649 lines
115 KiB
Plaintext
649 lines
115 KiB
Plaintext
13x7 (13x7.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 0.0910 0.0434 0.001 0.082 0.083 0.968 0.009 0.368 38.807 0.05 16307. 0.5040
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0.30 0.0241 0.0492 0.0896 0.0438 0.001 0.083 0.082 0.976 0.009 0.363 37.882 0.05 16318. 0.4883
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0.59 0.0482 0.0961 0.0881 0.0442 0.001 0.083 0.080 0.984 0.009 0.357 36.949 0.05 16329. 0.4722
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0.89 0.0723 0.1404 0.0865 0.0445 0.001 0.084 0.079 0.991 0.009 0.350 36.012 0.05 16342. 0.4560
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1.19 0.0963 0.1824 0.0847 0.0447 0.001 0.084 0.077 0.997 0.010 0.343 35.073 0.05 16356. 0.4395
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1.48 0.1204 0.2218 0.0828 0.0449 0.001 0.085 0.075 1.001 0.010 0.335 34.132 0.05 16370. 0.4229
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1.78 0.1445 0.2589 0.0807 0.0451 0.001 0.085 0.073 1.004 0.010 0.327 33.190 0.05 16386. 0.4061
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2.08 0.1686 0.2934 0.0785 0.0451 0.001 0.085 0.071 1.006 0.010 0.318 32.248 0.05 16403. 0.3892
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2.37 0.1927 0.3255 0.0762 0.0451 0.001 0.085 0.069 1.005 0.010 0.308 31.304 0.05 16421. 0.3721
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2.67 0.2168 0.3552 0.0737 0.0450 0.001 0.085 0.067 1.002 0.010 0.298 30.358 0.05 16440. 0.3549
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2.97 0.2409 0.3823 0.0710 0.0448 0.001 0.084 0.065 0.997 0.010 0.288 29.409 0.05 16460. 0.3375
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3.26 0.2649 0.4068 0.0682 0.0444 0.001 0.084 0.062 0.990 0.009 0.276 28.454 0.05 16482. 0.3200
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3.56 0.2890 0.4288 0.0652 0.0440 0.001 0.083 0.059 0.980 0.009 0.264 27.490 0.05 16505. 0.3024
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3.85 0.3131 0.4481 0.0621 0.0434 0.001 0.082 0.057 0.967 0.009 0.252 26.517 0.05 16529. 0.2846
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4.15 0.3372 0.4646 0.0589 0.0427 0.001 0.080 0.054 0.952 0.009 0.238 25.528 0.05 16554. 0.2667
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4.45 0.3613 0.4781 0.0555 0.0419 0.001 0.079 0.051 0.935 0.009 0.225 24.521 0.05 16580. 0.2488
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4.74 0.3854 0.4885 0.0520 0.0410 0.001 0.077 0.047 0.914 0.009 0.211 23.489 0.05 16608. 0.2307
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5.04 0.4095 0.4956 0.0484 0.0400 0.001 0.075 0.044 0.892 0.009 0.196 22.427 0.05 16638. 0.2125
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5.34 0.4335 0.4990 0.0448 0.0389 0.001 0.073 0.041 0.866 0.008 0.181 21.325 0.05 16668. 0.1943
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5.63 0.4576 0.4983 0.0410 0.0376 0.001 0.071 0.037 0.839 0.008 0.166 20.175 0.05 16700. 0.1759
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5.93 0.4817 0.4930 0.0371 0.0363 0.001 0.068 0.034 0.808 0.008 0.150 18.965 0.05 16733. 0.1574
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6.23 0.5058 0.4826 0.0332 0.0348 0.001 0.066 0.030 0.775 0.007 0.134 17.679 0.05 16767. 0.1387
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6.52 0.5299 0.4661 0.0292 0.0332 0.001 0.063 0.027 0.740 0.007 0.118 16.298 0.05 16803. 0.1199
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6.82 0.5540 0.4424 0.0251 0.0315 0.001 0.059 0.023 0.702 0.007 0.102 14.797 0.05 16840. 0.1010
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7.12 0.5780 0.4100 0.0210 0.0297 0.001 0.056 0.019 0.661 0.006 0.085 13.142 0.05 16879. 0.0821
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7.41 0.6021 0.3668 0.0169 0.0277 0.001 0.052 0.015 0.618 0.006 0.068 11.287 0.05 16919. 0.0632
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7.71 0.6262 0.3099 0.0127 0.0257 0.001 0.048 0.012 0.572 0.005 0.051 9.171 0.05 16960. 0.0445
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8.01 0.6503 0.2353 0.0085 0.0235 0.001 0.044 0.008 0.524 0.005 0.034 6.704 0.05 17002. 0.0266
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8.30 0.6744 0.1366 0.0043 0.0213 0.001 0.040 0.004 0.474 0.005 0.017 3.754 0.05 17046. 0.0106
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8.60 0.6985 0.0043 0.0001 0.0189 0.001 0.036 0.000 0.422 0.004 0.000 0.115 0.05 17091. 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 0.0915 0.0375 0.009 0.283 0.333 6.686 0.032 1.481 22.589 0.10 32614. 0.5883
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0.60 0.0243 0.0577 0.0901 0.0380 0.009 0.286 0.328 6.766 0.032 1.459 21.984 0.10 32636. 0.5682
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1.20 0.0486 0.1122 0.0886 0.0384 0.009 0.289 0.322 6.840 0.033 1.434 21.380 0.10 32659. 0.5480
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1.80 0.0729 0.1636 0.0869 0.0388 0.009 0.292 0.316 6.908 0.033 1.408 20.780 0.10 32685. 0.5276
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2.39 0.0972 0.2118 0.0852 0.0391 0.009 0.294 0.310 6.967 0.033 1.379 20.185 0.10 32712. 0.5073
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2.99 0.1215 0.2571 0.0832 0.0394 0.009 0.296 0.303 7.015 0.033 1.348 19.596 0.10 32742. 0.4869
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3.59 0.1458 0.2993 0.0812 0.0396 0.009 0.298 0.296 7.051 0.034 1.315 19.013 0.10 32773. 0.4665
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4.19 0.1701 0.3386 0.0790 0.0397 0.009 0.299 0.287 7.072 0.034 1.279 18.437 0.10 32808. 0.4462
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4.79 0.1945 0.3750 0.0766 0.0397 0.009 0.299 0.279 7.078 0.034 1.240 17.868 0.10 32844. 0.4259
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5.39 0.2188 0.4086 0.0741 0.0396 0.009 0.299 0.270 7.067 0.034 1.199 17.305 0.10 32883. 0.4056
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5.98 0.2431 0.4394 0.0714 0.0395 0.009 0.297 0.260 7.037 0.034 1.156 16.748 0.10 32924. 0.3853
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6.58 0.2674 0.4674 0.0685 0.0392 0.009 0.295 0.249 6.986 0.033 1.110 16.195 0.10 32968. 0.3651
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7.18 0.2917 0.4926 0.0655 0.0388 0.009 0.292 0.239 6.914 0.033 1.061 15.646 0.10 33014. 0.3449
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7.78 0.3160 0.5150 0.0624 0.0383 0.009 0.288 0.227 6.820 0.033 1.010 15.099 0.10 33063. 0.3247
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8.38 0.3403 0.5345 0.0591 0.0376 0.009 0.283 0.215 6.704 0.032 0.957 14.551 0.10 33114. 0.3046
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8.98 0.3646 0.5510 0.0557 0.0368 0.009 0.277 0.203 6.565 0.031 0.901 14.001 0.10 33168. 0.2845
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9.58 0.3889 0.5644 0.0521 0.0359 0.009 0.271 0.190 6.404 0.031 0.844 13.445 0.10 33225. 0.2644
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10.17 0.4132 0.5745 0.0485 0.0349 0.008 0.263 0.177 6.221 0.030 0.786 12.880 0.10 33284. 0.2443
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10.77 0.4375 0.5809 0.0448 0.0337 0.008 0.254 0.163 6.014 0.029 0.725 12.301 0.10 33346. 0.2242
