649 lines
115 KiB
Plaintext
649 lines
115 KiB
Plaintext
14x5N (14x5N.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 0.0593 0.0262 0.001 0.071 0.073 0.845 0.008 0.323 38.955 0.06 16617. 0.4399
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0.23 0.0176 0.0390 0.0581 0.0263 0.001 0.072 0.071 0.848 0.008 0.317 38.064 0.06 16624. 0.4256
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0.47 0.0353 0.0762 0.0569 0.0263 0.001 0.072 0.070 0.850 0.008 0.310 37.157 0.06 16631. 0.4110
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0.70 0.0529 0.1114 0.0556 0.0264 0.001 0.072 0.068 0.852 0.008 0.303 36.236 0.06 16639. 0.3962
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0.94 0.0705 0.1447 0.0542 0.0264 0.001 0.072 0.066 0.853 0.008 0.295 35.301 0.06 16647. 0.3812
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1.17 0.0882 0.1760 0.0528 0.0264 0.001 0.072 0.065 0.853 0.008 0.287 34.353 0.06 16655. 0.3659
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1.40 0.1058 0.2053 0.0512 0.0264 0.001 0.072 0.063 0.852 0.008 0.279 33.390 0.06 16665. 0.3505
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1.64 0.1234 0.2325 0.0496 0.0264 0.001 0.072 0.061 0.850 0.008 0.270 32.413 0.06 16675. 0.3349
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1.87 0.1411 0.2576 0.0480 0.0263 0.001 0.072 0.059 0.848 0.008 0.261 31.421 0.06 16685. 0.3191
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2.10 0.1587 0.2805 0.0462 0.0262 0.001 0.071 0.057 0.844 0.008 0.252 30.414 0.06 16696. 0.3032
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2.34 0.1763 0.3012 0.0444 0.0260 0.001 0.071 0.054 0.839 0.008 0.242 29.389 0.06 16708. 0.2872
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2.57 0.1940 0.3195 0.0425 0.0258 0.001 0.070 0.052 0.833 0.008 0.232 28.346 0.06 16720. 0.2711
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2.81 0.2116 0.3355 0.0406 0.0256 0.001 0.070 0.050 0.826 0.008 0.221 27.283 0.06 16733. 0.2549
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3.04 0.2292 0.3490 0.0386 0.0253 0.001 0.069 0.047 0.817 0.008 0.210 26.197 0.06 16746. 0.2386
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3.27 0.2469 0.3599 0.0365 0.0250 0.001 0.068 0.045 0.808 0.008 0.199 25.085 0.06 16760. 0.2222
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3.51 0.2645 0.3681 0.0344 0.0247 0.001 0.067 0.042 0.797 0.008 0.187 23.945 0.06 16775. 0.2058
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3.74 0.2821 0.3734 0.0322 0.0243 0.001 0.066 0.039 0.784 0.007 0.175 22.772 0.06 16791. 0.1894
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3.97 0.2997 0.3756 0.0299 0.0239 0.001 0.065 0.037 0.771 0.007 0.163 21.562 0.06 16807. 0.1730
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4.21 0.3174 0.3746 0.0276 0.0234 0.001 0.064 0.034 0.755 0.007 0.150 20.308 0.06 16824. 0.1565
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4.44 0.3350 0.3700 0.0253 0.0229 0.001 0.062 0.031 0.739 0.007 0.138 19.004 0.06 16842. 0.1401
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4.68 0.3526 0.3616 0.0229 0.0223 0.001 0.061 0.028 0.720 0.007 0.125 17.641 0.06 16860. 0.1238
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4.91 0.3703 0.3488 0.0205 0.0217 0.001 0.059 0.025 0.701 0.007 0.111 16.210 0.06 16879. 0.1075
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5.14 0.3879 0.3314 0.0180 0.0211 0.001 0.057 0.022 0.679 0.006 0.098 14.698 0.06 16899. 0.0914
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5.38 0.4055 0.3085 0.0155 0.0203 0.001 0.055 0.019 0.657 0.006 0.084 13.090 0.06 16920. 0.0755
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5.61 0.4232 0.2796 0.0129 0.0196 0.001 0.053 0.016 0.632 0.006 0.070 11.368 0.06 16942. 0.0600
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5.84 0.4408 0.2437 0.0104 0.0188 0.001 0.051 0.013 0.606 0.006 0.057 9.511 0.06 16964. 0.0449
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6.08 0.4584 0.1996 0.0078 0.0179 0.001 0.049 0.010 0.579 0.006 0.043 7.490 0.06 16987. 0.0307
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6.31 0.4761 0.1459 0.0052 0.0170 0.001 0.046 0.006 0.550 0.005 0.028 5.272 0.06 17010. 0.0177
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6.55 0.4937 0.0806 0.0026 0.0161 0.001 0.044 0.003 0.519 0.005 0.014 2.810 0.06 17035. 0.0067
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6.78 0.5113 0.0013 0.0000 0.0151 0.001 0.041 0.000 0.488 0.005 0.000 0.042 0.06 17060. 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 0.0596 0.0217 0.008 0.237 0.292 5.603 0.027 1.298 23.627 0.11 33234. 0.5350
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0.47 0.0178 0.0476 0.0584 0.0218 0.008 0.238 0.286 5.634 0.027 1.273 23.039 0.11 33247. 0.5166
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0.94 0.0356 0.0928 0.0572 0.0219 0.008 0.239 0.280 5.660 0.027 1.246 22.446 0.11 33262. 0.4979
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1.41 0.0533 0.1355 0.0559 0.0220 0.008 0.240 0.274 5.681 0.027 1.217 21.852 0.11 33277. 0.4791
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1.89 0.0711 0.1757 0.0545 0.0221 0.008 0.241 0.267 5.697 0.027 1.187 21.255 0.11 33294. 0.4603
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2.36 0.0889 0.2134 0.0531 0.0221 0.008 0.241 0.260 5.705 0.027 1.156 20.656 0.11 33312. 0.4413
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2.83 0.1067 0.2487 0.0515 0.0221 0.008 0.241 0.252 5.706 0.027 1.122 20.055 0.11 33330. 0.4222
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3.30 0.1244 0.2814 0.0499 0.0221 0.008 0.241 0.244 5.698 0.027 1.087 19.453 0.11 33350. 0.4031
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3.77 0.1422 0.3116 0.0482 0.0220 0.008 0.240 0.236 5.682 0.027 1.050 18.849 0.11 33371. 0.3839
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4.24 0.1600 0.3393 0.0465 0.0219 0.008 0.239 0.228 5.657 0.027 1.012 18.243 0.11 33393. 0.3647
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4.71 0.1778 0.3644 0.0446 0.0218 0.008 0.238 0.219 5.622 0.027 0.972 17.633 0.11 33417. 0.3455
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5.18 0.1955 0.3868 0.0427 0.0216 0.007 0.236 0.209 5.577 0.027 0.931 17.019 0.11 33442. 0.3263
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5.66 0.2133 0.4067 0.0408 0.0214 0.007 0.233 0.200 5.521 0.026 0.888 16.400 0.11 33468. 0.3071
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6.13 0.2311 0.4237 0.0387 0.0211 0.007 0.230 0.190 5.454 0.026 0.844 15.774 0.11 33495. 0.2879
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6.60 0.2489 0.4380 0.0366 0.0208 0.007 0.227 0.179 5.376 0.026 0.798 15.140 0.11 33524. 0.2688
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7.07 0.2666 0.4493 0.0345 0.0205 0.007 0.223 0.169 5.285 0.025 0.751 14.495 0.11 33554. 0.2497
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7.54 0.2844 0.4575 0.0323 0.0201 0.007 0.219 0.158 5.182 0.025 0.703 13.836 0.11 33586. 0.2306
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8.01 0.3022 0.4623 0.0300 0.0196 0.007 0.214 0.147 5.066 0.024 0.654 13.160 0.11 33619. 0.2115
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8.48 0.3200 0.4636 0.0277 0.0191 0.007 0.209 0.136 4.938 0.024 0.603 12.463 0.11 33653. 0.1924
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8.96 0.3378 0.4609 0.0253 0.0186 0.006 0.203 0.124 4.795 0.023 0.552 11.740 0.11 33689. 0.1733
