612 lines
109 KiB
Plaintext
612 lines
109 KiB
Plaintext
14x6E (14x6E.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 0.0765 0.0302 0.001 0.082 0.094 0.975 0.009 0.416 43.555 0.06 18278. 0.5585
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0.26 0.0194 0.0480 0.0751 0.0303 0.001 0.083 0.092 0.979 0.009 0.409 42.575 0.06 18287. 0.5409
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0.51 0.0388 0.0938 0.0736 0.0304 0.001 0.083 0.090 0.982 0.009 0.401 41.585 0.06 18298. 0.5230
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0.77 0.0582 0.1373 0.0720 0.0305 0.001 0.083 0.088 0.985 0.009 0.392 40.589 0.06 18308. 0.5049
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1.03 0.0776 0.1786 0.0703 0.0306 0.001 0.083 0.086 0.986 0.009 0.383 39.585 0.06 18320. 0.4867
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1.29 0.0970 0.2176 0.0685 0.0306 0.001 0.083 0.084 0.986 0.009 0.373 38.575 0.06 18332. 0.4682
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1.54 0.1164 0.2542 0.0666 0.0305 0.001 0.083 0.082 0.985 0.009 0.363 37.557 0.06 18345. 0.4496
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1.80 0.1359 0.2884 0.0647 0.0305 0.001 0.083 0.079 0.983 0.009 0.352 36.531 0.06 18358. 0.4308
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2.06 0.1553 0.3203 0.0626 0.0303 0.001 0.083 0.077 0.979 0.009 0.341 35.496 0.06 18373. 0.4118
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2.32 0.1747 0.3497 0.0604 0.0302 0.001 0.082 0.074 0.974 0.009 0.329 34.450 0.06 18388. 0.3927
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2.57 0.1941 0.3766 0.0581 0.0300 0.001 0.082 0.071 0.967 0.009 0.317 33.391 0.06 18404. 0.3733
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2.83 0.2135 0.4010 0.0557 0.0297 0.001 0.081 0.068 0.958 0.009 0.304 32.316 0.06 18421. 0.3538
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3.09 0.2329 0.4226 0.0533 0.0293 0.001 0.080 0.065 0.947 0.009 0.290 31.220 0.06 18438. 0.3341
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3.34 0.2523 0.4414 0.0507 0.0290 0.001 0.079 0.062 0.935 0.009 0.276 30.101 0.06 18457. 0.3142
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3.60 0.2717 0.4572 0.0480 0.0285 0.001 0.078 0.059 0.920 0.009 0.261 28.951 0.06 18477. 0.2940
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3.86 0.2911 0.4698 0.0452 0.0280 0.001 0.076 0.055 0.903 0.009 0.246 27.765 0.06 18497. 0.2736
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4.12 0.3105 0.4789 0.0423 0.0274 0.001 0.075 0.052 0.884 0.008 0.230 26.537 0.06 18518. 0.2530
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4.37 0.3299 0.4843 0.0393 0.0268 0.001 0.073 0.048 0.864 0.008 0.214 25.257 0.06 18541. 0.2322
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4.63 0.3493 0.4856 0.0362 0.0261 0.001 0.071 0.044 0.841 0.008 0.197 23.918 0.06 18564. 0.2111
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4.89 0.3687 0.4824 0.0331 0.0253 0.001 0.069 0.041 0.816 0.008 0.180 22.510 0.06 18588. 0.1899
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5.15 0.3881 0.4742 0.0299 0.0245 0.001 0.067 0.037 0.790 0.008 0.163 21.019 0.06 18613. 0.1686
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5.40 0.4076 0.4603 0.0267 0.0236 0.001 0.064 0.033 0.762 0.007 0.145 19.431 0.06 18639. 0.1471
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5.66 0.4270 0.4399 0.0234 0.0227 0.001 0.062 0.029 0.732 0.007 0.127 17.728 0.06 18666. 0.1257
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5.92 0.4464 0.4122 0.0200 0.0217 0.001 0.059 0.025 0.700 0.007 0.109 15.889 0.06 18694. 0.1043
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6.18 0.4658 0.3759 0.0167 0.0207 0.001 0.056 0.020 0.667 0.006 0.091 13.887 0.06 18723. 0.0831
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6.43 0.4852 0.3296 0.0133 0.0196 0.001 0.053 0.016 0.632 0.006 0.072 11.690 0.06 18753. 0.0625
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6.69 0.5046 0.2715 0.0099 0.0184 0.001 0.050 0.012 0.595 0.006 0.054 9.258 0.06 18784. 0.0428
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6.95 0.5240 0.1992 0.0066 0.0173 0.001 0.047 0.008 0.557 0.005 0.036 6.540 0.06 18816. 0.0246
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7.20 0.5434 0.1096 0.0032 0.0161 0.001 0.044 0.004 0.519 0.005 0.018 3.470 0.06 18849. 0.0092
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7.46 0.5628 -0.0015 0.0000 0.0148 0.001 0.040 0.000 0.479 0.005 0.000 -0.045 0.06 18883. 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 0.0767 0.0271 0.009 0.296 0.376 6.998 0.033 1.672 24.357 0.11 36556. 0.6258
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0.52 0.0195 0.0539 0.0753 0.0273 0.009 0.297 0.369 7.038 0.034 1.641 23.771 0.11 36575. 0.6051
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1.04 0.0390 0.1052 0.0738 0.0274 0.009 0.299 0.361 7.072 0.034 1.608 23.183 0.11 36595. 0.5842
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1.55 0.0586 0.1538 0.0722 0.0275 0.010 0.300 0.354 7.099 0.034 1.573 22.596 0.11 36617. 0.5632
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2.07 0.0781 0.1998 0.0705 0.0276 0.010 0.301 0.345 7.118 0.034 1.536 22.010 0.11 36639. 0.5422
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2.59 0.0976 0.2431 0.0687 0.0276 0.010 0.301 0.337 7.127 0.034 1.497 21.426 0.11 36664. 0.5210
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3.11 0.1171 0.2838 0.0669 0.0276 0.010 0.301 0.327 7.125 0.034 1.456 20.842 0.11 36690. 0.4999
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3.62 0.1366 0.3218 0.0649 0.0275 0.010 0.301 0.318 7.113 0.034 1.413 20.260 0.11 36717. 0.4786
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4.14 0.1562 0.3572 0.0628 0.0274 0.010 0.300 0.307 7.087 0.034 1.368 19.678 0.11 36746. 0.4573
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4.66 0.1757 0.3900 0.0606 0.0273 0.009 0.298 0.297 7.048 0.034 1.320 19.096 0.11 36777. 0.4360
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5.18 0.1952 0.4201 0.0583 0.0271 0.009 0.296 0.285 6.994 0.033 1.270 18.512 0.11 36809. 0.4145
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5.69 0.2147 0.4474 0.0559 0.0268 0.009 0.293 0.274 6.926 0.033 1.217 17.925 0.11 36844. 0.3930
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6.21 0.2343 0.4720 0.0534 0.0265 0.009 0.289 0.261 6.840 0.033 1.163 17.333 0.11 36879. 0.3714
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6.73 0.2538 0.4937 0.0508 0.0261 0.009 0.285 0.249 6.738 0.032 1.106 16.735 0.11 36917. 0.3497
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7.25 0.2733 0.5123 0.0480 0.0256 0.009 0.280 0.235 6.618 0.032 1.047 16.126 0.11 36956. 0.3278
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7.76 0.2928 0.5277 0.0452 0.0251 0.009 0.274 0.221 6.479 0.031 0.985 15.503 0.11 36998. 0.3058
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8.28 0.3123 0.5396 0.0423 0.0245 0.008 0.267 0.207 6.322 0.030 0.922 14.864 0.11 37041. 0.2836
