612 lines
109 KiB
Plaintext
612 lines
109 KiB
Plaintext
15x4W (15x4W.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 0.0664 0.0295 0.002 0.114 0.107 1.344 0.013 0.477 36.181 0.06 32102. 0.4633
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0.21 0.0150 0.0330 0.0648 0.0294 0.002 0.113 0.105 1.341 0.013 0.465 35.337 0.06 32114. 0.4469
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0.43 0.0300 0.0643 0.0631 0.0294 0.002 0.113 0.102 1.338 0.013 0.453 34.479 0.06 32128. 0.4302
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0.64 0.0449 0.0941 0.0613 0.0293 0.002 0.113 0.099 1.335 0.013 0.440 33.609 0.06 32142. 0.4135
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0.85 0.0599 0.1221 0.0595 0.0292 0.002 0.112 0.096 1.330 0.013 0.427 32.726 0.06 32156. 0.3966
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1.06 0.0749 0.1485 0.0576 0.0291 0.002 0.112 0.093 1.324 0.013 0.413 31.830 0.06 32171. 0.3796
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1.28 0.0899 0.1731 0.0557 0.0289 0.002 0.111 0.090 1.318 0.013 0.400 30.919 0.06 32187. 0.3625
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1.49 0.1049 0.1959 0.0537 0.0287 0.002 0.111 0.087 1.310 0.013 0.385 29.992 0.06 32204. 0.3453
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1.70 0.1198 0.2168 0.0517 0.0286 0.002 0.110 0.083 1.301 0.012 0.371 29.048 0.06 32221. 0.3280
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1.92 0.1348 0.2358 0.0496 0.0283 0.002 0.109 0.080 1.291 0.012 0.356 28.085 0.06 32239. 0.3107
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2.13 0.1498 0.2528 0.0474 0.0281 0.002 0.108 0.076 1.280 0.012 0.340 27.103 0.06 32257. 0.2932
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2.34 0.1648 0.2678 0.0452 0.0278 0.002 0.107 0.073 1.268 0.012 0.324 26.099 0.06 32276. 0.2757
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2.55 0.1798 0.2807 0.0429 0.0275 0.002 0.106 0.069 1.254 0.012 0.308 25.070 0.06 32296. 0.2581
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2.77 0.1948 0.2912 0.0406 0.0272 0.002 0.105 0.066 1.238 0.012 0.292 24.014 0.06 32317. 0.2405
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2.98 0.2097 0.2995 0.0383 0.0268 0.002 0.103 0.062 1.221 0.012 0.275 22.929 0.06 32339. 0.2229
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3.19 0.2247 0.3052 0.0359 0.0264 0.002 0.102 0.058 1.203 0.011 0.257 21.809 0.06 32361. 0.2052
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3.40 0.2397 0.3083 0.0334 0.0260 0.002 0.100 0.054 1.183 0.011 0.240 20.652 0.06 32384. 0.1875
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3.62 0.2547 0.3085 0.0309 0.0255 0.002 0.098 0.050 1.161 0.011 0.222 19.452 0.06 32408. 0.1698
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3.83 0.2697 0.3057 0.0283 0.0250 0.002 0.096 0.046 1.138 0.011 0.203 18.204 0.06 32433. 0.1522
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4.04 0.2846 0.2996 0.0257 0.0244 0.001 0.094 0.041 1.112 0.011 0.184 16.901 0.06 32459. 0.1346
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4.26 0.2996 0.2898 0.0230 0.0238 0.001 0.092 0.037 1.085 0.010 0.165 15.534 0.06 32485. 0.1171
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4.47 0.3146 0.2762 0.0203 0.0232 0.001 0.089 0.033 1.056 0.010 0.146 14.096 0.06 32513. 0.0999
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4.68 0.3296 0.2581 0.0176 0.0225 0.001 0.087 0.028 1.025 0.010 0.126 12.574 0.06 32541. 0.0829
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4.89 0.3446 0.2351 0.0149 0.0218 0.001 0.084 0.024 0.992 0.009 0.107 10.957 0.06 32570. 0.0663
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5.11 0.3595 0.2066 0.0121 0.0210 0.001 0.081 0.019 0.957 0.009 0.087 9.227 0.06 32600. 0.0504
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5.32 0.3745 0.1718 0.0093 0.0202 0.001 0.078 0.015 0.920 0.009 0.066 7.366 0.06 32631. 0.0352
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5.53 0.3895 0.1297 0.0064 0.0193 0.001 0.074 0.010 0.881 0.008 0.046 5.348 0.06 32662. 0.0213
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5.75 0.4045 0.0790 0.0036 0.0184 0.001 0.071 0.006 0.840 0.008 0.026 3.137 0.06 32693. 0.0094
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5.96 0.4195 0.0170 0.0007 0.0175 0.001 0.067 0.001 0.797 0.008 0.005 0.650 0.06 32719. 0.0009
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6.17 0.4345
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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 0.0668 0.0248 0.012 0.381 0.431 9.025 0.043 1.917 21.658 0.12 64203. 0.5562
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0.43 0.0153 0.0402 0.0651 0.0247 0.012 0.381 0.420 9.009 0.043 1.868 21.149 0.12 64229. 0.5362
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0.87 0.0305 0.0784 0.0634 0.0247 0.012 0.380 0.409 8.986 0.043 1.818 20.635 0.12 64256. 0.5161
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1.30 0.0458 0.1147 0.0616 0.0246 0.012 0.378 0.397 8.956 0.043 1.767 20.118 0.12 64285. 0.4960
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1.73 0.0610 0.1489 0.0597 0.0245 0.012 0.377 0.385 8.917 0.043 1.714 19.596 0.12 64314. 0.4758
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2.17 0.0763 0.1811 0.0578 0.0243 0.012 0.375 0.373 8.871 0.042 1.659 19.069 0.12 64345. 0.4555
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2.60 0.0915 0.2113 0.0558 0.0242 0.012 0.373 0.360 8.815 0.042 1.602 18.536 0.12 64378. 0.4352
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3.03 0.1068 0.2394 0.0538 0.0240 0.012 0.370 0.347 8.750 0.042 1.544 17.998 0.12 64411. 0.4148
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3.47 0.1220 0.2653 0.0517 0.0238 0.012 0.367 0.334 8.674 0.041 1.485 17.452 0.12 64446. 0.3944
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3.90 0.1373 0.2890 0.0496 0.0236 0.012 0.363 0.320 8.588 0.041 1.423 16.899 0.12 64483. 0.3739
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4.33 0.1526 0.3104 0.0474 0.0233 0.011 0.359 0.306 8.491 0.041 1.360 16.337 0.12 64521. 0.3534
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4.77 0.1678 0.3295 0.0451 0.0230 0.011 0.354 0.291 8.381 0.040 1.296 15.764 0.12 64560. 0.3328
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5.20 0.1831 0.3461 0.0428 0.0227 0.011 0.349 0.276 8.259 0.039 1.229 15.179 0.12 64602. 0.3122
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5.63 0.1983 0.3601 0.0405 0.0223 0.011 0.343 0.261 8.124 0.039 1.162 14.581 0.12 64644. 0.2915
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6.07 0.2136 0.3715 0.0381 0.0219 0.011 0.337 0.246 7.976 0.038 1.092 13.967 0.12 64689. 0.2708
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6.50 0.2288 0.3800 0.0356 0.0214 0.010 0.330 0.230 7.812 0.037 1.022 13.333 0.12 64735. 0.2500
