612 lines
109 KiB
Plaintext
612 lines
109 KiB
Plaintext
15x4E (15x4E.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 0.0522 0.0197 0.001 0.076 0.084 0.899 0.009 0.375 42.516 0.06 21003. 0.4829
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0.20 0.0138 0.0356 0.0511 0.0197 0.001 0.076 0.082 0.900 0.009 0.366 41.527 0.06 21009. 0.4662
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0.39 0.0276 0.0695 0.0498 0.0197 0.001 0.076 0.080 0.900 0.009 0.357 40.520 0.06 21016. 0.4494
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0.59 0.0413 0.1017 0.0485 0.0197 0.001 0.076 0.078 0.899 0.009 0.348 39.496 0.06 21024. 0.4323
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0.78 0.0551 0.1320 0.0472 0.0197 0.001 0.076 0.076 0.898 0.009 0.339 38.456 0.06 21031. 0.4151
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0.98 0.0689 0.1605 0.0458 0.0197 0.001 0.076 0.074 0.896 0.009 0.329 37.397 0.06 21040. 0.3977
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1.17 0.0827 0.1870 0.0444 0.0196 0.001 0.076 0.072 0.894 0.009 0.318 36.320 0.06 21048. 0.3801
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1.37 0.0965 0.2116 0.0429 0.0196 0.001 0.075 0.069 0.891 0.009 0.308 35.222 0.06 21057. 0.3624
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1.57 0.1102 0.2341 0.0414 0.0195 0.001 0.075 0.067 0.887 0.008 0.297 34.102 0.06 21066. 0.3446
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1.76 0.1240 0.2546 0.0398 0.0194 0.001 0.075 0.064 0.883 0.008 0.285 32.959 0.06 21076. 0.3265
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1.96 0.1378 0.2728 0.0381 0.0193 0.001 0.074 0.062 0.878 0.008 0.274 31.791 0.06 21086. 0.3084
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2.15 0.1516 0.2888 0.0364 0.0191 0.001 0.074 0.059 0.871 0.008 0.261 30.595 0.06 21097. 0.2902
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2.35 0.1654 0.3025 0.0347 0.0190 0.001 0.073 0.056 0.864 0.008 0.249 29.371 0.06 21107. 0.2718
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2.54 0.1792 0.3137 0.0329 0.0188 0.001 0.072 0.053 0.857 0.008 0.236 28.115 0.06 21119. 0.2534
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2.74 0.1929 0.3223 0.0311 0.0186 0.001 0.072 0.050 0.848 0.008 0.223 26.825 0.06 21131. 0.2350
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2.94 0.2067 0.3282 0.0292 0.0184 0.001 0.071 0.047 0.838 0.008 0.210 25.498 0.06 21143. 0.2165
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3.13 0.2205 0.3313 0.0273 0.0182 0.001 0.070 0.044 0.828 0.008 0.196 24.129 0.06 21156. 0.1981
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3.33 0.2343 0.3314 0.0253 0.0179 0.001 0.069 0.041 0.816 0.008 0.182 22.716 0.06 21169. 0.1797
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3.52 0.2481 0.3283 0.0234 0.0176 0.001 0.068 0.038 0.804 0.008 0.168 21.254 0.06 21183. 0.1614
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3.72 0.2618 0.3218 0.0213 0.0173 0.001 0.067 0.034 0.791 0.008 0.153 19.737 0.06 21198. 0.1432
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3.92 0.2756 0.3117 0.0193 0.0170 0.001 0.066 0.031 0.776 0.007 0.138 18.160 0.06 21213. 0.1252
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4.11 0.2894 0.2977 0.0172 0.0167 0.001 0.064 0.028 0.761 0.007 0.123 16.517 0.06 21228. 0.1075
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4.31 0.3032 0.2794 0.0151 0.0163 0.001 0.063 0.024 0.744 0.007 0.108 14.801 0.06 21244. 0.0902
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4.50 0.3170 0.2566 0.0129 0.0159 0.001 0.061 0.021 0.727 0.007 0.093 13.002 0.06 21260. 0.0734
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4.70 0.3307 0.2289 0.0108 0.0155 0.001 0.060 0.017 0.708 0.007 0.077 11.114 0.06 21278. 0.0573
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4.89 0.3445 0.1958 0.0086 0.0151 0.001 0.058 0.014 0.688 0.007 0.062 9.124 0.06 21295. 0.0420
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5.09 0.3583 0.1567 0.0064 0.0147 0.001 0.056 0.010 0.668 0.006 0.046 7.024 0.06 21313. 0.0279
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5.29 0.3721 0.1112 0.0042 0.0142 0.001 0.055 0.007 0.646 0.006 0.030 4.798 0.06 21332. 0.0155
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5.48 0.3859 0.0584 0.0021 0.0137 0.001 0.053 0.003 0.624 0.006 0.015 2.431 0.06 21351. 0.0055
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5.68 0.3997 -0.0030 -0.0001 0.0132 0.001 0.051 0.000 0.600 0.006 -0.001 -0.123 0.06 21370. 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 0.0524 0.0171 0.008 0.263 0.338 6.224 0.030 1.505 24.664 0.12 42005. 0.5613
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0.40 0.0141 0.0423 0.0512 0.0171 0.008 0.263 0.331 6.228 0.030 1.470 24.074 0.12 42019. 0.5415
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0.80 0.0282 0.0825 0.0500 0.0171 0.008 0.263 0.322 6.228 0.030 1.434 23.477 0.12 42033. 0.5214
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1.20 0.0423 0.1206 0.0486 0.0171 0.008 0.263 0.314 6.223 0.030 1.396 22.874 0.12 42048. 0.5013
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1.60 0.0565 0.1566 0.0473 0.0170 0.008 0.263 0.305 6.213 0.030 1.357 22.265 0.12 42064. 0.4810
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2.00 0.0706 0.1903 0.0458 0.0170 0.008 0.262 0.296 6.198 0.030 1.316 21.648 0.12 42081. 0.4606
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2.41 0.0847 0.2218 0.0444 0.0169 0.008 0.261 0.286 6.176 0.029 1.273 21.025 0.12 42098. 0.4401
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2.81 0.0988 0.2509 0.0428 0.0169 0.008 0.260 0.276 6.148 0.029 1.230 20.393 0.12 42117. 0.4194
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3.21 0.1129 0.2778 0.0413 0.0168 0.008 0.258 0.266 6.114 0.029 1.184 19.752 0.12 42136. 0.3987
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3.61 0.1270 0.3022 0.0396 0.0167 0.008 0.257 0.256 6.071 0.029 1.137 19.100 0.12 42156. 0.3778
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4.01 0.1411 0.3241 0.0379 0.0165 0.008 0.254 0.245 6.021 0.029 1.089 18.437 0.12 42177. 0.3568
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4.41 0.1553 0.3435 0.0362 0.0164 0.008 0.252 0.234 5.964 0.028 1.039 17.762 0.12 42199. 0.3358
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4.81 0.1694 0.3601 0.0344 0.0162 0.008 0.249 0.222 5.898 0.028 0.987 17.072 0.12 42221. 0.3147
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5.21 0.1835 0.3740 0.0326 0.0160 0.008 0.246 0.210 5.824 0.028 0.935 16.366 0.12 42245. 0.2935
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5.61 0.1976 0.3850 0.0307 0.0157 0.008 0.243 0.198 5.741 0.027 0.881 15.641 0.12 42270. 0.2722
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6.01 0.2117 0.3928 0.0288 0.0155 0.008 0.239 0.186 5.650 0.027 0.825 14.896 0.12 42296. 0.2510
