464 lines
82 KiB
Plaintext
464 lines
82 KiB
Plaintext
20x8 (20x8.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 0.0674 0.0250 0.006 0.406 0.344 4.801 0.046 1.529 32.468 0.08 31322. 0.5584
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0.38 0.0200 0.0524 0.0661 0.0252 0.006 0.409 0.337 4.835 0.046 1.499 31.621 0.08 31337. 0.5386
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0.76 0.0399 0.1020 0.0647 0.0253 0.007 0.411 0.330 4.865 0.046 1.468 30.773 0.08 31353. 0.5187
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1.13 0.0599 0.1488 0.0633 0.0255 0.007 0.413 0.323 4.889 0.047 1.435 29.929 0.08 31370. 0.4987
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1.51 0.0799 0.1929 0.0617 0.0256 0.007 0.415 0.315 4.907 0.047 1.400 29.087 0.08 31389. 0.4787
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1.89 0.0998 0.2341 0.0601 0.0256 0.007 0.416 0.306 4.918 0.047 1.363 28.249 0.08 31408. 0.4587
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2.27 0.1198 0.2727 0.0584 0.0256 0.007 0.416 0.298 4.923 0.047 1.323 27.415 0.08 31430. 0.4387
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2.65 0.1398 0.3085 0.0565 0.0256 0.007 0.416 0.288 4.919 0.047 1.282 26.584 0.08 31452. 0.4188
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3.03 0.1597 0.3416 0.0546 0.0256 0.007 0.415 0.279 4.907 0.047 1.239 25.755 0.08 31476. 0.3988
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3.40 0.1797 0.3719 0.0527 0.0254 0.007 0.413 0.268 4.885 0.047 1.194 24.929 0.08 31501. 0.3790
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3.78 0.1997 0.3996 0.0506 0.0253 0.007 0.410 0.258 4.854 0.046 1.147 24.103 0.08 31528. 0.3592
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4.16 0.2196 0.4245 0.0484 0.0251 0.006 0.407 0.247 4.813 0.046 1.099 23.277 0.08 31556. 0.3394
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4.54 0.2396 0.4466 0.0462 0.0248 0.006 0.402 0.236 4.762 0.045 1.048 22.449 0.08 31586. 0.3197
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4.92 0.2595 0.4659 0.0439 0.0245 0.006 0.397 0.224 4.699 0.045 0.996 21.617 0.08 31618. 0.3001
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5.29 0.2795 0.4822 0.0416 0.0241 0.006 0.391 0.212 4.625 0.044 0.942 20.778 0.08 31651. 0.2806
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5.67 0.2995 0.4955 0.0391 0.0236 0.006 0.384 0.199 4.539 0.043 0.887 19.928 0.08 31685. 0.2611
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6.05 0.3194 0.5057 0.0366 0.0231 0.006 0.375 0.187 4.441 0.042 0.830 19.065 0.08 31722. 0.2417
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6.43 0.3394 0.5124 0.0340 0.0225 0.006 0.366 0.174 4.330 0.041 0.772 18.182 0.08 31760. 0.2222
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6.81 0.3594 0.5154 0.0314 0.0219 0.006 0.355 0.160 4.206 0.040 0.712 17.274 0.08 31799. 0.2028
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7.18 0.3793 0.5145 0.0287 0.0212 0.005 0.344 0.147 4.068 0.039 0.652 16.334 0.08 31841. 0.1834
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7.56 0.3993 0.5089 0.0260 0.0204 0.005 0.331 0.133 3.917 0.037 0.590 15.350 0.08 31884. 0.1640
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7.94 0.4193 0.4982 0.0232 0.0195 0.005 0.317 0.118 3.752 0.036 0.527 14.312 0.08 31929. 0.1445
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8.32 0.4392 0.4815 0.0204 0.0186 0.005 0.302 0.104 3.574 0.034 0.463 13.203 0.08 31975. 0.1249
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8.70 0.4592 0.4576 0.0175 0.0176 0.005 0.286 0.089 3.381 0.032 0.398 12.001 0.08 32024. 0.1053
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9.08 0.4792 0.4249 0.0147 0.0165 0.004 0.268 0.075 3.174 0.030 0.332 10.679 0.08 32074. 0.0856
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9.45 0.4991 0.3811 0.0117 0.0154 0.004 0.250 0.060 2.953 0.028 0.266 9.197 0.08 32126. 0.0660
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9.83 0.5191 0.3232 0.0088 0.0142 0.004 0.230 0.045 2.719 0.026 0.200 7.498 0.08 32180. 0.0466
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10.21 0.5391 0.2462 0.0059 0.0129 0.003 0.209 0.030 2.471 0.024 0.133 5.500 0.08 32236. 0.0279
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10.59 0.5590 0.1425 0.0029 0.0115 0.003 0.187 0.015 2.210 0.021 0.067 3.071 0.08 32293. 0.0110
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10.97 0.5790 -0.0019 0.0000 0.0101 0.003 0.163 0.000 1.934 0.018 -0.001 -0.040 0.08 32349. 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 0.0678 0.0220 0.045 1.428 1.382 33.795 0.161 6.147 18.548 0.16 62642. 0.6397
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0.76 0.0201 0.0601 0.0665 0.0222 0.046 1.442 1.356 34.116 0.163 6.030 18.023 0.16 62672. 0.6156
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1.52 0.0401 0.1167 0.0651 0.0224 0.046 1.454 1.327 34.400 0.164 5.904 17.503 0.16 62705. 0.5916
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2.28 0.0602 0.1699 0.0636 0.0225 0.046 1.464 1.297 34.640 0.165 5.771 16.989 0.16 62740. 0.5677
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3.04 0.0803 0.2197 0.0621 0.0227 0.047 1.472 1.266 34.830 0.166 5.630 16.482 0.16 62777. 0.5440
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3.80 0.1003 0.2663 0.0604 0.0228 0.047 1.478 1.232 34.964 0.167 5.480 15.983 0.16 62817. 0.5205
