575 lines
102 KiB
Plaintext
575 lines
102 KiB
Plaintext
15x8 (15x8.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 0.0989 0.0446 0.003 0.172 0.160 2.031 0.019 0.709 35.630 0.06 26793. 0.5566
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0.34 0.0241 0.0521 0.0973 0.0449 0.003 0.173 0.157 2.048 0.020 0.698 34.759 0.06 26811. 0.5386
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0.68 0.0481 0.1016 0.0955 0.0453 0.003 0.174 0.154 2.063 0.020 0.686 33.886 0.06 26831. 0.5204
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1.03 0.0722 0.1485 0.0937 0.0456 0.003 0.176 0.151 2.077 0.020 0.672 33.012 0.06 26853. 0.5021
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1.37 0.0963 0.1927 0.0917 0.0458 0.003 0.176 0.148 2.088 0.020 0.658 32.139 0.06 26876. 0.4836
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1.71 0.1204 0.2344 0.0896 0.0460 0.003 0.177 0.144 2.096 0.020 0.643 31.268 0.06 26901. 0.4649
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2.05 0.1444 0.2734 0.0873 0.0461 0.003 0.178 0.141 2.101 0.020 0.626 30.399 0.06 26928. 0.4462
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2.39 0.1685 0.3099 0.0848 0.0461 0.003 0.178 0.137 2.102 0.020 0.609 29.533 0.06 26957. 0.4274
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2.74 0.1926 0.3438 0.0822 0.0461 0.003 0.177 0.133 2.099 0.020 0.590 28.670 0.06 26987. 0.4085
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3.08 0.2167 0.3752 0.0795 0.0459 0.003 0.177 0.128 2.092 0.020 0.570 27.807 0.06 27020. 0.3895
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3.42 0.2407 0.4039 0.0766 0.0456 0.003 0.176 0.124 2.079 0.020 0.549 26.946 0.06 27054. 0.3704
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3.76 0.2648 0.4301 0.0735 0.0452 0.003 0.174 0.119 2.061 0.020 0.527 26.083 0.06 27090. 0.3513
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4.10 0.2889 0.4536 0.0702 0.0447 0.003 0.172 0.113 2.038 0.019 0.504 25.217 0.06 27128. 0.3320
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4.45 0.3129 0.4744 0.0668 0.0441 0.003 0.170 0.108 2.009 0.019 0.480 24.345 0.06 27169. 0.3127
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4.79 0.3370 0.4924 0.0633 0.0433 0.003 0.167 0.102 1.974 0.019 0.454 23.464 0.06 27211. 0.2933
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5.13 0.3611 0.5075 0.0596 0.0424 0.003 0.163 0.096 1.934 0.018 0.428 22.570 0.06 27255. 0.2739
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5.47 0.3852 0.5195 0.0559 0.0414 0.003 0.160 0.090 1.887 0.018 0.401 21.658 0.06 27302. 0.2543
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5.81 0.4092 0.5281 0.0520 0.0403 0.002 0.155 0.084 1.835 0.018 0.373 20.722 0.06 27350. 0.2347
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6.15 0.4333 0.5330 0.0480 0.0390 0.002 0.150 0.077 1.778 0.017 0.344 19.754 0.06 27401. 0.2150
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6.50 0.4574 0.5339 0.0439 0.0376 0.002 0.145 0.071 1.714 0.016 0.315 18.746 0.06 27454. 0.1952
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6.84 0.4814 0.5302 0.0398 0.0361 0.002 0.139 0.064 1.645 0.016 0.285 17.686 0.06 27508. 0.1752
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7.18 0.5055 0.5213 0.0355 0.0344 0.002 0.133 0.057 1.570 0.015 0.255 16.559 0.06 27565. 0.1551
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7.52 0.5296 0.5060 0.0312 0.0327 0.002 0.126 0.050 1.489 0.014 0.224 15.344 0.06 27625. 0.1347
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7.86 0.5537 0.4833 0.0268 0.0308 0.002 0.118 0.043 1.402 0.013 0.193 14.016 0.06 27686. 0.1141
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8.21 0.5777 0.4512 0.0224 0.0287 0.002 0.111 0.036 1.309 0.012 0.161 12.540 0.06 27750. 0.0933
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8.55 0.6018 0.4072 0.0180 0.0266 0.002 0.102 0.029 1.211 0.012 0.129 10.865 0.06 27815. 0.0724
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8.89 0.6259 0.3476 0.0135 0.0243 0.001 0.094 0.022 1.106 0.011 0.097 8.918 0.06 27883. 0.0515
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9.23 0.6500 0.2668 0.0090 0.0219 0.001 0.084 0.014 0.997 0.010 0.064 6.591 0.06 27953. 0.0310
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9.57 0.6740 0.1558 0.0045 0.0194 0.001 0.075 0.007 0.883 0.008 0.032 3.712 0.06 28025. 0.0123
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9.92 0.6981 -0.0010 0.0000 0.0167 0.001 0.064 0.000 0.763 0.007 0.000 -0.024 0.06 28098. 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 0.0993 0.0395 0.019 0.608 0.641 14.383 0.069 2.852 20.216 0.12 53585. 0.6332
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0.69 0.0242 0.0594 0.0977 0.0399 0.020 0.615 0.631 14.541 0.069 2.806 19.675 0.12 53622. 0.6113
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1.38 0.0485 0.1156 0.0960 0.0403 0.020 0.621 0.620 14.686 0.070 2.756 19.137 0.12 53663. 0.5893
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2.07 0.0727 0.1685 0.0942 0.0406 0.020 0.626 0.608 14.815 0.071 2.703 18.603 0.12 53706. 0.5672
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2.76 0.0970 0.2183 0.0922 0.0409 0.020 0.631 0.595 14.924 0.071 2.645 18.075 0.12 53753. 0.5453
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3.44 0.1212 0.2650 0.0900 0.0412 0.020 0.634 0.581 15.010 0.072 2.584 17.553 0.12 53804. 0.5233
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4.13 0.1455 0.3087 0.0877 0.0413 0.020 0.637 0.566 15.069 0.072 2.518 17.037 0.12 53858. 0.5014
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4.82 0.1697 0.3494 0.0853 0.0414 0.020 0.638 0.550 15.098 0.072 2.447 16.529 0.12 53916. 0.4796
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5.51 0.1940 0.3872 0.0826 0.0414 0.020 0.638 0.533 15.093 0.072 2.372 16.027 0.12 53978. 0.4578
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6.20 0.2182 0.4221 0.0799 0.0413 0.020 0.636 0.515 15.050 0.072 2.292 15.532 0.12 54043. 0.4362
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6.89 0.2425 0.4542 0.0769 0.0411 0.020 0.632 0.496 14.966 0.071 2.208 15.043 0.12 54112. 0.4146
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7.58 0.2667 0.4836 0.0738 0.0407 0.020 0.627 0.476 14.836 0.071 2.118 14.559 0.12 54186. 0.3930
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8.27 0.2909 0.5102 0.0705 0.0402 0.020 0.620 0.455 14.660 0.070 2.024 14.080 0.12 54263. 0.3715
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8.95 0.3152 0.5340 0.0671 0.0396 0.019 0.610 0.433 14.436 0.069 1.926 13.603 0.12 54345. 0.3501
