1114
|
|
58.90 0.4860 0.5128 0.0093 0.0088 0.381 3.005 1.245 284.392 0.339 5.538 1.986 0.51 250441. 0.0813
|
|
61.17 0.5046 0.4078 0.0058 0.0072 0.312 2.461 0.781 232.933 0.278 3.474 1.521 0.51 250828. 0.0493
|
|
63.43 0.5233 0.2226 0.0024 0.0055 0.240 1.889 0.316 178.800 0.213 1.403 0.800 0.51 251220. 0.0165
|
|
65.70 0.5420
|
|
|
|
|
|
|
|
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 0.0809 0.0241 1.485 10.397 13.681 1107.100 1.175 60.851 5.605 0.57 274632. 0.7603
|
|
2.52 0.0185 0.0604 0.0792 0.0242 1.491 10.444 13.394 1112.118 1.180 59.578 5.463 0.57 274773. 0.7332
|
|
5.05 0.0370 0.1178 0.0774 0.0243 1.496 10.478 13.093 1115.740 1.184 58.238 5.323 0.57 274923. 0.7063
|
|
7.57 0.0555 0.1721 0.0755 0.0244 1.499 10.498 12.777 1117.787 1.186 56.830 5.184 0.57 275082. 0.6796
|
|
10.10 0.0740 0.2234 0.0736 0.0244 1.499 10.500 12.445 1118.095 1.186 55.354 5.048 0.57 275250. 0.6531
|
|
12.62 0.0925 0.2719 0.0715 0.0243 1.497 10.485 12.097 1116.481 1.185 53.807 4.914 0.57 275426. 0.6268
|
|
15.14 0.1110 0.3175 0.0694 0.0243 1.492 10.451 11.734 1112.782 1.181 52.191 4.783 0.57 275612. 0.6008
|
|
17.67 0.1296 0.3604 0.0671 0.0241 1.484 10.395 11.354 1106.849 1.174 50.505 4.653 0.57 275808. 0.5750
|
|
20.19 0.1481 0.4005 0.0648 0.0239 1.473 10.317 10.960 1098.551 1.166 48.750 4.525 0.57 276013. 0.5494
|
|
22.71 0.1666 0.4381 0.0624 0.0237 1.459 10.216 10.551 1087.761 1.154 46.930 4.399 0.57 276229. 0.5241
|
|
25.24 0.1851 0.4730 0.0599 0.0234 1.441 10.090 10.127 1074.360 1.140 45.045 4.275 0.57 276455. 0.4989
|
|
27.76 0.2036 0.5054 0.0573 0.0231 1.419 9.938 9.689 1058.231 1.123 43.097 4.153 0.57 276691. 0.4741
|
|
30.29 0.2221 0.5353 0.0546 0.0227 1.394 9.760 9.237 1039.250 1.103 41.088 4.032 0.57 276938. 0.4494
|
|
32.81 0.2406 0.5626 0.0519 0.0222 1.364 9.554 8.773 1017.299 1.079 39.021 3.911 0.57 277196. 0.4248
|
|
35.33 0.2591 0.5873 0.0490 0.0216 1.331 9.319 8.295 992.258 1.053 36.896 3.792 0.57 277466. 0.4005
|
|
37.86 0.2776 0.6094 0.0461 0.0210 1.293 9.053 7.805 964.011 1.023 34.716 3.672 0.57 277747. 0.3762
|
|
40.38 0.2961 0.6288 0.0432 0.0203 1.250 8.757 7.303 932.443 0.989 32.482 3.552 0.57 278039. 0.3520
|
|
42.90 0.3146 0.6454 0.0401 0.0196 1.203 8.428 6.789 897.443 0.952 30.198 3.431 0.57 278343. 0.3279
|
|
45.43 0.3331 0.6588 0.0370 0.0187 1.152 8.066 6.265 858.909 0.911 27.865 3.308 0.57 278659. 0.3037
|
|
47.95 0.3516 0.6689 0.0339 0.0178 1.095 7.670 5.730 816.744 0.867 25.485 3.182 0.57 278988. 0.2793
|
|
50.48 0.3702 0.6751 0.0306 0.0168 1.034 7.239 5.185 770.863 0.818 23.063 3.051 0.58 279328. 0.2548
|
|
53.00 0.3887 0.6767 0.0274 0.0157 0.967 6.773 4.631 721.190 0.765 20.599 2.913 0.58 279681. 0.2299
|
|
55.52 0.4072 0.6728 0.0241 0.0146 0.895 6.270 4.069 667.670 0.708 18.098 2.764 0.58 280047. 0.2045
|
|
58.05 0.4257 0.6618 0.0207 0.0133 0.818 5.731 3.499 610.260 0.648 15.564 2.601 0.58 280425. 0.1784