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6.93 0.2441 0.3854 0.0331 0.0209 0.010 0.323 0.213 7.634 0.036 0.949 12.678 0.12 64782. 0.2291
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7.37 0.2593 0.3875 0.0305 0.0204 0.010 0.314 0.197 7.441 0.036 0.875 11.997 0.12 64832. 0.2082
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7.80 0.2746 0.3859 0.0279 0.0198 0.010 0.306 0.180 7.232 0.035 0.800 11.284 0.12 64883. 0.1872
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8.23 0.2898 0.3803 0.0252 0.0192 0.009 0.296 0.163 7.006 0.033 0.724 10.535 0.12 64936. 0.1662
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8.67 0.3051 0.3702 0.0225 0.0186 0.009 0.286 0.145 6.763 0.032 0.646 9.742 0.12 64991. 0.1452
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9.10 0.3204 0.3549 0.0198 0.0178 0.009 0.275 0.128 6.503 0.031 0.567 8.896 0.12 65047. 0.1243
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9.53 0.3356 0.3338 0.0170 0.0171 0.008 0.263 0.110 6.225 0.030 0.488 7.985 0.12 65105. 0.1034
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9.97 0.3509 0.3057 0.0142 0.0163 0.008 0.251 0.091 5.930 0.028 0.407 6.996 0.12 65166. 0.0828
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10.40 0.3661 0.2695 0.0113 0.0154 0.008 0.237 0.073 5.617 0.027 0.326 5.910 0.12 65227. 0.0626
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10.83 0.3814 0.2234 0.0085 0.0145 0.007 0.223 0.055 5.287 0.025 0.244 4.702 0.12 65291. 0.0431
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11.27 0.3966 0.1648 0.0056 0.0135 0.007 0.209 0.036 4.938 0.024 0.162 3.337 0.12 65354. 0.0249
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11.70 0.4119 0.0901 0.0027 0.0125 0.006 0.193 0.018 4.570 0.022 0.079 1.755 0.12 65415. 0.0091
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12.13 0.4271 -0.0171 -0.0005 0.0114 0.006 0.175 -0.003 4.139 0.020 -0.013 -0.321 0.12 65399. 0.0000
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12.57 0.4424
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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 0.0671 0.0228 0.038 0.791 0.974 28.086 0.089 4.331 15.725 0.18 96303. 0.6070
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0.65 0.0152 0.0437 0.0654 0.0228 0.038 0.790 0.949 28.034 0.089 4.222 15.358 0.18 96342. 0.5853
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1.30 0.0305 0.0854 0.0636 0.0227 0.037 0.788 0.924 27.957 0.089 4.110 14.990 0.18 96383. 0.5636
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1.95 0.0457 0.1249 0.0618 0.0226 0.037 0.785 0.898 27.855 0.089 3.993 14.619 0.18 96426. 0.5419
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2.60 0.0610 0.1623 0.0600 0.0225 0.037 0.781 0.871 27.725 0.088 3.874 14.247 0.18 96470. 0.5201
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3.25 0.0762 0.1975 0.0581 0.0224 0.037 0.777 0.843 27.565 0.088 3.750 13.873 0.18 96517. 0.4983
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3.90 0.0915 0.2306 0.0561 0.0222 0.037 0.771 0.815 27.375 0.087 3.623 13.496 0.18 96565. 0.4765
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4.55 0.1067 0.2615 0.0541 0.0221 0.036 0.765 0.785 27.151 0.086 3.492 13.116 0.18 96616. 0.4546
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5.20 0.1219 0.2901 0.0520 0.0219 0.036 0.758 0.755 26.891 0.086 3.358 12.733 0.18 96668. 0.4328
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5.85 0.1372 0.3164 0.0499 0.0216 0.036 0.749 0.724 26.595 0.085 3.220 12.346 0.18 96723. 0.4109
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6.50 0.1524 0.3404 0.0477 0.0213 0.035 0.740 0.692 26.259 0.084 3.078 11.954 0.18 96780. 0.3890
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7.15 0.1677 0.3620 0.0454 0.0210 0.035 0.729 0.659 25.881 0.082 2.933 11.555 0.18 96840. 0.3670
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7.80 0.1829 0.3810 0.0431 0.0207 0.034 0.717 0.626 25.460 0.081 2.784 11.150 0.18 96901. 0.3451
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8.44 0.1982 0.3975 0.0407 0.0203 0.034 0.704 0.592 24.992 0.080 2.631 10.737 0.18 96965. 0.3230
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9.09 0.2134 0.4112 0.0383 0.0199 0.033 0.690 0.557 24.477 0.078 2.475 10.313 0.18 97032. 0.3010
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9.74 0.2287 0.4219 0.0359 0.0194 0.032 0.674 0.521 23.912 0.076 2.316 9.877 0.18 97101. 0.2788
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10.39 0.2439 0.4295 0.0333 0.0189 0.031 0.656 0.484 23.295 0.074 2.153 9.426 0.18 97172. 0.2566
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11.04 0.2591 0.4337 0.0308 0.0184 0.030 0.637 0.447 22.624 0.072 1.987 8.958 0.18 97246. 0.2342
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11.69 0.2744 0.4341 0.0282 0.0178 0.029 0.617 0.409 21.897 0.070 1.818 8.468 0.18 97323. 0.2118
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12.34 0.2896 0.4303 0.0255 0.0172 0.028 0.595 0.370 21.113 0.067 1.646 7.952 0.18 97402. 0.1892
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12.99 0.3049 0.4217 0.0228 0.0165 0.027 0.571 0.331 20.270 0.065 1.472 7.404 0.18 97484. 0.1666
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13.64 0.3201 0.4076 0.0200 0.0157 0.026 0.546 0.291 19.368 0.062 1.295 6.816 0.18 97569. 0.1438
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14.29 0.3354 0.3871 0.0173 0.0150 0.025 0.519 0.251 18.404 0.059 1.115 6.179 0.18 97657. 0.1210
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14.94 0.3506 0.3590 0.0145 0.0141 0.023 0.490 0.210 17.379 0.055 0.934 5.481 0.18 97747. 0.0982
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15.59 0.3658 0.3214 0.0116 0.0132 0.022 0.459 0.169 16.292 0.052 0.751 4.703 0.18 97839. 0.0756
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16.24 0.3811 0.2721 0.0088 0.0123 0.020 0.427 0.128 15.143 0.048 0.568 3.821 0.18 97934. 0.0534
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16.89 0.3963 0.2074 0.0059 0.0113 0.019 0.393 0.086 13.933 0.044 0.383 2.801 0.18 98029. 0.0321
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17.54 0.4116 0.1218 0.0030 0.0103 0.017 0.357 0.044 12.654 0.040 0.197 1.584 0.18 98121. 0.0130
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18.19 0.4268 -0.0045 -0.0001 0.0091 0.015 0.315 -0.001 11.186 0.036 -0.006 -0.057 0.18 98119. 0.0000
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18.84 0.4421
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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 0.0674 0.0218 0.085 1.342 1.739 63.503 0.152 7.736 12.423 0.24 128401. 0.6409
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0.86 0.0151 0.0456 0.0657 0.0217 0.085 1.339 1.696 63.380 0.151 7.544 12.138 0.24 128453. 0.6184
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1.71 0.0302 0.0890 0.0640 0.0217 0.085 1.335 1.651 63.199 0.151 7.346 11.852 0.24 128507. 0.5958