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9.64 0.3394 0.5550 0.0635 0.0389 0.019 0.599 0.410 14.163 0.068 1.823 13.129 0.12 54430. 0.3288
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10.33 0.3637 0.5731 0.0598 0.0380 0.019 0.585 0.386 13.842 0.066 1.717 12.653 0.12 54520. 0.3076
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11.02 0.3879 0.5882 0.0560 0.0370 0.018 0.569 0.362 13.470 0.064 1.608 12.174 0.12 54614. 0.2863
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11.71 0.4122 0.6000 0.0521 0.0358 0.017 0.551 0.336 13.049 0.062 1.496 11.688 0.12 54712. 0.2651
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12.40 0.4364 0.6083 0.0481 0.0345 0.017 0.532 0.310 12.578 0.060 1.380 11.191 0.12 54815. 0.2439
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13.09 0.4607 0.6127 0.0440 0.0331 0.016 0.509 0.284 12.056 0.058 1.263 10.679 0.12 54922. 0.2226
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13.78 0.4849 0.6127 0.0398 0.0315 0.015 0.485 0.257 11.482 0.055 1.142 10.145 0.12 55033. 0.2011
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14.46 0.5092 0.6075 0.0355 0.0298 0.015 0.459 0.229 10.857 0.052 1.020 9.579 0.12 55148. 0.1794
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15.15 0.5334 0.5960 0.0312 0.0279 0.014 0.430 0.201 10.180 0.049 0.896 8.971 0.12 55268. 0.1575
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15.84 0.5577 0.5767 0.0268 0.0259 0.013 0.399 0.173 9.452 0.045 0.770 8.304 0.12 55393. 0.1351
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16.53 0.5819 0.5474 0.0224 0.0238 0.012 0.366 0.144 8.672 0.041 0.642 7.553 0.12 55521. 0.1123
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17.22 0.6061 0.5045 0.0179 0.0215 0.011 0.331 0.116 7.842 0.037 0.514 6.683 0.12 55655. 0.0889
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17.91 0.6304 0.4425 0.0134 0.0191 0.009 0.294 0.087 6.964 0.033 0.385 5.636 0.12 55792. 0.0649
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18.60 0.6546 0.3519 0.0089 0.0166 0.008 0.255 0.057 6.038 0.029 0.256 4.316 0.12 55934. 0.0405
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19.29 0.6789 0.2149 0.0044 0.0139 0.007 0.214 0.028 5.068 0.024 0.126 2.542 0.12 56080. 0.0168
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19.98 0.7031 -0.0068 -0.0001 0.0111 0.005 0.171 -0.001 4.050 0.019 -0.003 -0.077 0.12 56226. 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 0.0997 0.0374 0.062 1.297 1.448 46.027 0.147 6.440 14.268 0.18 80375. 0.6716
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1.04 0.0243 0.0629 0.0981 0.0379 0.062 1.313 1.425 46.590 0.148 6.337 13.870 0.18 80432. 0.6476
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2.07 0.0486 0.1223 0.0964 0.0383 0.063 1.327 1.400 47.110 0.150 6.226 13.476 0.18 80493. 0.6237
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3.11 0.0729 0.1781 0.0945 0.0387 0.064 1.340 1.373 47.575 0.151 6.106 13.087 0.18 80558. 0.5998
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4.14 0.0972 0.2306 0.0925 0.0390 0.064 1.352 1.344 47.973 0.153 5.976 12.704 0.18 80629. 0.5760
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5.18 0.1214 0.2797 0.0904 0.0393 0.065 1.361 1.312 48.294 0.154 5.838 12.326 0.18 80705. 0.5524
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6.21 0.1457 0.3255 0.0881 0.0394 0.065 1.367 1.279 48.523 0.154 5.689 11.956 0.18 80787. 0.5289
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7.25 0.1700 0.3682 0.0856 0.0395 0.065 1.371 1.243 48.649 0.155 5.530 11.592 0.18 80874. 0.5056
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8.28 0.1943 0.4078 0.0830 0.0395 0.065 1.371 1.205 48.658 0.155 5.361 11.235 0.18 80967. 0.4825
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9.32 0.2186 0.4445 0.0802 0.0395 0.065 1.368 1.165 48.537 0.154 5.181 10.884 0.18 81065. 0.4595
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10.35 0.2429 0.4783 0.0773 0.0392 0.065 1.360 1.122 48.275 0.154 4.990 10.540 0.18 81170. 0.4367
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11.39 0.2672 0.5092 0.0741 0.0389 0.064 1.348 1.076 47.858 0.152 4.788 10.202 0.18 81280. 0.4140
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12.42 0.2915 0.5373 0.0708 0.0384 0.063 1.332 1.029 47.280 0.150 4.576 9.868 0.18 81397. 0.3915
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13.46 0.3157 0.5627 0.0674 0.0378 0.062 1.311 0.979 46.535 0.148 4.353 9.539 0.18 81519. 0.3692
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14.49 0.3400 0.5853 0.0638 0.0371 0.061 1.285 0.927 45.622 0.145 4.122 9.214 0.18 81648. 0.3470
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15.53 0.3643 0.6050 0.0601 0.0362 0.060 1.255 0.873 44.539 0.142 3.883 8.890 0.18 81783. 0.3249
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16.56 0.3886 0.6219 0.0563 0.0352 0.058 1.219 0.817 43.283 0.138 3.636 8.566 0.18 81925. 0.3029
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17.60 0.4129 0.6356 0.0524 0.0340 0.056 1.179 0.760 41.854 0.133 3.382 8.240 0.18 82073. 0.2810
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18.63 0.4372 0.6459 0.0483 0.0327 0.054 1.134 0.702 40.248 0.128 3.122 7.909 0.18 82227. 0.2592
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19.67 0.4615 0.6526 0.0442 0.0313 0.052 1.084 0.642 38.465 0.122 2.855 7.570 0.18 82388. 0.2373
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20.70 0.4858 0.6551 0.0400 0.0297 0.049 1.028 0.581 36.502 0.116 2.584 7.219 0.18 82555. 0.2152
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21.74 0.5101 0.6527 0.0357 0.0279 0.046 0.968 0.519 34.359 0.109 2.308 6.849 0.18 82729. 0.1930
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22.77 0.5343 0.6442 0.0314 0.0260 0.043 0.903 0.456 32.034 0.102 2.027 6.454 0.18 82910. 0.1704
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23.81 0.5586 0.6283 0.0270 0.0240 0.040 0.832 0.392 29.529 0.094 1.743 6.020 0.18 83097. 0.1474
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24.84 0.5829 0.6024 0.0225 0.0218 0.036 0.756 0.327 26.844 0.085 1.456 5.532 0.18 83290. 0.1238
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25.88 0.6072 0.5628 0.0181 0.0195 0.032 0.676 0.262 23.983 0.076 1.167 4.961 0.18 83491. 0.0994
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26.91 0.6315 0.5030 0.0136 0.0170 0.028 0.590 0.197 20.951 0.067 0.876 4.263 0.18 83698. 0.0740
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27.95 0.6558 0.4113 0.0091 0.0144 0.024 0.500 0.131 17.755 0.057 0.585 3.357 0.18 83911. 0.0476
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28.98 0.6801 0.2640 0.0045 0.0117 0.019 0.406 0.066 14.404 0.046 0.294 2.078 0.18 84130. 0.0209