|
|
60.57 0.4442 0.6413 0.0173 0.0120 0.736 5.155 2.923 548.947 0.582 13.000 2.415 0.58 280817. 0.1514
|
|
63.09 0.4627 0.6071 0.0138 0.0105 0.649 4.543 2.341 483.738 0.513 10.413 2.195 0.58 281220. 0.1232
|
|
65.62 0.4812 0.5522 0.0104 0.0090 0.556 3.894 1.755 414.677 0.440 7.806 1.920 0.58 281637. 0.0933
|
|
68.14 0.4997 0.4623 0.0069 0.0075 0.458 3.210 1.166 341.831 0.363 5.188 1.548 0.58 282065. 0.0613
|
|
70.67 0.5182 0.3051 0.0034 0.0058 0.356 2.491 0.576 265.245 0.281 2.562 0.985 0.58 282502. 0.0274
|
|
73.19 0.5367
|
|
|
|
|
|
|
|
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 0.0821 0.0244 2.060 12.986 17.137 1536.442 1.467 76.227 5.059 0.63 305119. 0.7680
|
|
2.81 0.0185 0.0607 0.0803 0.0245 2.070 13.044 16.779 1543.234 1.474 74.634 4.932 0.63 305278. 0.7408
|
|
5.62 0.0371 0.1184 0.0785 0.0246 2.076 13.084 16.402 1548.046 1.478 72.956 4.806 0.63 305446. 0.7137
|
|
8.43 0.0556 0.1730 0.0766 0.0246 2.079 13.106 16.006 1550.632 1.481 71.193 4.682 0.63 305624. 0.6869
|
|
11.24 0.0742 0.2246 0.0746 0.0246 2.080 13.107 15.590 1550.753 1.481 69.344 4.560 0.63 305812. 0.6603
|
|
14.05 0.0927 0.2734 0.0726 0.0246 2.076 13.085 15.154 1548.166 1.478 67.407 4.440 0.63 306010. 0.6338
|
|
16.85 0.1112 0.3193 0.0704 0.0245 2.069 13.039 14.699 1542.636 1.473 65.381 4.322 0.64 306219. 0.6076
|
|
19.66 0.1298 0.3626 0.0681 0.0244 2.057 12.965 14.224 1533.950 1.465 63.267 4.206 0.64 306438. 0.5817
|
|
22.47 0.1483 0.4031 0.0657 0.0242 2.041 12.864 13.729 1521.928 1.453 61.067 4.092 0.64 306668. 0.5560
|
|
25.28 0.1669 0.4410 0.0633 0.0239 2.020 12.733 13.216 1506.405 1.439 58.784 3.979 0.64 306909. 0.5305
|
|
28.09 0.1854 0.4764 0.0607 0.0236 1.994 12.570 12.684 1487.209 1.420 56.419 3.868 0.64 307162. 0.5053
|
|
30.90 0.2039 0.5092 0.0581 0.0233 1.963 12.376 12.135 1464.175 1.398 53.976 3.759 0.64 307427. 0.4802
|
|
33.71 0.2225 0.5395 0.0554 0.0228 1.927 12.147 11.568 1437.143 1.372 51.456 3.651 0.64 307704. 0.4554
|
|
36.52 0.2410 0.5674 0.0526 0.0223 1.885 11.883 10.985 1405.944 1.343 48.861 3.544 0.64 307992. 0.4307
|
|
39.33 0.2596 0.5926 0.0497 0.0218 1.838 11.583 10.386 1370.415 1.309 46.195 3.437 0.64 308294. 0.4062
|
|
42.14 0.2781 0.6153 0.0468 0.0211 1.784 11.245 9.770 1330.397 1.270 43.459 3.331 0.64 308608. 0.3818
|
|
44.95 0.2966 0.6353 0.0438 0.0204 1.724 10.867 9.140 1285.730 1.228 40.656 3.224 0.64 308934. 0.3575
|
|
47.75 0.3152 0.6526 0.0407 0.0196 1.658 10.449 8.496 1236.261 1.181 37.789 3.117 0.64 309274. 0.3332
|
|
50.56 0.3337 0.6668 0.0375 0.0188 1.585 9.989 7.837 1181.851 1.129 34.861 3.008 0.64 309628. 0.3088
|
|
53.37 0.3523 0.6776 0.0343 0.0178 1.505 9.486 7.166 1122.364 1.072 31.874 2.896 0.64 309994. 0.2843
|
|
56.18 0.3708 0.6847 0.0310 0.0168 1.418 8.940 6.482 1057.681 1.010 28.833 2.780 0.64 310375. 0.2595
|
|
