612 lines
109 KiB
Plaintext
612 lines
109 KiB
Plaintext
14x8.5E (14x85E.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 0.0930 0.0404 0.002 0.110 0.114 1.304 0.012 0.507 39.625 0.06 18031. 0.5605
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0.34 0.0259 0.0581 0.0919 0.0409 0.002 0.112 0.112 1.320 0.013 0.500 38.639 0.06 18043. 0.5431
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0.69 0.0517 0.1132 0.0906 0.0414 0.002 0.113 0.111 1.336 0.013 0.493 37.648 0.06 18057. 0.5254
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1.03 0.0776 0.1654 0.0892 0.0418 0.002 0.114 0.109 1.351 0.013 0.486 36.657 0.06 18071. 0.5076
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1.37 0.1035 0.2145 0.0876 0.0423 0.002 0.115 0.107 1.364 0.013 0.477 35.668 0.06 18088. 0.4896
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1.72 0.1294 0.2608 0.0859 0.0426 0.002 0.116 0.105 1.376 0.013 0.468 34.685 0.06 18105. 0.4715
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2.06 0.1552 0.3041 0.0841 0.0429 0.002 0.117 0.103 1.385 0.013 0.458 33.709 0.06 18124. 0.4533
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2.40 0.1811 0.3447 0.0821 0.0431 0.002 0.118 0.101 1.393 0.013 0.447 32.742 0.06 18144. 0.4351
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2.74 0.2070 0.3824 0.0800 0.0433 0.002 0.118 0.098 1.397 0.013 0.435 31.785 0.06 18166. 0.4168
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3.09 0.2329 0.4174 0.0776 0.0433 0.002 0.118 0.095 1.398 0.013 0.423 30.838 0.06 18190. 0.3984
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3.43 0.2587 0.4496 0.0751 0.0432 0.002 0.118 0.092 1.395 0.013 0.409 29.900 0.06 18215. 0.3800
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3.77 0.2846 0.4792 0.0724 0.0430 0.002 0.117 0.089 1.388 0.013 0.394 28.969 0.06 18242. 0.3614
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4.12 0.3105 0.5060 0.0695 0.0426 0.002 0.116 0.085 1.376 0.013 0.378 28.043 0.06 18270. 0.3428
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4.46 0.3363 0.5301 0.0664 0.0421 0.002 0.115 0.081 1.360 0.013 0.362 27.116 0.06 18300. 0.3240
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4.80 0.3622 0.5512 0.0631 0.0415 0.002 0.113 0.077 1.338 0.013 0.344 26.183 0.06 18332. 0.3050
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5.15 0.3881 0.5693 0.0596 0.0406 0.002 0.111 0.073 1.311 0.013 0.325 25.238 0.06 18365. 0.2857
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5.49 0.4140 0.5840 0.0559 0.0396 0.002 0.108 0.068 1.279 0.012 0.305 24.273 0.06 18400. 0.2662
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5.83 0.4398 0.5951 0.0521 0.0385 0.002 0.105 0.064 1.242 0.012 0.284 23.279 0.06 18437. 0.2463
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6.17 0.4657 0.6021 0.0481 0.0372 0.002 0.101 0.059 1.200 0.011 0.262 22.244 0.06 18476. 0.2262
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6.52 0.4916 0.6044 0.0440 0.0358 0.002 0.098 0.054 1.154 0.011 0.239 21.155 0.06 18516. 0.2057
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6.86 0.5175 0.6014 0.0397 0.0342 0.001 0.093 0.049 1.103 0.011 0.216 19.996 0.06 18558. 0.1848
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7.20 0.5433 0.5920 0.0354 0.0325 0.001 0.089 0.043 1.049 0.010 0.193 18.748 0.06 18601. 0.1636
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7.55 0.5692 0.5752 0.0310 0.0307 0.001 0.084 0.038 0.991 0.009 0.169 17.387 0.06 18646. 0.1420
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7.89 0.5951 0.5493 0.0266 0.0288 0.001 0.079 0.033 0.929 0.009 0.145 15.882 0.06 18693. 0.1200
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8.23 0.6209 0.5121 0.0221 0.0268 0.001 0.073 0.027 0.864 0.008 0.120 14.191 0.06 18742. 0.0978
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8.58 0.6468 0.4608 0.0176 0.0247 0.001 0.067 0.022 0.796 0.008 0.096 12.257 0.06 18792. 0.0753
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8.92 0.6727 0.3910 0.0131 0.0225 0.001 0.061 0.016 0.725 0.007 0.071 10.002 0.06 18844. 0.0530
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9.26 0.6986 0.2968 0.0086 0.0202 0.001 0.055 0.011 0.652 0.006 0.047 7.309 0.06 18898. 0.0314
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9.60 0.7244 0.1688 0.0042 0.0179 0.001 0.049 0.005 0.577 0.006 0.023 4.008 0.06 18953. 0.0120
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9.95 0.7503 -0.0078 -0.0002 0.0155 0.001 0.042 0.000 0.501 0.005 -0.001 -0.178 0.06 19010. 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 0.0933 0.0368 0.013 0.402 0.457 9.502 0.045 2.033 21.819 0.11 36061. 0.6183
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0.69 0.0260 0.0641 0.0922 0.0374 0.013 0.408 0.451 9.646 0.046 2.008 21.223 0.11 36086. 0.5976
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1.38 0.0520 0.1246 0.0909 0.0379 0.013 0.414 0.445 9.786 0.047 1.980 20.629 0.11 36113. 0.5768
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2.07 0.0780 0.1816 0.0895 0.0384 0.013 0.419 0.438 9.919 0.047 1.949 20.038 0.11 36143. 0.5559
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2.76 0.1040 0.2351 0.0879 0.0389 0.013 0.424 0.431 10.041 0.048 1.916 19.453 0.11 36175. 0.5350
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3.45 0.1299 0.2851 0.0863 0.0393 0.014 0.429 0.422 10.150 0.048 1.879 18.876 0.11 36211. 0.5142
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4.13 0.1559 0.3318 0.0844 0.0397 0.014 0.433 0.413 10.242 0.049 1.839 18.307 0.11 36249. 0.4933
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4.82 0.1819 0.3753 0.0824 0.0399 0.014 0.436 0.404 10.315 0.049 1.795 17.749 0.11 36290. 0.4726
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5.51 0.2079 0.4157 0.0803 0.0401 0.014 0.438 0.393 10.363 0.049 1.748 17.201 0.11 36334. 0.4519
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6.20 0.2339 0.4531 0.0779 0.0402 0.014 0.439 0.381 10.384 0.050 1.697 16.664 0.11 36382. 0.4314
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6.89 0.2599 0.4875 0.0754 0.0402 0.014 0.438 0.369 10.373 0.050 1.642 16.138 0.11 36432. 0.4109
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7.58 0.2859 0.5191 0.0726 0.0400 0.014 0.437 0.356 10.329 0.049 1.582 15.621 0.11 36486. 0.3905
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8.27 0.3119 0.5479 0.0697 0.0397 0.014 0.433 0.341 10.247 0.049 1.519 15.113 0.11 36543. 0.3701
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8.96 0.3379 0.5738 0.0666 0.0392 0.014 0.428 0.326 10.125 0.048 1.451 14.610 0.11 36604. 0.3497
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9.65 0.3638 0.5968 0.0633 0.0386 0.013 0.421 0.310 9.960 0.048 1.378 14.112 0.11 36668. 0.3292
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10.34 0.3898 0.6169 0.0598 0.0378 0.013 0.412 0.293 9.749 0.047 1.302 13.614 0.11 36735. 0.3087
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11.03 0.4158 0.6338 0.0560 0.0368 0.013 0.401 0.274 9.494 0.045 1.221 13.113 0.11 36806. 0.2879
