464 lines
82 KiB
Plaintext
464 lines
82 KiB
Plaintext
19x8E (19x8E.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 0.0742 0.0264 0.005 0.332 0.308 3.925 0.037 1.371 35.606 0.08 33326. 0.6104
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0.35 0.0193 0.0530 0.0728 0.0266 0.005 0.334 0.302 3.946 0.038 1.345 34.741 0.08 33343. 0.5899
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0.70 0.0387 0.1034 0.0713 0.0267 0.005 0.335 0.296 3.964 0.038 1.317 33.874 0.08 33361. 0.5692
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1.04 0.0580 0.1511 0.0697 0.0268 0.005 0.336 0.289 3.977 0.038 1.287 33.008 0.08 33380. 0.5484
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1.39 0.0774 0.1962 0.0680 0.0268 0.005 0.337 0.282 3.986 0.038 1.257 32.143 0.08 33400. 0.5276
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1.74 0.0967 0.2386 0.0662 0.0269 0.005 0.337 0.275 3.990 0.038 1.224 31.279 0.08 33422. 0.5067
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2.09 0.1161 0.2785 0.0644 0.0268 0.005 0.337 0.267 3.987 0.038 1.189 30.416 0.08 33444. 0.4857
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2.44 0.1354 0.3156 0.0624 0.0268 0.005 0.336 0.259 3.979 0.038 1.153 29.553 0.08 33469. 0.4647
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2.78 0.1548 0.3502 0.0604 0.0267 0.005 0.335 0.251 3.963 0.038 1.115 28.690 0.08 33494. 0.4436
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3.13 0.1741 0.3821 0.0582 0.0265 0.005 0.333 0.242 3.941 0.038 1.075 27.825 0.08 33521. 0.4225
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3.48 0.1934 0.4113 0.0559 0.0263 0.005 0.330 0.232 3.910 0.037 1.034 26.956 0.08 33550. 0.4013
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3.83 0.2128 0.4378 0.0536 0.0260 0.005 0.327 0.223 3.870 0.037 0.990 26.081 0.08 33580. 0.3800
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4.18 0.2321 0.4614 0.0511 0.0257 0.005 0.323 0.212 3.822 0.036 0.944 25.198 0.08 33612. 0.3586
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4.52 0.2515 0.4821 0.0486 0.0253 0.005 0.318 0.202 3.764 0.036 0.897 24.303 0.08 33645. 0.3370
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4.87 0.2708 0.4997 0.0459 0.0249 0.005 0.312 0.191 3.696 0.035 0.848 23.393 0.08 33679. 0.3154
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5.22 0.2902 0.5141 0.0432 0.0244 0.005 0.306 0.179 3.619 0.035 0.797 22.462 0.08 33716. 0.2937
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5.57 0.3095 0.5250 0.0403 0.0238 0.005 0.299 0.168 3.533 0.034 0.745 21.505 0.08 33754. 0.2718
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5.92 0.3288 0.5322 0.0374 0.0231 0.005 0.291 0.156 3.438 0.033 0.692 20.517 0.08 33793. 0.2499
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6.26 0.3482 0.5353 0.0345 0.0224 0.004 0.282 0.143 3.333 0.032 0.637 19.489 0.08 33835. 0.2278
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6.61 0.3675 0.5338 0.0315 0.0217 0.004 0.272 0.131 3.219 0.031 0.581 18.412 0.08 33878. 0.2055
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6.96 0.3869 0.5272 0.0284 0.0208 0.004 0.262 0.118 3.096 0.030 0.524 17.275 0.08 33922. 0.1832
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7.31 0.4062 0.5147 0.0253 0.0199 0.004 0.250 0.105 2.963 0.028 0.467 16.063 0.08 33969. 0.1607
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7.66 0.4256 0.4955 0.0221 0.0190 0.004 0.238 0.092 2.821 0.027 0.408 14.760 0.08 34017. 0.1381
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8.01 0.4449 0.4682 0.0189 0.0180 0.004 0.226 0.079 2.671 0.026 0.349 13.342 0.08 34067. 0.1155
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8.35 0.4643 0.4314 0.0157 0.0169 0.003 0.212 0.065 2.512 0.024 0.290 11.780 0.08 34119. 0.0929
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8.70 0.4836 0.3828 0.0125 0.0158 0.003 0.198 0.052 2.345 0.022 0.231 10.036 0.08 34172. 0.0706
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9.05 0.5029 0.3197 0.0093 0.0146 0.003 0.184 0.039 2.171 0.021 0.172 8.058 0.08 34227. 0.0489
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9.40 0.5223 0.2379 0.0061 0.0134 0.003 0.168 0.025 1.990 0.019 0.113 5.774 0.08 34284. 0.0284
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9.75 0.5416 0.1316 0.0029 0.0121 0.002 0.152 0.012 1.803 0.017 0.054 3.080 0.08 34343. 0.0105
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10.09 0.5610 -0.0086 -0.0002 0.0108 0.002 0.136 -0.001 1.610 0.015 -0.003 -0.195 0.08 34403. 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 0.0745 0.0242 0.039 1.214 1.238 28.722 0.137 5.505 19.543 0.15 66652. 0.6714
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0.71 0.0197 0.0591 0.0731 0.0243 0.039 1.222 1.214 28.919 0.138 5.398 19.035 0.15 66686. 0.6476
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1.42 0.0394 0.1151 0.0715 0.0245 0.039 1.229 1.188 29.087 0.139 5.285 18.529 0.15 66722. 0.6238
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2.13 0.0591 0.1680 0.0699 0.0246 0.039 1.235 1.161 29.220 0.140 5.166 18.028 0.15 66761. 0.6000
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2.83 0.0787 0.2178 0.0682 0.0247 0.039 1.239 1.133 29.313 0.140 5.039 17.530 0.15 66803. 0.5762
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3.54 0.0984 0.2646 0.0664 0.0247 0.039 1.241 1.103 29.361 0.140 4.905 17.037 0.15 66847. 0.5525
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4.25 0.1181 0.3084 0.0645 0.0247 0.039 1.241 1.071 29.359 0.140 4.765 16.549 0.15 66893. 0.5289
