612 lines
109 KiB
Plaintext
612 lines
109 KiB
Plaintext
15x8E (15x8E.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 0.0879 0.0358 0.002 0.138 0.142 1.633 0.016 0.631 39.397 0.06 20945. 0.5804
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0.33 0.0231 0.0554 0.0866 0.0362 0.002 0.139 0.140 1.648 0.016 0.621 38.452 0.06 20958. 0.5622
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0.66 0.0463 0.1081 0.0851 0.0365 0.002 0.140 0.137 1.661 0.016 0.611 37.503 0.06 20972. 0.5437
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0.99 0.0694 0.1580 0.0836 0.0367 0.002 0.141 0.135 1.674 0.016 0.600 36.551 0.06 20987. 0.5251
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1.31 0.0926 0.2052 0.0819 0.0370 0.002 0.142 0.132 1.684 0.016 0.588 35.599 0.06 21004. 0.5063
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1.64 0.1157 0.2497 0.0801 0.0371 0.002 0.143 0.129 1.693 0.016 0.575 34.649 0.06 21022. 0.4874
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1.97 0.1389 0.2914 0.0782 0.0373 0.002 0.144 0.126 1.699 0.016 0.561 33.701 0.06 21041. 0.4683
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2.30 0.1620 0.3305 0.0762 0.0373 0.002 0.144 0.123 1.702 0.016 0.547 32.758 0.06 21062. 0.4492
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2.63 0.1851 0.3668 0.0740 0.0373 0.002 0.144 0.119 1.702 0.016 0.531 31.818 0.06 21084. 0.4300
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2.96 0.2083 0.4005 0.0716 0.0373 0.002 0.144 0.116 1.698 0.016 0.514 30.881 0.06 21107. 0.4107
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3.29 0.2314 0.4316 0.0692 0.0371 0.002 0.143 0.112 1.690 0.016 0.496 29.946 0.06 21132. 0.3913
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3.62 0.2546 0.4599 0.0665 0.0368 0.002 0.142 0.107 1.678 0.016 0.477 29.012 0.06 21158. 0.3718
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3.94 0.2777 0.4855 0.0637 0.0365 0.002 0.140 0.103 1.661 0.016 0.457 28.074 0.06 21186. 0.3521
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4.27 0.3009 0.5083 0.0608 0.0360 0.002 0.139 0.098 1.639 0.016 0.436 27.130 0.06 21215. 0.3323
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4.60 0.3240 0.5281 0.0577 0.0354 0.002 0.136 0.093 1.613 0.015 0.414 26.175 0.06 21246. 0.3124
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4.93 0.3471 0.5448 0.0544 0.0347 0.002 0.134 0.088 1.581 0.015 0.391 25.202 0.06 21279. 0.2922
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5.26 0.3703 0.5581 0.0510 0.0339 0.002 0.130 0.082 1.543 0.015 0.366 24.204 0.06 21313. 0.2717
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5.59 0.3934 0.5677 0.0475 0.0329 0.002 0.127 0.077 1.501 0.014 0.341 23.171 0.06 21349. 0.2510
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5.92 0.4166 0.5732 0.0439 0.0319 0.002 0.123 0.071 1.452 0.014 0.315 22.095 0.06 21386. 0.2299
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6.25 0.4397 0.5740 0.0401 0.0307 0.002 0.118 0.065 1.399 0.013 0.288 20.963 0.06 21425. 0.2085
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6.57 0.4629 0.5696 0.0362 0.0294 0.002 0.113 0.058 1.341 0.013 0.260 19.760 0.06 21465. 0.1869
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6.90 0.4860 0.5589 0.0323 0.0281 0.002 0.108 0.052 1.279 0.012 0.232 18.468 0.06 21507. 0.1649
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7.23 0.5092 0.5411 0.0283 0.0266 0.002 0.102 0.046 1.213 0.012 0.203 17.066 0.06 21551. 0.1426
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7.56 0.5323 0.5146 0.0242 0.0251 0.002 0.097 0.039 1.142 0.011 0.174 15.524 0.06 21596. 0.1200
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7.89 0.5554 0.4775 0.0201 0.0234 0.001 0.090 0.032 1.067 0.010 0.144 13.805 0.06 21643. 0.0973
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8.22 0.5786 0.4272 0.0160 0.0217 0.001 0.084 0.026 0.989 0.009 0.115 11.858 0.06 21692. 0.0746
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8.55 0.6017 0.3603 0.0119 0.0199 0.001 0.077 0.019 0.908 0.009 0.086 9.615 0.06 21742. 0.0522
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8.88 0.6249 0.2716 0.0079 0.0181 0.001 0.070 0.013 0.824 0.008 0.056 6.979 0.06 21794. 0.0307
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9.20 0.6480 0.1537 0.0038 0.0162 0.001 0.062 0.006 0.738 0.007 0.028 3.810 0.06 21847. 0.0117
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9.53 0.6712 -0.0047 -0.0001 0.0143 0.001 0.055 0.000 0.650 0.006 -0.001 -0.113 0.06 21902. 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 0.0882 0.0326 0.016 0.503 0.569 11.893 0.057 2.532 21.712 0.12 41889. 0.6408
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0.66 0.0232 0.0612 0.0869 0.0330 0.016 0.508 0.561 12.027 0.057 2.494 21.146 0.12 41915. 0.6194
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1.32 0.0465 0.1192 0.0855 0.0333 0.016 0.514 0.551 12.153 0.058 2.453 20.582 0.12 41944. 0.5979
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1.98 0.0697 0.1739 0.0839 0.0337 0.016 0.518 0.541 12.267 0.059 2.408 20.020 0.12 41975. 0.5763
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2.64 0.0930 0.2254 0.0822 0.0339 0.017 0.523 0.531 12.368 0.059 2.361 19.463 0.12 42008. 0.5546
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3.30 0.1162 0.2738 0.0804 0.0342 0.017 0.526 0.519 12.452 0.059 2.309 18.910 0.12 42044. 0.5330
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3.96 0.1395 0.3191 0.0785 0.0343 0.017 0.529 0.507 12.516 0.060 2.254 18.365 0.12 42083. 0.5114
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4.62 0.1627 0.3613 0.0765 0.0344 0.017 0.531 0.493 12.556 0.060 2.195 17.825 0.12 42124. 0.4898
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5.28 0.1860 0.4006 0.0743 0.0345 0.017 0.531 0.479 12.569 0.060 2.132 17.293 0.12 42169. 0.4683
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5.94 0.2092 0.4370 0.0719 0.0344 0.017 0.530 0.464 12.553 0.060 2.064 16.768 0.12 42216. 0.4468
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6.61 0.2325 0.4705 0.0694 0.0343 0.017 0.528 0.448 12.502 0.060 1.992 16.250 0.12 42266. 0.4254
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7.27 0.2557 0.5012 0.0668 0.0341 0.017 0.525 0.431 12.416 0.059 1.916 15.737 0.12 42319. 0.4040
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7.93 0.2790 0.5291 0.0639 0.0337 0.016 0.519 0.413 12.290 0.059 1.835 15.228 0.12 42375. 0.3826
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8.59 0.3022 0.5542 0.0610 0.0333 0.016 0.512 0.393 12.123 0.058 1.750 14.722 0.12 42434. 0.3612
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9.25 0.3255 0.5763 0.0579 0.0327 0.016 0.503 0.373 11.913 0.057 1.661 14.215 0.12 42497. 0.3398
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9.91 0.3487 0.5953 0.0546 0.0320 0.016 0.493 0.352 11.657 0.056 1.567 13.706 0.12 42562. 0.3182
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10.57 0.3720 0.6111 0.0512 0.0311 0.015 0.480 0.330 11.355 0.054 1.469 13.190 0.12 42631. 0.2965