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6.42 0.2258 0.3973 0.0268 0.0152 0.007 0.235 0.173 5.549 0.026 0.769 14.127 0.12 42322. 0.2297
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6.82 0.2400 0.3984 0.0248 0.0149 0.007 0.230 0.160 5.439 0.026 0.711 13.330 0.12 42350. 0.2085
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7.22 0.2541 0.3956 0.0227 0.0146 0.007 0.225 0.147 5.319 0.025 0.652 12.502 0.12 42379. 0.1872
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7.62 0.2682 0.3887 0.0206 0.0142 0.007 0.219 0.133 5.190 0.025 0.592 11.637 0.12 42409. 0.1661
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8.02 0.2823 0.3773 0.0185 0.0139 0.007 0.213 0.119 5.050 0.024 0.531 10.731 0.12 42440. 0.1451
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8.42 0.2964 0.3609 0.0164 0.0134 0.007 0.207 0.106 4.901 0.023 0.470 9.776 0.12 42472. 0.1243
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8.82 0.3105 0.3390 0.0142 0.0130 0.006 0.200 0.092 4.741 0.023 0.408 8.764 0.12 42505. 0.1038
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9.22 0.3246 0.3108 0.0120 0.0125 0.006 0.193 0.077 4.572 0.022 0.345 7.687 0.12 42540. 0.0837
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9.62 0.3388 0.2756 0.0098 0.0120 0.006 0.186 0.063 4.392 0.021 0.281 6.532 0.12 42575. 0.0643
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10.02 0.3529 0.2323 0.0076 0.0115 0.006 0.178 0.049 4.203 0.020 0.218 5.286 0.12 42612. 0.0458
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10.43 0.3670 0.1797 0.0054 0.0110 0.005 0.169 0.035 4.004 0.019 0.154 3.933 0.12 42650. 0.0287
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10.83 0.3811 0.1162 0.0032 0.0104 0.005 0.160 0.020 3.796 0.018 0.091 2.448 0.12 42689. 0.0137
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11.23 0.3952 0.0393 0.0010 0.0098 0.005 0.151 0.006 3.579 0.017 0.028 0.799 0.12 42728. 0.0025
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11.63 0.4093
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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 0.0526 0.0159 0.026 0.552 0.764 19.584 0.062 3.399 17.697 0.18 63007. 0.6051
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0.60 0.0140 0.0452 0.0514 0.0159 0.026 0.552 0.747 19.599 0.062 3.321 17.276 0.18 63027. 0.5839
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1.19 0.0280 0.0882 0.0502 0.0159 0.026 0.552 0.728 19.599 0.062 3.239 16.852 0.18 63049. 0.5625
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1.79 0.0420 0.1289 0.0488 0.0159 0.026 0.552 0.709 19.582 0.062 3.154 16.425 0.18 63072. 0.5411
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2.39 0.0560 0.1674 0.0475 0.0159 0.026 0.551 0.689 19.548 0.062 3.066 15.996 0.18 63095. 0.5195
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2.98 0.0700 0.2036 0.0461 0.0158 0.026 0.549 0.669 19.494 0.062 2.975 15.563 0.18 63120. 0.4979
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3.58 0.0840 0.2374 0.0446 0.0158 0.026 0.547 0.648 19.419 0.062 2.881 15.126 0.18 63146. 0.4762
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4.18 0.0980 0.2689 0.0431 0.0157 0.026 0.544 0.626 19.322 0.062 2.783 14.686 0.18 63173. 0.4544
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4.77 0.1120 0.2980 0.0415 0.0156 0.026 0.541 0.603 19.200 0.061 2.681 14.240 0.18 63202. 0.4325
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5.37 0.1260 0.3247 0.0399 0.0155 0.026 0.537 0.579 19.053 0.061 2.577 13.789 0.18 63232. 0.4105
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5.97 0.1400 0.3488 0.0382 0.0153 0.025 0.532 0.555 18.880 0.060 2.468 13.332 0.18 63263. 0.3885
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6.56 0.1540 0.3703 0.0365 0.0152 0.025 0.526 0.530 18.679 0.059 2.357 12.868 0.18 63295. 0.3664
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7.16 0.1681 0.3891 0.0347 0.0150 0.025 0.520 0.504 18.449 0.059 2.243 12.395 0.18 63329. 0.3443
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7.76 0.1821 0.4051 0.0329 0.0148 0.024 0.513 0.478 18.191 0.058 2.125 11.912 0.18 63364. 0.3221
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8.35 0.1961 0.4182 0.0310 0.0146 0.024 0.504 0.451 17.902 0.057 2.004 11.418 0.18 63401. 0.2998
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8.95 0.2101 0.4282 0.0291 0.0143 0.024 0.495 0.423 17.582 0.056 1.881 10.911 0.18 63439. 0.2776
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9.55 0.2241 0.4348 0.0272 0.0140 0.023 0.485 0.395 17.229 0.055 1.755 10.388 0.18 63478. 0.2552
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10.15 0.2381 0.4379 0.0252 0.0137 0.023 0.475 0.366 16.844 0.054 1.626 9.846 0.18 63519. 0.2329
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10.74 0.2521 0.4372 0.0232 0.0133 0.022 0.463 0.336 16.424 0.052 1.495 9.284 0.18 63562. 0.2106
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11.34 0.2661 0.4323 0.0211 0.0130 0.021 0.450 0.306 15.971 0.051 1.362 8.696 0.18 63606. 0.1882
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11.94 0.2801 0.4227 0.0190 0.0126 0.021 0.436 0.276 15.482 0.049 1.227 8.079 0.18 63652. 0.1660
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12.53 0.2941 0.4080 0.0169 0.0122 0.020 0.421 0.245 14.958 0.048 1.089 7.426 0.18 63700. 0.1438
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13.13 0.3081 0.3875 0.0147 0.0117 0.019 0.406 0.214 14.398 0.046 0.950 6.732 0.18 63749. 0.1217
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13.73 0.3221 0.3603 0.0125 0.0112 0.019 0.389 0.182 13.802 0.044 0.810 5.987 0.18 63800. 0.1000
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14.32 0.3361 0.3254 0.0104 0.0107 0.018 0.371 0.150 13.172 0.042 0.669 5.182 0.18 63853. 0.0786
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14.92 0.3501 0.2815 0.0082 0.0102 0.017 0.352 0.119 12.507 0.040 0.528 4.304 0.18 63907. 0.0580
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15.52 0.3641 0.2269 0.0060 0.0096 0.016 0.333 0.087 11.808 0.038 0.386 3.336 0.18 63964. 0.0385
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16.11 0.3781 0.1594 0.0038 0.0090 0.015 0.312 0.055 11.077 0.035 0.245 2.257 0.18 64021. 0.0207
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16.71 0.3921 0.0757 0.0016 0.0084 0.014 0.291 0.024 10.314 0.033 0.105 1.034 0.18 64080. 0.0062
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17.31 0.4061
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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 0.0528 0.0153 0.060 0.940 1.364 44.500 0.106 6.066 13.901 0.24 84008. 0.6351
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0.79 0.0139 0.0471 0.0516 0.0153 0.060 0.941 1.333 44.534 0.106 5.928 13.573 0.24 84035. 0.6129
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1.58 0.0278 0.0919 0.0504 0.0153 0.060 0.941 1.300 44.531 0.106 5.783 13.242 0.24 84064. 0.5907