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30.02 0.7044 0.0022 0.0000 0.0088 0.015 0.306 0.000 10.877 0.035 0.002 0.016 0.18 84348. 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 0.1001 0.0363 0.142 2.239 2.585 105.964 0.253 11.497 11.064 0.24 107164. 0.6958
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1.38 0.0243 0.0652 0.0985 0.0368 0.144 2.268 2.544 107.345 0.256 11.314 10.747 0.24 107239. 0.6705
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2.77 0.0487 0.1265 0.0968 0.0372 0.146 2.295 2.499 108.624 0.259 11.115 10.435 0.24 107321. 0.6453
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4.15 0.0730 0.1842 0.0949 0.0376 0.147 2.320 2.451 109.772 0.262 10.902 10.127 0.24 107409. 0.6202
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5.53 0.0974 0.2383 0.0929 0.0380 0.149 2.340 2.399 110.761 0.264 10.671 9.825 0.24 107504. 0.5953
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6.92 0.1217 0.2889 0.0908 0.0383 0.150 2.357 2.344 111.563 0.266 10.424 9.528 0.24 107606. 0.5706
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8.30 0.1461 0.3361 0.0885 0.0385 0.150 2.370 2.284 112.147 0.268 10.159 9.237 0.24 107715. 0.5461
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9.68 0.1704 0.3800 0.0860 0.0386 0.151 2.377 2.220 112.482 0.269 9.876 8.953 0.24 107832. 0.5218
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11.06 0.1947 0.4208 0.0834 0.0386 0.151 2.378 2.152 112.536 0.269 9.573 8.675 0.24 107956. 0.4978
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12.45 0.2191 0.4585 0.0806 0.0385 0.151 2.372 2.080 112.278 0.268 9.252 8.402 0.24 108088. 0.4740
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13.83 0.2434 0.4933 0.0776 0.0383 0.150 2.360 2.003 111.677 0.267 8.910 8.136 0.24 108228. 0.4505
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15.21 0.2678 0.5252 0.0745 0.0380 0.148 2.339 1.922 110.705 0.264 8.549 7.875 0.24 108376. 0.4271
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16.60 0.2921 0.5544 0.0712 0.0375 0.147 2.310 1.837 109.343 0.261 8.170 7.619 0.24 108532. 0.4039
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17.98 0.3165 0.5807 0.0677 0.0369 0.144 2.273 1.747 107.578 0.257 7.772 7.367 0.24 108696. 0.3810
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19.36 0.3408 0.6043 0.0641 0.0361 0.141 2.227 1.654 105.405 0.252 7.359 7.119 0.24 108868. 0.3582
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20.75 0.3651 0.6252 0.0604 0.0353 0.138 2.173 1.558 102.820 0.245 6.931 6.874 0.24 109049. 0.3356
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22.13 0.3895 0.6431 0.0565 0.0342 0.134 2.109 1.459 99.817 0.238 6.489 6.629 0.24 109239. 0.3132
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23.51 0.4138 0.6581 0.0526 0.0331 0.129 2.037 1.357 96.391 0.230 6.035 6.384 0.24 109437. 0.2909
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24.90 0.4382 0.6698 0.0485 0.0317 0.124 1.955 1.252 92.538 0.221 5.569 6.137 0.24 109644. 0.2686
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26.28 0.4625 0.6780 0.0444 0.0303 0.118 1.865 1.145 88.252 0.211 5.094 5.885 0.24 109859. 0.2464
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27.66 0.4869 0.6822 0.0401 0.0286 0.112 1.765 1.036 83.530 0.199 4.608 5.626 0.24 110083. 0.2240
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29.05 0.5112 0.6817 0.0358 0.0269 0.105 1.656 0.925 78.369 0.187 4.115 5.354 0.24 110316. 0.2014
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30.43 0.5355 0.6754 0.0315 0.0250 0.098 1.538 0.812 72.767 0.174 3.613 5.063 0.24 110558. 0.1785
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31.81 0.5599 0.6619 0.0270 0.0229 0.089 1.410 0.698 66.724 0.159 3.105 4.746 0.24 110808. 0.1551
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33.19 0.5842 0.6385 0.0226 0.0207 0.081 1.273 0.583 60.246 0.144 2.592 4.388 0.24 111068. 0.1310
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34.58 0.6086 0.6014 0.0181 0.0183 0.072 1.127 0.467 53.340 0.127 2.075 3.967 0.24 111336. 0.1060
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35.96 0.6329 0.5434 0.0135 0.0158 0.062 0.972 0.350 46.018 0.110 1.556 3.447 0.24 111613. 0.0797
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37.34 0.6572 0.4512 0.0090 0.0131 0.051 0.809 0.233 38.298 0.091 1.035 2.756 0.24 111899. 0.0520
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38.73 0.6816 0.2956 0.0045 0.0104 0.040 0.638 0.116 30.200 0.072 0.516 1.741 0.24 112192. 0.0232
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40.11 0.7059 -0.0057 -0.0001 0.0074 0.029 0.457 -0.002 21.647 0.052 -0.007 -0.033 0.24 112480. 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 0.1006 0.0357 0.273 3.440 4.058 203.512 0.389 18.051 9.045 0.30 133950. 0.7128
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1.73 0.0244 0.0667 0.0990 0.0362 0.277 3.487 3.994 206.280 0.394 17.765 8.782 0.30 134045. 0.6866
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3.46 0.0488 0.1294 0.0973 0.0367 0.280 3.530 3.924 208.847 0.399 17.456 8.523 0.30 134147. 0.6605
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5.19 0.0731 0.1883 0.0954 0.0371 0.283 3.569 3.849 211.157 0.403 17.121 8.268 0.30 134258. 0.6346
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6.93 0.0975 0.2434 0.0934 0.0374 0.286 3.603 3.768 213.153 0.407 16.761 8.018 0.30 134377. 0.6089
|
|
8.66 0.1219 0.2950 0.0913 0.0377 0.288 3.631 3.681 214.779 0.410 16.374 7.774 0.30 134504. 0.5835
|
|
10.39 0.1463 0.3431 0.0890 0.0379 0.290 3.651 3.588 215.973 0.412 15.959 7.535 0.30 134641. 0.5583
|
|
12.12 0.1706 0.3879 0.0865 0.0380 0.291 3.663 3.488 216.674 0.414 15.514 7.301 0.30 134788. 0.5334
|
|
13.85 0.1950 0.4295 0.0838 0.0381 0.291 3.665 3.381 216.819 0.414 15.040 7.073 0.30 134943. 0.5088
|
|
15.58 0.2194 0.4680 0.0810 0.0380 0.290 3.657 3.268 216.346 0.413 14.535 6.851 0.30 135109. 0.4844
|
|
17.31 0.2438 0.5035 0.0780 0.0378 0.289 3.638 3.147 215.194 0.411 13.999 6.634 0.30 135284. 0.4604
|
|
19.04 0.2681 0.5361 0.0749 0.0374 0.286 3.606 3.020 213.306 0.407 13.432 6.421 0.30 135470. 0.4365
|
|
20.78 0.2925 0.5659 0.0715 0.0370 0.282 3.561 2.886 210.643 0.402 12.836 6.214 0.30 135666. 0.4129
|
|
22.51 0.3169 0.5930 0.0681 0.0364 0.278 3.502 2.745 207.182 0.396 12.211 6.010 0.30 135872. 0.3896
|
|
24.24 0.3413 0.6174 0.0644 0.0356 0.272 3.430 2.599 202.910 0.388 11.562 5.810 0.30 136088. 0.3664
|
|
25.97 0.3657 0.6390 0.0607 0.0347 0.265 3.344 2.448 197.816 0.378 10.889 5.613 0.30 136315. 0.3435
|
|