58.99 0.3893 0.6872 0.0277 0.0157 1.325 8.348 5.787 987.701 0.943 25.740 2.657 0.64 310769. 0.2344
|
|
61.80 0.4079 0.6844 0.0243 0.0145 1.223 7.711 5.081 912.344 0.871 22.600 2.526 0.64 311177. 0.2088
|
|
64.61 0.4264 0.6744 0.0209 0.0132 1.115 7.029 4.365 831.556 0.794 19.418 2.381 0.64 311599. 0.1825
|
|
67.42 0.4450 0.6550 0.0174 0.0118 0.999 6.300 3.642 745.315 0.712 16.199 2.216 0.64 312036. 0.1551
|
|
70.23 0.4635 0.6219 0.0139 0.0104 0.877 5.525 2.911 653.637 0.624 12.949 2.020 0.64 312486. 0.1264
|
|
73.04 0.4820 0.5676 0.0104 0.0088 0.746 4.704 2.175 556.582 0.531 9.676 1.773 0.64 312950. 0.0959
|
|
75.85 0.5006 0.4767 0.0069 0.0072 0.609 3.839 1.436 454.250 0.434 6.387 1.434 0.64 313428. 0.0630
|
|
78.65 0.5191 0.3132 0.0033 0.0055 0.465 2.930 0.694 346.695 0.331 3.089 0.908 0.64 313915. 0.0278
|
|
81.46 0.5377
|
|
|
|
|
|
|
|
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 0.0835 0.0248 2.789 15.982 21.093 2080.004 1.806 93.823 4.600 0.70 335594. 0.7747
|
|
3.08 0.0185 0.0607 0.0817 0.0249 2.801 16.050 20.655 2088.821 1.813 91.873 4.485 0.70 335770. 0.7475
|
|
6.17 0.0370 0.1182 0.0799 0.0250 2.809 16.097 20.193 2094.918 1.819 89.818 4.372 0.70 335957. 0.7205
|
|
9.25 0.0555 0.1728 0.0780 0.0251 2.813 16.121 19.708 2097.971 1.821 87.659 4.261 0.70 336154. 0.6936
|
|
12.34 0.0740 0.2245 0.0760 0.0250 2.813 16.118 19.198 2097.660 1.821 85.394 4.151 0.70 336362. 0.6670
|
|
15.42 0.0925 0.2734 0.0739 0.0250 2.808 16.087 18.665 2093.651 1.818 83.020 4.044 0.70 336581. 0.6406
|
|
18.51 0.1110 0.3195 0.0716 0.0249 2.797 16.026 18.106 2085.630 1.811 80.537 3.938 0.70 336812. 0.6145
|
|
21.59 0.1296 0.3629 0.0693 0.0248 2.780 15.931 17.524 2073.313 1.800 77.946 3.834 0.70 337054. 0.5885
|
|
24.68 0.1481 0.4037 0.0669 0.0246 2.758 15.802 16.917 2056.456 1.785 75.248 3.731 0.70 337309. 0.5628
|
|
27.76 0.1666 0.4419 0.0645 0.0243 2.729 15.635 16.288 2034.832 1.766 72.448 3.631 0.70 337576. 0.5373
|
|
30.85 0.1851 0.4775 0.0619 0.0240 2.693 15.431 15.636 2008.225 1.743 69.547 3.531 0.70 337855. 0.5121
|
|
33.93 0.2036 0.5107 0.0592 0.0236 2.650 15.187 14.962 1976.419 1.716 66.550 3.434 0.70 338147. 0.4871
|
|
37.02 0.2221 0.5415 0.0565 0.0232 2.601 14.900 14.267 1939.193 1.683 63.457 3.337 0.70 338452. 0.4622
|
|
40.10 0.2406 0.5698 0.0536 0.0226 2.543 14.571 13.551 1896.337 1.646 60.274 3.241 0.70 338770. 0.4375
|
|
43.18 0.2591 0.5956 0.0507 0.0221 2.478 14.197 12.815 1847.635 1.604 57.002 3.146 0.70 339102. 0.4130
|
|
46.27 0.2776 0.6189 0.0477 0.0214 2.404 13.776 12.060 1792.869 1.556 53.645 3.051 0.70 339448. 0.3886
|
|
49.35 0.2961 0.6396 0.0447 0.0207 2.322 13.307 11.287 1731.838 1.503 50.205 2.956 0.70 339808. 0.3642
|
|
52.44 0.3146 0.6576 0.0415 0.0199 2.232 12.789 10.496 1664.334 1.445 46.686 2.860 0.70 340182. 0.3398
|
|
55.52 0.3331 0.6726 0.0383 0.0190 2.132 12.219 9.688 1590.171 1.380 43.092 2.763 0.70 340571. 0.3154
