501 lines
89 KiB
Plaintext
501 lines
89 KiB
Plaintext
17x13 (17x13.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 0.1172 0.0563 0.006 0.400 0.308 4.729 0.045 1.372 29.582 0.07 34419. 0.5687
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0.52 0.0322 0.0652 0.1162 0.0574 0.006 0.408 0.306 4.823 0.046 1.360 28.762 0.07 34450. 0.5506
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1.03 0.0644 0.1266 0.1151 0.0586 0.007 0.416 0.303 4.918 0.047 1.347 27.934 0.07 34485. 0.5322
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1.55 0.0966 0.1843 0.1139 0.0597 0.007 0.424 0.300 5.012 0.048 1.332 27.105 0.07 34524. 0.5135
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2.07 0.1288 0.2383 0.1124 0.0608 0.007 0.431 0.296 5.104 0.049 1.315 26.279 0.07 34567. 0.4947
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2.59 0.1611 0.2885 0.1108 0.0618 0.007 0.439 0.291 5.192 0.050 1.296 25.460 0.07 34615. 0.4758
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3.10 0.1933 0.3353 0.1089 0.0628 0.007 0.446 0.287 5.273 0.050 1.275 24.652 0.07 34667. 0.4568
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3.62 0.2255 0.3786 0.1069 0.0636 0.007 0.452 0.281 5.344 0.051 1.250 23.858 0.07 34725. 0.4379
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4.14 0.2577 0.4185 0.1045 0.0644 0.007 0.457 0.275 5.404 0.052 1.223 23.080 0.07 34787. 0.4189
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4.65 0.2899 0.4553 0.1019 0.0649 0.007 0.461 0.268 5.449 0.052 1.193 22.319 0.07 34854. 0.4001
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5.17 0.3221 0.4890 0.0990 0.0652 0.007 0.463 0.261 5.477 0.052 1.159 21.575 0.07 34926. 0.3812
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5.69 0.3543 0.5198 0.0958 0.0653 0.007 0.464 0.252 5.485 0.052 1.121 20.848 0.07 35003. 0.3624
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6.20 0.3865 0.5477 0.0923 0.0652 0.007 0.462 0.243 5.471 0.052 1.080 20.137 0.07 35086. 0.3435
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6.72 0.4188 0.5728 0.0885 0.0647 0.007 0.459 0.233 5.431 0.052 1.035 19.439 0.07 35174. 0.3247
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7.24 0.4510 0.5951 0.0843 0.0639 0.007 0.453 0.222 5.364 0.051 0.986 18.754 0.07 35267. 0.3057
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7.76 0.4832 0.6146 0.0798 0.0627 0.007 0.445 0.210 5.267 0.050 0.934 18.076 0.07 35365. 0.2867
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8.27 0.5154 0.6312 0.0750 0.0612 0.007 0.435 0.197 5.142 0.049 0.878 17.404 0.07 35468. 0.2676
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8.79 0.5476 0.6447 0.0700 0.0594 0.007 0.422 0.184 4.990 0.048 0.819 16.730 0.07 35577. 0.2485
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9.31 0.5798 0.6549 0.0647 0.0573 0.006 0.407 0.170 4.811 0.046 0.757 16.050 0.07 35690. 0.2293
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9.82 0.6120 0.6613 0.0593 0.0549 0.006 0.389 0.156 4.608 0.044 0.694 15.355 0.07 35809. 0.2099
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10.34 0.6442 0.6635 0.0537 0.0522 0.006 0.370 0.141 4.380 0.042 0.629 14.636 0.07 35932. 0.1905
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10.86 0.6764 0.6607 0.0480 0.0492 0.006 0.349 0.126 4.128 0.039 0.562 13.879 0.07 36061. 0.1708
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11.38 0.7087 0.6517 0.0422 0.0459 0.005 0.326 0.111 3.853 0.037 0.494 13.068 0.07 36194. 0.1507
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11.89 0.7409 0.6349 0.0363 0.0424 0.005 0.301 0.095 3.556 0.034 0.425 12.178 0.07 36333. 0.1303
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12.41 0.7731 0.6079 0.0303 0.0386 0.004 0.274 0.080 3.237 0.031 0.355 11.174 0.07 36476. 0.1092
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12.93 0.8053 0.5666 0.0243 0.0345 0.004 0.245 0.064 2.897 0.028 0.284 10.000 0.07 36624. 0.0875
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13.44 0.8375 0.5047 0.0182 0.0302 0.003 0.214 0.048 2.537 0.024 0.213 8.563 0.07 36777. 0.0649
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13.96 0.8697 0.4101 0.0121 0.0257 0.003 0.182 0.032 2.157 0.021 0.142 6.702 0.07 36935. 0.0414
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14.48 0.9019 0.2598 0.0060 0.0210 0.002 0.149 0.016 1.760 0.017 0.071 4.094 0.07 37098. 0.0179
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14.99 0.9341 0.0000 0.0000 0.0160 0.002 0.114 0.000 1.347 0.013 0.000 0.000 0.07 37264. 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 0.1177 0.0513 0.046 1.457 1.239 34.487 0.165 5.509 16.290 0.13 68837. 0.6276
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1.04 0.0324 0.0720 0.1167 0.0525 0.047 1.491 1.228 35.275 0.168 5.464 15.796 0.13 68900. 0.6060
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2.08 0.0648 0.1396 0.1156 0.0537 0.048 1.525 1.217 36.075 0.172 5.413 15.300 0.13 68970. 0.5842
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3.12 0.0972 0.2026 0.1144 0.0549 0.049 1.558 1.204 36.874 0.176 5.354 14.806 0.13 69049. 0.5623
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4.16 0.1296 0.2612 0.1130 0.0561 0.050 1.591 1.189 37.656 0.180 5.287 14.318 0.13 69136. 0.5404
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5.20 0.1620 0.3155 0.1113 0.0572 0.052 1.623 1.172 38.405 0.183 5.211 13.837 0.13 69232. 0.5185
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6.24 0.1944 0.3657 0.1095 0.0582 0.052 1.652 1.152 39.102 0.187 5.125 13.366 0.13 69338. 0.4967
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7.28 0.2268 0.4120 0.1074 0.0591 0.053 1.679 1.130 39.725 0.190 5.028 12.907 0.13 69453. 0.4750
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8.32 0.2592 0.4546 0.1051 0.0599 0.054 1.701 1.106 40.254 0.192 4.919 12.461 0.13 69579. 0.4536