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2.57 0.0452 0.1303 0.0622 0.0216 0.084 1.330 1.605 62.958 0.150 7.141 11.566 0.24 128563. 0.5732
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3.43 0.0603 0.1695 0.0604 0.0215 0.084 1.324 1.558 62.651 0.150 6.929 11.279 0.24 128622. 0.5507
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4.28 0.0754 0.2064 0.0585 0.0214 0.084 1.316 1.509 62.274 0.149 6.712 10.991 0.24 128684. 0.5281
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5.14 0.0905 0.2412 0.0565 0.0212 0.083 1.306 1.459 61.824 0.148 6.488 10.701 0.24 128748. 0.5056
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6.00 0.1056 0.2737 0.0545 0.0210 0.082 1.295 1.407 61.295 0.146 6.258 10.411 0.24 128814. 0.4831
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6.85 0.1206 0.3040 0.0524 0.0208 0.081 1.282 1.354 60.683 0.145 6.021 10.118 0.24 128884. 0.4605
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7.71 0.1357 0.3321 0.0503 0.0206 0.080 1.267 1.299 59.982 0.143 5.778 9.824 0.24 128956. 0.4380
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8.57 0.1508 0.3578 0.0482 0.0203 0.079 1.251 1.243 59.189 0.141 5.529 9.526 0.24 129031. 0.4155
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9.42 0.1659 0.3811 0.0459 0.0200 0.078 1.232 1.186 58.297 0.139 5.274 9.224 0.24 129109. 0.3929
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10.28 0.1810 0.4020 0.0436 0.0196 0.077 1.211 1.127 57.303 0.137 5.012 8.919 0.24 129190. 0.3703
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11.14 0.1960 0.4203 0.0413 0.0193 0.075 1.188 1.066 56.200 0.134 4.744 8.607 0.24 129274. 0.3477
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12.00 0.2111 0.4359 0.0389 0.0189 0.074 1.162 1.005 54.985 0.131 4.470 8.289 0.24 129361. 0.3250
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12.85 0.2262 0.4486 0.0365 0.0184 0.072 1.134 0.942 53.652 0.128 4.189 7.963 0.24 129452. 0.3023
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13.71 0.2413 0.4583 0.0340 0.0179 0.070 1.103 0.878 52.197 0.125 3.904 7.626 0.24 129545. 0.2795
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14.57 0.2564 0.4647 0.0315 0.0174 0.068 1.070 0.812 50.615 0.121 3.612 7.277 0.24 129643. 0.2565
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15.42 0.2714 0.4674 0.0289 0.0168 0.066 1.033 0.745 48.901 0.117 3.315 6.913 0.24 129743. 0.2334
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16.28 0.2865 0.4660 0.0262 0.0161 0.063 0.994 0.677 47.053 0.112 3.013 6.529 0.24 129847. 0.2102
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17.14 0.3016 0.4600 0.0236 0.0155 0.060 0.952 0.608 45.066 0.108 2.706 6.123 0.24 129955. 0.1868
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17.99 0.3167 0.4486 0.0209 0.0147 0.058 0.907 0.538 42.938 0.103 2.395 5.687 0.24 130066. 0.1632
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18.85 0.3317 0.4309 0.0181 0.0139 0.055 0.859 0.467 40.666 0.097 2.079 5.214 0.24 130180. 0.1395
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19.71 0.3468 0.4055 0.0153 0.0131 0.051 0.808 0.396 38.249 0.091 1.761 4.694 0.24 130299. 0.1155
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20.56 0.3619 0.3708 0.0125 0.0122 0.048 0.754 0.324 35.686 0.085 1.439 4.113 0.24 130420. 0.0915
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21.42 0.3770 0.3240 0.0097 0.0113 0.044 0.697 0.251 32.978 0.079 1.116 3.451 0.24 130544. 0.0676
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22.28 0.3921 0.2615 0.0069 0.0103 0.040 0.637 0.178 30.124 0.072 0.791 2.677 0.24 130670. 0.0442
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23.13 0.4071 0.1769 0.0040 0.0093 0.036 0.573 0.104 27.117 0.065 0.464 1.744 0.24 130794. 0.0220
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23.99 0.4222 0.0573 0.0011 0.0082 0.032 0.504 0.029 23.875 0.057 0.128 0.545 0.24 130884. 0.0036
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24.85 0.4373
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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 0.0678 0.0211 0.161 2.035 2.733 120.397 0.230 12.156 10.296 0.30 160497. 0.6658
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1.07 0.0151 0.0472 0.0661 0.0211 0.161 2.031 2.665 120.149 0.229 11.855 10.061 0.30 160562. 0.6425
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2.14 0.0302 0.0923 0.0643 0.0210 0.161 2.025 2.595 119.787 0.229 11.543 9.826 0.30 160630. 0.6192
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3.21 0.0452 0.1351 0.0625 0.0209 0.160 2.017 2.523 119.304 0.228 11.221 9.591 0.30 160701. 0.5959
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4.28 0.0603 0.1757 0.0607 0.0208 0.159 2.006 2.448 118.691 0.227 10.889 9.355 0.30 160774. 0.5726
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5.36 0.0754 0.2141 0.0588 0.0207 0.158 1.994 2.371 117.939 0.225 10.548 9.120 0.30 160851. 0.5493
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6.43 0.0905 0.2503 0.0568 0.0205 0.157 1.979 2.292 117.041 0.224 10.196 8.883 0.30 160932. 0.5261
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7.50 0.1056 0.2842 0.0548 0.0204 0.156 1.961 2.211 115.986 0.222 9.835 8.647 0.30 161015. 0.5029
|
|
8.57 0.1206 0.3159 0.0528 0.0201 0.154 1.940 2.128 114.766 0.219 9.464 8.409 0.30 161102. 0.4798
|
|
9.64 0.1357 0.3452 0.0506 0.0199 0.152 1.916 2.042 113.371 0.217 9.082 8.169 0.30 161192. 0.4566
|
|
10.71 0.1508 0.3723 0.0484 0.0196 0.150 1.890 1.954 111.791 0.214 8.691 7.928 0.30 161286. 0.4335
|
|
11.78 0.1659 0.3969 0.0462 0.0193 0.148 1.860 1.864 110.017 0.210 8.290 7.684 0.30 161384. 0.4103
|
|
12.85 0.1810 0.4190 0.0439 0.0190 0.145 1.826 1.771 108.038 0.206 7.879 7.437 0.30 161485. 0.3872
|
|
13.92 0.1961 0.4386 0.0416 0.0186 0.142 1.789 1.677 105.845 0.202 7.458 7.185 0.30 161591. 0.3640
|
|
15.00 0.2111 0.4555 0.0392 0.0182 0.139 1.748 1.580 103.428 0.198 7.028 6.929 0.30 161700. 0.3407
|
|
16.07 0.2262 0.4696 0.0367 0.0177 0.135 1.704 1.481 100.778 0.192 6.589 6.667 0.30 161813. 0.3174
|
|
17.14 0.2413 0.4806 0.0342 0.0172 0.131 1.655 1.380 97.885 0.187 6.140 6.396 0.30 161931. 0.2940
|
|
18.21 0.2564 0.4883 0.0317 0.0166 0.127 1.602 1.278 94.741 0.181 5.683 6.116 0.30 162052. 0.2704
|
|
19.28 0.2715 0.4923 0.0291 0.0160 0.122 1.544 1.173 91.336 0.174 5.217 5.824 0.30 162178. 0.2467
|
|
20.35 0.2865 0.4922 0.0264 0.0154 0.118 1.482 1.066 87.663 0.167 4.743 5.517 0.30 162308. 0.2229
|
|
21.42 0.3016 0.4875 0.0238 0.0147 0.112 1.415 0.958 83.716 0.160 4.261 5.191 0.30 162443. 0.1987
|
|
22.49 0.3167 0.4773 0.0210 0.0140 0.107 1.344 0.848 79.489 0.152 3.773 4.840 0.30 162582. 0.1744
|
|
23.56 0.3318 0.4606 0.0183 0.0132 0.101 1.267 0.737 74.976 0.143 3.279 4.459 0.30 162725. 0.1498
|
|
24.64 0.3469 0.4361 0.0155 0.0123 0.094 1.186 0.625 70.176 0.134 2.779 4.038 0.30 162873. 0.1248
|
|
