501 lines
89 KiB
Plaintext
501 lines
89 KiB
Plaintext
18x8W (18x8W.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 0.0859 0.0346 0.005 0.332 0.287 3.928 0.038 1.278 33.165 0.07 38449. 0.5794
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0.36 0.0209 0.0505 0.0842 0.0348 0.005 0.334 0.282 3.948 0.038 1.253 32.348 0.07 38471. 0.5596
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0.71 0.0418 0.0985 0.0824 0.0350 0.005 0.335 0.276 3.965 0.038 1.226 31.532 0.07 38495. 0.5396
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1.07 0.0627 0.1440 0.0805 0.0351 0.005 0.336 0.269 3.977 0.038 1.198 30.716 0.07 38521. 0.5196
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1.43 0.0836 0.1869 0.0785 0.0351 0.005 0.337 0.263 3.984 0.038 1.168 29.902 0.07 38548. 0.4995
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1.78 0.1045 0.2273 0.0764 0.0351 0.005 0.337 0.256 3.985 0.038 1.137 29.090 0.07 38577. 0.4794
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2.14 0.1255 0.2651 0.0742 0.0351 0.005 0.336 0.248 3.980 0.038 1.104 28.280 0.07 38607. 0.4592
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2.49 0.1464 0.3005 0.0719 0.0350 0.005 0.335 0.240 3.969 0.038 1.069 27.471 0.07 38640. 0.4391
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2.85 0.1673 0.3333 0.0694 0.0348 0.005 0.334 0.232 3.951 0.038 1.033 26.663 0.07 38674. 0.4189
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3.21 0.1882 0.3636 0.0669 0.0346 0.005 0.332 0.224 3.925 0.037 0.995 25.855 0.07 38710. 0.3987
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3.56 0.2091 0.3913 0.0642 0.0343 0.005 0.329 0.215 3.891 0.037 0.956 25.046 0.07 38748. 0.3785
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3.92 0.2300 0.4165 0.0615 0.0340 0.005 0.325 0.206 3.850 0.037 0.915 24.235 0.07 38788. 0.3583
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4.28 0.2509 0.4391 0.0586 0.0335 0.005 0.321 0.196 3.800 0.036 0.873 23.418 0.07 38830. 0.3381
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4.63 0.2718 0.4589 0.0557 0.0330 0.005 0.316 0.186 3.742 0.036 0.829 22.595 0.07 38874. 0.3180
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4.99 0.2927 0.4760 0.0527 0.0324 0.005 0.311 0.176 3.675 0.035 0.784 21.761 0.07 38920. 0.2979
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5.35 0.3136 0.4902 0.0496 0.0317 0.005 0.304 0.166 3.599 0.034 0.738 20.914 0.07 38968. 0.2777
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5.70 0.3346 0.5012 0.0464 0.0310 0.005 0.297 0.155 3.513 0.034 0.691 20.049 0.07 39018. 0.2575
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6.06 0.3555 0.5090 0.0432 0.0301 0.005 0.289 0.144 3.418 0.033 0.642 19.161 0.07 39070. 0.2373
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6.42 0.3764 0.5131 0.0398 0.0292 0.004 0.280 0.133 3.313 0.032 0.593 18.243 0.07 39125. 0.2171
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6.77 0.3973 0.5132 0.0364 0.0282 0.004 0.270 0.122 3.198 0.031 0.542 17.287 0.07 39182. 0.1967
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7.13 0.4182 0.5089 0.0330 0.0271 0.004 0.260 0.110 3.072 0.029 0.491 16.283 0.07 39241. 0.1763
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7.48 0.4391 0.4993 0.0295 0.0259 0.004 0.248 0.099 2.937 0.028 0.438 15.218 0.07 39302. 0.1557
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7.84 0.4600 0.4837 0.0259 0.0246 0.004 0.236 0.087 2.790 0.027 0.385 14.073 0.07 39366. 0.1350
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8.20 0.4809 0.4609 0.0223 0.0232 0.004 0.223 0.074 2.633 0.025 0.331 12.825 0.07 39432. 0.1141
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8.55 0.5018 0.4291 0.0186 0.0217 0.003 0.208 0.062 2.466 0.024 0.277 11.444 0.07 39500. 0.0930
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8.91 0.5227 0.3861 0.0149 0.0202 0.003 0.193 0.050 2.288 0.022 0.222 9.884 0.07 39570. 0.0719
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9.27 0.5436 0.3284 0.0112 0.0185 0.003 0.177 0.037 2.100 0.020 0.166 8.084 0.07 39643. 0.0510
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9.62 0.5646 0.2510 0.0075 0.0168 0.003 0.161 0.025 1.901 0.018 0.111 5.949 0.07 39718. 0.0306
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9.98 0.5855 0.1457 0.0037 0.0149 0.002 0.143 0.012 1.693 0.016 0.055 3.331 0.07 39795. 0.0121
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10.34 0.6064 -0.0015 0.0000 0.0130 0.002 0.125 0.000 1.475 0.014 0.000 -0.033 0.07 39870. 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 0.0863 0.0309 0.038 1.184 1.155 28.014 0.134 5.136 18.694 0.14 76897. 0.6548
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0.72 0.0210 0.0572 0.0846 0.0311 0.038 1.192 1.132 28.206 0.135 5.035 18.204 0.14 76942. 0.6314
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1.43 0.0420 0.1112 0.0828 0.0313 0.038 1.199 1.108 28.367 0.135 4.929 17.718 0.14 76990. 0.6080
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2.15 0.0630 0.1623 0.0809 0.0314 0.038 1.204 1.083 28.491 0.136 4.816 17.236 0.14 77042. 0.5846
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2.86 0.0840 0.2105 0.0789 0.0315 0.038 1.208 1.056 28.574 0.136 4.697 16.760 0.14 77096. 0.5614
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3.58 0.1050 0.2557 0.0768 0.0315 0.038 1.209 1.028 28.612 0.137 4.571 16.289 0.14 77154. 0.5383
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4.30 0.1260 0.2981 0.0746 0.0315 0.038 1.209 0.998 28.599 0.137 4.438 15.824 0.14 77216. 0.5152
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5.01 0.1470 0.3376 0.0722 0.0315 0.038 1.206 0.966 28.531 0.136 4.299 15.364 0.14 77281. 0.4923
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5.73 0.1681 0.3744 0.0698 0.0313 0.038 1.200 0.934 28.405 0.136 4.153 14.908 0.14 77350. 0.4696
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6.45 0.1891 0.4085 0.0672 0.0311 0.038 1.192 0.899 28.216 0.135 4.001 14.458 0.14 77422. 0.4470