|
|
58.61 0.3516 0.6844 0.0351 0.0180 2.024 11.596 8.864 1509.171 1.310 39.425 2.664 0.70 340974. 0.2908
|
|
61.69 0.3702 0.6926 0.0318 0.0170 1.906 10.920 8.024 1421.172 1.234 35.691 2.561 0.70 341392. 0.2660
|
|
64.78 0.3887 0.6965 0.0284 0.0158 1.778 10.189 7.170 1326.041 1.151 31.893 2.453 0.70 341825. 0.2408
|
|
67.86 0.4072 0.6951 0.0249 0.0146 1.641 9.403 6.303 1223.676 1.062 28.036 2.336 0.70 342274. 0.2151
|
|
70.95 0.4257 0.6869 0.0215 0.0133 1.494 8.560 5.424 1114.015 0.967 24.127 2.208 0.70 342737. 0.1886
|
|
74.03 0.4442 0.6695 0.0179 0.0119 1.337 7.661 4.535 997.044 0.866 20.171 2.063 0.71 343217. 0.1611
|
|
77.12 0.4627 0.6390 0.0144 0.0104 1.170 6.707 3.637 872.812 0.758 16.177 1.890 0.71 343711. 0.1322
|
|
80.20 0.4812 0.5877 0.0108 0.0089 0.994 5.697 2.732 741.435 0.644 12.153 1.671 0.71 344221. 0.1013
|
|
83.28 0.4997 0.5006 0.0072 0.0072 0.809 4.634 1.823 603.102 0.524 8.108 1.371 0.71 344745. 0.0679
|
|
86.37 0.5182 0.3415 0.0036 0.0055 0.614 3.519 0.911 457.967 0.398 4.051 0.902 0.71 345280. 0.0316
|
|
89.45 0.5367
|
|
|
|
|
|
|
|
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 0.0852 0.0255 3.721 19.543 25.612 2774.632 2.208 113.924 4.187 0.76 366053. 0.7771
|
|
3.36 0.0185 0.0603 0.0834 0.0256 3.732 19.604 25.083 2783.226 2.215 111.569 4.088 0.76 366247. 0.7508
|
|
6.73 0.0370 0.1177 0.0815 0.0256 3.739 19.641 24.525 2788.500 2.219 109.085 3.989 0.76 366453. 0.7245
|
|
10.09 0.0555 0.1722 0.0796 0.0257 3.741 19.652 23.938 2790.015 2.220 106.474 3.892 0.76 366671. 0.6982
|
|
13.46 0.0740 0.2239 0.0775 0.0256 3.738 19.633 23.321 2787.339 2.218 103.734 3.795 0.76 366900. 0.6721
|
|
16.82 0.0925 0.2728 0.0754 0.0256 3.728 19.581 22.675 2780.007 2.212 100.861 3.700 0.76 367142. 0.6461
|
|
20.19 0.1110 0.3191 0.0731 0.0255 3.711 19.493 22.000 2767.563 2.202 97.854 3.605 0.76 367396. 0.6202
|
|
23.55 0.1295 0.3627 0.0708 0.0253 3.687 19.367 21.294 2749.603 2.188 94.715 3.513 0.76 367663. 0.5944
|
|
26.92 0.1480 0.4037 0.0684 0.0251 3.655 19.199 20.559 2725.757 2.169 91.447 3.421 0.76 367943. 0.5689
|
|
30.28 0.1665 0.4422 0.0658 0.0248 3.615 18.987 19.796 2695.691 2.145 88.053 3.331 0.76 368236. 0.5435
|
|
33.64 0.1850 0.4782 0.0632 0.0245 3.566 18.729 19.005 2659.086 2.116 84.536 3.242 0.76 368543. 0.5183
|
|
37.01 0.2035 0.5117 0.0605 0.0241 3.508 18.423 18.188 2615.630 2.081 80.900 3.154 0.76 368864. 0.4933
|
|
40.37 0.2221 0.5429 0.0577 0.0236 3.440 18.067 17.345 2565.011 2.041 77.150 3.067 0.76 369199. 0.4684
|
|
43.74 0.2406 0.5716 0.0548 0.0231 3.362 17.658 16.477 2506.928 1.995 73.289 2.981 0.76 369548. 0.4438
|
|
47.10 0.2591 0.5979 0.0518 0.0225 3.274 17.194 15.584 2441.102 1.943 69.319 2.896 0.76 369912. 0.4192
|
|
50.47 0.2776 0.6218 0.0488 0.0218 3.175 16.674 14.669 2367.268 1.884 65.246 2.811 0.76 370291. 0.3948
|
|