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8.80 0.3319 0.5479 0.0393 0.0238 0.008 0.260 0.192 6.147 0.029 0.856 14.202 0.11 37086. 0.2612
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9.32 0.3514 0.5520 0.0362 0.0231 0.008 0.252 0.177 5.955 0.028 0.789 13.514 0.11 37133. 0.2386
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9.83 0.3709 0.5515 0.0331 0.0222 0.008 0.243 0.162 5.744 0.027 0.721 12.792 0.11 37182. 0.2158
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10.35 0.3904 0.5459 0.0299 0.0214 0.007 0.233 0.146 5.517 0.026 0.651 12.029 0.11 37232. 0.1928
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10.87 0.4099 0.5343 0.0266 0.0204 0.007 0.223 0.130 5.273 0.025 0.580 11.213 0.11 37285. 0.1697
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11.39 0.4295 0.5159 0.0233 0.0194 0.007 0.212 0.114 5.012 0.024 0.508 10.334 0.11 37340. 0.1463
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11.90 0.4490 0.4892 0.0200 0.0183 0.006 0.200 0.098 4.734 0.023 0.435 9.374 0.11 37396. 0.1229
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12.42 0.4685 0.4527 0.0166 0.0172 0.006 0.188 0.081 4.442 0.021 0.362 8.312 0.11 37455. 0.0994
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12.94 0.4880 0.4039 0.0133 0.0160 0.006 0.175 0.065 4.134 0.020 0.289 7.120 0.11 37516. 0.0760
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13.46 0.5075 0.3398 0.0099 0.0148 0.005 0.161 0.048 3.813 0.018 0.215 5.760 0.11 37578. 0.0531
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13.98 0.5271 0.2560 0.0065 0.0135 0.005 0.147 0.032 3.480 0.017 0.143 4.178 0.11 37643. 0.0314
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14.49 0.5466 0.1459 0.0032 0.0121 0.004 0.133 0.016 3.136 0.015 0.071 2.296 0.11 37710. 0.0121
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15.01 0.5661 -0.0008 0.0000 0.0108 0.004 0.118 0.000 2.782 0.013 0.000 -0.012 0.11 37777. 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 0.0770 0.0258 0.030 0.633 0.848 22.455 0.071 3.772 17.131 0.17 54833. 0.6612
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0.78 0.0196 0.0570 0.0756 0.0259 0.030 0.637 0.832 22.603 0.072 3.703 16.705 0.17 54862. 0.6388
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1.56 0.0391 0.1111 0.0740 0.0261 0.030 0.640 0.816 22.730 0.072 3.629 16.280 0.17 54892. 0.6163
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2.33 0.0587 0.1623 0.0724 0.0262 0.031 0.643 0.798 22.832 0.073 3.550 15.857 0.17 54925. 0.5938
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3.11 0.0783 0.2107 0.0708 0.0263 0.031 0.645 0.780 22.905 0.073 3.467 15.437 0.17 54959. 0.5712
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3.89 0.0978 0.2562 0.0690 0.0263 0.031 0.646 0.760 22.946 0.073 3.380 15.019 0.17 54996. 0.5487
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4.67 0.1174 0.2989 0.0671 0.0263 0.031 0.647 0.739 22.951 0.073 3.287 14.604 0.17 55035. 0.5262
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5.45 0.1370 0.3389 0.0651 0.0263 0.031 0.646 0.717 22.915 0.073 3.189 14.192 0.17 55076. 0.5037
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6.23 0.1565 0.3761 0.0630 0.0262 0.031 0.643 0.694 22.836 0.073 3.086 13.782 0.17 55120. 0.4812
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7.00 0.1761 0.4106 0.0608 0.0261 0.030 0.640 0.670 22.710 0.072 2.978 13.374 0.17 55166. 0.4587
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7.78 0.1957 0.4424 0.0585 0.0259 0.030 0.635 0.644 22.532 0.072 2.865 12.967 0.17 55215. 0.4362
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8.56 0.2152 0.4713 0.0560 0.0256 0.030 0.628 0.618 22.301 0.071 2.747 12.560 0.17 55266. 0.4137
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9.34 0.2348 0.4975 0.0535 0.0253 0.030 0.620 0.590 22.013 0.070 2.623 12.152 0.17 55320. 0.3912
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10.12 0.2544 0.5208 0.0509 0.0249 0.029 0.610 0.561 21.665 0.069 2.495 11.742 0.17 55377. 0.3686
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10.89 0.2739 0.5410 0.0482 0.0244 0.029 0.599 0.531 21.253 0.068 2.361 11.327 0.17 55436. 0.3459
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11.67 0.2935 0.5580 0.0453 0.0238 0.028 0.585 0.500 20.776 0.066 2.222 10.905 0.17 55499. 0.3230
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12.45 0.3131 0.5717 0.0424 0.0232 0.027 0.570 0.467 20.234 0.064 2.078 10.474 0.17 55564. 0.3001
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13.23 0.3326 0.5817 0.0394 0.0225 0.026 0.553 0.434 19.628 0.062 1.931 10.030 0.17 55631. 0.2770
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14.01 0.3522 0.5877 0.0363 0.0218 0.025 0.534 0.400 18.958 0.060 1.779 9.570 0.17 55702. 0.2537
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14.79 0.3718 0.5891 0.0331 0.0209 0.024 0.514 0.365 18.226 0.058 1.625 9.089 0.17 55776. 0.2302
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15.56 0.3913 0.5855 0.0299 0.0200 0.023 0.491 0.330 17.432 0.055 1.467 8.581 0.17 55852. 0.2065
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16.34 0.4109 0.5759 0.0267 0.0190 0.022 0.467 0.294 16.577 0.053 1.307 8.039 0.17 55931. 0.1826
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17.12 0.4304 0.5593 0.0234 0.0180 0.021 0.441 0.257 15.661 0.050 1.145 7.452 0.17 56014. 0.1584
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17.90 0.4500 0.5343 0.0200 0.0169 0.020 0.414 0.220 14.688 0.047 0.981 6.809 0.17 56099. 0.1340
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18.68 0.4696 0.4988 0.0166 0.0157 0.018 0.385 0.183 13.658 0.043 0.816 6.092 0.17 56187. 0.1093
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19.45 0.4891 0.4500 0.0133 0.0144 0.017 0.354 0.146 12.576 0.040 0.651 5.276 0.17 56279. 0.0846
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20.23 0.5087 0.3840 0.0099 0.0131 0.015 0.322 0.109 11.445 0.036 0.486 4.329 0.17 56373. 0.0600
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21.01 0.5283 0.2946 0.0066 0.0118 0.014 0.289 0.072 10.269 0.033 0.322 3.199 0.17 56471. 0.0361
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21.79 0.5478 0.1726 0.0033 0.0104 0.012 0.255 0.036 9.055 0.029 0.160 1.807 0.17 56571. 0.0144
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22.57 0.5674 0.0013 0.0000 0.0090 0.010 0.220 0.000 7.804 0.025 0.001 0.013 0.17 56672. 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 0.0772 0.0250 0.069 1.092 1.513 51.684 0.123 6.730 13.278 0.22 73110. 0.6845
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1.04 0.0196 0.0590 0.0758 0.0252 0.070 1.100 1.485 52.052 0.124 6.606 12.941 0.22 73148. 0.6610
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2.08 0.0392 0.1149 0.0743 0.0254 0.070 1.107 1.455 52.369 0.125 6.474 12.606 0.22 73189. 0.6374
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3.12 0.0588 0.1677 0.0727 0.0255 0.071 1.112 1.424 52.626 0.126 6.334 12.273 0.22 73232. 0.6138