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7.16 0.2101 0.4399 0.0646 0.0308 0.037 1.182 0.864 27.963 0.134 3.842 14.011 0.14 77499. 0.4245
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7.88 0.2311 0.4685 0.0618 0.0305 0.037 1.168 0.827 27.643 0.132 3.678 13.568 0.14 77579. 0.4022
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8.59 0.2521 0.4945 0.0589 0.0300 0.037 1.152 0.789 27.252 0.130 3.508 13.126 0.14 77664. 0.3800
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9.31 0.2731 0.5177 0.0560 0.0295 0.036 1.132 0.749 26.789 0.128 3.332 12.685 0.14 77753. 0.3579
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10.03 0.2941 0.5381 0.0530 0.0289 0.035 1.109 0.709 26.249 0.125 3.152 12.244 0.14 77845. 0.3360
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10.74 0.3151 0.5557 0.0498 0.0283 0.034 1.083 0.667 25.632 0.122 2.966 11.800 0.14 77942. 0.3141
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11.46 0.3361 0.5702 0.0466 0.0275 0.033 1.054 0.624 24.935 0.119 2.776 11.351 0.14 78044. 0.2923
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12.17 0.3571 0.5814 0.0434 0.0266 0.032 1.021 0.580 24.154 0.115 2.581 10.894 0.14 78149. 0.2705
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12.89 0.3781 0.5892 0.0400 0.0257 0.031 0.984 0.535 23.289 0.111 2.381 10.426 0.14 78259. 0.2487
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13.61 0.3991 0.5931 0.0366 0.0246 0.030 0.944 0.490 22.337 0.107 2.178 9.943 0.14 78374. 0.2268
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14.32 0.4201 0.5926 0.0331 0.0235 0.029 0.900 0.443 21.296 0.102 1.971 9.438 0.14 78493. 0.2048
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15.04 0.4411 0.5869 0.0296 0.0222 0.027 0.852 0.396 20.166 0.096 1.761 8.903 0.14 78616. 0.1826
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15.75 0.4621 0.5752 0.0260 0.0209 0.025 0.801 0.348 18.945 0.090 1.547 8.327 0.14 78745. 0.1601
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16.47 0.4832 0.5558 0.0224 0.0194 0.024 0.745 0.299 17.632 0.084 1.331 7.697 0.14 78878. 0.1372
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17.19 0.5042 0.5266 0.0187 0.0179 0.022 0.686 0.250 16.228 0.077 1.112 6.989 0.14 79015. 0.1139
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17.90 0.5252 0.4845 0.0150 0.0162 0.020 0.623 0.201 14.733 0.070 0.892 6.173 0.14 79157. 0.0901
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18.62 0.5462 0.4242 0.0113 0.0145 0.018 0.556 0.151 13.150 0.063 0.670 5.197 0.14 79304. 0.0658
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19.34 0.5672 0.3371 0.0075 0.0127 0.015 0.485 0.101 11.479 0.055 0.448 3.977 0.15 79455. 0.0411
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20.05 0.5882 0.2076 0.0038 0.0107 0.013 0.411 0.051 9.725 0.046 0.225 2.361 0.15 79609. 0.0173
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20.77 0.6092 0.0014 0.0000 0.0087 0.011 0.333 0.000 7.873 0.038 0.001 0.015 0.15 79754. 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 0.0867 0.0294 0.121 2.537 2.611 90.064 0.287 11.612 13.147 0.21 115343. 0.6924
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1.08 0.0211 0.0604 0.0850 0.0296 0.122 2.557 2.560 90.755 0.289 11.385 12.792 0.21 115410. 0.6672
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2.15 0.0421 0.1175 0.0832 0.0298 0.122 2.573 2.506 91.339 0.291 11.144 12.442 0.21 115483. 0.6420
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3.23 0.0632 0.1714 0.0813 0.0300 0.123 2.586 2.448 91.799 0.292 10.889 12.096 0.21 115561. 0.6170
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4.31 0.0843 0.2221 0.0793 0.0301 0.124 2.595 2.388 92.118 0.293 10.620 11.756 0.21 115643. 0.5921
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5.39 0.1053 0.2697 0.0772 0.0301 0.124 2.600 2.323 92.280 0.294 10.335 11.420 0.21 115731. 0.5675
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6.46 0.1264 0.3143 0.0749 0.0301 0.124 2.600 2.256 92.267 0.294 10.035 11.090 0.21 115823. 0.5430
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7.54 0.1475 0.3559 0.0726 0.0301 0.123 2.594 2.185 92.065 0.293 9.719 10.765 0.21 115922. 0.5187
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8.62 0.1685 0.3947 0.0701 0.0299 0.123 2.582 2.111 91.660 0.292 9.389 10.445 0.21 116026. 0.4947
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9.70 0.1896 0.4306 0.0675 0.0297 0.122 2.565 2.033 91.041 0.290 9.045 10.130 0.21 116135. 0.4709
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10.77 0.2107 0.4638 0.0649 0.0295 0.121 2.541 1.953 90.197 0.287 8.686 9.820 0.21 116251. 0.4473
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11.85 0.2318 0.4942 0.0621 0.0291 0.120 2.511 1.869 89.119 0.284 8.314 9.513 0.21 116372. 0.4240
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12.93 0.2528 0.5219 0.0592 0.0287 0.118 2.474 1.783 87.797 0.279 7.929 9.209 0.21 116499. 0.4008
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14.01 0.2739 0.5469 0.0562 0.0282 0.116 2.429 1.693 86.220 0.274 7.531 8.907 0.22 116633. 0.3778
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15.08 0.2950 0.5691 0.0532 0.0276 0.113 2.377 1.601 84.380 0.269 7.122 8.607 0.22 116773. 0.3550
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16.16 0.3160 0.5885 0.0500 0.0269 0.110 2.318 1.507 82.268 0.262 6.701 8.306 0.22 116919. 0.3324
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17.24 0.3371 0.6049 0.0468 0.0261 0.107 2.250 1.410 79.875 0.254 6.270 8.004 0.22 117072. 0.3098
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18.32 0.3582 0.6182 0.0435 0.0252 0.104 2.175 1.310 77.192 0.246 5.828 7.699 0.22 117231. 0.2873
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19.39 0.3792 0.6281 0.0401 0.0242 0.100 2.091 1.209 74.213 0.236 5.377 7.388 0.22 117397. 0.2648
