612 lines
109 KiB
Plaintext
612 lines
109 KiB
Plaintext
15x7E (15x7E.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 0.0807 0.0317 0.002 0.122 0.130 1.446 0.014 0.579 40.863 0.06 20957. 0.5769
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0.30 0.0208 0.0517 0.0793 0.0319 0.002 0.123 0.128 1.455 0.014 0.569 39.913 0.06 20969. 0.5586
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0.59 0.0416 0.1009 0.0778 0.0321 0.002 0.124 0.126 1.462 0.014 0.559 38.956 0.06 20981. 0.5400
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0.89 0.0624 0.1476 0.0763 0.0322 0.002 0.124 0.123 1.469 0.014 0.547 37.995 0.06 20995. 0.5213
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1.18 0.0832 0.1918 0.0746 0.0323 0.002 0.125 0.120 1.473 0.014 0.535 37.032 0.06 21009. 0.5024
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1.48 0.1040 0.2335 0.0728 0.0324 0.002 0.125 0.117 1.476 0.014 0.522 36.067 0.06 21024. 0.4834
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1.77 0.1248 0.2727 0.0709 0.0324 0.002 0.125 0.114 1.477 0.014 0.508 35.100 0.06 21041. 0.4642
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2.07 0.1456 0.3094 0.0688 0.0324 0.002 0.125 0.111 1.476 0.014 0.494 34.131 0.06 21058. 0.4449
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2.36 0.1664 0.3435 0.0667 0.0323 0.002 0.124 0.108 1.472 0.014 0.479 33.159 0.06 21076. 0.4255
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2.66 0.1872 0.3751 0.0644 0.0322 0.002 0.124 0.104 1.465 0.014 0.462 32.184 0.06 21096. 0.4059
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2.95 0.2080 0.4041 0.0621 0.0319 0.002 0.123 0.100 1.455 0.014 0.445 31.202 0.06 21117. 0.3862
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3.25 0.2288 0.4304 0.0596 0.0317 0.002 0.122 0.096 1.443 0.014 0.427 30.213 0.06 21139. 0.3664
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3.54 0.2496 0.4540 0.0569 0.0313 0.002 0.121 0.092 1.427 0.014 0.409 29.212 0.06 21162. 0.3464
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3.84 0.2704 0.4747 0.0542 0.0309 0.002 0.119 0.087 1.407 0.013 0.389 28.195 0.06 21186. 0.3262
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4.14 0.2912 0.4924 0.0514 0.0304 0.002 0.117 0.083 1.384 0.013 0.369 27.158 0.06 21211. 0.3058
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4.43 0.3120 0.5069 0.0484 0.0298 0.002 0.115 0.078 1.357 0.013 0.347 26.094 0.06 21238. 0.2852
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4.73 0.3327 0.5179 0.0453 0.0291 0.002 0.112 0.073 1.326 0.013 0.325 24.995 0.06 21266. 0.2643
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5.02 0.3535 0.5252 0.0421 0.0283 0.002 0.109 0.068 1.291 0.012 0.302 23.854 0.06 21295. 0.2432
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5.32 0.3743 0.5283 0.0388 0.0275 0.002 0.106 0.063 1.253 0.012 0.279 22.662 0.06 21326. 0.2218
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5.61 0.3951 0.5267 0.0354 0.0266 0.002 0.102 0.057 1.212 0.012 0.254 21.407 0.06 21357. 0.2002
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5.91 0.4159 0.5200 0.0320 0.0256 0.002 0.099 0.052 1.167 0.011 0.230 20.075 0.06 21390. 0.1785
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6.20 0.4367 0.5072 0.0285 0.0245 0.001 0.095 0.046 1.118 0.011 0.205 18.651 0.06 21424. 0.1565
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6.50 0.4575 0.4876 0.0250 0.0234 0.001 0.090 0.040 1.067 0.010 0.179 17.114 0.06 21460. 0.1343
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6.79 0.4783 0.4599 0.0214 0.0222 0.001 0.086 0.034 1.013 0.010 0.153 15.439 0.06 21497. 0.1121
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7.09 0.4991 0.4225 0.0177 0.0210 0.001 0.081 0.029 0.955 0.009 0.127 13.595 0.06 21535. 0.0900
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7.39 0.5199 0.3736 0.0141 0.0196 0.001 0.076 0.023 0.895 0.009 0.101 11.538 0.06 21574. 0.0681
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7.68 0.5407 0.3104 0.0105 0.0183 0.001 0.070 0.017 0.833 0.008 0.075 9.217 0.06 21615. 0.0469
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7.98 0.5615 0.2293 0.0069 0.0169 0.001 0.065 0.011 0.768 0.007 0.049 6.559 0.06 21657. 0.0270
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8.27 0.5823 0.1256 0.0033 0.0154 0.001 0.059 0.005 0.701 0.007 0.024 3.465 0.06 21701. 0.0099
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8.57 0.6031 -0.0080 -0.0002 0.0139 0.001 0.053 0.000 0.633 0.006 -0.001 -0.212 0.06 21745. 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 0.0810 0.0287 0.014 0.442 0.523 10.467 0.050 2.326 22.659 0.12 41914. 0.6409
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0.59 0.0209 0.0575 0.0796 0.0289 0.014 0.446 0.514 10.550 0.050 2.286 22.092 0.12 41937. 0.6195
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1.19 0.0418 0.1120 0.0781 0.0291 0.014 0.449 0.504 10.624 0.051 2.243 21.526 0.12 41962. 0.5979
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1.78 0.0626 0.1635 0.0765 0.0293 0.014 0.452 0.494 10.687 0.051 2.197 20.963 0.12 41989. 0.5763
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2.37 0.0835 0.2122 0.0748 0.0295 0.014 0.454 0.483 10.737 0.051 2.148 20.402 0.12 42018. 0.5546
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2.97 0.1044 0.2580 0.0730 0.0295 0.014 0.455 0.471 10.772 0.051 2.096 19.844 0.12 42049. 0.5329
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3.56 0.1253 0.3010 0.0711 0.0296 0.014 0.456 0.459 10.791 0.052 2.041 19.291 0.12 42082. 0.5112
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4.15 0.1462 0.3412 0.0691 0.0296 0.014 0.456 0.446 10.790 0.052 1.983 18.741 0.12 42117. 0.4895
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4.75 0.1670 0.3785 0.0669 0.0295 0.014 0.455 0.432 10.768 0.051 1.921 18.196 0.12 42154. 0.4678
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5.34 0.1879 0.4132 0.0647 0.0294 0.014 0.453 0.417 10.724 0.051 1.856 17.653 0.12 42193. 0.4461
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5.93 0.2088 0.4450 0.0623 0.0292 0.014 0.450 0.402 10.654 0.051 1.788 17.113 0.12 42235. 0.4244
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6.53 0.2297 0.4741 0.0598 0.0290 0.014 0.446 0.386 10.557 0.050 1.716 16.574 0.12 42279. 0.4027
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7.12 0.2506 0.5004 0.0571 0.0286 0.014 0.441 0.369 10.432 0.050 1.640 16.034 0.12 42326. 0.3809
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7.71 0.2714 0.5237 0.0544 0.0282 0.014 0.434 0.351 10.277 0.049 1.561 15.492 0.12 42374. 0.3590
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8.30 0.2923 0.5441 0.0515 0.0277 0.014 0.426 0.332 10.090 0.048 1.479 14.945 0.12 42426. 0.3371
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8.90 0.3132 0.5613 0.0485 0.0271 0.013 0.417 0.313 9.871 0.047 1.393 14.390 0.12 42479. 0.3150
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9.49 0.3341 0.5752 0.0454 0.0264 0.013 0.406 0.293 9.618 0.046 1.304 13.823 0.12 42535. 0.2928
