464 lines
82 KiB
Plaintext
464 lines
82 KiB
Plaintext
20x12 (20x12.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 0.0838 0.0337 0.009 0.547 0.427 6.468 0.062 1.900 29.961 0.08 31277. 0.5746
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0.51 0.0271 0.0654 0.0829 0.0344 0.009 0.558 0.423 6.601 0.063 1.881 29.058 0.08 31297. 0.5544
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1.03 0.0542 0.1267 0.0820 0.0351 0.009 0.569 0.418 6.732 0.064 1.859 28.158 0.08 31320. 0.5340
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1.54 0.0813 0.1840 0.0809 0.0357 0.009 0.580 0.412 6.859 0.065 1.834 27.264 0.08 31346. 0.5136
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2.05 0.1084 0.2374 0.0796 0.0363 0.009 0.590 0.406 6.979 0.067 1.806 26.381 0.08 31373. 0.4931
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2.57 0.1355 0.2870 0.0782 0.0369 0.010 0.599 0.399 7.090 0.068 1.774 25.511 0.08 31404. 0.4727
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3.08 0.1626 0.3329 0.0766 0.0374 0.010 0.608 0.391 7.188 0.069 1.738 24.659 0.08 31437. 0.4522
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3.59 0.1897 0.3752 0.0749 0.0379 0.010 0.614 0.382 7.270 0.069 1.699 23.824 0.08 31473. 0.4319
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4.11 0.2168 0.4141 0.0729 0.0382 0.010 0.620 0.372 7.333 0.070 1.655 23.009 0.08 31512. 0.4117
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4.62 0.2439 0.4498 0.0708 0.0384 0.010 0.623 0.361 7.372 0.070 1.606 22.213 0.08 31555. 0.3916
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5.13 0.2710 0.4823 0.0685 0.0385 0.010 0.624 0.349 7.386 0.071 1.553 21.436 0.08 31600. 0.3716
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5.64 0.2981 0.5117 0.0659 0.0384 0.010 0.623 0.336 7.371 0.070 1.495 20.678 0.08 31648. 0.3517
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6.16 0.3251 0.5382 0.0632 0.0382 0.010 0.619 0.322 7.328 0.070 1.433 19.936 0.08 31700. 0.3319
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6.67 0.3522 0.5618 0.0602 0.0378 0.010 0.613 0.307 7.253 0.069 1.366 19.208 0.08 31755. 0.3123
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7.18 0.3793 0.5824 0.0572 0.0372 0.010 0.604 0.291 7.149 0.068 1.296 18.490 0.08 31813. 0.2929
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7.70 0.4064 0.6000 0.0539 0.0365 0.009 0.593 0.275 7.014 0.067 1.223 17.779 0.08 31875. 0.2735
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8.21 0.4335 0.6145 0.0505 0.0357 0.009 0.579 0.258 6.848 0.065 1.146 17.070 0.08 31939. 0.2543
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8.72 0.4606 0.6256 0.0471 0.0346 0.009 0.562 0.240 6.653 0.064 1.067 16.358 0.08 32007. 0.2351
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9.24 0.4877 0.6332 0.0435 0.0335 0.009 0.543 0.222 6.428 0.061 0.986 15.637 0.08 32078. 0.2160
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9.75 0.5148 0.6369 0.0398 0.0321 0.008 0.522 0.203 6.173 0.059 0.902 14.900 0.08 32153. 0.1968
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10.26 0.5419 0.6361 0.0360 0.0307 0.008 0.498 0.184 5.888 0.056 0.816 14.136 0.08 32230. 0.1777
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10.78 0.5690 0.6300 0.0321 0.0290 0.007 0.471 0.164 5.574 0.053 0.729 13.335 0.08 32311. 0.1584
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11.29 0.5961 0.6176 0.0282 0.0272 0.007 0.442 0.144 5.230 0.050 0.640 12.479 0.08 32396. 0.1389
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11.80 0.6232 0.5974 0.0242 0.0253 0.007 0.411 0.124 4.858 0.046 0.550 11.544 0.08 32483. 0.1191
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12.32 0.6503 0.5669 0.0202 0.0232 0.006 0.377 0.103 4.457 0.043 0.459 10.499 0.08 32574. 0.0989
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12.83 0.6774 0.5226 0.0162 0.0210 0.005 0.341 0.083 4.029 0.038 0.367 9.293 0.08 32668. 0.0783
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13.34 0.7045 0.4588 0.0121 0.0186 0.005 0.302 0.062 3.574 0.034 0.275 7.844 0.08 32765. 0.0572
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13.86 0.7316 0.3656 0.0081 0.0161 0.004 0.261 0.041 3.093 0.030 0.183 6.019 0.08 32866. 0.0358
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14.37 0.7587 0.2246 0.0040 0.0135 0.003 0.219 0.020 2.589 0.025 0.091 3.565 0.08 32969. 0.0149
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14.88 0.7858 -0.0035 0.0000 0.0107 0.003 0.174 0.000 2.063 0.020 -0.001 -0.054 0.08 33075. 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 0.0842 0.0302 0.062 1.961 1.717 46.409 0.222 7.636 16.777 0.16 62553. 0.6449
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1.03 0.0272 0.0733 0.0833 0.0309 0.064 2.009 1.699 47.531 0.227 7.559 16.216 0.16 62594. 0.6202
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2.06 0.0545 0.1416 0.0824 0.0317 0.065 2.056 1.680 48.647 0.232 7.471 15.661 0.16 62640. 0.5955
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3.09 0.0817 0.2050 0.0813 0.0324 0.067 2.102 1.657 49.737 0.237 7.372 15.115 0.16 62691. 0.5709
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4.13 0.1089 0.2637 0.0800 0.0331 0.068 2.146 1.632 50.777 0.242 7.260 14.579 0.16 62747. 0.5465
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5.16 0.1361 0.3178 0.0786 0.0337 0.069 2.187 1.604 51.744 0.247 7.133 14.057 0.16 62808. 0.5223
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6.19 0.1634 0.3676 0.0771 0.0342 0.071 2.223 1.572 52.611 0.251 6.991 13.550 0.16 62875. 0.4984
