649 lines
115 KiB
Plaintext
649 lines
115 KiB
Plaintext
13.5x9 (135x9.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 0.0954 0.0471 0.002 0.107 0.101 1.268 0.012 0.449 36.124 0.05 18462. 0.4990
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0.36 0.0285 0.0562 0.0944 0.0478 0.002 0.109 0.100 1.287 0.012 0.445 35.216 0.05 18475. 0.4839
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0.73 0.0570 0.1095 0.0933 0.0485 0.002 0.110 0.099 1.306 0.012 0.439 34.297 0.05 18490. 0.4684
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1.09 0.0855 0.1598 0.0920 0.0492 0.002 0.112 0.097 1.324 0.013 0.433 33.372 0.05 18507. 0.4527
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1.46 0.1139 0.2072 0.0906 0.0498 0.002 0.113 0.096 1.341 0.013 0.427 32.445 0.05 18526. 0.4368
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1.82 0.1424 0.2516 0.0891 0.0504 0.002 0.115 0.094 1.357 0.013 0.419 31.518 0.05 18546. 0.4207
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2.18 0.1709 0.2931 0.0874 0.0510 0.002 0.116 0.092 1.371 0.013 0.411 30.595 0.05 18568. 0.4044
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2.55 0.1994 0.3316 0.0855 0.0514 0.002 0.117 0.090 1.383 0.013 0.402 29.677 0.05 18592. 0.3880
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2.91 0.2279 0.3674 0.0834 0.0517 0.002 0.118 0.088 1.392 0.013 0.393 28.767 0.05 18618. 0.3715
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3.28 0.2564 0.4003 0.0811 0.0519 0.002 0.118 0.086 1.397 0.013 0.382 27.864 0.05 18646. 0.3548
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3.64 0.2848 0.4305 0.0786 0.0520 0.002 0.118 0.083 1.399 0.013 0.370 26.968 0.05 18676. 0.3381
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4.01 0.3133 0.4580 0.0759 0.0519 0.002 0.118 0.080 1.397 0.013 0.357 26.079 0.05 18709. 0.3212
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4.37 0.3418 0.4826 0.0729 0.0517 0.002 0.117 0.077 1.390 0.013 0.343 25.194 0.05 18743. 0.3043
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4.73 0.3703 0.5045 0.0697 0.0512 0.002 0.116 0.074 1.377 0.013 0.328 24.311 0.05 18780. 0.2871
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5.10 0.3988 0.5236 0.0663 0.0505 0.002 0.115 0.070 1.359 0.013 0.312 23.427 0.05 18818. 0.2698
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5.46 0.4273 0.5397 0.0627 0.0496 0.002 0.113 0.066 1.336 0.013 0.295 22.538 0.05 18859. 0.2524
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5.83 0.4558 0.5527 0.0589 0.0486 0.002 0.110 0.062 1.307 0.012 0.277 21.637 0.05 18902. 0.2348
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6.19 0.4842 0.5623 0.0549 0.0473 0.002 0.108 0.058 1.273 0.012 0.259 20.718 0.05 18947. 0.2171
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6.55 0.5127 0.5682 0.0508 0.0458 0.002 0.104 0.054 1.233 0.012 0.239 19.774 0.05 18994. 0.1993
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6.92 0.5412 0.5700 0.0466 0.0442 0.002 0.101 0.049 1.189 0.011 0.219 18.793 0.05 19044. 0.1813
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7.28 0.5697 0.5672 0.0422 0.0424 0.002 0.096 0.045 1.140 0.011 0.199 17.765 0.05 19095. 0.1632
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7.65 0.5982 0.5590 0.0377 0.0404 0.001 0.092 0.040 1.087 0.010 0.178 16.674 0.05 19149. 0.1448
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8.01 0.6267 0.5444 0.0332 0.0382 0.001 0.087 0.035 1.028 0.010 0.156 15.500 0.05 19205. 0.1263
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8.38 0.6551 0.5219 0.0286 0.0359 0.001 0.082 0.030 0.966 0.009 0.135 14.215 0.05 19263. 0.1075
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8.74 0.6836 0.4897 0.0239 0.0334 0.001 0.076 0.025 0.899 0.009 0.113 12.782 0.05 19323. 0.0884
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9.10 0.7121 0.4449 0.0192 0.0307 0.001 0.070 0.020 0.827 0.008 0.090 11.148 0.05 19385. 0.0691
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9.47 0.7406 0.3834 0.0145 0.0279 0.001 0.064 0.015 0.752 0.007 0.068 9.237 0.06 19449. 0.0497
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9.83 0.7691 0.2986 0.0097 0.0250 0.001 0.057 0.010 0.672 0.006 0.046 6.927 0.06 19516. 0.0305
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10.20 0.7976 0.1801 0.0049 0.0219 0.001 0.050 0.005 0.590 0.006 0.023 4.029 0.06 19584. 0.0127
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10.56 0.8261 0.0096 0.0002 0.0187 0.001 0.043 0.000 0.503 0.005 0.001 0.208 0.06 19654. 0.0001
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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 0.0959 0.0411 0.012 0.374 0.406 8.852 0.042 1.806 20.802 0.11 36923. 0.5761
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0.74 0.0288 0.0651 0.0949 0.0419 0.012 0.381 0.402 9.017 0.043 1.787 20.208 0.11 36950. 0.5567
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1.47 0.0575 0.1264 0.0938 0.0427 0.012 0.388 0.397 9.182 0.044 1.766 19.613 0.11 36981. 0.5371
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2.21 0.0863 0.1839 0.0925 0.0434 0.013 0.395 0.392 9.343 0.045 1.743 19.018 0.11 37015. 0.5174
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2.94 0.1150 0.2376 0.0911 0.0441 0.013 0.401 0.386 9.497 0.045 1.716 18.428 0.11 37052. 0.4975
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3.68 0.1438 0.2876 0.0896 0.0448 0.013 0.407 0.379 9.641 0.046 1.687 17.845 0.11 37093. 0.4777
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4.41 0.1725 0.3340 0.0879 0.0454 0.013 0.413 0.372 9.771 0.047 1.655 17.269 0.11 37138. 0.4578
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5.15 0.2013 0.3769 0.0860 0.0459 0.013 0.418 0.364 9.882 0.047 1.619 16.704 0.11 37187. 0.4380
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5.88 0.2300 0.4164 0.0839 0.0463 0.013 0.421 0.355 9.972 0.048 1.579 16.150 0.11 37240. 0.4183
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6.62 0.2588 0.4527 0.0815 0.0466 0.013 0.424 0.345 10.035 0.048 1.536 15.607 0.11 37297. 0.3986
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7.35 0.2875 0.4859 0.0790 0.0468 0.013 0.425 0.335 10.067 0.048 1.488 15.075 0.11 37359. 0.3790
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8.09 0.3163 0.5160 0.0763 0.0467 0.013 0.425 0.323 10.063 0.048 1.436 14.555 0.11 37424. 0.3595
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8.82 0.3450 0.5432 0.0733 0.0465 0.013 0.423 0.310 10.020 0.048 1.380 14.044 0.11 37494. 0.3400
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9.56 0.3738 0.5674 0.0700 0.0461 0.013 0.420 0.297 9.933 0.047 1.319 13.543 0.11 37568. 0.3205
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10.29 0.4025 0.5888 0.0666 0.0455 0.013 0.414 0.282 9.799 0.047 1.254 13.048 0.11 37647. 0.3011
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11.03 0.4313 0.6072 0.0629 0.0447 0.013 0.406 0.266 9.619 0.046 1.185 12.559 0.11 37730. 0.2817
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11.76 0.4601 0.6225 0.0590 0.0436 0.013 0.397 0.250 9.392 0.045 1.112 12.072 0.11 37817. 0.2623
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12.50 0.4888 0.6347 0.0550 0.0424 0.012 0.385 0.233 9.119 0.044 1.036 11.584 0.11 37909. 0.2430
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13.23 0.5176 0.6433 0.0508 0.0409 0.012 0.372 0.215 8.802 0.042 0.957 11.090 0.11 38005. 0.2236