27.70 0.3900 0.6579 0.0568 0.0337 0.257 3.244 2.292 191.892 0.366 10.194 5.417 0.30 136553. 0.3208
|
|
29.43 0.4144 0.6738 0.0528 0.0325 0.248 3.129 2.131 185.128 0.354 9.480 5.222 0.30 136801. 0.2982
|
|
31.16 0.4388 0.6866 0.0488 0.0312 0.238 3.001 1.967 177.512 0.339 8.749 5.026 0.30 137060. 0.2757
|
|
32.89 0.4632 0.6960 0.0446 0.0297 0.227 2.857 1.799 169.036 0.323 8.000 4.826 0.30 137330. 0.2532
|
|
34.63 0.4875 0.7015 0.0403 0.0280 0.214 2.699 1.627 159.691 0.305 7.237 4.621 0.30 137611. 0.2306
|
|
36.36 0.5119 0.7026 0.0360 0.0262 0.200 2.527 1.453 149.471 0.285 6.461 4.408 0.30 137903. 0.2078
|
|
38.09 0.5363 0.6981 0.0316 0.0243 0.186 2.339 1.275 138.372 0.264 5.673 4.181 0.30 138206. 0.1847
|
|
39.82 0.5607 0.6865 0.0272 0.0222 0.170 2.137 1.096 126.398 0.241 4.875 3.933 0.30 138520. 0.1610
|
|
41.55 0.5850 0.6654 0.0227 0.0199 0.152 1.920 0.915 113.556 0.217 4.068 3.653 0.30 138845. 0.1367
|
|
43.28 0.6094 0.6307 0.0181 0.0175 0.134 1.688 0.732 99.861 0.191 3.255 3.324 0.30 139182. 0.1112
|
|
45.01 0.6338 0.5750 0.0136 0.0150 0.114 1.443 0.548 85.339 0.163 2.438 2.914 0.30 139529. 0.0844
|
|
46.75 0.6582 0.4836 0.0090 0.0123 0.094 1.184 0.364 70.026 0.134 1.621 2.360 0.30 139887. 0.0557
|
|
48.48 0.6825 0.3230 0.0045 0.0095 0.072 0.912 0.181 53.962 0.103 0.804 1.520 0.30 140255. 0.0253
|
|
50.21 0.7069 -0.0119 -0.0001 0.0065 0.050 0.624 -0.004 36.932 0.071 -0.020 -0.054 0.30 140609. 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 0.1012 0.0354 0.467 4.910 5.878 348.514 0.555 26.144 7.650 0.36 160733. 0.7255
|
|
2.08 0.0244 0.0677 0.0996 0.0359 0.474 4.978 5.785 353.409 0.562 25.733 7.425 0.36 160846. 0.6986
|
|
4.16 0.0488 0.1314 0.0979 0.0364 0.480 5.042 5.685 357.950 0.570 25.287 7.204 0.36 160970. 0.6719
|
|
6.24 0.0732 0.1911 0.0960 0.0368 0.486 5.100 5.577 362.040 0.576 24.805 6.987 0.36 161103. 0.6454
|
|
8.32 0.0976 0.2471 0.0940 0.0371 0.490 5.150 5.460 365.582 0.582 24.286 6.774 0.36 161246. 0.6192
|
|
10.40 0.1220 0.2993 0.0918 0.0374 0.494 5.191 5.334 368.474 0.586 23.727 6.566 0.36 161400. 0.5932
|
|
12.48 0.1464 0.3481 0.0895 0.0377 0.497 5.221 5.199 370.610 0.590 23.127 6.363 0.36 161565. 0.5676
|
|
14.56 0.1708 0.3935 0.0870 0.0378 0.499 5.239 5.055 371.880 0.592 22.485 6.166 0.36 161741. 0.5423
|
|
16.64 0.1952 0.4357 0.0844 0.0378 0.499 5.243 4.901 372.176 0.592 21.799 5.973 0.36 161929. 0.5172
|
|
18.72 0.2196 0.4747 0.0816 0.0377 0.498 5.232 4.737 371.388 0.591 21.069 5.785 0.36 162128. 0.4925
|
|
20.80 0.2440 0.5107 0.0786 0.0375 0.495 5.204 4.562 369.409 0.588 20.293 5.602 0.36 162339. 0.4680
|
|
22.88 0.2684 0.5439 0.0754 0.0372 0.491 5.158 4.378 366.140 0.583 19.472 5.423 0.36 162563. 0.4439
|
|
24.96 0.2928 0.5743 0.0720 0.0367 0.485 5.093 4.183 361.510 0.575 18.608 5.249 0.36 162798. 0.4200
|
|
27.04 0.3172 0.6019 0.0685 0.0361 0.477 5.008 3.980 355.479 0.566 17.703 5.078 0.36 163046. 0.3963
|
|
29.12 0.3416 0.6269 0.0649 0.0354 0.467 4.903 3.768 348.023 0.554 16.762 4.911 0.36 163307. 0.3729
|
|
31.20 0.3660 0.6492 0.0611 0.0345 0.455 4.777 3.549 339.126 0.540 15.786 4.747 0.36 163580. 0.3498
|
|
33.28 0.3904 0.6687 0.0572 0.0334 0.441 4.631 3.323 328.769 0.523 14.779 4.584 0.36 163866. 0.3269
|
|
35.36 0.4148 0.6854 0.0532 0.0322 0.425 4.465 3.090 316.935 0.504 13.744 4.422 0.36 164165. 0.3041
|
|
37.44 0.4393 0.6991 0.0491 0.0308 0.407 4.277 2.851 303.605 0.483 12.683 4.260 0.36 164477. 0.2814
|
|
39.52 0.4637 0.7095 0.0449 0.0293 0.387 4.068 2.607 288.764 0.460 11.598 4.095 0.36 164802. 0.2587
|
|
41.60 0.4881 0.7162 0.0406 0.0277 0.365 3.837 2.359 272.396 0.434 10.491 3.927 0.36 165140. 0.2359
|
|
43.68 0.5125 0.7185 0.0363 0.0259 0.341 3.585 2.105 254.490 0.405 9.365 3.752 0.36 165491. 0.2130
|
|
45.76 0.5369 0.7155 0.0318 0.0239 0.315 3.311 1.848 235.041 0.374 8.222 3.567 0.36 165855. 0.1897
|
|
47.84 0.5613 0.7057 0.0273 0.0217 0.287 3.015 1.588 214.053 0.341 7.064 3.365 0.36 166233. 0.1659
|
|
49.92 0.5857 0.6866 0.0228 0.0195 0.257 2.698 1.325 191.540 0.305 5.894 3.138 0.36 166624. 0.1413
|
|
51.99 0.6101 0.6541 0.0182 0.0170 0.225 2.360 1.060 167.530 0.267 4.714 2.870 0.36 167029. 0.1156
|
|
54.07 0.6345 0.6006 0.0137 0.0144 0.191 2.001 0.794 142.067 0.226 3.530 2.534 0.36 167446. 0.0883
|
|
56.15 0.6589 0.5106 0.0091 0.0117 0.155 1.623 0.527 115.215 0.183 2.343 2.074 0.36 167877. 0.0589
|
|
58.23 0.6833 0.3468 0.0045 0.0088 0.117 1.226 0.261 87.044 0.139 1.160 1.358 0.37 168319. 0.0271
|
|
60.31 0.7077 -0.0188 -0.0002 0.0058 0.077 0.804 -0.009 57.059 0.091 -0.040 -0.071 0.37 168737. 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 0.1019 0.0353 0.740 6.660 8.055 551.573 0.752 35.827 6.623 0.42 187511. 0.7353
|
|
2.43 0.0244 0.0684 0.1003 0.0358 0.750 6.756 7.929 559.516 0.763 35.268 6.428 0.42 187644. 0.7080
|
|
4.86 0.0488 0.1328 0.0986 0.0363 0.760 6.845 7.793 566.890 0.773 34.662 6.235 0.42 187788. 0.6809
|
|
7.29 0.0733 0.1931 0.0967 0.0367 0.769 6.925 7.645 573.537 0.782 34.006 6.046 0.42 187944. 0.6540
|
|
9.71 0.0977 0.2496 0.0947 0.0371 0.777 6.995 7.486 579.297 0.790 33.298 5.861 0.42 188112. 0.6273
|
|
12.14 0.1221 0.3024 0.0925 0.0374 0.783 7.052 7.315 584.006 0.797 32.536 5.681 0.42 188292. 0.6010
|
|
14.57 0.1465 0.3517 0.0902 0.0376 0.788 7.094 7.131 587.494 0.801 31.717 5.505 0.42 188485. 0.5750
|
|
17.00 0.1710 0.3975 0.0877 0.0377 0.791 7.119 6.933 589.586 0.804 30.839 5.334 0.42 188692. 0.5494
|
|
19.43 0.1954 0.4401 0.0850 0.0378 0.791 7.125 6.722 590.104 0.805 29.901 5.167 0.42 188911. 0.5241
|
|
21.86 0.2198 0.4796 0.0822 0.0377 0.790 7.110 6.498 588.872 0.803 28.902 5.005 0.42 189145. 0.4990
|
|
24.29 0.2442 0.5160 0.0792 0.0375 0.785 7.072 6.259 585.720 0.799 27.840 4.847 0.42 189392. 0.4743
|
|
26.71 0.2687 0.5496 0.0760 0.0371 0.778 7.009 6.006 580.487 0.792 26.716 4.693 0.42 189653. 0.4499
|
|
29.14 0.2931 0.5805 0.0726 0.0367 0.768 6.919 5.740 573.057 0.782 25.532 4.543 0.42 189929. 0.4258
|
|
31.57 0.3175 0.6086 0.0691 0.0360 0.755 6.802 5.461 563.365 0.769 24.292 4.397 0.42 190220. 0.4019
|
|
34.00 0.3419 0.6340 0.0654 0.0353 0.739 6.658 5.171 551.373 0.752 23.000 4.254 0.42 190525. 0.3784
|
|
36.43 0.3664 0.6569 0.0616 0.0344 0.720 6.485 4.870 537.053 0.733 21.662 4.113 0.42 190844. 0.3551
|
|
38.86 0.3908 0.6770 0.0577 0.0333 0.698 6.283 4.560 520.378 0.710 20.281 3.974 0.42 191179. 0.3320
|
|
41.29 0.4152 0.6944 0.0536 0.0321 0.672 6.053 4.240 501.319 0.684 18.860 3.836 0.42 191528. 0.3090
|
|
43.72 0.4396 0.7088 0.0495 0.0307 0.643 5.794 3.913 479.848 0.655 17.404 3.698 0.42 191893. 0.2862
|
|
46.14 0.4641 0.7200 0.0453 0.0292 0.611 5.505 3.578 455.937 0.622 15.915 3.559 0.42 192273. 0.2634
|
|