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9.43 0.3555 0.4539 0.0229 0.0180 0.006 0.196 0.112 4.639 0.022 0.500 10.984 0.11 33727. 0.1543
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9.90 0.3733 0.4420 0.0205 0.0173 0.006 0.189 0.100 4.468 0.021 0.446 10.186 0.11 33766. 0.1352
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10.37 0.3911 0.4245 0.0180 0.0166 0.006 0.181 0.088 4.284 0.020 0.392 9.337 0.11 33806. 0.1162
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10.84 0.4089 0.4004 0.0155 0.0158 0.005 0.173 0.076 4.085 0.020 0.337 8.424 0.11 33848. 0.0973
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11.31 0.4266 0.3684 0.0129 0.0150 0.005 0.164 0.063 3.872 0.018 0.282 7.429 0.11 33892. 0.0784
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11.78 0.4444 0.3270 0.0104 0.0141 0.005 0.154 0.051 3.644 0.017 0.226 6.330 0.11 33937. 0.0598
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12.25 0.4622 0.2737 0.0078 0.0132 0.005 0.144 0.038 3.402 0.016 0.170 5.095 0.11 33984. 0.0417
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12.73 0.4800 0.2054 0.0052 0.0122 0.004 0.133 0.026 3.147 0.015 0.114 3.682 0.11 34032. 0.0247
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13.20 0.4977 0.1174 0.0026 0.0111 0.004 0.122 0.013 2.878 0.014 0.057 2.028 0.11 34081. 0.0096
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13.67 0.5155 0.0019 0.0000 0.0101 0.003 0.110 0.000 2.596 0.012 0.001 0.031 0.11 34130. 0.0000
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PROP RPM = 3000
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V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
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(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
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0.00 0.0000 0.0000 0.0598 0.0199 0.023 0.488 0.659 17.310 0.055 2.933 17.279 0.17 49850. 0.5881
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0.71 0.0178 0.0524 0.0587 0.0200 0.023 0.491 0.647 17.425 0.055 2.876 16.829 0.17 49871. 0.5672
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1.42 0.0357 0.1019 0.0574 0.0201 0.024 0.494 0.633 17.525 0.056 2.815 16.379 0.17 49893. 0.5461
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2.13 0.0535 0.1487 0.0561 0.0202 0.024 0.496 0.618 17.607 0.056 2.751 15.930 0.17 49916. 0.5250
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2.84 0.0714 0.1927 0.0547 0.0203 0.024 0.498 0.603 17.669 0.056 2.683 15.482 0.17 49941. 0.5039
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3.55 0.0892 0.2339 0.0533 0.0203 0.024 0.499 0.587 17.707 0.056 2.611 15.035 0.17 49968. 0.4828
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4.26 0.1071 0.2723 0.0517 0.0203 0.024 0.499 0.570 17.718 0.056 2.535 14.590 0.17 49996. 0.4616
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4.97 0.1249 0.3081 0.0501 0.0203 0.024 0.499 0.552 17.702 0.056 2.456 14.146 0.17 50026. 0.4405
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5.68 0.1427 0.3411 0.0484 0.0203 0.024 0.497 0.533 17.655 0.056 2.373 13.704 0.17 50057. 0.4195
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6.39 0.1606 0.3713 0.0466 0.0202 0.024 0.495 0.514 17.576 0.056 2.286 13.263 0.17 50091. 0.3985
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7.10 0.1784 0.3989 0.0448 0.0200 0.023 0.492 0.494 17.463 0.056 2.196 12.822 0.17 50126. 0.3776
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7.81 0.1963 0.4237 0.0429 0.0199 0.023 0.488 0.473 17.313 0.055 2.102 12.381 0.17 50164. 0.3567
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8.52 0.2141 0.4457 0.0409 0.0197 0.023 0.483 0.451 17.127 0.055 2.005 11.939 0.17 50203. 0.3360
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9.23 0.2319 0.4649 0.0389 0.0194 0.023 0.476 0.428 16.900 0.054 1.905 11.495 0.17 50245. 0.3153
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9.93 0.2498 0.4812 0.0368 0.0191 0.022 0.469 0.405 16.633 0.053 1.802 11.048 0.17 50288. 0.2947
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10.64 0.2676 0.4944 0.0346 0.0187 0.022 0.460 0.381 16.322 0.052 1.696 10.596 0.17 50334. 0.2742
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11.35 0.2855 0.5045 0.0324 0.0183 0.021 0.450 0.357 15.968 0.051 1.587 10.136 0.17 50381. 0.2538
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12.06 0.3033 0.5112 0.0301 0.0179 0.021 0.439 0.332 15.568 0.050 1.476 9.666 0.17 50431. 0.2334
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12.77 0.3212 0.5143 0.0278 0.0174 0.020 0.426 0.306 15.120 0.048 1.362 9.184 0.17 50483. 0.2130
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13.48 0.3390 0.5133 0.0254 0.0168 0.020 0.412 0.280 14.625 0.047 1.245 8.684 0.17 50538. 0.1926
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14.19 0.3568 0.5079 0.0230 0.0162 0.019 0.397 0.253 14.080 0.045 1.127 8.162 0.17 50594. 0.1722
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14.90 0.3747 0.4973 0.0205 0.0155 0.018 0.380 0.226 13.484 0.043 1.007 7.612 0.17 50653. 0.1518
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15.61 0.3925 0.4808 0.0180 0.0147 0.017 0.362 0.199 12.837 0.041 0.884 7.024 0.17 50714. 0.1313
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16.32 0.4104 0.4571 0.0155 0.0139 0.016 0.342 0.171 12.140 0.039 0.761 6.388 0.17 50778. 0.1107
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17.03 0.4282 0.4247 0.0130 0.0131 0.015 0.321 0.143 11.390 0.036 0.635 5.689 0.17 50843. 0.0901
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17.74 0.4460 0.3814 0.0104 0.0122 0.014 0.298 0.115 10.590 0.034 0.509 4.904 0.17 50912. 0.0696
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18.45 0.4639 0.3239 0.0078 0.0112 0.013 0.274 0.086 9.740 0.031 0.383 4.005 0.17 50982. 0.0492
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19.16 0.4817 0.2475 0.0052 0.0101 0.012 0.249 0.057 8.841 0.028 0.255 2.946 0.17 51055. 0.0296
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19.87 0.4996 0.1444 0.0026 0.0091 0.011 0.222 0.029 7.895 0.025 0.128 1.658 0.17 51129. 0.0118
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20.58 0.5174 0.0012 0.0000 0.0079 0.009 0.194 0.000 6.897 0.022 0.001 0.013 0.17 51203. 0.0000
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PROP RPM = 4000
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V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
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(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
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0.00 0.0000 0.0000 0.0601 0.0189 0.052 0.823 1.177 38.936 0.093 5.237 13.716 0.22 66466. 0.6238
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0.95 0.0179 0.0555 0.0589 0.0190 0.053 0.829 1.154 39.225 0.094 5.135 13.349 0.22 66494. 0.6012
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1.90 0.0358 0.1080 0.0577 0.0191 0.053 0.834 1.130 39.478 0.094 5.027 12.984 0.22 66523. 0.5785
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2.85 0.0537 0.1574 0.0564 0.0192 0.053 0.839 1.104 39.687 0.095 4.912 12.620 0.22 66554. 0.5558
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3.79 0.0715 0.2039 0.0550 0.0193 0.053 0.842 1.077 39.846 0.095 4.790 12.258 0.22 66588. 0.5332
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4.74 0.0894 0.2474 0.0535 0.0193 0.054 0.844 1.048 39.948 0.095 4.662 11.899 0.22 66623. 0.5106
