427 lines
76 KiB
Plaintext
427 lines
76 KiB
Plaintext
21x10W (21x10W.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 0.0904 0.0349 0.011 0.724 0.560 8.562 0.082 2.492 29.675 0.08 52431. 0.6206
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0.44 0.0221 0.0556 0.0887 0.0352 0.012 0.729 0.550 8.626 0.082 2.445 28.907 0.08 52463. 0.5989
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0.88 0.0442 0.1083 0.0869 0.0354 0.012 0.734 0.539 8.681 0.083 2.396 28.143 0.08 52498. 0.5771
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1.32 0.0662 0.1581 0.0850 0.0356 0.012 0.738 0.527 8.726 0.083 2.343 27.385 0.08 52536. 0.5554
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1.76 0.0883 0.2051 0.0830 0.0357 0.012 0.740 0.514 8.758 0.084 2.287 26.633 0.08 52576. 0.5336
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2.20 0.1104 0.2491 0.0808 0.0358 0.012 0.742 0.501 8.777 0.084 2.228 25.887 0.08 52619. 0.5119
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2.63 0.1325 0.2904 0.0786 0.0358 0.012 0.742 0.487 8.782 0.084 2.166 25.148 0.08 52664. 0.4903
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3.07 0.1546 0.3290 0.0762 0.0358 0.012 0.741 0.472 8.769 0.084 2.100 24.415 0.08 52712. 0.4687
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3.51 0.1766 0.3648 0.0736 0.0357 0.012 0.739 0.456 8.739 0.083 2.030 23.688 0.08 52763. 0.4471
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3.95 0.1987 0.3979 0.0710 0.0355 0.012 0.734 0.440 8.689 0.083 1.957 22.966 0.08 52817. 0.4257
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4.39 0.2208 0.4283 0.0682 0.0352 0.012 0.729 0.423 8.619 0.082 1.881 22.250 0.08 52874. 0.4042
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4.83 0.2429 0.4560 0.0653 0.0348 0.011 0.721 0.405 8.528 0.081 1.801 21.536 0.08 52934. 0.3829
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5.27 0.2649 0.4810 0.0623 0.0343 0.011 0.711 0.386 8.415 0.080 1.719 20.825 0.08 52996. 0.3617
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5.71 0.2870 0.5033 0.0592 0.0338 0.011 0.700 0.367 8.280 0.079 1.633 20.113 0.08 53063. 0.3405
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6.15 0.3091 0.5227 0.0560 0.0331 0.011 0.686 0.347 8.121 0.078 1.545 19.397 0.08 53132. 0.3194
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6.59 0.3312 0.5392 0.0527 0.0324 0.011 0.671 0.327 7.939 0.076 1.454 18.676 0.08 53204. 0.2984
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7.03 0.3533 0.5527 0.0494 0.0316 0.010 0.654 0.306 7.732 0.074 1.361 17.945 0.08 53280. 0.2773
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7.46 0.3753 0.5628 0.0459 0.0306 0.010 0.634 0.284 7.501 0.072 1.265 17.200 0.08 53359. 0.2563
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7.90 0.3974 0.5694 0.0423 0.0296 0.010 0.612 0.262 7.244 0.069 1.167 16.434 0.08 53442. 0.2352
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8.34 0.4195 0.5720 0.0387 0.0284 0.009 0.588 0.240 6.961 0.066 1.068 15.640 0.08 53528. 0.2141
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8.78 0.4416 0.5701 0.0350 0.0271 0.009 0.562 0.217 6.652 0.064 0.966 14.809 0.08 53617. 0.1928
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9.22 0.4637 0.5630 0.0313 0.0258 0.008 0.534 0.194 6.317 0.060 0.863 13.927 0.08 53710. 0.1714
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9.66 0.4857 0.5496 0.0275 0.0243 0.008 0.503 0.170 5.954 0.057 0.758 12.979 0.08 53806. 0.1497
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10.10 0.5078 0.5286 0.0236 0.0227 0.007 0.470 0.147 5.565 0.053 0.652 11.941 0.08 53906. 0.1277
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10.54 0.5299 0.4980 0.0197 0.0210 0.007 0.435 0.122 5.149 0.049 0.544 10.779 0.08 54009. 0.1054
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10.98 0.5520 0.4546 0.0158 0.0192 0.006 0.398 0.098 4.706 0.045 0.436 9.447 0.08 54116. 0.0826
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11.42 0.5740 0.3938 0.0119 0.0173 0.006 0.358 0.074 4.237 0.040 0.327 7.870 0.08 54226. 0.0596
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11.85 0.5961 0.3082 0.0079 0.0153 0.005 0.316 0.049 3.742 0.036 0.218 5.930 0.08 54340. 0.0367
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12.29 0.6182 0.1845 0.0039 0.0132 0.004 0.272 0.024 3.223 0.031 0.108 3.424 0.08 54457. 0.0149
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12.73 0.6403 -0.0033 -0.0001 0.0109 0.004 0.226 0.000 2.678 0.026 -0.002 -0.059 0.09 54572. 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 0.0909 0.0318 0.084 2.634 2.253 62.320 0.298 10.019 16.394 0.17 104859. 0.6875
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0.88 0.0222 0.0616 0.0892 0.0321 0.084 2.658 2.211 62.892 0.300 9.833 15.944 0.17 104925. 0.6624
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1.76 0.0443 0.1198 0.0874 0.0323 0.085 2.679 2.166 63.393 0.303 9.635 15.499 0.17 104995. 0.6374
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2.64 0.0665 0.1746 0.0855 0.0325 0.086 2.697 2.119 63.810 0.305 9.424 15.060 0.17 105071. 0.6125