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11.71 0.4418 0.6473 0.0522 0.0356 0.012 0.389 0.256 9.195 0.044 1.136 12.604 0.11 36880. 0.2670
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12.40 0.4678 0.6569 0.0482 0.0343 0.012 0.374 0.236 8.854 0.042 1.049 12.081 0.11 36958. 0.2459
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13.09 0.4938 0.6622 0.0440 0.0328 0.011 0.358 0.216 8.474 0.040 0.959 11.538 0.11 37039. 0.2245
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13.78 0.5198 0.6626 0.0398 0.0312 0.011 0.340 0.195 8.056 0.038 0.866 10.966 0.11 37123. 0.2028
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14.47 0.5458 0.6569 0.0354 0.0294 0.010 0.321 0.174 7.602 0.036 0.772 10.355 0.11 37211. 0.1808
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15.16 0.5717 0.6441 0.0310 0.0276 0.010 0.301 0.152 7.114 0.034 0.676 9.692 0.11 37302. 0.1584
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15.85 0.5977 0.6223 0.0266 0.0255 0.009 0.279 0.130 6.593 0.031 0.579 8.956 0.11 37396. 0.1354
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16.54 0.6237 0.5890 0.0221 0.0234 0.008 0.255 0.108 6.041 0.029 0.481 8.124 0.11 37494. 0.1120
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17.23 0.6497 0.5404 0.0176 0.0212 0.007 0.231 0.086 5.462 0.026 0.383 7.155 0.11 37596. 0.0880
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17.92 0.6757 0.4707 0.0131 0.0188 0.007 0.205 0.064 4.858 0.023 0.285 5.993 0.11 37701. 0.0636
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18.61 0.7017 0.3706 0.0087 0.0164 0.006 0.179 0.042 4.232 0.020 0.189 4.543 0.11 37809. 0.0392
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19.29 0.7277 0.2238 0.0043 0.0139 0.005 0.152 0.021 3.590 0.017 0.093 2.646 0.11 37921. 0.0161
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19.98 0.7537 -0.0004 0.0000 0.0114 0.004 0.124 0.000 2.936 0.014 0.000 -0.005 0.11 38035. 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 0.0936 0.0353 0.041 0.866 1.031 30.727 0.098 4.587 15.222 0.17 54091. 0.6479
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1.04 0.0260 0.0672 0.0924 0.0358 0.042 0.880 1.018 31.235 0.099 4.530 14.788 0.17 54128. 0.6255
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2.07 0.0521 0.1304 0.0911 0.0364 0.043 0.894 1.004 31.729 0.101 4.467 14.356 0.17 54169. 0.6030
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3.11 0.0781 0.1898 0.0897 0.0370 0.043 0.907 0.989 32.199 0.102 4.398 13.928 0.17 54214. 0.5805
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4.14 0.1042 0.2454 0.0882 0.0375 0.044 0.919 0.972 32.635 0.104 4.323 13.506 0.17 54263. 0.5580
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5.18 0.1302 0.2973 0.0865 0.0379 0.044 0.930 0.953 33.027 0.105 4.240 13.091 0.17 54316. 0.5357
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6.22 0.1563 0.3457 0.0847 0.0383 0.045 0.940 0.933 33.362 0.106 4.150 12.684 0.17 54374. 0.5135
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7.25 0.1823 0.3906 0.0827 0.0386 0.045 0.947 0.911 33.629 0.107 4.052 12.286 0.17 54436. 0.4915
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8.29 0.2084 0.4323 0.0805 0.0388 0.045 0.953 0.887 33.814 0.108 3.945 11.897 0.17 54502. 0.4696
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9.32 0.2344 0.4708 0.0781 0.0389 0.045 0.955 0.861 33.906 0.108 3.830 11.518 0.17 54573. 0.4479
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10.36 0.2605 0.5063 0.0756 0.0389 0.045 0.955 0.833 33.891 0.108 3.705 11.147 0.17 54650. 0.4264
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11.40 0.2865 0.5389 0.0729 0.0387 0.045 0.951 0.803 33.758 0.107 3.571 10.786 0.17 54731. 0.4050
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12.43 0.3126 0.5686 0.0699 0.0384 0.045 0.944 0.770 33.497 0.107 3.427 10.432 0.17 54817. 0.3838
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13.47 0.3386 0.5955 0.0668 0.0380 0.044 0.932 0.736 33.097 0.105 3.273 10.085 0.17 54908. 0.3626
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14.50 0.3647 0.6195 0.0634 0.0374 0.044 0.917 0.699 32.547 0.104 3.110 9.742 0.17 55005. 0.3414
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15.54 0.3907 0.6406 0.0599 0.0365 0.043 0.897 0.660 31.840 0.101 2.936 9.403 0.17 55106. 0.3202
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16.58 0.4168 0.6587 0.0562 0.0355 0.042 0.873 0.619 30.975 0.099 2.753 9.064 0.17 55213. 0.2989
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17.61 0.4428 0.6735 0.0523 0.0344 0.040 0.844 0.576 29.958 0.095 2.562 8.722 0.17 55324. 0.2775
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18.65 0.4689 0.6846 0.0483 0.0330 0.039 0.811 0.532 28.795 0.092 2.365 8.374 0.17 55441. 0.2559
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19.68 0.4949 0.6917 0.0441 0.0316 0.037 0.775 0.486 27.492 0.088 2.161 8.015 0.17 55563. 0.2342
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20.72 0.5210 0.6940 0.0398 0.0299 0.035 0.734 0.439 26.055 0.083 1.952 7.640 0.17 55690. 0.2121
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21.76 0.5470 0.6907 0.0355 0.0281 0.033 0.690 0.391 24.488 0.078 1.739 7.241 0.17 55823. 0.1898
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22.79 0.5731 0.6805 0.0311 0.0262 0.031 0.642 0.342 22.798 0.073 1.523 6.810 0.17 55960. 0.1670
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23.83 0.5991 0.6616 0.0266 0.0241 0.028 0.591 0.293 20.991 0.067 1.304 6.333 0.17 56102. 0.1437
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24.86 0.6252 0.6312 0.0221 0.0219 0.026 0.537 0.244 19.075 0.061 1.083 5.791 0.17 56250. 0.1198
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25.90 0.6512 0.5854 0.0176 0.0196 0.023 0.481 0.194 17.059 0.054 0.862 5.155 0.17 56403. 0.0951
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26.94 0.6773 0.5173 0.0131 0.0172 0.020 0.421 0.144 14.954 0.048 0.642 4.381 0.17 56561. 0.0698
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27.97 0.7033 0.4156 0.0087 0.0147 0.017 0.360 0.095 12.773 0.041 0.425 3.389 0.17 56724. 0.0439
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29.01 0.7294 0.2589 0.0043 0.0121 0.014 0.297 0.047 10.532 0.034 0.210 2.036 0.17 56892. 0.0185
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30.05 0.7554 0.0014 0.0000 0.0095 0.011 0.232 0.000 8.245 0.026 0.001 0.011 0.17 57064. 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 0.0939 0.0344 0.095 1.502 1.839 71.066 0.170 8.178 11.735 0.22 72120. 0.6669
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1.38 0.0261 0.0691 0.0927 0.0350 0.097 1.528 1.816 72.303 0.173 8.077 11.391 0.22 72170. 0.6433
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2.77 0.0522 0.1341 0.0914 0.0356 0.099 1.553 1.791 73.508 0.175 7.965 11.050 0.22 72225. 0.6197
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4.15 0.0783 0.1949 0.0900 0.0361 0.100 1.578 1.763 74.658 0.178 7.843 10.713 0.22 72285. 0.5962