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13.97 0.5463 0.6482 0.0465 0.0392 0.011 0.357 0.197 8.442 0.040 0.876 10.585 0.11 38106. 0.2042
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14.70 0.5751 0.6486 0.0421 0.0374 0.011 0.340 0.178 8.040 0.038 0.793 10.062 0.11 38210. 0.1847
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15.44 0.6038 0.6439 0.0376 0.0353 0.010 0.321 0.159 7.596 0.036 0.709 9.513 0.11 38320. 0.1650
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16.17 0.6326 0.6329 0.0331 0.0330 0.010 0.301 0.140 7.111 0.034 0.622 8.926 0.11 38433. 0.1451
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16.91 0.6613 0.6141 0.0284 0.0306 0.009 0.278 0.120 6.586 0.031 0.535 8.284 0.11 38551. 0.1249
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17.64 0.6901 0.5851 0.0237 0.0280 0.008 0.254 0.100 6.022 0.029 0.447 7.564 0.11 38673. 0.1042
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18.38 0.7188 0.5421 0.0190 0.0252 0.007 0.229 0.080 5.419 0.026 0.358 6.728 0.11 38800. 0.0829
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19.11 0.7476 0.4790 0.0142 0.0222 0.006 0.202 0.060 4.780 0.023 0.268 5.717 0.11 38930. 0.0610
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19.85 0.7763 0.3853 0.0095 0.0191 0.006 0.174 0.040 4.106 0.020 0.178 4.428 0.11 39066. 0.0385
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20.58 0.8051 0.2407 0.0047 0.0158 0.005 0.144 0.020 3.400 0.016 0.089 2.667 0.11 39205. 0.0164
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21.32 0.8338 0.0008 0.0000 0.0124 0.004 0.113 0.000 2.666 0.013 0.000 0.009 0.11 39347. 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 0.0962 0.0387 0.038 0.791 0.916 28.091 0.089 4.075 14.793 0.16 55384. 0.6155
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1.11 0.0289 0.0696 0.0952 0.0395 0.038 0.808 0.907 28.671 0.091 4.034 14.346 0.16 55425. 0.5938
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2.21 0.0577 0.1349 0.0941 0.0403 0.039 0.824 0.896 29.250 0.093 3.987 13.899 0.16 55471. 0.5719
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3.32 0.0866 0.1958 0.0928 0.0410 0.040 0.840 0.884 29.817 0.095 3.934 13.455 0.16 55522. 0.5500
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4.43 0.1154 0.2526 0.0915 0.0418 0.041 0.855 0.871 30.363 0.097 3.876 13.016 0.16 55579. 0.5280
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5.53 0.1443 0.3052 0.0899 0.0425 0.041 0.870 0.857 30.875 0.098 3.810 12.583 0.16 55641. 0.5062
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6.64 0.1731 0.3539 0.0882 0.0431 0.042 0.883 0.840 31.340 0.100 3.737 12.160 0.16 55709. 0.4845
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7.75 0.2020 0.3989 0.0863 0.0437 0.043 0.894 0.822 31.744 0.101 3.657 11.746 0.16 55782. 0.4629
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8.85 0.2308 0.4402 0.0842 0.0441 0.043 0.904 0.802 32.073 0.102 3.567 11.342 0.16 55862. 0.4415
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9.96 0.2597 0.4780 0.0819 0.0445 0.043 0.910 0.780 32.311 0.103 3.469 10.949 0.16 55948. 0.4203
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11.07 0.2885 0.5126 0.0793 0.0447 0.044 0.914 0.756 32.444 0.103 3.362 10.566 0.16 56041. 0.3993
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12.17 0.3174 0.5440 0.0766 0.0447 0.044 0.914 0.729 32.455 0.103 3.245 10.194 0.16 56140. 0.3784
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13.28 0.3462 0.5723 0.0736 0.0445 0.043 0.911 0.701 32.329 0.103 3.117 9.832 0.16 56245. 0.3577
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14.39 0.3751 0.5978 0.0703 0.0441 0.043 0.903 0.670 32.053 0.102 2.979 9.478 0.16 56357. 0.3372
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15.49 0.4039 0.6203 0.0668 0.0435 0.042 0.891 0.637 31.617 0.101 2.832 9.133 0.16 56476. 0.3167
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16.60 0.4328 0.6399 0.0631 0.0427 0.042 0.874 0.601 31.018 0.099 2.675 8.793 0.16 56601. 0.2964
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17.71 0.4617 0.6566 0.0592 0.0416 0.041 0.852 0.564 30.257 0.096 2.510 8.459 0.16 56733. 0.2762
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18.81 0.4905 0.6702 0.0552 0.0404 0.039 0.827 0.526 29.338 0.093 2.338 8.126 0.16 56872. 0.2561
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19.92 0.5194 0.6805 0.0510 0.0389 0.038 0.796 0.486 28.264 0.090 2.160 7.793 0.16 57017. 0.2360
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21.03 0.5482 0.6872 0.0467 0.0372 0.036 0.762 0.444 27.038 0.086 1.977 7.456 0.16 57168. 0.2160
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22.13 0.5771 0.6898 0.0422 0.0353 0.034 0.723 0.402 25.663 0.082 1.789 7.109 0.16 57327. 0.1960
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23.24 0.6059 0.6875 0.0377 0.0332 0.032 0.680 0.359 24.141 0.077 1.598 6.749 0.16 57492. 0.1758
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24.34 0.6348 0.6794 0.0331 0.0309 0.030 0.633 0.315 22.474 0.072 1.403 6.365 0.16 57663. 0.1554
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25.45 0.6636 0.6637 0.0284 0.0284 0.028 0.582 0.271 20.664 0.066 1.205 5.948 0.16 57841. 0.1346
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26.56 0.6925 0.6380 0.0237 0.0258 0.025 0.527 0.226 18.716 0.060 1.006 5.480 0.16 58025. 0.1133
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27.66 0.7213 0.5983 0.0190 0.0229 0.022 0.469 0.181 16.632 0.053 0.805 4.933 0.16 58216. 0.0912
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28.77 0.7502 0.5376 0.0142 0.0198 0.019 0.406 0.135 14.418 0.046 0.603 4.262 0.17 58414. 0.0682
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29.88 0.7790 0.4429 0.0095 0.0166 0.016 0.340 0.090 12.083 0.038 0.401 3.381 0.17 58618. 0.0441
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30.98 0.8079 0.2867 0.0047 0.0133 0.013 0.271 0.045 9.635 0.031 0.199 2.111 0.17 58828. 0.0194
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32.09 0.8367 -0.0003 0.0000 0.0098 0.010 0.200 0.000 7.085 0.023 0.000 -0.002 0.17 59042. 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 0.0965 0.0373 0.086 1.358 1.634 64.273 0.153 7.266 11.528 0.21 73844. 0.6404
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1.48 0.0289 0.0724 0.0955 0.0381 0.088 1.388 1.617 65.681 0.157 7.193 11.167 0.21 73899. 0.6172
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2.96 0.0578 0.1400 0.0944 0.0390 0.090 1.418 1.599 67.088 0.160 7.110 10.808 0.21 73960. 0.5939
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4.43 0.0867 0.2031 0.0932 0.0398 0.092 1.447 1.578 68.472 0.163 7.018 10.451 0.21 74029. 0.5706
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5.91 0.1156 0.2618 0.0918 0.0405 0.094 1.475 1.554 69.805 0.167 6.914 10.100 0.21 74104. 0.5473
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7.39 0.1445 0.3160 0.0902 0.0413 0.095 1.502 1.528 71.059 0.170 6.798 9.756 0.21 74187. 0.5242
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8.87 0.1734 0.3662 0.0885 0.0419 0.097 1.526 1.499 72.202 0.172 6.669 9.419 0.21 74278. 0.5013
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10.35 0.2023 0.4123 0.0866 0.0425 0.098 1.547 1.467 73.201 0.175 6.526 9.091 0.21 74376. 0.4786
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11.82 0.2312 0.4547 0.0845 0.0430 0.099 1.564 1.432 74.021 0.177 6.368 8.772 0.21 74483. 0.4562