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9.36 0.2916 0.4937 0.1025 0.0605 0.055 1.719 1.078 40.667 0.194 4.797 12.028 0.14 69714. 0.4324
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10.40 0.3241 0.5294 0.0996 0.0609 0.055 1.730 1.048 40.941 0.195 4.661 11.609 0.14 69860. 0.4114
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11.44 0.3565 0.5620 0.0964 0.0611 0.055 1.735 1.014 41.053 0.196 4.510 11.203 0.14 70017. 0.3905
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12.48 0.3889 0.5917 0.0928 0.0610 0.055 1.732 0.977 40.979 0.196 4.345 10.811 0.14 70184. 0.3699
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13.52 0.4213 0.6184 0.0889 0.0606 0.055 1.720 0.936 40.697 0.194 4.163 10.430 0.14 70361. 0.3493
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14.56 0.4537 0.6424 0.0847 0.0598 0.054 1.698 0.891 40.186 0.192 3.965 10.061 0.14 70549. 0.3288
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15.60 0.4861 0.6636 0.0802 0.0587 0.053 1.667 0.843 39.437 0.188 3.752 9.701 0.14 70748. 0.3084
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16.64 0.5185 0.6822 0.0753 0.0572 0.052 1.625 0.793 38.450 0.184 3.525 9.349 0.14 70957. 0.2881
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17.69 0.5509 0.6979 0.0702 0.0554 0.050 1.574 0.739 37.234 0.178 3.287 9.002 0.14 71176. 0.2679
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18.73 0.5833 0.7106 0.0649 0.0533 0.048 1.513 0.683 35.797 0.171 3.039 8.657 0.14 71405. 0.2477
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19.77 0.6157 0.7201 0.0595 0.0508 0.046 1.443 0.626 34.147 0.163 2.783 8.310 0.14 71645. 0.2275
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20.81 0.6481 0.7258 0.0538 0.0481 0.043 1.365 0.566 32.290 0.154 2.520 7.957 0.14 71895. 0.2073
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21.85 0.6805 0.7272 0.0481 0.0450 0.041 1.278 0.506 30.232 0.144 2.251 7.592 0.14 72155. 0.1870
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22.89 0.7129 0.7231 0.0422 0.0416 0.038 1.182 0.445 27.977 0.134 1.977 7.207 0.14 72425. 0.1663
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23.93 0.7453 0.7120 0.0363 0.0380 0.034 1.079 0.382 25.528 0.122 1.699 6.788 0.14 72705. 0.1452
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24.97 0.7777 0.6916 0.0303 0.0341 0.031 0.967 0.319 22.892 0.109 1.418 6.318 0.14 72995. 0.1235
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26.01 0.8101 0.6574 0.0242 0.0299 0.027 0.848 0.255 20.073 0.096 1.135 5.766 0.14 73294. 0.1008
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27.05 0.8425 0.6019 0.0182 0.0254 0.023 0.722 0.191 17.081 0.082 0.850 5.076 0.14 73604. 0.0768
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28.09 0.8749 0.5096 0.0121 0.0207 0.019 0.588 0.127 13.925 0.066 0.565 4.139 0.14 73923. 0.0511
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29.13 0.9073 0.3447 0.0060 0.0158 0.014 0.449 0.063 10.619 0.051 0.281 2.699 0.14 74251. 0.0235
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30.17 0.9398 -0.0015 0.0000 0.0107 0.010 0.303 0.000 7.177 0.034 -0.001 -0.012 0.14 74585. 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 0.1181 0.0494 0.150 3.154 2.795 111.935 0.356 12.433 11.326 0.20 103253. 0.6555
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1.56 0.0325 0.0752 0.1171 0.0506 0.154 3.230 2.773 114.655 0.365 12.333 10.969 0.20 103348. 0.6323
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3.13 0.0650 0.1455 0.1160 0.0518 0.157 3.308 2.747 117.423 0.374 12.220 10.612 0.20 103454. 0.6089
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4.69 0.0974 0.2110 0.1148 0.0530 0.161 3.386 2.718 120.195 0.383 12.090 10.257 0.20 103572. 0.5853
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6.26 0.1299 0.2717 0.1134 0.0542 0.165 3.463 2.685 122.916 0.391 11.941 9.906 0.20 103703. 0.5619
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7.82 0.1624 0.3279 0.1118 0.0554 0.168 3.537 2.647 125.528 0.400 11.772 9.563 0.20 103848. 0.5385
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9.39 0.1949 0.3797 0.1100 0.0564 0.172 3.605 2.603 127.964 0.407 11.580 9.227 0.20 104007. 0.5154
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10.95 0.2274 0.4273 0.1079 0.0574 0.175 3.667 2.554 130.156 0.414 11.362 8.902 0.20 104181. 0.4925
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12.51 0.2599 0.4710 0.1056 0.0582 0.177 3.720 2.499 132.029 0.420 11.117 8.586 0.20 104370. 0.4699
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14.08 0.2923 0.5111 0.1030 0.0589 0.179 3.761 2.438 133.506 0.425 10.842 8.281 0.20 104574. 0.4476
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15.64 0.3248 0.5477 0.1000 0.0593 0.180 3.790 2.369 134.510 0.428 10.536 7.987 0.20 104794. 0.4256
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17.21 0.3573 0.5811 0.0968 0.0595 0.181 3.802 2.292 134.961 0.430 10.197 7.704 0.20 105030. 0.4038
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18.77 0.3898 0.6115 0.0933 0.0594 0.181 3.797 2.208 134.775 0.429 9.822 7.432 0.20 105282. 0.3823
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20.33 0.4223 0.6390 0.0894 0.0591 0.180 3.772 2.116 133.875 0.426 9.411 7.169 0.20 105549. 0.3610
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21.90 0.4548 0.6638 0.0851 0.0583 0.177 3.724 2.015 132.192 0.421 8.964 6.915 0.20 105833. 0.3398
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23.46 0.4872 0.6860 0.0805 0.0572 0.174 3.654 1.907 129.688 0.413 8.482 6.669 0.20 106132. 0.3188
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25.03 0.5197 0.7055 0.0757 0.0557 0.169 3.560 1.791 126.367 0.402 7.969 6.430 0.20 106446. 0.2979
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26.59 0.5522 0.7224 0.0705 0.0539 0.164 3.444 1.670 122.253 0.389 7.429 6.197 0.20 106777. 0.2772
