575 lines
102 KiB
Plaintext
575 lines
102 KiB
Plaintext
16x7E(3D) (16x7E(3D).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 0.0776 0.0295 0.002 0.157 0.162 1.857 0.018 0.721 39.571 0.06 24326. 0.5842
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0.30 0.0198 0.0509 0.0762 0.0297 0.003 0.158 0.159 1.867 0.018 0.708 38.641 0.06 24339. 0.5652
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0.60 0.0397 0.0994 0.0746 0.0298 0.003 0.159 0.156 1.875 0.018 0.693 37.705 0.06 24353. 0.5460
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0.90 0.0595 0.1453 0.0730 0.0299 0.003 0.159 0.153 1.882 0.018 0.679 36.766 0.06 24367. 0.5266
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1.20 0.0794 0.1888 0.0713 0.0300 0.003 0.159 0.149 1.886 0.018 0.663 35.824 0.06 24383. 0.5071
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1.50 0.0992 0.2298 0.0695 0.0300 0.003 0.160 0.145 1.889 0.018 0.646 34.880 0.06 24399. 0.4875
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1.80 0.1190 0.2683 0.0676 0.0300 0.003 0.160 0.141 1.888 0.018 0.628 33.934 0.06 24417. 0.4677
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2.10 0.1389 0.3043 0.0656 0.0300 0.003 0.159 0.137 1.885 0.018 0.610 32.985 0.06 24436. 0.4479
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2.40 0.1587 0.3377 0.0635 0.0299 0.003 0.159 0.133 1.879 0.018 0.590 32.033 0.06 24456. 0.4279
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2.71 0.1785 0.3685 0.0613 0.0297 0.003 0.158 0.128 1.869 0.018 0.570 31.076 0.06 24476. 0.4078
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3.01 0.1984 0.3968 0.0590 0.0295 0.002 0.157 0.123 1.855 0.018 0.548 30.112 0.06 24499. 0.3876
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3.31 0.2182 0.4224 0.0565 0.0292 0.002 0.155 0.118 1.838 0.018 0.525 29.139 0.06 24522. 0.3672
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3.61 0.2381 0.4452 0.0540 0.0289 0.002 0.154 0.113 1.817 0.017 0.502 28.154 0.06 24546. 0.3467
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3.91 0.2579 0.4651 0.0513 0.0285 0.002 0.151 0.107 1.791 0.017 0.477 27.153 0.06 24572. 0.3261
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4.21 0.2777 0.4821 0.0486 0.0280 0.002 0.149 0.101 1.761 0.017 0.451 26.131 0.06 24599. 0.3052
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4.51 0.2976 0.4958 0.0457 0.0274 0.002 0.146 0.095 1.727 0.016 0.425 25.081 0.06 24627. 0.2842
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4.81 0.3174 0.5060 0.0428 0.0268 0.002 0.143 0.089 1.687 0.016 0.397 24.000 0.06 24657. 0.2630
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5.11 0.3372 0.5125 0.0397 0.0261 0.002 0.139 0.083 1.644 0.016 0.369 22.878 0.06 24688. 0.2416
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5.41 0.3571 0.5149 0.0366 0.0254 0.002 0.135 0.076 1.596 0.015 0.340 21.707 0.06 24720. 0.2200
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5.71 0.3769 0.5127 0.0334 0.0245 0.002 0.131 0.070 1.545 0.015 0.310 20.477 0.06 24753. 0.1983
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6.01 0.3968 0.5054 0.0301 0.0237 0.002 0.126 0.063 1.489 0.014 0.280 19.177 0.06 24788. 0.1764
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6.31 0.4166 0.4923 0.0268 0.0227 0.002 0.121 0.056 1.429 0.014 0.249 17.790 0.06 24824. 0.1544
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6.61 0.4364 0.4725 0.0235 0.0217 0.002 0.115 0.049 1.365 0.013 0.218 16.298 0.06 24862. 0.1324
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6.91 0.4563 0.4449 0.0201 0.0206 0.002 0.110 0.042 1.297 0.012 0.187 14.679 0.06 24900. 0.1103
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7.21 0.4761 0.4080 0.0167 0.0195 0.002 0.104 0.035 1.225 0.012 0.155 12.902 0.06 24941. 0.0883
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7.51 0.4960 0.3601 0.0133 0.0183 0.002 0.097 0.028 1.150 0.011 0.123 10.931 0.06 24982. 0.0667
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7.82 0.5158 0.2986 0.0099 0.0170 0.001 0.091 0.021 1.072 0.010 0.092 8.717 0.06 25025. 0.0459
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8.12 0.5356 0.2204 0.0065 0.0158 0.001 0.084 0.014 0.991 0.009 0.060 6.194 0.06 25070. 0.0264
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8.42 0.5555 0.1208 0.0031 0.0144 0.001 0.077 0.007 0.908 0.009 0.029 3.275 0.06 25115. 0.0097
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8.72 0.5753 -0.0067 -0.0002 0.0131 0.001 0.069 0.000 0.822 0.008 -0.001 -0.175 0.06 25162. 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 0.0779 0.0267 0.018 0.568 0.651 13.452 0.064 2.894 21.937 0.13 48652. 0.6489
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0.62 0.0203 0.0577 0.0764 0.0269 0.018 0.572 0.638 13.545 0.065 2.840 21.378 0.13 48679. 0.6264
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1.23 0.0406 0.1123 0.0749 0.0271 0.018 0.576 0.625 13.626 0.065 2.782 20.819 0.13 48707. 0.6038
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1.85 0.0609 0.1640 0.0732 0.0272 0.018 0.579 0.612 13.692 0.065 2.721 20.263 0.13 48737. 0.5812
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2.46 0.0812 0.2126 0.0715 0.0273 0.018 0.581 0.597 13.741 0.066 2.656 19.709 0.13 48769. 0.5585
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3.08 0.1015 0.2584 0.0696 0.0274 0.018 0.582 0.582 13.769 0.066 2.587 19.159 0.13 48803. 0.5358
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3.69 0.1218 0.3012 0.0677 0.0274 0.018 0.582 0.565 13.775 0.066 2.514 18.612 0.13 48839. 0.5132
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4.31 0.1421 0.3412 0.0656 0.0273 0.018 0.581 0.548 13.756 0.066 2.438 18.069 0.13 48878. 0.4905
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4.92 0.1624 0.3782 0.0634 0.0272 0.018 0.579 0.530 13.710 0.065 2.357 17.528 0.13 48919. 0.4679
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5.54 0.1827 0.4124 0.0611 0.0271 0.018 0.576 0.511 13.633 0.065 2.271 16.990 0.13 48962. 0.4453
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6.15 0.2030 0.4438 0.0587 0.0269 0.018 0.572 0.491 13.524 0.065 2.182 16.453 0.13 49008. 0.4226
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6.77 0.2233 0.4722 0.0562 0.0266 0.018 0.565 0.470 13.380 0.064 2.088 15.916 0.13 49056. 0.4000
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7.38 0.2436 0.4977 0.0536 0.0262 0.018 0.558 0.448 13.199 0.063 1.991 15.378 0.13 49107. 0.3773
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8.00 0.2640 0.5202 0.0508 0.0258 0.017 0.549 0.425 12.980 0.062 1.888 14.835 0.13 49160. 0.3545