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11.23 0.3952 0.6233 0.0476 0.0302 0.015 0.465 0.307 11.005 0.053 1.367 12.663 0.12 42703. 0.2746
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11.89 0.4185 0.6317 0.0439 0.0291 0.014 0.448 0.283 10.609 0.051 1.261 12.120 0.12 42778. 0.2524
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12.55 0.4417 0.6356 0.0401 0.0279 0.014 0.430 0.259 10.169 0.049 1.152 11.554 0.12 42857. 0.2300
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13.21 0.4650 0.6345 0.0363 0.0266 0.013 0.409 0.234 9.687 0.046 1.041 10.957 0.12 42938. 0.2073
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13.87 0.4882 0.6275 0.0323 0.0251 0.012 0.387 0.208 9.164 0.044 0.927 10.319 0.12 43023. 0.1843
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14.53 0.5115 0.6133 0.0283 0.0236 0.012 0.364 0.183 8.603 0.041 0.812 9.628 0.12 43111. 0.1609
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15.19 0.5347 0.5903 0.0242 0.0220 0.011 0.338 0.156 8.004 0.038 0.696 8.864 0.12 43203. 0.1371
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15.85 0.5580 0.5562 0.0202 0.0202 0.010 0.311 0.130 7.371 0.035 0.578 8.003 0.12 43297. 0.1129
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16.51 0.5812 0.5075 0.0161 0.0184 0.009 0.283 0.104 6.705 0.032 0.461 7.010 0.12 43395. 0.0883
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17.17 0.6045 0.4390 0.0120 0.0165 0.008 0.254 0.077 6.010 0.029 0.344 5.832 0.12 43496. 0.0634
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17.83 0.6277 0.3428 0.0079 0.0145 0.007 0.224 0.051 5.291 0.025 0.228 4.385 0.12 43601. 0.0388
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18.49 0.6510 0.2054 0.0039 0.0125 0.006 0.192 0.025 4.550 0.022 0.113 2.533 0.12 43709. 0.0158
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19.15 0.6742 0.0021 0.0000 0.0104 0.005 0.160 0.000 3.794 0.018 0.001 0.026 0.12 43819. 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 0.0885 0.0313 0.052 1.084 1.285 38.464 0.122 5.715 15.152 0.18 62833. 0.6719
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1.01 0.0237 0.0652 0.0871 0.0317 0.052 1.097 1.265 38.948 0.124 5.628 14.735 0.18 62873. 0.6483
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2.02 0.0474 0.1268 0.0857 0.0320 0.053 1.110 1.244 39.404 0.125 5.533 14.319 0.18 62917. 0.6247
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3.03 0.0711 0.1848 0.0841 0.0324 0.053 1.122 1.221 39.821 0.127 5.431 13.908 0.18 62964. 0.6012
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4.04 0.0948 0.2391 0.0824 0.0327 0.054 1.132 1.196 40.190 0.128 5.321 13.501 0.18 63016. 0.5776
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5.05 0.1185 0.2900 0.0806 0.0329 0.054 1.141 1.170 40.498 0.129 5.203 13.100 0.18 63071. 0.5542
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6.06 0.1422 0.3376 0.0786 0.0331 0.055 1.148 1.141 40.734 0.130 5.075 12.705 0.18 63131. 0.5309
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7.07 0.1659 0.3818 0.0765 0.0332 0.055 1.152 1.110 40.885 0.130 4.938 12.316 0.18 63195. 0.5076
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8.08 0.1896 0.4228 0.0742 0.0333 0.055 1.153 1.077 40.940 0.130 4.792 11.935 0.18 63263. 0.4846
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9.09 0.2133 0.4607 0.0718 0.0332 0.055 1.152 1.042 40.886 0.130 4.635 11.561 0.18 63336. 0.4616
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10.10 0.2370 0.4956 0.0692 0.0331 0.055 1.147 1.005 40.710 0.130 4.468 11.193 0.18 63413. 0.4388
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11.11 0.2607 0.5276 0.0664 0.0328 0.054 1.138 0.965 40.403 0.129 4.291 10.831 0.18 63496. 0.4161
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12.12 0.2844 0.5565 0.0635 0.0325 0.054 1.126 0.923 39.953 0.127 4.104 10.473 0.18 63583. 0.3935
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13.13 0.3082 0.5826 0.0605 0.0320 0.053 1.109 0.878 39.353 0.125 3.905 10.120 0.18 63675. 0.3709
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14.14 0.3319 0.6056 0.0572 0.0314 0.052 1.087 0.831 38.595 0.123 3.697 9.768 0.18 63771. 0.3484
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15.15 0.3556 0.6255 0.0539 0.0306 0.051 1.061 0.782 37.673 0.120 3.479 9.416 0.18 63873. 0.3257
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16.16 0.3793 0.6420 0.0503 0.0297 0.049 1.031 0.731 36.580 0.116 3.251 9.061 0.18 63980. 0.3030
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17.17 0.4030 0.6550 0.0467 0.0287 0.047 0.995 0.677 35.314 0.112 3.013 8.700 0.18 64091. 0.2801
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18.18 0.4267 0.6639 0.0429 0.0275 0.045 0.955 0.622 33.883 0.108 2.768 8.330 0.18 64208. 0.2570
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19.19 0.4504 0.6684 0.0390 0.0262 0.043 0.910 0.566 32.294 0.103 2.516 7.944 0.18 64330. 0.2337
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20.20 0.4741 0.6676 0.0350 0.0248 0.041 0.861 0.508 30.551 0.097 2.258 7.537 0.18 64456. 0.2101
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21.21 0.4978 0.6604 0.0309 0.0233 0.038 0.808 0.449 28.662 0.091 1.996 7.102 0.18 64588. 0.1861
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22.22 0.5215 0.6456 0.0268 0.0216 0.036 0.750 0.389 26.631 0.085 1.731 6.626 0.18 64725. 0.1617
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23.23 0.5452 0.6208 0.0226 0.0199 0.033 0.689 0.329 24.467 0.078 1.463 6.096 0.18 64867. 0.1367
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24.24 0.5689 0.5832 0.0185 0.0180 0.030 0.625 0.268 22.177 0.071 1.193 5.487 0.18 65014. 0.1112
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25.25 0.5926 0.5277 0.0143 0.0161 0.027 0.557 0.208 19.773 0.063 0.924 4.766 0.18 65166. 0.0850
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26.26 0.6163 0.4465 0.0102 0.0140 0.023 0.486 0.148 17.267 0.055 0.657 3.878 0.18 65324. 0.0583
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27.27 0.6400 0.3261 0.0061 0.0119 0.020 0.414 0.088 14.677 0.047 0.393 2.728 0.18 65486. 0.0317
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28.28 0.6637 0.1405 0.0021 0.0098 0.016 0.339 0.030 12.019 0.038 0.134 1.133 0.18 65653. 0.0077
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29.29 0.6874
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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 0.0888 0.0305 0.119 1.881 2.292 89.010 0.212 10.197 11.681 0.24 83775. 0.6919
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1.35 0.0237 0.0671 0.0875 0.0309 0.121 1.906 2.257 90.194 0.215 10.041 11.353 0.24 83829. 0.6672
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2.70 0.0474 0.1303 0.0860 0.0313 0.122 1.929 2.220 91.312 0.218 9.873 11.026 0.24 83888. 0.6426
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4.04 0.0712 0.1897 0.0844 0.0317 0.124 1.951 2.179 92.340 0.220 9.692 10.703 0.24 83951. 0.6180