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7.22 0.1906 0.4133 0.0753 0.0347 0.072 2.255 1.536 53.350 0.255 6.832 13.059 0.16 62948. 0.4748
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8.25 0.2178 0.4552 0.0734 0.0351 0.072 2.279 1.496 53.932 0.258 6.655 12.583 0.16 63027. 0.4516
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9.28 0.2451 0.4934 0.0712 0.0354 0.073 2.296 1.452 54.331 0.259 6.460 12.124 0.16 63113. 0.4287
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10.31 0.2723 0.5282 0.0688 0.0355 0.073 2.304 1.404 54.519 0.260 6.246 11.682 0.16 63204. 0.4061
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11.35 0.2995 0.5598 0.0663 0.0355 0.073 2.302 1.352 54.478 0.260 6.013 11.255 0.16 63302. 0.3839
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12.38 0.3268 0.5883 0.0635 0.0353 0.073 2.290 1.295 54.192 0.259 5.762 10.842 0.16 63406. 0.3620
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13.41 0.3540 0.6138 0.0606 0.0349 0.072 2.268 1.235 53.657 0.256 5.495 10.442 0.16 63517. 0.3405
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14.44 0.3812 0.6364 0.0575 0.0344 0.071 2.234 1.172 52.867 0.252 5.212 10.053 0.16 63634. 0.3193
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15.47 0.4084 0.6561 0.0542 0.0337 0.069 2.190 1.105 51.822 0.247 4.916 9.674 0.16 63758. 0.2984
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16.50 0.4357 0.6729 0.0508 0.0329 0.068 2.135 1.036 50.522 0.241 4.608 9.300 0.16 63889. 0.2777
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17.53 0.4629 0.6865 0.0473 0.0319 0.066 2.069 0.964 48.966 0.234 4.289 8.931 0.16 64026. 0.2573
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18.57 0.4901 0.6970 0.0436 0.0307 0.063 1.993 0.890 47.155 0.225 3.960 8.563 0.16 64169. 0.2370
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19.60 0.5174 0.7038 0.0399 0.0294 0.060 1.906 0.814 45.090 0.215 3.622 8.192 0.16 64320. 0.2169
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20.63 0.5446 0.7066 0.0361 0.0278 0.057 1.808 0.737 42.770 0.204 3.277 7.814 0.16 64476. 0.1968
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21.66 0.5718 0.7048 0.0322 0.0262 0.054 1.699 0.658 40.197 0.192 2.926 7.422 0.16 64640. 0.1766
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22.69 0.5991 0.6971 0.0283 0.0243 0.050 1.579 0.577 37.371 0.178 2.568 7.008 0.16 64810. 0.1562
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23.72 0.6263 0.6822 0.0243 0.0223 0.046 1.449 0.496 34.297 0.164 2.206 6.559 0.16 64987. 0.1355
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24.75 0.6535 0.6574 0.0203 0.0202 0.042 1.309 0.414 30.977 0.148 1.840 6.058 0.16 65170. 0.1143
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25.79 0.6807 0.6188 0.0162 0.0178 0.037 1.159 0.331 27.420 0.131 1.472 5.474 0.16 65360. 0.0924
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26.82 0.7080 0.5591 0.0121 0.0154 0.032 0.999 0.248 23.633 0.113 1.102 4.756 0.16 65556. 0.0694
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27.85 0.7352 0.4645 0.0081 0.0128 0.026 0.830 0.165 19.629 0.094 0.732 3.804 0.16 65759. 0.0453
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28.88 0.7624 0.3047 0.0040 0.0100 0.021 0.652 0.082 15.423 0.074 0.364 2.407 0.16 65968. 0.0202
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29.91 0.7897 -0.0037 0.0000 0.0072 0.015 0.465 -0.001 11.011 0.053 -0.003 -0.028 0.16 66178. 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 0.0845 0.0289 0.201 4.215 3.878 149.622 0.476 17.251 11.757 0.24 93828. 0.6793
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1.55 0.0273 0.0771 0.0837 0.0296 0.206 4.325 3.840 153.522 0.489 17.082 11.346 0.24 93890. 0.6523
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3.10 0.0546 0.1487 0.0827 0.0304 0.211 4.435 3.797 157.410 0.501 16.888 10.940 0.24 93959. 0.6254
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4.65 0.0818 0.2149 0.0817 0.0311 0.216 4.542 3.747 161.216 0.513 16.668 10.542 0.24 94035. 0.5987
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6.20 0.1091 0.2760 0.0804 0.0318 0.221 4.645 3.691 164.865 0.525 16.418 10.155 0.24 94119. 0.5724
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7.75 0.1364 0.3322 0.0790 0.0325 0.226 4.741 3.627 168.270 0.536 16.135 9.778 0.24 94212. 0.5464
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9.30 0.1637 0.3837 0.0775 0.0330 0.230 4.827 3.556 171.340 0.545 15.817 9.413 0.24 94312. 0.5208
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10.85 0.1909 0.4309 0.0757 0.0336 0.233 4.902 3.476 173.977 0.554 15.460 9.061 0.24 94422. 0.4956
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12.40 0.2182 0.4741 0.0738 0.0340 0.236 4.961 3.386 176.085 0.560 15.063 8.723 0.24 94541. 0.4709
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13.95 0.2455 0.5135 0.0716 0.0342 0.238 5.003 3.288 177.565 0.565 14.623 8.398 0.24 94669. 0.4467
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15.50 0.2728 0.5493 0.0693 0.0344 0.239 5.024 3.179 178.329 0.568 14.140 8.086 0.24 94807. 0.4230
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17.05 0.3000 0.5819 0.0667 0.0344 0.239 5.024 3.061 178.303 0.568 13.614 7.786 0.24 94954. 0.3996
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18.60 0.3273 0.6113 0.0639 0.0342 0.238 4.999 2.933 177.440 0.565 13.048 7.498 0.24 95111. 0.3768
