612 lines
109 KiB
Plaintext
612 lines
109 KiB
Plaintext
15x10E (15x10E.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 0.0985 0.0434 0.003 0.167 0.159 1.979 0.019 0.707 36.403 0.06 20958. 0.5676
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0.40 0.0279 0.0617 0.0974 0.0441 0.003 0.170 0.157 2.008 0.019 0.699 35.487 0.06 20974. 0.5503
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0.79 0.0558 0.1201 0.0962 0.0447 0.003 0.172 0.155 2.037 0.019 0.691 34.560 0.06 20991. 0.5327
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1.19 0.0837 0.1753 0.0949 0.0453 0.003 0.175 0.153 2.066 0.020 0.681 33.629 0.06 21011. 0.5148
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1.59 0.1116 0.2272 0.0935 0.0459 0.003 0.177 0.151 2.093 0.020 0.671 32.697 0.06 21032. 0.4968
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1.98 0.1395 0.2760 0.0919 0.0465 0.003 0.179 0.148 2.118 0.020 0.660 31.767 0.06 21055. 0.4786
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2.38 0.1674 0.3215 0.0902 0.0470 0.003 0.181 0.146 2.140 0.020 0.647 30.844 0.06 21080. 0.4603
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2.77 0.1953 0.3640 0.0883 0.0474 0.003 0.182 0.142 2.159 0.021 0.634 29.930 0.06 21107. 0.4419
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3.17 0.2232 0.4035 0.0862 0.0477 0.003 0.184 0.139 2.173 0.021 0.619 29.027 0.06 21137. 0.4234
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3.57 0.2511 0.4400 0.0839 0.0479 0.003 0.184 0.135 2.182 0.021 0.602 28.136 0.06 21169. 0.4050
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3.96 0.2790 0.4736 0.0814 0.0480 0.003 0.185 0.131 2.186 0.021 0.584 27.259 0.06 21203. 0.3865
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4.36 0.3069 0.5044 0.0787 0.0479 0.003 0.184 0.127 2.182 0.021 0.565 26.394 0.06 21239. 0.3679
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4.76 0.3348 0.5325 0.0758 0.0476 0.003 0.183 0.122 2.171 0.021 0.544 25.541 0.06 21278. 0.3493
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5.15 0.3627 0.5578 0.0726 0.0472 0.003 0.182 0.117 2.151 0.021 0.521 24.696 0.06 21319. 0.3306
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5.55 0.3906 0.5803 0.0692 0.0466 0.003 0.179 0.112 2.122 0.020 0.497 23.856 0.06 21363. 0.3118
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5.94 0.4185 0.5998 0.0655 0.0457 0.003 0.176 0.106 2.084 0.020 0.470 23.015 0.06 21409. 0.2928
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6.34 0.4464 0.6163 0.0617 0.0447 0.003 0.172 0.099 2.036 0.019 0.443 22.168 0.06 21457. 0.2735
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6.74 0.4743 0.6293 0.0576 0.0434 0.003 0.167 0.093 1.977 0.019 0.413 21.305 0.06 21508. 0.2540
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7.13 0.5022 0.6384 0.0533 0.0419 0.003 0.161 0.086 1.909 0.018 0.382 20.415 0.06 21561. 0.2341
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7.53 0.5301 0.6432 0.0488 0.0402 0.002 0.155 0.079 1.831 0.017 0.350 19.485 0.06 21617. 0.2138
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7.93 0.5580 0.6429 0.0441 0.0383 0.002 0.147 0.071 1.745 0.017 0.317 18.500 0.06 21675. 0.1931
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8.32 0.5859 0.6364 0.0393 0.0362 0.002 0.140 0.063 1.651 0.016 0.282 17.442 0.06 21735. 0.1719
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8.72 0.6138 0.6225 0.0345 0.0340 0.002 0.131 0.056 1.549 0.015 0.247 16.285 0.06 21798. 0.1502
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9.12 0.6417 0.5993 0.0295 0.0316 0.002 0.122 0.048 1.441 0.014 0.212 14.998 0.06 21863. 0.1280
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9.51 0.6696 0.5645 0.0245 0.0291 0.002 0.112 0.040 1.326 0.013 0.176 13.537 0.06 21930. 0.1053
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9.91 0.6975 0.5142 0.0195 0.0265 0.002 0.102 0.031 1.206 0.012 0.140 11.839 0.06 22000. 0.0822
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10.30 0.7254 0.4433 0.0145 0.0237 0.001 0.091 0.023 1.081 0.010 0.104 9.813 0.06 22072. 0.0587
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10.70 0.7533 0.3433 0.0095 0.0209 0.001 0.080 0.015 0.952 0.009 0.068 7.318 0.06 22146. 0.0355
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11.10 0.7812 0.2005 0.0046 0.0180 0.001 0.069 0.007 0.820 0.008 0.033 4.121 0.06 22223. 0.0139
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11.49 0.8091 -0.0093 -0.0002 0.0150 0.001 0.058 0.000 0.685 0.007 -0.001 -0.185 0.06 22302. 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 0.0988 0.0399 0.019 0.614 0.638 14.530 0.069 2.836 19.904 0.12 41916. 0.6217
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0.80 0.0280 0.0676 0.0977 0.0405 0.020 0.625 0.631 14.780 0.071 2.806 19.357 0.12 41947. 0.6014
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1.59 0.0560 0.1313 0.0966 0.0412 0.020 0.635 0.623 15.031 0.072 2.772 18.807 0.12 41983. 0.5808
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2.39 0.0841 0.1912 0.0953 0.0419 0.020 0.646 0.615 15.277 0.073 2.735 18.257 0.12 42022. 0.5600
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3.18 0.1121 0.2472 0.0939 0.0426 0.021 0.656 0.606 15.514 0.074 2.694 17.709 0.12 42064. 0.5392
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3.98 0.1401 0.2996 0.0923 0.0432 0.021 0.665 0.596 15.736 0.075 2.649 17.168 0.12 42111. 0.5183
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4.78 0.1681 0.3483 0.0906 0.0437 0.021 0.673 0.584 15.937 0.076 2.599 16.633 0.12 42161. 0.4974
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5.57 0.1962 0.3935 0.0887 0.0442 0.022 0.681 0.572 16.110 0.077 2.545 16.108 0.12 42216. 0.4766
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6.37 0.2242 0.4354 0.0866 0.0446 0.022 0.687 0.559 16.248 0.078 2.485 15.593 0.12 42276. 0.4559
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7.17 0.2522 0.4740 0.0843 0.0448 0.022 0.691 0.544 16.345 0.078 2.419 15.089 0.12 42340. 0.4353
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7.96 0.2802 0.5095 0.0818 0.0450 0.022 0.693 0.528 16.393 0.078 2.347 14.598 0.12 42409. 0.4148
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8.76 0.3083 0.5420 0.0790 0.0449 0.022 0.692 0.510 16.385 0.078 2.268 14.118 0.12 42482. 0.3944
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9.55 0.3363 0.5717 0.0761 0.0447 0.022 0.689 0.491 16.313 0.078 2.183 13.649 0.12 42560. 0.3741
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10.35 0.3643 0.5985 0.0729 0.0444 0.022 0.683 0.470 16.170 0.077 2.092 13.190 0.12 42643. 0.3538
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11.15 0.3923 0.6225 0.0694 0.0438 0.021 0.674 0.448 15.953 0.076 1.993 12.740 0.12 42731. 0.3336
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11.94 0.4204 0.6437 0.0658 0.0429 0.021 0.662 0.424 15.655 0.075 1.888 12.295 0.12 42824. 0.3133
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12.74 0.4484 0.6619 0.0618 0.0419 0.020 0.645 0.399 15.274 0.073 1.775 11.853 0.12 42921. 0.2929