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11.37 0.4618 0.5833 0.0410 0.0325 0.008 0.244 0.149 5.785 0.028 0.664 11.702 0.10 33411. 0.2040
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11.97 0.4861 0.5812 0.0371 0.0310 0.007 0.234 0.135 5.532 0.026 0.601 11.076 0.10 33478. 0.1837
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12.57 0.5104 0.5737 0.0331 0.0295 0.007 0.222 0.121 5.256 0.025 0.537 10.413 0.10 33548. 0.1633
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13.17 0.5348 0.5599 0.0291 0.0278 0.007 0.209 0.106 4.957 0.024 0.472 9.701 0.10 33621. 0.1426
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13.76 0.5591 0.5384 0.0250 0.0260 0.006 0.196 0.091 4.635 0.022 0.406 8.922 0.10 33697. 0.1216
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14.36 0.5834 0.5070 0.0209 0.0241 0.006 0.181 0.076 4.289 0.020 0.339 8.051 0.10 33775. 0.1003
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14.96 0.6077 0.4627 0.0168 0.0220 0.005 0.166 0.061 3.921 0.019 0.271 7.054 0.11 33856. 0.0786
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15.56 0.6320 0.4007 0.0126 0.0198 0.005 0.149 0.046 3.531 0.017 0.203 5.874 0.11 33939. 0.0567
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16.16 0.6563 0.3135 0.0084 0.0175 0.004 0.132 0.030 3.120 0.015 0.135 4.425 0.11 34026. 0.0348
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16.76 0.6806 0.1879 0.0042 0.0151 0.004 0.114 0.015 2.689 0.013 0.067 2.557 0.11 34115. 0.0142
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17.36 0.7049 -0.0013 0.0000 0.0126 0.003 0.095 0.000 2.239 0.011 0.000 -0.018 0.11 34205. 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 0.0918 0.0351 0.028 0.595 0.752 21.105 0.067 3.344 16.156 0.15 48921. 0.6322
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0.92 0.0248 0.0630 0.0904 0.0356 0.029 0.603 0.740 21.398 0.068 3.292 15.690 0.15 48954. 0.6093
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1.83 0.0496 0.1223 0.0888 0.0360 0.029 0.611 0.728 21.672 0.069 3.237 15.229 0.15 48990. 0.5863
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2.75 0.0744 0.1780 0.0872 0.0364 0.029 0.618 0.714 21.921 0.070 3.176 14.773 0.15 49029. 0.5634
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3.67 0.0992 0.2301 0.0853 0.0368 0.030 0.624 0.699 22.139 0.070 3.110 14.323 0.15 49071. 0.5405
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4.58 0.1240 0.2788 0.0834 0.0371 0.030 0.629 0.683 22.320 0.071 3.038 13.880 0.15 49117. 0.5178
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5.50 0.1489 0.3240 0.0813 0.0373 0.030 0.633 0.666 22.457 0.071 2.961 13.445 0.15 49166. 0.4951
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6.41 0.1737 0.3660 0.0790 0.0375 0.030 0.635 0.647 22.543 0.072 2.878 13.018 0.15 49219. 0.4726
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7.33 0.1985 0.4048 0.0765 0.0375 0.030 0.636 0.627 22.574 0.072 2.789 12.598 0.16 49275. 0.4503
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8.25 0.2233 0.4406 0.0739 0.0375 0.030 0.635 0.606 22.541 0.072 2.694 12.186 0.16 49335. 0.4280
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9.16 0.2481 0.4732 0.0712 0.0373 0.030 0.632 0.583 22.440 0.071 2.593 11.781 0.16 49399. 0.4060
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10.08 0.2729 0.5029 0.0682 0.0370 0.030 0.627 0.559 22.265 0.071 2.485 11.382 0.16 49467. 0.3840
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11.00 0.2977 0.5297 0.0651 0.0366 0.030 0.620 0.533 22.013 0.070 2.372 10.989 0.16 49539. 0.3622
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11.91 0.3225 0.5535 0.0619 0.0360 0.029 0.611 0.507 21.681 0.069 2.254 10.599 0.16 49615. 0.3405
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12.83 0.3473 0.5743 0.0585 0.0354 0.029 0.599 0.479 21.269 0.068 2.130 10.212 0.16 49694. 0.3190
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13.74 0.3721 0.5921 0.0549 0.0345 0.028 0.585 0.450 20.776 0.066 2.002 9.826 0.16 49778. 0.2976
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14.66 0.3970 0.6066 0.0513 0.0336 0.027 0.569 0.420 20.201 0.064 1.870 9.438 0.16 49866. 0.2762
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15.58 0.4218 0.6177 0.0476 0.0325 0.026 0.551 0.390 19.543 0.062 1.734 9.046 0.16 49959. 0.2549
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16.49 0.4466 0.6251 0.0437 0.0313 0.025 0.530 0.358 18.801 0.060 1.594 8.646 0.16 50055. 0.2336
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17.41 0.4714 0.6284 0.0398 0.0299 0.024 0.506 0.326 17.975 0.057 1.451 8.233 0.16 50156. 0.2123
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18.33 0.4962 0.6268 0.0358 0.0284 0.023 0.481 0.294 17.064 0.054 1.306 7.802 0.16 50260. 0.1908
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19.24 0.5210 0.6196 0.0318 0.0267 0.022 0.453 0.260 16.068 0.051 1.157 7.345 0.16 50369. 0.1691
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20.16 0.5458 0.6055 0.0276 0.0249 0.020 0.422 0.226 14.986 0.048 1.007 6.851 0.16 50483. 0.1471
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21.07 0.5706 0.5825 0.0235 0.0230 0.019 0.389 0.192 13.819 0.044 0.854 6.305 0.16 50600. 0.1247
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21.99 0.5954 0.5479 0.0192 0.0209 0.017 0.354 0.157 12.569 0.040 0.700 5.683 0.16 50722. 0.1018
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22.91 0.6202 0.4970 0.0150 0.0187 0.015 0.317 0.123 11.236 0.036 0.545 4.949 0.16 50848. 0.0782
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23.82 0.6451 0.4223 0.0107 0.0163 0.013 0.277 0.088 9.824 0.031 0.390 4.044 0.16 50978. 0.0540
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24.74 0.6699 0.3101 0.0064 0.0139 0.011 0.235 0.053 8.337 0.027 0.234 2.859 0.16 51113. 0.0296
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25.66 0.6947 0.1325 0.0021 0.0113 0.009 0.191 0.018 6.779 0.022 0.078 1.178 0.16 51251. 0.0071
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26.57 0.7195
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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 0.0338 0.065 1.017 1.341 48.128 0.115 5.965 12.638 0.21 65226. 0.6605
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1.20 0.0244 0.0647 0.0907 0.0342 0.065 1.032 1.321 48.836 0.117 5.875 12.268 0.21 65270. 0.6364
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2.40 0.0488 0.1255 0.0892 0.0347 0.066 1.046 1.299 49.502 0.118 5.778 11.902 0.21 65317. 0.6123
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3.61 0.0732 0.1825 0.0876 0.0351 0.067 1.059 1.275 50.112 0.120 5.672 11.542 0.21 65368. 0.5883
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4.81 0.0976 0.2359 0.0858 0.0355 0.068 1.070 1.249 50.651 0.121 5.557 11.188 0.21 65423. 0.5645
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6.01 0.1221 0.2857 0.0839 0.0358 0.069 1.080 1.221 51.105 0.122 5.433 10.841 0.21 65483. 0.5408
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7.21 0.1465 0.3320 0.0818 0.0361 0.069 1.087 1.191 51.460 0.123 5.299 10.501 0.21 65547. 0.5173
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8.41 0.1709 0.3751 0.0796 0.0363 0.069 1.092 1.159 51.701 0.123 5.155 10.168 0.21 65616. 0.4941
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9.62 0.1953 0.4149 0.0772 0.0363 0.069 1.095 1.124 51.812 0.124 5.001 9.842 0.21 65689. 0.4710
