538 lines
95 KiB
Plaintext
538 lines
95 KiB
Plaintext
17x10WE (17x10WE.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 0.1071 0.0448 0.005 0.318 0.282 3.762 0.036 1.253 33.973 0.07 33489. 0.6243
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0.40 0.0252 0.0588 0.1055 0.0453 0.005 0.321 0.278 3.801 0.036 1.235 33.118 0.07 33514. 0.6040
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0.81 0.0505 0.1146 0.1038 0.0457 0.005 0.324 0.273 3.838 0.037 1.214 32.265 0.07 33542. 0.5836
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1.21 0.0757 0.1673 0.1019 0.0461 0.005 0.327 0.268 3.871 0.037 1.193 31.415 0.07 33571. 0.5631
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1.62 0.1009 0.2171 0.0999 0.0464 0.005 0.330 0.263 3.899 0.037 1.169 30.571 0.07 33603. 0.5425
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2.02 0.1261 0.2640 0.0977 0.0467 0.005 0.331 0.257 3.922 0.037 1.144 29.735 0.07 33637. 0.5219
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2.43 0.1514 0.3079 0.0954 0.0469 0.005 0.333 0.251 3.938 0.038 1.116 28.907 0.07 33673. 0.5013
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2.83 0.1766 0.3491 0.0929 0.0470 0.005 0.334 0.244 3.946 0.038 1.087 28.089 0.07 33712. 0.4807
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3.24 0.2018 0.3875 0.0902 0.0470 0.005 0.334 0.237 3.946 0.038 1.056 27.281 0.07 33754. 0.4601
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3.64 0.2271 0.4231 0.0873 0.0469 0.005 0.333 0.230 3.936 0.038 1.022 26.481 0.07 33798. 0.4394
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4.05 0.2523 0.4561 0.0843 0.0466 0.005 0.331 0.222 3.915 0.037 0.986 25.691 0.07 33845. 0.4188
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4.45 0.2775 0.4864 0.0810 0.0462 0.005 0.328 0.213 3.882 0.037 0.948 24.907 0.07 33895. 0.3981
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4.86 0.3028 0.5140 0.0776 0.0457 0.005 0.324 0.204 3.837 0.037 0.908 24.127 0.07 33948. 0.3773
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5.26 0.3280 0.5389 0.0739 0.0450 0.005 0.319 0.194 3.777 0.036 0.865 23.348 0.07 34003. 0.3564
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5.67 0.3532 0.5609 0.0701 0.0441 0.005 0.313 0.184 3.704 0.035 0.820 22.565 0.07 34062. 0.3353
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6.07 0.3784 0.5799 0.0660 0.0431 0.005 0.306 0.174 3.617 0.035 0.772 21.774 0.07 34123. 0.3141
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6.48 0.4037 0.5956 0.0618 0.0419 0.005 0.297 0.163 3.517 0.034 0.723 20.968 0.07 34187. 0.2927
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6.88 0.4289 0.6079 0.0574 0.0405 0.005 0.288 0.151 3.403 0.032 0.672 20.140 0.07 34254. 0.2710
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7.29 0.4541 0.6162 0.0530 0.0390 0.004 0.277 0.139 3.277 0.031 0.620 19.281 0.07 34324. 0.2491
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7.69 0.4794 0.6200 0.0484 0.0374 0.004 0.265 0.127 3.139 0.030 0.566 18.381 0.07 34396. 0.2269
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8.10 0.5046 0.6188 0.0437 0.0356 0.004 0.253 0.115 2.989 0.029 0.511 17.426 0.07 34472. 0.2044
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8.50 0.5298 0.6115 0.0389 0.0337 0.004 0.239 0.102 2.828 0.027 0.455 16.401 0.07 34550. 0.1816
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8.91 0.5551 0.5970 0.0340 0.0316 0.004 0.224 0.089 2.655 0.025 0.398 15.284 0.07 34632. 0.1583
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9.31 0.5803 0.5736 0.0291 0.0294 0.003 0.209 0.077 2.472 0.024 0.341 14.046 0.07 34716. 0.1345
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9.72 0.6055 0.5389 0.0242 0.0271 0.003 0.193 0.064 2.279 0.022 0.283 12.648 0.07 34803. 0.1104
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10.12 0.6307 0.4897 0.0192 0.0247 0.003 0.176 0.051 2.077 0.020 0.225 11.033 0.07 34893. 0.0859
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10.53 0.6560 0.4209 0.0143 0.0222 0.003 0.158 0.038 1.867 0.018 0.167 9.119 0.07 34987. 0.0612
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10.93 0.6812 0.3249 0.0094 0.0196 0.002 0.139 0.025 1.650 0.016 0.110 6.777 0.07 35083. 0.0368
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11.34 0.7064 0.1889 0.0045 0.0170 0.002 0.121 0.012 1.427 0.014 0.053 3.801 0.07 35181. 0.0144
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11.74 0.7317 -0.0096 -0.0002 0.0143 0.002 0.101 0.000 1.199 0.011 -0.002 -0.187 0.07 35282. 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 0.1075 0.0417 0.038 1.183 1.131 27.983 0.134 5.032 18.335 0.13 66978. 0.6751
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0.81 0.0253 0.0636 0.1059 0.0422 0.038 1.197 1.114 28.327 0.135 4.957 17.843 0.13 67028. 0.6520
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1.63 0.0506 0.1236 0.1042 0.0427 0.038 1.211 1.096 28.650 0.137 4.876 17.353 0.13 67083. 0.6289
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2.44 0.0759 0.1803 0.1023 0.0431 0.039 1.223 1.076 28.943 0.138 4.788 16.869 0.13 67142. 0.6059
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3.25 0.1013 0.2336 0.1003 0.0435 0.039 1.234 1.055 29.200 0.139 4.694 16.391 0.13 67205. 0.5829
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4.06 0.1266 0.2836 0.0981 0.0438 0.039 1.243 1.032 29.411 0.140 4.592 15.920 0.13 67274. 0.5599
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4.88 0.1519 0.3304 0.0958 0.0440 0.040 1.250 1.008 29.570 0.141 4.482 15.458 0.13 67347. 0.5372
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5.69 0.1772 0.3741 0.0933 0.0442 0.040 1.254 0.981 29.666 0.142 4.365 15.003 0.13 67426. 0.5145
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6.50 0.2025 0.4149 0.0906 0.0442 0.040 1.255 0.953 29.692 0.142 4.239 14.558 0.13 67510. 0.4920
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7.31 0.2278 0.4527 0.0877 0.0441 0.040 1.253 0.923 29.637 0.142 4.104 14.121 0.13 67599. 0.4695
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8.13 0.2531 0.4878 0.0846 0.0439 0.040 1.246 0.890 29.494 0.141 3.960 13.692 0.13 67694. 0.4472
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8.94 0.2784 0.5201 0.0813 0.0435 0.039 1.236 0.856 29.252 0.140 3.807 13.271 0.13 67794. 0.4250
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9.75 0.3038 0.5496 0.0779 0.0430 0.039 1.222 0.819 28.905 0.138 3.644 12.857 0.14 67900. 0.4029