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10.08 0.3550 0.5853 0.0422 0.0256 0.013 0.394 0.272 9.333 0.045 1.212 13.240 0.12 42594. 0.2703
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10.68 0.3758 0.5915 0.0389 0.0247 0.012 0.381 0.251 9.015 0.043 1.117 12.635 0.12 42655. 0.2477
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11.27 0.3967 0.5931 0.0355 0.0238 0.012 0.366 0.229 8.666 0.041 1.020 12.003 0.12 42719. 0.2249
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11.86 0.4176 0.5895 0.0321 0.0227 0.011 0.350 0.207 8.287 0.040 0.921 11.335 0.12 42786. 0.2018
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12.46 0.4385 0.5800 0.0286 0.0216 0.011 0.333 0.184 7.878 0.038 0.820 10.620 0.12 42855. 0.1784
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13.05 0.4594 0.5634 0.0250 0.0204 0.010 0.314 0.162 7.440 0.036 0.718 9.847 0.12 42926. 0.1548
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13.64 0.4802 0.5382 0.0214 0.0191 0.009 0.295 0.138 6.974 0.033 0.615 8.999 0.12 43000. 0.1309
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14.24 0.5011 0.5025 0.0178 0.0178 0.009 0.274 0.115 6.481 0.031 0.512 8.051 0.12 43077. 0.1068
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14.83 0.5220 0.4533 0.0142 0.0164 0.008 0.252 0.092 5.964 0.028 0.408 6.972 0.12 43157. 0.0826
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15.42 0.5429 0.3865 0.0106 0.0149 0.007 0.229 0.068 5.423 0.026 0.304 5.717 0.12 43239. 0.0585
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16.02 0.5638 0.2962 0.0070 0.0133 0.007 0.206 0.045 4.863 0.023 0.201 4.218 0.12 43324. 0.0351
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16.61 0.5846 0.1726 0.0035 0.0118 0.006 0.181 0.022 4.285 0.020 0.100 2.371 0.12 43411. 0.0139
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17.20 0.6055 -0.0002 0.0000 0.0101 0.005 0.156 0.000 3.692 0.018 0.000 -0.003 0.12 43500. 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 0.0813 0.0274 0.045 0.951 1.180 33.747 0.107 5.250 15.864 0.18 62870. 0.6742
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0.89 0.0209 0.0605 0.0799 0.0277 0.046 0.959 1.160 34.046 0.108 5.159 15.453 0.18 62905. 0.6510
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1.79 0.0419 0.1177 0.0784 0.0279 0.046 0.967 1.138 34.314 0.109 5.062 15.044 0.18 62943. 0.6278
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2.68 0.0628 0.1718 0.0768 0.0281 0.046 0.973 1.115 34.546 0.110 4.959 14.638 0.18 62983. 0.6046
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3.57 0.0838 0.2228 0.0751 0.0282 0.047 0.979 1.090 34.734 0.111 4.849 14.236 0.18 63027. 0.5814
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4.46 0.1047 0.2707 0.0733 0.0283 0.047 0.982 1.064 34.871 0.111 4.732 13.838 0.18 63073. 0.5583
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5.36 0.1257 0.3156 0.0713 0.0284 0.047 0.985 1.036 34.950 0.111 4.608 13.444 0.18 63123. 0.5353
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6.25 0.1466 0.3576 0.0693 0.0284 0.047 0.985 1.006 34.962 0.111 4.476 13.055 0.18 63176. 0.5123
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7.14 0.1676 0.3966 0.0671 0.0284 0.047 0.983 0.975 34.902 0.111 4.337 12.670 0.18 63232. 0.4894
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8.03 0.1885 0.4328 0.0649 0.0283 0.047 0.979 0.942 34.761 0.111 4.189 12.290 0.18 63291. 0.4666
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8.93 0.2094 0.4661 0.0625 0.0281 0.046 0.973 0.907 34.533 0.110 4.034 11.913 0.18 63354. 0.4438
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9.82 0.2304 0.4966 0.0599 0.0278 0.046 0.964 0.870 34.211 0.109 3.871 11.539 0.18 63421. 0.4211
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10.71 0.2513 0.5243 0.0573 0.0275 0.045 0.952 0.832 33.790 0.108 3.700 11.167 0.18 63491. 0.3984
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11.60 0.2723 0.5491 0.0545 0.0270 0.045 0.937 0.792 33.264 0.106 3.521 10.795 0.18 63564. 0.3757
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12.50 0.2932 0.5709 0.0516 0.0265 0.044 0.919 0.750 32.628 0.104 3.335 10.422 0.18 63641. 0.3530
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13.39 0.3142 0.5896 0.0486 0.0259 0.043 0.898 0.706 31.877 0.101 3.140 10.046 0.18 63722. 0.3302
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14.28 0.3351 0.6050 0.0455 0.0252 0.042 0.874 0.661 31.007 0.099 2.938 9.664 0.18 63807. 0.3072
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15.17 0.3561 0.6168 0.0423 0.0244 0.040 0.846 0.614 30.021 0.096 2.730 9.273 0.18 63896. 0.2842
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16.07 0.3770 0.6247 0.0390 0.0235 0.039 0.815 0.566 28.922 0.092 2.516 8.870 0.18 63988. 0.2609
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16.96 0.3980 0.6282 0.0356 0.0225 0.037 0.781 0.516 27.712 0.088 2.296 8.450 0.18 64085. 0.2375
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17.85 0.4189 0.6267 0.0321 0.0215 0.035 0.744 0.466 26.392 0.084 2.073 8.008 0.18 64185. 0.2138
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18.74 0.4398 0.6193 0.0286 0.0203 0.033 0.703 0.415 24.967 0.079 1.845 7.536 0.18 64289. 0.1899
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19.64 0.4608 0.6048 0.0250 0.0190 0.031 0.660 0.363 23.437 0.075 1.615 7.026 0.18 64397. 0.1656
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20.53 0.4817 0.5816 0.0214 0.0177 0.029 0.614 0.311 21.808 0.069 1.382 6.463 0.18 64509. 0.1409
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21.42 0.5027 0.5474 0.0178 0.0163 0.027 0.566 0.258 20.083 0.064 1.148 5.829 0.18 64625. 0.1159
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22.31 0.5236 0.4989 0.0141 0.0148 0.024 0.515 0.205 18.269 0.058 0.914 5.100 0.18 64745. 0.0904
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23.21 0.5446 0.4309 0.0105 0.0133 0.022 0.461 0.153 16.374 0.052 0.680 4.236 0.18 64869. 0.0648
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24.10 0.5655 0.3354 0.0069 0.0117 0.019 0.406 0.101 14.407 0.046 0.449 3.175 0.18 64997. 0.0394
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24.99 0.5865 0.1988 0.0034 0.0101 0.017 0.349 0.050 12.379 0.039 0.220 1.815 0.18 65129. 0.0158
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25.88 0.6074 -0.0046 -0.0001 0.0084 0.014 0.290 -0.001 10.295 0.033 -0.004 -0.040 0.18 65262. 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 0.0816 0.0267 0.105 1.647 2.106 77.943 0.186 9.368 12.257 0.24 83824. 0.6958
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1.19 0.0210 0.0623 0.0802 0.0270 0.106 1.663 2.070 78.680 0.188 9.207 11.933 0.24 83871. 0.6716
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2.38 0.0419 0.1212 0.0787 0.0272 0.106 1.677 2.031 79.345 0.189 9.035 11.611 0.24 83922. 0.6473
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3.57 0.0629 0.1769 0.0771 0.0274 0.107 1.689 1.990 79.921 0.191 8.851 11.293 0.24 83976. 0.6231
