686 lines
122 KiB
Plaintext
686 lines
122 KiB
Plaintext
13x5.5E (13x55E.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 0.0826 0.0339 0.001 0.063 0.074 0.741 0.007 0.329 45.287 0.05 17783. 0.5582
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0.24 0.0193 0.0459 0.0810 0.0340 0.001 0.063 0.073 0.743 0.007 0.323 44.298 0.05 17793. 0.5407
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0.47 0.0385 0.0897 0.0793 0.0341 0.001 0.063 0.071 0.744 0.007 0.316 43.298 0.05 17803. 0.5230
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0.71 0.0578 0.1314 0.0775 0.0341 0.001 0.063 0.069 0.745 0.007 0.309 42.288 0.05 17814. 0.5050
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0.95 0.0771 0.1710 0.0756 0.0341 0.001 0.063 0.068 0.745 0.007 0.302 41.270 0.05 17826. 0.4869
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1.18 0.0963 0.2084 0.0737 0.0341 0.001 0.063 0.066 0.744 0.007 0.294 40.241 0.05 17838. 0.4685
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1.42 0.1156 0.2437 0.0716 0.0340 0.001 0.063 0.064 0.742 0.007 0.285 39.203 0.05 17851. 0.4500
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1.65 0.1349 0.2766 0.0694 0.0338 0.001 0.063 0.062 0.740 0.007 0.277 38.153 0.05 17864. 0.4312
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1.89 0.1541 0.3074 0.0671 0.0337 0.001 0.062 0.060 0.736 0.007 0.268 37.089 0.05 17879. 0.4123
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2.13 0.1734 0.3357 0.0648 0.0335 0.001 0.062 0.058 0.731 0.007 0.258 36.011 0.05 17894. 0.3931
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2.36 0.1927 0.3617 0.0623 0.0332 0.001 0.061 0.056 0.725 0.007 0.248 34.915 0.05 17910. 0.3738
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2.60 0.2120 0.3851 0.0597 0.0329 0.001 0.061 0.053 0.718 0.007 0.238 33.798 0.05 17926. 0.3542
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2.84 0.2312 0.4059 0.0570 0.0325 0.001 0.060 0.051 0.709 0.007 0.227 32.656 0.05 17944. 0.3344
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3.07 0.2505 0.4240 0.0542 0.0320 0.001 0.059 0.049 0.700 0.007 0.216 31.485 0.05 17962. 0.3144
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3.31 0.2698 0.4391 0.0513 0.0315 0.001 0.058 0.046 0.688 0.007 0.204 30.278 0.05 17981. 0.2941
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3.54 0.2890 0.4511 0.0483 0.0309 0.001 0.057 0.043 0.676 0.006 0.192 29.029 0.05 18001. 0.2735
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3.78 0.3083 0.4596 0.0451 0.0303 0.001 0.056 0.040 0.662 0.006 0.180 27.731 0.05 18022. 0.2527
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4.02 0.3276 0.4645 0.0419 0.0296 0.001 0.055 0.038 0.646 0.006 0.167 26.377 0.05 18044. 0.2317
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4.25 0.3468 0.4654 0.0387 0.0288 0.001 0.053 0.035 0.630 0.006 0.154 24.958 0.05 18066. 0.2105
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4.49 0.3661 0.4618 0.0353 0.0280 0.001 0.052 0.032 0.612 0.006 0.141 23.462 0.05 18090. 0.1891
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4.73 0.3854 0.4533 0.0319 0.0271 0.001 0.050 0.029 0.593 0.006 0.127 21.878 0.05 18114. 0.1676
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4.96 0.4046 0.4392 0.0284 0.0262 0.001 0.048 0.025 0.572 0.005 0.113 20.190 0.05 18140. 0.1460
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5.20 0.4239 0.4189 0.0249 0.0252 0.001 0.047 0.022 0.551 0.005 0.099 18.382 0.05 18166. 0.1244
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5.43 0.4432 0.3915 0.0213 0.0242 0.001 0.045 0.019 0.528 0.005 0.085 16.430 0.05 18193. 0.1029
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5.67 0.4624 0.3558 0.0177 0.0231 0.001 0.043 0.016 0.504 0.005 0.071 14.311 0.05 18221. 0.0818
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5.91 0.4817 0.3106 0.0141 0.0219 0.001 0.040 0.013 0.479 0.005 0.056 11.992 0.05 18250. 0.0611
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6.14 0.5010 0.2541 0.0105 0.0207 0.001 0.038 0.009 0.453 0.004 0.042 9.434 0.05 18280. 0.0415
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6.38 0.5202 0.1843 0.0069 0.0195 0.001 0.036 0.006 0.426 0.004 0.028 6.591 0.05 18311. 0.0235
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6.62 0.5395 0.0986 0.0033 0.0182 0.001 0.034 0.003 0.398 0.004 0.013 3.400 0.05 18342. 0.0084
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6.85 0.5588 -0.0068 -0.0002 0.0169 0.000 0.031 0.000 0.369 0.004 -0.001 -0.227 0.05 18374. 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 0.0829 0.0304 0.007 0.225 0.297 5.319 0.025 1.321 25.332 0.10 35567. 0.6256
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0.47 0.0193 0.0515 0.0813 0.0305 0.007 0.226 0.291 5.339 0.025 1.296 24.747 0.10 35586. 0.6052
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0.95 0.0387 0.1005 0.0796 0.0306 0.007 0.226 0.285 5.355 0.026 1.269 24.160 0.10 35607. 0.5847
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1.42 0.0580 0.1471 0.0778 0.0307 0.007 0.227 0.279 5.366 0.026 1.240 23.572 0.10 35628. 0.5640
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1.90 0.0774 0.1913 0.0759 0.0307 0.007 0.227 0.272 5.370 0.026 1.210 22.984 0.10 35652. 0.5433
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2.37 0.0967 0.2329 0.0739 0.0307 0.007 0.227 0.265 5.368 0.026 1.179 22.395 0.10 35676. 0.5224
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2.85 0.1161 0.2722 0.0719 0.0306 0.007 0.226 0.258 5.358 0.026 1.146 21.806 0.10 35702. 0.5015
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3.32 0.1354 0.3089 0.0697 0.0305 0.007 0.226 0.250 5.340 0.025 1.111 21.216 0.10 35729. 0.4804
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3.80 0.1548 0.3432 0.0674 0.0304 0.007 0.225 0.242 5.313 0.025 1.075 20.624 0.10 35758. 0.4593
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4.27 0.1741 0.3750 0.0650 0.0302 0.007 0.223 0.233 5.277 0.025 1.036 20.029 0.10 35789. 0.4381
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4.75 0.1935 0.4042 0.0625 0.0299 0.007 0.221 0.224 5.230 0.025 0.997 19.431 0.10 35821. 0.4167
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5.22 0.2128 0.4308 0.0599 0.0296 0.007 0.219 0.215 5.173 0.025 0.955 18.826 0.10 35854. 0.3953
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5.69 0.2322 0.4547 0.0572 0.0292 0.007 0.216 0.205 5.105 0.024 0.912 18.215 0.10 35890. 0.3737
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6.17 0.2515 0.4758 0.0544 0.0287 0.007 0.212 0.195 5.025 0.024 0.867 17.593 0.10 35926. 0.3519
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6.64 0.2709 0.4939 0.0514 0.0282 0.007 0.208 0.184 4.932 0.024 0.820 16.957 0.10 35965. 0.3300
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7.12 0.2902 0.5088 0.0484 0.0276 0.006 0.204 0.174 4.827 0.023 0.772 16.306 0.10 36005. 0.3078
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7.59 0.3096 0.5203 0.0453 0.0269 0.006 0.199 0.162 4.710 0.022 0.722 15.633 0.10 36047. 0.2854
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8.07 0.3289 0.5282 0.0421 0.0262 0.006 0.194 0.151 4.581 0.022 0.671 14.936 0.10 36091. 0.2628
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8.54 0.3483 0.5320 0.0388 0.0254 0.006 0.188 0.139 4.439 0.021 0.619 14.208 0.10 36136. 0.2401
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9.02 0.3676 0.5313 0.0354 0.0245 0.006 0.181 0.127 4.286 0.020 0.565 13.442 0.10 36184. 0.2171
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9.49 0.3870 0.5255 0.0320 0.0236 0.006 0.174 0.115 4.121 0.020 0.510 12.631 0.10 36233. 0.1939
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9.96 0.4063 0.5139 0.0285 0.0226 0.005 0.167 0.102 3.944 0.019 0.455 11.764 0.10 36284. 0.1705