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20.47 0.4003 0.6343 0.0367 0.0232 0.095 1.998 1.105 70.931 0.226 4.917 7.068 0.22 117570. 0.2422
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21.55 0.4214 0.6362 0.0332 0.0220 0.090 1.897 1.000 67.338 0.214 4.448 6.735 0.22 117750. 0.2196
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22.62 0.4424 0.6332 0.0297 0.0207 0.085 1.787 0.893 63.431 0.202 3.971 6.384 0.22 117936. 0.1966
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23.70 0.4635 0.6242 0.0260 0.0193 0.079 1.668 0.784 59.207 0.188 3.488 6.007 0.22 118130. 0.1734
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24.78 0.4846 0.6077 0.0224 0.0179 0.073 1.540 0.674 54.663 0.174 2.999 5.594 0.22 118330. 0.1497
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25.86 0.5056 0.5812 0.0187 0.0163 0.067 1.403 0.563 49.800 0.159 2.504 5.127 0.22 118537. 0.1254
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26.93 0.5267 0.5412 0.0150 0.0146 0.060 1.257 0.451 44.620 0.142 2.005 4.583 0.22 118752. 0.1003
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28.01 0.5478 0.4813 0.0112 0.0128 0.052 1.102 0.338 39.130 0.125 1.504 3.919 0.22 118973. 0.0743
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29.09 0.5689 0.3905 0.0075 0.0109 0.045 0.939 0.225 33.338 0.106 1.001 3.062 0.22 119200. 0.0474
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30.17 0.5899 0.2465 0.0037 0.0089 0.037 0.768 0.112 27.253 0.087 0.498 1.864 0.22 119433. 0.0203
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31.24 0.6110 -0.0072 -0.0001 0.0068 0.028 0.586 -0.002 20.789 0.066 -0.011 -0.053 0.22 119639. 0.0000
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PROP RPM = 4000
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V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
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(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
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0.00 0.0000 0.0000 0.0872 0.0287 0.279 4.401 4.669 208.273 0.497 20.768 10.168 0.29 153785. 0.7162
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1.44 0.0211 0.0624 0.0855 0.0289 0.282 4.437 4.578 209.972 0.501 20.364 9.890 0.29 153876. 0.6898
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2.88 0.0422 0.1213 0.0837 0.0291 0.284 4.467 4.482 211.414 0.505 19.934 9.615 0.29 153973. 0.6635
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4.32 0.0633 0.1768 0.0818 0.0293 0.285 4.491 4.379 212.557 0.507 19.478 9.345 0.29 154077. 0.6374
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5.76 0.0844 0.2291 0.0798 0.0294 0.286 4.508 4.271 213.362 0.509 18.996 9.079 0.29 154187. 0.6116
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7.19 0.1055 0.2781 0.0776 0.0295 0.287 4.517 4.156 213.786 0.510 18.487 8.818 0.29 154304. 0.5860
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8.63 0.1266 0.3240 0.0754 0.0295 0.287 4.518 4.036 213.790 0.510 17.951 8.562 0.29 154428. 0.5607
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10.07 0.1477 0.3670 0.0730 0.0294 0.286 4.508 3.909 213.335 0.509 17.387 8.311 0.29 154560. 0.5356
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11.51 0.1688 0.4069 0.0705 0.0293 0.285 4.488 3.776 212.392 0.507 16.796 8.064 0.29 154699. 0.5108
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12.95 0.1899 0.4440 0.0680 0.0291 0.283 4.457 3.638 210.931 0.504 16.180 7.822 0.29 154846. 0.4863
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14.39 0.2110 0.4784 0.0653 0.0288 0.280 4.415 3.493 208.926 0.499 15.538 7.584 0.29 155000. 0.4620
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15.83 0.2321 0.5099 0.0625 0.0284 0.277 4.360 3.344 206.354 0.493 14.872 7.349 0.29 155163. 0.4381
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17.27 0.2532 0.5388 0.0596 0.0280 0.272 4.294 3.189 203.189 0.485 14.183 7.118 0.29 155334. 0.4143
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18.70 0.2743 0.5649 0.0566 0.0275 0.267 4.214 3.029 199.409 0.476 13.471 6.889 0.29 155512. 0.3908
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20.14 0.2954 0.5883 0.0535 0.0269 0.261 4.120 2.864 194.991 0.466 12.739 6.662 0.29 155700. 0.3675
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21.58 0.3165 0.6089 0.0503 0.0262 0.255 4.013 2.695 189.913 0.453 11.986 6.435 0.29 155895. 0.3444
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23.02 0.3376 0.6266 0.0471 0.0254 0.247 3.891 2.521 184.154 0.440 11.213 6.209 0.29 156100. 0.3214
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24.46 0.3587 0.6414 0.0438 0.0245 0.238 3.755 2.343 177.694 0.424 10.422 5.981 0.29 156313. 0.2984
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25.90 0.3798 0.6528 0.0404 0.0235 0.229 3.603 2.162 170.514 0.407 9.614 5.750 0.29 156535. 0.2756
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27.34 0.4010 0.6607 0.0369 0.0224 0.218 3.436 1.976 162.598 0.388 8.790 5.513 0.29 156767. 0.2526
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28.78 0.4221 0.6645 0.0334 0.0212 0.206 3.253 1.788 153.930 0.367 7.951 5.267 0.29 157007. 0.2296
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30.22 0.4432 0.6635 0.0298 0.0199 0.194 3.053 1.596 144.501 0.345 7.098 5.009 0.29 157256. 0.2063
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31.65 0.4643 0.6568 0.0262 0.0185 0.180 2.838 1.401 134.300 0.321 6.233 4.733 0.29 157515. 0.1826
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33.09 0.4854 0.6426 0.0225 0.0170 0.165 2.606 1.204 123.325 0.294 5.357 4.430 0.29 157783. 0.1585
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34.53 0.5065 0.6187 0.0188 0.0154 0.150 2.358 1.005 111.575 0.266 4.472 4.087 0.29 158060. 0.1336
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35.97 0.5276 0.5811 0.0150 0.0137 0.133 2.093 0.805 99.059 0.236 3.580 3.685 0.29 158347. 0.1078