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4.56 0.1204 0.3097 0.0587 0.0228 0.047 1.481 1.197 35.038 0.167 5.323 15.491 0.16 62860. 0.4972
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5.32 0.1405 0.3501 0.0568 0.0228 0.047 1.481 1.159 35.046 0.167 5.157 15.006 0.16 62905. 0.4740
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6.08 0.1605 0.3873 0.0549 0.0228 0.047 1.478 1.120 34.982 0.167 4.984 14.527 0.16 62953. 0.4512
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6.84 0.1806 0.4216 0.0529 0.0227 0.047 1.472 1.080 34.843 0.166 4.803 14.055 0.16 63004. 0.4285
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7.60 0.2007 0.4529 0.0509 0.0225 0.046 1.463 1.037 34.622 0.165 4.614 13.589 0.16 63059. 0.4060
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8.36 0.2208 0.4812 0.0487 0.0223 0.046 1.450 0.993 34.316 0.164 4.418 13.128 0.16 63116. 0.3838
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9.12 0.2408 0.5067 0.0465 0.0221 0.045 1.433 0.948 33.919 0.162 4.215 12.670 0.16 63176. 0.3618
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9.88 0.2609 0.5292 0.0441 0.0218 0.045 1.413 0.900 33.428 0.160 4.004 12.216 0.16 63239. 0.3400
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10.64 0.2810 0.5488 0.0418 0.0214 0.044 1.388 0.852 32.838 0.157 3.788 11.762 0.16 63306. 0.3184
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11.40 0.3010 0.5653 0.0393 0.0209 0.043 1.359 0.801 32.146 0.153 3.565 11.308 0.16 63376. 0.2970
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12.16 0.3211 0.5786 0.0368 0.0204 0.042 1.325 0.750 31.347 0.150 3.336 10.852 0.16 63449. 0.2757
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12.92 0.3412 0.5886 0.0342 0.0198 0.041 1.286 0.697 30.438 0.145 3.101 10.390 0.16 63526. 0.2545
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13.68 0.3612 0.5950 0.0315 0.0191 0.039 1.243 0.643 29.417 0.140 2.861 9.919 0.16 63606. 0.2334
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14.44 0.3813 0.5974 0.0288 0.0184 0.038 1.195 0.588 28.280 0.135 2.617 9.435 0.16 63690. 0.2123
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15.20 0.4014 0.5954 0.0261 0.0176 0.036 1.142 0.532 27.024 0.129 2.367 8.932 0.16 63777. 0.1912
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15.96 0.4214 0.5881 0.0233 0.0167 0.034 1.084 0.475 25.649 0.122 2.114 8.403 0.16 63867. 0.1699
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16.72 0.4415 0.5746 0.0205 0.0157 0.032 1.021 0.417 24.153 0.115 1.856 7.838 0.16 63962. 0.1485
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17.48 0.4616 0.5535 0.0176 0.0147 0.030 0.952 0.359 22.535 0.108 1.596 7.222 0.16 64060. 0.1269
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18.24 0.4816 0.5227 0.0147 0.0135 0.028 0.879 0.300 20.795 0.099 1.333 6.535 0.16 64161. 0.1050
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19.00 0.5017 0.4790 0.0118 0.0123 0.025 0.800 0.240 18.936 0.090 1.068 5.749 0.16 64266. 0.0826
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19.76 0.5218 0.4174 0.0088 0.0110 0.023 0.717 0.180 16.958 0.081 0.801 4.817 0.16 64375. 0.0600
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20.52 0.5419 0.3295 0.0059 0.0097 0.020 0.628 0.120 14.864 0.071 0.534 3.662 0.16 64487. 0.0372
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21.28 0.5619 0.2003 0.0029 0.0082 0.017 0.535 0.060 12.657 0.060 0.266 2.146 0.16 64602. 0.0154
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22.05 0.5820 -0.0058 -0.0001 0.0067 0.014 0.435 -0.001 10.286 0.049 -0.006 -0.060 0.16 64711. 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 0.0682 0.0208 0.145 3.044 3.128 108.045 0.344 13.913 13.131 0.24 93961. 0.6813
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1.16 0.0204 0.0649 0.0668 0.0211 0.146 3.077 3.067 109.220 0.348 13.644 12.738 0.24 94007. 0.6545
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2.32 0.0409 0.1258 0.0654 0.0213 0.148 3.106 3.003 110.261 0.351 13.356 12.352 0.24 94057. 0.6279
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3.49 0.0613 0.1829 0.0639 0.0214 0.149 3.131 2.934 111.144 0.354 13.049 11.972 0.24 94111. 0.6016
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4.65 0.0818 0.2363 0.0623 0.0216 0.150 3.151 2.860 111.850 0.356 12.723 11.599 0.24 94169. 0.5755
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5.81 0.1022 0.2861 0.0606 0.0217 0.151 3.166 2.783 112.358 0.358 12.378 11.234 0.24 94230. 0.5498
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6.97 0.1227 0.3324 0.0589 0.0217 0.151 3.174 2.701 112.647 0.359 12.014 10.875 0.24 94296. 0.5244
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8.13 0.1431 0.3752 0.0570 0.0217 0.151 3.175 2.615 112.698 0.359 11.631 10.524 0.24 94366. 0.4993
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9.29 0.1636 0.4148 0.0550 0.0217 0.151 3.169 2.525 112.492 0.358 11.230 10.180 0.24 94440. 0.4745
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10.46 0.1840 0.4511 0.0530 0.0216 0.150 3.156 2.430 112.011 0.357 10.810 9.842 0.24 94519. 0.4501
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11.62 0.2045 0.4844 0.0508 0.0215 0.149 3.134 2.332 111.236 0.354 10.373 9.509 0.24 94602. 0.4260
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12.78 0.2249 0.5145 0.0486 0.0212 0.148 3.103 2.230 110.150 0.351 9.919 9.182 0.24 94691. 0.4023
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13.94 0.2454 0.5415 0.0463 0.0210 0.146 3.064 2.124 108.736 0.346 9.448 8.860 0.24 94784. 0.3788