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5.69 0.1073 0.2880 0.0520 0.0194 0.054 0.845 1.018 39.988 0.095 4.527 11.543 0.22 66661. 0.4881
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6.64 0.1252 0.3257 0.0503 0.0193 0.054 0.844 0.986 39.960 0.095 4.385 11.190 0.22 66701. 0.4656
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7.59 0.1431 0.3605 0.0486 0.0193 0.053 0.842 0.952 39.857 0.095 4.236 10.839 0.22 66744. 0.4433
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8.54 0.1610 0.3925 0.0468 0.0192 0.053 0.838 0.918 39.676 0.095 4.081 10.490 0.22 66788. 0.4211
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9.48 0.1788 0.4217 0.0450 0.0191 0.053 0.833 0.881 39.412 0.094 3.920 10.143 0.22 66836. 0.3991
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10.43 0.1967 0.4481 0.0431 0.0189 0.052 0.825 0.844 39.060 0.093 3.753 9.798 0.22 66886. 0.3772
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11.38 0.2146 0.4716 0.0411 0.0187 0.052 0.816 0.805 38.615 0.092 3.580 9.453 0.22 66939. 0.3554
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12.33 0.2325 0.4923 0.0390 0.0184 0.051 0.805 0.765 38.075 0.091 3.401 9.108 0.22 66994. 0.3338
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13.28 0.2504 0.5100 0.0369 0.0181 0.050 0.791 0.723 37.434 0.089 3.216 8.762 0.22 67052. 0.3123
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14.23 0.2683 0.5247 0.0347 0.0178 0.049 0.775 0.681 36.688 0.088 3.027 8.413 0.22 67113. 0.2909
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15.17 0.2861 0.5362 0.0325 0.0173 0.048 0.757 0.637 35.834 0.086 2.832 8.060 0.22 67177. 0.2696
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16.12 0.3040 0.5443 0.0302 0.0169 0.047 0.737 0.592 34.868 0.083 2.633 7.701 0.22 67244. 0.2483
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17.07 0.3219 0.5488 0.0279 0.0164 0.045 0.714 0.546 33.786 0.081 2.430 7.333 0.22 67314. 0.2271
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18.02 0.3398 0.5492 0.0255 0.0158 0.044 0.689 0.499 32.585 0.078 2.222 6.952 0.22 67387. 0.2059
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18.97 0.3577 0.5452 0.0231 0.0151 0.042 0.661 0.452 31.263 0.075 2.010 6.556 0.22 67462. 0.1847
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19.92 0.3756 0.5359 0.0206 0.0144 0.040 0.630 0.404 29.818 0.071 1.795 6.138 0.22 67541. 0.1634
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20.86 0.3934 0.5205 0.0181 0.0137 0.038 0.597 0.354 28.247 0.067 1.576 5.691 0.22 67623. 0.1420
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21.81 0.4113 0.4978 0.0156 0.0129 0.036 0.561 0.305 26.551 0.063 1.355 5.205 0.22 67708. 0.1204
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22.76 0.4292 0.4658 0.0130 0.0120 0.033 0.523 0.254 24.728 0.059 1.132 4.668 0.22 67796. 0.0987
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23.71 0.4471 0.4219 0.0104 0.0110 0.031 0.481 0.204 22.781 0.054 0.907 4.059 0.22 67888. 0.0768
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24.66 0.4650 0.3622 0.0078 0.0100 0.028 0.438 0.153 20.711 0.049 0.681 3.351 0.22 67982. 0.0549
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25.61 0.4829 0.2804 0.0052 0.0090 0.025 0.391 0.102 18.521 0.044 0.454 2.498 0.22 68079. 0.0334
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26.56 0.5008 0.1662 0.0026 0.0079 0.022 0.343 0.051 16.217 0.039 0.227 1.428 0.22 68179. 0.0135
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27.50 0.5186 -0.0007 0.0000 0.0067 0.018 0.291 0.000 13.778 0.033 -0.001 -0.006 0.23 68275. 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 0.0604 0.0182 0.099 1.243 1.849 73.515 0.140 8.225 11.409 0.28 83081. 0.6502
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1.20 0.0180 0.0582 0.0592 0.0184 0.099 1.253 1.813 74.104 0.142 8.063 11.096 0.28 83116. 0.6261
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2.39 0.0361 0.1131 0.0580 0.0185 0.100 1.261 1.774 74.620 0.143 7.892 10.784 0.28 83153. 0.6021
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3.59 0.0541 0.1648 0.0566 0.0186 0.101 1.269 1.733 75.048 0.143 7.710 10.476 0.28 83192. 0.5780
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4.78 0.0722 0.2133 0.0552 0.0187 0.101 1.274 1.690 75.375 0.144 7.517 10.170 0.28 83235. 0.5541
|
|
5.98 0.0902 0.2587 0.0537 0.0187 0.101 1.278 1.644 75.589 0.144 7.314 9.867 0.28 83280. 0.5303
|
|
7.18 0.1083 0.3010 0.0522 0.0188 0.101 1.279 1.596 75.675 0.145 7.100 9.567 0.28 83328. 0.5066
|
|
8.37 0.1263 0.3403 0.0505 0.0187 0.101 1.278 1.546 75.623 0.144 6.875 9.271 0.28 83378. 0.4831
|
|
9.57 0.1443 0.3766 0.0488 0.0187 0.101 1.275 1.493 75.421 0.144 6.640 8.977 0.28 83432. 0.4597
|
|
10.76 0.1624 0.4099 0.0470 0.0186 0.101 1.269 1.437 75.059 0.143 6.394 8.686 0.28 83489. 0.4365
|
|
11.96 0.1804 0.4404 0.0451 0.0185 0.100 1.260 1.380 74.528 0.142 6.138 8.398 0.28 83550. 0.4135
|
|
13.16 0.1985 0.4679 0.0431 0.0183 0.099 1.248 1.320 73.819 0.141 5.872 8.112 0.28 83613. 0.3906
|
|
14.35 0.2165 0.4925 0.0411 0.0181 0.098 1.233 1.258 72.923 0.139 5.597 7.827 0.28 83680. 0.3680
|
|
15.55 0.2346 0.5142 0.0390 0.0178 0.096 1.214 1.195 71.831 0.137 5.313 7.543 0.28 83751. 0.3455
|
|
16.74 0.2526 0.5328 0.0369 0.0175 0.095 1.192 1.129 70.534 0.135 5.021 7.259 0.28 83824. 0.3232
|
|
17.94 0.2707 0.5484 0.0347 0.0171 0.093 1.167 1.061 69.024 0.132 4.720 6.973 0.28 83902. 0.3010
|
|
19.14 0.2887 0.5608 0.0324 0.0167 0.090 1.138 0.992 67.293 0.129 4.411 6.684 0.28 83983. 0.2790
|
|
20.33 0.3067 0.5697 0.0301 0.0162 0.088 1.104 0.921 65.333 0.125 4.095 6.391 0.28 84068. 0.2570
|
|
21.53 0.3248 0.5749 0.0277 0.0157 0.085 1.067 0.848 63.138 0.121 3.772 6.091 0.28 84156. 0.2351
|
|
22.73 0.3428 0.5760 0.0253 0.0150 0.081 1.026 0.774 60.701 0.116 3.442 5.782 0.28 84249. 0.2132
|
|
23.92 0.3609 0.5725 0.0228 0.0144 0.078 0.981 0.698 58.016 0.111 3.106 5.459 0.28 84345. 0.1912
|
|
25.12 0.3789 0.5635 0.0203 0.0137 0.074 0.931 0.621 55.081 0.105 2.764 5.118 0.28 84445. 0.1691
|
|
26.31 0.3970 0.5482 0.0178 0.0129 0.070 0.877 0.544 51.890 0.099 2.418 4.752 0.28 84549. 0.1468
|
|
27.51 0.4150 0.5249 0.0152 0.0120 0.065 0.819 0.465 48.444 0.093 2.068 4.352 0.28 84657. 0.1244
|
|
28.71 0.4330 0.4915 0.0126 0.0111 0.060 0.756 0.385 44.742 0.085 1.714 3.905 0.28 84769. 0.1016
|
|
29.90 0.4511 0.4447 0.0100 0.0101 0.055 0.689 0.305 40.788 0.078 1.357 3.393 0.28 84885. 0.0785
|
|
31.10 0.4691 0.3795 0.0073 0.0091 0.049 0.618 0.225 36.585 0.070 0.999 2.784 0.28 85005. 0.0553
|
|
32.29 0.4872 0.2874 0.0047 0.0080 0.043 0.543 0.144 32.143 0.061 0.640 2.030 0.28 85129. 0.0323
|
|
33.49 0.5052 0.1535 0.0021 0.0068 0.037 0.464 0.063 27.467 0.052 0.282 1.046 0.28 85255. 0.0110
|
|
34.69 0.5233
|
|
|
|
|
|
|
|
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 0.0608 0.0178 0.167 1.750 2.679 124.221 0.198 11.915 9.781 0.33 99695. 0.6709
|
|
1.43 0.0179 0.0595 0.0596 0.0180 0.168 1.765 2.627 125.258 0.199 11.683 9.511 0.33 99737. 0.6461
|
|
2.85 0.0359 0.1156 0.0583 0.0181 0.169 1.777 2.571 126.167 0.201 11.437 9.244 0.33 99781. 0.6212
|
|
4.28 0.0538 0.1684 0.0570 0.0182 0.170 1.788 2.513 126.926 0.202 11.176 8.979 0.33 99828. 0.5965
|
|
5.70 0.0717 0.2180 0.0556 0.0183 0.171 1.796 2.450 127.512 0.203 10.900 8.717 0.33 99878. 0.5719
|
|
7.13 0.0896 0.2644 0.0541 0.0183 0.172 1.802 2.385 127.902 0.204 10.608 8.458 0.33 99932. 0.5474
|
|