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37.41 0.5487 0.5229 0.0113 0.0118 0.115 1.813 0.603 85.791 0.205 2.682 3.188 0.29 158643. 0.0807
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38.85 0.5698 0.4312 0.0075 0.0099 0.096 1.517 0.401 71.790 0.171 1.783 2.532 0.29 158947. 0.0523
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40.29 0.5909 0.2785 0.0037 0.0079 0.077 1.206 0.198 57.080 0.136 0.883 1.577 0.29 159258. 0.0229
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41.73 0.6120 -0.0150 -0.0001 0.0057 0.055 0.874 -0.007 41.356 0.099 -0.033 -0.082 0.29 159514. 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 0.0879 0.0284 0.539 6.795 7.350 401.965 0.768 32.695 8.294 0.36 192222. 0.7330
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1.80 0.0211 0.0637 0.0862 0.0286 0.544 6.853 7.208 405.369 0.774 32.060 8.065 0.36 192336. 0.7058
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3.60 0.0423 0.1238 0.0844 0.0288 0.547 6.901 7.056 408.260 0.780 31.385 7.839 0.36 192458. 0.6788
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5.40 0.0634 0.1804 0.0824 0.0290 0.551 6.940 6.895 410.559 0.784 30.669 7.617 0.36 192588. 0.6520
|
|
7.20 0.0845 0.2337 0.0804 0.0291 0.553 6.968 6.725 412.184 0.787 29.912 7.400 0.36 192727. 0.6256
|
|
9.00 0.1056 0.2837 0.0783 0.0291 0.554 6.982 6.545 413.053 0.789 29.111 7.187 0.36 192874. 0.5993
|
|
10.80 0.1268 0.3305 0.0760 0.0291 0.554 6.983 6.355 413.085 0.789 28.268 6.978 0.36 193030. 0.5734
|
|
12.60 0.1479 0.3743 0.0736 0.0291 0.553 6.968 6.156 412.206 0.787 27.380 6.773 0.36 193196. 0.5478
|
|
14.41 0.1690 0.4151 0.0711 0.0290 0.550 6.937 5.947 410.353 0.784 26.451 6.573 0.36 193370. 0.5225
|
|
16.21 0.1902 0.4530 0.0685 0.0287 0.546 6.888 5.728 407.470 0.778 25.480 6.377 0.36 193554. 0.4975
|
|
18.01 0.2113 0.4882 0.0658 0.0285 0.541 6.821 5.501 403.504 0.771 24.470 6.184 0.36 193748. 0.4728
|
|
19.81 0.2324 0.5205 0.0630 0.0281 0.534 6.735 5.265 398.408 0.761 23.421 5.994 0.36 193952. 0.4484
|
|
21.61 0.2535 0.5502 0.0600 0.0277 0.526 6.629 5.021 392.133 0.749 22.335 5.808 0.36 194166. 0.4243
|
|
23.41 0.2747 0.5772 0.0570 0.0271 0.516 6.502 4.769 384.634 0.735 21.215 5.624 0.36 194391. 0.4004
|
|
25.21 0.2958 0.6015 0.0539 0.0265 0.504 6.354 4.510 375.864 0.718 20.060 5.442 0.36 194626. 0.3768
|
|
27.01 0.3169 0.6230 0.0507 0.0258 0.491 6.183 4.243 365.781 0.699 18.874 5.262 0.36 194871. 0.3533
|
|
28.81 0.3380 0.6418 0.0475 0.0250 0.475 5.990 3.970 354.342 0.677 17.657 5.081 0.36 195128. 0.3300
|
|
30.61 0.3592 0.6576 0.0441 0.0241 0.458 5.773 3.689 341.508 0.652 16.411 4.900 0.36 195395. 0.3068
|
|
32.41 0.3803 0.6703 0.0407 0.0231 0.439 5.532 3.403 327.241 0.625 15.138 4.717 0.36 195674. 0.2837
|
|
34.21 0.4014 0.6795 0.0372 0.0220 0.418 5.266 3.111 311.509 0.595 13.839 4.530 0.36 195964. 0.2605
|
|
36.01 0.4226 0.6848 0.0336 0.0208 0.395 4.975 2.814 294.282 0.562 12.517 4.337 0.36 196265. 0.2372
|
|
37.81 0.4437 0.6855 0.0300 0.0194 0.370 4.658 2.512 275.538 0.526 11.173 4.135 0.36 196577. 0.2136
|
|
39.62 0.4648 0.6805 0.0264 0.0180 0.342 4.315 2.205 255.260 0.488 9.809 3.919 0.36 196902. 0.1897
|
|
41.42 0.4859 0.6685 0.0227 0.0165 0.313 3.946 1.895 233.440 0.446 8.428 3.682 0.36 197238. 0.1652
|
|
43.22 0.5071 0.6468 0.0189 0.0148 0.282 3.551 1.581 210.081 0.401 7.033 3.414 0.36 197585. 0.1399
|
|
45.02 0.5282 0.6115 0.0151 0.0131 0.248 3.131 1.265 185.197 0.354 5.627 3.098 0.36 197944. 0.1136
|
|
46.82 0.5493 0.5552 0.0113 0.0112 0.213 2.685 0.947 158.816 0.303 4.213 2.705 0.36 198315. 0.0858
|
|
48.62 0.5705 0.4638 0.0075 0.0092 0.176 2.214 0.628 130.982 0.250 2.795 2.176 0.36 198696. 0.0562
|
|
50.42 0.5916 0.3051 0.0037 0.0072 0.136 1.720 0.310 101.736 0.194 1.377 1.380 0.36 199086. 0.0250
|
|
52.22 0.6127 -0.0264 -0.0002 0.0050 0.094 1.186 -0.018 70.178 0.134 -0.079 -0.115 0.36 199369. 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 0.0887 0.0283 0.928 9.752 10.683 692.293 1.102 47.516 6.999 0.43 230652. 0.7457
|
|
2.16 0.0212 0.0645 0.0870 0.0285 0.936 9.837 10.476 698.293 1.111 46.597 6.805 0.43 230790. 0.7179
|
|
4.33 0.0423 0.1254 0.0852 0.0287 0.943 9.909 10.256 703.390 1.119 45.620 6.614 0.43 230937. 0.6904
|
|
6.49 0.0635 0.1828 0.0832 0.0289 0.949 9.966 10.023 707.439 1.126 44.582 6.426 0.43 231094. 0.6632
|
|
8.65 0.0846 0.2368 0.0812 0.0290 0.953 10.006 9.776 710.300 1.130 43.484 6.243 0.43 231262. 0.6363
|
|
10.82 0.1058 0.2875 0.0790 0.0291 0.955 10.028 9.515 711.828 1.133 42.322 6.063 0.43 231439. 0.6096
|
|
12.98 0.1269 0.3350 0.0767 0.0291 0.955 10.028 9.240 711.880 1.133 41.097 5.887 0.43 231628. 0.5833
|
|
15.14 0.1481 0.3794 0.0743 0.0290 0.953 10.006 8.950 710.323 1.131 39.809 5.715 0.43 231827. 0.5573
|
|
17.31 0.1692 0.4208 0.0718 0.0289 0.948 9.960 8.646 707.049 1.125 38.459 5.547 0.43 232038. 0.5317
|
|
19.47 0.1904 0.4593 0.0692 0.0287 0.941 9.889 8.329 701.958 1.117 37.048 5.382 0.43 232260. 0.5063
|
|
21.63 0.2115 0.4951 0.0664 0.0284 0.932 9.790 7.999 694.959 1.106 35.580 5.221 0.43 232493. 0.4813
|
|
23.80 0.2327 0.5281 0.0636 0.0280 0.920 9.663 7.656 685.966 1.092 34.055 5.062 0.43 232739. 0.4566
|
|
25.96 0.2538 0.5584 0.0606 0.0276 0.905 9.507 7.301 674.896 1.074 32.476 4.907 0.43 232997. 0.4322
|
|
28.12 0.2750 0.5861 0.0576 0.0270 0.887 9.321 6.935 661.671 1.053 30.847 4.754 0.43 233268. 0.4081
|
|
30.28 0.2961 0.6111 0.0544 0.0264 0.867 9.103 6.557 646.209 1.028 29.168 4.603 0.43 233550. 0.3842
|
|
32.45 0.3173 0.6334 0.0512 0.0257 0.843 8.853 6.169 628.435 1.000 27.442 4.453 0.43 233846. 0.3605
|
|
34.61 0.3384 0.6530 0.0479 0.0248 0.816 8.569 5.771 608.276 0.968 25.671 4.304 0.43 234155. 0.3370
|
|
36.77 0.3596 0.6697 0.0445 0.0239 0.785 8.250 5.364 585.662 0.932 23.859 4.154 0.43 234477. 0.3136
|
|
38.94 0.3807 0.6834 0.0411 0.0229 0.752 7.896 4.947 560.528 0.892 22.006 4.003 0.43 234813. 0.2903
|
|
41.10 0.4019 0.6937 0.0376 0.0218 0.715 7.506 4.523 532.817 0.848 20.117 3.850 0.43 235161. 0.2669