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10.82 0.2197 0.4517 0.0747 0.0363 0.069 1.094 1.087 51.781 0.124 4.836 9.523 0.21 65768. 0.4482
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12.02 0.2441 0.4854 0.0719 0.0362 0.069 1.090 1.048 51.592 0.123 4.660 9.211 0.21 65851. 0.4256
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13.22 0.2685 0.5162 0.0691 0.0359 0.069 1.083 1.006 51.234 0.122 4.474 8.905 0.21 65939. 0.4031
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14.43 0.2929 0.5442 0.0660 0.0356 0.068 1.071 0.962 50.696 0.121 4.278 8.605 0.21 66032. 0.3809
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15.63 0.3174 0.5693 0.0629 0.0350 0.067 1.056 0.915 49.974 0.119 4.072 8.309 0.21 66131. 0.3588
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16.83 0.3418 0.5915 0.0596 0.0344 0.066 1.037 0.867 49.065 0.117 3.857 8.017 0.21 66235. 0.3370
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18.03 0.3662 0.6109 0.0561 0.0336 0.064 1.014 0.817 47.966 0.115 3.635 7.727 0.21 66343. 0.3153
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19.23 0.3906 0.6272 0.0526 0.0327 0.063 0.986 0.765 46.675 0.111 3.405 7.439 0.21 66458. 0.2938
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20.44 0.4150 0.6405 0.0489 0.0317 0.061 0.955 0.712 45.191 0.108 3.168 7.149 0.21 66577. 0.2723
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21.64 0.4394 0.6503 0.0452 0.0305 0.058 0.919 0.658 43.511 0.104 2.925 6.856 0.21 66702. 0.2509
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22.84 0.4638 0.6565 0.0413 0.0292 0.056 0.880 0.602 41.632 0.099 2.677 6.556 0.21 66832. 0.2295
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24.04 0.4882 0.6584 0.0374 0.0277 0.053 0.836 0.545 39.555 0.094 2.423 6.246 0.21 66968. 0.2081
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25.24 0.5127 0.6553 0.0334 0.0261 0.050 0.788 0.487 37.276 0.089 2.165 5.922 0.21 67109. 0.1865
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26.45 0.5371 0.6463 0.0294 0.0244 0.047 0.735 0.428 34.797 0.083 1.902 5.575 0.21 67256. 0.1646
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27.65 0.5615 0.6298 0.0253 0.0225 0.043 0.679 0.368 32.116 0.077 1.636 5.196 0.21 67408. 0.1422
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28.85 0.5859 0.6033 0.0211 0.0205 0.039 0.618 0.307 29.237 0.070 1.368 4.770 0.21 67566. 0.1194
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30.05 0.6103 0.5632 0.0169 0.0183 0.035 0.553 0.247 26.163 0.062 1.097 4.275 0.21 67729. 0.0958
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31.25 0.6347 0.5030 0.0127 0.0161 0.031 0.484 0.185 22.899 0.055 0.824 3.671 0.21 67898. 0.0713
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32.46 0.6591 0.4113 0.0085 0.0136 0.026 0.411 0.124 19.453 0.046 0.551 2.891 0.21 68072. 0.0459
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33.66 0.6835 0.2651 0.0043 0.0111 0.021 0.335 0.063 15.836 0.038 0.279 1.797 0.21 68251. 0.0203
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34.86 0.7079 0.0089 0.0001 0.0084 0.016 0.254 0.002 12.041 0.029 0.007 0.058 0.21 68432. 0.0001
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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 0.0924 0.0329 0.123 1.551 2.103 91.726 0.175 9.355 10.400 0.26 81531. 0.6807
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1.51 0.0245 0.0666 0.0911 0.0334 0.125 1.575 2.072 93.150 0.178 9.216 10.088 0.26 81586. 0.6554
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3.01 0.0490 0.1292 0.0895 0.0339 0.127 1.597 2.038 94.491 0.180 9.064 9.781 0.26 81645. 0.6302
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4.52 0.0734 0.1879 0.0879 0.0344 0.128 1.618 2.000 95.721 0.183 8.898 9.479 0.26 81709. 0.6051
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6.03 0.0979 0.2426 0.0861 0.0348 0.130 1.637 1.960 96.813 0.185 8.718 9.183 0.26 81778. 0.5803
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7.53 0.1224 0.2937 0.0842 0.0351 0.131 1.652 1.916 97.737 0.187 8.524 8.893 0.26 81853. 0.5556
|
|
9.04 0.1469 0.3412 0.0821 0.0354 0.132 1.664 1.869 98.464 0.188 8.314 8.610 0.26 81934. 0.5313
|
|
10.55 0.1714 0.3853 0.0799 0.0355 0.133 1.673 1.818 98.965 0.189 8.087 8.333 0.26 82020. 0.5072
|
|
12.05 0.1958 0.4261 0.0775 0.0356 0.133 1.677 1.764 99.210 0.189 7.845 8.063 0.26 82112. 0.4833
|
|
13.56 0.2203 0.4637 0.0750 0.0356 0.133 1.676 1.705 99.171 0.189 7.586 7.800 0.26 82211. 0.4598
|
|
15.07 0.2448 0.4983 0.0722 0.0355 0.133 1.670 1.643 98.820 0.189 7.310 7.543 0.26 82315. 0.4365
|
|
16.58 0.2693 0.5299 0.0693 0.0352 0.132 1.659 1.578 98.130 0.187 7.017 7.292 0.26 82426. 0.4134
|
|
18.08 0.2938 0.5586 0.0663 0.0349 0.130 1.641 1.508 97.085 0.185 6.709 7.046 0.26 82544. 0.3906
|
|
19.59 0.3182 0.5844 0.0631 0.0344 0.128 1.617 1.435 95.672 0.183 6.385 6.805 0.26 82667. 0.3680
|
|
21.10 0.3427 0.6074 0.0597 0.0337 0.126 1.587 1.360 93.885 0.179 6.047 6.568 0.26 82798. 0.3457
|
|
22.60 0.3672 0.6276 0.0563 0.0329 0.123 1.550 1.281 91.720 0.175 5.697 6.334 0.26 82934. 0.3235
|
|
24.11 0.3917 0.6448 0.0527 0.0320 0.120 1.507 1.199 89.173 0.170 5.335 6.101 0.26 83078. 0.3016
|
|
25.62 0.4162 0.6590 0.0490 0.0310 0.116 1.458 1.116 86.238 0.165 4.963 5.868 0.26 83228. 0.2798
|
|
27.12 0.4406 0.6699 0.0453 0.0298 0.111 1.402 1.030 82.912 0.158 4.581 5.634 0.26 83385. 0.2580
|
|
28.63 0.4651 0.6771 0.0414 0.0284 0.106 1.339 0.942 79.189 0.151 4.190 5.395 0.26 83549. 0.2363
|
|
30.14 0.4896 0.6803 0.0375 0.0270 0.101 1.269 0.852 75.068 0.143 3.791 5.149 0.26 83720. 0.2145
|
|
31.64 0.5141 0.6786 0.0334 0.0253 0.095 1.193 0.761 70.545 0.135 3.384 4.892 0.26 83897. 0.1926
|
|
33.15 0.5386 0.6711 0.0294 0.0236 0.088 1.109 0.668 65.619 0.125 2.972 4.618 0.26 84081. 0.1704
|
|
34.66 0.5630 0.6562 0.0252 0.0216 0.081 1.019 0.574 60.291 0.115 2.554 4.319 0.26 84273. 0.1477
|
|
36.16 0.5875 0.6314 0.0211 0.0196 0.073 0.922 0.479 54.567 0.104 2.131 3.983 0.26 84471. 0.1244
|
|
37.67 0.6120 0.5927 0.0168 0.0174 0.065 0.819 0.383 48.451 0.093 1.705 3.589 0.26 84676. 0.1003
|
|
39.18 0.6365 0.5331 0.0126 0.0151 0.056 0.709 0.287 41.957 0.080 1.277 3.104 0.26 84888. 0.0751
|
|
40.68 0.6610 0.4396 0.0084 0.0126 0.047 0.593 0.191 35.100 0.067 0.848 2.465 0.26 85107. 0.0486
|
|
42.19 0.6854 0.2843 0.0042 0.0100 0.037 0.472 0.095 27.901 0.053 0.421 1.537 0.26 85332. 0.0213
|
|
43.70 0.7099 -0.0075 -0.0001 0.0073 0.027 0.344 -0.002 20.329 0.039 -0.008 -0.039 0.26 85556. 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 0.0928 0.0324 0.209 2.198 3.042 156.010 0.248 13.529 8.843 0.31 97835. 0.6961
|
|
1.83 0.0247 0.0687 0.0914 0.0329 0.213 2.234 2.996 158.551 0.252 13.327 8.571 0.31 97901. 0.6697
|
|
3.65 0.0495 0.1330 0.0899 0.0334 0.216 2.267 2.947 160.945 0.256 13.106 8.304 0.31 97973. 0.6434
|
|
5.48 0.0742 0.1933 0.0883 0.0339 0.219 2.298 2.892 163.141 0.260 12.865 8.042 0.31 98051. 0.6173
|
|
7.31 0.0990 0.2494 0.0865 0.0343 0.221 2.326 2.834 165.091 0.263 12.604 7.785 0.31 98135. 0.5915
|
|
9.14 0.1237 0.3018 0.0845 0.0346 0.224 2.349 2.770 166.741 0.265 12.319 7.534 0.31 98226. 0.5659
|
|
10.96 0.1484 0.3504 0.0824 0.0349 0.225 2.367 2.701 168.038 0.267 12.012 7.290 0.31 98325. 0.5407
|
|
12.79 0.1732 0.3954 0.0801 0.0351 0.227 2.380 2.626 168.929 0.269 11.682 7.051 0.31 98430. 0.5158
|
|