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2.37 0.0418 0.1343 0.0491 0.0153 0.060 0.940 1.266 44.489 0.106 5.633 12.911 0.24 84094. 0.5683
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3.16 0.0557 0.1745 0.0477 0.0152 0.060 0.938 1.231 44.404 0.106 5.477 12.578 0.24 84125. 0.5460
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3.96 0.0696 0.2123 0.0463 0.0152 0.059 0.935 1.195 44.272 0.106 5.315 12.243 0.24 84158. 0.5235
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4.75 0.0835 0.2478 0.0448 0.0151 0.059 0.932 1.157 44.090 0.105 5.148 11.906 0.24 84193. 0.5011
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5.54 0.0975 0.2808 0.0433 0.0150 0.059 0.927 1.118 43.854 0.105 4.975 11.567 0.24 84229. 0.4785
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6.33 0.1114 0.3115 0.0418 0.0149 0.058 0.920 1.078 43.559 0.104 4.795 11.226 0.24 84267. 0.4559
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7.12 0.1253 0.3396 0.0401 0.0148 0.058 0.913 1.036 43.203 0.103 4.610 10.880 0.24 84306. 0.4333
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7.91 0.1392 0.3652 0.0385 0.0147 0.057 0.904 0.993 42.782 0.102 4.418 10.531 0.24 84347. 0.4106
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8.70 0.1532 0.3883 0.0368 0.0145 0.057 0.894 0.949 42.295 0.101 4.221 10.177 0.24 84390. 0.3878
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9.49 0.1671 0.4086 0.0350 0.0143 0.056 0.882 0.903 41.739 0.100 4.019 9.818 0.24 84435. 0.3650
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10.28 0.1810 0.4261 0.0332 0.0141 0.055 0.869 0.857 41.113 0.098 3.811 9.452 0.24 84481. 0.3422
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11.08 0.1949 0.4407 0.0313 0.0139 0.054 0.854 0.809 40.412 0.096 3.598 9.078 0.24 84530. 0.3193
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11.87 0.2088 0.4523 0.0294 0.0136 0.053 0.838 0.760 39.636 0.095 3.379 8.694 0.24 84580. 0.2964
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12.66 0.2228 0.4605 0.0275 0.0133 0.052 0.819 0.710 38.782 0.093 3.156 8.299 0.24 84633. 0.2735
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13.45 0.2367 0.4652 0.0255 0.0130 0.051 0.800 0.658 37.848 0.090 2.929 7.891 0.24 84687. 0.2505
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14.24 0.2506 0.4661 0.0235 0.0126 0.049 0.778 0.606 36.832 0.088 2.697 7.467 0.24 84743. 0.2274
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15.03 0.2645 0.4628 0.0214 0.0123 0.048 0.755 0.553 35.731 0.085 2.461 7.024 0.24 84802. 0.2044
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15.82 0.2785 0.4549 0.0193 0.0118 0.046 0.730 0.499 34.546 0.082 2.222 6.558 0.24 84863. 0.1813
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16.61 0.2924 0.4417 0.0172 0.0114 0.045 0.703 0.445 33.274 0.079 1.979 6.065 0.24 84925. 0.1582
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17.40 0.3063 0.4226 0.0151 0.0109 0.043 0.674 0.390 31.916 0.076 1.733 5.538 0.24 84991. 0.1352
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18.20 0.3202 0.3966 0.0129 0.0104 0.041 0.644 0.334 30.472 0.073 1.486 4.972 0.24 85058. 0.1124
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18.99 0.3342 0.3625 0.0108 0.0099 0.039 0.612 0.278 28.942 0.069 1.236 4.355 0.24 85127. 0.0898
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19.78 0.3481 0.3189 0.0086 0.0094 0.037 0.577 0.222 27.328 0.065 0.986 3.678 0.24 85199. 0.0677
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20.57 0.3620 0.2637 0.0064 0.0088 0.034 0.542 0.165 25.633 0.061 0.735 2.925 0.24 85273. 0.0465
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21.36 0.3759 0.1942 0.0042 0.0082 0.032 0.504 0.109 23.859 0.057 0.485 2.074 0.24 85349. 0.0268
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22.15 0.3899 0.1063 0.0021 0.0075 0.030 0.465 0.053 22.007 0.053 0.236 1.095 0.24 85427. 0.0099
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22.94 0.4038 -0.0093 -0.0002 0.0069 0.027 0.423 -0.004 20.022 0.048 -0.018 -0.092 0.24 85496. 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 0.0531 0.0148 0.113 1.429 2.141 84.542 0.161 9.524 11.488 0.30 105009. 0.6576
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1.01 0.0143 0.0499 0.0518 0.0149 0.113 1.430 2.091 84.604 0.162 9.301 11.210 0.30 105044. 0.6341
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2.03 0.0286 0.0972 0.0505 0.0149 0.113 1.430 2.039 84.589 0.162 9.067 10.931 0.30 105081. 0.6105
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3.04 0.0429 0.1421 0.0492 0.0148 0.113 1.428 1.984 84.489 0.161 8.825 10.651 0.30 105119. 0.5869
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4.06 0.0571 0.1845 0.0478 0.0148 0.113 1.425 1.927 84.299 0.161 8.573 10.371 0.30 105160. 0.5632
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5.07 0.0714 0.2243 0.0463 0.0147 0.113 1.420 1.869 84.010 0.160 8.312 10.089 0.30 105202. 0.5395
|
|
6.09 0.0857 0.2617 0.0448 0.0147 0.112 1.413 1.808 83.614 0.160 8.041 9.806 0.30 105247. 0.5158
|
|
7.10 0.1000 0.2964 0.0433 0.0146 0.111 1.405 1.745 83.103 0.159 7.760 9.522 0.30 105294. 0.4920
|
|
8.12 0.1143 0.3286 0.0416 0.0145 0.111 1.394 1.679 82.467 0.158 7.469 9.236 0.30 105342. 0.4682
|
|
9.13 0.1286 0.3581 0.0400 0.0143 0.110 1.381 1.612 81.701 0.156 7.169 8.947 0.30 105394. 0.4443
|
|
10.14 0.1428 0.3849 0.0382 0.0142 0.108 1.366 1.542 80.797 0.154 6.858 8.656 0.30 105447. 0.4204
|
|
11.16 0.1571 0.4090 0.0364 0.0140 0.107 1.348 1.470 79.753 0.152 6.539 8.360 0.30 105503. 0.3965
|
|
12.17 0.1714 0.4302 0.0346 0.0138 0.105 1.328 1.396 78.562 0.150 6.210 8.060 0.30 105561. 0.3725
|
|
13.19 0.1857 0.4483 0.0327 0.0136 0.104 1.305 1.320 77.219 0.147 5.872 7.755 0.30 105621. 0.3485
|
|
14.20 0.2000 0.4634 0.0308 0.0133 0.102 1.280 1.242 75.720 0.145 5.526 7.442 0.30 105684. 0.3245
|
|
15.22 0.2143 0.4751 0.0288 0.0130 0.099 1.252 1.163 74.059 0.141 5.172 7.122 0.30 105750. 0.3004
|
|
16.23 0.2285 0.4832 0.0268 0.0127 0.097 1.221 1.081 72.231 0.138 4.810 6.791 0.30 105818. 0.2763
|
|
17.25 0.2428 0.4875 0.0248 0.0123 0.094 1.187 0.998 70.233 0.134 4.441 6.448 0.30 105889. 0.2520
|
|
18.26 0.2571 0.4876 0.0227 0.0119 0.091 1.151 0.914 68.059 0.130 4.065 6.091 0.30 105963. 0.2278
|
|
19.27 0.2714 0.4829 0.0205 0.0115 0.088 1.111 0.828 65.707 0.125 3.683 5.715 0.30 106039. 0.2034
|
|
20.29 0.2857 0.4730 0.0184 0.0111 0.085 1.068 0.741 63.174 0.121 3.295 5.318 0.30 106118. 0.1790
|
|
21.30 0.3000 0.4571 0.0162 0.0106 0.081 1.022 0.652 60.459 0.115 2.902 4.894 0.30 106201. 0.1546
|
|
22.32 0.3142 0.4341 0.0140 0.0101 0.077 0.973 0.563 57.561 0.110 2.505 4.437 0.30 106286. 0.1302
|
|
23.33 0.3285 0.4029 0.0117 0.0096 0.073 0.921 0.473 54.481 0.104 2.104 3.939 0.30 106374. 0.1060
|
|
24.35 0.3428 0.3616 0.0095 0.0090 0.069 0.866 0.383 51.224 0.098 1.702 3.388 0.30 106465. 0.0820
|
|
25.36 0.3571 0.3081 0.0072 0.0084 0.064 0.808 0.292 47.792 0.091 1.299 2.771 0.30 106559. 0.0586