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10.56 0.3291 0.5764 0.0742 0.0423 0.038 1.202 0.781 28.444 0.136 3.472 12.447 0.14 68011. 0.3807
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11.38 0.3544 0.6005 0.0703 0.0415 0.037 1.178 0.740 27.865 0.133 3.290 12.040 0.14 68129. 0.3584
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12.19 0.3797 0.6217 0.0662 0.0404 0.036 1.148 0.697 27.170 0.130 3.100 11.634 0.14 68252. 0.3362
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13.00 0.4050 0.6398 0.0620 0.0392 0.035 1.114 0.652 26.360 0.126 2.902 11.225 0.14 68381. 0.3138
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13.81 0.4303 0.6547 0.0576 0.0379 0.034 1.075 0.606 25.440 0.121 2.697 10.810 0.14 68515. 0.2914
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14.63 0.4556 0.6659 0.0531 0.0363 0.033 1.032 0.559 24.411 0.117 2.486 10.384 0.14 68656. 0.2687
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15.44 0.4809 0.6731 0.0485 0.0347 0.031 0.984 0.510 23.276 0.111 2.270 9.944 0.14 68802. 0.2459
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16.25 0.5063 0.6755 0.0438 0.0328 0.030 0.931 0.461 22.038 0.105 2.049 9.481 0.14 68954. 0.2228
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17.06 0.5316 0.6724 0.0390 0.0308 0.028 0.875 0.410 20.700 0.099 1.824 8.987 0.14 69112. 0.1993
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17.88 0.5569 0.6624 0.0341 0.0287 0.026 0.814 0.359 19.265 0.092 1.597 8.452 0.14 69276. 0.1753
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18.69 0.5822 0.6439 0.0292 0.0264 0.024 0.750 0.307 17.738 0.085 1.367 7.858 0.14 69445. 0.1508
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19.50 0.6075 0.6141 0.0243 0.0240 0.022 0.681 0.255 16.123 0.077 1.136 7.183 0.14 69621. 0.1256
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20.32 0.6328 0.5692 0.0193 0.0215 0.019 0.610 0.203 14.428 0.069 0.904 6.391 0.14 69802. 0.0997
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21.13 0.6581 0.5026 0.0144 0.0188 0.017 0.535 0.151 12.660 0.060 0.674 5.426 0.14 69989. 0.0731
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21.94 0.6834 0.4033 0.0095 0.0161 0.015 0.458 0.100 10.830 0.052 0.445 4.193 0.14 70182. 0.0459
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22.75 0.7088 0.2508 0.0047 0.0133 0.012 0.378 0.050 8.949 0.043 0.221 2.514 0.14 70381. 0.0194
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23.57 0.7341 0.0008 0.0000 0.0105 0.009 0.297 0.000 7.025 0.034 0.001 0.007 0.14 70582. 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 0.1079 0.0404 0.123 2.578 2.554 91.519 0.291 11.360 12.658 0.20 100464. 0.7002
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1.22 0.0254 0.0659 0.1063 0.0409 0.124 2.613 2.516 92.732 0.295 11.192 12.307 0.20 100540. 0.6758
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2.44 0.0508 0.1281 0.1045 0.0414 0.126 2.645 2.475 93.871 0.299 11.009 11.959 0.20 100622. 0.6513
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3.67 0.0761 0.1867 0.1027 0.0419 0.127 2.674 2.431 94.910 0.302 10.812 11.616 0.20 100711. 0.6269
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4.89 0.1015 0.2417 0.1006 0.0423 0.129 2.700 2.383 95.825 0.305 10.599 11.279 0.20 100807. 0.6027
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6.11 0.1269 0.2933 0.0985 0.0426 0.130 2.721 2.331 96.587 0.307 10.369 10.947 0.20 100910. 0.5786
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7.33 0.1523 0.3415 0.0961 0.0429 0.130 2.738 2.276 97.167 0.309 10.122 10.623 0.20 101021. 0.5547
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8.55 0.1776 0.3865 0.0936 0.0430 0.131 2.748 2.216 97.536 0.310 9.857 10.305 0.20 101139. 0.5310
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9.78 0.2030 0.4284 0.0909 0.0431 0.131 2.751 2.152 97.660 0.311 9.572 9.995 0.20 101266. 0.5075
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11.00 0.2284 0.4673 0.0880 0.0430 0.131 2.747 2.083 97.510 0.310 9.267 9.691 0.20 101400. 0.4842
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12.22 0.2538 0.5033 0.0849 0.0428 0.130 2.734 2.010 97.053 0.309 8.942 9.395 0.20 101543. 0.4611
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13.44 0.2792 0.5366 0.0816 0.0425 0.129 2.712 1.932 96.260 0.306 8.595 9.105 0.20 101694. 0.4382
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14.66 0.3045 0.5671 0.0781 0.0419 0.128 2.679 1.850 95.102 0.303 8.227 8.821 0.20 101854. 0.4153
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15.89 0.3299 0.5949 0.0744 0.0413 0.125 2.636 1.762 93.549 0.298 7.836 8.542 0.20 102022. 0.3925
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17.11 0.3553 0.6200 0.0705 0.0404 0.123 2.580 1.669 91.588 0.292 7.425 8.266 0.20 102199. 0.3697
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18.33 0.3807 0.6423 0.0664 0.0394 0.120 2.514 1.572 89.221 0.284 6.993 7.993 0.20 102384. 0.3469
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19.55 0.4060 0.6617 0.0621 0.0381 0.116 2.436 1.471 86.459 0.275 6.545 7.719 0.20 102579. 0.3241
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20.78 0.4314 0.6779 0.0577 0.0367 0.112 2.347 1.367 83.308 0.265 6.081 7.444 0.20 102782. 0.3013
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22.00 0.4568 0.6908 0.0532 0.0352 0.107 2.248 1.260 79.777 0.254 5.604 7.163 0.20 102993. 0.2783
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23.22 0.4822 0.6997 0.0486 0.0335 0.102 2.138 1.150 75.875 0.242 5.115 6.874 0.20 103214. 0.2552
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24.44 0.5076 0.7042 0.0438 0.0316 0.096 2.018 1.038 71.609 0.228 4.615 6.572 0.20 103443. 0.2318
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25.66 0.5329 0.7034 0.0390 0.0295 0.090 1.887 0.923 66.990 0.213 4.108 6.252 0.20 103681. 0.2080
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26.89 0.5583 0.6962 0.0341 0.0274 0.083 1.748 0.808 62.029 0.197 3.593 5.906 0.20 103927. 0.1838
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28.11 0.5837 0.6806 0.0292 0.0250 0.076 1.599 0.691 56.742 0.181 3.073 5.523 0.21 104183. 0.1589
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29.33 0.6091 0.6540 0.0242 0.0226 0.069 1.441 0.574 51.148 0.163 2.551 5.087 0.21 104447. 0.1334
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30.55 0.6344 0.6121 0.0193 0.0200 0.061 1.275 0.456 45.269 0.144 2.029 4.570 0.21 104721. 0.1069