8.56 0.1076 0.3077 0.0525 0.0184 0.172 1.804 2.316 128.072 0.204 10.301 8.202 0.33 99989. 0.5231
|
|
9.98 0.1255 0.3479 0.0509 0.0184 0.172 1.803 2.243 128.003 0.204 9.979 7.949 0.33 100050. 0.4990
|
|
11.41 0.1434 0.3852 0.0492 0.0183 0.171 1.799 2.167 127.675 0.203 9.641 7.700 0.33 100114. 0.4751
|
|
12.84 0.1614 0.4194 0.0474 0.0182 0.170 1.790 2.088 127.073 0.202 9.288 7.454 0.33 100182. 0.4514
|
|
14.26 0.1793 0.4508 0.0455 0.0181 0.169 1.777 2.006 126.178 0.201 8.921 7.210 0.33 100254. 0.4280
|
|
15.69 0.1972 0.4793 0.0436 0.0179 0.168 1.761 1.920 124.975 0.199 8.540 6.968 0.33 100329. 0.4047
|
|
17.11 0.2152 0.5049 0.0416 0.0177 0.166 1.739 1.831 123.449 0.196 8.146 6.729 0.33 100409. 0.3817
|
|
18.54 0.2331 0.5276 0.0395 0.0174 0.163 1.713 1.740 121.584 0.194 7.739 6.490 0.33 100493. 0.3588
|
|
19.97 0.2510 0.5473 0.0373 0.0171 0.160 1.682 1.645 119.366 0.190 7.319 6.253 0.33 100581. 0.3362
|
|
21.39 0.2689 0.5641 0.0351 0.0168 0.157 1.645 1.548 116.779 0.186 6.887 6.014 0.33 100673. 0.3137
|
|
22.82 0.2869 0.5777 0.0329 0.0163 0.153 1.603 1.449 113.810 0.181 6.445 5.774 0.33 100769. 0.2913
|
|
24.25 0.3048 0.5879 0.0306 0.0158 0.148 1.556 1.347 110.445 0.176 5.991 5.531 0.33 100870. 0.2690
|
|
25.67 0.3227 0.5946 0.0282 0.0153 0.143 1.503 1.243 106.674 0.170 5.527 5.283 0.33 100975. 0.2468
|
|
27.10 0.3407 0.5974 0.0258 0.0147 0.137 1.444 1.136 102.483 0.163 5.054 5.029 0.34 101085. 0.2247
|
|
28.52 0.3586 0.5957 0.0233 0.0140 0.131 1.379 1.028 97.865 0.156 4.572 4.764 0.34 101199. 0.2024
|
|
29.95 0.3765 0.5889 0.0208 0.0133 0.124 1.307 0.918 92.811 0.148 4.082 4.485 0.34 101318. 0.1801
|
|
31.38 0.3945 0.5759 0.0183 0.0125 0.117 1.230 0.806 87.316 0.139 3.585 4.186 0.34 101441. 0.1575
|
|
32.80 0.4124 0.5553 0.0157 0.0117 0.109 1.146 0.693 81.377 0.130 3.082 3.861 0.34 101570. 0.1347
|
|
34.23 0.4303 0.5250 0.0131 0.0108 0.101 1.056 0.578 74.994 0.119 2.573 3.499 0.34 101703. 0.1115
|
|
35.66 0.4482 0.4819 0.0105 0.0098 0.091 0.960 0.463 68.170 0.108 2.061 3.083 0.34 101840. 0.0879
|
|
37.08 0.4662 0.4207 0.0079 0.0087 0.082 0.858 0.348 60.915 0.097 1.546 2.588 0.34 101982. 0.0639
|
|
38.51 0.4841 0.3330 0.0053 0.0076 0.071 0.750 0.232 53.241 0.085 1.030 1.973 0.34 102129. 0.0398
|
|
39.93 0.5020 0.2034 0.0026 0.0065 0.061 0.636 0.116 45.161 0.072 0.515 1.162 0.34 102280. 0.0166
|
|
41.36 0.5200 -0.0028 0.0000 0.0052 0.049 0.515 -0.001 36.571 0.058 -0.006 -0.016 0.34 102420. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 7000
|
|
|
|
V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
|
|
(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
|
|
0.00 0.0000 0.0000 0.0612 0.0176 0.261 2.348 3.672 194.445 0.265 16.333 8.565 0.39 116308. 0.6879
|
|
1.69 0.0182 0.0616 0.0600 0.0177 0.263 2.368 3.600 196.143 0.268 16.011 8.324 0.39 116357. 0.6619
|
|
3.37 0.0364 0.1196 0.0587 0.0179 0.265 2.386 3.523 197.631 0.270 15.669 8.085 0.39 116409. 0.6360
|
|
5.06 0.0545 0.1741 0.0574 0.0180 0.267 2.401 3.441 198.868 0.271 15.306 7.849 0.39 116466. 0.6102
|
|
6.75 0.0727 0.2253 0.0559 0.0181 0.268 2.413 3.355 199.817 0.273 14.923 7.615 0.39 116526. 0.5846
|
|
8.43 0.0909 0.2731 0.0544 0.0181 0.269 2.420 3.264 200.439 0.273 14.517 7.385 0.39 116590. 0.5592
|
|
10.12 0.1091 0.3177 0.0528 0.0181 0.269 2.423 3.168 200.696 0.274 14.089 7.159 0.39 116658. 0.5340
|
|
11.81 0.1272 0.3590 0.0511 0.0181 0.269 2.422 3.067 200.553 0.274 13.640 6.935 0.39 116730. 0.5090
|
|
13.50 0.1454 0.3973 0.0494 0.0181 0.268 2.415 2.961 199.980 0.273 13.169 6.715 0.39 116806. 0.4843
|
|
15.18 0.1636 0.4325 0.0475 0.0180 0.267 2.402 2.850 198.948 0.271 12.678 6.498 0.39 116887. 0.4598
|
|
16.87 0.1818 0.4647 0.0456 0.0178 0.265 2.384 2.735 197.429 0.269 12.166 6.284 0.39 116973. 0.4355
|
|
18.56 0.2000 0.4939 0.0436 0.0177 0.262 2.359 2.616 195.396 0.267 11.634 6.072 0.39 117063. 0.4115
|
|
20.24 0.2181 0.5202 0.0415 0.0174 0.259 2.328 2.492 192.824 0.263 11.084 5.861 0.39 117158. 0.3878
|
|
21.93 0.2363 0.5435 0.0394 0.0171 0.254 2.290 2.364 189.686 0.259 10.515 5.653 0.39 117258. 0.3643
|
|
23.62 0.2545 0.5638 0.0372 0.0168 0.249 2.245 2.232 185.958 0.254 9.929 5.445 0.39 117363. 0.3410
|
|
25.30 0.2727 0.5810 0.0350 0.0164 0.244 2.193 2.097 181.615 0.248 9.327 5.237 0.39 117474. 0.3178
|
|
26.99 0.2909 0.5949 0.0326 0.0160 0.237 2.133 1.958 176.635 0.241 8.709 5.028 0.39 117589. 0.2948
|
|
28.68 0.3090 0.6055 0.0303 0.0154 0.229 2.065 1.816 170.996 0.233 8.076 4.816 0.39 117709. 0.2720
|
|
30.37 0.3272 0.6123 0.0278 0.0149 0.221 1.988 1.670 164.676 0.225 7.428 4.600 0.39 117835. 0.2491
|
|
32.05 0.3454 0.6151 0.0254 0.0142 0.211 1.904 1.522 157.660 0.215 6.768 4.377 0.39 117966. 0.2263
|
|
33.74 0.3636 0.6132 0.0228 0.0135 0.201 1.810 1.370 149.930 0.205 6.096 4.146 0.39 118103. 0.2034
|
|
35.43 0.3817 0.6059 0.0203 0.0128 0.190 1.708 1.217 141.476 0.193 5.412 3.901 0.39 118245. 0.1804
|
|
37.11 0.3999 0.5919 0.0177 0.0120 0.177 1.597 1.061 132.288 0.180 4.719 3.638 0.39 118393. 0.1570
|
|
38.80 0.4181 0.5695 0.0151 0.0111 0.164 1.477 0.903 122.364 0.167 4.018 3.348 0.39 118547. 0.1334
|
|
40.49 0.4363 0.5363 0.0124 0.0101 0.150 1.349 0.744 111.705 0.152 3.310 3.021 0.39 118706. 0.1092
|
|
42.17 0.4545 0.4880 0.0097 0.0091 0.135 1.211 0.584 100.321 0.137 2.597 2.639 0.39 118870. 0.0845
|
|
43.86 0.4726 0.4180 0.0070 0.0080 0.118 1.065 0.423 88.228 0.120 1.881 2.174 0.39 119040. 0.0592
|
|
45.55 0.4908 0.3142 0.0044 0.0068 0.101 0.911 0.262 75.449 0.103 1.164 1.574 0.39 119216. 0.0337
|
|
47.24 0.5090 0.1528 0.0017 0.0056 0.083 0.749 0.101 61.997 0.085 0.449 0.738 0.39 119395. 0.0098
|
|
48.92 0.5272
|
|
|
|
|
|
|
|
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 0.0617 0.0174 0.386 3.042 4.835 287.882 0.344 21.508 7.618 0.44 132919. 0.7021
|
|
1.93 0.0182 0.0626 0.0605 0.0176 0.390 3.069 4.740 290.456 0.347 21.086 7.403 0.44 132975. 0.6755
|
|
3.86 0.0364 0.1216 0.0592 0.0177 0.393 3.093 4.639 292.711 0.349 20.636 7.189 0.44 133035. 0.6490
|
|
5.79 0.0546 0.1771 0.0578 0.0178 0.395 3.112 4.532 294.585 0.352 20.159 6.978 0.44 133100. 0.6226
|
|
7.72 0.0728 0.2291 0.0564 0.0179 0.397 3.128 4.419 296.021 0.353 19.655 6.770 0.44 133169. 0.5965
|
|
9.65 0.0910 0.2777 0.0549 0.0180 0.398 3.137 4.299 296.959 0.354 19.121 6.566 0.44 133242. 0.5706
|
|
11.58 0.1092 0.3230 0.0533 0.0180 0.399 3.142 4.172 297.344 0.355 18.558 6.364 0.44 133320. 0.5449
|
|
13.51 0.1274 0.3652 0.0516 0.0180 0.398 3.139 4.039 297.121 0.355 17.967 6.166 0.44 133403. 0.5194
|
|
15.44 0.1456 0.4041 0.0498 0.0179 0.397 3.130 3.900 296.245 0.354 17.347 5.971 0.44 133491. 0.4942
|
|
17.37 0.1638 0.4400 0.0479 0.0178 0.395 3.113 3.754 294.670 0.352 16.700 5.779 0.44 133584. 0.4693
|
|
19.30 0.1819 0.4729 0.0460 0.0177 0.392 3.089 3.603 292.356 0.349 16.026 5.590 0.45 133682. 0.4447
|
|
21.23 0.2001 0.5028 0.0440 0.0175 0.388 3.056 3.446 289.262 0.345 15.326 5.403 0.45 133786. 0.4203
|
|
23.16 0.2183 0.5297 0.0419 0.0173 0.383 3.015 3.283 285.349 0.341 14.601 5.218 0.45 133895. 0.3962
|
|
25.09 0.2365 0.5537 0.0397 0.0170 0.376 2.964 3.114 280.577 0.335 13.852 5.034 0.45 134009. 0.3723
|
|
27.02 0.2547 0.5746 0.0375 0.0166 0.369 2.905 2.941 274.910 0.328 13.080 4.852 0.45 134130. 0.3487
|
|
28.95 0.2729 0.5925 0.0353 0.0162 0.360 2.835 2.762 268.310 0.320 12.286 4.669 0.45 134256. 0.3253
|
|
30.88 0.2911 0.6073 0.0329 0.0158 0.350 2.755 2.579 260.742 0.311 11.472 4.486 0.45 134388. 0.3020
|
|