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10.44 0.4257 0.4956 0.0250 0.0215 0.005 0.159 0.090 3.756 0.018 0.399 10.828 0.10 36336. 0.1469
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10.91 0.4450 0.4692 0.0215 0.0203 0.005 0.150 0.077 3.557 0.017 0.342 9.807 0.10 36391. 0.1232
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11.39 0.4643 0.4334 0.0179 0.0191 0.004 0.141 0.064 3.347 0.016 0.285 8.680 0.10 36447. 0.0995
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11.86 0.4837 0.3859 0.0143 0.0179 0.004 0.132 0.051 3.127 0.015 0.228 7.420 0.10 36506. 0.0760
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12.34 0.5030 0.3239 0.0107 0.0166 0.004 0.122 0.038 2.897 0.014 0.170 5.988 0.10 36566. 0.0531
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12.81 0.5224 0.2435 0.0071 0.0152 0.004 0.112 0.025 2.658 0.013 0.113 4.335 0.10 36628. 0.0313
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13.29 0.5417 0.1390 0.0035 0.0138 0.003 0.102 0.013 2.412 0.012 0.056 2.386 0.10 36692. 0.0122
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13.76 0.5611 0.0016 0.0000 0.0123 0.003 0.091 0.000 2.158 0.010 0.001 0.027 0.10 36757. 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 0.0831 0.0289 0.023 0.481 0.670 17.059 0.054 2.981 17.821 0.15 53349. 0.6611
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0.71 0.0194 0.0545 0.0815 0.0290 0.023 0.483 0.657 17.137 0.055 2.924 17.397 0.15 53379. 0.6391
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1.43 0.0388 0.1063 0.0798 0.0292 0.023 0.485 0.644 17.199 0.055 2.863 16.974 0.15 53409. 0.6170
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2.14 0.0582 0.1554 0.0780 0.0292 0.023 0.486 0.629 17.243 0.055 2.799 16.551 0.15 53442. 0.5949
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2.86 0.0776 0.2020 0.0761 0.0293 0.023 0.486 0.614 17.264 0.055 2.731 16.131 0.15 53477. 0.5727
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3.57 0.0970 0.2459 0.0741 0.0293 0.023 0.486 0.598 17.263 0.055 2.660 15.712 0.15 53514. 0.5505
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4.28 0.1164 0.2872 0.0721 0.0292 0.023 0.486 0.581 17.235 0.055 2.585 15.294 0.15 53553. 0.5283
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5.00 0.1359 0.3260 0.0699 0.0291 0.023 0.484 0.563 17.178 0.055 2.506 14.878 0.15 53595. 0.5060
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5.71 0.1553 0.3621 0.0676 0.0290 0.023 0.482 0.545 17.091 0.054 2.424 14.462 0.15 53638. 0.4837
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6.43 0.1747 0.3957 0.0652 0.0288 0.023 0.478 0.526 16.971 0.054 2.338 14.047 0.15 53684. 0.4614
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7.14 0.1941 0.4267 0.0627 0.0285 0.023 0.474 0.505 16.815 0.054 2.248 13.631 0.15 53732. 0.4390
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7.85 0.2135 0.4549 0.0600 0.0282 0.022 0.468 0.484 16.621 0.053 2.154 13.213 0.15 53783. 0.4166
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8.57 0.2329 0.4805 0.0573 0.0278 0.022 0.462 0.462 16.388 0.052 2.056 12.792 0.15 53836. 0.3941
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9.28 0.2523 0.5032 0.0545 0.0273 0.022 0.454 0.439 16.114 0.051 1.954 12.367 0.15 53892. 0.3714
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10.00 0.2717 0.5230 0.0515 0.0268 0.021 0.445 0.416 15.796 0.050 1.849 11.934 0.15 53950. 0.3486
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10.71 0.2911 0.5396 0.0485 0.0262 0.021 0.435 0.391 15.433 0.049 1.739 11.493 0.15 54010. 0.3257
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11.42 0.3105 0.5529 0.0453 0.0255 0.020 0.423 0.366 15.027 0.048 1.627 11.040 0.15 54074. 0.3025
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12.14 0.3299 0.5625 0.0421 0.0247 0.020 0.411 0.340 14.577 0.046 1.511 10.571 0.15 54140. 0.2792
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12.85 0.3493 0.5681 0.0388 0.0239 0.019 0.397 0.313 14.084 0.045 1.393 10.084 0.16 54208. 0.2557
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13.57 0.3687 0.5693 0.0355 0.0230 0.018 0.382 0.286 13.548 0.043 1.272 9.573 0.16 54280. 0.2319
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14.28 0.3882 0.5654 0.0320 0.0220 0.017 0.365 0.258 12.970 0.041 1.149 9.031 0.16 54354. 0.2080
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14.99 0.4076 0.5556 0.0285 0.0209 0.017 0.348 0.230 12.349 0.039 1.024 8.452 0.16 54430. 0.1837
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15.71 0.4270 0.5388 0.0250 0.0198 0.016 0.329 0.202 11.688 0.037 0.897 7.825 0.16 54510. 0.1592
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16.42 0.4464 0.5138 0.0214 0.0186 0.015 0.310 0.173 10.986 0.035 0.769 7.137 0.16 54592. 0.1344
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17.14 0.4658 0.4785 0.0178 0.0174 0.014 0.289 0.144 10.245 0.033 0.640 6.370 0.16 54677. 0.1095
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17.85 0.4852 0.4304 0.0142 0.0160 0.013 0.267 0.115 9.467 0.030 0.511 5.501 0.16 54765. 0.0845
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18.56 0.5046 0.3658 0.0106 0.0147 0.012 0.244 0.086 8.654 0.028 0.381 4.495 0.16 54856. 0.0597
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19.28 0.5240 0.2792 0.0071 0.0132 0.010 0.220 0.057 7.810 0.025 0.253 3.304 0.16 54950. 0.0357
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19.99 0.5434 0.1623 0.0035 0.0118 0.009 0.195 0.028 6.938 0.022 0.126 1.852 0.16 55046. 0.0141
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20.71 0.5628 0.0006 0.0000 0.0102 0.008 0.170 0.000 6.038 0.019 0.000 0.007 0.16 55143. 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 0.0834 0.0281 0.053 0.829 1.195 39.241 0.094 5.316 13.815 0.21 71132. 0.6843
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0.95 0.0194 0.0564 0.0817 0.0282 0.053 0.833 1.172 39.438 0.094 5.214 13.481 0.21 71170. 0.6613
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1.91 0.0389 0.1099 0.0800 0.0283 0.053 0.837 1.148 39.596 0.095 5.105 13.147 0.21 71212. 0.6382
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2.86 0.0583 0.1608 0.0783 0.0284 0.053 0.839 1.122 39.709 0.095 4.991 12.816 0.21 71256. 0.6151
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3.82 0.0778 0.2088 0.0764 0.0284 0.053 0.840 1.095 39.770 0.095 4.870 12.487 0.21 71303. 0.5920
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4.77 0.0972 0.2542 0.0744 0.0284 0.053 0.840 1.066 39.774 0.095 4.743 12.160 0.21 71352. 0.5690
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5.72 0.1167 0.2969 0.0723 0.0284 0.053 0.839 1.036 39.714 0.095 4.609 11.835 0.21 71404. 0.5459
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6.68 0.1361 0.3369 0.0701 0.0283 0.053 0.836 1.005 39.586 0.095 4.469 11.512 0.21 71460. 0.5228
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7.63 0.1556 0.3743 0.0678 0.0282 0.053 0.832 0.972 39.382 0.094 4.322 11.190 0.21 71518. 0.4998
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8.58 0.1750 0.4091 0.0653 0.0280 0.052 0.826 0.937 39.098 0.093 4.168 10.870 0.21 71579. 0.4768
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9.54 0.1944 0.4412 0.0628 0.0277 0.052 0.818 0.901 38.728 0.092 4.007 10.550 0.21 71644. 0.4537
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10.49 0.2139 0.4706 0.0602 0.0274 0.051 0.809 0.863 38.267 0.091 3.839 10.231 0.21 71712. 0.4307
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11.45 0.2333 0.4972 0.0575 0.0270 0.051 0.797 0.824 37.709 0.090 3.665 9.910 0.21 71783. 0.4076
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12.40 0.2528 0.5211 0.0546 0.0265 0.050 0.783 0.783 37.050 0.088 3.483 9.586 0.21 71857. 0.3844