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4.16 0.0784 0.2176 0.0710 0.0256 0.071 1.116 1.391 52.815 0.126 6.186 11.943 0.22 73278. 0.5903
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5.20 0.0980 0.2646 0.0692 0.0256 0.071 1.118 1.355 52.925 0.126 6.029 11.617 0.22 73327. 0.5668
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6.23 0.1176 0.3087 0.0673 0.0256 0.071 1.119 1.318 52.948 0.126 5.864 11.293 0.22 73379. 0.5434
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7.27 0.1372 0.3499 0.0653 0.0256 0.071 1.117 1.279 52.874 0.126 5.689 10.973 0.22 73435. 0.5201
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8.31 0.1568 0.3883 0.0632 0.0255 0.071 1.113 1.238 52.694 0.126 5.506 10.655 0.22 73493. 0.4968
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9.35 0.1764 0.4239 0.0610 0.0254 0.070 1.107 1.195 52.399 0.125 5.313 10.340 0.22 73555. 0.4736
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10.39 0.1960 0.4568 0.0587 0.0252 0.070 1.098 1.149 51.981 0.124 5.111 10.027 0.22 73620. 0.4505
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11.43 0.2155 0.4868 0.0562 0.0249 0.069 1.087 1.102 51.431 0.123 4.900 9.715 0.22 73689. 0.4273
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12.47 0.2351 0.5140 0.0537 0.0246 0.068 1.072 1.052 50.743 0.121 4.679 9.403 0.22 73761. 0.4042
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13.51 0.2547 0.5384 0.0511 0.0242 0.067 1.055 1.000 49.909 0.119 4.449 9.090 0.22 73837. 0.3810
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14.55 0.2743 0.5597 0.0483 0.0237 0.066 1.034 0.947 48.921 0.117 4.210 8.776 0.22 73917. 0.3578
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15.59 0.2939 0.5779 0.0455 0.0231 0.064 1.009 0.891 47.773 0.114 3.962 8.457 0.22 74000. 0.3345
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16.63 0.3135 0.5928 0.0425 0.0225 0.062 0.982 0.833 46.465 0.111 3.706 8.132 0.22 74087. 0.3111
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17.67 0.3331 0.6040 0.0395 0.0218 0.060 0.951 0.774 45.000 0.107 3.442 7.799 0.22 74177. 0.2876
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18.70 0.3527 0.6114 0.0364 0.0210 0.058 0.917 0.713 43.379 0.104 3.172 7.455 0.22 74272. 0.2639
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19.74 0.3723 0.6143 0.0332 0.0201 0.056 0.879 0.651 41.604 0.099 2.895 7.097 0.22 74370. 0.2400
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20.78 0.3919 0.6121 0.0300 0.0192 0.053 0.838 0.588 39.676 0.095 2.614 6.718 0.22 74472. 0.2159
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21.82 0.4115 0.6041 0.0267 0.0182 0.050 0.794 0.523 37.598 0.090 2.328 6.315 0.22 74578. 0.1915
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22.86 0.4311 0.5891 0.0234 0.0171 0.047 0.747 0.458 35.371 0.084 2.039 5.878 0.22 74689. 0.1668
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23.90 0.4507 0.5655 0.0200 0.0160 0.044 0.697 0.393 33.001 0.079 1.747 5.397 0.22 74803. 0.1418
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24.94 0.4703 0.5312 0.0167 0.0148 0.041 0.644 0.327 30.493 0.073 1.453 4.859 0.22 74921. 0.1164
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25.98 0.4899 0.4830 0.0133 0.0135 0.037 0.589 0.260 27.854 0.066 1.158 4.241 0.22 75043. 0.0907
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27.02 0.5095 0.4162 0.0099 0.0121 0.034 0.530 0.194 25.095 0.060 0.865 3.514 0.23 75169. 0.0649
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28.06 0.5291 0.3235 0.0066 0.0108 0.030 0.470 0.129 22.227 0.053 0.573 2.630 0.23 75300. 0.0396
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29.10 0.5487 0.1927 0.0033 0.0093 0.026 0.407 0.064 19.266 0.046 0.285 1.511 0.23 75434. 0.0160
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30.14 0.5683 0.0013 0.0000 0.0078 0.022 0.343 0.000 16.210 0.039 0.002 0.010 0.23 75568. 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 0.0776 0.0246 0.133 1.675 2.374 99.110 0.189 10.558 10.863 0.28 91386. 0.7015
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1.30 0.0196 0.0604 0.0761 0.0248 0.134 1.688 2.330 99.852 0.191 10.364 10.584 0.28 91433. 0.6771
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2.60 0.0393 0.1176 0.0746 0.0249 0.135 1.699 2.283 100.493 0.192 10.157 10.306 0.28 91484. 0.6527
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3.90 0.0589 0.1717 0.0730 0.0250 0.135 1.708 2.234 101.016 0.193 9.937 10.031 0.28 91539. 0.6284
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5.21 0.0785 0.2228 0.0713 0.0251 0.136 1.714 2.182 101.402 0.194 9.705 9.759 0.28 91597. 0.6042
|
|
6.51 0.0982 0.2708 0.0695 0.0252 0.136 1.718 2.127 101.632 0.194 9.459 9.490 0.28 91658. 0.5800
|
|
7.81 0.1178 0.3158 0.0676 0.0252 0.136 1.719 2.068 101.688 0.194 9.199 9.225 0.28 91724. 0.5560
|
|
9.11 0.1375 0.3580 0.0656 0.0252 0.136 1.717 2.006 101.551 0.194 8.925 8.962 0.28 91793. 0.5320
|
|
10.41 0.1571 0.3973 0.0634 0.0251 0.136 1.711 1.942 101.203 0.193 8.636 8.702 0.28 91867. 0.5082
|
|
11.71 0.1767 0.4337 0.0612 0.0249 0.135 1.701 1.874 100.626 0.192 8.333 8.445 0.28 91944. 0.4845
|
|
13.02 0.1964 0.4673 0.0589 0.0247 0.134 1.687 1.802 99.803 0.191 8.016 8.190 0.28 92026. 0.4608
|
|
14.32 0.2160 0.4982 0.0564 0.0245 0.132 1.669 1.727 98.718 0.189 7.683 7.936 0.28 92113. 0.4372
|
|
15.62 0.2356 0.5262 0.0539 0.0241 0.131 1.646 1.649 97.356 0.186 7.336 7.684 0.28 92203. 0.4136
|
|
16.92 0.2553 0.5513 0.0512 0.0237 0.128 1.618 1.568 95.702 0.183 6.975 7.432 0.28 92298. 0.3900
|
|
18.22 0.2749 0.5735 0.0485 0.0232 0.126 1.585 1.484 93.739 0.179 6.599 7.178 0.28 92398. 0.3664
|
|
19.52 0.2945 0.5925 0.0456 0.0227 0.123 1.546 1.396 91.455 0.175 6.208 6.922 0.28 92503. 0.3428
|
|
20.83 0.3142 0.6083 0.0426 0.0220 0.119 1.502 1.305 88.852 0.170 5.805 6.662 0.28 92612. 0.3190
|
|
22.13 0.3338 0.6205 0.0396 0.0213 0.115 1.453 1.212 85.933 0.164 5.390 6.396 0.28 92725. 0.2951
|
|
23.43 0.3535 0.6288 0.0365 0.0205 0.111 1.398 1.116 82.702 0.158 4.965 6.122 0.28 92844. 0.2711
|
|
24.73 0.3731 0.6328 0.0333 0.0196 0.106 1.338 1.019 79.160 0.151 4.531 5.837 0.28 92967. 0.2469
|
|
26.03 0.3927 0.6318 0.0300 0.0187 0.101 1.273 0.919 75.311 0.144 4.089 5.536 0.28 93096. 0.2225
|
|
27.33 0.4124 0.6250 0.0267 0.0176 0.095 1.203 0.818 71.158 0.136 3.640 5.216 0.28 93229. 0.1977
|
|
28.64 0.4320 0.6112 0.0234 0.0165 0.089 1.128 0.716 66.707 0.127 3.185 4.868 0.28 93367. 0.1727
|
|
29.94 0.4516 0.5887 0.0200 0.0154 0.083 1.048 0.613 61.967 0.118 2.726 4.486 0.28 93510. 0.1472
|
|
31.24 0.4713 0.5552 0.0166 0.0141 0.076 0.963 0.509 56.950 0.109 2.264 4.054 0.28 93659. 0.1212
|
|
32.54 0.4909 0.5073 0.0132 0.0128 0.069 0.873 0.405 51.670 0.099 1.802 3.556 0.28 93812. 0.0949
|
|
33.84 0.5105 0.4396 0.0098 0.0114 0.062 0.780 0.301 46.148 0.088 1.341 2.963 0.28 93970. 0.0682
|
|
35.14 0.5302 0.3435 0.0065 0.0100 0.054 0.683 0.199 40.409 0.077 0.884 2.230 0.28 94134. 0.0416
|
|
36.45 0.5498 0.2043 0.0032 0.0085 0.046 0.583 0.097 34.483 0.066 0.432 1.278 0.28 94302. 0.0167
|
|