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20.15 0.3546 0.6378 0.0610 0.0339 0.236 4.951 2.798 175.713 0.559 12.444 7.221 0.24 95278. 0.3544
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21.70 0.3819 0.6614 0.0578 0.0334 0.232 4.877 2.654 173.109 0.551 11.805 6.954 0.24 95455. 0.3324
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23.25 0.4091 0.6822 0.0546 0.0327 0.227 4.779 2.503 169.621 0.540 11.135 6.694 0.24 95641. 0.3107
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24.80 0.4364 0.7002 0.0511 0.0319 0.222 4.656 2.347 165.246 0.526 10.438 6.441 0.24 95838. 0.2895
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26.35 0.4637 0.7152 0.0476 0.0309 0.215 4.507 2.184 159.985 0.509 9.715 6.192 0.24 96044. 0.2685
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27.90 0.4910 0.7272 0.0439 0.0297 0.206 4.334 2.017 153.836 0.490 8.971 5.946 0.24 96260. 0.2478
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29.45 0.5182 0.7359 0.0402 0.0283 0.197 4.136 1.845 146.799 0.467 8.207 5.701 0.24 96486. 0.2272
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31.00 0.5455 0.7409 0.0364 0.0268 0.186 3.913 1.669 138.874 0.442 7.426 5.452 0.24 96722. 0.2067
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32.55 0.5728 0.7416 0.0325 0.0251 0.174 3.664 1.490 130.065 0.414 6.630 5.198 0.24 96968. 0.1862
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34.09 0.6001 0.7370 0.0285 0.0232 0.161 3.392 1.309 120.377 0.383 5.821 4.931 0.24 97224. 0.1655
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35.64 0.6273 0.7257 0.0245 0.0212 0.147 3.094 1.124 109.818 0.350 5.001 4.644 0.24 97490. 0.1445
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37.19 0.6546 0.7052 0.0204 0.0190 0.132 2.772 0.938 98.403 0.313 4.174 4.325 0.24 97766. 0.1229
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38.74 0.6819 0.6715 0.0164 0.0166 0.116 2.427 0.751 86.156 0.274 3.340 3.953 0.24 98052. 0.1005
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40.29 0.7092 0.6169 0.0123 0.0141 0.098 2.060 0.563 73.108 0.233 2.504 3.492 0.24 98347. 0.0769
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41.84 0.7365 0.5260 0.0082 0.0114 0.080 1.671 0.375 59.303 0.189 1.667 2.867 0.24 98652. 0.0515
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43.39 0.7637 0.3616 0.0041 0.0086 0.060 1.262 0.188 44.796 0.143 0.835 1.901 0.24 98967. 0.0242
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44.94 0.7910 0.0031 0.0000 0.0057 0.040 0.832 0.001 29.540 0.094 0.005 0.016 0.25 99281. 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 0.0849 0.0282 0.465 7.322 6.929 346.509 0.827 30.821 9.070 0.32 125100. 0.7005
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2.08 0.0275 0.0798 0.0841 0.0290 0.477 7.523 6.863 356.031 0.850 30.524 8.743 0.32 125183. 0.6719
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4.16 0.0549 0.1536 0.0832 0.0297 0.490 7.724 6.786 365.544 0.873 30.185 8.420 0.32 125276. 0.6435
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6.24 0.0824 0.2218 0.0821 0.0305 0.503 7.921 6.699 374.872 0.895 29.797 8.105 0.32 125379. 0.6155
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8.32 0.1099 0.2846 0.0809 0.0312 0.515 8.111 6.600 383.830 0.916 29.355 7.799 0.32 125492. 0.5878
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10.40 0.1373 0.3422 0.0795 0.0319 0.526 8.288 6.487 392.206 0.936 28.853 7.502 0.32 125616. 0.5605
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12.49 0.1648 0.3949 0.0779 0.0325 0.536 8.447 6.359 399.771 0.954 28.286 7.215 0.32 125752. 0.5338
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14.57 0.1923 0.4432 0.0762 0.0331 0.545 8.585 6.216 406.286 0.970 27.649 6.940 0.32 125901. 0.5076
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16.65 0.2198 0.4872 0.0742 0.0335 0.552 8.695 6.056 411.507 0.982 26.938 6.675 0.32 126061. 0.4819
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18.73 0.2472 0.5273 0.0721 0.0338 0.557 8.773 5.879 415.195 0.991 26.148 6.422 0.32 126234. 0.4568
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20.81 0.2747 0.5638 0.0697 0.0339 0.559 8.814 5.683 417.125 0.996 25.280 6.180 0.32 126420. 0.4322
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22.89 0.3022 0.5969 0.0671 0.0339 0.559 8.814 5.470 417.120 0.996 24.332 5.948 0.32 126619. 0.4082
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24.97 0.3296 0.6270 0.0642 0.0338 0.557 8.770 5.241 415.061 0.991 23.310 5.727 0.32 126831. 0.3846
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27.05 0.3571 0.6540 0.0612 0.0334 0.551 8.682 4.995 410.883 0.981 22.219 5.514 0.32 127057. 0.3616
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29.13 0.3846 0.6782 0.0581 0.0329 0.543 8.548 4.736 404.552 0.966 21.066 5.310 0.32 127295. 0.3390
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31.21 0.4120 0.6996 0.0547 0.0322 0.531 8.369 4.464 396.053 0.946 19.855 5.112 0.32 127547. 0.3169
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33.30 0.4395 0.7182 0.0512 0.0314 0.517 8.143 4.180 385.378 0.920 18.595 4.920 0.32 127813. 0.2951
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35.38 0.4670 0.7340 0.0476 0.0303 0.500 7.872 3.887 372.524 0.889 17.289 4.733 0.32 128091. 0.2737
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37.46 0.4944 0.7468 0.0439 0.0291 0.479 7.554 3.584 357.488 0.853 15.944 4.548 0.32 128383. 0.2526