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13.30 0.2601 0.4935 0.0822 0.0433 0.100 1.577 1.392 74.625 0.178 6.193 8.463 0.21 74598. 0.4340
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14.78 0.2890 0.5289 0.0797 0.0435 0.101 1.584 1.349 74.977 0.179 6.002 8.163 0.22 74722. 0.4121
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16.26 0.3179 0.5610 0.0769 0.0436 0.101 1.586 1.302 75.037 0.179 5.793 7.872 0.22 74855. 0.3905
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17.74 0.3468 0.5901 0.0739 0.0434 0.100 1.580 1.251 74.769 0.178 5.565 7.590 0.22 74996. 0.3690
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19.21 0.3757 0.6163 0.0706 0.0431 0.099 1.567 1.196 74.140 0.177 5.320 7.317 0.22 75146. 0.3478
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20.69 0.4046 0.6395 0.0671 0.0425 0.098 1.545 1.137 73.125 0.175 5.056 7.051 0.22 75304. 0.3267
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22.17 0.4335 0.6600 0.0634 0.0416 0.096 1.515 1.074 71.717 0.171 4.776 6.791 0.22 75472. 0.3059
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23.65 0.4624 0.6776 0.0595 0.0406 0.094 1.477 1.008 69.919 0.167 4.482 6.536 0.22 75649. 0.2852
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25.12 0.4913 0.6922 0.0554 0.0393 0.091 1.431 0.939 67.736 0.162 4.174 6.284 0.22 75834. 0.2646
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26.60 0.5202 0.7037 0.0512 0.0378 0.087 1.377 0.867 65.178 0.156 3.857 6.034 0.22 76028. 0.2442
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28.08 0.5491 0.7117 0.0469 0.0361 0.083 1.315 0.793 62.251 0.149 3.529 5.781 0.22 76231. 0.2238
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29.56 0.5780 0.7159 0.0424 0.0342 0.079 1.246 0.718 58.962 0.141 3.194 5.524 0.22 76443. 0.2035
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31.04 0.6069 0.7155 0.0379 0.0321 0.074 1.169 0.641 55.314 0.132 2.852 5.258 0.22 76663. 0.1830
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32.51 0.6358 0.7095 0.0332 0.0298 0.069 1.084 0.563 51.313 0.123 2.505 4.977 0.22 76892. 0.1623
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33.99 0.6647 0.6964 0.0286 0.0273 0.063 0.992 0.484 46.965 0.112 2.152 4.673 0.22 77130. 0.1413
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35.47 0.6936 0.6736 0.0238 0.0245 0.057 0.893 0.404 42.277 0.101 1.796 4.332 0.22 77377. 0.1196
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36.95 0.7225 0.6371 0.0191 0.0216 0.050 0.787 0.323 37.259 0.089 1.437 3.933 0.22 77633. 0.0972
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38.43 0.7514 0.5795 0.0143 0.0185 0.043 0.675 0.242 31.925 0.076 1.077 3.440 0.22 77897. 0.0736
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39.90 0.7803 0.4863 0.0095 0.0153 0.035 0.556 0.161 26.294 0.063 0.717 2.780 0.22 78169. 0.0485
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41.38 0.8092 0.3250 0.0048 0.0118 0.027 0.431 0.081 20.390 0.049 0.358 1.792 0.22 78450. 0.0221
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42.86 0.8381 0.0036 0.0000 0.0083 0.019 0.301 0.001 14.235 0.034 0.003 0.019 0.22 78736. 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 0.0968 0.0365 0.165 2.075 2.561 122.775 0.234 11.390 9.460 0.27 92302. 0.6580
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1.85 0.0289 0.0742 0.0958 0.0373 0.168 2.123 2.535 125.577 0.240 11.277 9.157 0.27 92372. 0.6337
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3.70 0.0579 0.1436 0.0947 0.0382 0.172 2.170 2.507 128.384 0.245 11.150 8.856 0.27 92449. 0.6094
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5.55 0.0868 0.2082 0.0935 0.0390 0.176 2.217 2.474 131.146 0.250 11.006 8.558 0.27 92534. 0.5851
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7.40 0.1157 0.2680 0.0921 0.0398 0.179 2.262 2.438 133.812 0.256 10.845 8.265 0.27 92629. 0.5609
|
|
9.25 0.1447 0.3234 0.0906 0.0405 0.183 2.304 2.398 136.324 0.260 10.665 7.978 0.27 92733. 0.5369
|
|
11.10 0.1736 0.3745 0.0889 0.0412 0.186 2.343 2.353 138.621 0.265 10.464 7.698 0.27 92846. 0.5132
|
|
12.95 0.2025 0.4215 0.0870 0.0418 0.189 2.377 2.302 140.635 0.269 10.241 7.426 0.27 92970. 0.4897
|
|
14.80 0.2315 0.4646 0.0849 0.0423 0.191 2.405 2.247 142.297 0.272 9.994 7.162 0.27 93104. 0.4666
|
|
16.65 0.2604 0.5040 0.0826 0.0427 0.192 2.426 2.186 143.534 0.274 9.721 6.906 0.27 93248. 0.4438
|
|
18.49 0.2893 0.5400 0.0800 0.0429 0.193 2.439 2.118 144.273 0.276 9.422 6.660 0.27 93403. 0.4213
|
|
20.34 0.3183 0.5727 0.0773 0.0429 0.194 2.442 2.045 144.438 0.276 9.095 6.421 0.27 93569. 0.3991
|
|
22.19 0.3472 0.6023 0.0742 0.0428 0.193 2.433 1.965 143.954 0.275 8.739 6.190 0.27 93746. 0.3771
|
|
24.04 0.3761 0.6290 0.0710 0.0424 0.191 2.413 1.878 142.754 0.273 8.354 5.967 0.27 93934. 0.3554
|
|
25.89 0.4051 0.6528 0.0675 0.0419 0.189 2.380 1.785 140.793 0.269 7.940 5.751 0.27 94133. 0.3340
|
|
27.74 0.4340 0.6738 0.0637 0.0410 0.185 2.334 1.686 138.052 0.264 7.501 5.540 0.27 94343. 0.3127
|
|
29.59 0.4630 0.6921 0.0598 0.0400 0.180 2.274 1.582 134.535 0.257 7.038 5.335 0.27 94564. 0.2917
|
|
31.44 0.4919 0.7075 0.0557 0.0387 0.175 2.202 1.474 130.255 0.249 6.556 5.133 0.27 94796. 0.2708
|
|
33.29 0.5208 0.7198 0.0515 0.0372 0.168 2.117 1.362 125.228 0.239 6.057 4.932 0.27 95039. 0.2502
|
|
35.14 0.5498 0.7289 0.0471 0.0355 0.160 2.020 1.246 119.467 0.228 5.543 4.732 0.27 95294. 0.2296
|
|
36.99 0.5787 0.7343 0.0426 0.0336 0.152 1.910 1.128 112.983 0.216 5.017 4.528 0.27 95559. 0.2090
|
|
38.84 0.6076 0.7353 0.0381 0.0315 0.142 1.788 1.007 105.784 0.202 4.480 4.319 0.27 95835. 0.1884
|
|
40.69 0.6366 0.7311 0.0334 0.0291 0.131 1.655 0.884 97.882 0.187 3.934 4.099 0.27 96122. 0.1675
|
|
42.54 0.6655 0.7200 0.0287 0.0265 0.120 1.509 0.760 89.287 0.171 3.381 3.861 0.27 96421. 0.1463
|
|
44.39 0.6944 0.6997 0.0240 0.0238 0.107 1.353 0.634 80.014 0.153 2.821 3.596 0.27 96730. 0.1245
|
|
46.24 0.7234 0.6660 0.0192 0.0208 0.094 1.185 0.508 70.082 0.134 2.258 3.286 0.27 97050. 0.1018
|
|
48.09 0.7523 0.6114 0.0144 0.0177 0.080 1.006 0.381 59.520 0.114 1.693 2.900 0.28 97381. 0.0778
|
|
49.94 0.7812 0.5204 0.0096 0.0144 0.065 0.818 0.253 48.365 0.092 1.127 2.377 0.28 97722. 0.0520
|
|
51.79 0.8102 0.3567 0.0048 0.0109 0.049 0.620 0.127 36.668 0.070 0.565 1.571 0.28 98074. 0.0243
|
|
53.64 0.8391 0.0069 0.0001 0.0073 0.033 0.414 0.002 24.466 0.047 0.007 0.029 0.28 98432. 0.0001
|
|
|
|
|
|
|
|
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 0.0971 0.0360 0.280 2.946 3.701 209.155 0.333 16.462 8.026 0.32 110760. 0.6711
|
|
2.22 0.0290 0.0756 0.0962 0.0368 0.287 3.016 3.665 214.085 0.341 16.301 7.764 0.32 110843. 0.6461
|
|
4.44 0.0579 0.1462 0.0951 0.0377 0.294 3.085 3.624 219.027 0.349 16.120 7.505 0.32 110936. 0.6210
|
|
6.67 0.0869 0.2118 0.0939 0.0385 0.300 3.154 3.578 223.897 0.356 15.915 7.249 0.32 111039. 0.5959
|
|
8.89 0.1159 0.2726 0.0925 0.0393 0.307 3.220 3.526 228.603 0.364 15.686 6.997 0.32 111152. 0.5711
|
|
11.11 0.1448 0.3288 0.0910 0.0401 0.313 3.283 3.469 233.045 0.371 15.428 6.751 0.32 111277. 0.5465
|
|
13.33 0.1738 0.3805 0.0893 0.0408 0.318 3.340 3.404 237.112 0.377 15.140 6.511 0.32 111414. 0.5221
|
|
15.55 0.2028 0.4281 0.0874 0.0414 0.323 3.391 3.332 240.688 0.383 14.820 6.279 0.32 111562. 0.4981
|
|
17.78 0.2317 0.4717 0.0853 0.0419 0.327 3.432 3.252 243.651 0.388 14.465 6.054 0.32 111723. 0.4745
|
|
20.00 0.2607 0.5116 0.0830 0.0423 0.330 3.464 3.164 245.872 0.391 14.072 5.836 0.32 111897. 0.4512
|
|