48.57 0.4885 0.7277 0.0409 0.0275 0.576 5.187 3.236 429.563 0.586 14.396 3.417 0.42 192669. 0.2405
|
|
51.00 0.5129 0.7311 0.0365 0.0256 0.537 4.838 2.889 400.708 0.547 12.850 3.270 0.42 193079. 0.2174
|
|
53.43 0.5373 0.7295 0.0321 0.0236 0.495 4.460 2.536 369.365 0.504 11.280 3.114 0.42 193505. 0.1940
|
|
55.86 0.5618 0.7212 0.0276 0.0215 0.450 4.051 2.179 335.538 0.458 9.691 2.945 0.42 193947. 0.1700
|
|
58.29 0.5862 0.7039 0.0230 0.0191 0.401 3.613 1.817 299.250 0.408 8.084 2.755 0.42 194404. 0.1453
|
|
60.72 0.6106 0.6735 0.0184 0.0167 0.349 3.146 1.453 260.548 0.355 6.465 2.530 0.42 194877. 0.1193
|
|
63.14 0.6350 0.6222 0.0138 0.0140 0.294 2.650 1.088 219.505 0.299 4.838 2.248 0.42 195365. 0.0917
|
|
65.57 0.6595 0.5338 0.0091 0.0113 0.236 2.128 0.721 176.222 0.240 3.209 1.857 0.43 195869. 0.0617
|
|
68.00 0.6839 0.3679 0.0045 0.0084 0.175 1.580 0.356 130.813 0.178 1.583 1.234 0.43 196386. 0.0288
|
|
70.43 0.7083 -0.0274 -0.0002 0.0053 0.110 0.993 -0.016 82.240 0.112 -0.072 -0.089 0.43 196862. 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 0.1027 0.0353 1.105 8.709 10.604 824.316 0.984 47.165 5.834 0.48 214284. 0.7432
|
|
2.78 0.0244 0.0689 0.1011 0.0359 1.122 8.837 10.440 836.444 0.998 46.437 5.661 0.48 214436. 0.7155
|
|
5.56 0.0489 0.1337 0.0994 0.0363 1.137 8.956 10.262 847.706 1.012 45.647 5.491 0.48 214602. 0.6881
|
|
8.33 0.0733 0.1945 0.0975 0.0368 1.150 9.064 10.070 857.859 1.024 44.790 5.324 0.48 214781. 0.6609
|
|
11.11 0.0978 0.2514 0.0955 0.0371 1.162 9.157 9.862 866.663 1.035 43.865 5.161 0.48 214973. 0.6340
|
|
13.89 0.1222 0.3046 0.0933 0.0375 1.172 9.233 9.637 873.864 1.043 42.867 5.002 0.48 215180. 0.6074
|
|
16.67 0.1467 0.3542 0.0910 0.0377 1.179 9.289 9.396 879.207 1.049 41.793 4.847 0.48 215402. 0.5812
|
|
19.45 0.1711 0.4004 0.0885 0.0378 1.183 9.323 9.137 882.422 1.053 40.642 4.697 0.48 215638. 0.5553
|
|
22.22 0.1956 0.4433 0.0858 0.0379 1.184 9.332 8.860 883.243 1.054 39.411 4.550 0.48 215890. 0.5298
|
|
25.00 0.2200 0.4831 0.0830 0.0378 1.182 9.312 8.565 881.406 1.052 38.098 4.408 0.48 216158. 0.5046
|
|
27.78 0.2445 0.5199 0.0799 0.0376 1.176 9.262 8.251 876.649 1.046 36.702 4.269 0.48 216442. 0.4797
|
|
30.56 0.2689 0.5539 0.0767 0.0372 1.165 9.178 7.919 868.734 1.037 35.224 4.135 0.48 216742. 0.4551
|
|
33.33 0.2933 0.5851 0.0733 0.0368 1.150 9.060 7.569 857.480 1.024 33.665 4.003 0.48 217058. 0.4308
|
|
36.11 0.3178 0.6136 0.0697 0.0361 1.130 8.904 7.201 842.787 1.006 32.032 3.876 0.48 217391. 0.4068
|
|
38.89 0.3422 0.6395 0.0660 0.0353 1.106 8.712 6.819 824.601 0.984 30.331 3.751 0.48 217741. 0.3831
|
|
41.67 0.3667 0.6628 0.0622 0.0344 1.077 8.483 6.422 802.879 0.958 28.567 3.628 0.48 218107. 0.3597
|
|
44.45 0.3911 0.6834 0.0582 0.0333 1.043 8.215 6.013 777.581 0.928 26.747 3.508 0.48 218491. 0.3365
|
|
47.22 0.4156 0.7014 0.0542 0.0321 1.004 7.910 5.592 748.666 0.894 24.874 3.388 0.48 218892. 0.3134
|
|
50.00 0.4400 0.7165 0.0500 0.0307 0.960 7.566 5.160 716.090 0.855 22.953 3.269 0.48 219310. 0.2905
|
|
52.78 0.4645 0.7285 0.0457 0.0291 0.912 7.182 4.719 679.814 0.811 20.989 3.148 0.48 219745. 0.2675
|
|
55.56 0.4889 0.7370 0.0413 0.0274 0.858 6.760 4.268 639.802 0.764 18.986 3.026 0.48 220198. 0.2446
|
|
58.34 0.5134 0.7415 0.0369 0.0255 0.799 6.297 3.810 596.028 0.711 16.947 2.899 0.48 220668. 0.2214
|
|
61.11 0.5378 0.7410 0.0324 0.0235 0.736 5.795 3.344 548.479 0.655 14.876 2.766 0.48 221157. 0.1978
|
|
63.89 0.5622 0.7341 0.0278 0.0213 0.667 5.253 2.873 497.164 0.593 12.778 2.621 0.48 221662. 0.1738
|
|
66.67 0.5867 0.7184 0.0232 0.0189 0.593 4.671 2.396 442.119 0.528 10.658 2.458 0.48 222186. 0.1488
|
|
69.45 0.6111 0.6899 0.0186 0.0164 0.514 4.051 1.916 383.412 0.458 8.521 2.266 0.48 222727. 0.1227
|
|
72.22 0.6356 0.6408 0.0139 0.0138 0.431 3.393 1.433 321.156 0.383 6.373 2.024 0.49 223286. 0.0948
|
|
75.00 0.6600 0.5542 0.0092 0.0110 0.343 2.700 0.949 255.507 0.305 4.223 1.685 0.49 223863. 0.0642
|
|
77.78 0.6845 0.3869 0.0045 0.0080 0.250 1.972 0.467 186.636 0.223 2.077 1.135 0.49 224454. 0.0303
|
|
80.56 0.7089 -0.0394 -0.0003 0.0048 0.151 1.188 -0.028 112.436 0.134 -0.123 -0.112 0.49 224979. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 9000
|
|
|
|
V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
|
|
(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
|
|
0.00 0.0000 0.0000 0.1036 0.0355 1.582 11.079 13.543 1179.735 1.252 60.237 5.207 0.54 241050. 0.7495
|
|
3.13 0.0245 0.0693 0.1021 0.0360 1.606 11.246 13.337 1197.439 1.271 59.321 5.052 0.54 241222. 0.7217
|
|
6.26 0.0489 0.1344 0.1003 0.0365 1.628 11.400 13.112 1213.881 1.288 58.324 4.899 0.54 241409. 0.6940
|
|
9.38 0.0734 0.1954 0.0985 0.0370 1.648 11.539 12.869 1228.703 1.304 57.241 4.750 0.54 241611. 0.6666
|
|
12.51 0.0979 0.2526 0.0965 0.0374 1.665 11.660 12.605 1241.552 1.317 56.069 4.605 0.54 241829. 0.6396
|
|
15.64 0.1223 0.3060 0.0943 0.0377 1.679 11.759 12.321 1252.069 1.328 54.803 4.463 0.54 242063. 0.6128
|
|
18.77 0.1468 0.3559 0.0919 0.0379 1.690 11.832 12.014 1259.870 1.337 53.440 4.325 0.54 242313. 0.5865
|
|
21.89 0.1713 0.4023 0.0894 0.0381 1.696 11.876 11.685 1264.575 1.342 51.976 4.191 0.54 242580. 0.5604
|
|
25.02 0.1957 0.4455 0.0867 0.0381 1.697 11.888 11.333 1265.793 1.343 50.409 4.061 0.54 242865. 0.5348
|
|
28.15 0.2202 0.4855 0.0838 0.0380 1.694 11.863 10.957 1263.146 1.340 48.737 3.934 0.54 243168. 0.5095
|
|
31.28 0.2447 0.5226 0.0808 0.0378 1.685 11.798 10.557 1256.256 1.333 46.957 3.812 0.54 243488. 0.4844
|
|
34.41 0.2691 0.5569 0.0775 0.0375 1.669 11.690 10.133 1244.778 1.321 45.071 3.692 0.54 243827. 0.4597
|
|
37.53 0.2936 0.5884 0.0741 0.0370 1.647 11.537 9.685 1228.452 1.303 43.081 3.576 0.54 244185. 0.4353
|
|
40.66 0.3181 0.6173 0.0705 0.0363 1.619 11.337 9.216 1207.132 1.281 40.995 3.463 0.54 244561. 0.4112
|
|
43.79 0.3425 0.6436 0.0668 0.0355 1.583 11.089 8.728 1180.740 1.253 38.820 3.353 0.54 244955. 0.3874
|
|
46.92 0.3670 0.6673 0.0629 0.0346 1.541 10.793 8.221 1149.217 1.219 36.565 3.244 0.54 245369. 0.3639
|
|
50.04 0.3915 0.6885 0.0589 0.0335 1.492 10.448 7.697 1112.506 1.180 34.237 3.138 0.54 245802. 0.3406
|
|
53.17 0.4159 0.7070 0.0548 0.0322 1.436 10.054 7.158 1070.552 1.136 31.840 3.033 0.54 246254. 0.3174
|
|
56.30 0.4404 0.7227 0.0506 0.0308 1.372 9.610 6.606 1023.296 1.086 29.383 2.928 0.54 246726. 0.2944
|
|
59.43 0.4648 0.7354 0.0462 0.0292 1.302 9.116 6.041 970.680 1.030 26.869 2.823 0.54 247217. 0.2714
|
|
62.55 0.4893 0.7447 0.0418 0.0275 1.224 8.571 5.464 912.655 0.968 24.304 2.715 0.54 247728. 0.2483
|
|
65.68 0.5138 0.7501 0.0373 0.0256 1.139 7.975 4.877 849.183 0.901 21.693 2.605 0.54 248259. 0.2250