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4.96 0.1378 0.3492 0.0625 0.0247 0.039 1.238 1.038 29.302 0.140 4.616 16.064 0.15 66943. 0.5054
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5.67 0.1575 0.3872 0.0604 0.0246 0.039 1.233 1.003 29.186 0.139 4.460 15.584 0.15 66996. 0.4819
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6.38 0.1772 0.4222 0.0581 0.0244 0.039 1.226 0.966 29.004 0.138 4.297 15.106 0.15 67051. 0.4585
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7.08 0.1969 0.4544 0.0558 0.0242 0.039 1.215 0.927 28.752 0.137 4.125 14.631 0.15 67110. 0.4352
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7.79 0.2166 0.4836 0.0534 0.0239 0.038 1.201 0.887 28.425 0.136 3.946 14.157 0.15 67172. 0.4118
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8.50 0.2362 0.5099 0.0509 0.0236 0.038 1.184 0.845 28.016 0.134 3.759 13.682 0.15 67237. 0.3885
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9.21 0.2559 0.5332 0.0482 0.0232 0.037 1.163 0.801 27.525 0.131 3.565 13.206 0.15 67305. 0.3651
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9.92 0.2756 0.5533 0.0455 0.0227 0.036 1.139 0.756 26.951 0.129 3.363 12.725 0.15 67376. 0.3417
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10.63 0.2953 0.5701 0.0427 0.0221 0.035 1.111 0.709 26.293 0.126 3.155 12.238 0.15 67451. 0.3183
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11.33 0.3150 0.5834 0.0398 0.0215 0.034 1.080 0.661 25.551 0.122 2.942 11.740 0.15 67529. 0.2949
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12.04 0.3347 0.5929 0.0368 0.0208 0.033 1.045 0.612 24.724 0.118 2.723 11.229 0.15 67611. 0.2713
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12.75 0.3544 0.5981 0.0338 0.0200 0.032 1.006 0.562 23.813 0.114 2.499 10.700 0.15 67696. 0.2477
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13.46 0.3740 0.5987 0.0307 0.0192 0.031 0.964 0.510 22.817 0.109 2.270 10.146 0.15 67785. 0.2238
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14.17 0.3937 0.5938 0.0276 0.0183 0.029 0.919 0.458 21.738 0.104 2.038 9.560 0.15 67877. 0.1998
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14.88 0.4134 0.5827 0.0244 0.0173 0.028 0.870 0.405 20.574 0.098 1.803 8.934 0.15 67973. 0.1756
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15.59 0.4331 0.5639 0.0212 0.0163 0.026 0.817 0.352 19.330 0.092 1.565 8.254 0.15 68072. 0.1512
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16.29 0.4528 0.5359 0.0179 0.0151 0.024 0.761 0.298 18.006 0.086 1.325 7.502 0.15 68176. 0.1264
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17.00 0.4725 0.4961 0.0147 0.0140 0.022 0.702 0.244 16.606 0.079 1.084 6.656 0.15 68282. 0.1015
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17.71 0.4922 0.4411 0.0114 0.0127 0.020 0.640 0.190 15.134 0.072 0.843 5.682 0.15 68393. 0.0764
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18.42 0.5118 0.3655 0.0082 0.0114 0.018 0.575 0.136 13.597 0.065 0.604 4.527 0.15 68507. 0.0515
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19.13 0.5315 0.2609 0.0050 0.0101 0.016 0.507 0.082 12.001 0.057 0.366 3.111 0.15 68625. 0.0276
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19.84 0.5512 0.1131 0.0018 0.0087 0.014 0.437 0.030 10.352 0.049 0.132 1.301 0.15 68746. 0.0069
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20.54 0.5709
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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 0.0748 0.0232 0.125 2.627 2.797 93.248 0.297 12.442 13.606 0.23 99976. 0.7028
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1.06 0.0196 0.0613 0.0734 0.0234 0.126 2.647 2.744 93.949 0.299 12.204 13.246 0.23 100027. 0.6776
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2.11 0.0391 0.1194 0.0719 0.0236 0.127 2.664 2.687 94.549 0.301 11.951 12.889 0.23 100081. 0.6525
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3.17 0.0587 0.1742 0.0703 0.0237 0.127 2.677 2.627 95.031 0.302 11.683 12.536 0.23 100139. 0.6274
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4.23 0.0783 0.2258 0.0686 0.0238 0.128 2.687 2.563 95.379 0.304 11.400 12.187 0.23 100201. 0.6025
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5.28 0.0979 0.2742 0.0668 0.0238 0.128 2.693 2.496 95.576 0.304 11.100 11.843 0.23 100266. 0.5778
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6.34 0.1174 0.3196 0.0649 0.0238 0.128 2.694 2.425 95.603 0.304 10.785 11.503 0.23 100336. 0.5532
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7.39 0.1370 0.3620 0.0629 0.0238 0.128 2.689 2.350 95.444 0.304 10.453 11.167 0.23 100410. 0.5287
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8.45 0.1566 0.4014 0.0608 0.0237 0.128 2.679 2.271 95.081 0.303 10.104 10.836 0.23 100488. 0.5043
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9.51 0.1761 0.4380 0.0586 0.0236 0.127 2.662 2.189 94.497 0.301 9.738 10.508 0.23 100571. 0.4801
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10.56 0.1957 0.4716 0.0563 0.0233 0.126 2.639 2.103 93.675 0.298 9.354 10.183 0.23 100658. 0.4560
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11.62 0.2153 0.5023 0.0539 0.0231 0.124 2.609 2.013 92.593 0.295 8.953 9.860 0.23 100750. 0.4320
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12.68 0.2348 0.5301 0.0513 0.0227 0.122 2.570 1.919 91.235 0.290 8.535 9.539 0.23 100847. 0.4081
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13.73 0.2544 0.5550 0.0487 0.0223 0.120 2.524 1.821 89.593 0.285 8.099 9.218 0.23 100948. 0.3842
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14.79 0.2740 0.5768 0.0460 0.0219 0.118 2.470 1.720 87.665 0.279 7.649 8.897 0.23 101055. 0.3603