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13.53 0.4764 0.6769 0.0577 0.0406 0.020 0.626 0.372 14.807 0.071 1.657 11.409 0.12 43024. 0.2724
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14.33 0.5044 0.6885 0.0534 0.0391 0.019 0.602 0.344 14.254 0.068 1.532 10.958 0.12 43131. 0.2516
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15.13 0.5325 0.6960 0.0488 0.0374 0.018 0.576 0.315 13.621 0.065 1.402 10.495 0.12 43243. 0.2305
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15.92 0.5605 0.6988 0.0442 0.0354 0.017 0.546 0.285 12.914 0.062 1.268 10.011 0.12 43360. 0.2091
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16.72 0.5885 0.6961 0.0394 0.0333 0.016 0.513 0.254 12.136 0.058 1.130 9.497 0.12 43482. 0.1873
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17.52 0.6165 0.6865 0.0345 0.0310 0.015 0.477 0.223 11.293 0.054 0.990 8.940 0.12 43608. 0.1650
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18.31 0.6446 0.6681 0.0295 0.0285 0.014 0.439 0.191 10.390 0.050 0.848 8.323 0.12 43739. 0.1422
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19.11 0.6726 0.6383 0.0246 0.0259 0.013 0.399 0.158 9.431 0.045 0.705 7.620 0.12 43875. 0.1186
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19.90 0.7006 0.5928 0.0195 0.0231 0.011 0.356 0.126 8.421 0.040 0.561 6.793 0.12 44016. 0.0944
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20.70 0.7286 0.5247 0.0146 0.0202 0.010 0.311 0.094 7.367 0.035 0.418 5.782 0.12 44161. 0.0693
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21.50 0.7567 0.4223 0.0096 0.0172 0.008 0.265 0.062 6.277 0.030 0.276 4.481 0.12 44311. 0.0436
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22.29 0.7847 0.2635 0.0048 0.0142 0.007 0.218 0.031 5.159 0.025 0.136 2.696 0.12 44465. 0.0185
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23.09 0.8127 0.0013 0.0000 0.0110 0.005 0.170 0.000 4.022 0.019 0.000 0.013 0.12 44624. 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 0.0991 0.0383 0.063 1.329 1.438 47.165 0.150 6.398 13.833 0.18 62873. 0.6490
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1.20 0.0281 0.0705 0.0980 0.0390 0.064 1.354 1.423 48.042 0.153 6.331 13.437 0.18 62921. 0.6271
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2.40 0.0562 0.1369 0.0969 0.0398 0.066 1.378 1.406 48.920 0.156 6.256 13.039 0.18 62974. 0.6049
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3.59 0.0843 0.1991 0.0956 0.0405 0.067 1.403 1.388 49.784 0.158 6.173 12.643 0.18 63032. 0.5826
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4.79 0.1124 0.2573 0.0942 0.0411 0.068 1.426 1.367 50.618 0.161 6.081 12.250 0.18 63096. 0.5603
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5.99 0.1405 0.3114 0.0926 0.0418 0.069 1.448 1.344 51.402 0.164 5.979 11.862 0.18 63166. 0.5380
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7.19 0.1686 0.3616 0.0908 0.0424 0.070 1.468 1.319 52.116 0.166 5.868 11.481 0.18 63243. 0.5158
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8.38 0.1967 0.4082 0.0889 0.0429 0.071 1.486 1.291 52.737 0.168 5.744 11.107 0.18 63326. 0.4937
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9.58 0.2248 0.4512 0.0868 0.0433 0.071 1.500 1.261 53.241 0.169 5.609 10.742 0.18 63415. 0.4719
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10.78 0.2529 0.4908 0.0845 0.0436 0.072 1.510 1.227 53.602 0.171 5.460 10.387 0.18 63512. 0.4502
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11.98 0.2810 0.5272 0.0820 0.0437 0.072 1.516 1.191 53.795 0.171 5.297 10.041 0.18 63615. 0.4287
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13.17 0.3091 0.5605 0.0793 0.0437 0.072 1.516 1.151 53.795 0.171 5.120 9.706 0.18 63726. 0.4073
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14.37 0.3372 0.5909 0.0763 0.0435 0.072 1.509 1.108 53.576 0.171 4.928 9.379 0.18 63844. 0.3862
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15.57 0.3653 0.6185 0.0731 0.0432 0.071 1.497 1.061 53.117 0.169 4.720 9.062 0.18 63969. 0.3652
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16.77 0.3934 0.6433 0.0696 0.0426 0.070 1.476 1.011 52.396 0.167 4.497 8.752 0.18 64102. 0.3442
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17.96 0.4215 0.6653 0.0659 0.0418 0.069 1.448 0.957 51.397 0.164 4.258 8.448 0.18 64241. 0.3233
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19.16 0.4496 0.6844 0.0620 0.0407 0.067 1.412 0.900 50.109 0.160 4.004 8.148 0.18 64389. 0.3024
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20.36 0.4777 0.7005 0.0578 0.0394 0.065 1.367 0.840 48.522 0.154 3.735 7.849 0.18 64543. 0.2813
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21.56 0.5058 0.7133 0.0535 0.0379 0.063 1.314 0.776 46.638 0.148 3.452 7.548 0.18 64705. 0.2601
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22.75 0.5339 0.7223 0.0489 0.0361 0.060 1.253 0.710 44.472 0.142 3.158 7.242 0.18 64874. 0.2387
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23.95 0.5620 0.7270 0.0442 0.0342 0.056 1.185 0.642 42.043 0.134 2.855 6.924 0.18 65050. 0.2170
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25.15 0.5901 0.7264 0.0394 0.0320 0.053 1.109 0.572 39.368 0.125 2.544 6.589 0.18 65233. 0.1949
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26.35 0.6183 0.7194 0.0345 0.0296 0.049 1.027 0.501 36.463 0.116 2.227 6.228 0.18 65424. 0.1724
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27.54 0.6464 0.7040 0.0295 0.0271 0.045 0.939 0.429 33.342 0.106 1.906 5.830 0.18 65621. 0.1493
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28.74 0.6745 0.6775 0.0245 0.0244 0.040 0.846 0.356 30.022 0.096 1.583 5.377 0.18 65826. 0.1255
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29.94 0.7026 0.6353 0.0195 0.0216 0.036 0.747 0.283 26.523 0.084 1.259 4.841 0.18 66038. 0.1007
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31.14 0.7307 0.5700 0.0145 0.0186 0.031 0.644 0.211 22.867 0.073 0.936 4.176 0.18 66257. 0.0749
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32.33 0.7588 0.4676 0.0096 0.0155 0.026 0.538 0.139 19.082 0.061 0.617 3.299 0.18 66483. 0.0481
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33.53 0.7869 0.3000 0.0047 0.0124 0.020 0.428 0.068 15.198 0.048 0.304 2.041 0.18 66717. 0.0209
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34.73 0.8150 -0.0011 0.0000 0.0091 0.015 0.317 0.000 11.249 0.036 -0.001 -0.007 0.18 66955. 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 0.0994 0.0375 0.147 2.311 2.565 109.372 0.261 11.408 10.636 0.24 83829. 0.6663
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1.60 0.0282 0.0724 0.0983 0.0382 0.150 2.356 2.538 111.499 0.266 11.289 10.324 0.24 83893. 0.6434
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3.20 0.0563 0.1404 0.0972 0.0390 0.152 2.401 2.508 113.633 0.271 11.156 10.011 0.24 83963. 0.6202
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4.80 0.0845 0.2040 0.0959 0.0397 0.155 2.446 2.475 115.737 0.276 11.009 9.700 0.24 84042. 0.5970