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28.16 0.5847 0.7365 0.0652 0.0518 0.157 3.307 1.544 117.375 0.374 6.868 5.967 0.21 107123. 0.2567
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29.72 0.6172 0.7476 0.0597 0.0493 0.150 3.149 1.414 111.758 0.356 6.289 5.738 0.21 107484. 0.2362
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31.28 0.6496 0.7553 0.0541 0.0465 0.141 2.970 1.280 105.423 0.336 5.694 5.507 0.21 107860. 0.2157
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32.85 0.6821 0.7590 0.0483 0.0434 0.132 2.772 1.143 98.387 0.313 5.085 5.271 0.21 108252. 0.1951
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34.41 0.7146 0.7578 0.0424 0.0400 0.122 2.554 1.004 90.664 0.289 4.466 5.023 0.21 108658. 0.1743
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35.98 0.7471 0.7504 0.0364 0.0363 0.110 2.318 0.863 82.269 0.262 3.838 4.758 0.21 109080. 0.1530
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37.54 0.7796 0.7342 0.0304 0.0323 0.098 2.063 0.720 73.217 0.233 3.203 4.461 0.21 109517. 0.1311
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39.10 0.8121 0.7053 0.0243 0.0280 0.085 1.790 0.576 63.531 0.202 2.563 4.114 0.21 109968. 0.1081
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40.67 0.8445 0.6557 0.0182 0.0235 0.071 1.500 0.432 53.239 0.169 1.920 3.678 0.21 110435. 0.0836
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42.23 0.8770 0.5688 0.0121 0.0187 0.057 1.194 0.287 42.379 0.135 1.277 3.072 0.21 110915. 0.0570
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43.80 0.9095 0.4018 0.0060 0.0137 0.042 0.873 0.143 30.998 0.099 0.636 2.092 0.21 111410. 0.0274
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45.36 0.9420 0.0003 0.0000 0.0084 0.026 0.539 0.000 19.136 0.061 0.000 0.001 0.21 111911. 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 0.1184 0.0484 0.349 5.492 4.985 259.930 0.621 22.173 8.699 0.27 137667. 0.6723
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2.09 0.0325 0.0771 0.1175 0.0496 0.357 5.631 4.946 266.493 0.636 22.000 8.418 0.27 137793. 0.6481
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4.18 0.0651 0.1490 0.1164 0.0508 0.366 5.773 4.902 273.187 0.652 21.802 8.138 0.27 137934. 0.6237
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6.27 0.0976 0.2159 0.1152 0.0521 0.375 5.914 4.851 279.897 0.668 21.575 7.860 0.27 138092. 0.5993
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8.35 0.1301 0.2778 0.1138 0.0533 0.384 6.054 4.792 286.497 0.684 21.315 7.587 0.27 138268. 0.5749
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10.44 0.1626 0.3350 0.1123 0.0545 0.393 6.188 4.725 292.844 0.699 21.018 7.319 0.27 138461. 0.5507
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12.53 0.1952 0.3877 0.1105 0.0556 0.401 6.313 4.649 298.780 0.713 20.679 7.058 0.27 138674. 0.5268
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14.62 0.2277 0.4361 0.1084 0.0566 0.408 6.427 4.563 304.134 0.726 20.295 6.805 0.27 138906. 0.5032
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16.71 0.2602 0.4805 0.1061 0.0575 0.414 6.524 4.465 308.728 0.737 19.862 6.560 0.27 139159. 0.4799
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18.80 0.2927 0.5212 0.1035 0.0581 0.419 6.601 4.356 312.377 0.746 19.375 6.325 0.27 139432. 0.4569
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20.88 0.3253 0.5583 0.1006 0.0586 0.422 6.654 4.234 314.892 0.752 18.831 6.098 0.27 139727. 0.4343
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22.97 0.3578 0.5922 0.0974 0.0588 0.424 6.679 4.098 316.078 0.755 18.227 5.880 0.27 140042. 0.4121
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25.06 0.3903 0.6231 0.0938 0.0588 0.423 6.672 3.948 315.738 0.754 17.560 5.671 0.27 140378. 0.3901
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27.15 0.4229 0.6511 0.0899 0.0584 0.421 6.628 3.783 313.679 0.749 16.827 5.470 0.27 140736. 0.3683
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29.24 0.4554 0.6764 0.0856 0.0576 0.415 6.545 3.604 309.738 0.739 16.028 5.277 0.27 141115. 0.3468
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31.33 0.4879 0.6991 0.0810 0.0565 0.407 6.420 3.410 303.821 0.725 15.167 5.090 0.27 141515. 0.3254
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33.42 0.5204 0.7193 0.0761 0.0551 0.397 6.253 3.204 295.934 0.706 14.250 4.910 0.27 141936. 0.3042
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35.50 0.5530 0.7370 0.0710 0.0532 0.384 6.046 2.987 286.132 0.683 13.286 4.735 0.27 142378. 0.2833
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37.59 0.5855 0.7520 0.0656 0.0511 0.368 5.800 2.761 274.483 0.655 12.282 4.563 0.27 142840. 0.2625
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39.68 0.6180 0.7642 0.0601 0.0486 0.350 5.516 2.528 261.049 0.623 11.246 4.393 0.27 143323. 0.2418
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41.77 0.6505 0.7732 0.0544 0.0458 0.330 5.196 2.289 245.877 0.587 10.181 4.223 0.27 143827. 0.2211
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43.86 0.6831 0.7786 0.0486 0.0426 0.307 4.839 2.044 229.006 0.547 9.094 4.049 0.28 144350. 0.2004
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45.95 0.7156 0.7794 0.0427 0.0392 0.282 4.447 1.796 210.470 0.502 7.987 3.870 0.28 144894. 0.1795
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48.03 0.7481 0.7745 0.0367 0.0354 0.255 4.021 1.543 190.304 0.454 6.864 3.678 0.28 145458. 0.1581
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50.12 0.7807 0.7614 0.0306 0.0314 0.226 3.562 1.288 168.549 0.402 5.728 3.465 0.28 146042. 0.1361
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52.21 0.8132 0.7364 0.0245 0.0270 0.195 3.069 1.030 145.255 0.347 4.583 3.217 0.28 146645. 0.1131
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54.30 0.8457 0.6917 0.0183 0.0224 0.162 2.546 0.772 120.493 0.288 3.433 2.906 0.28 147269. 0.0884