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15.85 0.2936 0.5955 0.0432 0.0213 0.115 2.407 1.615 85.448 0.272 7.183 8.573 0.23 101166. 0.3364
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16.90 0.3131 0.6108 0.0403 0.0207 0.111 2.337 1.507 82.940 0.264 6.705 8.244 0.23 101282. 0.3126
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17.96 0.3327 0.6226 0.0374 0.0200 0.107 2.258 1.397 80.139 0.255 6.215 7.908 0.23 101404. 0.2887
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19.01 0.3523 0.6303 0.0344 0.0192 0.103 2.171 1.284 77.044 0.245 5.713 7.562 0.23 101530. 0.2647
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20.07 0.3718 0.6337 0.0313 0.0184 0.099 2.075 1.169 73.655 0.234 5.202 7.202 0.23 101662. 0.2405
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21.13 0.3914 0.6320 0.0282 0.0174 0.094 1.971 1.053 69.972 0.223 4.682 6.823 0.23 101799. 0.2162
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22.18 0.4110 0.6243 0.0250 0.0165 0.089 1.859 0.934 65.999 0.210 4.155 6.419 0.23 101941. 0.1916
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23.24 0.4305 0.6094 0.0218 0.0154 0.083 1.739 0.814 61.740 0.197 3.622 5.982 0.23 102089. 0.1667
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24.30 0.4501 0.5857 0.0186 0.0143 0.077 1.612 0.693 57.204 0.182 3.085 5.499 0.23 102242. 0.1414
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25.35 0.4697 0.5505 0.0153 0.0131 0.070 1.476 0.572 52.401 0.167 2.545 4.953 0.23 102400. 0.1157
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26.41 0.4893 0.5001 0.0121 0.0118 0.063 1.334 0.451 47.346 0.151 2.006 4.320 0.23 102564. 0.0896
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27.47 0.5088 0.4286 0.0088 0.0105 0.056 1.185 0.330 42.058 0.134 1.468 3.560 0.23 102734. 0.0632
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28.52 0.5284 0.3262 0.0056 0.0091 0.049 1.030 0.210 36.561 0.116 0.935 2.609 0.23 102909. 0.0370
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29.58 0.5480 0.1756 0.0025 0.0077 0.041 0.870 0.092 30.879 0.098 0.410 1.354 0.23 103088. 0.0127
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30.63 0.5675
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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 0.0753 0.0228 0.291 4.579 5.002 216.710 0.517 22.249 10.469 0.30 133297. 0.7231
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1.40 0.0194 0.0625 0.0738 0.0230 0.293 4.615 4.907 218.413 0.521 21.827 10.191 0.30 133365. 0.6971
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2.80 0.0389 0.1217 0.0723 0.0231 0.295 4.646 4.806 219.878 0.525 21.379 9.915 0.30 133437. 0.6713
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4.20 0.0583 0.1775 0.0707 0.0232 0.296 4.671 4.700 221.064 0.528 20.904 9.643 0.30 133514. 0.6456
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5.60 0.0778 0.2301 0.0690 0.0233 0.298 4.690 4.587 221.930 0.530 20.402 9.374 0.30 133596. 0.6200
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7.00 0.0972 0.2795 0.0672 0.0234 0.298 4.700 4.468 222.437 0.531 19.872 9.110 0.30 133683. 0.5947
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8.40 0.1167 0.3258 0.0653 0.0234 0.298 4.702 4.342 222.542 0.531 19.313 8.850 0.30 133775. 0.5695
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9.80 0.1361 0.3691 0.0634 0.0234 0.298 4.695 4.210 222.205 0.530 18.725 8.593 0.30 133873. 0.5445
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11.20 0.1556 0.4094 0.0613 0.0233 0.297 4.678 4.071 221.385 0.529 18.107 8.340 0.30 133977. 0.5197
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12.60 0.1750 0.4468 0.0591 0.0231 0.295 4.650 3.925 220.039 0.525 17.459 8.091 0.30 134086. 0.4950
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14.00 0.1945 0.4813 0.0568 0.0229 0.293 4.609 3.773 218.126 0.521 16.781 7.845 0.30 134202. 0.4706
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15.40 0.2139 0.5130 0.0544 0.0227 0.289 4.556 3.613 215.598 0.515 16.071 7.601 0.30 134323. 0.4462
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16.79 0.2334 0.5418 0.0519 0.0223 0.285 4.488 3.446 212.412 0.507 15.330 7.359 0.30 134451. 0.4219
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18.19 0.2528 0.5678 0.0493 0.0219 0.280 4.407 3.273 208.548 0.498 14.559 7.119 0.30 134585. 0.3977
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19.59 0.2723 0.5908 0.0466 0.0215 0.274 4.311 3.094 203.997 0.487 13.760 6.878 0.30 134726. 0.3736
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20.99 0.2917 0.6108 0.0438 0.0209 0.267 4.200 2.908 198.754 0.474 12.937 6.637 0.30 134873. 0.3496
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22.39 0.3111 0.6277 0.0409 0.0203 0.259 4.074 2.718 192.813 0.460 12.089 6.394 0.30 135026. 0.3255
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23.79 0.3306 0.6410 0.0380 0.0196 0.250 3.934 2.523 186.168 0.444 11.220 6.146 0.30 135187. 0.3014
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25.19 0.3500 0.6507 0.0350 0.0188 0.240 3.778 2.323 178.816 0.427 10.332 5.892 0.30 135354. 0.2773
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26.59 0.3695 0.6562 0.0319 0.0180 0.229 3.608 2.119 170.754 0.408 9.425 5.629 0.30 135527. 0.2530
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27.99 0.3889 0.6569 0.0288 0.0170 0.217 3.423 1.912 161.986 0.387 8.504 5.353 0.30 135708. 0.2286
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29.39 0.4084 0.6520 0.0256 0.0160 0.205 3.223 1.702 152.517 0.364 7.569 5.060 0.30 135896. 0.2039