25.71 0.3619 0.4016 0.0127 0.0114 0.087 1.100 0.511 65.089 0.124 2.275 3.564 0.30 163025. 0.0997
|
|
26.78 0.3770 0.3543 0.0099 0.0105 0.080 1.009 0.397 59.713 0.114 1.767 3.018 0.30 163180. 0.0744
|
|
27.85 0.3921 0.2897 0.0070 0.0095 0.072 0.914 0.283 54.050 0.103 1.258 2.373 0.30 163338. 0.0494
|
|
28.92 0.4072 0.2003 0.0042 0.0084 0.064 0.813 0.167 48.083 0.092 0.745 1.580 0.30 163492. 0.0253
|
|
29.99 0.4223 0.0700 0.0012 0.0073 0.056 0.704 0.049 41.653 0.080 0.218 0.533 0.30 163606. 0.0046
|
|
31.06 0.4373
|
|
|
|
|
|
|
|
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 0.0682 0.0207 0.274 2.876 3.962 204.177 0.325 17.623 8.802 0.36 192590. 0.6853
|
|
1.26 0.0148 0.0475 0.0666 0.0207 0.273 2.870 3.866 203.739 0.324 17.195 8.606 0.36 192666. 0.6619
|
|
2.52 0.0295 0.0928 0.0648 0.0206 0.272 2.861 3.766 203.109 0.323 16.753 8.411 0.36 192746. 0.6385
|
|
3.77 0.0443 0.1359 0.0631 0.0206 0.271 2.849 3.664 202.276 0.322 16.298 8.216 0.36 192830. 0.6152
|
|
5.03 0.0590 0.1769 0.0613 0.0204 0.270 2.835 3.559 201.226 0.320 15.828 8.021 0.36 192916. 0.5919
|
|
6.29 0.0738 0.2158 0.0594 0.0203 0.268 2.817 3.450 199.945 0.318 15.345 7.826 0.36 193007. 0.5686
|
|
7.55 0.0886 0.2525 0.0575 0.0202 0.266 2.795 3.338 198.417 0.316 14.849 7.631 0.36 193101. 0.5454
|
|
8.81 0.1033 0.2871 0.0555 0.0200 0.264 2.770 3.224 196.630 0.313 14.338 7.436 0.36 193199. 0.5222
|
|
10.06 0.1181 0.3194 0.0535 0.0198 0.261 2.741 3.106 194.566 0.310 13.814 7.240 0.36 193300. 0.4991
|
|
11.32 0.1328 0.3496 0.0514 0.0195 0.258 2.708 2.985 192.212 0.306 13.276 7.043 0.36 193406. 0.4760
|
|
12.58 0.1476 0.3775 0.0493 0.0193 0.254 2.670 2.861 189.550 0.302 12.724 6.845 0.36 193516. 0.4529
|
|
13.84 0.1624 0.4032 0.0471 0.0190 0.250 2.628 2.734 186.565 0.297 12.159 6.646 0.36 193630. 0.4298
|
|
15.10 0.1771 0.4265 0.0448 0.0186 0.246 2.581 2.603 183.242 0.292 11.580 6.444 0.36 193748. 0.4067
|
|
16.35 0.1919 0.4473 0.0425 0.0182 0.241 2.530 2.470 179.563 0.286 10.987 6.240 0.36 193871. 0.3836
|
|
17.61 0.2066 0.4657 0.0402 0.0178 0.235 2.472 2.334 175.514 0.279 10.382 6.032 0.36 193998. 0.3605
|
|
18.87 0.2214 0.4814 0.0378 0.0174 0.229 2.410 2.195 171.077 0.272 9.763 5.819 0.36 194130. 0.3372
|
|
20.13 0.2362 0.4942 0.0353 0.0169 0.223 2.342 2.053 166.239 0.265 9.131 5.601 0.36 194266. 0.3139
|
|
21.39 0.2509 0.5040 0.0329 0.0164 0.216 2.268 1.908 160.984 0.256 8.488 5.376 0.36 194408. 0.2905
|
|
22.64 0.2657 0.5105 0.0303 0.0158 0.208 2.188 1.761 155.298 0.247 7.832 5.143 0.36 194554. 0.2669
|
|
23.90 0.2804 0.5132 0.0277 0.0152 0.200 2.101 1.611 149.168 0.237 7.165 4.898 0.36 194705. 0.2432
|
|
25.16 0.2952 0.5117 0.0251 0.0145 0.191 2.009 1.458 142.583 0.227 6.487 4.639 0.36 194861. 0.2192
|
|
26.42 0.3100 0.5053 0.0224 0.0138 0.182 1.909 1.304 135.531 0.216 5.799 4.363 0.36 195022. 0.1949
|
|
27.68 0.3247 0.4932 0.0198 0.0130 0.172 1.803 1.147 128.006 0.204 5.103 4.065 0.36 195189. 0.1703
|
|
28.93 0.3395 0.4740 0.0170 0.0122 0.161 1.690 0.989 120.001 0.191 4.398 3.737 0.36 195360. 0.1454
|
|
30.19 0.3542 0.4462 0.0143 0.0113 0.150 1.571 0.829 111.514 0.177 3.687 3.371 0.36 195536. 0.1201
|
|
31.45 0.3690 0.4072 0.0115 0.0104 0.138 1.445 0.668 102.545 0.163 2.970 2.954 0.36 195716. 0.0944
|
|
32.71 0.3838 0.3534 0.0087 0.0095 0.125 1.311 0.506 93.096 0.148 2.250 2.464 0.36 195900. 0.0686
|
|
33.97 0.3985 0.2787 0.0059 0.0084 0.112 1.171 0.343 83.160 0.132 1.526 1.871 0.36 196085. 0.0429
|
|
35.22 0.4133 0.1725 0.0031 0.0074 0.097 1.024 0.179 72.675 0.116 0.796 1.117 0.36 196260. 0.0185
|
|
36.48 0.4281
|
|
|
|
|
|
|
|
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 0.0688 0.0205 0.430 3.872 5.436 320.687 0.437 24.179 7.688 0.42 224679. 0.7012
|
|
1.47 0.0148 0.0486 0.0671 0.0205 0.429 3.863 5.303 319.944 0.436 23.590 7.518 0.42 224769. 0.6773
|
|
2.95 0.0296 0.0949 0.0654 0.0204 0.428 3.850 5.166 318.888 0.435 22.980 7.349 0.42 224863. 0.6534
|
|
4.42 0.0445 0.1391 0.0636 0.0203 0.426 3.834 5.025 317.501 0.433 22.353 7.179 0.42 224961. 0.6295
|
|
5.89 0.0593 0.1811 0.0617 0.0202 0.423 3.813 4.880 315.760 0.431 21.706 7.010 0.42 225063. 0.6057
|
|
7.37 0.0741 0.2210 0.0598 0.0201 0.421 3.787 4.730 313.643 0.428 21.041 6.841 0.42 225170. 0.5820
|
|
8.84 0.0889 0.2586 0.0579 0.0199 0.417 3.757 4.576 311.126 0.424 20.356 6.672 0.42 225280. 0.5583
|
|
10.32 0.1037 0.2941 0.0559 0.0197 0.413 3.721 4.418 308.185 0.420 19.653 6.503 0.42 225396. 0.5347
|
|
11.79 0.1186 0.3273 0.0538 0.0195 0.409 3.680 4.256 304.796 0.416 18.931 6.333 0.42 225515. 0.5111
|
|
13.26 0.1334 0.3584 0.0517 0.0193 0.404 3.634 4.089 300.933 0.411 18.189 6.163 0.42 225640. 0.4876
|
|
14.74 0.1482 0.3872 0.0496 0.0190 0.398 3.581 3.918 296.572 0.405 17.429 5.993 0.42 225769. 0.4640
|
|
16.21 0.1630 0.4136 0.0474 0.0187 0.391 3.522 3.743 291.686 0.398 16.650 5.821 0.42 225903. 0.4405
|
|
17.68 0.1778 0.4378 0.0451 0.0183 0.384 3.456 3.564 286.249 0.390 15.852 5.647 0.42 226042. 0.4170
|
|
19.16 0.1927 0.4595 0.0428 0.0179 0.376 3.384 3.380 280.235 0.382 15.036 5.471 0.42 226187. 0.3935
|
|
20.63 0.2075 0.4787 0.0404 0.0175 0.367 3.304 3.193 273.619 0.373 14.201 5.292 0.42 226336. 0.3699
|
|
22.10 0.2223 0.4952 0.0380 0.0170 0.357 3.216 3.001 266.375 0.363 13.349 5.110 0.42 226491. 0.3463
|
|
23.58 0.2371 0.5089 0.0355 0.0165 0.347 3.121 2.805 258.479 0.353 12.479 4.923 0.42 226652. 0.3226
|
|
25.05 0.2520 0.5195 0.0330 0.0160 0.335 3.018 2.606 249.907 0.341 11.592 4.730 0.42 226818. 0.2987
|
|
26.53 0.2668 0.5267 0.0304 0.0154 0.323 2.906 2.403 240.635 0.328 10.689 4.529 0.42 226990. 0.2747
|
|
28.00 0.2816 0.5302 0.0278 0.0148 0.309 2.785 2.196 230.644 0.315 9.770 4.319 0.42 227168. 0.2504
|
|
29.47 0.2964 0.5294 0.0251 0.0141 0.295 2.655 1.987 219.914 0.300 8.836 4.097 0.42 227352. 0.2259
|
|
30.95 0.3112 0.5236 0.0224 0.0133 0.280 2.517 1.774 208.429 0.284 7.889 3.860 0.42 227541. 0.2011
|
|
32.42 0.3261 0.5119 0.0197 0.0126 0.263 2.369 1.558 196.176 0.268 6.929 3.602 0.42 227736. 0.1759
|
|
33.89 0.3409 0.4930 0.0169 0.0117 0.246 2.211 1.340 183.147 0.250 5.959 3.318 0.42 227938. 0.1502
|
|
35.37 0.3557 0.4650 0.0142 0.0108 0.227 2.045 1.120 169.339 0.231 4.980 2.999 0.42 228145. 0.1241
|
|
36.84 0.3705 0.4250 0.0114 0.0099 0.208 1.869 0.898 154.752 0.211 3.994 2.632 0.42 228357. 0.0975
|
|
38.31 0.3853 0.3689 0.0085 0.0089 0.187 1.683 0.675 139.389 0.190 3.002 2.196 0.42 228573. 0.0706
|
|
39.79 0.4002 0.2896 0.0057 0.0079 0.165 1.488 0.451 123.237 0.168 2.006 1.660 0.42 228789. 0.0436
|
|
41.26 0.4150 0.1737 0.0028 0.0068 0.142 1.282 0.225 106.171 0.145 1.000 0.960 0.42 228990. 0.0178
|
|
42.74 0.4298
|
|
|
|
|
|
|
|
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 0.0694 0.0204 0.639 5.033 7.167 476.391 0.569 31.879 6.824 0.48 256763. 0.7146
|
|
1.73 0.0152 0.0506 0.0677 0.0204 0.637 5.020 6.987 475.157 0.567 31.079 6.670 0.48 256869. 0.6897
|
|
3.46 0.0305 0.0989 0.0659 0.0203 0.635 5.002 6.801 473.418 0.565 30.252 6.516 0.48 256981. 0.6647