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6.40 0.1126 0.2634 0.0945 0.0404 0.158 2.489 2.439 117.769 0.281 10.847 9.392 0.24 84127. 0.5737
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8.00 0.1408 0.3186 0.0929 0.0410 0.161 2.529 2.398 119.686 0.286 10.667 9.088 0.24 84221. 0.5505
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9.60 0.1689 0.3698 0.0912 0.0416 0.163 2.566 2.353 121.436 0.290 10.468 8.790 0.24 84323. 0.5275
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11.20 0.1971 0.4172 0.0893 0.0422 0.165 2.598 2.304 122.965 0.294 10.249 8.499 0.24 84434. 0.5047
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12.80 0.2252 0.4609 0.0872 0.0426 0.167 2.625 2.250 124.214 0.297 10.008 8.216 0.24 84554. 0.4821
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14.40 0.2534 0.5011 0.0849 0.0429 0.168 2.644 2.190 125.122 0.299 9.743 7.940 0.24 84683. 0.4597
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15.99 0.2815 0.5380 0.0823 0.0431 0.168 2.655 2.125 125.628 0.300 9.453 7.673 0.24 84822. 0.4376
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17.59 0.3097 0.5719 0.0796 0.0431 0.169 2.655 2.054 125.669 0.300 9.137 7.414 0.24 84970. 0.4157
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19.19 0.3378 0.6028 0.0766 0.0429 0.168 2.645 1.977 125.184 0.299 8.794 7.163 0.24 85128. 0.3940
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20.79 0.3660 0.6308 0.0734 0.0426 0.166 2.623 1.894 124.119 0.296 8.423 6.920 0.24 85295. 0.3725
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22.39 0.3941 0.6561 0.0699 0.0420 0.164 2.587 1.804 122.424 0.292 8.024 6.684 0.24 85472. 0.3512
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23.99 0.4223 0.6787 0.0662 0.0412 0.161 2.537 1.708 120.058 0.287 7.597 6.453 0.24 85659. 0.3299
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25.59 0.4504 0.6985 0.0622 0.0401 0.157 2.472 1.606 116.991 0.279 7.143 6.226 0.24 85856. 0.3086
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27.19 0.4786 0.7153 0.0580 0.0388 0.152 2.392 1.498 113.201 0.270 6.661 6.001 0.24 86063. 0.2873
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28.79 0.5067 0.7290 0.0536 0.0373 0.146 2.297 1.384 108.690 0.259 6.156 5.775 0.24 86279. 0.2658
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30.39 0.5349 0.7390 0.0490 0.0355 0.139 2.187 1.266 103.496 0.247 5.630 5.547 0.24 86505. 0.2441
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31.99 0.5630 0.7450 0.0443 0.0335 0.131 2.064 1.144 97.661 0.233 5.088 5.312 0.24 86741. 0.2222
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33.59 0.5912 0.7460 0.0395 0.0313 0.122 1.928 1.019 91.225 0.218 4.532 5.066 0.24 86986. 0.2000
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35.19 0.6193 0.7408 0.0345 0.0289 0.113 1.780 0.892 84.224 0.201 3.966 4.802 0.24 87241. 0.1774
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36.79 0.6475 0.7276 0.0296 0.0263 0.103 1.621 0.763 76.696 0.183 3.393 4.512 0.24 87506. 0.1541
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38.39 0.6756 0.7037 0.0245 0.0236 0.092 1.451 0.633 68.682 0.164 2.816 4.181 0.24 87780. 0.1301
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39.99 0.7038 0.6643 0.0195 0.0207 0.081 1.273 0.503 60.228 0.144 2.238 3.790 0.24 88063. 0.1052
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41.59 0.7319 0.6016 0.0145 0.0176 0.069 1.086 0.374 51.390 0.123 1.663 3.300 0.24 88356. 0.0789
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43.19 0.7601 0.5002 0.0095 0.0145 0.057 0.892 0.246 42.235 0.101 1.094 2.642 0.24 88659. 0.0513
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44.78 0.7882 0.3272 0.0047 0.0113 0.044 0.694 0.121 32.841 0.078 0.537 1.667 0.25 88970. 0.0227
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46.38 0.8164 -0.0051 -0.0001 0.0080 0.031 0.492 -0.001 23.286 0.056 -0.006 -0.025 0.25 89290. 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 0.0997 0.0370 0.283 3.564 4.021 210.852 0.403 17.886 8.650 0.30 104783. 0.6785
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2.00 0.0282 0.0736 0.0987 0.0378 0.288 3.636 3.980 215.084 0.411 17.701 8.392 0.30 104863. 0.6549
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4.00 0.0563 0.1427 0.0975 0.0385 0.294 3.708 3.933 219.333 0.419 17.496 8.134 0.30 104952. 0.6311
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6.00 0.0845 0.2073 0.0963 0.0392 0.300 3.779 3.882 223.528 0.427 17.268 7.878 0.30 105050. 0.6072
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8.00 0.1127 0.2675 0.0948 0.0400 0.305 3.847 3.825 227.587 0.435 17.016 7.624 0.30 105157. 0.5833
|
|
10.00 0.1409 0.3234 0.0933 0.0406 0.310 3.912 3.763 231.421 0.442 16.736 7.374 0.30 105275. 0.5595
|
|
12.01 0.1690 0.3753 0.0916 0.0412 0.315 3.971 3.693 234.929 0.449 16.426 7.130 0.30 105403. 0.5360
|
|
14.01 0.1972 0.4231 0.0897 0.0418 0.319 4.023 3.616 238.004 0.455 16.084 6.891 0.30 105542. 0.5126
|
|
16.01 0.2254 0.4673 0.0876 0.0422 0.323 4.066 3.531 240.529 0.459 15.708 6.659 0.30 105692. 0.4895
|
|
18.01 0.2536 0.5080 0.0852 0.0426 0.325 4.097 3.438 242.383 0.463 15.294 6.434 0.30 105853. 0.4667
|
|
20.01 0.2817 0.5453 0.0827 0.0427 0.326 4.115 3.336 243.442 0.465 14.840 6.216 0.30 106027. 0.4442
|
|
22.01 0.3099 0.5795 0.0800 0.0428 0.327 4.118 3.225 243.583 0.465 14.345 6.005 0.30 106212. 0.4219
|
|
24.01 0.3381 0.6107 0.0770 0.0426 0.325 4.102 3.104 242.685 0.463 13.808 5.802 0.30 106410. 0.3999
|
|
26.01 0.3662 0.6391 0.0737 0.0422 0.323 4.068 2.974 240.637 0.460 13.226 5.605 0.30 106620. 0.3781
|
|
28.01 0.3944 0.6648 0.0702 0.0417 0.318 4.012 2.833 237.341 0.453 12.600 5.414 0.30 106842. 0.3564
|
|
30.01 0.4226 0.6878 0.0665 0.0409 0.312 3.934 2.682 232.715 0.444 11.930 5.227 0.30 107076. 0.3349
|
|
32.01 0.4508 0.7081 0.0625 0.0398 0.304 3.832 2.522 226.697 0.433 11.216 5.045 0.30 107323. 0.3134
|
|
34.02 0.4789 0.7255 0.0583 0.0385 0.294 3.706 2.352 219.243 0.419 10.460 4.865 0.30 107582. 0.2919
|
|
36.02 0.5071 0.7399 0.0539 0.0369 0.282 3.556 2.173 210.354 0.402 9.666 4.686 0.30 107852. 0.2702
|
|
38.02 0.5353 0.7508 0.0493 0.0351 0.268 3.383 1.987 200.103 0.382 8.840 4.505 0.30 108136. 0.2484
|
|
40.02 0.5635 0.7578 0.0445 0.0331 0.253 3.188 1.796 188.574 0.360 7.988 4.319 0.30 108431. 0.2264
|
|
42.02 0.5916 0.7600 0.0397 0.0309 0.236 2.973 1.600 175.844 0.336 7.115 4.126 0.30 108738. 0.2041
|
|
44.02 0.6198 0.7564 0.0347 0.0284 0.217 2.738 1.400 161.983 0.309 6.226 3.919 0.30 109057. 0.1814
|
|
46.02 0.6480 0.7451 0.0297 0.0258 0.197 2.486 1.197 147.066 0.281 5.326 3.693 0.30 109388. 0.1581
|
|
48.02 0.6761 0.7233 0.0246 0.0230 0.176 2.217 0.994 131.174 0.251 4.420 3.436 0.30 109731. 0.1340
|
|
50.02 0.7043 0.6865 0.0196 0.0201 0.153 1.934 0.790 114.401 0.218 3.512 3.131 0.30 110086. 0.1088
|
|
52.02 0.7325 0.6265 0.0145 0.0170 0.130 1.637 0.587 96.860 0.185 2.609 2.747 0.31 110453. 0.0823
|
|
54.02 0.7607 0.5270 0.0096 0.0138 0.106 1.330 0.386 78.683 0.150 1.717 2.225 0.31 110832. 0.0541
|
|
56.03 0.7888 0.3516 0.0047 0.0105 0.081 1.015 0.189 60.030 0.115 0.843 1.431 0.31 111222. 0.0244