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31.77 0.6598 0.5476 0.0143 0.0173 0.052 1.103 0.339 39.135 0.125 1.509 3.932 0.21 105003. 0.0793
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33.00 0.6852 0.4474 0.0094 0.0145 0.044 0.924 0.224 32.783 0.104 0.994 3.093 0.21 105294. 0.0506
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34.22 0.7106 0.2846 0.0046 0.0116 0.035 0.740 0.110 26.254 0.084 0.488 1.897 0.21 105594. 0.0218
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35.44 0.7360 -0.0061 -0.0001 0.0086 0.026 0.551 -0.002 19.565 0.062 -0.008 -0.039 0.21 105895. 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 0.1083 0.0397 0.286 4.511 4.559 213.461 0.510 20.280 9.688 0.27 133948. 0.7161
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1.65 0.0257 0.0681 0.1067 0.0403 0.290 4.574 4.491 216.447 0.517 19.978 9.412 0.27 134050. 0.6905
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3.30 0.0514 0.1322 0.1049 0.0408 0.294 4.633 4.418 219.252 0.523 19.649 9.139 0.27 134162. 0.6649
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4.95 0.0771 0.1924 0.1031 0.0413 0.297 4.687 4.338 221.813 0.530 19.293 8.870 0.27 134282. 0.6395
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6.60 0.1028 0.2489 0.1010 0.0417 0.300 4.735 4.251 224.068 0.535 18.909 8.605 0.27 134412. 0.6142
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8.25 0.1285 0.3018 0.0988 0.0420 0.303 4.774 4.158 225.946 0.539 18.494 8.347 0.27 134552. 0.5891
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9.90 0.1542 0.3512 0.0964 0.0423 0.305 4.805 4.057 227.376 0.543 18.047 8.093 0.27 134703. 0.5643
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11.55 0.1799 0.3972 0.0938 0.0425 0.306 4.824 3.949 228.280 0.545 17.566 7.847 0.27 134864. 0.5398
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13.20 0.2056 0.4401 0.0911 0.0425 0.307 4.830 3.833 228.580 0.546 17.049 7.606 0.27 135035. 0.5155
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14.85 0.2312 0.4798 0.0881 0.0425 0.306 4.822 3.709 228.196 0.545 16.496 7.371 0.27 135218. 0.4914
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16.50 0.2569 0.5166 0.0849 0.0423 0.304 4.798 3.576 227.051 0.542 15.904 7.143 0.27 135413. 0.4675
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18.15 0.2826 0.5505 0.0816 0.0419 0.302 4.756 3.434 225.071 0.537 15.273 6.920 0.27 135618. 0.4439
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19.80 0.3083 0.5817 0.0780 0.0413 0.298 4.695 3.283 222.181 0.530 14.603 6.702 0.27 135836. 0.4204
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21.45 0.3340 0.6101 0.0742 0.0406 0.293 4.613 3.123 218.310 0.521 13.891 6.489 0.27 136065. 0.3969
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23.10 0.3597 0.6357 0.0702 0.0397 0.286 4.510 2.954 213.429 0.510 13.141 6.279 0.27 136306. 0.3736
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24.75 0.3854 0.6586 0.0660 0.0386 0.278 4.386 2.778 207.549 0.495 12.356 6.071 0.27 136559. 0.3503
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26.40 0.4111 0.6785 0.0616 0.0373 0.269 4.241 2.595 200.689 0.479 11.540 5.864 0.27 136823. 0.3270
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28.05 0.4368 0.6954 0.0571 0.0359 0.259 4.075 2.405 192.869 0.460 10.697 5.656 0.27 137100. 0.3036
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29.69 0.4625 0.7088 0.0525 0.0343 0.247 3.890 2.210 184.108 0.440 9.830 5.444 0.27 137388. 0.2802
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31.34 0.4882 0.7183 0.0478 0.0325 0.234 3.686 2.010 174.425 0.416 8.941 5.227 0.27 137689. 0.2565
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32.99 0.5139 0.7233 0.0429 0.0305 0.220 3.462 1.806 163.842 0.391 8.035 5.001 0.27 138001. 0.2327
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34.64 0.5396 0.7230 0.0380 0.0284 0.204 3.220 1.599 152.385 0.364 7.114 4.760 0.27 138325. 0.2084
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36.29 0.5653 0.7159 0.0330 0.0261 0.188 2.960 1.390 140.084 0.334 6.181 4.499 0.27 138662. 0.1836
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37.94 0.5910 0.7001 0.0280 0.0236 0.170 2.683 1.178 126.979 0.303 5.241 4.209 0.27 139010. 0.1581
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39.59 0.6167 0.6723 0.0230 0.0211 0.152 2.390 0.966 113.120 0.270 4.297 3.873 0.27 139371. 0.1318
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41.24 0.6424 0.6274 0.0179 0.0183 0.132 2.083 0.754 98.571 0.235 3.354 3.470 0.27 139744. 0.1043
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42.89 0.6680 0.5557 0.0129 0.0155 0.112 1.763 0.543 83.411 0.199 2.417 2.955 0.27 140128. 0.0754
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44.54 0.6937 0.4389 0.0080 0.0126 0.091 1.431 0.336 67.737 0.162 1.493 2.247 0.28 140525. 0.0451
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46.19 0.7194 0.2344 0.0031 0.0096 0.069 1.092 0.132 51.659 0.123 0.586 1.158 0.28 140933. 0.0146
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47.84 0.7451
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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 0.1089 0.0394 0.555 6.993 7.161 413.693 0.790 31.850 7.851 0.34 167427. 0.7272
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2.04 0.0254 0.0682 0.1073 0.0400 0.563 7.093 7.056 419.583 0.801 31.384 7.627 0.34 167554. 0.7013
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4.08 0.0508 0.1325 0.1056 0.0405 0.570 7.187 6.942 425.128 0.812 30.877 7.406 0.34 167692. 0.6755
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6.12 0.0763 0.1929 0.1037 0.0410 0.577 7.272 6.819 430.209 0.822 30.329 7.189 0.34 167841. 0.6498
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8.16 0.1017 0.2495 0.1017 0.0414 0.583 7.348 6.685 434.701 0.830 29.737 6.976 0.34 168002. 0.6244
|
|
10.20 0.1271 0.3026 0.0995 0.0418 0.588 7.412 6.542 438.474 0.837 29.098 6.767 0.34 168175. 0.5991
|
|
12.24 0.1525 0.3522 0.0971 0.0421 0.592 7.461 6.387 441.388 0.843 28.409 6.563 0.34 168360. 0.5742
|
|
14.28 0.1779 0.3984 0.0946 0.0422 0.594 7.494 6.220 443.297 0.847 27.667 6.364 0.34 168559. 0.5495
|
|
16.32 0.2033 0.4415 0.0919 0.0423 0.595 7.506 6.041 444.050 0.848 26.872 6.171 0.34 168770. 0.5250
|
|
18.36 0.2288 0.4815 0.0889 0.0423 0.595 7.497 5.850 443.494 0.847 26.019 5.983 0.34 168996. 0.5009