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8.61 0.2843 0.5395 0.0480 0.0253 0.017 0.538 0.401 12.721 0.061 1.782 14.286 0.13 49216. 0.3316
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9.23 0.3046 0.5554 0.0450 0.0247 0.017 0.525 0.376 12.420 0.059 1.672 13.726 0.13 49275. 0.3086
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9.84 0.3249 0.5677 0.0419 0.0240 0.016 0.510 0.350 12.079 0.058 1.558 13.153 0.13 49336. 0.2855
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10.46 0.3452 0.5760 0.0388 0.0232 0.016 0.494 0.324 11.698 0.056 1.441 12.562 0.13 49401. 0.2622
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11.07 0.3655 0.5801 0.0356 0.0224 0.015 0.477 0.297 11.278 0.054 1.321 11.948 0.13 49467. 0.2388
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11.69 0.3858 0.5793 0.0323 0.0215 0.015 0.457 0.270 10.819 0.052 1.199 11.303 0.13 49537. 0.2152
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12.31 0.4061 0.5728 0.0289 0.0205 0.014 0.436 0.242 10.322 0.049 1.075 10.619 0.13 49610. 0.1914
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12.92 0.4264 0.5599 0.0255 0.0194 0.013 0.414 0.213 9.787 0.047 0.949 9.885 0.13 49685. 0.1674
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13.54 0.4467 0.5392 0.0221 0.0183 0.012 0.389 0.185 9.215 0.044 0.821 9.086 0.13 49763. 0.1432
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14.15 0.4670 0.5089 0.0186 0.0171 0.012 0.364 0.156 8.608 0.041 0.693 8.204 0.13 49844. 0.1187
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14.77 0.4873 0.4669 0.0152 0.0158 0.011 0.337 0.127 7.967 0.038 0.563 7.212 0.13 49928. 0.0941
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15.38 0.5076 0.4096 0.0117 0.0145 0.010 0.308 0.098 7.295 0.035 0.435 6.074 0.13 50015. 0.0696
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16.00 0.5279 0.3321 0.0082 0.0131 0.009 0.279 0.069 6.595 0.031 0.306 4.736 0.13 50105. 0.0456
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16.61 0.5482 0.2270 0.0048 0.0117 0.008 0.248 0.040 5.869 0.028 0.179 3.118 0.13 50197. 0.0230
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17.23 0.5685 0.0822 0.0015 0.0102 0.007 0.216 0.012 5.122 0.024 0.055 1.089 0.13 50292. 0.0044
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17.84 0.5888
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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 0.0782 0.0255 0.058 1.223 1.469 43.396 0.138 6.535 15.355 0.19 72978. 0.6825
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0.91 0.0200 0.0595 0.0767 0.0257 0.059 1.232 1.442 43.727 0.139 6.415 14.959 0.19 73016. 0.6588
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1.82 0.0399 0.1159 0.0752 0.0259 0.059 1.240 1.413 44.017 0.140 6.287 14.565 0.19 73057. 0.6351
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2.72 0.0599 0.1692 0.0736 0.0261 0.059 1.247 1.383 44.258 0.141 6.152 14.174 0.19 73101. 0.6113
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3.63 0.0799 0.2194 0.0719 0.0262 0.060 1.252 1.351 44.441 0.141 6.009 13.787 0.19 73149. 0.5877
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4.54 0.0998 0.2666 0.0701 0.0262 0.060 1.255 1.317 44.559 0.142 5.857 13.403 0.19 73199. 0.5640
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5.45 0.1198 0.3109 0.0681 0.0263 0.060 1.257 1.281 44.603 0.142 5.697 13.024 0.19 73252. 0.5405
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6.35 0.1398 0.3523 0.0661 0.0262 0.060 1.256 1.243 44.565 0.142 5.527 12.648 0.19 73309. 0.5171
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7.26 0.1597 0.3907 0.0640 0.0262 0.060 1.252 1.203 44.435 0.141 5.349 12.276 0.19 73369. 0.4937
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8.17 0.1797 0.4264 0.0617 0.0260 0.059 1.245 1.160 44.206 0.141 5.162 11.907 0.19 73432. 0.4704
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9.08 0.1997 0.4592 0.0594 0.0258 0.059 1.236 1.116 43.869 0.140 4.965 11.541 0.19 73499. 0.4472
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9.98 0.2196 0.4892 0.0569 0.0256 0.058 1.223 1.070 43.418 0.138 4.759 11.177 0.19 73570. 0.4240
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10.89 0.2396 0.5163 0.0543 0.0252 0.057 1.207 1.022 42.846 0.136 4.544 10.814 0.19 73644. 0.4008
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11.80 0.2596 0.5406 0.0517 0.0248 0.057 1.187 0.971 42.145 0.134 4.320 10.451 0.19 73722. 0.3777
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12.71 0.2795 0.5618 0.0489 0.0243 0.055 1.164 0.919 41.307 0.131 4.086 10.086 0.19 73804. 0.3545
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13.61 0.2995 0.5800 0.0460 0.0237 0.054 1.136 0.864 40.331 0.128 3.843 9.717 0.19 73890. 0.3313
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14.52 0.3195 0.5948 0.0430 0.0231 0.053 1.105 0.808 39.218 0.125 3.593 9.343 0.19 73979. 0.3079
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15.43 0.3394 0.6060 0.0399 0.0223 0.051 1.070 0.750 37.969 0.121 3.336 8.959 0.19 74073. 0.2845
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16.34 0.3594 0.6133 0.0367 0.0215 0.049 1.031 0.691 36.586 0.116 3.072 8.563 0.19 74170. 0.2610
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17.24 0.3794 0.6162 0.0335 0.0206 0.047 0.988 0.630 35.069 0.112 2.803 8.151 0.19 74272. 0.2373
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18.15 0.3993 0.6141 0.0302 0.0197 0.045 0.942 0.569 33.420 0.106 2.529 7.717 0.19 74378. 0.2134
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19.06 0.4193 0.6061 0.0269 0.0186 0.042 0.891 0.506 31.640 0.101 2.251 7.254 0.19 74487. 0.1892
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19.97 0.4393 0.5912 0.0236 0.0175 0.040 0.838 0.443 29.734 0.095 1.969 6.754 0.19 74601. 0.1648
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20.87 0.4592 0.5678 0.0202 0.0163 0.037 0.781 0.379 27.703 0.088 1.686 6.204 0.19 74719. 0.1401
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21.78 0.4792 0.5336 0.0167 0.0150 0.034 0.720 0.315 25.555 0.081 1.400 5.587 0.19 74841. 0.1150
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22.69 0.4992 0.4854 0.0133 0.0137 0.031 0.656 0.251 23.295 0.074 1.115 4.880 0.19 74968. 0.0896
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23.60 0.5191 0.4184 0.0099 0.0123 0.028 0.590 0.187 20.934 0.067 0.830 4.045 0.19 75098. 0.0641
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24.50 0.5391 0.3250 0.0066 0.0109 0.025 0.521 0.123 18.481 0.059 0.548 3.026 0.19 75233. 0.0390
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25.41 0.5591 0.1927 0.0032 0.0094 0.021 0.449 0.061 15.950 0.051 0.270 1.729 0.19 75372. 0.0156