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5.53 0.1044 0.2519 0.0885 0.0367 0.102 1.600 1.733 75.728 0.181 7.709 10.381 0.22 72350. 0.5728
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6.92 0.1305 0.3050 0.0868 0.0371 0.103 1.621 1.700 76.692 0.183 7.562 10.055 0.22 72421. 0.5495
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8.30 0.1566 0.3544 0.0850 0.0375 0.104 1.638 1.664 77.523 0.185 7.402 9.736 0.22 72498. 0.5264
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9.69 0.1826 0.4002 0.0829 0.0379 0.105 1.652 1.625 78.190 0.187 7.227 9.425 0.22 72581. 0.5035
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11.07 0.2087 0.4427 0.0808 0.0381 0.105 1.662 1.582 78.663 0.188 7.037 9.122 0.22 72670. 0.4809
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12.45 0.2348 0.4819 0.0784 0.0382 0.106 1.667 1.536 78.910 0.188 6.831 8.828 0.22 72765. 0.4585
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13.84 0.2609 0.5181 0.0759 0.0382 0.106 1.667 1.486 78.903 0.188 6.609 8.541 0.22 72867. 0.4363
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15.22 0.2870 0.5513 0.0731 0.0381 0.105 1.661 1.432 78.611 0.188 6.369 8.262 0.22 72976. 0.4144
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16.60 0.3131 0.5816 0.0702 0.0378 0.105 1.648 1.374 78.010 0.186 6.112 7.990 0.22 73091. 0.3926
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17.99 0.3392 0.6091 0.0670 0.0373 0.103 1.629 1.313 77.073 0.184 5.838 7.724 0.22 73213. 0.3709
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19.37 0.3653 0.6338 0.0637 0.0367 0.102 1.601 1.247 75.776 0.181 5.546 7.463 0.22 73342. 0.3493
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20.76 0.3914 0.6556 0.0601 0.0359 0.099 1.566 1.177 74.097 0.177 5.236 7.205 0.22 73478. 0.3276
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22.14 0.4175 0.6745 0.0563 0.0349 0.097 1.522 1.104 72.035 0.172 4.909 6.949 0.22 73620. 0.3060
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23.52 0.4436 0.6901 0.0524 0.0337 0.093 1.471 1.027 69.604 0.166 4.568 6.692 0.22 73770. 0.2843
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24.91 0.4697 0.7023 0.0484 0.0323 0.090 1.412 0.948 66.816 0.160 4.215 6.432 0.22 73926. 0.2624
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26.29 0.4958 0.7106 0.0442 0.0308 0.085 1.346 0.866 63.686 0.152 3.851 6.166 0.22 74089. 0.2404
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27.67 0.5218 0.7144 0.0399 0.0292 0.081 1.273 0.782 60.226 0.144 3.478 5.888 0.23 74259. 0.2182
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29.06 0.5479 0.7127 0.0355 0.0273 0.076 1.193 0.696 56.448 0.135 3.097 5.595 0.23 74436. 0.1957
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30.44 0.5740 0.7044 0.0311 0.0254 0.070 1.107 0.609 52.368 0.125 2.711 5.278 0.23 74620. 0.1727
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31.82 0.6001 0.6876 0.0266 0.0232 0.064 1.014 0.522 48.000 0.115 2.320 4.929 0.23 74811. 0.1492
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33.21 0.6262 0.6597 0.0221 0.0210 0.058 0.916 0.433 43.363 0.104 1.927 4.531 0.23 75008. 0.1250
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34.59 0.6523 0.6161 0.0176 0.0186 0.052 0.813 0.345 38.480 0.092 1.533 4.063 0.23 75212. 0.1000
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35.98 0.6784 0.5498 0.0131 0.0162 0.045 0.705 0.257 33.377 0.080 1.141 3.486 0.23 75424. 0.0740
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37.36 0.7045 0.4476 0.0086 0.0136 0.038 0.594 0.169 28.088 0.067 0.753 2.733 0.23 75642. 0.0471
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38.74 0.7306 0.2839 0.0043 0.0110 0.030 0.479 0.083 22.650 0.054 0.371 1.672 0.23 75867. 0.0202
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40.13 0.7567 -0.0013 0.0000 0.0083 0.023 0.361 0.000 17.102 0.041 -0.001 -0.007 0.23 76096. 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 0.0942 0.0339 0.183 2.311 2.883 136.719 0.261 12.821 9.563 0.28 90148. 0.6805
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1.73 0.0261 0.0704 0.0930 0.0345 0.187 2.353 2.847 139.186 0.266 12.664 9.278 0.28 90210. 0.6561
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3.46 0.0522 0.1365 0.0917 0.0351 0.190 2.394 2.808 141.591 0.270 12.490 8.995 0.28 90279. 0.6318
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5.19 0.0784 0.1985 0.0903 0.0357 0.193 2.432 2.765 143.890 0.275 12.300 8.717 0.28 90354. 0.6075
|
|
6.93 0.1045 0.2563 0.0888 0.0362 0.196 2.469 2.718 146.035 0.279 12.091 8.443 0.28 90436. 0.5834
|
|
8.66 0.1306 0.3102 0.0871 0.0367 0.198 2.501 2.667 147.973 0.283 11.862 8.174 0.28 90525. 0.5594
|
|
10.39 0.1567 0.3603 0.0853 0.0371 0.201 2.530 2.610 149.648 0.286 11.611 7.912 0.28 90621. 0.5358
|
|
12.12 0.1828 0.4068 0.0833 0.0374 0.202 2.553 2.549 151.002 0.288 11.338 7.656 0.28 90725. 0.5123
|
|
13.85 0.2089 0.4498 0.0811 0.0377 0.204 2.569 2.482 151.973 0.290 11.041 7.408 0.28 90837. 0.4892
|
|
15.58 0.2351 0.4896 0.0787 0.0378 0.205 2.578 2.410 152.500 0.291 10.718 7.167 0.28 90956. 0.4663
|
|
17.31 0.2612 0.5262 0.0762 0.0378 0.205 2.578 2.331 152.522 0.291 10.370 6.933 0.28 91084. 0.4437
|
|
19.04 0.2873 0.5598 0.0734 0.0377 0.204 2.569 2.247 151.983 0.290 9.994 6.706 0.28 91220. 0.4213
|
|
20.78 0.3134 0.5906 0.0705 0.0374 0.202 2.550 2.156 150.830 0.288 9.591 6.484 0.28 91365. 0.3991
|
|
22.51 0.3395 0.6185 0.0673 0.0369 0.200 2.519 2.060 149.013 0.285 9.161 6.269 0.28 91518. 0.3771
|
|
24.24 0.3656 0.6437 0.0639 0.0363 0.196 2.476 1.956 146.480 0.280 8.702 6.058 0.28 91679. 0.3551
|
|
25.97 0.3918 0.6661 0.0603 0.0355 0.192 2.421 1.847 143.188 0.273 8.215 5.850 0.28 91849. 0.3332
|
|
27.70 0.4179 0.6855 0.0566 0.0345 0.187 2.352 1.732 139.136 0.266 7.702 5.645 0.28 92028. 0.3113
|
|
29.43 0.4440 0.7019 0.0526 0.0333 0.180 2.271 1.611 134.346 0.257 7.167 5.440 0.28 92215. 0.2894
|
|
31.16 0.4701 0.7149 0.0486 0.0319 0.173 2.178 1.487 128.845 0.246 6.612 5.233 0.28 92411. 0.2674
|
|
32.89 0.4962 0.7242 0.0444 0.0304 0.164 2.073 1.358 122.658 0.234 6.041 5.022 0.28 92615. 0.2453
|
|
34.63 0.5223 0.7291 0.0401 0.0287 0.155 1.958 1.226 115.810 0.221 5.455 4.803 0.28 92828. 0.2229
|
|
36.36 0.5485 0.7287 0.0357 0.0269 0.145 1.831 1.092 108.325 0.207 4.857 4.572 0.28 93050. 0.2002
|
|
38.09 0.5746 0.7220 0.0312 0.0248 0.134 1.694 0.956 100.233 0.191 4.250 4.324 0.28 93280. 0.1772
|
|
39.82 0.6007 0.7071 0.0267 0.0227 0.123 1.548 0.818 91.563 0.175 3.637 4.050 0.28 93518. 0.1535
|
|
41.55 0.6268 0.6811 0.0222 0.0204 0.110 1.392 0.679 82.353 0.157 3.020 3.739 0.28 93766. 0.1291
|
|
43.28 0.6529 0.6397 0.0176 0.0180 0.097 1.228 0.540 72.648 0.139 2.402 3.371 0.28 94022. 0.1038
|
|
45.01 0.6790 0.5752 0.0131 0.0155 0.084 1.057 0.402 62.502 0.119 1.787 2.915 0.28 94286. 0.0774
|
|
46.74 0.7052 0.4735 0.0087 0.0129 0.070 0.879 0.265 51.982 0.099 1.178 2.311 0.28 94559. 0.0498
|
|
48.48 0.7313 0.3053 0.0043 0.0102 0.055 0.696 0.130 41.166 0.079 0.580 1.437 0.29 94841. 0.0217
|
|