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30.79 0.4278 0.6404 0.0224 0.0150 0.191 3.008 1.489 142.358 0.340 6.623 4.744 0.30 136090. 0.1788
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32.19 0.4473 0.6204 0.0192 0.0138 0.176 2.779 1.275 131.527 0.314 5.670 4.396 0.30 136292. 0.1533
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33.59 0.4667 0.5895 0.0159 0.0126 0.161 2.537 1.060 120.048 0.287 4.713 4.003 0.30 136501. 0.1273
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34.99 0.4862 0.5440 0.0127 0.0114 0.145 2.281 0.844 107.956 0.258 3.755 3.547 0.31 136717. 0.1006
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36.39 0.5056 0.4779 0.0095 0.0100 0.128 2.014 0.629 95.295 0.228 2.800 2.996 0.31 136941. 0.0734
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37.79 0.5251 0.3811 0.0063 0.0086 0.110 1.735 0.417 82.120 0.196 1.853 2.300 0.31 137171. 0.0459
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39.19 0.5445 0.2347 0.0031 0.0072 0.092 1.447 0.206 68.494 0.164 0.918 1.366 0.31 137408. 0.0192
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40.59 0.5639 -0.0029 0.0000 0.0057 0.073 1.148 -0.002 54.350 0.130 -0.009 -0.017 0.31 137642. 0.0000
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PROP RPM = 5000
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V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
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(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
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0.00 0.0000 0.0000 0.0758 0.0226 0.562 7.090 7.874 419.443 0.801 35.024 8.515 0.38 166615. 0.7379
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1.75 0.0195 0.0636 0.0744 0.0228 0.567 7.148 7.725 422.840 0.808 34.361 8.286 0.38 166700. 0.7113
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3.50 0.0389 0.1237 0.0729 0.0229 0.571 7.197 7.567 425.762 0.813 33.656 8.061 0.38 166790. 0.6848
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5.25 0.0584 0.1805 0.0713 0.0231 0.574 7.237 7.399 428.128 0.818 32.910 7.839 0.38 166887. 0.6585
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7.00 0.0778 0.2339 0.0696 0.0231 0.576 7.267 7.221 429.858 0.821 32.121 7.620 0.38 166990. 0.6324
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8.75 0.0973 0.2842 0.0677 0.0232 0.578 7.284 7.034 430.871 0.823 31.287 7.404 0.38 167099. 0.6065
|
|
10.50 0.1168 0.3312 0.0658 0.0232 0.578 7.287 6.836 431.084 0.823 30.408 7.193 0.38 167215. 0.5808
|
|
12.26 0.1362 0.3753 0.0638 0.0232 0.577 7.276 6.628 430.416 0.822 29.482 6.985 0.38 167338. 0.5553
|
|
14.01 0.1557 0.4163 0.0617 0.0231 0.575 7.248 6.409 428.784 0.819 28.509 6.780 0.38 167468. 0.5301
|
|
15.76 0.1751 0.4544 0.0595 0.0229 0.571 7.203 6.180 426.106 0.814 27.489 6.578 0.38 167605. 0.5050
|
|
17.51 0.1946 0.4897 0.0572 0.0227 0.566 7.139 5.940 422.296 0.807 26.420 6.380 0.38 167750. 0.4802
|
|
19.26 0.2141 0.5221 0.0548 0.0225 0.560 7.054 5.689 417.261 0.797 25.303 6.184 0.38 167903. 0.4555
|
|
21.01 0.2335 0.5516 0.0523 0.0221 0.551 6.946 5.426 410.914 0.785 24.135 5.989 0.38 168063. 0.4309
|
|
22.76 0.2530 0.5784 0.0496 0.0217 0.541 6.816 5.153 403.214 0.770 22.921 5.797 0.38 168231. 0.4064
|
|
24.51 0.2725 0.6022 0.0469 0.0212 0.529 6.663 4.870 394.143 0.753 21.663 5.604 0.38 168407. 0.3820
|
|
26.26 0.2919 0.6231 0.0441 0.0207 0.515 6.486 4.578 383.689 0.733 20.364 5.412 0.38 168591. 0.3576
|
|
28.01 0.3114 0.6408 0.0412 0.0200 0.499 6.286 4.278 371.837 0.710 19.029 5.218 0.38 168784. 0.3333
|
|
29.76 0.3308 0.6552 0.0382 0.0193 0.481 6.062 3.970 358.578 0.685 17.659 5.022 0.38 168984. 0.3090
|
|
31.51 0.3503 0.6660 0.0352 0.0185 0.461 5.814 3.655 343.903 0.657 16.258 4.821 0.38 169194. 0.2846
|
|
33.26 0.3698 0.6727 0.0321 0.0176 0.440 5.541 3.334 327.810 0.626 14.830 4.613 0.38 169411. 0.2601
|
|
35.01 0.3892 0.6748 0.0290 0.0167 0.416 5.245 3.007 310.302 0.593 13.377 4.396 0.38 169638. 0.2354
|
|
36.77 0.4087 0.6714 0.0258 0.0157 0.391 4.926 2.676 291.390 0.557 11.903 4.166 0.38 169873. 0.2104
|
|
38.52 0.4281 0.6614 0.0225 0.0146 0.364 4.583 2.341 271.098 0.518 10.414 3.917 0.38 170117. 0.1851
|
|
40.27 0.4476 0.6431 0.0193 0.0134 0.335 4.217 2.004 249.460 0.476 8.912 3.643 0.38 170369. 0.1592
|
|
42.02 0.4671 0.6138 0.0160 0.0122 0.304 3.829 1.664 226.527 0.433 7.403 3.332 0.38 170631. 0.1328
|
|
43.77 0.4865 0.5698 0.0128 0.0109 0.271 3.421 1.325 202.367 0.386 5.893 2.969 0.38 170902. 0.1055
|
|
45.52 0.5060 0.5043 0.0095 0.0095 0.237 2.993 0.987 177.071 0.338 4.388 2.527 0.38 171181. 0.0775
|
|
47.27 0.5254 0.4060 0.0063 0.0081 0.202 2.548 0.651 150.750 0.288 2.896 1.959 0.38 171470. 0.0488
|
|
49.02 0.5449 0.2526 0.0031 0.0067 0.166 2.088 0.320 123.531 0.236 1.424 1.175 0.38 171766. 0.0205
|
|
50.77 0.5644 -0.0093 -0.0001 0.0051 0.128 1.609 -0.009 95.211 0.182 -0.039 -0.042 0.38 172055. 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 0.0765 0.0225 0.970 10.194 11.444 723.677 1.152 50.901 7.172 0.45 199928. 0.7493
|
|
2.10 0.0195 0.0643 0.0751 0.0227 0.978 10.278 11.228 729.631 1.161 49.941 6.980 0.45 200030. 0.7223
|
|
4.20 0.0389 0.1251 0.0736 0.0229 0.985 10.350 10.998 734.749 1.169 48.920 6.789 0.45 200139. 0.6954
|
|
6.30 0.0584 0.1824 0.0719 0.0230 0.991 10.409 10.755 738.883 1.176 47.839 6.602 0.45 200256. 0.6687
|
|
8.40 0.0778 0.2364 0.0702 0.0231 0.995 10.451 10.498 741.895 1.181 46.694 6.418 0.45 200380. 0.6422
|
|
10.50 0.0973 0.2872 0.0684 0.0232 0.997 10.476 10.226 743.641 1.184 45.485 6.237 0.45 200511. 0.6159