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5.39 0.0949 0.2454 0.0827 0.0320 0.125 1.970 2.135 93.250 0.223 9.496 10.384 0.24 84020. 0.5935
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6.74 0.1186 0.2975 0.0809 0.0322 0.126 1.987 2.087 94.017 0.224 9.285 10.071 0.24 84094. 0.5692
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8.09 0.1423 0.3461 0.0789 0.0324 0.127 1.999 2.036 94.612 0.226 9.058 9.763 0.24 84174. 0.5450
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9.43 0.1660 0.3913 0.0768 0.0326 0.127 2.007 1.982 95.004 0.227 8.814 9.461 0.24 84259. 0.5210
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10.78 0.1898 0.4332 0.0745 0.0326 0.128 2.011 1.923 95.164 0.227 8.553 9.165 0.24 84350. 0.4972
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12.13 0.2135 0.4720 0.0721 0.0326 0.127 2.009 1.860 95.061 0.227 8.275 8.876 0.24 84448. 0.4736
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13.48 0.2372 0.5077 0.0695 0.0325 0.127 2.000 1.793 94.668 0.226 7.977 8.593 0.24 84551. 0.4501
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14.82 0.2609 0.5404 0.0667 0.0322 0.126 1.985 1.722 93.958 0.224 7.661 8.315 0.24 84661. 0.4269
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16.17 0.2846 0.5701 0.0638 0.0319 0.125 1.963 1.647 92.904 0.222 7.326 8.041 0.24 84777. 0.4037
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17.52 0.3083 0.5969 0.0607 0.0314 0.123 1.933 1.568 91.487 0.218 6.973 7.772 0.24 84900. 0.3807
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18.87 0.3321 0.6208 0.0575 0.0308 0.120 1.895 1.484 89.688 0.214 6.601 7.505 0.24 85029. 0.3577
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20.21 0.3558 0.6416 0.0541 0.0300 0.117 1.849 1.396 87.490 0.209 6.212 7.240 0.24 85165. 0.3347
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21.56 0.3795 0.6592 0.0506 0.0291 0.114 1.794 1.305 84.879 0.203 5.804 6.973 0.24 85307. 0.3116
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22.91 0.4032 0.6733 0.0469 0.0281 0.110 1.730 1.210 81.849 0.195 5.380 6.703 0.24 85456. 0.2884
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24.26 0.4269 0.6835 0.0430 0.0269 0.105 1.657 1.111 78.417 0.187 4.943 6.427 0.24 85612. 0.2650
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25.61 0.4507 0.6894 0.0391 0.0256 0.100 1.576 1.010 74.597 0.178 4.493 6.142 0.24 85774. 0.2415
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26.95 0.4744 0.6903 0.0351 0.0241 0.094 1.488 0.907 70.403 0.168 4.034 5.842 0.24 85944. 0.2176
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28.30 0.4981 0.6851 0.0311 0.0226 0.088 1.391 0.802 65.849 0.157 3.566 5.522 0.24 86120. 0.1934
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29.65 0.5218 0.6725 0.0269 0.0209 0.082 1.288 0.695 60.949 0.146 3.092 5.174 0.24 86302. 0.1687
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31.00 0.5455 0.6502 0.0228 0.0191 0.075 1.177 0.588 55.720 0.133 2.614 4.785 0.24 86492. 0.1435
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32.34 0.5693 0.6150 0.0186 0.0172 0.067 1.060 0.480 50.184 0.120 2.135 4.337 0.24 86688. 0.1175
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33.69 0.5930 0.5619 0.0144 0.0152 0.059 0.938 0.372 44.367 0.106 1.655 3.804 0.24 86892. 0.0908
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35.04 0.6167 0.4820 0.0103 0.0131 0.051 0.809 0.265 38.301 0.091 1.179 3.138 0.24 87102. 0.0632
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36.39 0.6404 0.3598 0.0062 0.0110 0.043 0.677 0.159 32.027 0.076 0.708 2.255 0.24 87319. 0.0352
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37.73 0.6641 0.1631 0.0022 0.0088 0.034 0.541 0.056 25.589 0.061 0.247 0.986 0.24 87542. 0.0091
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39.08 0.6878
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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 0.0892 0.0301 0.230 2.897 3.597 171.396 0.327 16.000 9.519 0.30 104716. 0.7062
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1.66 0.0234 0.0673 0.0879 0.0305 0.233 2.937 3.543 173.728 0.332 15.761 9.251 0.30 104783. 0.6812
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3.32 0.0467 0.1307 0.0864 0.0309 0.236 2.974 3.486 175.936 0.336 15.504 8.986 0.30 104855. 0.6562
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4.98 0.0701 0.1903 0.0849 0.0312 0.239 3.009 3.423 177.972 0.340 15.226 8.724 0.30 104933. 0.6314
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6.63 0.0934 0.2462 0.0832 0.0316 0.241 3.039 3.356 179.790 0.343 14.926 8.465 0.30 105017. 0.6066
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8.29 0.1168 0.2985 0.0814 0.0318 0.243 3.065 3.283 181.336 0.346 14.602 8.211 0.30 105108. 0.5820
|
|
9.95 0.1401 0.3474 0.0795 0.0320 0.245 3.086 3.205 182.557 0.349 14.255 7.963 0.30 105205. 0.5576
|
|
11.61 0.1635 0.3929 0.0774 0.0322 0.246 3.100 3.121 183.397 0.350 13.882 7.719 0.30 105310. 0.5334
|
|
13.27 0.1868 0.4351 0.0752 0.0323 0.246 3.107 3.031 183.799 0.351 13.483 7.481 0.30 105421. 0.5095
|
|
14.93 0.2102 0.4743 0.0728 0.0323 0.246 3.105 2.935 183.706 0.351 13.057 7.248 0.30 105540. 0.4857
|
|
16.59 0.2335 0.5104 0.0702 0.0321 0.245 3.095 2.833 183.063 0.350 12.602 7.020 0.30 105667. 0.4622
|
|
18.24 0.2569 0.5436 0.0676 0.0319 0.244 3.074 2.725 181.819 0.347 12.120 6.797 0.30 105801. 0.4389
|
|
19.90 0.2802 0.5740 0.0647 0.0316 0.241 3.042 2.610 179.925 0.344 11.608 6.579 0.30 105943. 0.4157
|
|
21.56 0.3036 0.6016 0.0617 0.0311 0.238 2.998 2.488 177.339 0.339 11.068 6.364 0.30 106092. 0.3927
|
|
23.22 0.3269 0.6263 0.0585 0.0306 0.233 2.942 2.361 174.024 0.332 10.500 6.153 0.30 106250. 0.3698
|
|
24.88 0.3503 0.6481 0.0552 0.0298 0.228 2.873 2.227 169.950 0.325 9.904 5.943 0.30 106415. 0.3469
|
|
26.54 0.3736 0.6670 0.0517 0.0290 0.221 2.791 2.087 165.086 0.315 9.282 5.733 0.30 106588. 0.3240
|
|
28.20 0.3970 0.6826 0.0481 0.0280 0.214 2.695 1.941 159.413 0.304 8.633 5.522 0.30 106770. 0.3009
|
|
29.85 0.4203 0.6947 0.0444 0.0269 0.205 2.586 1.790 152.952 0.292 7.962 5.308 0.30 106959. 0.2778
|
|
31.51 0.4437 0.7030 0.0405 0.0256 0.195 2.464 1.635 145.734 0.278 7.272 5.089 0.30 107157. 0.2545
|
|
33.17 0.4670 0.7067 0.0366 0.0242 0.185 2.329 1.476 137.785 0.263 6.567 4.860 0.30 107363. 0.2310
|
|
34.83 0.4904 0.7052 0.0326 0.0227 0.173 2.183 1.315 129.128 0.247 5.848 4.618 0.30 107577. 0.2071
|
|
36.49 0.5137 0.6971 0.0285 0.0210 0.161 2.025 1.151 119.791 0.229 5.119 4.358 0.30 107799. 0.1829
|
|
38.15 0.5371 0.6807 0.0244 0.0193 0.147 1.856 0.985 109.804 0.210 4.383 4.070 0.30 108030. 0.1581
|
|
39.80 0.5605 0.6534 0.0203 0.0174 0.133 1.677 0.819 99.204 0.189 3.643 3.744 0.30 108268. 0.1325
|
|
41.46 0.5838 0.6109 0.0162 0.0155 0.118 1.488 0.652 88.037 0.168 2.901 3.361 0.30 108515. 0.1062
|
|
43.12 0.6072 0.5462 0.0121 0.0134 0.102 1.291 0.486 76.361 0.146 2.163 2.889 0.30 108771. 0.0788
|
|
44.78 0.6305 0.4465 0.0080 0.0113 0.086 1.086 0.322 64.247 0.123 1.433 2.274 0.30 109034. 0.0505
|
|
46.44 0.6539 0.2866 0.0040 0.0091 0.069 0.875 0.161 51.778 0.099 0.715 1.408 0.30 109306. 0.0221