50.21 0.7574 -0.0029 0.0000 0.0075 0.040 0.509 -0.001 30.125 0.058 -0.004 -0.013 0.29 95128. 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 0.0946 0.0336 0.314 3.298 4.167 234.103 0.373 18.536 8.074 0.33 108174. 0.6908
|
|
2.08 0.0261 0.0714 0.0934 0.0342 0.320 3.359 4.116 238.444 0.379 18.310 7.830 0.33 108250. 0.6659
|
|
4.16 0.0523 0.1383 0.0921 0.0348 0.325 3.419 4.061 242.680 0.386 18.061 7.589 0.33 108332. 0.6410
|
|
6.24 0.0784 0.2010 0.0907 0.0354 0.331 3.476 3.999 246.733 0.393 17.788 7.352 0.33 108423. 0.6162
|
|
8.31 0.1045 0.2595 0.0892 0.0359 0.336 3.529 3.932 250.520 0.399 17.488 7.118 0.33 108521. 0.5915
|
|
10.39 0.1307 0.3139 0.0875 0.0364 0.341 3.577 3.858 253.949 0.404 17.158 6.890 0.33 108628. 0.5672
|
|
12.47 0.1568 0.3645 0.0857 0.0369 0.345 3.619 3.777 256.921 0.409 16.798 6.667 0.33 108744. 0.5430
|
|
14.55 0.1829 0.4115 0.0837 0.0372 0.348 3.653 3.688 259.334 0.413 16.405 6.450 0.33 108868. 0.5192
|
|
16.63 0.2091 0.4549 0.0815 0.0375 0.350 3.678 3.592 261.079 0.416 15.976 6.240 0.33 109003. 0.4956
|
|
18.71 0.2352 0.4950 0.0791 0.0376 0.351 3.692 3.487 262.049 0.417 15.511 6.036 0.33 109146. 0.4724
|
|
20.79 0.2613 0.5320 0.0766 0.0376 0.352 3.693 3.374 262.137 0.417 15.008 5.838 0.33 109300. 0.4495
|
|
22.87 0.2875 0.5660 0.0738 0.0375 0.350 3.680 3.252 261.243 0.416 14.466 5.646 0.33 109464. 0.4268
|
|
24.94 0.3136 0.5971 0.0708 0.0372 0.348 3.652 3.121 259.274 0.413 13.884 5.460 0.33 109637. 0.4043
|
|
27.02 0.3397 0.6254 0.0676 0.0367 0.343 3.608 2.981 256.141 0.408 13.261 5.279 0.34 109821. 0.3821
|
|
29.10 0.3658 0.6510 0.0643 0.0361 0.338 3.546 2.832 251.754 0.401 12.598 5.103 0.34 110015. 0.3599
|
|
31.18 0.3920 0.6738 0.0607 0.0353 0.330 3.466 2.674 246.035 0.392 11.893 4.929 0.34 110220. 0.3378
|
|
33.26 0.4181 0.6938 0.0569 0.0343 0.320 3.367 2.507 238.979 0.380 11.151 4.758 0.34 110434. 0.3158
|
|
35.34 0.4442 0.7107 0.0529 0.0331 0.309 3.249 2.333 230.625 0.367 10.376 4.588 0.34 110659. 0.2937
|
|
37.42 0.4704 0.7245 0.0488 0.0317 0.296 3.113 2.152 221.018 0.352 9.573 4.417 0.34 110895. 0.2716
|
|
39.49 0.4965 0.7345 0.0446 0.0302 0.282 2.961 1.966 210.200 0.335 8.745 4.242 0.34 111140. 0.2493
|
|
41.57 0.5226 0.7403 0.0403 0.0284 0.266 2.792 1.775 198.216 0.315 7.896 4.062 0.34 111396. 0.2268
|
|
43.65 0.5488 0.7412 0.0359 0.0266 0.248 2.608 1.581 185.108 0.295 7.030 3.873 0.34 111662. 0.2041
|
|
45.73 0.5749 0.7358 0.0314 0.0245 0.229 2.408 1.383 170.924 0.272 6.152 3.670 0.34 111939. 0.1809
|
|
47.81 0.6010 0.7224 0.0268 0.0223 0.209 2.194 1.183 155.719 0.248 5.263 3.447 0.34 112226. 0.1571
|
|
49.89 0.6272 0.6982 0.0223 0.0200 0.187 1.966 0.982 139.559 0.222 4.369 3.193 0.34 112523. 0.1326
|
|
51.97 0.6533 0.6588 0.0177 0.0176 0.164 1.726 0.781 122.523 0.195 3.475 2.892 0.34 112830. 0.1071
|
|
54.05 0.6794 0.5962 0.0132 0.0150 0.140 1.475 0.581 104.708 0.167 2.584 2.516 0.34 113148. 0.0804
|
|
56.12 0.7056 0.4954 0.0087 0.0124 0.116 1.215 0.383 86.231 0.137 1.703 2.013 0.34 113476. 0.0522
|
|
58.20 0.7317 0.3240 0.0043 0.0096 0.090 0.947 0.188 67.233 0.107 0.837 1.270 0.34 113815. 0.0231
|
|
60.28 0.7578 -0.0044 0.0000 0.0069 0.064 0.674 -0.002 47.835 0.076 -0.008 -0.017 0.34 114159. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 7000
|
|
|
|
V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
|
|
(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
|
|
0.00 0.0000 0.0000 0.0950 0.0334 0.496 4.467 5.698 369.960 0.505 25.345 6.986 0.39 126199. 0.6989
|
|
2.43 0.0261 0.0720 0.0938 0.0341 0.506 4.552 5.629 376.970 0.514 25.040 6.773 0.39 126287. 0.6736
|
|
4.85 0.0523 0.1396 0.0926 0.0347 0.515 4.634 5.554 383.816 0.524 24.704 6.563 0.39 126384. 0.6483
|
|
7.28 0.0784 0.2028 0.0912 0.0353 0.524 4.714 5.471 390.374 0.533 24.333 6.356 0.39 126489. 0.6231
|
|
9.70 0.1046 0.2617 0.0897 0.0358 0.532 4.788 5.379 396.508 0.541 23.926 6.153 0.39 126604. 0.5981
|
|
12.13 0.1307 0.3166 0.0880 0.0363 0.539 4.855 5.279 402.071 0.548 23.479 5.955 0.39 126729. 0.5734
|
|
14.55 0.1568 0.3676 0.0862 0.0368 0.546 4.913 5.168 406.905 0.555 22.989 5.761 0.39 126864. 0.5489
|
|
16.98 0.1830 0.4149 0.0842 0.0371 0.551 4.961 5.048 410.843 0.560 22.454 5.573 0.39 127010. 0.5248
|
|
19.41 0.2091 0.4586 0.0820 0.0374 0.555 4.995 4.917 413.709 0.564 21.871 5.391 0.39 127167. 0.5010
|
|
21.83 0.2353 0.4991 0.0796 0.0375 0.557 5.015 4.775 415.331 0.567 21.237 5.214 0.39 127335. 0.4775
|
|
24.26 0.2614 0.5363 0.0770 0.0375 0.557 5.017 4.620 415.536 0.567 20.551 5.043 0.39 127515. 0.4543
|
|
26.68 0.2875 0.5706 0.0742 0.0374 0.555 5.001 4.454 414.161 0.565 19.811 4.878 0.39 127706. 0.4314
|
|
29.11 0.3137 0.6020 0.0713 0.0371 0.551 4.963 4.275 411.055 0.561 19.016 4.717 0.39 127909. 0.4088
|
|
31.54 0.3398 0.6306 0.0681 0.0367 0.545 4.903 4.084 406.076 0.554 18.165 4.562 0.39 128123. 0.3864
|
|
33.96 0.3659 0.6565 0.0647 0.0361 0.535 4.819 3.880 399.078 0.544 17.258 4.410 0.39 128350. 0.3640
|
|
36.39 0.3921 0.6797 0.0611 0.0352 0.523 4.708 3.663 389.932 0.532 16.294 4.261 0.39 128589. 0.3418
|
|
38.81 0.4182 0.7001 0.0573 0.0342 0.508 4.572 3.435 378.629 0.517 15.278 4.115 0.39 128840. 0.3196
|
|
41.24 0.4444 0.7176 0.0533 0.0330 0.490 4.410 3.196 365.227 0.498 14.217 3.969 0.39 129103. 0.2974
|
|
43.66 0.4705 0.7319 0.0492 0.0316 0.469 4.224 2.949 349.798 0.477 13.116 3.824 0.39 129378. 0.2752
|
|
46.09 0.4966 0.7427 0.0449 0.0300 0.446 4.014 2.694 332.410 0.453 11.982 3.676 0.39 129664. 0.2528
|
|
48.52 0.5228 0.7494 0.0405 0.0283 0.420 3.781 2.432 313.131 0.427 10.819 3.523 0.39 129963. 0.2303
|
|
50.94 0.5489 0.7512 0.0361 0.0264 0.392 3.526 2.166 292.032 0.398 9.633 3.364 0.39 130274. 0.2075
|
|
53.37 0.5751 0.7470 0.0316 0.0243 0.361 3.250 1.895 269.189 0.367 8.428 3.193 0.40 130597. 0.1842
|
|
55.79 0.6012 0.7350 0.0270 0.0221 0.328 2.955 1.621 244.691 0.334 7.211 3.005 0.40 130932. 0.1604
|
|
58.22 0.6273 0.7125 0.0224 0.0198 0.293 2.640 1.346 218.645 0.298 5.986 2.792 0.40 131279. 0.1357
|
|
60.65 0.6535 0.6749 0.0178 0.0173 0.256 2.308 1.070 191.177 0.261 4.759 2.539 0.40 131638. 0.1101
|
|
63.07 0.6796 0.6142 0.0133 0.0147 0.218 1.961 0.796 162.446 0.222 3.539 2.221 0.40 132009. 0.0830
|
|
65.50 0.7058 0.5145 0.0087 0.0120 0.178 1.602 0.524 132.644 0.181 2.331 1.792 0.40 132392. 0.0544
|
|
67.92 0.7319 0.3409 0.0043 0.0092 0.137 1.232 0.257 101.999 0.139 1.145 1.145 0.40 132787. 0.0243
|
|
70.35 0.7580 -0.0056 0.0000 0.0064 0.095 0.854 -0.003 70.704 0.096 -0.013 -0.018 0.40 133189. 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 0.0955 0.0334 0.740 5.826 7.482 551.462 0.658 33.278 6.154 0.44 144222. 0.7054
|
|
2.77 0.0261 0.0725 0.0944 0.0340 0.754 5.939 7.393 562.103 0.671 32.884 5.966 0.44 144323. 0.6798
|
|
5.55 0.0523 0.1405 0.0931 0.0346 0.768 6.049 7.295 572.505 0.683 32.448 5.780 0.44 144433. 0.6542
|
|
8.32 0.0784 0.2041 0.0917 0.0353 0.781 6.154 7.187 582.476 0.695 31.968 5.596 0.44 144554. 0.6288
|
|
11.09 0.1046 0.2634 0.0902 0.0358 0.794 6.253 7.068 591.813 0.706 31.439 5.417 0.44 144686. 0.6036
|
|
13.86 0.1307 0.3186 0.0885 0.0363 0.805 6.342 6.937 600.293 0.717 30.857 5.242 0.44 144829. 0.5786