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39.54 0.5219 0.7565 0.0401 0.0277 0.456 7.190 3.274 340.269 0.812 14.563 4.364 0.32 128689. 0.2317
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41.62 0.5494 0.7626 0.0362 0.0261 0.430 6.780 2.957 320.869 0.766 13.152 4.180 0.32 129008. 0.2108
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43.70 0.5769 0.7646 0.0323 0.0244 0.401 6.324 2.633 299.294 0.715 11.713 3.991 0.32 129340. 0.1900
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45.78 0.6043 0.7614 0.0283 0.0224 0.370 5.823 2.305 275.559 0.658 10.252 3.794 0.32 129686. 0.1690
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47.86 0.6318 0.7517 0.0242 0.0203 0.335 5.276 1.972 249.685 0.596 8.772 3.582 0.32 130045. 0.1476
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49.94 0.6593 0.7329 0.0201 0.0180 0.297 4.685 1.636 221.713 0.529 7.277 3.347 0.32 130418. 0.1256
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52.02 0.6867 0.7004 0.0159 0.0156 0.257 4.051 1.298 191.702 0.458 5.773 3.071 0.32 130804. 0.1026
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54.11 0.7142 0.6458 0.0118 0.0130 0.214 3.375 0.959 159.735 0.381 4.265 2.722 0.33 131203. 0.0782
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56.19 0.7417 0.5500 0.0076 0.0102 0.169 2.661 0.620 125.928 0.301 2.758 2.233 0.33 131616. 0.0516
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58.27 0.7691 0.3626 0.0035 0.0074 0.121 1.911 0.283 90.415 0.216 1.258 1.419 0.33 132040. 0.0221
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60.35 0.7966
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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 0.0854 0.0279 0.897 11.312 10.892 669.167 1.278 48.446 7.383 0.40 156370. 0.7148
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2.59 0.0274 0.0808 0.0847 0.0287 0.923 11.632 10.791 688.113 1.314 48.001 7.113 0.40 156473. 0.6856
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5.18 0.0547 0.1556 0.0838 0.0295 0.948 11.953 10.676 707.079 1.350 47.488 6.848 0.40 156588. 0.6565
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7.77 0.0821 0.2245 0.0827 0.0302 0.973 12.268 10.544 725.724 1.386 46.900 6.590 0.40 156716. 0.6278
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|
10.36 0.1094 0.2880 0.0815 0.0310 0.997 12.572 10.393 743.679 1.420 46.228 6.339 0.40 156857. 0.5995
|
|
12.95 0.1368 0.3461 0.0802 0.0317 1.020 12.856 10.221 760.528 1.453 45.462 6.096 0.40 157011. 0.5717
|
|
15.54 0.1641 0.3994 0.0787 0.0323 1.040 13.115 10.026 775.816 1.482 44.595 5.861 0.40 157181. 0.5445
|
|
18.13 0.1915 0.4481 0.0769 0.0329 1.058 13.339 9.806 789.071 1.507 43.616 5.637 0.40 157365. 0.5178
|
|
20.72 0.2189 0.4925 0.0750 0.0333 1.073 13.520 9.559 799.806 1.528 42.520 5.421 0.40 157564. 0.4917
|
|
23.32 0.2462 0.5331 0.0728 0.0336 1.083 13.651 9.285 807.543 1.542 41.301 5.215 0.40 157779. 0.4662
|
|
25.91 0.2736 0.5700 0.0705 0.0338 1.089 13.724 8.983 811.837 1.550 39.956 5.019 0.40 158011. 0.4413
|
|
28.50 0.3009 0.6036 0.0679 0.0338 1.089 13.732 8.652 812.323 1.551 38.486 4.831 0.40 158258. 0.4169
|
|
31.09 0.3283 0.6340 0.0651 0.0337 1.085 13.672 8.295 808.758 1.545 36.897 4.652 0.40 158522. 0.3931
|
|
33.68 0.3556 0.6616 0.0621 0.0334 1.074 13.541 7.913 801.003 1.530 35.198 4.481 0.40 158802. 0.3698
|
|
36.27 0.3830 0.6863 0.0589 0.0329 1.058 13.337 7.509 788.989 1.507 33.398 4.316 0.40 159098. 0.3470
|
|
38.86 0.4104 0.7084 0.0556 0.0322 1.036 13.062 7.084 772.682 1.476 31.508 4.158 0.40 159412. 0.3247
|
|
41.45 0.4377 0.7277 0.0521 0.0313 1.009 12.713 6.640 752.069 1.436 29.537 4.005 0.40 159741. 0.3028
|
|
44.04 0.4651 0.7444 0.0485 0.0303 0.975 12.292 6.181 727.142 1.389 27.494 3.856 0.40 160087. 0.2812
|
|
46.63 0.4924 0.7583 0.0448 0.0291 0.936 11.798 5.708 697.897 1.333 25.387 3.709 0.40 160450. 0.2600
|
|
49.22 0.5198 0.7692 0.0410 0.0277 0.891 11.230 5.221 664.332 1.269 23.224 3.565 0.40 160829. 0.2390
|
|
51.81 0.5471 0.7768 0.0371 0.0261 0.840 10.590 4.724 626.450 1.196 21.011 3.420 0.40 161225. 0.2181
|
|
54.40 0.5745 0.7807 0.0331 0.0243 0.784 9.877 4.216 584.262 1.116 18.755 3.273 0.40 161638. 0.1972
|
|
56.99 0.6018 0.7799 0.0290 0.0224 0.721 9.091 3.701 537.793 1.027 16.462 3.121 0.40 162067. 0.1762
|
|
59.58 0.6292 0.7732 0.0249 0.0203 0.653 8.234 3.179 487.087 0.930 14.138 2.960 0.40 162513. 0.1548
|
|
62.17 0.6566 0.7582 0.0208 0.0180 0.580 7.306 2.651 432.217 0.825 11.791 2.782 0.41 162976. 0.1329
|
|
64.76 0.6839 0.7312 0.0166 0.0156 0.501 6.310 2.119 373.293 0.713 9.427 2.575 0.41 163455. 0.1100
|
|
67.36 0.7113 0.6842 0.0124 0.0129 0.416 5.248 1.586 310.476 0.593 7.055 2.317 0.41 163950. 0.0856
|
|
69.95 0.7386 0.6003 0.0083 0.0102 0.327 4.124 1.053 243.986 0.466 4.684 1.958 0.41 164462. 0.0589
|
|
72.54 0.7660 0.4329 0.0041 0.0073 0.233 2.943 0.522 174.090 0.332 2.324 1.361 0.41 164988. 0.0289
|
|
75.13 0.7933 -0.0147 -0.0001 0.0042 0.134 1.692 -0.010 100.119 0.191 -0.044 -0.045 0.41 165503. 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 0.0861 0.0278 1.545 16.233 15.796 1152.334 1.834 70.260 6.217 0.48 187635. 0.7250
|
|
3.13 0.0275 0.0822 0.0853 0.0286 1.591 16.709 15.657 1186.129 1.888 69.642 5.987 0.48 187760. 0.6950
|
|
6.26 0.0551 0.1581 0.0844 0.0294 1.636 17.187 15.496 1220.038 1.942 68.928 5.761 0.48 187899. 0.6653
|
|
9.39 0.0826 0.2281 0.0834 0.0302 1.681 17.657 15.311 1253.440 1.995 68.103 5.540 0.48 188053. 0.6360
|
|
12.52 0.1102 0.2923 0.0822 0.0310 1.724 18.111 15.097 1285.667 2.046 67.153 5.326 0.48 188224. 0.6072