|
|
68.81 0.5382 0.7507 0.0328 0.0235 1.046 7.328 4.281 780.248 0.828 19.041 2.488 0.54 248809. 0.2014
|
|
71.94 0.5627 0.7451 0.0281 0.0212 0.947 6.629 3.677 705.860 0.749 16.353 2.362 0.54 249380. 0.1772
|
|
75.07 0.5872 0.7309 0.0235 0.0188 0.840 5.880 3.066 626.072 0.664 13.637 2.221 0.54 249970. 0.1521
|
|
78.19 0.6116 0.7042 0.0188 0.0163 0.725 5.081 2.450 540.985 0.574 10.899 2.054 0.55 250580. 0.1258
|
|
81.32 0.6361 0.6571 0.0140 0.0136 0.604 4.233 1.832 450.762 0.478 8.147 1.843 0.55 251210. 0.0976
|
|
84.45 0.6606 0.5723 0.0093 0.0107 0.477 3.340 1.212 355.631 0.377 5.391 1.546 0.55 251860. 0.0666
|
|
87.58 0.6850 0.4039 0.0045 0.0077 0.343 2.403 0.593 255.840 0.271 2.640 1.052 0.55 252526. 0.0317
|
|
90.70 0.7095 -0.0614 -0.0004 0.0044 0.197 1.377 -0.050 146.644 0.156 -0.222 -0.154 0.55 253059. 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 0.1047 0.0358 2.189 13.800 16.894 1632.708 1.559 75.145 4.693 0.59 267808. 0.7546
|
|
3.48 0.0245 0.0694 0.1032 0.0364 2.223 14.011 16.642 1657.693 1.583 74.022 4.553 0.60 268000. 0.7266
|
|
6.96 0.0490 0.1347 0.1014 0.0369 2.254 14.207 16.366 1680.891 1.605 72.795 4.416 0.60 268209. 0.6989
|
|
10.44 0.0735 0.1959 0.0996 0.0373 2.282 14.384 16.066 1701.803 1.625 71.462 4.282 0.60 268434. 0.6714
|
|
13.91 0.0980 0.2532 0.0976 0.0377 2.306 14.537 15.741 1719.930 1.642 70.015 4.151 0.60 268677. 0.6442
|
|
17.39 0.1224 0.3068 0.0954 0.0381 2.326 14.663 15.389 1734.757 1.657 68.450 4.024 0.60 268938. 0.6174
|
|
20.87 0.1469 0.3568 0.0930 0.0383 2.341 14.756 15.009 1745.758 1.667 66.761 3.900 0.60 269218. 0.5910
|
|
24.35 0.1714 0.4034 0.0905 0.0385 2.350 14.812 14.601 1752.387 1.673 64.946 3.779 0.60 269517. 0.5649
|
|
27.83 0.1959 0.4468 0.0878 0.0385 2.352 14.826 14.163 1754.109 1.675 62.999 3.662 0.60 269835. 0.5392
|
|
31.31 0.2204 0.4871 0.0849 0.0384 2.347 14.795 13.696 1750.391 1.671 60.919 3.549 0.60 270173. 0.5138
|
|
34.79 0.2449 0.5244 0.0818 0.0382 2.334 14.713 13.198 1740.714 1.662 58.703 3.439 0.60 270531. 0.4887
|
|
38.26 0.2694 0.5589 0.0785 0.0378 2.313 14.577 12.669 1724.597 1.647 56.352 3.332 0.60 270909. 0.4639
|
|
41.74 0.2939 0.5908 0.0751 0.0373 2.282 14.383 12.111 1701.676 1.625 53.871 3.228 0.60 271308. 0.4395
|
|
45.22 0.3184 0.6200 0.0714 0.0367 2.242 14.130 11.526 1671.748 1.596 51.267 3.127 0.60 271728. 0.4153
|
|
48.70 0.3429 0.6466 0.0677 0.0359 2.192 13.817 10.916 1634.706 1.561 48.552 3.029 0.60 272168. 0.3914
|
|
52.18 0.3673 0.6708 0.0637 0.0349 2.133 13.443 10.282 1590.473 1.519 45.735 2.932 0.60 272630. 0.3678
|
|
55.66 0.3918 0.6924 0.0597 0.0338 2.064 13.008 9.628 1538.977 1.470 42.824 2.838 0.60 273113. 0.3444
|
|
59.14 0.4163 0.7114 0.0555 0.0325 1.985 12.511 8.954 1480.145 1.413 39.829 2.744 0.60 273617. 0.3212
|
|
62.62 0.4408 0.7277 0.0512 0.0310 1.896 11.951 8.263 1413.895 1.350 36.755 2.651 0.60 274143. 0.2981
|
|
66.09 0.4653 0.7410 0.0468 0.0294 1.797 11.327 7.556 1340.156 1.280 33.610 2.557 0.60 274691. 0.2750
|
|
69.57 0.4898 0.7511 0.0424 0.0276 1.688 10.640 6.835 1258.859 1.202 30.400 2.463 0.60 275260. 0.2518
|
|
73.05 0.5143 0.7573 0.0378 0.0257 1.569 9.889 6.100 1169.953 1.117 27.132 2.365 0.60 275852. 0.2285
|
|
76.53 0.5388 0.7589 0.0332 0.0236 1.439 9.073 5.354 1073.416 1.025 23.812 2.262 0.60 276465. 0.2047
|
|
80.01 0.5633 0.7545 0.0285 0.0213 1.300 8.192 4.597 969.265 0.926 20.448 2.151 0.60 277100. 0.1804
|
|
83.49 0.5877 0.7418 0.0238 0.0188 1.150 7.248 3.832 857.573 0.819 17.046 2.027 0.61 277758. 0.1552
|
|
86.97 0.6122 0.7168 0.0190 0.0162 0.990 6.242 3.061 738.479 0.705 13.616 1.880 0.61 278438. 0.1287
|
|
90.44 0.6367 0.6715 0.0142 0.0134 0.821 5.175 2.286 612.215 0.585 10.168 1.694 0.61 279139. 0.1002
|
|
93.92 0.6612 0.5884 0.0094 0.0105 0.642 4.050 1.509 479.104 0.458 6.714 1.429 0.61 279863. 0.0687
|
|
97.40 0.6857 0.4188 0.0046 0.0075 0.455 2.869 0.734 339.490 0.324 3.266 0.981 0.61 280605. 0.0329
|
|
100.88 0.7102
|
|
|
|
|
|
|
|
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 0.1060 0.0363 2.953 16.919 20.685 2201.864 1.911 92.009 4.261 0.65 294556. 0.7581
|
|
3.82 0.0245 0.0693 0.1044 0.0369 2.998 17.180 20.384 2235.890 1.941 90.667 4.135 0.65 294768. 0.7303
|
|
7.64 0.0489 0.1344 0.1027 0.0374 3.041 17.423 20.054 2267.520 1.968 89.199 4.011 0.65 294998. 0.7027
|
|
11.46 0.0734 0.1955 0.1009 0.0379 3.079 17.643 19.694 2296.064 1.993 87.597 3.890 0.65 295246. 0.6753
|
|
15.28 0.0978 0.2527 0.0989 0.0383 3.112 17.833 19.302 2320.841 2.015 85.855 3.772 0.65 295514. 0.6483
|
|
19.10 0.1223 0.3063 0.0967 0.0386 3.140 17.989 18.877 2341.141 2.032 83.966 3.657 0.65 295802. 0.6216
|
|
22.92 0.1467 0.3563 0.0944 0.0388 3.160 18.105 18.418 2356.226 2.045 81.925 3.546 0.66 296111. 0.5952
|
|
26.75 0.1712 0.4030 0.0918 0.0390 3.172 18.175 17.924 2365.355 2.053 79.726 3.437 0.66 296440. 0.5692
|
|
30.57 0.1956 0.4465 0.0891 0.0390 3.175 18.194 17.393 2367.798 2.056 77.364 3.332 0.66 296791. 0.5435
|
|
34.39 0.2201 0.4869 0.0862 0.0390 3.169 18.156 16.825 2362.840 2.051 74.836 3.230 0.66 297163. 0.5182
|
|
38.21 0.2445 0.5244 0.0831 0.0387 3.151 18.055 16.219 2349.785 2.040 72.141 3.131 0.66 297558. 0.4932
|
|
42.03 0.2690 0.5591 0.0798 0.0384 3.122 17.888 15.575 2327.990 2.021 69.279 3.035 0.66 297974. 0.4685
|
|
45.85 0.2934 0.5912 0.0763 0.0379 3.080 17.650 14.895 2296.959 1.994 66.254 2.941 0.66 298414. 0.4441
|
|
49.67 0.3179 0.6207 0.0726 0.0372 3.026 17.338 14.181 2256.419 1.959 63.077 2.851 0.66 298876. 0.4199
|
|
53.49 0.3423 0.6477 0.0688 0.0364 2.959 16.952 13.436 2206.224 1.915 59.762 2.762 0.66 299361. 0.3961
|
|
57.31 0.3668 0.6723 0.0649 0.0354 2.878 16.492 12.662 2146.279 1.863 56.319 2.676 0.66 299869. 0.3725
|
|
61.13 0.3912 0.6944 0.0608 0.0342 2.785 15.955 11.862 2076.493 1.803 52.761 2.591 0.66 300400. 0.3491
|
|
64.95 0.4157 0.7139 0.0565 0.0329 2.678 15.343 11.038 1996.776 1.733 49.096 2.507 0.66 300955. 0.3258
|
|
68.77 0.4402 0.7309 0.0522 0.0314 2.557 14.653 10.192 1907.030 1.656 45.335 2.424 0.66 301533. 0.3027
|
|
72.59 0.4646 0.7450 0.0478 0.0298 2.423 13.886 9.327 1807.161 1.569 41.484 2.341 0.66 302135. 0.2796
|
|
76.42 0.4891 0.7559 0.0432 0.0280 2.276 13.040 8.443 1697.083 1.473 37.553 2.256 0.66 302761. 0.2565
|
|
80.24 0.5135 0.7632 0.0386 0.0260 2.114 12.115 7.543 1576.732 1.369 33.549 2.170 0.66 303411. 0.2331
|
|
84.06 0.5380 0.7661 0.0340 0.0238 1.939 11.111 6.628 1446.076 1.255 29.481 2.079 0.66 304085. 0.2094
|
|
87.88 0.5624 0.7632 0.0292 0.0215 1.750 10.028 5.700 1305.132 1.133 25.355 1.981 0.66 304783. 0.1850
|
|
91.70 0.5869 0.7525 0.0244 0.0190 1.548 8.867 4.762 1153.991 1.002 21.182 1.872 0.67 305505. 0.1598