|
|
16.64 0.1568 0.3698 0.0867 0.0368 0.815 6.420 6.794 607.676 0.725 30.219 5.071 0.44 144983. 0.5540
|
|
19.41 0.1830 0.4173 0.0847 0.0371 0.823 6.484 6.637 613.708 0.733 29.521 4.905 0.45 145150. 0.5296
|
|
22.18 0.2091 0.4613 0.0825 0.0374 0.829 6.531 6.466 618.124 0.738 28.759 4.744 0.45 145330. 0.5056
|
|
24.95 0.2353 0.5020 0.0801 0.0376 0.832 6.557 6.279 620.657 0.741 27.930 4.589 0.45 145522. 0.4819
|
|
27.73 0.2614 0.5395 0.0776 0.0376 0.833 6.562 6.077 621.049 0.741 27.032 4.438 0.45 145728. 0.4586
|
|
30.50 0.2876 0.5740 0.0748 0.0375 0.830 6.540 5.859 619.050 0.739 26.063 4.293 0.45 145946. 0.4355
|
|
33.27 0.3137 0.6057 0.0718 0.0372 0.824 6.492 5.625 614.430 0.733 25.020 4.152 0.45 146178. 0.4128
|
|
36.04 0.3398 0.6346 0.0686 0.0367 0.814 6.413 5.374 606.973 0.725 23.904 4.016 0.45 146424. 0.3902
|
|
38.82 0.3660 0.6608 0.0652 0.0361 0.800 6.302 5.106 596.459 0.712 22.713 3.883 0.45 146684. 0.3678
|
|
41.59 0.3921 0.6843 0.0615 0.0353 0.781 6.156 4.822 582.691 0.696 21.447 3.753 0.45 146957. 0.3454
|
|
44.36 0.4183 0.7051 0.0577 0.0342 0.759 5.976 4.522 565.646 0.675 20.112 3.626 0.45 147244. 0.3231
|
|
47.13 0.4444 0.7231 0.0537 0.0330 0.731 5.762 4.208 545.412 0.651 18.717 3.499 0.45 147545. 0.3009
|
|
49.91 0.4705 0.7379 0.0496 0.0316 0.700 5.516 3.882 522.095 0.623 17.269 3.373 0.45 147859. 0.2785
|
|
52.68 0.4967 0.7494 0.0453 0.0300 0.665 5.238 3.547 495.799 0.592 15.777 3.245 0.45 148187. 0.2561
|
|
55.45 0.5228 0.7568 0.0409 0.0282 0.626 4.930 3.203 466.626 0.557 14.246 3.113 0.45 148529. 0.2335
|
|
58.22 0.5490 0.7595 0.0364 0.0263 0.583 4.593 2.852 434.682 0.519 12.685 2.976 0.45 148885. 0.2106
|
|
61.00 0.5751 0.7564 0.0318 0.0242 0.537 4.227 2.495 400.083 0.478 11.099 2.829 0.45 149254. 0.1873
|
|
63.77 0.6012 0.7458 0.0272 0.0220 0.487 3.835 2.135 362.965 0.433 9.495 2.668 0.45 149637. 0.1634
|
|
66.54 0.6274 0.7248 0.0226 0.0196 0.434 3.418 1.772 323.487 0.386 7.882 2.485 0.45 150033. 0.1386
|
|
69.31 0.6535 0.6889 0.0180 0.0171 0.378 2.978 1.409 281.847 0.336 6.266 2.267 0.45 150444. 0.1128
|
|
72.09 0.6797 0.6300 0.0134 0.0144 0.320 2.518 1.047 238.284 0.284 4.658 1.994 0.45 150868. 0.0855
|
|
74.86 0.7058 0.5317 0.0088 0.0117 0.259 2.040 0.690 193.091 0.230 3.068 1.620 0.46 151306. 0.0564
|
|
77.63 0.7319 0.3564 0.0043 0.0089 0.197 1.549 0.339 146.619 0.175 1.506 1.047 0.46 151757. 0.0255
|
|
80.40 0.7581 -0.0068 -0.0001 0.0060 0.133 1.048 -0.004 99.156 0.118 -0.019 -0.019 0.46 152216. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 9000
|
|
|
|
V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
|
|
(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
|
|
0.00 0.0000 0.0000 0.0961 0.0334 1.055 7.385 9.526 786.353 0.834 42.373 5.495 0.50 162243. 0.7108
|
|
3.12 0.0261 0.0728 0.0949 0.0341 1.075 7.530 9.415 801.773 0.851 41.879 5.326 0.50 162356. 0.6850
|
|
6.24 0.0523 0.1411 0.0937 0.0347 1.095 7.671 9.293 816.858 0.867 41.334 5.160 0.50 162480. 0.6592
|
|
9.36 0.0784 0.2049 0.0923 0.0353 1.115 7.807 9.157 831.331 0.882 40.730 4.996 0.50 162616. 0.6336
|
|
12.48 0.1046 0.2645 0.0908 0.0359 1.133 7.935 9.007 844.897 0.896 40.065 4.836 0.50 162765. 0.6082
|
|
15.59 0.1307 0.3199 0.0892 0.0364 1.150 8.051 8.843 857.234 0.910 39.333 4.679 0.50 162926. 0.5831
|
|
18.71 0.1568 0.3713 0.0873 0.0369 1.164 8.152 8.662 867.995 0.921 38.528 4.526 0.50 163100. 0.5583
|
|
21.83 0.1830 0.4190 0.0853 0.0373 1.176 8.234 8.464 876.809 0.930 37.646 4.378 0.50 163288. 0.5338
|
|
24.95 0.2091 0.4632 0.0832 0.0375 1.185 8.295 8.247 883.293 0.937 36.682 4.235 0.50 163490. 0.5097
|
|
28.07 0.2352 0.5040 0.0808 0.0377 1.190 8.331 8.011 887.062 0.941 35.633 4.096 0.50 163707. 0.4859
|
|
31.19 0.2614 0.5417 0.0782 0.0377 1.190 8.337 7.755 887.736 0.942 34.494 3.962 0.50 163938. 0.4625
|
|
34.31 0.2875 0.5765 0.0754 0.0376 1.187 8.311 7.478 884.953 0.939 33.263 3.833 0.50 164185. 0.4393
|
|
37.43 0.3137 0.6083 0.0724 0.0373 1.178 8.249 7.181 878.381 0.932 31.939 3.708 0.50 164446. 0.4164
|
|
40.54 0.3398 0.6375 0.0692 0.0369 1.164 8.149 6.861 867.706 0.921 30.520 3.587 0.50 164723. 0.3938
|
|
43.66 0.3659 0.6640 0.0658 0.0362 1.143 8.007 6.521 852.611 0.905 29.004 3.469 0.50 165016. 0.3713
|
|
46.78 0.3921 0.6878 0.0621 0.0354 1.117 7.821 6.158 832.808 0.884 27.392 3.354 0.50 165323. 0.3488
|
|
49.90 0.4182 0.7090 0.0582 0.0344 1.084 7.591 5.776 808.254 0.858 25.690 3.241 0.50 165646. 0.3265
|
|
53.02 0.4443 0.7274 0.0542 0.0331 1.045 7.317 5.376 779.073 0.827 23.911 3.130 0.50 165985. 0.3041
|
|
56.14 0.4705 0.7428 0.0500 0.0317 1.000 7.001 4.960 745.418 0.791 22.064 3.018 0.51 166339. 0.2817
|
|
59.26 0.4966 0.7549 0.0457 0.0301 0.949 6.644 4.532 707.438 0.751 20.159 2.906 0.51 166708. 0.2593
|
|
62.38 0.5228 0.7630 0.0413 0.0283 0.892 6.248 4.093 665.283 0.706 18.205 2.790 0.51 167093. 0.2366
|
|
65.49 0.5489 0.7666 0.0368 0.0263 0.830 5.814 3.644 619.103 0.657 16.211 2.670 0.51 167493. 0.2136
|
|
68.61 0.5750 0.7645 0.0322 0.0242 0.763 5.344 3.189 569.069 0.604 14.185 2.542 0.51 167909. 0.1902
|
|
71.73 0.6012 0.7551 0.0275 0.0219 0.691 4.840 2.728 515.376 0.547 12.136 2.401 0.51 168340. 0.1662
|
|
74.85 0.6273 0.7356 0.0228 0.0195 0.615 4.304 2.265 458.257 0.486 10.074 2.242 0.51 168786. 0.1414
|
|
77.97 0.6535 0.7014 0.0182 0.0169 0.534 3.738 1.801 397.996 0.422 8.009 2.052 0.51 169248. 0.1154
|
|
81.09 0.6796 0.6443 0.0135 0.0142 0.449 3.146 1.338 334.944 0.355 5.953 1.812 0.51 169725. 0.0879
|
|
84.21 0.7057 0.5474 0.0089 0.0115 0.361 2.531 0.881 269.529 0.286 3.919 1.483 0.51 170218. 0.0583
|
|
87.33 0.7319 0.3711 0.0044 0.0086 0.271 1.900 0.432 202.262 0.215 1.923 0.969 0.51 170725. 0.0267
|
|
90.44 0.7580 -0.0082 -0.0001 0.0057 0.179 1.254 -0.006 133.553 0.142 -0.027 -0.021 0.51 171241. 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 0.0967 0.0336 1.452 9.155 11.841 1083.112 1.034 52.670 4.959 0.56 180260. 0.7152
|
|
3.46 0.0261 0.0730 0.0956 0.0342 1.481 9.337 11.707 1104.671 1.055 52.071 4.807 0.56 180386. 0.6893
|
|
6.93 0.0523 0.1414 0.0944 0.0349 1.510 9.515 11.557 1125.781 1.075 51.406 4.656 0.56 180524. 0.6634
|
|
10.39 0.0784 0.2054 0.0930 0.0355 1.537 9.687 11.391 1146.049 1.094 50.669 4.508 0.56 180676. 0.6377
|
|
13.86 0.1045 0.2651 0.0916 0.0361 1.562 9.847 11.208 1165.068 1.113 49.855 4.363 0.56 180841. 0.6123
|
|
17.32 0.1307 0.3206 0.0899 0.0366 1.586 9.994 11.006 1182.387 1.129 48.956 4.222 0.56 181020. 0.5871
|
|
20.79 0.1568 0.3722 0.0881 0.0371 1.606 10.122 10.784 1197.517 1.144 47.967 4.085 0.56 181214. 0.5622
|
|
24.25 0.1829 0.4201 0.0861 0.0375 1.623 10.227 10.540 1209.944 1.155 46.882 3.951 0.56 181423. 0.5376
|
|
27.71 0.2090 0.4644 0.0839 0.0378 1.635 10.304 10.273 1219.128 1.164 45.694 3.822 0.56 181648. 0.5134
|
|
31.18 0.2352 0.5054 0.0815 0.0379 1.642 10.350 9.982 1224.531 1.169 44.398 3.697 0.56 181889. 0.4896
|
|
34.64 0.2613 0.5432 0.0789 0.0380 1.644 10.359 9.665 1225.618 1.170 42.990 3.577 0.56 182147. 0.4660
|
|