37.75 0.5695 -0.0081 -0.0001 0.0070 0.038 0.479 -0.003 28.358 0.054 -0.014 -0.049 0.28 94469. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 6000
|
|
|
|
V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
|
|
(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
|
|
0.00 0.0000 0.0000 0.0779 0.0243 0.227 2.385 3.435 169.334 0.270 15.278 9.200 0.33 109660. 0.7146
|
|
1.56 0.0196 0.0613 0.0765 0.0245 0.229 2.404 3.372 170.642 0.272 14.998 8.962 0.33 109717. 0.6897
|
|
3.12 0.0392 0.1194 0.0750 0.0246 0.230 2.420 3.305 171.776 0.273 14.699 8.726 0.33 109778. 0.6648
|
|
4.68 0.0588 0.1743 0.0734 0.0248 0.232 2.433 3.233 172.701 0.275 14.382 8.492 0.33 109844. 0.6400
|
|
6.24 0.0785 0.2260 0.0717 0.0249 0.233 2.443 3.158 173.388 0.276 14.047 8.261 0.33 109913. 0.6153
|
|
7.80 0.0981 0.2748 0.0698 0.0249 0.233 2.448 3.078 173.803 0.277 13.692 8.033 0.33 109987. 0.5907
|
|
9.36 0.1177 0.3205 0.0679 0.0249 0.233 2.450 2.994 173.914 0.277 13.317 7.808 0.33 110066. 0.5662
|
|
10.92 0.1373 0.3633 0.0659 0.0249 0.233 2.447 2.905 173.688 0.276 12.921 7.586 0.33 110149. 0.5419
|
|
12.48 0.1569 0.4032 0.0638 0.0248 0.232 2.438 2.811 173.093 0.275 12.505 7.367 0.33 110238. 0.5177
|
|
14.04 0.1765 0.4402 0.0616 0.0247 0.231 2.424 2.713 172.097 0.274 12.068 7.150 0.33 110331. 0.4936
|
|
15.60 0.1962 0.4745 0.0592 0.0245 0.229 2.404 2.610 170.671 0.272 11.609 6.936 0.33 110429. 0.4696
|
|
17.16 0.2158 0.5059 0.0568 0.0242 0.226 2.378 2.502 168.787 0.269 11.129 6.723 0.33 110533. 0.4457
|
|
18.72 0.2354 0.5346 0.0542 0.0239 0.223 2.344 2.389 166.417 0.265 10.628 6.512 0.33 110641. 0.4219
|
|
20.28 0.2550 0.5604 0.0515 0.0235 0.219 2.304 2.272 163.536 0.260 10.106 6.301 0.33 110755. 0.3981
|
|
21.85 0.2746 0.5832 0.0488 0.0230 0.215 2.256 2.150 160.114 0.255 9.562 6.090 0.33 110875. 0.3742
|
|
23.41 0.2942 0.6031 0.0459 0.0224 0.209 2.199 2.023 156.129 0.248 8.999 5.877 0.33 111000. 0.3504
|
|
24.97 0.3139 0.6197 0.0429 0.0217 0.203 2.135 1.892 151.583 0.241 8.416 5.662 0.33 111131. 0.3264
|
|
26.53 0.3335 0.6328 0.0399 0.0210 0.196 2.064 1.757 146.482 0.233 7.817 5.442 0.34 111267. 0.3023
|
|
28.09 0.3531 0.6422 0.0367 0.0202 0.189 1.984 1.619 140.831 0.224 7.203 5.215 0.34 111410. 0.2782
|
|
29.65 0.3727 0.6473 0.0335 0.0193 0.181 1.897 1.478 134.633 0.214 6.575 4.980 0.34 111557. 0.2538
|
|
31.21 0.3923 0.6476 0.0303 0.0183 0.172 1.802 1.335 127.894 0.204 5.936 4.733 0.34 111711. 0.2292
|
|
32.77 0.4119 0.6421 0.0270 0.0173 0.162 1.699 1.189 120.619 0.192 5.287 4.470 0.34 111871. 0.2043
|
|
34.33 0.4316 0.6298 0.0236 0.0162 0.151 1.589 1.041 112.820 0.180 4.630 4.185 0.34 112036. 0.1790
|
|
35.89 0.4512 0.6090 0.0202 0.0150 0.140 1.472 0.892 104.510 0.166 3.967 3.871 0.34 112208. 0.1532
|
|
37.45 0.4708 0.5773 0.0168 0.0137 0.128 1.348 0.742 95.710 0.152 3.300 3.516 0.34 112386. 0.1269
|
|
39.01 0.4904 0.5310 0.0134 0.0124 0.116 1.218 0.592 86.446 0.138 2.632 3.105 0.34 112570. 0.1001
|
|
40.57 0.5100 0.4646 0.0100 0.0110 0.103 1.081 0.442 76.755 0.122 1.966 2.612 0.34 112759. 0.0728
|
|
42.13 0.5296 0.3686 0.0067 0.0096 0.089 0.939 0.293 66.682 0.106 1.305 1.996 0.34 112955. 0.0453
|
|
43.69 0.5493 0.2266 0.0033 0.0081 0.075 0.793 0.147 56.278 0.090 0.653 1.183 0.34 113157. 0.0190
|
|
45.25 0.5689 0.0041 0.0000 0.0065 0.061 0.641 0.002 45.531 0.072 0.009 0.021 0.34 113358. 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 0.0784 0.0241 0.358 3.227 4.702 267.223 0.365 20.915 7.981 0.39 127933. 0.7253
|
|
1.82 0.0196 0.0621 0.0769 0.0243 0.361 3.252 4.616 269.336 0.367 20.532 7.773 0.39 128000. 0.7000
|
|
3.64 0.0393 0.1209 0.0754 0.0245 0.364 3.274 4.524 271.167 0.370 20.123 7.567 0.39 128071. 0.6746
|
|
5.47 0.0589 0.1765 0.0738 0.0246 0.366 3.292 4.427 272.663 0.372 19.690 7.364 0.39 128148. 0.6494
|
|
7.29 0.0785 0.2289 0.0721 0.0247 0.367 3.306 4.324 273.773 0.373 19.231 7.163 0.39 128229. 0.6242
|
|
9.11 0.0982 0.2782 0.0703 0.0248 0.368 3.314 4.214 274.444 0.374 18.745 6.965 0.39 128316. 0.5993
|
|
10.93 0.1178 0.3245 0.0683 0.0248 0.368 3.316 4.099 274.624 0.375 18.232 6.770 0.39 128408. 0.5744
|
|
12.76 0.1375 0.3678 0.0663 0.0248 0.368 3.312 3.977 274.260 0.374 17.690 6.577 0.39 128506. 0.5498
|
|
14.58 0.1571 0.4082 0.0642 0.0247 0.367 3.300 3.849 273.300 0.373 17.120 6.388 0.39 128609. 0.5252
|
|
16.40 0.1767 0.4458 0.0619 0.0245 0.364 3.281 3.714 271.692 0.371 16.521 6.201 0.39 128718. 0.5008
|
|
18.22 0.1964 0.4806 0.0596 0.0243 0.361 3.253 3.573 269.389 0.367 15.892 6.016 0.39 128833. 0.4766
|
|
20.05 0.2160 0.5126 0.0571 0.0241 0.357 3.216 3.425 266.345 0.363 15.234 5.833 0.39 128954. 0.4524
|
|
21.87 0.2356 0.5417 0.0545 0.0237 0.352 3.170 3.271 262.517 0.358 14.548 5.651 0.39 129082. 0.4283
|
|
23.69 0.2553 0.5681 0.0518 0.0233 0.346 3.114 3.110 257.862 0.352 13.832 5.470 0.39 129215. 0.4043
|
|
25.51 0.2749 0.5915 0.0490 0.0228 0.338 3.047 2.942 252.333 0.344 13.087 5.289 0.39 129355. 0.3802
|
|
27.33 0.2945 0.6119 0.0462 0.0222 0.330 2.969 2.768 245.894 0.335 12.314 5.107 0.39 129502. 0.3561
|
|
29.16 0.3142 0.6292 0.0432 0.0215 0.320 2.880 2.589 238.547 0.325 11.516 4.923 0.39 129654. 0.3320
|
|
30.98 0.3338 0.6431 0.0401 0.0208 0.309 2.781 2.404 230.301 0.314 10.694 4.735 0.39 129814. 0.3077
|
|
32.80 0.3535 0.6532 0.0369 0.0200 0.297 2.670 2.215 221.164 0.302 9.852 4.542 0.39 129980. 0.2833
|
|
34.62 0.3731 0.6592 0.0337 0.0191 0.283 2.549 2.022 211.142 0.288 8.992 4.343 0.39 130153. 0.2588
|
|
36.45 0.3927 0.6603 0.0304 0.0181 0.269 2.418 1.825 200.241 0.273 8.115 4.133 0.39 130333. 0.2340
|
|
38.27 0.4124 0.6559 0.0271 0.0170 0.253 2.276 1.624 188.473 0.257 7.226 3.909 0.39 130520. 0.2088
|
|
40.09 0.4320 0.6446 0.0237 0.0159 0.236 2.123 1.422 175.854 0.240 6.325 3.668 0.39 130713. 0.1833
|
|
41.91 0.4516 0.6248 0.0203 0.0147 0.218 1.961 1.218 162.408 0.222 5.416 3.400 0.39 130914. 0.1573
|
|
43.74 0.4713 0.5940 0.0169 0.0134 0.199 1.789 1.012 148.167 0.202 4.502 3.098 0.39 131122. 0.1306
|
|
45.56 0.4909 0.5484 0.0134 0.0120 0.179 1.608 0.806 133.177 0.182 3.586 2.746 0.39 131337. 0.1033
|
|
47.38 0.5105 0.4819 0.0100 0.0106 0.158 1.419 0.601 117.496 0.160 2.673 2.320 0.39 131559. 0.0754
|
|
49.20 0.5302 0.3842 0.0066 0.0091 0.136 1.222 0.397 101.198 0.138 1.768 1.781 0.39 131788. 0.0471
|
|
51.02 0.5498 0.2364 0.0033 0.0076 0.113 1.019 0.197 84.367 0.115 0.875 1.057 0.39 132023. 0.0196
|
|
52.85 0.5694 -0.0030 0.0000 0.0060 0.090 0.808 -0.002 66.955 0.091 -0.009 -0.013 0.40 132256. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 8000
|
|
|
|
V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
|
|
(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
|
|
0.00 0.0000 0.0000 0.0789 0.0241 0.534 4.205 6.183 398.012 0.475 27.501 7.046 0.44 146203. 0.7343
|
|
2.08 0.0196 0.0627 0.0775 0.0243 0.538 4.239 6.070 401.208 0.479 26.998 6.862 0.44 146280. 0.7085
|
|
4.17 0.0393 0.1220 0.0759 0.0244 0.542 4.268 5.949 403.976 0.482 26.463 6.680 0.44 146362. 0.6829
|
|
6.25 0.0589 0.1781 0.0743 0.0246 0.545 4.292 5.822 406.236 0.485 25.895 6.500 0.44 146450. 0.6573
|
|