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15.10 0.2658 0.5656 0.0439 0.0206 0.143 3.014 2.015 106.979 0.341 8.961 8.542 0.24 94882. 0.3557
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16.27 0.2863 0.5866 0.0414 0.0202 0.141 2.954 1.902 104.862 0.334 8.459 8.226 0.24 94985. 0.3328
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17.43 0.3067 0.6044 0.0389 0.0197 0.137 2.884 1.786 102.371 0.326 7.942 7.911 0.24 95094. 0.3101
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18.59 0.3272 0.6190 0.0363 0.0192 0.133 2.803 1.666 99.494 0.317 7.411 7.596 0.24 95207. 0.2877
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19.75 0.3476 0.6302 0.0336 0.0186 0.129 2.711 1.544 96.216 0.306 6.868 7.279 0.24 95326. 0.2653
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20.91 0.3681 0.6378 0.0309 0.0178 0.124 2.607 1.419 92.527 0.295 6.312 6.956 0.24 95451. 0.2431
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22.08 0.3885 0.6412 0.0281 0.0171 0.119 2.491 1.292 88.417 0.281 5.745 6.626 0.24 95580. 0.2209
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23.24 0.4090 0.6400 0.0253 0.0162 0.112 2.363 1.162 83.877 0.267 5.167 6.282 0.24 95716. 0.1987
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24.40 0.4294 0.6332 0.0224 0.0152 0.106 2.223 1.030 78.902 0.251 4.581 5.920 0.24 95856. 0.1762
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25.56 0.4499 0.6197 0.0195 0.0142 0.099 2.070 0.896 73.487 0.234 3.986 5.530 0.24 96003. 0.1536
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26.72 0.4703 0.5977 0.0166 0.0130 0.091 1.905 0.761 67.631 0.215 3.384 5.102 0.24 96155. 0.1305
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27.88 0.4908 0.5642 0.0136 0.0118 0.082 1.728 0.624 61.338 0.195 2.776 4.615 0.24 96312. 0.1070
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29.05 0.5112 0.5146 0.0106 0.0105 0.073 1.539 0.487 54.611 0.174 2.164 4.041 0.24 96476. 0.0827
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30.21 0.5317 0.4411 0.0076 0.0092 0.064 1.337 0.349 47.462 0.151 1.550 3.331 0.24 96644. 0.0577
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31.37 0.5521 0.3289 0.0046 0.0077 0.054 1.124 0.210 39.901 0.127 0.936 2.391 0.24 96818. 0.0322
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32.53 0.5726 0.1458 0.0016 0.0062 0.043 0.899 0.072 31.911 0.102 0.320 1.022 0.24 96994. 0.0080
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33.69 0.5930
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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 0.0687 0.0203 0.334 5.267 5.603 249.261 0.595 24.922 10.195 0.32 125277. 0.7080
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1.53 0.0202 0.0665 0.0674 0.0205 0.338 5.328 5.496 252.126 0.602 24.448 9.888 0.32 125338. 0.6801
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3.07 0.0405 0.1289 0.0660 0.0207 0.342 5.381 5.382 254.676 0.608 23.940 9.585 0.32 125404. 0.6524
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4.60 0.0607 0.1873 0.0645 0.0209 0.344 5.428 5.261 256.858 0.613 23.399 9.289 0.32 125475. 0.6251
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6.13 0.0810 0.2420 0.0629 0.0210 0.347 5.465 5.132 258.622 0.617 22.825 9.000 0.32 125551. 0.5981
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7.67 0.1012 0.2929 0.0612 0.0211 0.349 5.492 4.995 259.919 0.621 22.217 8.716 0.32 125632. 0.5715
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9.20 0.1214 0.3404 0.0595 0.0212 0.350 5.509 4.851 260.701 0.622 21.576 8.439 0.32 125719. 0.5453
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10.73 0.1417 0.3843 0.0576 0.0212 0.350 5.513 4.699 260.924 0.623 20.902 8.169 0.32 125811. 0.5195
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12.27 0.1619 0.4250 0.0557 0.0212 0.349 5.505 4.540 260.541 0.622 20.195 7.904 0.32 125909. 0.4941
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13.80 0.1821 0.4625 0.0536 0.0211 0.348 5.484 4.374 259.509 0.620 19.456 7.645 0.32 126013. 0.4691
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15.33 0.2024 0.4968 0.0515 0.0210 0.346 5.447 4.201 257.786 0.615 18.685 7.391 0.32 126123. 0.4444
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16.87 0.2226 0.5281 0.0493 0.0208 0.342 5.395 4.021 255.331 0.610 17.884 7.142 0.32 126239. 0.4202
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18.40 0.2429 0.5564 0.0470 0.0205 0.338 5.327 3.834 252.103 0.602 17.054 6.898 0.32 126361. 0.3963
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19.93 0.2631 0.5818 0.0446 0.0202 0.333 5.242 3.641 248.066 0.592 16.196 6.658 0.32 126490. 0.3727
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21.47 0.2833 0.6042 0.0422 0.0198 0.326 5.139 3.442 243.181 0.581 15.311 6.420 0.32 126626. 0.3495
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23.00 0.3036 0.6236 0.0397 0.0193 0.318 5.017 3.237 237.415 0.567 14.400 6.185 0.32 126768. 0.3265
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24.53 0.3238 0.6399 0.0371 0.0188 0.309 4.876 3.027 230.736 0.551 13.464 5.950 0.32 126917. 0.3037
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26.07 0.3441 0.6531 0.0345 0.0182 0.299 4.714 2.811 223.112 0.533 12.505 5.715 0.32 127073. 0.2812
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27.60 0.3643 0.6628 0.0318 0.0175 0.288 4.533 2.591 214.517 0.512 11.525 5.478 0.32 127236. 0.2587