|
|
58.03 0.8170 -0.0051 0.0000 0.0072 0.055 0.694 -0.002 41.053 0.078 -0.008 -0.020 0.31 111621. 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 0.1001 0.0367 0.485 5.095 5.814 361.684 0.576 25.860 7.291 0.36 125736. 0.6877
|
|
2.40 0.0282 0.0745 0.0991 0.0375 0.495 5.200 5.754 369.119 0.587 25.596 7.071 0.36 125832. 0.6635
|
|
4.80 0.0564 0.1443 0.0979 0.0383 0.505 5.305 5.689 376.593 0.599 25.303 6.851 0.36 125939. 0.6392
|
|
7.21 0.0845 0.2095 0.0967 0.0390 0.515 5.409 5.616 383.977 0.611 24.978 6.633 0.36 126056. 0.6149
|
|
9.61 0.1127 0.2703 0.0953 0.0397 0.525 5.510 5.535 391.132 0.623 24.618 6.418 0.36 126185. 0.5906
|
|
12.01 0.1409 0.3267 0.0937 0.0404 0.534 5.605 5.445 397.898 0.633 24.217 6.206 0.36 126326. 0.5665
|
|
14.41 0.1691 0.3790 0.0920 0.0411 0.542 5.693 5.345 404.103 0.643 23.774 5.999 0.36 126480. 0.5425
|
|
16.81 0.1973 0.4273 0.0901 0.0416 0.549 5.769 5.234 409.554 0.652 23.283 5.797 0.36 126647. 0.5188
|
|
19.21 0.2254 0.4718 0.0880 0.0421 0.555 5.833 5.113 414.048 0.659 22.741 5.601 0.36 126827. 0.4954
|
|
21.62 0.2536 0.5127 0.0857 0.0424 0.560 5.880 4.979 417.373 0.664 22.146 5.411 0.36 127022. 0.4723
|
|
24.02 0.2818 0.5503 0.0832 0.0426 0.562 5.907 4.832 419.310 0.667 21.492 5.227 0.36 127230. 0.4494
|
|
26.42 0.3100 0.5848 0.0804 0.0426 0.563 5.912 4.672 419.643 0.668 20.779 5.049 0.36 127453. 0.4269
|
|
28.82 0.3382 0.6163 0.0774 0.0425 0.561 5.891 4.497 418.158 0.666 20.003 4.878 0.36 127691. 0.4046
|
|
31.22 0.3663 0.6450 0.0742 0.0421 0.556 5.841 4.308 414.662 0.660 19.163 4.712 0.36 127943. 0.3826
|
|
33.62 0.3945 0.6710 0.0707 0.0416 0.548 5.761 4.105 408.979 0.651 18.258 4.552 0.36 128209. 0.3608
|
|
36.03 0.4227 0.6944 0.0669 0.0407 0.538 5.648 3.887 400.965 0.638 17.288 4.397 0.36 128491. 0.3391
|
|
38.43 0.4509 0.7151 0.0629 0.0397 0.524 5.501 3.655 390.509 0.622 16.256 4.245 0.36 128787. 0.3174
|
|
40.83 0.4791 0.7330 0.0587 0.0384 0.506 5.318 3.409 377.532 0.601 15.162 4.095 0.36 129098. 0.2958
|
|
43.23 0.5072 0.7480 0.0542 0.0368 0.485 5.100 3.150 362.035 0.576 14.012 3.947 0.36 129424. 0.2740
|
|
45.63 0.5354 0.7596 0.0496 0.0350 0.461 4.848 2.881 344.140 0.548 12.815 3.797 0.36 129764. 0.2521
|
|
48.03 0.5636 0.7675 0.0448 0.0329 0.434 4.564 2.603 323.994 0.516 11.580 3.645 0.36 130118. 0.2300
|
|
50.44 0.5918 0.7708 0.0399 0.0307 0.405 4.250 2.319 301.728 0.480 10.315 3.486 0.36 130487. 0.2077
|
|
52.84 0.6200 0.7685 0.0349 0.0282 0.372 3.909 2.029 277.467 0.442 9.027 3.318 0.36 130870. 0.1849
|
|
55.24 0.6481 0.7588 0.0299 0.0255 0.337 3.541 1.736 251.340 0.400 7.723 3.133 0.36 131268. 0.1615
|
|
57.64 0.6763 0.7390 0.0248 0.0227 0.300 3.148 1.441 223.491 0.356 6.410 2.925 0.37 131680. 0.1373
|
|
60.04 0.7045 0.7046 0.0197 0.0197 0.260 2.734 1.145 194.085 0.309 5.095 2.677 0.37 132106. 0.1121
|
|
62.45 0.7327 0.6472 0.0147 0.0166 0.219 2.301 0.851 163.321 0.260 3.786 2.364 0.37 132547. 0.0853
|
|
64.85 0.7609 0.5501 0.0097 0.0134 0.176 1.852 0.561 131.435 0.209 2.494 1.935 0.37 133001. 0.0567
|
|
67.25 0.7890 0.3738 0.0048 0.0100 0.132 1.391 0.276 98.708 0.157 1.227 1.268 0.37 133470. 0.0261
|
|
69.65 0.8172 -0.0021 0.0000 0.0066 0.088 0.921 -0.001 65.409 0.104 -0.004 -0.007 0.37 133949. 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 0.1006 0.0366 0.768 6.913 7.950 572.501 0.781 35.361 6.298 0.42 146687. 0.6947
|
|
2.80 0.0282 0.0751 0.0996 0.0374 0.784 7.058 7.870 584.508 0.797 35.008 6.107 0.42 146799. 0.6702
|
|
5.61 0.0564 0.1454 0.0984 0.0382 0.800 7.204 7.782 596.590 0.814 34.615 5.916 0.42 146923. 0.6456
|
|
8.41 0.0846 0.2112 0.0972 0.0389 0.816 7.348 7.684 608.539 0.830 34.177 5.727 0.42 147060. 0.6210
|
|
11.21 0.1128 0.2723 0.0958 0.0397 0.832 7.488 7.574 620.127 0.846 33.691 5.540 0.42 147211. 0.5964
|
|
14.02 0.1410 0.3291 0.0943 0.0404 0.846 7.620 7.453 631.102 0.861 33.150 5.356 0.42 147376. 0.5720
|
|
16.82 0.1692 0.3817 0.0926 0.0410 0.860 7.742 7.318 641.179 0.875 32.549 5.177 0.42 147556. 0.5478
|
|
19.62 0.1974 0.4303 0.0907 0.0416 0.872 7.849 7.168 650.051 0.887 31.884 5.001 0.42 147751. 0.5238
|
|
22.43 0.2256 0.4750 0.0886 0.0421 0.882 7.938 7.003 657.387 0.897 31.148 4.832 0.42 147962. 0.5001
|
|
25.23 0.2537 0.5162 0.0863 0.0424 0.889 8.004 6.821 662.844 0.904 30.338 4.667 0.42 148189. 0.4768
|
|
28.03 0.2819 0.5541 0.0837 0.0426 0.893 8.043 6.620 666.070 0.909 29.448 4.508 0.42 148433. 0.4538
|
|
30.84 0.3101 0.5888 0.0810 0.0427 0.894 8.050 6.402 666.711 0.910 28.475 4.355 0.42 148693. 0.4310
|
|
33.64 0.3383 0.6205 0.0780 0.0425 0.891 8.023 6.164 664.425 0.906 27.415 4.208 0.42 148971. 0.4086
|
|
36.44 0.3665 0.6495 0.0747 0.0422 0.884 7.956 5.905 658.896 0.899 26.267 4.065 0.42 149265. 0.3864
|
|
39.25 0.3947 0.6758 0.0712 0.0416 0.871 7.847 5.627 649.840 0.887 25.029 3.928 0.42 149577. 0.3645
|
|
42.05 0.4229 0.6994 0.0674 0.0408 0.854 7.692 5.329 637.023 0.869 23.702 3.794 0.42 149906. 0.3426
|
|
44.85 0.4511 0.7205 0.0634 0.0397 0.832 7.489 5.011 620.265 0.846 22.288 3.664 0.42 150252. 0.3208
|
|
47.66 0.4793 0.7389 0.0591 0.0384 0.804 7.238 4.674 599.436 0.818 20.788 3.536 0.42 150616. 0.2991
|
|
50.46 0.5075 0.7543 0.0546 0.0368 0.770 6.937 4.319 574.534 0.784 19.212 3.410 0.42 150996. 0.2772
|
|
53.26 0.5357 0.7666 0.0500 0.0349 0.732 6.590 3.950 545.754 0.745 17.570 3.283 0.42 151393. 0.2552
|
|
56.07 0.5639 0.7752 0.0452 0.0328 0.688 6.198 3.569 513.327 0.700 15.876 3.154 0.42 151808. 0.2331
|
|
58.87 0.5921 0.7794 0.0402 0.0305 0.640 5.765 3.179 477.466 0.651 14.141 3.020 0.42 152239. 0.2106
|
|
61.67 0.6203 0.7782 0.0352 0.0280 0.588 5.293 2.782 438.372 0.598 12.373 2.878 0.42 152686. 0.1878
|
|
64.48 0.6485 0.7699 0.0301 0.0254 0.531 4.785 2.379 396.253 0.541 10.583 2.724 0.43 153151. 0.1643
|
|
67.28 0.6767 0.7517 0.0250 0.0225 0.471 4.242 1.974 351.341 0.479 8.781 2.549 0.43 153632. 0.1401
|
|
70.08 0.7049 0.7192 0.0198 0.0194 0.408 3.670 1.568 303.905 0.415 6.976 2.341 0.43 154130. 0.1147
|
|
72.89 0.7330 0.6639 0.0147 0.0163 0.341 3.070 1.165 254.267 0.347 5.181 2.078 0.43 154644. 0.0877
|
|
75.69 0.7612 0.5685 0.0097 0.0130 0.272 2.449 0.766 202.815 0.277 3.407 1.713 0.43 155175. 0.0587
|
|
78.50 0.7894 0.3906 0.0047 0.0096 0.201 1.811 0.375 150.006 0.205 1.670 1.135 0.43 155722. 0.0272
|
|
81.30 0.8176 -0.0076 -0.0001 0.0062 0.129 1.162 -0.005 96.269 0.131 -0.020 -0.021 0.43 156281. 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 0.1011 0.0366 1.146 9.030 10.439 854.675 1.020 46.433 5.540 0.48 167635. 0.7002
|
|
3.20 0.0282 0.0754 0.1001 0.0374 1.171 9.223 10.337 872.905 1.042 45.980 5.371 0.48 167763. 0.6756
|
|
6.40 0.0564 0.1461 0.0990 0.0382 1.195 9.416 10.224 891.264 1.064 45.476 5.203 0.48 167905. 0.6508
|
|
9.61 0.0845 0.2121 0.0978 0.0390 1.220 9.608 10.097 909.439 1.086 44.913 5.036 0.48 168062. 0.6260
|
|
12.81 0.1127 0.2735 0.0964 0.0397 1.243 9.795 9.956 927.088 1.107 44.286 4.871 0.48 168234. 0.6012
|
|
16.01 0.1409 0.3306 0.0949 0.0405 1.266 9.972 9.799 943.822 1.127 43.587 4.709 0.48 168423. 0.5766
|
|