|
|
5.19 0.0457 0.1449 0.0640 0.0202 0.632 4.978 6.610 471.147 0.562 29.399 6.363 0.48 257097. 0.6399
|
|
6.92 0.0609 0.1885 0.0621 0.0201 0.628 4.948 6.412 468.305 0.559 28.521 6.210 0.48 257218. 0.6151
|
|
8.66 0.0762 0.2299 0.0601 0.0199 0.623 4.911 6.209 464.855 0.555 27.616 6.058 0.48 257344. 0.5905
|
|
10.39 0.0914 0.2689 0.0581 0.0197 0.618 4.868 5.999 460.760 0.550 26.685 5.906 0.48 257476. 0.5658
|
|
12.12 0.1066 0.3056 0.0560 0.0195 0.611 4.818 5.784 455.981 0.544 25.727 5.753 0.48 257613. 0.5413
|
|
13.85 0.1219 0.3401 0.0539 0.0193 0.604 4.759 5.563 450.476 0.538 24.743 5.601 0.48 257755. 0.5168
|
|
15.58 0.1371 0.3721 0.0517 0.0190 0.596 4.693 5.336 444.207 0.530 23.733 5.448 0.48 257903. 0.4923
|
|
17.31 0.1523 0.4018 0.0494 0.0187 0.586 4.618 5.103 437.129 0.522 22.697 5.295 0.48 258057. 0.4679
|
|
19.04 0.1676 0.4291 0.0471 0.0184 0.576 4.535 4.864 429.202 0.512 21.635 5.140 0.48 258217. 0.4434
|
|
20.77 0.1828 0.4539 0.0447 0.0180 0.564 4.441 4.619 420.383 0.502 20.546 4.984 0.48 258383. 0.4190
|
|
22.50 0.1980 0.4761 0.0423 0.0176 0.551 4.338 4.369 410.630 0.490 19.433 4.826 0.48 258555. 0.3946
|
|
24.24 0.2133 0.4956 0.0398 0.0171 0.536 4.225 4.113 399.902 0.477 18.294 4.665 0.48 258734. 0.3701
|
|
25.97 0.2285 0.5123 0.0373 0.0166 0.521 4.101 3.851 388.156 0.463 17.130 4.500 0.48 258919. 0.3455
|
|
27.70 0.2437 0.5259 0.0347 0.0161 0.503 3.966 3.584 375.355 0.448 15.943 4.331 0.48 259111. 0.3207
|
|
29.43 0.2590 0.5362 0.0321 0.0155 0.485 3.819 3.312 361.460 0.431 14.732 4.156 0.48 259310. 0.2959
|
|
31.16 0.2742 0.5428 0.0294 0.0148 0.465 3.660 3.035 346.434 0.414 13.499 3.973 0.48 259516. 0.2708
|
|
32.89 0.2894 0.5452 0.0267 0.0142 0.443 3.489 2.753 330.246 0.394 12.245 3.781 0.48 259728. 0.2454
|
|
34.62 0.3047 0.5427 0.0239 0.0134 0.420 3.306 2.467 312.868 0.373 10.971 3.576 0.48 259948. 0.2197
|
|
36.35 0.3199 0.5346 0.0211 0.0126 0.395 3.109 2.176 294.274 0.351 9.680 3.354 0.48 260175. 0.1936
|
|
38.08 0.3351 0.5194 0.0182 0.0118 0.368 2.900 1.882 274.450 0.328 8.372 3.111 0.48 260409. 0.1669
|
|
39.82 0.3504 0.4953 0.0154 0.0109 0.340 2.677 1.585 253.386 0.302 7.051 2.838 0.48 260650. 0.1398
|
|
41.55 0.3656 0.4597 0.0125 0.0099 0.310 2.441 1.286 231.082 0.276 5.719 2.524 0.48 260897. 0.1119
|
|
43.28 0.3808 0.4082 0.0095 0.0089 0.278 2.193 0.985 207.543 0.248 4.379 2.152 0.48 261150. 0.0835
|
|
45.01 0.3961 0.3339 0.0066 0.0078 0.245 1.931 0.682 182.763 0.218 3.033 1.692 0.48 261405. 0.0547
|
|
46.74 0.4113 0.2237 0.0037 0.0067 0.210 1.655 0.377 156.630 0.187 1.677 1.092 0.48 261650. 0.0262
|
|
48.47 0.4265 0.0389 0.0005 0.0055 0.171 1.345 0.051 127.310 0.152 0.228 0.183 0.48 261706. 0.0016
|
|
50.20 0.4418
|
|
|
|
|
|
|
|
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 0.0702 0.0204 0.910 6.373 9.170 678.609 0.720 40.790 6.129 0.54 288840. 0.7261
|
|
1.90 0.0148 0.0499 0.0685 0.0204 0.908 6.356 8.946 676.752 0.718 39.793 5.996 0.54 288958. 0.7015
|
|
3.80 0.0297 0.0976 0.0667 0.0203 0.904 6.332 8.715 674.203 0.715 38.763 5.863 0.54 289081. 0.6770
|
|
5.69 0.0445 0.1430 0.0649 0.0202 0.900 6.301 8.476 670.919 0.712 37.701 5.730 0.54 289209. 0.6526
|
|
7.59 0.0594 0.1863 0.0630 0.0201 0.894 6.263 8.230 666.854 0.708 36.608 5.598 0.54 289342. 0.6282
|
|
9.49 0.0742 0.2274 0.0610 0.0199 0.888 6.217 7.977 661.960 0.702 35.484 5.466 0.54 289481. 0.6039
|
|
11.39 0.0891 0.2663 0.0591 0.0198 0.880 6.162 7.717 656.184 0.696 34.327 5.334 0.54 289625. 0.5797
|
|
13.28 0.1039 0.3030 0.0570 0.0196 0.871 6.099 7.450 649.478 0.689 33.139 5.203 0.54 289775. 0.5555
|
|
15.18 0.1188 0.3376 0.0549 0.0193 0.861 6.027 7.176 641.786 0.681 31.919 5.072 0.54 289931. 0.5314
|
|
17.08 0.1336 0.3699 0.0528 0.0191 0.849 5.945 6.895 633.056 0.672 30.667 4.940 0.54 290092. 0.5074
|
|
18.98 0.1484 0.4000 0.0506 0.0188 0.836 5.853 6.606 623.233 0.661 29.384 4.808 0.54 290260. 0.4834
|
|
20.88 0.1633 0.4278 0.0483 0.0184 0.821 5.750 6.310 612.260 0.650 28.069 4.675 0.54 290435. 0.4594
|
|
22.77 0.1781 0.4534 0.0460 0.0181 0.805 5.636 6.008 600.081 0.637 26.723 4.541 0.54 290615. 0.4354
|
|
24.67 0.1930 0.4765 0.0436 0.0177 0.787 5.509 5.698 586.644 0.622 25.345 4.406 0.54 290803. 0.4114
|
|
26.57 0.2078 0.4971 0.0412 0.0172 0.767 5.371 5.382 571.889 0.607 23.937 4.268 0.54 290997. 0.3873
|
|
28.47 0.2227 0.5152 0.0387 0.0167 0.745 5.219 5.058 555.766 0.590 22.499 4.128 0.54 291198. 0.3632
|
|
30.36 0.2375 0.5304 0.0362 0.0162 0.722 5.055 4.728 538.218 0.571 21.032 3.985 0.54 291406. 0.3389
|
|
32.26 0.2524 0.5427 0.0336 0.0156 0.696 4.876 4.392 519.196 0.551 19.536 3.837 0.54 291621. 0.3146
|
|
34.16 0.2672 0.5516 0.0310 0.0150 0.669 4.683 4.050 498.651 0.529 18.013 3.684 0.54 291844. 0.2900
|
|
36.06 0.2821 0.5569 0.0283 0.0143 0.639 4.475 3.701 476.538 0.506 16.464 3.523 0.54 292074. 0.2651
|
|
37.96 0.2969 0.5579 0.0256 0.0136 0.607 4.253 3.347 452.816 0.480 14.890 3.353 0.54 292312. 0.2400
|
|
39.85 0.3117 0.5540 0.0229 0.0129 0.573 4.014 2.988 427.452 0.454 13.293 3.171 0.54 292557. 0.2144
|
|
41.75 0.3266 0.5442 0.0201 0.0121 0.537 3.760 2.625 400.419 0.425 11.675 2.973 0.54 292809. 0.1884
|
|
43.65 0.3414 0.5270 0.0173 0.0112 0.498 3.491 2.257 371.699 0.394 10.039 2.754 0.54 293069. 0.1619
|
|
45.55 0.3563 0.5005 0.0144 0.0103 0.458 3.205 1.886 341.286 0.362 8.389 2.506 0.54 293337. 0.1346
|
|
47.44 0.3711 0.4614 0.0116 0.0093 0.415 2.904 1.512 309.184 0.328 6.726 2.218 0.54 293610. 0.1067
|
|
49.34 0.3860 0.4049 0.0087 0.0083 0.369 2.586 1.136 275.400 0.292 5.055 1.872 0.54 293889. 0.0780
|
|
51.24 0.4008 0.3223 0.0058 0.0072 0.322 2.253 0.759 239.905 0.255 3.376 1.435 0.54 294169. 0.0489
|
|
53.14 0.4157 0.1970 0.0029 0.0061 0.271 1.901 0.377 202.413 0.215 1.679 0.846 0.54 294425. 0.0203
|
|
55.04 0.4305
|
|
|
|
|
|
|
|
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 0.0711 0.0205 1.255 7.910 11.467 935.847 0.894 51.003 5.557 0.59 320911. 0.7361
|
|
2.13 0.0150 0.0507 0.0693 0.0205 1.251 7.886 11.184 933.017 0.891 49.745 5.437 0.60 321044. 0.7112
|
|
4.25 0.0299 0.0991 0.0675 0.0204 1.246 7.854 10.891 929.199 0.887 48.445 5.316 0.60 321183. 0.6863
|
|
6.38 0.0449 0.1453 0.0656 0.0203 1.240 7.813 10.590 924.334 0.883 47.105 5.197 0.60 321327. 0.6615
|
|
8.50 0.0599 0.1893 0.0637 0.0202 1.232 7.762 10.280 918.356 0.877 45.725 5.077 0.60 321478. 0.6368
|
|
10.63 0.0748 0.2311 0.0617 0.0200 1.222 7.702 9.961 911.197 0.870 44.306 4.958 0.60 321635. 0.6121
|
|
12.76 0.0898 0.2706 0.0597 0.0198 1.211 7.631 9.633 902.786 0.862 42.846 4.840 0.60 321798. 0.5876
|
|
14.88 0.1048 0.3080 0.0576 0.0196 1.198 7.548 9.296 893.049 0.853 41.347 4.721 0.60 321967. 0.5631
|
|
17.01 0.1197 0.3432 0.0555 0.0194 1.183 7.454 8.949 881.913 0.842 39.807 4.603 0.60 322143. 0.5386
|
|
19.13 0.1347 0.3761 0.0533 0.0191 1.166 7.348 8.594 869.301 0.830 38.227 4.484 0.60 322325. 0.5142
|
|