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29.13 0.3845 0.6688 0.0290 0.0167 0.275 4.330 2.366 204.926 0.489 10.524 5.237 0.32 127406. 0.2363
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30.66 0.4048 0.6705 0.0262 0.0158 0.261 4.106 2.137 194.319 0.464 9.505 4.988 0.32 127583. 0.2139
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32.20 0.4250 0.6673 0.0233 0.0149 0.245 3.860 1.904 182.681 0.436 8.469 4.727 0.32 127767. 0.1914
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33.73 0.4453 0.6580 0.0204 0.0138 0.228 3.592 1.668 170.001 0.406 7.418 4.450 0.32 127959. 0.1686
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35.26 0.4655 0.6410 0.0175 0.0127 0.210 3.302 1.429 156.274 0.373 6.355 4.147 0.32 128158. 0.1454
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36.80 0.4857 0.6139 0.0146 0.0115 0.190 2.990 1.187 141.504 0.338 5.281 3.805 0.32 128364. 0.1216
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38.33 0.5060 0.5724 0.0116 0.0102 0.169 2.656 0.944 125.703 0.300 4.199 3.406 0.32 128577. 0.0971
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39.86 0.5262 0.5093 0.0086 0.0089 0.146 2.301 0.700 108.890 0.260 3.112 2.914 0.32 128798. 0.0715
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41.40 0.5464 0.4110 0.0056 0.0074 0.122 1.925 0.455 91.093 0.217 2.023 2.265 0.32 129026. 0.0448
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42.93 0.5667 0.2479 0.0026 0.0059 0.097 1.528 0.210 72.313 0.173 0.934 1.317 0.32 129259. 0.0177
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44.46 0.5869
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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 0.0693 0.0200 0.645 8.129 8.839 480.896 0.918 39.315 8.336 0.40 156589. 0.7271
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1.91 0.0201 0.0676 0.0680 0.0203 0.653 8.226 8.673 486.638 0.929 38.576 8.083 0.40 156666. 0.6984
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3.81 0.0403 0.1310 0.0666 0.0205 0.659 8.313 8.495 491.761 0.939 37.785 7.835 0.40 156748. 0.6700
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5.72 0.0604 0.1904 0.0652 0.0207 0.665 8.387 8.305 496.158 0.948 36.942 7.593 0.40 156836. 0.6419
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7.63 0.0805 0.2459 0.0636 0.0208 0.670 8.448 8.104 499.730 0.954 36.047 7.355 0.40 156931. 0.6143
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9.53 0.1007 0.2977 0.0619 0.0209 0.674 8.493 7.891 502.382 0.959 35.098 7.124 0.40 157032. 0.5871
|
|
11.44 0.1208 0.3460 0.0601 0.0210 0.676 8.520 7.666 504.020 0.963 34.097 6.898 0.40 157140. 0.5604
|
|
13.35 0.1409 0.3907 0.0583 0.0210 0.677 8.529 7.429 504.556 0.964 33.044 6.678 0.40 157255. 0.5340
|
|
15.25 0.1611 0.4322 0.0563 0.0210 0.676 8.518 7.181 503.901 0.962 31.939 6.463 0.40 157377. 0.5081
|
|
17.16 0.1812 0.4704 0.0543 0.0209 0.673 8.486 6.921 501.970 0.959 30.784 6.254 0.40 157506. 0.4827
|
|
19.07 0.2013 0.5056 0.0522 0.0208 0.669 8.430 6.650 498.678 0.952 29.580 6.049 0.40 157642. 0.4576
|
|
20.97 0.2215 0.5377 0.0500 0.0206 0.662 8.350 6.369 493.947 0.943 28.329 5.848 0.40 157786. 0.4330
|
|
22.88 0.2416 0.5669 0.0477 0.0203 0.654 8.244 6.077 487.698 0.931 27.031 5.652 0.40 157939. 0.4088
|
|
24.79 0.2617 0.5932 0.0453 0.0200 0.643 8.112 5.775 479.857 0.916 25.688 5.459 0.40 158099. 0.3849
|
|
26.69 0.2819 0.6166 0.0429 0.0196 0.631 7.951 5.464 470.352 0.898 24.304 5.269 0.40 158267. 0.3613
|
|
28.60 0.3020 0.6371 0.0403 0.0191 0.616 7.761 5.143 459.116 0.877 22.878 5.081 0.40 158443. 0.3381
|
|
30.51 0.3221 0.6547 0.0378 0.0186 0.598 7.541 4.814 446.083 0.852 21.414 4.895 0.40 158628. 0.3151
|
|
32.41 0.3423 0.6692 0.0351 0.0180 0.578 7.289 4.477 431.196 0.824 19.914 4.709 0.40 158822. 0.2923
|
|
34.32 0.3624 0.6804 0.0324 0.0173 0.556 7.005 4.132 414.398 0.791 18.379 4.523 0.40 159024. 0.2697
|
|
36.23 0.3825 0.6882 0.0297 0.0165 0.531 6.688 3.780 395.644 0.756 16.812 4.333 0.40 159234. 0.2472
|
|
38.13 0.4027 0.6919 0.0268 0.0156 0.503 6.337 3.421 374.891 0.716 15.216 4.139 0.40 159454. 0.2246
|
|
40.04 0.4228 0.6910 0.0240 0.0147 0.472 5.952 3.056 352.109 0.672 13.594 3.937 0.40 159682. 0.2019
|
|
41.95 0.4429 0.6845 0.0211 0.0136 0.439 5.532 2.686 327.274 0.625 11.947 3.723 0.40 159920. 0.1790
|
|
43.85 0.4631 0.6709 0.0181 0.0125 0.403 5.078 2.311 300.377 0.574 10.280 3.490 0.40 160166. 0.1557
|
|
45.76 0.4832 0.6479 0.0152 0.0113 0.364 4.588 1.933 271.422 0.518 8.597 3.230 0.40 160422. 0.1317
|
|
47.67 0.5033 0.6115 0.0122 0.0100 0.322 4.064 1.551 240.429 0.459 6.900 2.926 0.40 160686. 0.1069
|
|
49.57 0.5235 0.5549 0.0092 0.0086 0.278 3.507 1.168 207.438 0.396 5.195 2.554 0.40 160960. 0.0810
|
|
51.48 0.5436 0.4650 0.0061 0.0072 0.231 2.916 0.784 172.498 0.329 3.486 2.061 0.40 161242. 0.0535
|
|
53.39 0.5637 0.3125 0.0031 0.0057 0.182 2.293 0.399 135.635 0.259 1.776 1.335 0.40 161531. 0.0248
|
|
55.29 0.5839 0.0017 0.0000 0.0040 0.128 1.612 0.001 95.351 0.182 0.007 0.007 0.40 161783. 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 0.0702 0.0200 1.112 11.682 12.880 829.275 1.320 57.290 7.045 0.48 187896. 0.7417
|
|
2.29 0.0201 0.0684 0.0689 0.0202 1.126 11.826 12.641 839.482 1.336 56.225 6.830 0.48 187988. 0.7124
|
|
4.57 0.0402 0.1326 0.0675 0.0205 1.138 11.954 12.384 848.594 1.351 55.084 6.619 0.48 188087. 0.6834
|
|