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4.76 0.0838 0.2292 0.0754 0.0276 0.108 1.699 1.946 80.392 0.192 8.655 10.978 0.24 84035. 0.5990
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5.95 0.1048 0.2784 0.0736 0.0277 0.108 1.706 1.899 80.740 0.193 8.446 10.667 0.24 84097. 0.5750
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7.15 0.1258 0.3245 0.0716 0.0278 0.109 1.710 1.849 80.948 0.193 8.225 10.361 0.24 84163. 0.5511
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8.34 0.1467 0.3676 0.0696 0.0278 0.109 1.712 1.796 80.998 0.193 7.990 10.058 0.24 84234. 0.5273
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9.53 0.1677 0.4077 0.0674 0.0277 0.108 1.709 1.740 80.872 0.193 7.741 9.761 0.24 84309. 0.5037
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10.72 0.1886 0.4448 0.0651 0.0276 0.108 1.702 1.681 80.551 0.192 7.478 9.467 0.24 84388. 0.4802
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11.91 0.2096 0.4791 0.0627 0.0274 0.107 1.691 1.619 80.021 0.191 7.202 9.177 0.24 84472. 0.4568
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13.10 0.2306 0.5106 0.0602 0.0272 0.106 1.675 1.554 79.264 0.189 6.911 8.891 0.24 84561. 0.4335
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14.29 0.2515 0.5392 0.0575 0.0268 0.105 1.654 1.485 78.266 0.187 6.606 8.606 0.24 84654. 0.4103
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15.48 0.2725 0.5649 0.0548 0.0264 0.103 1.627 1.413 77.014 0.184 6.286 8.324 0.24 84753. 0.3871
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16.67 0.2934 0.5877 0.0519 0.0259 0.101 1.595 1.338 75.496 0.180 5.953 8.041 0.24 84856. 0.3639
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17.86 0.3144 0.6075 0.0488 0.0253 0.099 1.557 1.260 73.698 0.176 5.606 7.757 0.24 84964. 0.3407
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19.05 0.3354 0.6240 0.0457 0.0246 0.096 1.513 1.179 71.612 0.171 5.246 7.470 0.24 85077. 0.3174
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20.24 0.3563 0.6371 0.0425 0.0237 0.093 1.463 1.096 69.242 0.165 4.874 7.178 0.24 85196. 0.2939
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21.44 0.3773 0.6463 0.0391 0.0228 0.089 1.407 1.010 66.595 0.159 4.492 6.878 0.24 85319. 0.2704
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22.63 0.3982 0.6513 0.0357 0.0218 0.085 1.346 0.922 63.677 0.152 4.100 6.566 0.24 85448. 0.2466
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23.82 0.4192 0.6514 0.0322 0.0207 0.081 1.278 0.832 60.491 0.144 3.701 6.239 0.24 85581. 0.2226
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25.01 0.4401 0.6458 0.0287 0.0196 0.076 1.205 0.741 57.045 0.136 3.295 5.891 0.24 85720. 0.1983
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26.20 0.4611 0.6333 0.0251 0.0183 0.072 1.127 0.648 53.344 0.127 2.884 5.514 0.24 85864. 0.1737
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27.39 0.4821 0.6121 0.0215 0.0169 0.066 1.044 0.555 49.397 0.118 2.470 5.098 0.24 86014. 0.1486
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28.58 0.5030 0.5800 0.0179 0.0155 0.061 0.955 0.461 45.217 0.108 2.052 4.629 0.24 86169. 0.1230
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29.77 0.5240 0.5331 0.0142 0.0140 0.055 0.863 0.368 40.818 0.097 1.635 4.084 0.24 86329. 0.0969
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30.96 0.5449 0.4657 0.0106 0.0124 0.049 0.765 0.274 36.218 0.086 1.219 3.431 0.24 86495. 0.0703
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32.15 0.5659 0.3686 0.0070 0.0108 0.042 0.664 0.181 31.443 0.075 0.806 2.615 0.24 86666. 0.0435
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33.34 0.5869 0.2248 0.0035 0.0091 0.036 0.560 0.090 26.519 0.063 0.400 1.538 0.24 86842. 0.0180
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34.54 0.6078 0.0003 0.0000 0.0074 0.029 0.453 0.000 21.456 0.051 0.000 0.002 0.24 87019. 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 0.0820 0.0263 0.201 2.534 3.306 149.896 0.286 14.705 10.003 0.30 104778. 0.7115
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1.49 0.0210 0.0636 0.0806 0.0266 0.203 2.559 3.249 151.374 0.289 14.452 9.735 0.30 104837. 0.6864
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2.98 0.0420 0.1238 0.0790 0.0268 0.205 2.581 3.188 152.710 0.292 14.182 9.470 0.30 104900. 0.6614
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4.47 0.0630 0.1805 0.0774 0.0270 0.206 2.601 3.123 153.872 0.294 13.893 9.207 0.30 104969. 0.6365
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5.96 0.0840 0.2339 0.0757 0.0272 0.208 2.617 3.054 154.825 0.296 13.586 8.948 0.30 105041. 0.6117
|
|
7.45 0.1049 0.2840 0.0739 0.0273 0.209 2.629 2.981 155.535 0.297 13.258 8.692 0.30 105119. 0.5871
|
|
8.94 0.1259 0.3310 0.0720 0.0274 0.209 2.637 2.903 155.967 0.298 12.911 8.441 0.30 105203. 0.5626
|
|
10.43 0.1469 0.3748 0.0699 0.0274 0.209 2.639 2.820 156.085 0.298 12.542 8.194 0.30 105291. 0.5382
|
|
11.93 0.1679 0.4157 0.0677 0.0274 0.209 2.635 2.732 155.852 0.298 12.152 7.951 0.30 105385. 0.5141
|
|
13.42 0.1889 0.4536 0.0654 0.0273 0.208 2.624 2.639 155.234 0.296 11.739 7.711 0.30 105485. 0.4900
|
|
14.91 0.2099 0.4885 0.0630 0.0271 0.207 2.607 2.541 154.198 0.294 11.304 7.476 0.30 105590. 0.4662
|
|
16.40 0.2309 0.5207 0.0605 0.0268 0.205 2.581 2.439 152.711 0.292 10.847 7.243 0.30 105701. 0.4425
|
|
17.89 0.2519 0.5500 0.0578 0.0265 0.202 2.548 2.331 150.744 0.288 10.367 7.013 0.30 105819. 0.4188
|
|
19.38 0.2729 0.5764 0.0550 0.0260 0.199 2.506 2.218 148.271 0.283 9.866 6.785 0.30 105942. 0.3953
|
|
20.87 0.2938 0.6000 0.0521 0.0255 0.195 2.456 2.100 145.266 0.277 9.342 6.558 0.30 106072. 0.3718
|
|
22.36 0.3148 0.6205 0.0490 0.0249 0.190 2.395 1.978 141.704 0.271 8.796 6.330 0.30 106207. 0.3482
|
|
23.85 0.3358 0.6379 0.0459 0.0242 0.184 2.325 1.850 137.566 0.263 8.230 6.100 0.30 106349. 0.3246
|
|
25.34 0.3568 0.6519 0.0426 0.0233 0.178 2.246 1.719 132.862 0.254 7.645 5.867 0.30 106498. 0.3009
|
|
26.83 0.3778 0.6621 0.0393 0.0224 0.171 2.157 1.584 127.602 0.244 7.044 5.629 0.30 106652. 0.2771
|
|
28.32 0.3988 0.6682 0.0358 0.0214 0.163 2.059 1.445 121.799 0.233 6.428 5.382 0.30 106813. 0.2531
|
|
29.81 0.4198 0.6696 0.0323 0.0203 0.155 1.952 1.304 115.460 0.221 5.801 5.123 0.30 106981. 0.2289
|
|
31.30 0.4408 0.6653 0.0288 0.0191 0.146 1.836 1.161 108.598 0.207 5.163 4.848 0.30 107155. 0.2043
|
|
32.80 0.4618 0.6542 0.0252 0.0178 0.136 1.711 1.016 101.225 0.193 4.517 4.550 0.30 107336. 0.1794
|
|
34.29 0.4827 0.6346 0.0215 0.0164 0.125 1.578 0.869 93.359 0.178 3.865 4.222 0.30 107524. 0.1539
|
|
35.78 0.5037 0.6038 0.0179 0.0149 0.114 1.437 0.722 85.024 0.162 3.210 3.850 0.30 107718. 0.1279
|
|
37.27 0.5247 0.5581 0.0142 0.0134 0.102 1.289 0.574 76.249 0.146 2.554 3.416 0.30 107918. 0.1012
|
|
38.76 0.5457 0.4910 0.0106 0.0118 0.090 1.134 0.427 67.075 0.128 1.901 2.890 0.30 108126. 0.0739
|
|
40.25 0.5667 0.3919 0.0070 0.0101 0.077 0.973 0.282 57.549 0.110 1.253 2.221 0.30 108340. 0.0461
|