14.62 0.1979 0.4370 0.0777 0.0352 0.227 2.386 2.546 169.360 0.270 11.326 6.820 0.31 98543. 0.4912
|
|
16.45 0.2226 0.4754 0.0751 0.0352 0.227 2.385 2.461 169.281 0.269 10.947 6.594 0.31 98663. 0.4669
|
|
18.27 0.2474 0.5106 0.0723 0.0350 0.226 2.376 2.370 168.640 0.268 10.542 6.374 0.31 98790. 0.4429
|
|
20.10 0.2721 0.5428 0.0694 0.0348 0.224 2.358 2.273 167.393 0.266 10.112 6.160 0.31 98926. 0.4192
|
|
21.93 0.2969 0.5721 0.0663 0.0344 0.222 2.331 2.172 165.506 0.263 9.659 5.951 0.31 99069. 0.3958
|
|
23.75 0.3216 0.5984 0.0630 0.0339 0.219 2.296 2.065 162.961 0.259 9.184 5.747 0.31 99221. 0.3727
|
|
25.58 0.3463 0.6220 0.0596 0.0332 0.214 2.250 1.953 159.747 0.254 8.688 5.546 0.31 99380. 0.3498
|
|
27.41 0.3711 0.6426 0.0561 0.0324 0.209 2.196 1.838 155.855 0.248 8.174 5.348 0.31 99547. 0.3272
|
|
29.24 0.3958 0.6603 0.0524 0.0314 0.203 2.131 1.718 151.276 0.241 7.643 5.152 0.31 99723. 0.3048
|
|
31.06 0.4205 0.6749 0.0487 0.0303 0.196 2.057 1.595 146.003 0.232 7.096 4.956 0.31 99906. 0.2825
|
|
32.89 0.4453 0.6862 0.0448 0.0291 0.188 1.973 1.469 140.028 0.223 6.535 4.759 0.31 100098. 0.2604
|
|
34.72 0.4700 0.6939 0.0409 0.0277 0.179 1.878 1.340 133.341 0.212 5.962 4.559 0.31 100299. 0.2382
|
|
36.54 0.4948 0.6974 0.0369 0.0262 0.169 1.774 1.209 125.939 0.200 5.376 4.353 0.31 100507. 0.2160
|
|
38.37 0.5195 0.6960 0.0328 0.0245 0.158 1.660 1.075 117.816 0.188 4.781 4.138 0.31 100724. 0.1936
|
|
40.20 0.5442 0.6886 0.0287 0.0226 0.146 1.535 0.939 108.971 0.173 4.176 3.907 0.31 100950. 0.1709
|
|
42.03 0.5690 0.6734 0.0244 0.0207 0.133 1.400 0.801 99.408 0.158 3.563 3.655 0.31 101184. 0.1477
|
|
43.85 0.5937 0.6476 0.0202 0.0185 0.120 1.256 0.662 89.135 0.142 2.944 3.368 0.31 101426. 0.1237
|
|
45.68 0.6185 0.6063 0.0159 0.0162 0.105 1.101 0.522 78.166 0.124 2.321 3.028 0.32 101677. 0.0987
|
|
47.51 0.6432 0.5411 0.0116 0.0138 0.089 0.937 0.381 66.524 0.106 1.695 2.598 0.32 101937. 0.0724
|
|
49.34 0.6679 0.4345 0.0073 0.0113 0.073 0.764 0.240 54.241 0.086 1.068 2.009 0.32 102204. 0.0444
|
|
51.16 0.6927 0.2455 0.0030 0.0086 0.055 0.583 0.100 41.354 0.066 0.444 1.095 0.32 102479. 0.0156
|
|
52.99 0.7174
|
|
|
|
|
|
|
|
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 0.0933 0.0321 0.329 2.962 4.160 245.300 0.335 18.506 7.693 0.36 114136. 0.7082
|
|
2.14 0.0248 0.0698 0.0919 0.0326 0.334 3.012 4.099 249.425 0.340 18.232 7.454 0.36 114214. 0.6811
|
|
4.27 0.0496 0.1352 0.0904 0.0331 0.340 3.059 4.031 253.315 0.346 17.931 7.218 0.36 114298. 0.6542
|
|
6.41 0.0744 0.1964 0.0887 0.0336 0.344 3.102 3.958 256.889 0.350 17.604 6.988 0.36 114390. 0.6274
|
|
8.55 0.0992 0.2534 0.0869 0.0340 0.349 3.140 3.877 260.064 0.355 17.247 6.762 0.36 114489. 0.6010
|
|
10.68 0.1240 0.3064 0.0850 0.0344 0.352 3.173 3.790 262.757 0.358 16.859 6.543 0.36 114596. 0.5749
|
|
12.82 0.1488 0.3557 0.0829 0.0347 0.355 3.198 3.696 264.880 0.361 16.440 6.329 0.36 114711. 0.5492
|
|
14.96 0.1736 0.4013 0.0806 0.0349 0.357 3.216 3.594 266.346 0.363 15.987 6.121 0.36 114834. 0.5238
|
|
17.09 0.1984 0.4435 0.0781 0.0349 0.358 3.225 3.485 267.071 0.364 15.502 5.919 0.36 114966. 0.4987
|
|
19.23 0.2231 0.4824 0.0755 0.0349 0.358 3.224 3.368 266.971 0.364 14.982 5.722 0.36 115107. 0.4740
|
|
21.37 0.2479 0.5181 0.0727 0.0348 0.357 3.211 3.244 265.963 0.363 14.427 5.531 0.36 115257. 0.4496
|
|
23.50 0.2727 0.5508 0.0698 0.0345 0.354 3.187 3.111 263.975 0.360 13.839 5.346 0.36 115416. 0.4256
|
|
25.64 0.2975 0.5805 0.0666 0.0341 0.350 3.151 2.971 260.953 0.356 13.217 5.165 0.36 115584. 0.4019
|
|
27.78 0.3223 0.6074 0.0633 0.0336 0.344 3.102 2.825 256.867 0.350 12.565 4.988 0.36 115761. 0.3784
|
|
29.91 0.3471 0.6314 0.0599 0.0329 0.338 3.039 2.672 251.699 0.343 11.885 4.815 0.36 115948. 0.3553
|
|
32.05 0.3719 0.6526 0.0564 0.0321 0.329 2.964 2.513 245.435 0.335 11.180 4.645 0.36 116144. 0.3324
|
|
34.19 0.3967 0.6709 0.0527 0.0312 0.319 2.875 2.350 238.061 0.325 10.451 4.477 0.36 116350. 0.3097
|
|
36.32 0.4215 0.6862 0.0489 0.0300 0.308 2.772 2.181 229.563 0.313 9.701 4.309 0.36 116565. 0.2872
|
|
38.46 0.4463 0.6982 0.0450 0.0288 0.295 2.656 2.008 219.929 0.300 8.931 4.141 0.36 116790. 0.2649
|
|
40.60 0.4711 0.7067 0.0411 0.0274 0.280 2.525 1.831 209.144 0.285 8.144 3.971 0.37 117025. 0.2425
|
|
42.73 0.4959 0.7111 0.0370 0.0258 0.264 2.381 1.650 197.201 0.269 7.341 3.796 0.37 117269. 0.2201
|
|
44.87 0.5207 0.7107 0.0329 0.0241 0.247 2.223 1.467 184.093 0.251 6.523 3.613 0.37 117524. 0.1975
|
|
47.01 0.5455 0.7045 0.0287 0.0222 0.228 2.050 1.280 169.817 0.232 5.693 3.419 0.37 117788. 0.1746
|
|
49.14 0.5703 0.6905 0.0245 0.0202 0.207 1.864 1.091 154.380 0.211 4.852 3.205 0.37 118062. 0.1511
|
|
51.28 0.5951 0.6660 0.0202 0.0180 0.185 1.664 0.900 137.793 0.188 4.003 2.962 0.37 118346. 0.1268
|
|
53.42 0.6199 0.6259 0.0159 0.0157 0.161 1.450 0.708 120.083 0.164 3.148 2.673 0.37 118640. 0.1015
|
|
55.55 0.6446 0.5612 0.0115 0.0133 0.136 1.223 0.515 101.287 0.138 2.289 2.304 0.37 118944. 0.0746
|
|
57.69 0.6694 0.4526 0.0072 0.0107 0.109 0.984 0.321 81.457 0.111 1.429 1.790 0.37 119258. 0.0458
|
|
59.83 0.6942 0.2526 0.0029 0.0079 0.081 0.732 0.129 60.651 0.083 0.573 0.963 0.37 119579. 0.0156
|
|
61.96 0.7190
|
|
|
|
|
|
|
|
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 0.0938 0.0319 0.488 3.848 5.465 364.193 0.435 24.308 6.806 0.41 130436. 0.7181
|
|
2.44 0.0247 0.0704 0.0924 0.0325 0.497 3.914 5.385 370.457 0.442 23.953 6.593 0.41 130525. 0.6906
|
|
4.87 0.0495 0.1363 0.0909 0.0330 0.505 3.976 5.298 376.370 0.449 23.564 6.384 0.41 130621. 0.6632
|
|
7.31 0.0742 0.1979 0.0893 0.0335 0.512 4.034 5.202 381.810 0.456 23.138 6.180 0.41 130725. 0.6362
|
|
9.74 0.0989 0.2554 0.0875 0.0339 0.519 4.085 5.098 386.654 0.462 22.674 5.980 0.41 130838. 0.6094
|
|
12.18 0.1236 0.3088 0.0856 0.0343 0.524 4.129 4.984 390.773 0.466 22.171 5.785 0.41 130960. 0.5830
|
|
14.61 0.1484 0.3585 0.0835 0.0345 0.528 4.163 4.862 394.039 0.470 21.625 5.596 0.41 131091. 0.5569
|
|
17.05 0.1731 0.4045 0.0812 0.0347 0.531 4.187 4.729 396.319 0.473 21.036 5.412 0.41 131232. 0.5313
|
|
19.48 0.1978 0.4470 0.0787 0.0348 0.533 4.200 4.587 397.486 0.474 20.403 5.234 0.41 131383. 0.5060
|
|
21.92 0.2225 0.4863 0.0761 0.0348 0.533 4.199 4.434 397.415 0.474 19.725 5.061 0.41 131543. 0.4810
|
|
24.35 0.2473 0.5224 0.0733 0.0347 0.531 4.184 4.272 395.983 0.473 19.001 4.893 0.41 131714. 0.4565
|
|
26.79 0.2720 0.5555 0.0704 0.0345 0.527 4.153 4.099 393.079 0.469 18.233 4.730 0.41 131895. 0.4322
|
|
29.22 0.2967 0.5856 0.0672 0.0341 0.521 4.106 3.917 388.621 0.464 17.421 4.571 0.41 132087. 0.4083
|
|
31.66 0.3215 0.6130 0.0639 0.0335 0.513 4.042 3.725 382.563 0.457 16.569 4.416 0.41 132289. 0.3847
|
|
34.09 0.3462 0.6375 0.0605 0.0329 0.503 3.961 3.525 374.877 0.447 15.680 4.265 0.42 132501. 0.3614
|
|
36.53 0.3709 0.6593 0.0570 0.0320 0.490 3.862 3.318 365.542 0.436 14.757 4.117 0.42 132725. 0.3384
|
|
38.96 0.3956 0.6782 0.0533 0.0311 0.475 3.746 3.103 354.538 0.423 13.804 3.970 0.42 132959. 0.3157
|
|
41.40 0.4204 0.6942 0.0495 0.0300 0.458 3.612 2.883 341.844 0.408 12.822 3.825 0.42 133204. 0.2931
|
|
43.84 0.4451 0.7071 0.0456 0.0287 0.439 3.460 2.656 327.440 0.391 11.814 3.679 0.42 133460. 0.2706
|
|
46.27 0.4698 0.7165 0.0416 0.0273 0.417 3.289 2.424 311.308 0.372 10.784 3.532 0.42 133728. 0.2482
|
|
48.71 0.4946 0.7221 0.0376 0.0257 0.393 3.100 2.188 293.433 0.350 9.732 3.382 0.42 134006. 0.2258