|
|
43.26 0.4230 0.7002 0.0340 0.0205 0.674 7.078 4.090 502.478 0.800 18.192 3.692 0.43 235524. 0.2434
|
|
45.43 0.4442 0.7023 0.0303 0.0192 0.630 6.613 3.650 469.470 0.747 16.236 3.527 0.43 235900. 0.2196
|
|
47.59 0.4653 0.6990 0.0266 0.0177 0.582 6.110 3.204 433.765 0.690 14.252 3.350 0.43 236290. 0.1955
|
|
49.75 0.4865 0.6887 0.0229 0.0161 0.530 5.569 2.752 395.350 0.629 12.242 3.158 0.43 236694. 0.1708
|
|
51.92 0.5076 0.6690 0.0191 0.0145 0.475 4.990 2.296 354.227 0.564 10.211 2.940 0.43 237113. 0.1452
|
|
54.08 0.5288 0.6358 0.0152 0.0127 0.416 4.373 1.836 310.424 0.494 8.164 2.682 0.43 237545. 0.1184
|
|
56.24 0.5499 0.5815 0.0114 0.0108 0.354 3.719 1.373 263.992 0.420 6.106 2.359 0.43 237990. 0.0901
|
|
58.41 0.5711 0.4908 0.0075 0.0088 0.288 3.029 0.909 215.007 0.342 4.042 1.917 0.44 238449. 0.0596
|
|
60.57 0.5922 0.3274 0.0037 0.0067 0.219 2.304 0.445 163.542 0.260 1.977 1.233 0.44 238917. 0.0268
|
|
62.73 0.6134
|
|
|
|
|
|
|
|
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 0.0897 0.0284 1.479 13.320 14.703 1103.111 1.505 65.399 6.046 0.50 269073. 0.7557
|
|
2.53 0.0212 0.0652 0.0880 0.0286 1.492 13.437 14.420 1112.826 1.518 64.139 5.877 0.50 269236. 0.7275
|
|
5.06 0.0424 0.1267 0.0861 0.0288 1.503 13.536 14.118 1121.063 1.529 62.797 5.712 0.50 269409. 0.6996
|
|
7.59 0.0636 0.1847 0.0842 0.0290 1.512 13.615 13.798 1127.586 1.538 61.372 5.550 0.50 269594. 0.6720
|
|
10.12 0.0848 0.2392 0.0821 0.0291 1.518 13.671 13.458 1132.170 1.544 59.862 5.392 0.50 269791. 0.6448
|
|
12.65 0.1060 0.2904 0.0799 0.0292 1.521 13.700 13.099 1134.575 1.548 58.264 5.237 0.50 269999. 0.6178
|
|
15.18 0.1272 0.3384 0.0776 0.0292 1.521 13.700 12.720 1134.574 1.548 56.578 5.085 0.50 270221. 0.5912
|
|
17.71 0.1484 0.3833 0.0752 0.0291 1.518 13.668 12.321 1131.949 1.544 54.804 4.937 0.50 270455. 0.5649
|
|
20.24 0.1696 0.4252 0.0726 0.0290 1.511 13.602 11.903 1126.523 1.537 52.944 4.792 0.50 270703. 0.5390
|
|
22.77 0.1908 0.4642 0.0699 0.0287 1.499 13.501 11.466 1118.132 1.525 51.000 4.651 0.50 270964. 0.5134
|
|
25.30 0.2120 0.5005 0.0672 0.0285 1.484 13.362 11.010 1106.633 1.510 48.974 4.513 0.50 271239. 0.4881
|
|
27.83 0.2332 0.5340 0.0643 0.0281 1.464 13.184 10.538 1091.890 1.490 46.871 4.377 0.50 271527. 0.4632
|
|
30.36 0.2544 0.5649 0.0613 0.0276 1.440 12.965 10.048 1073.770 1.465 44.694 4.244 0.50 271830. 0.4386
|
|
32.89 0.2756 0.5931 0.0582 0.0271 1.411 12.704 9.543 1052.142 1.435 42.445 4.114 0.50 272148. 0.4142
|
|
35.42 0.2968 0.6187 0.0550 0.0264 1.377 12.399 9.022 1026.882 1.401 40.128 3.985 0.50 272480. 0.3902
|
|
37.95 0.3180 0.6417 0.0518 0.0257 1.338 12.049 8.486 997.868 1.361 37.746 3.857 0.50 272827. 0.3663
|
|
40.48 0.3392 0.6619 0.0484 0.0248 1.294 11.652 7.936 964.981 1.316 35.302 3.730 0.50 273190. 0.3426
|
|
43.01 0.3604 0.6794 0.0450 0.0239 1.245 11.207 7.374 928.109 1.266 32.799 3.604 0.50 273568. 0.3190
|
|
45.54 0.3816 0.6939 0.0415 0.0228 1.190 10.712 6.799 887.152 1.210 30.241 3.476 0.50 273961. 0.2955
|
|
48.07 0.4028 0.7051 0.0379 0.0216 1.129 10.167 6.212 842.013 1.149 27.631 3.346 0.50 274371. 0.2719
|
|
50.60 0.4240 0.7127 0.0343 0.0204 1.063 9.571 5.615 792.613 1.081 24.974 3.213 0.50 274796. 0.2482
|
|
53.13 0.4452 0.7159 0.0305 0.0190 0.991 8.922 5.007 738.887 1.008 22.272 3.074 0.50 275237. 0.2242
|
|
55.66 0.4664 0.7138 0.0268 0.0175 0.913 8.220 4.391 680.789 0.929 19.531 2.925 0.51 275695. 0.1998
|
|
58.18 0.4876 0.7049 0.0230 0.0159 0.829 7.466 3.767 618.298 0.843 16.755 2.763 0.51 276169. 0.1748
|
|
60.71 0.5088 0.6866 0.0191 0.0142 0.739 6.658 3.136 551.423 0.752 13.950 2.580 0.51 276659. 0.1489
|
|
63.24 0.5300 0.6548 0.0153 0.0123 0.644 5.798 2.500 480.207 0.655 11.122 2.362 0.51 277165. 0.1217
|
|
65.77 0.5512 0.6014 0.0114 0.0104 0.543 4.887 1.861 404.737 0.552 8.278 2.086 0.51 277688. 0.0928
|
|
68.30 0.5725 0.5096 0.0074 0.0084 0.436 3.926 1.220 325.141 0.444 5.427 1.702 0.51 278225. 0.0613
|
|
70.83 0.5937 0.3376 0.0035 0.0062 0.324 2.916 0.579 241.531 0.329 2.575 1.087 0.51 278772. 0.0270
|
|
73.36 0.6149
|
|
|
|
|
|
|
|
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 0.0909 0.0286 2.229 17.562 19.462 1662.193 1.984 86.566 5.311 0.57 307484. 0.7637
|
|
2.89 0.0212 0.0653 0.0892 0.0289 2.249 17.717 19.090 1676.922 2.002 84.912 5.163 0.57 307670. 0.7354
|
|
5.77 0.0423 0.1270 0.0873 0.0291 2.266 17.849 18.694 1689.386 2.017 83.150 5.019 0.57 307869. 0.7074
|
|
8.66 0.0635 0.1852 0.0853 0.0293 2.279 17.953 18.273 1699.227 2.028 81.278 4.878 0.57 308081. 0.6797
|
|
11.55 0.0847 0.2399 0.0833 0.0294 2.288 18.025 17.827 1706.103 2.037 79.294 4.739 0.57 308307. 0.6523
|
|
14.43 0.1058 0.2913 0.0811 0.0294 2.293 18.063 17.354 1709.659 2.041 77.193 4.604 0.57 308547. 0.6252
|
|
17.32 0.1270 0.3396 0.0787 0.0294 2.293 18.062 16.856 1709.537 2.041 74.974 4.472 0.57 308801. 0.5985
|
|
20.21 0.1482 0.3847 0.0763 0.0294 2.287 18.018 16.330 1705.419 2.036 72.638 4.343 0.57 309070. 0.5721
|
|
23.09 0.1694 0.4270 0.0737 0.0292 2.276 17.930 15.779 1697.027 2.026 70.187 4.217 0.57 309353. 0.5461
|
|
25.98 0.1905 0.4663 0.0710 0.0290 2.258 17.793 15.203 1684.118 2.010 67.624 4.095 0.57 309652. 0.5204
|
|
28.87 0.2117 0.5030 0.0682 0.0287 2.235 17.607 14.603 1666.479 1.989 64.953 3.974 0.57 309967. 0.4951
|
|
31.75 0.2329 0.5369 0.0653 0.0283 2.205 17.368 13.979 1643.909 1.962 62.179 3.857 0.57 310298. 0.4701
|
|
34.64 0.2540 0.5682 0.0623 0.0278 2.167 17.076 13.333 1616.211 1.929 59.306 3.742 0.57 310644. 0.4454
|
|
37.53 0.2752 0.5970 0.0592 0.0273 2.123 16.727 12.666 1583.195 1.890 56.338 3.629 0.57 311008. 0.4210
|
|
40.41 0.2964 0.6231 0.0559 0.0266 2.071 16.320 11.978 1544.674 1.844 53.279 3.517 0.57 311388. 0.3968
|
|
43.30 0.3175 0.6467 0.0526 0.0258 2.012 15.853 11.271 1500.467 1.791 50.133 3.407 0.57 311785. 0.3729
|
|
46.19 0.3387 0.6677 0.0493 0.0250 1.945 15.324 10.545 1450.396 1.731 46.906 3.298 0.57 312199. 0.3491
|
|