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3.53 0.0887 0.2262 0.0834 0.0327 0.086 2.710 2.068 64.130 0.306 9.200 14.628 0.17 105151. 0.5878
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4.41 0.1108 0.2745 0.0813 0.0328 0.086 2.719 2.015 64.341 0.307 8.962 14.203 0.17 105237. 0.5633
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5.29 0.1330 0.3197 0.0790 0.0329 0.086 2.723 1.958 64.430 0.308 8.710 13.786 0.17 105328. 0.5390
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6.17 0.1552 0.3619 0.0766 0.0328 0.086 2.721 1.899 64.383 0.307 8.445 13.375 0.17 105425. 0.5149
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7.05 0.1773 0.4011 0.0740 0.0327 0.086 2.713 1.836 64.186 0.306 8.165 12.971 0.17 105528. 0.4910
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7.93 0.1995 0.4374 0.0714 0.0326 0.086 2.698 1.770 63.830 0.305 7.871 12.574 0.17 105636. 0.4674
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8.82 0.2217 0.4709 0.0686 0.0323 0.085 2.675 1.700 63.304 0.302 7.564 12.184 0.17 105751. 0.4439
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9.70 0.2438 0.5016 0.0657 0.0319 0.084 2.646 1.628 62.601 0.299 7.243 11.799 0.17 105871. 0.4207
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10.58 0.2660 0.5296 0.0627 0.0315 0.083 2.608 1.554 61.716 0.295 6.911 11.419 0.17 105998. 0.3977
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11.46 0.2882 0.5548 0.0596 0.0309 0.081 2.563 1.476 60.641 0.290 6.567 11.042 0.17 106131. 0.3749
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12.34 0.3103 0.5773 0.0563 0.0303 0.080 2.509 1.396 59.372 0.283 6.212 10.668 0.17 106271. 0.3523
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13.22 0.3325 0.5969 0.0530 0.0295 0.078 2.447 1.314 57.903 0.276 5.846 10.295 0.17 106417. 0.3298
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14.11 0.3547 0.6135 0.0496 0.0287 0.075 2.376 1.230 56.227 0.268 5.471 9.921 0.17 106570. 0.3074
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14.99 0.3768 0.6271 0.0461 0.0277 0.073 2.297 1.143 54.341 0.259 5.086 9.544 0.17 106729. 0.2851
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15.87 0.3990 0.6373 0.0426 0.0266 0.070 2.208 1.055 52.239 0.249 4.693 9.160 0.17 106895. 0.2629
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16.75 0.4212 0.6438 0.0389 0.0255 0.067 2.110 0.965 49.917 0.238 4.291 8.766 0.17 107069. 0.2406
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17.63 0.4433 0.6461 0.0352 0.0242 0.064 2.002 0.873 47.371 0.226 3.883 8.358 0.17 107249. 0.2182
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18.51 0.4655 0.6434 0.0314 0.0227 0.060 1.885 0.779 44.598 0.213 3.467 7.927 0.17 107435. 0.1955
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19.40 0.4877 0.6348 0.0276 0.0212 0.056 1.758 0.685 41.596 0.199 3.045 7.466 0.17 107629. 0.1726
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20.28 0.5098 0.6187 0.0237 0.0196 0.051 1.621 0.589 38.365 0.183 2.619 6.960 0.17 107830. 0.1492
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21.16 0.5320 0.5927 0.0198 0.0178 0.047 1.475 0.492 34.905 0.167 2.187 6.390 0.17 108038. 0.1252
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22.04 0.5542 0.5531 0.0159 0.0159 0.042 1.319 0.394 31.219 0.149 1.752 5.724 0.17 108254. 0.1004
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22.92 0.5763 0.4935 0.0119 0.0139 0.037 1.154 0.296 27.310 0.130 1.315 4.910 0.17 108476. 0.0746
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23.80 0.5985 0.4024 0.0080 0.0118 0.031 0.980 0.197 23.187 0.111 0.877 3.856 0.17 108705. 0.0478
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24.69 0.6207 0.2565 0.0040 0.0096 0.025 0.797 0.099 18.856 0.090 0.438 2.370 0.17 108940. 0.0208
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25.57 0.6428 -0.0028 0.0000 0.0073 0.019 0.603 -0.001 14.273 0.068 -0.003 -0.025 0.17 109166. 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 0.0914 0.0306 0.272 5.710 5.099 202.680 0.645 22.680 11.410 0.25 157283. 0.7199
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1.33 0.0222 0.0644 0.0897 0.0309 0.275 5.767 5.005 204.706 0.652 22.260 11.089 0.25 157382. 0.6931
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2.65 0.0444 0.1252 0.0879 0.0312 0.277 5.818 4.904 206.489 0.657 21.812 10.772 0.25 157488. 0.6665
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3.98 0.0666 0.1823 0.0860 0.0314 0.279 5.860 4.797 207.983 0.662 21.335 10.461 0.25 157602. 0.6401
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5.30 0.0889 0.2360 0.0839 0.0316 0.280 5.893 4.683 209.148 0.666 20.829 10.155 0.25 157723. 0.6140
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6.63 0.1111 0.2863 0.0818 0.0317 0.282 5.915 4.562 209.937 0.668 20.291 9.856 0.25 157852. 0.5882
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7.95 0.1333 0.3333 0.0795 0.0318 0.282 5.925 4.434 210.306 0.669 19.722 9.563 0.25 157990. 0.5626
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9.28 0.1555 0.3772 0.0771 0.0318 0.282 5.922 4.299 210.207 0.669 19.121 9.276 0.25 158136. 0.5374