|
|
48.10 0.6772 0.0066 0.0001 0.0068 0.052 0.660 0.003 39.014 0.075 0.012 0.031 0.30 109581. 0.0001
|
|
|
|
|
|
|
|
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 0.0896 0.0299 0.394 4.140 5.206 293.854 0.468 23.156 8.036 0.36 125655. 0.7172
|
|
1.99 0.0234 0.0682 0.0883 0.0303 0.400 4.198 5.129 297.969 0.474 22.813 7.807 0.36 125735. 0.6916
|
|
3.99 0.0468 0.1325 0.0869 0.0307 0.405 4.252 5.045 301.868 0.480 22.442 7.581 0.36 125822. 0.6661
|
|
5.98 0.0701 0.1928 0.0853 0.0310 0.410 4.303 4.955 305.469 0.486 22.041 7.358 0.36 125916. 0.6407
|
|
7.97 0.0935 0.2494 0.0836 0.0314 0.414 4.348 4.858 308.685 0.491 21.608 7.138 0.36 126018. 0.6154
|
|
9.96 0.1169 0.3024 0.0818 0.0316 0.418 4.387 4.753 311.428 0.496 21.142 6.922 0.36 126127. 0.5904
|
|
11.96 0.1403 0.3518 0.0799 0.0319 0.421 4.418 4.640 313.600 0.499 20.640 6.711 0.36 126244. 0.5655
|
|
13.95 0.1637 0.3978 0.0778 0.0320 0.423 4.439 4.519 315.103 0.502 20.101 6.505 0.36 126370. 0.5409
|
|
15.94 0.1871 0.4406 0.0756 0.0321 0.424 4.449 4.389 315.838 0.503 19.524 6.303 0.36 126504. 0.5166
|
|
17.94 0.2104 0.4802 0.0732 0.0321 0.423 4.447 4.251 315.704 0.502 18.907 6.107 0.36 126648. 0.4925
|
|
19.93 0.2338 0.5167 0.0706 0.0320 0.422 4.432 4.103 314.604 0.501 18.249 5.915 0.36 126800. 0.4687
|
|
21.92 0.2572 0.5504 0.0679 0.0317 0.419 4.401 3.945 312.447 0.497 17.549 5.727 0.36 126961. 0.4450
|
|
23.91 0.2806 0.5812 0.0651 0.0314 0.415 4.355 3.779 309.147 0.492 16.808 5.544 0.36 127132. 0.4216
|
|
25.91 0.3040 0.6092 0.0620 0.0309 0.409 4.291 3.603 304.630 0.485 16.025 5.364 0.36 127312. 0.3983
|
|
27.90 0.3274 0.6344 0.0588 0.0304 0.401 4.210 3.418 298.831 0.476 15.201 5.187 0.36 127502. 0.3751
|
|
29.89 0.3507 0.6568 0.0555 0.0296 0.391 4.109 3.223 291.695 0.464 14.337 5.012 0.36 127701. 0.3520
|
|
31.89 0.3741 0.6762 0.0520 0.0288 0.380 3.989 3.020 283.167 0.451 13.434 4.838 0.36 127909. 0.3289
|
|
33.88 0.3975 0.6925 0.0484 0.0278 0.366 3.849 2.809 273.216 0.435 12.493 4.663 0.36 128128. 0.3057
|
|
35.87 0.4209 0.7054 0.0446 0.0266 0.351 3.689 2.590 261.876 0.417 11.520 4.486 0.36 128356. 0.2824
|
|
37.86 0.4443 0.7145 0.0407 0.0253 0.334 3.510 2.365 249.200 0.397 10.519 4.304 0.36 128594. 0.2589
|
|
39.86 0.4676 0.7192 0.0368 0.0239 0.315 3.314 2.135 235.232 0.374 9.495 4.116 0.36 128842. 0.2352
|
|
41.85 0.4910 0.7187 0.0327 0.0224 0.295 3.099 1.900 220.015 0.350 8.453 3.918 0.36 129099. 0.2113
|
|
43.84 0.5144 0.7119 0.0286 0.0207 0.273 2.868 1.663 203.596 0.324 7.395 3.704 0.36 129366. 0.1868
|
|
45.83 0.5378 0.6969 0.0245 0.0189 0.249 2.621 1.423 186.027 0.296 6.327 3.468 0.36 129644. 0.1618
|
|
47.83 0.5612 0.6711 0.0203 0.0170 0.224 2.358 1.181 167.375 0.266 5.253 3.201 0.36 129931. 0.1361
|
|
49.82 0.5846 0.6300 0.0162 0.0150 0.198 2.081 0.939 147.723 0.235 4.179 2.885 0.36 130228. 0.1094
|
|
51.81 0.6079 0.5662 0.0120 0.0129 0.171 1.792 0.699 127.174 0.202 3.109 2.493 0.36 130535. 0.0815
|
|
53.81 0.6313 0.4659 0.0079 0.0108 0.142 1.491 0.461 105.854 0.168 2.050 1.975 0.36 130852. 0.0525
|
|
55.80 0.6547 0.3002 0.0039 0.0085 0.113 1.182 0.227 83.913 0.134 1.010 1.227 0.36 131179. 0.0229
|
|
57.79 0.6781 -0.0036 0.0000 0.0062 0.082 0.865 -0.002 61.438 0.098 -0.009 -0.014 0.37 131509. 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 0.0902 0.0298 0.624 5.616 7.128 465.148 0.635 31.706 6.951 0.42 146592. 0.7259
|
|
2.33 0.0234 0.0688 0.0888 0.0302 0.633 5.697 7.023 471.805 0.644 31.240 6.752 0.42 146686. 0.7000
|
|
4.65 0.0468 0.1337 0.0874 0.0306 0.641 5.773 6.910 478.116 0.652 30.735 6.555 0.42 146787. 0.6741
|
|
6.98 0.0702 0.1946 0.0859 0.0310 0.649 5.843 6.787 483.947 0.660 30.190 6.361 0.42 146897. 0.6483
|
|
9.30 0.0936 0.2516 0.0842 0.0313 0.656 5.906 6.655 489.162 0.667 29.600 6.171 0.42 147016. 0.6227
|
|
11.63 0.1169 0.3050 0.0824 0.0316 0.662 5.960 6.512 493.613 0.673 28.964 5.984 0.42 147144. 0.5973
|
|
13.95 0.1403 0.3548 0.0804 0.0318 0.667 6.003 6.358 497.147 0.678 28.280 5.801 0.42 147281. 0.5721
|
|
16.28 0.1637 0.4012 0.0783 0.0320 0.670 6.033 6.193 499.605 0.682 27.545 5.622 0.42 147428. 0.5473
|
|
18.60 0.1871 0.4443 0.0761 0.0320 0.672 6.047 6.015 500.823 0.683 26.756 5.448 0.42 147585. 0.5227
|
|
20.93 0.2105 0.4843 0.0737 0.0320 0.671 6.045 5.826 500.642 0.683 25.913 5.278 0.42 147752. 0.4983
|
|
23.25 0.2339 0.5212 0.0711 0.0319 0.669 6.024 5.623 498.905 0.681 25.013 5.112 0.42 147930. 0.4742
|
|
25.58 0.2573 0.5552 0.0684 0.0317 0.664 5.983 5.408 495.462 0.676 24.056 4.951 0.42 148119. 0.4504
|
|
27.91 0.2807 0.5864 0.0655 0.0314 0.657 5.919 5.180 490.178 0.669 23.042 4.793 0.42 148318. 0.4268
|
|
30.23 0.3040 0.6148 0.0625 0.0309 0.648 5.831 4.939 482.930 0.659 21.970 4.639 0.42 148529. 0.4033
|
|
32.56 0.3274 0.6405 0.0593 0.0303 0.635 5.719 4.686 473.615 0.646 20.841 4.487 0.42 148750. 0.3800
|
|
34.88 0.3508 0.6633 0.0559 0.0296 0.620 5.580 4.419 462.141 0.630 19.657 4.337 0.42 148983. 0.3567
|
|
37.21 0.3742 0.6832 0.0524 0.0287 0.601 5.415 4.141 448.423 0.612 18.419 4.189 0.42 149227. 0.3334
|
|
39.53 0.3976 0.7001 0.0487 0.0277 0.580 5.221 3.851 432.406 0.590 17.130 4.040 0.42 149482. 0.3101
|
|
41.86 0.4210 0.7137 0.0449 0.0265 0.555 5.001 3.551 414.145 0.565 15.795 3.889 0.42 149749. 0.2867
|
|
44.18 0.4444 0.7236 0.0410 0.0252 0.528 4.754 3.243 393.722 0.537 14.423 3.735 0.42 150026. 0.2631
|
|
46.51 0.4678 0.7292 0.0370 0.0237 0.498 4.482 2.927 371.209 0.506 13.019 3.576 0.42 150316. 0.2393
|
|
48.84 0.4911 0.7298 0.0330 0.0222 0.465 4.186 2.605 346.674 0.473 11.589 3.409 0.42 150616. 0.2152
|
|
51.16 0.5145 0.7242 0.0288 0.0205 0.429 3.866 2.279 320.191 0.437 10.139 3.229 0.42 150929. 0.1907
|
|
53.49 0.5379 0.7107 0.0247 0.0187 0.391 3.524 1.950 291.847 0.398 8.674 3.031 0.42 151252. 0.1656
|
|
55.81 0.5613 0.6864 0.0205 0.0167 0.351 3.161 1.619 261.750 0.357 7.201 2.805 0.42 151588. 0.1396
|
|
58.14 0.5847 0.6471 0.0163 0.0147 0.308 2.778 1.288 230.033 0.314 5.727 2.539 0.42 151935. 0.1127
|
|
60.46 0.6081 0.5849 0.0121 0.0126 0.264 2.377 0.958 196.864 0.269 4.260 2.207 0.42 152293. 0.0845
|
|
62.79 0.6315 0.4852 0.0080 0.0104 0.218 1.962 0.631 162.448 0.222 2.808 1.763 0.42 152663. 0.0548
|
|
65.11 0.6549 0.3166 0.0039 0.0081 0.170 1.534 0.311 127.031 0.173 1.382 1.109 0.43 153045. 0.0242
|
|
67.44 0.6782 -0.0050 0.0000 0.0058 0.122 1.096 -0.003 90.740 0.124 -0.015 -0.017 0.43 153429. 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 0.0908 0.0298 0.932 7.341 9.375 694.777 0.829 41.701 6.120 0.48 167526. 0.7331
|
|
2.66 0.0234 0.0693 0.0895 0.0302 0.945 7.447 9.239 704.898 0.841 41.094 5.945 0.48 167633. 0.7068
|
|
5.32 0.0468 0.1345 0.0880 0.0306 0.958 7.549 9.091 714.497 0.853 40.436 5.771 0.48 167749. 0.6806
|
|
7.97 0.0702 0.1957 0.0865 0.0310 0.970 7.643 8.931 723.368 0.863 39.724 5.600 0.48 167875. 0.6546
|
|
10.63 0.0936 0.2531 0.0848 0.0313 0.981 7.726 8.758 731.305 0.873 38.953 5.432 0.48 168011. 0.6288
|
|
13.29 0.1169 0.3068 0.0830 0.0316 0.990 7.798 8.571 738.086 0.881 38.122 5.267 0.48 168158. 0.6032