6.86 0.0603 0.1928 0.0660 0.0206 1.148 12.064 12.110 856.418 1.363 53.866 6.414 0.48 188194. 0.6548
|
|
9.14 0.0804 0.2490 0.0644 0.0208 1.157 12.154 11.819 862.782 1.373 52.571 6.213 0.48 188308. 0.6267
|
|
11.43 0.1006 0.3015 0.0627 0.0209 1.163 12.221 11.510 867.516 1.381 51.198 6.018 0.48 188429. 0.5990
|
|
13.71 0.1207 0.3503 0.0609 0.0210 1.167 12.262 11.184 870.459 1.385 49.748 5.828 0.48 188559. 0.5718
|
|
16.00 0.1408 0.3957 0.0591 0.0210 1.169 12.276 10.841 871.453 1.387 48.221 5.643 0.48 188697. 0.5451
|
|
18.28 0.1609 0.4378 0.0571 0.0210 1.167 12.261 10.481 870.344 1.385 46.619 5.462 0.48 188844. 0.5188
|
|
20.57 0.1810 0.4767 0.0550 0.0209 1.163 12.213 10.104 866.983 1.380 44.943 5.286 0.48 188999. 0.4930
|
|
22.85 0.2011 0.5124 0.0529 0.0208 1.155 12.132 9.711 861.225 1.371 43.195 5.114 0.48 189163. 0.4676
|
|
25.14 0.2212 0.5452 0.0507 0.0206 1.144 12.015 9.302 852.930 1.357 41.377 4.947 0.48 189336. 0.4426
|
|
27.43 0.2413 0.5751 0.0484 0.0203 1.129 11.861 8.879 841.966 1.340 39.492 4.783 0.48 189519. 0.4181
|
|
29.71 0.2615 0.6021 0.0460 0.0200 1.111 11.667 8.440 828.201 1.318 37.541 4.622 0.48 189711. 0.3940
|
|
32.00 0.2816 0.6262 0.0435 0.0196 1.088 11.432 7.988 811.509 1.292 35.529 4.464 0.48 189913. 0.3702
|
|
34.28 0.3017 0.6476 0.0410 0.0191 1.062 11.154 7.522 791.773 1.260 33.456 4.309 0.48 190125. 0.3467
|
|
36.57 0.3218 0.6660 0.0384 0.0185 1.031 10.831 7.043 768.880 1.224 31.328 4.155 0.48 190347. 0.3235
|
|
38.85 0.3419 0.6816 0.0357 0.0179 0.996 10.463 6.552 742.729 1.182 29.145 4.001 0.48 190579. 0.3005
|
|
41.14 0.3620 0.6939 0.0330 0.0172 0.956 10.047 6.051 713.223 1.135 26.913 3.848 0.48 190821. 0.2777
|
|
43.42 0.3821 0.7029 0.0302 0.0164 0.912 9.583 5.538 680.278 1.083 24.633 3.692 0.48 191074. 0.2549
|
|
45.71 0.4022 0.7081 0.0273 0.0155 0.863 9.070 5.016 643.823 1.025 22.311 3.534 0.48 191337. 0.2322
|
|
47.99 0.4223 0.7089 0.0244 0.0146 0.810 8.506 4.485 603.801 0.961 19.949 3.369 0.48 191611. 0.2093
|
|
50.28 0.4425 0.7043 0.0215 0.0135 0.751 7.891 3.946 560.173 0.892 17.552 3.195 0.48 191896. 0.1862
|
|
52.56 0.4626 0.6929 0.0185 0.0124 0.688 7.226 3.400 512.919 0.816 15.125 3.007 0.48 192191. 0.1627
|
|
54.85 0.4827 0.6725 0.0155 0.0111 0.620 6.509 2.849 462.047 0.735 12.672 2.797 0.48 192497. 0.1385
|
|
57.14 0.5028 0.6392 0.0125 0.0098 0.547 5.742 2.293 407.591 0.649 10.200 2.552 0.48 192814. 0.1134
|
|
59.42 0.5229 0.5862 0.0094 0.0084 0.469 4.925 1.735 349.617 0.556 7.716 2.250 0.48 193142. 0.0870
|
|
61.71 0.5430 0.5001 0.0064 0.0069 0.387 4.060 1.175 288.218 0.459 5.225 1.849 0.48 193479. 0.0588
|
|
63.99 0.5631 0.3499 0.0033 0.0054 0.300 3.148 0.614 223.441 0.356 2.733 1.247 0.48 193826. 0.0287
|
|
66.28 0.5832 0.0342 0.0002 0.0037 0.206 2.160 0.040 153.351 0.244 0.177 0.118 0.48 194143. 0.0007
|
|
|
|
|
|
|
|
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 0.0712 0.0201 1.777 16.000 17.788 1325.088 1.808 79.119 6.089 0.56 219195. 0.7534
|
|
2.68 0.0202 0.0693 0.0699 0.0204 1.800 16.203 17.459 1341.899 1.831 77.660 5.901 0.56 219304. 0.7234
|
|
5.36 0.0404 0.1344 0.0685 0.0206 1.820 16.384 17.107 1356.892 1.851 76.092 5.718 0.56 219421. 0.6939
|
|
8.04 0.0606 0.1953 0.0670 0.0208 1.837 16.539 16.730 1369.742 1.869 74.416 5.540 0.56 219547. 0.6648
|
|
10.72 0.0809 0.2522 0.0654 0.0210 1.851 16.665 16.329 1380.163 1.883 72.631 5.366 0.56 219681. 0.6362
|
|
13.40 0.1011 0.3053 0.0637 0.0211 1.861 16.758 15.903 1387.878 1.893 70.736 5.197 0.56 219825. 0.6081
|
|
16.08 0.1213 0.3548 0.0618 0.0211 1.868 16.815 15.452 1392.617 1.900 68.732 5.033 0.56 219978. 0.5804
|
|
18.76 0.1415 0.4007 0.0599 0.0212 1.870 16.834 14.977 1394.121 1.902 66.619 4.873 0.56 220141. 0.5533
|
|
21.44 0.1617 0.4433 0.0579 0.0211 1.867 16.810 14.478 1392.144 1.899 64.400 4.717 0.56 220314. 0.5266
|
|
24.12 0.1819 0.4828 0.0559 0.0211 1.859 16.741 13.956 1386.442 1.891 62.077 4.566 0.56 220497. 0.5004
|
|
26.80 0.2021 0.5191 0.0537 0.0209 1.846 16.624 13.411 1376.783 1.878 59.653 4.418 0.56 220691. 0.4747
|
|
29.48 0.2223 0.5524 0.0514 0.0207 1.828 16.457 12.844 1362.939 1.859 57.130 4.274 0.56 220896. 0.4494
|
|
32.16 0.2426 0.5828 0.0491 0.0204 1.803 16.237 12.255 1344.693 1.834 54.512 4.134 0.56 221111. 0.4246
|
|
34.84 0.2628 0.6103 0.0466 0.0201 1.773 15.961 11.646 1321.836 1.803 51.803 3.996 0.56 221338. 0.4001
|
|
37.52 0.2830 0.6351 0.0441 0.0196 1.736 15.627 11.018 1294.164 1.765 49.007 3.861 0.56 221577. 0.3760
|
|
40.20 0.3032 0.6571 0.0415 0.0192 1.692 15.232 10.370 1261.486 1.721 46.126 3.729 0.56 221826. 0.3523
|
|
42.88 0.3234 0.6762 0.0388 0.0186 1.641 14.775 9.705 1223.623 1.669 43.167 3.597 0.56 222088. 0.3288
|
|
45.56 0.3436 0.6924 0.0361 0.0179 1.583 14.253 9.022 1180.406 1.610 40.132 3.467 0.56 222362. 0.3055
|
|
48.24 0.3638 0.7055 0.0333 0.0172 1.518 13.665 8.324 1131.682 1.544 37.027 3.336 0.56 222648. 0.2824
|
|
50.92 0.3841 0.7153 0.0305 0.0164 1.445 13.008 7.611 1077.317 1.470 33.856 3.205 0.56 222946. 0.2594
|
|
53.60 0.4043 0.7213 0.0276 0.0154 1.364 12.282 6.885 1017.194 1.388 30.624 3.070 0.56 223256. 0.2363
|
|
56.28 0.4245 0.7230 0.0246 0.0144 1.276 11.486 6.146 951.222 1.298 27.338 2.931 0.56 223579. 0.2132
|
|
58.96 0.4447 0.7194 0.0216 0.0134 1.179 10.618 5.396 879.340 1.200 24.002 2.783 0.56 223914. 0.1897
|
|
61.64 0.4649 0.7090 0.0186 0.0122 1.075 9.678 4.637 801.522 1.093 20.624 2.624 0.56 224262. 0.1658
|
|
64.32 0.4851 0.6894 0.0155 0.0109 0.963 8.667 3.869 717.782 0.979 17.211 2.445 0.56 224623. 0.1411