|
|
20.40 0.2542 0.5186 0.0858 0.0421 0.592 7.463 5.645 441.481 0.843 25.108 5.799 0.34 169235. 0.4770
|
|
22.44 0.2796 0.5530 0.0825 0.0417 0.587 7.402 5.426 437.865 0.836 24.137 5.621 0.34 169488. 0.4533
|
|
24.48 0.3050 0.5846 0.0790 0.0412 0.580 7.311 5.194 432.505 0.826 23.104 5.447 0.34 169755. 0.4297
|
|
26.52 0.3304 0.6135 0.0752 0.0405 0.570 7.189 4.948 425.259 0.812 22.008 5.277 0.34 170037. 0.4063
|
|
28.56 0.3558 0.6398 0.0713 0.0396 0.558 7.033 4.688 416.054 0.795 20.851 5.110 0.34 170333. 0.3830
|
|
30.60 0.3813 0.6635 0.0671 0.0386 0.543 6.845 4.415 404.901 0.773 19.639 4.946 0.34 170644. 0.3598
|
|
32.64 0.4067 0.6844 0.0628 0.0373 0.525 6.624 4.132 391.835 0.748 18.379 4.783 0.34 170969. 0.3366
|
|
34.68 0.4321 0.7024 0.0584 0.0359 0.505 6.371 3.839 376.892 0.720 17.076 4.620 0.34 171309. 0.3134
|
|
36.72 0.4575 0.7172 0.0538 0.0343 0.483 6.087 3.537 360.107 0.688 15.734 4.455 0.34 171663. 0.2901
|
|
38.76 0.4829 0.7285 0.0491 0.0325 0.458 5.773 3.228 341.517 0.652 14.359 4.287 0.34 172032. 0.2667
|
|
40.80 0.5084 0.7357 0.0443 0.0306 0.431 5.429 2.913 321.161 0.613 12.955 4.113 0.34 172415. 0.2430
|
|
42.84 0.5338 0.7381 0.0394 0.0285 0.401 5.056 2.592 299.084 0.571 11.527 3.930 0.34 172813. 0.2190
|
|
44.88 0.5592 0.7345 0.0345 0.0262 0.369 4.655 2.266 275.345 0.526 10.081 3.733 0.34 173226. 0.1946
|
|
46.92 0.5846 0.7233 0.0295 0.0238 0.335 4.226 1.938 250.014 0.477 8.622 3.516 0.34 173653. 0.1695
|
|
48.96 0.6100 0.7016 0.0245 0.0213 0.299 3.773 1.609 223.184 0.426 7.155 3.269 0.34 174095. 0.1435
|
|
51.00 0.6354 0.6651 0.0194 0.0186 0.261 3.296 1.279 194.969 0.372 5.688 2.975 0.34 174552. 0.1164
|
|
53.04 0.6609 0.6057 0.0145 0.0158 0.222 2.798 0.951 165.514 0.316 4.228 2.605 0.34 175024. 0.0879
|
|
55.08 0.6863 0.5078 0.0095 0.0129 0.181 2.282 0.626 135.000 0.258 2.784 2.103 0.34 175511. 0.0576
|
|
57.12 0.7117 0.3366 0.0047 0.0099 0.139 1.752 0.307 103.636 0.198 1.366 1.344 0.34 176011. 0.0258
|
|
59.16 0.7371 -0.0098 -0.0001 0.0068 0.096 1.208 -0.006 71.433 0.136 -0.026 -0.038 0.35 176509. 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 0.1096 0.0393 0.957 10.050 10.375 713.390 1.135 46.149 6.597 0.40 200902. 0.7355
|
|
2.45 0.0254 0.0688 0.1080 0.0399 0.971 10.196 10.225 723.765 1.152 45.479 6.408 0.40 201055. 0.7093
|
|
4.90 0.0508 0.1335 0.1062 0.0404 0.984 10.333 10.061 733.537 1.167 44.752 6.221 0.40 201220. 0.6831
|
|
7.34 0.0762 0.1944 0.1044 0.0409 0.996 10.460 9.884 742.496 1.182 43.964 6.038 0.40 201399. 0.6571
|
|
9.79 0.1017 0.2514 0.1023 0.0414 1.006 10.571 9.692 750.429 1.194 43.111 5.858 0.40 201593. 0.6313
|
|
12.24 0.1271 0.3049 0.1002 0.0417 1.015 10.665 9.485 757.102 1.205 42.190 5.682 0.40 201801. 0.6058
|
|
14.69 0.1525 0.3548 0.0978 0.0420 1.022 10.738 9.262 762.274 1.213 41.196 5.511 0.40 202024. 0.5806
|
|
17.13 0.1779 0.4014 0.0953 0.0422 1.027 10.786 9.021 765.686 1.219 40.127 5.344 0.40 202262. 0.5556
|
|
19.58 0.2033 0.4448 0.0925 0.0423 1.029 10.806 8.763 767.075 1.221 38.977 5.181 0.40 202517. 0.5310
|
|
22.03 0.2287 0.4852 0.0896 0.0422 1.027 10.793 8.486 766.172 1.219 37.746 5.024 0.40 202788. 0.5066
|
|
24.48 0.2542 0.5226 0.0865 0.0421 1.023 10.744 8.190 762.716 1.214 36.428 4.870 0.40 203075. 0.4825
|
|
26.93 0.2796 0.5573 0.0831 0.0417 1.014 10.656 7.874 756.451 1.204 35.023 4.721 0.41 203379. 0.4586
|
|
29.37 0.3050 0.5893 0.0796 0.0412 1.002 10.525 7.538 747.131 1.189 33.528 4.576 0.41 203701. 0.4349
|
|
31.82 0.3304 0.6186 0.0758 0.0405 0.985 10.347 7.181 734.506 1.169 31.941 4.434 0.41 204040. 0.4114
|
|
34.27 0.3558 0.6454 0.0718 0.0396 0.963 10.121 6.804 718.440 1.143 30.266 4.296 0.41 204395. 0.3879
|
|
36.72 0.3812 0.6695 0.0677 0.0385 0.937 9.846 6.410 698.949 1.112 28.510 4.159 0.41 204769. 0.3645
|
|
39.16 0.4066 0.6910 0.0633 0.0373 0.907 9.524 5.999 676.092 1.076 26.683 4.025 0.41 205159. 0.3412
|
|
41.61 0.4321 0.7096 0.0589 0.0358 0.872 9.156 5.574 649.932 1.034 24.793 3.890 0.41 205567. 0.3179
|
|
44.06 0.4575 0.7252 0.0542 0.0342 0.832 8.741 5.137 620.528 0.988 22.847 3.754 0.41 205993. 0.2946
|
|
46.51 0.4829 0.7374 0.0495 0.0324 0.788 8.282 4.688 587.945 0.936 20.852 3.617 0.41 206435. 0.2711
|
|
48.95 0.5083 0.7456 0.0447 0.0304 0.741 7.780 4.230 552.249 0.879 18.816 3.474 0.41 206896. 0.2474
|
|
51.40 0.5337 0.7493 0.0397 0.0283 0.689 7.234 3.764 513.523 0.817 16.744 3.325 0.41 207374. 0.2233
|
|
53.85 0.5591 0.7471 0.0348 0.0260 0.633 6.647 3.292 471.866 0.751 14.645 3.165 0.41 207869. 0.1988
|
|
56.30 0.5846 0.7376 0.0297 0.0236 0.573 6.021 2.816 427.404 0.680 12.526 2.989 0.41 208382. 0.1736
|
|
58.75 0.6100 0.7180 0.0247 0.0210 0.510 5.357 2.338 380.297 0.605 10.397 2.788 0.41 208913. 0.1476
|
|
61.19 0.6354 0.6838 0.0196 0.0182 0.444 4.659 1.859 330.749 0.526 8.268 2.549 0.41 209462. 0.1203
|
|
63.64 0.6608 0.6270 0.0146 0.0154 0.374 3.931 1.382 279.016 0.444 6.149 2.247 0.41 210028. 0.0915
|
|
66.09 0.6862 0.5312 0.0096 0.0124 0.302 3.175 0.911 225.417 0.359 4.053 1.834 0.41 210612. 0.0606
|
|
68.54 0.7116 0.3588 0.0047 0.0094 0.228 2.399 0.448 170.323 0.271 1.995 1.194 0.41 211212. 0.0277
|
|
70.98 0.7371 -0.0078 -0.0001 0.0063 0.153 1.602 -0.006 113.722 0.181 -0.028 -0.025 0.41 211808. 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 0.1104 0.0394 1.523 13.712 14.227 1135.597 1.549 63.280 5.682 0.47 234370. 0.7419
|
|
2.89 0.0257 0.0698 0.1088 0.0400 1.546 13.917 14.020 1152.567 1.572 62.362 5.517 0.47 234550. 0.7151
|
|
5.77 0.0514 0.1355 0.1070 0.0406 1.567 14.110 13.796 1168.542 1.594 61.362 5.355 0.47 234747. 0.6885
|
|
8.66 0.0771 0.1972 0.1051 0.0411 1.587 14.286 13.552 1183.174 1.614 60.278 5.195 0.47 234959. 0.6620
|
|
11.54 0.1027 0.2550 0.1031 0.0415 1.604 14.442 13.287 1196.102 1.632 59.101 5.039 0.47 235188. 0.6358
|
|
14.43 0.1284 0.3091 0.1009 0.0419 1.619 14.573 13.001 1206.939 1.646 57.828 4.886 0.47 235435. 0.6098
|
|
17.32 0.1541 0.3596 0.0985 0.0422 1.630 14.674 12.692 1215.278 1.658 56.453 4.737 0.47 235699. 0.5842
|
|
20.20 0.1798 0.4067 0.0959 0.0424 1.637 14.739 12.359 1220.690 1.665 54.971 4.592 0.47 235982. 0.5588
|
|
23.09 0.2055 0.4506 0.0931 0.0425 1.640 14.764 12.000 1222.734 1.668 53.376 4.451 0.47 236285. 0.5338
|
|
25.97 0.2312 0.4913 0.0901 0.0424 1.637 14.743 11.615 1220.964 1.666 51.663 4.315 0.47 236607. 0.5090
|
|
28.86 0.2569 0.5292 0.0869 0.0422 1.629 14.670 11.203 1214.945 1.657 49.830 4.182 0.47 236949. 0.4846