|
|
51.14 0.5193 0.7231 0.0334 0.0240 0.367 2.893 1.947 273.804 0.327 8.661 3.225 0.42 134295. 0.2031
|
|
53.58 0.5440 0.7186 0.0292 0.0221 0.338 2.667 1.703 252.419 0.301 7.573 3.059 0.42 134596. 0.1802
|
|
56.01 0.5687 0.7067 0.0250 0.0201 0.307 2.422 1.455 229.284 0.274 6.471 2.878 0.42 134908. 0.1567
|
|
58.45 0.5935 0.6849 0.0207 0.0179 0.274 2.160 1.205 204.418 0.244 5.358 2.673 0.42 135231. 0.1324
|
|
60.88 0.6182 0.6483 0.0164 0.0156 0.239 1.879 0.952 177.858 0.212 4.237 2.429 0.42 135566. 0.1070
|
|
63.32 0.6429 0.5883 0.0120 0.0131 0.201 1.581 0.699 149.658 0.179 3.110 2.119 0.42 135912. 0.0800
|
|
65.75 0.6676 0.4861 0.0077 0.0105 0.161 1.267 0.446 119.897 0.143 1.983 1.686 0.42 136268. 0.0508
|
|
68.19 0.6924 0.2952 0.0033 0.0078 0.119 0.937 0.193 88.662 0.106 0.859 0.988 0.42 136634. 0.0196
|
|
70.62 0.7171
|
|
|
|
|
|
|
|
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 0.0944 0.0319 0.694 4.861 6.961 517.649 0.549 30.963 6.099 0.46 146734. 0.7263
|
|
2.72 0.0245 0.0704 0.0931 0.0324 0.706 4.946 6.862 526.682 0.559 30.521 5.909 0.46 146832. 0.6987
|
|
5.44 0.0491 0.1364 0.0916 0.0330 0.718 5.026 6.752 535.221 0.568 30.035 5.722 0.46 146940. 0.6712
|
|
8.15 0.0736 0.1980 0.0900 0.0334 0.728 5.100 6.633 543.090 0.576 29.504 5.540 0.46 147056. 0.6440
|
|
10.87 0.0981 0.2555 0.0882 0.0339 0.738 5.166 6.503 550.117 0.584 28.924 5.362 0.46 147183. 0.6171
|
|
13.59 0.1227 0.3091 0.0863 0.0342 0.746 5.223 6.361 556.122 0.590 28.294 5.188 0.46 147319. 0.5906
|
|
16.31 0.1472 0.3588 0.0842 0.0345 0.752 5.268 6.208 560.919 0.595 27.611 5.020 0.46 147465. 0.5645
|
|
19.02 0.1717 0.4050 0.0820 0.0347 0.757 5.300 6.042 564.324 0.599 26.874 4.856 0.46 147622. 0.5388
|
|
21.74 0.1962 0.4478 0.0795 0.0349 0.759 5.317 5.863 566.155 0.601 26.081 4.697 0.47 147790. 0.5134
|
|
24.46 0.2208 0.4872 0.0769 0.0349 0.759 5.318 5.672 566.237 0.601 25.231 4.544 0.47 147968. 0.4884
|
|
27.18 0.2453 0.5236 0.0742 0.0347 0.757 5.300 5.468 564.398 0.599 24.323 4.395 0.47 148158. 0.4638
|
|
29.90 0.2698 0.5570 0.0712 0.0345 0.752 5.264 5.252 560.478 0.595 23.359 4.250 0.47 148360. 0.4396
|
|
32.61 0.2944 0.5875 0.0681 0.0341 0.743 5.206 5.022 554.355 0.588 22.339 4.109 0.47 148573. 0.4157
|
|
35.33 0.3189 0.6153 0.0649 0.0336 0.732 5.127 4.782 545.963 0.579 21.269 3.972 0.47 148797. 0.3921
|
|
38.05 0.3434 0.6404 0.0614 0.0330 0.718 5.027 4.530 535.260 0.568 20.151 3.839 0.47 149034. 0.3688
|
|
40.77 0.3680 0.6627 0.0579 0.0322 0.700 4.904 4.269 522.216 0.554 18.990 3.708 0.47 149282. 0.3458
|
|
43.49 0.3925 0.6823 0.0542 0.0312 0.680 4.760 3.999 506.803 0.538 17.789 3.579 0.47 149542. 0.3231
|
|
46.20 0.4170 0.6992 0.0505 0.0301 0.656 4.592 3.721 488.993 0.519 16.552 3.452 0.47 149815. 0.3005
|
|
48.92 0.4415 0.7130 0.0466 0.0289 0.629 4.402 3.436 468.759 0.497 15.283 3.325 0.47 150099. 0.2781
|
|
51.64 0.4661 0.7237 0.0426 0.0275 0.598 4.189 3.144 446.074 0.473 13.983 3.197 0.47 150396. 0.2558
|
|
54.36 0.4906 0.7307 0.0386 0.0259 0.564 3.953 2.845 420.916 0.447 12.657 3.066 0.47 150705. 0.2335
|
|
57.07 0.5151 0.7335 0.0345 0.0242 0.527 3.693 2.542 393.270 0.417 11.306 2.931 0.47 151026. 0.2109
|
|
59.79 0.5397 0.7311 0.0303 0.0224 0.487 3.410 2.233 363.129 0.385 9.933 2.789 0.47 151360. 0.1881
|
|
62.51 0.5642 0.7222 0.0260 0.0203 0.443 3.104 1.920 330.500 0.351 8.542 2.635 0.47 151706. 0.1648
|
|
65.23 0.5887 0.7043 0.0218 0.0182 0.396 2.774 1.604 295.407 0.313 7.135 2.463 0.47 152064. 0.1408
|
|
67.95 0.6133 0.6734 0.0174 0.0159 0.346 2.422 1.285 257.894 0.274 5.717 2.261 0.47 152435. 0.1157
|
|
70.66 0.6378 0.6219 0.0131 0.0134 0.292 2.048 0.965 218.033 0.231 4.292 2.007 0.47 152818. 0.0890
|
|
73.38 0.6623 0.5341 0.0087 0.0108 0.236 1.652 0.644 175.929 0.187 2.865 1.660 0.47 153214. 0.0601
|
|
76.10 0.6868 0.3719 0.0044 0.0081 0.177 1.237 0.324 131.709 0.140 1.440 1.115 0.48 153621. 0.0286
|
|
78.82 0.7114 0.0040 0.0000 0.0052 0.114 0.799 0.002 85.049 0.090 0.010 0.011 0.48 154020. 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 0.0951 0.0319 0.954 6.010 8.656 711.092 0.679 38.504 5.521 0.52 163029. 0.7332
|
|
3.02 0.0246 0.0709 0.0938 0.0325 0.971 6.118 8.535 723.774 0.691 37.962 5.348 0.52 163139. 0.7052
|
|
6.05 0.0491 0.1373 0.0923 0.0330 0.987 6.219 8.401 735.768 0.703 37.366 5.179 0.52 163258. 0.6775
|
|
9.07 0.0737 0.1993 0.0907 0.0335 1.002 6.312 8.254 746.827 0.713 36.713 5.013 0.52 163388. 0.6500
|
|
12.09 0.0982 0.2572 0.0889 0.0340 1.015 6.396 8.093 756.708 0.723 35.998 4.851 0.52 163529. 0.6229
|
|
15.12 0.1228 0.3111 0.0870 0.0343 1.026 6.467 7.918 765.158 0.731 35.221 4.694 0.52 163681. 0.5962
|
|
18.14 0.1474 0.3611 0.0849 0.0346 1.035 6.524 7.728 771.918 0.737 34.376 4.541 0.52 163844. 0.5698
|
|
21.16 0.1719 0.4076 0.0827 0.0349 1.042 6.565 7.523 776.729 0.742 33.463 4.393 0.52 164019. 0.5439
|
|
24.19 0.1965 0.4506 0.0802 0.0350 1.045 6.587 7.302 779.336 0.744 32.480 4.250 0.52 164206. 0.5183
|
|
27.21 0.2210 0.4904 0.0776 0.0350 1.045 6.588 7.065 779.494 0.744 31.425 4.111 0.52 164406. 0.4932
|
|
30.23 0.2456 0.5270 0.0748 0.0349 1.042 6.567 6.812 776.963 0.742 30.298 3.976 0.52 164617. 0.4684
|
|
33.26 0.2701 0.5607 0.0719 0.0346 1.035 6.521 6.542 771.523 0.737 29.099 3.846 0.52 164842. 0.4440
|
|
36.28 0.2947 0.5916 0.0687 0.0342 1.023 6.449 6.257 763.004 0.729 27.831 3.719 0.52 165080. 0.4199
|
|
39.30 0.3193 0.6197 0.0655 0.0337 1.008 6.350 5.957 751.311 0.717 26.498 3.596 0.52 165330. 0.3962
|
|
42.33 0.3438 0.6451 0.0620 0.0331 0.988 6.224 5.644 736.389 0.703 25.106 3.477 0.52 165594. 0.3728
|
|
45.35 0.3684 0.6678 0.0584 0.0322 0.963 6.070 5.319 718.197 0.686 23.659 3.359 0.52 165871. 0.3497
|
|
48.37 0.3929 0.6879 0.0547 0.0313 0.934 5.889 4.983 696.697 0.665 22.163 3.244 0.52 166161. 0.3268
|
|
51.40 0.4175 0.7052 0.0509 0.0302 0.901 5.679 4.636 671.854 0.642 20.621 3.130 0.52 166464. 0.3042
|
|
54.42 0.4421 0.7196 0.0470 0.0289 0.863 5.440 4.280 643.628 0.615 19.038 3.016 0.52 166781. 0.2817
|
|
57.44 0.4666 0.7309 0.0430 0.0275 0.821 5.173 3.916 611.984 0.584 17.418 2.902 0.52 167112. 0.2592
|
|
60.47 0.4912 0.7386 0.0389 0.0259 0.774 4.876 3.544 576.892 0.551 15.763 2.786 0.52 167456. 0.2367
|
|
63.49 0.5157 0.7422 0.0348 0.0242 0.722 4.550 3.165 538.329 0.514 14.077 2.667 0.52 167814. 0.2141
|
|
66.51 0.5403 0.7408 0.0305 0.0223 0.666 4.195 2.780 496.289 0.474 12.365 2.541 0.52 168186. 0.1912
|
|
69.54 0.5649 0.7329 0.0263 0.0202 0.605 3.810 2.389 450.780 0.430 10.628 2.404 0.52 168572. 0.1677
|
|
72.56 0.5894 0.7163 0.0219 0.0180 0.539 3.396 1.995 401.837 0.384 8.873 2.252 0.52 168971. 0.1435
|
|
75.58 0.6140 0.6867 0.0175 0.0157 0.469 2.954 1.597 349.520 0.334 7.103 2.072 0.53 169384. 0.1182
|
|
78.61 0.6385 0.6365 0.0132 0.0132 0.394 2.484 1.197 293.934 0.281 5.324 1.847 0.53 169811. 0.0912
|
|
81.63 0.6631 0.5495 0.0087 0.0106 0.315 1.988 0.796 235.223 0.225 3.542 1.536 0.53 170251. 0.0618
|
|
84.65 0.6876 0.3845 0.0044 0.0078 0.233 1.467 0.396 173.567 0.166 1.763 1.036 0.53 170704. 0.0294
|
|
87.68 0.7122 -0.0098 -0.0001 0.0049 0.145 0.916 -0.006 108.322 0.103 -0.027 -0.026 0.53 171142. 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 0.0959 0.0321 1.275 7.304 10.560 950.534 0.825 46.969 5.039 0.57 179320. 0.7390
|
|
3.33 0.0246 0.0712 0.0946 0.0326 1.298 7.437 10.414 967.841 0.840 46.321 4.880 0.57 179441. 0.7109
|
|