53.83 0.2961 0.6431 0.0457 0.0210 3.064 16.096 13.730 2285.172 1.818 61.072 2.725 0.76 370685. 0.3703
|
|
57.20 0.3146 0.6618 0.0425 0.0202 2.943 15.458 12.770 2194.581 1.746 56.802 2.639 0.77 371095. 0.3459
|
|
60.56 0.3331 0.6776 0.0392 0.0193 2.810 14.758 11.789 2095.277 1.667 52.439 2.552 0.77 371521. 0.3214
|
|
63.92 0.3516 0.6901 0.0359 0.0183 2.665 13.996 10.789 1987.080 1.581 47.988 2.463 0.77 371962. 0.2966
|
|
67.29 0.3701 0.6991 0.0325 0.0172 2.508 13.170 9.769 1869.843 1.488 43.454 2.370 0.77 372419. 0.2716
|
|
70.65 0.3886 0.7037 0.0290 0.0160 2.338 12.280 8.733 1743.476 1.387 38.842 2.272 0.77 372893. 0.2462
|
|
74.02 0.4071 0.7029 0.0255 0.0148 2.156 11.326 7.680 1607.944 1.280 34.158 2.166 0.77 373383. 0.2201
|
|
77.38 0.4256 0.6952 0.0220 0.0135 1.962 10.307 6.612 1463.285 1.164 29.409 2.049 0.77 373890. 0.1933
|
|
80.75 0.4441 0.6781 0.0184 0.0120 1.756 9.224 5.531 1309.628 1.042 24.602 1.916 0.77 374413. 0.1652
|
|
84.11 0.4626 0.6472 0.0148 0.0106 1.538 8.080 4.439 1147.193 0.913 19.746 1.755 0.77 374953. 0.1356
|
|
87.47 0.4811 0.5949 0.0111 0.0090 1.309 6.877 3.339 976.317 0.777 14.852 1.551 0.77 375510. 0.1039
|
|
90.84 0.4996 0.5057 0.0074 0.0073 1.069 5.617 2.233 797.444 0.635 9.930 1.270 0.77 376082. 0.0696
|
|
94.20 0.5181 0.3440 0.0037 0.0056 0.819 4.303 1.122 610.983 0.486 4.991 0.833 0.77 376665. 0.0324
|
|
97.57 0.5366 -0.0214 -0.0001 0.0037 0.545 2.862 -0.045 406.359 0.323 -0.199 -0.050 0.77 377002. 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 0.0872 0.0272 5.043 24.451 30.778 3760.690 2.762 136.899 3.712 0.83 396490. 0.7552
|
|
3.65 0.0185 0.0582 0.0854 0.0272 5.038 24.427 30.146 3756.975 2.760 134.088 3.639 0.83 396704. 0.7328
|
|
7.30 0.0370 0.1140 0.0835 0.0271 5.028 24.378 29.479 3749.412 2.754 131.122 3.566 0.83 396931. 0.7101
|
|
10.94 0.0556 0.1675 0.0815 0.0270 5.012 24.300 28.777 3737.539 2.745 128.001 3.492 0.83 397170. 0.6870
|
|
14.59 0.0741 0.2186 0.0794 0.0269 4.990 24.192 28.040 3720.861 2.733 124.723 3.418 0.83 397422. 0.6638
|
|
18.24 0.0926 0.2673 0.0773 0.0268 4.960 24.049 27.267 3698.859 2.717 121.284 3.344 0.83 397687. 0.6403
|
|
21.89 0.1111 0.3136 0.0750 0.0266 4.923 23.868 26.457 3670.996 2.697 117.682 3.269 0.83 397966. 0.6166
|
|
25.53 0.1296 0.3575 0.0726 0.0263 4.877 23.645 25.612 3636.786 2.671 113.920 3.194 0.83 398258. 0.5928
|
|
29.18 0.1481 0.3991 0.0701 0.0260 4.822 23.379 24.730 3595.776 2.641 110.000 3.119 0.83 398565. 0.5689
|
|
32.83 0.1667 0.4382 0.0675 0.0257 4.757 23.065 23.815 3547.559 2.606 105.928 3.045 0.83 398886. 0.5449
|
|
36.48 0.1852 0.4750 0.0648 0.0253 4.682 22.702 22.866 3491.714 2.565 101.707 2.970 0.83 399222. 0.5209
|
|
40.12 0.2037 0.5094 0.0620 0.0248 4.597 22.287 21.884 3427.816 2.518 97.342 2.896 0.83 399573. 0.4968
|
|
43.77 0.2222 0.5414 0.0591 0.0243 4.500 21.816 20.872 3355.432 2.465 92.838 2.821 0.83 399939. 0.4727