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13.35 0.2722 0.5420 0.0517 0.0259 0.049 0.767 0.741 36.284 0.087 3.294 9.259 0.21 71935. 0.3610
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14.31 0.2917 0.5598 0.0486 0.0253 0.047 0.748 0.697 35.409 0.085 3.099 8.925 0.21 72016. 0.3376
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15.26 0.3111 0.5743 0.0454 0.0246 0.046 0.727 0.652 34.427 0.082 2.898 8.585 0.21 72101. 0.3140
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16.21 0.3306 0.5853 0.0422 0.0238 0.045 0.704 0.605 33.337 0.080 2.692 8.233 0.21 72189. 0.2902
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17.17 0.3500 0.5922 0.0389 0.0230 0.043 0.679 0.558 32.142 0.077 2.480 7.869 0.21 72281. 0.2662
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18.12 0.3694 0.5948 0.0355 0.0221 0.041 0.652 0.509 30.842 0.074 2.264 7.487 0.21 72376. 0.2421
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19.08 0.3889 0.5923 0.0321 0.0210 0.039 0.622 0.460 29.436 0.070 2.045 7.083 0.21 72475. 0.2176
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20.03 0.4083 0.5840 0.0286 0.0200 0.037 0.590 0.410 27.927 0.067 1.822 6.651 0.21 72578. 0.1929
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20.98 0.4278 0.5687 0.0250 0.0188 0.035 0.556 0.359 26.316 0.063 1.596 6.183 0.21 72684. 0.1678
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21.94 0.4472 0.5450 0.0214 0.0176 0.033 0.520 0.307 24.604 0.059 1.367 5.667 0.21 72794. 0.1424
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22.89 0.4667 0.5106 0.0178 0.0163 0.031 0.482 0.256 22.797 0.054 1.138 5.088 0.21 72908. 0.1166
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23.84 0.4861 0.4627 0.0142 0.0149 0.028 0.442 0.204 20.898 0.050 0.907 4.427 0.21 73026. 0.0906
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24.80 0.5056 0.3969 0.0106 0.0135 0.025 0.400 0.152 18.914 0.045 0.677 3.651 0.21 73148. 0.0645
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25.75 0.5250 0.3064 0.0070 0.0121 0.023 0.356 0.101 16.853 0.040 0.449 2.714 0.21 73273. 0.0390
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26.71 0.5444 0.1804 0.0035 0.0105 0.020 0.311 0.050 14.724 0.035 0.222 1.541 0.21 73402. 0.0156
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27.66 0.5639 -0.0012 0.0000 0.0090 0.017 0.265 0.000 12.524 0.030 -0.001 -0.010 0.21 73531. 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 0.0837 0.0275 0.101 1.271 1.874 75.189 0.144 8.336 11.306 0.26 88913. 0.7013
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1.19 0.0195 0.0577 0.0820 0.0277 0.101 1.278 1.838 75.589 0.144 8.176 11.029 0.26 88961. 0.6775
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2.39 0.0389 0.1125 0.0803 0.0278 0.102 1.283 1.800 75.911 0.145 8.006 10.754 0.26 89013. 0.6537
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3.58 0.0584 0.1644 0.0785 0.0279 0.102 1.287 1.760 76.143 0.145 7.826 10.481 0.26 89068. 0.6300
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4.77 0.0778 0.2136 0.0766 0.0279 0.102 1.289 1.717 76.273 0.146 7.637 10.211 0.26 89127. 0.6062
|
|
5.96 0.0973 0.2599 0.0746 0.0279 0.102 1.290 1.672 76.289 0.146 7.438 9.942 0.26 89189. 0.5826
|
|
7.16 0.1167 0.3036 0.0725 0.0279 0.102 1.288 1.625 76.181 0.145 7.229 9.676 0.26 89254. 0.5589
|
|
8.35 0.1362 0.3445 0.0703 0.0278 0.102 1.284 1.576 75.935 0.145 7.009 9.412 0.26 89324. 0.5353
|
|
9.54 0.1556 0.3827 0.0680 0.0277 0.101 1.277 1.524 75.541 0.144 6.778 9.150 0.26 89397. 0.5118
|
|
10.73 0.1751 0.4183 0.0656 0.0275 0.101 1.268 1.470 74.987 0.143 6.537 8.889 0.26 89473. 0.4883
|
|
11.93 0.1945 0.4512 0.0631 0.0272 0.100 1.255 1.413 74.261 0.142 6.285 8.630 0.26 89554. 0.4648
|
|
13.12 0.2140 0.4815 0.0604 0.0269 0.098 1.240 1.354 73.354 0.140 6.022 8.371 0.26 89639. 0.4413
|
|
14.31 0.2334 0.5090 0.0577 0.0265 0.097 1.221 1.292 72.255 0.138 5.748 8.112 0.26 89728. 0.4178
|
|
15.50 0.2529 0.5337 0.0548 0.0260 0.095 1.199 1.228 70.955 0.136 5.463 7.851 0.26 89821. 0.3943
|
|
16.70 0.2723 0.5555 0.0519 0.0254 0.093 1.174 1.162 69.441 0.133 5.168 7.588 0.26 89919. 0.3706
|
|
17.89 0.2918 0.5742 0.0488 0.0248 0.091 1.145 1.093 67.710 0.129 4.862 7.322 0.26 90020. 0.3468
|
|
19.08 0.3112 0.5897 0.0456 0.0241 0.088 1.112 1.022 65.764 0.126 4.546 7.049 0.26 90126. 0.3229
|
|
20.28 0.3307 0.6017 0.0424 0.0233 0.085 1.075 0.949 63.605 0.121 4.223 6.770 0.26 90237. 0.2989
|
|
21.47 0.3501 0.6099 0.0390 0.0224 0.082 1.035 0.875 61.233 0.117 3.891 6.480 0.26 90351. 0.2746
|
|
22.66 0.3696 0.6137 0.0357 0.0215 0.079 0.991 0.799 58.650 0.112 3.553 6.177 0.26 90471. 0.2502
|
|
23.85 0.3890 0.6125 0.0322 0.0204 0.075 0.944 0.721 55.857 0.107 3.208 5.857 0.26 90595. 0.2254
|
|
25.05 0.4085 0.6056 0.0287 0.0194 0.071 0.893 0.643 52.855 0.101 2.859 5.515 0.26 90723. 0.2003
|
|
26.24 0.4279 0.5917 0.0251 0.0182 0.067 0.839 0.563 49.648 0.095 2.505 5.144 0.26 90856. 0.1749
|
|
27.43 0.4474 0.5694 0.0215 0.0169 0.062 0.782 0.483 46.241 0.088 2.147 4.735 0.26 90994. 0.1490
|
|
28.62 0.4668 0.5363 0.0179 0.0156 0.057 0.721 0.402 42.640 0.081 1.787 4.274 0.26 91137. 0.1228
|
|
29.82 0.4863 0.4893 0.0143 0.0142 0.052 0.657 0.321 38.856 0.074 1.426 3.743 0.26 91284. 0.0960
|
|
31.01 0.5058 0.4235 0.0107 0.0128 0.047 0.590 0.240 34.901 0.067 1.066 3.115 0.26 91436. 0.0691
|
|
32.20 0.5252 0.3311 0.0071 0.0113 0.041 0.521 0.159 30.792 0.059 0.708 2.345 0.26 91593. 0.0424
|
|
33.40 0.5447 0.1993 0.0036 0.0097 0.036 0.449 0.080 26.547 0.051 0.354 1.361 0.26 91754. 0.0174
|
|
34.59 0.5641 0.0030 0.0000 0.0081 0.030 0.375 0.001 22.158 0.042 0.004 0.020 0.26 91915. 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 0.0840 0.0272 0.172 1.808 2.710 128.333 0.204 12.055 9.578 0.31 106693. 0.7145
|
|
1.43 0.0195 0.0587 0.0824 0.0273 0.173 1.818 2.658 129.042 0.205 11.822 9.342 0.31 106751. 0.6901
|
|
2.87 0.0390 0.1145 0.0807 0.0275 0.174 1.826 2.603 129.614 0.206 11.577 9.108 0.31 106814. 0.6658
|
|
4.30 0.0585 0.1673 0.0789 0.0275 0.174 1.832 2.544 130.028 0.207 11.317 8.875 0.31 106880. 0.6415
|
|
5.73 0.0779 0.2173 0.0770 0.0276 0.175 1.835 2.483 130.263 0.207 11.043 8.645 0.31 106951. 0.6172
|
|
7.17 0.0974 0.2645 0.0749 0.0276 0.175 1.836 2.418 130.299 0.207 10.755 8.417 0.31 107025. 0.5930
|
|
8.60 0.1169 0.3089 0.0728 0.0276 0.174 1.833 2.350 130.115 0.207 10.452 8.191 0.31 107104. 0.5689
|
|
10.04 0.1364 0.3505 0.0706 0.0275 0.174 1.827 2.278 129.690 0.206 10.133 7.968 0.31 107188. 0.5449
|
|
11.47 0.1559 0.3895 0.0683 0.0273 0.173 1.817 2.203 129.003 0.205 9.800 7.746 0.31 107276. 0.5210
|
|
12.90 0.1754 0.4257 0.0659 0.0271 0.172 1.804 2.125 128.034 0.204 9.450 7.526 0.31 107368. 0.4971
|
|
14.34 0.1948 0.4593 0.0633 0.0269 0.170 1.786 2.042 126.764 0.202 9.085 7.308 0.31 107466. 0.4732
|
|
15.77 0.2143 0.4902 0.0607 0.0265 0.168 1.763 1.957 125.174 0.199 8.704 7.090 0.31 107568. 0.4494
|
|
17.20 0.2338 0.5183 0.0579 0.0261 0.165 1.736 1.868 123.247 0.196 8.307 6.873 0.31 107675. 0.4256
|
|
18.64 0.2533 0.5437 0.0550 0.0256 0.162 1.704 1.775 120.964 0.193 7.894 6.655 0.31 107787. 0.4017
|
|
20.07 0.2728 0.5662 0.0520 0.0251 0.159 1.667 1.679 118.305 0.188 7.466 6.435 0.31 107904. 0.3778
|
|
21.50 0.2923 0.5857 0.0489 0.0244 0.155 1.624 1.579 115.263 0.183 7.023 6.213 0.31 108027. 0.3537
|
|
22.94 0.3117 0.6020 0.0458 0.0237 0.150 1.576 1.476 111.842 0.178 6.566 5.987 0.31 108154. 0.3296
|
|
24.37 0.3312 0.6148 0.0425 0.0229 0.145 1.522 1.371 108.043 0.172 6.097 5.754 0.31 108287. 0.3053
|
|
25.80 0.3507 0.6238 0.0391 0.0220 0.139 1.463 1.263 103.869 0.165 5.617 5.514 0.31 108426. 0.2808
|
|
27.24 0.3702 0.6285 0.0357 0.0210 0.133 1.399 1.153 99.321 0.158 5.127 5.264 0.31 108569. 0.2560
|
|