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26.32 0.5790 -0.0029 0.0000 0.0079 0.018 0.376 -0.001 13.342 0.042 -0.003 -0.025 0.19 75511. 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 0.0785 0.0249 0.135 2.120 2.623 100.312 0.239 11.667 11.860 0.25 97301. 0.7044
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1.21 0.0200 0.0613 0.0771 0.0251 0.136 2.137 2.575 101.126 0.241 11.453 11.549 0.25 97353. 0.6796
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2.42 0.0400 0.1194 0.0755 0.0253 0.137 2.152 2.524 101.842 0.243 11.226 11.240 0.25 97408. 0.6549
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3.63 0.0600 0.1742 0.0739 0.0254 0.137 2.165 2.470 102.439 0.245 10.985 10.935 0.25 97467. 0.6302
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4.85 0.0800 0.2259 0.0722 0.0256 0.138 2.174 2.412 102.899 0.246 10.729 10.632 0.25 97530. 0.6056
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6.06 0.0999 0.2744 0.0704 0.0256 0.138 2.181 2.351 103.201 0.246 10.458 10.334 0.25 97597. 0.5811
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7.27 0.1199 0.3199 0.0684 0.0257 0.139 2.183 2.287 103.325 0.247 10.172 10.039 0.25 97668. 0.5568
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8.48 0.1399 0.3624 0.0664 0.0256 0.138 2.182 2.219 103.249 0.246 9.870 9.748 0.25 97744. 0.5325
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9.69 0.1599 0.4019 0.0643 0.0256 0.138 2.175 2.147 102.953 0.246 9.552 9.461 0.25 97824. 0.5084
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10.90 0.1799 0.4386 0.0620 0.0254 0.137 2.164 2.072 102.417 0.245 9.217 9.177 0.25 97909. 0.4845
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12.11 0.1999 0.4725 0.0596 0.0252 0.136 2.147 1.993 101.622 0.243 8.866 8.896 0.25 97999. 0.4606
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13.33 0.2199 0.5034 0.0572 0.0250 0.135 2.125 1.911 100.549 0.240 8.498 8.618 0.25 98093. 0.4369
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14.54 0.2399 0.5316 0.0546 0.0246 0.133 2.096 1.824 99.182 0.237 8.114 8.342 0.25 98193. 0.4132
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15.75 0.2598 0.5569 0.0519 0.0242 0.131 2.060 1.734 97.502 0.233 7.713 8.066 0.25 98297. 0.3895
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16.96 0.2798 0.5792 0.0491 0.0237 0.128 2.018 1.640 95.491 0.228 7.295 7.790 0.25 98406. 0.3659
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18.17 0.2998 0.5984 0.0462 0.0231 0.125 1.968 1.543 93.144 0.222 6.862 7.512 0.26 98521. 0.3422
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19.38 0.3198 0.6144 0.0432 0.0225 0.121 1.912 1.442 90.462 0.216 6.415 7.231 0.26 98641. 0.3185
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20.59 0.3398 0.6269 0.0401 0.0217 0.117 1.848 1.339 87.449 0.209 5.955 6.944 0.26 98766. 0.2947
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21.80 0.3598 0.6356 0.0369 0.0209 0.113 1.777 1.233 84.108 0.201 5.484 6.649 0.26 98896. 0.2708
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23.02 0.3798 0.6400 0.0337 0.0200 0.108 1.700 1.125 80.439 0.192 5.003 6.343 0.26 99032. 0.2467
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24.23 0.3998 0.6395 0.0304 0.0190 0.103 1.615 1.015 76.447 0.183 4.514 6.021 0.26 99173. 0.2224
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25.44 0.4197 0.6333 0.0270 0.0179 0.097 1.524 0.903 72.136 0.172 4.017 5.679 0.26 99319. 0.1979
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26.65 0.4397 0.6202 0.0236 0.0168 0.091 1.427 0.790 67.513 0.161 3.515 5.309 0.26 99472. 0.1731
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27.86 0.4597 0.5986 0.0202 0.0155 0.084 1.323 0.676 62.587 0.149 3.008 4.901 0.26 99629. 0.1478
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29.07 0.4797 0.5661 0.0168 0.0142 0.077 1.212 0.562 57.372 0.137 2.499 4.442 0.26 99792. 0.1221
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30.28 0.4997 0.5191 0.0134 0.0129 0.070 1.096 0.447 51.884 0.124 1.990 3.910 0.26 99961. 0.0959
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31.50 0.5197 0.4523 0.0100 0.0115 0.062 0.975 0.333 46.146 0.110 1.482 3.275 0.26 100136. 0.0693
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32.71 0.5397 0.3564 0.0066 0.0100 0.054 0.849 0.220 40.186 0.096 0.980 2.486 0.26 100316. 0.0428
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33.92 0.5597 0.2158 0.0033 0.0085 0.046 0.719 0.109 34.036 0.081 0.484 1.451 0.26 100501. 0.0176
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35.13 0.5796 -0.0022 0.0000 0.0069 0.037 0.585 -0.001 27.690 0.066 -0.004 -0.014 0.26 100686. 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 0.0789 0.0246 0.259 3.265 4.120 193.126 0.369 18.326 9.676 0.32 121623. 0.7203
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1.52 0.0200 0.0626 0.0775 0.0248 0.261 3.292 4.045 194.755 0.372 17.991 9.420 0.32 121688. 0.6948
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3.03 0.0400 0.1219 0.0759 0.0249 0.263 3.316 3.965 196.189 0.375 17.634 9.166 0.32 121757. 0.6693
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4.55 0.0601 0.1778 0.0743 0.0251 0.265 3.337 3.879 197.390 0.377 17.255 8.914 0.32 121831. 0.6439
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6.07 0.0801 0.2304 0.0726 0.0252 0.266 3.352 3.789 198.316 0.379 16.854 8.666 0.32 121910. 0.6186
|
|
7.58 0.1001 0.2799 0.0707 0.0253 0.267 3.363 3.693 198.930 0.380 16.428 8.421 0.32 121994. 0.5935
|
|
9.10 0.1201 0.3263 0.0688 0.0253 0.267 3.367 3.592 199.188 0.380 15.979 8.180 0.32 122084. 0.5686
|
|
10.62 0.1401 0.3696 0.0668 0.0253 0.267 3.365 3.486 199.050 0.380 15.504 7.943 0.32 122179. 0.5438
|
|
12.13 0.1601 0.4100 0.0646 0.0252 0.266 3.355 3.373 198.474 0.379 15.003 7.708 0.32 122280. 0.5192
|
|
13.65 0.1802 0.4474 0.0623 0.0251 0.265 3.337 3.255 197.419 0.377 14.477 7.478 0.32 122386. 0.4947
|
|
15.16 0.2002 0.4820 0.0600 0.0249 0.263 3.311 3.131 195.848 0.374 13.925 7.250 0.32 122499. 0.4704
|
|
16.68 0.2202 0.5137 0.0575 0.0246 0.260 3.275 3.000 193.724 0.370 13.346 7.025 0.32 122617. 0.4462
|
|
18.20 0.2402 0.5426 0.0549 0.0243 0.256 3.229 2.864 191.013 0.365 12.741 6.802 0.32 122742. 0.4222
|
|
19.71 0.2602 0.5687 0.0521 0.0239 0.252 3.173 2.723 187.678 0.358 12.110 6.580 0.32 122873. 0.3981
|
|
21.23 0.2802 0.5918 0.0493 0.0234 0.246 3.105 2.575 183.684 0.351 11.453 6.358 0.32 123010. 0.3741
|
|
22.75 0.3003 0.6118 0.0464 0.0228 0.240 3.026 2.422 179.018 0.342 10.771 6.135 0.32 123154. 0.3501
|
|