|
|
47.42 0.2407 0.5710 0.0562 0.0237 4.391 21.287 19.829 3274.114 2.405 88.198 2.747 0.83 400321. 0.4486
|
|
51.07 0.2593 0.5982 0.0531 0.0230 4.270 20.701 18.756 3183.886 2.339 83.428 2.672 0.83 400719. 0.4244
|
|
54.71 0.2778 0.6227 0.0500 0.0223 4.137 20.055 17.655 3084.612 2.266 78.531 2.596 0.83 401132. 0.4000
|
|
58.36 0.2963 0.6444 0.0468 0.0215 3.991 19.350 16.527 2976.131 2.186 73.513 2.519 0.83 401563. 0.3755
|
|
62.01 0.3148 0.6631 0.0436 0.0207 3.833 18.583 15.373 2858.198 2.100 68.377 2.439 0.83 402009. 0.3508
|
|
65.66 0.3333 0.6787 0.0402 0.0197 3.661 17.749 14.193 2729.907 2.005 63.129 2.358 0.83 402473. 0.3258
|
|
69.30 0.3518 0.6908 0.0368 0.0187 3.475 16.847 12.989 2591.109 1.903 57.775 2.274 0.83 402954. 0.3005
|
|
72.95 0.3704 0.6987 0.0333 0.0177 3.275 15.877 11.762 2441.924 1.794 52.319 2.185 0.83 403452. 0.2748
|
|
76.60 0.3889 0.7016 0.0298 0.0165 3.061 14.840 10.514 2282.410 1.677 46.768 2.089 0.83 403967. 0.2485
|
|
80.25 0.4074 0.6983 0.0262 0.0153 2.833 13.737 9.247 2112.803 1.552 41.129 1.985 0.83 404500. 0.2214
|
|
83.89 0.4259 0.6868 0.0226 0.0140 2.593 12.571 7.961 1933.452 1.420 35.409 1.867 0.83 405051. 0.1932
|
|
87.54 0.4444 0.6643 0.0189 0.0126 2.340 11.345 6.659 1744.850 1.282 29.618 1.731 0.83 405620. 0.1638
|
|
91.19 0.4630 0.6260 0.0151 0.0112 2.075 10.062 5.343 1547.599 1.137 23.766 1.566 0.83 406207. 0.1327
|
|
94.84 0.4815 0.5642 0.0114 0.0097 1.800 8.728 4.016 1342.461 0.986 17.865 1.357 0.83 406812. 0.0997
|
|
98.48 0.5000 0.4647 0.0076 0.0082 1.516 7.349 2.682 1130.328 0.830 11.930 1.076 0.84 407433. 0.0646
|
|
102.13 0.5185 0.2989 0.0038 0.0066 1.223 5.930 1.342 911.999 0.670 5.971 0.668 0.84 408067. 0.0284
|
|
105.78 0.5370 -0.0180 -0.0002 0.0049 0.903 4.377 -0.057 673.274 0.495 -0.256 -0.039 0.84 408474. 0.0000
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|
|
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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) - - -
|
|
0.00 0.0000 0.0000 0.0894 0.0311 7.209 32.454 36.614 5375.636 3.667 162.857 3.089 0.89 426904. 0.6855
|
|
3.94 0.0186 0.0527 0.0876 0.0309 7.156 32.215 35.876 5335.909 3.640 159.575 3.050 0.89 427138. 0.6699
|
|
7.88 0.0372 0.1039 0.0857 0.0306 7.095 31.942 35.095 5290.842 3.609 156.101 3.009 0.89 427386. 0.6536
|
|
11.82 0.0557 0.1537 0.0837 0.0303 7.027 31.636 34.271 5240.111 3.574 152.436 2.966 0.89 427648. 0.6368
|
|
15.76 0.0743 0.2020 0.0816 0.0300 6.951 31.293 33.403 5183.289 3.535 148.576 2.923 0.89 427924. 0.6195
|
|
19.70 0.0929 0.2486 0.0794 0.0297 6.866 30.911 32.490 5119.940 3.492 144.517 2.878 0.89 428215. 0.6017
|
|
23.64 0.1115 0.2936 0.0770 0.0292 6.772 30.486 31.533 5049.625 3.444 140.259 2.832 0.89 428520. 0.5833
|
|
27.58 0.1300 0.3368 0.0746 0.0288 6.668 30.017 30.531 4971.959 3.391 135.802 2.785 0.89 428840. 0.5644
|
|