|
|
31.75 0.2825 0.5642 0.0835 0.0418 1.615 14.541 10.763 1204.254 1.643 47.872 4.054 0.47 237311. 0.4603
|
|
34.63 0.3082 0.5965 0.0799 0.0413 1.594 14.350 10.294 1188.477 1.621 45.787 3.929 0.47 237693. 0.4363
|
|
37.52 0.3339 0.6261 0.0760 0.0405 1.565 14.094 9.796 1167.209 1.592 43.572 3.807 0.47 238096. 0.4124
|
|
40.41 0.3596 0.6532 0.0719 0.0396 1.529 13.768 9.270 1140.253 1.556 41.233 3.687 0.47 238519. 0.3886
|
|
43.29 0.3853 0.6776 0.0676 0.0385 1.485 13.374 8.719 1107.647 1.511 38.783 3.570 0.47 238963. 0.3650
|
|
46.18 0.4110 0.6994 0.0632 0.0371 1.434 12.914 8.146 1069.490 1.459 36.233 3.455 0.47 239428. 0.3413
|
|
49.06 0.4367 0.7183 0.0586 0.0356 1.376 12.387 7.553 1025.890 1.400 33.596 3.339 0.48 239913. 0.3177
|
|
51.95 0.4623 0.7341 0.0539 0.0339 1.310 11.796 6.943 976.945 1.333 30.881 3.223 0.48 240419. 0.2940
|
|
54.84 0.4880 0.7465 0.0490 0.0320 1.237 11.142 6.317 922.760 1.259 28.099 3.105 0.48 240946. 0.2702
|
|
57.72 0.5137 0.7549 0.0441 0.0300 1.158 10.426 5.679 863.456 1.178 25.259 2.983 0.48 241493. 0.2461
|
|
60.61 0.5394 0.7585 0.0390 0.0277 1.072 9.650 5.030 799.171 1.090 22.372 2.855 0.48 242062. 0.2216
|
|
63.49 0.5651 0.7561 0.0339 0.0253 0.979 8.815 4.372 730.080 0.996 19.448 2.716 0.48 242651. 0.1966
|
|
66.38 0.5908 0.7459 0.0288 0.0228 0.880 7.926 3.710 656.407 0.895 16.500 2.563 0.48 243261. 0.1709
|
|
69.27 0.6165 0.7248 0.0236 0.0201 0.776 6.984 3.044 578.434 0.789 13.540 2.387 0.48 243893. 0.1442
|
|
72.15 0.6422 0.6874 0.0185 0.0172 0.666 5.995 2.379 496.524 0.677 10.582 2.173 0.48 244545. 0.1160
|
|
75.04 0.6678 0.6236 0.0133 0.0143 0.551 4.964 1.718 411.134 0.561 7.643 1.896 0.48 245219. 0.0860
|
|
77.92 0.6935 0.5118 0.0083 0.0112 0.433 3.898 1.066 322.826 0.440 4.743 1.498 0.48 245913. 0.0535
|
|
80.81 0.7192 0.2955 0.0033 0.0081 0.311 2.804 0.427 232.229 0.317 1.900 0.834 0.48 246626. 0.0189
|
|
83.70 0.7449
|
|
|
|
|
|
|
|
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 0.1113 0.0397 2.288 18.024 18.744 1705.960 2.036 83.375 4.984 0.54 267830. 0.7469
|
|
3.26 0.0254 0.0692 0.1098 0.0403 2.322 18.294 18.480 1731.528 2.067 82.197 4.841 0.54 268034. 0.7203
|
|
6.52 0.0508 0.1343 0.1080 0.0408 2.354 18.549 18.191 1755.628 2.096 80.914 4.700 0.54 268256. 0.6939
|
|
9.78 0.0761 0.1955 0.1062 0.0414 2.384 18.782 17.878 1777.743 2.122 79.521 4.561 0.54 268496. 0.6676
|
|
13.04 0.1015 0.2529 0.1042 0.0418 2.410 18.989 17.538 1797.344 2.145 78.009 4.426 0.54 268754. 0.6416
|
|
16.30 0.1269 0.3067 0.1020 0.0422 2.432 19.164 17.170 1813.868 2.165 76.373 4.294 0.54 269033. 0.6159
|
|
19.55 0.1523 0.3570 0.0996 0.0425 2.450 19.300 16.772 1826.718 2.180 74.604 4.165 0.54 269331. 0.5904
|
|
22.81 0.1777 0.4040 0.0971 0.0427 2.461 19.390 16.344 1835.265 2.191 72.696 4.039 0.54 269650. 0.5653
|
|
26.07 0.2030 0.4478 0.0943 0.0428 2.466 19.428 15.882 1838.863 2.195 70.643 3.917 0.54 269991. 0.5404
|
|
29.33 0.2284 0.4885 0.0914 0.0427 2.463 19.407 15.386 1836.860 2.193 68.437 3.799 0.54 270353. 0.5159
|
|
32.59 0.2538 0.5264 0.0882 0.0425 2.452 19.320 14.855 1828.614 2.183 66.075 3.685 0.54 270738. 0.4916
|
|
35.85 0.2792 0.5616 0.0849 0.0422 2.432 19.160 14.288 1813.503 2.165 63.552 3.573 0.54 271145. 0.4676
|
|
39.11 0.3046 0.5942 0.0813 0.0417 2.402 18.922 13.684 1790.925 2.138 60.864 3.465 0.54 271574. 0.4438
|
|
42.37 0.3299 0.6241 0.0775 0.0409 2.361 18.598 13.041 1760.273 2.101 58.008 3.360 0.54 272027. 0.4201
|
|
45.63 0.3553 0.6516 0.0734 0.0400 2.308 18.185 12.362 1721.181 2.055 54.988 3.258 0.54 272502. 0.3965
|
|
48.89 0.3807 0.6766 0.0692 0.0389 2.244 17.683 11.650 1673.656 1.998 51.819 3.157 0.54 273001. 0.3730
|
|
52.14 0.4061 0.6991 0.0648 0.0376 2.170 17.093 10.908 1617.843 1.931 48.518 3.058 0.54 273522. 0.3496
|
|
55.40 0.4315 0.7188 0.0602 0.0361 2.084 16.417 10.139 1553.897 1.855 45.100 2.960 0.54 274066. 0.3262
|
|
58.66 0.4568 0.7357 0.0555 0.0345 1.987 15.657 9.347 1481.971 1.769 41.577 2.861 0.54 274634. 0.3028
|
|
61.92 0.4822 0.7495 0.0507 0.0326 1.880 14.815 8.535 1402.216 1.674 37.964 2.761 0.54 275224. 0.2792
|
|
65.18 0.5076 0.7595 0.0458 0.0306 1.763 13.891 7.705 1314.803 1.569 34.273 2.658 0.54 275838. 0.2554
|
|
68.44 0.5330 0.7653 0.0407 0.0284 1.636 12.889 6.861 1219.927 1.456 30.516 2.551 0.55 276474. 0.2313
|
|
71.70 0.5583 0.7658 0.0357 0.0260 1.499 11.810 6.004 1117.836 1.334 26.708 2.436 0.55 277134. 0.2067
|
|
74.96 0.5837 0.7594 0.0305 0.0235 1.353 10.659 5.140 1008.834 1.204 22.862 2.311 0.55 277818. 0.1814
|
|
78.22 0.6091 0.7435 0.0254 0.0208 1.198 9.438 4.271 893.313 1.066 18.996 2.168 0.55 278524. 0.1551
|
|
81.48 0.6345 0.7139 0.0202 0.0180 1.035 8.154 3.401 771.773 0.921 15.127 1.999 0.55 279255. 0.1276
|
|
84.73 0.6599 0.6623 0.0151 0.0150 0.865 6.813 2.535 644.844 0.770 11.275 1.783 0.55 280008. 0.0983
|
|
87.99 0.6852 0.5720 0.0100 0.0119 0.688 5.423 1.678 513.309 0.613 7.464 1.483 0.55 280785. 0.0665
|
|
91.25 0.7106 0.4013 0.0050 0.0088 0.507 3.995 0.836 378.096 0.451 3.719 1.003 0.55 281584. 0.0318
|
|
94.51 0.7360 0.0071 0.0001 0.0056 0.321 2.527 0.009 239.199 0.286 0.040 0.017 0.55 282377. 0.0001
|
|
|
|
|
|
|
|
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 0.1125 0.0401 3.291 23.044 23.967 2453.771 2.604 106.604 4.430 0.61 301279. 0.7508
|
|
3.67 0.0254 0.0692 0.1109 0.0407 3.341 23.395 23.634 2491.065 2.643 105.124 4.303 0.61 301509. 0.7242
|
|
7.34 0.0508 0.1344 0.1092 0.0413 3.388 23.725 23.271 2526.222 2.680 103.509 4.178 0.61 301760. 0.6977
|
|
11.00 0.0762 0.1956 0.1074 0.0418 3.431 24.028 22.876 2558.485 2.715 101.751 4.055 0.61 302031. 0.6714
|
|
14.67 0.1016 0.2531 0.1053 0.0423 3.469 24.296 22.446 2587.081 2.745 99.840 3.935 0.61 302323. 0.6454
|
|
18.34 0.1269 0.3070 0.1032 0.0427 3.502 24.523 21.980 2611.182 2.771 97.768 3.818 0.61 302638. 0.6196
|
|
22.01 0.1523 0.3573 0.1008 0.0430 3.527 24.699 21.476 2629.920 2.790 95.525 3.704 0.61 302975. 0.5942
|
|
25.67 0.1777 0.4044 0.0982 0.0432 3.543 24.816 20.931 2642.378 2.804 93.101 3.593 0.61 303336. 0.5690
|
|
29.34 0.2031 0.4483 0.0955 0.0433 3.551 24.865 20.344 2647.618 2.809 90.489 3.485 0.61 303720. 0.5442
|
|
33.01 0.2285 0.4892 0.0925 0.0432 3.547 24.837 19.712 2644.691 2.806 87.681 3.381 0.61 304130. 0.5196
|
|
36.68 0.2539 0.5273 0.0893 0.0430 3.530 24.724 19.035 2632.659 2.793 84.669 3.280 0.61 304564. 0.4953
|
|