49.07 0.3599 0.6860 0.0458 0.0240 1.870 14.731 9.802 1394.301 1.664 43.600 3.189 0.57 312631. 0.3254
|
|
51.96 0.3810 0.7014 0.0422 0.0229 1.786 14.073 9.042 1332.023 1.590 40.221 3.079 0.58 313080. 0.3018
|
|
54.85 0.4022 0.7136 0.0386 0.0218 1.694 13.348 8.267 1263.422 1.508 36.773 2.968 0.58 313548. 0.2782
|
|
57.73 0.4234 0.7223 0.0349 0.0205 1.594 12.556 7.478 1188.378 1.419 33.260 2.854 0.58 314033. 0.2544
|
|
60.62 0.4445 0.7269 0.0312 0.0191 1.484 11.694 6.675 1106.793 1.321 29.689 2.735 0.58 314537. 0.2304
|
|
63.51 0.4657 0.7265 0.0274 0.0175 1.366 10.762 5.860 1018.597 1.216 26.065 2.609 0.58 315059. 0.2059
|
|
66.39 0.4869 0.7195 0.0235 0.0159 1.239 9.760 5.035 923.757 1.103 22.394 2.472 0.58 315600. 0.1808
|
|
69.28 0.5081 0.7037 0.0196 0.0142 1.103 8.688 4.200 822.283 0.982 18.683 2.317 0.58 316159. 0.1548
|
|
72.17 0.5292 0.6749 0.0157 0.0123 0.958 7.546 3.359 714.239 0.853 14.941 2.133 0.58 316736. 0.1274
|
|
75.05 0.5504 0.6253 0.0117 0.0103 0.804 6.337 2.513 599.753 0.716 11.177 1.900 0.58 317332. 0.0982
|
|
77.94 0.5716 0.5384 0.0078 0.0083 0.642 5.061 1.664 479.017 0.572 7.402 1.576 0.58 317945. 0.0663
|
|
80.83 0.5927 0.3720 0.0038 0.0061 0.472 3.721 0.815 352.215 0.420 3.626 1.050 0.58 318569. 0.0309
|
|
83.71 0.6139
|
|
|
|
|
|
|
|
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 0.0923 0.0291 3.223 22.569 25.025 2403.185 2.550 111.310 4.723 0.64 345880. 0.7702
|
|
3.25 0.0212 0.0654 0.0906 0.0293 3.251 22.770 24.551 2424.552 2.573 109.204 4.593 0.64 346091. 0.7418
|
|
6.50 0.0424 0.1272 0.0887 0.0295 3.276 22.939 24.046 2442.565 2.592 106.956 4.465 0.64 346317. 0.7138
|
|
9.75 0.0635 0.1855 0.0868 0.0297 3.295 23.072 23.508 2456.713 2.607 104.566 4.340 0.64 346557. 0.6860
|
|
13.00 0.0847 0.2403 0.0846 0.0298 3.308 23.164 22.938 2466.488 2.617 102.028 4.218 0.64 346813. 0.6586
|
|
16.24 0.1059 0.2919 0.0824 0.0299 3.314 23.210 22.334 2471.379 2.622 99.340 4.099 0.64 347085. 0.6314
|
|
19.49 0.1271 0.3403 0.0801 0.0299 3.313 23.205 21.695 2470.872 2.622 96.499 3.982 0.64 347373. 0.6047
|
|
22.74 0.1482 0.3857 0.0776 0.0298 3.305 23.145 21.022 2464.493 2.615 93.505 3.869 0.64 347677. 0.5782
|
|
25.99 0.1694 0.4282 0.0750 0.0297 3.288 23.026 20.315 2451.833 2.601 90.361 3.758 0.64 347999. 0.5522
|
|
29.24 0.1906 0.4679 0.0722 0.0294 3.262 22.845 19.575 2432.553 2.581 87.071 3.650 0.64 348337. 0.5264
|
|
32.49 0.2118 0.5048 0.0694 0.0291 3.227 22.599 18.804 2406.347 2.553 83.641 3.544 0.64 348693. 0.5010
|
|
35.74 0.2330 0.5391 0.0664 0.0287 3.182 22.285 18.003 2372.929 2.518 80.077 3.441 0.64 349067. 0.4760
|
|
38.99 0.2541 0.5709 0.0634 0.0282 3.127 21.901 17.173 2332.025 2.474 76.384 3.340 0.64 349460. 0.4512
|
|
42.24 0.2753 0.6001 0.0602 0.0276 3.062 21.444 16.315 2283.366 2.423 72.568 3.241 0.65 349870. 0.4267
|
|
45.48 0.2965 0.6267 0.0569 0.0269 2.986 20.912 15.430 2226.688 2.363 68.634 3.143 0.65 350300. 0.4025
|
|
48.73 0.3177 0.6509 0.0536 0.0262 2.899 20.302 14.521 2161.734 2.294 64.588 3.047 0.65 350749. 0.3785
|
|
51.98 0.3388 0.6725 0.0501 0.0253 2.800 19.612 13.587 2088.257 2.216 60.435 2.951 0.65 351217. 0.3546
|
|
55.23 0.3600 0.6915 0.0466 0.0243 2.690 18.839 12.631 2006.020 2.128 56.181 2.856 0.65 351704. 0.3309
|
|
58.48 0.3812 0.7076 0.0430 0.0232 2.568 17.983 11.653 1914.804 2.032 51.831 2.760 0.65 352212. 0.3071
|
|
61.73 0.4024 0.7208 0.0393 0.0220 2.433 17.040 10.655 1814.412 1.925 47.392 2.663 0.65 352739. 0.2834
|
|
64.98 0.4236 0.7305 0.0356 0.0206 2.286 16.009 9.638 1704.665 1.809 42.869 2.564 0.65 353287. 0.2595
|
|
68.23 0.4447 0.7362 0.0318 0.0192 2.126 14.889 8.604 1585.423 1.682 38.269 2.461 0.65 353855. 0.2354
|
|
71.48 0.4659 0.7371 0.0279 0.0176 1.953 13.679 7.554 1456.588 1.545 33.600 2.352 0.65 354444. 0.2107
|
|
74.72 0.4871 0.7316 0.0240 0.0159 1.768 12.379 6.490 1318.112 1.399 28.869 2.233 0.65 355053. 0.1855
|
|
77.97 0.5083 0.7176 0.0200 0.0142 1.569 10.988 5.415 1170.008 1.241 24.087 2.099 0.65 355683. 0.1592
|
|
81.22 0.5294 0.6909 0.0160 0.0122 1.358 9.508 4.331 1012.373 1.074 19.262 1.940 0.65 356334. 0.1316
|
|
84.47 0.5506 0.6436 0.0120 0.0102 1.134 7.939 3.239 845.393 0.897 14.409 1.738 0.65 357005. 0.1020
|
|
87.72 0.5718 0.5589 0.0079 0.0081 0.898 6.286 2.145 669.349 0.710 9.540 1.453 0.65 357695. 0.0694
|
|
90.97 0.5930 0.3918 0.0039 0.0059 0.650 4.550 1.049 484.516 0.514 4.668 0.982 0.65 358399. 0.0328
|
|
94.22 0.6142
|
|
|
|
|
|
|
|
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 0.0941 0.0297 4.523 28.505 31.482 3372.471 3.220 140.032 4.234 0.71 384256. 0.7744
|
|
3.60 0.0211 0.0650 0.0924 0.0300 4.561 28.749 30.895 3401.325 3.248 137.423 4.120 0.71 384492. 0.7465
|
|
7.20 0.0422 0.1265 0.0905 0.0302 4.594 28.954 30.269 3425.623 3.271 134.634 4.008 0.71 384745. 0.7188
|
|
10.80 0.0634 0.1846 0.0885 0.0304 4.619 29.115 29.601 3444.619 3.289 131.665 3.898 0.71 385014. 0.6913
|
|
14.40 0.0845 0.2393 0.0864 0.0305 4.637 29.224 28.891 3457.583 3.302 128.509 3.790 0.71 385300. 0.6641
|
|
18.00 0.1056 0.2908 0.0841 0.0305 4.645 29.277 28.139 3463.758 3.308 125.162 3.685 0.71 385603. 0.6372
|
|
21.60 0.1267 0.3392 0.0817 0.0305 4.643 29.265 27.343 3462.392 3.306 121.621 3.582 0.71 385925. 0.6106
|
|
25.20 0.1479 0.3847 0.0792 0.0305 4.630 29.184 26.503 3452.774 3.297 117.886 3.482 0.71 386265. 0.5843
|
|
28.81 0.1690 0.4273 0.0766 0.0303 4.605 29.028 25.620 3434.308 3.280 113.959 3.384 0.72 386623. 0.5583
|
|
32.41 0.1901 0.4671 0.0738 0.0300 4.568 28.793 24.696 3406.516 3.253 109.847 3.288 0.72 387001. 0.5327
|
|
36.01 0.2112 0.5043 0.0709 0.0297 4.518 28.475 23.731 3368.982 3.217 105.557 3.195 0.72 387397. 0.5074
|
|
39.61 0.2324 0.5389 0.0679 0.0293 4.454 28.073 22.728 3321.324 3.172 101.096 3.104 0.72 387814. 0.4824
|
|
43.21 0.2535 0.5710 0.0648 0.0288 4.376 27.581 21.689 3263.174 3.116 96.472 3.015 0.72 388251. 0.4577
|
|
46.81 0.2746 0.6007 0.0616 0.0282 4.283 26.998 20.614 3194.176 3.050 91.691 2.927 0.72 388708. 0.4332