24.26 0.3203 0.6287 0.0433 0.0221 0.233 2.936 2.263 173.683 0.332 10.067 5.911 0.32 123304. 0.3261
|
|
25.78 0.3403 0.6422 0.0402 0.0213 0.225 2.835 2.101 167.686 0.320 9.344 5.682 0.32 123461. 0.3020
|
|
27.30 0.3603 0.6519 0.0370 0.0205 0.216 2.722 1.934 161.029 0.308 8.603 5.448 0.32 123624. 0.2779
|
|
28.81 0.3803 0.6575 0.0338 0.0195 0.206 2.599 1.764 153.719 0.294 7.847 5.205 0.32 123794. 0.2535
|
|
30.33 0.4003 0.6582 0.0305 0.0185 0.195 2.464 1.591 145.760 0.278 7.076 4.951 0.32 123971. 0.2290
|
|
31.85 0.4204 0.6534 0.0271 0.0174 0.184 2.319 1.415 137.161 0.262 6.295 4.680 0.32 124155. 0.2042
|
|
33.36 0.4404 0.6417 0.0237 0.0163 0.172 2.163 1.238 127.936 0.244 5.504 4.387 0.32 124346. 0.1790
|
|
34.88 0.4604 0.6215 0.0203 0.0150 0.158 1.996 1.058 118.105 0.226 4.707 4.064 0.32 124543. 0.1533
|
|
36.40 0.4804 0.5903 0.0168 0.0137 0.144 1.820 0.878 107.693 0.206 3.907 3.699 0.32 124748. 0.1271
|
|
37.91 0.5004 0.5442 0.0134 0.0123 0.130 1.635 0.698 96.736 0.185 3.106 3.274 0.32 124959. 0.1003
|
|
39.43 0.5205 0.4772 0.0099 0.0108 0.114 1.442 0.519 85.279 0.163 2.309 2.761 0.32 125178. 0.0729
|
|
40.94 0.5405 0.3790 0.0065 0.0093 0.098 1.240 0.342 73.379 0.140 1.519 2.111 0.32 125404. 0.0452
|
|
42.46 0.5605 0.2303 0.0032 0.0078 0.082 1.033 0.167 61.102 0.117 0.741 1.237 0.32 125636. 0.0185
|
|
43.98 0.5805 -0.0108 -0.0001 0.0062 0.065 0.818 -0.006 48.407 0.092 -0.027 -0.056 0.32 125866. 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 0.0794 0.0244 0.444 4.667 5.971 331.292 0.527 26.559 8.175 0.38 145942. 0.7326
|
|
1.84 0.0202 0.0640 0.0780 0.0246 0.448 4.708 5.861 334.180 0.532 26.070 7.955 0.38 146021. 0.7063
|
|
3.67 0.0404 0.1246 0.0764 0.0248 0.452 4.743 5.744 336.720 0.536 25.549 7.737 0.38 146105. 0.6800
|
|
5.51 0.0606 0.1817 0.0747 0.0249 0.454 4.773 5.619 338.839 0.539 24.995 7.522 0.38 146195. 0.6539
|
|
7.35 0.0808 0.2354 0.0730 0.0251 0.457 4.796 5.487 340.468 0.542 24.408 7.310 0.38 146292. 0.6280
|
|
9.18 0.1010 0.2859 0.0711 0.0251 0.458 4.811 5.347 341.534 0.544 23.785 7.102 0.38 146394. 0.6022
|
|
11.02 0.1212 0.3332 0.0692 0.0252 0.459 4.817 5.199 341.962 0.544 23.127 6.896 0.38 146503. 0.5767
|
|
12.86 0.1414 0.3773 0.0671 0.0251 0.458 4.813 5.043 341.677 0.544 22.431 6.694 0.38 146619. 0.5513
|
|
14.69 0.1616 0.4184 0.0649 0.0251 0.457 4.798 4.878 340.605 0.542 21.697 6.496 0.38 146742. 0.5261
|
|
16.53 0.1818 0.4565 0.0626 0.0249 0.454 4.771 4.704 338.674 0.539 20.925 6.300 0.38 146872. 0.5011
|
|
18.37 0.2020 0.4918 0.0601 0.0247 0.450 4.731 4.522 335.813 0.534 20.114 6.108 0.38 147009. 0.4763
|
|
20.20 0.2222 0.5241 0.0576 0.0244 0.445 4.676 4.331 331.957 0.528 19.264 5.918 0.38 147153. 0.4516
|
|
22.04 0.2424 0.5536 0.0549 0.0241 0.439 4.607 4.131 327.045 0.521 18.376 5.729 0.38 147305. 0.4271
|
|
23.88 0.2626 0.5801 0.0522 0.0236 0.430 4.522 3.923 321.010 0.511 17.448 5.543 0.38 147465. 0.4026
|
|
25.71 0.2828 0.6038 0.0493 0.0231 0.421 4.420 3.706 313.791 0.499 16.483 5.356 0.38 147632. 0.3781
|
|
27.55 0.3030 0.6243 0.0463 0.0225 0.410 4.302 3.480 305.367 0.486 15.481 5.170 0.38 147807. 0.3537
|
|
29.39 0.3232 0.6417 0.0432 0.0218 0.397 4.166 3.248 295.747 0.471 14.447 4.981 0.38 147991. 0.3292
|
|
31.22 0.3434 0.6556 0.0400 0.0210 0.382 4.014 3.009 284.939 0.453 13.385 4.790 0.38 148182. 0.3047
|
|
33.06 0.3636 0.6658 0.0368 0.0201 0.366 3.845 2.765 272.951 0.434 12.297 4.594 0.38 148381. 0.2801
|
|
34.89 0.3838 0.6717 0.0334 0.0191 0.348 3.660 2.515 259.789 0.413 11.186 4.391 0.38 148589. 0.2554
|
|
36.73 0.4040 0.6727 0.0301 0.0181 0.329 3.458 2.261 245.465 0.391 10.057 4.178 0.38 148805. 0.2304
|
|
38.57 0.4242 0.6680 0.0266 0.0169 0.308 3.240 2.003 229.996 0.366 8.910 3.951 0.38 149029. 0.2051
|
|
40.40 0.4444 0.6561 0.0232 0.0157 0.286 3.006 1.743 213.408 0.340 7.752 3.704 0.38 149262. 0.1793
|
|
42.24 0.4647 0.6352 0.0197 0.0144 0.262 2.757 1.480 195.739 0.312 6.584 3.430 0.38 149503. 0.1530
|
|
44.08 0.4849 0.6024 0.0162 0.0130 0.237 2.494 1.217 177.040 0.282 5.412 3.117 0.39 149753. 0.1261
|
|
45.91 0.5051 0.5532 0.0127 0.0116 0.211 2.217 0.954 157.378 0.250 4.242 2.748 0.39 150011. 0.0984
|
|
47.75 0.5253 0.4800 0.0092 0.0101 0.184 1.928 0.692 136.841 0.218 3.077 2.293 0.39 150278. 0.0699
|
|
49.59 0.5455 0.3695 0.0058 0.0085 0.155 1.628 0.433 115.538 0.184 1.926 1.700 0.39 150554. 0.0410
|
|
51.42 0.5657 0.1949 0.0024 0.0069 0.125 1.318 0.178 93.584 0.149 0.794 0.865 0.39 150836. 0.0134
|
|
53.26 0.5859
|
|
|
|
|
|
|
|
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 0.0800 0.0243 0.704 6.340 8.190 525.058 0.716 36.427 7.075 0.44 170258. 0.7425
|
|
2.15 0.0202 0.0647 0.0786 0.0245 0.710 6.396 8.039 529.711 0.723 35.758 6.883 0.44 170350. 0.7157
|
|
4.29 0.0405 0.1259 0.0770 0.0247 0.716 6.445 7.879 533.798 0.728 35.044 6.694 0.44 170449. 0.6891
|
|
6.44 0.0607 0.1836 0.0753 0.0249 0.720 6.487 7.708 537.203 0.733 34.286 6.508 0.44 170555. 0.6626
|
|
8.58 0.0809 0.2380 0.0736 0.0250 0.724 6.518 7.527 539.813 0.736 33.480 6.324 0.44 170668. 0.6363
|
|
10.73 0.1011 0.2890 0.0717 0.0251 0.726 6.539 7.335 541.511 0.739 32.627 6.144 0.44 170788. 0.6102
|
|
12.87 0.1214 0.3367 0.0697 0.0251 0.727 6.547 7.132 542.174 0.740 31.723 5.966 0.44 170916. 0.5843
|
|
15.02 0.1416 0.3814 0.0676 0.0251 0.726 6.541 6.917 541.682 0.739 30.768 5.792 0.44 171052. 0.5587
|
|
17.16 0.1618 0.4230 0.0654 0.0250 0.724 6.519 6.691 539.914 0.737 29.761 5.621 0.44 171196. 0.5332
|
|
19.31 0.1821 0.4616 0.0631 0.0249 0.720 6.481 6.452 536.753 0.732 28.700 5.452 0.45 171348. 0.5079
|
|
21.46 0.2023 0.4973 0.0606 0.0247 0.714 6.425 6.202 532.087 0.726 27.586 5.287 0.45 171508. 0.4828
|
|
23.60 0.2225 0.5301 0.0580 0.0244 0.705 6.349 5.939 525.809 0.717 26.419 5.123 0.45 171678. 0.4579
|
|
25.75 0.2428 0.5601 0.0554 0.0240 0.694 6.252 5.665 517.818 0.706 25.198 4.962 0.45 171856. 0.4331
|
|
27.89 0.2630 0.5872 0.0526 0.0235 0.681 6.134 5.378 508.012 0.693 23.923 4.802 0.45 172043. 0.4084
|
|
30.04 0.2832 0.6114 0.0496 0.0230 0.666 5.992 5.080 496.286 0.677 22.596 4.643 0.45 172239. 0.3838
|
|
32.18 0.3034 0.6326 0.0466 0.0224 0.647 5.827 4.770 482.609 0.658 21.219 4.483 0.45 172444. 0.3591
|
|
34.33 0.3237 0.6506 0.0435 0.0216 0.626 5.639 4.451 466.994 0.637 19.798 4.323 0.45 172659. 0.3345
|
|
36.48 0.3439 0.6652 0.0403 0.0208 0.603 5.427 4.122 449.454 0.613 18.337 4.160 0.45 172883. 0.3098
|
|
38.62 0.3641 0.6762 0.0370 0.0199 0.577 5.192 3.786 429.999 0.587 16.841 3.994 0.45 173116. 0.2850
|
|
40.77 0.3844 0.6829 0.0336 0.0189 0.548 4.934 3.443 408.642 0.557 15.314 3.821 0.45 173359. 0.2600
|
|
42.91 0.4046 0.6849 0.0302 0.0179 0.517 4.654 3.093 385.400 0.526 13.760 3.641 0.45 173612. 0.2348