32.81 0.3093 0.6186 0.0305 0.0153 0.338 2.664 2.392 252.174 0.301 10.638 4.302 0.45 134526. 0.2788
|
|
34.73 0.3275 0.6263 0.0281 0.0147 0.325 2.563 2.200 242.574 0.290 9.785 4.113 0.45 134670. 0.2557
|
|
36.66 0.3457 0.6300 0.0256 0.0140 0.311 2.450 2.004 231.916 0.277 8.915 3.920 0.45 134821. 0.2326
|
|
38.59 0.3639 0.6291 0.0230 0.0133 0.295 2.326 1.805 220.177 0.263 8.029 3.718 0.45 134977. 0.2094
|
|
40.52 0.3821 0.6228 0.0205 0.0125 0.278 2.191 1.603 207.338 0.247 7.128 3.506 0.45 135140. 0.1860
|
|
42.45 0.4003 0.6099 0.0178 0.0117 0.259 2.043 1.397 193.386 0.231 6.215 3.277 0.45 135309. 0.1623
|
|
44.38 0.4185 0.5886 0.0152 0.0108 0.239 1.884 1.189 178.317 0.213 5.290 3.025 0.45 135485. 0.1383
|
|
46.31 0.4367 0.5564 0.0125 0.0098 0.217 1.713 0.980 162.134 0.194 4.357 2.740 0.45 135667. 0.1137
|
|
48.24 0.4549 0.5088 0.0098 0.0088 0.194 1.530 0.768 144.851 0.173 3.417 2.406 0.45 135856. 0.0884
|
|
50.17 0.4731 0.4386 0.0071 0.0077 0.170 1.336 0.556 126.493 0.151 2.474 1.994 0.45 136051. 0.0623
|
|
52.10 0.4913 0.3326 0.0044 0.0065 0.144 1.132 0.344 107.096 0.128 1.529 1.456 0.45 136252. 0.0358
|
|
54.03 0.5094 0.1633 0.0017 0.0052 0.116 0.916 0.132 86.678 0.103 0.586 0.690 0.45 136456. 0.0105
|
|
55.96 0.5276
|
|
|
|
|
|
|
|
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 0.0623 0.0174 0.548 3.838 6.178 408.642 0.434 27.481 6.858 0.50 149528. 0.7144
|
|
2.16 0.0181 0.0630 0.0611 0.0175 0.553 3.872 6.058 412.330 0.437 26.947 6.664 0.50 149591. 0.6875
|
|
4.31 0.0361 0.1223 0.0598 0.0177 0.557 3.903 5.931 415.560 0.441 26.379 6.473 0.50 149658. 0.6607
|
|
6.47 0.0542 0.1782 0.0584 0.0178 0.561 3.928 5.795 418.247 0.444 25.777 6.285 0.50 149731. 0.6341
|
|
8.62 0.0723 0.2306 0.0570 0.0179 0.564 3.947 5.652 420.309 0.446 25.139 6.099 0.50 149808. 0.6077
|
|
10.78 0.0903 0.2796 0.0555 0.0179 0.565 3.960 5.500 421.663 0.447 24.464 5.916 0.50 149890. 0.5815
|
|
12.93 0.1084 0.3253 0.0539 0.0179 0.566 3.965 5.340 422.228 0.448 23.753 5.737 0.50 149977. 0.5556
|
|
15.09 0.1265 0.3678 0.0522 0.0179 0.566 3.962 5.172 421.929 0.448 23.006 5.560 0.50 150070. 0.5300
|
|
17.25 0.1445 0.4072 0.0504 0.0179 0.564 3.951 4.996 420.699 0.446 22.223 5.387 0.50 150168. 0.5046
|
|
19.40 0.1626 0.4436 0.0485 0.0178 0.561 3.930 4.812 418.477 0.444 21.405 5.216 0.50 150272. 0.4795
|
|
21.56 0.1807 0.4770 0.0466 0.0176 0.557 3.899 4.621 415.202 0.441 20.553 5.048 0.50 150382. 0.4548
|
|
23.71 0.1987 0.5075 0.0446 0.0175 0.551 3.858 4.422 410.820 0.436 19.668 4.882 0.50 150497. 0.4303
|
|
25.87 0.2168 0.5351 0.0425 0.0172 0.543 3.806 4.216 405.274 0.430 18.752 4.718 0.50 150619. 0.4060
|
|
28.02 0.2349 0.5597 0.0404 0.0169 0.534 3.743 4.003 398.509 0.423 17.805 4.556 0.50 150746. 0.3820
|
|
30.18 0.2529 0.5815 0.0382 0.0166 0.524 3.667 3.784 390.473 0.414 16.830 4.395 0.50 150881. 0.3583
|
|
32.34 0.2710 0.6003 0.0359 0.0162 0.511 3.579 3.558 381.113 0.404 15.826 4.234 0.50 151021. 0.3348
|
|
34.49 0.2891 0.6160 0.0335 0.0157 0.497 3.478 3.326 370.380 0.393 14.796 4.074 0.50 151168. 0.3114
|
|
36.65 0.3071 0.6284 0.0312 0.0152 0.480 3.364 3.089 358.228 0.380 13.741 3.911 0.50 151322. 0.2881
|
|
38.80 0.3252 0.6374 0.0287 0.0146 0.462 3.236 2.847 344.612 0.366 12.662 3.747 0.50 151482. 0.2650
|
|
40.96 0.3433 0.6425 0.0262 0.0140 0.442 3.094 2.599 329.494 0.350 11.562 3.578 0.50 151649. 0.2418
|
|
43.11 0.3613 0.6432 0.0237 0.0133 0.420 2.938 2.347 312.840 0.332 10.440 3.403 0.50 151824. 0.2185
|
|
45.27 0.3794 0.6389 0.0211 0.0125 0.395 2.767 2.091 294.624 0.313 9.301 3.219 0.50 152005. 0.1951
|
|
47.43 0.3975 0.6283 0.0185 0.0117 0.369 2.581 1.831 274.825 0.292 8.144 3.022 0.50 152193. 0.1714
|
|
49.58 0.4155 0.6099 0.0158 0.0108 0.340 2.380 1.568 253.436 0.269 6.974 2.806 0.50 152388. 0.1472
|
|
51.74 0.4336 0.5812 0.0131 0.0098 0.309 2.164 1.302 230.458 0.245 5.791 2.562 0.50 152590. 0.1225
|
|
53.89 0.4517 0.5382 0.0104 0.0088 0.276 1.934 1.034 205.909 0.218 4.600 2.278 0.50 152800. 0.0971
|
|
56.05 0.4697 0.4742 0.0077 0.0076 0.241 1.689 0.765 179.822 0.191 3.403 1.930 0.51 153016. 0.0707
|
|
58.20 0.4878 0.3768 0.0050 0.0065 0.204 1.430 0.496 152.247 0.162 2.205 1.477 0.51 153240. 0.0436
|
|
60.36 0.5059 0.2206 0.0023 0.0052 0.165 1.157 0.226 123.224 0.131 1.007 0.834 0.51 153468. 0.0166
|
|
62.52 0.5239
|
|
|
|
|
|
|
|
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 0.0630 0.0174 0.753 4.745 7.711 561.401 0.536 34.301 6.230 0.56 166134. 0.7251
|
|
2.38 0.0180 0.0633 0.0618 0.0176 0.760 4.788 7.563 566.494 0.541 33.640 6.055 0.56 166204. 0.6980
|
|
4.77 0.0360 0.1230 0.0605 0.0177 0.766 4.826 7.405 570.951 0.545 32.938 5.883 0.56 166279. 0.6709
|
|
7.15 0.0539 0.1791 0.0591 0.0178 0.771 4.857 7.237 574.655 0.549 32.192 5.712 0.56 166360. 0.6441
|
|
9.54 0.0719 0.2318 0.0577 0.0179 0.774 4.881 7.060 577.495 0.551 31.403 5.545 0.56 166445. 0.6175
|
|
11.92 0.0899 0.2811 0.0561 0.0180 0.777 4.897 6.872 579.354 0.553 30.568 5.380 0.56 166536. 0.5911
|
|
14.30 0.1079 0.3272 0.0545 0.0180 0.778 4.903 6.675 580.123 0.554 29.689 5.219 0.56 166633. 0.5651
|
|
16.69 0.1259 0.3701 0.0528 0.0180 0.777 4.900 6.467 579.698 0.554 28.763 5.060 0.56 166736. 0.5393
|
|
19.07 0.1438 0.4100 0.0510 0.0179 0.775 4.885 6.249 577.986 0.552 27.794 4.904 0.56 166845. 0.5137
|
|
21.45 0.1618 0.4468 0.0492 0.0178 0.771 4.859 6.021 574.904 0.549 26.781 4.750 0.56 166959. 0.4885
|
|
23.84 0.1798 0.4807 0.0472 0.0177 0.765 4.821 5.784 570.371 0.545 25.726 4.599 0.56 167081. 0.4636
|
|
26.22 0.1978 0.5116 0.0452 0.0175 0.757 4.770 5.537 564.310 0.539 24.630 4.451 0.56 167209. 0.4390
|
|
28.61 0.2158 0.5398 0.0431 0.0172 0.746 4.705 5.282 556.645 0.532 23.495 4.304 0.56 167343. 0.4146
|
|
30.99 0.2338 0.5651 0.0410 0.0170 0.734 4.626 5.019 547.301 0.523 22.323 4.159 0.56 167484. 0.3905
|
|
33.37 0.2517 0.5875 0.0388 0.0166 0.719 4.532 4.747 536.208 0.512 21.114 4.015 0.56 167632. 0.3667
|
|
35.76 0.2697 0.6070 0.0365 0.0162 0.702 4.423 4.467 523.294 0.500 19.871 3.872 0.56 167788. 0.3430
|
|
38.14 0.2877 0.6235 0.0341 0.0158 0.682 4.298 4.180 508.491 0.486 18.594 3.729 0.56 167950. 0.3195
|
|
40.53 0.3057 0.6369 0.0317 0.0152 0.659 4.156 3.886 491.735 0.470 17.287 3.585 0.56 168120. 0.2962
|
|
42.91 0.3237 0.6469 0.0293 0.0147 0.634 3.998 3.586 472.966 0.452 15.950 3.439 0.56 168297. 0.2729
|
|
45.29 0.3416 0.6532 0.0268 0.0140 0.606 3.822 3.279 452.131 0.432 14.585 3.289 0.56 168481. 0.2496
|
|
47.68 0.3596 0.6553 0.0242 0.0133 0.576 3.628 2.966 429.183 0.410 13.195 3.135 0.56 168673. 0.2263
|
|
50.06 0.3776 0.6525 0.0216 0.0125 0.542 3.415 2.649 404.084 0.386 11.781 2.973 0.56 168873. 0.2028
|
|
52.44 0.3956 0.6438 0.0190 0.0117 0.505 3.185 2.326 376.806 0.360 10.347 2.800 0.56 169080. 0.1790
|
|
54.83 0.4136 0.6276 0.0163 0.0108 0.466 2.936 2.000 347.335 0.332 8.894 2.611 0.56 169295. 0.1548
|
|
57.21 0.4315 0.6017 0.0136 0.0098 0.423 2.668 1.670 315.674 0.301 7.426 2.399 0.56 169518. 0.1299
|
|
59.60 0.4495 0.5622 0.0109 0.0087 0.378 2.382 1.337 281.842 0.269 5.947 2.152 0.56 169749. 0.1043
|
|
61.98 0.4675 0.5026 0.0082 0.0076 0.330 2.078 1.003 245.883 0.235 4.460 1.850 0.56 169988. 0.0776
|
|
64.36 0.4855 0.4112 0.0055 0.0064 0.279 1.757 0.668 207.863 0.198 2.970 1.457 0.56 170234. 0.0499
|
|
66.75 0.5035 0.2634 0.0027 0.0052 0.225 1.419 0.333 167.847 0.160 1.482 0.900 0.56 170486. 0.0218
|
|
69.13 0.5215 -0.0083 -0.0001 0.0039 0.168 1.056 -0.008 124.928 0.119 -0.034 -0.027 0.56 170703. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 11000