|
|
15.95 0.1403 0.3569 0.0811 0.0319 0.997 7.855 8.369 743.475 0.887 37.226 5.106 0.48 168315. 0.5778
|
|
18.60 0.1637 0.4036 0.0790 0.0320 1.002 7.895 8.153 747.233 0.892 36.263 4.949 0.48 168483. 0.5527
|
|
21.26 0.1871 0.4470 0.0767 0.0321 1.005 7.915 7.920 749.112 0.894 35.229 4.796 0.48 168663. 0.5279
|
|
23.92 0.2105 0.4872 0.0743 0.0321 1.004 7.912 7.672 748.867 0.894 34.123 4.646 0.48 168855. 0.5034
|
|
26.58 0.2339 0.5245 0.0717 0.0320 1.001 7.884 7.406 746.263 0.891 32.942 4.501 0.48 169059. 0.4792
|
|
29.23 0.2573 0.5588 0.0690 0.0318 0.994 7.830 7.123 741.073 0.885 31.685 4.360 0.48 169275. 0.4552
|
|
31.89 0.2807 0.5903 0.0661 0.0314 0.983 7.745 6.824 733.089 0.875 30.352 4.222 0.48 169503. 0.4314
|
|
34.55 0.3040 0.6190 0.0630 0.0310 0.968 7.629 6.507 722.125 0.862 28.942 4.087 0.48 169744. 0.4078
|
|
37.21 0.3274 0.6451 0.0598 0.0303 0.949 7.480 6.173 708.024 0.845 27.458 3.955 0.48 169998. 0.3843
|
|
39.87 0.3508 0.6683 0.0564 0.0296 0.926 7.297 5.823 690.651 0.824 25.900 3.824 0.48 170264. 0.3610
|
|
42.52 0.3742 0.6888 0.0528 0.0287 0.898 7.077 5.457 669.873 0.800 24.271 3.695 0.48 170543. 0.3376
|
|
45.18 0.3976 0.7062 0.0491 0.0277 0.866 6.821 5.075 645.605 0.771 22.573 3.565 0.48 170835. 0.3142
|
|
47.84 0.4210 0.7204 0.0453 0.0265 0.829 6.529 4.680 617.928 0.738 20.815 3.435 0.48 171140. 0.2907
|
|
50.50 0.4444 0.7310 0.0414 0.0252 0.787 6.201 4.273 586.966 0.701 19.008 3.302 0.48 171458. 0.2670
|
|
53.15 0.4678 0.7375 0.0374 0.0237 0.741 5.841 3.857 552.825 0.660 17.158 3.165 0.48 171788. 0.2432
|
|
55.81 0.4911 0.7391 0.0333 0.0221 0.691 5.448 3.434 515.609 0.615 15.274 3.021 0.48 172132. 0.2190
|
|
58.47 0.5145 0.7346 0.0291 0.0204 0.638 5.023 3.004 475.431 0.568 13.362 2.866 0.48 172489. 0.1943
|
|
61.13 0.5379 0.7224 0.0249 0.0185 0.580 4.569 2.570 432.423 0.516 11.432 2.696 0.48 172860. 0.1691
|
|
63.78 0.5613 0.6997 0.0207 0.0166 0.519 4.086 2.134 386.747 0.462 9.490 2.502 0.48 173243. 0.1430
|
|
66.44 0.5847 0.6620 0.0164 0.0145 0.454 3.577 1.697 338.607 0.404 7.547 2.273 0.48 173639. 0.1158
|
|
69.10 0.6081 0.6014 0.0122 0.0124 0.387 3.046 1.262 288.260 0.344 5.612 1.985 0.48 174049. 0.0872
|
|
71.76 0.6315 0.5027 0.0081 0.0101 0.317 2.494 0.832 236.021 0.282 3.699 1.598 0.49 174472. 0.0570
|
|
74.42 0.6549 0.3318 0.0040 0.0078 0.244 1.926 0.409 182.262 0.218 1.818 1.017 0.49 174908. 0.0254
|
|
77.07 0.6782 -0.0064 -0.0001 0.0055 0.171 1.344 -0.005 127.162 0.152 -0.024 -0.019 0.49 175347. 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 0.0915 0.0299 1.332 9.328 11.961 993.233 1.054 53.204 5.462 0.54 188456. 0.7390
|
|
2.99 0.0234 0.0695 0.0902 0.0303 1.352 9.466 11.789 1007.920 1.069 52.439 5.305 0.54 188577. 0.7126
|
|
5.98 0.0468 0.1350 0.0888 0.0308 1.370 9.597 11.603 1021.853 1.084 51.608 5.150 0.54 188708. 0.6862
|
|
8.97 0.0701 0.1965 0.0872 0.0311 1.388 9.718 11.400 1034.733 1.098 50.708 4.997 0.54 188850. 0.6600
|
|
11.96 0.0935 0.2541 0.0856 0.0315 1.403 9.826 11.181 1046.260 1.110 49.734 4.847 0.54 189003. 0.6340
|
|
14.95 0.1169 0.3080 0.0837 0.0318 1.416 9.918 10.944 1056.109 1.121 48.681 4.700 0.54 189168. 0.6083
|
|
17.94 0.1403 0.3583 0.0818 0.0320 1.427 9.992 10.689 1063.943 1.129 47.545 4.557 0.54 189346. 0.5828
|
|
20.93 0.1637 0.4052 0.0797 0.0322 1.434 10.043 10.414 1069.411 1.135 46.322 4.417 0.54 189536. 0.5576
|
|
23.91 0.1871 0.4488 0.0774 0.0323 1.438 10.069 10.119 1072.157 1.138 45.009 4.281 0.54 189739. 0.5327
|
|
26.90 0.2104 0.4893 0.0750 0.0323 1.437 10.066 9.803 1071.825 1.137 43.602 4.148 0.54 189955. 0.5080
|
|
29.89 0.2338 0.5267 0.0724 0.0322 1.432 10.031 9.465 1068.073 1.133 42.099 4.019 0.54 190185. 0.4837
|
|
32.88 0.2572 0.5613 0.0697 0.0319 1.422 9.960 9.105 1060.574 1.125 40.498 3.894 0.54 190428. 0.4596
|
|
35.87 0.2806 0.5931 0.0667 0.0316 1.407 9.852 8.723 1049.027 1.113 38.799 3.772 0.54 190685. 0.4357
|
|
38.86 0.3040 0.6222 0.0637 0.0311 1.385 9.703 8.319 1033.164 1.096 37.002 3.652 0.54 190957. 0.4120
|
|
41.85 0.3274 0.6486 0.0604 0.0305 1.358 9.511 7.893 1012.755 1.075 35.109 3.535 0.54 191242. 0.3885
|
|
44.84 0.3507 0.6722 0.0570 0.0297 1.324 9.275 7.446 987.607 1.048 33.121 3.420 0.54 191542. 0.3650
|
|
47.83 0.3741 0.6931 0.0534 0.0288 1.284 8.993 6.978 957.530 1.016 31.040 3.306 0.54 191857. 0.3416
|
|
50.82 0.3975 0.7111 0.0497 0.0278 1.237 8.663 6.491 922.395 0.979 28.871 3.192 0.54 192186. 0.3181
|
|
53.81 0.4209 0.7259 0.0458 0.0266 1.183 8.286 5.986 882.320 0.936 26.625 3.077 0.54 192529. 0.2945
|
|
56.80 0.4443 0.7372 0.0418 0.0252 1.123 7.865 5.467 837.477 0.889 24.315 2.961 0.54 192887. 0.2708
|
|
59.79 0.4677 0.7445 0.0378 0.0237 1.057 7.401 4.935 788.024 0.836 21.950 2.840 0.54 193259. 0.2468
|
|
62.78 0.4910 0.7470 0.0336 0.0221 0.984 6.894 4.393 734.111 0.779 19.541 2.714 0.54 193646. 0.2225
|
|
65.76 0.5144 0.7436 0.0294 0.0203 0.906 6.348 3.844 675.898 0.717 17.096 2.579 0.54 194048. 0.1978
|
|
68.75 0.5378 0.7327 0.0252 0.0185 0.823 5.762 3.288 613.579 0.651 14.627 2.431 0.54 194464. 0.1724
|
|
71.74 0.5612 0.7114 0.0209 0.0165 0.734 5.141 2.730 547.390 0.581 12.142 2.262 0.54 194896. 0.1462
|
|
74.73 0.5846 0.6754 0.0166 0.0144 0.641 4.486 2.171 477.627 0.507 9.656 2.061 0.54 195342. 0.1188
|
|
77.72 0.6080 0.6165 0.0124 0.0122 0.543 3.800 1.614 404.661 0.429 7.180 1.809 0.55 195803. 0.0899
|
|
80.71 0.6313 0.5189 0.0081 0.0099 0.441 3.089 1.064 328.954 0.349 4.731 1.466 0.55 196279. 0.0592
|
|
83.70 0.6547 0.3463 0.0040 0.0076 0.337 2.358 0.522 251.049 0.266 2.324 0.944 0.55 196769. 0.0267
|
|
86.69 0.6781 -0.0077 -0.0001 0.0052 0.230 1.608 -0.008 171.183 0.182 -0.034 -0.020 0.55 197262. 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 0.0924 0.0301 1.840 11.599 14.904 1372.341 1.310 66.295 4.926 0.59 209381. 0.7439
|
|
3.32 0.0234 0.0696 0.0911 0.0306 1.868 11.773 14.693 1392.913 1.330 65.356 4.785 0.60 209516. 0.7174
|
|
6.64 0.0467 0.1352 0.0897 0.0310 1.894 11.938 14.464 1412.430 1.349 64.334 4.645 0.60 209662. 0.6910
|
|
9.96 0.0701 0.1968 0.0881 0.0314 1.918 12.091 14.214 1430.473 1.366 63.226 4.507 0.60 209820. 0.6647
|
|
13.28 0.0935 0.2545 0.0864 0.0317 1.940 12.227 13.944 1446.622 1.381 62.024 4.372 0.60 209991. 0.6386
|
|
16.60 0.1169 0.3086 0.0846 0.0320 1.958 12.344 13.652 1460.423 1.395 60.724 4.240 0.60 210175. 0.6128
|
|
19.92 0.1402 0.3590 0.0827 0.0323 1.973 12.437 13.336 1471.401 1.405 59.319 4.111 0.60 210373. 0.5873
|
|
23.24 0.1636 0.4061 0.0806 0.0325 1.983 12.501 12.996 1479.067 1.412 57.806 3.985 0.60 210584. 0.5620
|
|
26.56 0.1870 0.4498 0.0783 0.0325 1.989 12.534 12.630 1482.920 1.416 56.178 3.863 0.60 210810. 0.5370
|
|
29.88 0.2104 0.4905 0.0759 0.0325 1.988 12.530 12.237 1482.467 1.416 54.432 3.744 0.60 211051. 0.5123
|
|
33.20 0.2337 0.5281 0.0733 0.0324 1.981 12.486 11.818 1477.229 1.411 52.565 3.629 0.60 211307. 0.4879
|
|
36.52 0.2571 0.5630 0.0705 0.0322 1.967 12.397 11.370 1466.746 1.401 50.576 3.516 0.60 211578. 0.4638
|
|
39.84 0.2805 0.5950 0.0675 0.0318 1.945 12.261 10.895 1450.603 1.385 48.462 3.407 0.60 211865. 0.4399