|
|
45.06 0.4248 0.6811 0.0268 0.0167 0.483 4.351 2.739 360.302 0.492 12.184 3.448 0.45 173874. 0.2093
|
|
47.20 0.4451 0.6703 0.0233 0.0154 0.447 4.026 2.381 333.391 0.455 10.590 3.239 0.45 174147. 0.1833
|
|
49.35 0.4653 0.6505 0.0197 0.0141 0.409 3.679 2.020 304.727 0.416 8.985 3.007 0.45 174429. 0.1567
|
|
51.49 0.4855 0.6187 0.0162 0.0127 0.368 3.313 1.658 274.396 0.374 7.374 2.740 0.45 174721. 0.1294
|
|
53.64 0.5057 0.5700 0.0127 0.0112 0.325 2.928 1.296 242.507 0.331 5.765 2.424 0.45 175023. 0.1012
|
|
55.79 0.5260 0.4965 0.0091 0.0097 0.281 2.526 0.936 209.207 0.285 4.165 2.030 0.45 175336. 0.0720
|
|
57.93 0.5462 0.3829 0.0057 0.0081 0.234 2.109 0.581 174.673 0.238 2.583 1.508 0.45 175658. 0.0421
|
|
60.08 0.5664 0.1984 0.0023 0.0064 0.187 1.679 0.231 139.093 0.190 1.027 0.753 0.45 175989. 0.0133
|
|
62.22 0.5867
|
|
|
|
|
|
|
|
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 0.0808 0.0244 1.054 8.302 10.794 785.789 0.938 48.011 6.230 0.51 194570. 0.7507
|
|
2.44 0.0202 0.0650 0.0793 0.0246 1.063 8.376 10.597 792.788 0.946 47.135 6.063 0.51 194676. 0.7238
|
|
4.89 0.0403 0.1264 0.0777 0.0248 1.071 8.441 10.387 798.932 0.954 46.201 5.897 0.51 194789. 0.6970
|
|
7.33 0.0605 0.1843 0.0760 0.0250 1.078 8.495 10.164 804.042 0.960 45.208 5.733 0.51 194910. 0.6703
|
|
9.78 0.0807 0.2388 0.0743 0.0251 1.083 8.536 9.927 807.950 0.964 44.154 5.573 0.51 195039. 0.6439
|
|
12.22 0.1008 0.2901 0.0724 0.0252 1.087 8.563 9.675 810.479 0.967 43.036 5.415 0.51 195176. 0.6177
|
|
14.66 0.1210 0.3381 0.0704 0.0252 1.088 8.573 9.409 811.448 0.969 41.852 5.259 0.51 195322. 0.5916
|
|
17.11 0.1411 0.3830 0.0683 0.0252 1.087 8.565 9.128 810.674 0.968 40.601 5.107 0.51 195477. 0.5658
|
|
19.55 0.1613 0.4249 0.0661 0.0251 1.084 8.537 8.831 807.978 0.964 39.281 4.957 0.51 195641. 0.5403
|
|
22.00 0.1815 0.4639 0.0637 0.0249 1.077 8.486 8.519 803.181 0.959 37.890 4.811 0.51 195815. 0.5149
|
|
24.44 0.2016 0.5000 0.0613 0.0247 1.068 8.411 8.190 796.116 0.950 36.430 4.666 0.51 195998. 0.4897
|
|
26.88 0.2218 0.5332 0.0587 0.0244 1.055 8.311 7.846 786.624 0.939 34.899 4.524 0.51 196191. 0.4647
|
|
29.33 0.2420 0.5636 0.0560 0.0240 1.039 8.183 7.486 774.554 0.925 33.298 4.384 0.51 196394. 0.4399
|
|
31.77 0.2621 0.5913 0.0532 0.0236 1.019 8.027 7.110 759.752 0.907 31.627 4.245 0.51 196607. 0.4151
|
|
34.22 0.2823 0.6160 0.0503 0.0230 0.995 7.840 6.719 742.060 0.886 29.885 4.107 0.51 196831. 0.3904
|
|
36.66 0.3024 0.6378 0.0472 0.0224 0.967 7.622 6.313 721.424 0.861 28.078 3.969 0.51 197064. 0.3657
|
|
39.10 0.3226 0.6566 0.0441 0.0217 0.936 7.373 5.893 697.861 0.833 26.212 3.830 0.51 197309. 0.3410
|
|
41.55 0.3428 0.6721 0.0409 0.0208 0.900 7.093 5.462 671.389 0.801 24.294 3.690 0.51 197564. 0.3162
|
|
43.99 0.3629 0.6840 0.0376 0.0199 0.861 6.783 5.020 642.025 0.766 22.330 3.547 0.51 197829. 0.2914
|
|
46.44 0.3831 0.6919 0.0342 0.0189 0.818 6.443 4.569 609.787 0.728 20.324 3.399 0.51 198106. 0.2664
|
|
48.88 0.4033 0.6951 0.0307 0.0178 0.771 6.072 4.110 574.701 0.686 18.282 3.244 0.51 198393. 0.2412
|
|
51.32 0.4234 0.6929 0.0273 0.0167 0.720 5.672 3.644 536.810 0.641 16.211 3.079 0.51 198692. 0.2156
|
|
53.77 0.4436 0.6838 0.0237 0.0154 0.665 5.242 3.174 496.175 0.592 14.116 2.901 0.51 199001. 0.1895
|
|
56.21 0.4638 0.6661 0.0202 0.0141 0.607 4.785 2.699 452.887 0.541 12.005 2.703 0.51 199322. 0.1629
|
|
58.66 0.4839 0.6368 0.0166 0.0126 0.546 4.301 2.223 407.070 0.486 9.886 2.476 0.51 199654. 0.1354
|
|
61.10 0.5041 0.5912 0.0131 0.0111 0.481 3.792 1.746 358.889 0.428 7.768 2.207 0.51 199998. 0.1070
|
|
63.54 0.5242 0.5212 0.0095 0.0096 0.414 3.260 1.273 308.559 0.368 5.661 1.871 0.51 200352. 0.0774
|
|
65.99 0.5444 0.4116 0.0060 0.0080 0.344 2.708 0.804 256.347 0.306 3.577 1.423 0.52 200719. 0.0468
|
|
68.43 0.5646 0.2306 0.0026 0.0063 0.272 2.140 0.343 202.541 0.242 1.527 0.769 0.52 201095. 0.0165
|
|
70.88 0.5847
|
|
|
|
|
|
|
|
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 0.0816 0.0246 1.511 10.579 13.807 1126.415 1.195 61.414 5.560 0.57 218877. 0.7576
|
|
2.72 0.0200 0.0646 0.0801 0.0248 1.524 10.672 13.559 1136.392 1.206 60.309 5.412 0.57 218995. 0.7308
|
|
5.45 0.0399 0.1257 0.0786 0.0250 1.536 10.754 13.294 1145.141 1.215 59.132 5.265 0.57 219122. 0.7041
|
|
8.17 0.0599 0.1835 0.0769 0.0251 1.545 10.823 13.013 1152.416 1.223 57.880 5.121 0.57 219257. 0.6775
|
|
10.89 0.0799 0.2378 0.0752 0.0252 1.553 10.875 12.714 1157.975 1.229 56.550 4.980 0.57 219401. 0.6512
|
|
13.62 0.0999 0.2890 0.0733 0.0253 1.558 10.909 12.397 1161.571 1.232 55.141 4.841 0.57 219555. 0.6250
|
|
16.34 0.1198 0.3370 0.0713 0.0254 1.560 10.922 12.061 1162.951 1.234 53.648 4.704 0.57 219718. 0.5991
|
|
19.07 0.1398 0.3820 0.0692 0.0253 1.558 10.911 11.707 1161.854 1.233 52.071 4.570 0.57 219891. 0.5734
|
|
21.79 0.1598 0.4240 0.0670 0.0252 1.553 10.875 11.332 1158.029 1.229 50.406 4.439 0.57 220074. 0.5480
|
|
24.51 0.1798 0.4631 0.0647 0.0251 1.544 10.812 10.938 1151.227 1.221 48.653 4.310 0.57 220267. 0.5227
|
|
27.24 0.1997 0.4995 0.0622 0.0249 1.530 10.718 10.524 1141.210 1.211 46.812 4.183 0.57 220471. 0.4976
|
|
29.96 0.2197 0.5330 0.0596 0.0246 1.512 10.591 10.090 1127.755 1.197 44.881 4.058 0.57 220686. 0.4727
|
|
32.68 0.2397 0.5639 0.0570 0.0242 1.489 10.431 9.636 1110.651 1.178 42.861 3.935 0.57 220911. 0.4480
|
|
35.41 0.2597 0.5920 0.0542 0.0238 1.461 10.234 9.162 1089.683 1.156 40.754 3.814 0.57 221148. 0.4233
|
|
38.13 0.2796 0.6174 0.0512 0.0232 1.428 9.998 8.668 1064.630 1.130 38.557 3.693 0.57 221396. 0.3987
|
|
40.86 0.2996 0.6399 0.0482 0.0226 1.388 9.724 8.156 1035.383 1.099 36.276 3.573 0.57 221656. 0.3742
|
|
43.58 0.3196 0.6595 0.0451 0.0218 1.344 9.410 7.626 1001.962 1.063 33.920 3.452 0.57 221927. 0.3496
|
|
46.30 0.3396 0.6760 0.0419 0.0210 1.293 9.057 7.081 964.397 1.023 31.497 3.330 0.57 222210. 0.3250
|
|
49.03 0.3595 0.6891 0.0386 0.0201 1.237 8.666 6.523 922.710 0.979 29.013 3.206 0.57 222504. 0.3003
|
|
51.75 0.3795 0.6985 0.0352 0.0191 1.176 8.236 5.952 876.926 0.930 26.476 3.079 0.58 222811. 0.2755
|
|
54.47 0.3995 0.7035 0.0318 0.0180 1.109 7.767 5.371 827.080 0.878 23.892 2.946 0.58 223129. 0.2504
|
|
57.20 0.4194 0.7033 0.0283 0.0169 1.037 7.262 4.782 773.228 0.820 21.269 2.805 0.58 223460. 0.2249
|
|
59.92 0.4394 0.6969 0.0247 0.0156 0.959 6.719 4.185 715.452 0.759 18.615 2.653 0.58 223802. 0.1990
|
|
62.64 0.4594 0.6826 0.0212 0.0143 0.877 6.141 3.583 653.870 0.694 15.938 2.486 0.58 224158. 0.1725
|
|
65.37 0.4794 0.6577 0.0176 0.0128 0.789 5.528 2.978 588.648 0.625 13.248 2.295 0.58 224525. 0.1453
|
|