19.21 0.1691 0.3834 0.0932 0.0411 1.286 10.134 9.624 959.215 1.145 42.809 4.551 0.48 168628. 0.5523
|
|
22.42 0.1973 0.4321 0.0913 0.0417 1.305 10.278 9.430 972.794 1.161 41.945 4.397 0.48 168851. 0.5282
|
|
25.62 0.2255 0.4770 0.0892 0.0422 1.320 10.397 9.215 984.061 1.175 40.988 4.247 0.48 169092. 0.5044
|
|
28.82 0.2536 0.5184 0.0869 0.0425 1.331 10.486 8.978 992.493 1.185 39.933 4.103 0.48 169352. 0.4809
|
|
32.02 0.2818 0.5564 0.0844 0.0428 1.338 10.539 8.717 997.554 1.191 38.772 3.963 0.48 169631. 0.4577
|
|
35.23 0.3100 0.5913 0.0817 0.0428 1.339 10.552 8.431 998.706 1.192 37.501 3.829 0.48 169929. 0.4349
|
|
38.43 0.3382 0.6233 0.0786 0.0427 1.335 10.517 8.119 995.430 1.188 36.115 3.700 0.48 170246. 0.4124
|
|
41.63 0.3664 0.6525 0.0754 0.0423 1.324 10.431 7.781 987.243 1.178 34.611 3.575 0.48 170583. 0.3901
|
|
44.83 0.3945 0.6790 0.0718 0.0417 1.306 10.288 7.416 973.715 1.162 32.988 3.455 0.48 170940. 0.3680
|
|
48.04 0.4227 0.7030 0.0680 0.0409 1.280 10.084 7.025 954.487 1.139 31.246 3.338 0.48 171316. 0.3461
|
|
51.24 0.4509 0.7244 0.0640 0.0398 1.246 9.818 6.607 929.285 1.109 29.388 3.225 0.48 171712. 0.3243
|
|
54.44 0.4791 0.7432 0.0597 0.0385 1.204 9.487 6.164 897.911 1.072 27.418 3.114 0.48 172127. 0.3024
|
|
57.64 0.5073 0.7591 0.0552 0.0369 1.154 9.090 5.698 860.350 1.027 25.345 3.004 0.48 172562. 0.2805
|
|
60.85 0.5355 0.7720 0.0505 0.0350 1.095 8.631 5.212 816.891 0.975 23.185 2.894 0.48 173016. 0.2585
|
|
64.05 0.5636 0.7814 0.0456 0.0329 1.030 8.113 4.711 767.883 0.917 20.955 2.783 0.48 173489. 0.2363
|
|
67.25 0.5918 0.7865 0.0406 0.0306 0.957 7.540 4.197 713.646 0.852 18.669 2.668 0.48 173981. 0.2138
|
|
70.45 0.6200 0.7864 0.0356 0.0281 0.878 6.915 3.674 654.484 0.781 16.341 2.546 0.49 174493. 0.1909
|
|
73.66 0.6482 0.7794 0.0304 0.0253 0.792 6.241 3.143 590.714 0.705 13.982 2.414 0.49 175024. 0.1674
|
|
76.86 0.6764 0.7629 0.0253 0.0224 0.701 5.522 2.609 522.686 0.624 11.606 2.264 0.49 175573. 0.1431
|
|
80.06 0.7045 0.7325 0.0201 0.0193 0.605 4.763 2.074 450.810 0.538 9.227 2.087 0.49 176142. 0.1176
|
|
83.26 0.7327 0.6798 0.0149 0.0161 0.504 3.968 1.542 375.576 0.448 6.859 1.862 0.49 176730. 0.0905
|
|
86.47 0.7609 0.5872 0.0098 0.0128 0.399 3.144 1.016 297.574 0.355 4.520 1.549 0.49 177336. 0.0611
|
|
89.67 0.7891 0.4108 0.0049 0.0093 0.292 2.298 0.501 217.502 0.260 2.229 1.045 0.49 177961. 0.0289
|
|
92.87 0.8173 0.0001 0.0000 0.0058 0.182 1.437 0.000 136.021 0.162 0.000 0.000 0.49 178599. 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 0.1017 0.0367 1.637 11.463 13.292 1220.548 1.295 59.125 4.940 0.54 188579. 0.7045
|
|
3.60 0.0282 0.0756 0.1008 0.0375 1.672 11.711 13.167 1247.003 1.323 58.565 4.789 0.54 188724. 0.6798
|
|
7.21 0.0564 0.1465 0.0997 0.0383 1.708 11.962 13.026 1273.673 1.351 57.940 4.639 0.54 188884. 0.6549
|
|
10.81 0.0846 0.2127 0.0985 0.0391 1.743 12.210 12.869 1300.104 1.379 57.240 4.490 0.54 189060. 0.6300
|
|
14.41 0.1127 0.2744 0.0971 0.0399 1.778 12.451 12.693 1325.800 1.407 56.458 4.342 0.54 189254. 0.6052
|
|
18.02 0.1409 0.3315 0.0956 0.0406 1.811 12.680 12.497 1350.198 1.433 55.585 4.198 0.54 189467. 0.5805
|
|
21.62 0.1691 0.3845 0.0940 0.0413 1.841 12.891 12.277 1372.670 1.456 54.610 4.057 0.54 189698. 0.5560
|
|
25.22 0.1973 0.4334 0.0921 0.0419 1.867 13.078 12.033 1392.537 1.478 53.525 3.919 0.54 189949. 0.5319
|
|
28.82 0.2255 0.4785 0.0900 0.0424 1.890 13.233 11.763 1409.066 1.495 52.320 3.786 0.54 190221. 0.5080
|
|
32.43 0.2537 0.5200 0.0877 0.0428 1.906 13.350 11.463 1421.496 1.508 50.988 3.658 0.54 190514. 0.4844
|
|
36.03 0.2818 0.5581 0.0852 0.0430 1.916 13.421 11.133 1429.046 1.516 49.519 3.534 0.54 190828. 0.4612
|
|
39.63 0.3100 0.5932 0.0824 0.0431 1.919 13.438 10.771 1430.937 1.518 47.909 3.414 0.54 191164. 0.4383
|
|
43.24 0.3382 0.6253 0.0794 0.0429 1.913 13.396 10.375 1426.411 1.513 46.149 3.299 0.54 191521. 0.4157
|
|
46.84 0.3664 0.6547 0.0761 0.0426 1.897 13.287 9.946 1414.765 1.501 44.238 3.189 0.54 191901. 0.3933
|
|
50.44 0.3946 0.6815 0.0726 0.0420 1.871 13.104 9.481 1395.372 1.481 42.172 3.082 0.54 192303. 0.3712
|
|
54.05 0.4228 0.7058 0.0687 0.0412 1.834 12.845 8.982 1367.711 1.451 39.953 2.979 0.54 192726. 0.3492
|
|
57.65 0.4509 0.7275 0.0647 0.0401 1.785 12.504 8.450 1331.384 1.413 37.584 2.879 0.54 193172. 0.3273
|
|
61.25 0.4791 0.7467 0.0603 0.0387 1.725 12.078 7.884 1286.101 1.365 35.070 2.781 0.54 193640. 0.3054
|
|
64.86 0.5073 0.7631 0.0558 0.0371 1.652 11.569 7.289 1231.836 1.307 32.422 2.684 0.54 194130. 0.2834
|
|
68.46 0.5355 0.7765 0.0510 0.0352 1.568 10.978 6.668 1168.996 1.240 29.661 2.587 0.54 194641. 0.2614
|
|
72.06 0.5637 0.7865 0.0461 0.0331 1.473 10.313 6.027 1098.087 1.165 26.810 2.490 0.54 195174. 0.2391
|
|
75.66 0.5919 0.7924 0.0411 0.0307 1.367 9.575 5.370 1019.570 1.082 23.886 2.389 0.54 195729. 0.2166
|
|
79.27 0.6200 0.7933 0.0360 0.0281 1.252 8.771 4.700 933.891 0.991 20.906 2.283 0.55 196305. 0.1936
|
|
82.87 0.6482 0.7874 0.0308 0.0253 1.128 7.903 4.021 841.505 0.893 17.887 2.167 0.55 196902. 0.1700
|
|
86.47 0.6764 0.7724 0.0255 0.0224 0.996 6.977 3.337 742.925 0.788 14.844 2.037 0.55 197521. 0.1456
|
|
90.08 0.7046 0.7437 0.0203 0.0192 0.857 5.999 2.652 638.746 0.678 11.797 1.883 0.55 198161. 0.1200
|
|
93.68 0.7328 0.6930 0.0151 0.0159 0.710 4.974 1.970 529.684 0.562 8.765 1.687 0.55 198822. 0.0927
|
|
97.28 0.7610 0.6022 0.0099 0.0125 0.559 3.912 1.297 416.601 0.442 5.769 1.412 0.55 199504. 0.0629
|
|
100.89 0.7891 0.4252 0.0049 0.0090 0.403 2.822 0.637 300.521 0.319 2.833 0.961 0.55 200207. 0.0300
|
|
104.49 0.8173 -0.0056 0.0000 0.0055 0.245 1.713 -0.005 182.391 0.194 -0.022 -0.012 0.55 200924. 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 0.1024 0.0369 2.258 14.231 16.523 1683.740 1.608 73.495 4.451 0.59 209520. 0.7078
|
|
4.00 0.0282 0.0757 0.1015 0.0378 2.308 14.545 16.373 1720.793 1.643 72.825 4.316 0.60 209680. 0.6831
|
|
8.00 0.0564 0.1467 0.1004 0.0386 2.358 14.861 16.204 1758.197 1.679 72.074 4.180 0.60 209858. 0.6582
|
|
12.01 0.0845 0.2130 0.0993 0.0394 2.408 15.174 16.014 1795.310 1.714 71.230 4.046 0.60 210054. 0.6333
|
|
16.01 0.1127 0.2746 0.0979 0.0402 2.456 15.480 15.801 1831.444 1.749 70.284 3.913 0.60 210270. 0.6085
|
|
20.01 0.1409 0.3319 0.0965 0.0409 2.502 15.770 15.563 1865.801 1.782 69.223 3.783 0.60 210506. 0.5838
|
|
24.01 0.1691 0.3849 0.0948 0.0416 2.545 16.038 15.296 1897.502 1.812 68.036 3.656 0.60 210764. 0.5594
|
|
28.02 0.1972 0.4339 0.0930 0.0423 2.582 16.276 14.998 1925.586 1.839 66.710 3.533 0.60 211043. 0.5352
|
|
32.02 0.2254 0.4791 0.0909 0.0428 2.614 16.474 14.666 1949.027 1.861 65.233 3.413 0.60 211346. 0.5113
|
|
36.02 0.2536 0.5207 0.0886 0.0432 2.637 16.623 14.298 1966.753 1.878 63.595 3.297 0.60 211671. 0.4877
|
|
40.02 0.2818 0.5590 0.0861 0.0434 2.652 16.716 13.891 1977.662 1.889 61.787 3.186 0.60 212021. 0.4645
|
|
44.02 0.3099 0.5942 0.0833 0.0435 2.656 16.741 13.444 1980.662 1.891 59.797 3.079 0.60 212394. 0.4416
|
|
48.03 0.3381 0.6265 0.0803 0.0433 2.648 16.691 12.954 1974.685 1.886 57.621 2.976 0.60 212792. 0.4189
|
|