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10.60 0.1777 0.4181 0.0745 0.0317 0.281 5.905 4.156 209.595 0.667 18.488 8.995 0.25 158291. 0.5124
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11.93 0.1999 0.4559 0.0718 0.0315 0.280 5.872 4.007 208.429 0.663 17.823 8.720 0.25 158454. 0.4877
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13.25 0.2221 0.4909 0.0690 0.0312 0.277 5.823 3.850 206.678 0.658 17.127 8.450 0.25 158627. 0.4633
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14.58 0.2443 0.5231 0.0661 0.0309 0.274 5.756 3.687 204.317 0.650 16.401 8.186 0.25 158808. 0.4392
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15.90 0.2666 0.5526 0.0631 0.0304 0.270 5.672 3.518 201.322 0.641 15.648 7.926 0.25 159000. 0.4154
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17.23 0.2888 0.5793 0.0599 0.0299 0.265 5.569 3.343 197.673 0.629 14.868 7.670 0.25 159200. 0.3918
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18.55 0.3110 0.6033 0.0567 0.0292 0.259 5.447 3.162 193.348 0.615 14.063 7.417 0.25 159411. 0.3685
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19.88 0.3332 0.6245 0.0533 0.0285 0.253 5.306 2.975 188.327 0.599 13.235 7.166 0.25 159631. 0.3454
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21.20 0.3554 0.6429 0.0499 0.0276 0.245 5.144 2.784 182.591 0.581 12.384 6.916 0.25 159861. 0.3224
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22.53 0.3776 0.6583 0.0464 0.0266 0.236 4.962 2.588 176.123 0.561 11.512 6.665 0.25 160101. 0.2996
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23.85 0.3998 0.6706 0.0428 0.0255 0.227 4.759 2.388 168.904 0.538 10.621 6.412 0.25 160352. 0.2769
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25.18 0.4221 0.6793 0.0391 0.0243 0.216 4.534 2.183 160.920 0.512 9.712 6.154 0.25 160612. 0.2541
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26.50 0.4443 0.6841 0.0354 0.0230 0.204 4.287 1.975 152.158 0.484 8.786 5.888 0.25 160883. 0.2312
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27.83 0.4665 0.6843 0.0316 0.0216 0.191 4.018 1.764 142.606 0.454 7.844 5.609 0.25 161165. 0.2081
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29.16 0.4887 0.6789 0.0278 0.0200 0.177 3.726 1.549 132.259 0.421 6.889 5.311 0.25 161457. 0.1847
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30.48 0.5109 0.6662 0.0239 0.0183 0.162 3.412 1.331 121.114 0.386 5.922 4.986 0.25 161760. 0.1607
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31.81 0.5331 0.6440 0.0199 0.0165 0.146 3.076 1.112 109.172 0.348 4.945 4.619 0.25 162073. 0.1361
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33.13 0.5553 0.6082 0.0160 0.0146 0.129 2.717 0.890 96.444 0.307 3.960 4.187 0.25 162397. 0.1104
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34.46 0.5775 0.5516 0.0120 0.0125 0.111 2.337 0.668 82.944 0.264 2.970 3.652 0.25 162732. 0.0834
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35.78 0.5998 0.4605 0.0080 0.0104 0.092 1.936 0.445 68.698 0.219 1.978 2.936 0.25 163077. 0.0547
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37.11 0.6220 0.3043 0.0040 0.0081 0.072 1.514 0.222 53.730 0.171 0.986 1.871 0.25 163430. 0.0246
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38.43 0.6442 -0.0088 -0.0001 0.0057 0.051 1.065 -0.004 37.802 0.120 -0.019 -0.052 0.26 163758. 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 0.0921 0.0302 0.634 9.993 9.136 472.931 1.129 40.636 8.762 0.33 209700. 0.7400
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1.77 0.0222 0.0660 0.0904 0.0305 0.641 10.098 8.968 477.885 1.141 39.888 8.511 0.33 209832. 0.7122
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3.54 0.0445 0.1282 0.0886 0.0307 0.647 10.190 8.788 482.251 1.151 39.089 8.265 0.33 209974. 0.6846
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5.31 0.0667 0.1867 0.0867 0.0310 0.652 10.268 8.596 485.923 1.160 38.237 8.024 0.33 210127. 0.6574
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7.08 0.0890 0.2417 0.0846 0.0312 0.655 10.329 8.393 488.796 1.167 37.331 7.788 0.33 210289. 0.6304
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8.85 0.1112 0.2931 0.0825 0.0313 0.658 10.370 8.177 490.763 1.172 36.370 7.557 0.33 210462. 0.6038
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10.62 0.1335 0.3412 0.0801 0.0313 0.659 10.390 7.948 491.715 1.174 35.353 7.331 0.33 210647. 0.5775
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12.39 0.1557 0.3861 0.0777 0.0313 0.659 10.386 7.706 491.536 1.173 34.277 7.111 0.33 210842. 0.5516
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14.16 0.1780 0.4279 0.0751 0.0312 0.657 10.356 7.451 490.115 1.170 33.143 6.896 0.33 211049. 0.5259
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15.93 0.2002 0.4667 0.0724 0.0311 0.654 10.298 7.183 487.355 1.163 31.951 6.685 0.33 211269. 0.5006
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17.69 0.2224 0.5027 0.0696 0.0308 0.648 10.210 6.903 483.180 1.154 30.704 6.480 0.33 211500. 0.4757