|
|
67.00 0.5053 0.6566 0.0124 0.0095 0.842 7.585 3.096 628.182 0.857 13.771 2.235 0.56 224996. 0.1154
|
|
69.67 0.5255 0.6029 0.0093 0.0081 0.715 6.434 2.319 532.839 0.727 10.314 1.974 0.56 225382. 0.0882
|
|
72.35 0.5458 0.5129 0.0062 0.0066 0.579 5.215 1.540 431.906 0.589 6.848 1.617 0.56 225780. 0.0589
|
|
75.03 0.5660 0.3484 0.0030 0.0049 0.436 3.929 0.760 325.420 0.444 3.380 1.059 0.56 226187. 0.0271
|
|
77.71 0.5862
|
|
|
|
|
|
|
|
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 0.0725 0.0204 2.690 21.192 23.644 2005.802 2.394 105.170 5.347 0.63 250485. 0.7627
|
|
3.09 0.0204 0.0703 0.0711 0.0207 2.725 21.470 23.211 2032.095 2.426 103.243 5.181 0.63 250612. 0.7323
|
|
6.19 0.0408 0.1362 0.0697 0.0209 2.756 21.717 22.744 2055.490 2.454 101.167 5.019 0.63 250748. 0.7022
|
|
9.28 0.0613 0.1978 0.0682 0.0211 2.783 21.928 22.244 2075.471 2.477 98.942 4.861 0.63 250894. 0.6726
|
|
12.38 0.0817 0.2554 0.0665 0.0213 2.805 22.098 21.710 2091.573 2.497 96.565 4.708 0.63 251051. 0.6436
|
|
15.47 0.1021 0.3092 0.0648 0.0214 2.821 22.223 21.141 2103.359 2.511 94.036 4.559 0.64 251219. 0.6150
|
|
18.56 0.1225 0.3593 0.0629 0.0215 2.830 22.297 20.539 2110.405 2.519 91.356 4.414 0.64 251397. 0.5869
|
|
21.66 0.1429 0.4058 0.0610 0.0215 2.833 22.317 19.903 2112.309 2.521 88.527 4.274 0.64 251588. 0.5594
|
|
24.75 0.1634 0.4489 0.0589 0.0214 2.828 22.279 19.234 2108.679 2.517 85.551 4.137 0.64 251789. 0.5323
|
|
27.85 0.1838 0.4889 0.0568 0.0214 2.815 22.178 18.532 2099.149 2.506 82.432 4.004 0.64 252003. 0.5057
|
|
30.94 0.2042 0.5257 0.0545 0.0212 2.794 22.011 17.800 2083.356 2.487 79.173 3.875 0.64 252229. 0.4797
|
|
34.04 0.2246 0.5595 0.0522 0.0210 2.764 21.775 17.037 2060.957 2.460 75.779 3.749 0.64 252468. 0.4540
|
|
37.13 0.2451 0.5903 0.0498 0.0207 2.724 21.465 16.245 2031.618 2.425 72.256 3.627 0.64 252720. 0.4288
|
|
40.22 0.2655 0.6184 0.0473 0.0203 2.675 21.078 15.424 1995.017 2.381 68.607 3.507 0.64 252984. 0.4041
|
|
43.32 0.2859 0.6436 0.0447 0.0198 2.616 20.611 14.577 1950.845 2.329 64.839 3.389 0.64 253262. 0.3796
|
|
46.41 0.3063 0.6661 0.0420 0.0193 2.546 20.062 13.704 1898.810 2.267 60.956 3.274 0.64 253554. 0.3555
|
|
49.51 0.3267 0.6857 0.0392 0.0187 2.466 19.426 12.807 1838.633 2.195 56.965 3.159 0.64 253859. 0.3317
|
|
52.60 0.3472 0.7024 0.0364 0.0180 2.374 18.701 11.887 1770.059 2.113 52.872 3.046 0.64 254178. 0.3081
|
|
55.69 0.3676 0.7160 0.0335 0.0172 2.270 17.886 10.945 1692.856 2.021 48.683 2.932 0.64 254511. 0.2846
|
|
58.79 0.3880 0.7263 0.0306 0.0163 2.155 16.977 9.983 1606.817 1.918 44.404 2.818 0.64 254859. 0.2612
|
|
61.88 0.4084 0.7328 0.0276 0.0154 2.027 15.972 9.003 1511.772 1.805 40.044 2.701 0.64 255221. 0.2378
|
|
64.98 0.4288 0.7348 0.0245 0.0143 1.888 14.872 8.006 1407.584 1.680 35.609 2.580 0.64 255597. 0.2141
|
|
68.07 0.4493 0.7314 0.0214 0.0132 1.736 13.673 6.994 1294.169 1.545 31.107 2.451 0.64 255988. 0.1902
|
|
71.17 0.4697 0.7210 0.0183 0.0119 1.571 12.377 5.969 1171.496 1.398 26.549 2.311 0.64 256394. 0.1656
|
|
74.26 0.4901 0.7007 0.0151 0.0106 1.394 10.984 4.933 1039.604 1.241 21.944 2.152 0.64 256814. 0.1403
|
|
77.35 0.5105 0.6659 0.0119 0.0091 1.205 9.494 3.890 898.613 1.073 17.303 1.964 0.64 257250. 0.1136
|
|
80.45 0.5310 0.6072 0.0087 0.0076 1.004 7.910 2.842 748.723 0.894 12.641 1.722 0.64 257699. 0.0852
|
|
83.54 0.5514 0.5044 0.0055 0.0060 0.791 6.235 1.792 590.176 0.704 7.970 1.377 0.64 258162. 0.0541
|
|
86.64 0.5718 0.3015 0.0023 0.0043 0.567 4.467 0.740 422.765 0.505 3.291 0.794 0.65 258633. 0.0200
|
|
89.73 0.5922
|
|
|
|
|
|
|
|
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 0.0740 0.0210 3.933 27.545 30.562 2933.022 3.112 135.941 4.726 0.71 281763. 0.7665
|
|
3.47 0.0203 0.0697 0.0727 0.0212 3.982 27.887 30.019 2969.423 3.151 133.523 4.585 0.71 281906. 0.7370
|
|
6.93 0.0407 0.1351 0.0713 0.0214 4.026 28.192 29.431 3001.864 3.185 130.911 4.447 0.71 282060. 0.7078
|
|
10.40 0.0610 0.1965 0.0697 0.0216 4.063 28.452 28.800 3029.577 3.214 128.101 4.312 0.71 282225. 0.6789
|
|
13.86 0.0813 0.2540 0.0681 0.0218 4.093 28.661 28.123 3051.873 3.238 125.092 4.180 0.71 282401. 0.6503
|
|
17.33 0.1017 0.3077 0.0663 0.0219 4.114 28.813 27.402 3068.079 3.255 121.883 4.051 0.71 282590. 0.6221
|
|
20.79 0.1220 0.3579 0.0645 0.0220 4.127 28.903 26.636 3077.556 3.265 118.475 3.926 0.71 282791. 0.5944
|
|
24.26 0.1423 0.4045 0.0625 0.0220 4.130 28.923 25.825 3079.686 3.268 114.870 3.803 0.71 283006. 0.5671
|
|
27.73 0.1627 0.4479 0.0605 0.0220 4.122 28.868 24.971 3073.873 3.261 111.072 3.685 0.71 283233. 0.5402
|
|
31.19 0.1830 0.4880 0.0583 0.0219 4.103 28.733 24.075 3059.542 3.246 107.086 3.569 0.72 283473. 0.5138
|
|
34.66 0.2033 0.5252 0.0560 0.0217 4.072 28.514 23.138 3036.143 3.221 102.917 3.457 0.72 283728. 0.4878
|
|
38.12 0.2236 0.5594 0.0537 0.0215 4.027 28.204 22.161 3003.153 3.186 98.570 3.347 0.72 283996. 0.4622
|
|
41.59 0.2440 0.5907 0.0512 0.0211 3.970 27.799 21.145 2960.075 3.141 94.054 3.240 0.72 284279. 0.4371
|
|
45.05 0.2643 0.6193 0.0486 0.0208 3.898 27.296 20.093 2906.443 3.084 89.373 3.136 0.72 284576. 0.4124
|
|
48.52 0.2846 0.6452 0.0460 0.0203 3.811 26.689 19.005 2841.822 3.015 84.536 3.033 0.72 284888. 0.3880
|
|
51.98 0.3050 0.6684 0.0433 0.0198 3.709 25.975 17.884 2765.800 2.935 79.550 2.933 0.72 285215. 0.3639
|
|
55.45 0.3253 0.6889 0.0405 0.0191 3.591 25.150 16.732 2677.981 2.841 74.422 2.834 0.72 285557. 0.3401