52.03 0.3663 0.6561 0.0770 0.0430 2.627 16.556 12.422 1958.745 1.870 55.252 2.876 0.60 213214. 0.3966
|
|
56.03 0.3945 0.6831 0.0734 0.0424 2.591 16.329 11.845 1931.962 1.845 52.688 2.781 0.60 213661. 0.3744
|
|
60.03 0.4226 0.7076 0.0696 0.0416 2.539 16.005 11.225 1893.607 1.808 49.929 2.689 0.60 214133. 0.3524
|
|
64.04 0.4508 0.7297 0.0655 0.0404 2.472 15.578 10.562 1843.118 1.760 46.981 2.599 0.60 214628. 0.3304
|
|
68.04 0.4790 0.7492 0.0611 0.0391 2.387 15.046 9.858 1780.094 1.700 43.849 2.512 0.60 215149. 0.3085
|
|
72.04 0.5072 0.7661 0.0565 0.0374 2.286 14.407 9.116 1704.481 1.628 40.547 2.426 0.60 215693. 0.2865
|
|
76.04 0.5353 0.7801 0.0517 0.0355 2.168 13.666 8.341 1616.838 1.544 37.102 2.340 0.60 216262. 0.2644
|
|
80.05 0.5635 0.7907 0.0467 0.0333 2.035 12.829 7.541 1517.867 1.449 33.541 2.253 0.60 216854. 0.2421
|
|
84.05 0.5917 0.7974 0.0416 0.0309 1.888 11.903 6.719 1408.221 1.345 29.888 2.164 0.61 217471. 0.2195
|
|
88.05 0.6199 0.7992 0.0365 0.0283 1.728 10.891 5.882 1288.517 1.230 26.162 2.070 0.61 218111. 0.1964
|
|
92.05 0.6480 0.7946 0.0312 0.0254 1.555 9.800 5.033 1159.401 1.107 22.386 1.969 0.61 218774. 0.1728
|
|
96.05 0.6762 0.7810 0.0259 0.0224 1.370 8.635 4.177 1021.586 0.976 18.580 1.855 0.61 219462. 0.1483
|
|
100.06 0.7044 0.7540 0.0206 0.0192 1.175 7.403 3.320 875.912 0.836 14.765 1.719 0.61 220173. 0.1225
|
|
104.06 0.7326 0.7054 0.0153 0.0159 0.970 6.114 2.466 723.384 0.691 10.969 1.546 0.61 220907. 0.0950
|
|
108.06 0.7607 0.6168 0.0101 0.0124 0.758 4.777 1.622 565.214 0.540 7.216 1.302 0.61 221665. 0.0649
|
|
112.06 0.7889 0.4402 0.0049 0.0088 0.540 3.405 0.796 402.850 0.385 3.540 0.896 0.61 222446. 0.0313
|
|
116.07 0.8171 -0.0080 -0.0001 0.0052 0.319 2.008 -0.008 237.616 0.227 -0.036 -0.016 0.61 223242. 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 0.1032 0.0373 3.031 17.366 20.147 2260.093 1.962 89.613 4.043 0.65 230456. 0.7099
|
|
4.40 0.0282 0.0756 0.1023 0.0381 3.098 17.753 19.972 2310.443 2.006 88.833 3.921 0.65 230633. 0.6854
|
|
8.80 0.0563 0.1466 0.1013 0.0389 3.167 18.145 19.774 2361.389 2.050 87.956 3.798 0.65 230828. 0.6607
|
|
13.20 0.0845 0.2128 0.1002 0.0398 3.235 18.534 19.552 2412.056 2.094 86.966 3.677 0.65 231044. 0.6359
|
|
17.60 0.1127 0.2745 0.0989 0.0406 3.301 18.914 19.301 2461.490 2.137 85.851 3.557 0.65 231281. 0.6112
|
|
22.00 0.1408 0.3317 0.0974 0.0414 3.364 19.276 19.019 2508.590 2.178 84.595 3.439 0.66 231541. 0.5866
|
|
26.41 0.1690 0.3847 0.0958 0.0421 3.422 19.610 18.701 2552.139 2.216 83.183 3.324 0.66 231825. 0.5622
|
|
30.81 0.1972 0.4338 0.0940 0.0427 3.474 19.907 18.345 2590.817 2.249 81.600 3.212 0.66 232133. 0.5381
|
|
35.21 0.2253 0.4790 0.0919 0.0433 3.518 20.156 17.948 2623.212 2.277 79.831 3.103 0.66 232466. 0.5143
|
|
39.61 0.2535 0.5207 0.0897 0.0437 3.551 20.346 17.505 2647.852 2.299 77.862 2.999 0.66 232824. 0.4908
|
|
44.01 0.2817 0.5591 0.0872 0.0439 3.571 20.464 17.014 2663.230 2.312 75.680 2.898 0.66 233209. 0.4676
|
|
48.41 0.3098 0.5944 0.0844 0.0440 3.578 20.499 16.474 2667.842 2.316 73.275 2.801 0.66 233621. 0.4447
|
|
52.81 0.3380 0.6269 0.0813 0.0439 3.567 20.441 15.880 2660.235 2.309 70.636 2.708 0.66 234059. 0.4221
|
|
57.21 0.3662 0.6567 0.0780 0.0435 3.539 20.278 15.233 2639.054 2.291 67.757 2.618 0.66 234524. 0.3997
|
|
61.61 0.3943 0.6839 0.0744 0.0429 3.491 20.002 14.532 2603.103 2.260 64.636 2.532 0.66 235016. 0.3776
|
|
66.01 0.4225 0.7087 0.0706 0.0421 3.421 19.604 13.775 2551.382 2.215 61.273 2.449 0.66 235535. 0.3556
|
|
70.42 0.4507 0.7311 0.0664 0.0409 3.330 19.080 12.966 2483.133 2.156 57.673 2.368 0.66 236082. 0.3336
|
|
74.82 0.4788 0.7510 0.0620 0.0395 3.216 18.424 12.105 2397.813 2.082 53.844 2.290 0.66 236654. 0.3116
|
|
79.22 0.5070 0.7684 0.0574 0.0378 3.078 17.637 11.197 2295.326 1.993 49.803 2.213 0.66 237254. 0.2896
|
|
83.62 0.5352 0.7829 0.0525 0.0359 2.919 16.723 10.248 2176.416 1.889 45.583 2.136 0.66 237880. 0.2674
|
|
88.02 0.5633 0.7942 0.0475 0.0337 2.738 15.691 9.266 2042.040 1.773 41.217 2.058 0.66 238532. 0.2451
|
|
92.42 0.5915 0.8017 0.0423 0.0312 2.539 14.546 8.258 1893.087 1.643 36.733 1.979 0.67 239210. 0.2224
|
|
96.82 0.6197 0.8044 0.0370 0.0285 2.321 13.296 7.230 1730.402 1.502 32.159 1.895 0.67 239914. 0.1993
|
|
101.22 0.6478 0.8009 0.0317 0.0256 2.085 11.947 6.187 1554.866 1.350 27.519 1.805 0.67 240644. 0.1756
|
|
105.62 0.6760 0.7887 0.0263 0.0225 1.834 10.507 5.135 1367.454 1.187 22.840 1.703 0.67 241401. 0.1510
|
|
110.02 0.7042 0.7634 0.0209 0.0193 1.568 8.985 4.080 1169.311 1.015 18.149 1.583 0.67 242183. 0.1251
|
|
114.42 0.7323 0.7168 0.0155 0.0159 1.290 7.390 3.030 961.812 0.835 13.478 1.429 0.67 242990. 0.0973
|
|
118.83 0.7605 0.6304 0.0102 0.0123 1.001 5.737 1.992 746.629 0.648 8.860 1.210 0.67 243824. 0.0668
|
|
123.23 0.7886 0.4541 0.0050 0.0087 0.705 4.040 0.974 525.785 0.456 4.334 0.841 0.67 244682. 0.0325
|
|
127.63 0.8168 -0.0131 -0.0001 0.0050 0.404 2.314 -0.016 301.149 0.261 -0.069 -0.023 0.68 245557. 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 0.1041 0.0379 4.004 21.032 24.179 2985.952 2.376 107.548 3.673 0.71 251387. 0.7065
|
|
4.79 0.0281 0.0749 0.1032 0.0387 4.091 21.485 23.981 3050.331 2.427 106.669 3.566 0.71 251579. 0.6831
|
|
9.59 0.0563 0.1454 0.1023 0.0396 4.178 21.945 23.758 3115.641 2.479 105.674 3.459 0.71 251792. 0.6594
|
|
14.38 0.0844 0.2113 0.1012 0.0404 4.266 22.404 23.504 3180.812 2.531 104.546 3.352 0.71 252027. 0.6356
|
|
19.18 0.1125 0.2728 0.0999 0.0412 4.351 22.854 23.216 3244.634 2.582 103.267 3.245 0.71 252286. 0.6117
|
|
23.97 0.1406 0.3301 0.0985 0.0420 4.433 23.284 22.891 3305.717 2.631 101.818 3.141 0.71 252569. 0.5878
|
|
28.77 0.1688 0.3831 0.0969 0.0427 4.509 23.684 22.523 3362.488 2.676 100.180 3.038 0.72 252878. 0.5640
|
|
33.56 0.1969 0.4322 0.0952 0.0433 4.577 24.041 22.108 3413.222 2.716 98.335 2.938 0.72 253214. 0.5403
|
|
38.35 0.2250 0.4776 0.0932 0.0439 4.635 24.343 21.642 3456.036 2.750 96.263 2.840 0.72 253577. 0.5169
|
|
43.15 0.2531 0.5194 0.0909 0.0443 4.679 24.575 21.121 3488.945 2.776 93.947 2.746 0.72 253968. 0.4936
|
|
47.94 0.2813 0.5579 0.0884 0.0446 4.707 24.722 20.542 3509.878 2.793 91.370 2.655 0.72 254388. 0.4706
|
|
52.74 0.3094 0.5934 0.0857 0.0447 4.716 24.770 19.901 3516.746 2.799 88.518 2.567 0.72 254837. 0.4479
|
|
57.53 0.3375 0.6260 0.0826 0.0445 4.704 24.705 19.195 3507.507 2.791 85.380 2.482 0.72 255315. 0.4254
|
|
62.32 0.3656 0.6560 0.0793 0.0442 4.667 24.513 18.424 3480.271 2.770 81.948 2.401 0.72 255822. 0.4031
|
|
67.12 0.3938 0.6836 0.0757 0.0436 4.604 24.183 17.585 3433.400 2.732 78.217 2.323 0.72 256359. 0.3811
|
|
71.91 0.4219 0.7087 0.0718 0.0427 4.513 23.705 16.679 3365.555 2.678 74.189 2.248 0.72 256925. 0.3591
|
|
76.71 0.4500 0.7314 0.0676 0.0416 4.393 23.073 15.708 3275.731 2.607 69.870 2.175 0.72 257521. 0.3372
|
|
81.50 0.4781 0.7518 0.0632 0.0402 4.242 22.280 14.674 3163.212 2.517 65.269 2.104 0.72 258145. 0.3153
|
|
86.30 0.5063 0.7696 0.0585 0.0385 4.060 21.327 13.580 3027.828 2.409 60.405 2.034 0.72 258799. 0.2933
|
|