22.22 0.2897 0.5481 0.0805 0.0425 0.332 3.483 3.067 247.222 0.393 13.641 5.627 0.32 112084. 0.4283
|
|
24.44 0.3186 0.5812 0.0777 0.0426 0.332 3.487 2.961 247.566 0.394 13.169 5.424 0.32 112283. 0.4057
|
|
26.66 0.3476 0.6112 0.0747 0.0425 0.331 3.476 2.845 246.776 0.393 12.655 5.229 0.32 112496. 0.3834
|
|
28.88 0.3766 0.6383 0.0714 0.0421 0.328 3.448 2.720 244.733 0.390 12.098 5.041 0.32 112722. 0.3613
|
|
31.11 0.4055 0.6626 0.0678 0.0415 0.324 3.400 2.585 241.355 0.384 11.500 4.859 0.32 112962. 0.3395
|
|
33.33 0.4345 0.6841 0.0641 0.0407 0.317 3.333 2.442 236.609 0.377 10.864 4.682 0.32 113214. 0.3180
|
|
35.55 0.4635 0.7029 0.0601 0.0397 0.309 3.247 2.292 230.500 0.367 10.194 4.510 0.32 113480. 0.2967
|
|
37.77 0.4924 0.7189 0.0560 0.0384 0.299 3.142 2.135 223.053 0.355 9.496 4.341 0.33 113760. 0.2757
|
|
39.99 0.5214 0.7319 0.0518 0.0369 0.287 3.019 1.972 214.291 0.341 8.773 4.175 0.33 114052. 0.2548
|
|
42.22 0.5504 0.7418 0.0474 0.0351 0.274 2.877 1.805 204.239 0.325 8.028 4.008 0.33 114358. 0.2341
|
|
44.44 0.5793 0.7482 0.0429 0.0332 0.259 2.718 1.634 192.914 0.307 7.266 3.841 0.33 114677. 0.2134
|
|
46.66 0.6083 0.7504 0.0383 0.0310 0.242 2.540 1.459 180.333 0.287 6.488 3.669 0.33 115010. 0.1926
|
|
48.88 0.6373 0.7476 0.0336 0.0286 0.223 2.346 1.281 166.513 0.265 5.697 3.489 0.33 115355. 0.1716
|
|
51.10 0.6662 0.7382 0.0289 0.0261 0.203 2.134 1.100 151.474 0.241 4.895 3.295 0.33 115714. 0.1502
|
|
53.33 0.6952 0.7199 0.0241 0.0233 0.181 1.905 0.918 135.240 0.215 4.084 3.079 0.33 116086. 0.1283
|
|
55.55 0.7242 0.6886 0.0193 0.0203 0.158 1.660 0.735 117.848 0.188 3.268 2.828 0.33 116471. 0.1053
|
|
57.77 0.7531 0.6365 0.0144 0.0171 0.133 1.400 0.550 99.347 0.158 2.449 2.513 0.33 116868. 0.0811
|
|
59.99 0.7821 0.5476 0.0096 0.0137 0.107 1.124 0.366 79.804 0.127 1.630 2.082 0.33 117279. 0.0548
|
|
62.21 0.8111 0.3821 0.0048 0.0102 0.080 0.835 0.183 59.306 0.094 0.815 1.401 0.33 117702. 0.0261
|
|
64.43 0.8400 0.0048 0.0000 0.0065 0.051 0.534 0.001 37.918 0.060 0.006 0.017 0.33 118131. 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 0.0975 0.0357 0.442 3.975 5.058 329.230 0.449 22.499 6.968 0.37 129216. 0.6812
|
|
2.59 0.0290 0.0766 0.0966 0.0365 0.452 4.072 5.010 337.197 0.460 22.284 6.739 0.37 129313. 0.6556
|
|
5.19 0.0580 0.1481 0.0955 0.0374 0.463 4.168 4.955 345.193 0.471 22.041 6.511 0.37 129421. 0.6300
|
|
7.78 0.0870 0.2145 0.0944 0.0383 0.473 4.263 4.894 353.079 0.482 21.767 6.286 0.37 129541. 0.6044
|
|
10.38 0.1160 0.2759 0.0930 0.0391 0.484 4.355 4.824 360.710 0.492 21.458 6.066 0.38 129674. 0.5791
|
|
12.97 0.1449 0.3327 0.0915 0.0399 0.493 4.442 4.746 367.920 0.502 21.110 5.851 0.38 129820. 0.5540
|
|
15.56 0.1739 0.3850 0.0898 0.0406 0.502 4.522 4.659 374.533 0.511 20.721 5.642 0.38 129979. 0.5292
|
|
18.16 0.2029 0.4330 0.0879 0.0412 0.510 4.593 4.561 380.359 0.519 20.287 5.439 0.38 130153. 0.5049
|
|
20.75 0.2319 0.4770 0.0858 0.0417 0.517 4.651 4.453 385.201 0.525 19.805 5.243 0.38 130341. 0.4808
|
|
23.35 0.2609 0.5173 0.0835 0.0421 0.521 4.695 4.333 388.853 0.530 19.272 5.054 0.38 130545. 0.4572
|
|
25.94 0.2899 0.5540 0.0810 0.0424 0.524 4.722 4.201 391.102 0.534 18.684 4.872 0.38 130763. 0.4340
|
|
28.54 0.3189 0.5875 0.0782 0.0424 0.525 4.730 4.056 391.736 0.534 18.041 4.696 0.38 130996. 0.4111
|
|
31.13 0.3479 0.6178 0.0752 0.0423 0.524 4.716 3.898 390.543 0.533 17.339 4.527 0.38 131245. 0.3885
|
|
33.72 0.3769 0.6453 0.0719 0.0420 0.519 4.677 3.727 387.335 0.528 16.578 4.364 0.38 131510. 0.3662
|
|
36.32 0.4058 0.6699 0.0683 0.0414 0.512 4.612 3.543 381.974 0.521 15.760 4.207 0.38 131790. 0.3442
|
|
38.91 0.4348 0.6918 0.0645 0.0406 0.502 4.521 3.348 374.408 0.511 14.890 4.055 0.38 132085. 0.3225
|
|
41.51 0.4638 0.7111 0.0606 0.0395 0.489 4.403 3.142 364.645 0.497 13.974 3.908 0.38 132396. 0.3010
|
|
44.10 0.4928 0.7276 0.0564 0.0382 0.473 4.259 2.927 352.721 0.481 13.017 3.763 0.38 132723. 0.2798
|
|
46.69 0.5218 0.7413 0.0521 0.0367 0.454 4.089 2.704 338.677 0.462 12.027 3.621 0.38 133065. 0.2588
|
|
49.29 0.5508 0.7519 0.0477 0.0349 0.433 3.895 2.475 322.548 0.440 11.007 3.480 0.38 133422. 0.2379
|
|
51.88 0.5798 0.7591 0.0432 0.0330 0.408 3.675 2.240 304.366 0.415 9.962 3.338 0.38 133795. 0.2171
|
|
54.48 0.6088 0.7624 0.0386 0.0308 0.381 3.431 2.000 284.156 0.388 8.895 3.192 0.38 134184. 0.1962
|
|
57.07 0.6377 0.7607 0.0339 0.0284 0.351 3.163 1.756 261.944 0.357 7.811 3.041 0.38 134587. 0.1751
|
|
59.67 0.6667 0.7529 0.0291 0.0258 0.319 2.871 1.509 237.763 0.324 6.711 2.878 0.38 135006. 0.1537
|
|
62.26 0.6957 0.7364 0.0243 0.0229 0.284 2.556 1.259 211.654 0.289 5.600 2.698 0.38 135441. 0.1316
|
|
64.85 0.7247 0.7073 0.0194 0.0199 0.246 2.218 1.007 183.675 0.251 4.481 2.488 0.38 135891. 0.1085
|
|
67.45 0.7537 0.6577 0.0146 0.0167 0.206 1.858 0.755 153.904 0.210 3.357 2.224 0.39 136356. 0.0840
|
|
70.04 0.7827 0.5713 0.0097 0.0133 0.164 1.479 0.502 122.451 0.167 2.234 1.861 0.39 136835. 0.0573
|
|
72.64 0.8117 0.4054 0.0048 0.0097 0.120 1.080 0.251 89.460 0.122 1.117 1.273 0.39 137330. 0.0277
|
|
75.23 0.8407 0.0050 0.0000 0.0060 0.074 0.664 0.002 55.020 0.075 0.008 0.015 0.39 137830. 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 0.0980 0.0355 0.656 5.168 6.637 489.162 0.584 29.523 6.154 0.43 147669. 0.6892
|
|
2.97 0.0290 0.0774 0.0971 0.0364 0.672 5.296 6.576 501.274 0.598 29.249 5.950 0.43 147780. 0.6632
|
|
5.93 0.0580 0.1495 0.0960 0.0373 0.689 5.425 6.506 513.442 0.613 28.938 5.747 0.43 147904. 0.6372
|
|
8.90 0.0870 0.2164 0.0949 0.0381 0.705 5.552 6.427 525.457 0.627 28.586 5.547 0.43 148041. 0.6113
|
|
11.87 0.1160 0.2784 0.0935 0.0390 0.720 5.675 6.337 537.095 0.641 28.188 5.352 0.43 148193. 0.5856
|
|
14.83 0.1450 0.3356 0.0921 0.0398 0.735 5.791 6.236 548.105 0.654 27.739 5.161 0.43 148360. 0.5601
|
|
17.80 0.1740 0.3882 0.0904 0.0405 0.749 5.898 6.123 558.217 0.666 27.235 4.975 0.43 148543. 0.5351
|
|
20.77 0.2030 0.4366 0.0885 0.0412 0.761 5.992 5.996 567.144 0.677 26.672 4.796 0.43 148742. 0.5104
|
|
23.73 0.2321 0.4809 0.0864 0.0417 0.771 6.071 5.855 574.582 0.686 26.044 4.622 0.43 148958. 0.4861
|
|
26.70 0.2611 0.5215 0.0841 0.0421 0.778 6.130 5.699 580.218 0.693 25.349 4.455 0.43 149190. 0.4623
|
|
29.67 0.2901 0.5585 0.0816 0.0424 0.783 6.167 5.527 583.733 0.697 24.582 4.294 0.43 149440. 0.4388
|
|
32.63 0.3191 0.5922 0.0788 0.0424 0.784 6.179 5.337 584.800 0.698 23.740 4.140 0.43 149708. 0.4157
|
|
35.60 0.3481 0.6228 0.0757 0.0423 0.782 6.161 5.131 583.101 0.696 22.821 3.991 0.43 149993. 0.3929
|
|
38.57 0.3771 0.6506 0.0724 0.0420 0.776 6.110 4.906 578.348 0.690 21.824 3.848 0.43 150296. 0.3705
|
|
41.53 0.4061 0.6755 0.0689 0.0414 0.765 6.026 4.665 570.333 0.681 20.751 3.710 0.43 150616. 0.3483
|
|
44.50 0.4351 0.6978 0.0651 0.0406 0.750 5.906 4.408 558.971 0.667 19.608 3.577 0.43 150955. 0.3264
|
|
47.47 0.4641 0.7175 0.0611 0.0395 0.730 5.750 4.137 544.274 0.650 18.403 3.448 0.43 151311. 0.3048
|
|
50.43 0.4931 0.7345 0.0569 0.0382 0.706 5.560 3.855 526.298 0.628 17.145 3.322 0.43 151685. 0.2835
|
|
53.40 0.5221 0.7487 0.0526 0.0367 0.677 5.337 3.562 505.104 0.603 15.842 3.198 0.43 152077. 0.2623
|
|
56.37 0.5511 0.7600 0.0481 0.0349 0.645 5.079 3.260 480.747 0.574 14.500 3.076 0.43 152486. 0.2414
|
|
59.33 0.5801 0.7680 0.0436 0.0329 0.608 4.789 2.951 453.273 0.541 13.124 2.952 0.44 152913. 0.2204
|
|
62.30 0.6091 0.7721 0.0389 0.0307 0.567 4.466 2.635 422.722 0.505 11.720 2.827 0.44 153358. 0.1995
|