|
|
|
|
V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
|
|
(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
|
|
0.00 0.0000 0.0000 0.0638 0.0175 1.008 5.775 9.449 751.599 0.652 42.029 5.702 0.61 182737. 0.7346
|
|
2.62 0.0180 0.0638 0.0626 0.0177 1.017 5.828 9.268 758.459 0.658 41.223 5.542 0.61 182815. 0.7072
|
|
5.25 0.0360 0.1239 0.0613 0.0178 1.025 5.874 9.075 764.447 0.664 40.365 5.384 0.61 182898. 0.6798
|
|
7.87 0.0540 0.1805 0.0599 0.0179 1.032 5.912 8.870 769.405 0.668 39.454 5.229 0.61 182987. 0.6527
|
|
10.50 0.0720 0.2337 0.0584 0.0180 1.037 5.941 8.653 773.181 0.671 38.489 5.076 0.61 183082. 0.6258
|
|
13.12 0.0900 0.2834 0.0569 0.0181 1.040 5.960 8.424 775.619 0.673 37.469 4.926 0.61 183183. 0.5992
|
|
15.75 0.1080 0.3299 0.0552 0.0181 1.041 5.967 8.182 776.567 0.674 36.392 4.779 0.61 183290. 0.5729
|
|
18.37 0.1260 0.3733 0.0535 0.0181 1.040 5.962 7.927 775.888 0.674 35.260 4.634 0.61 183404. 0.5468
|
|
21.00 0.1440 0.4135 0.0517 0.0180 1.037 5.943 7.660 773.455 0.671 34.073 4.492 0.61 183524. 0.5211
|
|
23.62 0.1620 0.4508 0.0498 0.0179 1.031 5.910 7.381 769.154 0.668 32.832 4.353 0.61 183651. 0.4956
|
|
26.25 0.1800 0.4851 0.0479 0.0178 1.023 5.862 7.091 762.879 0.662 31.539 4.216 0.61 183785. 0.4705
|
|
28.87 0.1980 0.5166 0.0458 0.0176 1.012 5.798 6.789 754.525 0.655 30.197 4.081 0.61 183926. 0.4457
|
|
31.50 0.2160 0.5452 0.0437 0.0173 0.998 5.717 6.476 743.993 0.646 28.806 3.948 0.61 184075. 0.4211
|
|
34.12 0.2340 0.5710 0.0415 0.0170 0.981 5.618 6.153 731.182 0.635 27.368 3.817 0.61 184231. 0.3968
|
|
36.75 0.2520 0.5939 0.0393 0.0167 0.960 5.502 5.820 715.996 0.622 25.886 3.687 0.61 184395. 0.3728
|
|
39.37 0.2700 0.6140 0.0370 0.0163 0.936 5.366 5.477 698.340 0.606 24.361 3.557 0.61 184566. 0.3489
|
|
42.00 0.2880 0.6311 0.0346 0.0158 0.909 5.211 5.125 678.123 0.589 22.796 3.428 0.61 184745. 0.3253
|
|
44.62 0.3060 0.6452 0.0322 0.0153 0.879 5.035 4.764 655.259 0.569 21.192 3.298 0.61 184932. 0.3017
|
|
47.25 0.3240 0.6559 0.0297 0.0147 0.844 4.838 4.396 629.669 0.547 19.552 3.166 0.61 185128. 0.2782
|
|
49.87 0.3420 0.6629 0.0271 0.0140 0.806 4.620 4.019 601.278 0.522 17.878 3.032 0.61 185331. 0.2548
|
|
52.50 0.3600 0.6658 0.0245 0.0133 0.764 4.380 3.636 570.026 0.495 16.173 2.893 0.61 185543. 0.2312
|
|
55.12 0.3780 0.6640 0.0219 0.0125 0.719 4.117 3.246 535.859 0.465 14.438 2.748 0.62 185764. 0.2075
|
|
57.75 0.3960 0.6562 0.0192 0.0116 0.669 3.832 2.850 498.741 0.433 12.678 2.592 0.62 185992. 0.1834
|
|
60.37 0.4140 0.6411 0.0165 0.0107 0.615 3.524 2.449 458.655 0.398 10.895 2.422 0.62 186230. 0.1589
|
|
63.00 0.4320 0.6162 0.0138 0.0097 0.557 3.193 2.044 415.602 0.361 9.093 2.231 0.62 186476. 0.1337
|
|
65.62 0.4500 0.5776 0.0110 0.0086 0.496 2.840 1.636 369.611 0.321 7.277 2.008 0.62 186730. 0.1076
|
|
68.25 0.4680 0.5186 0.0083 0.0075 0.430 2.465 1.226 320.741 0.278 5.452 1.733 0.62 186993. 0.0804
|
|
70.87 0.4860 0.4265 0.0055 0.0063 0.361 2.068 0.814 269.083 0.234 3.623 1.373 0.62 187264. 0.0519
|
|
73.50 0.5040 0.2746 0.0027 0.0050 0.288 1.650 0.404 214.726 0.186 1.795 0.852 0.62 187542. 0.0227
|
|
76.12 0.5220 -0.0168 -0.0001 0.0036 0.209 1.199 -0.017 156.054 0.135 -0.077 -0.050 0.62 187766. 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 0.0647 0.0177 1.322 6.944 11.409 985.814 0.784 50.745 5.249 0.67 199336. 0.7431
|
|
2.87 0.0180 0.0641 0.0635 0.0178 1.334 7.007 11.191 994.819 0.792 49.778 5.102 0.67 199421. 0.7154
|
|
5.73 0.0360 0.1246 0.0622 0.0180 1.345 7.062 10.959 1002.652 0.798 48.746 4.958 0.67 199513. 0.6878
|
|
8.60 0.0540 0.1815 0.0608 0.0181 1.353 7.108 10.713 1009.107 0.803 47.651 4.815 0.67 199611. 0.6605
|
|
11.46 0.0721 0.2350 0.0593 0.0182 1.360 7.142 10.452 1013.980 0.807 46.489 4.675 0.67 199715. 0.6335
|
|
14.33 0.0901 0.2851 0.0577 0.0182 1.364 7.164 10.175 1017.067 0.809 45.261 4.538 0.67 199826. 0.6067
|
|
17.20 0.1081 0.3319 0.0561 0.0183 1.365 7.171 9.884 1018.167 0.810 43.964 4.403 0.67 199944. 0.5802
|
|
20.06 0.1261 0.3756 0.0543 0.0182 1.364 7.164 9.577 1017.094 0.809 42.599 4.271 0.67 200069. 0.5539
|
|
22.93 0.1441 0.4162 0.0525 0.0182 1.359 7.140 9.255 1013.684 0.807 41.167 4.141 0.67 200201. 0.5280
|
|
25.79 0.1621 0.4539 0.0506 0.0181 1.351 7.098 8.919 1007.788 0.802 39.670 4.014 0.67 200340. 0.5024
|
|
28.66 0.1801 0.4886 0.0486 0.0179 1.340 7.038 8.568 999.266 0.795 38.110 3.889 0.67 200487. 0.4771
|
|
31.53 0.1982 0.5205 0.0465 0.0177 1.325 6.959 8.204 987.981 0.786 36.489 3.766 0.67 200642. 0.4521
|
|
34.39 0.2162 0.5496 0.0444 0.0175 1.306 6.859 7.826 973.804 0.775 34.810 3.645 0.67 200805. 0.4274
|
|
37.26 0.2342 0.5759 0.0422 0.0172 1.283 6.738 7.436 956.605 0.761 33.074 3.526 0.67 200976. 0.4029
|
|
40.12 0.2522 0.5993 0.0399 0.0168 1.256 6.595 7.033 936.260 0.745 31.284 3.407 0.67 201156. 0.3787
|
|
42.99 0.2702 0.6200 0.0375 0.0164 1.224 6.428 6.619 912.640 0.726 29.442 3.290 0.67 201343. 0.3547
|
|
45.86 0.2882 0.6377 0.0351 0.0159 1.188 6.238 6.194 885.631 0.705 27.551 3.172 0.67 201540. 0.3309
|
|
48.72 0.3062 0.6524 0.0327 0.0153 1.147 6.023 5.758 855.120 0.680 25.613 3.054 0.67 201745. 0.3072
|
|
51.59 0.3243 0.6638 0.0301 0.0147 1.101 5.783 5.313 821.001 0.653 23.631 2.935 0.67 201958. 0.2835
|
|
54.45 0.3423 0.6716 0.0276 0.0140 1.050 5.516 4.858 783.179 0.623 21.607 2.813 0.67 202181. 0.2599
|
|
57.32 0.3603 0.6754 0.0249 0.0133 0.994 5.223 4.394 741.572 0.590 19.545 2.688 0.67 202413. 0.2361
|
|
60.18 0.3783 0.6744 0.0223 0.0125 0.934 4.903 3.923 696.112 0.554 17.448 2.556 0.67 202654. 0.2122
|
|
63.05 0.3963 0.6676 0.0195 0.0116 0.867 4.555 3.444 646.752 0.515 15.319 2.415 0.67 202904. 0.1879
|
|
65.92 0.4143 0.6536 0.0168 0.0106 0.796 4.180 2.959 593.467 0.472 13.163 2.262 0.67 203164. 0.1631
|
|
68.78 0.4323 0.6298 0.0140 0.0096 0.719 3.777 2.469 536.260 0.427 10.984 2.089 0.67 203433. 0.1376
|
|
71.65 0.4504 0.5923 0.0112 0.0085 0.637 3.347 1.975 475.170 0.378 8.787 1.886 0.67 203711. 0.1111
|
|
74.51 0.4684 0.5341 0.0084 0.0074 0.550 2.890 1.479 410.279 0.326 6.578 1.635 0.67 203999. 0.0833
|
|
77.38 0.4864 0.4419 0.0056 0.0061 0.458 2.407 0.981 341.713 0.272 4.365 1.303 0.67 204295. 0.0541
|
|
80.25 0.5044 0.2865 0.0027 0.0048 0.362 1.899 0.484 269.602 0.215 2.153 0.814 0.67 204599. 0.0237
|
|
83.11 0.5224 -0.0255 -0.0002 0.0034 0.256 1.346 -0.030 191.128 0.152 -0.131 -0.070 0.68 204820. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 13000
|
|
|
|
V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
|
|
(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
|
|
0.00 0.0000 0.0000 0.0658 0.0180 1.708 8.282 13.613 1273.831 0.936 60.552 4.847 0.72 215930. 0.7496
|
|
3.14 0.0182 0.0649 0.0645 0.0181 1.723 8.355 13.353 1285.071 0.944 59.393 4.713 0.72 216025. 0.7218
|
|
6.28 0.0364 0.1261 0.0632 0.0183 1.736 8.419 13.075 1294.825 0.951 58.156 4.580 0.72 216126. 0.6941
|
|
9.42 0.0546 0.1837 0.0618 0.0184 1.747 8.470 12.779 1302.803 0.957 56.840 4.449 0.72 216234. 0.6666
|
|
12.56 0.0729 0.2378 0.0602 0.0185 1.755 8.509 12.465 1308.726 0.961 55.443 4.320 0.72 216349. 0.6392
|
|
15.70 0.0911 0.2886 0.0586 0.0185 1.760 8.532 12.132 1312.304 0.964 53.963 4.193 0.72 216472. 0.6121
|
|
18.84 0.1093 0.3360 0.0569 0.0185 1.761 8.538 11.780 1313.251 0.965 52.400 4.069 0.72 216602. 0.5853
|
|
21.98 0.1275 0.3802 0.0551 0.0185 1.758 8.526 11.410 1311.311 0.963 50.752 3.947 0.72 216741. 0.5587
|
|