91.09 0.5344 0.7848 0.0535 0.0365 3.849 20.219 12.437 2870.523 2.284 55.319 1.965 0.72 259481. 0.2711
|
|
95.88 0.5625 0.7968 0.0484 0.0342 3.611 18.965 11.252 2692.567 2.143 50.051 1.895 0.73 260191. 0.2487
|
|
100.68 0.5906 0.8051 0.0432 0.0317 3.346 17.575 10.035 2495.151 1.986 44.635 1.824 0.73 260930. 0.2260
|
|
105.47 0.6188 0.8089 0.0378 0.0289 3.057 16.055 8.791 2279.419 1.814 39.104 1.749 0.73 261698. 0.2029
|
|
110.27 0.6469 0.8066 0.0324 0.0260 2.745 14.415 7.529 2046.594 1.629 33.490 1.669 0.73 262493. 0.1791
|
|
115.06 0.6750 0.7959 0.0269 0.0228 2.411 12.665 6.255 1798.060 1.431 27.823 1.578 0.73 263316. 0.1544
|
|
119.86 0.7032 0.7725 0.0214 0.0195 2.059 10.815 4.977 1535.474 1.222 22.138 1.470 0.73 264168. 0.1283
|
|
124.65 0.7313 0.7280 0.0159 0.0160 1.691 8.881 3.703 1260.872 1.003 16.472 1.332 0.73 265047. 0.1003
|
|
129.44 0.7594 0.6437 0.0105 0.0124 1.310 6.880 2.443 976.778 0.777 10.866 1.134 0.73 265954. 0.0694
|
|
134.24 0.7875 0.4693 0.0052 0.0087 0.920 4.834 1.206 686.248 0.546 5.366 0.797 0.74 266888. 0.0343
|
|
139.03 0.8157 0.0021 0.0000 0.0050 0.526 2.763 0.003 392.238 0.312 0.013 0.003 0.74 267841. 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 0.1050 0.0397 5.325 25.820 28.630 3971.187 2.917 127.346 3.270 0.77 272312. 0.6844
|
|
5.19 0.0281 0.0724 0.1042 0.0404 5.428 26.316 28.414 4047.492 2.973 126.387 3.184 0.77 272519. 0.6640
|
|
10.37 0.0562 0.1409 0.1033 0.0412 5.531 26.817 28.168 4124.626 3.030 125.293 3.098 0.77 272749. 0.6431
|
|
15.56 0.0843 0.2054 0.1023 0.0420 5.634 27.315 27.888 4201.214 3.086 124.044 3.011 0.77 273003. 0.6220
|
|
20.75 0.1124 0.2660 0.1011 0.0427 5.734 27.800 27.567 4275.759 3.141 122.618 2.924 0.77 273283. 0.6006
|
|
25.94 0.1405 0.3228 0.0998 0.0434 5.829 28.260 27.201 4346.563 3.193 120.990 2.838 0.77 273590. 0.5791
|
|
31.12 0.1686 0.3757 0.0982 0.0441 5.916 28.684 26.784 4411.743 3.241 119.137 2.754 0.77 273924. 0.5575
|
|
36.31 0.1966 0.4251 0.0965 0.0446 5.993 29.058 26.312 4469.228 3.283 117.034 2.670 0.78 274288. 0.5358
|
|
41.50 0.2247 0.4709 0.0945 0.0451 6.057 29.367 25.777 4516.791 3.318 114.658 2.589 0.78 274681. 0.5141
|
|
46.69 0.2528 0.5134 0.0923 0.0455 6.104 29.596 25.177 4552.069 3.344 111.986 2.509 0.78 275105. 0.4924
|
|
51.87 0.2809 0.5528 0.0899 0.0457 6.132 29.730 24.505 4572.590 3.359 108.998 2.431 0.78 275560. 0.4707
|
|
57.06 0.3090 0.5891 0.0871 0.0457 6.136 29.751 23.758 4575.802 3.361 105.674 2.355 0.78 276047. 0.4490
|
|
62.25 0.3371 0.6226 0.0841 0.0455 6.114 29.643 22.932 4559.181 3.349 102.002 2.281 0.78 276565. 0.4274
|
|
67.44 0.3652 0.6534 0.0808 0.0452 6.062 29.390 22.025 4520.313 3.320 97.969 2.210 0.78 277115. 0.4057
|
|
72.62 0.3933 0.6816 0.0772 0.0445 5.977 28.978 21.037 4456.985 3.274 93.571 2.141 0.78 277697. 0.3841
|
|
77.81 0.4214 0.7073 0.0732 0.0436 5.857 28.395 19.966 4367.282 3.208 88.809 2.074 0.78 278310. 0.3624
|
|
83.00 0.4495 0.7307 0.0690 0.0424 5.699 27.630 18.815 4249.666 3.122 83.690 2.008 0.78 278956. 0.3407
|
|
88.19 0.4776 0.7516 0.0645 0.0410 5.502 26.676 17.587 4102.966 3.014 78.226 1.944 0.78 279633. 0.3189
|
|
93.37 0.5057 0.7701 0.0597 0.0392 5.266 25.531 16.286 3926.742 2.884 72.441 1.881 0.78 280340. 0.2970
|
|
98.56 0.5337 0.7858 0.0547 0.0372 4.991 24.200 14.923 3722.019 2.734 66.379 1.819 0.78 281079. 0.2748
|
|
103.75 0.5618 0.7985 0.0495 0.0349 4.681 22.694 13.510 3490.494 2.564 60.091 1.756 0.79 281849. 0.2524
|
|
108.94 0.5899 0.8074 0.0442 0.0323 4.337 21.026 12.055 3233.880 2.375 53.619 1.691 0.79 282649. 0.2296
|
|
114.12 0.6180 0.8117 0.0388 0.0295 3.961 19.206 10.567 2953.969 2.170 47.001 1.622 0.79 283479. 0.2063
|
|
119.31 0.6461 0.8098 0.0332 0.0265 3.557 17.247 9.055 2652.701 1.949 40.275 1.548 0.79 284340. 0.1822
|
|
124.50 0.6742 0.7989 0.0276 0.0233 3.128 15.164 7.527 2332.321 1.713 33.478 1.464 0.79 285231. 0.1571
|
|
129.69 0.7023 0.7743 0.0220 0.0199 2.676 12.975 5.992 1995.591 1.466 26.651 1.362 0.79 286152. 0.1304
|
|
134.87 0.7304 0.7267 0.0164 0.0164 2.207 10.701 4.460 1645.826 1.209 19.838 1.229 0.79 287103. 0.1015
|
|
140.06 0.7585 0.6367 0.0108 0.0129 1.726 8.368 2.942 1287.037 0.945 13.088 1.037 0.80 288084. 0.0696
|
|
145.25 0.7866 0.4538 0.0053 0.0092 1.239 6.007 1.452 923.939 0.679 6.457 0.713 0.80 289094. 0.0336
|
|
150.43 0.8147 -0.0008 0.0000 0.0056 0.752 3.647 -0.001 560.942 0.412 -0.007 -0.001 0.80 290124. 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 0.1059 0.0435 7.298 32.854 33.495 5441.838 3.712 148.987 2.792 0.83 293229. 0.6320
|
|
5.58 0.0281 0.0668 0.1052 0.0442 7.411 33.366 33.268 5526.634 3.770 147.974 2.730 0.83 293451. 0.6160
|
|
11.17 0.0562 0.1307 0.1044 0.0449 7.525 33.876 33.006 5611.065 3.827 146.812 2.668 0.83 293698. 0.5996
|
|
16.75 0.0843 0.1914 0.1034 0.0455 7.635 34.372 32.706 5693.234 3.883 145.474 2.606 0.83 293971. 0.5829
|
|
22.34 0.1123 0.2491 0.1023 0.0462 7.739 34.842 32.359 5771.136 3.936 143.932 2.543 0.83 294272. 0.5659
|
|
27.92 0.1404 0.3037 0.1011 0.0467 7.835 35.273 31.959 5842.515 3.985 142.155 2.481 0.83 294602. 0.5487
|
|
33.51 0.1685 0.3554 0.0996 0.0472 7.919 35.651 31.500 5905.052 4.028 140.113 2.420 0.83 294963. 0.5312
|
|
39.09 0.1966 0.4043 0.0980 0.0476 7.988 35.960 30.974 5956.285 4.063 137.774 2.359 0.83 295355. 0.5135
|
|
44.68 0.2247 0.4502 0.0961 0.0479 8.038 36.186 30.375 5993.676 4.088 135.108 2.299 0.84 295779. 0.4956
|
|
50.26 0.2528 0.4935 0.0939 0.0481 8.066 36.312 29.696 6014.619 4.103 132.087 2.239 0.84 296236. 0.4774
|
|
55.85 0.2808 0.5340 0.0915 0.0481 8.068 36.323 28.931 6016.458 4.104 128.684 2.181 0.84 296728. 0.4589
|
|
61.43 0.3089 0.5719 0.0888 0.0480 8.041 36.203 28.075 5996.496 4.090 124.877 2.124 0.84 297253. 0.4401
|
|
67.02 0.3370 0.6073 0.0858 0.0476 7.982 35.934 27.123 5952.038 4.060 120.645 2.067 0.84 297812. 0.4211
|
|
72.60 0.3651 0.6401 0.0825 0.0470 7.886 35.502 26.074 5880.449 4.011 115.975 2.011 0.84 298406. 0.4017
|
|
78.19 0.3932 0.6705 0.0788 0.0462 7.750 34.891 24.923 5779.264 3.942 110.859 1.956 0.84 299035. 0.3820
|
|
83.77 0.4213 0.6984 0.0749 0.0452 7.572 34.089 23.673 5646.425 3.851 105.297 1.902 0.84 299698. 0.3619
|
|
89.36 0.4493 0.7238 0.0706 0.0438 7.349 33.086 22.324 5480.243 3.738 99.299 1.848 0.84 300394. 0.3415
|
|
94.94 0.4774 0.7467 0.0660 0.0422 7.080 31.873 20.881 5279.373 3.601 92.879 1.794 0.84 301125. 0.3207
|
|
100.53 0.5055 0.7669 0.0612 0.0403 6.763 30.449 19.349 5043.463 3.440 86.063 1.740 0.84 301889. 0.2994
|
|
106.11 0.5336 0.7838 0.0561 0.0382 6.405 28.834 17.740 4775.891 3.258 78.907 1.685 0.84 302686. 0.2776
|
|
111.70 0.5617 0.7970 0.0508 0.0358 6.005 27.034 16.068 4477.755 3.054 71.469 1.628 0.85 303516. 0.2552
|
|
117.28 0.5898 0.8055 0.0454 0.0332 5.569 25.071 14.343 4152.659 2.832 63.800 1.567 0.85 304379. 0.2321
|
|
122.87 0.6179 0.8084 0.0398 0.0304 5.098 22.949 12.578 3801.219 2.593 55.947 1.501 0.85 305274. 0.2082
|
|
128.45 0.6459 0.8037 0.0341 0.0274 4.595 20.686 10.781 3426.326 2.337 47.956 1.427 0.85 306202. 0.1833
|
|
134.04 0.6740 0.7881 0.0283 0.0242 4.065 18.303 8.964 3031.618 2.068 39.872 1.341 0.85 307162. 0.1571