|
65.26 0.6381 0.7716 0.0342 0.0282 0.522 4.111 2.314 389.135 0.464 10.291 2.697 0.44 153820. 0.1783
|
|
68.23 0.6672 0.7650 0.0293 0.0256 0.473 3.725 1.988 352.559 0.421 8.843 2.558 0.44 154299. 0.1567
|
|
71.20 0.6962 0.7502 0.0245 0.0227 0.420 3.308 1.659 313.057 0.374 7.379 2.404 0.44 154797. 0.1346
|
|
74.16 0.7252 0.7231 0.0196 0.0197 0.363 2.860 1.327 270.716 0.323 5.904 2.224 0.44 155311. 0.1114
|
|
77.13 0.7542 0.6760 0.0147 0.0164 0.303 2.384 0.995 225.657 0.269 4.424 1.999 0.44 155843. 0.0867
|
|
80.10 0.7832 0.5921 0.0098 0.0129 0.239 1.881 0.662 178.047 0.213 2.944 1.686 0.44 156392. 0.0596
|
|
83.06 0.8122 0.4265 0.0049 0.0093 0.172 1.353 0.331 128.105 0.153 1.471 1.171 0.44 156958. 0.0293
|
|
86.03 0.8412 0.0050 0.0000 0.0055 0.102 0.802 0.002 75.952 0.091 0.010 0.013 0.44 157529. 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 0.0985 0.0355 0.933 6.532 8.444 695.543 0.738 37.560 5.507 0.48 166121. 0.6955
|
|
3.34 0.0290 0.0779 0.0976 0.0364 0.956 6.697 8.368 713.128 0.757 37.223 5.323 0.48 166245. 0.6692
|
|
6.68 0.0580 0.1505 0.0966 0.0373 0.980 6.863 8.282 730.818 0.775 36.839 5.140 0.48 166385. 0.6430
|
|
10.02 0.0871 0.2178 0.0955 0.0381 1.003 7.028 8.184 748.308 0.794 36.403 4.961 0.48 166539. 0.6168
|
|
13.36 0.1161 0.2802 0.0942 0.0390 1.026 7.187 8.073 765.266 0.812 35.908 4.785 0.48 166710. 0.5909
|
|
16.70 0.1451 0.3377 0.0927 0.0398 1.048 7.338 7.947 781.332 0.829 35.348 4.613 0.48 166899. 0.5652
|
|
20.03 0.1741 0.3906 0.0910 0.0406 1.068 7.477 7.805 796.107 0.845 34.717 4.447 0.48 167105. 0.5400
|
|
23.37 0.2031 0.4392 0.0892 0.0413 1.085 7.599 7.646 809.172 0.859 34.010 4.286 0.48 167329. 0.5151
|
|
26.71 0.2322 0.4837 0.0871 0.0418 1.100 7.702 7.469 820.087 0.870 33.220 4.131 0.48 167572. 0.4906
|
|
30.05 0.2612 0.5245 0.0848 0.0422 1.111 7.780 7.271 828.395 0.879 32.343 3.981 0.48 167834. 0.4666
|
|
33.39 0.2902 0.5618 0.0823 0.0425 1.118 7.829 7.053 833.633 0.885 31.373 3.838 0.48 168116. 0.4430
|
|
36.73 0.3192 0.5957 0.0795 0.0426 1.120 7.845 6.814 835.329 0.886 30.307 3.700 0.48 168418. 0.4197
|
|
40.07 0.3483 0.6266 0.0764 0.0425 1.117 7.823 6.551 833.022 0.884 29.140 3.567 0.48 168739. 0.3968
|
|
43.41 0.3773 0.6546 0.0731 0.0421 1.108 7.760 6.266 826.294 0.877 27.873 3.440 0.49 169081. 0.3743
|
|
46.75 0.4063 0.6798 0.0695 0.0415 1.093 7.652 5.959 814.840 0.865 26.508 3.317 0.49 169442. 0.3520
|
|
50.09 0.4353 0.7024 0.0657 0.0407 1.071 7.499 5.632 798.536 0.847 25.052 3.199 0.49 169824. 0.3300
|
|
53.43 0.4643 0.7225 0.0617 0.0396 1.043 7.301 5.287 777.397 0.825 23.517 3.085 0.49 170225. 0.3083
|
|
56.76 0.4934 0.7399 0.0575 0.0383 1.008 7.058 4.926 751.504 0.797 21.913 2.973 0.49 170647. 0.2868
|
|
60.10 0.5224 0.7547 0.0531 0.0368 0.967 6.771 4.553 720.949 0.765 20.250 2.864 0.49 171088. 0.2656
|
|
63.44 0.5514 0.7665 0.0486 0.0350 0.920 6.441 4.167 685.813 0.728 18.536 2.756 0.49 171549. 0.2445
|
|
66.78 0.5804 0.7752 0.0440 0.0329 0.867 6.068 3.772 646.163 0.686 16.779 2.648 0.49 172030. 0.2235
|
|
70.12 0.6094 0.7802 0.0393 0.0307 0.807 5.654 3.369 602.056 0.639 14.985 2.538 0.49 172531. 0.2025
|
|
73.46 0.6385 0.7807 0.0345 0.0282 0.742 5.199 2.959 553.554 0.587 13.160 2.424 0.49 173052. 0.1812
|
|
76.80 0.6675 0.7754 0.0297 0.0255 0.671 4.702 2.542 500.724 0.531 11.309 2.303 0.49 173592. 0.1596
|
|
80.14 0.6965 0.7621 0.0247 0.0226 0.595 4.167 2.122 443.657 0.471 9.438 2.169 0.49 174153. 0.1373
|
|
83.48 0.7255 0.7368 0.0198 0.0195 0.513 3.592 1.698 382.479 0.406 7.552 2.013 0.49 174732. 0.1140
|
|
86.82 0.7545 0.6920 0.0148 0.0162 0.426 2.981 1.272 317.366 0.337 5.659 1.818 0.50 175331. 0.0891
|
|
90.16 0.7836 0.6107 0.0099 0.0127 0.333 2.334 0.847 248.560 0.264 3.766 1.545 0.50 175950. 0.0618
|
|
93.49 0.8126 0.4461 0.0049 0.0090 0.237 1.656 0.423 176.380 0.187 1.883 1.088 0.50 176587. 0.0308
|
|
96.83 0.8416 0.0053 0.0000 0.0051 0.135 0.948 0.003 100.979 0.107 0.012 0.013 0.50 177229. 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 0.0991 0.0355 1.281 8.076 10.485 955.497 0.912 46.637 4.977 0.54 184569. 0.7005
|
|
3.71 0.0290 0.0783 0.0982 0.0364 1.314 8.284 10.395 980.143 0.936 46.237 4.810 0.54 184707. 0.6741
|
|
7.42 0.0581 0.1512 0.0972 0.0373 1.348 8.494 10.292 1004.974 0.960 45.778 4.645 0.54 184862. 0.6477
|
|
11.14 0.0871 0.2188 0.0961 0.0383 1.381 8.702 10.174 1029.556 0.983 45.253 4.482 0.54 185034. 0.6214
|
|
14.85 0.1161 0.2814 0.0948 0.0391 1.413 8.904 10.040 1053.426 1.006 44.656 4.323 0.54 185225. 0.5953
|
|
18.56 0.1452 0.3391 0.0934 0.0400 1.443 9.095 9.887 1076.069 1.028 43.977 4.167 0.54 185434. 0.5695
|
|
22.27 0.1742 0.3922 0.0918 0.0408 1.471 9.271 9.714 1096.926 1.047 43.209 4.017 0.54 185663. 0.5441
|
|
25.98 0.2032 0.4410 0.0899 0.0415 1.496 9.428 9.520 1115.401 1.065 42.345 3.871 0.54 185913. 0.5192
|
|
29.69 0.2323 0.4857 0.0879 0.0420 1.517 9.558 9.302 1130.874 1.080 41.377 3.731 0.54 186183. 0.4946
|
|
33.41 0.2613 0.5266 0.0856 0.0425 1.532 9.658 9.060 1142.706 1.091 40.299 3.596 0.54 186476. 0.4705
|
|
37.12 0.2903 0.5641 0.0831 0.0427 1.543 9.722 8.791 1150.245 1.098 39.103 3.467 0.54 186790. 0.4467
|
|
40.83 0.3194 0.5982 0.0803 0.0428 1.546 9.744 8.495 1152.833 1.101 37.786 3.342 0.54 187125. 0.4234
|
|
44.54 0.3484 0.6293 0.0772 0.0427 1.542 9.719 8.171 1149.828 1.098 36.343 3.223 0.54 187483. 0.4004
|
|
48.25 0.3774 0.6576 0.0739 0.0424 1.530 9.641 7.817 1140.643 1.089 34.772 3.109 0.54 187864. 0.3778
|
|
51.96 0.4065 0.6831 0.0703 0.0418 1.508 9.508 7.436 1124.850 1.074 33.077 2.999 0.54 188266. 0.3554
|
|
55.68 0.4355 0.7060 0.0664 0.0410 1.478 9.317 7.030 1102.268 1.053 31.268 2.893 0.54 188691. 0.3333
|
|
59.39 0.4645 0.7264 0.0624 0.0399 1.439 9.069 6.600 1072.921 1.025 29.357 2.790 0.54 189138. 0.3116
|
|
63.10 0.4936 0.7443 0.0581 0.0385 1.391 8.764 6.151 1036.924 0.990 27.360 2.691 0.54 189607. 0.2900
|
|
66.81 0.5226 0.7595 0.0537 0.0370 1.334 8.405 5.685 994.408 0.950 25.287 2.593 0.54 190099. 0.2687
|
|
70.52 0.5516 0.7719 0.0492 0.0351 1.268 7.992 5.205 945.490 0.903 23.151 2.497 0.54 190612. 0.2476
|
|
74.23 0.5807 0.7813 0.0445 0.0331 1.194 7.525 4.712 890.268 0.850 20.959 2.401 0.54 191147. 0.2265
|
|
77.95 0.6097 0.7871 0.0398 0.0308 1.111 7.005 4.209 828.824 0.791 18.721 2.303 0.55 191705. 0.2054
|
|
81.66 0.6387 0.7885 0.0349 0.0283 1.021 6.434 3.697 761.242 0.727 16.443 2.203 0.55 192284. 0.1841
|
|
85.37 0.6678 0.7843 0.0300 0.0256 0.922 5.812 3.177 687.617 0.657 14.132 2.096 0.55 192886. 0.1624
|
|
89.08 0.6968 0.7724 0.0251 0.0226 0.815 5.140 2.652 608.076 0.581 11.795 1.978 0.55 193509. 0.1400
|
|
92.79 0.7258 0.7490 0.0200 0.0194 0.701 4.419 2.122 522.795 0.499 9.439 1.841 0.55 194154. 0.1166
|
|
96.50 0.7549 0.7064 0.0150 0.0161 0.579 3.652 1.590 432.019 0.413 7.074 1.670 0.55 194820. 0.0915
|
|
100.22 0.7839 0.6276 0.0100 0.0125 0.451 2.841 1.059 336.087 0.321 4.708 1.429 0.55 195508. 0.0639
|
|
103.93 0.8129 0.4644 0.0050 0.0088 0.316 1.990 0.529 235.449 0.225 2.354 1.019 0.55 196216. 0.0322
|
|
107.64 0.8420 0.0056 0.0000 0.0048 0.175 1.101 0.003 130.286 0.124 0.015 0.012 0.55 196928. 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 0.0997 0.0357 1.712 9.811 12.767 1276.828 1.108 56.788 4.535 0.59 203014. 0.7043
|
|
4.08 0.0290 0.0785 0.0989 0.0366 1.757 10.069 12.663 1310.425 1.138 56.325 4.383 0.59 203166. 0.6779
|
|
8.17 0.0581 0.1516 0.0979 0.0375 1.803 10.330 12.543 1344.331 1.167 55.792 4.232 0.59 203336. 0.6514
|
|