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56.39 0.8782 0.6101 0.0122 0.0176 0.127 1.994 0.513 94.354 0.225 2.284 2.468 0.28 147911. 0.0612
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58.48 0.9108 0.4446 0.0061 0.0125 0.090 1.415 0.256 66.959 0.160 1.139 1.734 0.28 148572. 0.0304
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60.57 0.9433 0.0016 0.0000 0.0071 0.051 0.811 0.000 38.383 0.092 0.002 0.006 0.28 149240. 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 0.1189 0.0478 0.673 8.488 7.817 502.097 0.959 34.771 7.062 0.34 172078. 0.6835
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2.61 0.0326 0.0783 0.1180 0.0491 0.691 8.708 7.758 515.142 0.984 34.509 6.831 0.34 172235. 0.6587
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5.23 0.0651 0.1513 0.1169 0.0504 0.709 8.933 7.691 528.466 1.009 34.208 6.601 0.34 172412. 0.6337
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7.84 0.0977 0.2191 0.1157 0.0516 0.727 9.160 7.613 541.844 1.035 33.861 6.372 0.34 172610. 0.6086
|
|
10.46 0.1303 0.2818 0.1144 0.0529 0.744 9.382 7.523 555.024 1.060 33.462 6.148 0.34 172829. 0.5837
|
|
13.07 0.1628 0.3397 0.1128 0.0541 0.761 9.597 7.420 567.721 1.084 33.005 5.928 0.34 173072. 0.5590
|
|
15.68 0.1954 0.3929 0.1110 0.0552 0.777 9.798 7.303 579.616 1.107 32.483 5.715 0.34 173338. 0.5346
|
|
18.30 0.2280 0.4418 0.1090 0.0562 0.792 9.980 7.169 590.369 1.128 31.888 5.508 0.34 173629. 0.5105
|
|
20.91 0.2606 0.4866 0.1067 0.0571 0.804 10.136 7.018 599.625 1.145 31.215 5.308 0.34 173946. 0.4868
|
|
23.53 0.2931 0.5277 0.1041 0.0578 0.814 10.261 6.847 607.012 1.159 30.457 5.116 0.34 174289. 0.4635
|
|
26.14 0.3257 0.5652 0.1012 0.0583 0.821 10.348 6.657 612.152 1.169 29.609 4.932 0.34 174658. 0.4405
|
|
28.75 0.3583 0.5994 0.0980 0.0586 0.824 10.391 6.444 614.660 1.174 28.665 4.755 0.34 175053. 0.4179
|
|
31.37 0.3908 0.6306 0.0944 0.0585 0.824 10.382 6.210 614.141 1.173 27.620 4.586 0.34 175475. 0.3956
|
|
33.98 0.4234 0.6590 0.0905 0.0581 0.818 10.315 5.951 610.211 1.165 26.471 4.424 0.34 175924. 0.3736
|
|
36.59 0.4560 0.6847 0.0862 0.0574 0.808 10.186 5.669 602.543 1.151 25.217 4.268 0.34 176399. 0.3518
|
|
39.21 0.4885 0.7078 0.0816 0.0563 0.792 9.990 5.365 590.954 1.129 23.864 4.118 0.34 176900. 0.3302
|
|
41.82 0.5211 0.7285 0.0766 0.0548 0.772 9.728 5.041 575.445 1.099 22.422 3.973 0.34 177428. 0.3088
|
|
44.44 0.5537 0.7467 0.0715 0.0530 0.746 9.401 4.700 556.130 1.062 20.905 3.833 0.34 177982. 0.2877
|
|
47.05 0.5862 0.7624 0.0661 0.0508 0.715 9.012 4.345 533.141 1.018 19.326 3.696 0.34 178562. 0.2667
|
|
49.66 0.6188 0.7755 0.0605 0.0483 0.679 8.564 3.978 506.597 0.968 17.694 3.562 0.34 179167. 0.2459
|
|
52.28 0.6514 0.7855 0.0548 0.0454 0.639 8.057 3.601 476.594 0.910 16.018 3.427 0.34 179798. 0.2251
|
|
54.89 0.6839 0.7921 0.0489 0.0422 0.594 7.492 3.216 443.207 0.846 14.306 3.291 0.34 180455. 0.2043
|
|
57.51 0.7165 0.7944 0.0429 0.0387 0.545 6.872 2.824 406.505 0.776 12.562 3.151 0.34 181136. 0.1833
|
|
60.12 0.7491 0.7914 0.0369 0.0349 0.492 6.196 2.427 366.556 0.700 10.793 3.003 0.35 181843. 0.1619
|
|
62.73 0.7817 0.7807 0.0308 0.0308 0.434 5.468 2.024 323.441 0.618 9.004 2.839 0.35 182574. 0.1398
|
|
65.35 0.8142 0.7588 0.0246 0.0264 0.372 4.687 1.619 277.263 0.530 7.201 2.649 0.35 183331. 0.1167
|
|
67.96 0.8468 0.7178 0.0184 0.0217 0.306 3.857 1.212 228.160 0.436 5.391 2.409 0.35 184112. 0.0918
|
|
70.58 0.8794 0.6405 0.0122 0.0168 0.236 2.981 0.805 176.318 0.337 3.580 2.070 0.35 184917. 0.0643
|
|
73.19 0.9119 0.4766 0.0061 0.0116 0.164 2.062 0.399 121.979 0.233 1.777 1.485 0.35 185745. 0.0325
|
|
75.80 0.9445 -0.0073 0.0000 0.0062 0.088 1.103 -0.003 65.253 0.125 -0.014 -0.022 0.35 186577. 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 0.1194 0.0476 1.158 12.161 11.304 863.262 1.374 50.280 5.939 0.40 206485. 0.6912
|
|
3.15 0.0327 0.0794 0.1185 0.0489 1.189 12.485 11.222 886.306 1.411 49.915 5.743 0.40 206674. 0.6660
|
|
6.30 0.0655 0.1533 0.1175 0.0502 1.220 12.818 11.127 909.885 1.448 49.494 5.547 0.40 206887. 0.6405
|
|
9.46 0.0982 0.2219 0.1163 0.0515 1.252 13.152 11.018 933.600 1.486 49.007 5.353 0.40 207126. 0.6150
|
|
12.61 0.1309 0.2853 0.1150 0.0528 1.283 13.481 10.891 956.998 1.523 48.445 5.162 0.40 207391. 0.5897
|
|
15.76 0.1636 0.3437 0.1135 0.0540 1.314 13.799 10.745 979.563 1.559 47.796 4.976 0.40 207684. 0.5646
|
|
18.91 0.1964 0.3975 0.1117 0.0552 1.342 14.097 10.578 1000.726 1.593 47.051 4.794 0.40 208006. 0.5398
|
|
22.06 0.2291 0.4468 0.1097 0.0562 1.368 14.367 10.387 1019.873 1.623 46.199 4.619 0.40 208358. 0.5153
|
|
25.21 0.2618 0.4920 0.1074 0.0571 1.390 14.599 10.169 1036.363 1.649 45.231 4.450 0.40 208741. 0.4913
|
|
28.37 0.2945 0.5333 0.1048 0.0579 1.407 14.785 9.923 1049.531 1.670 44.138 4.288 0.41 209156. 0.4676
|
|
31.52 0.3273 0.5711 0.1019 0.0584 1.420 14.914 9.647 1058.699 1.685 42.911 4.133 0.41 209603. 0.4444
|
|
34.67 0.3600 0.6056 0.0986 0.0586 1.426 14.977 9.339 1063.178 1.692 41.542 3.984 0.41 210082. 0.4215
|
|
37.82 0.3927 0.6370 0.0950 0.0586 1.425 14.964 8.998 1062.265 1.691 40.023 3.842 0.41 210593. 0.3989
|
|
40.97 0.4254 0.6656 0.0910 0.0582 1.415 14.866 8.622 1055.281 1.680 38.350 3.706 0.41 211136. 0.3767
|
|
44.13 0.4582 0.6916 0.0867 0.0574 1.397 14.674 8.211 1041.647 1.658 36.521 3.575 0.41 211712. 0.3546
|
|
47.28 0.4909 0.7150 0.0820 0.0563 1.369 14.384 7.766 1021.049 1.625 34.545 3.450 0.41 212320. 0.3328
|
|
50.43 0.5236 0.7361 0.0770 0.0548 1.332 13.996 7.293 993.502 1.581 32.439 3.330 0.41 212959. 0.3113
|
|
53.58 0.5563 0.7547 0.0717 0.0529 1.286 13.512 6.795 959.213 1.527 30.224 3.213 0.41 213630. 0.2899
|
|
56.73 0.5891 0.7709 0.0663 0.0506 1.232 12.938 6.276 918.419 1.462 27.917 3.100 0.41 214332. 0.2688
|
|
59.88 0.6218 0.7845 0.0606 0.0480 1.168 12.274 5.740 871.328 1.387 25.533 2.988 0.41 215066. 0.2478
|
|
63.04 0.6545 0.7951 0.0548 0.0451 1.097 11.525 5.190 818.107 1.302 23.084 2.877 0.41 215830. 0.2269