|
|
26.38 0.3714 0.2392 0.0050 0.0078 0.059 0.747 0.202 44.194 0.084 0.896 2.069 0.30 106655. 0.0363
|
|
27.39 0.3857 0.1501 0.0028 0.0071 0.054 0.683 0.111 40.433 0.077 0.496 1.250 0.30 106755. 0.0163
|
|
28.40 0.3999 0.0327 0.0005 0.0064 0.049 0.617 0.021 36.475 0.070 0.094 0.262 0.30 106851. 0.0015
|
|
29.42 0.4142
|
|
|
|
|
|
|
|
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 0.0534 0.0146 0.192 2.020 3.101 143.424 0.228 13.795 9.808 0.36 126008. 0.6756
|
|
1.21 0.0142 0.0507 0.0522 0.0146 0.192 2.022 3.029 143.516 0.228 13.473 9.573 0.36 126050. 0.6518
|
|
2.41 0.0283 0.0988 0.0509 0.0146 0.192 2.021 2.954 143.475 0.228 13.138 9.338 0.36 126094. 0.6278
|
|
3.62 0.0425 0.1445 0.0495 0.0146 0.192 2.019 2.876 143.289 0.228 12.790 9.102 0.36 126140. 0.6038
|
|
4.83 0.0566 0.1877 0.0481 0.0145 0.192 2.014 2.794 142.944 0.228 12.429 8.867 0.36 126188. 0.5798
|
|
6.04 0.0708 0.2283 0.0467 0.0145 0.191 2.006 2.710 142.429 0.227 12.054 8.630 0.36 126239. 0.5558
|
|
7.24 0.0850 0.2665 0.0452 0.0144 0.190 1.997 2.623 141.729 0.226 11.666 8.393 0.36 126292. 0.5317
|
|
8.45 0.0991 0.3021 0.0436 0.0143 0.189 1.984 2.532 140.831 0.224 11.263 8.155 0.36 126347. 0.5077
|
|
9.66 0.1133 0.3351 0.0420 0.0142 0.187 1.968 2.439 139.718 0.222 10.847 7.916 0.36 126406. 0.4836
|
|
10.86 0.1275 0.3655 0.0403 0.0141 0.186 1.949 2.342 138.377 0.220 10.416 7.675 0.36 126466. 0.4594
|
|
12.07 0.1416 0.3933 0.0386 0.0139 0.183 1.927 2.242 136.801 0.218 9.971 7.432 0.36 126530. 0.4353
|
|
13.28 0.1558 0.4183 0.0368 0.0137 0.181 1.901 2.139 134.980 0.215 9.513 7.187 0.36 126596. 0.4111
|
|
14.48 0.1699 0.4405 0.0350 0.0135 0.178 1.872 2.033 132.906 0.212 9.042 6.938 0.36 126665. 0.3869
|
|
15.69 0.1841 0.4598 0.0331 0.0133 0.175 1.839 1.924 130.570 0.208 8.559 6.684 0.36 126737. 0.3627
|
|
16.90 0.1983 0.4760 0.0312 0.0130 0.172 1.803 1.813 127.963 0.204 8.064 6.426 0.36 126811. 0.3384
|
|
18.11 0.2124 0.4890 0.0293 0.0127 0.168 1.762 1.699 125.076 0.199 7.557 6.161 0.36 126889. 0.3141
|
|
19.31 0.2266 0.4985 0.0272 0.0124 0.163 1.717 1.582 121.901 0.194 7.039 5.888 0.36 126970. 0.2897
|
|
20.52 0.2408 0.5042 0.0252 0.0120 0.159 1.668 1.464 118.430 0.188 6.510 5.605 0.36 127054. 0.2653
|
|
21.73 0.2549 0.5059 0.0231 0.0116 0.154 1.615 1.343 114.656 0.182 5.972 5.311 0.36 127141. 0.2407
|
|
22.93 0.2691 0.5029 0.0210 0.0112 0.148 1.558 1.219 110.573 0.176 5.424 5.002 0.36 127232. 0.2161
|
|
24.14 0.2832 0.4948 0.0188 0.0108 0.142 1.496 1.095 106.177 0.169 4.869 4.676 0.36 127326. 0.1914
|
|
25.35 0.2974 0.4808 0.0167 0.0103 0.136 1.429 0.968 101.465 0.161 4.306 4.327 0.36 127423. 0.1665
|
|
26.55 0.3116 0.4600 0.0145 0.0098 0.129 1.359 0.840 96.437 0.153 3.737 3.951 0.36 127523. 0.1417
|
|
27.76 0.3257 0.4309 0.0122 0.0093 0.122 1.283 0.711 91.093 0.145 3.163 3.541 0.36 127627. 0.1168
|
|
28.97 0.3399 0.3920 0.0100 0.0087 0.115 1.204 0.581 85.439 0.136 2.586 3.087 0.36 127735. 0.0921
|
|
30.18 0.3541 0.3408 0.0078 0.0081 0.107 1.120 0.451 79.482 0.126 2.008 2.576 0.36 127846. 0.0677
|
|
31.38 0.3682 0.2740 0.0055 0.0074 0.098 1.032 0.322 73.233 0.117 1.430 1.991 0.36 127961. 0.0442
|
|
32.59 0.3824 0.1866 0.0033 0.0068 0.089 0.940 0.192 66.704 0.106 0.855 1.306 0.36 128078. 0.0224
|
|
33.80 0.3965 0.0707 0.0011 0.0061 0.080 0.843 0.063 59.870 0.095 0.280 0.477 0.36 128196. 0.0047
|
|
35.00 0.4107
|
|
|
|
|
|
|
|
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 0.0538 0.0144 0.302 2.718 4.250 225.091 0.307 18.906 8.565 0.42 147006. 0.6907
|
|
1.38 0.0139 0.0508 0.0525 0.0144 0.302 2.719 4.153 225.208 0.307 18.473 8.364 0.42 147054. 0.6668
|
|
2.77 0.0278 0.0991 0.0513 0.0144 0.302 2.718 4.052 225.117 0.307 18.022 8.163 0.42 147104. 0.6428
|
|
4.15 0.0418 0.1449 0.0499 0.0144 0.301 2.714 3.946 224.798 0.307 17.553 7.962 0.42 147157. 0.6188
|
|
5.54 0.0557 0.1884 0.0485 0.0143 0.301 2.708 3.837 224.233 0.306 17.067 7.762 0.42 147213. 0.5947
|
|
6.92 0.0696 0.2294 0.0471 0.0143 0.300 2.697 3.724 223.402 0.305 16.564 7.560 0.42 147271. 0.5707
|
|
8.30 0.0835 0.2679 0.0456 0.0142 0.298 2.684 3.607 222.285 0.303 16.042 7.359 0.42 147332. 0.5467
|
|
9.69 0.0974 0.3040 0.0441 0.0141 0.296 2.667 3.485 220.859 0.301 15.502 7.157 0.42 147395. 0.5227
|
|
11.07 0.1114 0.3376 0.0425 0.0140 0.294 2.646 3.359 219.102 0.299 14.943 6.954 0.42 147462. 0.4986
|
|
12.46 0.1253 0.3686 0.0409 0.0139 0.291 2.620 3.229 216.992 0.296 14.365 6.750 0.42 147531. 0.4745
|
|
13.84 0.1392 0.3971 0.0392 0.0137 0.288 2.590 3.095 214.514 0.293 13.768 6.545 0.42 147603. 0.4504
|
|
15.22 0.1531 0.4230 0.0374 0.0135 0.284 2.556 2.957 211.656 0.289 13.155 6.338 0.42 147679. 0.4263
|
|
16.61 0.1670 0.4462 0.0356 0.0133 0.279 2.516 2.816 208.405 0.284 12.524 6.128 0.42 147757. 0.4022
|
|
17.99 0.1810 0.4665 0.0338 0.0131 0.275 2.472 2.670 204.748 0.279 11.876 5.915 0.42 147839. 0.3781
|
|
19.38 0.1949 0.4840 0.0319 0.0128 0.269 2.423 2.521 200.669 0.274 11.212 5.698 0.42 147924. 0.3539
|
|
20.76 0.2088 0.4984 0.0300 0.0126 0.263 2.369 2.368 196.157 0.268 10.533 5.476 0.42 148013. 0.3296
|
|
22.14 0.2227 0.5094 0.0280 0.0122 0.256 2.309 2.212 191.198 0.261 9.839 5.248 0.42 148105. 0.3053
|
|
23.53 0.2366 0.5170 0.0260 0.0119 0.249 2.243 2.053 185.780 0.253 9.131 5.012 0.42 148200. 0.2809
|
|
24.91 0.2506 0.5207 0.0239 0.0115 0.241 2.172 1.891 179.891 0.245 8.410 4.767 0.42 148299. 0.2564
|
|
26.30 0.2645 0.5201 0.0218 0.0111 0.233 2.095 1.726 173.522 0.237 7.676 4.511 0.42 148402. 0.2318
|
|
27.68 0.2784 0.5147 0.0197 0.0107 0.224 2.012 1.558 166.666 0.227 6.932 4.241 0.42 148508. 0.2071
|
|
29.06 0.2923 0.5038 0.0176 0.0102 0.214 1.924 1.389 159.318 0.217 6.177 3.954 0.42 148618. 0.1822
|
|
30.45 0.3062 0.4865 0.0154 0.0097 0.203 1.829 1.217 151.475 0.207 5.413 3.644 0.42 148732. 0.1573
|
|
31.83 0.3201 0.4616 0.0132 0.0092 0.192 1.728 1.044 143.138 0.195 4.643 3.308 0.42 148850. 0.1322
|
|
33.22 0.3341 0.4276 0.0110 0.0086 0.180 1.622 0.870 134.314 0.183 3.868 2.936 0.42 148972. 0.1071
|
|
34.60 0.3480 0.3823 0.0088 0.0080 0.168 1.509 0.695 125.012 0.171 3.090 2.520 0.42 149098. 0.0822
|
|
35.98 0.3619 0.3226 0.0066 0.0074 0.155 1.392 0.520 115.248 0.157 2.311 2.045 0.42 149227. 0.0577
|
|
37.37 0.3758 0.2440 0.0044 0.0067 0.141 1.268 0.345 105.039 0.143 1.534 1.489 0.42 149361. 0.0342
|
|
38.75 0.3897 0.1397 0.0022 0.0060 0.127 1.140 0.171 94.392 0.129 0.761 0.822 0.42 149496. 0.0133
|
|
40.14 0.4037 -0.0075 -0.0001 0.0053 0.111 1.001 -0.008 82.904 0.113 -0.035 -0.043 0.42 149611. 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 0.0542 0.0143 0.448 3.527 5.597 333.826 0.398 24.895 7.605 0.48 168001. 0.7037
|
|
1.59 0.0140 0.0517 0.0530 0.0143 0.448 3.528 5.468 333.947 0.399 24.322 7.427 0.48 168057. 0.6794
|
|
3.17 0.0279 0.1008 0.0517 0.0143 0.448 3.526 5.334 333.748 0.398 23.726 7.249 0.48 168115. 0.6549
|
|