|
|
43.16 0.3039 0.6244 0.0644 0.0313 1.916 12.073 10.392 1428.424 1.364 46.225 3.300 0.60 212167. 0.4161
|
|
46.48 0.3272 0.6511 0.0611 0.0307 1.877 11.832 9.862 1399.891 1.337 43.866 3.195 0.60 212485. 0.3925
|
|
49.80 0.3506 0.6752 0.0577 0.0299 1.830 11.535 9.305 1364.736 1.303 41.389 3.093 0.60 212818. 0.3690
|
|
53.12 0.3740 0.6965 0.0541 0.0290 1.774 11.180 8.722 1322.697 1.263 38.794 2.991 0.60 213168. 0.3455
|
|
56.44 0.3974 0.7150 0.0503 0.0279 1.708 10.765 8.113 1273.592 1.216 36.089 2.889 0.60 213534. 0.3220
|
|
59.76 0.4207 0.7304 0.0464 0.0267 1.633 10.291 7.483 1217.574 1.163 33.286 2.788 0.60 213915. 0.2983
|
|
63.08 0.4441 0.7423 0.0424 0.0253 1.549 9.761 6.835 1154.887 1.103 30.401 2.684 0.60 214313. 0.2745
|
|
66.40 0.4675 0.7504 0.0382 0.0238 1.456 9.177 6.171 1085.751 1.037 27.447 2.578 0.60 214727. 0.2505
|
|
69.72 0.4908 0.7538 0.0341 0.0222 1.355 8.540 5.494 1010.374 0.965 24.437 2.466 0.60 215157. 0.2261
|
|
73.04 0.5142 0.7515 0.0298 0.0204 1.246 7.852 4.807 928.985 0.887 21.382 2.347 0.60 215604. 0.2013
|
|
76.36 0.5376 0.7418 0.0255 0.0185 1.129 7.116 4.113 841.850 0.804 18.294 2.216 0.60 216066. 0.1758
|
|
79.68 0.5610 0.7220 0.0212 0.0164 1.005 6.333 3.415 749.301 0.716 15.188 2.067 0.60 216546. 0.1494
|
|
83.00 0.5843 0.6876 0.0168 0.0143 0.874 5.509 2.715 651.754 0.622 12.078 1.890 0.61 217041. 0.1218
|
|
86.32 0.6077 0.6305 0.0125 0.0121 0.737 4.646 2.019 549.729 0.525 8.981 1.666 0.61 217553. 0.0926
|
|
89.64 0.6311 0.5342 0.0082 0.0097 0.595 3.752 1.330 443.872 0.424 5.917 1.359 0.61 218082. 0.0613
|
|
92.96 0.6545 0.3605 0.0040 0.0074 0.449 2.831 0.653 334.951 0.320 2.905 0.884 0.61 218626. 0.0280
|
|
96.28 0.6778 -0.0088 -0.0001 0.0049 0.299 1.887 -0.010 223.271 0.213 -0.046 -0.021 0.61 219172. 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 0.0934 0.0304 2.475 14.184 18.227 1845.893 1.602 81.072 4.479 0.65 230301. 0.7480
|
|
3.65 0.0234 0.0696 0.0921 0.0309 2.513 14.399 17.973 1873.911 1.627 79.945 4.350 0.65 230450. 0.7215
|
|
7.30 0.0467 0.1352 0.0907 0.0313 2.549 14.603 17.697 1900.495 1.650 78.717 4.224 0.65 230611. 0.6950
|
|
10.95 0.0701 0.1968 0.0891 0.0317 2.582 14.792 17.397 1925.078 1.671 77.381 4.099 0.65 230786. 0.6688
|
|
14.60 0.0934 0.2545 0.0874 0.0321 2.611 14.961 17.071 1947.075 1.690 75.931 3.977 0.65 230974. 0.6427
|
|
18.25 0.1168 0.3086 0.0856 0.0324 2.636 15.105 16.717 1965.873 1.707 74.359 3.857 0.65 231177. 0.6169
|
|
21.90 0.1402 0.3591 0.0837 0.0327 2.656 15.220 16.335 1980.826 1.720 72.658 3.740 0.66 231395. 0.5913
|
|
25.55 0.1635 0.4062 0.0816 0.0328 2.670 15.301 15.922 1991.262 1.729 70.821 3.627 0.66 231629. 0.5661
|
|
29.20 0.1869 0.4501 0.0793 0.0329 2.677 15.341 15.477 1996.505 1.733 68.843 3.516 0.66 231878. 0.5411
|
|
32.85 0.2102 0.4909 0.0768 0.0329 2.677 15.336 15.000 1995.882 1.733 66.720 3.409 0.66 232143. 0.5164
|
|
36.50 0.2336 0.5288 0.0742 0.0328 2.667 15.281 14.489 1988.739 1.726 64.447 3.304 0.66 232425. 0.4920
|
|
40.15 0.2570 0.5638 0.0714 0.0326 2.648 15.171 13.944 1974.463 1.714 62.021 3.203 0.66 232724. 0.4679
|
|
43.80 0.2803 0.5961 0.0685 0.0322 2.618 15.003 13.364 1952.484 1.695 59.442 3.104 0.66 233040. 0.4439
|
|
47.45 0.3037 0.6258 0.0653 0.0317 2.578 14.771 12.749 1922.299 1.669 56.710 3.008 0.66 233373. 0.4202
|
|
51.10 0.3270 0.6528 0.0620 0.0311 2.526 14.472 12.101 1883.477 1.635 53.826 2.914 0.66 233723. 0.3966
|
|
54.75 0.3504 0.6773 0.0585 0.0303 2.462 14.105 11.420 1835.655 1.594 50.796 2.822 0.66 234091. 0.3730
|
|
58.40 0.3738 0.6990 0.0548 0.0293 2.385 13.666 10.706 1778.489 1.544 47.621 2.730 0.66 234476. 0.3495
|
|
62.05 0.3971 0.7180 0.0510 0.0282 2.295 13.153 9.961 1711.727 1.486 44.308 2.640 0.66 234878. 0.3259
|
|
65.70 0.4205 0.7340 0.0471 0.0270 2.193 12.567 9.189 1635.563 1.420 40.873 2.548 0.66 235298. 0.3022
|
|
69.35 0.4438 0.7466 0.0430 0.0256 2.079 11.913 8.394 1550.332 1.346 37.337 2.456 0.66 235736. 0.2783
|
|
73.00 0.4672 0.7555 0.0388 0.0240 1.953 11.190 7.580 1456.332 1.264 33.715 2.361 0.66 236192. 0.2542
|
|
76.65 0.4906 0.7598 0.0346 0.0223 1.816 10.403 6.749 1353.851 1.175 30.021 2.261 0.66 236665. 0.2298
|
|
80.30 0.5139 0.7586 0.0303 0.0205 1.667 9.553 5.906 1243.195 1.079 26.271 2.155 0.66 237156. 0.2049
|
|
83.95 0.5373 0.7501 0.0259 0.0185 1.508 8.642 5.054 1124.733 0.976 22.481 2.038 0.66 237665. 0.1792
|
|
87.60 0.5606 0.7318 0.0215 0.0165 1.340 7.675 4.196 998.911 0.867 18.666 1.905 0.66 238192. 0.1527
|
|
91.25 0.5840 0.6990 0.0171 0.0143 1.162 6.657 3.337 866.297 0.752 14.845 1.747 0.67 238737. 0.1249
|
|
94.90 0.6074 0.6437 0.0127 0.0120 0.976 5.591 2.482 727.599 0.632 11.039 1.547 0.67 239300. 0.0953
|
|
98.55 0.6307 0.5489 0.0084 0.0096 0.783 4.485 1.635 583.702 0.507 7.273 1.271 0.67 239880. 0.0635
|
|
102.20 0.6541 0.3744 0.0041 0.0072 0.584 3.348 0.803 435.672 0.378 3.571 0.836 0.67 240478. 0.0293
|
|
105.85 0.6774 -0.0098 -0.0001 0.0047 0.381 2.182 -0.013 283.930 0.246 -0.059 -0.021 0.67 241078. 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 0.0945 0.0309 3.264 17.146 21.956 2434.326 1.937 97.659 4.091 0.71 251215. 0.7498
|
|
3.98 0.0233 0.0693 0.0932 0.0314 3.313 17.402 21.658 2470.660 1.966 96.334 3.976 0.71 251377. 0.7238
|
|
7.96 0.0467 0.1347 0.0918 0.0318 3.360 17.646 21.332 2505.266 1.994 94.886 3.862 0.71 251553. 0.6978
|
|
11.94 0.0700 0.1962 0.0903 0.0322 3.403 17.872 20.978 2537.385 2.019 93.308 3.750 0.71 251744. 0.6718
|
|
15.91 0.0934 0.2539 0.0886 0.0326 3.441 18.075 20.591 2566.236 2.042 91.590 3.639 0.71 251951. 0.6460
|
|
19.89 0.1167 0.3080 0.0868 0.0329 3.475 18.250 20.172 2590.964 2.062 89.723 3.531 0.71 252173. 0.6204
|
|
23.87 0.1400 0.3585 0.0849 0.0332 3.501 18.388 19.716 2610.684 2.078 87.699 3.425 0.71 252411. 0.5950
|
|
27.85 0.1634 0.4056 0.0827 0.0333 3.519 18.486 19.224 2624.468 2.088 85.509 3.322 0.71 252667. 0.5698
|
|
31.83 0.1867 0.4496 0.0805 0.0334 3.529 18.534 18.693 2631.369 2.094 83.147 3.222 0.72 252939. 0.5450
|
|
35.81 0.2101 0.4905 0.0780 0.0334 3.528 18.528 18.122 2630.467 2.093 80.606 3.125 0.72 253230. 0.5203
|
|
39.79 0.2334 0.5285 0.0754 0.0333 3.515 18.460 17.510 2620.885 2.086 77.883 3.030 0.72 253538. 0.4960
|
|
43.76 0.2567 0.5638 0.0726 0.0330 3.489 18.326 16.855 2601.805 2.070 74.972 2.938 0.72 253865. 0.4719
|
|
47.74 0.2801 0.5963 0.0696 0.0327 3.450 18.119 16.159 2572.481 2.047 71.874 2.849 0.72 254210. 0.4480
|
|
51.72 0.3034 0.6263 0.0664 0.0322 3.396 17.836 15.420 2532.241 2.015 68.589 2.762 0.72 254574. 0.4243
|
|
55.70 0.3268 0.6537 0.0630 0.0315 3.326 17.472 14.640 2480.523 1.974 65.118 2.677 0.72 254957. 0.4007
|
|
59.68 0.3501 0.6785 0.0595 0.0307 3.241 17.023 13.819 2416.848 1.923 61.467 2.593 0.72 255358. 0.3771
|
|
63.66 0.3735 0.7007 0.0558 0.0297 3.139 16.487 12.959 2340.778 1.863 57.640 2.511 0.72 255779. 0.3536
|
|
67.64 0.3968 0.7202 0.0519 0.0286 3.020 15.862 12.060 2251.967 1.792 53.642 2.429 0.72 256219. 0.3300
|
|
71.61 0.4201 0.7368 0.0479 0.0273 2.884 15.148 11.128 2150.657 1.711 49.496 2.347 0.72 256677. 0.3062