21.26 0.1497 0.4068 0.0510 0.0188 1.147 7.228 8.230 855.137 0.817 36.606 4.365 0.60 322515. 0.4899
|
|
23.39 0.1646 0.4353 0.0487 0.0184 1.126 7.094 7.857 839.340 0.802 34.946 4.246 0.60 322712. 0.4655
|
|
25.51 0.1796 0.4614 0.0463 0.0180 1.102 6.946 7.475 821.835 0.785 33.247 4.125 0.60 322916. 0.4412
|
|
27.64 0.1946 0.4851 0.0439 0.0176 1.076 6.783 7.084 802.542 0.766 31.508 4.003 0.60 323128. 0.4168
|
|
29.76 0.2095 0.5063 0.0414 0.0171 1.048 6.604 6.684 781.384 0.746 29.731 3.880 0.60 323347. 0.3924
|
|
31.89 0.2245 0.5248 0.0389 0.0166 1.017 6.409 6.276 758.284 0.724 27.916 3.754 0.60 323574. 0.3679
|
|
34.02 0.2395 0.5406 0.0363 0.0161 0.983 6.197 5.860 733.167 0.700 26.064 3.625 0.60 323809. 0.3433
|
|
36.14 0.2544 0.5533 0.0337 0.0155 0.947 5.967 5.435 705.962 0.674 24.176 3.492 0.60 324052. 0.3185
|
|
38.27 0.2694 0.5627 0.0310 0.0148 0.907 5.719 5.003 676.603 0.646 22.254 3.354 0.60 324303. 0.2935
|
|
40.39 0.2844 0.5683 0.0283 0.0142 0.865 5.452 4.563 645.025 0.616 20.298 3.209 0.60 324563. 0.2682
|
|
42.52 0.2993 0.5695 0.0255 0.0134 0.820 5.166 4.117 611.174 0.584 18.312 3.055 0.60 324831. 0.2425
|
|
44.65 0.3143 0.5657 0.0227 0.0126 0.771 4.860 3.664 575.003 0.549 16.297 2.890 0.60 325107. 0.2164
|
|
46.77 0.3293 0.5556 0.0199 0.0118 0.719 4.534 3.205 536.476 0.512 14.256 2.710 0.60 325392. 0.1898
|
|
48.90 0.3442 0.5378 0.0170 0.0109 0.665 4.189 2.741 495.573 0.473 12.193 2.509 0.60 325686. 0.1625
|
|
51.02 0.3592 0.5100 0.0141 0.0099 0.607 3.823 2.273 452.288 0.432 10.112 2.280 0.60 325987. 0.1345
|
|
53.15 0.3742 0.4684 0.0112 0.0089 0.545 3.437 1.802 406.629 0.388 8.016 2.010 0.60 326296. 0.1056
|
|
55.28 0.3891 0.4073 0.0082 0.0079 0.481 3.031 1.329 358.605 0.342 5.910 1.681 0.60 326609. 0.0758
|
|
57.40 0.4041 0.3159 0.0053 0.0068 0.413 2.605 0.853 308.149 0.294 3.794 1.255 0.60 326921. 0.0454
|
|
59.53 0.4191 0.1718 0.0023 0.0056 0.341 2.152 0.370 254.598 0.243 1.644 0.658 0.60 327190. 0.0157
|
|
61.65 0.4340
|
|
|
|
|
|
|
|
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 0.0721 0.0207 1.687 9.669 14.081 1258.297 1.092 62.633 5.076 0.65 352971. 0.7451
|
|
2.34 0.0150 0.0509 0.0704 0.0207 1.682 9.636 13.733 1254.109 1.089 61.086 4.967 0.65 353119. 0.7200
|
|
4.68 0.0299 0.0996 0.0685 0.0206 1.674 9.594 13.374 1248.572 1.084 59.488 4.858 0.65 353274. 0.6950
|
|
7.02 0.0449 0.1461 0.0666 0.0205 1.665 9.540 13.004 1241.612 1.078 57.842 4.750 0.65 353434. 0.6701
|
|
9.35 0.0599 0.1904 0.0647 0.0203 1.654 9.475 12.623 1233.135 1.071 56.147 4.643 0.65 353601. 0.6453
|
|
11.69 0.0748 0.2325 0.0627 0.0202 1.640 9.398 12.231 1223.055 1.062 54.403 4.536 0.65 353775. 0.6205
|
|
14.03 0.0898 0.2724 0.0606 0.0200 1.624 9.307 11.828 1211.270 1.052 52.611 4.429 0.65 353956. 0.5959
|
|
16.37 0.1048 0.3102 0.0585 0.0197 1.606 9.203 11.414 1197.695 1.040 50.769 4.322 0.65 354143. 0.5713
|
|
18.71 0.1197 0.3458 0.0563 0.0195 1.585 9.084 10.989 1182.220 1.026 48.879 4.216 0.65 354338. 0.5467
|
|
21.05 0.1347 0.3792 0.0541 0.0192 1.562 8.950 10.553 1164.749 1.011 46.940 4.109 0.66 354541. 0.5222
|
|
23.38 0.1497 0.4103 0.0518 0.0189 1.536 8.799 10.106 1145.181 0.994 44.951 4.003 0.66 354751. 0.4977
|
|
25.72 0.1646 0.4393 0.0494 0.0185 1.507 8.632 9.648 1123.407 0.975 42.915 3.895 0.66 354968. 0.4733
|
|
28.06 0.1796 0.4659 0.0470 0.0181 1.474 8.447 9.179 1099.326 0.954 40.830 3.787 0.66 355194. 0.4489
|
|
30.40 0.1946 0.4902 0.0446 0.0177 1.439 8.244 8.700 1072.835 0.931 38.697 3.678 0.66 355428. 0.4244
|
|
32.74 0.2095 0.5120 0.0421 0.0172 1.400 8.021 8.210 1043.827 0.906 36.517 3.567 0.66 355670. 0.3998
|
|
35.08 0.2245 0.5312 0.0395 0.0167 1.357 7.778 7.709 1012.203 0.879 34.291 3.455 0.66 355921. 0.3752
|
|
37.41 0.2395 0.5477 0.0369 0.0161 1.311 7.514 7.199 977.864 0.849 32.020 3.339 0.66 356181. 0.3504
|
|
39.75 0.2544 0.5612 0.0342 0.0155 1.262 7.228 6.678 940.714 0.817 29.705 3.220 0.66 356449. 0.3255
|
|
42.09 0.2694 0.5714 0.0315 0.0148 1.208 6.921 6.148 900.663 0.782 27.348 3.096 0.66 356726. 0.3003
|
|
44.43 0.2844 0.5778 0.0287 0.0141 1.150 6.590 5.609 857.628 0.745 24.951 2.967 0.66 357013. 0.2748
|
|
46.77 0.2993 0.5801 0.0259 0.0134 1.088 6.236 5.062 811.536 0.705 22.515 2.829 0.66 357308. 0.2490
|
|
49.11 0.3143 0.5772 0.0231 0.0126 1.022 5.858 4.507 762.325 0.662 20.045 2.681 0.66 357613. 0.2227
|
|
51.45 0.3293 0.5683 0.0202 0.0117 0.952 5.455 3.944 709.948 0.616 17.543 2.520 0.66 357927. 0.1958
|
|
53.78 0.3442 0.5517 0.0173 0.0108 0.878 5.028 3.375 654.377 0.568 15.014 2.340 0.66 358250. 0.1681
|
|
56.12 0.3592 0.5249 0.0144 0.0098 0.799 4.577 2.802 595.605 0.517 12.462 2.134 0.66 358582. 0.1397
|
|
58.46 0.3741 0.4845 0.0114 0.0088 0.716 4.100 2.224 533.647 0.463 9.893 1.890 0.66 358922. 0.1103
|
|
60.80 0.3891 0.4241 0.0084 0.0077 0.628 3.600 1.643 468.516 0.407 7.310 1.591 0.66 359268. 0.0798
|
|
63.14 0.4041 0.3326 0.0054 0.0066 0.537 3.075 1.060 400.128 0.347 4.715 1.202 0.66 359611. 0.0484
|
|
65.48 0.4190 0.1859 0.0024 0.0054 0.439 2.517 0.468 327.632 0.284 2.081 0.648 0.66 359909. 0.0173
|
|
67.81 0.4340
|
|
|
|
|
|
|
|
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 0.0734 0.0211 2.224 11.683 17.048 1658.678 1.320 75.832 4.662 0.71 385020. 0.7530
|
|
2.54 0.0149 0.0507 0.0716 0.0210 2.216 11.640 16.629 1652.596 1.315 73.967 4.564 0.71 385182. 0.7281
|
|
5.07 0.0298 0.0993 0.0697 0.0209 2.206 11.585 16.197 1644.735 1.309 72.042 4.467 0.71 385351. 0.7032
|
|
7.61 0.0446 0.1457 0.0678 0.0208 2.193 11.516 15.751 1634.998 1.301 70.060 4.369 0.71 385527. 0.6784
|
|
10.14 0.0595 0.1900 0.0658 0.0206 2.177 11.434 15.292 1623.274 1.292 68.019 4.273 0.71 385711. 0.6536
|
|
12.68 0.0744 0.2322 0.0638 0.0204 2.158 11.336 14.820 1609.440 1.281 65.921 4.177 0.71 385901. 0.6290
|
|
15.22 0.0893 0.2722 0.0617 0.0202 2.137 11.223 14.336 1593.386 1.268 63.765 4.081 0.71 386098. 0.6044
|
|
17.75 0.1042 0.3102 0.0596 0.0200 2.112 11.093 13.838 1574.982 1.253 61.551 3.985 0.71 386303. 0.5799
|
|
20.29 0.1190 0.3460 0.0574 0.0197 2.084 10.946 13.327 1554.103 1.237 59.278 3.890 0.71 386516. 0.5554
|
|
22.83 0.1339 0.3797 0.0551 0.0194 2.053 10.781 12.803 1530.622 1.218 56.948 3.794 0.71 386737. 0.5310
|
|
25.36 0.1488 0.4112 0.0528 0.0191 2.017 10.596 12.266 1504.406 1.197 54.559 3.698 0.71 386966. 0.5066
|
|
27.90 0.1637 0.4405 0.0504 0.0187 1.978 10.392 11.716 1475.325 1.174 52.113 3.602 0.71 387204. 0.4823
|
|
30.43 0.1786 0.4677 0.0480 0.0183 1.935 10.166 11.153 1443.244 1.148 49.609 3.505 0.72 387450. 0.4579
|
|
32.97 0.1934 0.4925 0.0455 0.0179 1.888 9.918 10.578 1408.031 1.120 47.049 3.407 0.72 387704. 0.4335
|
|
35.51 0.2083 0.5150 0.0430 0.0174 1.837 9.647 9.989 1369.554 1.090 44.433 3.308 0.72 387968. 0.4090
|
|
38.04 0.2232 0.5349 0.0404 0.0169 1.780 9.352 9.389 1327.685 1.057 41.761 3.207 0.72 388240. 0.3844
|
|
40.58 0.2381 0.5523 0.0378 0.0163 1.720 9.032 8.776 1282.296 1.020 39.037 3.104 0.72 388522. 0.3597
|
|