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19.46 0.2447 0.5358 0.0667 0.0304 0.640 10.090 6.611 477.527 1.140 29.404 6.279 0.33 211743. 0.4511
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21.23 0.2669 0.5662 0.0636 0.0300 0.631 9.939 6.307 470.340 1.123 28.054 6.082 0.33 211999. 0.4268
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23.00 0.2892 0.5939 0.0604 0.0294 0.619 9.753 5.993 461.566 1.102 26.656 5.889 0.33 212268. 0.4028
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24.77 0.3114 0.6189 0.0572 0.0288 0.605 9.533 5.668 451.155 1.077 25.212 5.699 0.33 212549. 0.3791
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26.54 0.3337 0.6412 0.0538 0.0280 0.589 9.278 5.334 439.060 1.048 23.727 5.510 0.34 212844. 0.3556
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28.31 0.3559 0.6608 0.0503 0.0271 0.570 8.985 4.991 425.233 1.015 22.201 5.324 0.34 213152. 0.3323
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30.08 0.3782 0.6775 0.0468 0.0261 0.549 8.656 4.640 409.630 0.978 20.637 5.137 0.34 213474. 0.3092
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31.85 0.4004 0.6912 0.0432 0.0250 0.526 8.288 4.280 392.209 0.936 19.039 4.950 0.34 213809. 0.2861
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33.62 0.4226 0.7015 0.0395 0.0238 0.500 7.880 3.913 372.935 0.890 17.407 4.760 0.34 214157. 0.2631
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35.39 0.4449 0.7081 0.0357 0.0224 0.472 7.433 3.540 351.774 0.840 15.746 4.564 0.34 214520. 0.2399
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37.16 0.4671 0.7104 0.0319 0.0210 0.441 6.946 3.160 328.701 0.785 14.057 4.361 0.34 214897. 0.2166
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38.93 0.4894 0.7073 0.0280 0.0194 0.407 6.417 2.775 303.701 0.725 12.343 4.144 0.34 215287. 0.1929
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40.70 0.5116 0.6973 0.0241 0.0176 0.371 5.848 2.385 276.766 0.661 10.608 3.908 0.34 215692. 0.1687
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42.47 0.5339 0.6781 0.0201 0.0158 0.332 5.238 1.991 247.903 0.592 8.855 3.643 0.34 216111. 0.1436
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44.24 0.5561 0.6456 0.0161 0.0138 0.291 4.588 1.594 217.134 0.518 7.089 3.329 0.34 216545. 0.1174
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46.01 0.5784 0.5922 0.0120 0.0118 0.247 3.899 1.194 184.499 0.440 5.313 2.936 0.34 216992. 0.0897
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47.78 0.6006 0.5028 0.0080 0.0096 0.201 3.171 0.794 150.056 0.358 3.533 2.401 0.34 217453. 0.0598
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49.54 0.6229 0.3410 0.0040 0.0073 0.153 2.406 0.394 113.867 0.272 1.753 1.570 0.34 217926. 0.0275
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51.31 0.6451 -0.0191 -0.0001 0.0048 0.101 1.586 -0.014 75.064 0.179 -0.063 -0.085 0.34 218340. 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 0.0931 0.0300 1.234 15.559 14.418 920.424 1.758 64.132 7.105 0.42 262106. 0.7538
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2.21 0.0223 0.0669 0.0914 0.0304 1.248 15.727 14.155 930.342 1.777 62.960 6.901 0.42 262272. 0.7254
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4.43 0.0445 0.1300 0.0895 0.0307 1.259 15.875 13.873 939.086 1.794 61.706 6.700 0.42 262451. 0.6973
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6.64 0.0668 0.1893 0.0876 0.0309 1.269 15.999 13.572 946.444 1.808 60.369 6.504 0.42 262642. 0.6695
|
|
8.85 0.0890 0.2450 0.0855 0.0311 1.277 16.097 13.252 952.206 1.819 58.946 6.313 0.42 262846. 0.6421
|
|
11.06 0.1113 0.2971 0.0833 0.0312 1.282 16.163 12.913 956.161 1.826 57.435 6.125 0.42 263064. 0.6150
|
|
13.28 0.1335 0.3459 0.0810 0.0313 1.285 16.196 12.553 958.091 1.830 55.834 5.943 0.42 263295. 0.5883
|
|
15.49 0.1558 0.3915 0.0786 0.0313 1.284 16.191 12.172 957.767 1.829 54.141 5.764 0.42 263541. 0.5619
|
|
17.70 0.1780 0.4339 0.0760 0.0312 1.281 16.143 11.771 954.968 1.824 52.356 5.591 0.42 263801. 0.5359
|
|
19.92 0.2003 0.4733 0.0732 0.0310 1.273 16.051 11.349 949.500 1.813 50.478 5.421 0.42 264076. 0.5103
|
|
22.13 0.2226 0.5099 0.0704 0.0307 1.262 15.911 10.907 941.210 1.798 48.513 5.256 0.42 264366. 0.4850
|
|
24.34 0.2448 0.5437 0.0674 0.0304 1.247 15.721 10.446 929.972 1.776 46.463 5.095 0.42 264671. 0.4601
|
|
26.56 0.2671 0.5748 0.0643 0.0299 1.228 15.479 9.967 915.675 1.749 44.333 4.937 0.42 264993. 0.4355
|
|
28.77 0.2893 0.6032 0.0611 0.0293 1.205 15.184 9.471 898.218 1.715 42.127 4.783 0.42 265330. 0.4112
|
|
30.98 0.3116 0.6290 0.0578 0.0286 1.177 14.834 8.959 877.501 1.676 39.850 4.631 0.42 265683. 0.3873
|
|
33.19 0.3338 0.6521 0.0544 0.0279 1.144 14.427 8.432 853.429 1.630 37.505 4.481 0.42 266052. 0.3636
|
|
35.41 0.3561 0.6726 0.0509 0.0270 1.108 13.962 7.890 825.910 1.577 35.096 4.333 0.42 266438. 0.3401
|
|
37.62 0.3784 0.6903 0.0473 0.0259 1.066 13.437 7.335 794.857 1.518 32.628 4.186 0.42 266841. 0.3168
|
|
39.83 0.4006 0.7052 0.0437 0.0248 1.019 12.851 6.768 760.187 1.452 30.103 4.038 0.42 267261. 0.2935
|
|