|
41.74 0.5877 0.2409 0.0034 0.0084 0.064 0.807 0.139 47.728 0.091 0.616 1.316 0.30 108561. 0.0192
|
|
43.23 0.6087 -0.0056 -0.0001 0.0066 0.050 0.636 -0.002 37.617 0.072 -0.011 -0.030 0.30 108782. 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 0.0824 0.0261 0.344 3.617 4.786 256.771 0.409 21.290 8.455 0.36 125730. 0.7236
|
|
1.81 0.0213 0.0653 0.0810 0.0264 0.348 3.654 4.703 259.409 0.413 20.921 8.224 0.36 125801. 0.6977
|
|
3.62 0.0425 0.1270 0.0794 0.0266 0.351 3.688 4.614 261.792 0.417 20.525 7.995 0.36 125879. 0.6718
|
|
5.44 0.0638 0.1851 0.0778 0.0268 0.354 3.717 4.519 263.860 0.420 20.102 7.769 0.36 125962. 0.6461
|
|
7.25 0.0850 0.2397 0.0761 0.0270 0.356 3.741 4.418 265.552 0.423 19.652 7.546 0.36 126051. 0.6205
|
|
9.06 0.1063 0.2910 0.0742 0.0271 0.358 3.758 4.310 266.805 0.425 19.171 7.327 0.36 126147. 0.5950
|
|
10.87 0.1275 0.3389 0.0722 0.0272 0.359 3.769 4.195 267.553 0.426 18.660 7.112 0.36 126248. 0.5698
|
|
12.68 0.1488 0.3836 0.0701 0.0272 0.359 3.772 4.073 267.732 0.426 18.118 6.901 0.36 126357. 0.5448
|
|
14.49 0.1701 0.4253 0.0679 0.0272 0.358 3.765 3.944 267.276 0.425 17.543 6.693 0.36 126472. 0.5200
|
|
16.31 0.1913 0.4639 0.0656 0.0270 0.357 3.749 3.807 266.121 0.424 16.935 6.489 0.36 126594. 0.4953
|
|
18.12 0.2126 0.4995 0.0631 0.0268 0.354 3.722 3.663 264.206 0.420 16.294 6.289 0.36 126723. 0.4709
|
|
19.93 0.2338 0.5322 0.0605 0.0266 0.351 3.683 3.512 261.474 0.416 15.620 6.092 0.36 126859. 0.4465
|
|
21.74 0.2551 0.5620 0.0577 0.0262 0.346 3.633 3.353 257.872 0.410 14.912 5.897 0.36 127003. 0.4224
|
|
23.55 0.2763 0.5889 0.0549 0.0257 0.340 3.569 3.186 253.351 0.403 14.171 5.704 0.36 127154. 0.3983
|
|
25.36 0.2976 0.6129 0.0519 0.0252 0.332 3.492 3.012 247.867 0.394 13.398 5.512 0.36 127313. 0.3742
|
|
27.18 0.3189 0.6338 0.0487 0.0245 0.324 3.400 2.831 241.369 0.384 12.592 5.320 0.36 127480. 0.3501
|
|
28.99 0.3401 0.6515 0.0455 0.0238 0.314 3.294 2.643 233.834 0.372 11.756 5.127 0.36 127654. 0.3260
|
|
30.80 0.3614 0.6657 0.0422 0.0229 0.302 3.174 2.449 225.281 0.359 10.893 4.931 0.36 127836. 0.3018
|
|
32.61 0.3826 0.6762 0.0387 0.0219 0.289 3.039 2.250 215.730 0.343 10.006 4.730 0.36 128026. 0.2775
|
|
34.42 0.4039 0.6823 0.0352 0.0208 0.275 2.891 2.046 205.198 0.327 9.099 4.522 0.36 128224. 0.2530
|
|
36.23 0.4251 0.6836 0.0316 0.0197 0.260 2.729 1.838 193.704 0.308 8.175 4.303 0.36 128430. 0.2282
|
|
38.05 0.4464 0.6789 0.0280 0.0184 0.243 2.554 1.627 181.266 0.288 7.236 4.071 0.36 128643. 0.2031
|
|
39.86 0.4677 0.6670 0.0243 0.0171 0.225 2.365 1.413 167.913 0.267 6.286 3.817 0.36 128865. 0.1775
|
|
41.67 0.4889 0.6458 0.0206 0.0156 0.206 2.165 1.198 153.679 0.245 5.328 3.535 0.36 129096. 0.1514
|
|
43.48 0.5102 0.6123 0.0169 0.0141 0.186 1.953 0.982 138.609 0.221 4.367 3.212 0.36 129334. 0.1245
|
|
45.29 0.5314 0.5616 0.0132 0.0125 0.165 1.729 0.766 122.765 0.195 3.405 2.829 0.36 129581. 0.0968
|
|
47.10 0.5527 0.4856 0.0095 0.0108 0.142 1.496 0.551 106.222 0.169 2.450 2.352 0.36 129836. 0.0683
|
|
48.92 0.5739 0.3695 0.0058 0.0091 0.119 1.255 0.338 89.077 0.142 1.505 1.723 0.36 130099. 0.0392
|
|
50.73 0.5952 0.1831 0.0022 0.0073 0.096 1.006 0.130 71.431 0.114 0.577 0.823 0.36 130369. 0.0116
|
|
52.54 0.6165
|
|
|
|
|
|
|
|
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 0.0829 0.0260 0.545 4.905 6.557 406.229 0.554 29.165 7.321 0.42 146679. 0.7333
|
|
2.09 0.0210 0.0652 0.0815 0.0263 0.550 4.956 6.445 410.442 0.560 28.667 7.122 0.42 146762. 0.7073
|
|
4.18 0.0420 0.1268 0.0800 0.0265 0.556 5.002 6.325 414.256 0.565 28.134 6.925 0.42 146851. 0.6813
|
|
6.27 0.0630 0.1849 0.0784 0.0267 0.560 5.042 6.197 417.575 0.570 27.565 6.731 0.42 146947. 0.6555
|
|
8.36 0.0840 0.2396 0.0767 0.0269 0.564 5.075 6.061 420.306 0.573 26.958 6.540 0.42 147050. 0.6299
|
|
10.44 0.1050 0.2909 0.0748 0.0270 0.566 5.100 5.915 422.350 0.576 26.312 6.353 0.42 147160. 0.6044
|
|
12.53 0.1260 0.3389 0.0729 0.0271 0.568 5.115 5.761 423.607 0.578 25.625 6.168 0.42 147277. 0.5792
|
|
14.62 0.1471 0.3838 0.0708 0.0271 0.569 5.119 5.597 423.974 0.578 24.895 5.988 0.42 147402. 0.5541
|
|
16.71 0.1681 0.4256 0.0686 0.0271 0.568 5.112 5.423 423.350 0.578 24.122 5.810 0.42 147534. 0.5293
|
|
18.80 0.1891 0.4645 0.0663 0.0270 0.565 5.091 5.239 421.634 0.575 23.305 5.636 0.42 147674. 0.5047
|
|
20.89 0.2101 0.5005 0.0638 0.0268 0.562 5.056 5.046 418.733 0.571 22.443 5.465 0.42 147822. 0.4802
|
|
22.98 0.2311 0.5336 0.0612 0.0265 0.556 5.006 4.842 414.556 0.566 21.536 5.297 0.42 147979. 0.4560
|
|
25.07 0.2521 0.5639 0.0585 0.0262 0.549 4.939 4.628 409.017 0.558 20.584 5.132 0.42 148144. 0.4318
|
|
27.15 0.2731 0.5914 0.0557 0.0257 0.539 4.855 4.404 402.043 0.548 19.588 4.968 0.42 148317. 0.4078
|
|
29.24 0.2941 0.6161 0.0527 0.0252 0.528 4.752 4.170 393.560 0.537 18.548 4.806 0.42 148499. 0.3839
|
|
31.33 0.3151 0.6379 0.0497 0.0245 0.514 4.631 3.926 383.496 0.523 17.464 4.644 0.42 148690. 0.3599
|
|
33.42 0.3361 0.6566 0.0465 0.0238 0.499 4.489 3.673 371.797 0.507 16.339 4.481 0.42 148889. 0.3360
|
|
35.51 0.3571 0.6720 0.0432 0.0229 0.481 4.329 3.412 358.484 0.489 15.176 4.317 0.42 149098. 0.3119
|
|
37.60 0.3781 0.6839 0.0398 0.0220 0.461 4.149 3.143 343.589 0.469 13.981 4.149 0.42 149315. 0.2878
|
|
39.69 0.3991 0.6919 0.0363 0.0209 0.439 3.950 2.868 327.141 0.446 12.758 3.977 0.42 149541. 0.2635
|
|
41.78 0.4202 0.6953 0.0327 0.0198 0.415 3.733 2.588 309.165 0.422 11.511 3.797 0.42 149777. 0.2389
|
|
43.87 0.4412 0.6934 0.0291 0.0185 0.388 3.498 2.303 289.692 0.395 10.243 3.606 0.42 150021. 0.2140
|
|
45.95 0.4622 0.6848 0.0255 0.0172 0.360 3.245 2.014 268.759 0.367 8.959 3.399 0.42 150275. 0.1887
|
|
48.04 0.4832 0.6680 0.0218 0.0158 0.330 2.975 1.723 246.417 0.336 7.664 3.172 0.42 150538. 0.1628
|
|
50.13 0.5042 0.6401 0.0181 0.0143 0.299 2.689 1.430 222.734 0.304 6.362 2.913 0.42 150810. 0.1363
|
|
52.22 0.5252 0.5971 0.0144 0.0127 0.265 2.388 1.137 197.797 0.270 5.059 2.608 0.42 151092. 0.1088
|
|
54.31 0.5462 0.5317 0.0107 0.0110 0.230 2.073 0.846 171.719 0.234 3.761 2.233 0.42 151383. 0.0803
|
|
56.40 0.5672 0.4315 0.0070 0.0093 0.194 1.746 0.557 144.640 0.197 2.476 1.745 0.42 151684. 0.0509
|
|
58.49 0.5882 0.2711 0.0034 0.0075 0.157 1.409 0.272 116.725 0.159 1.210 1.057 0.42 151993. 0.0216
|
|
60.58 0.6092 -0.0112 -0.0001 0.0056 0.118 1.062 -0.008 87.940 0.120 -0.036 -0.042 0.42 152300. 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 0.0836 0.0260 0.813 6.409 8.629 606.609 0.724 38.382 6.452 0.48 167625. 0.7414
|
|
2.38 0.0210 0.0656 0.0822 0.0263 0.822 6.476 8.483 612.990 0.732 37.731 6.277 0.48 167720. 0.7151
|
|
4.77 0.0420 0.1276 0.0806 0.0265 0.830 6.537 8.326 618.765 0.739 37.034 6.103 0.48 167823. 0.6889
|
|
7.15 0.0629 0.1860 0.0790 0.0267 0.837 6.591 8.158 623.791 0.745 36.289 5.932 0.48 167933. 0.6628
|
|
9.54 0.0839 0.2410 0.0773 0.0269 0.842 6.634 7.980 627.926 0.750 35.494 5.764 0.48 168050. 0.6369
|
|
11.92 0.1049 0.2926 0.0754 0.0270 0.846 6.667 7.789 631.021 0.753 34.647 5.599 0.48 168176. 0.6113