8.33 0.0786 0.2310 0.0726 0.0247 0.547 4.310 5.686 407.909 0.487 25.292 6.323 0.44 146543. 0.6319
|
|
10.42 0.0982 0.2808 0.0707 0.0247 0.548 4.320 5.543 408.917 0.488 24.654 6.148 0.44 146643. 0.6066
|
|
12.50 0.1179 0.3275 0.0688 0.0248 0.549 4.323 5.391 409.179 0.488 23.979 5.976 0.44 146748. 0.5815
|
|
14.58 0.1375 0.3712 0.0668 0.0247 0.548 4.317 5.231 408.615 0.488 23.268 5.807 0.44 146860. 0.5566
|
|
16.67 0.1571 0.4121 0.0646 0.0246 0.546 4.302 5.063 407.146 0.486 22.518 5.640 0.44 146979. 0.5318
|
|
18.75 0.1768 0.4501 0.0624 0.0245 0.543 4.276 4.885 404.696 0.483 21.730 5.475 0.44 147104. 0.5072
|
|
20.83 0.1964 0.4853 0.0600 0.0243 0.538 4.239 4.700 401.191 0.479 20.904 5.313 0.45 147236. 0.4827
|
|
22.92 0.2161 0.5177 0.0575 0.0240 0.532 4.190 4.505 396.562 0.473 20.039 5.153 0.45 147374. 0.4584
|
|
25.00 0.2357 0.5473 0.0549 0.0236 0.524 4.128 4.302 390.743 0.466 19.135 4.994 0.45 147520. 0.4341
|
|
27.08 0.2554 0.5741 0.0522 0.0232 0.515 4.054 4.090 383.670 0.458 18.194 4.836 0.45 147673. 0.4099
|
|
29.17 0.2750 0.5981 0.0494 0.0227 0.503 3.965 3.870 375.272 0.448 17.214 4.678 0.45 147833. 0.3857
|
|
31.25 0.2946 0.6191 0.0465 0.0221 0.490 3.862 3.641 365.493 0.436 16.197 4.519 0.45 148001. 0.3614
|
|
33.33 0.3143 0.6369 0.0435 0.0214 0.475 3.744 3.405 354.336 0.423 15.146 4.359 0.45 148176. 0.3371
|
|
35.42 0.3339 0.6515 0.0404 0.0207 0.458 3.611 3.162 341.814 0.408 14.065 4.196 0.45 148359. 0.3127
|
|
37.50 0.3536 0.6623 0.0372 0.0198 0.440 3.465 2.913 327.938 0.391 12.956 4.029 0.45 148549. 0.2882
|
|
39.58 0.3732 0.6691 0.0339 0.0189 0.419 3.304 2.658 312.717 0.373 11.824 3.856 0.45 148747. 0.2635
|
|
41.67 0.3929 0.6711 0.0306 0.0179 0.397 3.129 2.399 296.160 0.354 10.671 3.674 0.45 148953. 0.2385
|
|
43.75 0.4125 0.6676 0.0273 0.0168 0.373 2.940 2.136 278.286 0.332 9.500 3.481 0.45 149167. 0.2132
|
|
45.83 0.4321 0.6574 0.0239 0.0157 0.347 2.738 1.869 259.119 0.309 8.314 3.272 0.45 149388. 0.1875
|
|
47.92 0.4518 0.6387 0.0204 0.0144 0.320 2.522 1.600 238.694 0.285 7.117 3.040 0.45 149618. 0.1612
|
|
50.00 0.4714 0.6090 0.0170 0.0131 0.291 2.293 1.330 217.062 0.259 5.914 2.778 0.45 149855. 0.1343
|
|
52.08 0.4911 0.5643 0.0135 0.0118 0.261 2.053 1.059 194.293 0.232 4.709 2.471 0.45 150101. 0.1066
|
|
54.17 0.5107 0.4982 0.0101 0.0103 0.229 1.801 0.788 170.475 0.203 3.507 2.098 0.45 150355. 0.0781
|
|
56.25 0.5304 0.3996 0.0066 0.0088 0.195 1.540 0.521 145.721 0.174 2.315 1.620 0.45 150617. 0.0490
|
|
58.33 0.5500 0.2474 0.0033 0.0073 0.161 1.270 0.256 120.161 0.143 1.140 0.968 0.45 150886. 0.0205
|
|
60.42 0.5696 -0.0066 -0.0001 0.0057 0.126 0.990 -0.005 93.692 0.112 -0.023 -0.025 0.45 151151. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 9000
|
|
|
|
V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
|
|
(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
|
|
0.00 0.0000 0.0000 0.0795 0.0241 0.761 5.329 7.886 567.434 0.602 35.078 6.304 0.50 164471. 0.7419
|
|
2.34 0.0196 0.0631 0.0781 0.0243 0.767 5.372 7.742 572.038 0.607 34.438 6.139 0.50 164558. 0.7159
|
|
4.69 0.0393 0.1228 0.0765 0.0245 0.772 5.410 7.589 576.018 0.611 33.757 5.976 0.50 164651. 0.6900
|
|
7.03 0.0589 0.1793 0.0749 0.0246 0.777 5.440 7.427 579.260 0.615 33.034 5.815 0.50 164750. 0.6642
|
|
9.38 0.0786 0.2325 0.0732 0.0247 0.780 5.463 7.254 581.652 0.617 32.267 5.657 0.50 164855. 0.6386
|
|
11.72 0.0982 0.2827 0.0713 0.0248 0.782 5.476 7.072 583.078 0.619 31.454 5.501 0.50 164968. 0.6131
|
|
14.07 0.1179 0.3297 0.0694 0.0248 0.782 5.479 6.878 583.424 0.619 30.595 5.347 0.50 165087. 0.5878
|
|
16.41 0.1375 0.3738 0.0673 0.0248 0.781 5.471 6.675 582.573 0.618 29.688 5.197 0.50 165213. 0.5627
|
|
18.75 0.1572 0.4150 0.0651 0.0247 0.778 5.451 6.460 580.410 0.616 28.733 5.048 0.50 165347. 0.5377
|
|
21.10 0.1768 0.4534 0.0629 0.0245 0.774 5.417 6.234 576.826 0.612 27.728 4.902 0.50 165488. 0.5130
|
|
23.44 0.1965 0.4889 0.0605 0.0243 0.767 5.369 5.997 571.713 0.607 26.674 4.758 0.50 165637. 0.4883
|
|
25.79 0.2161 0.5217 0.0580 0.0240 0.758 5.306 5.749 564.974 0.599 25.571 4.615 0.50 165793. 0.4638
|
|
28.13 0.2358 0.5518 0.0554 0.0237 0.746 5.226 5.490 556.514 0.590 24.418 4.474 0.50 165958. 0.4394
|
|
30.47 0.2554 0.5790 0.0526 0.0232 0.733 5.130 5.220 546.238 0.580 23.217 4.334 0.50 166130. 0.4150
|
|
32.82 0.2751 0.6035 0.0498 0.0227 0.716 5.015 4.939 534.046 0.567 21.967 4.194 0.50 166311. 0.3907
|
|
35.16 0.2947 0.6250 0.0469 0.0221 0.697 4.882 4.647 519.856 0.552 20.669 4.054 0.50 166500. 0.3663
|
|
37.51 0.3143 0.6434 0.0438 0.0214 0.675 4.730 4.345 503.671 0.534 19.327 3.913 0.50 166697. 0.3418
|
|
39.85 0.3340 0.6585 0.0407 0.0206 0.651 4.560 4.035 485.509 0.515 17.947 3.769 0.50 166903. 0.3173
|
|
42.20 0.3536 0.6701 0.0375 0.0198 0.624 4.371 3.717 465.386 0.494 16.531 3.622 0.50 167117. 0.2927
|
|
44.54 0.3733 0.6776 0.0342 0.0188 0.594 4.163 3.392 443.314 0.470 15.086 3.470 0.50 167340. 0.2678
|
|
46.88 0.3929 0.6804 0.0309 0.0178 0.562 3.938 3.060 419.308 0.445 13.613 3.310 0.50 167572. 0.2427
|
|
49.23 0.4126 0.6778 0.0275 0.0167 0.528 3.695 2.724 393.393 0.417 12.117 3.141 0.50 167813. 0.2173
|
|
51.57 0.4322 0.6686 0.0240 0.0155 0.490 3.434 2.384 365.606 0.388 10.602 2.957 0.50 168062. 0.1913
|
|
53.92 0.4519 0.6509 0.0206 0.0143 0.451 3.155 2.040 335.997 0.357 9.074 2.754 0.50 168321. 0.1649
|
|
56.26 0.4715 0.6223 0.0171 0.0129 0.409 2.861 1.694 304.642 0.323 7.537 2.523 0.51 168588. 0.1376
|
|
58.61 0.4912 0.5785 0.0136 0.0115 0.364 2.551 1.348 271.639 0.288 5.998 2.252 0.51 168865. 0.1096
|
|
60.95 0.5108 0.5129 0.0101 0.0101 0.318 2.227 1.003 237.119 0.252 4.463 1.919 0.51 169151. 0.0806
|
|
63.29 0.5305 0.4135 0.0067 0.0086 0.270 1.890 0.661 201.248 0.214 2.941 1.490 0.51 169445. 0.0508
|
|
65.64 0.5501 0.2574 0.0033 0.0070 0.220 1.542 0.324 164.215 0.174 1.440 0.894 0.51 169748. 0.0213
|
|
67.98 0.5698 -0.0114 -0.0001 0.0053 0.169 1.182 -0.011 125.818 0.133 -0.047 -0.038 0.51 170045. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 10000
|
|
|
|
V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
|
|
(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
|
|
0.00 0.0000 0.0000 0.0802 0.0242 1.049 6.609 9.824 781.894 0.747 43.695 5.699 0.56 182736. 0.7486
|
|
2.64 0.0199 0.0641 0.0788 0.0244 1.057 6.663 9.643 788.344 0.753 42.892 5.548 0.56 182834. 0.7221
|
|
5.27 0.0398 0.1248 0.0772 0.0246 1.065 6.710 9.450 793.896 0.758 42.035 5.399 0.56 182939. 0.6957
|
|
7.91 0.0596 0.1821 0.0755 0.0247 1.071 6.748 9.246 798.386 0.762 41.125 5.253 0.56 183051. 0.6694
|
|
10.54 0.0795 0.2361 0.0737 0.0248 1.075 6.776 9.028 801.649 0.766 40.158 5.108 0.56 183171. 0.6433
|
|
13.18 0.0994 0.2869 0.0719 0.0249 1.078 6.792 8.798 803.521 0.767 39.133 4.966 0.56 183298. 0.6174
|
|
15.81 0.1193 0.3346 0.0699 0.0249 1.078 6.794 8.554 803.833 0.768 38.048 4.827 0.56 183433. 0.5917
|
|
18.45 0.1392 0.3793 0.0678 0.0249 1.076 6.782 8.296 802.418 0.766 36.902 4.689 0.56 183576. 0.5661
|
|
21.09 0.1591 0.4210 0.0655 0.0248 1.072 6.754 8.025 799.114 0.763 35.693 4.555 0.56 183728. 0.5408