42.05 0.4229 0.7168 0.0399 0.0236 0.968 12.202 6.189 721.828 1.379 27.527 3.889 0.42 267698. 0.2703
|
|
44.26 0.4451 0.7249 0.0361 0.0222 0.912 11.490 5.599 679.717 1.298 24.903 3.736 0.42 268152. 0.2470
|
|
46.47 0.4674 0.7288 0.0323 0.0207 0.850 10.714 4.999 633.802 1.210 22.235 3.577 0.42 268624. 0.2235
|
|
48.69 0.4896 0.7277 0.0283 0.0191 0.783 9.873 4.390 584.052 1.115 19.528 3.410 0.42 269113. 0.1996
|
|
50.90 0.5119 0.7201 0.0244 0.0173 0.711 8.967 3.774 530.453 1.013 16.787 3.227 0.42 269620. 0.1752
|
|
53.11 0.5341 0.7036 0.0203 0.0154 0.634 7.996 3.152 473.018 0.903 14.018 3.022 0.42 270145. 0.1499
|
|
55.32 0.5564 0.6742 0.0163 0.0134 0.552 6.961 2.524 411.792 0.786 11.226 2.780 0.42 270687. 0.1234
|
|
57.54 0.5787 0.6244 0.0122 0.0113 0.465 5.863 1.893 346.852 0.662 8.420 2.475 0.42 271247. 0.0952
|
|
59.75 0.6009 0.5380 0.0081 0.0091 0.373 4.705 1.260 278.319 0.532 5.606 2.054 0.42 271824. 0.0644
|
|
61.96 0.6232 0.3751 0.0041 0.0067 0.277 3.488 0.628 206.314 0.394 2.793 1.381 0.42 272415. 0.0306
|
|
64.18 0.6454 -0.0197 -0.0001 0.0042 0.173 2.177 -0.020 128.779 0.246 -0.088 -0.070 0.43 272917. 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 0.0942 0.0302 2.144 22.526 21.024 1599.046 2.545 93.513 5.963 0.50 314497. 0.7640
|
|
2.68 0.0224 0.0679 0.0925 0.0305 2.168 22.775 20.640 1616.720 2.573 91.807 5.791 0.50 314700. 0.7351
|
|
5.35 0.0448 0.1319 0.0907 0.0308 2.189 22.994 20.229 1632.278 2.598 89.979 5.621 0.50 314917. 0.7064
|
|
8.03 0.0673 0.1920 0.0887 0.0311 2.206 23.178 19.790 1645.323 2.619 88.026 5.456 0.50 315150. 0.6781
|
|
10.70 0.0897 0.2484 0.0866 0.0313 2.220 23.321 19.322 1655.485 2.635 85.946 5.294 0.50 315399. 0.6502
|
|
13.38 0.1121 0.3012 0.0844 0.0314 2.229 23.418 18.825 1662.385 2.646 83.734 5.136 0.50 315664. 0.6227
|
|
16.05 0.1345 0.3507 0.0820 0.0315 2.234 23.464 18.298 1665.627 2.651 81.388 4.983 0.50 315946. 0.5955
|
|
18.73 0.1570 0.3968 0.0795 0.0314 2.233 23.452 17.739 1664.806 2.650 78.904 4.833 0.50 316245. 0.5688
|
|
21.40 0.1794 0.4398 0.0769 0.0313 2.225 23.378 17.150 1659.521 2.641 76.283 4.687 0.50 316562. 0.5424
|
|
24.08 0.2018 0.4798 0.0741 0.0312 2.212 23.236 16.530 1649.426 2.625 73.524 4.545 0.50 316897. 0.5164
|
|
26.76 0.2242 0.5170 0.0712 0.0309 2.192 23.022 15.880 1634.245 2.601 70.634 4.407 0.50 317250. 0.4907
|
|
29.43 0.2467 0.5513 0.0681 0.0305 2.164 22.733 15.202 1613.758 2.568 67.618 4.273 0.50 317623. 0.4655
|
|
32.11 0.2691 0.5829 0.0650 0.0300 2.129 22.367 14.497 1587.773 2.527 64.483 4.141 0.50 318014. 0.4406
|
|
34.78 0.2915 0.6119 0.0617 0.0294 2.087 21.921 13.767 1556.111 2.477 61.235 4.013 0.50 318425. 0.4160
|
|
37.46 0.3139 0.6382 0.0583 0.0287 2.036 21.393 13.013 1518.595 2.417 57.881 3.887 0.50 318855. 0.3917
|
|
40.13 0.3364 0.6620 0.0548 0.0279 1.978 20.779 12.236 1475.063 2.348 54.427 3.763 0.50 319305. 0.3678
|
|
42.81 0.3588 0.6831 0.0513 0.0269 1.911 20.079 11.439 1425.348 2.269 50.879 3.640 0.50 319775. 0.3440
|
|
45.48 0.3812 0.7015 0.0476 0.0259 1.836 19.289 10.621 1369.299 2.179 47.242 3.518 0.50 320266. 0.3204
|
|
48.16 0.4036 0.7170 0.0439 0.0247 1.752 18.409 9.785 1306.771 2.080 43.522 3.396 0.50 320777. 0.2968
|
|
50.84 0.4261 0.7294 0.0400 0.0234 1.660 17.435 8.931 1237.637 1.970 39.725 3.273 0.50 321309. 0.2733
|
|
53.51 0.4485 0.7383 0.0361 0.0219 1.558 16.366 8.062 1161.787 1.849 35.858 3.147 0.50 321862. 0.2497
|
|
56.19 0.4709 0.7431 0.0322 0.0204 1.447 15.202 7.178 1079.135 1.717 31.926 3.017 0.51 322437. 0.2258
|
|
58.86 0.4933 0.7428 0.0282 0.0187 1.327 13.941 6.281 989.626 1.575 27.937 2.879 0.51 323032. 0.2016
|
|
61.54 0.5157 0.7360 0.0241 0.0169 1.198 12.583 5.373 893.245 1.422 23.898 2.728 0.51 323650. 0.1767
|
|
64.21 0.5382 0.7201 0.0200 0.0149 1.059 11.129 4.455 790.020 1.257 19.817 2.558 0.51 324288. 0.1509
|
|
66.89 0.5606 0.6906 0.0158 0.0128 0.912 9.580 3.531 680.043 1.082 15.705 2.355 0.51 324948. 0.1236
|
|
69.57 0.5830 0.6386 0.0117 0.0106 0.756 7.938 2.601 563.470 0.897 11.571 2.094 0.51 325630. 0.0944
|
|
72.24 0.6054 0.5446 0.0075 0.0083 0.591 6.206 1.670 440.526 0.701 7.429 1.720 0.51 326331. 0.0621
|
|
74.92 0.6279 0.3537 0.0033 0.0059 0.418 4.387 0.739 311.392 0.496 3.289 1.077 0.51 327049. 0.0259
|
|
77.59 0.6503
|
|
|
|
|
|
|
|
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 0.0957 0.0306 3.450 31.065 29.059 2572.742 3.510 129.257 5.123 0.58 366869. 0.7717
|
|
3.10 0.0223 0.0676 0.0940 0.0309 3.489 31.411 28.540 2601.387 3.549 126.944 4.976 0.58 367106. 0.7428
|
|
6.20 0.0445 0.1313 0.0921 0.0312 3.522 31.715 27.982 2626.582 3.583 124.463 4.832 0.58 367359. 0.7142
|
|
9.30 0.0668 0.1913 0.0902 0.0315 3.551 31.970 27.386 2647.709 3.612 121.811 4.691 0.58 367631. 0.6860
|
|
12.40 0.0891 0.2476 0.0881 0.0317 3.573 32.169 26.750 2664.179 3.634 118.983 4.554 0.58 367920. 0.6581
|
|
15.50 0.1114 0.3004 0.0859 0.0318 3.588 32.304 26.073 2675.382 3.650 115.974 4.420 0.58 368229. 0.6307
|
|
18.60 0.1336 0.3499 0.0835 0.0319 3.595 32.368 25.355 2680.694 3.657 112.780 4.290 0.58 368557. 0.6036
|
|