12.25 0.0871 0.2193 0.0969 0.0385 1.848 10.588 12.405 1377.955 1.196 55.179 4.083 0.59 203526. 0.6251
|
|
16.34 0.1162 0.2820 0.0956 0.0394 1.892 10.839 12.247 1410.664 1.225 54.476 3.938 0.59 203735. 0.5990
|
|
20.42 0.1452 0.3399 0.0942 0.0403 1.933 11.078 12.067 1441.739 1.252 53.674 3.796 0.59 203966. 0.5732
|
|
24.51 0.1743 0.3931 0.0926 0.0411 1.972 11.298 11.862 1470.411 1.276 52.762 3.659 0.59 204218. 0.5477
|
|
28.59 0.2033 0.4420 0.0908 0.0418 2.006 11.494 11.630 1495.861 1.299 51.731 3.526 0.59 204493. 0.5227
|
|
32.68 0.2324 0.4869 0.0888 0.0424 2.035 11.658 11.369 1517.233 1.317 50.571 3.399 0.59 204792. 0.4981
|
|
36.76 0.2614 0.5280 0.0865 0.0428 2.057 11.784 11.078 1533.651 1.331 49.274 3.276 0.59 205114. 0.4739
|
|
40.84 0.2904 0.5656 0.0840 0.0431 2.071 11.866 10.754 1544.229 1.341 47.832 3.159 0.59 205460. 0.4502
|
|
44.93 0.3195 0.5999 0.0812 0.0432 2.076 11.895 10.395 1548.073 1.344 46.238 3.046 0.59 205830. 0.4268
|
|
49.01 0.3485 0.6312 0.0781 0.0431 2.071 11.866 10.002 1544.309 1.341 44.488 2.938 0.59 206225. 0.4038
|
|
53.10 0.3776 0.6597 0.0747 0.0428 2.055 11.773 9.573 1532.142 1.330 42.579 2.834 0.59 206644. 0.3811
|
|
57.18 0.4066 0.6854 0.0711 0.0422 2.026 11.610 9.109 1510.985 1.312 40.516 2.734 0.59 207088. 0.3587
|
|
61.27 0.4357 0.7087 0.0672 0.0413 1.986 11.377 8.613 1480.589 1.285 38.310 2.639 0.59 207557. 0.3366
|
|
65.35 0.4647 0.7294 0.0632 0.0402 1.932 11.072 8.089 1440.983 1.251 35.978 2.546 0.60 208049. 0.3147
|
|
69.44 0.4938 0.7477 0.0589 0.0389 1.867 10.698 7.540 1392.330 1.209 33.538 2.456 0.60 208567. 0.2931
|
|
73.52 0.5228 0.7634 0.0544 0.0373 1.790 10.257 6.970 1334.814 1.159 31.004 2.368 0.60 209108. 0.2718
|
|
77.60 0.5519 0.7764 0.0498 0.0354 1.701 9.748 6.383 1268.605 1.101 28.390 2.282 0.60 209674. 0.2506
|
|
81.69 0.5809 0.7863 0.0451 0.0333 1.601 9.173 5.779 1193.836 1.036 25.707 2.196 0.60 210264. 0.2294
|
|
85.77 0.6099 0.7929 0.0403 0.0310 1.489 8.534 5.163 1110.627 0.964 22.965 2.109 0.60 210878. 0.2082
|
|
89.86 0.6390 0.7952 0.0354 0.0285 1.367 7.831 4.536 1019.089 0.885 20.174 2.019 0.60 211516. 0.1869
|
|
93.94 0.6680 0.7921 0.0304 0.0257 1.233 7.064 3.899 919.354 0.798 17.341 1.923 0.60 212179. 0.1651
|
|
98.03 0.6971 0.7816 0.0254 0.0227 1.088 6.236 3.254 811.593 0.705 14.476 1.819 0.60 212865. 0.1426
|
|
102.11 0.7261 0.7599 0.0203 0.0194 0.933 5.348 2.605 696.043 0.604 11.587 1.697 0.60 213575. 0.1191
|
|
106.20 0.7552 0.7195 0.0152 0.0160 0.768 4.403 1.952 573.039 0.497 8.685 1.545 0.61 214309. 0.0939
|
|
110.28 0.7842 0.6433 0.0101 0.0124 0.594 3.404 1.300 443.040 0.385 5.781 1.331 0.61 215066. 0.0659
|
|
114.36 0.8133 0.4819 0.0051 0.0086 0.411 2.356 0.650 306.661 0.266 2.891 0.961 0.61 215846. 0.0337
|
|
118.45 0.8423 0.0060 0.0000 0.0046 0.220 1.261 0.004 164.106 0.142 0.018 0.011 0.61 216628. 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 0.1004 0.0359 2.239 11.760 15.298 1669.653 1.329 68.045 4.156 0.64 221456. 0.7065
|
|
4.46 0.0291 0.0785 0.0996 0.0369 2.299 12.074 15.181 1714.133 1.364 67.526 4.017 0.64 221622. 0.6803
|
|
8.91 0.0581 0.1516 0.0987 0.0378 2.359 12.391 15.046 1759.155 1.400 66.923 3.879 0.64 221807. 0.6540
|
|
13.37 0.0872 0.2195 0.0977 0.0388 2.419 12.706 14.889 1803.940 1.436 66.225 3.744 0.64 222013. 0.6278
|
|
17.83 0.1162 0.2822 0.0965 0.0397 2.478 13.014 14.708 1847.632 1.470 65.420 3.611 0.64 222242. 0.6018
|
|
22.29 0.1453 0.3401 0.0951 0.0406 2.534 13.307 14.500 1889.275 1.503 64.495 3.481 0.64 222493. 0.5761
|
|
26.74 0.1743 0.3934 0.0936 0.0415 2.585 13.579 14.262 1927.813 1.534 63.435 3.355 0.64 222769. 0.5508
|
|
31.20 0.2034 0.4424 0.0918 0.0422 2.631 13.820 13.991 1962.128 1.561 62.230 3.234 0.64 223070. 0.5258
|
|
35.66 0.2324 0.4873 0.0898 0.0428 2.670 14.024 13.684 1991.050 1.584 60.868 3.117 0.64 223396. 0.5012
|
|
40.12 0.2615 0.5285 0.0875 0.0433 2.700 14.181 13.340 2013.388 1.602 59.337 3.005 0.64 223748. 0.4771
|
|
44.57 0.2906 0.5662 0.0850 0.0436 2.720 14.284 12.956 2027.944 1.614 57.629 2.898 0.65 224127. 0.4534
|
|
49.03 0.3196 0.6007 0.0822 0.0437 2.727 14.323 12.530 2033.534 1.618 55.735 2.795 0.65 224532. 0.4300
|
|
53.49 0.3487 0.6322 0.0791 0.0436 2.721 14.291 12.061 2029.003 1.615 53.649 2.696 0.65 224964. 0.4070
|
|
57.95 0.3777 0.6609 0.0758 0.0433 2.700 14.181 11.548 2013.292 1.602 51.368 2.602 0.65 225422. 0.3843
|
|
62.40 0.4068 0.6870 0.0721 0.0427 2.663 13.986 10.993 1985.618 1.580 48.896 2.511 0.65 225908. 0.3619
|
|
66.86 0.4358 0.7105 0.0682 0.0418 2.609 13.704 10.398 1945.634 1.548 46.250 2.424 0.65 226420. 0.3397
|
|
71.32 0.4649 0.7316 0.0641 0.0407 2.539 13.336 9.768 1893.386 1.507 43.448 2.340 0.65 226959. 0.3179
|
|
75.77 0.4939 0.7503 0.0598 0.0393 2.453 12.883 9.108 1829.096 1.456 40.511 2.258 0.65 227525. 0.2962
|
|
80.23 0.5230 0.7664 0.0553 0.0377 2.351 12.348 8.422 1753.030 1.395 37.459 2.179 0.65 228117. 0.2748
|
|
84.69 0.5520 0.7799 0.0506 0.0358 2.233 11.730 7.713 1665.416 1.325 34.309 2.101 0.65 228735. 0.2536
|
|
89.15 0.5811 0.7905 0.0458 0.0337 2.101 11.033 6.986 1566.451 1.247 31.074 2.023 0.65 229380. 0.2324
|
|
93.60 0.6102 0.7978 0.0410 0.0313 1.953 10.257 6.242 1456.291 1.159 27.766 1.944 0.65 230051. 0.2111
|
|
98.06 0.6392 0.8010 0.0360 0.0287 1.790 9.404 5.485 1335.089 1.062 24.396 1.863 0.66 230748. 0.1897
|
|
102.52 0.6683 0.7990 0.0309 0.0259 1.613 8.474 4.716 1203.020 0.957 20.975 1.778 0.66 231472. 0.1678
|
|
106.98 0.6973 0.7898 0.0258 0.0228 1.422 7.468 3.937 1060.312 0.844 17.512 1.684 0.66 232221. 0.1452
|
|
111.43 0.7264 0.7698 0.0207 0.0195 1.217 6.390 3.152 907.277 0.722 14.020 1.576 0.66 232997. 0.1216
|
|
115.89 0.7554 0.7315 0.0155 0.0160 0.998 5.243 2.363 744.356 0.592 10.510 1.440 0.66 233798. 0.0962
|
|
120.35 0.7845 0.6580 0.0103 0.0123 0.767 4.030 1.573 572.164 0.455 6.998 1.247 0.66 234625. 0.0680
|
|
124.81 0.8135 0.4988 0.0052 0.0084 0.525 2.758 0.787 391.515 0.312 3.500 0.912 0.66 235477. 0.0352
|
|
129.26 0.8426 0.0064 0.0000 0.0044 0.272 1.427 0.005 202.639 0.161 0.022 0.011 0.67 236329. 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 0.1011 0.0365 2.897 14.044 18.084 2159.966 1.587 80.436 3.797 0.70 239894. 0.7019
|
|
4.83 0.0291 0.0778 0.1004 0.0375 2.972 14.410 17.957 2216.362 1.628 79.871 3.675 0.70 240073. 0.6768
|
|
9.66 0.0581 0.1505 0.0995 0.0385 3.049 14.782 17.808 2273.516 1.670 79.211 3.553 0.70 240273. 0.6516
|
|
14.49 0.0872 0.2180 0.0986 0.0394 3.125 15.152 17.635 2330.440 1.712 78.439 3.432 0.70 240496. 0.6265
|
|
19.32 0.1163 0.2807 0.0975 0.0404 3.200 15.513 17.433 2386.058 1.753 77.541 3.314 0.70 240743. 0.6014
|
|
24.15 0.1453 0.3386 0.0961 0.0413 3.271 15.859 17.198 2439.157 1.792 76.499 3.198 0.70 241016. 0.5765
|
|
28.98 0.1744 0.3920 0.0946 0.0421 3.337 16.179 16.928 2488.405 1.828 75.297 3.086 0.70 241315. 0.5518
|
|
33.81 0.2035 0.4412 0.0929 0.0428 3.396 16.465 16.618 2532.372 1.860 73.918 2.976 0.70 241641. 0.5274
|
|
38.64 0.2325 0.4864 0.0909 0.0435 3.446 16.707 16.266 2569.558 1.887 72.349 2.871 0.70 241995. 0.5033
|
|
43.47 0.2616 0.5278 0.0887 0.0440 3.485 16.894 15.867 2598.414 1.909 70.575 2.770 0.70 242378. 0.4795
|
|
48.30 0.2906 0.5658 0.0862 0.0443 3.510 17.017 15.419 2617.373 1.923 68.585 2.672 0.70 242789. 0.4560
|
|
53.13 0.3197 0.6006 0.0834 0.0444 3.520 17.066 14.921 2624.850 1.928 66.369 2.578 0.70 243229. 0.4329
|
|
57.96 0.3488 0.6323 0.0803 0.0443 3.513 17.030 14.370 2619.294 1.924 63.918 2.488 0.70 243698. 0.4100
|
|