|
|
12.61 0.1168 0.3348 0.0665 0.0232 0.998 10.480 9.939 743.977 1.184 44.209 6.059 0.45 200651. 0.5899
|
|
14.71 0.1362 0.3794 0.0645 0.0231 0.996 10.463 9.637 742.758 1.182 42.865 5.885 0.45 200799. 0.5642
|
|
16.81 0.1557 0.4210 0.0623 0.0231 0.992 10.422 9.320 739.840 1.177 41.453 5.713 0.45 200956. 0.5387
|
|
18.91 0.1751 0.4596 0.0601 0.0229 0.986 10.355 8.986 735.079 1.170 39.972 5.545 0.45 201121. 0.5133
|
|
21.01 0.1946 0.4954 0.0578 0.0227 0.977 10.260 8.637 728.324 1.159 38.419 5.379 0.45 201295. 0.4882
|
|
23.11 0.2141 0.5284 0.0553 0.0224 0.965 10.134 8.272 719.413 1.145 36.795 5.215 0.45 201479. 0.4633
|
|
25.21 0.2335 0.5586 0.0528 0.0221 0.950 9.976 7.891 708.193 1.127 35.099 5.054 0.45 201671. 0.4384
|
|
27.31 0.2530 0.5859 0.0501 0.0216 0.931 9.785 7.494 694.586 1.105 33.334 4.894 0.45 201874. 0.4137
|
|
29.41 0.2724 0.6105 0.0474 0.0211 0.910 9.559 7.083 678.561 1.080 31.505 4.734 0.45 202085. 0.3891
|
|
31.51 0.2919 0.6321 0.0445 0.0206 0.885 9.299 6.659 660.094 1.051 29.617 4.575 0.45 202307. 0.3646
|
|
33.61 0.3114 0.6506 0.0416 0.0199 0.857 9.004 6.222 639.163 1.017 27.675 4.415 0.45 202538. 0.3401
|
|
35.71 0.3308 0.6659 0.0386 0.0192 0.826 8.674 5.774 615.747 0.980 25.683 4.253 0.45 202779. 0.3156
|
|
37.82 0.3503 0.6777 0.0356 0.0184 0.791 8.309 5.316 589.834 0.939 23.646 4.088 0.46 203031. 0.2911
|
|
39.92 0.3697 0.6855 0.0324 0.0175 0.753 7.909 4.849 561.417 0.894 21.568 3.917 0.46 203292. 0.2664
|
|
42.02 0.3892 0.6888 0.0293 0.0165 0.711 7.473 4.374 530.503 0.844 19.454 3.739 0.46 203564. 0.2415
|
|
44.12 0.4087 0.6868 0.0260 0.0155 0.667 7.003 3.892 497.111 0.791 17.311 3.551 0.46 203846. 0.2163
|
|
46.22 0.4281 0.6783 0.0228 0.0144 0.619 6.498 3.404 461.283 0.734 15.143 3.347 0.46 204139. 0.1907
|
|
48.32 0.4476 0.6615 0.0195 0.0132 0.567 5.960 2.913 423.080 0.673 12.957 3.123 0.46 204443. 0.1646
|
|
50.42 0.4671 0.6340 0.0162 0.0119 0.513 5.390 2.419 382.591 0.609 10.762 2.868 0.46 204757. 0.1378
|
|
52.52 0.4865 0.5915 0.0129 0.0106 0.456 4.789 1.925 339.939 0.541 8.564 2.569 0.46 205082. 0.1101
|
|
54.62 0.5060 0.5272 0.0096 0.0092 0.396 4.160 1.433 295.283 0.470 6.375 2.202 0.46 205417. 0.0814
|
|
56.72 0.5254 0.4284 0.0063 0.0078 0.334 3.505 0.945 248.824 0.396 4.204 1.723 0.46 205763. 0.0517
|
|
58.82 0.5449 0.2700 0.0031 0.0063 0.269 2.828 0.463 200.784 0.320 2.062 1.047 0.46 206120. 0.0220
|
|
60.92 0.5644 -0.0127 -0.0001 0.0047 0.202 2.123 -0.016 150.714 0.240 -0.070 -0.048 0.46 206463. 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 0.0774 0.0227 1.548 13.940 15.752 1154.513 1.575 70.067 6.189 0.53 233235. 0.7585
|
|
2.45 0.0195 0.0647 0.0760 0.0228 1.561 14.056 15.457 1164.076 1.588 68.751 6.023 0.53 233355. 0.7312
|
|
4.90 0.0389 0.1259 0.0744 0.0230 1.572 14.155 15.142 1172.271 1.599 67.352 5.859 0.53 233483. 0.7041
|
|
7.35 0.0584 0.1836 0.0728 0.0231 1.581 14.234 14.809 1178.866 1.608 65.869 5.698 0.53 233619. 0.6771
|
|
9.80 0.0778 0.2380 0.0710 0.0232 1.587 14.292 14.456 1183.634 1.615 64.299 5.539 0.53 233764. 0.6504
|
|
12.25 0.0973 0.2892 0.0692 0.0233 1.591 14.325 14.082 1186.343 1.618 62.638 5.384 0.53 233919. 0.6240
|
|
14.70 0.1167 0.3372 0.0673 0.0233 1.591 14.330 13.688 1186.761 1.619 60.886 5.232 0.53 234082. 0.5978
|
|
17.15 0.1362 0.3821 0.0652 0.0232 1.589 14.304 13.273 1184.652 1.616 59.040 5.082 0.53 234256. 0.5718
|
|
19.60 0.1556 0.4241 0.0631 0.0231 1.582 14.245 12.837 1179.786 1.609 57.100 4.935 0.53 234439. 0.5461
|
|
22.05 0.1751 0.4632 0.0608 0.0230 1.572 14.151 12.379 1171.929 1.599 55.063 4.791 0.53 234633. 0.5206
|
|
24.50 0.1945 0.4994 0.0585 0.0228 1.557 14.017 11.899 1160.844 1.584 52.928 4.649 0.53 234837. 0.4953
|
|
26.95 0.2140 0.5328 0.0560 0.0225 1.537 13.841 11.397 1146.268 1.564 50.695 4.510 0.53 235051. 0.4702
|
|
29.40 0.2334 0.5635 0.0534 0.0221 1.513 13.620 10.872 1127.951 1.539 48.361 4.372 0.53 235277. 0.4452
|
|
31.85 0.2529 0.5914 0.0507 0.0217 1.483 13.352 10.326 1105.764 1.508 45.932 4.236 0.53 235513. 0.4204
|
|
34.30 0.2723 0.6166 0.0480 0.0212 1.448 13.036 9.760 1079.656 1.473 43.414 4.100 0.53 235760. 0.3956
|
|
36.75 0.2918 0.6389 0.0451 0.0206 1.408 12.673 9.176 1049.588 1.432 40.815 3.965 0.53 236019. 0.3709
|
|
39.20 0.3113 0.6582 0.0421 0.0199 1.362 12.262 8.575 1015.524 1.385 38.140 3.830 0.53 236289. 0.3463
|
|
41.65 0.3307 0.6743 0.0391 0.0192 1.311 11.802 7.958 977.433 1.333 35.396 3.693 0.53 236571. 0.3217
|
|
44.10 0.3502 0.6870 0.0360 0.0184 1.254 11.293 7.327 935.295 1.276 32.589 3.553 0.53 236865. 0.2970
|
|
46.55 0.3696 0.6958 0.0328 0.0174 1.192 10.736 6.683 889.098 1.213 29.726 3.409 0.53 237170. 0.2722
|
|
49.00 0.3891 0.7002 0.0296 0.0165 1.125 10.129 6.028 838.852 1.144 26.813 3.259 0.53 237488. 0.2471
|
|
51.45 0.4085 0.6994 0.0264 0.0154 1.052 9.474 5.364 784.594 1.070 23.859 3.101 0.53 237817. 0.2218
|
|
53.90 0.4280 0.6923 0.0231 0.0143 0.974 8.771 4.692 726.386 0.991 20.870 2.930 0.53 238159. 0.1960
|
|
56.35 0.4474 0.6771 0.0197 0.0130 0.891 8.022 4.015 664.330 0.906 17.857 2.741 0.53 238513. 0.1696
|
|
58.80 0.4669 0.6513 0.0164 0.0117 0.803 7.228 3.334 598.571 0.817 14.830 2.526 0.53 238879. 0.1425
|
|
61.25 0.4863 0.6104 0.0130 0.0104 0.710 6.391 2.653 529.308 0.722 11.800 2.273 0.53 239258. 0.1143
|
|
63.70 0.5058 0.5474 0.0097 0.0090 0.613 5.516 1.974 456.801 0.623 8.781 1.960 0.53 239649. 0.0850
|
|
66.15 0.5252 0.4487 0.0064 0.0075 0.511 4.605 1.301 381.378 0.520 5.786 1.547 0.53 240053. 0.0545
|
|
68.60 0.5447 0.2862 0.0031 0.0060 0.407 3.663 0.637 303.404 0.414 2.832 0.952 0.54 240468. 0.0234