|
|
75.59 0.4435 0.7501 0.0438 0.0259 2.732 14.350 10.167 2037.297 1.621 45.224 2.264 0.72 257155. 0.2823
|
|
79.57 0.4668 0.7598 0.0395 0.0243 2.564 13.469 9.183 1912.285 1.522 40.846 2.178 0.72 257652. 0.2582
|
|
83.55 0.4902 0.7651 0.0352 0.0226 2.382 12.509 8.179 1776.014 1.413 36.379 2.089 0.72 258168. 0.2337
|
|
87.53 0.5135 0.7649 0.0308 0.0207 2.184 11.473 7.159 1628.922 1.296 31.842 1.993 0.72 258704. 0.2086
|
|
91.51 0.5368 0.7576 0.0264 0.0187 1.973 10.365 6.127 1471.536 1.171 27.253 1.889 0.72 259259. 0.1829
|
|
95.49 0.5602 0.7406 0.0219 0.0166 1.749 9.188 5.088 1304.511 1.038 22.633 1.769 0.73 259833. 0.1561
|
|
99.46 0.5835 0.7093 0.0174 0.0143 1.514 7.950 4.048 1128.683 0.898 18.004 1.627 0.73 260427. 0.1280
|
|
103.44 0.6069 0.6552 0.0130 0.0120 1.267 6.657 3.011 945.118 0.752 13.391 1.445 0.73 261040. 0.0981
|
|
107.42 0.6302 0.5611 0.0085 0.0096 1.013 5.319 1.984 755.149 0.601 8.824 1.192 0.73 261673. 0.0656
|
|
111.40 0.6535 0.3850 0.0042 0.0071 0.751 3.947 0.974 560.382 0.446 4.332 0.788 0.73 262325. 0.0304
|
|
115.38 0.6769 -0.0103 -0.0001 0.0046 0.485 2.546 -0.016 361.515 0.288 -0.072 -0.020 0.73 262978. 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 0.0958 0.0321 4.304 20.867 26.122 3209.439 2.358 116.192 3.692 0.77 272119. 0.7381
|
|
4.30 0.0233 0.0679 0.0946 0.0325 4.358 21.131 25.779 3250.044 2.387 114.667 3.598 0.77 272296. 0.7146
|
|
8.61 0.0466 0.1322 0.0932 0.0328 4.410 21.381 25.403 3288.513 2.416 112.995 3.504 0.77 272487. 0.6908
|
|
12.91 0.0699 0.1931 0.0917 0.0332 4.458 21.611 24.992 3323.958 2.442 111.165 3.410 0.77 272695. 0.6669
|
|
17.22 0.0932 0.2504 0.0900 0.0335 4.500 21.816 24.543 3355.464 2.465 109.168 3.318 0.77 272919. 0.6429
|
|
21.52 0.1165 0.3044 0.0882 0.0338 4.535 21.989 24.054 3382.022 2.484 106.991 3.226 0.77 273160. 0.6189
|
|
25.83 0.1399 0.3550 0.0863 0.0340 4.563 22.123 23.521 3402.568 2.499 104.623 3.135 0.77 273419. 0.5948
|
|
30.13 0.1632 0.4024 0.0842 0.0341 4.581 22.210 22.944 3415.966 2.509 102.055 3.046 0.77 273697. 0.5708
|
|
34.43 0.1865 0.4467 0.0819 0.0342 4.588 22.243 22.320 3421.052 2.513 99.278 2.959 0.77 273993. 0.5469
|
|
38.74 0.2098 0.4880 0.0794 0.0341 4.582 22.214 21.647 3416.649 2.510 96.284 2.874 0.78 274308. 0.5230
|
|
43.04 0.2331 0.5265 0.0767 0.0340 4.562 22.116 20.924 3401.593 2.499 93.068 2.790 0.78 274643. 0.4992
|
|
47.35 0.2564 0.5621 0.0739 0.0337 4.526 21.942 20.149 3374.756 2.479 89.625 2.708 0.78 274998. 0.4755
|
|
51.65 0.2797 0.5951 0.0709 0.0333 4.472 21.684 19.324 3335.076 2.450 85.954 2.628 0.78 275373. 0.4519
|
|
55.96 0.3030 0.6255 0.0677 0.0328 4.401 21.336 18.448 3281.587 2.411 82.055 2.550 0.78 275768. 0.4284
|
|
60.26 0.3263 0.6533 0.0643 0.0321 4.309 20.893 17.521 3213.441 2.360 77.932 2.473 0.78 276183. 0.4049
|
|
64.56 0.3496 0.6786 0.0607 0.0313 4.197 20.350 16.544 3129.918 2.299 73.589 2.398 0.78 276618. 0.3815
|
|
68.87 0.3729 0.7013 0.0569 0.0303 4.064 19.703 15.520 3030.392 2.226 69.033 2.323 0.78 277074. 0.3580
|
|
73.17 0.3963 0.7214 0.0530 0.0291 3.908 18.948 14.449 2914.372 2.141 64.270 2.249 0.78 277551. 0.3344
|
|
77.48 0.4196 0.7385 0.0489 0.0278 3.731 18.089 13.337 2782.201 2.044 59.325 2.174 0.78 278048. 0.3106
|
|
81.78 0.4429 0.7525 0.0447 0.0263 3.533 17.129 12.191 2634.532 1.935 54.225 2.099 0.78 278565. 0.2867
|
|
86.09 0.4662 0.7627 0.0404 0.0247 3.315 16.072 11.015 2472.000 1.816 48.994 2.021 0.78 279104. 0.2624
|
|
90.39 0.4895 0.7685 0.0360 0.0229 3.078 14.923 9.814 2295.286 1.686 43.654 1.939 0.78 279663. 0.2377
|
|
94.69 0.5128 0.7687 0.0315 0.0210 2.823 13.687 8.594 2105.124 1.546 38.226 1.852 0.78 280242. 0.2123
|
|
99.00 0.5361 0.7614 0.0270 0.0190 2.551 12.369 7.359 1902.420 1.397 32.732 1.754 0.78 280843. 0.1862
|
|
103.30 0.5594 0.7439 0.0224 0.0169 2.264 10.977 6.114 1688.313 1.240 27.196 1.643 0.79 281464. 0.1589
|
|
107.61 0.5827 0.7111 0.0178 0.0146 1.964 9.520 4.866 1464.199 1.076 21.644 1.507 0.79 282106. 0.1301
|
|
111.91 0.6060 0.6542 0.0133 0.0123 1.652 8.009 3.621 1231.811 0.905 16.107 1.333 0.79 282770. 0.0993
|
|
116.22 0.6294 0.5555 0.0088 0.0099 1.332 6.458 2.387 993.251 0.730 10.619 1.090 0.79 283454. 0.0659
|
|
120.52 0.6527 0.3744 0.0043 0.0075 1.007 4.882 1.173 750.949 0.552 5.218 0.709 0.79 284158. 0.0300
|
|
124.82 0.6760 -0.0091 -0.0001 0.0051 0.679 3.290 -0.019 506.023 0.372 -0.083 -0.017 0.79 284865. 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 0.0973 0.0349 5.844 26.311 30.753 4358.014 2.973 136.791 3.201 0.83 293013. 0.6943
|
|
4.63 0.0233 0.0637 0.0960 0.0351 5.891 26.522 30.367 4392.992 2.996 135.073 3.135 0.83 293203. 0.6759
|
|
9.27 0.0466 0.1247 0.0947 0.0354 5.933 26.712 29.941 4424.509 3.018 133.179 3.069 0.83 293410. 0.6570
|
|
13.90 0.0699 0.1830 0.0932 0.0356 5.970 26.876 29.474 4451.602 3.036 131.099 3.003 0.83 293635. 0.6378
|
|
18.53 0.0932 0.2386 0.0916 0.0358 5.999 27.007 28.961 4473.292 3.051 128.817 2.936 0.83 293877. 0.6182
|
|
23.17 0.1165 0.2915 0.0898 0.0359 6.019 27.099 28.399 4488.515 3.062 126.321 2.870 0.83 294138. 0.5982
|
|
27.80 0.1398 0.3416 0.0879 0.0360 6.029 27.144 27.787 4496.120 3.067 123.595 2.803 0.83 294418. 0.5780
|
|
32.43 0.1631 0.3891 0.0858 0.0359 6.028 27.137 27.120 4494.908 3.066 120.628 2.737 0.83 294719. 0.5575
|
|
37.07 0.1864 0.4339 0.0835 0.0359 6.013 27.069 26.396 4483.625 3.058 117.409 2.670 0.83 295039. 0.5367
|
|
41.70 0.2097 0.4761 0.0810 0.0357 5.982 26.932 25.613 4460.982 3.043 113.928 2.604 0.83 295381. 0.5156
|
|
46.33 0.2330 0.5157 0.0783 0.0354 5.935 26.719 24.770 4425.703 3.019 110.177 2.539 0.84 295743. 0.4942
|
|
50.97 0.2563 0.5526 0.0755 0.0350 5.869 26.423 23.865 4376.552 2.985 106.152 2.473 0.84 296127. 0.4726
|
|
55.60 0.2796 0.5871 0.0724 0.0345 5.783 26.035 22.898 4312.352 2.941 101.850 2.408 0.84 296532. 0.4508
|
|
60.23 0.3029 0.6189 0.0692 0.0338 5.675 25.550 21.869 4231.999 2.887 97.272 2.344 0.84 296959. 0.4287
|
|
64.87 0.3262 0.6482 0.0657 0.0331 5.544 24.961 20.778 4134.487 2.820 92.421 2.279 0.84 297408. 0.4064
|
|
69.50 0.3495 0.6750 0.0621 0.0321 5.389 24.263 19.628 4018.917 2.741 87.306 2.215 0.84 297879. 0.3839
|
|
74.13 0.3728 0.6989 0.0583 0.0311 5.210 23.456 18.420 3885.144 2.650 81.931 2.150 0.84 298371. 0.3610
|
|
78.77 0.3961 0.7197 0.0543 0.0299 5.006 22.539 17.155 3733.315 2.546 76.305 2.084 0.84 298886. 0.3377
|
|
83.40 0.4194 0.7373 0.0501 0.0285 4.778 21.510 15.840 3562.802 2.430 70.457 2.017 0.84 299422. 0.3140
|
|
88.04 0.4427 0.7511 0.0458 0.0270 4.526 20.378 14.483 3375.382 2.302 64.419 1.946 0.84 299981. 0.2897
|
|
92.67 0.4660 0.7606 0.0414 0.0254 4.252 19.144 13.089 3171.006 2.163 58.220 1.872 0.84 300561. 0.2650
|
|
97.30 0.4893 0.7650 0.0369 0.0236 3.957 17.812 11.665 2950.386 2.012 51.886 1.793 0.84 301164. 0.2396
|
|
101.94 0.5126 0.7627 0.0323 0.0217 3.641 16.392 10.216 2715.053 1.852 45.442 1.707 0.84 301789. 0.2134
|
|
106.57 0.5359 0.7517 0.0277 0.0197 3.308 14.891 8.749 2466.558 1.682 38.917 1.609 0.85 302436. 0.1862
|
|