4.76 0.0419 0.1476 0.0503 0.0143 0.447 3.520 5.195 333.199 0.398 23.106 7.071 0.48 168176. 0.6305
|
|
6.35 0.0558 0.1918 0.0489 0.0142 0.446 3.511 5.050 332.273 0.397 22.463 6.894 0.48 168240. 0.6060
|
|
7.93 0.0698 0.2336 0.0475 0.0142 0.444 3.496 4.900 330.940 0.395 21.797 6.716 0.48 168307. 0.5816
|
|
9.52 0.0838 0.2729 0.0460 0.0141 0.441 3.478 4.745 329.167 0.393 21.107 6.539 0.48 168377. 0.5572
|
|
11.11 0.0977 0.3097 0.0444 0.0140 0.438 3.454 4.585 326.922 0.390 20.392 6.361 0.48 168450. 0.5327
|
|
12.69 0.1117 0.3440 0.0428 0.0139 0.435 3.425 4.418 324.170 0.387 19.653 6.182 0.48 168527. 0.5083
|
|
14.28 0.1257 0.3758 0.0411 0.0138 0.430 3.390 4.246 320.876 0.383 18.888 6.003 0.48 168607. 0.4839
|
|
15.87 0.1396 0.4050 0.0394 0.0136 0.425 3.349 4.069 317.020 0.378 18.100 5.822 0.48 168690. 0.4594
|
|
17.45 0.1536 0.4315 0.0376 0.0134 0.419 3.303 3.887 312.583 0.373 17.288 5.640 0.48 168777. 0.4349
|
|
19.04 0.1675 0.4554 0.0358 0.0132 0.412 3.249 3.699 307.543 0.367 16.453 5.455 0.48 168867. 0.4104
|
|
20.63 0.1815 0.4764 0.0340 0.0129 0.405 3.189 3.506 301.881 0.360 15.597 5.268 0.48 168961. 0.3859
|
|
22.21 0.1955 0.4945 0.0320 0.0127 0.396 3.123 3.309 295.576 0.353 14.719 5.078 0.48 169059. 0.3613
|
|
23.80 0.2094 0.5095 0.0301 0.0124 0.387 3.049 3.107 288.607 0.344 13.821 4.883 0.48 169161. 0.3367
|
|
25.39 0.2234 0.5212 0.0281 0.0120 0.377 2.968 2.901 280.953 0.335 12.903 4.683 0.48 169267. 0.3120
|
|
26.97 0.2374 0.5293 0.0261 0.0117 0.366 2.880 2.690 272.597 0.325 11.967 4.476 0.48 169376. 0.2872
|
|
28.56 0.2513 0.5336 0.0240 0.0113 0.353 2.784 2.476 263.522 0.315 11.013 4.262 0.48 169490. 0.2623
|
|
30.15 0.2653 0.5334 0.0219 0.0109 0.340 2.681 2.258 253.713 0.303 10.043 4.036 0.48 169608. 0.2373
|
|
31.73 0.2792 0.5284 0.0197 0.0104 0.326 2.569 2.036 243.160 0.290 9.058 3.799 0.48 169731. 0.2120
|
|
33.32 0.2932 0.5178 0.0175 0.0099 0.311 2.450 1.812 231.854 0.277 8.060 3.545 0.48 169857. 0.1867
|
|
34.91 0.3072 0.5006 0.0154 0.0094 0.295 2.322 1.585 219.794 0.262 7.051 3.271 0.48 169988. 0.1611
|
|
36.49 0.3211 0.4755 0.0131 0.0089 0.278 2.187 1.356 206.981 0.247 6.033 2.972 0.48 170124. 0.1354
|
|
38.08 0.3351 0.4408 0.0109 0.0083 0.259 2.044 1.126 193.424 0.231 5.008 2.640 0.48 170264. 0.1096
|
|
39.67 0.3491 0.3940 0.0087 0.0077 0.240 1.893 0.895 179.141 0.214 3.980 2.266 0.48 170408. 0.0838
|
|
41.25 0.3630 0.3316 0.0064 0.0070 0.220 1.734 0.664 164.156 0.196 2.952 1.834 0.48 170557. 0.0584
|
|
42.84 0.3770 0.2485 0.0042 0.0064 0.199 1.569 0.433 148.496 0.177 1.926 1.323 0.48 170711. 0.0341
|
|
44.43 0.3909 0.1360 0.0020 0.0057 0.177 1.396 0.204 132.163 0.158 0.905 0.699 0.48 170866. 0.0123
|
|
46.01 0.4049
|
|
|
|
|
|
|
|
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 0.0547 0.0143 0.636 4.455 7.151 474.391 0.503 31.809 6.837 0.54 188995. 0.7153
|
|
1.78 0.0139 0.0520 0.0535 0.0143 0.636 4.456 6.987 474.469 0.503 31.079 6.680 0.54 189057. 0.6907
|
|
3.55 0.0278 0.1016 0.0522 0.0143 0.636 4.452 6.816 474.085 0.503 30.320 6.521 0.54 189123. 0.6660
|
|
5.33 0.0417 0.1487 0.0508 0.0142 0.635 4.444 6.639 473.197 0.502 29.531 6.364 0.54 189192. 0.6414
|
|
7.11 0.0556 0.1934 0.0494 0.0142 0.633 4.431 6.455 471.765 0.501 28.713 6.206 0.54 189264. 0.6168
|
|
8.89 0.0695 0.2356 0.0479 0.0141 0.630 4.412 6.265 469.748 0.498 27.865 6.049 0.54 189339. 0.5922
|
|
10.66 0.0834 0.2754 0.0464 0.0141 0.626 4.387 6.067 467.098 0.496 26.986 5.891 0.54 189418. 0.5676
|
|
12.44 0.0973 0.3127 0.0449 0.0140 0.622 4.355 5.863 463.771 0.492 26.077 5.734 0.54 189500. 0.5431
|
|
14.22 0.1112 0.3475 0.0432 0.0138 0.616 4.317 5.651 459.716 0.488 25.137 5.576 0.54 189586. 0.5185
|
|
15.99 0.1251 0.3798 0.0416 0.0137 0.610 4.272 5.433 454.885 0.483 24.165 5.417 0.54 189676. 0.4939
|
|
17.77 0.1390 0.4096 0.0398 0.0135 0.602 4.219 5.207 449.247 0.477 23.162 5.257 0.54 189769. 0.4693
|
|
19.55 0.1529 0.4368 0.0381 0.0133 0.594 4.158 4.975 442.773 0.470 22.129 5.096 0.54 189866. 0.4447
|
|
21.33 0.1668 0.4613 0.0362 0.0131 0.584 4.089 4.737 435.437 0.462 21.068 4.934 0.54 189968. 0.4200
|
|
23.10 0.1807 0.4830 0.0344 0.0129 0.573 4.012 4.492 427.209 0.453 19.980 4.769 0.54 190073. 0.3954
|
|
24.88 0.1946 0.5019 0.0325 0.0126 0.561 3.926 4.241 418.058 0.444 18.864 4.601 0.54 190183. 0.3707
|
|
26.66 0.2085 0.5177 0.0305 0.0123 0.547 3.831 3.984 407.956 0.433 17.722 4.430 0.54 190297. 0.3459
|
|
28.43 0.2224 0.5303 0.0285 0.0119 0.532 3.727 3.722 396.874 0.421 16.556 4.254 0.54 190415. 0.3210
|
|
30.21 0.2363 0.5393 0.0264 0.0116 0.516 3.614 3.455 384.786 0.408 15.366 4.072 0.54 190538. 0.2961
|
|
31.99 0.2502 0.5446 0.0243 0.0112 0.498 3.490 3.182 371.669 0.394 14.153 3.883 0.54 190665. 0.2710
|
|
33.77 0.2641 0.5455 0.0222 0.0108 0.479 3.357 2.905 357.501 0.379 12.920 3.685 0.54 190797. 0.2457
|
|
35.54 0.2780 0.5417 0.0201 0.0103 0.459 3.214 2.623 342.266 0.363 11.669 3.476 0.54 190934. 0.2203
|
|
37.32 0.2919 0.5323 0.0179 0.0098 0.437 3.061 2.338 325.955 0.346 10.400 3.254 0.54 191076. 0.1946
|
|
39.10 0.3058 0.5164 0.0157 0.0093 0.414 2.898 2.050 308.561 0.327 9.117 3.013 0.54 191222. 0.1687
|
|
40.87 0.3197 0.4927 0.0135 0.0087 0.389 2.724 1.759 290.089 0.308 7.823 2.750 0.54 191374. 0.1426
|
|
42.65 0.3336 0.4595 0.0112 0.0081 0.363 2.541 1.466 270.550 0.287 6.519 2.457 0.54 191530. 0.1164
|
|
44.43 0.3475 0.4141 0.0090 0.0075 0.335 2.348 1.172 249.967 0.265 5.211 2.126 0.54 191691. 0.0900
|
|
46.21 0.3614 0.3530 0.0067 0.0069 0.306 2.145 0.877 228.376 0.242 3.902 1.742 0.54 191858. 0.0638
|
|
47.98 0.3753 0.2706 0.0045 0.0062 0.276 1.933 0.584 205.817 0.218 2.597 1.287 0.54 192029. 0.0385
|
|
49.76 0.3892 0.1583 0.0022 0.0055 0.244 1.712 0.292 182.301 0.193 1.297 0.725 0.54 192203. 0.0153
|
|
51.54 0.4031 -0.0066 -0.0001 0.0047 0.210 1.473 -0.010 156.875 0.166 -0.045 -0.029 0.54 192347. 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 0.0553 0.0143 0.875 5.513 8.928 652.219 0.623 39.710 6.208 0.59 209986. 0.7256
|
|
2.01 0.0142 0.0535 0.0540 0.0143 0.875 5.512 8.718 652.161 0.623 38.779 6.063 0.60 210057. 0.7003
|
|
4.03 0.0284 0.1045 0.0527 0.0143 0.874 5.506 8.500 651.425 0.622 37.808 5.918 0.60 210132. 0.6750
|
|
6.04 0.0425 0.1529 0.0513 0.0143 0.872 5.494 8.274 649.952 0.621 36.801 5.774 0.60 210210. 0.6496
|
|
8.05 0.0567 0.1988 0.0498 0.0142 0.869 5.474 8.038 647.680 0.618 35.755 5.629 0.60 210293. 0.6243
|
|
10.07 0.0709 0.2421 0.0483 0.0141 0.864 5.448 7.795 644.550 0.616 34.670 5.485 0.60 210379. 0.5990
|
|
12.08 0.0851 0.2829 0.0467 0.0141 0.859 5.414 7.542 640.493 0.612 33.547 5.341 0.60 210469. 0.5738
|
|
14.10 0.0992 0.3211 0.0451 0.0139 0.852 5.371 7.280 635.442 0.607 32.383 5.197 0.60 210563. 0.5485
|
|
16.11 0.1134 0.3568 0.0434 0.0138 0.844 5.319 7.009 629.321 0.601 31.178 5.052 0.60 210662. 0.5232
|
|
18.12 0.1276 0.3898 0.0417 0.0137 0.834 5.258 6.729 622.064 0.594 29.933 4.907 0.60 210764. 0.4979
|
|