|
|
139.62 0.7021 0.7558 0.0226 0.0210 3.516 15.828 7.137 2621.760 1.788 31.744 1.235 0.85 308154. 0.1290
|
|
145.21 0.7302 0.6964 0.0168 0.0176 2.953 13.295 5.311 2202.175 1.502 23.624 1.094 0.86 309179. 0.0986
|
|
150.79 0.7583 0.5903 0.0111 0.0142 2.386 10.740 3.502 1778.987 1.213 15.577 0.893 0.86 310235. 0.0654
|
|
156.38 0.7864 0.3945 0.0055 0.0109 1.822 8.204 1.724 1358.810 0.927 7.668 0.575 0.86 311323. 0.0296
|
|
161.96 0.8144 -0.0032 0.0000 0.0076 1.270 5.718 -0.009 947.125 0.646 -0.042 -0.005 0.86 312434. 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 0.1062 0.0494 10.190 42.818 38.561 7598.735 4.838 171.521 2.302 0.89 314161. 0.5591
|
|
6.00 0.0282 0.0594 0.1056 0.0501 10.327 43.395 38.337 7701.132 4.903 170.524 2.258 0.89 314397. 0.5469
|
|
12.01 0.0564 0.1166 0.1049 0.0507 10.461 43.956 38.077 7800.819 4.966 169.366 2.214 0.89 314660. 0.5344
|
|
18.01 0.0845 0.1714 0.1041 0.0513 10.587 44.486 37.773 7894.815 5.026 168.016 2.170 0.89 314951. 0.5217
|
|
24.02 0.1127 0.2239 0.1031 0.0519 10.701 44.966 37.418 7979.939 5.080 166.437 2.127 0.89 315272. 0.5089
|
|
30.02 0.1409 0.2743 0.1019 0.0524 10.799 45.376 37.004 8052.794 5.127 164.593 2.084 0.89 315626. 0.4960
|
|
36.03 0.1691 0.3226 0.1006 0.0527 10.876 45.698 36.520 8109.908 5.163 162.442 2.042 0.89 316012. 0.4828
|
|
42.03 0.1973 0.3688 0.0991 0.0530 10.926 45.911 35.958 8147.808 5.187 159.943 2.002 0.89 316433. 0.4695
|
|
48.03 0.2254 0.4132 0.0973 0.0531 10.946 45.994 35.309 8162.481 5.196 157.053 1.962 0.89 316889. 0.4561
|
|
54.04 0.2536 0.4556 0.0952 0.0530 10.931 45.932 34.563 8151.457 5.189 153.737 1.923 0.90 317381. 0.4423
|
|
60.04 0.2818 0.4962 0.0929 0.0527 10.878 45.709 33.714 8111.841 5.164 149.960 1.885 0.90 317911. 0.4282
|
|
66.05 0.3100 0.5350 0.0902 0.0523 10.783 45.309 32.754 8040.949 5.119 145.690 1.848 0.90 318477. 0.4136
|
|
72.05 0.3382 0.5719 0.0873 0.0516 10.643 44.720 31.678 7936.427 5.052 140.903 1.810 0.90 319082. 0.3986
|
|
78.06 0.3663 0.6068 0.0840 0.0507 10.455 43.930 30.481 7796.244 4.963 135.581 1.773 0.90 319723. 0.3830
|
|
84.06 0.3945 0.6398 0.0803 0.0495 10.217 42.930 29.162 7618.686 4.850 129.714 1.736 0.90 320402. 0.3667
|
|
90.06 0.4227 0.6707 0.0764 0.0481 9.927 41.711 27.721 7402.363 4.712 123.302 1.699 0.90 321119. 0.3498
|
|
96.07 0.4509 0.6993 0.0721 0.0465 9.583 40.268 26.159 7146.182 4.549 116.356 1.660 0.90 321872. 0.3322
|
|
102.07 0.4791 0.7255 0.0674 0.0445 9.185 38.594 24.481 6849.239 4.360 108.892 1.621 0.90 322662. 0.3138
|
|
108.08 0.5072 0.7490 0.0625 0.0423 8.732 36.690 22.694 6511.247 4.145 100.945 1.581 0.90 323487. 0.2946
|
|
114.08 0.5354 0.7692 0.0573 0.0399 8.231 34.587 20.813 6138.092 3.908 92.578 1.538 0.91 324349. 0.2745
|
|
120.09 0.5636 0.7844 0.0519 0.0373 7.696 32.340 18.853 5739.229 3.654 83.857 1.490 0.91 325246. 0.2531
|
|
126.09 0.5918 0.7934 0.0464 0.0346 7.131 29.965 16.828 5317.826 3.385 74.850 1.435 0.91 326178. 0.2303
|
|
132.09 0.6200 0.7916 0.0406 0.0318 6.562 27.574 14.748 4893.507 3.115 65.600 1.367 0.91 327144. 0.2054
|
|
138.10 0.6481 0.7791 0.0348 0.0289 5.970 25.083 12.631 4451.467 2.834 56.181 1.287 0.91 328146. 0.1789
|
|
144.10 0.6763 0.7522 0.0289 0.0260 5.358 22.512 10.488 3995.142 2.543 46.651 1.191 0.91 329182. 0.1508
|
|
150.11 0.7045 0.7047 0.0230 0.0230 4.735 19.895 8.335 3530.664 2.248 37.075 1.071 0.91 330253. 0.1209
|
|
156.11 0.7327 0.6265 0.0170 0.0199 4.112 17.277 6.188 3066.136 1.952 27.524 0.915 0.92 331357. 0.0891
|
|
162.12 0.7609 0.5021 0.0112 0.0170 3.500 14.705 4.065 2609.585 1.661 18.080 0.707 0.92 332497. 0.0557
|
|
168.12 0.7890 0.3062 0.0055 0.0141 2.908 12.220 1.987 2168.671 1.381 8.837 0.416 0.92 333670. 0.0229
|
|
174.12 0.8172 -0.0057 -0.0001 0.0114 2.343 9.843 -0.029 1746.879 1.112 -0.128 -0.007 0.92 334874. 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 0.1045 0.0544 13.611 53.618 43.168 10149.915 6.058 192.010 1.929 0.95 335155. 0.4958
|
|
6.54 0.0288 0.0543 0.1040 0.0551 13.798 54.353 42.957 10288.988 6.141 191.073 1.894 0.95 335407. 0.4855
|
|
13.08 0.0576 0.1066 0.1034 0.0559 13.985 55.091 42.712 10428.737 6.224 189.983 1.858 0.95 335688. 0.4749
|
|
19.63 0.0864 0.1567 0.1027 0.0566 14.168 55.812 42.424 10565.198 6.306 188.704 1.821 0.95 336001. 0.4640
|
|
26.17 0.1151 0.2048 0.1019 0.0573 14.340 56.491 42.085 10693.703 6.382 187.194 1.785 0.95 336347. 0.4530
|
|
32.71 0.1439 0.2508 0.1009 0.0579 14.495 57.099 41.683 10808.743 6.451 185.405 1.749 0.95 336729. 0.4418
|
|
39.25 0.1727 0.2949 0.0998 0.0584 14.623 57.602 41.206 10904.062 6.508 183.285 1.714 0.95 337147. 0.4304
|
|
45.79 0.2015 0.3373 0.0984 0.0588 14.715 57.965 40.642 10972.798 6.549 180.776 1.680 0.95 337604. 0.4190
|
|
52.34 0.2303 0.3779 0.0968 0.0590 14.762 58.150 39.978 11007.729 6.570 177.820 1.647 0.95 338101. 0.4074
|
|
58.88 0.2591 0.4171 0.0949 0.0589 14.754 58.118 39.199 11001.693 6.566 174.358 1.616 0.96 338639. 0.3958
|
|
65.42 0.2878 0.4550 0.0927 0.0587 14.682 57.835 38.294 10948.074 6.534 170.332 1.586 0.96 339219. 0.3840
|
|
71.96 0.3166 0.4917 0.0902 0.0581 14.539 57.271 37.251 10841.367 6.470 165.691 1.558 0.96 339842. 0.3721
|
|
78.50 0.3454 0.5272 0.0873 0.0572 14.319 56.406 36.060 10677.562 6.373 160.394 1.532 0.96 340507. 0.3598
|
|
85.05 0.3742 0.5615 0.0841 0.0560 14.020 55.227 34.714 10454.354 6.239 154.409 1.506 0.96 341215. 0.3471
|
|
91.59 0.4030 0.5947 0.0804 0.0545 13.640 53.730 33.211 10171.013 6.070 147.722 1.481 0.96 341966. 0.3339
|
|
98.13 0.4318 0.6264 0.0764 0.0527 13.180 51.918 31.549 9827.983 5.866 140.332 1.456 0.96 342759. 0.3199
|
|
104.67 0.4606 0.6565 0.0720 0.0505 12.641 49.797 29.733 9426.484 5.626 132.251 1.431 0.96 343593. 0.3052
|
|
111.21 0.4893 0.6847 0.0672 0.0480 12.026 47.375 27.766 8968.086 5.352 123.505 1.404 0.96 344469. 0.2895
|
|
117.76 0.5181 0.7106 0.0621 0.0453 11.340 44.670 25.663 8455.895 5.047 114.150 1.377 0.96 345385. 0.2728
|
|
124.30 0.5469 0.7335 0.0568 0.0423 10.594 41.731 23.445 7899.577 4.715 104.282 1.346 0.97 346340. 0.2550
|
|
130.84 0.5757 0.7501 0.0512 0.0393 9.827 38.711 21.129 7327.861 4.373 93.981 1.308 0.97 347335. 0.2352
|
|
137.38 0.6045 0.7593 0.0454 0.0361 9.040 35.610 18.736 6740.933 4.023 83.338 1.261 0.97 348369. 0.2135
|
|
143.92 0.6333 0.7476 0.0394 0.0334 8.352 32.900 16.268 6227.974 3.717 72.362 1.185 0.97 349442. 0.1869
|
|
150.47 0.6620 0.7172 0.0333 0.0307 7.695 30.313 13.756 5738.309 3.425 61.187 1.087 0.97 350553. 0.1578
|
|
157.01 0.6908 0.6677 0.0272 0.0281 7.039 27.730 11.227 5249.184 3.133 49.938 0.970 0.97 351702. 0.1272
|
|
163.55 0.7196 0.5937 0.0211 0.0256 6.396 25.194 8.707 4769.225 2.846 38.729 0.828 0.98 352889. 0.0956
|
|
170.09 0.7484 0.4890 0.0151 0.0231 5.774 22.746 6.225 4305.874 2.570 27.690 0.656 0.98 354114. 0.0640
|
|
176.63 0.7772 0.3464 0.0092 0.0207 5.185 20.424 3.813 3866.262 2.308 16.962 0.447 0.98 355378. 0.0342
|
|
183.18 0.8060 0.1578 0.0036 0.0185 4.634 18.255 1.497 3455.600 2.062 6.659 0.196 0.98 356688. 0.0094
|
|
189.72 0.8348
|
|
|
|
|
|
|