68.09 0.4993 0.6180 0.0140 0.0113 0.697 4.884 2.373 520.005 0.552 10.557 2.070 0.58 224905. 0.1170
|
|
70.82 0.5193 0.5563 0.0105 0.0098 0.601 4.210 1.771 448.231 0.476 7.876 1.792 0.58 225298. 0.0874
|
|
73.54 0.5393 0.4593 0.0069 0.0081 0.501 3.509 1.174 373.687 0.396 5.220 1.425 0.58 225703. 0.0566
|
|
76.26 0.5593 0.2992 0.0035 0.0065 0.398 2.787 0.586 296.789 0.315 2.605 0.895 0.58 226119. 0.0251
|
|
78.99 0.5792 0.0032 0.0000 0.0047 0.291 2.040 0.004 217.250 0.231 0.019 0.009 0.58 226529. 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 0.0826 0.0248 2.095 13.203 17.259 1562.109 1.492 76.769 5.011 0.63 243177. 0.7635
|
|
3.03 0.0200 0.0647 0.0812 0.0250 2.113 13.320 16.951 1575.925 1.505 75.396 4.879 0.63 243309. 0.7366
|
|
6.05 0.0399 0.1260 0.0796 0.0252 2.130 13.422 16.621 1588.005 1.516 73.932 4.747 0.63 243451. 0.7098
|
|
9.08 0.0599 0.1838 0.0779 0.0254 2.143 13.507 16.271 1597.997 1.526 72.374 4.618 0.63 243602. 0.6832
|
|
12.11 0.0799 0.2384 0.0761 0.0255 2.153 13.571 15.899 1605.572 1.533 70.719 4.491 0.63 243763. 0.6568
|
|
15.13 0.0999 0.2897 0.0742 0.0256 2.160 13.611 15.504 1610.379 1.538 68.962 4.367 0.63 243935. 0.6306
|
|
18.16 0.1198 0.3379 0.0722 0.0256 2.162 13.626 15.086 1612.060 1.539 67.102 4.245 0.64 244117. 0.6046
|
|
21.18 0.1398 0.3831 0.0701 0.0256 2.159 13.610 14.643 1610.258 1.538 65.133 4.125 0.64 244310. 0.5788
|
|
24.21 0.1598 0.4253 0.0679 0.0255 2.152 13.563 14.176 1604.620 1.532 63.056 4.007 0.64 244514. 0.5533
|
|
27.24 0.1798 0.4647 0.0655 0.0253 2.139 13.480 13.684 1594.798 1.523 60.867 3.892 0.64 244730. 0.5280
|
|
30.26 0.1997 0.5013 0.0630 0.0251 2.119 13.358 13.167 1580.464 1.509 58.566 3.779 0.64 244958. 0.5028
|
|
33.29 0.2197 0.5352 0.0604 0.0248 2.094 13.197 12.624 1561.308 1.491 56.153 3.667 0.64 245197. 0.4779
|
|
36.32 0.2397 0.5664 0.0577 0.0244 2.061 12.991 12.057 1537.034 1.468 53.629 3.558 0.64 245449. 0.4531
|
|
39.34 0.2597 0.5950 0.0549 0.0240 2.021 12.741 11.464 1507.353 1.439 50.993 3.450 0.64 245713. 0.4283
|
|
42.37 0.2796 0.6208 0.0519 0.0234 1.974 12.441 10.846 1471.953 1.406 48.245 3.342 0.64 245990. 0.4037
|
|
45.39 0.2996 0.6438 0.0489 0.0227 1.919 12.092 10.205 1430.678 1.366 45.391 3.235 0.64 246279. 0.3790
|
|
48.42 0.3196 0.6640 0.0457 0.0220 1.855 11.694 9.542 1383.559 1.321 42.442 3.128 0.64 246581. 0.3544
|
|
51.45 0.3396 0.6811 0.0424 0.0211 1.784 11.247 8.860 1330.636 1.271 39.408 3.020 0.64 246896. 0.3297
|
|
54.47 0.3595 0.6949 0.0391 0.0202 1.706 10.751 8.160 1271.943 1.215 36.298 2.910 0.64 247224. 0.3049
|
|
57.50 0.3795 0.7050 0.0357 0.0192 1.619 10.206 7.446 1207.518 1.153 33.120 2.797 0.64 247565. 0.2799
|
|
60.53 0.3995 0.7109 0.0322 0.0181 1.525 9.614 6.718 1137.410 1.086 29.883 2.679 0.64 247919. 0.2547
|
|
63.55 0.4194 0.7117 0.0286 0.0169 1.424 8.974 5.979 1061.698 1.014 26.596 2.554 0.64 248287. 0.2291
|
|
66.58 0.4394 0.7064 0.0250 0.0156 1.315 8.287 5.232 980.497 0.936 23.270 2.420 0.64 248668. 0.2030
|
|
69.61 0.4594 0.6932 0.0214 0.0142 1.199 7.556 4.477 893.977 0.854 19.915 2.272 0.64 249063. 0.1763
|
|
72.63 0.4794 0.6695 0.0178 0.0128 1.076 6.782 3.719 802.368 0.766 16.543 2.102 0.64 249472. 0.1487
|
|
75.66 0.4993 0.6309 0.0142 0.0112 0.947 5.967 2.961 705.981 0.674 13.169 1.902 0.64 249894. 0.1200
|
|
78.68 0.5193 0.5700 0.0106 0.0096 0.812 5.115 2.205 605.224 0.578 9.808 1.652 0.64 250330. 0.0900
|
|
81.71 0.5393 0.4727 0.0070 0.0080 0.671 4.231 1.456 500.606 0.478 6.478 1.320 0.64 250781. 0.0584
|
|
84.74 0.5593 0.3084 0.0034 0.0062 0.527 3.319 0.719 392.717 0.375 3.198 0.830 0.64 251244. 0.0258
|
|
87.76 0.5792 -0.0070 -0.0001 0.0045 0.377 2.375 -0.011 280.936 0.268 -0.050 -0.018 0.65 251695. 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 0.0839 0.0252 2.832 16.225 21.190 2111.522 1.833 94.254 4.552 0.70 267469. 0.7684
|
|
3.33 0.0200 0.0646 0.0824 0.0254 2.856 16.367 20.815 2130.056 1.849 92.583 4.432 0.70 267616. 0.7416
|
|
6.65 0.0399 0.1258 0.0808 0.0256 2.878 16.491 20.413 2146.192 1.863 90.799 4.314 0.70 267772. 0.7148
|
|
9.98 0.0599 0.1836 0.0791 0.0258 2.896 16.593 19.986 2159.462 1.875 88.899 4.198 0.70 267940. 0.6882
|
|
13.30 0.0798 0.2382 0.0773 0.0259 2.909 16.669 19.532 2169.410 1.883 86.879 4.084 0.70 268118. 0.6619
|
|
16.63 0.0998 0.2895 0.0754 0.0260 2.917 16.717 19.050 2175.563 1.889 84.733 3.972 0.70 268308. 0.6357
|
|
19.95 0.1197 0.3378 0.0734 0.0260 2.920 16.731 18.538 2177.438 1.890 82.459 3.862 0.70 268509. 0.6097
|
|
23.28 0.1397 0.3831 0.0712 0.0260 2.916 16.709 17.997 2174.550 1.888 80.052 3.754 0.70 268723. 0.5840
|
|
26.61 0.1596 0.4255 0.0690 0.0259 2.905 16.646 17.426 2166.421 1.881 77.509 3.648 0.70 268948. 0.5585
|
|
29.93 0.1796 0.4652 0.0666 0.0257 2.887 16.540 16.823 2152.583 1.869 74.829 3.545 0.70 269187. 0.5332
|
|
33.26 0.1995 0.5020 0.0641 0.0255 2.860 16.387 16.189 2132.592 1.851 72.010 3.443 0.70 269438. 0.5081
|
|
36.58 0.2195 0.5362 0.0614 0.0251 2.824 16.182 15.524 2106.028 1.828 69.053 3.343 0.70 269702. 0.4831
|
|
39.91 0.2395 0.5678 0.0587 0.0247 2.779 15.925 14.828 2072.505 1.799 65.957 3.245 0.70 269980. 0.4583
|
|
43.24 0.2594 0.5967 0.0558 0.0243 2.724 15.611 14.101 2031.630 1.764 62.723 3.148 0.70 270271. 0.4335
|
|
46.56 0.2794 0.6230 0.0528 0.0237 2.659 15.237 13.343 1982.991 1.721 59.351 3.052 0.70 270576. 0.4089
|
|
49.89 0.2993 0.6466 0.0497 0.0230 2.583 14.802 12.556 1926.367 1.672 55.848 2.956 0.70 270895. 0.3842
|
|
53.21 0.3193 0.6673 0.0465 0.0222 2.497 14.306 11.742 1861.791 1.616 52.227 2.860 0.70 271227. 0.3595
|
|
56.54 0.3392 0.6851 0.0431 0.0214 2.400 13.749 10.904 1789.327 1.553 48.499 2.764 0.70 271574. 0.3347
|
|
59.86 0.3592 0.6996 0.0397 0.0204 2.292 13.132 10.044 1709.025 1.484 44.677 2.666 0.70 271935. 0.3098
|
|
63.19 0.3791 0.7105 0.0363 0.0194 2.174 12.455 9.166 1620.939 1.407 40.770 2.565 0.70 272310. 0.2848
|
|
66.52 0.3991 0.7173 0.0327 0.0182 2.045 11.719 8.271 1525.140 1.324 36.790 2.460 0.70 272700. 0.2594
|
|
69.84 0.4191 0.7192 0.0291 0.0170 1.907 10.924 7.362 1421.737 1.234 32.748 2.349 0.70 273105. 0.2337
|
|
73.17 0.4390 0.7150 0.0255 0.0157 1.758 10.073 6.442 1310.906 1.138 28.656 2.229 0.70 273524. 0.2075
|
|
76.49 0.4590 0.7031 0.0218 0.0142 1.600 9.166 5.514 1192.892 1.036 24.527 2.097 0.71 273958. 0.1806
|
|
79.82 0.4789 0.6808 0.0181 0.0128 1.432 8.207 4.581 1068.037 0.927 20.376 1.945 0.71 274408. 0.1527
|
|
83.15 0.4989 0.6436 0.0144 0.0112 1.256 7.198 3.647 936.803 0.813 16.221 1.766 0.71 274872. 0.1237
|
|
86.47 0.5188 0.5839 0.0107 0.0095 1.073 6.146 2.716 799.795 0.694 12.081 1.540 0.71 275351. 0.0931
|
|
89.80 0.5388 0.4869 0.0071 0.0079 0.882 5.054 1.794 657.777 0.571 7.979 1.237 0.71 275846. 0.0608