28.67 0.3897 0.6284 0.0322 0.0200 0.127 1.330 1.040 94.400 0.150 4.628 4.999 0.31 108718. 0.2310
|
|
30.11 0.4092 0.6224 0.0287 0.0189 0.120 1.255 0.927 89.111 0.142 4.121 4.716 0.31 108873. 0.2057
|
|
31.54 0.4287 0.6096 0.0251 0.0177 0.112 1.176 0.811 83.459 0.133 3.608 4.409 0.31 109034. 0.1799
|
|
32.97 0.4481 0.5882 0.0215 0.0164 0.104 1.091 0.695 77.453 0.123 3.091 4.069 0.31 109199. 0.1537
|
|
34.41 0.4676 0.5559 0.0179 0.0151 0.095 1.002 0.578 71.105 0.113 2.570 3.685 0.31 109371. 0.1269
|
|
35.84 0.4871 0.5092 0.0143 0.0137 0.086 0.908 0.460 64.433 0.103 2.048 3.240 0.31 109548. 0.0996
|
|
37.27 0.5066 0.4426 0.0106 0.0122 0.077 0.809 0.343 57.459 0.091 1.526 2.709 0.31 109732. 0.0719
|
|
38.71 0.5261 0.3476 0.0070 0.0106 0.067 0.707 0.227 50.214 0.080 1.009 2.048 0.31 109920. 0.0442
|
|
40.14 0.5456 0.2088 0.0035 0.0091 0.057 0.602 0.112 42.730 0.068 0.497 1.187 0.31 110114. 0.0180
|
|
41.57 0.5650 -0.0053 -0.0001 0.0074 0.047 0.493 -0.002 34.978 0.056 -0.010 -0.029 0.31 110305. 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 0.0844 0.0270 0.271 2.442 3.707 202.264 0.276 16.488 8.312 0.36 124471. 0.7252
|
|
1.69 0.0197 0.0602 0.0828 0.0271 0.273 2.456 3.635 203.421 0.278 16.167 8.104 0.36 124541. 0.7001
|
|
3.39 0.0395 0.1173 0.0810 0.0273 0.274 2.467 3.558 204.353 0.279 15.827 7.897 0.36 124615. 0.6750
|
|
5.08 0.0592 0.1714 0.0792 0.0274 0.275 2.476 3.477 205.022 0.280 15.467 7.693 0.36 124694. 0.6500
|
|
6.78 0.0789 0.2225 0.0772 0.0274 0.275 2.480 3.392 205.396 0.280 15.087 7.490 0.36 124777. 0.6251
|
|
8.47 0.0987 0.2707 0.0752 0.0274 0.275 2.481 3.302 205.439 0.280 14.687 7.290 0.36 124866. 0.6002
|
|
10.16 0.1184 0.3160 0.0730 0.0274 0.275 2.477 3.207 205.116 0.280 14.266 7.092 0.36 124960. 0.5755
|
|
11.86 0.1381 0.3585 0.0708 0.0273 0.274 2.468 3.108 204.393 0.279 13.824 6.897 0.36 125059. 0.5509
|
|
13.55 0.1579 0.3982 0.0684 0.0271 0.273 2.454 3.003 203.235 0.277 13.359 6.703 0.36 125163. 0.5264
|
|
15.24 0.1776 0.4351 0.0659 0.0269 0.270 2.434 2.894 201.609 0.275 12.873 6.511 0.36 125274. 0.5019
|
|
16.94 0.1973 0.4693 0.0633 0.0266 0.268 2.409 2.780 199.481 0.272 12.364 6.321 0.36 125390. 0.4775
|
|
18.63 0.2171 0.5008 0.0606 0.0263 0.264 2.377 2.661 196.822 0.269 11.834 6.131 0.36 125511. 0.4531
|
|
20.33 0.2368 0.5295 0.0578 0.0258 0.260 2.338 2.536 193.600 0.264 11.281 5.942 0.36 125639. 0.4288
|
|
22.02 0.2565 0.5553 0.0548 0.0253 0.255 2.292 2.407 189.786 0.259 10.707 5.753 0.36 125772. 0.4044
|
|
23.71 0.2763 0.5782 0.0518 0.0247 0.249 2.238 2.273 185.349 0.253 10.110 5.562 0.36 125912. 0.3799
|
|
25.41 0.2960 0.5980 0.0486 0.0241 0.242 2.177 2.134 180.277 0.246 9.492 5.369 0.36 126058. 0.3554
|
|
27.10 0.3157 0.6146 0.0453 0.0233 0.234 2.108 1.991 174.578 0.238 8.856 5.173 0.36 126210. 0.3307
|
|
28.80 0.3355 0.6276 0.0420 0.0224 0.226 2.032 1.844 168.255 0.230 8.203 4.971 0.36 126369. 0.3059
|
|
30.49 0.3552 0.6366 0.0386 0.0215 0.216 1.948 1.694 161.310 0.220 7.535 4.763 0.36 126534. 0.2809
|
|
32.18 0.3749 0.6413 0.0351 0.0205 0.206 1.856 1.541 153.747 0.210 6.853 4.545 0.36 126705. 0.2556
|
|
33.88 0.3946 0.6408 0.0315 0.0194 0.195 1.758 1.385 145.567 0.199 6.159 4.315 0.36 126883. 0.2300
|
|
35.57 0.4144 0.6342 0.0279 0.0182 0.183 1.652 1.226 136.778 0.187 5.455 4.067 0.36 127068. 0.2041
|
|
37.26 0.4341 0.6202 0.0243 0.0170 0.171 1.538 1.066 127.390 0.174 4.743 3.796 0.36 127259. 0.1776
|
|
38.96 0.4538 0.5969 0.0206 0.0157 0.157 1.418 0.905 117.421 0.160 4.024 3.495 0.36 127457. 0.1506
|
|
40.65 0.4736 0.5614 0.0169 0.0143 0.143 1.291 0.742 106.892 0.146 3.302 3.150 0.36 127662. 0.1230
|
|
42.35 0.4933 0.5094 0.0132 0.0128 0.129 1.157 0.580 95.836 0.131 2.579 2.744 0.36 127874. 0.0947
|
|
44.04 0.5130 0.4341 0.0095 0.0112 0.113 1.018 0.418 84.296 0.115 1.859 2.248 0.36 128092. 0.0659
|
|
45.73 0.5328 0.3235 0.0059 0.0096 0.097 0.873 0.257 72.324 0.099 1.144 1.613 0.36 128318. 0.0371
|
|
47.43 0.5525 0.1554 0.0023 0.0080 0.080 0.724 0.099 59.973 0.082 0.440 0.748 0.37 128548. 0.0106
|
|
49.12 0.5722
|
|
|
|
|
|
|
|
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 0.0849 0.0269 0.403 3.178 4.869 300.794 0.359 21.658 7.342 0.41 142248. 0.7341
|
|
1.94 0.0197 0.0608 0.0832 0.0270 0.406 3.196 4.774 302.543 0.361 21.237 7.158 0.41 142328. 0.7087
|
|
3.87 0.0395 0.1184 0.0815 0.0272 0.408 3.211 4.674 303.947 0.363 20.790 6.975 0.41 142412. 0.6833
|
|
5.81 0.0592 0.1730 0.0796 0.0273 0.409 3.222 4.568 304.957 0.364 20.318 6.794 0.41 142503. 0.6580
|
|
7.74 0.0789 0.2246 0.0777 0.0273 0.410 3.228 4.456 305.518 0.365 19.820 6.615 0.41 142599. 0.6327
|
|
9.68 0.0987 0.2733 0.0756 0.0273 0.410 3.229 4.338 305.578 0.365 19.295 6.439 0.41 142700. 0.6076
|
|
11.62 0.1184 0.3190 0.0735 0.0273 0.409 3.223 4.214 305.084 0.364 18.742 6.264 0.41 142808. 0.5827
|
|
13.55 0.1381 0.3620 0.0712 0.0272 0.408 3.212 4.083 303.984 0.363 18.161 6.092 0.41 142921. 0.5578
|
|
15.49 0.1579 0.4021 0.0688 0.0270 0.405 3.193 3.946 302.226 0.361 17.552 5.922 0.41 143041. 0.5330
|
|
17.42 0.1776 0.4395 0.0663 0.0268 0.402 3.167 3.802 299.757 0.358 16.913 5.753 0.41 143167. 0.5083
|
|
19.36 0.1974 0.4742 0.0637 0.0265 0.398 3.133 3.652 296.531 0.354 16.245 5.586 0.41 143300. 0.4837
|
|
21.30 0.2171 0.5061 0.0609 0.0261 0.392 3.090 3.496 292.499 0.349 15.548 5.420 0.41 143439. 0.4592
|
|
23.23 0.2368 0.5352 0.0581 0.0257 0.386 3.039 3.332 287.617 0.343 14.822 5.255 0.41 143586. 0.4347
|
|
25.17 0.2566 0.5616 0.0551 0.0252 0.378 2.978 3.163 281.838 0.336 14.067 5.090 0.41 143739. 0.4101
|
|
27.11 0.2763 0.5850 0.0521 0.0246 0.369 2.907 2.986 275.114 0.328 13.283 4.923 0.41 143899. 0.3855
|
|
29.04 0.2960 0.6054 0.0489 0.0239 0.359 2.825 2.804 267.431 0.319 12.472 4.755 0.41 144066. 0.3608
|
|
30.98 0.3158 0.6226 0.0456 0.0231 0.347 2.734 2.616 258.795 0.309 11.636 4.585 0.41 144240. 0.3360
|
|
32.91 0.3355 0.6363 0.0422 0.0223 0.334 2.633 2.423 249.215 0.297 10.778 4.410 0.41 144421. 0.3110
|
|
34.85 0.3552 0.6461 0.0388 0.0213 0.320 2.522 2.226 238.691 0.285 9.900 4.229 0.41 144610. 0.2859
|
|
36.79 0.3750 0.6516 0.0353 0.0203 0.305 2.401 2.024 227.228 0.271 9.004 4.040 0.41 144806. 0.2605
|
|
38.72 0.3947 0.6520 0.0317 0.0192 0.288 2.270 1.819 214.831 0.256 8.092 3.841 0.41 145009. 0.2347
|
|
40.66 0.4144 0.6464 0.0281 0.0180 0.270 2.129 1.611 201.509 0.241 7.167 3.627 0.41 145221. 0.2086
|
|
42.59 0.4342 0.6335 0.0244 0.0167 0.251 1.979 1.401 187.279 0.224 6.231 3.393 0.41 145439. 0.1819
|
|
44.53 0.4539 0.6113 0.0207 0.0154 0.231 1.819 1.189 172.166 0.206 5.287 3.131 0.42 145666. 0.1547
|
|
46.47 0.4736 0.5768 0.0170 0.0140 0.209 1.650 0.975 156.204 0.186 4.338 2.832 0.42 145900. 0.1267
|
|
48.40 0.4934 0.5257 0.0133 0.0125 0.187 1.473 0.762 139.444 0.166 3.388 2.477 0.42 146142. 0.0980
|
|
50.34 0.5131 0.4504 0.0096 0.0109 0.164 1.288 0.549 121.950 0.146 2.441 2.041 0.42 146392. 0.0685
|
|
52.27 0.5329 0.3383 0.0059 0.0093 0.139 1.097 0.338 103.802 0.124 1.503 1.476 0.42 146650. 0.0389
|
|
54.21 0.5526 0.1643 0.0023 0.0076 0.114 0.899 0.130 85.080 0.102 0.577 0.692 0.42 146913. 0.0113
|
|
56.15 0.5723
|
|
|
|
|
|
|
|
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 0.0855 0.0269 0.574 4.020 6.203 428.034 0.454 27.590 6.573 0.46 160022. 0.7417
|
|
2.15 0.0195 0.0604 0.0838 0.0270 0.577 4.043 6.084 430.513 0.457 27.062 6.410 0.46 160111. 0.7164
|
|
4.30 0.0389 0.1177 0.0821 0.0272 0.580 4.062 5.958 432.509 0.459 26.503 6.248 0.46 160205. 0.6911
|
|
6.44 0.0584 0.1720 0.0803 0.0272 0.582 4.075 5.826 433.949 0.460 25.912 6.089 0.46 160306. 0.6659
|
|
8.59 0.0779 0.2234 0.0783 0.0273 0.583 4.083 5.685 434.762 0.461 25.289 5.931 0.46 160412. 0.6408
|
|
10.74 0.0973 0.2720 0.0763 0.0273 0.583 4.084 5.538 434.874 0.461 24.632 5.776 0.46 160525. 0.6159
|