6.65 0.0491 0.1379 0.0931 0.0332 1.320 7.563 10.253 984.217 0.854 45.606 4.725 0.57 179573. 0.6829
|
|
9.98 0.0737 0.2001 0.0915 0.0337 1.340 7.679 10.077 999.324 0.868 44.820 4.573 0.57 179717. 0.6553
|
|
13.31 0.0983 0.2582 0.0897 0.0342 1.358 7.782 9.883 1012.831 0.879 43.960 4.426 0.57 179872. 0.6280
|
|
16.64 0.1229 0.3123 0.0878 0.0345 1.374 7.871 9.672 1024.391 0.889 43.020 4.282 0.57 180039. 0.6011
|
|
19.96 0.1474 0.3626 0.0857 0.0349 1.386 7.942 9.442 1033.653 0.897 41.999 4.143 0.57 180220. 0.5746
|
|
23.29 0.1720 0.4093 0.0835 0.0351 1.395 7.993 9.193 1040.265 0.903 40.892 4.008 0.57 180413. 0.5486
|
|
26.62 0.1966 0.4525 0.0810 0.0352 1.400 8.021 8.925 1043.878 0.906 39.698 3.878 0.57 180619. 0.5229
|
|
29.95 0.2211 0.4925 0.0784 0.0352 1.400 8.023 8.637 1044.163 0.906 38.416 3.752 0.57 180839. 0.4977
|
|
33.27 0.2457 0.5294 0.0756 0.0351 1.396 7.997 8.329 1040.797 0.904 37.045 3.629 0.57 181073. 0.4728
|
|
36.60 0.2703 0.5634 0.0726 0.0348 1.386 7.941 8.000 1033.479 0.897 35.585 3.511 0.57 181321. 0.4482
|
|
39.93 0.2949 0.5945 0.0695 0.0345 1.371 7.853 7.653 1021.982 0.887 34.039 3.396 0.57 181583. 0.4241
|
|
43.26 0.3194 0.6229 0.0662 0.0339 1.349 7.731 7.287 1006.177 0.873 32.413 3.285 0.57 181860. 0.4002
|
|
46.58 0.3440 0.6487 0.0627 0.0332 1.322 7.576 6.905 985.991 0.856 30.714 3.176 0.57 182151. 0.3767
|
|
49.91 0.3686 0.6718 0.0591 0.0324 1.289 7.387 6.508 961.372 0.835 28.947 3.070 0.57 182456. 0.3535
|
|
53.24 0.3931 0.6923 0.0554 0.0314 1.250 7.163 6.097 932.273 0.809 27.119 2.966 0.57 182776. 0.3306
|
|
56.57 0.4177 0.7101 0.0515 0.0303 1.205 6.905 5.673 898.647 0.780 25.235 2.864 0.57 183111. 0.3079
|
|
59.89 0.4423 0.7250 0.0476 0.0290 1.154 6.612 5.238 860.444 0.747 23.300 2.761 0.57 183460. 0.2853
|
|
63.22 0.4669 0.7369 0.0435 0.0276 1.096 6.282 4.793 817.619 0.710 21.319 2.659 0.57 183825. 0.2627
|
|
66.55 0.4914 0.7453 0.0394 0.0260 1.033 5.918 4.338 770.130 0.669 19.295 2.555 0.57 184204. 0.2402
|
|
69.87 0.5160 0.7498 0.0352 0.0242 0.963 5.517 3.874 717.949 0.623 17.233 2.448 0.57 184599. 0.2174
|
|
73.20 0.5406 0.7493 0.0309 0.0223 0.887 5.080 3.403 661.064 0.574 15.137 2.335 0.58 185008. 0.1944
|
|
76.53 0.5651 0.7426 0.0266 0.0202 0.804 4.606 2.925 599.490 0.520 13.012 2.213 0.58 185433. 0.1709
|
|
79.86 0.5897 0.7272 0.0222 0.0180 0.715 4.098 2.442 533.270 0.463 10.863 2.077 0.58 185873. 0.1465
|
|
83.18 0.6143 0.6993 0.0178 0.0156 0.620 3.554 1.955 462.491 0.401 8.697 1.917 0.58 186328. 0.1210
|
|
86.51 0.6389 0.6509 0.0133 0.0131 0.519 2.976 1.465 387.291 0.336 6.518 1.716 0.58 186798. 0.0938
|
|
89.84 0.6634 0.5656 0.0089 0.0104 0.413 2.366 0.975 307.868 0.267 4.335 1.436 0.58 187283. 0.0640
|
|
93.17 0.6880 0.4002 0.0044 0.0076 0.301 1.725 0.485 224.466 0.195 2.157 0.980 0.58 187782. 0.0308
|
|
96.49 0.7126 -0.0127 -0.0001 0.0046 0.182 1.046 -0.009 136.073 0.118 -0.040 -0.030 0.58 188260. 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 0.0968 0.0323 1.667 8.754 12.681 1242.773 0.989 56.406 4.628 0.62 195608. 0.7439
|
|
3.63 0.0246 0.0714 0.0954 0.0329 1.698 8.916 12.510 1265.881 1.007 55.646 4.483 0.62 195740. 0.7156
|
|
7.26 0.0492 0.1382 0.0940 0.0334 1.727 9.070 12.321 1287.759 1.025 54.805 4.340 0.62 195885. 0.6876
|
|
10.89 0.0738 0.2006 0.0924 0.0340 1.754 9.213 12.113 1307.952 1.041 53.877 4.200 0.62 196042. 0.6598
|
|
14.53 0.0983 0.2589 0.0907 0.0344 1.778 9.340 11.884 1326.018 1.055 52.859 4.065 0.62 196211. 0.6325
|
|
18.16 0.1229 0.3131 0.0888 0.0348 1.799 9.449 11.633 1341.495 1.068 51.745 3.933 0.62 196395. 0.6055
|
|
21.79 0.1475 0.3635 0.0867 0.0352 1.816 9.536 11.360 1353.911 1.077 50.530 3.806 0.62 196592. 0.5790
|
|
25.42 0.1721 0.4104 0.0844 0.0354 1.828 9.599 11.064 1362.798 1.084 49.211 3.682 0.62 196804. 0.5528
|
|
29.05 0.1967 0.4538 0.0820 0.0355 1.834 9.633 10.743 1367.697 1.088 47.787 3.563 0.62 197030. 0.5271
|
|
32.68 0.2213 0.4940 0.0793 0.0355 1.835 9.637 10.399 1368.167 1.089 46.254 3.447 0.62 197271. 0.5018
|
|
36.32 0.2458 0.5311 0.0765 0.0354 1.829 9.606 10.030 1363.786 1.085 44.613 3.336 0.62 197527. 0.4768
|
|
39.95 0.2704 0.5653 0.0735 0.0352 1.816 9.538 9.636 1354.158 1.078 42.863 3.228 0.62 197798. 0.4522
|
|
43.58 0.2950 0.5967 0.0703 0.0348 1.796 9.431 9.219 1338.983 1.066 41.008 3.123 0.62 198085. 0.4280
|
|
47.21 0.3196 0.6254 0.0670 0.0342 1.768 9.284 8.780 1318.088 1.049 39.056 3.021 0.62 198388. 0.4041
|
|
50.84 0.3442 0.6515 0.0635 0.0335 1.732 9.096 8.321 1291.384 1.028 37.013 2.923 0.62 198706. 0.3805
|
|
54.47 0.3688 0.6750 0.0598 0.0327 1.688 8.866 7.844 1258.808 1.002 34.889 2.826 0.62 199040. 0.3573
|
|
58.11 0.3933 0.6959 0.0561 0.0317 1.636 8.595 7.349 1220.303 0.971 32.690 2.732 0.62 199390. 0.3343
|
|
61.74 0.4179 0.7141 0.0522 0.0305 1.577 8.282 6.840 1175.810 0.936 30.423 2.638 0.62 199756. 0.3114
|
|
65.37 0.4425 0.7296 0.0482 0.0292 1.509 7.926 6.316 1125.267 0.895 28.093 2.546 0.62 200138. 0.2888
|
|
69.00 0.4671 0.7420 0.0441 0.0278 1.433 7.527 5.779 1068.619 0.850 25.706 2.453 0.63 200537. 0.2662
|
|
72.63 0.4917 0.7511 0.0399 0.0261 1.349 7.084 5.231 1005.811 0.800 23.268 2.359 0.63 200952. 0.2435
|
|
76.26 0.5163 0.7564 0.0356 0.0243 1.256 6.598 4.673 936.807 0.745 20.783 2.262 0.63 201383. 0.2207
|
|
79.90 0.5408 0.7568 0.0313 0.0224 1.155 6.069 4.105 861.592 0.686 18.257 2.161 0.63 201830. 0.1976
|
|
83.53 0.5654 0.7512 0.0269 0.0203 1.046 5.495 3.529 780.184 0.621 15.696 2.051 0.63 202295. 0.1739
|
|
87.16 0.5900 0.7372 0.0225 0.0180 0.929 4.879 2.946 692.644 0.551 13.105 1.929 0.63 202775. 0.1495
|
|
90.79 0.6146 0.7107 0.0180 0.0156 0.803 4.220 2.359 599.083 0.477 10.491 1.786 0.63 203272. 0.1238
|
|
94.42 0.6392 0.6642 0.0135 0.0130 0.670 3.520 1.768 499.686 0.398 7.863 1.605 0.63 203786. 0.0963
|
|
98.05 0.6638 0.5807 0.0090 0.0103 0.529 2.780 1.176 394.716 0.314 5.229 1.351 0.63 204316. 0.0661
|
|
101.69 0.6883 0.4153 0.0045 0.0074 0.382 2.004 0.584 284.495 0.226 2.599 0.932 0.63 204860. 0.0321
|
|
105.32 0.7129 -0.0161 -0.0001 0.0044 0.225 1.180 -0.013 167.479 0.133 -0.057 -0.035 0.63 205377. 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 0.0977 0.0326 2.141 10.381 15.033 1596.583 1.173 66.868 4.271 0.67 211891. 0.7474
|
|
3.94 0.0246 0.0714 0.0965 0.0332 2.181 10.576 14.837 1626.612 1.195 65.994 4.137 0.67 212035. 0.7193
|
|
7.87 0.0492 0.1383 0.0950 0.0338 2.220 10.761 14.618 1655.121 1.216 65.022 4.006 0.67 212192. 0.6913
|
|
11.81 0.0738 0.2008 0.0935 0.0344 2.255 10.933 14.376 1681.503 1.235 63.946 3.878 0.67 212362. 0.6637
|
|
15.74 0.0984 0.2591 0.0917 0.0348 2.287 11.087 14.110 1705.165 1.253 62.761 3.753 0.67 212547. 0.6363
|
|
19.68 0.1230 0.3134 0.0898 0.0353 2.314 11.219 13.817 1725.488 1.267 61.459 3.632 0.67 212746. 0.6094
|
|
23.62 0.1476 0.3639 0.0877 0.0356 2.336 11.325 13.498 1741.833 1.279 60.037 3.515 0.67 212961. 0.5828
|
|
27.55 0.1722 0.4108 0.0855 0.0358 2.352 11.401 13.150 1753.575 1.288 58.489 3.401 0.67 213191. 0.5567
|
|
31.49 0.1968 0.4544 0.0830 0.0360 2.360 11.444 12.773 1760.103 1.293 56.813 3.291 0.67 213437. 0.5310
|
|
35.43 0.2214 0.4947 0.0804 0.0360 2.361 11.449 12.367 1760.843 1.293 55.007 3.185 0.67 213699. 0.5056
|
|
39.36 0.2460 0.5320 0.0776 0.0359 2.354 11.412 11.931 1755.247 1.289 53.069 3.083 0.67 213977. 0.4807
|
|
43.30 0.2706 0.5664 0.0745 0.0356 2.337 11.331 11.466 1742.807 1.280 50.999 2.984 0.67 214273. 0.4561
|
|