|
|
23.72 0.1789 0.4599 0.0632 0.0246 1.064 6.709 7.739 793.761 0.758 34.422 4.422 0.56 183888. 0.5156
|
|
26.36 0.1988 0.4959 0.0608 0.0244 1.054 6.645 7.439 786.209 0.751 33.086 4.291 0.56 184056. 0.4905
|
|
28.99 0.2187 0.5291 0.0582 0.0241 1.041 6.562 7.124 776.314 0.741 31.688 4.162 0.56 184234. 0.4656
|
|
31.63 0.2386 0.5595 0.0555 0.0237 1.024 6.457 6.796 763.943 0.730 30.227 4.035 0.56 184420. 0.4408
|
|
34.27 0.2585 0.5870 0.0527 0.0232 1.004 6.330 6.453 748.961 0.715 28.703 3.908 0.56 184616. 0.4161
|
|
36.90 0.2783 0.6117 0.0498 0.0227 0.981 6.180 6.096 731.220 0.698 27.116 3.781 0.56 184821. 0.3913
|
|
39.54 0.2982 0.6335 0.0468 0.0220 0.953 6.006 5.726 710.620 0.679 25.469 3.655 0.56 185036. 0.3665
|
|
42.17 0.3181 0.6521 0.0436 0.0213 0.922 5.808 5.343 687.173 0.656 23.767 3.527 0.56 185260. 0.3417
|
|
44.81 0.3380 0.6673 0.0404 0.0205 0.886 5.586 4.950 660.907 0.631 22.017 3.397 0.56 185493. 0.3168
|
|
47.44 0.3579 0.6788 0.0371 0.0196 0.847 5.340 4.546 631.842 0.603 20.222 3.264 0.56 185737. 0.2917
|
|
50.08 0.3777 0.6862 0.0338 0.0186 0.805 5.071 4.134 599.997 0.573 18.390 3.125 0.56 185990. 0.2663
|
|
52.72 0.3976 0.6887 0.0303 0.0175 0.758 4.779 3.715 565.396 0.540 16.524 2.980 0.56 186253. 0.2407
|
|
55.35 0.4175 0.6855 0.0269 0.0164 0.708 4.463 3.289 528.078 0.504 14.629 2.825 0.56 186526. 0.2147
|
|
57.99 0.4374 0.6751 0.0233 0.0151 0.655 4.126 2.858 488.102 0.466 12.712 2.656 0.56 186810. 0.1882
|
|
60.62 0.4573 0.6556 0.0198 0.0138 0.597 3.766 2.423 445.550 0.425 10.779 2.467 0.56 187103. 0.1610
|
|
63.26 0.4772 0.6239 0.0162 0.0124 0.537 3.385 1.987 400.539 0.382 8.837 2.250 0.56 187407. 0.1329
|
|
65.89 0.4970 0.5749 0.0127 0.0109 0.474 2.986 1.550 353.225 0.337 6.894 1.990 0.56 187721. 0.1038
|
|
68.53 0.5169 0.5001 0.0091 0.0094 0.407 2.568 1.115 303.813 0.290 4.960 1.665 0.56 188046. 0.0737
|
|
71.17 0.5368 0.3836 0.0056 0.0078 0.339 2.135 0.685 252.559 0.241 3.045 1.230 0.56 188380. 0.0426
|
|
73.80 0.5567 0.1917 0.0021 0.0062 0.268 1.688 0.261 199.723 0.191 1.160 0.592 0.56 188723. 0.0127
|
|
76.44 0.5766
|
|
|
|
|
|
|
|
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 0.0811 0.0244 1.406 8.058 12.009 1048.707 0.910 53.417 5.194 0.61 200997. 0.7544
|
|
2.86 0.0196 0.0635 0.0796 0.0246 1.418 8.124 11.792 1057.271 0.918 52.453 5.059 0.61 201104. 0.7281
|
|
5.72 0.0393 0.1236 0.0780 0.0248 1.428 8.181 11.561 1064.644 0.924 51.425 4.925 0.61 201219. 0.7019
|
|
8.59 0.0589 0.1805 0.0764 0.0249 1.436 8.226 11.316 1070.606 0.929 50.332 4.794 0.61 201341. 0.6759
|
|
11.45 0.0785 0.2341 0.0746 0.0250 1.442 8.260 11.055 1074.949 0.933 49.172 4.665 0.61 201471. 0.6500
|
|
14.31 0.0981 0.2847 0.0728 0.0251 1.445 8.279 10.778 1077.455 0.935 47.942 4.537 0.61 201609. 0.6243
|
|
17.17 0.1178 0.3322 0.0708 0.0251 1.445 8.282 10.486 1077.906 0.936 46.641 4.412 0.61 201756. 0.5988
|
|
20.03 0.1374 0.3768 0.0687 0.0251 1.443 8.268 10.177 1076.086 0.934 45.266 4.289 0.61 201911. 0.5735
|
|
22.90 0.1570 0.4185 0.0665 0.0250 1.437 8.235 9.851 1071.781 0.930 43.817 4.169 0.61 202075. 0.5484
|
|
25.76 0.1766 0.4574 0.0642 0.0248 1.428 8.182 9.508 1064.786 0.924 42.292 4.050 0.61 202249. 0.5234
|
|
28.62 0.1963 0.4935 0.0618 0.0246 1.415 8.106 9.148 1054.903 0.916 40.691 3.933 0.61 202431. 0.4986
|
|
31.48 0.2159 0.5270 0.0592 0.0243 1.397 8.006 8.771 1041.946 0.905 39.014 3.818 0.61 202623. 0.4739
|
|
34.35 0.2355 0.5577 0.0566 0.0239 1.376 7.882 8.377 1025.742 0.890 37.262 3.704 0.61 202825. 0.4494
|
|
37.21 0.2551 0.5858 0.0538 0.0234 1.349 7.731 7.966 1006.117 0.873 35.434 3.591 0.61 203037. 0.4248
|
|
40.07 0.2748 0.6111 0.0509 0.0229 1.318 7.552 7.539 982.885 0.853 33.532 3.479 0.61 203258. 0.4003
|
|
42.93 0.2944 0.6336 0.0479 0.0223 1.282 7.345 7.094 955.890 0.830 31.556 3.366 0.61 203490. 0.3758
|
|
45.79 0.3140 0.6531 0.0448 0.0215 1.241 7.109 6.635 925.128 0.803 29.512 3.253 0.61 203731. 0.3512
|
|
48.66 0.3336 0.6694 0.0416 0.0207 1.194 6.844 6.162 890.636 0.773 27.409 3.138 0.61 203983. 0.3265
|
|
51.52 0.3533 0.6823 0.0383 0.0198 1.143 6.550 5.677 852.442 0.740 25.253 3.021 0.61 204246. 0.3017
|
|
54.38 0.3729 0.6912 0.0350 0.0189 1.087 6.228 5.182 810.573 0.704 23.048 2.900 0.62 204518. 0.2766
|
|
57.24 0.3925 0.6958 0.0316 0.0178 1.026 5.879 4.677 765.056 0.664 20.802 2.773 0.62 204802. 0.2513
|
|
60.10 0.4121 0.6951 0.0281 0.0167 0.960 5.501 4.164 715.939 0.622 18.520 2.638 0.62 205096. 0.2256
|
|
62.97 0.4318 0.6879 0.0246 0.0154 0.889 5.097 3.644 663.291 0.576 16.209 2.492 0.62 205401. 0.1994
|
|
65.83 0.4514 0.6725 0.0211 0.0141 0.814 4.666 3.120 607.210 0.527 13.876 2.330 0.62 205716. 0.1725
|
|
68.69 0.4710 0.6463 0.0175 0.0128 0.735 4.209 2.592 547.834 0.476 11.530 2.146 0.62 206043. 0.1448
|
|
71.55 0.4906 0.6049 0.0139 0.0113 0.651 3.729 2.064 485.353 0.421 9.179 1.928 0.62 206381. 0.1161
|
|
74.41 0.5103 0.5413 0.0104 0.0098 0.563 3.227 1.537 420.014 0.365 6.835 1.659 0.62 206730. 0.0862
|
|
77.28 0.5299 0.4424 0.0068 0.0082 0.472 2.706 1.014 352.132 0.306 4.510 1.306 0.62 207089. 0.0551
|
|
80.14 0.5495 0.2814 0.0034 0.0066 0.378 2.167 0.498 282.068 0.245 2.216 0.801 0.62 207459. 0.0237
|
|
83.00 0.5692 -0.0104 -0.0001 0.0049 0.281 1.609 -0.013 209.397 0.182 -0.059 -0.029 0.62 207819. 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 0.0820 0.0247 1.846 9.695 14.461 1376.464 1.095 64.324 4.765 0.67 219254. 0.7595
|
|
3.14 0.0197 0.0638 0.0806 0.0249 1.861 9.775 14.201 1387.737 1.104 63.164 4.641 0.67 219372. 0.7331
|
|
6.27 0.0394 0.1242 0.0790 0.0251 1.874 9.843 13.923 1397.400 1.112 61.927 4.519 0.67 219498. 0.7067
|
|
9.41 0.0591 0.1814 0.0773 0.0252 1.884 9.897 13.627 1405.158 1.118 60.611 4.399 0.67 219632. 0.6805
|
|
12.54 0.0788 0.2354 0.0755 0.0253 1.892 9.937 13.312 1410.734 1.123 59.212 4.280 0.67 219776. 0.6545
|
|
15.68 0.0986 0.2862 0.0736 0.0254 1.896 9.958 12.978 1413.834 1.125 57.728 4.164 0.67 219928. 0.6287
|
|
18.81 0.1183 0.3340 0.0716 0.0254 1.896 9.961 12.625 1414.167 1.125 56.156 4.049 0.67 220090. 0.6030
|
|
21.95 0.1380 0.3789 0.0695 0.0253 1.893 9.942 12.251 1411.442 1.123 54.494 3.937 0.67 220261. 0.5776
|
|
25.09 0.1577 0.4209 0.0673 0.0252 1.885 9.899 11.857 1405.378 1.118 52.741 3.827 0.67 220442. 0.5523
|
|
28.22 0.1774 0.4601 0.0649 0.0250 1.872 9.831 11.442 1395.697 1.111 50.895 3.718 0.67 220633. 0.5272
|
|
31.36 0.1971 0.4965 0.0624 0.0248 1.853 9.735 11.006 1382.139 1.100 48.956 3.612 0.67 220835. 0.5022
|
|
34.49 0.2168 0.5303 0.0598 0.0245 1.830 9.611 10.550 1364.458 1.086 46.925 3.507 0.67 221046. 0.4774
|
|
37.63 0.2365 0.5614 0.0571 0.0241 1.800 9.455 10.072 1342.423 1.068 44.801 3.403 0.67 221269. 0.4527
|
|
40.77 0.2562 0.5898 0.0543 0.0236 1.765 9.268 9.574 1315.810 1.047 42.585 3.300 0.67 221502. 0.4280
|
|
43.90 0.2759 0.6155 0.0514 0.0230 1.722 9.046 9.055 1284.368 1.022 40.278 3.198 0.67 221746. 0.4033
|
|
47.04 0.2957 0.6383 0.0483 0.0224 1.673 8.790 8.516 1247.895 0.993 37.880 3.095 0.67 222001. 0.3786
|
|