|
12.89 0.1168 0.3177 0.0741 0.0273 0.582 4.078 5.382 434.213 0.461 23.940 5.622 0.46 160644. 0.5910
|
|
15.04 0.1362 0.3606 0.0719 0.0272 0.580 4.064 5.219 432.706 0.459 23.214 5.471 0.46 160770. 0.5663
|
|
17.18 0.1557 0.4009 0.0695 0.0270 0.577 4.041 5.048 430.281 0.457 22.452 5.321 0.46 160902. 0.5417
|
|
19.33 0.1752 0.4384 0.0671 0.0268 0.572 4.009 4.868 426.866 0.453 21.655 5.173 0.46 161042. 0.5172
|
|
21.48 0.1946 0.4733 0.0645 0.0265 0.566 3.967 4.681 422.395 0.448 20.821 5.026 0.46 161188. 0.4928
|
|
23.63 0.2141 0.5056 0.0618 0.0262 0.559 3.914 4.485 416.801 0.442 19.951 4.881 0.46 161342. 0.4684
|
|
25.78 0.2336 0.5352 0.0590 0.0257 0.550 3.851 4.282 410.023 0.435 19.044 4.736 0.46 161503. 0.4441
|
|
27.92 0.2530 0.5621 0.0561 0.0252 0.539 3.775 4.070 401.998 0.427 18.102 4.592 0.46 161672. 0.4197
|
|
30.07 0.2725 0.5863 0.0530 0.0246 0.527 3.688 3.850 392.657 0.417 17.124 4.447 0.46 161848. 0.3954
|
|
32.22 0.2919 0.6075 0.0499 0.0240 0.512 3.587 3.622 381.967 0.405 16.110 4.301 0.46 162032. 0.3709
|
|
34.37 0.3114 0.6257 0.0467 0.0232 0.496 3.474 3.387 369.938 0.393 15.066 4.153 0.46 162224. 0.3463
|
|
36.52 0.3309 0.6407 0.0433 0.0224 0.478 3.349 3.146 356.578 0.378 13.994 4.002 0.46 162424. 0.3216
|
|
38.66 0.3503 0.6520 0.0399 0.0215 0.458 3.211 2.899 341.892 0.363 12.896 3.846 0.47 162631. 0.2968
|
|
40.81 0.3698 0.6593 0.0365 0.0205 0.437 3.061 2.647 325.885 0.346 11.776 3.685 0.47 162847. 0.2717
|
|
42.96 0.3893 0.6619 0.0329 0.0194 0.414 2.898 2.391 308.561 0.327 10.635 3.514 0.47 163071. 0.2462
|
|
45.11 0.4087 0.6591 0.0293 0.0182 0.389 2.723 2.130 289.933 0.308 9.476 3.333 0.47 163303. 0.2204
|
|
47.26 0.4282 0.6496 0.0257 0.0170 0.362 2.536 1.867 270.021 0.287 8.303 3.136 0.47 163543. 0.1941
|
|
49.40 0.4476 0.6318 0.0220 0.0156 0.334 2.337 1.601 248.855 0.264 7.119 2.917 0.47 163792. 0.1672
|
|
51.55 0.4671 0.6032 0.0184 0.0142 0.304 2.127 1.333 226.480 0.240 5.928 2.669 0.47 164049. 0.1396
|
|
53.70 0.4866 0.5599 0.0147 0.0127 0.272 1.906 1.064 202.957 0.215 4.734 2.378 0.47 164315. 0.1112
|
|
55.85 0.5060 0.4957 0.0110 0.0112 0.239 1.675 0.796 178.368 0.189 3.542 2.025 0.47 164589. 0.0819
|
|
58.00 0.5255 0.4000 0.0073 0.0096 0.205 1.435 0.530 152.819 0.162 2.358 1.573 0.47 164872. 0.0519
|
|
60.15 0.5450 0.2526 0.0037 0.0079 0.170 1.187 0.267 126.430 0.134 1.188 0.958 0.47 165162. 0.0224
|
|
62.29 0.5644 0.0077 0.0001 0.0062 0.133 0.931 0.006 99.094 0.105 0.028 0.028 0.47 165448. 0.0001
|
|
|
|
|
|
|
|
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 0.0861 0.0269 0.789 4.974 7.715 588.485 0.562 34.316 5.946 0.51 177794. 0.7484
|
|
2.39 0.0195 0.0608 0.0844 0.0271 0.794 5.003 7.567 591.906 0.565 33.660 5.799 0.51 177893. 0.7228
|
|
4.78 0.0390 0.1185 0.0827 0.0272 0.797 5.026 7.411 594.652 0.568 32.965 5.653 0.51 177999. 0.6973
|
|
7.17 0.0585 0.1731 0.0809 0.0273 0.800 5.043 7.246 596.619 0.570 32.230 5.509 0.51 178111. 0.6719
|
|
9.56 0.0780 0.2249 0.0789 0.0274 0.802 5.052 7.072 597.707 0.571 31.455 5.366 0.51 178230. 0.6466
|
|
11.95 0.0974 0.2738 0.0769 0.0274 0.802 5.053 6.888 597.816 0.571 30.637 5.226 0.51 178355. 0.6215
|
|
14.34 0.1169 0.3198 0.0747 0.0273 0.800 5.045 6.694 596.841 0.570 29.777 5.087 0.51 178488. 0.5964
|
|
16.73 0.1364 0.3631 0.0724 0.0272 0.797 5.026 6.491 594.683 0.568 28.873 4.951 0.51 178629. 0.5715
|
|
19.12 0.1559 0.4037 0.0701 0.0271 0.793 4.997 6.278 591.240 0.565 27.924 4.816 0.51 178777. 0.5468
|
|
21.51 0.1754 0.4416 0.0676 0.0268 0.786 4.957 6.054 586.415 0.560 26.930 4.683 0.51 178933. 0.5221
|
|
23.90 0.1949 0.4768 0.0650 0.0265 0.778 4.903 5.821 580.113 0.554 25.891 4.551 0.51 179096. 0.4975
|
|
26.29 0.2144 0.5095 0.0622 0.0262 0.767 4.837 5.577 572.244 0.546 24.807 4.421 0.51 179268. 0.4730
|
|
28.68 0.2339 0.5394 0.0594 0.0258 0.755 4.756 5.323 562.721 0.537 23.678 4.291 0.52 179448. 0.4486
|
|
31.07 0.2534 0.5668 0.0565 0.0252 0.740 4.661 5.059 551.456 0.527 22.503 4.161 0.52 179636. 0.4241
|
|
33.46 0.2728 0.5913 0.0534 0.0246 0.722 4.550 4.785 538.355 0.514 21.283 4.031 0.52 179833. 0.3996
|
|
35.85 0.2923 0.6130 0.0502 0.0240 0.702 4.424 4.501 523.373 0.500 20.020 3.901 0.52 180038. 0.3750
|
|
38.24 0.3118 0.6317 0.0470 0.0232 0.679 4.281 4.208 506.520 0.484 18.719 3.768 0.52 180252. 0.3503
|
|
40.63 0.3313 0.6472 0.0436 0.0223 0.654 4.123 3.908 487.811 0.466 17.382 3.633 0.52 180474. 0.3255
|
|
43.02 0.3508 0.6590 0.0402 0.0214 0.627 3.949 3.600 467.251 0.446 16.013 3.495 0.52 180706. 0.3004
|
|
45.41 0.3703 0.6669 0.0367 0.0204 0.597 3.760 3.286 444.846 0.425 14.616 3.350 0.52 180946. 0.2752
|
|
47.80 0.3898 0.6702 0.0331 0.0192 0.564 3.555 2.966 420.605 0.402 13.193 3.199 0.52 181196. 0.2496
|
|
50.19 0.4093 0.6681 0.0295 0.0181 0.529 3.335 2.641 394.544 0.377 11.749 3.036 0.52 181454. 0.2236
|
|
52.58 0.4288 0.6593 0.0258 0.0168 0.492 3.099 2.313 366.691 0.350 10.286 2.860 0.52 181722. 0.1971
|
|
54.97 0.4482 0.6422 0.0221 0.0154 0.452 2.849 1.981 337.091 0.322 8.810 2.665 0.52 181999. 0.1699
|
|
57.36 0.4677 0.6141 0.0184 0.0140 0.410 2.585 1.647 305.805 0.292 7.324 2.442 0.52 182286. 0.1420
|
|
59.75 0.4872 0.5711 0.0146 0.0125 0.366 2.307 1.312 272.922 0.261 5.836 2.180 0.52 182582. 0.1132
|
|
62.14 0.5067 0.5065 0.0109 0.0109 0.320 2.016 0.978 238.558 0.228 4.350 1.859 0.52 182887. 0.0833
|
|
64.53 0.5262 0.4087 0.0072 0.0093 0.272 1.715 0.646 202.862 0.194 2.874 1.445 0.52 183202. 0.0526
|
|
66.92 0.5457 0.2552 0.0036 0.0076 0.223 1.403 0.318 166.002 0.159 1.416 0.870 0.52 183526. 0.0222
|
|
69.31 0.5652 -0.0081 -0.0001 0.0058 0.171 1.079 -0.008 127.707 0.122 -0.033 -0.027 0.52 183839. 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 0.0868 0.0271 1.056 6.048 9.415 787.156 0.683 41.876 5.425 0.57 195563. 0.7542
|
|
2.63 0.0195 0.0610 0.0852 0.0272 1.062 6.083 9.235 791.725 0.687 41.078 5.291 0.57 195672. 0.7285
|
|
5.26 0.0390 0.1189 0.0834 0.0273 1.067 6.112 9.045 795.376 0.690 40.232 5.158 0.57 195789. 0.7029
|
|
7.89 0.0585 0.1738 0.0816 0.0274 1.070 6.131 8.844 797.968 0.693 39.337 5.027 0.57 195913. 0.6774
|
|
10.51 0.0779 0.2257 0.0796 0.0275 1.072 6.142 8.631 799.367 0.694 38.392 4.898 0.57 196044. 0.6520
|
|
13.14 0.0974 0.2748 0.0775 0.0275 1.072 6.143 8.407 799.437 0.694 37.397 4.770 0.57 196183. 0.6267
|
|
15.77 0.1169 0.3211 0.0754 0.0274 1.070 6.132 8.172 798.040 0.693 36.348 4.644 0.57 196330. 0.6016
|
|
18.40 0.1364 0.3646 0.0731 0.0273 1.066 6.109 7.924 795.039 0.690 35.246 4.521 0.57 196484. 0.5766
|
|
21.03 0.1559 0.4055 0.0707 0.0272 1.060 6.073 7.664 790.298 0.686 34.089 4.398 0.57 196648. 0.5517
|
|
23.66 0.1754 0.4436 0.0682 0.0269 1.051 6.022 7.391 783.688 0.680 32.877 4.278 0.57 196820. 0.5270
|
|
26.28 0.1949 0.4792 0.0655 0.0266 1.039 5.956 7.106 775.080 0.673 31.609 4.159 0.57 197000. 0.5023
|
|
28.91 0.2143 0.5122 0.0628 0.0263 1.025 5.873 6.809 764.353 0.664 30.287 4.041 0.57 197189. 0.4777
|
|
31.54 0.2338 0.5425 0.0599 0.0258 1.008 5.774 6.499 751.392 0.652 28.908 3.923 0.57 197388. 0.4532
|
|
34.17 0.2533 0.5702 0.0570 0.0253 0.987 5.656 6.177 736.078 0.639 27.475 3.806 0.57 197595. 0.4286
|
|
36.80 0.2728 0.5951 0.0539 0.0247 0.963 5.519 5.842 718.287 0.624 25.986 3.689 0.57 197812. 0.4040
|
|
39.43 0.2923 0.6173 0.0507 0.0240 0.936 5.363 5.496 697.954 0.606 24.445 3.571 0.57 198038. 0.3794
|
|
42.06 0.3118 0.6365 0.0474 0.0232 0.905 5.187 5.138 675.094 0.586 22.855 3.452 0.57 198274. 0.3546
|
|
44.68 0.3313 0.6525 0.0440 0.0223 0.871 4.992 4.771 649.726 0.564 21.223 3.331 0.57 198519. 0.3297
|
|
47.31 0.3507 0.6650 0.0405 0.0214 0.834 4.778 4.396 621.859 0.540 19.552 3.206 0.57 198774. 0.3046
|
|
49.94 0.3702 0.6735 0.0370 0.0203 0.793 4.545 4.012 591.499 0.513 17.845 3.076 0.57 199039. 0.2792
|
|