|
|
66.19 0.6872 0.8025 0.0489 0.0418 1.018 10.691 4.627 758.892 1.208 20.582 2.766 0.41 216625. 0.2059
|
|
69.34 0.7200 0.8057 0.0428 0.0383 0.930 9.774 4.054 693.804 1.104 18.034 2.651 0.41 217450. 0.1848
|
|
72.49 0.7527 0.8037 0.0367 0.0343 0.835 8.776 3.473 622.964 0.991 15.450 2.529 0.41 218306. 0.1632
|
|
75.64 0.7854 0.7942 0.0305 0.0301 0.733 7.699 2.886 546.520 0.870 12.836 2.395 0.42 219192. 0.1408
|
|
78.79 0.8181 0.7734 0.0242 0.0256 0.623 6.546 2.294 464.660 0.740 10.202 2.239 0.42 220108. 0.1174
|
|
81.95 0.8509 0.7331 0.0179 0.0208 0.506 5.320 1.699 377.639 0.601 7.558 2.041 0.42 221053. 0.0921
|
|
85.10 0.8836 0.6541 0.0117 0.0158 0.383 4.026 1.105 285.799 0.455 4.914 1.753 0.42 222028. 0.0638
|
|
88.25 0.9163 0.4751 0.0054 0.0105 0.254 2.671 0.513 189.583 0.302 2.283 1.228 0.42 223030. 0.0305
|
|
91.40 0.9491
|
|
|
|
|
|
|
|
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 0.1199 0.0476 1.837 16.541 15.459 1369.895 1.869 68.762 5.118 0.47 240886. 0.6967
|
|
3.66 0.0326 0.0795 0.1191 0.0489 1.887 16.990 15.354 1407.044 1.919 68.293 4.949 0.47 241106. 0.6713
|
|
7.33 0.0652 0.1535 0.1182 0.0502 1.938 17.450 15.231 1445.138 1.971 67.748 4.780 0.47 241353. 0.6458
|
|
10.99 0.0978 0.2223 0.1171 0.0515 1.989 17.913 15.089 1483.536 2.024 67.115 4.613 0.47 241629. 0.6203
|
|
14.65 0.1304 0.2858 0.1158 0.0528 2.040 18.372 14.924 1521.513 2.076 66.380 4.449 0.47 241937. 0.5949
|
|
18.32 0.1630 0.3443 0.1143 0.0541 2.090 18.815 14.732 1558.238 2.126 65.528 4.288 0.47 242277. 0.5698
|
|
21.98 0.1956 0.3982 0.1126 0.0553 2.136 19.232 14.511 1592.784 2.173 64.544 4.132 0.47 242650. 0.5449
|
|
25.64 0.2282 0.4476 0.1106 0.0564 2.178 19.611 14.257 1624.163 2.216 63.415 3.981 0.47 243059. 0.5204
|
|
29.31 0.2608 0.4929 0.1084 0.0573 2.214 19.939 13.967 1651.332 2.253 62.125 3.836 0.47 243504. 0.4963
|
|
32.97 0.2934 0.5343 0.1058 0.0581 2.244 20.204 13.638 1673.220 2.283 60.664 3.697 0.47 243985. 0.4726
|
|
36.63 0.3260 0.5723 0.1029 0.0586 2.265 20.391 13.268 1688.737 2.304 59.017 3.564 0.47 244504. 0.4494
|
|
40.30 0.3586 0.6070 0.0997 0.0589 2.275 20.488 12.854 1696.778 2.315 57.175 3.436 0.47 245060. 0.4264
|
|
43.96 0.3912 0.6387 0.0961 0.0589 2.275 20.481 12.394 1696.222 2.314 55.128 3.314 0.47 245653. 0.4039
|
|
47.62 0.4238 0.6675 0.0922 0.0585 2.261 20.358 11.885 1685.978 2.300 52.866 3.197 0.47 246284. 0.3816
|
|
51.28 0.4564 0.6938 0.0879 0.0578 2.233 20.105 11.329 1665.102 2.272 50.390 3.086 0.48 246952. 0.3595
|
|
54.95 0.4890 0.7176 0.0832 0.0567 2.190 19.718 10.726 1633.051 2.228 47.708 2.979 0.48 247657. 0.3377
|
|
58.61 0.5216 0.7391 0.0782 0.0552 2.132 19.196 10.082 1589.813 2.169 44.845 2.876 0.48 248399. 0.3162
|
|
62.27 0.5542 0.7583 0.0730 0.0533 2.059 18.543 9.404 1535.706 2.095 41.828 2.777 0.48 249178. 0.2948
|
|
65.94 0.5868 0.7751 0.0675 0.0511 1.973 17.763 8.696 1471.117 2.007 38.682 2.681 0.48 249992. 0.2737
|
|
69.60 0.6194 0.7894 0.0618 0.0485 1.873 16.861 7.965 1396.390 1.905 35.428 2.587 0.48 250843. 0.2527
|
|
73.26 0.6520 0.8010 0.0560 0.0455 1.759 15.839 7.213 1311.799 1.790 32.083 2.494 0.48 251729. 0.2319
|
|
76.93 0.6846 0.8095 0.0500 0.0423 1.633 14.702 6.444 1217.569 1.661 28.662 2.400 0.48 252651. 0.2109
|
|
80.59 0.7172 0.8143 0.0439 0.0387 1.494 13.450 5.660 1113.895 1.520 25.177 2.305 0.48 253608. 0.1898
|
|
84.25 0.7499 0.8142 0.0377 0.0348 1.342 12.086 4.865 1000.971 1.366 21.639 2.204 0.48 254601. 0.1683
|
|
87.92 0.7825 0.8075 0.0315 0.0305 1.179 10.614 4.060 879.024 1.199 18.059 2.095 0.49 255628. 0.1461
|
|
91.58 0.8151 0.7905 0.0252 0.0260 1.004 9.036 3.249 748.347 1.021 14.450 1.969 0.49 256689. 0.1229
|
|
95.24 0.8477 0.7563 0.0189 0.0212 0.817 7.357 2.433 609.333 0.831 10.823 1.811 0.49 257785. 0.0978
|
|
98.91 0.8803 0.6878 0.0125 0.0161 0.620 5.585 1.618 462.515 0.631 7.195 1.586 0.49 258915. 0.0698
|
|
102.57 0.9129 0.5322 0.0062 0.0107 0.414 3.726 0.805 308.587 0.421 3.582 1.184 0.49 260077. 0.0368
|
|
106.23 0.9455 -0.0035 0.0000 0.0051 0.198 1.784 -0.002 147.722 0.202 -0.011 -0.008 0.49 261236. 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 0.1206 0.0477 2.750 21.665 20.299 2050.584 2.448 90.290 4.490 0.54 275282. 0.7003
|
|
4.19 0.0326 0.0797 0.1198 0.0490 2.826 22.264 20.170 2107.256 2.515 89.717 4.341 0.54 275532. 0.6750
|
|
8.38 0.0652 0.1540 0.1189 0.0504 2.904 22.880 20.019 2165.534 2.585 89.047 4.193 0.54 275814. 0.6494
|
|
12.57 0.0979 0.2229 0.1179 0.0517 2.983 23.502 19.843 2224.432 2.655 88.262 4.046 0.54 276130. 0.6239
|
|
16.76 0.1305 0.2866 0.1166 0.0531 3.061 24.119 19.637 2282.838 2.725 87.345 3.902 0.54 276481. 0.5985
|
|
20.94 0.1631 0.3453 0.1152 0.0544 3.137 24.717 19.396 2339.456 2.793 86.273 3.760 0.54 276869. 0.5733
|
|
25.13 0.1957 0.3993 0.1135 0.0557 3.209 25.281 19.116 2392.852 2.856 85.027 3.623 0.54 277297. 0.5484
|
|
29.32 0.2284 0.4488 0.1116 0.0568 3.274 25.795 18.792 2441.486 2.914 83.586 3.491 0.54 277765. 0.5239
|
|
33.51 0.2610 0.4942 0.1094 0.0578 3.331 26.241 18.420 2483.729 2.965 81.931 3.364 0.54 278274. 0.4997
|
|
37.70 0.2936 0.5358 0.1069 0.0586 3.377 26.603 17.996 2517.923 3.006 80.045 3.242 0.54 278825. 0.4760
|
|
41.89 0.3262 0.5739 0.1040 0.0591 3.409 26.861 17.516 2542.388 3.035 77.911 3.125 0.54 279419. 0.4527
|
|
46.08 0.3588 0.6087 0.1008 0.0594 3.427 26.999 16.977 2555.429 3.050 75.515 3.013 0.54 280056. 0.4298
|
|
50.27 0.3915 0.6406 0.0973 0.0594 3.427 26.998 16.376 2555.336 3.050 72.842 2.907 0.54 280736. 0.4072
|
|
54.46 0.4241 0.6697 0.0933 0.0591 3.407 26.841 15.711 2540.444 3.032 69.882 2.805 0.54 281459. 0.3849
|
|
58.65 0.4567 0.6962 0.0890 0.0584 3.365 26.512 14.980 2509.308 2.995 66.633 2.708 0.54 282225. 0.3628
|
|
62.83 0.4893 0.7203 0.0843 0.0572 3.300 26.002 14.188 2461.081 2.938 63.107 2.615 0.54 283033. 0.3409
|
|
67.02 0.5219 0.7421 0.0792 0.0557 3.213 25.312 13.340 2395.737 2.860 59.337 2.526 0.55 283883. 0.3193