|
|
15.65 0.1377 0.3512 0.0809 0.0317 1.765 18.538 14.853 1315.959 2.094 66.065 5.119 0.48 188412. 0.5788
|
|
18.78 0.1653 0.4051 0.0794 0.0324 1.802 18.926 14.574 1343.489 2.138 64.824 4.920 0.48 188617. 0.5511
|
|
21.91 0.1928 0.4543 0.0777 0.0330 1.834 19.262 14.257 1367.384 2.176 63.417 4.729 0.48 188840. 0.5239
|
|
25.04 0.2204 0.4991 0.0757 0.0334 1.860 19.535 13.902 1386.757 2.207 61.834 4.547 0.48 189083. 0.4974
|
|
28.17 0.2479 0.5400 0.0736 0.0338 1.878 19.732 13.504 1400.736 2.229 60.066 4.373 0.48 189344. 0.4714
|
|
31.30 0.2754 0.5773 0.0712 0.0340 1.889 19.842 13.064 1408.509 2.242 58.109 4.207 0.48 189625. 0.4461
|
|
34.43 0.3030 0.6112 0.0685 0.0340 1.890 19.855 12.582 1409.414 2.243 55.963 4.049 0.48 189926. 0.4214
|
|
37.56 0.3305 0.6420 0.0657 0.0338 1.881 19.764 12.059 1403.018 2.233 53.639 3.898 0.48 190247. 0.3972
|
|
40.69 0.3581 0.6698 0.0626 0.0335 1.863 19.568 11.499 1389.076 2.211 51.149 3.755 0.48 190588. 0.3736
|
|
43.82 0.3856 0.6949 0.0594 0.0330 1.834 19.264 10.906 1367.468 2.176 48.509 3.617 0.48 190948. 0.3505
|
|
46.95 0.4132 0.7173 0.0560 0.0323 1.794 18.851 10.282 1338.143 2.130 45.734 3.485 0.48 191329. 0.3279
|
|
50.08 0.4407 0.7371 0.0525 0.0314 1.745 18.328 9.631 1301.084 2.071 42.838 3.357 0.48 191730. 0.3057
|
|
53.21 0.4683 0.7543 0.0488 0.0303 1.685 17.697 8.956 1256.282 1.999 39.835 3.233 0.48 192151. 0.2839
|
|
56.34 0.4958 0.7687 0.0450 0.0290 1.614 16.957 8.259 1203.736 1.916 36.736 3.112 0.48 192592. 0.2624
|
|
59.47 0.5234 0.7802 0.0411 0.0276 1.533 16.108 7.544 1143.447 1.820 33.554 2.992 0.48 193054. 0.2411
|
|
62.60 0.5509 0.7885 0.0371 0.0259 1.442 15.150 6.812 1075.422 1.712 30.298 2.873 0.48 193535. 0.2200
|
|
65.73 0.5784 0.7930 0.0330 0.0241 1.341 14.083 6.065 999.686 1.591 26.979 2.752 0.48 194037. 0.1988
|
|
68.86 0.6060 0.7930 0.0289 0.0221 1.229 12.908 5.307 916.286 1.458 23.604 2.627 0.48 194559. 0.1775
|
|
71.99 0.6335 0.7871 0.0247 0.0199 1.107 11.626 4.538 825.309 1.314 20.185 2.494 0.49 195101. 0.1559
|
|
75.12 0.6611 0.7730 0.0205 0.0175 0.975 10.240 3.761 726.895 1.157 16.731 2.347 0.49 195663. 0.1335
|
|
78.25 0.6886 0.7463 0.0162 0.0150 0.833 8.752 2.980 621.255 0.989 13.253 2.175 0.49 196246. 0.1102
|
|
81.38 0.7162 0.6983 0.0120 0.0123 0.682 7.166 2.195 508.694 0.810 9.764 1.957 0.49 196848. 0.0851
|
|
84.51 0.7437 0.6088 0.0077 0.0094 0.522 5.489 1.412 389.627 0.620 6.279 1.643 0.49 197470. 0.0573
|
|
87.64 0.7713 0.4164 0.0034 0.0064 0.355 3.727 0.632 264.536 0.421 2.812 1.084 0.49 198109. 0.0253
|
|
90.77 0.7988
|
|
|
|
|
|
|
|
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 0.0868 0.0279 2.460 22.150 21.678 1834.435 2.503 96.422 5.360 0.56 218895. 0.7321
|
|
3.63 0.0274 0.0821 0.0861 0.0287 2.534 22.813 21.502 1889.310 2.577 95.639 5.162 0.56 219039. 0.7022
|
|
7.26 0.0547 0.1581 0.0852 0.0295 2.608 23.479 21.296 1944.529 2.653 94.726 4.967 0.56 219201. 0.6725
|
|
10.89 0.0821 0.2280 0.0843 0.0304 2.681 24.139 21.058 1999.112 2.727 93.665 4.778 0.56 219379. 0.6432
|
|
14.52 0.1095 0.2923 0.0832 0.0312 2.752 24.777 20.781 2051.973 2.799 92.436 4.594 0.56 219577. 0.6144
|
|
18.15 0.1369 0.3513 0.0819 0.0319 2.819 25.379 20.462 2101.885 2.867 91.017 4.416 0.56 219794. 0.5860
|
|
21.77 0.1642 0.4052 0.0804 0.0326 2.880 25.930 20.096 2147.505 2.930 89.389 4.245 0.56 220031. 0.5582
|
|
25.40 0.1916 0.4545 0.0788 0.0332 2.933 26.412 19.679 2187.408 2.984 87.533 4.081 0.56 220290. 0.5311
|
|
29.03 0.2190 0.4994 0.0769 0.0337 2.977 26.808 19.207 2220.153 3.029 85.434 3.924 0.56 220570. 0.5045
|
|
32.66 0.2464 0.5405 0.0748 0.0341 3.010 27.099 18.677 2244.307 3.062 83.077 3.775 0.56 220873. 0.4786
|
|
36.29 0.2737 0.5779 0.0724 0.0343 3.029 27.271 18.088 2258.537 3.081 80.456 3.633 0.56 221198. 0.4533
|
|
39.92 0.3011 0.6121 0.0698 0.0343 3.033 27.310 17.440 2261.732 3.085 77.572 3.497 0.56 221546. 0.4285
|
|
43.55 0.3285 0.6432 0.0670 0.0342 3.022 27.206 16.735 2253.148 3.074 74.436 3.369 0.56 221917. 0.4043
|
|
47.18 0.3559 0.6714 0.0639 0.0339 2.994 26.955 15.977 2232.363 3.045 71.066 3.246 0.56 222311. 0.3807
|
|
50.81 0.3832 0.6970 0.0607 0.0334 2.949 26.554 15.171 2199.182 3.000 67.483 3.129 0.56 222728. 0.3576
|
|
54.44 0.4106 0.7199 0.0573 0.0327 2.888 26.003 14.323 2153.523 2.938 63.708 3.017 0.56 223168. 0.3349
|
|
58.07 0.4380 0.7403 0.0538 0.0318 2.810 25.301 13.436 2095.374 2.858 59.761 2.908 0.56 223632. 0.3128
|
|
61.69 0.4654 0.7582 0.0501 0.0307 2.715 24.448 12.514 2024.737 2.762 55.663 2.803 0.56 224118. 0.2909
|
|
65.32 0.4927 0.7735 0.0463 0.0295 2.604 23.444 11.562 1941.620 2.649 51.430 2.701 0.56 224628. 0.2695
|
|
68.95 0.5201 0.7861 0.0424 0.0280 2.476 22.290 10.584 1846.035 2.518 47.077 2.600 0.56 225161. 0.2482
|
|
72.58 0.5475 0.7957 0.0383 0.0264 2.331 20.986 9.582 1738.000 2.371 42.619 2.501 0.56 225717. 0.2271
|
|
76.21 0.5748 0.8018 0.0343 0.0246 2.169 19.531 8.559 1617.551 2.207 38.069 2.400 0.56 226296. 0.2060
|
|
79.84 0.6022 0.8039 0.0301 0.0225 1.991 17.928 7.518 1484.766 2.025 33.441 2.297 0.57 226899. 0.1848
|
|
83.47 0.6296 0.8006 0.0259 0.0203 1.797 16.177 6.463 1339.769 1.828 28.747 2.188 0.57 227525. 0.1632
|
|
87.10 0.6570 0.7901 0.0216 0.0180 1.586 14.282 5.396 1182.769 1.614 24.002 2.069 0.57 228173. 0.1410
|
|
90.73 0.6843 0.7687 0.0173 0.0154 1.360 12.245 4.321 1014.084 1.383 19.219 1.933 0.57 228845. 0.1179
|
|
94.36 0.7117 0.7290 0.0130 0.0127 1.119 10.072 3.241 834.171 1.138 14.416 1.762 0.57 229540. 0.0931