52.57 0.3897 0.6776 0.0334 0.0192 0.749 4.293 3.621 558.660 0.485 16.108 2.940 0.57 199313. 0.2535
|
|
55.20 0.4092 0.6763 0.0297 0.0180 0.702 4.021 3.225 523.363 0.454 14.344 2.795 0.57 199598. 0.2274
|
|
57.83 0.4287 0.6684 0.0260 0.0167 0.651 3.732 2.823 485.648 0.422 12.557 2.637 0.57 199893. 0.2007
|
|
60.45 0.4482 0.6523 0.0223 0.0153 0.598 3.424 2.418 445.573 0.387 10.754 2.461 0.57 200198. 0.1734
|
|
63.08 0.4677 0.6252 0.0185 0.0139 0.541 3.098 2.010 403.223 0.350 8.939 2.261 0.57 200513. 0.1452
|
|
65.71 0.4871 0.5831 0.0148 0.0123 0.481 2.756 1.601 358.718 0.311 7.120 2.024 0.57 200839. 0.1160
|
|
68.34 0.5066 0.5191 0.0110 0.0107 0.419 2.399 1.193 312.214 0.271 5.305 1.733 0.57 201175. 0.0857
|
|
70.97 0.5261 0.4210 0.0073 0.0091 0.354 2.028 0.787 263.915 0.229 3.502 1.353 0.57 201521. 0.0544
|
|
73.60 0.5456 0.2644 0.0036 0.0074 0.287 1.645 0.387 214.050 0.186 1.720 0.820 0.57 201877. 0.0231
|
|
76.23 0.5651 -0.0111 -0.0001 0.0056 0.218 1.246 -0.012 162.193 0.141 -0.053 -0.033 0.57 202220. 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 0.0877 0.0273 1.381 7.253 11.313 1029.744 0.819 50.319 4.983 0.62 213327. 0.7594
|
|
2.87 0.0195 0.0611 0.0860 0.0274 1.389 7.295 11.098 1035.687 0.824 49.362 4.860 0.62 213448. 0.7336
|
|
5.73 0.0390 0.1191 0.0842 0.0276 1.395 7.328 10.870 1040.407 0.828 48.349 4.739 0.62 213575. 0.7079
|
|
8.60 0.0585 0.1742 0.0824 0.0276 1.400 7.351 10.629 1043.721 0.831 47.276 4.619 0.62 213711. 0.6823
|
|
11.47 0.0779 0.2263 0.0804 0.0277 1.402 7.364 10.374 1045.451 0.832 46.144 4.501 0.62 213855. 0.6569
|
|
14.34 0.0974 0.2756 0.0783 0.0277 1.402 7.363 10.105 1045.419 0.832 44.949 4.384 0.62 214007. 0.6315
|
|
17.20 0.1169 0.3220 0.0761 0.0276 1.399 7.349 9.823 1043.439 0.830 43.691 4.270 0.62 214168. 0.6063
|
|
20.07 0.1364 0.3657 0.0738 0.0275 1.394 7.321 9.525 1039.335 0.827 42.367 4.157 0.62 214338. 0.5813
|
|
22.94 0.1559 0.4068 0.0714 0.0274 1.385 7.275 9.213 1032.932 0.822 40.978 4.045 0.62 214517. 0.5564
|
|
25.80 0.1754 0.4452 0.0689 0.0271 1.373 7.213 8.885 1024.056 0.815 39.523 3.936 0.62 214705. 0.5316
|
|
28.67 0.1948 0.4810 0.0662 0.0268 1.358 7.132 8.543 1012.540 0.806 38.000 3.827 0.62 214902. 0.5068
|
|
31.54 0.2143 0.5143 0.0634 0.0264 1.339 7.031 8.186 998.224 0.794 36.411 3.719 0.62 215109. 0.4822
|
|
34.41 0.2338 0.5449 0.0605 0.0260 1.315 6.909 7.814 980.959 0.781 34.755 3.613 0.62 215326. 0.4576
|
|
37.27 0.2533 0.5730 0.0575 0.0254 1.288 6.766 7.426 960.592 0.764 33.032 3.506 0.62 215553. 0.4330
|
|
40.14 0.2728 0.5984 0.0544 0.0248 1.256 6.600 7.024 936.959 0.746 31.242 3.400 0.62 215790. 0.4083
|
|
43.01 0.2923 0.6209 0.0512 0.0241 1.220 6.409 6.607 909.973 0.724 29.389 3.293 0.62 216038. 0.3836
|
|
45.88 0.3117 0.6406 0.0479 0.0233 1.180 6.196 6.177 879.654 0.700 27.477 3.185 0.62 216295. 0.3587
|
|
48.74 0.3312 0.6571 0.0444 0.0224 1.135 5.959 5.736 846.026 0.673 25.514 3.075 0.62 216563. 0.3337
|
|
51.61 0.3507 0.6702 0.0409 0.0214 1.085 5.699 5.284 809.103 0.644 23.504 2.962 0.62 216842. 0.3085
|
|
54.48 0.3702 0.6794 0.0374 0.0204 1.031 5.416 4.823 768.894 0.612 21.451 2.845 0.62 217131. 0.2831
|
|
57.34 0.3897 0.6842 0.0337 0.0192 0.973 5.110 4.353 725.417 0.577 19.361 2.722 0.62 217431. 0.2573
|
|
60.21 0.4092 0.6837 0.0300 0.0180 0.910 4.780 3.876 678.704 0.540 17.238 2.590 0.62 217741. 0.2310
|
|
63.08 0.4287 0.6767 0.0263 0.0167 0.843 4.429 3.392 628.802 0.500 15.089 2.447 0.62 218063. 0.2042
|
|
65.95 0.4481 0.6614 0.0225 0.0152 0.772 4.056 2.904 575.792 0.458 12.919 2.288 0.62 218396. 0.1767
|
|
68.81 0.4676 0.6353 0.0187 0.0138 0.697 3.661 2.413 519.787 0.414 10.735 2.106 0.62 218740. 0.1482
|
|
71.68 0.4871 0.5941 0.0149 0.0122 0.618 3.247 1.921 460.943 0.367 8.545 1.890 0.62 219096. 0.1187
|
|
74.55 0.5066 0.5306 0.0111 0.0106 0.536 2.814 1.430 399.470 0.318 6.360 1.624 0.62 219463. 0.0880
|
|
77.41 0.5261 0.4320 0.0073 0.0089 0.450 2.364 0.942 335.637 0.267 4.190 1.273 0.63 219840. 0.0560
|
|
80.28 0.5456 0.2722 0.0036 0.0071 0.362 1.900 0.460 269.747 0.215 2.046 0.773 0.63 220228. 0.0238
|
|
83.15 0.5650 -0.0172 -0.0002 0.0053 0.270 1.417 -0.021 201.114 0.160 -0.093 -0.047 0.63 220599. 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 0.0886 0.0276 1.774 8.601 13.423 1322.906 0.972 59.705 4.602 0.67 231088. 0.7640
|
|
3.14 0.0197 0.0618 0.0869 0.0277 1.784 8.651 13.166 1330.536 0.977 58.561 4.488 0.67 231220. 0.7379
|
|
6.28 0.0394 0.1205 0.0851 0.0278 1.792 8.690 12.893 1336.529 0.982 57.348 4.375 0.67 231361. 0.7119
|
|
9.42 0.0591 0.1761 0.0832 0.0279 1.798 8.716 12.604 1340.641 0.985 56.063 4.264 0.67 231511. 0.6860
|
|
12.56 0.0788 0.2288 0.0812 0.0280 1.801 8.729 12.299 1342.633 0.986 54.704 4.155 0.67 231669. 0.6602
|
|
15.70 0.0985 0.2786 0.0791 0.0280 1.800 8.727 11.976 1342.265 0.986 53.270 4.047 0.67 231837. 0.6346
|
|
18.84 0.1182 0.3256 0.0768 0.0279 1.796 8.708 11.636 1339.297 0.984 51.758 3.941 0.67 232015. 0.6091
|
|
21.99 0.1379 0.3697 0.0745 0.0278 1.788 8.670 11.278 1333.488 0.980 50.166 3.836 0.67 232203. 0.5838
|
|
25.13 0.1576 0.4112 0.0720 0.0276 1.776 8.612 10.903 1324.606 0.973 48.494 3.733 0.67 232400. 0.5585
|
|
28.27 0.1773 0.4500 0.0694 0.0273 1.760 8.533 10.508 1312.421 0.964 46.741 3.632 0.67 232608. 0.5334
|
|
31.41 0.1970 0.4862 0.0667 0.0270 1.739 8.431 10.096 1296.715 0.953 44.906 3.531 0.67 232827. 0.5084
|
|
34.55 0.2167 0.5198 0.0638 0.0266 1.713 8.305 9.665 1277.278 0.938 42.990 3.432 0.67 233056. 0.4835
|
|
37.69 0.2364 0.5508 0.0609 0.0261 1.682 8.153 9.216 1253.912 0.921 40.992 3.334 0.67 233296. 0.4585
|
|
40.83 0.2561 0.5791 0.0578 0.0255 1.645 7.974 8.748 1226.415 0.901 38.913 3.235 0.67 233546. 0.4336
|
|
43.97 0.2758 0.6048 0.0546 0.0249 1.602 7.767 8.263 1194.571 0.877 36.753 3.137 0.67 233808. 0.4086
|
|
47.11 0.2955 0.6276 0.0512 0.0241 1.553 7.531 7.760 1158.294 0.851 34.515 3.039 0.67 234082. 0.3835
|
|
50.25 0.3152 0.6474 0.0478 0.0233 1.499 7.266 7.241 1117.615 0.821 32.208 2.939 0.67 234366. 0.3583
|
|
53.39 0.3349 0.6640 0.0443 0.0223 1.438 6.974 6.708 1072.566 0.788 29.839 2.837 0.67 234663. 0.3329
|
|
56.53 0.3546 0.6771 0.0407 0.0213 1.372 6.652 6.163 1023.164 0.752 27.414 2.732 0.67 234971. 0.3073
|
|
59.67 0.3743 0.6862 0.0370 0.0202 1.300 6.303 5.607 969.426 0.712 24.938 2.623 0.67 235290. 0.2814
|
|
62.81 0.3940 0.6907 0.0333 0.0190 1.222 5.926 5.040 911.377 0.669 22.417 2.508 0.67 235622. 0.2551
|
|
65.96 0.4137 0.6896 0.0295 0.0177 1.139 5.520 4.464 849.066 0.624 19.858 2.385 0.67 235966. 0.2283
|
|
69.10 0.4334 0.6816 0.0256 0.0163 1.049 5.088 3.882 782.569 0.575 17.268 2.250 0.67 236321. 0.2009
|
|
72.24 0.4531 0.6646 0.0218 0.0148 0.955 4.629 3.294 712.000 0.523 14.654 2.099 0.67 236689. 0.1726
|
|
75.38 0.4728 0.6356 0.0179 0.0133 0.855 4.145 2.704 637.528 0.468 12.025 1.923 0.68 237070. 0.1433
|
|
78.52 0.4925 0.5894 0.0139 0.0117 0.750 3.637 2.112 559.383 0.411 9.393 1.712 0.68 237463. 0.1127
|
|
81.66 0.5122 0.5171 0.0100 0.0100 0.641 3.107 1.522 477.875 0.351 6.769 1.444 0.68 237868. 0.0807
|
|
84.80 0.5319 0.4016 0.0062 0.0082 0.528 2.558 0.937 393.401 0.289 4.167 1.080 0.68 238286. 0.0474
|
|
87.94 0.5516 0.2053 0.0024 0.0064 0.411 1.992 0.360 306.353 0.225 1.600 0.532 0.68 238713. 0.0145
|
|
91.08 0.5713
|
|
|
|
|
|
|
|
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 0.0897 0.0279 2.246 10.111 15.762 1674.814 1.142 70.111 4.269 0.72 248842. 0.7679
|
|
3.34 0.0194 0.0610 0.0881 0.0281 2.259 10.168 15.466 1684.172 1.149 68.793 4.165 0.72 248984. 0.7422
|
|
6.68 0.0389 0.1189 0.0863 0.0282 2.268 10.212 15.152 1691.496 1.154 67.394 4.063 0.72 249134. 0.7166
|
|
10.02 0.0583 0.1740 0.0844 0.0283 2.275 10.242 14.819 1696.474 1.157 65.913 3.962 0.72 249294. 0.6911
|
|
13.35 0.0778 0.2261 0.0824 0.0283 2.278 10.256 14.466 1698.813 1.159 64.347 3.862 0.72 249463. 0.6657