40.35 0.2793 0.5627 0.0859 0.0426 3.501 24.517 18.311 2610.629 2.770 81.449 3.181 0.61 305024. 0.4713
|
|
44.01 0.3047 0.5955 0.0823 0.0421 3.457 24.208 17.539 2577.720 2.735 78.015 3.086 0.61 305509. 0.4474
|
|
47.68 0.3301 0.6258 0.0785 0.0414 3.397 23.789 16.718 2533.060 2.688 74.363 2.994 0.61 306020. 0.4237
|
|
51.35 0.3554 0.6536 0.0744 0.0405 3.320 23.254 15.849 2476.090 2.627 70.498 2.903 0.61 306556. 0.4001
|
|
55.02 0.3808 0.6789 0.0701 0.0393 3.228 22.603 14.937 2406.817 2.554 66.440 2.815 0.61 307119. 0.3766
|
|
58.68 0.4062 0.7018 0.0656 0.0380 3.118 21.839 13.986 2325.449 2.467 62.209 2.728 0.61 307707. 0.3531
|
|
62.35 0.4316 0.7221 0.0610 0.0365 2.993 20.964 13.000 2232.221 2.368 57.825 2.642 0.61 308321. 0.3297
|
|
66.02 0.4570 0.7395 0.0562 0.0348 2.853 19.979 11.984 2127.357 2.257 53.306 2.555 0.61 308961. 0.3062
|
|
69.69 0.4824 0.7539 0.0513 0.0329 2.697 18.887 10.942 2011.086 2.134 48.668 2.468 0.61 309627. 0.2826
|
|
73.36 0.5078 0.7648 0.0463 0.0308 2.526 17.690 9.876 1883.658 1.999 43.928 2.378 0.61 310318. 0.2587
|
|
77.02 0.5332 0.7714 0.0413 0.0285 2.341 16.391 8.791 1745.366 1.852 39.103 2.285 0.61 311036. 0.2345
|
|
80.69 0.5586 0.7729 0.0361 0.0261 2.141 14.994 7.691 1596.565 1.694 34.210 2.185 0.61 311780. 0.2098
|
|
84.36 0.5839 0.7677 0.0309 0.0235 1.928 13.502 6.580 1437.708 1.525 29.267 2.076 0.62 312550. 0.1843
|
|
88.03 0.6093 0.7532 0.0256 0.0207 1.702 11.921 5.462 1269.368 1.347 24.296 1.952 0.62 313346. 0.1579
|
|
91.69 0.6347 0.7251 0.0204 0.0178 1.465 10.258 4.344 1092.275 1.159 19.321 1.804 0.62 314169. 0.1301
|
|
95.36 0.6601 0.6750 0.0152 0.0148 1.217 8.521 3.230 907.355 0.963 14.367 1.615 0.62 315017. 0.1005
|
|
99.03 0.6855 0.5855 0.0100 0.0117 0.960 6.722 2.128 715.762 0.759 9.466 1.349 0.62 315892. 0.0681
|
|
102.70 0.7109 0.4115 0.0049 0.0085 0.696 4.873 1.045 518.858 0.551 4.650 0.914 0.62 316792. 0.0323
|
|
106.37 0.7363 -0.0140 -0.0001 0.0052 0.424 2.969 -0.021 316.180 0.335 -0.093 -0.030 0.62 317674. 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 0.1138 0.0407 4.578 28.855 29.942 3413.945 3.260 133.183 3.978 0.67 334715. 0.7535
|
|
4.07 0.0254 0.0690 0.1123 0.0413 4.649 29.299 29.536 3466.450 3.310 131.377 3.865 0.67 334972. 0.7271
|
|
8.15 0.0507 0.1340 0.1106 0.0419 4.715 29.718 29.092 3515.979 3.358 129.401 3.753 0.67 335251. 0.7007
|
|
12.22 0.0761 0.1951 0.1087 0.0424 4.776 30.102 28.607 3561.439 3.401 127.245 3.643 0.67 335553. 0.6746
|
|
16.29 0.1015 0.2525 0.1067 0.0429 4.830 30.443 28.079 3601.737 3.439 124.897 3.536 0.67 335879. 0.6486
|
|
20.36 0.1269 0.3063 0.1046 0.0433 4.876 30.730 27.505 3635.708 3.472 122.344 3.431 0.67 336230. 0.6230
|
|
24.44 0.1522 0.3567 0.1022 0.0436 4.911 30.953 26.883 3662.113 3.497 119.574 3.330 0.67 336605. 0.5976
|
|
28.51 0.1776 0.4038 0.0996 0.0438 4.935 31.102 26.209 3679.677 3.514 116.577 3.231 0.67 337008. 0.5725
|
|
32.58 0.2030 0.4477 0.0969 0.0439 4.944 31.164 25.481 3687.078 3.521 113.340 3.135 0.67 337437. 0.5477
|
|
36.65 0.2284 0.4888 0.0939 0.0439 4.939 31.130 24.698 3682.990 3.517 109.855 3.042 0.67 337893. 0.5233
|
|
40.73 0.2537 0.5270 0.0907 0.0437 4.916 30.987 23.856 3666.101 3.501 106.113 2.951 0.67 338377. 0.4990
|
|
44.80 0.2791 0.5625 0.0873 0.0433 4.875 30.725 22.955 3635.156 3.471 102.106 2.864 0.67 338889. 0.4750
|
|
48.87 0.3045 0.5955 0.0836 0.0427 4.813 30.335 21.994 3588.938 3.427 97.828 2.780 0.68 339430. 0.4512
|
|
52.94 0.3298 0.6261 0.0797 0.0420 4.729 29.805 20.970 3526.232 3.367 93.275 2.697 0.68 339999. 0.4276
|
|
57.02 0.3552 0.6542 0.0756 0.0410 4.621 29.128 19.885 3446.215 3.291 88.450 2.617 0.68 340596. 0.4040
|
|
61.09 0.3806 0.6799 0.0713 0.0399 4.491 28.305 18.745 3348.864 3.198 83.378 2.539 0.68 341222. 0.3805
|
|
65.16 0.4060 0.7033 0.0667 0.0385 4.338 27.339 17.555 3234.483 3.089 78.086 2.462 0.68 341877. 0.3571
|
|
69.24 0.4313 0.7240 0.0620 0.0370 4.162 26.231 16.321 3103.412 2.964 72.598 2.385 0.68 342561. 0.3336
|
|
73.31 0.4567 0.7421 0.0572 0.0352 3.964 24.985 15.049 2955.976 2.823 66.936 2.309 0.68 343272. 0.3101
|
|
77.38 0.4821 0.7572 0.0522 0.0333 3.745 23.603 13.742 2792.513 2.667 61.123 2.232 0.68 344013. 0.2864
|
|
81.45 0.5075 0.7688 0.0472 0.0311 3.505 22.089 12.405 2613.374 2.496 55.179 2.153 0.68 344782. 0.2625
|
|
85.53 0.5328 0.7764 0.0420 0.0288 3.244 20.446 11.044 2418.982 2.310 49.124 2.071 0.68 345580. 0.2382
|
|
89.60 0.5582 0.7791 0.0367 0.0263 2.963 18.678 9.663 2209.831 2.110 42.981 1.983 0.68 346407. 0.2134
|
|
93.67 0.5836 0.7752 0.0314 0.0237 2.664 16.791 8.268 1986.561 1.897 36.774 1.888 0.68 347262. 0.1879
|
|
97.74 0.6089 0.7623 0.0261 0.0208 2.347 14.791 6.863 1749.976 1.671 30.529 1.779 0.68 348147. 0.1613
|
|
101.82 0.6343 0.7360 0.0207 0.0179 2.013 12.688 5.457 1501.113 1.433 24.274 1.649 0.69 349060. 0.1334
|
|
105.89 0.6597 0.6882 0.0154 0.0148 1.665 10.492 4.057 1241.308 1.185 18.045 1.482 0.69 350002. 0.1034
|
|
109.96 0.6851 0.6006 0.0102 0.0116 1.304 8.218 2.671 972.250 0.928 11.880 1.246 0.69 350974. 0.0705
|
|
114.03 0.7104 0.4263 0.0050 0.0083 0.933 5.882 1.308 695.968 0.665 5.820 0.853 0.69 351972. 0.0338
|
|
118.11 0.7358 -0.0200 -0.0001 0.0049 0.552 3.479 -0.035 411.657 0.393 -0.156 -0.039 0.69 352947. 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 0.1154 0.0417 6.244 35.776 36.731 4656.046 4.042 163.378 3.578 0.74 368134. 0.7507
|
|
4.51 0.0255 0.0688 0.1139 0.0423 6.335 36.296 36.245 4723.693 4.101 161.216 3.480 0.74 368420. 0.7253
|
|
9.02 0.0511 0.1338 0.1122 0.0428 6.420 36.788 35.710 4787.655 4.156 158.840 3.383 0.74 368731. 0.6998
|
|
13.53 0.0766 0.1950 0.1103 0.0434 6.499 37.240 35.125 4846.478 4.207 156.237 3.287 0.74 369067. 0.6744
|
|
18.04 0.1022 0.2525 0.1083 0.0438 6.569 37.641 34.485 4898.658 4.253 153.390 3.193 0.74 369430. 0.6491
|
|
22.55 0.1277 0.3065 0.1061 0.0442 6.628 37.978 33.787 4942.559 4.291 150.284 3.101 0.74 369821. 0.6239
|
|
27.06 0.1533 0.3571 0.1038 0.0445 6.674 38.238 33.027 4976.447 4.320 146.903 3.010 0.74 370241. 0.5988
|
|
31.57 0.1788 0.4044 0.1012 0.0447 6.703 38.408 32.201 4998.471 4.339 143.232 2.922 0.74 370690. 0.5740
|
|
36.08 0.2043 0.4486 0.0984 0.0448 6.714 38.471 31.308 5006.726 4.346 139.257 2.836 0.74 371169. 0.5494
|
|
40.59 0.2299 0.4899 0.0953 0.0447 6.704 38.414 30.343 4999.269 4.340 134.965 2.753 0.74 371678. 0.5249
|
|
45.10 0.2554 0.5283 0.0921 0.0445 6.670 38.221 29.305 4974.183 4.318 130.347 2.672 0.74 372219. 0.5007
|
|