20.14 0.1418 0.4203 0.0399 0.0135 0.823 5.187 6.441 613.626 0.586 28.648 4.761 0.60 210872. 0.4726
|
|
22.15 0.1559 0.4480 0.0381 0.0133 0.810 5.105 6.143 603.967 0.577 27.324 4.613 0.60 210983. 0.4473
|
|
24.16 0.1701 0.4729 0.0362 0.0130 0.795 5.013 5.837 593.045 0.566 25.964 4.464 0.60 211100. 0.4219
|
|
26.18 0.1843 0.4950 0.0342 0.0127 0.779 4.909 5.523 580.817 0.555 24.568 4.313 0.60 211221. 0.3965
|
|
28.19 0.1985 0.5141 0.0322 0.0124 0.761 4.794 5.202 567.241 0.542 23.138 4.159 0.60 211346. 0.3711
|
|
30.21 0.2126 0.5299 0.0302 0.0121 0.741 4.668 4.873 552.273 0.527 21.674 4.002 0.60 211477. 0.3456
|
|
32.22 0.2268 0.5424 0.0281 0.0118 0.719 4.529 4.537 535.872 0.512 20.178 3.840 0.60 211613. 0.3199
|
|
34.23 0.2410 0.5511 0.0260 0.0114 0.695 4.378 4.194 518.002 0.495 18.653 3.672 0.60 211754. 0.2941
|
|
36.25 0.2552 0.5557 0.0238 0.0109 0.669 4.215 3.844 498.629 0.476 17.099 3.497 0.60 211901. 0.2682
|
|
38.26 0.2693 0.5556 0.0216 0.0105 0.641 4.038 3.489 477.725 0.456 15.520 3.313 0.60 212053. 0.2421
|
|
40.27 0.2835 0.5503 0.0194 0.0100 0.611 3.848 3.129 455.270 0.435 13.916 3.117 0.60 212210. 0.2157
|
|
42.29 0.2977 0.5389 0.0171 0.0095 0.578 3.645 2.764 431.250 0.412 12.293 2.907 0.60 212373. 0.1890
|
|
44.30 0.3119 0.5200 0.0148 0.0089 0.544 3.429 2.395 405.664 0.387 10.652 2.677 0.60 212541. 0.1621
|
|
46.31 0.3261 0.4921 0.0125 0.0083 0.508 3.199 2.023 378.523 0.361 8.997 2.424 0.60 212715. 0.1348
|
|
48.33 0.3402 0.4529 0.0102 0.0077 0.469 2.957 1.649 349.852 0.334 7.333 2.137 0.60 212895. 0.1074
|
|
50.34 0.3544 0.3989 0.0079 0.0070 0.429 2.702 1.274 319.694 0.305 5.666 1.807 0.60 213081. 0.0798
|
|
52.36 0.3686 0.3250 0.0056 0.0063 0.386 2.435 0.899 288.106 0.275 4.000 1.416 0.60 213272. 0.0525
|
|
54.37 0.3828 0.2230 0.0033 0.0056 0.342 2.157 0.526 255.144 0.244 2.341 0.936 0.60 213469. 0.0266
|
|
56.38 0.3969 0.0779 0.0010 0.0048 0.296 1.865 0.153 220.629 0.211 0.682 0.315 0.60 213663. 0.0048
|
|
58.40 0.4111
|
|
|
|
|
|
|
|
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 0.0561 0.0144 1.172 6.713 10.943 873.706 0.758 48.676 5.681 0.65 230973. 0.7352
|
|
2.17 0.0139 0.0528 0.0548 0.0144 1.171 6.711 10.692 873.385 0.758 47.557 5.552 0.65 231050. 0.7102
|
|
4.34 0.0278 0.1032 0.0534 0.0144 1.170 6.702 10.430 872.176 0.757 46.391 5.424 0.65 231131. 0.6852
|
|
6.51 0.0416 0.1511 0.0520 0.0143 1.167 6.685 10.158 870.003 0.755 45.181 5.296 0.65 231216. 0.6602
|
|
8.68 0.0555 0.1966 0.0506 0.0143 1.162 6.660 9.876 866.790 0.752 43.927 5.168 0.65 231305. 0.6353
|
|
10.85 0.0694 0.2396 0.0491 0.0142 1.157 6.627 9.583 862.460 0.749 42.627 5.040 0.65 231399. 0.6103
|
|
13.02 0.0833 0.2803 0.0475 0.0141 1.149 6.585 9.281 856.930 0.744 41.281 4.912 0.65 231496. 0.5854
|
|
15.18 0.0972 0.3185 0.0459 0.0140 1.140 6.532 8.968 850.114 0.738 39.888 4.785 0.65 231597. 0.5605
|
|
17.35 0.1111 0.3543 0.0443 0.0139 1.129 6.469 8.644 841.918 0.731 38.448 4.657 0.65 231703. 0.5356
|
|
19.52 0.1249 0.3876 0.0426 0.0137 1.116 6.395 8.309 832.256 0.722 36.959 4.528 0.66 231814. 0.5106
|
|
21.69 0.1388 0.4184 0.0408 0.0135 1.101 6.309 7.964 821.063 0.713 35.424 4.399 0.66 231929. 0.4857
|
|
23.86 0.1527 0.4466 0.0390 0.0133 1.084 6.211 7.609 808.290 0.702 33.843 4.270 0.66 232048. 0.4607
|
|
26.03 0.1666 0.4723 0.0371 0.0131 1.065 6.100 7.243 793.890 0.689 32.219 4.138 0.66 232173. 0.4357
|
|
28.20 0.1805 0.4952 0.0352 0.0128 1.043 5.977 6.869 777.804 0.675 30.552 4.005 0.66 232302. 0.4106
|
|
30.37 0.1944 0.5153 0.0332 0.0125 1.019 5.840 6.485 759.980 0.660 28.844 3.870 0.66 232437. 0.3855
|
|
32.54 0.2082 0.5324 0.0312 0.0122 0.993 5.689 6.092 740.364 0.643 27.097 3.732 0.66 232577. 0.3603
|
|
34.71 0.2221 0.5463 0.0292 0.0119 0.964 5.524 5.691 718.905 0.624 25.312 3.590 0.66 232722. 0.3350
|
|
36.88 0.2360 0.5568 0.0271 0.0115 0.933 5.345 5.281 695.554 0.604 23.491 3.444 0.66 232873. 0.3096
|
|
39.05 0.2499 0.5635 0.0249 0.0111 0.899 5.150 4.864 670.268 0.582 21.636 3.292 0.66 233029. 0.2840
|
|
41.22 0.2638 0.5659 0.0227 0.0106 0.862 4.941 4.440 643.008 0.558 19.750 3.132 0.66 233190. 0.2582
|
|
43.39 0.2777 0.5636 0.0205 0.0101 0.823 4.716 4.010 613.746 0.533 17.835 2.963 0.66 233357. 0.2321
|
|
45.55 0.2915 0.5557 0.0183 0.0096 0.781 4.476 3.573 582.461 0.506 15.894 2.783 0.66 233531. 0.2058
|
|
47.72 0.3054 0.5412 0.0160 0.0091 0.736 4.220 3.132 549.146 0.477 13.931 2.587 0.66 233710. 0.1791
|
|
49.89 0.3193 0.5187 0.0138 0.0085 0.689 3.948 2.686 513.808 0.446 11.949 2.372 0.66 233894. 0.1521
|
|
52.06 0.3332 0.4863 0.0115 0.0079 0.639 3.661 2.238 476.469 0.414 9.955 2.131 0.66 234086. 0.1247
|
|
54.23 0.3471 0.4410 0.0092 0.0072 0.586 3.359 1.788 437.175 0.380 7.953 1.855 0.66 234283. 0.0970
|
|
56.40 0.3610 0.3788 0.0069 0.0065 0.531 3.043 1.338 395.992 0.344 5.950 1.532 0.66 234486. 0.0693
|
|
58.57 0.3748 0.2931 0.0046 0.0058 0.473 2.712 0.888 353.000 0.306 3.951 1.141 0.66 234694. 0.0421
|
|
60.74 0.3887 0.1727 0.0023 0.0051 0.413 2.368 0.441 308.224 0.268 1.961 0.649 0.66 234907. 0.0168
|
|
62.91 0.4026 -0.0123 -0.0001 0.0043 0.348 1.993 -0.025 259.390 0.225 -0.113 -0.044 0.66 235069. 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 0.0569 0.0146 1.538 8.077 13.223 1146.744 0.913 58.816 5.230 0.71 251955. 0.7440
|
|
2.38 0.0140 0.0533 0.0556 0.0146 1.537 8.071 12.916 1145.904 0.912 57.452 5.113 0.71 252041. 0.7188
|
|
4.76 0.0279 0.1042 0.0542 0.0145 1.534 8.057 12.597 1143.864 0.910 56.033 4.995 0.71 252131. 0.6935
|
|
7.14 0.0419 0.1526 0.0528 0.0145 1.529 8.033 12.266 1140.520 0.908 54.560 4.878 0.71 252225. 0.6683
|
|
9.52 0.0558 0.1986 0.0513 0.0144 1.523 8.000 11.923 1135.773 0.904 53.032 4.761 0.71 252323. 0.6431
|
|
11.89 0.0698 0.2422 0.0498 0.0143 1.515 7.956 11.567 1129.518 0.899 51.449 4.645 0.71 252426. 0.6179
|
|
14.27 0.0837 0.2833 0.0482 0.0142 1.504 7.900 11.198 1121.648 0.893 49.809 4.528 0.71 252534. 0.5928
|
|
16.65 0.0977 0.3221 0.0466 0.0141 1.491 7.833 10.817 1112.046 0.885 48.113 4.412 0.71 252646. 0.5676
|
|
19.03 0.1116 0.3583 0.0449 0.0140 1.476 7.752 10.422 1100.592 0.876 46.358 4.295 0.71 252763. 0.5424
|
|
21.41 0.1256 0.3921 0.0431 0.0138 1.458 7.657 10.014 1087.165 0.865 44.544 4.178 0.71 252885. 0.5172
|
|
23.79 0.1396 0.4234 0.0413 0.0136 1.437 7.548 9.594 1071.684 0.853 42.674 4.060 0.71 253013. 0.4920
|
|
26.17 0.1535 0.4522 0.0394 0.0134 1.414 7.424 9.161 1054.083 0.839 40.748 3.942 0.71 253145. 0.4667
|
|
28.55 0.1675 0.4783 0.0375 0.0131 1.387 7.285 8.716 1034.296 0.823 38.770 3.822 0.72 253283. 0.4414
|
|
30.92 0.1814 0.5017 0.0356 0.0129 1.357 7.130 8.260 1012.253 0.806 36.739 3.701 0.72 253426. 0.4161
|
|
33.30 0.1954 0.5223 0.0335 0.0125 1.325 6.958 7.792 987.881 0.786 34.659 3.578 0.72 253574. 0.3907
|
|
35.68 0.2093 0.5399 0.0315 0.0122 1.289 6.770 7.314 961.111 0.765 32.531 3.451 0.72 253729. 0.3651
|
|
38.06 0.2233 0.5543 0.0294 0.0118 1.250 6.564 6.825 931.879 0.742 30.357 3.322 0.72 253889. 0.3395
|
|