|
|
71.21 0.5546 0.7617 0.0739 0.0538 3.103 24.446 12.445 2313.763 2.762 55.357 2.440 0.55 284775. 0.2979
|
|
75.40 0.5872 0.7789 0.0684 0.0515 2.971 23.410 11.512 2215.767 2.645 51.204 2.356 0.55 285708. 0.2768
|
|
79.59 0.6198 0.7938 0.0626 0.0489 2.819 22.211 10.545 2102.288 2.509 46.905 2.275 0.55 286683. 0.2557
|
|
83.78 0.6524 0.8061 0.0567 0.0459 2.647 20.853 9.551 1973.758 2.356 42.483 2.195 0.55 287698. 0.2348
|
|
87.97 0.6851 0.8155 0.0507 0.0426 2.455 19.340 8.534 1830.521 2.185 37.958 2.114 0.55 288753. 0.2138
|
|
92.16 0.7177 0.8212 0.0445 0.0389 2.243 17.675 7.497 1672.882 1.997 33.345 2.033 0.55 289849. 0.1927
|
|
96.35 0.7503 0.8224 0.0383 0.0349 2.013 15.860 6.444 1501.137 1.792 28.662 1.947 0.55 290985. 0.1711
|
|
100.54 0.7829 0.8172 0.0319 0.0306 1.764 13.900 5.378 1315.635 1.570 23.921 1.854 0.55 292161. 0.1488
|
|
104.72 0.8155 0.8023 0.0256 0.0260 1.498 11.800 4.303 1116.817 1.333 19.138 1.747 0.56 293376. 0.1255
|
|
108.91 0.8482 0.7708 0.0191 0.0211 1.214 9.565 3.222 905.282 1.081 14.331 1.614 0.56 294630. 0.1003
|
|
113.10 0.8808 0.7059 0.0127 0.0159 0.914 7.204 2.140 681.845 0.814 9.520 1.424 0.56 295923. 0.0721
|
|
117.29 0.9134 0.5539 0.0063 0.0104 0.600 4.729 1.063 447.570 0.534 4.728 1.077 0.56 297252. 0.0384
|
|
121.48 0.9460 -0.0113 -0.0001 0.0047 0.272 2.140 -0.010 202.541 0.242 -0.042 -0.021 0.56 298571. 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 0.1213 0.0480 3.938 27.581 25.842 2936.869 3.116 114.943 3.991 0.61 309671. 0.7023
|
|
4.71 0.0326 0.0798 0.1206 0.0493 4.049 28.357 25.692 3019.479 3.204 114.278 3.859 0.61 309952. 0.6772
|
|
9.43 0.0653 0.1541 0.1197 0.0507 4.164 29.158 25.516 3104.740 3.294 113.495 3.728 0.61 310268. 0.6518
|
|
14.14 0.0979 0.2230 0.1188 0.0521 4.279 29.970 25.308 3191.219 3.386 112.570 3.597 0.61 310622. 0.6264
|
|
18.86 0.1305 0.2868 0.1176 0.0535 4.395 30.778 25.062 3277.273 3.477 111.476 3.469 0.61 311016. 0.6011
|
|
23.57 0.1632 0.3455 0.1163 0.0549 4.507 31.564 24.772 3360.977 3.566 110.187 3.343 0.61 311453. 0.5760
|
|
28.29 0.1958 0.3995 0.1147 0.0562 4.613 32.308 24.432 3440.183 3.650 108.674 3.221 0.61 311934. 0.5512
|
|
33.00 0.2284 0.4490 0.1128 0.0574 4.710 32.988 24.035 3512.562 3.727 106.909 3.104 0.61 312461. 0.5267
|
|
37.72 0.2611 0.4945 0.1106 0.0584 4.795 33.581 23.576 3575.685 3.794 104.866 2.991 0.61 313034. 0.5027
|
|
42.43 0.2937 0.5361 0.1082 0.0593 4.864 34.063 23.049 3627.071 3.848 102.521 2.882 0.61 313656. 0.4790
|
|
47.14 0.3263 0.5743 0.1053 0.0599 4.914 34.412 22.449 3664.223 3.888 99.851 2.779 0.61 314326. 0.4558
|
|
51.86 0.3590 0.6093 0.1022 0.0602 4.941 34.604 21.771 3684.644 3.910 96.838 2.680 0.61 315044. 0.4329
|
|
56.57 0.3916 0.6413 0.0986 0.0602 4.943 34.615 21.012 3685.849 3.911 93.463 2.586 0.61 315811. 0.4103
|
|
61.29 0.4242 0.6706 0.0947 0.0599 4.915 34.423 20.169 3665.403 3.889 89.713 2.496 0.61 316626. 0.3880
|
|
66.00 0.4569 0.6973 0.0903 0.0592 4.856 34.008 19.241 3621.191 3.842 85.583 2.410 0.61 317490. 0.3659
|
|
70.72 0.4895 0.7217 0.0856 0.0580 4.763 33.358 18.231 3551.949 3.769 81.090 2.328 0.61 318402. 0.3441
|
|
75.43 0.5221 0.7439 0.0805 0.0565 4.637 32.472 17.148 3457.622 3.669 76.274 2.249 0.61 319361. 0.3225
|
|
80.15 0.5548 0.7638 0.0751 0.0545 4.478 31.357 16.003 3338.935 3.543 71.183 2.174 0.61 320367. 0.3011
|
|
84.86 0.5874 0.7816 0.0695 0.0522 4.287 30.022 14.807 3196.801 3.392 65.862 2.101 0.62 321419. 0.2798
|
|
89.57 0.6201 0.7970 0.0637 0.0495 4.066 28.475 13.568 3032.041 3.217 60.349 2.030 0.62 322518. 0.2588
|
|
94.29 0.6527 0.8100 0.0577 0.0465 3.816 26.721 12.292 2845.311 3.019 54.674 1.959 0.62 323662. 0.2378
|
|
99.00 0.6853 0.8201 0.0516 0.0431 3.536 24.766 10.985 2637.125 2.798 48.863 1.889 0.62 324852. 0.2168
|
|
103.72 0.7180 0.8267 0.0453 0.0393 3.229 22.614 9.653 2407.936 2.555 42.935 1.818 0.62 326087. 0.1956
|
|
108.43 0.7506 0.8291 0.0389 0.0353 2.894 20.268 8.299 2158.181 2.290 36.912 1.744 0.62 327366. 0.1739
|
|
113.15 0.7832 0.8253 0.0325 0.0308 2.532 17.734 6.927 1888.365 2.004 30.813 1.664 0.62 328691. 0.1516
|
|
117.86 0.8159 0.8124 0.0260 0.0261 2.144 15.018 5.543 1599.129 1.697 24.656 1.572 0.63 330060. 0.1281
|
|
122.58 0.8485 0.7836 0.0195 0.0211 1.732 12.127 4.151 1291.343 1.370 18.465 1.458 0.63 331472. 0.1028
|
|
127.29 0.8811 0.7224 0.0129 0.0158 1.296 9.074 2.758 966.188 1.025 12.266 1.295 0.63 332928. 0.0744
|
|
132.00 0.9138 0.5746 0.0064 0.0102 0.838 5.872 1.369 625.230 0.663 6.088 0.993 0.63 334425. 0.0402
|
|
136.72 0.9464 -0.0153 -0.0001 0.0044 0.360 2.520 -0.015 268.359 0.285 -0.067 -0.026 0.63 335902. 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 0.1220 0.0486 5.472 34.491 32.102 4080.746 3.897 142.790 3.568 0.67 344053. 0.6998
|
|
5.24 0.0326 0.0793 0.1214 0.0500 5.626 35.458 31.938 4195.065 4.006 142.059 3.453 0.67 344363. 0.6755
|
|
10.48 0.0653 0.1533 0.1207 0.0514 5.785 36.459 31.743 4313.553 4.119 141.191 3.338 0.67 344713. 0.6510
|
|
15.72 0.0979 0.2221 0.1198 0.0528 5.946 37.480 31.510 4434.282 4.234 140.155 3.223 0.67 345105. 0.6263
|
|
20.96 0.1306 0.2858 0.1187 0.0542 6.108 38.500 31.231 4554.987 4.350 138.914 3.110 0.67 345542. 0.6016
|
|
26.20 0.1632 0.3445 0.1174 0.0557 6.267 39.497 30.897 4672.980 4.462 137.431 2.999 0.67 346026. 0.5771
|
|
31.44 0.1959 0.3985 0.1159 0.0570 6.417 40.446 30.501 4785.238 4.570 135.668 2.891 0.67 346560. 0.5527
|
|
36.68 0.2285 0.4481 0.1142 0.0582 6.555 41.318 30.033 4888.425 4.668 133.587 2.787 0.67 347146. 0.5286
|
|
41.92 0.2612 0.4936 0.1121 0.0593 6.677 42.084 29.486 4979.025 4.755 131.152 2.686 0.67 347784. 0.5049
|
|
47.16 0.2938 0.5354 0.1097 0.0602 6.777 42.713 28.851 5053.416 4.826 128.329 2.590 0.68 348475. 0.4815
|
|
52.40 0.3265 0.5737 0.1069 0.0608 6.850 43.174 28.122 5107.952 4.878 125.089 2.497 0.68 349221. 0.4584
|
|