|
|
50.41 0.2957 0.6279 0.0583 0.0275 4.176 26.320 19.506 3113.977 2.974 86.761 2.841 0.72 389186. 0.4090
|
|
54.01 0.3169 0.6526 0.0549 0.0267 4.053 25.545 18.365 3022.226 2.886 81.689 2.756 0.72 389684. 0.3850
|
|
57.61 0.3380 0.6749 0.0514 0.0257 3.914 24.669 17.195 2918.587 2.787 76.482 2.672 0.72 390204. 0.3612
|
|
61.21 0.3591 0.6946 0.0478 0.0247 3.759 23.689 15.995 2802.737 2.676 71.146 2.588 0.72 390746. 0.3375
|
|
64.81 0.3802 0.7117 0.0441 0.0236 3.586 22.604 14.768 2674.379 2.554 65.688 2.505 0.72 391309. 0.3138
|
|
68.41 0.4014 0.7258 0.0404 0.0223 3.397 21.412 13.515 2533.244 2.419 60.117 2.420 0.72 391894. 0.2900
|
|
72.01 0.4225 0.7366 0.0366 0.0210 3.190 20.109 12.239 2379.086 2.272 54.439 2.333 0.72 392502. 0.2661
|
|
75.61 0.4436 0.7437 0.0327 0.0195 2.966 18.694 10.940 2211.720 2.112 48.662 2.244 0.72 393132. 0.2419
|
|
79.22 0.4647 0.7462 0.0288 0.0179 2.724 17.167 9.621 2031.033 1.939 42.796 2.149 0.72 393784. 0.2173
|
|
82.82 0.4859 0.7427 0.0248 0.0162 2.463 15.527 8.285 1837.006 1.754 36.851 2.046 0.72 394459. 0.1919
|
|
86.42 0.5070 0.7310 0.0207 0.0144 2.185 13.775 6.933 1629.723 1.556 30.837 1.929 0.72 395157. 0.1656
|
|
90.02 0.5281 0.7072 0.0166 0.0124 1.890 11.913 5.569 1409.413 1.346 24.769 1.792 0.72 395878. 0.1379
|
|
93.62 0.5492 0.6638 0.0125 0.0104 1.578 9.944 4.195 1176.467 1.123 18.660 1.617 0.72 396621. 0.1080
|
|
97.22 0.5703 0.5846 0.0084 0.0082 1.249 7.873 2.817 931.458 0.889 12.528 1.372 0.73 397385. 0.0750
|
|
100.82 0.5915 0.4266 0.0043 0.0060 0.905 5.705 1.437 675.020 0.645 6.390 0.965 0.73 398164. 0.0377
|
|
104.42 0.6126 0.0116 0.0001 0.0035 0.537 3.385 0.022 400.483 0.382 0.100 0.025 0.73 398743. 0.0001
|
|
|
|
|
|
|
|
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 0.0962 0.0313 6.328 36.260 38.951 4718.940 4.097 173.255 3.744 0.79 422606. 0.7617
|
|
3.97 0.0212 0.0636 0.0945 0.0314 6.363 36.461 38.238 4745.181 4.119 170.082 3.655 0.79 422869. 0.7368
|
|
7.93 0.0423 0.1241 0.0926 0.0316 6.391 36.619 37.473 4765.690 4.137 166.681 3.566 0.79 423151. 0.7117
|
|
11.90 0.0635 0.1815 0.0906 0.0317 6.410 36.726 36.657 4779.603 4.149 163.051 3.479 0.79 423450. 0.6866
|
|
15.87 0.0846 0.2360 0.0884 0.0317 6.418 36.775 35.788 4786.042 4.155 159.185 3.392 0.79 423769. 0.6614
|
|
19.84 0.1058 0.2875 0.0861 0.0317 6.416 36.760 34.864 4784.076 4.153 155.077 3.305 0.79 424107. 0.6362
|
|
23.80 0.1270 0.3361 0.0837 0.0316 6.400 36.673 33.886 4772.721 4.143 150.724 3.220 0.79 424465. 0.6111
|
|
27.77 0.1481 0.3818 0.0812 0.0315 6.371 36.506 32.852 4751.011 4.124 146.124 3.136 0.79 424843. 0.5860
|
|
31.74 0.1693 0.4249 0.0785 0.0313 6.327 36.253 31.763 4718.104 4.096 141.282 3.053 0.79 425242. 0.5610
|
|
35.71 0.1904 0.4652 0.0756 0.0310 6.267 35.909 30.621 4673.271 4.057 136.203 2.972 0.79 425662. 0.5361
|
|
39.67 0.2116 0.5029 0.0727 0.0306 6.190 35.468 29.429 4615.883 4.007 130.898 2.892 0.79 426103. 0.5114
|
|
43.64 0.2327 0.5381 0.0696 0.0301 6.095 34.926 28.187 4545.353 3.946 125.377 2.813 0.79 426566. 0.4868
|
|
47.61 0.2539 0.5708 0.0665 0.0296 5.982 34.278 26.900 4461.095 3.873 119.649 2.735 0.79 427051. 0.4624
|
|
51.58 0.2751 0.6010 0.0632 0.0289 5.850 33.521 25.568 4362.520 3.787 113.724 2.658 0.79 427559. 0.4382
|
|
55.54 0.2962 0.6288 0.0598 0.0282 5.698 32.649 24.193 4249.042 3.689 107.612 2.583 0.79 428089. 0.4141
|
|
59.51 0.3174 0.6542 0.0563 0.0273 5.525 31.658 22.779 4120.102 3.577 101.319 2.508 0.79 428642. 0.3901
|
|
63.48 0.3385 0.6771 0.0527 0.0263 5.331 30.545 21.326 3975.262 3.451 94.857 2.433 0.79 429219. 0.3663
|
|
67.44 0.3597 0.6975 0.0490 0.0253 5.115 29.306 19.836 3814.007 3.311 88.232 2.359 0.79 429819. 0.3425
|
|
71.41 0.3809 0.7152 0.0452 0.0241 4.876 27.938 18.312 3635.988 3.156 81.454 2.284 0.79 430443. 0.3187
|
|
75.38 0.4020 0.7299 0.0414 0.0228 4.614 26.440 16.756 3440.942 2.987 74.531 2.209 0.79 431091. 0.2947
|
|
79.35 0.4232 0.7413 0.0375 0.0214 4.330 24.809 15.169 3228.774 2.803 67.474 2.131 0.79 431763. 0.2706
|
|
83.31 0.4443 0.7486 0.0335 0.0199 4.022 23.048 13.555 2999.490 2.604 60.291 2.050 0.79 432460. 0.2460
|
|
87.28 0.4655 0.7510 0.0294 0.0182 3.692 21.156 11.914 2753.245 2.390 52.994 1.963 0.79 433182. 0.2208
|
|
91.25 0.4867 0.7468 0.0253 0.0165 3.340 19.136 10.251 2490.392 2.162 45.594 1.867 0.79 433928. 0.1948
|
|
95.22 0.5078 0.7334 0.0212 0.0147 2.966 16.993 8.567 2211.467 1.920 38.106 1.757 0.80 434700. 0.1676
|
|
99.18 0.5290 0.7064 0.0170 0.0127 2.571 14.732 6.867 1917.260 1.664 30.545 1.625 0.80 435496. 0.1388
|
|
103.15 0.5501 0.6572 0.0127 0.0107 2.157 12.362 5.155 1608.834 1.397 22.929 1.453 0.80 436316. 0.1076
|
|
107.12 0.5713 0.5683 0.0085 0.0085 1.727 9.893 3.435 1287.520 1.118 15.279 1.210 0.80 437160. 0.0731
|
|
111.08 0.5925 0.3961 0.0042 0.0063 1.280 7.336 1.712 954.724 0.829 7.615 0.813 0.80 438020. 0.0347
|
|
115.05 0.6136
|
|
|
|
|
|
|
|
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 0.0987 0.0354 9.289 48.791 47.534 6927.083 5.512 211.430 3.112 0.86 460922. 0.6995
|
|
4.33 0.0212 0.0582 0.0969 0.0353 9.279 48.735 46.689 6919.121 5.506 207.673 3.061 0.86 461212. 0.6817
|
|
8.67 0.0424 0.1143 0.0950 0.0352 9.257 48.620 45.780 6902.853 5.493 203.631 3.008 0.86 461523. 0.6635
|
|
13.00 0.0636 0.1685 0.0930 0.0351 9.223 48.442 44.806 6877.490 5.473 199.297 2.955 0.86 461855. 0.6448
|
|
17.34 0.0848 0.2205 0.0908 0.0349 9.176 48.193 43.764 6842.192 5.445 194.664 2.901 0.86 462207. 0.6256
|
|
21.67 0.1060 0.2705 0.0885 0.0347 9.114 47.869 42.654 6796.162 5.408 189.727 2.847 0.86 462581. 0.6061
|
|
26.01 0.1272 0.3183 0.0861 0.0344 9.037 47.463 41.474 6738.549 5.362 184.478 2.792 0.86 462977. 0.5861
|
|
30.34 0.1483 0.3639 0.0835 0.0340 8.943 46.970 40.224 6668.514 5.307 178.918 2.736 0.86 463395. 0.5656
|
|
34.68 0.1695 0.4074 0.0808 0.0336 8.831 46.384 38.906 6585.307 5.240 173.052 2.680 0.86 463836. 0.5449
|
|