62.79 0.3778 0.6613 0.0770 0.0440 3.486 16.900 13.766 2599.278 1.909 61.231 2.402 0.70 244197. 0.3874
|
|
67.62 0.4069 0.6876 0.0733 0.0434 3.438 16.669 13.110 2563.707 1.883 58.312 2.319 0.70 244724. 0.3650
|
|
72.45 0.4360 0.7115 0.0693 0.0425 3.369 16.333 12.405 2512.064 1.845 55.178 2.240 0.70 245281. 0.3429
|
|
77.29 0.4650 0.7329 0.0652 0.0413 3.278 15.893 11.658 2444.381 1.796 51.854 2.163 0.70 245866. 0.3210
|
|
82.12 0.4941 0.7520 0.0608 0.0399 3.166 15.350 10.874 2360.958 1.734 48.366 2.089 0.70 246480. 0.2994
|
|
86.95 0.5232 0.7687 0.0562 0.0383 3.034 14.708 10.058 2262.158 1.662 44.736 2.017 0.71 247123. 0.2780
|
|
91.78 0.5522 0.7827 0.0515 0.0363 2.881 13.968 9.214 2148.310 1.578 40.985 1.945 0.71 247795. 0.2567
|
|
96.61 0.5813 0.7940 0.0467 0.0342 2.708 13.131 8.348 2019.676 1.484 37.131 1.875 0.71 248494. 0.2354
|
|
101.44 0.6104 0.8020 0.0417 0.0317 2.516 12.200 7.461 1876.478 1.378 33.187 1.803 0.71 249223. 0.2141
|
|
106.27 0.6394 0.8061 0.0367 0.0291 2.305 11.176 6.557 1718.912 1.263 29.167 1.730 0.71 249980. 0.1926
|
|
111.10 0.6685 0.8052 0.0315 0.0262 2.075 10.060 5.639 1547.205 1.137 25.084 1.653 0.71 250765. 0.1706
|
|
115.93 0.6975 0.7973 0.0263 0.0230 1.826 8.853 4.710 1361.654 1.000 20.949 1.569 0.71 251578. 0.1480
|
|
120.76 0.7266 0.7789 0.0211 0.0197 1.559 7.559 3.772 1162.663 0.854 16.776 1.471 0.71 252419. 0.1242
|
|
125.59 0.7557 0.7428 0.0158 0.0161 1.275 6.182 2.828 950.834 0.698 12.580 1.349 0.72 253288. 0.0986
|
|
130.42 0.7847 0.6719 0.0105 0.0123 0.975 4.727 1.884 727.051 0.534 8.379 1.175 0.72 254185. 0.0701
|
|
135.25 0.8138 0.5147 0.0053 0.0083 0.661 3.203 0.943 492.563 0.362 4.193 0.868 0.72 255108. 0.0366
|
|
140.08 0.8429 0.0070 0.0000 0.0042 0.332 1.612 0.006 247.871 0.182 0.028 0.011 0.72 256030. 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 0.1018 0.0381 3.769 16.968 21.125 2810.488 1.917 93.966 3.409 0.75 258328. 0.6811
|
|
5.20 0.0291 0.0754 0.1012 0.0390 3.861 17.382 20.992 2879.082 1.964 93.374 3.307 0.75 258519. 0.6586
|
|
10.41 0.0581 0.1462 0.1004 0.0399 3.954 17.800 20.835 2948.335 2.011 92.675 3.205 0.75 258734. 0.6359
|
|
15.61 0.0872 0.2124 0.0995 0.0409 4.046 18.214 20.650 3016.959 2.058 91.850 3.104 0.75 258973. 0.6132
|
|
20.81 0.1163 0.2742 0.0985 0.0418 4.135 18.617 20.431 3083.580 2.103 90.877 3.005 0.75 259239. 0.5904
|
|
26.01 0.1453 0.3316 0.0972 0.0426 4.220 18.998 20.175 3146.690 2.146 89.736 2.908 0.75 259532. 0.5677
|
|
31.22 0.1744 0.3850 0.0958 0.0434 4.298 19.348 19.876 3204.662 2.186 88.406 2.813 0.75 259854. 0.5451
|
|
36.42 0.2035 0.4344 0.0941 0.0441 4.366 19.656 19.529 3255.779 2.221 86.866 2.721 0.75 260206. 0.5226
|
|
41.62 0.2326 0.4801 0.0922 0.0447 4.423 19.913 19.132 3298.262 2.250 85.097 2.631 0.75 260588. 0.5002
|
|
46.83 0.2616 0.5222 0.0900 0.0451 4.466 20.106 18.678 3330.260 2.272 83.081 2.544 0.75 261001. 0.4779
|
|
52.03 0.2907 0.5610 0.0876 0.0454 4.492 20.225 18.166 3349.924 2.285 80.803 2.460 0.75 261445. 0.4556
|
|
57.23 0.3198 0.5967 0.0848 0.0454 4.500 20.257 17.592 3355.377 2.289 78.250 2.378 0.75 261920. 0.4335
|
|
62.43 0.3488 0.6293 0.0817 0.0453 4.485 20.193 16.954 3344.763 2.281 75.413 2.299 0.75 262427. 0.4115
|
|
67.64 0.3779 0.6591 0.0783 0.0449 4.447 20.022 16.252 3316.331 2.262 72.289 2.223 0.76 262966. 0.3895
|
|
72.84 0.4070 0.6862 0.0746 0.0443 4.383 19.734 15.487 3268.685 2.230 68.884 2.149 0.76 263535. 0.3676
|
|
78.04 0.4360 0.7108 0.0707 0.0434 4.293 19.326 14.662 3201.098 2.183 65.218 2.078 0.76 264136. 0.3458
|
|
83.25 0.4651 0.7329 0.0664 0.0422 4.175 18.797 13.786 3113.476 2.124 61.320 2.008 0.76 264769. 0.3241
|
|
88.45 0.4942 0.7526 0.0620 0.0407 4.031 18.149 12.864 3006.064 2.050 57.220 1.941 0.76 265432. 0.3026
|
|
93.65 0.5233 0.7699 0.0574 0.0390 3.861 17.383 11.904 2879.205 1.964 52.948 1.875 0.76 266126. 0.2812
|
|
98.85 0.5523 0.7846 0.0526 0.0370 3.665 16.501 10.910 2733.225 1.864 48.528 1.810 0.76 266850. 0.2599
|
|
104.06 0.5814 0.7966 0.0477 0.0348 3.444 15.506 9.888 2568.390 1.752 43.981 1.746 0.76 267606. 0.2386
|
|
109.26 0.6105 0.8054 0.0426 0.0323 3.198 14.399 8.841 2384.932 1.627 39.325 1.681 0.76 268392. 0.2173
|
|
114.46 0.6395 0.8104 0.0375 0.0296 2.928 13.180 7.773 2183.103 1.489 34.575 1.615 0.77 269208. 0.1957
|
|
119.67 0.6686 0.8106 0.0322 0.0266 2.633 11.853 6.688 1963.245 1.339 29.747 1.545 0.77 270054. 0.1737
|
|
124.87 0.6977 0.8039 0.0269 0.0234 2.314 10.420 5.588 1725.870 1.177 24.855 1.469 0.77 270931. 0.1509
|
|
130.07 0.7267 0.7868 0.0216 0.0199 1.974 8.886 4.477 1471.768 1.004 19.914 1.380 0.77 271838. 0.1269
|
|
135.27 0.7558 0.7516 0.0162 0.0163 1.612 7.258 3.359 1202.126 0.820 14.941 1.267 0.77 272775. 0.1010
|
|
140.48 0.7849 0.6807 0.0108 0.0124 1.232 5.546 2.239 918.605 0.627 9.957 1.105 0.77 273742. 0.0719
|
|
145.68 0.8140 0.5209 0.0054 0.0084 0.836 3.764 1.121 623.396 0.425 4.986 0.816 0.77 274736. 0.0375
|
|
150.88 0.8430 0.0070 0.0000 0.0043 0.426 1.918 0.007 317.622 0.217 0.033 0.011 0.78 275729. 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 0.1025 0.0412 5.016 21.078 24.417 3740.614 2.381 108.608 2.961 0.80 276757. 0.6359
|
|
5.58 0.0291 0.0704 0.1020 0.0421 5.125 21.536 24.283 3821.999 2.433 108.012 2.882 0.80 276961. 0.6172
|
|
11.15 0.0582 0.1370 0.1013 0.0430 5.235 21.995 24.123 3903.432 2.485 107.301 2.803 0.80 277189. 0.5984
|
|
16.73 0.0872 0.1998 0.1005 0.0439 5.341 22.444 23.932 3983.039 2.536 106.451 2.725 0.80 277445. 0.5795
|
|
22.30 0.1163 0.2590 0.0995 0.0447 5.443 22.871 23.704 4058.863 2.584 105.436 2.649 0.80 277728. 0.5605
|
|
27.88 0.1454 0.3146 0.0984 0.0455 5.537 23.265 23.433 4128.850 2.629 104.228 2.574 0.80 278042. 0.5416
|
|
33.45 0.1745 0.3668 0.0970 0.0461 5.620 23.615 23.111 4190.934 2.668 102.799 2.501 0.80 278387. 0.5226
|
|
39.03 0.2035 0.4158 0.0955 0.0467 5.690 23.909 22.735 4243.048 2.701 101.123 2.430 0.80 278763. 0.5036
|
|
44.61 0.2326 0.4617 0.0936 0.0472 5.744 24.135 22.297 4283.170 2.727 99.175 2.361 0.81 279173. 0.4846
|
|
50.18 0.2617 0.5046 0.0915 0.0475 5.779 24.282 21.792 4309.297 2.743 96.931 2.294 0.81 279616. 0.4654
|
|
55.76 0.2908 0.5446 0.0891 0.0476 5.792 24.339 21.217 4319.430 2.750 94.372 2.228 0.81 280093. 0.4460
|
|
61.33 0.3198 0.5817 0.0864 0.0475 5.782 24.295 20.567 4311.622 2.745 91.482 2.164 0.81 280604. 0.4265
|
|
66.91 0.3489 0.6161 0.0833 0.0472 5.745 24.139 19.840 4283.972 2.727 88.248 2.101 0.81 281149. 0.4067
|
|
72.48 0.3780 0.6478 0.0799 0.0466 5.679 23.862 19.034 4234.688 2.696 84.665 2.039 0.81 281728. 0.3866
|
|
78.06 0.4071 0.6769 0.0762 0.0458 5.582 23.454 18.152 4162.332 2.650 80.742 1.978 0.81 282341. 0.3663
|
|
83.64 0.4361 0.7034 0.0722 0.0448 5.453 22.912 17.199 4066.214 2.589 76.501 1.918 0.81 282987. 0.3458
|
|
89.21 0.4652 0.7274 0.0679 0.0435 5.292 22.237 16.182 3946.317 2.512 71.977 1.860 0.81 283667. 0.3252
|
|
94.79 0.4943 0.7488 0.0634 0.0419 5.100 21.429 15.109 3802.943 2.421 67.207 1.802 0.81 284379. 0.3045
|
|
100.36 0.5234 0.7677 0.0587 0.0400 4.877 20.491 13.989 3636.465 2.315 62.225 1.745 0.81 285125. 0.2837
|
|
105.94 0.5524 0.7839 0.0539 0.0380 4.623 19.424 12.828 3447.212 2.195 57.061 1.688 0.82 285904. 0.2628
|
|
111.51 0.5815 0.7972 0.0488 0.0356 4.339 18.231 11.633 3235.380 2.060 51.742 1.631 0.82 286715. 0.2417
|
|
117.09 0.6106 0.8073 0.0437 0.0330 4.025 16.911 10.407 3001.071 1.911 46.288 1.573 0.82 287559. 0.2205
|
|
122.66 0.6397 0.8133 0.0384 0.0302 3.682 15.470 9.155 2745.361 1.748 40.719 1.512 0.82 288435. 0.1989