|
|
71.05 0.5641 -0.0163 -0.0001 0.0044 0.298 2.681 -0.026 221.996 0.303 -0.114 -0.052 0.54 240864. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 8000
|
|
|
|
V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
|
|
(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
|
|
0.00 0.0000 0.0000 0.0785 0.0229 2.335 18.398 20.857 1741.355 2.079 92.772 5.433 0.60 266533. 0.7662
|
|
2.80 0.0194 0.0649 0.0770 0.0231 2.355 18.550 20.468 1755.766 2.096 91.041 5.287 0.60 266671. 0.7387
|
|
5.60 0.0389 0.1262 0.0754 0.0232 2.371 18.680 20.054 1768.071 2.110 89.199 5.144 0.60 266818. 0.7115
|
|
8.39 0.0583 0.1841 0.0738 0.0234 2.384 18.784 19.614 1777.913 2.122 87.245 5.004 0.60 266975. 0.6844
|
|
11.19 0.0778 0.2388 0.0720 0.0235 2.394 18.859 19.149 1784.948 2.131 85.175 4.866 0.60 267142. 0.6576
|
|
13.99 0.0972 0.2901 0.0702 0.0235 2.399 18.899 18.657 1788.822 2.135 82.985 4.731 0.60 267319. 0.6310
|
|
16.79 0.1166 0.3384 0.0682 0.0235 2.399 18.903 18.137 1789.180 2.136 80.672 4.598 0.60 267507. 0.6047
|
|
19.59 0.1361 0.3836 0.0662 0.0235 2.395 18.866 17.589 1785.671 2.131 78.235 4.468 0.60 267706. 0.5786
|
|
22.38 0.1555 0.4259 0.0640 0.0234 2.384 18.784 17.012 1777.941 2.122 75.671 4.340 0.60 267917. 0.5528
|
|
25.18 0.1750 0.4653 0.0617 0.0232 2.368 18.654 16.407 1765.638 2.108 72.979 4.215 0.60 268139. 0.5272
|
|
27.98 0.1944 0.5019 0.0593 0.0230 2.345 18.472 15.773 1748.405 2.087 70.158 4.092 0.60 268373. 0.5019
|
|
30.78 0.2138 0.5358 0.0568 0.0227 2.314 18.234 15.109 1725.852 2.060 67.204 3.971 0.60 268618. 0.4767
|
|
33.58 0.2333 0.5669 0.0542 0.0223 2.277 17.936 14.415 1697.594 2.026 64.117 3.851 0.60 268877. 0.4516
|
|
36.37 0.2527 0.5954 0.0515 0.0219 2.231 17.575 13.692 1663.424 1.986 60.903 3.733 0.60 269148. 0.4266
|
|
39.17 0.2721 0.6211 0.0487 0.0213 2.177 17.150 12.943 1623.267 1.938 57.570 3.616 0.61 269431. 0.4018
|
|
41.97 0.2916 0.6440 0.0458 0.0207 2.115 16.662 12.169 1577.064 1.882 54.128 3.500 0.61 269727. 0.3770
|
|
44.77 0.3110 0.6640 0.0428 0.0200 2.045 16.110 11.373 1524.767 1.820 50.585 3.383 0.61 270037. 0.3523
|
|
47.57 0.3305 0.6809 0.0397 0.0193 1.966 15.492 10.555 1466.329 1.750 46.950 3.265 0.61 270359. 0.3276
|
|
50.37 0.3499 0.6944 0.0366 0.0184 1.880 14.810 9.719 1401.716 1.673 43.230 3.145 0.61 270695. 0.3028
|
|
53.16 0.3693 0.7042 0.0334 0.0175 1.785 14.062 8.866 1330.919 1.589 39.434 3.021 0.61 271044. 0.2778
|
|
55.96 0.3888 0.7097 0.0301 0.0165 1.682 13.248 7.997 1253.953 1.497 35.573 2.893 0.61 271407. 0.2526
|
|
58.76 0.4082 0.7101 0.0268 0.0154 1.570 12.371 7.117 1170.871 1.398 31.654 2.757 0.61 271783. 0.2271
|
|
61.56 0.4277 0.7044 0.0234 0.0142 1.451 11.429 6.225 1081.768 1.291 27.690 2.610 0.61 272174. 0.2011
|
|
64.36 0.4471 0.6908 0.0200 0.0130 1.323 10.426 5.327 986.805 1.178 23.693 2.448 0.61 272578. 0.1745
|
|
67.15 0.4665 0.6665 0.0166 0.0116 1.188 9.363 4.424 886.199 1.058 19.676 2.264 0.61 272997. 0.1471
|
|
69.95 0.4860 0.6274 0.0132 0.0103 1.046 8.244 3.520 780.257 0.931 15.655 2.046 0.61 273429. 0.1185
|
|
72.75 0.5054 0.5659 0.0099 0.0088 0.898 7.072 2.619 669.377 0.799 11.647 1.774 0.61 273876. 0.0887
|
|
75.55 0.5249 0.4677 0.0065 0.0073 0.743 5.854 1.725 554.060 0.661 7.672 1.412 0.61 274337. 0.0573
|
|
78.35 0.5443 0.3020 0.0032 0.0057 0.583 4.595 0.843 434.871 0.519 3.749 0.879 0.61 274811. 0.0249
|
|
81.14 0.5637 -0.0197 -0.0001 0.0041 0.416 3.278 -0.038 310.250 0.370 -0.168 -0.055 0.61 275259. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 9000
|
|
|
|
V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
|
|
(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
|
|
0.00 0.0000 0.0000 0.0798 0.0233 3.380 23.669 26.835 2520.269 2.674 119.361 4.829 0.68 299821. 0.7726
|
|
3.14 0.0194 0.0648 0.0783 0.0235 3.407 23.863 26.338 2540.971 2.696 117.153 4.701 0.68 299977. 0.7451
|
|
6.29 0.0388 0.1261 0.0767 0.0236 3.431 24.028 25.810 2558.560 2.715 114.802 4.575 0.68 300144. 0.7179
|
|
9.43 0.0583 0.1841 0.0751 0.0237 3.450 24.159 25.248 2572.513 2.730 112.304 4.452 0.68 300321. 0.6908
|
|
12.58 0.0777 0.2388 0.0733 0.0238 3.463 24.252 24.653 2582.330 2.740 109.656 4.330 0.68 300510. 0.6640
|
|
15.72 0.0971 0.2902 0.0714 0.0239 3.470 24.300 24.023 2587.494 2.745 106.853 4.211 0.68 300711. 0.6374
|
|
18.87 0.1165 0.3386 0.0694 0.0239 3.470 24.300 23.357 2587.491 2.745 103.891 4.094 0.68 300924. 0.6111
|
|
22.01 0.1359 0.3840 0.0673 0.0238 3.462 24.247 22.655 2581.807 2.739 100.768 3.980 0.68 301149. 0.5850
|
|
25.16 0.1553 0.4265 0.0651 0.0237 3.446 24.135 21.915 2569.937 2.727 97.480 3.868 0.68 301387. 0.5592
|
|
28.30 0.1748 0.4662 0.0628 0.0236 3.421 23.961 21.139 2551.372 2.707 94.026 3.758 0.68 301637. 0.5336
|
|
31.44 0.1942 0.5032 0.0604 0.0233 3.387 23.719 20.325 2525.605 2.680 90.404 3.650 0.68 301901. 0.5082
|
|
34.59 0.2136 0.5374 0.0579 0.0230 3.342 23.404 19.472 2492.075 2.644 86.611 3.544 0.68 302179. 0.4830
|
|
37.73 0.2330 0.5690 0.0552 0.0226 3.286 23.011 18.580 2450.229 2.600 82.645 3.439 0.68 302471. 0.4578
|
|
40.88 0.2524 0.5979 0.0525 0.0222 3.218 22.537 17.651 2399.746 2.546 78.513 3.336 0.68 302776. 0.4329
|
|
44.02 0.2719 0.6241 0.0496 0.0216 3.139 21.981 16.688 2340.514 2.483 74.226 3.234 0.68 303096. 0.4080
|
|
47.17 0.2913 0.6476 0.0466 0.0210 3.047 21.342 15.692 2272.459 2.411 69.798 3.132 0.68 303430. 0.3832
|
|
50.31 0.3107 0.6683 0.0436 0.0203 2.944 20.619 14.667 2195.515 2.330 65.238 3.030 0.68 303778. 0.3584
|
|
53.46 0.3301 0.6860 0.0405 0.0195 2.829 19.812 13.615 2109.621 2.238 60.557 2.927 0.68 304141. 0.3335