43.12 0.2529 0.5667 0.0351 0.0157 1.654 8.687 8.152 1233.268 0.981 36.259 2.998 0.72 388814. 0.3348
|
|
45.65 0.2678 0.5780 0.0324 0.0150 1.583 8.315 7.516 1180.488 0.939 33.432 2.888 0.72 389115. 0.3097
|
|
48.19 0.2827 0.5857 0.0296 0.0143 1.507 7.916 6.870 1123.857 0.894 30.556 2.772 0.72 389425. 0.2842
|
|
50.72 0.2976 0.5893 0.0267 0.0135 1.426 7.489 6.213 1063.287 0.846 27.634 2.650 0.72 389746. 0.2584
|
|
53.26 0.3125 0.5882 0.0239 0.0127 1.339 7.034 5.546 998.708 0.795 24.671 2.519 0.72 390076. 0.2321
|
|
55.80 0.3273 0.5811 0.0210 0.0118 1.247 6.551 4.872 930.071 0.740 21.669 2.376 0.72 390417. 0.2051
|
|
58.33 0.3422 0.5667 0.0180 0.0109 1.150 6.039 4.189 857.355 0.682 18.633 2.216 0.72 390767. 0.1774
|
|
60.87 0.3571 0.5428 0.0151 0.0099 1.047 5.498 3.500 780.569 0.621 15.570 2.034 0.72 391126. 0.1489
|
|
63.41 0.3720 0.5057 0.0121 0.0089 0.938 4.929 2.807 699.752 0.557 12.484 1.819 0.72 391495. 0.1192
|
|
65.94 0.3869 0.4497 0.0091 0.0078 0.825 4.331 2.109 614.960 0.489 9.382 1.556 0.72 391869. 0.0884
|
|
68.48 0.4017 0.3645 0.0061 0.0067 0.706 3.706 1.409 526.155 0.419 6.266 1.214 0.72 392244. 0.0564
|
|
71.01 0.4166 0.2286 0.0030 0.0055 0.580 3.047 0.700 432.637 0.344 3.115 0.734 0.72 392586. 0.0240
|
|
73.55 0.4315
|
|
|
|
|
|
|
|
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 0.0749 0.0215 2.889 14.007 20.415 2154.421 1.583 90.808 4.298 0.77 417052. 0.7597
|
|
2.82 0.0153 0.0520 0.0730 0.0214 2.877 13.947 19.899 2145.168 1.576 88.511 4.207 0.77 417235. 0.7342
|
|
5.64 0.0306 0.1018 0.0710 0.0213 2.861 13.871 19.366 2133.476 1.567 86.138 4.117 0.77 417427. 0.7087
|
|
8.46 0.0458 0.1494 0.0690 0.0212 2.842 13.779 18.816 2119.210 1.557 83.693 4.027 0.77 417626. 0.6833
|
|
11.28 0.0611 0.1948 0.0669 0.0210 2.819 13.668 18.250 2102.209 1.544 81.176 3.938 0.77 417833. 0.6580
|
|
14.11 0.0764 0.2380 0.0648 0.0208 2.792 13.539 17.668 2082.316 1.530 78.587 3.848 0.77 418048. 0.6328
|
|
16.93 0.0917 0.2790 0.0626 0.0206 2.762 13.389 17.069 2059.359 1.513 75.924 3.759 0.77 418271. 0.6076
|
|
19.75 0.1069 0.3178 0.0603 0.0203 2.727 13.219 16.454 2033.178 1.493 73.189 3.671 0.77 418504. 0.5825
|
|
22.57 0.1222 0.3544 0.0580 0.0200 2.687 13.027 15.823 2003.600 1.472 70.381 3.582 0.77 418745. 0.5574
|
|
25.39 0.1375 0.3888 0.0557 0.0197 2.642 12.811 15.175 1970.467 1.447 67.500 3.493 0.77 418995. 0.5323
|
|
28.21 0.1528 0.4210 0.0532 0.0193 2.593 12.572 14.511 1933.597 1.420 64.547 3.404 0.77 419254. 0.5072
|
|
31.03 0.1681 0.4509 0.0507 0.0189 2.538 12.307 13.831 1892.824 1.390 61.522 3.314 0.77 419523. 0.4822
|
|
33.85 0.1833 0.4785 0.0482 0.0185 2.478 12.015 13.135 1847.986 1.357 58.425 3.224 0.77 419802. 0.4571
|
|
36.68 0.1986 0.5036 0.0456 0.0180 2.412 11.696 12.423 1798.919 1.321 55.258 3.132 0.78 420090. 0.4319
|
|
39.50 0.2139 0.5262 0.0429 0.0174 2.341 11.349 11.695 1745.472 1.282 52.021 3.039 0.78 420389. 0.4066
|
|
42.32 0.2292 0.5461 0.0402 0.0169 2.263 10.972 10.952 1687.493 1.240 48.716 2.944 0.78 420699. 0.3811
|
|
45.14 0.2444 0.5631 0.0374 0.0162 2.179 10.564 10.194 1624.845 1.194 45.344 2.846 0.78 421018. 0.3554
|
|
47.96 0.2597 0.5769 0.0346 0.0156 2.089 10.126 9.422 1557.413 1.144 41.907 2.744 0.78 421349. 0.3295
|
|
50.78 0.2750 0.5871 0.0317 0.0148 1.992 9.656 8.635 1485.087 1.091 38.408 2.637 0.78 421690. 0.3031
|
|
53.60 0.2903 0.5932 0.0287 0.0141 1.888 9.153 7.835 1407.788 1.034 34.850 2.524 0.78 422043. 0.2764
|
|
56.42 0.3056 0.5944 0.0258 0.0132 1.777 8.618 7.022 1325.459 0.974 31.236 2.403 0.78 422407. 0.2491
|
|
59.24 0.3208 0.5898 0.0227 0.0124 1.660 8.050 6.199 1238.077 0.909 27.571 2.271 0.78 422781. 0.2212
|
|
62.07 0.3361 0.5779 0.0197 0.0114 1.536 7.449 5.364 1145.664 0.842 23.861 2.124 0.78 423167. 0.1924
|
|
64.89 0.3514 0.5565 0.0166 0.0105 1.406 6.816 4.522 1048.285 0.770 20.112 1.956 0.78 423564. 0.1627
|
|
67.71 0.3667 0.5225 0.0135 0.0094 1.269 6.151 3.672 946.056 0.695 16.332 1.760 0.78 423972. 0.1320
|
|
70.53 0.3819 0.4707 0.0103 0.0084 1.125 5.456 2.817 839.130 0.616 12.529 1.522 0.78 424387. 0.1000
|
|
73.35 0.3972 0.3923 0.0072 0.0073 0.976 4.731 1.957 727.602 0.534 8.706 1.220 0.78 424806. 0.0668
|
|
76.17 0.4125 0.2705 0.0040 0.0061 0.819 3.973 1.091 611.032 0.449 4.855 0.810 0.78 425208. 0.0331
|
|
78.99 0.4278 0.0540 0.0006 0.0048 0.643 3.119 0.165 479.681 0.352 0.734 0.156 0.78 425271. 0.0025
|
|
81.81 0.4431
|
|
|
|
|
|
|
|
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 0.0767 0.0223 3.746 16.863 24.247 2793.111 1.905 107.852 3.937 0.83 449062. 0.7584
|
|
2.99 0.0150 0.0506 0.0748 0.0222 3.723 16.763 23.645 2776.491 1.894 105.171 3.863 0.83 449260. 0.7347
|
|
5.97 0.0300 0.0991 0.0728 0.0221 3.697 16.646 23.022 2757.127 1.881 102.402 3.787 0.83 449465. 0.7108
|
|
8.96 0.0450 0.1458 0.0708 0.0219 3.668 16.511 22.381 2734.867 1.865 99.551 3.712 0.83 449679. 0.6869
|
|
11.94 0.0601 0.1904 0.0687 0.0217 3.634 16.358 21.721 2709.523 1.848 96.617 3.636 0.83 449901. 0.6629
|
|
14.93 0.0751 0.2330 0.0665 0.0214 3.595 16.185 21.043 2680.897 1.829 93.601 3.560 0.83 450131. 0.6389
|
|
17.91 0.0901 0.2736 0.0643 0.0212 3.552 15.993 20.347 2649.039 1.807 90.502 3.484 0.83 450370. 0.6147
|
|
20.90 0.1051 0.3121 0.0621 0.0209 3.506 15.783 19.631 2614.271 1.783 87.321 3.406 0.83 450618. 0.5903
|
|
23.89 0.1201 0.3484 0.0598 0.0206 3.455 15.552 18.898 2576.046 1.757 84.056 3.327 0.83 450875. 0.5658
|
|
26.87 0.1351 0.3826 0.0574 0.0203 3.398 15.300 18.145 2534.215 1.729 80.709 3.248 0.83 451142. 0.5411
|
|
29.86 0.1501 0.4145 0.0549 0.0199 3.337 15.025 17.374 2488.705 1.698 77.279 3.166 0.83 451418. 0.5163
|
|
32.84 0.1652 0.4441 0.0524 0.0195 3.271 14.725 16.584 2438.976 1.664 73.767 3.084 0.83 451703. 0.4913
|
|
35.83 0.1802 0.4713 0.0499 0.0191 3.198 14.397 15.777 2384.716 1.627 70.175 3.001 0.83 451999. 0.4662
|
|
38.81 0.1952 0.4961 0.0473 0.0186 3.119 14.042 14.951 2325.796 1.586 66.501 2.916 0.83 452305. 0.4410
|
|
41.80 0.2102 0.5183 0.0446 0.0181 3.034 13.658 14.107 2262.191 1.543 62.749 2.828 0.83 452622. 0.4156
|
|
44.79 0.2252 0.5377 0.0419 0.0175 2.942 13.245 13.246 2193.794 1.496 58.918 2.739 0.84 452949. 0.3899
|
|
47.77 0.2402 0.5540 0.0391 0.0170 2.844 12.802 12.367 2120.434 1.446 55.010 2.645 0.84 453286. 0.3639
|
|
50.76 0.2552 0.5670 0.0363 0.0163 2.738 12.329 11.472 2042.051 1.393 51.029 2.548 0.84 453635. 0.3376
|
|
53.74 0.2702 0.5762 0.0334 0.0157 2.627 11.825 10.561 1958.632 1.336 46.975 2.446 0.84 453995. 0.3109
|
|
56.73 0.2853 0.5811 0.0305 0.0150 2.508 11.291 9.634 1870.199 1.276 42.853 2.337 0.84 454367. 0.2837
|
|
59.71 0.3003 0.5809 0.0275 0.0142 2.383 10.727 8.693 1776.729 1.212 38.666 2.219 0.84 454749. 0.2559
|
|
62.70 0.3153 0.5748 0.0245 0.0134 2.251 10.132 7.738 1678.295 1.145 34.418 2.091 0.84 455144. 0.2276
|
|
65.69 0.3303 0.5615 0.0214 0.0126 2.112 9.509 6.771 1575.026 1.074 30.116 1.950 0.84 455549. 0.1985
|
|
68.67 0.3453 0.5391 0.0183 0.0117 1.967 8.857 5.793 1467.094 1.001 25.766 1.791 0.84 455967. 0.1686