47.23 0.2951 0.5980 0.0713 0.0352 2.311 11.203 10.972 1723.130 1.266 48.803 2.888 0.67 214585. 0.4318
|
|
51.17 0.3197 0.6270 0.0679 0.0346 2.274 11.027 10.452 1696.000 1.246 46.489 2.795 0.67 214913. 0.4079
|
|
55.11 0.3443 0.6534 0.0644 0.0339 2.228 10.801 9.907 1661.303 1.220 44.065 2.705 0.67 215259. 0.3843
|
|
59.04 0.3689 0.6773 0.0607 0.0331 2.171 10.526 9.340 1618.970 1.189 41.543 2.617 0.67 215622. 0.3609
|
|
62.98 0.3935 0.6986 0.0569 0.0321 2.104 10.201 8.752 1568.934 1.152 38.931 2.530 0.68 216003. 0.3379
|
|
66.92 0.4181 0.7173 0.0530 0.0309 2.026 9.825 8.147 1511.128 1.110 36.236 2.445 0.68 216400. 0.3150
|
|
70.85 0.4427 0.7333 0.0489 0.0295 1.938 9.398 7.524 1445.479 1.062 33.465 2.361 0.68 216816. 0.2923
|
|
74.79 0.4673 0.7464 0.0448 0.0280 1.840 8.920 6.885 1371.920 1.008 30.626 2.276 0.68 217248. 0.2696
|
|
78.72 0.4919 0.7562 0.0405 0.0264 1.730 8.390 6.233 1290.383 0.948 27.725 2.191 0.68 217699. 0.2469
|
|
82.66 0.5165 0.7622 0.0362 0.0245 1.610 7.807 5.568 1200.819 0.882 24.767 2.103 0.68 218167. 0.2240
|
|
86.60 0.5411 0.7636 0.0318 0.0225 1.479 7.173 4.892 1103.212 0.810 21.760 2.011 0.68 218653. 0.2008
|
|
90.53 0.5657 0.7590 0.0273 0.0204 1.338 6.486 4.206 997.585 0.733 18.708 1.912 0.68 219157. 0.1770
|
|
94.47 0.5903 0.7463 0.0228 0.0181 1.185 5.748 3.512 884.016 0.649 15.621 1.802 0.68 219678. 0.1524
|
|
98.41 0.6149 0.7214 0.0183 0.0156 1.023 4.959 2.812 762.653 0.560 12.506 1.672 0.68 220217. 0.1266
|
|
102.34 0.6395 0.6767 0.0137 0.0129 0.850 4.120 2.107 633.731 0.466 9.373 1.508 0.68 220775. 0.0988
|
|
106.28 0.6641 0.5951 0.0091 0.0102 0.667 3.235 1.401 497.596 0.366 6.232 1.277 0.69 221349. 0.0682
|
|
110.21 0.6887 0.4301 0.0045 0.0072 0.476 2.306 0.696 354.677 0.261 3.096 0.890 0.69 221940. 0.0335
|
|
114.15 0.7133 -0.0199 -0.0001 0.0041 0.272 1.318 -0.018 202.682 0.149 -0.079 -0.040 0.69 222494. 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 0.0988 0.0333 2.732 12.298 17.628 2037.028 1.389 78.411 3.925 0.72 228169. 0.7438
|
|
4.24 0.0246 0.0708 0.0976 0.0339 2.780 12.517 17.407 2073.330 1.414 77.425 3.808 0.72 228324. 0.7171
|
|
8.48 0.0492 0.1373 0.0962 0.0345 2.827 12.725 17.159 2107.771 1.438 76.323 3.692 0.72 228493. 0.6904
|
|
12.72 0.0738 0.1996 0.0946 0.0350 2.869 12.918 16.883 2139.623 1.459 75.097 3.579 0.72 228677. 0.6638
|
|
16.96 0.0984 0.2579 0.0929 0.0355 2.908 13.090 16.578 2168.176 1.479 73.740 3.468 0.72 228877. 0.6374
|
|
21.20 0.1230 0.3123 0.0910 0.0359 2.940 13.238 16.242 2192.666 1.496 72.244 3.360 0.72 229092. 0.6111
|
|
25.45 0.1476 0.3630 0.0890 0.0362 2.967 13.356 15.873 2212.323 1.509 70.602 3.254 0.72 229324. 0.5852
|
|
29.69 0.1722 0.4102 0.0867 0.0364 2.986 13.441 15.470 2226.362 1.519 68.810 3.152 0.72 229573. 0.5595
|
|
33.93 0.1969 0.4539 0.0843 0.0365 2.996 13.487 15.032 2233.997 1.524 66.863 3.052 0.72 229839. 0.5341
|
|
38.17 0.2215 0.4945 0.0816 0.0365 2.996 13.490 14.559 2234.459 1.524 64.760 2.955 0.72 230123. 0.5090
|
|
42.41 0.2461 0.5321 0.0788 0.0364 2.986 13.445 14.051 2227.005 1.519 62.499 2.862 0.72 230424. 0.4842
|
|
46.65 0.2707 0.5667 0.0757 0.0362 2.965 13.348 13.507 2210.930 1.508 60.080 2.771 0.72 230743. 0.4597
|
|
50.89 0.2953 0.5986 0.0725 0.0358 2.931 13.196 12.929 2185.672 1.491 57.509 2.683 0.73 231081. 0.4354
|
|
55.13 0.3199 0.6279 0.0691 0.0352 2.884 12.986 12.319 2150.899 1.467 54.795 2.598 0.73 231436. 0.4115
|
|
59.37 0.3445 0.6546 0.0655 0.0345 2.825 12.717 11.680 2106.443 1.437 51.951 2.515 0.73 231810. 0.3879
|
|
63.61 0.3691 0.6788 0.0617 0.0336 2.752 12.390 11.013 2052.206 1.400 48.988 2.434 0.73 232202. 0.3646
|
|
67.85 0.3937 0.7006 0.0579 0.0325 2.666 12.003 10.323 1988.120 1.356 45.916 2.355 0.73 232613. 0.3415
|
|
72.10 0.4183 0.7197 0.0539 0.0313 2.567 11.556 9.610 1914.107 1.306 42.745 2.277 0.73 233043. 0.3186
|
|
76.34 0.4429 0.7363 0.0498 0.0299 2.454 11.049 8.877 1830.091 1.248 39.484 2.200 0.73 233492. 0.2959
|
|
80.58 0.4675 0.7499 0.0455 0.0284 2.328 10.481 8.125 1735.985 1.184 36.141 2.123 0.73 233959. 0.2731
|
|
84.82 0.4921 0.7604 0.0412 0.0267 2.188 9.851 7.357 1631.718 1.113 32.723 2.045 0.73 234445. 0.2504
|
|
89.06 0.5167 0.7672 0.0368 0.0248 2.035 9.160 6.573 1517.223 1.035 29.237 1.965 0.73 234950. 0.2274
|
|
93.30 0.5413 0.7695 0.0324 0.0228 1.867 8.407 5.776 1392.478 0.950 25.691 1.881 0.73 235475. 0.2041
|
|
97.54 0.5660 0.7661 0.0278 0.0206 1.686 7.592 4.967 1257.517 0.858 22.093 1.791 0.73 236018. 0.1802
|
|
101.78 0.5906 0.7546 0.0233 0.0182 1.492 6.716 4.148 1112.470 0.759 18.450 1.691 0.73 236581. 0.1555
|
|
106.02 0.6152 0.7312 0.0186 0.0157 1.284 5.781 3.321 957.570 0.653 14.773 1.573 0.74 237163. 0.1294
|
|
110.26 0.6398 0.6881 0.0140 0.0130 1.064 4.789 2.489 793.204 0.541 11.073 1.424 0.74 237764. 0.1014
|
|
114.50 0.6644 0.6080 0.0093 0.0101 0.831 3.743 1.655 619.949 0.423 7.363 1.211 0.74 238383. 0.0703
|
|
118.75 0.6890 0.4427 0.0046 0.0072 0.588 2.648 0.822 438.537 0.299 3.657 0.850 0.74 239020. 0.0348
|
|
122.99 0.7136 -0.0234 -0.0001 0.0040 0.330 1.484 -0.024 245.746 0.168 -0.105 -0.043 0.74 239611. 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 0.1000 0.0350 3.525 14.811 20.477 2628.401 1.673 91.080 3.534 0.77 244441. 0.7217
|
|
4.55 0.0246 0.0685 0.0988 0.0355 3.578 15.035 20.232 2668.225 1.699 89.993 3.439 0.77 244607. 0.6982
|
|
9.09 0.0492 0.1333 0.0975 0.0360 3.628 15.245 19.957 2705.416 1.722 88.769 3.346 0.77 244788. 0.6746
|
|
13.64 0.0738 0.1945 0.0959 0.0364 3.673 15.435 19.649 2739.133 1.744 87.399 3.254 0.77 244986. 0.6510
|
|
18.18 0.0985 0.2521 0.0943 0.0368 3.713 15.600 19.306 2768.570 1.763 85.872 3.163 0.77 245200. 0.6272
|
|
22.73 0.1231 0.3062 0.0924 0.0371 3.745 15.737 18.925 2792.887 1.778 84.180 3.073 0.77 245432. 0.6035
|
|
27.27 0.1477 0.3570 0.0904 0.0374 3.770 15.841 18.506 2811.230 1.790 82.313 2.986 0.77 245681. 0.5797
|
|
31.82 0.1723 0.4044 0.0881 0.0375 3.785 15.906 18.046 2822.744 1.797 80.267 2.900 0.77 245949. 0.5560
|
|
36.36 0.1969 0.4488 0.0857 0.0376 3.790 15.927 17.544 2826.566 1.799 78.036 2.815 0.78 246235. 0.5322
|
|
40.91 0.2215 0.4900 0.0830 0.0375 3.784 15.901 17.000 2821.853 1.796 75.618 2.733 0.78 246541. 0.5085
|
|
45.45 0.2461 0.5284 0.0802 0.0373 3.765 15.821 16.414 2807.753 1.787 73.010 2.652 0.78 246865. 0.4849
|
|
50.00 0.2708 0.5638 0.0771 0.0370 3.733 15.684 15.786 2783.432 1.772 70.215 2.572 0.78 247209. 0.4613
|
|
54.54 0.2954 0.5965 0.0738 0.0365 3.685 15.486 15.116 2748.194 1.750 67.236 2.495 0.78 247572. 0.4378
|
|
59.09 0.3200 0.6266 0.0704 0.0359 3.623 15.223 14.408 2701.615 1.720 64.086 2.419 0.78 247954. 0.4144
|
|
63.63 0.3446 0.6540 0.0667 0.0352 3.545 14.895 13.664 2643.445 1.683 60.779 2.345 0.78 248357. 0.3912
|
|
68.18 0.3692 0.6790 0.0629 0.0342 3.451 14.501 12.889 2573.488 1.638 57.329 2.272 0.78 248779. 0.3681
|
|
72.72 0.3938 0.7013 0.0590 0.0331 3.341 14.039 12.084 2491.542 1.586 53.749 2.200 0.78 249221. 0.3451
|
|
77.27 0.4184 0.7211 0.0549 0.0319 3.215 13.509 11.252 2397.421 1.526 50.051 2.129 0.78 249682. 0.3223
|
|
81.81 0.4431 0.7383 0.0508 0.0305 3.072 12.909 10.397 2290.921 1.458 46.245 2.058 0.78 250164. 0.2996
|
|
86.36 0.4677 0.7526 0.0465 0.0289 2.913 12.238 9.519 2171.894 1.383 42.340 1.988 0.78 250666. 0.2768
|
|
90.90 0.4923 0.7638 0.0421 0.0271 2.736 11.496 8.621 2040.227 1.299 38.347 1.917 0.78 251189. 0.2540
|
|