21.70 0.1559 0.3961 0.0810 0.0319 3.593 32.354 24.595 2679.482 3.655 109.397 4.163 0.58 368905. 0.5769
|
|
24.80 0.1782 0.4393 0.0783 0.0318 3.582 32.253 23.791 2671.106 3.644 105.823 4.040 0.58 369273. 0.5506
|
|
27.90 0.2004 0.4795 0.0756 0.0316 3.560 32.058 22.945 2655.002 3.622 102.060 3.920 0.58 369662. 0.5246
|
|
31.00 0.2227 0.5169 0.0726 0.0313 3.528 31.765 22.058 2630.729 3.589 98.115 3.803 0.58 370073. 0.4991
|
|
34.10 0.2450 0.5516 0.0696 0.0309 3.484 31.369 21.132 2597.932 3.544 93.994 3.689 0.58 370505. 0.4739
|
|
37.20 0.2673 0.5837 0.0664 0.0304 3.428 30.867 20.168 2556.314 3.487 89.709 3.579 0.59 370958. 0.4490
|
|
40.30 0.2895 0.6131 0.0631 0.0298 3.360 30.254 19.170 2505.606 3.418 85.268 3.470 0.59 371434. 0.4245
|
|
43.40 0.3118 0.6401 0.0597 0.0291 3.280 29.529 18.138 2445.535 3.336 80.679 3.364 0.59 371933. 0.4003
|
|
46.50 0.3341 0.6646 0.0562 0.0283 3.186 28.687 17.075 2375.847 3.241 75.951 3.260 0.59 372454. 0.3764
|
|
49.60 0.3563 0.6865 0.0526 0.0273 3.079 27.727 15.983 2296.290 3.133 71.093 3.157 0.59 372998. 0.3527
|
|
52.71 0.3786 0.7059 0.0489 0.0263 2.959 26.644 14.863 2206.624 3.010 66.112 3.055 0.59 373565. 0.3291
|
|
55.81 0.4009 0.7226 0.0452 0.0251 2.825 25.437 13.717 2106.623 2.874 61.015 2.953 0.59 374157. 0.3056
|
|
58.91 0.4232 0.7363 0.0413 0.0237 2.677 24.102 12.548 1996.086 2.723 55.811 2.851 0.59 374772. 0.2822
|
|
62.01 0.4454 0.7468 0.0374 0.0223 2.514 22.638 11.355 1874.839 2.558 50.509 2.747 0.59 375411. 0.2587
|
|
65.11 0.4677 0.7535 0.0334 0.0207 2.337 21.043 10.143 1742.740 2.377 45.116 2.640 0.59 376074. 0.2349
|
|
68.21 0.4900 0.7556 0.0293 0.0190 2.145 19.316 8.912 1599.695 2.182 39.641 2.527 0.59 376761. 0.2108
|
|
71.31 0.5122 0.7518 0.0252 0.0172 1.939 17.456 7.665 1445.667 1.972 34.095 2.405 0.59 377474. 0.1860
|
|
74.41 0.5345 0.7399 0.0211 0.0152 1.717 15.464 6.405 1280.694 1.747 28.489 2.268 0.59 378210. 0.1604
|
|
77.51 0.5568 0.7161 0.0169 0.0131 1.482 13.341 5.134 1104.898 1.507 22.836 2.108 0.59 378972. 0.1334
|
|
80.61 0.5791 0.6728 0.0127 0.0109 1.232 11.091 3.856 918.512 1.253 17.150 1.904 0.59 379757. 0.1045
|
|
83.71 0.6013 0.5934 0.0085 0.0086 0.968 8.716 2.574 721.878 0.985 11.448 1.617 0.59 380567. 0.0725
|
|
86.81 0.6236 0.4326 0.0043 0.0061 0.691 6.223 1.292 515.348 0.703 5.745 1.137 0.59 381397. 0.0361
|
|
89.91 0.6459 -0.0198 -0.0001 0.0035 0.391 3.517 -0.032 291.311 0.397 -0.144 -0.050 0.60 382051. 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 0.0975 0.0313 5.260 41.442 38.674 3922.490 4.682 172.024 4.472 0.67 419216. 0.7771
|
|
3.55 0.0223 0.0676 0.0958 0.0316 5.319 41.907 37.993 3966.490 4.735 168.995 4.345 0.67 419488. 0.7482
|
|
7.10 0.0446 0.1313 0.0939 0.0319 5.371 42.315 37.261 4005.135 4.781 165.737 4.220 0.67 419781. 0.7197
|
|
10.65 0.0669 0.1912 0.0920 0.0322 5.414 42.657 36.476 4037.431 4.819 162.247 4.098 0.67 420094. 0.6915
|
|
14.19 0.0892 0.2476 0.0898 0.0324 5.448 42.921 35.638 4062.460 4.849 158.519 3.979 0.67 420429. 0.6637
|
|
17.74 0.1115 0.3005 0.0876 0.0325 5.470 43.099 34.745 4079.272 4.869 154.545 3.863 0.67 420785. 0.6363
|
|
21.29 0.1338 0.3501 0.0852 0.0326 5.481 43.180 33.795 4086.929 4.878 150.320 3.751 0.67 421164. 0.6092
|
|
24.84 0.1561 0.3965 0.0827 0.0326 5.477 43.154 32.788 4084.454 4.875 145.840 3.641 0.67 421565. 0.5825
|
|
28.39 0.1784 0.4399 0.0800 0.0324 5.459 43.010 31.722 4070.869 4.859 141.101 3.534 0.67 421990. 0.5562
|
|
31.94 0.2007 0.4803 0.0771 0.0322 5.425 42.740 30.599 4045.295 4.829 136.105 3.431 0.67 422439. 0.5303
|
|
35.48 0.2230 0.5180 0.0742 0.0319 5.374 42.336 29.420 4007.048 4.783 130.860 3.330 0.67 422912. 0.5047
|
|
39.03 0.2453 0.5531 0.0711 0.0315 5.305 41.792 28.188 3955.605 4.722 125.379 3.232 0.67 423410. 0.4795
|
|
42.58 0.2677 0.5855 0.0678 0.0310 5.217 41.105 26.905 3890.523 4.644 119.673 3.137 0.67 423932. 0.4546
|
|
46.13 0.2900 0.6155 0.0645 0.0304 5.111 40.269 25.575 3811.408 4.550 113.755 3.043 0.67 424480. 0.4300
|
|
49.68 0.3123 0.6430 0.0610 0.0296 4.986 39.281 24.199 3717.880 4.438 107.639 2.952 0.67 425054. 0.4058
|
|
53.23 0.3346 0.6680 0.0574 0.0288 4.840 38.136 22.782 3609.558 4.309 101.334 2.863 0.67 425654. 0.3818
|
|
56.77 0.3569 0.6906 0.0538 0.0278 4.675 36.831 21.325 3486.073 4.161 94.852 2.775 0.67 426280. 0.3580
|
|
60.32 0.3792 0.7106 0.0500 0.0267 4.488 35.363 19.830 3347.073 3.995 88.204 2.687 0.67 426932. 0.3344
|
|
63.87 0.4015 0.7281 0.0461 0.0254 4.281 33.727 18.300 3192.220 3.810 81.400 2.600 0.67 427612. 0.3108
|
|
67.42 0.4238 0.7427 0.0422 0.0241 4.052 31.920 16.738 3021.212 3.606 74.451 2.513 0.67 428319. 0.2873
|
|
70.97 0.4461 0.7542 0.0382 0.0226 3.800 29.940 15.145 2833.790 3.383 67.367 2.424 0.67 429053. 0.2636
|
|
74.52 0.4684 0.7621 0.0341 0.0210 3.527 27.784 13.525 2629.743 3.139 60.160 2.333 0.67 429814. 0.2397
|
|
78.07 0.4907 0.7655 0.0300 0.0192 3.230 25.451 11.880 2408.933 2.875 52.843 2.237 0.67 430604. 0.2154
|
|
81.61 0.5130 0.7633 0.0257 0.0173 2.912 22.940 10.213 2171.304 2.592 45.427 2.133 0.68 431421. 0.1905
|
|
85.16 0.5353 0.7533 0.0215 0.0153 2.571 20.253 8.527 1916.915 2.288 37.929 2.018 0.68 432267. 0.1646