|
|
58.92 0.3456 0.7066 0.0376 0.0184 3.457 24.211 15.548 2578.005 2.735 69.159 2.736 0.72 285914. 0.3165
|
|
62.38 0.3660 0.7213 0.0347 0.0176 3.306 23.155 14.337 2465.535 2.616 63.771 2.637 0.72 286288. 0.2930
|
|
65.85 0.3863 0.7329 0.0317 0.0167 3.138 21.978 13.099 2340.279 2.483 58.265 2.539 0.72 286677. 0.2696
|
|
69.31 0.4066 0.7409 0.0287 0.0157 2.953 20.680 11.837 2201.990 2.336 52.650 2.438 0.72 287082. 0.2461
|
|
72.78 0.4270 0.7447 0.0255 0.0146 2.750 19.257 10.552 2050.471 2.176 46.936 2.334 0.72 287503. 0.2224
|
|
76.24 0.4473 0.7435 0.0224 0.0135 2.529 17.708 9.248 1885.593 2.001 41.133 2.224 0.72 287940. 0.1985
|
|
79.71 0.4676 0.7358 0.0192 0.0122 2.290 16.034 7.926 1707.300 1.812 35.253 2.106 0.72 288393. 0.1739
|
|
83.18 0.4880 0.7191 0.0160 0.0108 2.033 14.234 6.589 1515.636 1.608 29.310 1.972 0.72 288863. 0.1485
|
|
86.64 0.5083 0.6890 0.0127 0.0094 1.758 12.310 5.242 1310.763 1.391 23.317 1.814 0.72 289349. 0.1219
|
|
90.11 0.5286 0.6373 0.0094 0.0078 1.466 10.265 3.888 1092.976 1.160 17.292 1.613 0.72 289851. 0.0933
|
|
93.57 0.5490 0.5456 0.0061 0.0062 1.157 8.102 2.530 862.704 0.915 11.251 1.330 0.72 290369. 0.0621
|
|
97.04 0.5693 0.3639 0.0028 0.0044 0.831 5.823 1.169 620.019 0.658 5.201 0.855 0.73 290897. 0.0271
|
|
100.50 0.5896
|
|
|
|
|
|
|
|
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 0.0759 0.0228 5.869 36.991 38.682 4376.530 4.179 172.057 4.009 0.79 313024. 0.7315
|
|
3.84 0.0203 0.0658 0.0746 0.0230 5.912 37.264 38.022 4408.713 4.210 169.124 3.912 0.79 313183. 0.7077
|
|
7.67 0.0405 0.1284 0.0732 0.0231 5.948 37.487 37.306 4435.202 4.235 165.938 3.815 0.79 313354. 0.6837
|
|
11.51 0.0608 0.1877 0.0716 0.0232 5.974 37.656 36.532 4455.181 4.254 162.496 3.719 0.79 313539. 0.6595
|
|
15.35 0.0810 0.2439 0.0700 0.0233 5.992 37.764 35.700 4467.904 4.267 158.794 3.624 0.79 313736. 0.6353
|
|
19.19 0.1013 0.2969 0.0683 0.0233 5.998 37.804 34.809 4472.640 4.271 154.831 3.530 0.79 313947. 0.6110
|
|
23.02 0.1216 0.3469 0.0664 0.0233 5.993 37.770 33.860 4468.688 4.267 150.608 3.437 0.79 314171. 0.5867
|
|
26.86 0.1418 0.3938 0.0644 0.0232 5.975 37.658 32.852 4455.359 4.255 146.128 3.344 0.79 314410. 0.5624
|
|
30.70 0.1621 0.4378 0.0623 0.0231 5.943 37.460 31.788 4431.984 4.232 141.395 3.253 0.79 314663. 0.5381
|
|
34.53 0.1823 0.4789 0.0601 0.0229 5.898 37.172 30.669 4397.892 4.200 136.416 3.163 0.79 314932. 0.5139
|
|
38.37 0.2026 0.5171 0.0578 0.0227 5.837 36.788 29.496 4352.427 4.156 131.198 3.074 0.79 315215. 0.4898
|
|
42.21 0.2229 0.5525 0.0554 0.0224 5.760 36.301 28.271 4294.884 4.101 125.749 2.986 0.80 315514. 0.4657
|
|
46.05 0.2431 0.5851 0.0529 0.0220 5.665 35.707 26.996 4224.580 4.034 120.077 2.898 0.80 315828. 0.4418
|
|
49.88 0.2634 0.6150 0.0503 0.0216 5.553 34.999 25.673 4140.828 3.954 114.193 2.812 0.80 316159. 0.4180
|
|
53.72 0.2836 0.6421 0.0477 0.0211 5.422 34.172 24.304 4042.918 3.861 108.106 2.727 0.80 316505. 0.3944
|
|
57.56 0.3039 0.6666 0.0449 0.0205 5.270 33.218 22.892 3930.135 3.753 101.824 2.642 0.80 316868. 0.3709
|
|
61.39 0.3242 0.6884 0.0420 0.0198 5.098 32.134 21.439 3801.787 3.630 95.359 2.558 0.80 317248. 0.3474
|
|
65.23 0.3444 0.7074 0.0391 0.0190 4.904 30.911 19.946 3657.194 3.492 88.720 2.474 0.80 317645. 0.3241
|
|
69.07 0.3647 0.7235 0.0361 0.0182 4.688 29.547 18.416 3495.712 3.338 81.916 2.390 0.80 318059. 0.3009
|
|
72.91 0.3849 0.7366 0.0331 0.0173 4.448 28.034 16.852 3316.772 3.167 74.960 2.305 0.80 318490. 0.2776
|
|
76.74 0.4052 0.7462 0.0299 0.0162 4.184 26.371 15.256 3120.014 2.979 67.861 2.218 0.80 318939. 0.2542
|
|
80.58 0.4255 0.7517 0.0267 0.0151 3.896 24.558 13.631 2905.533 2.775 60.631 2.128 0.80 319405. 0.2305
|
|
84.42 0.4457 0.7523 0.0235 0.0139 3.584 22.592 11.979 2672.930 2.552 53.284 2.033 0.80 319889. 0.2064
|
|
88.25 0.4660 0.7464 0.0202 0.0126 3.249 20.476 10.304 2422.573 2.313 45.834 1.929 0.80 320391. 0.1817
|
|
92.09 0.4862 0.7317 0.0169 0.0112 2.890 18.213 8.610 2154.786 2.058 38.297 1.812 0.80 320910. 0.1560
|
|
95.93 0.5065 0.7037 0.0135 0.0097 2.508 15.809 6.900 1870.339 1.786 30.690 1.673 0.80 321448. 0.1289
|
|
99.77 0.5268 0.6542 0.0102 0.0082 2.106 13.273 5.178 1570.305 1.500 23.034 1.496 0.80 322003. 0.0999
|
|
103.60 0.5470 0.5659 0.0068 0.0065 1.684 10.617 3.451 1256.094 1.199 15.349 1.246 0.81 322575. 0.0679
|
|
107.44 0.5673 0.3955 0.0034 0.0048 1.245 7.849 1.719 928.622 0.887 7.647 0.840 0.81 323159. 0.0323
|
|
111.28 0.5875
|
|
|
|
|
|
|
|
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 0.0778 0.0277 9.510 54.489 47.992 7091.416 6.156 213.467 3.070 0.87 344272. 0.6239
|
|
4.29 0.0206 0.0568 0.0765 0.0277 9.510 54.492 47.218 7091.729 6.156 210.024 3.020 0.87 344450. 0.6088
|
|
8.58 0.0412 0.1118 0.0752 0.0277 9.494 54.400 46.367 7079.801 6.146 206.242 2.971 0.87 344643. 0.5934
|
|
12.87 0.0618 0.1649 0.0736 0.0276 9.461 54.209 45.439 7054.886 6.124 202.114 2.921 0.87 344850. 0.5777
|
|
17.16 0.0824 0.2161 0.0720 0.0275 9.409 53.913 44.432 7016.406 6.091 197.632 2.872 0.87 345073. 0.5617
|
|
21.45 0.1030 0.2655 0.0703 0.0272 9.339 53.510 43.344 6963.929 6.046 192.794 2.823 0.87 345311. 0.5453
|
|
25.74 0.1236 0.3130 0.0684 0.0270 9.249 52.997 42.176 6897.176 5.988 187.601 2.774 0.87 345566. 0.5285
|
|
30.03 0.1442 0.3586 0.0663 0.0267 9.140 52.373 40.930 6815.963 5.917 182.056 2.724 0.87 345837. 0.5112
|
|