|
|
128.24 0.6688 0.8139 0.0331 0.0272 3.311 13.913 7.880 2469.052 1.572 35.052 1.448 0.82 289344. 0.1766
|
|
133.82 0.6978 0.8069 0.0277 0.0239 2.913 12.242 6.588 2172.498 1.383 29.303 1.375 0.82 290285. 0.1534
|
|
139.39 0.7269 0.7880 0.0222 0.0205 2.491 10.466 5.281 1857.407 1.182 23.489 1.290 0.82 291258. 0.1288
|
|
144.97 0.7560 0.7487 0.0166 0.0168 2.047 8.599 3.964 1526.107 0.972 17.632 1.178 0.83 292263. 0.1020
|
|
150.54 0.7851 0.6695 0.0111 0.0130 1.585 6.658 2.643 1181.568 0.752 11.754 1.014 0.83 293299. 0.0717
|
|
156.12 0.8141 0.4963 0.0056 0.0091 1.110 4.663 1.323 827.451 0.527 5.884 0.725 0.83 294366. 0.0362
|
|
161.69 0.8432 0.0043 0.0000 0.0051 0.625 2.625 0.006 465.773 0.297 0.028 0.006 0.83 295432. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 16000
|
|
|
|
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 0.1030 0.0463 6.846 26.968 27.899 5105.005 3.047 124.095 2.479 0.86 295188. 0.5691
|
|
5.95 0.0291 0.0632 0.1025 0.0472 6.977 27.484 27.770 5202.657 3.105 123.520 2.421 0.86 295403. 0.5545
|
|
11.91 0.0582 0.1234 0.1019 0.0481 7.107 27.996 27.614 5299.660 3.163 122.829 2.363 0.86 295645. 0.5398
|
|
17.86 0.0873 0.1806 0.1012 0.0489 7.232 28.490 27.427 5393.180 3.219 121.994 2.307 0.86 295915. 0.5250
|
|
23.81 0.1164 0.2350 0.1004 0.0497 7.349 28.950 27.199 5480.125 3.271 120.981 2.251 0.86 296216. 0.5103
|
|
29.77 0.1455 0.2867 0.0994 0.0504 7.452 29.357 26.924 5557.230 3.317 119.757 2.197 0.86 296549. 0.4956
|
|
35.72 0.1746 0.3360 0.0981 0.0510 7.538 29.695 26.593 5621.242 3.355 118.284 2.146 0.86 296915. 0.4809
|
|
41.67 0.2037 0.3829 0.0967 0.0514 7.602 29.948 26.197 5669.127 3.384 116.525 2.096 0.86 297317. 0.4663
|
|
47.62 0.2328 0.4276 0.0950 0.0517 7.641 30.102 25.730 5698.241 3.401 114.446 2.048 0.86 297754. 0.4515
|
|
53.58 0.2619 0.4702 0.0929 0.0518 7.652 30.145 25.184 5706.383 3.406 112.016 2.002 0.86 298227. 0.4366
|
|
59.53 0.2910 0.5106 0.0906 0.0516 7.633 30.067 24.552 5691.579 3.397 109.209 1.957 0.86 298738. 0.4214
|
|
65.48 0.3201 0.5490 0.0879 0.0513 7.580 29.859 23.832 5652.349 3.373 106.004 1.912 0.86 299285. 0.4058
|
|
71.44 0.3492 0.5852 0.0849 0.0507 7.493 29.516 23.018 5587.338 3.335 102.385 1.869 0.86 299869. 0.3896
|
|
77.39 0.3784 0.6192 0.0816 0.0499 7.369 29.028 22.110 5495.030 3.280 98.344 1.825 0.86 300489. 0.3730
|
|
83.34 0.4075 0.6509 0.0779 0.0488 7.207 28.390 21.108 5374.263 3.208 93.888 1.781 0.86 301146. 0.3557
|
|
89.30 0.4366 0.6803 0.0739 0.0474 7.007 27.601 20.019 5224.832 3.118 89.043 1.738 0.87 301839. 0.3380
|
|
95.25 0.4657 0.7074 0.0696 0.0458 6.769 26.664 18.851 5047.487 3.012 83.851 1.694 0.87 302567. 0.3197
|
|
101.20 0.4948 0.7319 0.0650 0.0439 6.495 25.585 17.616 4843.289 2.891 78.357 1.650 0.87 303332. 0.3010
|
|
107.16 0.5239 0.7539 0.0602 0.0419 6.186 24.370 16.323 4613.130 2.753 72.604 1.605 0.87 304131. 0.2818
|
|
113.11 0.5530 0.7732 0.0553 0.0395 5.843 23.019 14.979 4357.470 2.601 66.628 1.559 0.87 304965. 0.2623
|
|
119.06 0.5821 0.7894 0.0502 0.0370 5.467 21.534 13.592 4076.417 2.433 60.459 1.512 0.87 305834. 0.2423
|
|
125.02 0.6112 0.8023 0.0449 0.0342 5.056 19.915 12.168 3769.955 2.250 54.122 1.464 0.87 306738. 0.2220
|
|
130.97 0.6403 0.8110 0.0395 0.0312 4.612 18.169 10.711 3439.305 2.053 47.643 1.413 0.87 307676. 0.2009
|
|
136.92 0.6694 0.8103 0.0340 0.0281 4.156 16.372 9.224 3099.154 1.850 41.028 1.350 0.88 308649. 0.1782
|
|
142.87 0.6985 0.7991 0.0285 0.0249 3.677 14.486 7.713 2742.216 1.637 34.307 1.276 0.88 309656. 0.1540
|
|
148.83 0.7276 0.7725 0.0228 0.0215 3.176 12.513 6.183 2368.677 1.414 27.504 1.184 0.88 310697. 0.1280
|
|
154.78 0.7567 0.7206 0.0171 0.0180 2.658 10.471 4.641 1982.163 1.183 20.642 1.062 0.88 311771. 0.0994
|
|
160.73 0.7858 0.6223 0.0114 0.0144 2.129 8.387 3.092 1587.727 0.948 13.751 0.883 0.88 312880. 0.0675
|
|
166.69 0.8149 0.4298 0.0057 0.0108 1.597 6.291 1.544 1190.883 0.711 6.869 0.588 0.89 314020. 0.0318
|
|
172.64 0.8440 0.0010 0.0000 0.0072 1.065 4.196 0.002 794.277 0.474 0.010 0.001 0.89 315165. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 17000
|
|
|
|
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 0.1021 0.0515 9.127 33.840 31.230 6806.288 3.823 138.910 2.081 0.91 313665. 0.5055
|
|
6.35 0.0292 0.0567 0.1017 0.0524 9.284 34.420 31.106 6922.910 3.889 138.361 2.038 0.91 313891. 0.4940
|
|
12.69 0.0584 0.1110 0.1012 0.0533 9.442 35.007 30.959 7040.874 3.955 137.707 1.994 0.91 314145. 0.4823
|
|
19.04 0.0876 0.1628 0.1006 0.0541 9.598 35.584 30.783 7156.995 4.020 136.921 1.951 0.91 314429. 0.4704
|
|
25.38 0.1168 0.2123 0.0999 0.0550 9.746 36.134 30.568 7267.563 4.082 135.968 1.908 0.91 314745. 0.4585
|
|
31.73 0.1460 0.2595 0.0991 0.0557 9.881 36.634 30.307 7368.289 4.139 134.808 1.866 0.91 315095. 0.4464
|
|
38.07 0.1752 0.3046 0.0980 0.0564 9.997 37.063 29.990 7454.485 4.187 133.397 1.825 0.91 315481. 0.4343
|
|
44.42 0.2044 0.3477 0.0968 0.0569 10.086 37.395 29.607 7521.162 4.225 131.691 1.785 0.91 315904. 0.4223
|
|
50.76 0.2336 0.3890 0.0953 0.0572 10.142 37.604 29.146 7563.226 4.248 129.640 1.748 0.91 316365. 0.4101
|
|
57.11 0.2628 0.4286 0.0935 0.0573 10.159 37.665 28.596 7575.663 4.255 127.196 1.712 0.91 316866. 0.3979
|
|
63.45 0.2920 0.4668 0.0914 0.0571 10.130 37.557 27.949 7553.867 4.243 124.316 1.678 0.91 317407. 0.3856
|
|
69.80 0.3212 0.5036 0.0889 0.0567 10.050 37.260 27.194 7494.109 4.210 120.960 1.646 0.92 317988. 0.3731
|
|
76.14 0.3504 0.5391 0.0861 0.0559 9.915 36.760 26.326 7393.597 4.153 117.098 1.615 0.92 318610. 0.3602
|
|
82.49 0.3796 0.5732 0.0828 0.0549 9.724 36.051 25.340 7251.009 4.073 112.713 1.585 0.92 319271. 0.3468
|
|
88.84 0.4088 0.6059 0.0792 0.0535 9.476 35.134 24.238 7066.572 3.969 107.811 1.556 0.92 319973. 0.3329
|
|
95.18 0.4380 0.6370 0.0753 0.0518 9.175 34.017 23.026 6841.787 3.843 102.422 1.527 0.92 320714. 0.3184
|
|
101.53 0.4672 0.6663 0.0710 0.0498 8.823 32.713 21.716 6579.490 3.696 96.594 1.497 0.92 321494. 0.3032
|
|
107.87 0.4963 0.6937 0.0664 0.0475 8.425 31.237 20.320 6282.721 3.529 90.384 1.467 0.92 322312. 0.2874
|
|
114.22 0.5255 0.7190 0.0616 0.0450 7.984 29.602 18.849 5953.860 3.344 83.841 1.436 0.92 323168. 0.2710
|
|
120.56 0.5547 0.7419 0.0566 0.0423 7.503 27.816 17.313 5594.680 3.143 77.010 1.404 0.92 324062. 0.2538
|
|
126.91 0.5839 0.7620 0.0514 0.0394 6.982 25.887 15.722 5206.722 2.925 69.932 1.370 0.93 324993. 0.2360
|
|
133.25 0.6131 0.7788 0.0460 0.0362 6.425 23.821 14.083 4791.114 2.691 62.642 1.333 0.93 325961. 0.2175
|
|
139.60 0.6423 0.7918 0.0405 0.0329 5.831 21.619 12.404 4348.330 2.443 55.172 1.294 0.93 326966. 0.1981
|
|
145.94 0.6715 0.7927 0.0349 0.0296 5.245 19.445 10.684 3910.888 2.197 47.520 1.239 0.93 328007. 0.1760
|
|
152.29 0.7007 0.7716 0.0292 0.0265 4.697 17.413 8.924 3502.206 1.967 39.695 1.156 0.93 329085. 0.1501
|
|
158.63 0.7299 0.7303 0.0233 0.0233 4.137 15.337 7.142 3084.720 1.733 31.766 1.050 0.93 330198. 0.1220
|
|
164.98 0.7591 0.6580 0.0175 0.0202 3.573 13.247 5.344 2664.414 1.497 23.772 0.910 0.94 331348. 0.0914
|
|
171.32 0.7883 0.5369 0.0116 0.0170 3.014 11.176 3.543 2247.768 1.263 15.758 0.715 0.94 332533. 0.0585
|
|
177.67 0.8175 0.3359 0.0057 0.0139 2.469 9.156 1.751 1841.487 1.034 7.787 0.431 0.94 333753. 0.0248
|
|
184.02 0.8467 -0.0056 -0.0001 0.0109 1.939 7.189 -0.022 1445.839 0.812 -0.099 -0.007 0.94 334988. 0.0000
|
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