|
|
95.52 0.6113 0.7300 0.0195 0.0164 1.331 7.629 3.816 992.842 0.862 16.973 1.743 0.67 306251. 0.1332
|
|
99.34 0.6358 0.6883 0.0147 0.0136 1.102 6.316 2.864 821.988 0.714 12.741 1.581 0.67 307022. 0.1046
|
|
103.16 0.6602 0.6106 0.0098 0.0106 0.861 4.932 1.911 641.861 0.557 8.499 1.350 0.67 307815. 0.0730
|
|
106.98 0.6847 0.4500 0.0049 0.0075 0.607 3.480 0.958 452.937 0.393 4.262 0.960 0.67 308630. 0.0367
|
|
110.80 0.7091 -0.0154 -0.0001 0.0041 0.335 1.919 -0.017 249.701 0.217 -0.078 -0.032 0.67 309359. 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 0.1074 0.0372 3.928 20.629 24.948 2928.738 2.331 110.969 3.864 0.71 321292. 0.7549
|
|
4.17 0.0245 0.0687 0.1059 0.0377 3.985 20.931 24.595 2971.694 2.365 109.399 3.754 0.71 321524. 0.7283
|
|
8.35 0.0490 0.1334 0.1042 0.0382 4.039 21.212 24.207 3011.519 2.396 107.672 3.646 0.71 321776. 0.7017
|
|
12.52 0.0734 0.1943 0.1024 0.0387 4.087 21.464 23.782 3047.341 2.425 105.782 3.540 0.71 322049. 0.6753
|
|
16.69 0.0979 0.2514 0.1004 0.0391 4.128 21.682 23.318 3078.289 2.450 103.718 3.436 0.71 322343. 0.6490
|
|
20.87 0.1224 0.3050 0.0982 0.0394 4.162 21.859 22.813 3103.443 2.470 101.474 3.334 0.71 322659. 0.6230
|
|
25.04 0.1469 0.3551 0.0958 0.0396 4.186 21.989 22.266 3121.844 2.484 99.041 3.235 0.71 322997. 0.5971
|
|
29.21 0.1714 0.4019 0.0933 0.0398 4.201 22.064 21.676 3132.508 2.493 96.413 3.138 0.72 323359. 0.5716
|
|
33.39 0.1959 0.4456 0.0906 0.0398 4.203 22.078 21.040 3134.453 2.494 93.584 3.045 0.72 323744. 0.5463
|
|
37.56 0.2203 0.4863 0.0876 0.0397 4.193 22.023 20.358 3126.707 2.488 90.551 2.953 0.72 324154. 0.5212
|
|
41.73 0.2448 0.5240 0.0845 0.0395 4.168 21.894 19.629 3108.327 2.474 87.311 2.864 0.72 324587. 0.4964
|
|
45.91 0.2693 0.5591 0.0812 0.0391 4.128 21.683 18.854 3078.439 2.450 83.864 2.778 0.72 325044. 0.4718
|
|
50.08 0.2938 0.5914 0.0776 0.0386 4.072 21.387 18.034 3036.355 2.416 80.217 2.694 0.72 325527. 0.4475
|
|
54.25 0.3183 0.6213 0.0739 0.0379 3.998 21.002 17.172 2981.677 2.373 76.383 2.612 0.72 326034. 0.4235
|
|
58.43 0.3428 0.6487 0.0700 0.0370 3.908 20.526 16.272 2914.194 2.319 72.378 2.533 0.72 326566. 0.3996
|
|
62.60 0.3672 0.6737 0.0660 0.0360 3.800 19.960 15.336 2833.755 2.255 68.216 2.455 0.72 327124. 0.3760
|
|
66.77 0.3917 0.6962 0.0618 0.0348 3.675 19.301 14.369 2740.226 2.181 63.911 2.378 0.72 327706. 0.3527
|
|
70.95 0.4162 0.7163 0.0576 0.0334 3.532 18.549 13.371 2633.489 2.096 59.476 2.303 0.72 328315. 0.3294
|
|
75.12 0.4407 0.7338 0.0531 0.0319 3.371 17.703 12.347 2513.427 2.000 54.921 2.228 0.72 328949. 0.3063
|
|
79.29 0.4652 0.7485 0.0486 0.0302 3.192 16.763 11.299 2379.919 1.894 50.256 2.153 0.72 329608. 0.2831
|
|
83.47 0.4897 0.7602 0.0440 0.0284 2.994 15.727 10.227 2232.864 1.777 45.492 2.078 0.72 330294. 0.2599
|
|
87.64 0.5141 0.7683 0.0393 0.0263 2.779 14.595 9.136 2072.176 1.649 40.637 2.000 0.72 331006. 0.2364
|
|
91.81 0.5386 0.7721 0.0345 0.0241 2.545 13.367 8.027 1897.818 1.510 35.702 1.918 0.72 331744. 0.2126
|
|
95.98 0.5631 0.7704 0.0297 0.0217 2.293 12.043 6.901 1709.816 1.361 30.697 1.831 0.73 332508. 0.1881
|
|
100.16 0.5876 0.7609 0.0248 0.0192 2.023 10.624 5.763 1508.283 1.200 25.633 1.733 0.73 333298. 0.1627
|
|
104.33 0.6121 0.7400 0.0199 0.0164 1.735 9.111 4.614 1293.467 1.029 20.523 1.618 0.73 334115. 0.1360
|
|
108.50 0.6366 0.7001 0.0149 0.0135 1.429 7.507 3.458 1065.781 0.848 15.383 1.472 0.73 334958. 0.1071
|
|
112.68 0.6610 0.6240 0.0099 0.0105 1.108 5.817 2.300 825.874 0.657 10.230 1.263 0.73 335826. 0.0749
|
|
116.85 0.6855 0.4620 0.0049 0.0073 0.770 4.047 1.142 574.542 0.457 5.082 0.902 0.73 336717. 0.0377
|
|
121.02 0.7100 -0.0572 -0.0003 0.0038 0.399 2.098 -0.071 297.865 0.237 -0.315 -0.108 0.73 337392. 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 0.1090 0.0392 5.268 25.541 29.714 3928.357 2.886 132.167 3.431 0.77 348014. 0.7315
|
|
4.52 0.0245 0.0663 0.1075 0.0397 5.332 25.849 29.311 3975.729 2.920 130.374 3.344 0.77 348265. 0.7082
|
|
9.05 0.0490 0.1292 0.1059 0.0401 5.389 26.128 28.865 4018.614 2.952 128.390 3.258 0.77 348539. 0.6847
|
|
13.57 0.0735 0.1888 0.1041 0.0405 5.439 26.371 28.374 4055.995 2.979 126.206 3.173 0.77 348836. 0.6611
|
|
18.10 0.0980 0.2451 0.1021 0.0408 5.481 26.572 27.835 4086.878 3.002 123.810 3.089 0.77 349156. 0.6375
|
|
22.62 0.1225 0.2982 0.0999 0.0411 5.512 26.724 27.247 4110.240 3.019 121.193 3.007 0.77 349501. 0.6139
|
|
27.15 0.1470 0.3482 0.0976 0.0412 5.532 26.820 26.607 4124.989 3.030 118.346 2.926 0.77 349870. 0.5903
|
|
31.67 0.1715 0.3951 0.0950 0.0413 5.538 26.852 25.913 4129.971 3.034 115.260 2.846 0.77 350264. 0.5667
|
|
36.20 0.1960 0.4392 0.0923 0.0412 5.530 26.813 25.164 4124.008 3.029 111.928 2.768 0.78 350684. 0.5431
|
|
40.72 0.2205 0.4803 0.0893 0.0410 5.506 26.696 24.358 4105.920 3.016 108.345 2.691 0.78 351131. 0.5195
|
|
45.24 0.2450 0.5188 0.0862 0.0407 5.464 26.492 23.496 4074.557 2.993 104.508 2.615 0.78 351603. 0.4959
|
|
49.77 0.2695 0.5545 0.0828 0.0402 5.403 26.194 22.576 4028.844 2.959 100.419 2.542 0.78 352102. 0.4724
|
|
54.29 0.2940 0.5877 0.0792 0.0396 5.321 25.798 21.601 3967.923 2.915 96.083 2.469 0.78 352628. 0.4489
|
|
58.82 0.3185 0.6184 0.0755 0.0389 5.218 25.300 20.575 3891.288 2.858 91.518 2.398 0.78 353181. 0.4255
|
|
63.34 0.3430 0.6466 0.0715 0.0379 5.094 24.698 19.502 3798.673 2.790 86.743 2.329 0.78 353761. 0.4022
|
|
67.87 0.3675 0.6724 0.0674 0.0369 4.948 23.990 18.385 3689.856 2.710 81.776 2.260 0.78 354369. 0.3791
|
|
72.39 0.3920 0.6957 0.0632 0.0356 4.780 23.176 17.229 3564.597 2.618 76.634 2.192 0.78 355003. 0.3560
|
|
76.92 0.4165 0.7166 0.0588 0.0342 4.590 22.253 16.037 3422.627 2.514 71.332 2.125 0.78 355665. 0.3329
|
|
81.44 0.4410 0.7349 0.0543 0.0326 4.377 21.220 14.812 3263.684 2.397 65.883 2.058 0.78 356355. 0.3099
|
|
85.96 0.4655 0.7505 0.0497 0.0308 4.140 20.074 13.556 3087.543 2.268 60.299 1.991 0.78 357073. 0.2868
|
|
90.49 0.4900 0.7631 0.0450 0.0289 3.881 18.816 12.274 2894.007 2.126 54.593 1.924 0.78 357819. 0.2636
|
|
95.01 0.5145 0.7722 0.0402 0.0268 3.598 17.444 10.966 2682.910 1.971 48.776 1.854 0.78 358593. 0.2401
|
|
99.54 0.5390 0.7771 0.0353 0.0245 3.291 15.957 9.636 2454.209 1.803 42.859 1.781 0.78 359395. 0.2162
|
|
104.06 0.5635 0.7765 0.0304 0.0221 2.961 14.356 8.286 2208.045 1.622 36.856 1.702 0.79 360225. 0.1917
|
|
108.59 0.5880 0.7682 0.0254 0.0194 2.608 12.645 6.920 1944.812 1.429 30.779 1.614 0.79 361084. 0.1661
|
|
113.11 0.6125 0.7483 0.0203 0.0166 2.233 10.827 5.540 1665.229 1.223 24.643 1.509 0.79 361971. 0.1389
|
|
117.64 0.6370 0.7086 0.0152 0.0137 1.838 8.910 4.152 1370.425 1.007 18.467 1.374 0.79 362887. 0.1095