|
|
88.71 0.5576 0.7316 0.0172 0.0131 2.207 17.390 6.827 1645.961 1.965 30.366 1.881 0.68 433140. 0.1373
|
|
92.26 0.5799 0.6907 0.0129 0.0108 1.822 14.356 5.116 1358.803 1.622 22.757 1.708 0.68 434041. 0.1079
|
|
95.81 0.6022 0.6134 0.0086 0.0084 1.416 11.157 3.400 1055.973 1.260 15.124 1.460 0.68 434969. 0.0752
|
|
99.36 0.6245 0.4507 0.0042 0.0059 0.990 7.797 1.683 738.006 0.881 7.488 1.035 0.68 435920. 0.0375
|
|
102.90 0.6468
|
|
|
|
|
|
|
|
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 0.0997 0.0326 7.820 54.763 50.071 5831.231 6.187 222.714 3.895 0.75 471526. 0.7700
|
|
4.02 0.0225 0.0669 0.0980 0.0329 7.893 55.276 49.205 5885.855 6.245 218.865 3.792 0.75 471838. 0.7432
|
|
8.04 0.0449 0.1301 0.0962 0.0332 7.956 55.718 48.271 5932.936 6.295 214.708 3.690 0.75 472173. 0.7164
|
|
12.07 0.0674 0.1899 0.0942 0.0334 8.007 56.077 47.266 5971.097 6.336 210.238 3.590 0.75 472532. 0.6897
|
|
16.09 0.0899 0.2463 0.0920 0.0336 8.045 56.339 46.188 5999.043 6.365 205.444 3.492 0.75 472915. 0.6631
|
|
20.11 0.1124 0.2994 0.0897 0.0337 8.067 56.494 45.036 6015.466 6.383 200.320 3.396 0.75 473324. 0.6367
|
|
24.13 0.1348 0.3492 0.0873 0.0337 8.072 56.526 43.808 6018.957 6.386 194.858 3.301 0.75 473758. 0.6105
|
|
28.15 0.1573 0.3960 0.0847 0.0336 8.057 56.424 42.503 6008.078 6.375 189.053 3.209 0.75 474219. 0.5845
|
|
32.18 0.1798 0.4398 0.0819 0.0335 8.021 56.173 41.120 5981.347 6.346 182.901 3.118 0.75 474707. 0.5587
|
|
36.20 0.2022 0.4808 0.0790 0.0332 7.962 55.760 39.659 5937.348 6.300 176.403 3.030 0.75 475222. 0.5331
|
|
40.22 0.2247 0.5189 0.0759 0.0329 7.878 55.174 38.123 5874.954 6.234 169.570 2.943 0.75 475764. 0.5078
|
|
44.24 0.2472 0.5545 0.0727 0.0324 7.769 54.407 36.515 5793.292 6.147 162.418 2.859 0.75 476335. 0.4827
|
|
48.26 0.2697 0.5874 0.0694 0.0319 7.633 53.452 34.839 5691.625 6.039 154.965 2.776 0.75 476934. 0.4579
|
|
52.28 0.2921 0.6179 0.0659 0.0312 7.469 52.303 33.100 5569.301 5.909 147.229 2.696 0.75 477563. 0.4333
|
|
56.31 0.3146 0.6459 0.0623 0.0304 7.276 50.955 31.301 5425.689 5.757 139.226 2.617 0.75 478220. 0.4090
|
|
60.33 0.3371 0.6715 0.0587 0.0294 7.054 49.400 29.445 5260.186 5.581 130.973 2.539 0.75 478907. 0.3850
|
|
64.35 0.3595 0.6947 0.0549 0.0284 6.802 47.635 27.537 5072.193 5.382 122.484 2.462 0.75 479624. 0.3610
|
|
68.37 0.3820 0.7154 0.0510 0.0272 6.519 45.653 25.579 4861.141 5.158 113.774 2.387 0.76 480371. 0.3373
|
|
72.39 0.4045 0.7335 0.0470 0.0259 6.204 43.449 23.574 4626.526 4.909 104.856 2.311 0.76 481148. 0.3135
|
|
76.42 0.4270 0.7488 0.0429 0.0244 5.857 41.021 21.525 4367.908 4.634 95.744 2.235 0.76 481957. 0.2898
|
|
80.44 0.4494 0.7610 0.0387 0.0229 5.478 38.363 19.436 4084.901 4.334 86.453 2.158 0.76 482796. 0.2658
|
|
84.46 0.4719 0.7697 0.0345 0.0211 5.065 35.473 17.311 3777.233 4.008 76.998 2.079 0.76 483667. 0.2416
|
|
88.48 0.4944 0.7739 0.0302 0.0193 4.620 32.351 15.152 3444.802 3.655 67.394 1.995 0.76 484569. 0.2170
|
|
92.50 0.5168 0.7722 0.0258 0.0173 4.141 28.998 12.963 3087.707 3.276 57.661 1.904 0.76 485503. 0.1916
|
|
96.53 0.5393 0.7624 0.0214 0.0151 3.629 25.416 10.750 2706.346 2.872 47.816 1.802 0.76 486468. 0.1651
|
|
100.55 0.5618 0.7399 0.0170 0.0129 3.086 21.614 8.517 2301.458 2.442 37.884 1.679 0.76 487465. 0.1369
|
|
104.57 0.5843 0.6956 0.0125 0.0105 2.513 17.601 6.270 1874.181 1.989 27.890 1.517 0.76 488494. 0.1062
|
|
108.59 0.6067 0.6081 0.0080 0.0080 1.912 13.393 4.016 1426.058 1.513 17.864 1.277 0.76 489553. 0.0715
|
|
112.61 0.6292 0.4112 0.0035 0.0054 1.285 9.002 1.760 958.540 1.017 7.829 0.833 0.76 490634. 0.0309
|
|
116.63 0.6517
|
|
|
|
|
|
|
|
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 0.1024 0.0369 12.122 76.406 63.474 9039.746 8.632 282.331 3.185 0.83 523785. 0.7090
|
|
4.46 0.0224 0.0611 0.1007 0.0370 12.157 76.623 62.424 9065.463 8.657 277.661 3.123 0.83 524134. 0.6895
|
|
8.93 0.0449 0.1198 0.0989 0.0370 12.176 76.741 61.284 9079.323 8.670 272.590 3.062 0.83 524510. 0.6697
|
|
13.39 0.0673 0.1761 0.0969 0.0370 12.176 76.746 60.052 9079.968 8.671 267.109 3.000 0.83 524913. 0.6495
|
|
17.85 0.0898 0.2299 0.0948 0.0370 12.158 76.628 58.724 9066.008 8.657 261.204 2.938 0.83 525343. 0.6291
|
|
22.31 0.1122 0.2813 0.0925 0.0369 12.118 76.375 57.299 9036.064 8.629 254.864 2.876 0.83 525802. 0.6083
|
|
26.78 0.1346 0.3304 0.0900 0.0367 12.054 75.975 55.774 8988.752 8.584 248.081 2.814 0.83 526289. 0.5873
|
|
31.24 0.1571 0.3770 0.0874 0.0364 11.965 75.416 54.147 8922.649 8.521 240.846 2.752 0.83 526806. 0.5659
|
|
35.70 0.1795 0.4211 0.0846 0.0361 11.850 74.687 52.418 8836.305 8.438 233.157 2.691 0.83 527353. 0.5443
|
|
40.16 0.2020 0.4629 0.0816 0.0356 11.705 73.773 50.588 8728.235 8.335 225.015 2.629 0.83 527930. 0.5224
|
|
44.63 0.2244 0.5022 0.0785 0.0351 11.529 72.666 48.659 8597.235 8.210 216.435 2.567 0.84 528539. 0.5003
|
|
49.09 0.2468 0.5392 0.0752 0.0344 11.321 71.357 46.636 8442.354 8.062 207.435 2.506 0.84 529178. 0.4781
|
|
53.55 0.2693 0.5738 0.0718 0.0337 11.080 69.838 44.524 8262.693 7.890 198.041 2.444 0.84 529849. 0.4557
|
|