40.44 0.2372 0.5651 0.0272 0.0114 1.207 6.340 6.326 900.125 0.716 28.139 3.188 0.72 254055. 0.3136
|
|
42.82 0.2512 0.5722 0.0250 0.0110 1.161 6.098 5.818 865.797 0.689 25.880 3.048 0.72 254227. 0.2876
|
|
45.20 0.2652 0.5749 0.0228 0.0105 1.112 5.838 5.302 828.854 0.660 23.582 2.901 0.72 254405. 0.2613
|
|
47.58 0.2791 0.5726 0.0206 0.0100 1.058 5.559 4.777 789.266 0.628 21.250 2.745 0.72 254590. 0.2347
|
|
49.95 0.2931 0.5646 0.0183 0.0095 1.002 5.262 4.246 747.018 0.594 18.887 2.578 0.72 254780. 0.2078
|
|
52.33 0.3070 0.5497 0.0160 0.0089 0.942 4.945 3.709 702.118 0.559 16.497 2.396 0.72 254978. 0.1805
|
|
54.71 0.3210 0.5263 0.0136 0.0083 0.878 4.611 3.167 654.590 0.521 14.086 2.194 0.72 255182. 0.1527
|
|
57.09 0.3349 0.4922 0.0113 0.0077 0.811 4.258 2.621 604.490 0.481 11.659 1.967 0.72 255392. 0.1246
|
|
59.47 0.3489 0.4443 0.0089 0.0070 0.740 3.887 2.074 551.904 0.439 9.223 1.704 0.72 255609. 0.0960
|
|
61.85 0.3628 0.3776 0.0066 0.0063 0.666 3.500 1.526 496.950 0.395 6.787 1.393 0.72 255833. 0.0673
|
|
64.23 0.3768 0.2845 0.0042 0.0056 0.590 3.097 0.980 439.763 0.350 4.357 1.010 0.72 256063. 0.0391
|
|
66.61 0.3908 0.1516 0.0019 0.0048 0.510 2.679 0.435 380.349 0.303 1.937 0.519 0.72 256295. 0.0134
|
|
68.98 0.4047
|
|
|
|
|
|
|
|
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 0.0579 0.0148 1.988 9.636 15.799 1482.090 1.089 70.275 4.835 0.77 272931. 0.7518
|
|
2.57 0.0139 0.0534 0.0566 0.0148 1.985 9.624 15.433 1480.260 1.087 68.644 4.729 0.77 273025. 0.7267
|
|
5.15 0.0279 0.1043 0.0552 0.0148 1.981 9.602 15.051 1476.873 1.085 66.946 4.622 0.77 273124. 0.7015
|
|
7.72 0.0418 0.1529 0.0537 0.0147 1.974 9.569 14.655 1471.791 1.081 65.183 4.516 0.77 273227. 0.6763
|
|
10.30 0.0558 0.1990 0.0522 0.0146 1.964 9.524 14.244 1464.886 1.076 63.356 4.410 0.77 273334. 0.6511
|
|
12.87 0.0697 0.2428 0.0507 0.0145 1.953 9.467 13.818 1456.027 1.070 61.462 4.304 0.77 273447. 0.6259
|
|
15.44 0.0836 0.2843 0.0491 0.0144 1.938 9.396 13.377 1445.082 1.062 59.502 4.199 0.77 273564. 0.6007
|
|
18.02 0.0976 0.3233 0.0474 0.0143 1.920 9.310 12.921 1431.903 1.052 57.474 4.093 0.77 273687. 0.5755
|
|
20.59 0.1115 0.3599 0.0457 0.0141 1.899 9.209 12.450 1416.354 1.040 55.377 3.987 0.77 273814. 0.5503
|
|
23.16 0.1254 0.3941 0.0439 0.0140 1.875 9.091 11.963 1398.278 1.027 53.209 3.880 0.77 273947. 0.5250
|
|
25.74 0.1394 0.4257 0.0420 0.0138 1.847 8.957 11.460 1377.580 1.012 50.974 3.773 0.77 274086. 0.4997
|
|
28.31 0.1533 0.4549 0.0401 0.0135 1.816 8.805 10.943 1354.188 0.995 48.673 3.665 0.77 274230. 0.4743
|
|
30.89 0.1673 0.4814 0.0382 0.0133 1.781 8.634 10.411 1328.030 0.976 46.308 3.556 0.77 274380. 0.4488
|
|
33.46 0.1812 0.5053 0.0362 0.0130 1.742 8.446 9.866 1299.041 0.954 43.882 3.445 0.77 274535. 0.4232
|
|
36.03 0.1951 0.5262 0.0341 0.0127 1.699 8.239 9.307 1267.147 0.931 41.397 3.331 0.77 274697. 0.3975
|
|
38.61 0.2091 0.5442 0.0320 0.0123 1.653 8.012 8.735 1232.281 0.905 38.854 3.215 0.78 274864. 0.3717
|
|
41.18 0.2230 0.5588 0.0299 0.0119 1.602 7.766 8.151 1194.385 0.877 36.256 3.095 0.78 275038. 0.3457
|
|
43.75 0.2369 0.5699 0.0277 0.0115 1.547 7.499 7.555 1153.414 0.847 33.607 2.971 0.78 275218. 0.3195
|
|
46.33 0.2509 0.5770 0.0255 0.0111 1.488 7.213 6.949 1109.335 0.815 30.908 2.841 0.78 275405. 0.2930
|
|
48.90 0.2648 0.5796 0.0232 0.0106 1.424 6.906 6.332 1062.130 0.780 28.163 2.704 0.78 275598. 0.2661
|
|
51.48 0.2788 0.5771 0.0209 0.0101 1.357 6.578 5.705 1011.804 0.743 25.376 2.557 0.78 275798. 0.2389
|
|
54.05 0.2927 0.5686 0.0186 0.0096 1.285 6.231 5.070 958.383 0.704 22.551 2.399 0.78 276005. 0.2113
|
|
56.62 0.3066 0.5527 0.0162 0.0090 1.209 5.864 4.428 901.924 0.663 19.695 2.227 0.78 276219. 0.1833
|
|
59.20 0.3206 0.5281 0.0139 0.0084 1.130 5.478 3.780 842.514 0.619 16.812 2.035 0.78 276439. 0.1548
|
|
61.77 0.3345 0.4923 0.0115 0.0078 1.046 5.073 3.127 780.280 0.573 13.911 1.818 0.78 276667. 0.1258
|
|
64.34 0.3484 0.4422 0.0091 0.0071 0.959 4.651 2.473 715.385 0.525 10.998 1.568 0.78 276902. 0.0964
|
|
66.92 0.3624 0.3731 0.0067 0.0065 0.869 4.213 1.817 648.037 0.476 8.083 1.272 0.78 277144. 0.0671
|
|
69.49 0.3763 0.2780 0.0043 0.0058 0.776 3.761 1.164 578.453 0.425 5.176 0.912 0.78 277393. 0.0385
|
|
72.07 0.3903 0.1449 0.0019 0.0051 0.679 3.294 0.512 506.647 0.372 2.279 0.459 0.78 277644. 0.0128
|
|
74.64 0.4042
|
|
|
|
|
|
|
|
PROP RPM = 14000
|
|
|
|
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 0.0592 0.0153 2.564 11.543 18.723 1911.883 1.304 83.278 4.442 0.83 293899. 0.7518
|
|
2.76 0.0139 0.0526 0.0578 0.0152 2.556 11.506 18.290 1905.839 1.300 81.353 4.353 0.83 294001. 0.7282
|
|
5.51 0.0277 0.1030 0.0564 0.0152 2.545 11.459 17.839 1898.052 1.295 79.350 4.263 0.83 294108. 0.7043
|
|
8.27 0.0416 0.1512 0.0549 0.0151 2.532 11.401 17.372 1888.368 1.288 77.272 4.173 0.83 294219. 0.6803
|
|
11.02 0.0554 0.1972 0.0534 0.0150 2.517 11.332 16.888 1876.936 1.280 75.117 4.081 0.83 294336. 0.6560
|
|
13.78 0.0693 0.2409 0.0518 0.0149 2.499 11.251 16.386 1863.594 1.271 72.885 3.988 0.83 294458. 0.6315
|
|
16.53 0.0831 0.2822 0.0502 0.0148 2.478 11.158 15.867 1848.204 1.261 70.575 3.894 0.83 294585. 0.6067
|
|
19.29 0.0970 0.3212 0.0485 0.0146 2.454 11.050 15.329 1830.243 1.248 68.185 3.799 0.83 294717. 0.5818
|
|
22.04 0.1108 0.3578 0.0467 0.0145 2.427 10.926 14.774 1809.784 1.234 65.715 3.703 0.83 294855. 0.5567
|
|
24.80 0.1247 0.3919 0.0449 0.0143 2.396 10.787 14.200 1786.700 1.219 63.163 3.605 0.83 294998. 0.5314
|
|
27.55 0.1386 0.4234 0.0430 0.0141 2.361 10.631 13.608 1760.892 1.201 60.530 3.505 0.83 295147. 0.5058
|
|
30.31 0.1524 0.4523 0.0411 0.0139 2.323 10.457 12.999 1732.028 1.181 57.821 3.404 0.83 295302. 0.4801
|
|
33.06 0.1663 0.4785 0.0391 0.0136 2.280 10.264 12.373 1700.016 1.160 55.037 3.301 0.83 295463. 0.4543
|
|
35.82 0.1801 0.5019 0.0371 0.0133 2.233 10.051 11.731 1664.820 1.136 52.181 3.196 0.83 295630. 0.4282
|
|
38.58 0.1940 0.5222 0.0350 0.0130 2.181 9.820 11.074 1626.482 1.109 49.256 3.088 0.83 295804. 0.4020
|
|
41.33 0.2078 0.5393 0.0329 0.0127 2.125 9.569 10.401 1584.973 1.081 46.263 2.976 0.83 295984. 0.3755
|
|
44.09 0.2217 0.5528 0.0307 0.0123 2.065 9.299 9.714 1540.227 1.051 43.206 2.860 0.84 296170. 0.3487
|
|
46.84 0.2355 0.5625 0.0285 0.0119 2.001 9.009 9.012 1492.253 1.018 40.087 2.739 0.84 296363. 0.3217
|
|
49.60 0.2494 0.5679 0.0262 0.0115 1.933 8.700 8.298 1441.087 0.983 36.911 2.612 0.84 296563. 0.2943
|
|
52.35 0.2633 0.5684 0.0239 0.0111 1.860 8.373 7.572 1386.809 0.946 33.680 2.476 0.84 296770. 0.2666
|
|
55.11 0.2771 0.5633 0.0216 0.0106 1.783 8.027 6.834 1329.512 0.907 30.399 2.332 0.84 296984. 0.2384
|
|
57.86 0.2910 0.5517 0.0192 0.0102 1.702 7.663 6.087 1269.279 0.866 27.074 2.175 0.84 297205. 0.2099
|
|
60.62 0.3048 0.5326 0.0169 0.0096 1.618 7.283 5.330 1206.259 0.823 23.710 2.004 0.84 297433. 0.1810
|
|
63.37 0.3187 0.5045 0.0144 0.0091 1.530 6.886 4.567 1140.635 0.778 20.314 1.816 0.84 297669. 0.1518