49.61 0.2810 0.5641 0.0886 0.0441 6.611 37.878 28.191 4929.617 4.279 125.393 2.594 0.74 372791. 0.4767
|
|
54.12 0.3065 0.5974 0.0848 0.0435 6.522 37.373 27.000 4863.795 4.222 120.095 2.518 0.74 373395. 0.4529
|
|
58.63 0.3321 0.6282 0.0808 0.0427 6.403 36.690 25.730 4774.985 4.145 114.447 2.444 0.74 374030. 0.4292
|
|
63.14 0.3576 0.6566 0.0766 0.0417 6.252 35.823 24.383 4662.066 4.047 108.456 2.372 0.74 374697. 0.4055
|
|
67.65 0.3831 0.6827 0.0721 0.0405 6.068 34.770 22.966 4525.050 3.928 102.152 2.302 0.75 375396. 0.3819
|
|
72.16 0.4087 0.7064 0.0675 0.0391 5.853 33.535 21.486 4364.378 3.789 95.570 2.233 0.75 376127. 0.3583
|
|
76.67 0.4342 0.7275 0.0627 0.0374 5.606 32.123 19.951 4180.546 3.629 88.740 2.165 0.75 376890. 0.3347
|
|
81.18 0.4598 0.7460 0.0577 0.0356 5.329 30.536 18.366 3974.046 3.450 81.692 2.096 0.75 377684. 0.3110
|
|
85.69 0.4853 0.7615 0.0526 0.0335 5.023 28.779 16.738 3745.401 3.251 74.452 2.027 0.75 378510. 0.2871
|
|
90.20 0.5109 0.7735 0.0474 0.0313 4.687 26.857 15.073 3495.195 3.034 67.046 1.956 0.75 379368. 0.2629
|
|
94.71 0.5364 0.7814 0.0420 0.0288 4.324 24.774 13.377 3224.129 2.799 59.501 1.882 0.75 380258. 0.2383
|
|
99.22 0.5619 0.7840 0.0366 0.0262 3.933 22.537 11.656 2933.092 2.546 51.846 1.802 0.75 381179. 0.2130
|
|
103.73 0.5875 0.7797 0.0312 0.0235 3.518 20.156 9.917 2623.214 2.277 44.110 1.715 0.75 382133. 0.1869
|
|
108.24 0.6130 0.7656 0.0257 0.0205 3.079 17.642 8.167 2295.969 1.993 36.326 1.613 0.75 383118. 0.1596
|
|
112.75 0.6386 0.7363 0.0202 0.0175 2.619 15.009 6.415 1953.255 1.696 28.533 1.490 0.75 384136. 0.1306
|
|
117.26 0.6641 0.6817 0.0147 0.0143 2.142 12.275 4.671 1597.478 1.387 20.775 1.326 0.76 385186. 0.0992
|
|
121.77 0.6897 0.5790 0.0093 0.0110 1.652 9.464 2.945 1231.618 1.069 13.100 1.085 0.76 386268. 0.0644
|
|
126.28 0.7152 0.3655 0.0039 0.0077 1.152 6.601 1.250 859.096 0.746 5.562 0.660 0.76 387378. 0.0256
|
|
130.79 0.7407
|
|
|
|
|
|
|
|
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 0.1172 0.0444 8.630 45.328 44.393 6435.376 5.121 197.460 3.129 0.81 401532. 0.7216
|
|
4.92 0.0255 0.0659 0.1157 0.0448 8.723 45.815 43.831 6504.614 5.176 194.960 3.056 0.81 401844. 0.7005
|
|
9.83 0.0511 0.1286 0.1141 0.0453 8.809 46.266 43.210 6568.561 5.227 192.199 2.984 0.81 402184. 0.6790
|
|
14.75 0.0766 0.1883 0.1123 0.0457 8.885 46.667 42.527 6625.548 5.272 189.160 2.911 0.81 402553. 0.6572
|
|
19.67 0.1021 0.2448 0.1103 0.0460 8.950 47.008 41.776 6673.882 5.311 185.821 2.839 0.81 402951. 0.6353
|
|
24.59 0.1276 0.2983 0.1081 0.0463 9.000 47.274 40.954 6711.663 5.341 182.163 2.768 0.81 403379. 0.6131
|
|
29.50 0.1532 0.3488 0.1057 0.0464 9.034 47.451 40.055 6736.872 5.361 178.165 2.697 0.81 403839. 0.5908
|
|
34.42 0.1787 0.3964 0.1031 0.0465 9.048 47.525 39.076 6747.321 5.369 173.808 2.627 0.81 404331. 0.5684
|
|
39.34 0.2042 0.4411 0.1003 0.0465 9.039 47.479 38.011 6740.743 5.364 169.075 2.558 0.81 404857. 0.5459
|
|
44.25 0.2297 0.4830 0.0973 0.0463 9.005 47.296 36.859 6714.776 5.343 163.949 2.490 0.81 405415. 0.5233
|
|
49.17 0.2553 0.5223 0.0940 0.0460 8.941 46.960 35.615 6667.070 5.305 158.416 2.423 0.81 406008. 0.5005
|
|
54.09 0.2808 0.5590 0.0905 0.0455 8.844 46.454 34.278 6595.281 5.248 152.467 2.357 0.81 406635. 0.4778
|
|
59.01 0.3063 0.5931 0.0867 0.0448 8.713 45.763 32.844 6497.117 5.170 146.091 2.293 0.81 407297. 0.4549
|
|
63.92 0.3319 0.6248 0.0827 0.0439 8.543 44.869 31.313 6370.186 5.069 139.280 2.230 0.81 407993. 0.4319
|
|
68.84 0.3574 0.6541 0.0784 0.0428 8.331 43.759 29.686 6212.702 4.944 132.042 2.167 0.81 408724. 0.4088
|
|
73.76 0.3829 0.6809 0.0738 0.0415 8.079 42.433 27.970 6024.355 4.794 124.412 2.106 0.81 409490. 0.3855
|
|
78.67 0.4084 0.7053 0.0691 0.0400 7.786 40.896 26.176 5806.105 4.620 116.432 2.045 0.81 410290. 0.3622
|
|
83.59 0.4340 0.7270 0.0642 0.0383 7.454 39.152 24.312 5558.613 4.423 108.141 1.984 0.81 411124. 0.3386
|
|
88.51 0.4595 0.7458 0.0591 0.0364 7.084 37.208 22.386 5282.527 4.204 99.574 1.922 0.82 411993. 0.3148
|
|
93.42 0.4850 0.7615 0.0539 0.0343 6.676 35.065 20.406 4978.339 3.962 90.765 1.859 0.82 412896. 0.2907
|
|
98.34 0.5106 0.7734 0.0485 0.0320 6.232 32.731 18.378 4646.993 3.698 81.747 1.794 0.82 413834. 0.2662
|
|
103.26 0.5361 0.7806 0.0431 0.0296 5.753 30.218 16.311 4290.210 3.414 72.550 1.724 0.82 414805. 0.2411
|
|
108.18 0.5616 0.7818 0.0375 0.0269 5.243 27.538 14.211 3909.684 3.111 63.209 1.649 0.82 415812. 0.2151
|
|
113.09 0.5871 0.7749 0.0319 0.0242 4.704 24.707 12.087 3507.757 2.791 53.761 1.563 0.82 416853. 0.1881
|
|
118.01 0.6127 0.7560 0.0263 0.0213 4.140 21.746 9.947 3087.415 2.457 44.245 1.461 0.82 417928. 0.1595
|
|
122.93 0.6382 0.7192 0.0206 0.0183 3.556 18.680 7.803 2652.038 2.110 34.709 1.335 0.82 419039. 0.1291
|
|
127.84 0.6637 0.6530 0.0150 0.0152 2.958 15.536 5.666 2205.772 1.755 25.204 1.165 0.82 420184. 0.0960
|
|
132.76 0.6892 0.5344 0.0094 0.0121 2.351 12.351 3.550 1753.466 1.395 15.790 0.918 0.83 421363. 0.0599
|
|
137.68 0.7148 0.3092 0.0039 0.0090 1.744 9.159 1.469 1300.370 1.035 6.532 0.512 0.83 422574. 0.0215
|
|
142.60 0.7403
|
|
|
|
|
|
|
|
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 0.1189 0.0504 12.478 60.497 52.879 9304.835 6.835 235.204 2.578 0.87 434911. 0.6488
|
|
5.28 0.0253 0.0587 0.1175 0.0507 12.542 60.810 52.260 9352.932 6.870 232.451 2.534 0.87 435246. 0.6342
|
|
10.56 0.0506 0.1153 0.1160 0.0509 12.593 61.057 51.571 9390.817 6.898 229.388 2.491 0.87 435611. 0.6192
|
|
15.84 0.0759 0.1700 0.1143 0.0510 12.628 61.225 50.808 9416.664 6.917 225.992 2.447 0.87 436007. 0.6038
|
|
21.12 0.1012 0.2226 0.1124 0.0511 12.644 61.303 49.964 9428.678 6.926 222.238 2.404 0.87 436435. 0.5881
|
|
26.40 0.1265 0.2731 0.1103 0.0511 12.639 61.279 49.033 9425.060 6.923 218.101 2.360 0.87 436896. 0.5720
|
|
31.69 0.1518 0.3217 0.1080 0.0510 12.611 61.142 48.012 9403.946 6.908 213.556 2.316 0.88 437390. 0.5554
|
|
36.97 0.1772 0.3681 0.1055 0.0508 12.556 60.878 46.893 9363.358 6.878 208.580 2.272 0.88 437920. 0.5385
|
|
42.25 0.2025 0.4125 0.1027 0.0504 12.473 60.474 45.673 9301.225 6.832 203.151 2.227 0.88 438485. 0.5210
|
|
47.53 0.2278 0.4548 0.0997 0.0500 12.358 59.916 44.346 9215.355 6.769 197.250 2.183 0.88 439086. 0.5031
|
|
52.81 0.2531 0.4949 0.0965 0.0493 12.208 59.188 42.909 9103.446 6.687 190.859 2.138 0.88 439724. 0.4848
|
|
58.09 0.2784 0.5330 0.0930 0.0486 12.020 58.276 41.358 8963.121 6.584 183.962 2.093 0.88 440398. 0.4659