57.64 0.3591 0.6087 0.1038 0.0612 6.891 43.436 27.295 5138.987 4.907 121.406 2.409 0.68 350021. 0.4357
|
|
62.88 0.3917 0.6409 0.1002 0.0612 6.897 43.469 26.362 5142.895 4.911 117.258 2.325 0.68 350876. 0.4132
|
|
68.12 0.4244 0.6704 0.0963 0.0609 6.861 43.243 25.321 5116.170 4.886 112.628 2.245 0.68 351785. 0.3910
|
|
73.36 0.4570 0.6974 0.0919 0.0602 6.780 42.733 24.170 5055.795 4.828 107.510 2.168 0.68 352747. 0.3690
|
|
78.60 0.4897 0.7220 0.0871 0.0591 6.651 41.923 22.914 4959.927 4.736 101.923 2.095 0.68 353763. 0.3472
|
|
83.84 0.5223 0.7445 0.0820 0.0575 6.475 40.811 21.564 4828.443 4.611 95.917 2.026 0.68 354832. 0.3256
|
|
89.08 0.5550 0.7649 0.0765 0.0555 6.252 39.408 20.134 4662.396 4.452 89.554 1.959 0.68 355953. 0.3042
|
|
94.32 0.5876 0.7831 0.0708 0.0532 5.985 37.724 18.636 4463.141 4.262 82.893 1.894 0.68 357125. 0.2830
|
|
99.56 0.6203 0.7991 0.0649 0.0504 5.675 35.769 17.082 4231.896 4.041 75.982 1.831 0.69 358349. 0.2619
|
|
104.80 0.6529 0.8127 0.0588 0.0473 5.323 33.552 15.481 3969.641 3.791 68.861 1.769 0.69 359623. 0.2409
|
|
110.04 0.6855 0.8236 0.0526 0.0438 4.931 31.080 13.840 3677.130 3.511 61.561 1.707 0.69 360948. 0.2199
|
|
115.28 0.7182 0.8312 0.0462 0.0400 4.499 28.357 12.165 3354.996 3.204 54.111 1.645 0.69 362322. 0.1986
|
|
120.52 0.7508 0.8346 0.0398 0.0358 4.028 25.389 10.462 3003.875 2.868 46.534 1.580 0.69 363747. 0.1769
|
|
125.76 0.7835 0.8323 0.0332 0.0313 3.519 22.183 8.735 2624.475 2.506 38.855 1.510 0.69 365221. 0.1545
|
|
131.00 0.8161 0.8212 0.0266 0.0264 2.974 18.744 6.992 2217.691 2.118 31.100 1.430 0.69 366743. 0.1309
|
|
136.24 0.8488 0.7949 0.0199 0.0213 2.393 15.085 5.237 1784.788 1.704 23.295 1.331 0.70 368315. 0.1054
|
|
141.48 0.8814 0.7372 0.0132 0.0158 1.780 11.221 3.479 1327.585 1.268 15.475 1.189 0.70 369934. 0.0767
|
|
146.72 0.9141 0.5934 0.0066 0.0101 1.138 7.172 1.726 848.560 0.810 7.677 0.923 0.70 371599. 0.0420
|
|
151.96 0.9467 -0.0203 -0.0001 0.0041 0.466 2.938 -0.023 347.643 0.332 -0.104 -0.030 0.70 373230. 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 0.1228 0.0505 7.564 43.342 39.082 5640.596 4.897 173.836 3.143 0.74 378427. 0.6801
|
|
5.77 0.0327 0.0770 0.1222 0.0518 7.765 44.493 38.912 5790.388 5.027 173.081 3.048 0.74 378766. 0.6582
|
|
11.53 0.0653 0.1493 0.1216 0.0532 7.973 45.687 38.708 5945.793 5.162 172.175 2.953 0.74 379148. 0.6360
|
|
17.30 0.0980 0.2167 0.1208 0.0546 8.186 46.903 38.462 6104.075 5.299 171.078 2.858 0.74 379577. 0.6136
|
|
23.06 0.1306 0.2795 0.1199 0.0560 8.398 48.117 38.162 6262.106 5.436 169.745 2.764 0.74 380056. 0.5911
|
|
28.83 0.1633 0.3377 0.1187 0.0574 8.604 49.301 37.798 6416.204 5.570 168.126 2.672 0.74 380587. 0.5687
|
|
34.59 0.1959 0.3916 0.1174 0.0587 8.800 50.423 37.358 6562.251 5.697 166.166 2.582 0.74 381173. 0.5463
|
|
40.36 0.2286 0.4414 0.1157 0.0599 8.979 51.450 36.829 6695.814 5.813 163.815 2.495 0.74 381816. 0.5241
|
|
46.13 0.2612 0.4874 0.1137 0.0610 9.135 52.344 36.201 6812.232 5.914 161.021 2.410 0.74 382518. 0.5020
|
|
51.89 0.2939 0.5298 0.1114 0.0618 9.262 53.071 35.463 6906.785 5.996 157.738 2.329 0.74 383280. 0.4801
|
|
57.66 0.3265 0.5688 0.1087 0.0624 9.353 53.593 34.606 6974.788 6.055 153.926 2.250 0.74 384102. 0.4583
|
|
63.42 0.3592 0.6047 0.1056 0.0627 9.403 53.876 33.622 7011.571 6.087 149.548 2.175 0.74 384984. 0.4366
|
|
69.19 0.3919 0.6377 0.1021 0.0627 9.404 53.883 32.504 7012.485 6.088 144.578 2.102 0.75 385927. 0.4149
|
|
74.95 0.4245 0.6679 0.0982 0.0624 9.351 53.579 31.248 6972.899 6.053 138.992 2.033 0.75 386931. 0.3933
|
|
80.72 0.4572 0.6956 0.0938 0.0616 9.238 52.931 29.853 6888.610 5.980 132.784 1.966 0.75 387993. 0.3718
|
|
86.48 0.4898 0.7208 0.0890 0.0605 9.061 51.918 28.322 6756.790 5.866 125.977 1.901 0.75 389114. 0.3502
|
|
92.25 0.5225 0.7439 0.0838 0.0588 8.820 50.535 26.671 6576.826 5.709 118.631 1.839 0.75 390294. 0.3288
|
|
98.02 0.5551 0.7648 0.0783 0.0568 8.515 48.791 24.916 6349.805 5.512 110.826 1.780 0.75 391530. 0.3075
|
|
103.78 0.5878 0.7835 0.0725 0.0544 8.150 46.697 23.075 6077.339 5.276 102.636 1.722 0.75 392824. 0.2864
|
|
109.55 0.6204 0.8001 0.0665 0.0515 7.726 44.266 21.161 5760.947 5.001 94.124 1.666 0.75 394174. 0.2653
|
|
115.31 0.6531 0.8144 0.0603 0.0483 7.244 41.508 19.186 5401.927 4.690 85.340 1.611 0.76 395579. 0.2443
|
|
121.08 0.6857 0.8260 0.0539 0.0448 6.707 38.430 17.160 5001.365 4.342 76.327 1.556 0.76 397040. 0.2232
|
|
126.84 0.7184 0.8346 0.0474 0.0408 6.115 35.040 15.089 4560.211 3.959 67.118 1.501 0.76 398555. 0.2018
|
|
132.61 0.7510 0.8391 0.0408 0.0365 5.471 31.347 12.982 4079.537 3.542 57.743 1.443 0.76 400125. 0.1800
|
|
138.38 0.7837 0.8379 0.0341 0.0319 4.775 27.360 10.844 3560.693 3.091 48.232 1.381 0.76 401749. 0.1575
|
|
144.14 0.8164 0.8279 0.0273 0.0269 4.030 23.094 8.682 3005.499 2.609 38.617 1.310 0.76 403426. 0.1336
|
|
149.91 0.8490 0.8023 0.0204 0.0216 3.241 18.568 6.504 2416.531 2.098 28.929 1.221 0.77 405157. 0.1078
|
|
155.67 0.8817 0.7438 0.0136 0.0161 2.410 13.811 4.319 1797.371 1.560 19.209 1.090 0.77 406940. 0.0784
|
|
161.44 0.9143 0.5949 0.0067 0.0103 1.546 8.858 2.136 1152.785 1.001 9.503 0.841 0.77 408772. 0.0425
|
|
167.20 0.9470 -0.0319 -0.0001 0.0043 0.649 3.717 -0.046 483.701 0.420 -0.207 -0.044 0.77 410557. 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 0.1234 0.0550 10.708 56.241 46.754 7984.774 6.354 207.964 2.656 0.81 412794. 0.6286
|
|
6.31 0.0328 0.0715 0.1230 0.0563 10.963 57.583 46.588 8175.361 6.506 207.222 2.585 0.81 413161. 0.6107
|
|
12.62 0.0655 0.1391 0.1225 0.0577 11.228 58.975 46.387 8372.914 6.663 206.331 2.513 0.81 413576. 0.5924
|
|
18.93 0.0983 0.2026 0.1218 0.0591 11.497 60.386 46.142 8573.257 6.822 205.241 2.441 0.81 414042. 0.5740
|
|
25.25 0.1311 0.2623 0.1210 0.0605 11.763 61.782 45.839 8771.428 6.980 203.893 2.370 0.81 414563. 0.5555
|
|
31.56 0.1638 0.3183 0.1200 0.0618 12.018 63.122 45.463 8961.660 7.131 202.219 2.301 0.81 415142. 0.5371