|
|
14.31 0.1259 0.3410 0.0735 0.0271 0.849 6.687 7.587 632.924 0.755 33.746 5.437 0.48 168310. 0.5858
|
|
16.69 0.1469 0.3862 0.0714 0.0272 0.850 6.693 7.372 633.480 0.756 32.789 5.278 0.48 168452. 0.5606
|
|
19.08 0.1679 0.4284 0.0692 0.0271 0.848 6.683 7.144 632.537 0.755 31.775 5.123 0.48 168604. 0.5356
|
|
21.46 0.1888 0.4676 0.0669 0.0270 0.845 6.656 6.903 629.943 0.752 30.703 4.970 0.48 168764. 0.5108
|
|
23.84 0.2098 0.5039 0.0644 0.0268 0.839 6.609 6.648 625.555 0.747 29.572 4.820 0.48 168934. 0.4862
|
|
26.23 0.2308 0.5374 0.0618 0.0265 0.830 6.542 6.381 619.236 0.739 28.381 4.674 0.48 169113. 0.4618
|
|
28.61 0.2518 0.5681 0.0591 0.0262 0.819 6.454 6.100 610.860 0.729 27.131 4.529 0.48 169301. 0.4376
|
|
31.00 0.2728 0.5961 0.0562 0.0257 0.805 6.342 5.805 600.312 0.717 25.822 4.386 0.48 169499. 0.4134
|
|
33.38 0.2938 0.6212 0.0532 0.0252 0.788 6.207 5.498 587.484 0.701 24.456 4.245 0.48 169707. 0.3894
|
|
35.77 0.3147 0.6435 0.0501 0.0245 0.767 6.046 5.178 572.264 0.683 23.032 4.104 0.48 169925. 0.3653
|
|
38.15 0.3357 0.6628 0.0469 0.0238 0.744 5.859 4.846 554.571 0.662 21.553 3.963 0.48 170153. 0.3412
|
|
40.54 0.3567 0.6790 0.0436 0.0229 0.717 5.646 4.502 534.431 0.638 20.024 3.821 0.48 170391. 0.3171
|
|
42.92 0.3777 0.6917 0.0402 0.0219 0.686 5.408 4.149 511.895 0.611 18.453 3.676 0.48 170639. 0.2929
|
|
45.30 0.3987 0.7005 0.0367 0.0209 0.653 5.145 3.787 487.002 0.581 16.845 3.527 0.48 170897. 0.2685
|
|
47.69 0.4197 0.7049 0.0331 0.0197 0.617 4.858 3.418 459.792 0.549 15.204 3.372 0.48 171166. 0.2439
|
|
50.07 0.4406 0.7041 0.0295 0.0184 0.577 4.546 3.043 430.310 0.514 13.536 3.208 0.48 171445. 0.2189
|
|
52.46 0.4616 0.6970 0.0258 0.0171 0.535 4.211 2.663 398.614 0.476 11.847 3.031 0.48 171735. 0.1935
|
|
54.84 0.4826 0.6816 0.0221 0.0156 0.489 3.854 2.280 364.780 0.435 10.142 2.835 0.48 172035. 0.1675
|
|
57.23 0.5036 0.6555 0.0184 0.0141 0.441 3.475 1.895 328.909 0.393 8.428 2.613 0.48 172345. 0.1407
|
|
59.61 0.5246 0.6144 0.0146 0.0125 0.390 3.076 1.509 291.133 0.348 6.713 2.351 0.48 172667. 0.1130
|
|
62.00 0.5456 0.5511 0.0109 0.0108 0.337 2.658 1.125 251.622 0.300 5.004 2.028 0.48 172999. 0.0841
|
|
64.38 0.5665 0.4525 0.0072 0.0090 0.282 2.225 0.744 210.590 0.251 3.311 1.603 0.48 173342. 0.0541
|
|
66.76 0.5875 0.2917 0.0036 0.0072 0.226 1.778 0.370 168.286 0.201 1.645 0.997 0.48 173694. 0.0237
|
|
69.15 0.6085 0.0010 0.0000 0.0053 0.167 1.317 0.001 124.696 0.149 0.004 0.003 0.48 174046. 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 0.0843 0.0261 1.163 8.144 11.017 867.180 0.920 49.005 5.763 0.54 188568. 0.7482
|
|
2.68 0.0210 0.0659 0.0829 0.0264 1.175 8.231 10.832 876.404 0.930 48.179 5.606 0.54 188675. 0.7217
|
|
5.36 0.0420 0.1282 0.0814 0.0266 1.186 8.309 10.633 884.748 0.939 47.294 5.451 0.54 188791. 0.6953
|
|
8.05 0.0629 0.1869 0.0797 0.0269 1.196 8.377 10.420 892.004 0.946 46.348 5.298 0.54 188915. 0.6690
|
|
10.73 0.0839 0.2422 0.0780 0.0270 1.204 8.433 10.193 897.963 0.953 45.338 5.148 0.54 189048. 0.6430
|
|
13.41 0.1049 0.2941 0.0761 0.0272 1.210 8.475 9.951 902.411 0.957 44.260 5.001 0.54 189190. 0.6171
|
|
16.09 0.1259 0.3427 0.0742 0.0272 1.214 8.500 9.693 905.128 0.960 43.113 4.857 0.54 189341. 0.5915
|
|
18.78 0.1469 0.3882 0.0721 0.0273 1.215 8.508 9.419 905.891 0.961 41.895 4.716 0.54 189502. 0.5662
|
|
21.46 0.1679 0.4306 0.0699 0.0272 1.213 8.494 9.128 904.478 0.960 40.603 4.578 0.54 189673. 0.5410
|
|
24.14 0.1888 0.4701 0.0675 0.0271 1.208 8.459 8.821 900.671 0.956 39.236 4.442 0.54 189854. 0.5161
|
|
26.82 0.2098 0.5068 0.0650 0.0269 1.199 8.398 8.497 894.264 0.949 37.793 4.309 0.54 190045. 0.4914
|
|
29.51 0.2308 0.5406 0.0624 0.0266 1.187 8.312 8.155 885.056 0.939 36.273 4.179 0.54 190247. 0.4669
|
|
32.19 0.2518 0.5717 0.0597 0.0263 1.171 8.197 7.796 872.868 0.926 34.678 4.051 0.54 190459. 0.4425
|
|
34.87 0.2728 0.6000 0.0568 0.0258 1.150 8.053 7.421 857.532 0.910 33.007 3.925 0.54 190683. 0.4182
|
|
37.55 0.2938 0.6256 0.0538 0.0253 1.125 7.878 7.028 838.896 0.890 31.262 3.800 0.54 190917. 0.3941
|
|
40.24 0.3147 0.6484 0.0507 0.0246 1.095 7.671 6.619 816.797 0.867 29.443 3.676 0.54 191163. 0.3699
|
|
42.92 0.3357 0.6682 0.0474 0.0238 1.061 7.430 6.194 791.118 0.839 27.553 3.551 0.54 191419. 0.3458
|
|
45.60 0.3567 0.6849 0.0440 0.0229 1.022 7.155 5.755 761.892 0.808 25.599 3.426 0.54 191687. 0.3215
|
|
48.28 0.3777 0.6983 0.0406 0.0220 0.978 6.848 5.304 729.191 0.774 23.591 3.299 0.54 191967. 0.2972
|
|
50.97 0.3987 0.7079 0.0370 0.0209 0.929 6.509 4.841 693.076 0.735 21.534 3.168 0.54 192258. 0.2727
|
|
53.65 0.4196 0.7132 0.0334 0.0197 0.876 6.138 4.370 653.601 0.693 19.436 3.032 0.54 192560. 0.2480
|
|
56.33 0.4406 0.7133 0.0298 0.0184 0.819 5.737 3.890 610.833 0.648 17.303 2.889 0.54 192874. 0.2229
|
|
59.01 0.4616 0.7072 0.0261 0.0170 0.757 5.305 3.404 564.856 0.599 15.143 2.734 0.54 193200. 0.1973
|
|
61.69 0.4826 0.6931 0.0223 0.0155 0.692 4.844 2.914 515.780 0.547 12.962 2.563 0.54 193538. 0.1711
|
|
64.38 0.5036 0.6683 0.0185 0.0140 0.622 4.355 2.421 463.751 0.492 10.769 2.368 0.54 193888. 0.1441
|
|
67.06 0.5246 0.6285 0.0148 0.0123 0.548 3.841 1.928 408.962 0.434 8.574 2.138 0.54 194250. 0.1161
|
|
69.74 0.5455 0.5663 0.0110 0.0106 0.472 3.303 1.436 351.661 0.373 6.388 1.852 0.54 194623. 0.0868
|
|
72.42 0.5665 0.4679 0.0073 0.0088 0.392 2.744 0.949 292.160 0.310 4.222 1.474 0.54 195009. 0.0562
|
|
75.11 0.5875 0.3040 0.0036 0.0069 0.310 2.168 0.470 230.822 0.245 2.090 0.923 0.54 195405. 0.0248
|
|
77.79 0.6085 -0.0023 0.0000 0.0050 0.225 1.574 -0.002 167.584 0.178 -0.011 -0.007 0.55 195799. 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 0.0852 0.0263 1.607 10.130 13.741 1198.483 1.144 61.118 5.200 0.59 209506. 0.7540
|
|
2.98 0.0210 0.0661 0.0837 0.0266 1.624 10.239 13.511 1211.338 1.157 60.097 5.059 0.60 209626. 0.7274
|
|
5.96 0.0420 0.1285 0.0822 0.0268 1.640 10.337 13.265 1222.954 1.168 59.001 4.920 0.60 209755. 0.7009
|
|
8.94 0.0629 0.1874 0.0806 0.0271 1.654 10.422 13.001 1233.037 1.177 57.828 4.782 0.60 209894. 0.6745
|
|
11.92 0.0839 0.2428 0.0788 0.0272 1.665 10.492 12.719 1241.304 1.185 56.575 4.648 0.60 210042. 0.6484
|
|
14.90 0.1049 0.2949 0.0770 0.0274 1.673 10.544 12.418 1247.448 1.191 55.237 4.515 0.60 210200. 0.6224
|
|
17.88 0.1259 0.3437 0.0750 0.0275 1.678 10.575 12.098 1251.165 1.195 53.813 4.386 0.60 210369. 0.5967
|
|
20.86 0.1468 0.3894 0.0729 0.0275 1.679 10.583 11.758 1252.143 1.196 52.298 4.259 0.60 210548. 0.5713
|
|
23.84 0.1678 0.4321 0.0706 0.0274 1.676 10.566 11.396 1250.072 1.194 50.691 4.135 0.60 210738. 0.5460
|
|
26.81 0.1888 0.4718 0.0683 0.0273 1.669 10.520 11.014 1244.652 1.189 48.990 4.014 0.60 210940. 0.5210
|
|
29.79 0.2098 0.5087 0.0658 0.0271 1.657 10.444 10.610 1235.592 1.180 47.193 3.895 0.60 211153. 0.4963
|
|
32.77 0.2307 0.5429 0.0631 0.0268 1.640 10.334 10.184 1222.618 1.168 45.300 3.778 0.60 211378. 0.4717
|
|
35.75 0.2517 0.5743 0.0604 0.0265 1.617 10.189 9.737 1205.474 1.151 43.312 3.664 0.60 211615. 0.4472