34.33 0.1648 0.4023 0.0642 0.0263 9.012 51.637 39.606 6720.189 5.834 176.168 2.673 0.87 346124. 0.4936
|
|
38.62 0.1854 0.4439 0.0619 0.0259 8.864 50.788 38.207 6609.729 5.738 169.944 2.622 0.87 346429. 0.4755
|
|
42.91 0.2060 0.4833 0.0595 0.0254 8.696 49.825 36.735 6484.425 5.629 163.397 2.570 0.87 346751. 0.4569
|
|
47.20 0.2265 0.5206 0.0570 0.0248 8.507 48.747 35.193 6344.019 5.507 156.537 2.516 0.87 347091. 0.4379
|
|
51.49 0.2471 0.5556 0.0544 0.0242 8.298 47.549 33.583 6188.122 5.372 149.378 2.462 0.88 347449. 0.4185
|
|
55.78 0.2677 0.5883 0.0517 0.0235 8.068 46.227 31.909 6016.183 5.223 141.932 2.406 0.88 347825. 0.3987
|
|
60.07 0.2883 0.6185 0.0489 0.0228 7.815 44.778 30.173 5827.512 5.059 134.211 2.348 0.88 348219. 0.3785
|
|
64.36 0.3089 0.6461 0.0460 0.0220 7.538 43.193 28.379 5621.264 4.880 126.231 2.290 0.88 348632. 0.3579
|
|
68.65 0.3295 0.6711 0.0430 0.0211 7.237 41.467 26.529 5396.583 4.685 118.002 2.230 0.88 349065. 0.3369
|
|
72.94 0.3501 0.6932 0.0399 0.0202 6.910 39.592 24.627 5152.590 4.473 109.541 2.168 0.88 349516. 0.3156
|
|
77.23 0.3707 0.7124 0.0368 0.0191 6.555 37.562 22.676 4888.414 4.244 100.862 2.104 0.88 349987. 0.2939
|
|
81.52 0.3913 0.7282 0.0335 0.0180 6.173 35.370 20.679 4603.189 3.996 91.979 2.038 0.88 350477. 0.2718
|
|
85.81 0.4119 0.7404 0.0302 0.0168 5.761 33.010 18.640 4296.077 3.730 82.910 1.968 0.88 350987. 0.2493
|
|
90.10 0.4325 0.7462 0.0268 0.0156 5.332 30.554 16.561 3976.371 3.452 73.665 1.889 0.88 351517. 0.2255
|
|
94.40 0.4531 0.7416 0.0234 0.0143 4.903 28.093 14.446 3656.122 3.174 64.254 1.792 0.88 352067. 0.1998
|
|
98.69 0.4737 0.7274 0.0199 0.0130 4.449 25.495 12.299 3317.952 2.880 54.706 1.681 0.88 352637. 0.1730
|
|
102.98 0.4943 0.6994 0.0164 0.0116 3.976 22.781 10.127 2964.748 2.574 45.043 1.549 0.88 353227. 0.1446
|
|
107.27 0.5149 0.6515 0.0129 0.0102 3.483 19.959 7.934 2597.490 2.255 35.291 1.385 0.88 353837. 0.1145
|
|
111.56 0.5355 0.5726 0.0093 0.0087 2.976 17.052 5.728 2219.206 1.927 25.479 1.171 0.89 354467. 0.0822
|
|
115.85 0.5561 0.4417 0.0057 0.0072 2.458 14.084 3.515 1832.934 1.591 15.634 0.870 0.89 355115. 0.0478
|
|
120.14 0.5767 0.2141 0.0021 0.0056 1.930 11.060 1.290 1439.416 1.250 5.739 0.407 0.89 355771. 0.0136
|
|
124.43 0.5973
|
|
|
|
|
|
|
|
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 0.0775 0.0336 14.961 78.579 56.917 11156.203 8.878 253.166 2.314 0.95 375578. 0.5122
|
|
4.71 0.0207 0.0471 0.0765 0.0337 14.988 78.725 56.134 11176.902 8.894 249.685 2.278 0.95 375768. 0.5007
|
|
9.43 0.0415 0.0926 0.0753 0.0337 14.993 78.748 55.266 11180.207 8.897 245.823 2.242 0.95 375975. 0.4890
|
|
14.14 0.0622 0.1368 0.0740 0.0336 14.970 78.630 54.308 11163.362 8.884 241.560 2.207 0.95 376198. 0.4771
|
|
18.85 0.0829 0.1795 0.0725 0.0335 14.917 78.350 53.254 11123.676 8.852 236.875 2.171 0.95 376438. 0.4649
|
|
23.56 0.1037 0.2208 0.0710 0.0333 14.830 77.891 52.103 11058.513 8.800 231.753 2.137 0.95 376696. 0.4526
|
|
28.28 0.1244 0.2607 0.0693 0.0330 14.705 77.235 50.849 10965.348 8.726 226.177 2.103 0.95 376972. 0.4400
|
|
32.99 0.1452 0.2995 0.0674 0.0327 14.539 76.365 49.492 10841.917 8.628 220.140 2.070 0.95 377267. 0.4273
|
|
37.70 0.1659 0.3370 0.0654 0.0322 14.330 75.267 48.028 10685.938 8.504 213.631 2.039 0.95 377581. 0.4145
|
|
42.42 0.1866 0.3733 0.0633 0.0316 14.076 73.932 46.459 10496.363 8.353 206.651 2.008 0.95 377914. 0.4015
|
|
47.13 0.2074 0.4086 0.0610 0.0310 13.776 72.355 44.785 10272.555 8.175 199.204 1.977 0.95 378268. 0.3882
|
|
51.84 0.2281 0.4427 0.0586 0.0302 13.430 70.538 43.007 10014.610 7.969 191.297 1.948 0.95 378642. 0.3748
|
|
56.56 0.2488 0.4757 0.0560 0.0293 13.039 68.488 41.130 9723.475 7.738 182.945 1.919 0.95 379036. 0.3610
|
|
61.27 0.2696 0.5074 0.0533 0.0283 12.607 66.214 39.155 9400.680 7.481 174.163 1.889 0.96 379451. 0.3468
|
|
65.98 0.2903 0.5378 0.0505 0.0273 12.134 63.730 37.089 9048.044 7.200 164.974 1.859 0.96 379888. 0.3322
|
|
70.69 0.3111 0.5666 0.0476 0.0261 11.623 61.049 34.937 8667.412 6.897 155.400 1.828 0.96 380345. 0.3170
|
|
75.41 0.3318 0.5936 0.0445 0.0249 11.077 58.182 32.703 8260.402 6.573 145.465 1.796 0.96 380824. 0.3013
|
|
80.12 0.3525 0.6186 0.0414 0.0236 10.498 55.138 30.394 7828.161 6.229 135.192 1.761 0.96 381324. 0.2848
|
|
84.83 0.3733 0.6411 0.0382 0.0222 9.885 51.921 28.014 7371.381 5.866 124.607 1.724 0.96 381846. 0.2677
|
|
89.55 0.3940 0.6608 0.0348 0.0208 9.240 48.532 25.569 6890.226 5.483 113.733 1.683 0.96 382389. 0.2497
|
|
94.26 0.4147 0.6771 0.0314 0.0192 8.562 44.971 23.065 6384.655 5.081 102.594 1.639 0.96 382954. 0.2309
|
|
98.97 0.4355 0.6882 0.0279 0.0177 7.864 41.304 20.506 5864.076 4.666 91.213 1.586 0.96 383541. 0.2107
|
|
103.68 0.4562 0.6849 0.0244 0.0162 7.223 37.936 17.892 5385.935 4.286 79.585 1.507 0.96 384150. 0.1870
|
|
108.40 0.4769 0.6560 0.0207 0.0151 6.707 35.229 15.223 5001.678 3.980 67.711 1.380 0.96 384782. 0.1580
|
|
113.11 0.4977 0.6091 0.0171 0.0139 6.199 32.560 12.519 4622.688 3.679 55.686 1.228 0.96 385435. 0.1275
|
|
117.82 0.5184 0.5399 0.0133 0.0128 5.699 29.931 9.792 4249.378 3.382 43.554 1.045 0.96 386111. 0.0959
|
|
122.54 0.5392 0.4427 0.0096 0.0117 5.205 27.341 7.052 3881.651 3.089 31.367 0.824 0.97 386808. 0.0642
|
|
127.25 0.5599 0.3098 0.0059 0.0106 4.723 24.807 4.312 3522.000 2.803 19.181 0.555 0.97 387527. 0.0338
|
|
131.96 0.5806 0.1302 0.0021 0.0095 4.244 22.293 1.570 3165.003 2.519 6.985 0.225 0.97 388261. 0.0083
|
|
136.68 0.6014
|
|
|
|
|
|
|