|
|
97.99 0.7391 0.6542 0.0086 0.0098 0.863 7.772 2.161 643.667 0.878 9.613 1.523 0.57 230258. 0.0657
|
|
101.61 0.7665 0.4948 0.0043 0.0067 0.595 5.353 1.086 443.352 0.605 4.829 1.111 0.57 230996. 0.0340
|
|
105.24 0.7938 0.0044 0.0000 0.0035 0.310 2.789 0.005 231.019 0.315 0.022 0.010 0.57 231713. 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 0.0876 0.0281 3.702 29.169 28.578 2760.851 3.296 127.113 4.695 0.63 250149. 0.7363
|
|
4.15 0.0274 0.0824 0.0869 0.0289 3.815 30.060 28.367 2845.196 3.396 126.177 4.522 0.63 250314. 0.7066
|
|
8.31 0.0548 0.1585 0.0862 0.0298 3.930 30.961 28.119 2930.467 3.498 125.074 4.352 0.63 250498. 0.6771
|
|
12.46 0.0823 0.2287 0.0853 0.0307 4.043 31.856 27.828 3015.152 3.599 123.778 4.186 0.63 250703. 0.6479
|
|
16.62 0.1097 0.2932 0.0842 0.0315 4.154 32.727 27.486 3097.567 3.697 122.260 4.025 0.64 250928. 0.6191
|
|
20.77 0.1371 0.3523 0.0830 0.0323 4.259 33.553 27.088 3175.767 3.791 120.489 3.869 0.64 251177. 0.5908
|
|
24.92 0.1645 0.4063 0.0816 0.0330 4.355 34.312 26.627 3247.609 3.877 118.437 3.719 0.64 251449. 0.5630
|
|
29.08 0.1919 0.4558 0.0800 0.0337 4.440 34.980 26.096 3310.815 3.952 116.076 3.575 0.64 251745. 0.5358
|
|
33.23 0.2193 0.5009 0.0781 0.0342 4.510 35.532 25.491 3363.049 4.014 113.384 3.438 0.64 252067. 0.5092
|
|
37.39 0.2468 0.5421 0.0760 0.0346 4.562 35.943 24.807 3402.030 4.061 110.340 3.307 0.64 252415. 0.4833
|
|
41.54 0.2742 0.5797 0.0737 0.0348 4.594 36.193 24.041 3425.629 4.089 106.933 3.183 0.64 252788. 0.4579
|
|
45.70 0.3016 0.6140 0.0711 0.0349 4.602 36.261 23.193 3432.073 4.097 103.165 3.065 0.64 253188. 0.4331
|
|
49.85 0.3290 0.6454 0.0682 0.0348 4.587 36.135 22.268 3420.156 4.083 99.047 2.953 0.64 253614. 0.4088
|
|
54.00 0.3564 0.6739 0.0652 0.0345 4.545 35.808 21.269 3389.219 4.046 94.606 2.846 0.64 254067. 0.3851
|
|
58.16 0.3838 0.6998 0.0619 0.0340 4.478 35.277 20.205 3338.962 3.986 89.871 2.745 0.64 254546. 0.3619
|
|
62.31 0.4113 0.7231 0.0585 0.0333 4.384 34.541 19.080 3269.304 3.902 84.870 2.647 0.64 255052. 0.3392
|
|
66.47 0.4387 0.7440 0.0549 0.0323 4.265 33.600 17.903 3180.253 3.796 79.633 2.553 0.64 255584. 0.3170
|
|
70.62 0.4661 0.7624 0.0511 0.0312 4.119 32.455 16.678 3071.853 3.667 74.186 2.463 0.64 256142. 0.2951
|
|
74.77 0.4935 0.7783 0.0472 0.0299 3.948 31.106 15.412 2944.155 3.514 68.552 2.374 0.64 256728. 0.2735
|
|
78.93 0.5209 0.7916 0.0432 0.0285 3.751 29.553 14.109 2797.199 3.339 62.755 2.288 0.64 257340. 0.2521
|
|
83.08 0.5483 0.8020 0.0391 0.0268 3.528 27.798 12.773 2631.029 3.141 56.812 2.202 0.64 257978. 0.2309
|
|
87.24 0.5758 0.8091 0.0350 0.0249 3.280 25.840 11.408 2445.714 2.919 50.743 2.116 0.65 258643. 0.2096
|
|
91.39 0.6032 0.8123 0.0307 0.0228 3.006 23.681 10.019 2241.380 2.675 44.565 2.027 0.65 259334. 0.1883
|
|
95.54 0.6306 0.8104 0.0264 0.0205 2.706 21.323 8.610 2018.227 2.409 38.295 1.935 0.65 260052. 0.1666
|
|
99.70 0.6580 0.8016 0.0220 0.0181 2.382 18.770 7.184 1776.579 2.121 31.953 1.834 0.65 260796. 0.1442
|
|
103.85 0.6854 0.7822 0.0176 0.0154 2.034 16.027 5.746 1516.930 1.811 25.558 1.718 0.65 261567. 0.1208
|
|
108.01 0.7128 0.7450 0.0132 0.0126 1.663 13.101 4.301 1239.993 1.480 19.133 1.573 0.65 262364. 0.0957
|
|
112.16 0.7403 0.6729 0.0088 0.0096 1.270 10.003 2.856 946.759 1.130 12.705 1.368 0.65 263186. 0.0679
|
|
116.31 0.7677 0.5133 0.0043 0.0065 0.856 6.745 1.417 638.442 0.762 6.302 1.007 0.65 264033. 0.0352
|
|
120.47 0.7951 -0.0333 -0.0001 0.0031 0.414 3.261 -0.043 308.684 0.368 -0.191 -0.063 0.65 264822. 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 0.0884 0.0290 5.441 38.107 36.529 4057.616 4.305 162.483 4.083 0.71 281397. 0.7241
|
|
4.68 0.0274 0.0808 0.0879 0.0298 5.601 39.222 36.296 4176.342 4.431 161.443 3.942 0.71 281582. 0.6967
|
|
9.36 0.0549 0.1559 0.0872 0.0307 5.762 40.351 36.016 4296.591 4.559 160.201 3.802 0.71 281788. 0.6694
|
|
14.03 0.0823 0.2255 0.0864 0.0315 5.922 41.474 35.683 4416.205 4.686 158.718 3.665 0.71 282018. 0.6423
|
|
18.71 0.1098 0.2896 0.0854 0.0324 6.079 42.569 35.287 4532.792 4.809 156.956 3.531 0.71 282271. 0.6154
|
|
23.39 0.1372 0.3487 0.0843 0.0332 6.227 43.610 34.818 4643.575 4.927 154.870 3.401 0.71 282551. 0.5887
|
|
28.07 0.1646 0.4030 0.0830 0.0339 6.364 44.567 34.267 4745.513 5.035 152.418 3.275 0.71 282857. 0.5625
|
|
32.74 0.1921 0.4527 0.0814 0.0345 6.484 45.411 33.624 4835.347 5.130 149.560 3.154 0.72 283191. 0.5366
|
|
37.42 0.2195 0.4983 0.0796 0.0351 6.584 46.109 32.882 4909.742 5.209 146.261 3.038 0.72 283554. 0.5111
|
|
42.10 0.2470 0.5401 0.0776 0.0355 6.659 46.632 32.035 4965.393 5.268 142.494 2.926 0.72 283946. 0.4859
|
|
46.78 0.2744 0.5782 0.0752 0.0357 6.704 46.949 31.079 4999.148 5.304 138.239 2.820 0.72 284368. 0.4612
|
|
51.45 0.3019 0.6131 0.0727 0.0358 6.716 47.035 30.012 5008.292 5.314 133.495 2.718 0.72 284820. 0.4369
|
|
56.13 0.3293 0.6449 0.0698 0.0357 6.693 46.871 28.839 4990.888 5.295 128.278 2.621 0.72 285301. 0.4129
|
|
60.81 0.3567 0.6740 0.0667 0.0353 6.632 46.448 27.567 4945.774 5.248 122.620 2.528 0.72 285813. 0.3894
|
|
65.49 0.3842 0.7003 0.0634 0.0348 6.534 45.758 26.205 4872.361 5.170 116.560 2.439 0.72 286354. 0.3664
|
|
70.16 0.4116 0.7242 0.0600 0.0341 6.397 44.801 24.761 4770.391 5.062 110.139 2.354 0.72 286926. 0.3437
|
|
74.84 0.4391 0.7456 0.0563 0.0331 6.222 43.574 23.246 4639.775 4.923 103.396 2.272 0.72 287527. 0.3214
|
|
79.52 0.4665 0.7646 0.0525 0.0320 6.008 42.078 21.666 4480.509 4.754 96.369 2.193 0.72 288158. 0.2995