|
|
16.69 0.0972 0.2755 0.0802 0.0283 2.277 10.253 14.095 1698.217 1.158 62.693 3.764 0.72 249643. 0.6404
|
|
20.03 0.1167 0.3221 0.0780 0.0283 2.272 10.230 13.703 1694.393 1.156 60.950 3.668 0.72 249832. 0.6152
|
|
23.37 0.1361 0.3661 0.0757 0.0281 2.262 10.185 13.290 1687.049 1.151 59.116 3.573 0.72 250031. 0.5902
|
|
26.71 0.1556 0.4074 0.0732 0.0279 2.247 10.118 12.857 1675.896 1.143 57.189 3.480 0.72 250242. 0.5654
|
|
30.05 0.1750 0.4462 0.0706 0.0277 2.227 10.026 12.403 1660.667 1.133 55.168 3.388 0.72 250462. 0.5406
|
|
33.38 0.1945 0.4825 0.0679 0.0274 2.201 9.908 11.928 1641.086 1.119 53.054 3.297 0.72 250694. 0.5159
|
|
36.72 0.2139 0.5162 0.0651 0.0270 2.168 9.762 11.431 1616.901 1.103 50.845 3.207 0.72 250937. 0.4912
|
|
40.06 0.2333 0.5475 0.0621 0.0265 2.129 9.586 10.913 1587.870 1.083 48.543 3.117 0.72 251191. 0.4666
|
|
43.40 0.2528 0.5762 0.0591 0.0259 2.084 9.381 10.375 1553.758 1.060 46.147 3.029 0.72 251457. 0.4420
|
|
46.74 0.2722 0.6024 0.0559 0.0253 2.031 9.142 9.815 1514.304 1.033 43.657 2.940 0.72 251735. 0.4173
|
|
50.08 0.2917 0.6258 0.0526 0.0245 1.970 8.871 9.235 1469.353 1.002 41.078 2.851 0.72 252024. 0.3925
|
|
53.42 0.3111 0.6465 0.0492 0.0237 1.903 8.567 8.637 1418.933 0.968 38.416 2.761 0.72 252325. 0.3676
|
|
56.75 0.3306 0.6641 0.0457 0.0227 1.828 8.229 8.022 1363.093 0.930 35.681 2.669 0.72 252638. 0.3426
|
|
60.09 0.3500 0.6785 0.0421 0.0217 1.746 7.860 7.392 1301.859 0.888 32.880 2.575 0.72 252963. 0.3173
|
|
63.43 0.3695 0.6891 0.0384 0.0206 1.657 7.458 6.749 1235.259 0.843 30.018 2.478 0.72 253300. 0.2917
|
|
66.77 0.3889 0.6954 0.0347 0.0194 1.560 7.023 6.093 1163.334 0.794 27.103 2.376 0.72 253650. 0.2657
|
|
70.11 0.4084 0.6966 0.0309 0.0181 1.457 6.557 5.428 1086.151 0.741 24.142 2.267 0.73 254013. 0.2393
|
|
73.45 0.4278 0.6915 0.0271 0.0167 1.346 6.060 4.753 1003.819 0.685 21.142 2.148 0.73 254388. 0.2122
|
|
76.78 0.4473 0.6783 0.0232 0.0153 1.229 5.533 4.072 916.494 0.625 18.111 2.015 0.73 254776. 0.1842
|
|
80.12 0.4667 0.6544 0.0193 0.0137 1.106 4.977 3.386 824.403 0.562 15.061 1.863 0.73 255176. 0.1553
|
|
83.46 0.4861 0.6152 0.0154 0.0121 0.976 4.394 2.698 727.854 0.496 12.002 1.681 0.73 255590. 0.1251
|
|
86.80 0.5056 0.5534 0.0115 0.0105 0.841 3.787 2.011 627.253 0.428 8.946 1.454 0.73 256017. 0.0935
|
|
90.14 0.5250 0.4553 0.0076 0.0087 0.702 3.158 1.329 523.120 0.357 5.910 1.152 0.73 256456. 0.0602
|
|
93.48 0.5445 0.2922 0.0037 0.0069 0.558 2.512 0.654 416.046 0.284 2.909 0.713 0.73 256908. 0.0261
|
|
96.82 0.5639 -0.0118 -0.0001 0.0051 0.409 1.841 -0.019 305.018 0.208 -0.083 -0.028 0.73 257340. 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 0.0910 0.0285 2.821 11.854 18.353 2103.700 1.339 81.636 3.957 0.77 266589. 0.7681
|
|
3.60 0.0195 0.0609 0.0893 0.0287 2.834 11.909 18.009 2113.388 1.345 80.103 3.865 0.77 266743. 0.7432
|
|
7.19 0.0391 0.1190 0.0875 0.0288 2.844 11.950 17.642 2120.695 1.350 78.473 3.773 0.77 266907. 0.7181
|
|
10.79 0.0586 0.1741 0.0856 0.0288 2.850 11.975 17.254 2125.244 1.353 76.746 3.682 0.77 267080. 0.6931
|
|
14.38 0.0782 0.2265 0.0835 0.0288 2.852 11.983 16.843 2126.647 1.354 74.918 3.592 0.77 267264. 0.6680
|
|
17.98 0.0977 0.2761 0.0814 0.0288 2.849 11.971 16.409 2124.512 1.353 72.986 3.503 0.77 267459. 0.6430
|
|
21.57 0.1173 0.3230 0.0791 0.0287 2.841 11.937 15.951 2118.443 1.349 70.948 3.415 0.77 267664. 0.6180
|
|
25.17 0.1368 0.3672 0.0767 0.0286 2.827 11.878 15.468 2108.033 1.342 68.801 3.328 0.77 267881. 0.5931
|
|
28.77 0.1564 0.4089 0.0742 0.0284 2.807 11.793 14.960 2092.894 1.332 66.544 3.242 0.77 268109. 0.5682
|
|
32.36 0.1759 0.4479 0.0716 0.0281 2.779 11.679 14.428 2072.641 1.319 64.176 3.157 0.77 268349. 0.5434
|
|
35.96 0.1955 0.4845 0.0688 0.0278 2.745 11.534 13.871 2046.905 1.303 61.696 3.074 0.77 268600. 0.5187
|
|
39.55 0.2150 0.5186 0.0659 0.0273 2.703 11.356 13.288 2015.335 1.283 59.104 2.991 0.77 268864. 0.4940
|
|
43.15 0.2346 0.5501 0.0629 0.0268 2.652 11.144 12.680 1977.612 1.259 56.402 2.908 0.77 269140. 0.4692
|
|
46.74 0.2541 0.5792 0.0597 0.0262 2.593 10.895 12.048 1933.443 1.231 53.588 2.826 0.77 269428. 0.4445
|
|
50.34 0.2737 0.6056 0.0565 0.0255 2.524 10.608 11.390 1882.513 1.198 50.664 2.744 0.77 269729. 0.4197
|
|
53.94 0.2932 0.6294 0.0531 0.0247 2.447 10.282 10.709 1824.658 1.162 47.632 2.662 0.77 270042. 0.3947
|
|
57.53 0.3128 0.6504 0.0496 0.0239 2.360 9.917 10.006 1759.955 1.120 44.505 2.579 0.77 270369. 0.3696
|
|
61.13 0.3323 0.6682 0.0460 0.0229 2.264 9.514 9.283 1688.503 1.075 41.290 2.494 0.77 270708. 0.3443
|
|
64.72 0.3519 0.6827 0.0424 0.0218 2.160 9.074 8.543 1610.380 1.025 37.997 2.406 0.78 271060. 0.3186
|
|
68.32 0.3714 0.6933 0.0386 0.0207 2.046 8.597 7.786 1525.679 0.971 34.634 2.315 0.78 271426. 0.2927
|
|
71.91 0.3910 0.6994 0.0348 0.0195 1.924 8.083 7.016 1434.513 0.913 31.207 2.218 0.78 271805. 0.2662
|
|
75.51 0.4105 0.7000 0.0309 0.0181 1.793 7.534 6.233 1337.056 0.851 27.725 2.114 0.78 272198. 0.2392
|
|
79.11 0.4301 0.6937 0.0270 0.0167 1.654 6.951 5.440 1233.531 0.785 24.198 2.000 0.78 272604. 0.2114
|
|
82.70 0.4496 0.6786 0.0230 0.0152 1.508 6.335 4.639 1124.252 0.716 20.636 1.872 0.78 273024. 0.1827
|
|
86.30 0.4692 0.6515 0.0190 0.0137 1.354 5.689 3.833 1009.632 0.643 17.049 1.722 0.78 273457. 0.1528
|
|
89.89 0.4887 0.6073 0.0150 0.0121 1.194 5.016 3.025 890.198 0.567 13.453 1.541 0.78 273905. 0.1214
|
|
93.49 0.5082 0.5377 0.0110 0.0104 1.028 4.320 2.217 766.616 0.488 9.863 1.312 0.78 274367. 0.0885
|
|
97.08 0.5278 0.4272 0.0070 0.0087 0.858 3.605 1.416 639.688 0.407 6.297 1.004 0.78 274843. 0.0541
|
|
100.68 0.5473 0.2445 0.0031 0.0069 0.684 2.875 0.623 510.262 0.325 2.772 0.554 0.78 275330. 0.0198
|
|
104.28 0.5669
|
|
|
|
|
|
|
|
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 0.0925 0.0298 3.580 14.104 21.222 2669.889 1.593 94.395 3.605 0.82 284327. 0.7526
|
|
3.84 0.0196 0.0595 0.0908 0.0299 3.586 14.127 20.826 2674.261 1.596 92.635 3.532 0.82 284493. 0.7304
|
|
7.69 0.0392 0.1166 0.0889 0.0299 3.588 14.136 20.405 2675.895 1.597 90.762 3.459 0.82 284670. 0.7079
|
|
11.53 0.0588 0.1711 0.0870 0.0299 3.586 14.128 19.958 2674.375 1.596 88.773 3.385 0.82 284857. 0.6852
|
|
15.38 0.0784 0.2232 0.0849 0.0298 3.580 14.101 19.484 2669.284 1.593 86.666 3.311 0.82 285055. 0.6622
|
|
19.22 0.0980 0.2727 0.0827 0.0297 3.567 14.053 18.983 2660.182 1.588 84.437 3.237 0.82 285265. 0.6390
|
|
23.06 0.1176 0.3198 0.0804 0.0296 3.549 13.981 18.454 2646.617 1.580 82.083 3.163 0.82 285486. 0.6156
|
|
26.91 0.1371 0.3643 0.0780 0.0294 3.524 13.883 17.896 2628.120 1.569 79.601 3.089 0.82 285720. 0.5920
|
|
30.75 0.1567 0.4064 0.0754 0.0291 3.492 13.757 17.309 2604.231 1.554 76.990 3.015 0.82 285966. 0.5683
|
|
34.60 0.1763 0.4460 0.0728 0.0288 3.452 13.600 16.692 2574.487 1.537 74.247 2.941 0.82 286224. 0.5444
|
|
38.44 0.1959 0.4832 0.0699 0.0284 3.404 13.410 16.046 2538.424 1.515 71.373 2.867 0.82 286495. 0.5204
|
|
42.29 0.2155 0.5179 0.0670 0.0279 3.347 13.183 15.371 2495.605 1.489 68.368 2.794 0.82 286779. 0.4963
|
|
46.13 0.2351 0.5500 0.0639 0.0273 3.280 12.920 14.666 2445.779 1.460 65.232 2.720 0.82 287076. 0.4719
|
|
49.97 0.2547 0.5795 0.0607 0.0267 3.203 12.619 13.931 2388.795 1.426 61.966 2.645 0.82 287386. 0.4474
|
|
53.82 0.2743 0.6062 0.0574 0.0260 3.117 12.279 13.168 2324.418 1.387 58.570 2.569 0.83 287710. 0.4225
|
|
57.66 0.2939 0.6301 0.0539 0.0252 3.020 11.897 12.376 2252.081 1.344 55.048 2.493 0.83 288047. 0.3973
|
|
61.51 0.3135 0.6509 0.0504 0.0243 2.912 11.473 11.559 2171.819 1.296 51.414 2.414 0.83 288397. 0.3719
|
|
65.35 0.3331 0.6684 0.0467 0.0233 2.794 11.008 10.719 2083.755 1.244 47.677 2.333 0.83 288762. 0.3461
|
|