|
|
38.73 0.2727 0.6030 0.0575 0.0260 1.588 10.007 9.269 1183.935 1.131 41.229 3.551 0.60 211863. 0.4229
|
|
41.71 0.2937 0.6290 0.0544 0.0254 1.553 9.786 8.780 1157.786 1.106 39.052 3.440 0.60 212124. 0.3987
|
|
44.69 0.3146 0.6522 0.0513 0.0247 1.511 9.524 8.270 1126.807 1.076 36.783 3.329 0.60 212397. 0.3745
|
|
47.67 0.3356 0.6725 0.0480 0.0239 1.463 9.220 7.739 1090.826 1.042 34.425 3.218 0.60 212683. 0.3502
|
|
50.65 0.3566 0.6898 0.0446 0.0230 1.408 8.874 7.191 1049.891 1.003 31.986 3.107 0.60 212981. 0.3259
|
|
53.63 0.3776 0.7038 0.0411 0.0220 1.347 8.487 6.627 1004.100 0.959 29.478 2.994 0.60 213292. 0.3015
|
|
56.61 0.3985 0.7142 0.0375 0.0209 1.279 8.060 6.050 953.538 0.911 26.910 2.878 0.60 213616. 0.2769
|
|
59.59 0.4195 0.7203 0.0338 0.0197 1.205 7.593 5.461 898.284 0.858 24.289 2.757 0.60 213952. 0.2520
|
|
62.57 0.4405 0.7214 0.0301 0.0184 1.124 7.087 4.861 838.429 0.801 21.624 2.630 0.60 214301. 0.2268
|
|
65.55 0.4615 0.7163 0.0264 0.0170 1.038 6.543 4.254 774.091 0.739 18.924 2.493 0.60 214663. 0.2011
|
|
68.53 0.4824 0.7034 0.0226 0.0155 0.946 5.962 3.642 705.425 0.674 16.198 2.341 0.60 215039. 0.1748
|
|
71.51 0.5034 0.6800 0.0188 0.0139 0.848 5.347 3.025 632.635 0.604 13.457 2.169 0.60 215427. 0.1476
|
|
74.49 0.5244 0.6416 0.0149 0.0122 0.746 4.699 2.408 555.991 0.531 10.713 1.965 0.60 215829. 0.1193
|
|
77.46 0.5454 0.5806 0.0111 0.0104 0.638 4.022 1.794 475.842 0.454 7.979 1.710 0.60 216244. 0.0896
|
|
80.44 0.5663 0.4827 0.0073 0.0086 0.527 3.319 1.185 392.624 0.375 5.270 1.369 0.60 216672. 0.0583
|
|
83.42 0.5873 0.3164 0.0036 0.0067 0.411 2.594 0.585 306.849 0.293 2.603 0.865 0.61 217113. 0.0259
|
|
86.40 0.6083 -0.0045 0.0000 0.0048 0.293 1.846 -0.006 218.381 0.209 -0.025 -0.012 0.61 217549. 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 0.0862 0.0266 2.163 12.393 16.822 1612.910 1.400 74.826 4.731 0.65 230439. 0.7590
|
|
3.28 0.0210 0.0661 0.0847 0.0269 2.186 12.527 16.544 1630.307 1.415 73.588 4.603 0.65 230571. 0.7323
|
|
6.55 0.0419 0.1286 0.0832 0.0271 2.207 12.648 16.245 1646.006 1.429 72.259 4.477 0.65 230714. 0.7058
|
|
9.83 0.0629 0.1875 0.0816 0.0274 2.226 12.752 15.925 1659.609 1.441 70.834 4.352 0.65 230867. 0.6794
|
|
13.10 0.0839 0.2430 0.0798 0.0275 2.240 12.838 15.582 1670.725 1.450 69.311 4.230 0.65 231031. 0.6532
|
|
16.38 0.1048 0.2951 0.0779 0.0277 2.252 12.901 15.217 1678.944 1.458 67.683 4.111 0.65 231206. 0.6273
|
|
19.65 0.1258 0.3441 0.0759 0.0278 2.258 12.938 14.826 1683.848 1.462 65.948 3.994 0.66 231392. 0.6015
|
|
22.93 0.1467 0.3899 0.0738 0.0278 2.260 12.947 14.411 1685.017 1.463 64.101 3.879 0.66 231590. 0.5761
|
|
26.20 0.1677 0.4328 0.0716 0.0277 2.256 12.924 13.970 1682.033 1.460 62.141 3.767 0.66 231800. 0.5508
|
|
29.48 0.1887 0.4727 0.0692 0.0276 2.246 12.867 13.504 1674.487 1.454 60.064 3.658 0.66 232022. 0.5258
|
|
32.76 0.2096 0.5099 0.0666 0.0274 2.229 12.770 13.010 1661.988 1.443 57.869 3.551 0.66 232258. 0.5010
|
|
36.03 0.2306 0.5443 0.0640 0.0271 2.205 12.634 12.490 1644.166 1.427 55.556 3.446 0.66 232506. 0.4763
|
|
39.31 0.2516 0.5760 0.0612 0.0267 2.173 12.453 11.943 1620.680 1.407 53.124 3.343 0.66 232767. 0.4519
|
|
42.58 0.2725 0.6050 0.0582 0.0262 2.134 12.227 11.370 1591.223 1.381 50.575 3.241 0.66 233041. 0.4275
|
|
45.86 0.2935 0.6314 0.0552 0.0256 2.086 11.952 10.771 1555.509 1.350 47.911 3.141 0.66 233328. 0.4032
|
|
49.13 0.3145 0.6551 0.0520 0.0249 2.029 11.628 10.147 1513.245 1.314 45.133 3.041 0.66 233629. 0.3790
|
|
52.41 0.3354 0.6759 0.0487 0.0241 1.964 11.251 9.497 1464.198 1.271 42.244 2.942 0.66 233944. 0.3547
|
|
55.68 0.3564 0.6938 0.0452 0.0232 1.889 10.822 8.826 1408.423 1.223 39.256 2.842 0.66 234272. 0.3303
|
|
58.96 0.3773 0.7085 0.0417 0.0222 1.805 10.343 8.134 1346.057 1.169 36.182 2.741 0.66 234615. 0.3058
|
|
62.23 0.3983 0.7195 0.0380 0.0211 1.713 9.814 7.426 1277.215 1.109 33.032 2.637 0.66 234971. 0.2811
|
|
65.51 0.4193 0.7265 0.0343 0.0198 1.612 9.236 6.703 1202.007 1.043 29.817 2.530 0.66 235341. 0.2562
|
|
68.79 0.4402 0.7285 0.0306 0.0185 1.503 8.610 5.968 1120.558 0.973 26.548 2.416 0.66 235725. 0.2309
|
|
72.06 0.4612 0.7245 0.0268 0.0170 1.385 7.938 5.224 1033.028 0.897 23.234 2.293 0.66 236124. 0.2050
|
|
75.34 0.4822 0.7129 0.0229 0.0155 1.260 7.220 4.471 939.626 0.816 19.888 2.158 0.66 236536. 0.1785
|
|
78.61 0.5031 0.6908 0.0190 0.0139 1.127 6.459 3.715 840.631 0.730 16.523 2.004 0.66 236964. 0.1511
|
|
81.89 0.5241 0.6538 0.0151 0.0121 0.988 5.658 2.957 736.412 0.639 13.153 1.821 0.66 237405. 0.1225
|
|
85.16 0.5450 0.5943 0.0113 0.0103 0.841 4.821 2.202 627.439 0.545 9.795 1.592 0.66 237862. 0.0924
|
|
88.44 0.5660 0.4972 0.0074 0.0085 0.690 3.952 1.454 514.312 0.446 6.468 1.282 0.67 238332. 0.0605
|
|
91.71 0.5870 0.3290 0.0037 0.0066 0.533 3.056 0.717 397.740 0.345 3.191 0.818 0.67 238817. 0.0271
|
|
94.99 0.6079 -0.0062 0.0000 0.0046 0.372 2.132 -0.009 277.507 0.241 -0.040 -0.015 0.67 239295. 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 0.0874 0.0270 2.852 14.978 20.293 2126.476 1.692 90.265 4.328 0.71 251365. 0.7628
|
|
3.57 0.0209 0.0659 0.0859 0.0273 2.882 15.138 19.962 2149.201 1.710 88.791 4.213 0.71 251510. 0.7363
|
|
7.14 0.0419 0.1283 0.0844 0.0276 2.910 15.283 19.606 2169.735 1.727 87.206 4.098 0.71 251667. 0.7099
|
|
10.71 0.0628 0.1872 0.0827 0.0278 2.934 15.408 19.223 2187.525 1.741 85.505 3.986 0.71 251834. 0.6836
|
|
14.28 0.0838 0.2426 0.0810 0.0280 2.953 15.510 18.814 2202.029 1.752 83.683 3.875 0.71 252014. 0.6575
|
|
17.85 0.1047 0.2948 0.0791 0.0281 2.967 15.585 18.376 2212.684 1.761 81.735 3.767 0.71 252205. 0.6316
|
|
21.42 0.1257 0.3438 0.0771 0.0282 2.976 15.629 17.908 2218.921 1.766 79.655 3.661 0.71 252409. 0.6060
|
|
24.99 0.1466 0.3897 0.0749 0.0282 2.977 15.638 17.410 2220.174 1.767 77.440 3.557 0.71 252626. 0.5805
|
|
28.56 0.1676 0.4327 0.0727 0.0281 2.972 15.608 16.881 2215.895 1.763 75.086 3.455 0.72 252856. 0.5553
|
|
32.13 0.1885 0.4728 0.0702 0.0280 2.958 15.535 16.320 2205.540 1.755 72.590 3.356 0.72 253100. 0.5304
|
|
35.70 0.2095 0.5101 0.0677 0.0278 2.935 15.415 15.726 2188.595 1.742 69.950 3.259 0.72 253357. 0.5056
|
|
39.27 0.2304 0.5448 0.0650 0.0275 2.903 15.246 15.100 2164.577 1.723 67.166 3.164 0.72 253629. 0.4810
|
|
42.84 0.2514 0.5768 0.0622 0.0271 2.860 15.024 14.442 2133.033 1.697 64.237 3.071 0.72 253914. 0.4565
|
|
46.41 0.2723 0.6062 0.0592 0.0266 2.808 14.746 13.751 2093.561 1.666 61.165 2.979 0.72 254214. 0.4322
|
|
49.98 0.2932 0.6330 0.0561 0.0260 2.743 14.410 13.029 2045.792 1.628 57.953 2.889 0.72 254528. 0.4079
|
|
53.56 0.3142 0.6571 0.0528 0.0253 2.668 14.012 12.276 1989.346 1.583 54.602 2.799 0.72 254857. 0.3836
|
|
57.13 0.3351 0.6785 0.0495 0.0244 2.580 13.551 11.492 1923.911 1.531 51.115 2.709 0.72 255201. 0.3593
|
|
60.70 0.3561 0.6970 0.0460 0.0235 2.480 13.027 10.681 1849.550 1.472 47.507 2.619 0.72 255560. 0.3348
|
|
64.27 0.3770 0.7123 0.0424 0.0224 2.369 12.442 9.846 1766.446 1.406 43.794 2.528 0.72 255933. 0.3103