95.45 0.5169 0.7713 0.0376 0.0252 2.542 10.683 7.705 1895.862 1.207 34.272 1.843 0.78 251732. 0.2309
|
|
99.99 0.5415 0.7744 0.0331 0.0231 2.332 9.798 6.772 1738.844 1.107 30.124 1.767 0.78 252294. 0.2075
|
|
104.54 0.5661 0.7716 0.0284 0.0209 2.105 8.843 5.826 1569.358 0.999 25.913 1.684 0.79 252878. 0.1834
|
|
109.08 0.5907 0.7607 0.0238 0.0185 1.861 7.820 4.867 1387.741 0.883 21.647 1.591 0.79 253482. 0.1584
|
|
113.63 0.6154 0.7373 0.0190 0.0159 1.602 6.731 3.898 1194.558 0.760 17.339 1.480 0.79 254106. 0.1319
|
|
118.18 0.6400 0.6933 0.0143 0.0132 1.328 5.582 2.923 990.596 0.631 13.001 1.338 0.79 254751. 0.1033
|
|
122.72 0.6646 0.6106 0.0095 0.0103 1.042 4.378 1.944 776.923 0.495 8.647 1.135 0.79 255415. 0.0714
|
|
127.27 0.6892 0.4404 0.0047 0.0074 0.744 3.126 0.966 554.832 0.353 4.295 0.789 0.79 256098. 0.0350
|
|
131.81 0.7138 -0.0237 -0.0001 0.0043 0.429 1.803 -0.029 319.953 0.204 -0.129 -0.041 0.79 256730. 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 0.1012 0.0383 4.684 18.450 23.582 3492.584 2.084 104.894 3.063 0.83 260705. 0.6713
|
|
4.85 0.0246 0.0637 0.1001 0.0387 4.736 18.656 23.320 3531.618 2.108 103.726 2.995 0.83 260882. 0.6528
|
|
9.70 0.0493 0.1245 0.0988 0.0391 4.782 18.839 23.021 3566.208 2.128 102.398 2.928 0.83 261075. 0.6341
|
|
14.55 0.0739 0.1826 0.0974 0.0394 4.821 18.993 22.684 3595.370 2.146 100.899 2.862 0.83 261286. 0.6152
|
|
19.40 0.0985 0.2379 0.0957 0.0396 4.852 19.114 22.306 3618.196 2.159 99.215 2.796 0.83 261516. 0.5961
|
|
24.25 0.1231 0.2904 0.0939 0.0398 4.873 19.196 21.883 3633.812 2.169 97.334 2.731 0.83 261763. 0.5767
|
|
29.11 0.1478 0.3403 0.0919 0.0399 4.883 19.236 21.413 3641.381 2.173 95.246 2.667 0.83 262031. 0.5571
|
|
33.96 0.1724 0.3876 0.0897 0.0399 4.881 19.229 20.895 3640.087 2.173 92.943 2.604 0.83 262318. 0.5372
|
|
38.81 0.1970 0.4322 0.0872 0.0398 4.867 19.172 20.328 3629.161 2.166 90.419 2.541 0.83 262625. 0.5170
|
|
43.66 0.2216 0.4743 0.0846 0.0395 4.838 19.059 19.710 3607.839 2.153 87.671 2.478 0.83 262952. 0.4965
|
|
48.51 0.2463 0.5137 0.0817 0.0392 4.795 18.888 19.042 3575.386 2.134 84.698 2.416 0.83 263300. 0.4758
|
|
53.36 0.2709 0.5506 0.0786 0.0387 4.735 18.653 18.323 3531.029 2.107 81.500 2.354 0.83 263669. 0.4547
|
|
58.21 0.2955 0.5849 0.0753 0.0381 4.659 18.352 17.555 3474.096 2.073 78.084 2.292 0.83 264058. 0.4334
|
|
63.06 0.3202 0.6166 0.0718 0.0373 4.565 17.983 16.740 3404.143 2.032 74.461 2.231 0.83 264469. 0.4119
|
|
67.91 0.3448 0.6459 0.0682 0.0364 4.453 17.543 15.884 3320.942 1.982 70.651 2.169 0.83 264900. 0.3902
|
|
72.76 0.3694 0.6726 0.0643 0.0353 4.324 17.033 14.988 3224.331 1.924 66.668 2.108 0.83 265352. 0.3684
|
|
77.61 0.3940 0.6967 0.0603 0.0341 4.176 16.451 14.058 3114.134 1.859 62.529 2.047 0.83 265826. 0.3465
|
|
82.46 0.4187 0.7181 0.0562 0.0328 4.010 15.796 13.095 2990.099 1.785 58.248 1.986 0.83 266321. 0.3245
|
|
87.32 0.4433 0.7369 0.0519 0.0313 3.825 15.066 12.104 2851.932 1.702 53.838 1.925 0.83 266837. 0.3023
|
|
92.17 0.4679 0.7527 0.0476 0.0296 3.620 14.259 11.086 2699.305 1.611 49.309 1.863 0.83 267374. 0.2799
|
|
97.02 0.4925 0.7648 0.0431 0.0278 3.397 13.382 10.043 2533.234 1.512 44.673 1.798 0.84 267933. 0.2572
|
|
101.87 0.5172 0.7727 0.0385 0.0258 3.156 12.434 8.979 2353.718 1.405 39.939 1.730 0.84 268514. 0.2340
|
|
106.72 0.5418 0.7754 0.0339 0.0237 2.897 11.414 7.895 2160.626 1.290 35.117 1.657 0.84 269116. 0.2102
|
|
111.57 0.5664 0.7714 0.0292 0.0214 2.620 10.321 6.793 1953.673 1.166 30.217 1.577 0.84 269740. 0.1855
|
|
116.42 0.5911 0.7581 0.0244 0.0190 2.325 9.158 5.677 1733.557 1.035 25.252 1.485 0.84 270386. 0.1597
|
|
121.27 0.6157 0.7305 0.0195 0.0165 2.013 7.932 4.549 1501.445 0.896 20.232 1.374 0.84 271053. 0.1323
|
|
126.12 0.6403 0.6796 0.0146 0.0138 1.688 6.650 3.411 1258.915 0.751 15.173 1.229 0.84 271742. 0.1025
|
|
130.97 0.6649 0.5864 0.0097 0.0110 1.351 5.324 2.269 1007.765 0.601 10.093 1.021 0.84 272452. 0.0694
|
|
135.82 0.6896 0.4055 0.0048 0.0082 1.006 3.963 1.126 750.105 0.448 5.009 0.681 0.84 273182. 0.0326
|
|
140.68 0.7142 -0.0203 -0.0001 0.0053 0.644 2.536 -0.035 480.087 0.287 -0.155 -0.033 0.85 273864. 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 0.0435 6.391 23.694 26.864 4765.485 2.677 119.492 2.557 0.88 276972. 0.5982
|
|
5.16 0.0247 0.0568 0.1011 0.0439 6.444 23.890 26.594 4805.019 2.699 118.292 2.510 0.88 277158. 0.5843
|
|
10.33 0.0493 0.1116 0.0999 0.0442 6.486 24.047 26.284 4836.638 2.717 116.913 2.465 0.88 277363. 0.5704
|
|
15.49 0.0740 0.1644 0.0986 0.0444 6.516 24.158 25.930 4858.924 2.729 115.335 2.420 0.88 277586. 0.5563
|
|
20.65 0.0987 0.2152 0.0970 0.0445 6.532 24.216 25.526 4870.634 2.736 113.541 2.377 0.88 277830. 0.5421
|
|
25.81 0.1233 0.2642 0.0953 0.0445 6.532 24.217 25.071 4870.684 2.736 111.515 2.335 0.88 278093. 0.5276
|
|
30.98 0.1480 0.3114 0.0934 0.0444 6.515 24.154 24.560 4858.158 2.729 109.243 2.293 0.88 278378. 0.5129
|
|
36.14 0.1727 0.3568 0.0912 0.0441 6.480 24.026 23.991 4832.272 2.714 106.713 2.252 0.88 278684. 0.4978
|
|
41.30 0.1974 0.4004 0.0888 0.0438 6.427 23.827 23.363 4792.413 2.692 103.917 2.211 0.88 279012. 0.4824
|
|
46.47 0.2220 0.4421 0.0862 0.0433 6.354 23.558 22.673 4738.144 2.662 100.849 2.170 0.88 279362. 0.4665
|
|
51.63 0.2467 0.4820 0.0833 0.0427 6.261 23.215 21.922 4669.165 2.623 97.509 2.130 0.88 279734. 0.4500
|
|
56.79 0.2714 0.5199 0.0803 0.0419 6.149 22.797 21.110 4585.205 2.576 93.898 2.088 0.88 280128. 0.4331
|
|
61.96 0.2960 0.5558 0.0769 0.0410 6.016 22.304 20.239 4486.091 2.520 90.024 2.046 0.88 280545. 0.4155
|
|
67.12 0.3207 0.5895 0.0734 0.0399 5.863 21.737 19.312 4371.900 2.456 85.902 2.004 0.88 280984. 0.3974
|
|
72.28 0.3454 0.6211 0.0697 0.0388 5.690 21.095 18.335 4242.853 2.383 81.553 1.960 0.88 281446. 0.3788
|
|
77.44 0.3700 0.6503 0.0658 0.0374 5.497 20.380 17.311 4099.115 2.303 76.999 1.915 0.88 281930. 0.3597
|
|
82.61 0.3947 0.6771 0.0618 0.0360 5.284 19.592 16.245 3940.631 2.214 72.256 1.870 0.88 282437. 0.3401
|
|
87.77 0.4194 0.7014 0.0576 0.0344 5.052 18.730 15.140 3767.148 2.116 67.341 1.823 0.88 282966. 0.3201
|
|
92.93 0.4441 0.7230 0.0532 0.0327 4.799 17.791 13.999 3578.317 2.010 62.269 1.774 0.89 283518. 0.2997
|
|
98.10 0.4687 0.7416 0.0488 0.0308 4.524 16.774 12.827 3373.778 1.895 57.054 1.724 0.89 284092. 0.2788
|
|
103.26 0.4934 0.7566 0.0442 0.0288 4.230 15.684 11.625 3154.587 1.772 51.708 1.671 0.89 284690. 0.2572
|
|
108.42 0.5181 0.7664 0.0395 0.0267 3.922 14.540 10.396 2924.493 1.643 46.242 1.612 0.89 285310. 0.2347
|
|
113.58 0.5427 0.7670 0.0348 0.0246 3.610 13.383 9.141 2691.807 1.512 40.661 1.540 0.89 285954. 0.2102
|
|
118.75 0.5674 0.7584 0.0299 0.0224 3.284 12.176 7.865 2448.874 1.376 34.985 1.457 0.89 286620. 0.1844
|
|
123.91 0.5921 0.7378 0.0250 0.0200 2.943 10.910 6.571 2194.341 1.233 29.229 1.358 0.89 287309. 0.1572
|
|
129.07 0.6167 0.6999 0.0200 0.0176 2.588 9.595 5.263 1929.801 1.084 23.408 1.237 0.89 288021. 0.1281
|
|
134.24 0.6414 0.6349 0.0150 0.0151 2.223 8.243 3.943 1657.948 0.931 17.540 1.079 0.89 288756. 0.0967
|
|
139.40 0.6661 0.5253 0.0100 0.0126 1.853 6.869 2.618 1381.644 0.776 11.646 0.860 0.90 289513. 0.0628
|
|
144.56 0.6908 0.3367 0.0049 0.0101 1.480 5.488 1.293 1103.795 0.620 5.751 0.531 0.90 290292. 0.0273
|
|
149.73 0.7154 -0.0186 -0.0002 0.0075 1.094 4.056 -0.051 815.714 0.458 -0.226 -0.028 0.90 291034. 0.0000
|
|
|
|
|
|
|