69.19 0.3527 0.6823 0.0430 0.0222 2.666 10.502 9.858 1988.050 1.187 43.848 2.249 0.83 289140. 0.3200
|
|
73.04 0.3723 0.6918 0.0391 0.0211 2.528 9.957 8.979 1884.900 1.125 39.936 2.161 0.83 289533. 0.2933
|
|
76.88 0.3918 0.6963 0.0352 0.0198 2.380 9.375 8.082 1774.610 1.059 35.950 2.066 0.83 289940. 0.2661
|
|
80.73 0.4114 0.6945 0.0313 0.0185 2.223 8.756 7.172 1657.595 0.989 31.900 1.962 0.83 290361. 0.2381
|
|
84.57 0.4310 0.6849 0.0272 0.0171 2.058 8.105 6.249 1534.300 0.916 27.795 1.847 0.83 290796. 0.2092
|
|
88.42 0.4506 0.6651 0.0232 0.0157 1.885 7.424 5.317 1405.289 0.839 23.648 1.716 0.83 291247. 0.1793
|
|
92.26 0.4702 0.6318 0.0191 0.0142 1.705 6.716 4.378 1271.264 0.759 19.473 1.562 0.83 291712. 0.1481
|
|
96.10 0.4898 0.5796 0.0150 0.0127 1.519 5.986 3.437 1133.077 0.676 15.286 1.376 0.83 292192. 0.1156
|
|
99.95 0.5094 0.5003 0.0109 0.0111 1.330 5.239 2.497 991.722 0.592 11.105 1.142 0.83 292687. 0.0818
|
|
103.79 0.5290 0.3803 0.0068 0.0095 1.138 4.482 1.563 848.363 0.506 6.953 0.836 0.83 293196. 0.0473
|
|
107.64 0.5486 0.1947 0.0028 0.0079 0.944 3.719 0.641 704.070 0.420 2.849 0.413 0.83 293718. 0.0150
|
|
111.48 0.5682
|
|
|
|
|
|
|
|
PROP RPM = 17000
|
|
|
|
V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
|
|
(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
|
|
0.00 0.0000 0.0000 0.0941 0.0325 4.680 17.350 24.369 3489.570 1.960 108.395 3.167 0.87 302056. 0.7085
|
|
4.08 0.0196 0.0558 0.0924 0.0324 4.665 17.297 23.923 3478.972 1.954 106.409 3.119 0.87 302234. 0.6912
|
|
8.17 0.0392 0.1099 0.0905 0.0323 4.647 17.227 23.447 3464.943 1.946 104.290 3.069 0.87 302423. 0.6734
|
|
12.25 0.0588 0.1621 0.0886 0.0321 4.623 17.139 22.940 3447.096 1.936 102.038 3.018 0.87 302623. 0.6551
|
|
16.34 0.0784 0.2125 0.0865 0.0319 4.593 17.029 22.403 3425.014 1.924 99.647 2.967 0.87 302836. 0.6363
|
|
20.42 0.0980 0.2609 0.0843 0.0317 4.557 16.896 21.833 3398.281 1.909 97.113 2.914 0.87 303060. 0.6170
|
|
24.50 0.1175 0.3073 0.0820 0.0314 4.515 16.738 21.230 3366.466 1.891 94.432 2.860 0.87 303298. 0.5972
|
|
28.59 0.1371 0.3516 0.0795 0.0310 4.464 16.552 20.594 3329.143 1.870 91.603 2.806 0.87 303548. 0.5769
|
|
32.67 0.1567 0.3939 0.0769 0.0306 4.406 16.337 19.924 3285.860 1.846 88.623 2.750 0.87 303811. 0.5563
|
|
36.76 0.1763 0.4341 0.0742 0.0301 4.340 16.090 19.220 3236.173 1.818 85.490 2.694 0.87 304087. 0.5351
|
|
40.84 0.1959 0.4720 0.0714 0.0296 4.264 15.809 18.481 3179.616 1.786 82.205 2.636 0.87 304377. 0.5135
|
|
44.92 0.2155 0.5077 0.0684 0.0290 4.178 15.491 17.708 3115.722 1.750 78.767 2.578 0.88 304681. 0.4915
|
|
49.01 0.2351 0.5411 0.0653 0.0284 4.082 15.135 16.901 3044.025 1.710 75.177 2.518 0.88 304998. 0.4691
|
|
53.09 0.2547 0.5718 0.0620 0.0276 3.976 14.741 16.060 2964.912 1.665 71.436 2.457 0.88 305329. 0.4461
|
|
57.18 0.2743 0.5996 0.0586 0.0268 3.861 14.315 15.185 2879.273 1.617 67.543 2.392 0.88 305675. 0.4224
|
|
61.26 0.2939 0.6239 0.0551 0.0260 3.738 13.859 14.277 2787.550 1.566 63.503 2.323 0.88 306035. 0.3977
|
|
65.34 0.3134 0.6445 0.0515 0.0250 3.606 13.369 13.339 2688.967 1.510 59.331 2.250 0.88 306409. 0.3723
|
|
69.43 0.3330 0.6607 0.0478 0.0241 3.467 12.855 12.374 2585.513 1.452 55.038 2.171 0.88 306798. 0.3460
|
|
73.51 0.3526 0.6723 0.0440 0.0231 3.319 12.306 11.384 2475.079 1.390 50.637 2.086 0.88 307201. 0.3189
|
|
77.60 0.3722 0.6790 0.0401 0.0220 3.161 11.720 10.373 2357.251 1.324 46.139 1.996 0.88 307619. 0.2913
|
|
81.68 0.3918 0.6797 0.0361 0.0208 2.994 11.100 9.342 2232.528 1.254 41.555 1.898 0.88 308053. 0.2629
|
|
85.76 0.4114 0.6731 0.0320 0.0196 2.818 10.449 8.295 2101.596 1.181 36.897 1.790 0.88 308501. 0.2336
|
|
89.85 0.4310 0.6576 0.0279 0.0183 2.636 9.772 7.234 1965.412 1.104 32.177 1.669 0.88 308965. 0.2035
|
|
93.93 0.4506 0.6307 0.0238 0.0170 2.447 9.073 6.162 1824.775 1.025 27.409 1.532 0.88 309444. 0.1723
|
|
98.01 0.4702 0.5894 0.0196 0.0157 2.254 8.356 5.083 1680.688 0.944 22.610 1.372 0.88 309938. 0.1401
|
|
102.10 0.4898 0.5294 0.0154 0.0143 2.058 7.629 4.001 1534.321 0.862 17.797 1.183 0.88 310449. 0.1072
|
|
106.18 0.5093 0.4447 0.0113 0.0129 1.860 6.896 2.921 1387.023 0.779 12.994 0.955 0.88 310975. 0.0740
|
|
110.27 0.5289 0.3269 0.0071 0.0116 1.663 6.166 1.849 1240.164 0.697 8.225 0.676 0.89 311517. 0.0417
|
|
114.35 0.5485 0.1641 0.0031 0.0102 1.468 5.444 0.790 1094.886 0.615 3.515 0.327 0.89 312072. 0.0132
|
|
118.43 0.5681
|
|
|
|
|
|
|
|
PROP RPM = 18000
|
|
|
|
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 0.0954 0.0369 6.299 22.056 27.689 4697.135 2.492 123.161 2.674 0.92 319787. 0.6375
|
|
4.31 0.0195 0.0500 0.0937 0.0366 6.255 21.901 27.203 4664.148 2.474 120.998 2.645 0.92 319975. 0.6252
|
|
8.63 0.0391 0.0990 0.0919 0.0363 6.203 21.721 26.682 4625.689 2.454 118.680 2.616 0.92 320175. 0.6123
|
|
12.94 0.0586 0.1467 0.0900 0.0360 6.144 21.514 26.125 4581.548 2.431 116.206 2.586 0.92 320387. 0.5990
|
|
17.26 0.0782 0.1933 0.0879 0.0356 6.077 21.278 25.533 4531.462 2.404 113.569 2.556 0.92 320612. 0.5851
|
|
21.57 0.0977 0.2387 0.0858 0.0351 6.001 21.014 24.902 4475.163 2.374 110.765 2.524 0.93 320850. 0.5707
|
|
25.88 0.1173 0.2827 0.0835 0.0346 5.917 20.719 24.234 4412.389 2.341 107.791 2.491 0.93 321102. 0.5557
|
|
30.20 0.1368 0.3253 0.0810 0.0341 5.824 20.393 23.526 4342.836 2.304 104.643 2.457 0.93 321367. 0.5400
|
|
34.51 0.1563 0.3664 0.0785 0.0335 5.721 20.033 22.778 4266.194 2.263 101.318 2.422 0.93 321646. 0.5237
|
|
38.82 0.1759 0.4059 0.0757 0.0328 5.608 19.638 21.991 4182.122 2.219 97.816 2.385 0.93 321939. 0.5068
|
|
43.14 0.1954 0.4438 0.0729 0.0321 5.485 19.206 21.164 4090.240 2.170 94.135 2.347 0.93 322247. 0.4892
|
|
47.45 0.2150 0.4799 0.0699 0.0313 5.351 18.736 20.296 3990.141 2.117 90.276 2.307 0.93 322569. 0.4709
|
|
51.77 0.2345 0.5142 0.0668 0.0305 5.205 18.226 19.388 3881.430 2.059 86.238 2.266 0.93 322905. 0.4520
|
|
56.08 0.2541 0.5463 0.0635 0.0295 5.047 17.674 18.441 3763.823 1.997 82.026 2.222 0.93 323257. 0.4324
|
|
60.39 0.2736 0.5759 0.0601 0.0286 4.881 17.090 17.455 3639.430 1.931 77.638 2.175 0.93 323623. 0.4118
|
|
64.71 0.2931 0.6020 0.0566 0.0276 4.709 16.489 16.430 3511.434 1.863 73.079 2.122 0.93 324004. 0.3898
|
|
69.02 0.3127 0.6236 0.0529 0.0265 4.536 15.882 15.369 3382.350 1.794 68.364 2.061 0.93 324401. 0.3661
|
|
73.33 0.3322 0.6402 0.0492 0.0255 4.361 15.270 14.278 3251.896 1.725 63.508 1.991 0.93 324812. 0.3410
|
|
77.65 0.3518 0.6484 0.0453 0.0246 4.201 14.710 13.156 3132.689 1.662 58.519 1.905 0.93 325239. 0.3131
|
|
81.96 0.3713 0.6504 0.0414 0.0236 4.036 14.132 12.010 3009.521 1.597 53.419 1.810 0.93 325682. 0.2842
|
|
86.28 0.3909 0.6455 0.0373 0.0226 3.864 13.529 10.841 2881.119 1.528 48.221 1.707 0.93 326140. 0.2546
|
|
90.59 0.4104 0.6327 0.0332 0.0216 3.685 12.905 9.653 2748.259 1.458 42.939 1.593 0.93 326614. 0.2243
|
|
94.90 0.4299 0.6105 0.0291 0.0205 3.503 12.266 8.451 2612.079 1.386 37.589 1.467 0.93 327104. 0.1933
|
|
99.22 0.4495 0.5771 0.0249 0.0194 3.318 11.617 7.237 2473.979 1.312 32.188 1.327 0.93 327610. 0.1617
|
|
103.53 0.4690 0.5303 0.0207 0.0183 3.132 10.966 6.016 2335.266 1.239 26.758 1.168 0.93 328132. 0.1299
|
|
107.84 0.4886 0.4679 0.0165 0.0172 2.946 10.317 4.794 2197.016 1.166 21.322 0.990 0.94 328671. 0.0982
|
|
112.16 0.5081 0.3871 0.0123 0.0162 2.763 9.676 3.576 2060.576 1.093 15.908 0.787 0.94 329226. 0.0675
|
|
116.47 0.5277 0.2849 0.0082 0.0151 2.584 9.050 2.371 1927.220 1.022 10.546 0.558 0.94 329798. 0.0389
|
|
120.79 0.5472 0.1582 0.0041 0.0141 2.411 8.441 1.184 1797.606 0.954 5.265 0.299 0.94 330387. 0.0147
|
|
125.10 0.5667 0.0002 0.0000 0.0130 2.230 7.807 0.001 1662.570 0.882 0.005 0.000 0.94 330983. 0.0000
|
|
|
|
|
|
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