38.11 0.2874 0.5781 0.0761 0.0379 1.639 10.328 9.322 1221.885 1.167 41.466 3.461 0.56 182421. 0.4428
|
|
41.57 0.3136 0.6102 0.0731 0.0376 1.626 10.251 8.953 1212.861 1.158 39.824 3.348 0.56 182712. 0.4199
|
|
45.04 0.3397 0.6396 0.0699 0.0371 1.607 10.127 8.557 1198.112 1.144 38.063 3.240 0.56 183020. 0.3972
|
|
48.50 0.3658 0.6664 0.0664 0.0365 1.579 9.950 8.134 1177.198 1.124 36.180 3.134 0.56 183345. 0.3746
|
|
51.97 0.3920 0.6905 0.0628 0.0356 1.542 9.718 7.683 1149.713 1.098 34.176 3.031 0.56 183687. 0.3521
|
|
55.43 0.4181 0.7121 0.0589 0.0346 1.496 9.429 7.208 1115.581 1.065 32.059 2.930 0.56 184047. 0.3297
|
|
58.89 0.4442 0.7309 0.0548 0.0333 1.442 9.086 6.709 1074.973 1.027 29.844 2.831 0.56 184423. 0.3073
|
|
62.36 0.4704 0.7468 0.0506 0.0319 1.379 8.690 6.192 1028.101 0.982 27.543 2.732 0.56 184817. 0.2849
|
|
65.82 0.4965 0.7594 0.0462 0.0302 1.308 8.242 5.658 975.176 0.931 25.168 2.632 0.56 185227. 0.2624
|
|
69.29 0.5226 0.7683 0.0417 0.0284 1.229 7.746 5.111 916.406 0.875 22.732 2.529 0.56 185655. 0.2397
|
|
72.75 0.5488 0.7727 0.0372 0.0264 1.143 7.201 4.551 852.002 0.814 20.244 2.423 0.56 186100. 0.2166
|
|
76.22 0.5749 0.7716 0.0325 0.0242 1.049 6.611 3.983 782.202 0.747 17.715 2.309 0.56 186562. 0.1932
|
|
79.68 0.6010 0.7634 0.0278 0.0219 0.948 5.978 3.408 707.279 0.675 15.157 2.185 0.57 187040. 0.1691
|
|
83.14 0.6271 0.7452 0.0231 0.0194 0.842 5.304 2.829 627.560 0.599 12.582 2.044 0.57 187536. 0.1441
|
|
86.61 0.6533 0.7127 0.0184 0.0168 0.729 4.593 2.249 543.444 0.519 10.003 1.877 0.57 188049. 0.1180
|
|
90.07 0.6794 0.6574 0.0137 0.0141 0.611 3.849 1.672 455.422 0.435 7.435 1.665 0.57 188579. 0.0902
|
|
93.54 0.7055 0.5621 0.0090 0.0113 0.488 3.077 1.100 364.094 0.348 4.894 1.371 0.57 189127. 0.0603
|
|
97.00 0.7317 0.3851 0.0044 0.0084 0.362 2.284 0.539 270.183 0.258 2.399 0.906 0.57 189690. 0.0279
|
|
100.47 0.7578 -0.0095 -0.0001 0.0054 0.234 1.473 -0.008 174.254 0.166 -0.037 -0.022 0.57 190263. 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 0.0975 0.0338 1.946 11.151 14.439 1451.217 1.260 64.224 4.513 0.61 198274. 0.7187
|
|
3.81 0.0261 0.0730 0.0964 0.0345 1.985 11.376 14.279 1480.521 1.285 63.512 4.374 0.61 198413. 0.6928
|
|
7.62 0.0522 0.1415 0.0952 0.0351 2.024 11.597 14.101 1509.241 1.310 62.720 4.238 0.61 198565. 0.6669
|
|
11.43 0.0784 0.2056 0.0939 0.0358 2.061 11.809 13.903 1536.845 1.334 61.841 4.103 0.61 198732. 0.6412
|
|
15.24 0.1045 0.2653 0.0924 0.0364 2.096 12.008 13.684 1562.777 1.357 60.867 3.972 0.61 198913. 0.6158
|
|
19.05 0.1306 0.3209 0.0907 0.0369 2.127 12.190 13.442 1586.421 1.377 59.790 3.843 0.61 199111. 0.5905
|
|
22.85 0.1567 0.3725 0.0889 0.0374 2.155 12.349 13.175 1607.114 1.395 58.601 3.718 0.61 199324. 0.5656
|
|
26.66 0.1828 0.4205 0.0870 0.0378 2.178 12.480 12.881 1624.156 1.410 57.293 3.597 0.61 199555. 0.5411
|
|
30.47 0.2090 0.4649 0.0848 0.0381 2.195 12.577 12.558 1636.812 1.421 55.859 3.480 0.61 199803. 0.5169
|
|
34.28 0.2351 0.5060 0.0824 0.0383 2.205 12.635 12.206 1644.346 1.427 54.291 3.367 0.61 200068. 0.4930
|
|
38.09 0.2612 0.5440 0.0798 0.0383 2.207 12.648 11.822 1646.030 1.429 52.585 3.258 0.61 200352. 0.4695
|
|
41.90 0.2873 0.5791 0.0770 0.0382 2.201 12.611 11.406 1641.175 1.425 50.736 3.152 0.61 200654. 0.4462
|
|
45.71 0.3134 0.6113 0.0740 0.0379 2.185 12.518 10.958 1629.140 1.414 48.741 3.051 0.61 200975. 0.4233
|
|
49.52 0.3396 0.6410 0.0707 0.0375 2.158 12.366 10.476 1609.336 1.397 46.598 2.953 0.61 201314. 0.4005
|
|
53.33 0.3657 0.6680 0.0672 0.0368 2.120 12.150 9.961 1581.176 1.373 44.305 2.857 0.61 201672. 0.3780
|
|
57.14 0.3918 0.6925 0.0635 0.0359 2.071 11.865 9.411 1544.098 1.340 41.862 2.765 0.62 202049. 0.3555
|
|
60.95 0.4179 0.7144 0.0596 0.0349 2.009 11.510 8.831 1497.983 1.300 39.278 2.674 0.62 202444. 0.3330
|
|
64.75 0.4440 0.7336 0.0555 0.0336 1.935 11.088 8.222 1443.054 1.253 36.572 2.584 0.62 202859. 0.3106
|
|
68.56 0.4702 0.7500 0.0512 0.0321 1.850 10.601 7.590 1379.602 1.198 33.759 2.495 0.62 203292. 0.2881
|
|
72.37 0.4963 0.7632 0.0468 0.0304 1.754 10.050 6.937 1307.914 1.135 30.854 2.406 0.62 203744. 0.2655
|
|
76.18 0.5224 0.7728 0.0423 0.0286 1.647 9.438 6.266 1228.275 1.066 27.872 2.314 0.62 204214. 0.2428
|
|
79.99 0.5485 0.7780 0.0377 0.0266 1.530 8.767 5.581 1140.977 0.991 24.825 2.219 0.62 204704. 0.2197
|
|
83.80 0.5746 0.7779 0.0330 0.0244 1.403 8.040 4.885 1046.339 0.908 21.728 2.117 0.62 205212. 0.1961
|
|
87.61 0.6007 0.7708 0.0282 0.0220 1.267 7.259 4.180 944.733 0.820 18.593 2.007 0.62 205738. 0.1720
|
|
91.42 0.6269 0.7540 0.0234 0.0195 1.122 6.428 3.470 836.605 0.726 15.436 1.881 0.62 206284. 0.1469
|
|
95.23 0.6530 0.7231 0.0186 0.0168 0.969 5.552 2.759 722.498 0.627 12.273 1.732 0.62 206848. 0.1206
|
|
99.04 0.6791 0.6697 0.0138 0.0140 0.809 4.634 2.051 603.079 0.524 9.122 1.542 0.62 207430. 0.0926
|
|
102.85 0.7052 0.5762 0.0091 0.0112 0.643 3.682 1.350 479.170 0.416 6.005 1.278 0.63 208032. 0.0622
|
|
106.65 0.7313 0.3989 0.0045 0.0082 0.472 2.703 0.662 351.761 0.305 2.943 0.853 0.63 208652. 0.0291
|
|
110.46 0.7575 -0.0105 -0.0001 0.0052 0.297 1.703 -0.011 221.613 0.192 -0.047 -0.022 0.63 209280. 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 0.0983 0.0341 2.550 13.396 17.332 1901.907 1.513 77.094 4.133 0.67 216284. 0.7212
|
|
4.15 0.0261 0.0730 0.0973 0.0348 2.603 13.670 17.147 1940.743 1.544 76.268 4.007 0.67 216435. 0.6955
|
|
8.31 0.0522 0.1414 0.0961 0.0355 2.654 13.938 16.939 1978.881 1.575 75.346 3.883 0.67 216602. 0.6697
|
|
12.46 0.0783 0.2054 0.0948 0.0361 2.703 14.197 16.708 2015.603 1.604 74.319 3.760 0.67 216783. 0.6441
|
|
16.61 0.1044 0.2651 0.0933 0.0368 2.749 14.440 16.452 2050.165 1.631 73.176 3.640 0.67 216982. 0.6187
|
|
20.76 0.1305 0.3206 0.0917 0.0373 2.792 14.663 16.167 2081.735 1.657 71.909 3.522 0.67 217197. 0.5936
|
|
24.92 0.1566 0.3723 0.0899 0.0378 2.829 14.858 15.851 2109.415 1.679 70.507 3.408 0.67 217431. 0.5687
|
|
29.07 0.1827 0.4203 0.0879 0.0382 2.859 15.019 15.504 2132.276 1.697 68.960 3.298 0.67 217683. 0.5442
|
|
33.22 0.2088 0.4648 0.0858 0.0385 2.882 15.139 15.121 2149.338 1.710 67.259 3.191 0.67 217953. 0.5201
|
|
37.38 0.2349 0.5060 0.0834 0.0387 2.896 15.211 14.702 2159.622 1.719 65.397 3.088 0.67 218243. 0.4962
|
|
41.53 0.2610 0.5441 0.0808 0.0388 2.899 15.229 14.246 2162.152 1.721 63.365 2.988 0.67 218553. 0.4727
|
|
45.68 0.2871 0.5793 0.0780 0.0387 2.891 15.186 13.750 2156.011 1.716 61.158 2.893 0.67 218883. 0.4495
|
|
49.83 0.3132 0.6118 0.0750 0.0384 2.870 15.076 13.214 2140.341 1.703 58.774 2.800 0.67 219233. 0.4266
|
|
53.99 0.3393 0.6416 0.0717 0.0379 2.835 14.893 12.637 2114.360 1.683 56.209 2.711 0.67 219604. 0.4039
|
|
58.14 0.3655 0.6689 0.0682 0.0372 2.786 14.632 12.019 2077.302 1.653 53.460 2.624 0.67 219995. 0.3813
|
|
62.29 0.3916 0.6937 0.0644 0.0364 2.720 14.287 11.360 2028.418 1.614 50.528 2.540 0.67 220407. 0.3588
|
|
66.45 0.4177 0.7160 0.0605 0.0353 2.638 13.858 10.662 1967.516 1.566 47.424 2.458 0.67 220839. 0.3364
|
|
70.60 0.4438 0.7356 0.0563 0.0340 2.541 13.347 9.930 1894.887 1.508 44.168 2.377 0.67 221291. 0.3139