|
|
93.12 0.5587 0.3203 0.0035 0.0061 0.686 3.931 0.885 511.636 0.444 3.936 0.784 0.71 276354. 0.0271
|
|
96.45 0.5787 -0.0083 -0.0001 0.0043 0.483 2.770 -0.016 360.511 0.313 -0.069 -0.020 0.71 276848. 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 0.0853 0.0258 3.765 19.776 25.653 2807.746 2.234 114.105 4.144 0.76 291750. 0.7697
|
|
3.62 0.0199 0.0642 0.0838 0.0260 3.795 19.932 25.204 2829.856 2.252 112.105 4.040 0.76 291911. 0.7437
|
|
7.25 0.0399 0.1250 0.0822 0.0262 3.821 20.067 24.723 2849.053 2.267 109.968 3.936 0.76 292084. 0.7177
|
|
10.87 0.0598 0.1826 0.0805 0.0263 3.842 20.178 24.211 2864.715 2.280 107.689 3.833 0.76 292268. 0.6917
|
|
14.49 0.0797 0.2371 0.0787 0.0265 3.857 20.259 23.665 2876.218 2.289 105.263 3.732 0.76 292463. 0.6658
|
|
18.11 0.0996 0.2884 0.0768 0.0265 3.866 20.306 23.086 2882.904 2.294 102.685 3.632 0.76 292672. 0.6400
|
|
21.74 0.1196 0.3368 0.0747 0.0265 3.868 20.314 22.470 2884.104 2.295 99.948 3.534 0.76 292893. 0.6143
|
|
25.36 0.1395 0.3821 0.0725 0.0265 3.861 20.279 21.819 2879.130 2.291 97.050 3.437 0.76 293127. 0.5888
|
|
28.98 0.1594 0.4247 0.0703 0.0264 3.845 20.196 21.130 2867.299 2.282 93.986 3.342 0.76 293374. 0.5635
|
|
32.61 0.1793 0.4645 0.0678 0.0262 3.819 20.060 20.403 2847.948 2.266 90.753 3.249 0.76 293635. 0.5383
|
|
36.23 0.1993 0.5016 0.0653 0.0259 3.782 19.866 19.638 2820.448 2.244 87.352 3.158 0.76 293910. 0.5133
|
|
39.85 0.2192 0.5361 0.0626 0.0256 3.734 19.611 18.835 2784.215 2.216 83.780 3.068 0.76 294200. 0.4884
|
|
43.47 0.2391 0.5680 0.0598 0.0252 3.673 19.290 17.995 2738.727 2.179 80.040 2.980 0.76 294504. 0.4636
|
|
47.10 0.2590 0.5973 0.0569 0.0247 3.599 18.901 17.116 2683.493 2.135 76.131 2.893 0.76 294822. 0.4389
|
|
50.72 0.2790 0.6240 0.0539 0.0241 3.511 18.440 16.199 2617.992 2.083 72.054 2.807 0.76 295156. 0.4142
|
|
54.34 0.2989 0.6481 0.0507 0.0234 3.409 17.904 15.246 2541.930 2.023 67.815 2.720 0.77 295504. 0.3896
|
|
57.97 0.3188 0.6694 0.0474 0.0226 3.293 17.295 14.261 2455.382 1.954 63.431 2.634 0.77 295867. 0.3648
|
|
61.59 0.3387 0.6878 0.0440 0.0217 3.163 16.612 13.246 2358.475 1.877 58.917 2.547 0.77 296246. 0.3400
|
|
65.21 0.3587 0.7029 0.0406 0.0207 3.019 15.857 12.205 2251.334 1.792 54.286 2.459 0.77 296640. 0.3150
|
|
68.83 0.3786 0.7145 0.0370 0.0196 2.862 15.032 11.140 2134.100 1.698 49.551 2.368 0.77 297049. 0.2898
|
|
72.46 0.3985 0.7218 0.0334 0.0185 2.691 14.136 10.055 2006.957 1.597 44.724 2.272 0.77 297475. 0.2643
|
|
76.08 0.4184 0.7242 0.0298 0.0172 2.508 13.173 8.952 1870.160 1.488 39.821 2.171 0.77 297916. 0.2382
|
|
79.70 0.4384 0.7203 0.0261 0.0159 2.312 12.143 7.836 1724.059 1.372 34.854 2.061 0.77 298373. 0.2116
|
|
83.33 0.4583 0.7084 0.0223 0.0144 2.104 11.052 6.709 1569.127 1.249 29.840 1.939 0.77 298846. 0.1842
|
|
86.95 0.4782 0.6855 0.0185 0.0129 1.885 9.903 5.575 1405.988 1.119 24.797 1.798 0.77 299335. 0.1557
|
|
90.57 0.4981 0.6471 0.0148 0.0114 1.657 8.702 4.439 1235.444 0.983 19.746 1.630 0.77 299841. 0.1259
|
|
94.19 0.5181 0.5852 0.0110 0.0097 1.419 7.456 3.307 1058.503 0.842 14.711 1.417 0.77 300363. 0.0945
|
|
97.82 0.5380 0.4848 0.0073 0.0081 1.175 6.173 2.185 876.391 0.697 9.717 1.131 0.77 300901. 0.0613
|
|
101.44 0.5579 0.3148 0.0036 0.0064 0.926 4.864 1.078 690.496 0.549 4.793 0.708 0.77 301455. 0.0269
|
|
105.06 0.5778 -0.0081 -0.0001 0.0046 0.670 3.519 -0.019 499.592 0.398 -0.087 -0.018 0.77 301993. 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 0.0870 0.0274 5.083 24.643 30.714 3790.198 2.784 136.616 3.676 0.83 316017. 0.7470
|
|
3.92 0.0199 0.0618 0.0855 0.0275 5.102 24.738 30.185 3804.793 2.795 134.261 3.598 0.83 316193. 0.7250
|
|
7.84 0.0398 0.1210 0.0839 0.0276 5.117 24.810 29.618 3815.913 2.803 131.740 3.520 0.83 316381. 0.7026
|
|
11.76 0.0597 0.1775 0.0822 0.0277 5.127 24.855 29.013 3822.884 2.808 129.048 3.442 0.83 316582. 0.6799
|
|
15.68 0.0796 0.2312 0.0804 0.0277 5.129 24.869 28.367 3825.014 2.810 126.177 3.364 0.83 316796. 0.6570
|
|
19.60 0.0995 0.2823 0.0784 0.0276 5.125 24.847 27.680 3821.577 2.807 123.121 3.285 0.83 317023. 0.6339
|
|
23.52 0.1194 0.3306 0.0764 0.0276 5.112 24.783 26.950 3811.797 2.800 119.874 3.207 0.83 317265. 0.6105
|
|
27.44 0.1393 0.3763 0.0742 0.0275 5.089 24.673 26.176 3794.880 2.788 116.430 3.129 0.83 317520. 0.5870
|
|
31.36 0.1592 0.4194 0.0718 0.0273 5.056 24.512 25.356 3770.005 2.769 112.784 3.051 0.83 317790. 0.5633
|
|
35.28 0.1791 0.4598 0.0694 0.0270 5.011 24.293 24.491 3736.345 2.745 108.935 2.973 0.83 318075. 0.5396
|
|
39.20 0.1990 0.4976 0.0668 0.0267 4.953 24.011 23.579 3693.091 2.713 104.879 2.896 0.83 318374. 0.5157
|
|
43.12 0.2189 0.5329 0.0641 0.0263 4.881 23.663 22.621 3639.461 2.673 100.617 2.819 0.83 318690. 0.4917
|
|
47.04 0.2388 0.5655 0.0612 0.0259 4.795 23.245 21.616 3575.271 2.626 96.149 2.742 0.83 319020. 0.4676
|
|
50.96 0.2587 0.5954 0.0583 0.0253 4.693 22.755 20.566 3499.814 2.571 91.477 2.665 0.83 319367. 0.4433
|
|
54.88 0.2786 0.6226 0.0552 0.0247 4.576 22.187 19.469 3412.458 2.507 86.600 2.588 0.83 319729. 0.4187
|
|
58.80 0.2985 0.6469 0.0519 0.0240 4.442 21.538 18.329 3312.674 2.433 81.527 2.510 0.83 320107. 0.3940
|
|
62.72 0.3184 0.6682 0.0486 0.0232 4.292 20.809 17.148 3200.531 2.351 76.275 2.430 0.83 320502. 0.3691
|
|
66.64 0.3383 0.6863 0.0451 0.0223 4.125 19.999 15.932 3075.965 2.259 70.864 2.349 0.83 320913. 0.3439
|
|
70.56 0.3582 0.7008 0.0416 0.0213 3.942 19.110 14.683 2939.291 2.159 65.310 2.266 0.83 321341. 0.3184
|
|
74.48 0.3781 0.7114 0.0380 0.0202 3.742 18.145 13.406 2790.766 2.050 59.628 2.179 0.83 321785. 0.2925
|
|
78.40 0.3980 0.7171 0.0343 0.0190 3.528 17.105 12.103 2630.871 1.933 53.834 2.087 0.83 322246. 0.2662
|
|
82.31 0.4179 0.7171 0.0305 0.0178 3.299 15.996 10.779 2460.233 1.807 47.944 1.987 0.83 322724. 0.2393
|
|
86.23 0.4378 0.7098 0.0267 0.0165 3.057 14.822 9.437 2279.737 1.675 41.974 1.877 0.83 323219. 0.2115
|
|
90.15 0.4577 0.6931 0.0229 0.0151 2.803 13.590 8.081 2090.257 1.535 35.946 1.754 0.83 323731. 0.1828
|
|
94.07 0.4776 0.6638 0.0190 0.0137 2.538 12.307 6.717 1892.935 1.390 29.879 1.610 0.83 324261. 0.1530
|
|
97.99 0.4975 0.6172 0.0152 0.0122 2.265 10.982 5.350 1689.167 1.241 23.799 1.437 0.84 324808. 0.1219
|
|
101.91 0.5174 0.5457 0.0113 0.0107 1.985 9.626 3.987 1480.572 1.088 17.733 1.221 0.84 325373. 0.0894
|
|
105.83 0.5373 0.4367 0.0075 0.0092 1.702 8.251 2.633 1269.018 0.932 11.713 0.941 0.84 325955. 0.0560
|
|
109.75 0.5572 0.2681 0.0037 0.0076 1.417 6.869 1.298 1056.484 0.776 5.774 0.557 0.84 326553. 0.0233
|
|