25.12 0.1457 0.4214 0.0533 0.0184 1.752 8.493 11.021 1306.248 0.960 49.023 3.827 0.72 216887. 0.5325
|
|
28.26 0.1639 0.4595 0.0513 0.0183 1.740 8.438 10.615 1297.857 0.953 47.213 3.710 0.72 217041. 0.5065
|
|
31.39 0.1822 0.4947 0.0493 0.0181 1.724 8.361 10.190 1285.951 0.945 45.327 3.594 0.72 217204. 0.4809
|
|
34.53 0.2004 0.5270 0.0471 0.0179 1.704 8.259 9.749 1270.354 0.933 43.366 3.481 0.72 217376. 0.4555
|
|
37.67 0.2186 0.5565 0.0449 0.0176 1.677 8.133 9.292 1250.893 0.919 41.333 3.369 0.72 217556. 0.4305
|
|
40.81 0.2368 0.5832 0.0426 0.0173 1.646 7.980 8.820 1227.399 0.902 39.231 3.259 0.72 217745. 0.4057
|
|
43.95 0.2550 0.6070 0.0403 0.0169 1.609 7.800 8.333 1199.705 0.881 37.063 3.150 0.72 217944. 0.3811
|
|
47.09 0.2732 0.6280 0.0378 0.0165 1.566 7.592 7.831 1167.649 0.858 34.832 3.042 0.72 218152. 0.3568
|
|
50.23 0.2915 0.6461 0.0354 0.0160 1.517 7.354 7.316 1131.076 0.831 32.541 2.934 0.73 218369. 0.3326
|
|
53.37 0.3097 0.6610 0.0328 0.0154 1.461 7.086 6.788 1089.839 0.801 30.193 2.825 0.73 218596. 0.3085
|
|
56.51 0.3279 0.6726 0.0302 0.0147 1.400 6.787 6.248 1043.800 0.767 27.792 2.715 0.73 218833. 0.2844
|
|
59.65 0.3461 0.6806 0.0275 0.0140 1.331 6.455 5.697 992.837 0.729 25.340 2.603 0.73 219080. 0.2603
|
|
62.79 0.3643 0.6844 0.0248 0.0132 1.256 6.091 5.135 936.847 0.688 22.841 2.486 0.73 219336. 0.2361
|
|
65.93 0.3825 0.6832 0.0221 0.0124 1.174 5.694 4.564 875.755 0.643 20.300 2.364 0.73 219603. 0.2116
|
|
69.07 0.4008 0.6759 0.0193 0.0114 1.086 5.263 3.984 809.520 0.595 17.721 2.232 0.73 219880. 0.1867
|
|
72.21 0.4190 0.6607 0.0164 0.0104 0.990 4.799 3.397 738.141 0.542 15.109 2.087 0.73 220167. 0.1612
|
|
75.35 0.4372 0.6348 0.0136 0.0093 0.887 4.302 2.803 661.662 0.486 12.470 1.922 0.73 220465. 0.1349
|
|
78.49 0.4554 0.5933 0.0107 0.0082 0.778 3.772 2.206 580.191 0.426 9.810 1.724 0.73 220772. 0.1073
|
|
81.63 0.4736 0.5274 0.0078 0.0070 0.662 3.211 1.605 493.906 0.363 7.138 1.474 0.73 221090. 0.0782
|
|
84.77 0.4918 0.4195 0.0048 0.0057 0.541 2.621 1.003 403.052 0.296 4.462 1.129 0.73 221418. 0.0474
|
|
87.91 0.5100 0.2281 0.0019 0.0043 0.413 2.001 0.402 307.810 0.226 1.787 0.592 0.73 221751. 0.0157
|
|
91.05 0.5283
|
|
|
|
|
|
|
|
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 0.0671 0.0186 2.211 9.953 16.093 1648.535 1.124 71.580 4.428 0.78 232518. 0.7444
|
|
3.35 0.0180 0.0633 0.0658 0.0187 2.225 10.016 15.791 1659.029 1.132 70.239 4.317 0.78 232619. 0.7190
|
|
6.69 0.0361 0.1234 0.0645 0.0188 2.237 10.069 15.469 1667.835 1.138 68.807 4.207 0.78 232728. 0.6935
|
|
10.04 0.0541 0.1803 0.0630 0.0189 2.246 10.110 15.127 1674.639 1.142 67.283 4.097 0.78 232844. 0.6678
|
|
13.38 0.0721 0.2340 0.0615 0.0190 2.252 10.137 14.763 1679.117 1.145 65.664 3.988 0.78 232968. 0.6422
|
|
16.73 0.0901 0.2845 0.0599 0.0190 2.254 10.148 14.377 1680.938 1.147 63.948 3.879 0.78 233100. 0.6165
|
|
20.07 0.1082 0.3320 0.0582 0.0190 2.253 10.141 13.969 1679.765 1.146 62.134 3.772 0.78 233239. 0.5909
|
|
23.42 0.1262 0.3764 0.0564 0.0189 2.247 10.114 13.539 1675.279 1.143 60.222 3.666 0.78 233387. 0.5653
|
|
26.77 0.1442 0.4178 0.0545 0.0188 2.236 10.065 13.088 1667.194 1.137 58.214 3.561 0.78 233543. 0.5399
|
|
30.11 0.1622 0.4563 0.0526 0.0187 2.220 9.993 12.615 1655.243 1.129 56.111 3.457 0.78 233708. 0.5146
|
|
33.46 0.1803 0.4920 0.0505 0.0185 2.198 9.896 12.122 1639.170 1.118 53.918 3.354 0.78 233882. 0.4895
|
|
36.80 0.1983 0.5248 0.0484 0.0183 2.171 9.773 11.609 1618.727 1.104 51.637 3.253 0.78 234065. 0.4645
|
|
40.15 0.2163 0.5549 0.0462 0.0180 2.137 9.621 11.077 1593.667 1.087 49.272 3.153 0.78 234257. 0.4398
|
|
43.50 0.2343 0.5823 0.0439 0.0177 2.097 9.441 10.528 1563.740 1.067 46.826 3.054 0.78 234458. 0.4152
|
|
46.84 0.2524 0.6068 0.0415 0.0173 2.050 9.229 9.960 1528.711 1.043 44.303 2.955 0.78 234669. 0.3909
|
|
50.19 0.2704 0.6287 0.0391 0.0168 1.996 8.986 9.376 1488.353 1.015 41.705 2.857 0.78 234890. 0.3667
|
|
53.53 0.2884 0.6476 0.0366 0.0163 1.934 8.709 8.776 1442.458 0.984 39.037 2.760 0.78 235121. 0.3426
|
|
56.88 0.3064 0.6637 0.0340 0.0157 1.865 8.397 8.161 1390.843 0.949 36.302 2.661 0.78 235362. 0.3187
|
|
60.22 0.3245 0.6765 0.0314 0.0151 1.788 8.050 7.532 1333.346 0.909 33.503 2.562 0.78 235613. 0.2947
|
|
63.57 0.3425 0.6858 0.0287 0.0143 1.703 7.667 6.889 1269.859 0.866 30.644 2.461 0.78 235875. 0.2707
|
|
66.92 0.3605 0.6911 0.0260 0.0136 1.610 7.247 6.234 1200.286 0.819 27.730 2.356 0.78 236147. 0.2465
|
|
70.26 0.3786 0.6917 0.0232 0.0127 1.508 6.790 5.567 1124.595 0.767 24.764 2.245 0.78 236429. 0.2221
|
|
73.61 0.3966 0.6864 0.0204 0.0118 1.398 6.296 4.890 1042.793 0.711 21.752 2.127 0.78 236722. 0.1972
|
|
76.95 0.4146 0.6737 0.0175 0.0108 1.281 5.765 4.204 954.955 0.651 18.700 1.997 0.78 237026. 0.1716
|
|
80.30 0.4326 0.6508 0.0146 0.0097 1.155 5.199 3.510 861.227 0.587 15.614 1.849 0.78 237341. 0.1452
|
|
83.64 0.4507 0.6135 0.0117 0.0086 1.022 4.599 2.810 761.838 0.520 12.500 1.673 0.79 237667. 0.1176
|
|
86.99 0.4687 0.5544 0.0088 0.0074 0.881 3.967 2.106 657.110 0.448 9.368 1.454 0.79 238003. 0.0884
|
|
90.34 0.4867 0.4593 0.0058 0.0062 0.734 3.305 1.400 547.464 0.373 6.226 1.160 0.79 238350. 0.0575
|
|
93.68 0.5047 0.2981 0.0029 0.0049 0.581 2.616 0.693 433.339 0.296 3.085 0.726 0.79 238704. 0.0253
|
|
97.03 0.5228 -0.0229 -0.0002 0.0035 0.415 1.870 -0.037 309.817 0.211 -0.163 -0.054 0.79 238957. 0.0000
|
|
|
|
|
|
|
|
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 0.0685 0.0202 2.953 12.407 18.880 2201.778 1.402 83.979 3.889 0.83 249097. 0.7083
|
|
3.60 0.0181 0.0602 0.0673 0.0202 2.956 12.421 18.530 2204.380 1.403 82.423 3.813 0.83 249208. 0.6879
|
|
7.21 0.0362 0.1180 0.0659 0.0202 2.957 12.424 18.156 2204.866 1.404 80.757 3.735 0.83 249326. 0.6670
|
|
10.81 0.0544 0.1732 0.0645 0.0202 2.954 12.413 17.756 2202.923 1.402 78.981 3.656 0.83 249453. 0.6457
|
|
14.41 0.0725 0.2259 0.0629 0.0202 2.948 12.387 17.331 2198.219 1.399 77.090 3.576 0.83 249587. 0.6240
|
|
18.01 0.0906 0.2760 0.0613 0.0201 2.937 12.343 16.880 2190.413 1.394 75.083 3.495 0.83 249730. 0.6019
|
|
21.62 0.1087 0.3235 0.0595 0.0200 2.922 12.279 16.402 2179.159 1.387 72.957 3.414 0.83 249882. 0.5795
|
|
25.22 0.1268 0.3684 0.0577 0.0199 2.902 12.195 15.898 2164.135 1.378 70.713 3.332 0.83 250043. 0.5568
|
|
28.82 0.1449 0.4106 0.0558 0.0197 2.877 12.087 15.367 2145.033 1.366 68.354 3.249 0.83 250213. 0.5339
|
|
32.43 0.1631 0.4501 0.0538 0.0195 2.845 11.955 14.811 2121.580 1.351 65.881 3.166 0.83 250393. 0.5108
|
|
36.03 0.1812 0.4870 0.0517 0.0192 2.807 11.796 14.231 2093.497 1.333 63.299 3.083 0.83 250582. 0.4875
|
|
39.63 0.1993 0.5212 0.0495 0.0189 2.763 11.611 13.627 2060.505 1.312 60.612 3.000 0.83 250780. 0.4641
|
|
43.23 0.2174 0.5526 0.0472 0.0186 2.712 11.395 13.000 2022.316 1.287 57.824 2.916 0.83 250989. 0.4406
|
|
46.84 0.2355 0.5814 0.0448 0.0182 2.653 11.149 12.351 1978.629 1.260 54.938 2.831 0.84 251208. 0.4170
|
|
50.44 0.2536 0.6073 0.0424 0.0177 2.587 10.870 11.682 1929.133 1.228 51.960 2.747 0.84 251437. 0.3934
|
|
54.04 0.2718 0.6305 0.0399 0.0172 2.512 10.557 10.992 1873.509 1.193 48.894 2.661 0.84 251677. 0.3698
|
|
57.64 0.2899 0.6505 0.0373 0.0166 2.430 10.210 10.284 1812.002 1.154 45.742 2.574 0.84 251928. 0.3460
|
|
61.25 0.3080 0.6672 0.0347 0.0160 2.339 9.830 9.557 1744.484 1.111 42.510 2.485 0.84 252189. 0.3220
|
|
64.85 0.3261 0.6803 0.0320 0.0153 2.240 9.413 8.813 1670.592 1.064 39.202 2.393 0.84 252462. 0.2977
|
|