|
|
74.75 0.4699 0.7525 0.0520 0.0325 2.428 12.755 9.168 1810.919 1.441 40.781 2.296 0.67 221764. 0.2914
|
|
78.90 0.4960 0.7663 0.0475 0.0308 2.301 12.087 8.382 1716.003 1.366 37.281 2.215 0.67 222257. 0.2688
|
|
83.06 0.5221 0.7766 0.0430 0.0289 2.160 11.344 7.573 1610.516 1.282 33.686 2.133 0.68 222770. 0.2460
|
|
87.21 0.5482 0.7827 0.0383 0.0268 2.005 10.529 6.747 1494.849 1.190 30.010 2.047 0.68 223304. 0.2229
|
|
91.36 0.5743 0.7835 0.0335 0.0246 1.836 9.646 5.906 1369.427 1.090 26.270 1.956 0.68 223858. 0.1992
|
|
95.52 0.6004 0.7775 0.0287 0.0221 1.656 8.697 5.055 1234.747 0.983 22.484 1.857 0.68 224432. 0.1750
|
|
99.67 0.6265 0.7622 0.0238 0.0196 1.464 7.687 4.197 1091.399 0.869 18.670 1.744 0.68 225027. 0.1498
|
|
103.82 0.6526 0.7330 0.0189 0.0169 1.261 6.622 3.338 940.106 0.748 14.846 1.610 0.68 225642. 0.1233
|
|
107.97 0.6787 0.6814 0.0141 0.0140 1.048 5.506 2.481 781.766 0.622 11.036 1.440 0.68 226277. 0.0950
|
|
112.13 0.7048 0.5897 0.0093 0.0111 0.828 4.349 1.633 617.501 0.491 7.265 1.200 0.68 226933. 0.0643
|
|
116.28 0.7309 0.4125 0.0045 0.0080 0.602 3.160 0.800 448.688 0.357 3.560 0.809 0.68 227608. 0.0303
|
|
120.43 0.7570 -0.0114 -0.0001 0.0050 0.371 1.947 -0.013 276.412 0.220 -0.059 -0.022 0.69 228293. 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 0.0993 0.0347 3.301 16.003 20.537 2461.306 1.808 91.348 3.785 0.72 234289. 0.7188
|
|
4.49 0.0261 0.0724 0.0982 0.0354 3.366 16.317 20.326 2509.714 1.844 90.412 3.673 0.72 234453. 0.6941
|
|
8.99 0.0522 0.1404 0.0971 0.0361 3.430 16.627 20.090 2557.389 1.879 89.361 3.563 0.72 234633. 0.6694
|
|
13.48 0.0782 0.2042 0.0958 0.0367 3.491 16.927 19.826 2603.443 1.912 88.185 3.454 0.72 234830. 0.6446
|
|
17.98 0.1043 0.2638 0.0944 0.0373 3.550 17.210 19.531 2646.948 1.944 86.872 3.347 0.72 235045. 0.6199
|
|
22.47 0.1304 0.3194 0.0928 0.0379 3.603 17.469 19.202 2686.863 1.974 85.409 3.241 0.72 235279. 0.5953
|
|
26.97 0.1565 0.3711 0.0910 0.0384 3.650 17.698 18.836 2722.051 2.000 83.784 3.139 0.72 235532. 0.5709
|
|
31.46 0.1826 0.4192 0.0891 0.0388 3.690 17.888 18.432 2751.277 2.021 81.985 3.039 0.72 235805. 0.5468
|
|
35.96 0.2086 0.4637 0.0869 0.0391 3.719 18.031 17.986 2773.258 2.037 80.001 2.942 0.72 236099. 0.5229
|
|
40.45 0.2347 0.5051 0.0846 0.0393 3.737 18.118 17.496 2786.663 2.047 77.822 2.848 0.72 236413. 0.4992
|
|
44.95 0.2608 0.5433 0.0820 0.0394 3.742 18.141 16.960 2790.169 2.050 75.439 2.757 0.72 236750. 0.4759
|
|
49.44 0.2869 0.5787 0.0792 0.0392 3.731 18.091 16.377 2782.497 2.044 72.844 2.670 0.72 237108. 0.4528
|
|
53.94 0.3130 0.6113 0.0761 0.0390 3.705 17.961 15.745 2762.462 2.029 70.034 2.585 0.73 237487. 0.4299
|
|
58.43 0.3391 0.6414 0.0728 0.0385 3.660 17.743 15.064 2729.008 2.005 67.006 2.504 0.73 237889. 0.4073
|
|
62.93 0.3651 0.6690 0.0693 0.0378 3.595 17.432 14.334 2681.136 1.969 63.756 2.425 0.73 238313. 0.3848
|
|
67.42 0.3912 0.6941 0.0655 0.0369 3.511 17.021 13.553 2617.874 1.923 60.284 2.348 0.73 238759. 0.3623
|
|
71.92 0.4173 0.7168 0.0615 0.0358 3.405 16.507 12.725 2538.922 1.865 56.602 2.273 0.73 239228. 0.3399
|
|
76.41 0.4434 0.7369 0.0573 0.0345 3.278 15.894 11.856 2444.646 1.796 52.735 2.200 0.73 239718. 0.3174
|
|
80.91 0.4695 0.7543 0.0529 0.0329 3.132 15.185 10.951 2335.562 1.716 48.709 2.127 0.73 240231. 0.2950
|
|
85.40 0.4955 0.7688 0.0484 0.0312 2.967 14.383 10.014 2212.188 1.625 44.543 2.053 0.73 240765. 0.2723
|
|
89.90 0.5216 0.7798 0.0437 0.0293 2.783 13.491 9.051 2075.026 1.524 40.260 1.978 0.73 241321. 0.2495
|
|
94.39 0.5477 0.7867 0.0390 0.0271 2.581 12.513 8.066 1924.596 1.414 35.879 1.901 0.73 241899. 0.2263
|
|
98.89 0.5738 0.7885 0.0341 0.0248 2.362 11.453 7.063 1761.492 1.294 31.418 1.819 0.73 242499. 0.2026
|
|
103.38 0.5999 0.7836 0.0292 0.0224 2.127 10.314 6.047 1586.420 1.165 26.899 1.729 0.73 243121. 0.1782
|
|
107.88 0.6259 0.7695 0.0243 0.0197 1.878 9.104 5.023 1400.242 1.029 22.343 1.627 0.74 243765. 0.1528
|
|
112.37 0.6520 0.7415 0.0193 0.0170 1.615 7.828 3.996 1204.036 0.884 17.773 1.505 0.74 244430. 0.1261
|
|
116.87 0.6781 0.6911 0.0144 0.0141 1.340 6.496 2.971 999.160 0.734 13.217 1.349 0.74 245117. 0.0974
|
|
121.36 0.7042 0.5998 0.0095 0.0111 1.056 5.119 1.957 787.309 0.578 8.703 1.127 0.74 245827. 0.0661
|
|
125.86 0.7303 0.4208 0.0046 0.0080 0.765 3.710 0.959 570.544 0.419 4.267 0.763 0.74 246557. 0.0313
|
|
130.35 0.7563 -0.0114 -0.0001 0.0049 0.470 2.279 -0.015 350.541 0.257 -0.069 -0.020 0.74 247298. 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 0.1003 0.0362 4.302 19.367 24.065 3207.830 2.188 107.043 3.403 0.78 252288. 0.6996
|
|
4.83 0.0260 0.0702 0.0993 0.0368 4.376 19.699 23.832 3262.950 2.226 106.006 3.313 0.78 252464. 0.6778
|
|
9.67 0.0521 0.1366 0.0982 0.0375 4.448 20.025 23.569 3316.909 2.262 104.837 3.223 0.78 252658. 0.6558
|
|
14.50 0.0781 0.1992 0.0970 0.0380 4.517 20.338 23.274 3368.667 2.298 103.521 3.134 0.78 252870. 0.6336
|
|
19.34 0.1042 0.2581 0.0956 0.0386 4.582 20.630 22.941 3417.123 2.331 102.043 3.045 0.78 253101. 0.6113
|
|
24.17 0.1302 0.3134 0.0941 0.0391 4.641 20.896 22.569 3461.060 2.361 100.388 2.958 0.78 253353. 0.5889
|
|
29.00 0.1563 0.3651 0.0923 0.0395 4.692 21.126 22.154 3499.155 2.387 98.541 2.872 0.78 253626. 0.5665
|
|
33.84 0.1823 0.4135 0.0904 0.0399 4.734 21.312 21.692 3529.996 2.408 96.487 2.787 0.78 253920. 0.5441
|
|
38.67 0.2084 0.4585 0.0883 0.0401 4.763 21.445 21.181 3552.087 2.423 94.211 2.705 0.78 254237. 0.5217
|
|
43.51 0.2344 0.5004 0.0859 0.0402 4.779 21.516 20.616 3563.875 2.431 91.702 2.624 0.78 254576. 0.4993
|
|
48.34 0.2604 0.5394 0.0833 0.0402 4.779 21.516 19.997 3563.786 2.431 88.948 2.545 0.78 254938. 0.4770
|
|
53.17 0.2865 0.5754 0.0805 0.0401 4.761 21.434 19.321 3550.274 2.422 85.941 2.468 0.78 255324. 0.4547
|
|
58.01 0.3125 0.6087 0.0775 0.0398 4.723 21.263 18.587 3521.852 2.402 82.674 2.394 0.78 255734. 0.4325
|
|
62.84 0.3386 0.6394 0.0742 0.0393 4.663 20.992 17.793 3477.118 2.372 79.145 2.321 0.78 256167. 0.4103
|
|
67.68 0.3646 0.6676 0.0706 0.0386 4.579 20.615 16.940 3414.669 2.329 75.349 2.250 0.78 256624. 0.3882
|
|
72.51 0.3907 0.6933 0.0668 0.0376 4.470 20.123 16.026 3333.107 2.273 71.286 2.181 0.78 257104. 0.3659
|
|
77.34 0.4167 0.7165 0.0627 0.0365 4.334 19.511 15.056 3231.804 2.204 66.968 2.113 0.78 257609. 0.3436
|
|
82.18 0.4428 0.7371 0.0585 0.0351 4.172 18.783 14.035 3111.089 2.122 62.426 2.046 0.79 258137. 0.3213
|
|
87.01 0.4688 0.7551 0.0541 0.0336 3.985 17.940 12.970 2971.566 2.027 57.689 1.980 0.79 258689. 0.2988
|
|
91.85 0.4948 0.7702 0.0495 0.0318 3.773 16.988 11.866 2813.881 1.919 52.782 1.913 0.79 259264. 0.2762
|
|
96.68 0.5209 0.7818 0.0447 0.0298 3.539 15.931 10.731 2638.830 1.800 47.731 1.844 0.79 259862. 0.2532
|
|
101.51 0.5469 0.7892 0.0399 0.0276 3.282 14.775 9.568 2447.218 1.669 42.559 1.773 0.79 260484. 0.2299
|
|
106.35 0.5730 0.7914 0.0349 0.0253 3.004 13.524 8.383 2240.007 1.528 37.288 1.697 0.79 261130. 0.2060
|
|