113.67 0.5771 -0.0066 -0.0001 0.0061 1.127 5.466 -0.025 840.755 0.618 -0.109 -0.013 0.84 327141. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 14000
|
|
|
|
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 0.0888 0.0312 7.221 32.509 36.356 5384.671 3.673 161.711 3.062 0.89 340271. 0.6772
|
|
4.23 0.0200 0.0560 0.0873 0.0311 7.202 32.423 35.747 5370.482 3.663 159.001 3.019 0.89 340463. 0.6620
|
|
8.47 0.0399 0.1104 0.0857 0.0310 7.176 32.307 35.092 5351.192 3.650 156.089 2.974 0.89 340668. 0.6462
|
|
12.70 0.0599 0.1631 0.0840 0.0308 7.143 32.156 34.391 5326.233 3.633 152.969 2.929 0.89 340887. 0.6298
|
|
16.94 0.0799 0.2140 0.0822 0.0307 7.101 31.967 33.640 5294.929 3.612 149.632 2.882 0.89 341120. 0.6129
|
|
21.17 0.0998 0.2630 0.0802 0.0304 7.049 31.736 32.839 5256.596 3.585 146.070 2.834 0.89 341368. 0.5955
|
|
25.41 0.1198 0.3101 0.0781 0.0302 6.987 31.457 31.986 5210.464 3.554 142.273 2.784 0.89 341631. 0.5775
|
|
29.64 0.1397 0.3553 0.0759 0.0299 6.914 31.127 31.078 5155.758 3.517 138.235 2.734 0.89 341910. 0.5590
|
|
33.88 0.1597 0.3984 0.0736 0.0295 6.828 30.740 30.115 5091.687 3.473 133.952 2.683 0.89 342204. 0.5399
|
|
38.11 0.1797 0.4394 0.0711 0.0291 6.729 30.292 29.096 5017.485 3.422 129.419 2.630 0.89 342515. 0.5203
|
|
42.35 0.1996 0.4783 0.0685 0.0286 6.614 29.778 28.020 4932.395 3.364 124.634 2.577 0.89 342842. 0.5002
|
|
46.58 0.2196 0.5150 0.0657 0.0280 6.485 29.194 26.888 4835.662 3.298 119.598 2.522 0.89 343186. 0.4796
|
|
50.81 0.2396 0.5494 0.0628 0.0274 6.338 28.536 25.700 4726.528 3.224 114.312 2.466 0.89 343546. 0.4585
|
|
55.05 0.2595 0.5811 0.0597 0.0267 6.178 27.813 24.455 4606.913 3.142 108.777 2.408 0.89 343923. 0.4367
|
|
59.28 0.2795 0.6097 0.0566 0.0259 6.003 27.027 23.155 4476.581 3.053 102.993 2.346 0.89 344318. 0.4140
|
|
63.52 0.2994 0.6350 0.0533 0.0251 5.814 26.177 21.800 4335.851 2.957 96.968 2.281 0.89 344730. 0.3905
|
|
67.75 0.3194 0.6567 0.0498 0.0242 5.612 25.264 20.397 4184.580 2.854 90.726 2.211 0.89 345159. 0.3662
|
|
71.99 0.3394 0.6737 0.0463 0.0233 5.399 24.306 18.949 4025.986 2.746 84.287 2.135 0.89 345607. 0.3408
|
|
76.22 0.3593 0.6851 0.0427 0.0224 5.180 23.322 17.462 3862.915 2.635 77.670 2.050 0.89 346071. 0.3142
|
|
80.46 0.3793 0.6912 0.0389 0.0214 4.947 22.274 15.939 3689.335 2.516 70.899 1.960 0.89 346554. 0.2869
|
|
84.69 0.3993 0.6912 0.0351 0.0203 4.700 21.161 14.387 3505.002 2.391 63.993 1.862 0.90 347055. 0.2590
|
|
88.93 0.4192 0.6840 0.0313 0.0192 4.440 19.990 12.808 3311.084 2.258 56.972 1.755 0.90 347574. 0.2303
|
|
93.16 0.4392 0.6679 0.0274 0.0180 4.169 18.770 11.209 3109.051 2.121 49.859 1.635 0.90 348111. 0.2008
|
|
97.39 0.4591 0.6405 0.0234 0.0168 3.890 17.514 9.595 2900.963 1.979 42.677 1.500 0.90 348667. 0.1704
|
|
101.63 0.4791 0.5992 0.0195 0.0156 3.605 16.230 7.971 2688.323 1.834 35.454 1.345 0.90 349241. 0.1392
|
|
105.86 0.4991 0.5400 0.0155 0.0143 3.317 14.931 6.345 2473.170 1.687 28.221 1.164 0.90 349835. 0.1075
|
|
110.10 0.5190 0.4581 0.0115 0.0131 3.028 13.631 4.724 2257.783 1.540 21.015 0.949 0.90 350447. 0.0757
|
|
114.33 0.5390 0.3469 0.0076 0.0118 2.742 12.343 3.120 2044.521 1.395 13.876 0.692 0.90 351078. 0.0448
|
|
118.57 0.5590 0.1977 0.0038 0.0106 2.461 11.081 1.539 1835.396 1.252 6.846 0.380 0.90 351727. 0.0173
|
|
122.80 0.5789 -0.0039 -0.0001 0.0094 2.177 9.801 -0.026 1623.465 1.107 -0.114 -0.007 0.90 352376. 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 0.0898 0.0373 10.616 44.609 42.178 7916.701 5.040 187.608 2.417 0.95 364543. 0.5755
|
|
4.59 0.0202 0.0481 0.0884 0.0371 10.558 44.362 41.525 7872.822 5.012 184.701 2.392 0.95 364748. 0.5653
|
|
9.17 0.0404 0.0952 0.0869 0.0368 10.483 44.050 40.814 7817.516 4.977 181.541 2.368 0.95 364968. 0.5548
|
|
13.76 0.0605 0.1413 0.0852 0.0365 10.393 43.671 40.045 7750.219 4.934 178.120 2.344 0.95 365204. 0.5439
|
|
18.34 0.0807 0.1865 0.0834 0.0361 10.286 43.221 39.214 7670.288 4.883 174.425 2.319 0.95 365456. 0.5325
|
|
22.93 0.1009 0.2306 0.0815 0.0357 10.161 42.696 38.319 7577.193 4.824 170.443 2.294 0.95 365725. 0.5207
|
|
27.51 0.1211 0.2736 0.0795 0.0352 10.018 42.094 37.357 7470.413 4.756 166.165 2.268 0.95 366011. 0.5084
|
|
32.10 0.1412 0.3155 0.0773 0.0346 9.856 41.413 36.327 7349.555 4.679 161.582 2.242 0.95 366315. 0.4955
|
|
36.68 0.1614 0.3562 0.0750 0.0340 9.675 40.651 35.227 7214.309 4.593 156.688 2.215 0.95 366636. 0.4821
|
|
41.27 0.1816 0.3956 0.0725 0.0333 9.474 39.807 34.055 7064.435 4.497 151.478 2.187 0.95 366975. 0.4679
|
|
45.85 0.2018 0.4336 0.0698 0.0325 9.253 38.879 32.813 6899.760 4.393 145.951 2.157 0.95 367332. 0.4531
|
|
50.44 0.2219 0.4701 0.0670 0.0316 9.012 37.866 31.499 6720.069 4.278 140.109 2.126 0.95 367708. 0.4376
|
|
55.02 0.2421 0.5050 0.0641 0.0307 8.750 36.768 30.116 6525.113 4.154 133.954 2.093 0.95 368103. 0.4213
|
|
59.61 0.2623 0.5380 0.0610 0.0297 8.468 35.582 28.663 6314.600 4.020 127.491 2.059 0.96 368516. 0.4042
|
|
64.20 0.2825 0.5684 0.0578 0.0287 8.173 34.344 27.140 6094.943 3.880 120.717 2.020 0.96 368948. 0.3859
|
|
68.78 0.3026 0.5955 0.0544 0.0276 7.869 33.065 25.550 5868.010 3.736 113.645 1.975 0.96 369399. 0.3661
|
|
73.37 0.3228 0.6185 0.0509 0.0265 7.560 31.766 23.899 5637.482 3.589 106.304 1.923 0.96 369869. 0.3447
|
|
77.95 0.3430 0.6366 0.0472 0.0254 7.247 30.450 22.195 5403.854 3.440 98.723 1.863 0.96 370359. 0.3219
|
|
82.54 0.3632 0.6465 0.0435 0.0244 6.959 29.240 20.440 5189.142 3.304 90.918 1.787 0.96 370868. 0.2962
|
|
87.12 0.3833 0.6445 0.0397 0.0236 6.719 28.232 18.639 5010.206 3.190 82.905 1.687 0.96 371396. 0.2672
|
|
91.71 0.4035 0.6350 0.0358 0.0227 6.471 27.190 16.803 4825.273 3.072 74.738 1.579 0.96 371944. 0.2374
|
|
96.29 0.4237 0.6170 0.0318 0.0218 6.217 26.121 14.938 4635.702 2.951 66.445 1.462 0.96 372512. 0.2072
|
|
100.88 0.4439 0.5893 0.0278 0.0209 5.958 25.035 13.053 4442.855 2.828 58.059 1.333 0.96 373100. 0.1766
|
|
105.46 0.4640 0.5506 0.0237 0.0200 5.698 23.942 11.155 4248.909 2.705 49.617 1.191 0.96 373707. 0.1458
|
|
110.05 0.4842 0.4992 0.0197 0.0191 5.439 22.855 9.254 4056.112 2.582 41.160 1.035 0.96 374336. 0.1154
|
|
114.64 0.5044 0.4339 0.0157 0.0182 5.186 21.789 7.360 3866.899 2.462 32.739 0.863 0.96 374984. 0.0859
|
|
119.22 0.5246 0.3533 0.0117 0.0173 4.938 20.749 5.487 3682.353 2.344 24.407 0.676 0.97 375654. 0.0581
|
|
123.81 0.5447 0.2563 0.0078 0.0165 4.699 19.743 3.647 3503.819 2.231 16.223 0.472 0.97 376345. 0.0331
|
|
128.39 0.5649 0.1418 0.0039 0.0157 4.467 18.771 1.851 3331.205 2.121 8.231 0.252 0.97 377060. 0.0126
|
|
132.98 0.5851 0.0057 0.0001 0.0148 4.219 17.728 0.068 3146.222 2.003 0.303 0.010 0.97 377816. 0.0001
|
|
|
|
|
|
|