|
|
84.20 0.4939 0.7811 0.0485 0.0307 5.757 40.314 20.029 4292.651 4.555 89.088 2.116 0.72 288819. 0.2779
|
|
88.87 0.5214 0.7952 0.0444 0.0291 5.466 38.282 18.342 4076.303 4.325 81.586 2.041 0.72 289510. 0.2564
|
|
93.55 0.5488 0.8065 0.0402 0.0274 5.138 35.984 16.611 3831.572 4.065 73.886 1.966 0.72 290231. 0.2351
|
|
98.23 0.5763 0.8146 0.0359 0.0254 4.772 33.420 14.841 3558.565 3.776 66.015 1.892 0.73 290981. 0.2138
|
|
102.91 0.6037 0.8190 0.0316 0.0233 4.368 30.592 13.038 3257.476 3.456 57.994 1.815 0.73 291762. 0.1923
|
|
107.58 0.6312 0.8186 0.0271 0.0209 3.927 27.504 11.207 2928.615 3.107 49.848 1.736 0.73 292571. 0.1705
|
|
112.26 0.6586 0.8116 0.0226 0.0184 3.450 24.159 9.353 2572.464 2.729 41.600 1.649 0.73 293411. 0.1480
|
|
116.94 0.6860 0.7945 0.0181 0.0156 2.936 20.565 7.482 2189.747 2.323 33.278 1.550 0.73 294280. 0.1244
|
|
121.62 0.7135 0.7602 0.0136 0.0127 2.389 16.731 5.601 1781.547 1.890 24.911 1.426 0.73 295179. 0.0990
|
|
126.29 0.7409 0.6918 0.0090 0.0096 1.810 12.674 3.717 1349.489 1.432 16.535 1.249 0.73 296106. 0.0707
|
|
130.97 0.7684 0.5350 0.0045 0.0064 1.201 8.412 1.840 895.766 0.950 8.185 0.932 0.74 297060. 0.0371
|
|
135.65 0.7958 -0.0532 -0.0002 0.0029 0.546 3.823 -0.080 407.111 0.432 -0.357 -0.090 0.74 297909. 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 0.0893 0.0321 8.258 52.046 45.532 6157.658 5.880 202.528 3.354 0.79 312637. 0.6640
|
|
5.20 0.0275 0.0742 0.0888 0.0329 8.467 53.364 45.292 6313.556 6.029 201.459 3.254 0.79 312841. 0.6424
|
|
10.40 0.0549 0.1439 0.0883 0.0337 8.677 54.690 45.001 6470.445 6.179 200.164 3.155 0.79 313069. 0.6208
|
|
15.61 0.0824 0.2091 0.0876 0.0345 8.884 55.996 44.648 6624.946 6.326 198.592 3.057 0.79 313323. 0.5992
|
|
20.81 0.1099 0.2701 0.0867 0.0353 9.083 57.249 44.219 6773.277 6.468 196.687 2.961 0.79 313604. 0.5777
|
|
26.01 0.1373 0.3270 0.0857 0.0360 9.268 58.415 43.702 6911.164 6.600 194.387 2.868 0.79 313914. 0.5563
|
|
31.21 0.1648 0.3801 0.0845 0.0366 9.433 59.454 43.082 7034.091 6.717 191.631 2.778 0.79 314254. 0.5350
|
|
36.41 0.1923 0.4296 0.0830 0.0372 9.571 60.327 42.346 7137.430 6.816 188.356 2.691 0.79 314626. 0.5138
|
|
41.62 0.2197 0.4756 0.0814 0.0376 9.678 60.997 41.481 7216.714 6.891 184.510 2.607 0.80 315030. 0.4926
|
|
46.82 0.2472 0.5185 0.0794 0.0378 9.746 61.429 40.478 7267.761 6.940 180.048 2.526 0.80 315467. 0.4715
|
|
52.02 0.2747 0.5583 0.0771 0.0379 9.772 61.590 39.330 7286.868 6.958 174.941 2.448 0.80 315937. 0.4504
|
|
57.22 0.3021 0.5952 0.0746 0.0379 9.751 61.457 38.035 7271.045 6.943 169.180 2.373 0.80 316441. 0.4293
|
|
62.42 0.3296 0.6293 0.0718 0.0376 9.680 61.012 36.597 7218.392 6.893 162.783 2.300 0.80 316979. 0.4081
|
|
67.63 0.3571 0.6607 0.0687 0.0371 9.559 60.248 35.024 7128.050 6.807 155.788 2.229 0.80 317550. 0.3870
|
|
72.83 0.3845 0.6895 0.0654 0.0365 9.387 59.164 33.329 6999.781 6.684 148.247 2.160 0.80 318155. 0.3658
|
|
78.03 0.4120 0.7157 0.0618 0.0356 9.164 57.760 31.523 6833.687 6.526 140.214 2.092 0.80 318793. 0.3446
|
|
83.23 0.4395 0.7394 0.0581 0.0345 8.891 56.038 29.618 6629.898 6.331 131.742 2.026 0.80 319465. 0.3235
|
|
88.43 0.4669 0.7604 0.0542 0.0333 8.567 53.997 27.626 6388.497 6.101 122.881 1.961 0.80 320170. 0.3025
|
|
93.64 0.4944 0.7789 0.0501 0.0318 8.193 51.638 25.557 6109.386 5.834 113.676 1.897 0.80 320908. 0.2814
|
|
98.84 0.5219 0.7946 0.0459 0.0302 7.768 48.958 23.419 5792.306 5.531 104.168 1.834 0.80 321679. 0.2604
|
|
104.04 0.5493 0.8075 0.0416 0.0283 7.291 45.954 21.221 5436.885 5.192 94.393 1.770 0.81 322483. 0.2393
|
|
109.24 0.5768 0.8172 0.0372 0.0263 6.763 42.623 18.971 5042.805 4.816 84.384 1.706 0.81 323320. 0.2180
|
|
114.44 0.6043 0.8232 0.0327 0.0240 6.182 38.964 16.675 4609.843 4.402 74.172 1.641 0.81 324190. 0.1966
|
|
119.65 0.6317 0.8242 0.0281 0.0216 5.551 34.986 14.340 4139.230 3.953 63.786 1.571 0.81 325093. 0.1746
|
|
124.85 0.6592 0.8184 0.0235 0.0189 4.870 30.698 11.973 3631.902 3.468 53.257 1.495 0.81 326028. 0.1518
|
|
130.05 0.6867 0.8019 0.0188 0.0161 4.143 26.116 9.582 3089.782 2.951 42.619 1.407 0.81 326997. 0.1277
|
|
135.25 0.7141 0.7668 0.0141 0.0131 3.374 21.265 7.174 2515.895 2.403 31.908 1.293 0.81 327998. 0.1016
|
|
140.45 0.7416 0.6942 0.0093 0.0100 2.568 16.183 4.759 1914.661 1.828 21.168 1.127 0.82 329030. 0.0722
|
|
145.66 0.7691 0.5265 0.0046 0.0067 1.732 10.918 2.348 1291.746 1.234 10.445 0.825 0.82 330093. 0.0371
|
|
150.86 0.7965
|
|
|
|
|
|
|
|
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 0.0896 0.0383 13.126 75.207 55.281 9787.694 8.497 245.892 2.562 0.87 343892. 0.5588
|
|
5.77 0.0277 0.0631 0.0892 0.0391 13.409 76.830 55.055 9998.821 8.680 244.883 2.497 0.87 344115. 0.5437
|
|
11.53 0.0554 0.1230 0.0888 0.0400 13.693 78.460 54.776 10211.029 8.864 243.645 2.433 0.87 344365. 0.5283
|
|
17.30 0.0831 0.1797 0.0882 0.0408 13.972 80.060 54.433 10419.260 9.045 242.119 2.370 0.87 344643. 0.5129
|
|
23.07 0.1107 0.2334 0.0875 0.0415 14.237 81.577 54.009 10616.674 9.217 240.231 2.307 0.87 344952. 0.4975
|
|
28.84 0.1384 0.2841 0.0867 0.0422 14.477 82.949 53.484 10795.234 9.372 237.897 2.247 0.87 345293. 0.4821
|
|
34.60 0.1661 0.3321 0.0856 0.0428 14.679 84.108 52.838 10946.097 9.503 235.024 2.189 0.87 345668. 0.4669
|
|
40.37 0.1938 0.3778 0.0844 0.0433 14.832 84.986 52.050 11060.292 9.602 231.519 2.135 0.87 346079. 0.4518
|
|
46.14 0.2215 0.4212 0.0828 0.0435 14.925 85.518 51.100 11129.504 9.662 227.292 2.083 0.87 346527. 0.4368