|
|
71.66 0.3603 0.5054 0.0152 0.0108 1.817 8.179 4.806 1354.729 0.924 21.376 1.609 0.84 456395. 0.1380
|
|
74.64 0.3753 0.4569 0.0121 0.0099 1.660 7.476 3.812 1238.217 0.845 16.955 1.396 0.84 456833. 0.1066
|
|
77.63 0.3904 0.3884 0.0089 0.0089 1.499 6.749 2.813 1117.825 0.762 12.510 1.141 0.84 457277. 0.0749
|
|
80.61 0.4054 0.2917 0.0057 0.0079 1.332 5.998 1.808 993.476 0.678 8.042 0.825 0.84 457719. 0.0434
|
|
83.60 0.4204 0.1520 0.0025 0.0069 1.157 5.208 0.789 862.660 0.588 3.507 0.415 0.84 458102. 0.0144
|
|
86.58 0.4354
|
|
|
|
|
|
|
|
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 0.0788 0.0244 5.024 21.109 28.603 3746.179 2.385 127.226 3.463 0.89 481045. 0.7245
|
|
3.26 0.0153 0.0487 0.0768 0.0241 4.972 20.893 27.882 3707.914 2.361 124.018 3.411 0.89 481265. 0.7045
|
|
6.51 0.0306 0.0958 0.0748 0.0238 4.917 20.660 27.137 3666.444 2.334 120.704 3.357 0.89 481493. 0.6841
|
|
9.77 0.0458 0.1414 0.0726 0.0235 4.857 20.408 26.369 3621.678 2.306 117.289 3.302 0.89 481731. 0.6634
|
|
13.02 0.0611 0.1853 0.0705 0.0232 4.792 20.136 25.579 3573.414 2.275 113.774 3.247 0.89 481978. 0.6423
|
|
16.28 0.0764 0.2276 0.0682 0.0229 4.722 19.843 24.766 3521.440 2.242 110.159 3.190 0.89 482234. 0.6210
|
|
19.53 0.0917 0.2682 0.0659 0.0225 4.647 19.528 23.931 3465.519 2.206 106.444 3.132 0.89 482499. 0.5994
|
|
22.79 0.1069 0.3069 0.0636 0.0221 4.567 19.191 23.073 3405.825 2.168 102.628 3.073 0.89 482775. 0.5774
|
|
26.04 0.1222 0.3435 0.0611 0.0218 4.486 18.848 22.192 3344.992 2.129 98.711 3.009 0.89 483061. 0.5545
|
|
29.30 0.1375 0.3778 0.0586 0.0213 4.402 18.498 21.289 3282.777 2.090 94.694 2.941 0.89 483356. 0.5309
|
|
32.55 0.1528 0.4094 0.0561 0.0209 4.317 18.141 20.363 3219.371 2.050 90.575 2.869 0.89 483663. 0.5064
|
|
35.81 0.1681 0.4379 0.0535 0.0205 4.233 17.788 19.414 3156.802 2.010 86.354 2.789 0.89 483980. 0.4808
|
|
39.06 0.1833 0.4629 0.0508 0.0201 4.150 17.436 18.443 3094.393 1.970 82.033 2.703 0.89 484308. 0.4541
|
|
42.32 0.1986 0.4850 0.0481 0.0197 4.060 17.058 17.450 3027.215 1.927 77.616 2.614 0.89 484648. 0.4272
|
|
45.57 0.2139 0.5039 0.0453 0.0192 3.963 16.652 16.435 2955.259 1.881 73.102 2.522 0.89 484999. 0.4000
|
|
48.83 0.2292 0.5193 0.0424 0.0187 3.861 16.222 15.399 2878.860 1.833 68.495 2.426 0.89 485362. 0.3724
|
|
52.08 0.2444 0.5308 0.0395 0.0182 3.752 15.767 14.343 2798.159 1.781 63.796 2.325 0.90 485736. 0.3444
|
|
55.34 0.2597 0.5381 0.0365 0.0176 3.638 15.286 13.266 2712.836 1.727 59.009 2.218 0.90 486123. 0.3160
|
|
58.59 0.2750 0.5406 0.0335 0.0171 3.518 14.780 12.171 2623.026 1.670 54.136 2.105 0.90 486522. 0.2872
|
|
61.85 0.2903 0.5377 0.0305 0.0164 3.391 14.250 11.057 2528.984 1.610 49.182 1.983 0.90 486934. 0.2580
|
|
65.10 0.3055 0.5286 0.0273 0.0158 3.260 13.698 9.926 2431.017 1.548 44.152 1.852 0.90 487358. 0.2283
|
|
68.36 0.3208 0.5124 0.0242 0.0151 3.124 13.125 8.780 2329.216 1.483 39.053 1.710 0.90 487794. 0.1982
|
|
71.61 0.3361 0.4879 0.0210 0.0145 2.982 12.531 7.620 2223.889 1.416 33.892 1.554 0.90 488244. 0.1678
|
|
74.87 0.3514 0.4537 0.0178 0.0138 2.837 11.921 6.447 2115.528 1.347 28.678 1.382 0.90 488705. 0.1373
|
|
78.12 0.3667 0.4081 0.0145 0.0130 2.688 11.295 5.266 2004.532 1.276 23.422 1.192 0.90 489179. 0.1070
|
|
81.38 0.3819 0.3488 0.0112 0.0123 2.536 10.657 4.077 1891.312 1.204 18.136 0.978 0.90 489662. 0.0772
|
|
84.63 0.3972 0.2733 0.0079 0.0115 2.382 10.008 2.884 1776.080 1.131 12.827 0.736 0.90 490152. 0.0489
|
|
87.89 0.4125 0.1775 0.0046 0.0108 2.223 9.341 1.684 1657.774 1.055 7.488 0.461 0.90 490630. 0.0234
|
|
91.14 0.4278 0.0526 0.0012 0.0099 2.043 8.583 0.442 1523.279 0.970 1.967 0.132 0.90 490950. 0.0034
|
|
94.40 0.4430
|
|
|
|
|
|
|
|
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 0.0811 0.0289 7.232 28.490 33.492 5393.078 3.219 148.971 2.817 0.95 513001. 0.6377
|
|
3.52 0.0155 0.0430 0.0791 0.0284 7.119 28.046 32.650 5308.995 3.169 145.227 2.789 0.95 513242. 0.6235
|
|
7.03 0.0309 0.0851 0.0769 0.0280 7.001 27.579 31.779 5220.702 3.116 141.351 2.761 0.95 513493. 0.6088
|
|
10.55 0.0464 0.1263 0.0748 0.0275 6.877 27.091 30.880 5128.323 3.061 137.353 2.731 0.95 513754. 0.5937
|
|
14.06 0.0619 0.1664 0.0725 0.0270 6.748 26.581 29.953 5031.776 3.003 133.233 2.700 0.95 514025. 0.5780
|
|
17.58 0.0773 0.2055 0.0702 0.0264 6.613 26.048 29.000 4930.950 2.943 128.990 2.668 0.95 514306. 0.5619
|
|
21.09 0.0928 0.2435 0.0678 0.0259 6.471 25.492 28.019 4825.676 2.880 124.627 2.633 0.95 514599. 0.5453
|
|
24.61 0.1083 0.2803 0.0654 0.0253 6.324 24.912 27.011 4715.777 2.815 120.143 2.598 0.95 514901. 0.5282
|
|
28.12 0.1237 0.3157 0.0629 0.0247 6.170 24.306 25.976 4601.003 2.746 115.539 2.561 0.95 515215. 0.5105
|
|
31.64 0.1392 0.3495 0.0603 0.0240 6.014 23.690 24.913 4484.559 2.677 110.814 2.520 0.95 515540. 0.4920
|
|
35.15 0.1547 0.3806 0.0577 0.0234 5.867 23.110 23.823 4374.754 2.611 105.964 2.470 0.95 515877. 0.4716
|
|
38.67 0.1701 0.4090 0.0550 0.0229 5.724 22.548 22.705 4268.253 2.547 100.992 2.413 0.95 516226. 0.4497
|
|
42.18 0.1856 0.4330 0.0522 0.0224 5.601 22.064 21.559 4176.697 2.493 95.895 2.341 0.95 516586. 0.4252
|
|
45.70 0.2011 0.4499 0.0494 0.0221 5.521 21.749 20.384 4117.133 2.457 90.667 2.246 0.95 516959. 0.3966
|
|
49.21 0.2165 0.4630 0.0464 0.0217 5.437 21.419 19.183 4054.558 2.420 85.325 2.146 0.95 517344. 0.3677
|
|
52.73 0.2320 0.4720 0.0435 0.0214 5.349 21.071 17.957 3988.809 2.381 79.874 2.042 0.95 517742. 0.3385
|
|
56.24 0.2475 0.4767 0.0405 0.0210 5.257 20.709 16.708 3920.145 2.340 74.316 1.933 0.95 518153. 0.3091
|
|
59.76 0.2629 0.4763 0.0374 0.0206 5.164 20.341 15.435 3850.437 2.298 68.655 1.818 0.96 518576. 0.2794
|
|
63.27 0.2784 0.4708 0.0342 0.0202 5.067 19.961 14.140 3778.623 2.255 62.896 1.697 0.96 519013. 0.2497
|
|
66.79 0.2939 0.4597 0.0311 0.0198 4.968 19.572 12.825 3704.908 2.211 57.047 1.570 0.96 519464. 0.2200
|
|
70.31 0.3093 0.4426 0.0278 0.0194 4.867 19.174 11.492 3629.656 2.166 51.115 1.436 0.96 519928. 0.1904
|
|
73.82 0.3248 0.4189 0.0246 0.0190 4.766 18.773 10.142 3553.789 2.121 45.111 1.294 0.96 520406. 0.1613
|
|
77.34 0.3403 0.3882 0.0213 0.0186 4.663 18.370 8.779 3477.418 2.075 39.048 1.145 0.96 520897. 0.1327
|
|
80.85 0.3557 0.3501 0.0179 0.0182 4.560 17.965 7.406 3400.682 2.030 32.941 0.988 0.96 521402. 0.1052
|
|
84.37 0.3712 0.3042 0.0146 0.0178 4.457 17.559 6.027 3323.857 1.984 26.807 0.822 0.96 521919. 0.0790
|
|
87.88 0.3867 0.2500 0.0112 0.0174 4.354 17.153 4.645 3247.109 1.938 20.662 0.649 0.96 522448. 0.0547
|
|
91.40 0.4021 0.1872 0.0079 0.0170 4.250 16.744 3.264 3169.537 1.892 14.520 0.467 0.96 522984. 0.0330
|
|
94.91 0.4176 0.1149 0.0046 0.0165 4.141 16.311 1.880 3087.625 1.843 8.364 0.276 0.96 523510. 0.0148
|
|
98.43 0.4331 0.0290 0.0011 0.0159 3.990 15.716 0.442 2975.037 1.776 1.964 0.067 0.96 523897. 0.0017
|
|
101.94 0.4485
|
|
|
|
|
|
|