|
|
56.60 0.3495 0.7004 0.0373 0.0186 2.702 18.921 12.537 2014.733 2.138 55.767 2.823 0.68 304519. 0.3086
|
|
59.74 0.3689 0.7111 0.0340 0.0176 2.562 17.945 11.438 1910.839 2.027 50.877 2.715 0.68 304912. 0.2836
|
|
62.89 0.3884 0.7177 0.0307 0.0166 2.411 16.885 10.319 1797.963 1.908 45.900 2.603 0.68 305320. 0.2583
|
|
66.03 0.4078 0.7194 0.0273 0.0155 2.248 15.742 9.184 1676.186 1.778 40.849 2.485 0.68 305744. 0.2326
|
|
69.18 0.4272 0.7150 0.0239 0.0143 2.073 14.516 8.035 1545.649 1.640 35.738 2.358 0.68 306183. 0.2064
|
|
72.32 0.4466 0.7030 0.0204 0.0130 1.886 13.210 6.876 1406.580 1.492 30.583 2.217 0.69 306637. 0.1795
|
|
75.47 0.4660 0.6805 0.0170 0.0116 1.689 11.827 5.710 1259.311 1.336 25.400 2.057 0.69 307108. 0.1518
|
|
78.61 0.4855 0.6432 0.0135 0.0102 1.481 10.371 4.544 1104.302 1.172 20.211 1.866 0.69 307594. 0.1229
|
|
81.75 0.5049 0.5833 0.0100 0.0087 1.263 8.848 3.381 942.162 1.000 15.037 1.628 0.69 308096. 0.0924
|
|
84.90 0.5243 0.4859 0.0066 0.0071 1.038 7.266 2.227 773.667 0.821 9.905 1.305 0.69 308614. 0.0602
|
|
88.04 0.5437 0.3176 0.0032 0.0055 0.804 5.632 1.088 599.699 0.636 4.839 0.823 0.69 309146. 0.0265
|
|
91.19 0.5631 -0.0222 -0.0002 0.0039 0.560 3.924 -0.051 417.781 0.443 -0.228 -0.056 0.69 309645. 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 0.0814 0.0239 4.757 29.983 33.795 3547.348 3.387 150.320 4.321 0.75 333094. 0.7758
|
|
3.49 0.0194 0.0644 0.0799 0.0241 4.792 30.206 33.177 3573.730 3.413 147.573 4.211 0.75 333268. 0.7490
|
|
6.98 0.0388 0.1254 0.0783 0.0242 4.822 30.395 32.519 3596.044 3.434 144.644 4.102 0.75 333455. 0.7223
|
|
10.46 0.0582 0.1832 0.0766 0.0243 4.846 30.542 31.819 3613.533 3.451 141.529 3.994 0.75 333654. 0.6957
|
|
13.95 0.0775 0.2378 0.0748 0.0244 4.862 30.643 31.075 3625.462 3.462 138.223 3.888 0.75 333866. 0.6693
|
|
17.44 0.0969 0.2892 0.0729 0.0244 4.869 30.691 30.288 3631.066 3.467 134.719 3.783 0.75 334090. 0.6430
|
|
20.93 0.1163 0.3377 0.0709 0.0244 4.867 30.678 29.454 3629.575 3.466 131.013 3.681 0.75 334328. 0.6169
|
|
24.42 0.1357 0.3832 0.0688 0.0244 4.855 30.599 28.575 3620.211 3.457 127.101 3.580 0.75 334580. 0.5910
|
|
27.90 0.1551 0.4259 0.0666 0.0242 4.831 30.447 27.648 3602.211 3.440 122.980 3.481 0.75 334845. 0.5653
|
|
31.39 0.1745 0.4658 0.0642 0.0241 4.794 30.215 26.674 3574.811 3.414 118.647 3.384 0.75 335125. 0.5398
|
|
34.88 0.1939 0.5030 0.0618 0.0238 4.744 29.898 25.652 3537.262 3.378 114.101 3.289 0.76 335420. 0.5145
|
|
38.37 0.2132 0.5375 0.0592 0.0235 4.679 29.488 24.581 3488.780 3.332 109.338 3.196 0.76 335730. 0.4893
|
|
41.85 0.2326 0.5695 0.0565 0.0231 4.598 28.979 23.461 3428.583 3.274 104.355 3.104 0.76 336055. 0.4643
|
|
45.34 0.2520 0.5989 0.0537 0.0226 4.501 28.367 22.293 3356.198 3.205 99.160 3.013 0.76 336395. 0.4393
|
|
48.83 0.2714 0.6257 0.0508 0.0220 4.387 27.651 21.081 3271.465 3.124 93.767 2.923 0.76 336751. 0.4144
|
|
52.32 0.2908 0.6498 0.0477 0.0214 4.257 26.830 19.828 3174.315 3.031 88.193 2.833 0.76 337123. 0.3896
|
|
55.81 0.3102 0.6712 0.0446 0.0206 4.110 25.903 18.536 3064.683 2.927 82.450 2.743 0.76 337510. 0.3648
|
|
59.29 0.3295 0.6896 0.0414 0.0198 3.946 24.871 17.210 2942.537 2.810 76.552 2.653 0.76 337914. 0.3399
|
|
62.78 0.3489 0.7048 0.0382 0.0189 3.765 23.733 15.853 2807.871 2.681 70.513 2.561 0.76 338334. 0.3149
|
|
66.27 0.3683 0.7164 0.0348 0.0179 3.568 22.489 14.466 2660.742 2.541 64.347 2.466 0.76 338771. 0.2897
|
|
69.76 0.3877 0.7240 0.0314 0.0168 3.354 21.141 13.055 2501.274 2.389 58.068 2.367 0.76 339224. 0.2642
|
|
73.25 0.4071 0.7265 0.0280 0.0157 3.124 19.691 11.622 2329.693 2.225 51.693 2.263 0.76 339695. 0.2382
|
|
76.73 0.4265 0.7230 0.0245 0.0144 2.878 18.141 10.171 2146.345 2.050 45.238 2.149 0.76 340182. 0.2117
|
|
80.22 0.4459 0.7115 0.0210 0.0131 2.617 16.496 8.706 1951.730 1.864 38.725 2.023 0.76 340686. 0.1844
|
|
83.71 0.4652 0.6894 0.0174 0.0118 2.342 14.762 7.233 1746.520 1.668 32.174 1.878 0.76 341208. 0.1560
|
|
87.20 0.4846 0.6518 0.0139 0.0103 2.054 12.945 5.758 1531.603 1.463 25.610 1.705 0.76 341747. 0.1264
|
|
90.68 0.5040 0.5908 0.0103 0.0088 1.754 11.056 4.286 1308.107 1.249 19.063 1.486 0.76 342304. 0.0950
|
|
94.17 0.5234 0.4909 0.0068 0.0073 1.445 9.106 2.825 1077.406 1.029 12.564 1.189 0.76 342878. 0.0617
|
|
97.66 0.5428 0.3190 0.0033 0.0057 1.128 7.109 1.381 841.036 0.803 6.145 0.745 0.76 343468. 0.0270
|
|
101.15 0.5622 -0.0208 -0.0001 0.0040 0.798 5.032 -0.062 595.388 0.569 -0.274 -0.047 0.77 344021. 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 0.0833 0.0257 6.807 39.004 41.885 5076.133 4.407 186.302 3.743 0.83 366345. 0.7480
|
|
3.83 0.0193 0.0615 0.0819 0.0257 6.825 39.106 41.134 5089.355 4.418 182.965 3.666 0.83 366539. 0.7261
|
|
7.65 0.0387 0.1204 0.0803 0.0258 6.836 39.169 40.332 5097.540 4.425 179.399 3.589 0.83 366747. 0.7038
|
|
11.48 0.0580 0.1767 0.0786 0.0258 6.839 39.187 39.478 5099.878 4.427 175.599 3.511 0.83 366968. 0.6813
|
|
15.31 0.0773 0.2304 0.0768 0.0258 6.833 39.154 38.570 5095.563 4.424 171.560 3.433 0.83 367202. 0.6585
|
|
19.13 0.0967 0.2814 0.0748 0.0257 6.817 39.063 37.606 5083.730 4.413 167.272 3.355 0.83 367451. 0.6354
|
|
22.96 0.1160 0.3299 0.0728 0.0256 6.790 38.907 36.585 5063.483 4.396 162.730 3.277 0.83 367714. 0.6122
|
|
26.79 0.1353 0.3757 0.0707 0.0255 6.751 38.680 35.506 5033.896 4.370 157.929 3.199 0.83 367993. 0.5887
|
|
30.61 0.1547 0.4189 0.0684 0.0253 6.697 38.373 34.367 4994.024 4.335 152.864 3.121 0.83 368287. 0.5651
|
|
34.44 0.1740 0.4595 0.0660 0.0250 6.629 37.980 33.169 4942.891 4.291 147.534 3.044 0.83 368597. 0.5413