68.45 0.3442 0.6892 0.0292 0.0146 2.133 8.963 8.053 1590.617 1.013 35.822 2.296 0.84 252745. 0.2731
|
|
72.06 0.3623 0.6935 0.0264 0.0138 2.017 8.473 7.279 1503.735 0.957 32.375 2.195 0.84 253040. 0.2482
|
|
75.66 0.3805 0.6925 0.0236 0.0129 1.891 7.945 6.490 1409.981 0.898 28.868 2.088 0.84 253346. 0.2229
|
|
79.26 0.3986 0.6847 0.0207 0.0120 1.756 7.379 5.689 1309.584 0.834 25.305 1.970 0.84 253664. 0.1970
|
|
82.86 0.4167 0.6681 0.0177 0.0110 1.613 6.778 4.877 1202.796 0.766 21.693 1.839 0.84 253993. 0.1702
|
|
86.47 0.4348 0.6398 0.0147 0.0100 1.462 6.142 4.056 1090.010 0.694 18.041 1.688 0.84 254334. 0.1425
|
|
90.07 0.4529 0.5949 0.0117 0.0089 1.303 5.476 3.227 971.730 0.619 14.356 1.506 0.84 254686. 0.1134
|
|
93.67 0.4710 0.5255 0.0087 0.0078 1.138 4.782 2.394 848.585 0.540 10.649 1.280 0.84 255050. 0.0830
|
|
97.28 0.4892 0.4179 0.0057 0.0066 0.967 4.065 1.559 721.319 0.459 6.932 0.980 0.84 255425. 0.0513
|
|
100.88 0.5073 0.2455 0.0026 0.0054 0.792 3.328 0.723 590.606 0.376 3.216 0.555 0.84 255808. 0.0198
|
|
104.48 0.5254
|
|
|
|
|
|
|
|
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 0.0700 0.0233 4.139 16.305 21.946 3086.468 1.842 97.616 3.225 0.89 265670. 0.6332
|
|
3.85 0.0182 0.0537 0.0688 0.0232 4.120 16.230 21.553 3072.269 1.834 95.868 3.182 0.89 265789. 0.6191
|
|
7.70 0.0363 0.1059 0.0674 0.0231 4.096 16.136 21.130 3054.458 1.823 93.988 3.138 0.89 265917. 0.6045
|
|
11.55 0.0545 0.1566 0.0660 0.0229 4.067 16.021 20.678 3032.831 1.810 91.974 3.092 0.89 266053. 0.5894
|
|
15.40 0.0726 0.2057 0.0644 0.0227 4.033 15.886 20.194 3007.154 1.795 89.822 3.046 0.89 266198. 0.5737
|
|
19.25 0.0908 0.2531 0.0628 0.0225 3.992 15.727 19.678 2977.194 1.777 87.529 2.998 0.89 266353. 0.5574
|
|
23.11 0.1089 0.2987 0.0610 0.0223 3.946 15.545 19.131 2942.738 1.756 85.093 2.949 0.89 266516. 0.5405
|
|
26.96 0.1271 0.3425 0.0592 0.0220 3.894 15.339 18.551 2903.581 1.733 82.514 2.898 0.89 266690. 0.5231
|
|
30.81 0.1452 0.3843 0.0572 0.0216 3.835 15.106 17.940 2859.545 1.707 79.795 2.846 0.89 266874. 0.5051
|
|
34.66 0.1634 0.4242 0.0552 0.0213 3.769 14.847 17.298 2810.465 1.677 76.940 2.792 0.89 267067. 0.4866
|
|
38.51 0.1815 0.4619 0.0530 0.0208 3.696 14.560 16.626 2756.157 1.645 73.952 2.736 0.89 267271. 0.4676
|
|
42.36 0.1997 0.4975 0.0508 0.0204 3.616 14.244 15.926 2696.434 1.609 70.838 2.679 0.89 267485. 0.4481
|
|
46.21 0.2179 0.5308 0.0485 0.0199 3.528 13.899 15.198 2631.089 1.570 67.601 2.620 0.89 267710. 0.4281
|
|
50.06 0.2360 0.5617 0.0461 0.0194 3.433 13.523 14.444 2559.885 1.528 64.248 2.559 0.89 267946. 0.4077
|
|
53.91 0.2542 0.5901 0.0436 0.0188 3.329 13.114 13.665 2482.558 1.482 60.783 2.497 0.89 268193. 0.3868
|
|
57.76 0.2723 0.6159 0.0410 0.0181 3.217 12.672 12.862 2398.791 1.432 57.212 2.432 0.89 268451. 0.3656
|
|
61.62 0.2905 0.6389 0.0384 0.0175 3.095 12.194 12.037 2308.247 1.378 53.539 2.365 0.89 268721. 0.3439
|
|
65.47 0.3086 0.6583 0.0357 0.0167 2.967 11.689 11.189 2212.744 1.321 49.770 2.294 0.89 269002. 0.3216
|
|
69.32 0.3268 0.6732 0.0329 0.0160 2.834 11.163 10.321 2113.146 1.261 45.909 2.215 0.89 269295. 0.2983
|
|
73.17 0.3449 0.6825 0.0301 0.0152 2.697 10.623 9.434 2010.942 1.200 41.960 2.128 0.89 269599. 0.2739
|
|
77.02 0.3631 0.6838 0.0272 0.0144 2.561 10.089 8.527 1909.870 1.140 37.929 2.025 0.89 269916. 0.2478
|
|
80.87 0.3812 0.6784 0.0243 0.0136 2.417 9.522 7.605 1802.594 1.076 33.825 1.913 0.90 270245. 0.2212
|
|
84.72 0.3994 0.6649 0.0213 0.0128 2.265 8.924 6.667 1689.335 1.008 29.656 1.790 0.90 270586. 0.1937
|
|
88.57 0.4176 0.6410 0.0182 0.0119 2.107 8.298 5.717 1570.822 0.938 25.431 1.651 0.90 270939. 0.1654
|
|
92.42 0.4357 0.6039 0.0152 0.0110 1.941 7.648 4.757 1447.665 0.864 21.158 1.490 0.90 271304. 0.1362
|
|
96.27 0.4539 0.5491 0.0121 0.0100 1.771 6.977 3.788 1320.713 0.788 16.850 1.301 0.90 271682. 0.1061
|
|
100.12 0.4720 0.4705 0.0090 0.0090 1.597 6.291 2.815 1190.900 0.711 12.519 1.072 0.90 272073. 0.0754
|
|
103.98 0.4902 0.3590 0.0059 0.0080 1.420 5.596 1.839 1059.226 0.632 8.182 0.788 0.90 272474. 0.0448
|
|
107.83 0.5083 0.2004 0.0028 0.0070 1.242 4.894 0.866 926.461 0.553 3.851 0.424 0.90 272886. 0.0165
|
|
111.68 0.5265
|
|
|
|
|
|
|
|
PROP RPM = 17000
|
|
|
|
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 0.0707 0.0275 5.850 21.688 25.028 4362.062 2.450 111.325 2.602 0.94 282256. 0.5457
|
|
4.11 0.0182 0.0463 0.0696 0.0274 5.824 21.593 24.622 4343.070 2.440 109.520 2.571 0.94 282381. 0.5348
|
|
8.21 0.0364 0.0915 0.0683 0.0272 5.789 21.464 24.181 4316.966 2.425 107.556 2.541 0.94 282515. 0.5236
|
|
12.32 0.0547 0.1355 0.0670 0.0270 5.744 21.295 23.703 4283.103 2.406 105.430 2.510 0.94 282659. 0.5122
|
|
16.42 0.0729 0.1785 0.0655 0.0267 5.687 21.085 23.186 4240.887 2.382 103.133 2.480 0.94 282813. 0.5005
|
|
20.53 0.0911 0.2205 0.0640 0.0264 5.619 20.832 22.630 4189.896 2.354 100.660 2.450 0.94 282977. 0.4884
|
|
24.63 0.1093 0.2613 0.0623 0.0260 5.538 20.533 22.034 4129.879 2.320 98.006 2.420 0.94 283152. 0.4761
|
|
28.74 0.1275 0.3011 0.0605 0.0256 5.446 20.190 21.396 4060.784 2.281 95.171 2.390 0.94 283337. 0.4633
|
|
32.85 0.1457 0.3398 0.0586 0.0251 5.341 19.802 20.719 3982.747 2.237 92.156 2.360 0.95 283534. 0.4501
|
|
36.95 0.1640 0.3772 0.0565 0.0246 5.225 19.371 20.002 3895.998 2.188 88.967 2.329 0.95 283741. 0.4365
|
|
41.06 0.1822 0.4134 0.0544 0.0240 5.097 18.897 19.247 3800.837 2.135 85.610 2.297 0.95 283960. 0.4223
|
|
45.16 0.2004 0.4482 0.0522 0.0233 4.958 18.384 18.456 3697.510 2.077 82.091 2.264 0.95 284190. 0.4076
|
|
49.27 0.2186 0.4816 0.0498 0.0226 4.809 17.831 17.630 3586.252 2.014 78.416 2.230 0.95 284431. 0.3924
|
|
53.37 0.2368 0.5133 0.0474 0.0219 4.650 17.239 16.770 3467.306 1.948 74.593 2.194 0.95 284685. 0.3765
|
|
57.48 0.2550 0.5432 0.0449 0.0211 4.480 16.611 15.879 3340.878 1.877 70.630 2.156 0.95 284950. 0.3600
|
|
61.59 0.2733 0.5711 0.0423 0.0202 4.301 15.945 14.958 3207.059 1.801 66.532 2.115 0.95 285227. 0.3429
|
|
65.69 0.2915 0.5968 0.0396 0.0193 4.111 15.243 14.008 3065.820 1.722 62.309 2.072 0.95 285517. 0.3251
|
|
69.80 0.3097 0.6200 0.0368 0.0184 3.912 14.503 13.032 2917.043 1.639 57.966 2.026 0.95 285819. 0.3066
|
|
73.90 0.3279 0.6396 0.0340 0.0174 3.707 13.743 12.030 2764.214 1.553 53.511 1.974 0.95 286133. 0.2870
|
|
78.01 0.3461 0.6532 0.0311 0.0165 3.504 12.993 11.005 2613.270 1.468 48.949 1.910 0.95 286460. 0.2656
|
|
82.11 0.3643 0.6553 0.0281 0.0156 3.326 12.332 9.955 2480.376 1.393 44.279 1.820 0.95 286800. 0.2407
|
|
86.22 0.3826 0.6428 0.0251 0.0149 3.177 11.779 8.883 2369.029 1.331 39.510 1.701 0.95 287152. 0.2124
|
|
90.32 0.4008 0.6207 0.0220 0.0142 3.024 11.212 7.793 2255.127 1.267 34.665 1.567 0.95 287518. 0.1834
|
|
94.43 0.4190 0.5874 0.0189 0.0135 2.868 10.632 6.690 2138.499 1.201 29.757 1.419 0.95 287896. 0.1538
|
|
98.54 0.4372 0.5407 0.0158 0.0127 2.710 10.046 5.576 2020.625 1.135 24.801 1.252 0.95 288288. 0.1239
|
|
102.64 0.4554 0.4780 0.0126 0.0120 2.551 9.457 4.455 1902.075 1.068 19.817 1.062 0.95 288693. 0.0940
|
|
106.75 0.4736 0.3966 0.0094 0.0112 2.392 8.869 3.333 1783.772 1.002 14.823 0.847 0.95 289110. 0.0648
|
|
110.85 0.4919 0.2928 0.0063 0.0105 2.235 8.285 2.214 1666.290 0.936 9.846 0.603 0.96 289541. 0.0376
|
|
114.96 0.5101 0.1627 0.0031 0.0098 2.078 7.705 1.103 1549.645 0.870 4.907 0.323 0.96 289982. 0.0142
|
|
119.06 0.5283 -0.0034 -0.0001 0.0090 1.907 7.070 -0.020 1421.949 0.799 -0.090 -0.006 0.96 290395. 0.0000
|
|
|
|
|
|
|