58.01 0.2917 0.6060 0.0683 0.0329 10.805 68.102 42.328 8057.307 7.694 188.274 2.383 0.84 530552. 0.4332
|
|
62.48 0.3142 0.6359 0.0646 0.0319 10.494 66.141 40.053 7825.227 7.473 178.156 2.322 0.84 531286. 0.4105
|
|
66.94 0.3366 0.6634 0.0608 0.0309 10.146 63.946 37.704 7565.555 7.225 167.708 2.260 0.84 532054. 0.3878
|
|
71.40 0.3591 0.6884 0.0569 0.0297 9.759 61.510 35.285 7277.378 6.949 156.950 2.199 0.84 532854. 0.3650
|
|
75.87 0.3815 0.7110 0.0529 0.0284 9.333 58.826 32.802 6959.770 6.646 145.902 2.138 0.84 533688. 0.3421
|
|
80.33 0.4039 0.7309 0.0488 0.0270 8.866 55.884 30.257 6611.747 6.314 134.582 2.076 0.84 534555. 0.3190
|
|
84.79 0.4264 0.7481 0.0446 0.0254 8.358 52.677 27.655 6232.367 5.951 123.009 2.013 0.84 535456. 0.2957
|
|
89.25 0.4488 0.7615 0.0403 0.0238 7.813 49.244 24.999 5826.141 5.564 111.197 1.946 0.84 536390. 0.2719
|
|
93.72 0.4713 0.7702 0.0360 0.0220 7.234 45.592 22.294 5394.053 5.151 99.163 1.875 0.84 537360. 0.2473
|
|
98.18 0.4937 0.7735 0.0315 0.0201 6.614 41.689 19.543 4932.309 4.710 86.929 1.797 0.84 538363. 0.2220
|
|
102.64 0.5161 0.7697 0.0270 0.0181 5.957 37.548 16.753 4442.404 4.242 74.517 1.710 0.84 539401. 0.1956
|
|
107.10 0.5386 0.7555 0.0225 0.0160 5.265 33.187 13.928 3926.360 3.749 61.951 1.609 0.85 540474. 0.1678
|
|
111.57 0.5610 0.7255 0.0179 0.0138 4.541 28.624 11.075 3386.533 3.234 49.259 1.483 0.85 541582. 0.1379
|
|
116.03 0.5835 0.6694 0.0132 0.0115 3.790 23.887 8.200 2826.120 2.699 36.474 1.316 0.85 542724. 0.1053
|
|
120.49 0.6059 0.5660 0.0086 0.0092 3.016 19.007 5.313 2248.804 2.147 23.632 1.072 0.85 543899. 0.0690
|
|
124.95 0.6283 0.3626 0.0039 0.0068 2.223 14.014 2.420 1657.973 1.583 10.764 0.662 0.85 545100. 0.0288
|
|
129.42 0.6508
|
|
|
|
|
|
|
|
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 0.1041 0.0452 19.767 113.264 78.051 14740.538 12.797 347.172 2.402 0.92 576066. 0.5929
|
|
4.90 0.0224 0.0509 0.1026 0.0452 19.758 113.213 76.913 14733.903 12.791 342.109 2.368 0.92 576443. 0.5802
|
|
9.80 0.0448 0.1003 0.1009 0.0451 19.714 112.959 75.659 14700.777 12.762 336.531 2.334 0.92 576850. 0.5673
|
|
14.70 0.0672 0.1483 0.0991 0.0449 19.631 112.481 74.284 14638.628 12.708 330.417 2.302 0.92 577288. 0.5543
|
|
19.60 0.0896 0.1950 0.0971 0.0446 19.506 111.764 72.783 14545.272 12.627 323.739 2.270 0.92 577757. 0.5410
|
|
24.49 0.1120 0.2403 0.0949 0.0442 19.337 110.796 71.151 14419.278 12.518 316.479 2.238 0.92 578259. 0.5275
|
|
29.39 0.1344 0.2844 0.0925 0.0437 19.123 109.572 69.385 14260.060 12.379 308.623 2.207 0.92 578794. 0.5136
|
|
34.29 0.1568 0.3271 0.0900 0.0431 18.864 108.088 67.482 14066.937 12.212 300.160 2.176 0.92 579363. 0.4994
|
|
39.19 0.1792 0.3685 0.0873 0.0424 18.559 106.339 65.441 13839.240 12.014 291.083 2.145 0.92 579966. 0.4848
|
|
44.09 0.2016 0.4085 0.0844 0.0416 18.206 104.320 63.262 13576.535 11.786 281.392 2.113 0.92 580603. 0.4697
|
|
48.99 0.2240 0.4471 0.0813 0.0407 17.807 102.033 60.949 13278.905 11.528 271.100 2.082 0.92 581275. 0.4541
|
|
53.89 0.2463 0.4842 0.0780 0.0397 17.362 99.483 58.506 12947.032 11.240 260.236 2.050 0.92 581982. 0.4380
|
|
58.79 0.2687 0.5198 0.0746 0.0386 16.872 96.677 55.943 12581.776 10.922 248.835 2.017 0.92 582723. 0.4215
|
|
63.69 0.2911 0.5536 0.0710 0.0374 16.339 93.618 53.266 12183.669 10.577 236.928 1.983 0.92 583500. 0.4044
|
|
68.59 0.3135 0.5858 0.0673 0.0360 15.761 90.306 50.482 11752.701 10.203 224.546 1.948 0.92 584313. 0.3868
|
|
73.48 0.3359 0.6161 0.0635 0.0346 15.138 86.739 47.598 11288.513 9.800 211.714 1.912 0.92 585161. 0.3687
|
|
78.38 0.3583 0.6445 0.0595 0.0331 14.471 82.915 44.618 10790.802 9.368 198.462 1.875 0.92 586045. 0.3500
|
|
83.28 0.3807 0.6707 0.0554 0.0315 13.758 78.831 41.551 10259.366 8.906 184.818 1.837 0.92 586966. 0.3309
|
|
88.18 0.4031 0.6946 0.0512 0.0297 13.000 74.486 38.401 9693.814 8.415 170.809 1.797 0.92 587923. 0.3111
|
|
93.08 0.4255 0.7160 0.0469 0.0279 12.194 69.872 35.176 9093.409 7.894 156.461 1.755 0.92 588916. 0.2908
|
|
97.98 0.4479 0.7340 0.0425 0.0259 11.347 65.017 31.879 8461.489 7.346 141.798 1.709 0.93 589947. 0.2696
|
|
102.88 0.4703 0.7421 0.0380 0.0241 10.538 60.381 28.507 7858.167 6.822 126.801 1.645 0.93 591015. 0.2455
|
|
107.78 0.4927 0.7364 0.0334 0.0224 9.782 56.047 25.065 7294.168 6.332 111.490 1.559 0.93 592120. 0.2180
|
|
112.68 0.5151 0.7198 0.0288 0.0206 9.003 51.586 21.569 6713.557 5.828 95.938 1.457 0.93 593262. 0.1891
|
|
117.57 0.5375 0.6884 0.0240 0.0188 8.210 47.040 18.026 6121.946 5.315 80.180 1.336 0.93 594442. 0.1584
|
|
122.47 0.5599 0.6371 0.0193 0.0169 7.405 42.432 14.447 5522.261 4.794 64.259 1.187 0.93 595659. 0.1260
|
|
127.37 0.5823 0.5580 0.0145 0.0151 6.599 37.813 10.842 4921.140 4.272 48.223 0.999 0.93 596914. 0.0919
|
|
132.27 0.6047 0.4395 0.0096 0.0133 5.798 33.220 7.224 4323.385 3.753 32.133 0.758 0.93 598205. 0.0569
|
|
137.17 0.6271 0.2635 0.0048 0.0114 5.008 28.693 3.608 3734.181 3.242 16.047 0.438 0.93 599527. 0.0233
|
|
142.07 0.6495 -0.0084 -0.0001 0.0095 4.162 23.847 -0.092 3103.552 2.694 -0.409 -0.013 0.94 600738. 0.0000
|
|
|
|
|
|
|