|
|
37.87 0.1966 0.3708 0.1188 0.0630 12.254 64.362 44.997 9137.699 7.272 200.148 2.234 0.81 415782. 0.5186
|
|
44.18 0.2294 0.4200 0.1173 0.0640 12.462 65.457 44.426 9293.135 7.395 197.605 2.168 0.81 416485. 0.5003
|
|
50.49 0.2621 0.4660 0.1154 0.0649 12.635 66.362 43.732 9421.693 7.498 194.520 2.105 0.81 417254. 0.4819
|
|
56.80 0.2949 0.5091 0.1132 0.0656 12.763 67.036 42.901 9517.363 7.574 190.824 2.045 0.81 418090. 0.4636
|
|
63.12 0.3277 0.5495 0.1107 0.0660 12.840 67.438 41.920 9574.465 7.619 186.459 1.986 0.81 418993. 0.4451
|
|
69.43 0.3604 0.5871 0.1076 0.0661 12.857 67.532 40.777 9587.782 7.630 181.375 1.929 0.81 419963. 0.4264
|
|
75.74 0.3932 0.6222 0.1042 0.0658 12.810 67.282 39.463 9552.375 7.602 175.533 1.874 0.81 421001. 0.4075
|
|
82.05 0.4260 0.6547 0.1002 0.0652 12.691 66.656 37.973 9463.430 7.531 168.905 1.820 0.81 422106. 0.3882
|
|
88.36 0.4587 0.6847 0.0958 0.0642 12.494 65.621 36.304 9316.552 7.414 161.481 1.767 0.82 423276. 0.3686
|
|
94.67 0.4915 0.7122 0.0910 0.0628 12.215 64.159 34.463 9108.945 7.249 153.292 1.716 0.82 424511. 0.3487
|
|
100.99 0.5243 0.7375 0.0857 0.0609 11.855 62.268 32.467 8840.388 7.035 144.412 1.666 0.82 425810. 0.3286
|
|
107.30 0.5570 0.7604 0.0801 0.0587 11.415 59.958 30.337 8512.462 6.774 134.941 1.616 0.82 427172. 0.3082
|
|
113.61 0.5898 0.7810 0.0742 0.0560 10.899 57.245 28.096 8127.343 6.468 124.972 1.568 0.82 428597. 0.2877
|
|
119.92 0.6226 0.7991 0.0680 0.0530 10.308 54.143 25.761 7686.934 6.117 114.587 1.520 0.82 430082. 0.2671
|
|
126.23 0.6553 0.8148 0.0616 0.0496 9.645 50.661 23.348 7192.567 5.724 103.851 1.472 0.82 431629. 0.2463
|
|
132.54 0.6881 0.8273 0.0551 0.0458 8.914 46.820 20.867 6647.300 5.290 92.816 1.424 0.83 433236. 0.2252
|
|
138.86 0.7209 0.8361 0.0484 0.0417 8.116 42.631 18.329 6052.435 4.816 81.526 1.374 0.83 434902. 0.2036
|
|
145.17 0.7537 0.8400 0.0416 0.0373 7.254 38.100 15.741 5409.282 4.305 70.017 1.320 0.83 436629. 0.1813
|
|
151.48 0.7864 0.8368 0.0346 0.0325 6.330 33.247 13.113 4720.166 3.756 58.325 1.260 0.83 438414. 0.1579
|
|
157.79 0.8192 0.8219 0.0276 0.0275 5.350 28.102 10.452 3989.701 3.175 46.488 1.188 0.83 440257. 0.1330
|
|
164.10 0.8520 0.7861 0.0205 0.0222 4.323 22.708 7.767 3223.922 2.566 34.547 1.093 0.84 442159. 0.1054
|
|
170.41 0.8847 0.7068 0.0134 0.0168 3.259 17.119 5.069 2430.467 1.934 22.549 0.946 0.84 444117. 0.0737
|
|
176.72 0.9175 0.5151 0.0063 0.0112 2.171 11.401 2.373 1618.699 1.288 10.554 0.665 0.84 446129. 0.0355
|
|
183.04 0.9503
|
|
|
|
|
|
|
|
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 0.1234 0.0629 15.559 75.433 54.874 11602.024 8.522 244.082 2.145 0.87 447176. 0.5501
|
|
6.82 0.0327 0.0626 0.1231 0.0642 15.885 77.016 54.719 11845.419 8.701 243.392 2.095 0.87 447568. 0.5365
|
|
13.64 0.0654 0.1223 0.1227 0.0656 16.225 78.666 54.536 12099.281 8.888 242.575 2.044 0.87 448011. 0.5226
|
|
20.46 0.0981 0.1788 0.1222 0.0670 16.572 80.348 54.312 12357.928 9.078 241.581 1.993 0.87 448508. 0.5085
|
|
27.28 0.1307 0.2324 0.1215 0.0684 16.916 82.012 54.034 12613.929 9.266 240.342 1.943 0.87 449063. 0.4944
|
|
34.10 0.1634 0.2831 0.1207 0.0697 17.241 83.588 53.681 12856.337 9.444 238.772 1.894 0.88 449681. 0.4803
|
|
40.92 0.1961 0.3313 0.1197 0.0709 17.535 85.016 53.234 13075.916 9.605 236.783 1.847 0.88 450364. 0.4664
|
|
47.74 0.2288 0.3770 0.1185 0.0719 17.784 86.221 52.670 13261.280 9.741 234.276 1.801 0.88 451117. 0.4526
|
|
54.56 0.2615 0.4207 0.1169 0.0726 17.971 87.132 51.966 13401.325 9.844 231.145 1.759 0.88 451941. 0.4389
|
|
61.38 0.2942 0.4625 0.1149 0.0731 18.085 87.684 51.100 13486.262 9.906 227.292 1.719 0.88 452839. 0.4253
|
|
68.20 0.3268 0.5025 0.1126 0.0732 18.115 87.827 50.052 13508.330 9.923 222.629 1.681 0.88 453811. 0.4116
|
|
75.02 0.3595 0.5408 0.1098 0.0730 18.053 87.525 48.804 13461.888 9.889 217.082 1.644 0.88 454858. 0.3977
|
|
81.84 0.3922 0.5774 0.1065 0.0723 17.893 86.752 47.346 13342.928 9.801 210.593 1.609 0.88 455979. 0.3834
|
|
88.66 0.4249 0.6123 0.1027 0.0713 17.632 85.486 45.665 13148.199 9.658 203.119 1.575 0.88 457173. 0.3685
|
|
95.48 0.4576 0.6453 0.0984 0.0698 17.266 83.709 43.759 12874.920 9.457 194.641 1.542 0.88 458439. 0.3530
|
|
102.30 0.4903 0.6764 0.0936 0.0679 16.791 81.411 41.633 12521.419 9.198 185.182 1.508 0.88 459776. 0.3368
|
|
109.12 0.5229 0.7054 0.0884 0.0655 16.213 78.604 39.305 12089.749 8.881 174.829 1.475 0.89 461182. 0.3200
|
|
115.94 0.5556 0.7324 0.0828 0.0628 15.536 75.323 36.805 11585.153 8.510 163.707 1.441 0.89 462657. 0.3026
|
|
122.76 0.5883 0.7571 0.0768 0.0597 14.768 71.602 34.159 11012.753 8.090 151.937 1.407 0.89 464199. 0.2846
|
|
129.58 0.6210 0.7795 0.0706 0.0562 13.915 67.464 31.390 10376.375 7.622 139.624 1.372 0.89 465807. 0.2661
|
|
136.40 0.6537 0.7992 0.0641 0.0525 12.978 62.924 28.518 9678.063 7.109 126.848 1.337 0.89 467480. 0.2471
|
|
143.22 0.6864 0.8159 0.0575 0.0484 11.962 57.998 25.557 8920.412 6.553 113.676 1.299 0.89 469218. 0.2274
|
|
150.04 0.7190 0.8271 0.0506 0.0440 10.891 52.803 22.515 8121.366 5.966 100.148 1.257 0.90 471020. 0.2065
|
|
156.86 0.7517 0.8291 0.0436 0.0396 9.789 47.459 19.402 7299.409 5.362 86.301 1.206 0.90 472886. 0.1838
|
|
163.68 0.7844 0.8188 0.0365 0.0350 8.651 41.943 16.230 6451.130 4.739 72.191 1.141 0.90 474815. 0.1591
|
|
170.50 0.8171 0.7923 0.0293 0.0302 7.467 36.204 13.013 5568.369 4.090 57.882 1.060 0.90 476806. 0.1324
|
|
177.32 0.8498 0.7383 0.0220 0.0253 6.253 30.317 9.764 4662.888 3.425 43.430 0.950 0.91 478859. 0.1027
|
|
184.14 0.8825 0.6351 0.0146 0.0203 5.025 24.363 6.500 3747.199 2.753 28.911 0.787 0.91 480973. 0.0694
|
|
190.96 0.9151 0.4342 0.0073 0.0154 3.802 18.434 3.242 2835.313 2.083 14.420 0.519 0.91 483146. 0.0323
|
|
197.78 0.9478 0.0015 0.0000 0.0105 2.595 12.579 0.008 1934.751 1.421 0.034 0.002 0.91 485335. 0.0000
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