39.01 0.1907 0.4486 0.0779 0.0331 8.701 45.701 37.520 6488.295 5.163 166.889 2.623 0.86 464301. 0.5237
|
|
43.35 0.2119 0.4875 0.0749 0.0325 8.552 44.916 36.070 6376.875 5.075 160.440 2.566 0.86 464788. 0.5023
|
|
47.68 0.2331 0.5242 0.0717 0.0319 8.382 44.025 34.559 6250.370 4.974 153.718 2.508 0.86 465299. 0.4806
|
|
52.02 0.2543 0.5586 0.0685 0.0312 8.191 43.022 32.989 6108.079 4.861 146.735 2.450 0.86 465835. 0.4587
|
|
56.35 0.2755 0.5907 0.0651 0.0304 7.978 41.904 31.363 5949.255 4.734 139.502 2.391 0.86 466395. 0.4365
|
|
60.69 0.2967 0.6204 0.0616 0.0295 7.742 40.664 29.684 5773.212 4.594 132.033 2.332 0.86 466979. 0.4142
|
|
65.02 0.3179 0.6478 0.0580 0.0285 7.482 39.297 27.953 5579.220 4.440 124.337 2.273 0.86 467589. 0.3917
|
|
69.36 0.3391 0.6726 0.0543 0.0274 7.197 37.802 26.175 5366.885 4.271 116.428 2.212 0.86 468223. 0.3689
|
|
73.69 0.3603 0.6943 0.0505 0.0262 6.892 36.200 24.351 5139.449 4.090 108.314 2.149 0.86 468884. 0.3457
|
|
78.03 0.3815 0.7125 0.0467 0.0250 6.565 34.482 22.484 4895.532 3.896 100.007 2.083 0.86 469570. 0.3220
|
|
82.36 0.4026 0.7262 0.0427 0.0237 6.222 32.679 20.574 4639.563 3.692 91.515 2.011 0.86 470282. 0.2974
|
|
86.69 0.4238 0.7355 0.0387 0.0223 5.854 30.749 18.627 4365.532 3.474 82.851 1.935 0.86 471021. 0.2723
|
|
91.03 0.4450 0.7396 0.0345 0.0208 5.462 28.690 16.643 4073.305 3.241 74.029 1.853 0.87 471786. 0.2465
|
|
95.36 0.4662 0.7370 0.0304 0.0192 5.047 26.509 14.627 3763.634 2.995 65.063 1.763 0.87 472578. 0.2198
|
|
99.70 0.4874 0.7256 0.0261 0.0175 4.610 24.214 12.582 3437.717 2.736 55.966 1.660 0.87 473397. 0.1920
|
|
104.03 0.5086 0.7021 0.0218 0.0158 4.153 21.816 10.512 3097.250 2.465 46.758 1.539 0.87 474243. 0.1627
|
|
108.37 0.5298 0.6613 0.0175 0.0140 3.680 19.327 8.421 2743.948 2.184 37.458 1.392 0.87 475115. 0.1317
|
|
112.70 0.5510 0.5946 0.0131 0.0121 3.192 16.764 6.315 2380.058 1.894 28.090 1.203 0.87 476014. 0.0986
|
|
117.04 0.5722 0.4868 0.0087 0.0102 2.693 14.144 4.200 2008.015 1.598 18.682 0.949 0.87 476939. 0.0634
|
|
121.37 0.5934 0.3083 0.0043 0.0083 2.186 11.482 2.082 1630.166 1.297 9.261 0.579 0.87 477880. 0.0273
|
|
125.71 0.6146 -0.0223 -0.0002 0.0062 1.642 8.623 -0.109 1224.250 0.974 -0.485 -0.040 0.87 478481. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 13000
|
|
|
|
V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
|
|
(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
|
|
0.00 0.0000 0.0000 0.1003 0.0428 14.285 69.258 56.731 10652.268 7.825 252.338 2.416 0.93 499247. 0.5931
|
|
4.72 0.0213 0.0494 0.0987 0.0426 14.223 68.959 55.816 10606.190 7.791 248.270 2.387 0.93 499560. 0.5813
|
|
9.44 0.0426 0.0976 0.0970 0.0423 14.135 68.533 54.817 10540.809 7.743 243.828 2.359 0.93 499896. 0.5693
|
|
14.16 0.0639 0.1447 0.0950 0.0420 14.021 67.978 53.733 10455.355 7.680 239.004 2.331 0.93 500255. 0.5570
|
|
18.88 0.0852 0.1907 0.0930 0.0415 13.879 67.288 52.560 10349.268 7.602 233.786 2.303 0.93 500639. 0.5444
|
|
23.60 0.1065 0.2355 0.0907 0.0410 13.708 66.462 51.296 10222.140 7.509 228.163 2.276 0.93 501047. 0.5314
|
|
28.32 0.1278 0.2792 0.0883 0.0404 13.509 65.497 49.939 10073.744 7.400 222.128 2.248 0.93 501481. 0.5180
|
|
33.04 0.1491 0.3217 0.0858 0.0398 13.282 64.393 48.489 9904.024 7.275 215.678 2.221 0.93 501940. 0.5041
|
|
37.76 0.1704 0.3629 0.0830 0.0390 13.026 63.153 46.947 9713.252 7.135 208.821 2.192 0.93 502424. 0.4897
|
|
42.48 0.1917 0.4029 0.0802 0.0381 12.742 61.779 45.317 9501.949 6.980 201.570 2.163 0.93 502935. 0.4747
|
|
47.20 0.2130 0.4414 0.0771 0.0372 12.432 60.275 43.602 9270.613 6.810 193.940 2.133 0.93 503471. 0.4592
|
|
51.92 0.2343 0.4785 0.0739 0.0362 12.095 58.642 41.805 9019.497 6.625 185.950 2.102 0.93 504034. 0.4431
|
|
56.64 0.2556 0.5141 0.0706 0.0351 11.732 56.881 39.932 8748.602 6.426 177.616 2.070 0.93 504624. 0.4265
|
|
61.36 0.2769 0.5480 0.0672 0.0340 11.342 54.990 37.984 8457.818 6.213 168.953 2.037 0.93 505241. 0.4092
|
|
66.08 0.2982 0.5801 0.0636 0.0327 10.926 52.971 35.966 8147.214 5.985 159.979 2.002 0.93 505884. 0.3914
|
|
70.80 0.3195 0.6103 0.0599 0.0314 10.483 50.823 33.883 7816.856 5.742 150.713 1.966 0.93 506555. 0.3731
|
|
75.53 0.3408 0.6384 0.0561 0.0300 10.013 48.545 31.738 7466.453 5.485 141.172 1.928 0.93 507254. 0.3541
|
|
80.25 0.3621 0.6642 0.0522 0.0285 9.515 46.134 29.535 7095.592 5.212 131.373 1.888 0.93 507981. 0.3345
|
|
84.97 0.3834 0.6856 0.0482 0.0270 9.013 43.697 27.275 6720.795 4.937 121.320 1.841 0.94 508735. 0.3134
|
|
89.69 0.4047 0.7018 0.0442 0.0255 8.506 41.238 24.961 6342.600 4.659 111.029 1.785 0.94 509518. 0.2907
|
|
94.41 0.4260 0.7044 0.0400 0.0242 8.073 39.140 22.589 6019.905 4.422 100.478 1.702 0.94 510330. 0.2637
|
|
99.13 0.4473 0.6989 0.0357 0.0228 7.629 36.990 20.172 5689.208 4.179 89.727 1.608 0.94 511170. 0.2355
|
|
103.85 0.4686 0.6840 0.0313 0.0215 7.172 34.771 17.716 5347.904 3.928 78.801 1.503 0.94 512039. 0.2062
|
|
108.57 0.4899 0.6576 0.0269 0.0201 6.703 32.498 15.226 4998.308 3.672 67.724 1.382 0.94 512937. 0.1757
|
|
113.29 0.5112 0.6166 0.0225 0.0186 6.226 30.184 12.708 4642.418 3.410 56.524 1.242 0.94 513864. 0.1443
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|
118.01 0.5325 0.5571 0.0180 0.0172 5.745 27.852 10.170 4283.837 3.147 45.238 1.077 0.94 514820. 0.1119
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|
122.73 0.5539 0.4741 0.0135 0.0158 5.263 25.516 7.624 3924.550 2.883 33.910 0.881 0.94 515805. 0.0793
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127.45 0.5752 0.3609 0.0090 0.0143 4.783 23.191 5.080 3566.856 2.620 22.595 0.646 0.94 516817. 0.0475
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|
132.17 0.5965 0.2087 0.0045 0.0129 4.307 20.882 2.551 3211.750 2.359 11.346 0.360 0.94 517850. 0.0188
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|
136.89 0.6178 0.0000 0.0000 0.0114 3.805 18.447 0.000 2837.306 2.084 0.002 0.000 0.95 518780. 0.0000
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