|
|
66.13 0.3325 0.4656 0.0120 0.0086 1.438 6.476 3.798 1072.650 0.732 16.894 1.606 0.84 297912. 0.1224
|
|
68.88 0.3464 0.4134 0.0096 0.0080 1.344 6.053 3.026 1002.559 0.684 13.459 1.369 0.84 298163. 0.0932
|
|
71.64 0.3602 0.3448 0.0071 0.0074 1.248 5.619 2.253 930.675 0.635 10.020 1.098 0.84 298421. 0.0645
|
|
74.39 0.3741 0.2555 0.0047 0.0069 1.150 5.176 1.481 857.302 0.585 6.587 0.784 0.84 298687. 0.0373
|
|
77.15 0.3880 0.1396 0.0023 0.0063 1.049 4.724 0.712 782.456 0.534 3.167 0.413 0.84 298956. 0.0136
|
|
79.91 0.4018
|
|
|
|
|
|
|
|
PROP RPM = 15000
|
|
|
|
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 0.0607 0.0166 3.424 14.389 22.027 2553.630 1.626 97.977 3.912 0.89 314856. 0.7183
|
|
3.03 0.0142 0.0512 0.0592 0.0165 3.397 14.276 21.507 2533.460 1.613 95.663 3.850 0.89 314970. 0.6985
|
|
6.07 0.0285 0.1007 0.0578 0.0163 3.368 14.150 20.965 2511.255 1.599 93.251 3.787 0.89 315090. 0.6782
|
|
9.10 0.0427 0.1484 0.0562 0.0162 3.335 14.013 20.402 2486.885 1.583 90.746 3.721 0.89 315215. 0.6574
|
|
12.13 0.0569 0.1943 0.0546 0.0160 3.299 13.863 19.817 2460.174 1.566 88.147 3.654 0.89 315345. 0.6362
|
|
15.16 0.0712 0.2382 0.0529 0.0158 3.261 13.702 19.211 2431.674 1.548 85.451 3.583 0.89 315482. 0.6144
|
|
18.20 0.0854 0.2799 0.0512 0.0156 3.221 13.534 18.583 2401.795 1.529 82.657 3.509 0.89 315624. 0.5918
|
|
21.23 0.0996 0.3192 0.0494 0.0154 3.180 13.363 17.933 2371.540 1.510 79.765 3.430 0.89 315772. 0.5681
|
|
24.26 0.1139 0.3561 0.0475 0.0152 3.136 13.177 17.260 2338.566 1.489 76.773 3.348 0.89 315927. 0.5440
|
|
27.29 0.1281 0.3903 0.0456 0.0150 3.089 12.979 16.565 2303.319 1.466 73.679 3.262 0.89 316088. 0.5193
|
|
30.33 0.1423 0.4216 0.0437 0.0147 3.040 12.772 15.847 2266.602 1.443 70.486 3.171 0.89 316255. 0.4938
|
|
33.36 0.1566 0.4492 0.0416 0.0145 2.992 12.570 15.107 2230.784 1.420 67.197 3.072 0.89 316429. 0.4670
|
|
36.39 0.1708 0.4731 0.0395 0.0143 2.943 12.367 14.347 2194.665 1.397 63.816 2.965 0.89 316610. 0.4393
|
|
39.43 0.1850 0.4935 0.0374 0.0140 2.890 12.145 13.567 2155.304 1.372 60.347 2.855 0.89 316798. 0.4114
|
|
42.46 0.1993 0.5102 0.0352 0.0137 2.833 11.905 12.768 2112.778 1.345 56.794 2.741 0.89 316992. 0.3831
|
|
45.49 0.2135 0.5229 0.0329 0.0134 2.772 11.649 11.951 2067.403 1.316 53.158 2.622 0.89 317194. 0.3546
|
|
48.52 0.2277 0.5311 0.0306 0.0131 2.708 11.379 11.116 2019.383 1.286 49.446 2.497 0.89 317404. 0.3256
|
|
51.56 0.2420 0.5346 0.0283 0.0128 2.640 11.092 10.265 1968.558 1.253 45.659 2.365 0.90 317621. 0.2964
|
|
54.59 0.2562 0.5327 0.0259 0.0125 2.568 10.791 9.398 1915.096 1.219 41.804 2.226 0.90 317845. 0.2669
|
|
57.62 0.2704 0.5249 0.0235 0.0121 2.493 10.476 8.518 1859.189 1.184 37.886 2.078 0.90 318078. 0.2372
|
|
60.65 0.2847 0.5105 0.0210 0.0117 2.415 10.149 7.624 1801.140 1.147 33.911 1.920 0.90 318318. 0.2074
|
|
63.69 0.2989 0.4887 0.0185 0.0113 2.335 9.812 6.719 1741.279 1.109 29.886 1.750 0.90 318566. 0.1775
|
|
66.72 0.3131 0.4585 0.0160 0.0109 2.253 9.465 5.805 1679.773 1.069 25.820 1.567 0.90 318823. 0.1477
|
|
69.75 0.3274 0.4189 0.0135 0.0105 2.168 9.111 4.884 1616.942 1.029 21.723 1.370 0.90 319088. 0.1184
|
|
72.79 0.3416 0.3688 0.0109 0.0101 2.083 8.752 3.958 1553.145 0.989 17.605 1.156 0.90 319362. 0.0900
|
|
75.82 0.3558 0.3069 0.0083 0.0097 1.997 8.389 3.031 1488.799 0.948 13.481 0.923 0.90 319644. 0.0629
|
|
78.85 0.3701 0.2317 0.0058 0.0093 1.910 8.025 2.105 1424.209 0.907 9.363 0.670 0.90 319934. 0.0380
|
|
81.88 0.3843 0.1417 0.0033 0.0088 1.823 7.660 1.183 1359.318 0.865 5.263 0.395 0.90 320232. 0.0168
|
|
84.92 0.3985 0.0336 0.0007 0.0084 1.730 7.270 0.257 1290.209 0.821 1.141 0.090 0.90 320526. 0.0018
|
|
87.95 0.4128
|
|
|
|
|
|
|
|
PROP RPM = 16000
|
|
|
|
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 0.0621 0.0195 4.880 19.222 25.662 3638.693 2.172 114.144 3.199 0.95 335807. 0.6339
|
|
3.30 0.0145 0.0458 0.0607 0.0192 4.814 18.963 25.057 3589.614 2.142 111.455 3.166 0.95 335933. 0.6200
|
|
6.60 0.0290 0.0906 0.0591 0.0190 4.744 18.688 24.426 3537.705 2.111 108.646 3.132 0.95 336065. 0.6054
|
|
9.90 0.0436 0.1344 0.0575 0.0187 4.671 18.399 23.768 3482.971 2.079 105.722 3.095 0.95 336202. 0.5903
|
|
13.20 0.0581 0.1769 0.0559 0.0184 4.593 18.095 23.085 3425.309 2.044 102.680 3.057 0.95 336346. 0.5745
|
|
16.50 0.0726 0.2182 0.0542 0.0180 4.512 17.774 22.374 3364.587 2.008 99.521 3.016 0.95 336497. 0.5581
|
|
19.80 0.0871 0.2581 0.0524 0.0177 4.426 17.436 21.637 3300.677 1.970 96.242 2.973 0.95 336654. 0.5410
|
|
23.10 0.1017 0.2962 0.0505 0.0173 4.341 17.102 20.873 3237.453 1.932 92.842 2.924 0.95 336818. 0.5226
|
|
26.40 0.1162 0.3320 0.0486 0.0170 4.258 16.775 20.080 3175.446 1.895 89.317 2.868 0.95 336988. 0.5028
|
|
29.70 0.1307 0.3653 0.0466 0.0167 4.176 16.452 19.260 3114.382 1.859 85.668 2.805 0.95 337166. 0.4815
|
|
33.01 0.1452 0.3962 0.0446 0.0163 4.090 16.112 18.413 3049.993 1.820 81.900 2.738 0.95 337351. 0.4596
|
|
36.31 0.1597 0.4237 0.0425 0.0160 4.008 15.788 17.539 2988.622 1.784 78.015 2.662 0.95 337543. 0.4361
|
|
39.61 0.1743 0.4457 0.0403 0.0158 3.943 15.532 16.640 2940.252 1.755 74.015 2.567 0.95 337743. 0.4096
|
|
42.91 0.1888 0.4609 0.0381 0.0156 3.901 15.367 15.715 2908.993 1.736 69.902 2.450 0.95 337951. 0.3800
|
|
46.21 0.2033 0.4719 0.0358 0.0154 3.856 15.191 14.768 2875.566 1.716 65.689 2.329 0.95 338166. 0.3502
|
|
49.51 0.2178 0.4783 0.0334 0.0152 3.809 15.004 13.800 2840.213 1.695 61.381 2.204 0.95 338390. 0.3202
|
|
52.81 0.2324 0.4799 0.0310 0.0150 3.759 14.808 12.811 2803.209 1.673 56.983 2.073 0.95 338622. 0.2902
|
|
56.11 0.2469 0.4761 0.0286 0.0148 3.709 14.611 11.803 2765.804 1.651 52.501 1.936 0.95 338862. 0.2601
|
|
59.41 0.2614 0.4668 0.0261 0.0146 3.658 14.409 10.779 2727.571 1.628 47.944 1.792 0.96 339110. 0.2302
|
|
62.71 0.2759 0.4517 0.0236 0.0144 3.605 14.203 9.739 2688.532 1.605 43.318 1.643 0.96 339367. 0.2006
|
|
66.01 0.2904 0.4304 0.0210 0.0142 3.552 13.994 8.686 2648.971 1.581 38.634 1.487 0.96 339633. 0.1715
|
|
69.31 0.3050 0.4026 0.0185 0.0140 3.499 13.783 7.622 2609.147 1.557 33.902 1.325 0.96 339908. 0.1431
|
|
72.61 0.3195 0.3681 0.0159 0.0138 3.446 13.573 6.550 2569.389 1.533 29.136 1.156 0.96 340192. 0.1158
|
|
75.91 0.3340 0.3266 0.0133 0.0136 3.393 13.366 5.474 2530.203 1.510 24.350 0.981 0.96 340485. 0.0898
|
|
79.21 0.3485 0.2780 0.0106 0.0133 3.341 13.161 4.397 2491.366 1.487 19.560 0.801 0.96 340788. 0.0657
|
|
82.51 0.3631 0.2223 0.0080 0.0131 3.289 12.958 3.324 2452.958 1.464 14.783 0.615 0.96 341100. 0.0438
|
|
85.81 0.3776 0.1595 0.0055 0.0129 3.238 12.756 2.256 2414.665 1.441 10.037 0.424 0.96 341423. 0.0249
|
|
89.11 0.3921 0.0892 0.0029 0.0127 3.185 12.545 1.196 2374.710 1.417 5.319 0.228 0.96 341756. 0.0098
|
|
92.41 0.4066 0.0080 0.0002 0.0124 3.105 12.233 0.101 2315.701 1.382 0.450 0.020 0.96 342099. 0.0002
|
|
95.71 0.4211
|
|
|
|
|
|
|