50.17 0.3154 0.6582 0.0451 0.0216 1.618 8.497 7.959 1206.395 0.960 35.401 2.992 0.67 222267. 0.3538
|
|
53.31 0.3351 0.6749 0.0419 0.0208 1.555 8.170 7.385 1159.917 0.923 32.849 2.888 0.67 222544. 0.3289
|
|
56.44 0.3548 0.6882 0.0386 0.0199 1.487 7.808 6.797 1108.501 0.882 30.232 2.781 0.67 222833. 0.3039
|
|
59.58 0.3745 0.6976 0.0351 0.0189 1.411 7.411 6.195 1052.183 0.837 27.557 2.671 0.67 223134. 0.2786
|
|
62.72 0.3942 0.7025 0.0317 0.0178 1.329 6.980 5.582 991.006 0.789 24.831 2.555 0.67 223446. 0.2530
|
|
65.85 0.4139 0.7021 0.0281 0.0166 1.240 6.516 4.960 925.034 0.736 22.061 2.432 0.67 223769. 0.2270
|
|
68.99 0.4336 0.6951 0.0246 0.0153 1.146 6.018 4.329 854.362 0.680 19.257 2.298 0.67 224105. 0.2004
|
|
72.12 0.4533 0.6797 0.0209 0.0140 1.045 5.488 3.693 779.130 0.620 16.426 2.150 0.67 224452. 0.1732
|
|
75.26 0.4731 0.6531 0.0173 0.0125 0.938 4.927 3.053 699.530 0.557 13.580 1.980 0.67 224811. 0.1450
|
|
78.39 0.4928 0.6106 0.0137 0.0110 0.826 4.338 2.412 615.828 0.490 10.729 1.777 0.67 225183. 0.1156
|
|
81.53 0.5125 0.5441 0.0101 0.0095 0.709 3.722 1.773 528.372 0.420 7.888 1.522 0.68 225566. 0.0850
|
|
84.67 0.5322 0.4386 0.0065 0.0078 0.587 3.082 1.140 437.609 0.348 5.071 1.182 0.68 225962. 0.0529
|
|
87.80 0.5519 0.2617 0.0029 0.0062 0.461 2.423 0.516 344.042 0.274 2.294 0.680 0.68 226368. 0.0205
|
|
90.94 0.5716
|
|
|
|
|
|
|
|
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 0.0831 0.0250 2.382 11.547 17.203 1775.971 1.305 76.519 4.394 0.72 237504. 0.7638
|
|
3.40 0.0197 0.0638 0.0817 0.0252 2.401 11.640 16.895 1790.315 1.315 75.150 4.280 0.72 237633. 0.7374
|
|
6.80 0.0395 0.1243 0.0801 0.0254 2.417 11.720 16.566 1802.598 1.324 73.686 4.168 0.72 237771. 0.7111
|
|
10.20 0.0592 0.1815 0.0784 0.0256 2.430 11.784 16.216 1812.416 1.331 72.128 4.058 0.72 237918. 0.6849
|
|
13.60 0.0789 0.2355 0.0766 0.0257 2.440 11.829 15.843 1819.383 1.336 70.470 3.950 0.72 238074. 0.6589
|
|
17.00 0.0986 0.2864 0.0747 0.0257 2.445 11.853 15.447 1823.104 1.339 68.709 3.843 0.72 238241. 0.6331
|
|
20.40 0.1184 0.3344 0.0726 0.0257 2.445 11.854 15.028 1823.195 1.339 66.843 3.739 0.72 238417. 0.6074
|
|
23.80 0.1381 0.3794 0.0705 0.0257 2.440 11.828 14.584 1819.279 1.336 64.868 3.636 0.72 238604. 0.5819
|
|
27.20 0.1578 0.4216 0.0682 0.0255 2.429 11.775 14.115 1810.988 1.330 62.784 3.535 0.72 238801. 0.5567
|
|
30.60 0.1776 0.4610 0.0658 0.0254 2.411 11.690 13.621 1797.968 1.321 60.588 3.436 0.72 239010. 0.5315
|
|
34.00 0.1973 0.4977 0.0633 0.0251 2.387 11.572 13.103 1779.880 1.307 58.281 3.339 0.72 239229. 0.5066
|
|
37.40 0.2170 0.5318 0.0607 0.0248 2.355 11.420 12.559 1756.409 1.290 55.861 3.243 0.72 239460. 0.4817
|
|
40.80 0.2367 0.5632 0.0580 0.0244 2.316 11.230 11.990 1727.261 1.269 53.331 3.148 0.72 239702. 0.4569
|
|
44.20 0.2565 0.5919 0.0551 0.0239 2.269 11.002 11.396 1692.149 1.243 50.691 3.055 0.72 239956. 0.4322
|
|
47.60 0.2762 0.6180 0.0521 0.0233 2.214 10.733 10.778 1650.753 1.213 47.940 2.961 0.72 240221. 0.4075
|
|
51.00 0.2959 0.6413 0.0490 0.0226 2.149 10.421 10.135 1602.813 1.177 45.081 2.868 0.73 240499. 0.3827
|
|
54.40 0.3156 0.6616 0.0458 0.0218 2.076 10.067 9.470 1548.326 1.137 42.124 2.774 0.73 240788. 0.3578
|
|
57.80 0.3354 0.6789 0.0425 0.0210 1.995 9.670 8.786 1487.365 1.093 39.079 2.679 0.73 241090. 0.3328
|
|
61.20 0.3551 0.6928 0.0391 0.0200 1.904 9.232 8.083 1419.987 1.043 35.955 2.582 0.73 241404. 0.3077
|
|
64.60 0.3748 0.7028 0.0356 0.0190 1.805 8.753 7.365 1346.250 0.989 32.761 2.482 0.73 241731. 0.2823
|
|
68.00 0.3946 0.7084 0.0321 0.0179 1.698 8.233 6.634 1266.229 0.930 29.506 2.376 0.73 242070. 0.2565
|
|
71.40 0.4143 0.7087 0.0285 0.0166 1.582 7.672 5.890 1180.029 0.867 26.199 2.264 0.73 242421. 0.2303
|
|
74.80 0.4340 0.7024 0.0248 0.0153 1.459 7.073 5.137 1087.807 0.799 22.849 2.142 0.73 242786. 0.2035
|
|
78.20 0.4537 0.6876 0.0212 0.0140 1.327 6.435 4.377 989.784 0.727 19.468 2.006 0.73 243163. 0.1759
|
|
81.60 0.4735 0.6613 0.0175 0.0125 1.189 5.762 3.612 886.267 0.651 16.066 1.849 0.73 243553. 0.1472
|
|
85.00 0.4932 0.6186 0.0138 0.0110 1.043 5.056 2.846 777.668 0.571 12.660 1.660 0.73 243957. 0.1174
|
|
88.40 0.5129 0.5509 0.0101 0.0094 0.891 4.321 2.083 664.520 0.488 9.264 1.422 0.73 244373. 0.0860
|
|
91.80 0.5327 0.4421 0.0064 0.0077 0.734 3.560 1.326 547.497 0.402 5.897 1.098 0.73 244802. 0.0530
|
|
95.20 0.5524 0.2568 0.0028 0.0060 0.573 2.778 0.580 427.347 0.314 2.578 0.615 0.73 245243. 0.0196
|
|
98.60 0.5721
|
|
|
|
|
|
|
|
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 0.0844 0.0257 3.055 13.753 20.264 2278.017 1.554 90.133 4.035 0.78 255748. 0.7612
|
|
3.66 0.0197 0.0631 0.0830 0.0259 3.075 13.842 19.906 2292.807 1.564 88.540 3.938 0.78 255887. 0.7363
|
|
7.31 0.0394 0.1231 0.0814 0.0260 3.091 13.917 19.522 2305.229 1.572 86.835 3.841 0.78 256037. 0.7113
|
|
10.97 0.0591 0.1800 0.0797 0.0261 3.104 13.975 19.114 2314.811 1.579 85.018 3.745 0.78 256196. 0.6862
|
|
14.62 0.0788 0.2340 0.0778 0.0262 3.113 14.013 18.678 2321.084 1.583 83.082 3.650 0.78 256365. 0.6612
|
|
18.28 0.0985 0.2849 0.0759 0.0262 3.116 14.028 18.216 2323.553 1.585 81.024 3.556 0.78 256545. 0.6361
|
|
21.93 0.1182 0.3329 0.0739 0.0262 3.113 14.017 17.725 2321.713 1.584 78.840 3.463 0.78 256736. 0.6110
|
|
25.59 0.1379 0.3781 0.0717 0.0261 3.105 13.977 17.205 2315.069 1.579 76.527 3.371 0.78 256938. 0.5860
|
|
29.24 0.1575 0.4205 0.0694 0.0260 3.089 13.905 16.655 2303.115 1.571 74.084 3.280 0.78 257151. 0.5610
|
|
32.90 0.1772 0.4601 0.0670 0.0258 3.065 13.797 16.076 2285.366 1.559 71.508 3.191 0.78 257376. 0.5362
|
|
36.55 0.1969 0.4971 0.0645 0.0255 3.033 13.652 15.467 2261.343 1.542 68.799 3.102 0.78 257613. 0.5114
|
|
40.21 0.2166 0.5315 0.0618 0.0252 2.991 13.467 14.829 2230.601 1.521 65.957 3.015 0.78 257862. 0.4866
|
|
43.86 0.2363 0.5632 0.0590 0.0248 2.941 13.238 14.160 2192.742 1.496 62.984 2.929 0.78 258124. 0.4619
|
|
47.52 0.2560 0.5923 0.0561 0.0242 2.880 12.964 13.462 2147.370 1.465 59.880 2.843 0.78 258397. 0.4373
|
|
51.17 0.2757 0.6188 0.0531 0.0236 2.808 12.643 12.735 2094.063 1.428 56.645 2.758 0.78 258684. 0.4126
|
|
54.83 0.2954 0.6425 0.0499 0.0230 2.726 12.271 11.979 2032.502 1.386 53.281 2.673 0.78 258983. 0.3878
|
|
58.48 0.3151 0.6634 0.0467 0.0222 2.632 11.849 11.196 1962.703 1.339 49.801 2.587 0.78 259295. 0.3629
|
|
62.14 0.3348 0.6811 0.0433 0.0213 2.528 11.379 10.390 1884.802 1.286 46.215 2.500 0.78 259620. 0.3378
|
|
65.79 0.3545 0.6954 0.0399 0.0203 2.412 10.861 9.563 1798.928 1.227 42.535 2.411 0.78 259958. 0.3125
|
|
69.45 0.3742 0.7059 0.0363 0.0193 2.287 10.295 8.716 1705.222 1.163 38.770 2.318 0.78 260309. 0.2869
|
|
73.10 0.3939 0.7118 0.0327 0.0181 2.151 9.683 7.853 1603.864 1.094 34.932 2.221 0.78 260674. 0.2609
|
|
76.76 0.4136 0.7122 0.0291 0.0169 2.005 9.026 6.976 1495.091 1.020 31.031 2.116 0.78 261052. 0.2343
|
|
80.41 0.4333 0.7057 0.0254 0.0156 1.850 8.327 6.087 1379.214 0.941 27.077 2.002 0.78 261444. 0.2070
|
|
84.07 0.4529 0.6904 0.0216 0.0142 1.685 7.587 5.190 1256.645 0.857 23.084 1.873 0.79 261850. 0.1788