111.20 0.5592 0.7284 0.0230 0.0176 2.960 13.324 7.270 2206.924 1.505 32.338 1.494 0.85 303106. 0.1576
|
|
115.84 0.5825 0.6875 0.0183 0.0155 2.600 11.704 5.786 1938.540 1.322 25.736 1.354 0.85 303797. 0.1274
|
|
120.47 0.6058 0.6197 0.0136 0.0133 2.232 10.046 4.305 1664.062 1.135 19.147 1.173 0.85 304512. 0.0952
|
|
125.10 0.6291 0.5087 0.0090 0.0111 1.860 8.372 2.836 1386.631 0.946 12.614 0.928 0.85 305248. 0.0611
|
|
129.74 0.6524 0.3230 0.0044 0.0089 1.488 6.699 1.389 1109.651 0.757 6.180 0.568 0.85 306007. 0.0262
|
|
134.37 0.6757 -0.0097 -0.0001 0.0067 1.118 5.035 -0.030 834.039 0.569 -0.135 -0.016 0.85 306770. 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 0.0984 0.0399 8.234 34.599 35.728 6140.271 3.909 158.917 2.639 0.89 313906. 0.6171
|
|
5.03 0.0236 0.0573 0.0973 0.0401 8.264 34.726 35.306 6162.669 3.923 157.039 2.598 0.89 314112. 0.6040
|
|
10.06 0.0472 0.1128 0.0960 0.0402 8.285 34.811 34.836 6177.816 3.933 154.951 2.558 0.89 314337. 0.5905
|
|
15.10 0.0709 0.1666 0.0945 0.0402 8.294 34.849 34.315 6184.492 3.937 152.635 2.517 0.89 314581. 0.5767
|
|
20.13 0.0945 0.2185 0.0929 0.0402 8.290 34.832 33.739 6181.489 3.935 150.072 2.476 0.89 314845. 0.5625
|
|
25.16 0.1181 0.2685 0.0912 0.0401 8.271 34.753 33.103 6167.598 3.926 147.244 2.434 0.89 315131. 0.5479
|
|
30.19 0.1417 0.3168 0.0893 0.0399 8.236 34.607 32.404 6141.629 3.910 144.132 2.393 0.89 315438. 0.5329
|
|
35.22 0.1653 0.3631 0.0872 0.0397 8.184 34.386 31.637 6102.461 3.885 140.721 2.351 0.89 315767. 0.5174
|
|
40.26 0.1889 0.4076 0.0848 0.0393 8.112 34.085 30.800 6048.906 3.851 136.996 2.309 0.89 316119. 0.5014
|
|
45.29 0.2126 0.4501 0.0823 0.0389 8.019 33.695 29.888 5979.855 3.807 132.944 2.267 0.89 316494. 0.4848
|
|
50.32 0.2362 0.4906 0.0796 0.0383 7.905 33.214 28.902 5894.459 3.753 128.557 2.224 0.90 316892. 0.4677
|
|
55.35 0.2598 0.5291 0.0767 0.0377 7.767 32.635 27.839 5791.694 3.687 123.830 2.180 0.90 317314. 0.4500
|
|
60.38 0.2834 0.5653 0.0736 0.0369 7.604 31.953 26.699 5670.576 3.610 118.759 2.136 0.90 317760. 0.4317
|
|
65.42 0.3070 0.5994 0.0702 0.0360 7.416 31.161 25.483 5530.118 3.521 113.346 2.090 0.90 318230. 0.4127
|
|
70.45 0.3306 0.6311 0.0666 0.0349 7.200 30.256 24.190 5369.376 3.418 107.596 2.043 0.90 318724. 0.3931
|
|
75.48 0.3543 0.6603 0.0629 0.0337 6.957 29.231 22.823 5187.490 3.302 101.518 1.996 0.90 319242. 0.3729
|
|
80.51 0.3779 0.6869 0.0589 0.0324 6.684 28.084 21.385 4983.937 3.173 95.119 1.946 0.90 319784. 0.3520
|
|
85.54 0.4015 0.7097 0.0548 0.0310 6.388 26.844 19.877 4763.865 3.033 88.412 1.892 0.90 320350. 0.3300
|
|
90.58 0.4251 0.7284 0.0504 0.0294 6.071 25.509 18.309 4526.951 2.882 81.437 1.834 0.90 320941. 0.3070
|
|
95.61 0.4487 0.7418 0.0460 0.0278 5.735 24.099 16.689 4276.871 2.723 74.231 1.770 0.90 321555. 0.2828
|
|
100.64 0.4723 0.7473 0.0414 0.0262 5.395 22.670 15.024 4023.165 2.561 66.825 1.694 0.90 322194. 0.2568
|
|
105.67 0.4960 0.7450 0.0367 0.0244 5.039 21.172 13.322 3757.283 2.392 59.258 1.608 0.90 322857. 0.2296
|
|
110.71 0.5196 0.7335 0.0319 0.0226 4.665 19.603 11.593 3478.896 2.215 51.564 1.511 0.90 323544. 0.2013
|
|
115.74 0.5432 0.7100 0.0271 0.0207 4.278 17.977 9.842 3190.356 2.031 43.778 1.399 0.91 324255. 0.1717
|
|
120.77 0.5668 0.6703 0.0223 0.0188 3.882 16.313 8.080 2894.966 1.843 35.941 1.266 0.91 324991. 0.1408
|
|
125.80 0.5904 0.6085 0.0174 0.0169 3.482 14.632 6.316 2596.794 1.653 28.096 1.103 0.91 325751. 0.1085
|
|
130.83 0.6140 0.5161 0.0126 0.0150 3.084 12.958 4.562 2299.557 1.464 20.292 0.900 0.91 326535. 0.0752
|
|
135.87 0.6377 0.3809 0.0078 0.0131 2.692 11.310 2.830 2007.238 1.278 12.588 0.640 0.91 327345. 0.0421
|
|
140.90 0.6613 0.1843 0.0031 0.0112 2.311 9.712 1.134 1723.589 1.097 5.044 0.298 0.91 328177. 0.0124
|
|
145.93 0.6849
|
|
|
|
|
|
|
|
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 0.0980 0.0455 11.382 44.837 40.473 8487.651 5.066 180.024 2.163 0.95 334842. 0.5382
|
|
5.36 0.0236 0.0500 0.0970 0.0457 11.435 45.046 40.065 8527.203 5.089 178.210 2.131 0.95 335056. 0.5277
|
|
10.71 0.0471 0.0986 0.0959 0.0458 11.473 45.196 39.606 8555.498 5.106 176.167 2.100 0.95 335290. 0.5169
|
|
16.07 0.0707 0.1458 0.0946 0.0459 11.492 45.272 39.090 8569.884 5.115 173.872 2.069 0.95 335545. 0.5060
|
|
21.43 0.0943 0.1915 0.0932 0.0459 11.489 45.260 38.511 8567.716 5.113 171.297 2.039 0.95 335821. 0.4949
|
|
26.78 0.1179 0.2360 0.0917 0.0458 11.461 45.148 37.863 8546.475 5.101 168.416 2.009 0.95 336121. 0.4837
|
|
32.14 0.1414 0.2791 0.0899 0.0456 11.404 44.923 37.141 8503.890 5.075 165.202 1.981 0.95 336444. 0.4723
|
|
37.50 0.1650 0.3211 0.0880 0.0452 11.316 44.575 36.338 8438.022 5.036 161.631 1.953 0.95 336791. 0.4606
|
|
42.86 0.1886 0.3619 0.0858 0.0447 11.194 44.097 35.450 8347.422 4.982 157.683 1.926 0.95 337163. 0.4486
|
|
48.21 0.2121 0.4015 0.0835 0.0441 11.038 43.482 34.474 8231.013 4.913 153.338 1.900 0.95 337561. 0.4363
|
|
53.57 0.2357 0.4399 0.0809 0.0433 10.846 42.727 33.405 8088.123 4.827 148.585 1.873 0.95 337983. 0.4235
|
|
58.93 0.2593 0.4771 0.0781 0.0424 10.619 41.830 32.242 7918.408 4.726 143.413 1.847 0.96 338432. 0.4102
|
|
64.28 0.2828 0.5129 0.0750 0.0414 10.355 40.791 30.984 7721.671 4.609 137.818 1.820 0.96 338907. 0.3963
|
|
69.64 0.3064 0.5473 0.0717 0.0402 10.055 39.608 29.631 7497.844 4.475 131.800 1.793 0.96 339407. 0.3817
|
|
75.00 0.3300 0.5800 0.0682 0.0388 9.718 38.284 28.185 7247.027 4.325 125.366 1.764 0.96 339933. 0.3663
|
|
80.35 0.3536 0.6109 0.0645 0.0373 9.346 36.818 26.647 6969.571 4.160 118.527 1.734 0.96 340485. 0.3502
|
|
85.71 0.3771 0.6398 0.0606 0.0357 8.939 35.213 25.022 6665.812 3.978 111.296 1.703 0.96 341063. 0.3331
|
|
91.07 0.4007 0.6661 0.0564 0.0340 8.499 33.480 23.312 6337.712 3.783 103.692 1.668 0.96 341667. 0.3151
|
|
96.43 0.4243 0.6878 0.0521 0.0322 8.047 31.700 21.527 6000.798 3.581 95.752 1.627 0.96 342296. 0.2953
|
|
101.78 0.4478 0.7044 0.0476 0.0303 7.582 29.867 19.679 5653.805 3.374 87.531 1.579 0.96 342951. 0.2739
|
|
107.14 0.4714 0.7130 0.0430 0.0285 7.122 28.056 17.775 5310.945 3.170 79.064 1.518 0.96 343632. 0.2504
|
|
112.50 0.4950 0.7042 0.0383 0.0269 6.738 26.542 15.818 5024.313 2.999 70.358 1.428 0.96 344338. 0.2222
|
|
117.85 0.5186 0.6842 0.0335 0.0254 6.350 25.015 13.826 4735.386 2.826 61.499 1.324 0.96 345070. 0.1926
|
|
123.21 0.5421 0.6513 0.0286 0.0238 5.958 23.472 11.812 4443.248 2.652 52.541 1.206 0.97 345827. 0.1621
|
|
128.57 0.5657 0.6028 0.0237 0.0222 5.568 21.932 9.789 4151.712 2.478 43.541 1.069 0.97 346610. 0.1309
|
|
133.92 0.5893 0.5355 0.0188 0.0207 5.182 20.411 7.770 3863.862 2.306 34.563 0.912 0.97 347418. 0.0995
|
|
139.28 0.6128 0.4462 0.0140 0.0192 4.805 18.930 5.773 3583.342 2.139 25.677 0.731 0.97 348253. 0.0687
|
|
144.64 0.6364 0.3310 0.0092 0.0178 4.444 17.506 3.814 3313.848 1.978 16.963 0.522 0.97 349115. 0.0399
|
|
150.00 0.6600 0.1865 0.0046 0.0164 4.100 16.149 1.911 3057.077 1.825 8.502 0.284 0.97 350005. 0.0153
|
|
155.35 0.6836 0.0062 0.0001 0.0150 3.757 14.801 0.056 2801.887 1.672 0.249 0.009 0.97 350940. 0.0001
|
|
|
|
|
|
|