111.18 0.5990 0.7866 0.0299 0.0228 2.707 12.186 7.181 2018.377 1.377 31.943 1.614 0.79 261798. 0.1813
|
|
116.01 0.6251 0.7719 0.0249 0.0201 2.392 10.769 5.969 1783.752 1.217 26.548 1.518 0.79 262490. 0.1554
|
|
120.85 0.6511 0.7423 0.0198 0.0174 2.062 9.285 4.751 1537.929 1.049 21.132 1.401 0.79 263206. 0.1280
|
|
125.68 0.6771 0.6886 0.0147 0.0145 1.721 7.746 3.535 1283.102 0.875 15.725 1.250 0.80 263945. 0.0985
|
|
130.52 0.7032 0.5917 0.0097 0.0115 1.370 6.170 2.330 1021.903 0.697 10.363 1.034 0.80 264707. 0.0662
|
|
135.35 0.7292 0.4063 0.0048 0.0086 1.016 4.573 1.143 757.410 0.517 5.086 0.685 0.80 265492. 0.0307
|
|
140.18 0.7553 -0.0098 -0.0001 0.0056 0.660 2.971 -0.017 492.118 0.336 -0.077 -0.016 0.80 266289. 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 0.1014 0.0395 5.768 24.236 27.922 4301.039 2.738 124.195 2.945 0.83 270280. 0.6521
|
|
5.22 0.0262 0.0659 0.1004 0.0400 5.844 24.558 27.668 4358.211 2.775 123.068 2.879 0.83 270470. 0.6348
|
|
10.44 0.0525 0.1288 0.0994 0.0405 5.918 24.866 27.380 4412.823 2.809 121.786 2.814 0.83 270679. 0.6172
|
|
15.66 0.0787 0.1887 0.0982 0.0410 5.986 25.151 27.053 4463.514 2.842 120.332 2.749 0.83 270909. 0.5993
|
|
20.88 0.1050 0.2456 0.0969 0.0414 6.047 25.407 26.683 4508.909 2.870 118.686 2.684 0.83 271159. 0.5811
|
|
26.09 0.1312 0.2997 0.0954 0.0417 6.098 25.625 26.266 4547.525 2.895 116.829 2.620 0.83 271432. 0.5627
|
|
31.31 0.1575 0.3508 0.0936 0.0420 6.139 25.795 25.796 4577.849 2.914 114.741 2.556 0.83 271728. 0.5441
|
|
36.53 0.1837 0.3992 0.0917 0.0422 6.166 25.911 25.270 4598.298 2.927 112.402 2.493 0.83 272048. 0.5252
|
|
41.75 0.2099 0.4448 0.0896 0.0423 6.178 25.961 24.684 4607.232 2.933 109.796 2.430 0.83 272392. 0.5060
|
|
46.97 0.2362 0.4877 0.0873 0.0423 6.173 25.937 24.034 4602.991 2.930 106.905 2.368 0.84 272761. 0.4866
|
|
52.19 0.2624 0.5279 0.0846 0.0421 6.147 25.829 23.317 4583.901 2.918 103.716 2.307 0.84 273156. 0.4669
|
|
57.41 0.2887 0.5655 0.0818 0.0418 6.099 25.629 22.531 4548.328 2.896 100.218 2.247 0.84 273576. 0.4470
|
|
62.63 0.3149 0.6005 0.0787 0.0413 6.027 25.327 21.673 4494.693 2.861 96.403 2.187 0.84 274022. 0.4267
|
|
67.84 0.3412 0.6329 0.0753 0.0406 5.929 24.914 20.744 4421.480 2.815 92.269 2.128 0.84 274494. 0.4062
|
|
73.06 0.3674 0.6628 0.0717 0.0397 5.803 24.382 19.741 4327.070 2.755 87.810 2.069 0.84 274991. 0.3853
|
|
78.28 0.3936 0.6901 0.0678 0.0386 5.645 23.721 18.665 4209.797 2.680 83.023 2.011 0.84 275515. 0.3641
|
|
83.50 0.4199 0.7149 0.0636 0.0374 5.457 22.928 17.520 4068.938 2.590 77.929 1.953 0.84 276064. 0.3426
|
|
88.72 0.4461 0.7369 0.0592 0.0359 5.237 22.005 16.313 3905.170 2.486 72.561 1.895 0.84 276640. 0.3207
|
|
93.94 0.4724 0.7557 0.0546 0.0342 4.990 20.966 15.053 3720.749 2.369 66.955 1.835 0.84 277240. 0.2984
|
|
99.16 0.4986 0.7708 0.0499 0.0323 4.715 19.812 13.746 3516.072 2.238 61.144 1.773 0.84 277866. 0.2756
|
|
104.38 0.5249 0.7817 0.0450 0.0302 4.415 18.552 12.400 3292.292 2.096 55.157 1.708 0.84 278518. 0.2521
|
|
109.59 0.5511 0.7874 0.0400 0.0280 4.090 17.188 11.021 3050.260 1.942 49.022 1.639 0.85 279194. 0.2280
|
|
114.81 0.5773 0.7866 0.0349 0.0256 3.742 15.725 9.615 2790.766 1.777 42.770 1.563 0.85 279896. 0.2031
|
|
120.03 0.6036 0.7768 0.0297 0.0231 3.374 14.179 8.190 2516.293 1.602 36.427 1.476 0.85 280624. 0.1771
|
|
125.25 0.6298 0.7542 0.0245 0.0205 2.989 12.561 6.750 2229.234 1.419 30.026 1.373 0.85 281376. 0.1496
|
|
130.47 0.6561 0.7122 0.0193 0.0177 2.592 10.890 5.306 1932.660 1.230 23.600 1.245 0.85 282154. 0.1202
|
|
135.69 0.6823 0.6395 0.0140 0.0150 2.186 9.186 3.864 1630.301 1.038 17.189 1.075 0.85 282957. 0.0886
|
|
140.91 0.7086 0.5148 0.0088 0.0122 1.778 7.473 2.437 1326.205 0.844 10.839 0.833 0.85 283785. 0.0545
|
|
146.12 0.7348 0.2932 0.0038 0.0094 1.374 5.774 1.034 1024.749 0.652 4.600 0.458 0.86 284638. 0.0195
|
|
151.34 0.7610
|
|
|
|
|
|
|
|
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 0.1020 0.0447 7.928 31.230 31.980 5911.864 3.528 142.249 2.454 0.89 288276. 0.5815
|
|
5.58 0.0263 0.0589 0.1012 0.0452 8.008 31.547 31.720 5971.839 3.564 141.091 2.409 0.89 288478. 0.5687
|
|
11.15 0.0526 0.1156 0.1003 0.0456 8.081 31.834 31.421 6026.070 3.597 139.760 2.365 0.89 288700. 0.5556
|
|
16.73 0.0789 0.1703 0.0992 0.0459 8.144 32.080 31.078 6072.677 3.624 138.233 2.321 0.89 288944. 0.5423
|
|
22.31 0.1052 0.2228 0.0979 0.0462 8.193 32.276 30.685 6109.804 3.647 136.488 2.278 0.89 289211. 0.5289
|
|
27.88 0.1315 0.2733 0.0965 0.0464 8.228 32.412 30.238 6135.598 3.662 134.497 2.235 0.89 289503. 0.5152
|
|
33.46 0.1577 0.3217 0.0949 0.0465 8.245 32.479 29.730 6148.226 3.669 132.237 2.193 0.89 289819. 0.5012
|
|
39.04 0.1840 0.3683 0.0930 0.0465 8.242 32.467 29.156 6145.884 3.668 129.684 2.152 0.89 290161. 0.4869
|
|
44.62 0.2103 0.4128 0.0910 0.0463 8.216 32.366 28.510 6126.787 3.657 126.813 2.111 0.89 290529. 0.4723
|
|
50.19 0.2366 0.4555 0.0887 0.0461 8.165 32.166 27.788 6088.961 3.634 123.602 2.070 0.89 290925. 0.4573
|
|
55.77 0.2629 0.4962 0.0861 0.0456 8.088 31.860 26.986 6031.153 3.600 120.034 2.029 0.89 291348. 0.4419
|
|
61.35 0.2892 0.5349 0.0833 0.0450 7.982 31.442 26.100 5951.858 3.552 116.094 1.989 0.89 291799. 0.4259
|
|
66.92 0.3155 0.5716 0.0802 0.0443 7.845 30.902 25.129 5849.784 3.491 111.774 1.948 0.89 292277. 0.4094
|
|
72.50 0.3418 0.6063 0.0768 0.0433 7.676 30.237 24.071 5723.811 3.416 107.067 1.907 0.89 292784. 0.3922
|
|
78.08 0.3681 0.6387 0.0731 0.0422 7.473 29.439 22.925 5572.775 3.326 101.970 1.866 0.89 293318. 0.3744
|
|
83.65 0.3944 0.6687 0.0692 0.0408 7.235 28.501 21.691 5395.292 3.220 96.481 1.823 0.90 293880. 0.3559
|
|
89.23 0.4207 0.6964 0.0650 0.0393 6.961 27.422 20.373 5190.976 3.098 90.620 1.780 0.90 294470. 0.3368
|
|
94.81 0.4470 0.7214 0.0606 0.0375 6.652 26.205 18.982 4960.648 2.961 84.431 1.736 0.90 295087. 0.3169
|
|
100.39 0.4732 0.7429 0.0559 0.0356 6.315 24.876 17.525 4709.040 2.811 77.953 1.688 0.90 295732. 0.2962
|
|
105.96 0.4995 0.7598 0.0511 0.0336 5.955 23.457 16.012 4440.301 2.650 71.221 1.636 0.90 296404. 0.2743
|
|
111.54 0.5258 0.7714 0.0461 0.0314 5.572 21.948 14.450 4154.775 2.480 64.273 1.577 0.90 297102. 0.2513
|
|
117.12 0.5521 0.7740 0.0410 0.0292 5.183 20.417 12.845 3864.825 2.307 57.135 1.507 0.90 297828. 0.2264
|
|
122.69 0.5784 0.7675 0.0358 0.0269 4.777 18.819 11.208 3562.390 2.126 49.851 1.427 0.90 298581. 0.2002
|
|
128.27 0.6047 0.7499 0.0305 0.0246 4.354 17.153 9.546 3247.109 1.938 42.462 1.333 0.90 299360. 0.1727
|
|
133.85 0.6310 0.7164 0.0251 0.0221 3.921 15.445 7.870 2923.747 1.745 35.005 1.221 0.91 300166. 0.1435
|
|
139.42 0.6573 0.6608 0.0197 0.0196 3.481 13.715 6.188 2596.140 1.549 27.525 1.081 0.91 300999. 0.1127
|
|
145.00 0.6836 0.5733 0.0144 0.0172 3.043 11.988 4.512 2269.265 1.354 20.071 0.902 0.91 301859. 0.0803
|
|
150.58 0.7099 0.4388 0.0091 0.0147 2.613 10.294 2.856 1948.644 1.163 12.702 0.665 0.91 302746. 0.0471
|
|
156.16 0.7362 0.2335 0.0039 0.0124 2.198 8.659 1.233 1639.103 0.978 5.483 0.341 0.91 303659. 0.0159
|
|
161.73 0.7625
|
|
|
|
|
|
|