31.52 0.1486 0.3782 0.0720 0.0283 6.553 29.502 29.486 4886.614 3.333 131.152 2.737 0.89 429176. 0.5450
|
|
35.46 0.1672 0.4178 0.0694 0.0278 6.428 28.939 28.398 4793.281 3.269 126.314 2.687 0.89 429527. 0.5251
|
|
39.40 0.1858 0.4554 0.0666 0.0272 6.292 28.325 27.269 4691.624 3.200 121.294 2.636 0.89 429895. 0.5049
|
|
43.34 0.2043 0.4910 0.0638 0.0265 6.144 27.659 26.102 4581.282 3.125 116.100 2.584 0.89 430278. 0.4842
|
|
47.28 0.2229 0.5246 0.0608 0.0258 5.983 26.938 24.896 4461.840 3.043 110.737 2.531 0.89 430678. 0.4631
|
|
51.22 0.2415 0.5560 0.0578 0.0251 5.810 26.159 23.653 4332.833 2.955 105.210 2.476 0.89 431095. 0.4416
|
|
55.17 0.2601 0.5853 0.0547 0.0243 5.624 25.319 22.375 4193.764 2.861 99.526 2.420 0.89 431529. 0.4198
|
|
59.11 0.2786 0.6119 0.0515 0.0234 5.425 24.426 21.063 4045.769 2.760 93.689 2.361 0.89 431980. 0.3974
|
|
63.05 0.2972 0.6353 0.0482 0.0225 5.218 23.490 19.718 3890.855 2.654 87.705 2.299 0.89 432449. 0.3743
|
|
66.99 0.3158 0.6549 0.0448 0.0216 5.002 22.521 18.340 3730.278 2.544 81.576 2.230 0.89 432936. 0.3502
|
|
70.93 0.3344 0.6680 0.0414 0.0207 4.793 21.578 16.930 3574.133 2.438 75.303 2.148 0.89 433441. 0.3242
|
|
74.87 0.3529 0.6763 0.0378 0.0197 4.573 20.587 15.490 3409.906 2.326 68.900 2.060 0.89 433964. 0.2974
|
|
78.81 0.3715 0.6791 0.0343 0.0187 4.339 19.535 14.023 3235.712 2.207 62.375 1.966 0.89 434505. 0.2699
|
|
82.75 0.3901 0.6754 0.0306 0.0177 4.094 18.429 12.530 3052.537 2.082 55.735 1.862 0.90 435066. 0.2417
|
|
86.69 0.4087 0.6636 0.0269 0.0166 3.836 17.271 11.014 2860.771 1.951 48.990 1.746 0.90 435645. 0.2125
|
|
90.63 0.4272 0.6417 0.0231 0.0154 3.569 16.067 9.476 2661.302 1.815 42.150 1.615 0.90 436243. 0.1823
|
|
94.57 0.4458 0.6066 0.0193 0.0142 3.292 14.822 7.920 2455.128 1.675 35.228 1.463 0.90 436861. 0.1510
|
|
98.51 0.4644 0.5543 0.0155 0.0130 3.009 13.545 6.348 2243.473 1.530 28.236 1.283 0.90 437497. 0.1186
|
|
102.45 0.4830 0.4787 0.0116 0.0117 2.719 12.241 4.765 2027.545 1.383 21.193 1.066 0.90 438153. 0.0853
|
|
106.39 0.5016 0.3712 0.0078 0.0105 2.425 10.919 3.174 1808.629 1.234 14.116 0.796 0.90 438827. 0.0520
|
|
110.33 0.5201 0.2182 0.0039 0.0092 2.129 9.585 1.579 1587.565 1.083 7.023 0.451 0.90 439515. 0.0208
|
|
114.27 0.5387 -0.0114 -0.0002 0.0078 1.804 8.123 -0.067 1345.505 0.918 -0.300 -0.023 0.90 440061. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 15000
|
|
|
|
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 0.0909 0.0375 10.679 44.873 42.717 7963.438 5.070 190.004 2.433 0.95 457336. 0.5832
|
|
4.26 0.0188 0.0450 0.0892 0.0372 10.587 44.487 41.923 7895.055 5.026 186.473 2.408 0.95 457586. 0.5719
|
|
8.53 0.0375 0.0891 0.0874 0.0368 10.478 44.026 41.072 7813.220 4.974 182.686 2.384 0.95 457852. 0.5604
|
|
12.79 0.0563 0.1323 0.0855 0.0363 10.349 43.487 40.163 7717.570 4.913 178.643 2.360 0.95 458134. 0.5486