|
|
67.84 0.3980 0.7241 0.0387 0.0213 2.246 11.796 8.990 1674.757 1.333 39.987 2.435 0.72 256322. 0.2856
|
|
71.41 0.4189 0.7319 0.0349 0.0200 2.112 11.091 8.116 1574.635 1.253 36.101 2.338 0.72 256726. 0.2605
|
|
74.98 0.4399 0.7349 0.0311 0.0186 1.966 10.328 7.227 1466.264 1.167 32.147 2.236 0.72 257145. 0.2351
|
|
78.55 0.4608 0.7320 0.0272 0.0171 1.810 9.508 6.326 1349.876 1.074 28.139 2.126 0.72 257580. 0.2091
|
|
82.12 0.4818 0.7215 0.0233 0.0156 1.644 8.634 5.416 1225.785 0.975 24.090 2.004 0.72 258030. 0.1824
|
|
85.69 0.5027 0.7006 0.0194 0.0139 1.468 7.709 4.500 1094.411 0.871 20.017 1.865 0.72 258495. 0.1548
|
|
89.26 0.5237 0.6649 0.0154 0.0121 1.282 6.736 3.583 956.301 0.761 15.936 1.699 0.72 258977. 0.1258
|
|
92.83 0.5446 0.6064 0.0115 0.0103 1.089 5.721 2.668 812.173 0.646 11.868 1.490 0.72 259474. 0.0952
|
|
96.40 0.5655 0.5093 0.0076 0.0084 0.889 4.669 1.762 662.928 0.528 7.835 1.205 0.73 259987. 0.0626
|
|
99.97 0.5865 0.3388 0.0037 0.0065 0.683 3.590 0.869 509.635 0.406 3.864 0.773 0.73 260515. 0.0282
|
|
103.54 0.6074 -0.0073 -0.0001 0.0045 0.472 2.480 -0.013 352.043 0.280 -0.056 -0.016 0.73 261035. 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 0.0887 0.0278 3.737 18.119 24.191 2786.784 2.047 107.601 3.937 0.77 272282. 0.7575
|
|
3.86 0.0209 0.0650 0.0873 0.0281 3.770 18.280 23.803 2811.531 2.065 105.876 3.840 0.77 272440. 0.7329
|
|
7.73 0.0418 0.1268 0.0858 0.0283 3.800 18.424 23.385 2833.709 2.082 104.017 3.743 0.77 272610. 0.7081
|
|
11.59 0.0628 0.1853 0.0841 0.0285 3.825 18.547 22.936 2852.659 2.095 102.019 3.647 0.77 272793. 0.6832
|
|
15.45 0.0837 0.2406 0.0824 0.0286 3.846 18.645 22.454 2867.719 2.107 99.874 3.551 0.77 272988. 0.6583
|
|
19.31 0.1046 0.2927 0.0805 0.0287 3.860 18.713 21.937 2878.194 2.114 97.577 3.457 0.77 273197. 0.6334
|
|
23.18 0.1255 0.3418 0.0784 0.0288 3.867 18.747 21.385 2883.365 2.118 95.121 3.364 0.77 273419. 0.6085
|
|
27.04 0.1464 0.3879 0.0763 0.0288 3.865 18.741 20.796 2882.486 2.117 92.501 3.272 0.77 273655. 0.5837
|
|
30.90 0.1673 0.4311 0.0740 0.0287 3.855 18.691 20.169 2874.813 2.112 89.712 3.182 0.77 273905. 0.5590
|
|
34.76 0.1883 0.4715 0.0715 0.0286 3.835 18.592 19.504 2859.602 2.101 86.753 3.094 0.77 274170. 0.5344
|
|
38.63 0.2092 0.5091 0.0689 0.0283 3.803 18.440 18.799 2836.134 2.083 83.619 3.006 0.78 274450. 0.5099
|
|
42.49 0.2301 0.5441 0.0662 0.0280 3.760 18.229 18.055 2803.707 2.059 80.311 2.921 0.78 274745. 0.4855
|
|
46.35 0.2510 0.5765 0.0633 0.0276 3.703 17.956 17.273 2761.682 2.029 76.828 2.837 0.78 275055. 0.4612
|
|
50.22 0.2719 0.6062 0.0603 0.0271 3.633 17.616 16.451 2709.462 1.990 73.173 2.754 0.78 275380. 0.4369
|
|
54.08 0.2929 0.6335 0.0572 0.0264 3.549 17.207 15.591 2646.536 1.944 69.348 2.672 0.78 275722. 0.4127
|
|
57.94 0.3138 0.6581 0.0539 0.0257 3.450 16.725 14.693 2572.396 1.890 65.355 2.591 0.78 276078. 0.3885
|
|
61.80 0.3347 0.6799 0.0505 0.0248 3.335 16.168 13.758 2486.655 1.827 61.198 2.510 0.78 276451. 0.3641
|
|
65.67 0.3556 0.6990 0.0469 0.0239 3.204 15.535 12.791 2389.424 1.755 56.893 2.428 0.78 276840. 0.3397
|
|
69.53 0.3765 0.7148 0.0433 0.0228 3.059 14.830 11.794 2280.993 1.676 52.460 2.345 0.78 277245. 0.3151
|
|
73.39 0.3974 0.7272 0.0395 0.0216 2.899 14.054 10.772 2161.651 1.588 47.914 2.260 0.78 277666. 0.2902
|
|
77.25 0.4184 0.7355 0.0357 0.0203 2.725 13.210 9.728 2031.706 1.492 43.270 2.172 0.78 278104. 0.2650
|
|
81.12 0.4393 0.7389 0.0318 0.0189 2.537 12.298 8.665 1891.503 1.389 38.542 2.078 0.78 278558. 0.2393
|
|
84.98 0.4602 0.7362 0.0278 0.0174 2.335 11.323 7.587 1741.485 1.279 33.747 1.976 0.78 279028. 0.2129
|
|
88.84 0.4811 0.7254 0.0238 0.0158 2.122 10.287 6.497 1582.241 1.162 28.901 1.863 0.78 279515. 0.1857
|
|
92.70 0.5020 0.7038 0.0198 0.0141 1.897 9.197 5.401 1414.502 1.039 24.022 1.732 0.78 280019. 0.1574
|
|
96.57 0.5229 0.6664 0.0158 0.0124 1.662 8.057 4.301 1239.207 0.910 19.131 1.574 0.78 280540. 0.1277
|
|
100.43 0.5439 0.6051 0.0118 0.0106 1.418 6.876 3.204 1057.527 0.777 14.252 1.374 0.79 281078. 0.0962
|
|
104.29 0.5648 0.5039 0.0078 0.0087 1.168 5.662 2.116 870.875 0.640 9.412 1.102 0.79 281632. 0.0627
|
|
108.16 0.5857 0.3296 0.0038 0.0068 0.913 4.427 1.044 680.865 0.500 4.642 0.695 0.79 282203. 0.0278
|
|
112.02 0.6066 -0.0069 -0.0001 0.0049 0.653 3.168 -0.015 487.199 0.358 -0.067 -0.014 0.79 282766. 0.0000
|
|
|
|
|
|
|
|
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 0.0903 0.0299 5.022 22.607 28.556 3744.583 2.554 127.016 3.459 0.83 293187. 0.7230
|
|
4.16 0.0209 0.0618 0.0889 0.0301 5.043 22.705 28.109 3760.825 2.565 125.030 3.390 0.83 293359. 0.7031
|
|
8.31 0.0418 0.1210 0.0874 0.0302 5.061 22.783 27.627 3773.704 2.574 122.883 3.321 0.83 293543. 0.6827
|
|
12.47 0.0627 0.1777 0.0857 0.0303 5.072 22.836 27.107 3782.545 2.580 120.570 3.250 0.83 293741. 0.6620
|
|
16.63 0.0836 0.2318 0.0840 0.0303 5.078 22.861 26.547 3786.636 2.583 118.081 3.180 0.83 293953. 0.6409
|
|
20.79 0.1045 0.2833 0.0821 0.0303 5.076 22.853 25.946 3785.228 2.582 115.409 3.109 0.83 294179. 0.6195
|
|
24.94 0.1254 0.3322 0.0800 0.0302 5.066 22.806 25.303 3777.512 2.577 112.546 3.038 0.83 294420. 0.5978
|
|
29.10 0.1463 0.3785 0.0778 0.0301 5.046 22.717 24.615 3762.701 2.567 109.485 2.967 0.83 294676. 0.5758
|
|
33.26 0.1672 0.4223 0.0755 0.0299 5.015 22.579 23.881 3739.975 2.551 106.222 2.896 0.83 294947. 0.5536
|
|
37.41 0.1881 0.4634 0.0731 0.0297 4.973 22.389 23.101 3708.519 2.530 102.751 2.825 0.83 295234. 0.5312
|
|
41.57 0.2090 0.5020 0.0704 0.0293 4.918 22.142 22.273 3667.522 2.502 99.072 2.755 0.83 295537. 0.5085
|
|
45.73 0.2300 0.5381 0.0677 0.0289 4.849 21.832 21.399 3616.192 2.467 95.181 2.684 0.84 295856. 0.4857
|
|
49.89 0.2509 0.5716 0.0648 0.0284 4.766 21.455 20.477 3553.753 2.424 91.081 2.613 0.84 296192. 0.4626
|
|
54.04 0.2718 0.6025 0.0617 0.0278 4.666 21.007 19.508 3479.465 2.373 86.773 2.543 0.84 296544. 0.4394
|
|
58.20 0.2927 0.6308 0.0585 0.0271 4.550 20.484 18.494 3392.957 2.314 82.261 2.472 0.84 296912. 0.4159
|
|
62.36 0.3136 0.6562 0.0551 0.0263 4.418 19.889 17.434 3294.420 2.247 77.546 2.400 0.84 297298. 0.3920
|
|
66.52 0.3345 0.6786 0.0516 0.0255 4.268 19.214 16.329 3182.559 2.171 72.634 2.327 0.84 297701. 0.3679
|
|
70.67 0.3554 0.6978 0.0480 0.0245 4.101 18.462 15.185 3057.941 2.086 67.542 2.252 0.84 298121. 0.3433
|
|
74.83 0.3763 0.7134 0.0443 0.0234 3.917 17.635 14.005 2920.929 1.992 62.294 2.175 0.84 298558. 0.3184
|
|
78.99 0.3972 0.7251 0.0405 0.0222 3.716 16.731 12.794 2771.245 1.890 56.908 2.094 0.84 299012. 0.2930
|
|
83.14 0.4181 0.7322 0.0365 0.0209 3.499 15.754 11.557 2609.488 1.780 51.404 2.009 0.84 299484. 0.2671
|
|
87.30 0.4390 0.7336 0.0326 0.0195 3.267 14.710 10.296 2436.451 1.662 45.797 1.917 0.84 299974. 0.2406
|
|
91.46 0.4599 0.7279 0.0285 0.0180 3.021 13.602 9.017 2252.919 1.537 40.108 1.815 0.84 300481. 0.2132
|
|
95.62 0.4808 0.7128 0.0244 0.0165 2.763 12.437 7.723 2060.016 1.405 34.354 1.701 0.84 301005. 0.1849
|
|