|
|
38.27 0.1933 0.4976 0.0635 0.0247 6.544 37.493 31.910 4879.512 4.236 141.935 2.966 0.83 368922. 0.5174
|
|
42.09 0.2127 0.5331 0.0609 0.0243 6.441 36.904 30.590 4802.790 4.169 136.064 2.889 0.83 369265. 0.4934
|
|
45.92 0.2320 0.5660 0.0581 0.0238 6.318 36.203 29.208 4711.551 4.090 129.917 2.812 0.83 369623. 0.4693
|
|
49.74 0.2513 0.5963 0.0553 0.0233 6.176 35.387 27.766 4605.428 3.998 123.501 2.735 0.83 369999. 0.4450
|
|
53.57 0.2707 0.6238 0.0523 0.0227 6.015 34.464 26.267 4485.247 3.894 116.835 2.656 0.83 370391. 0.4204
|
|
57.40 0.2900 0.6484 0.0492 0.0220 5.834 33.429 24.716 4350.562 3.777 109.937 2.577 0.83 370801. 0.3956
|
|
61.22 0.3093 0.6699 0.0460 0.0212 5.633 32.278 23.117 4200.794 3.647 102.825 2.496 0.83 371228. 0.3706
|
|
65.05 0.3287 0.6882 0.0427 0.0204 5.413 31.013 21.474 4036.127 3.504 95.518 2.413 0.83 371672. 0.3454
|
|
68.88 0.3480 0.7029 0.0394 0.0195 5.171 29.629 19.791 3856.069 3.348 88.030 2.328 0.83 372134. 0.3198
|
|
72.70 0.3673 0.7136 0.0360 0.0185 4.909 28.130 18.071 3660.864 3.178 80.380 2.239 0.83 372614. 0.2939
|
|
76.53 0.3867 0.7196 0.0325 0.0175 4.628 26.518 16.319 3451.092 2.996 72.586 2.145 0.84 373112. 0.2676
|
|
80.36 0.4060 0.7197 0.0289 0.0163 4.328 24.801 14.538 3227.637 2.802 64.667 2.043 0.84 373628. 0.2406
|
|
84.18 0.4253 0.7126 0.0253 0.0151 4.012 22.985 12.735 2991.380 2.597 56.645 1.931 0.84 374163. 0.2128
|
|
88.01 0.4447 0.6962 0.0217 0.0139 3.679 21.081 10.914 2743.493 2.382 48.544 1.804 0.84 374717. 0.1841
|
|
91.84 0.4640 0.6672 0.0181 0.0126 3.333 19.098 9.080 2485.431 2.158 40.390 1.657 0.84 375289. 0.1542
|
|
95.66 0.4833 0.6208 0.0144 0.0112 2.976 17.050 7.242 2218.955 1.926 32.214 1.480 0.84 375880. 0.1230
|
|
99.49 0.5027 0.5497 0.0108 0.0098 2.610 14.953 5.407 1946.051 1.689 24.051 1.260 0.84 376490. 0.0905
|
|
103.32 0.5220 0.4411 0.0071 0.0084 2.238 12.824 3.584 1669.012 1.449 15.941 0.974 0.84 377118. 0.0569
|
|
107.14 0.5413 0.2730 0.0035 0.0070 1.864 10.682 1.782 1390.212 1.207 7.924 0.581 0.84 377765. 0.0240
|
|
110.97 0.5607 -0.0022 0.0000 0.0056 1.483 8.497 -0.011 1105.765 0.960 -0.049 -0.004 0.84 378394. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 12000
|
|
|
|
V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
|
|
(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
|
|
0.00 0.0000 0.0000 0.0853 0.0304 10.452 54.897 51.037 7793.945 6.202 227.012 2.970 0.90 399582. 0.6553
|
|
4.19 0.0194 0.0539 0.0839 0.0302 10.402 54.635 50.158 7756.721 6.173 223.102 2.933 0.90 399796. 0.6415
|
|
8.38 0.0388 0.1064 0.0823 0.0300 10.340 54.311 49.213 7710.810 6.136 218.901 2.895 0.90 400025. 0.6272
|
|
12.57 0.0582 0.1574 0.0806 0.0298 10.266 53.923 48.202 7655.625 6.092 214.404 2.856 0.90 400269. 0.6123
|
|
16.76 0.0776 0.2070 0.0788 0.0296 10.179 53.464 47.123 7590.495 6.040 209.601 2.816 0.90 400528. 0.5969
|
|
20.96 0.0971 0.2549 0.0769 0.0293 10.077 52.930 45.972 7514.728 5.980 204.482 2.775 0.90 400804. 0.5810
|
|
25.15 0.1165 0.3012 0.0748 0.0289 9.961 52.316 44.748 7427.569 5.911 199.038 2.733 0.91 401095. 0.5645
|
|
29.34 0.1359 0.3459 0.0727 0.0285 9.827 51.617 43.449 7328.312 5.832 193.263 2.689 0.91 401404. 0.5474
|
|
33.53 0.1553 0.3887 0.0704 0.0281 9.677 50.828 42.076 7216.224 5.742 187.152 2.645 0.91 401729. 0.5298
|
|
37.72 0.1747 0.4297 0.0679 0.0276 9.509 49.943 40.626 7090.563 5.642 180.703 2.599 0.91 402072. 0.5115
|
|
41.91 0.1941 0.4688 0.0654 0.0271 9.321 48.956 39.099 6950.536 5.531 173.913 2.551 0.91 402433. 0.4927
|
|
46.10 0.2135 0.5058 0.0627 0.0265 9.112 47.862 37.495 6795.149 5.407 166.778 2.503 0.91 402812. 0.4733
|
|
50.29 0.2329 0.5407 0.0599 0.0258 8.882 46.651 35.812 6623.199 5.271 159.292 2.452 0.91 403208. 0.4532
|
|
54.49 0.2524 0.5734 0.0569 0.0251 8.628 45.318 34.053 6433.985 5.120 151.468 2.401 0.91 403624. 0.4326
|
|
58.68 0.2718 0.6037 0.0539 0.0243 8.351 43.864 32.223 6227.558 4.956 143.328 2.347 0.91 404058. 0.4114
|
|
62.87 0.2912 0.6304 0.0507 0.0234 8.065 42.361 30.327 6014.231 4.786 134.893 2.287 0.91 404510. 0.3890
|
|
67.06 0.3106 0.6529 0.0474 0.0226 7.769 40.806 28.369 5793.408 4.610 126.184 2.221 0.91 404982. 0.3653
|
|
71.25 0.3300 0.6711 0.0441 0.0217 7.462 39.191 26.354 5564.103 4.428 117.225 2.148 0.91 405473. 0.3406
|
|
75.44 0.3494 0.6824 0.0406 0.0208 7.159 37.604 24.287 5338.817 4.248 108.029 2.063 0.91 405983. 0.3140
|
|
79.63 0.3688 0.6873 0.0371 0.0199 6.850 35.980 22.173 5108.171 4.065 98.626 1.969 0.91 406512. 0.2863
|
|
83.82 0.3882 0.6859 0.0335 0.0189 6.523 34.263 20.019 4864.430 3.871 89.044 1.867 0.91 407062. 0.2579
|
|
88.02 0.4077 0.6770 0.0298 0.0180 6.181 32.467 17.831 4609.424 3.668 79.311 1.755 0.91 407631. 0.2288
|
|
92.21 0.4271 0.6588 0.0261 0.0169 5.827 30.608 15.615 4345.514 3.458 69.454 1.630 0.91 408220. 0.1989
|
|
96.40 0.4465 0.6293 0.0224 0.0159 5.465 28.703 13.378 4075.033 3.243 59.506 1.489 0.91 408829. 0.1682
|
|
100.59 0.4659 0.5858 0.0186 0.0148 5.096 26.766 11.130 3800.083 3.024 49.504 1.328 0.91 409459. 0.1369
|
|
104.78 0.4853 0.5250 0.0148 0.0137 4.725 24.817 8.878 3523.310 2.804 39.491 1.143 0.92 410109. 0.1052
|
|
108.97 0.5047 0.4427 0.0111 0.0126 4.355 22.874 6.635 3247.486 2.584 29.513 0.927 0.92 410780. 0.0737
|
|
113.16 0.5241 0.3337 0.0074 0.0116 3.990 20.958 4.412 2975.426 2.368 19.626 0.673 0.92 411472. 0.0436
|
|
117.35 0.5435 0.1914 0.0037 0.0106 3.633 19.081 2.222 2709.070 2.156 9.882 0.372 0.92 412183. 0.0171
|
|
121.55 0.5629 0.0045 0.0001 0.0095 3.268 17.165 0.046 2436.992 1.939 0.204 0.009 0.92 412897. 0.0001
|
|
|
|
|
|
|