|
|
51.91 0.2492 0.4627 0.0810 0.0436 14.948 85.650 49.971 11146.764 9.677 222.270 2.033 0.88 347013. 0.4217
|
|
57.67 0.2768 0.5023 0.0789 0.0435 14.895 85.344 48.650 11106.931 9.642 216.395 1.987 0.88 347536. 0.4065
|
|
63.44 0.3045 0.5402 0.0764 0.0431 14.761 84.576 47.132 11007.030 9.555 209.643 1.942 0.88 348098. 0.3912
|
|
69.21 0.3322 0.5763 0.0736 0.0424 14.546 83.344 45.420 10846.611 9.416 202.026 1.899 0.88 348699. 0.3755
|
|
74.98 0.3599 0.6106 0.0705 0.0416 14.251 81.659 43.523 10627.337 9.226 193.591 1.858 0.88 349337. 0.3595
|
|
80.74 0.3876 0.6430 0.0672 0.0405 13.882 79.544 41.458 10352.137 8.987 184.404 1.816 0.88 350014. 0.3431
|
|
86.51 0.4153 0.6734 0.0636 0.0392 13.443 77.026 39.239 10024.360 8.702 174.536 1.775 0.88 350728. 0.3263
|
|
92.28 0.4429 0.7015 0.0598 0.0377 12.937 74.127 36.884 9647.055 8.375 164.060 1.734 0.88 351480. 0.3090
|
|
98.05 0.4706 0.7274 0.0558 0.0361 12.367 70.864 34.408 9222.388 8.006 153.045 1.692 0.88 352269. 0.2912
|
|
103.81 0.4983 0.7506 0.0516 0.0342 11.737 67.250 31.824 8752.139 7.598 141.554 1.649 0.88 353095. 0.2730
|
|
109.58 0.5260 0.7710 0.0472 0.0322 11.046 63.291 29.147 8236.825 7.151 129.644 1.605 0.88 353958. 0.2542
|
|
115.35 0.5537 0.7884 0.0428 0.0300 10.294 58.983 26.386 7676.165 6.664 117.364 1.559 0.89 354857. 0.2350
|
|
121.12 0.5814 0.8023 0.0382 0.0277 9.480 54.321 23.552 7069.478 6.137 104.758 1.511 0.89 355794. 0.2151
|
|
126.88 0.6090 0.8122 0.0335 0.0251 8.604 49.301 20.654 6416.172 5.570 91.871 1.460 0.89 356767. 0.1947
|
|
132.65 0.6367 0.8162 0.0287 0.0224 7.672 43.957 17.703 5720.737 4.966 78.742 1.404 0.89 357776. 0.1733
|
|
138.42 0.6644 0.8041 0.0238 0.0197 6.747 38.658 14.697 5031.054 4.368 65.374 1.325 0.89 358822. 0.1490
|
|
144.19 0.6921 0.7748 0.0189 0.0169 5.784 33.143 11.656 4313.368 3.745 51.846 1.226 0.89 359905. 0.1228
|
|
149.95 0.7198 0.7168 0.0139 0.0140 4.792 27.456 8.590 3573.159 3.102 38.209 1.090 0.90 361023. 0.0938
|
|
155.72 0.7475 0.6056 0.0089 0.0110 3.780 21.660 5.514 2818.894 2.447 24.524 0.887 0.90 362176. 0.0611
|
|
161.49 0.7751 0.3801 0.0040 0.0081 2.765 15.843 2.441 2061.892 1.790 10.857 0.537 0.90 363361. 0.0246
|
|
167.25 0.8028
|
|
|
|
|
|
|
|
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 0.0874 0.0440 19.592 102.902 64.171 14609.407 11.626 285.434 1.992 0.95 375216. 0.4682
|
|
6.31 0.0278 0.0540 0.0871 0.0448 19.928 104.671 63.945 14860.527 11.826 284.426 1.952 0.95 375458. 0.4579
|
|
12.63 0.0556 0.1057 0.0867 0.0456 20.277 106.500 63.672 15120.268 12.032 283.214 1.910 0.95 375728. 0.4471
|
|
18.94 0.0833 0.1551 0.0863 0.0464 20.629 108.351 63.341 15382.985 12.241 281.740 1.868 0.95 376029. 0.4361
|
|
25.25 0.1111 0.2020 0.0857 0.0471 20.976 110.172 62.934 15641.559 12.447 279.929 1.825 0.95 376363. 0.4247
|
|
31.57 0.1389 0.2467 0.0850 0.0479 21.305 111.901 62.431 15887.044 12.643 277.694 1.782 0.95 376732. 0.4132
|
|
37.88 0.1667 0.2890 0.0842 0.0485 21.602 113.463 61.810 16108.832 12.819 274.933 1.740 0.95 377138. 0.4014
|
|
44.19 0.1944 0.3292 0.0831 0.0491 21.849 114.761 61.045 16293.146 12.966 271.529 1.699 0.95 377582. 0.3895
|
|
50.51 0.2222 0.3675 0.0819 0.0495 22.032 115.720 60.112 16429.297 13.074 267.380 1.660 0.95 378067. 0.3775
|
|
56.82 0.2500 0.4038 0.0803 0.0497 22.134 116.256 58.989 16505.291 13.134 262.384 1.621 0.96 378592. 0.3653
|
|
63.13 0.2778 0.4384 0.0785 0.0498 22.139 116.285 57.655 16509.416 13.138 256.450 1.584 0.96 379160. 0.3529
|
|
69.45 0.3056 0.4714 0.0764 0.0495 22.035 115.735 56.096 16431.375 13.076 249.513 1.548 0.96 379769. 0.3402
|
|
75.76 0.3333 0.5030 0.0740 0.0490 21.809 114.551 54.305 16263.228 12.942 241.548 1.515 0.96 380422. 0.3274
|
|
82.07 0.3611 0.5333 0.0712 0.0482 21.456 112.694 52.285 15999.588 12.732 232.564 1.482 0.96 381117. 0.3144
|
|
88.39 0.3889 0.5624 0.0682 0.0471 20.970 110.140 50.043 15637.046 12.444 222.591 1.452 0.96 381855. 0.3013
|
|
94.70 0.4167 0.5905 0.0648 0.0457 20.349 106.880 47.588 15174.153 12.075 211.673 1.422 0.96 382635. 0.2879
|
|
101.01 0.4445 0.6177 0.0612 0.0440 19.595 102.918 44.933 14611.720 11.628 199.862 1.395 0.96 383457. 0.2743
|
|
107.33 0.4722 0.6437 0.0573 0.0421 18.712 98.283 42.091 13953.674 11.104 187.220 1.368 0.96 384322. 0.2604
|
|
113.64 0.5000 0.6686 0.0532 0.0398 17.711 93.024 39.078 13206.970 10.510 173.820 1.342 0.96 385228. 0.2461
|
|
119.95 0.5278 0.6919 0.0489 0.0373 16.602 87.202 35.912 12380.401 9.852 159.739 1.316 0.97 386176. 0.2313
|
|
126.27 0.5556 0.7131 0.0444 0.0346 15.399 80.880 32.612 11482.896 9.138 145.058 1.288 0.97 387165. 0.2158
|
|
132.58 0.5833 0.7314 0.0398 0.0317 14.110 74.113 29.194 10522.087 8.373 129.856 1.258 0.97 388195. 0.1995
|
|
138.89 0.6111 0.7462 0.0350 0.0286 12.745 66.941 25.677 9503.923 7.563 114.211 1.225 0.97 389265. 0.1822
|
|
145.21 0.6389 0.7555 0.0301 0.0254 11.314 59.426 22.076 8437.006 6.714 98.196 1.187 0.97 390375. 0.1636
|
|
151.52 0.6667 0.7468 0.0250 0.0224 9.949 52.257 18.391 7419.148 5.904 81.802 1.124 0.97 391526. 0.1415
|
|
157.83 0.6945 0.6965 0.0199 0.0198 8.832 46.387 14.615 6585.732 5.241 65.006 1.007 0.97 392716. 0.1129
|
|
164.15 0.7222 0.6103 0.0147 0.0174 7.749 40.700 10.804 5778.402 4.598 48.058 0.848 0.98 393945. 0.0818
|
|
170.46 0.7500 0.4739 0.0095 0.0151 6.706 35.222 6.992 5000.657 3.979 31.101 0.634 0.98 395213. 0.0492
|
|
176.77 0.7778 0.2653 0.0044 0.0128 5.710 29.988 3.214 4257.575 3.388 14.294 0.342 0.98 396520. 0.0180
|
|
183.09 0.8056
|
|
|
|
|
|
|