99.77 0.5017 0.6851 0.0203 0.0149 2.493 11.224 6.420 1859.146 1.268 28.558 1.566 0.84 301548. 0.1553
|
|
103.93 0.5226 0.6398 0.0162 0.0132 2.215 9.972 5.114 1651.795 1.127 22.745 1.404 0.84 302109. 0.1242
|
|
108.09 0.5435 0.5687 0.0120 0.0115 1.931 8.693 3.810 1439.800 0.982 16.945 1.200 0.85 302688. 0.0916
|
|
112.24 0.5644 0.4582 0.0080 0.0098 1.643 7.397 2.516 1225.244 0.836 11.189 0.931 0.85 303285. 0.0578
|
|
116.40 0.5853 0.2839 0.0039 0.0081 1.355 6.100 1.239 1010.337 0.689 5.513 0.556 0.85 303899. 0.0242
|
|
120.56 0.6062 -0.0061 -0.0001 0.0064 1.065 4.794 -0.020 794.114 0.542 -0.090 -0.012 0.85 304508. 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 0.0918 0.0342 7.046 29.605 33.320 5253.873 3.345 148.209 2.877 0.89 314087. 0.6495
|
|
4.47 0.0210 0.0556 0.0904 0.0341 7.038 29.571 32.820 5247.907 3.341 145.985 2.837 0.89 314272. 0.6357
|
|
8.94 0.0420 0.1096 0.0889 0.0340 7.022 29.504 32.277 5236.060 3.333 143.568 2.796 0.89 314471. 0.6214
|
|
13.41 0.0629 0.1619 0.0873 0.0339 6.997 29.401 31.688 5217.725 3.322 140.950 2.755 0.89 314685. 0.6066
|
|
17.88 0.0839 0.2126 0.0855 0.0338 6.963 29.257 31.052 5192.257 3.305 138.121 2.713 0.89 314914. 0.5913
|
|
22.35 0.1049 0.2615 0.0837 0.0335 6.918 29.070 30.366 5159.035 3.284 135.070 2.670 0.89 315159. 0.5755
|
|
26.82 0.1259 0.3087 0.0816 0.0333 6.863 28.836 29.628 5117.401 3.258 131.787 2.626 0.89 315419. 0.5592
|
|
31.29 0.1468 0.3541 0.0794 0.0329 6.795 28.550 28.837 5066.698 3.226 128.267 2.581 0.89 315696. 0.5423
|
|
35.76 0.1678 0.3975 0.0771 0.0326 6.713 28.209 27.990 5006.255 3.187 124.501 2.536 0.89 315990. 0.5248
|
|
40.22 0.1888 0.4390 0.0746 0.0321 6.618 27.809 27.087 4935.245 3.142 120.483 2.489 0.89 316301. 0.5068
|
|
44.69 0.2098 0.4784 0.0720 0.0316 6.508 27.346 26.127 4853.082 3.090 116.212 2.442 0.89 316630. 0.4882
|
|
49.16 0.2307 0.5158 0.0692 0.0309 6.382 26.816 25.109 4759.020 3.030 111.687 2.393 0.89 316975. 0.4691
|
|
53.63 0.2517 0.5510 0.0662 0.0303 6.239 26.215 24.035 4652.306 2.962 106.907 2.343 0.90 317339. 0.4494
|
|
58.10 0.2727 0.5838 0.0631 0.0295 6.078 25.538 22.903 4532.220 2.885 101.875 2.292 0.90 317720. 0.4291
|
|
62.57 0.2937 0.6143 0.0598 0.0286 5.898 24.783 21.717 4398.094 2.800 96.595 2.240 0.90 318120. 0.4083
|
|
67.04 0.3146 0.6421 0.0564 0.0276 5.701 23.954 20.475 4251.024 2.706 91.072 2.185 0.90 318538. 0.3867
|
|
71.51 0.3356 0.6661 0.0528 0.0266 5.491 23.072 19.179 4094.477 2.607 85.309 2.125 0.90 318973. 0.3640
|
|
75.98 0.3566 0.6865 0.0491 0.0255 5.264 22.118 17.835 3925.193 2.499 79.330 2.061 0.90 319428. 0.3405
|
|
80.45 0.3776 0.7021 0.0453 0.0244 5.025 21.116 16.448 3747.489 2.386 73.162 1.991 0.90 319900. 0.3158
|
|
84.92 0.3986 0.7110 0.0414 0.0232 4.785 20.104 15.023 3567.845 2.271 66.823 1.910 0.90 320392. 0.2896
|
|
89.39 0.4195 0.7136 0.0374 0.0220 4.531 19.039 13.566 3378.896 2.151 60.340 1.821 0.90 320902. 0.2624
|
|
93.86 0.4405 0.7091 0.0333 0.0207 4.264 17.917 12.081 3179.767 2.024 53.736 1.723 0.90 321430. 0.2343
|
|
98.33 0.4615 0.6956 0.0291 0.0193 3.986 16.747 10.574 2972.045 1.892 47.034 1.614 0.90 321978. 0.2053
|
|
102.80 0.4825 0.6710 0.0249 0.0179 3.697 15.536 9.051 2757.213 1.755 40.258 1.489 0.90 322545. 0.1752
|
|
107.27 0.5034 0.6319 0.0207 0.0165 3.403 14.298 7.517 2537.416 1.615 33.437 1.344 0.90 323131. 0.1441
|
|
111.73 0.5244 0.5739 0.0165 0.0151 3.105 13.046 5.981 2315.222 1.474 26.602 1.172 0.90 323736. 0.1121
|
|
116.20 0.5454 0.4912 0.0123 0.0136 2.806 11.792 4.449 2092.777 1.332 19.789 0.964 0.91 324360. 0.0796
|
|
120.67 0.5664 0.3757 0.0081 0.0122 2.511 10.553 2.932 1872.733 1.192 13.044 0.710 0.91 325004. 0.0476
|
|
125.14 0.5873 0.2163 0.0040 0.0108 2.223 9.340 1.441 1657.507 1.055 6.409 0.394 0.91 325667. 0.0185
|
|
129.61 0.6083 -0.0055 -0.0001 0.0094 1.934 8.127 -0.031 1442.222 0.918 -0.137 -0.010 0.91 326332. 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 0.0921 0.0397 9.941 39.160 38.052 7412.901 4.424 169.256 2.328 0.95 335012. 0.5618
|
|
4.88 0.0215 0.0492 0.0909 0.0396 9.924 39.094 37.529 7400.416 4.417 166.931 2.300 0.95 335210. 0.5512
|
|
9.76 0.0429 0.0972 0.0895 0.0395 9.891 38.964 36.953 7375.787 4.402 164.368 2.272 0.95 335425. 0.5404
|
|
14.64 0.0644 0.1441 0.0879 0.0393 9.840 38.763 36.320 7337.801 4.379 161.553 2.245 0.95 335657. 0.5293
|
|
19.52 0.0859 0.1898 0.0863 0.0390 9.770 38.486 35.628 7285.393 4.348 158.471 2.218 0.95 335906. 0.5179
|
|
24.40 0.1073 0.2344 0.0844 0.0387 9.679 38.129 34.871 7217.716 4.308 155.107 2.191 0.95 336173. 0.5062
|
|
29.28 0.1288 0.2778 0.0824 0.0382 9.567 37.687 34.048 7134.085 4.258 151.446 2.165 0.95 336459. 0.4941
|
|
34.16 0.1503 0.3201 0.0803 0.0377 9.433 37.158 33.156 7034.016 4.198 147.478 2.138 0.95 336764. 0.4816
|
|
39.03 0.1718 0.3612 0.0779 0.0371 9.276 36.541 32.193 6917.127 4.128 143.194 2.111 0.95 337088. 0.4685
|
|
43.91 0.1932 0.4011 0.0754 0.0363 9.096 35.833 31.157 6783.088 4.048 138.587 2.083 0.95 337431. 0.4549
|
|
48.79 0.2147 0.4396 0.0728 0.0355 8.893 35.033 30.048 6631.629 3.958 133.652 2.055 0.95 337794. 0.4407
|
|
53.67 0.2362 0.4767 0.0699 0.0346 8.666 34.139 28.864 6462.490 3.857 128.388 2.026 0.95 338178. 0.4258
|
|
58.55 0.2576 0.5122 0.0668 0.0336 8.416 33.152 27.607 6275.581 3.745 122.796 1.995 0.96 338581. 0.4101
|
|
63.43 0.2791 0.5459 0.0636 0.0325 8.141 32.071 26.278 6070.919 3.623 116.883 1.963 0.96 339005. 0.3937
|
|
68.31 0.3006 0.5778 0.0602 0.0313 7.843 30.896 24.878 5848.557 3.491 110.655 1.929 0.96 339449. 0.3764
|
|
73.19 0.3220 0.6074 0.0567 0.0300 7.521 29.627 23.408 5608.304 3.347 104.120 1.893 0.96 339914. 0.3583
|
|
78.07 0.3435 0.6335 0.0530 0.0287 7.187 28.313 21.872 5359.604 3.199 97.289 1.851 0.96 340398. 0.3386
|
|
82.95 0.3650 0.6547 0.0491 0.0274 6.850 26.986 20.277 5108.373 3.049 90.192 1.800 0.96 340904. 0.3171
|
|
87.83 0.3864 0.6710 0.0451 0.0260 6.502 25.615 18.630 4848.909 2.894 82.868 1.743 0.96 341430. 0.2942
|
|
92.71 0.4079 0.6765 0.0410 0.0247 6.188 24.378 16.935 4614.650 2.754 75.329 1.665 0.96 341977. 0.2680
|
|
97.59 0.4294 0.6686 0.0368 0.0236 5.915 23.300 15.198 4410.654 2.632 67.601 1.563 0.96 342544. 0.2383
|
|
102.47 0.4509 0.6516 0.0325 0.0225 5.632 22.186 13.431 4199.879 2.507 59.741 1.450 0.96 343133. 0.2079
|
|
107.35 0.4723 0.6233 0.0282 0.0214 5.346 21.060 11.642 3986.632 2.379 51.784 1.325 0.96 343742. 0.1768
|
|
112.22 0.4938 0.5821 0.0238 0.0202 5.059 19.929 9.840 3772.521 2.252 43.770 1.183 0.96 344373. 0.1452
|
|
117.10 0.5153 0.5257 0.0195 0.0191 4.774 18.804 8.036 3559.633 2.124 35.744 1.024 0.96 345025. 0.1135
|
|
121.98 0.5367 0.4518 0.0151 0.0180 4.493 17.699 6.241 3350.419 2.000 27.759 0.845 0.97 345698. 0.0826
|
|
126.86 0.5582 0.3581 0.0108 0.0169 4.221 16.627 4.468 3147.554 1.879 19.873 0.644 0.97 346394. 0.0532
|
|
131.74 0.5797 0.2424 0.0066 0.0158 3.959 15.596 2.731 2952.310 1.762 12.149 0.420 0.97 347112. 0.0271
|
|
136.62 0.6011 0.1022 0.0025 0.0148 3.706 14.599 1.040 2763.626 1.649 4.626 0.171 0.97 347856. 0.0068
|
|
141.50 0.6226
|
|
|
|
|
|
|