|
|
122.16 0.6615 0.6310 0.0101 0.0106 1.424 6.904 2.759 1061.868 0.780 12.270 1.178 0.79 363829. 0.0766
|
|
126.68 0.6860 0.4640 0.0050 0.0074 0.994 4.819 1.365 741.242 0.544 6.073 0.835 0.79 364796. 0.0382
|
|
131.21 0.7105
|
|
|
|
|
|
|
|
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 0.1107 0.0436 7.305 32.889 34.996 5447.663 3.716 155.664 2.914 0.83 374716. 0.6743
|
|
4.88 0.0245 0.0611 0.1093 0.0439 7.363 33.146 34.548 5490.232 3.745 153.670 2.854 0.83 374988. 0.6562
|
|
9.76 0.0491 0.1196 0.1077 0.0442 7.409 33.357 34.048 5525.149 3.769 151.446 2.795 0.83 375284. 0.6380
|
|
14.65 0.0736 0.1757 0.1059 0.0444 7.444 33.515 33.494 5551.257 3.786 148.979 2.737 0.83 375605. 0.6195
|
|
19.53 0.0982 0.2293 0.1040 0.0445 7.466 33.613 32.881 5567.507 3.798 146.254 2.679 0.83 375952. 0.6009
|
|
24.41 0.1227 0.2805 0.1019 0.0446 7.473 33.645 32.207 5572.878 3.801 143.258 2.621 0.83 376326. 0.5819
|
|
29.29 0.1473 0.3293 0.0995 0.0445 7.465 33.606 31.470 5566.372 3.797 139.980 2.564 0.83 376727. 0.5627
|
|
34.17 0.1718 0.3757 0.0970 0.0444 7.439 33.489 30.668 5546.938 3.784 136.410 2.508 0.83 377155. 0.5432
|
|
39.05 0.1964 0.4197 0.0942 0.0441 7.394 33.287 29.798 5513.580 3.761 132.541 2.451 0.83 377612. 0.5234
|
|
43.94 0.2209 0.4613 0.0913 0.0437 7.329 32.995 28.859 5465.156 3.728 128.366 2.395 0.84 378097. 0.5033
|
|
48.82 0.2455 0.5006 0.0881 0.0432 7.242 32.604 27.851 5400.465 3.684 123.881 2.339 0.84 378611. 0.4829
|
|
53.70 0.2700 0.5375 0.0847 0.0425 7.132 32.108 26.773 5318.300 3.628 119.087 2.283 0.84 379154. 0.4622
|
|
58.58 0.2946 0.5721 0.0810 0.0417 6.997 31.501 25.627 5217.700 3.559 113.990 2.228 0.84 379725. 0.4412
|
|
63.46 0.3191 0.6044 0.0772 0.0408 6.837 30.780 24.418 5098.229 3.477 108.611 2.172 0.84 380326. 0.4199
|
|
68.35 0.3437 0.6343 0.0732 0.0397 6.651 29.944 23.151 4959.752 3.383 102.973 2.117 0.84 380956. 0.3985
|
|
73.23 0.3682 0.6619 0.0690 0.0384 6.440 28.992 21.830 4802.190 3.276 97.101 2.062 0.84 381616. 0.3768
|
|
78.11 0.3928 0.6871 0.0647 0.0370 6.203 27.925 20.462 4625.359 3.155 91.014 2.007 0.84 382305. 0.3550
|
|
82.99 0.4173 0.7098 0.0602 0.0354 5.939 26.739 19.049 4428.955 3.021 84.732 1.951 0.84 383024. 0.3331
|
|
87.87 0.4419 0.7299 0.0556 0.0337 5.649 25.433 17.597 4212.581 2.873 78.271 1.895 0.84 383772. 0.3109
|
|
92.75 0.4664 0.7472 0.0509 0.0318 5.332 24.003 16.107 3975.730 2.712 71.645 1.838 0.84 384551. 0.2885
|
|
97.64 0.4910 0.7615 0.0461 0.0297 4.986 22.446 14.584 3717.930 2.536 64.868 1.779 0.84 385359. 0.2658
|
|
102.52 0.5155 0.7723 0.0412 0.0275 4.612 20.762 13.029 3439.013 2.346 57.953 1.718 0.84 386198. 0.2426
|
|
107.40 0.5401 0.7783 0.0362 0.0251 4.212 18.963 11.447 3140.936 2.142 50.914 1.653 0.85 387067. 0.2188
|
|
112.28 0.5646 0.7770 0.0311 0.0226 3.791 17.069 9.839 2827.273 1.928 43.763 1.578 0.85 387966. 0.1937
|
|
117.16 0.5892 0.7663 0.0260 0.0200 3.347 15.069 8.210 2495.915 1.702 36.518 1.492 0.85 388896. 0.1672
|
|
122.05 0.6137 0.7414 0.0208 0.0172 2.881 12.972 6.564 2148.590 1.466 29.196 1.386 0.85 389856. 0.1389
|
|
126.93 0.6383 0.6927 0.0155 0.0143 2.397 10.790 4.906 1787.214 1.219 21.820 1.245 0.85 390847. 0.1079
|
|
131.81 0.6628 0.6003 0.0102 0.0113 1.897 8.540 3.240 1414.542 0.965 14.411 1.039 0.85 391866. 0.0732
|
|
136.69 0.6874 0.4136 0.0050 0.0083 1.386 6.239 1.573 1033.363 0.705 6.995 0.690 0.85 392912. 0.0339
|
|
141.57 0.7119
|
|
|
|
|
|
|
|
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 0.1115 0.0497 10.255 43.090 40.482 7647.145 4.868 180.066 2.401 0.89 401445. 0.5976
|
|
5.26 0.0247 0.0544 0.1102 0.0500 10.314 43.338 40.013 7691.023 4.896 177.976 2.360 0.89 401733. 0.5839
|
|
10.53 0.0494 0.1070 0.1088 0.0502 10.356 43.516 39.483 7722.607 4.916 175.621 2.319 0.89 402048. 0.5700
|
|
15.79 0.0741 0.1578 0.1071 0.0503 10.379 43.612 38.889 7739.722 4.927 172.980 2.279 0.89 402391. 0.5560
|
|
21.05 0.0988 0.2067 0.1053 0.0503 10.380 43.616 38.226 7740.415 4.928 170.030 2.240 0.89 402763. 0.5417
|
|
26.32 0.1235 0.2540 0.1033 0.0502 10.357 43.518 37.489 7723.021 4.917 166.750 2.202 0.89 403165. 0.5273
|
|
31.58 0.1482 0.2996 0.1010 0.0500 10.307 43.310 36.674 7686.197 4.893 163.124 2.164 0.89 403597. 0.5127
|
|
36.84 0.1729 0.3436 0.0986 0.0496 10.230 42.987 35.777 7628.869 4.857 159.136 2.127 0.89 404060. 0.4977
|
|
42.11 0.1976 0.3859 0.0959 0.0491 10.125 42.544 34.797 7550.173 4.807 154.775 2.090 0.89 404554. 0.4824
|
|
47.37 0.2223 0.4265 0.0929 0.0484 9.990 41.976 33.730 7449.342 4.742 150.033 2.054 0.89 405080. 0.4666
|
|
52.63 0.2470 0.4654 0.0897 0.0476 9.824 41.278 32.578 7325.584 4.664 144.905 2.017 0.90 405637. 0.4504
|
|
57.90 0.2717 0.5026 0.0863 0.0467 9.626 40.448 31.338 7178.136 4.570 139.390 1.980 0.90 406227. 0.4336
|
|
63.16 0.2964 0.5380 0.0827 0.0456 9.396 39.481 30.013 7006.557 4.461 133.498 1.943 0.90 406848. 0.4164
|
|
68.42 0.3211 0.5715 0.0788 0.0443 9.134 38.379 28.609 6811.041 4.336 127.253 1.905 0.90 407501. 0.3986
|
|
73.69 0.3458 0.6031 0.0747 0.0429 8.840 37.146 27.132 6592.152 4.197 120.685 1.867 0.90 408186. 0.3804
|
|
78.95 0.3705 0.6326 0.0705 0.0413 8.516 35.783 25.590 6350.309 4.043 113.823 1.828 0.90 408904. 0.3617
|
|
84.21 0.3952 0.6600 0.0661 0.0396 8.161 34.291 23.986 6085.549 3.874 106.691 1.788 0.90 409653. 0.3425
|
|
89.48 0.4199 0.6852 0.0615 0.0377 7.775 32.669 22.327 5797.733 3.691 99.311 1.747 0.90 410435. 0.3229
|
|
94.74 0.4446 0.7079 0.0568 0.0357 7.358 30.916 20.617 5486.655 3.493 91.706 1.704 0.90 411249. 0.3027
|
|
100.00 0.4693 0.7279 0.0520 0.0335 6.909 29.032 18.861 5152.192 3.280 83.894 1.660 0.90 412095. 0.2821
|
|
105.27 0.4940 0.7450 0.0470 0.0312 6.429 27.014 17.063 4794.125 3.052 75.894 1.614 0.90 412974. 0.2608
|
|
110.53 0.5188 0.7580 0.0419 0.0287 5.920 24.876 15.226 4414.611 2.810 67.724 1.564 0.90 413886. 0.2388
|
|
115.79 0.5435 0.7639 0.0368 0.0262 5.397 22.679 13.352 4024.798 2.562 59.392 1.505 0.91 414830. 0.2151
|
|
121.06 0.5682 0.7576 0.0315 0.0236 4.876 20.490 11.444 3636.318 2.315 50.905 1.428 0.91 415807. 0.1889
|
|
126.32 0.5929 0.7363 0.0262 0.0211 4.350 18.277 9.508 3243.587 2.065 42.290 1.330 0.91 416816. 0.1604
|
|
131.58 0.6176 0.6951 0.0208 0.0185 3.811 16.012 7.549 2841.554 1.809 33.577 1.205 0.91 417858. 0.1295
|
|
136.85 0.6423 0.6233 0.0154 0.0158 3.263 13.713 5.575 2433.556 1.549 24.795 1.039 0.91 418933. 0.0960
|
|
142.11 0.6670 0.5015 0.0099 0.0132 2.714 11.406 3.592 2024.193 1.289 15.979 0.805 0.91 420039. 0.0597
|
|
147.37 0.6917 0.2918 0.0044 0.0105 2.167 9.107 1.609 1616.182 1.029 7.157 0.452 0.91 421172. 0.0224
|
|
152.64 0.7164
|
|
|
|
|
|
|