|
|
87.72 0.4726 0.6629 0.0179 0.0127 1.513 6.810 4.286 1127.925 0.769 19.065 1.724 0.79 262269. 0.1496
|
|
91.38 0.4923 0.6182 0.0141 0.0112 1.333 5.999 3.381 993.731 0.678 15.038 1.543 0.79 262703. 0.1189
|
|
95.03 0.5120 0.5477 0.0103 0.0097 1.146 5.161 2.478 854.909 0.583 11.021 1.315 0.79 263150. 0.0867
|
|
98.69 0.5317 0.4356 0.0066 0.0080 0.955 4.301 1.582 712.474 0.486 7.035 1.007 0.79 263611. 0.0531
|
|
102.34 0.5514 0.2501 0.0029 0.0064 0.761 3.426 0.698 567.520 0.387 3.103 0.557 0.79 264085. 0.0195
|
|
106.00 0.5711
|
|
|
|
|
|
|
|
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 0.0860 0.0274 3.999 16.805 23.679 2982.338 1.899 105.323 3.601 0.83 273981. 0.7344
|
|
3.88 0.0195 0.0601 0.0845 0.0274 4.009 16.845 23.270 2989.373 1.903 103.504 3.531 0.83 274131. 0.7138
|
|
7.77 0.0391 0.1178 0.0829 0.0275 4.014 16.868 22.832 2993.596 1.906 101.556 3.459 0.83 274291. 0.6928
|
|
11.65 0.0586 0.1730 0.0812 0.0275 4.016 16.874 22.364 2994.545 1.906 99.475 3.387 0.83 274461. 0.6714
|
|
15.54 0.0781 0.2258 0.0794 0.0275 4.012 16.858 21.865 2991.731 1.905 97.257 3.315 0.83 274642. 0.6497
|
|
19.42 0.0977 0.2761 0.0775 0.0274 4.002 16.818 21.335 2984.652 1.900 94.897 3.242 0.83 274835. 0.6277
|
|
23.31 0.1172 0.3238 0.0754 0.0273 3.987 16.751 20.771 2972.782 1.893 92.390 3.169 0.83 275039. 0.6054
|
|
27.19 0.1367 0.3690 0.0732 0.0271 3.963 16.654 20.174 2955.577 1.882 89.733 3.096 0.83 275254. 0.5828
|
|
31.07 0.1563 0.4118 0.0709 0.0269 3.933 16.524 19.542 2932.498 1.867 86.923 3.023 0.83 275482. 0.5600
|
|
34.96 0.1758 0.4520 0.0685 0.0267 3.893 16.358 18.876 2903.002 1.848 83.959 2.949 0.83 275722. 0.5370
|
|
38.84 0.1953 0.4897 0.0660 0.0263 3.844 16.152 18.174 2866.545 1.825 80.839 2.876 0.83 275974. 0.5138
|
|
42.73 0.2149 0.5249 0.0633 0.0259 3.785 15.905 17.438 2822.608 1.797 77.564 2.802 0.83 276240. 0.4904
|
|
46.61 0.2344 0.5575 0.0605 0.0254 3.716 15.612 16.667 2770.700 1.764 74.135 2.728 0.84 276518. 0.4669
|
|
50.50 0.2539 0.5875 0.0576 0.0249 3.635 15.275 15.862 2710.890 1.726 70.553 2.654 0.84 276809. 0.4430
|
|
54.38 0.2735 0.6147 0.0545 0.0243 3.544 14.892 15.022 2642.779 1.682 66.819 2.578 0.84 277113. 0.4188
|
|
58.27 0.2930 0.6389 0.0514 0.0236 3.441 14.457 14.149 2565.687 1.633 62.934 2.501 0.84 277431. 0.3943
|
|
62.15 0.3125 0.6600 0.0481 0.0228 3.326 13.974 13.244 2479.865 1.579 58.910 2.422 0.84 277762. 0.3695
|
|
66.03 0.3321 0.6777 0.0447 0.0219 3.199 13.441 12.311 2385.282 1.519 54.761 2.341 0.84 278107. 0.3443
|
|
69.92 0.3516 0.6918 0.0412 0.0209 3.060 12.857 11.353 2281.719 1.453 50.500 2.257 0.84 278466. 0.3187
|
|
73.80 0.3711 0.7017 0.0377 0.0199 2.909 12.224 10.373 2169.336 1.381 46.138 2.169 0.84 278838. 0.2928
|
|
77.69 0.3907 0.7067 0.0340 0.0188 2.747 11.543 9.372 2048.535 1.304 41.688 2.075 0.84 279224. 0.2663
|
|
81.57 0.4102 0.7058 0.0303 0.0176 2.575 10.818 8.354 1919.829 1.222 37.160 1.974 0.84 279625. 0.2391
|
|
85.46 0.4297 0.6975 0.0266 0.0164 2.392 10.052 7.322 1783.876 1.136 32.569 1.862 0.84 280039. 0.2111
|
|
89.34 0.4493 0.6795 0.0228 0.0151 2.201 9.249 6.278 1641.339 1.045 27.927 1.735 0.84 280468. 0.1822
|
|
93.22 0.4688 0.6490 0.0190 0.0137 2.002 8.413 5.227 1493.090 0.951 23.251 1.588 0.84 280912. 0.1522
|
|
97.11 0.4883 0.6012 0.0151 0.0123 1.797 7.552 4.172 1340.161 0.853 18.559 1.412 0.84 281370. 0.1209
|
|
100.99 0.5079 0.5291 0.0113 0.0109 1.587 6.670 3.119 1183.759 0.754 13.872 1.195 0.84 281842. 0.0885
|
|
104.88 0.5274 0.4215 0.0075 0.0094 1.375 5.777 2.072 1025.290 0.653 9.217 0.917 0.84 282330. 0.0553
|
|
108.76 0.5469 0.2591 0.0038 0.0080 1.162 4.881 1.038 866.195 0.551 4.617 0.543 0.85 282830. 0.0232
|
|
112.65 0.5664 0.0044 0.0001 0.0065 0.946 3.974 0.014 705.334 0.449 0.061 0.009 0.85 283327. 0.0000
|
|
|
|
|
|
|
|
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 0.0875 0.0308 5.452 21.477 27.420 4065.544 2.426 121.963 3.059 0.89 292209. 0.6714
|
|
4.16 0.0196 0.0550 0.0860 0.0307 5.435 21.410 26.958 4052.869 2.419 119.910 3.017 0.89 292370. 0.6565
|
|
8.32 0.0392 0.1085 0.0844 0.0305 5.412 21.321 26.462 4036.086 2.409 117.703 2.974 0.89 292542. 0.6411
|
|
12.48 0.0588 0.1603 0.0827 0.0304 5.384 21.209 25.930 4014.781 2.396 115.338 2.929 0.89 292726. 0.6252
|
|
16.64 0.0785 0.2104 0.0809 0.0302 5.349 21.070 25.362 3988.482 2.380 112.809 2.884 0.89 292921. 0.6088
|
|
20.80 0.0981 0.2588 0.0790 0.0299 5.306 20.902 24.755 3956.720 2.361 110.108 2.838 0.89 293129. 0.5917
|
|
24.96 0.1177 0.3054 0.0769 0.0296 5.256 20.703 24.108 3919.030 2.339 107.232 2.790 0.89 293349. 0.5742
|
|
29.12 0.1373 0.3500 0.0747 0.0293 5.196 20.470 23.421 3874.939 2.313 104.176 2.741 0.89 293582. 0.5561
|
|
33.28 0.1569 0.3928 0.0724 0.0289 5.128 20.201 22.693 3823.978 2.282 100.937 2.692 0.89 293828. 0.5374
|
|
37.45 0.1765 0.4335 0.0699 0.0285 5.050 19.893 21.923 3765.677 2.247 97.512 2.641 0.89 294088. 0.5182
|
|
41.61 0.1961 0.4721 0.0674 0.0280 4.961 19.543 21.111 3699.561 2.208 93.902 2.588 0.89 294361. 0.4984
|
|
45.77 0.2158 0.5085 0.0646 0.0274 4.861 19.150 20.258 3625.144 2.164 90.107 2.535 0.89 294647. 0.4781
|
|
49.93 0.2354 0.5427 0.0618 0.0268 4.750 18.711 19.363 3541.934 2.114 86.128 2.480 0.89 294948. 0.4573
|
|
54.09 0.2550 0.5745 0.0588 0.0261 4.626 18.223 18.428 3449.677 2.059 81.967 2.423 0.89 295262. 0.4359
|
|
58.25 0.2746 0.6034 0.0557 0.0253 4.493 17.697 17.452 3350.089 1.999 77.625 2.363 0.89 295591. 0.4137
|
|
62.41 0.2942 0.6290 0.0524 0.0245 4.348 17.130 16.435 3242.662 1.935 73.102 2.299 0.89 295933. 0.3906
|
|
66.57 0.3138 0.6509 0.0491 0.0237 4.195 16.524 15.381 3127.917 1.867 68.414 2.230 0.89 296291. 0.3666
|
|
70.73 0.3334 0.6684 0.0456 0.0228 4.033 15.888 14.294 3007.489 1.795 63.578 2.156 0.89 296662. 0.3416
|
|
74.89 0.3531 0.6803 0.0420 0.0218 3.868 15.237 13.176 2884.313 1.721 58.606 2.072 0.89 297049. 0.3152
|
|
79.05 0.3727 0.6865 0.0384 0.0208 3.694 14.553 12.031 2754.787 1.644 53.516 1.981 0.89 297450. 0.2880
|
|
83.21 0.3923 0.6868 0.0347 0.0198 3.510 13.826 10.864 2617.189 1.562 48.323 1.883 0.90 297866. 0.2601
|
|
87.37 0.4119 0.6799 0.0309 0.0187 3.316 13.061 9.676 2472.440 1.476 43.040 1.775 0.90 298298. 0.2314
|
|
91.53 0.4315 0.6642 0.0270 0.0176 3.113 12.265 8.472 2321.671 1.386 37.684 1.655 0.90 298744. 0.2019
|
|
95.69 0.4511 0.6373 0.0231 0.0164 2.905 11.443 7.255 2166.181 1.293 32.272 1.519 0.90 299206. 0.1715
|
|
99.85 0.4707 0.5965 0.0192 0.0152 2.692 10.603 6.030 2007.119 1.198 26.823 1.363 0.90 299683. 0.1403
|
|
104.02 0.4904 0.5381 0.0153 0.0140 2.475 9.752 4.802 1845.976 1.102 21.361 1.180 0.90 300176. 0.1084
|
|
108.18 0.5100 0.4568 0.0114 0.0127 2.259 8.898 3.577 1684.361 1.005 15.912 0.963 0.90 300684. 0.0764
|
|
112.34 0.5296 0.3462 0.0075 0.0115 2.044 8.051 2.362 1523.998 0.910 10.507 0.703 0.90 301208. 0.0453
|
|
116.50 0.5492 0.1973 0.0037 0.0103 1.832 7.218 1.164 1366.412 0.816 5.177 0.386 0.90 301747. 0.0175
|
|
120.66 0.5688 -0.0050 -0.0001 0.0091 1.618 6.375 -0.025 1206.740 0.720 -0.112 -0.009 0.90 302283. 0.0000
|
|
|
|
|
|
|