|
|
63.37 0.3037 0.5689 0.0893 0.0477 11.790 57.162 39.692 8791.771 6.458 176.548 2.048 0.88 441110. 0.4466
|
|
68.65 0.3290 0.6026 0.0853 0.0465 11.515 55.831 37.906 8587.085 6.308 168.607 2.002 0.88 441858. 0.4267
|
|
73.93 0.3543 0.6341 0.0810 0.0452 11.193 54.270 36.003 8346.977 6.131 160.141 1.956 0.88 442643. 0.4064
|
|
79.21 0.3796 0.6633 0.0765 0.0438 10.824 52.476 33.990 8071.122 5.929 151.190 1.910 0.88 443465. 0.3855
|
|
84.49 0.4049 0.6902 0.0717 0.0421 10.407 50.455 31.880 7760.174 5.700 141.804 1.863 0.88 444324. 0.3642
|
|
89.77 0.4302 0.7141 0.0668 0.0402 9.950 48.242 29.683 7419.928 5.450 132.029 1.814 0.88 445219. 0.3422
|
|
95.06 0.4555 0.7344 0.0616 0.0382 9.459 45.859 27.407 7053.334 5.181 121.907 1.762 0.88 446150. 0.3194
|
|
100.34 0.4808 0.7503 0.0564 0.0361 8.937 43.328 25.062 6664.035 4.895 111.475 1.706 0.88 447118. 0.2956
|
|
105.62 0.5061 0.7601 0.0510 0.0339 8.394 40.696 22.655 6259.252 4.598 100.768 1.642 0.89 448122. 0.2705
|
|
110.90 0.5315 0.7640 0.0454 0.0316 7.817 37.901 20.197 5829.349 4.282 89.835 1.571 0.89 449162. 0.2445
|
|
116.18 0.5568 0.7602 0.0398 0.0292 7.211 34.964 17.697 5377.579 3.950 78.716 1.493 0.89 450239. 0.2174
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121.46 0.5821 0.7464 0.0341 0.0266 6.580 31.904 15.165 4907.007 3.604 67.454 1.402 0.89 451352. 0.1890
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|
126.74 0.6074 0.7187 0.0284 0.0240 5.931 28.754 12.612 4422.537 3.249 56.098 1.293 0.89 452502. 0.1590
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132.02 0.6327 0.6713 0.0226 0.0213 5.270 25.552 10.050 3930.012 2.887 44.704 1.160 0.89 453688. 0.1273
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|
137.30 0.6580 0.5957 0.0169 0.0186 4.606 22.333 7.495 3434.923 2.523 33.336 0.990 0.89 454911. 0.0938
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|
142.58 0.6833 0.4778 0.0112 0.0160 3.948 19.140 4.961 2943.782 2.162 22.067 0.764 0.89 456170. 0.0589
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|
147.86 0.7086 0.2947 0.0056 0.0134 3.303 16.015 2.469 2463.121 1.809 10.980 0.455 0.90 457464. 0.0247
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|
153.15 0.7339 0.0029 0.0000 0.0108 2.669 12.939 0.019 1990.089 1.462 0.083 0.004 0.90 458768. 0.0000
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PROP RPM = 14000
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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 0.1189 0.0585 18.072 81.359 61.304 13476.058 9.192 272.682 2.063 0.94 468362. 0.5592
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5.84 0.0260 0.0521 0.1177 0.0588 18.161 81.760 60.678 13542.516 9.237 269.895 2.032 0.94 468723. 0.5480
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|
11.69 0.0520 0.1026 0.1163 0.0590 18.222 82.035 59.967 13588.048 9.268 266.733 2.002 0.94 469118. 0.5366
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|
17.53 0.0780 0.1515 0.1147 0.0591 18.249 82.159 59.163 13608.511 9.282 263.158 1.972 0.94 469550. 0.5250
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|
23.37 0.1040 0.1991 0.1130 0.0590 18.238 82.108 58.257 13600.105 9.277 259.128 1.943 0.94 470019. 0.5133
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|
29.22 0.1300 0.2453 0.1110 0.0589 18.184 81.863 57.240 13559.487 9.249 254.604 1.915 0.94 470527. 0.5015
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|
35.06 0.1560 0.2901 0.1088 0.0585 18.082 81.406 56.104 13483.763 9.197 249.549 1.887 0.94 471076. 0.4893
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|
40.90 0.1820 0.3336 0.1064 0.0580 17.930 80.722 54.840 13370.513 9.120 243.926 1.860 0.94 471665. 0.4769
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|
46.75 0.2080 0.3758 0.1036 0.0574 17.725 79.799 53.441 13217.621 9.016 237.704 1.834 0.94 472296. 0.4641
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|
52.59 0.2340 0.4168 0.1007 0.0565 17.464 78.622 51.899 13022.680 8.883 230.847 1.808 0.94 472970. 0.4508
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|
58.44 0.2600 0.4563 0.0974 0.0555 17.145 77.187 50.211 12784.959 8.721 223.339 1.781 0.94 473686. 0.4369
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|
64.28 0.2860 0.4945 0.0938 0.0543 16.767 75.484 48.372 12502.831 8.528 215.160 1.755 0.95 474445. 0.4225
|
|
70.12 0.3120 0.5312 0.0899 0.0528 16.327 73.503 46.379 12174.801 8.304 206.294 1.728 0.95 475247. 0.4073
|
|
75.97 0.3380 0.5662 0.0858 0.0512 15.823 71.237 44.229 11799.480 8.048 196.731 1.700 0.95 476092. 0.3914
|
|
81.81 0.3640 0.5995 0.0813 0.0494 15.256 68.684 41.926 11376.645 7.760 186.486 1.672 0.95 476979. 0.3747
|
|
87.65 0.3901 0.6309 0.0766 0.0473 14.629 65.858 39.484 10908.499 7.441 175.623 1.642 0.95 477908. 0.3571
|
|
93.50 0.4161 0.6601 0.0716 0.0451 13.944 62.774 36.918 10397.672 7.092 164.211 1.610 0.95 478879. 0.3387
|
|
99.34 0.4421 0.6866 0.0664 0.0428 13.211 59.478 34.242 9851.728 6.720 152.310 1.577 0.95 479892. 0.3193
|
|
105.18 0.4681 0.7081 0.0610 0.0403 12.464 56.114 31.467 9294.536 6.340 139.964 1.536 0.95 480946. 0.2982
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|
111.03 0.4941 0.7239 0.0555 0.0379 11.699 52.667 28.604 8723.623 5.950 127.231 1.487 0.95 482041. 0.2753
|
|
116.87 0.5201 0.7256 0.0498 0.0357 11.018 49.603 25.654 8216.104 5.604 114.111 1.416 0.95 483177. 0.2483
|
|
122.71 0.5461 0.7155 0.0439 0.0335 10.354 46.614 22.641 7721.045 5.266 100.706 1.330 0.96 484354. 0.2191
|
|
128.56 0.5721 0.6937 0.0380 0.0313 9.676 43.563 19.582 7215.675 4.922 87.103 1.231 0.96 485572. 0.1886
|
|
134.40 0.5981 0.6573 0.0320 0.0291 8.994 40.492 16.496 6706.978 4.575 73.374 1.116 0.96 486830. 0.1568
|
|
140.24 0.6241 0.6027 0.0260 0.0269 8.316 37.437 13.401 6200.986 4.230 59.608 0.980 0.96 488130. 0.1242
|
|
146.09 0.6501 0.5255 0.0200 0.0248 7.651 34.443 10.321 5705.008 3.891 45.906 0.821 0.96 489472. 0.0912
|
|
151.93 0.6761 0.4209 0.0141 0.0227 7.009 31.554 7.281 5226.438 3.565 32.388 0.632 0.96 490855. 0.0590
|
|
157.78 0.7021 0.2839 0.0084 0.0207 6.396 28.797 4.316 4769.860 3.253 19.196 0.410 0.96 492281. 0.0295
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|
163.62 0.7281 0.1083 0.0028 0.0188 5.813 26.169 1.443 4334.572 2.957 6.416 0.151 0.97 493757. 0.0063
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|
169.46 0.7541
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