|
|
17.05 0.0750 0.1747 0.0834 0.0358 10.202 42.869 39.194 7607.896 4.843 174.337 2.337 0.95 458432. 0.5365
|
|
21.31 0.0938 0.2161 0.0812 0.0352 10.037 42.172 38.166 7484.237 4.765 169.763 2.313 0.95 458747. 0.5240
|
|
25.58 0.1125 0.2567 0.0789 0.0346 9.852 41.398 37.078 7346.729 4.677 164.922 2.289 0.95 459079. 0.5112
|
|
29.84 0.1313 0.2963 0.0765 0.0339 9.650 40.547 35.930 7195.730 4.581 159.816 2.265 0.95 459428. 0.4978
|
|
34.10 0.1500 0.3348 0.0739 0.0331 9.430 39.622 34.724 7031.713 4.477 154.452 2.240 0.95 459794. 0.4840
|
|
38.36 0.1688 0.3724 0.0712 0.0323 9.193 38.628 33.462 6855.216 4.364 148.839 2.214 0.95 460179. 0.4697
|
|
42.63 0.1876 0.4087 0.0684 0.0314 8.940 37.566 32.147 6666.709 4.244 142.989 2.187 0.95 460581. 0.4548
|
|
46.89 0.2063 0.4438 0.0655 0.0305 8.672 36.438 30.780 6466.528 4.117 136.910 2.159 0.95 461001. 0.4393
|
|
51.15 0.2251 0.4775 0.0625 0.0295 8.388 35.245 29.364 6254.829 3.982 130.611 2.129 0.95 461439. 0.4232
|
|
55.41 0.2438 0.5097 0.0594 0.0284 8.088 33.987 27.901 6031.565 3.840 124.102 2.098 0.95 461896. 0.4064
|
|
59.68 0.2626 0.5403 0.0562 0.0273 7.773 32.663 26.392 5796.613 3.690 117.389 2.065 0.96 462372. 0.3891
|
|
63.94 0.2813 0.5690 0.0529 0.0261 7.443 31.273 24.839 5549.917 3.533 110.484 2.030 0.96 462866. 0.3710
|
|
68.20 0.3001 0.5956 0.0495 0.0249 7.098 29.824 23.245 5292.818 3.370 103.394 1.992 0.96 463380. 0.3522
|
|
72.46 0.3188 0.6182 0.0460 0.0237 6.755 28.383 21.611 5036.985 3.207 96.125 1.946 0.96 463913. 0.3318
|
|
76.73 0.3376 0.6345 0.0424 0.0226 6.429 27.014 19.937 4794.084 3.052 88.681 1.886 0.96 464466. 0.3089
|
|
80.99 0.3564 0.6354 0.0388 0.0217 6.193 26.022 18.220 4618.153 2.940 81.043 1.789 0.96 465039. 0.2801
|
|
85.25 0.3751 0.6284 0.0350 0.0209 5.958 25.035 16.470 4442.861 2.828 73.257 1.681 0.96 465632. 0.2502
|
|
89.51 0.3939 0.6134 0.0313 0.0201 5.716 24.019 14.690 4262.636 2.714 65.339 1.563 0.96 466245. 0.2197
|
|
93.78 0.4126 0.5889 0.0274 0.0192 5.471 22.987 12.883 4079.368 2.597 57.305 1.432 0.96 466878. 0.1886
|
|
98.04 0.4314 0.5534 0.0235 0.0183 5.222 21.943 11.055 3894.120 2.479 49.172 1.288 0.96 467532. 0.1570
|
|
102.30 0.4501 0.5053 0.0196 0.0175 4.972 20.893 9.210 3707.756 2.360 40.966 1.127 0.96 468206. 0.1254
|
|
106.56 0.4689 0.4426 0.0157 0.0166 4.722 19.842 7.355 3521.240 2.242 32.714 0.947 0.96 468901. 0.0942
|
|
110.83 0.4876 0.3632 0.0117 0.0157 4.473 18.793 5.497 3335.186 2.123 24.450 0.748 0.96 469617. 0.0643
|
|
115.09 0.5064 0.2647 0.0078 0.0148 4.224 17.749 3.644 3149.863 2.005 16.207 0.525 0.96 470352. 0.0367
|
|
119.35 0.5251 0.1442 0.0038 0.0140 3.975 16.701 1.801 2963.967 1.887 8.009 0.276 0.97 471104. 0.0136
|
|
123.61 0.5439 -0.0091 -0.0002 0.0129 3.679 15.458 -0.101 2743.322 1.746 -0.450 -0.017 0.97 471785. 0.0000
|
|
|
|
|
|
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