649 lines
115 KiB
Plaintext
649 lines
115 KiB
Plaintext
13x8 (13x8.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 0.0982 0.0484 0.001 0.089 0.088 1.058 0.010 0.392 37.741 0.05 16340. 0.5074
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0.33 0.0269 0.0532 0.0970 0.0490 0.001 0.091 0.087 1.071 0.010 0.387 36.806 0.05 16352. 0.4918
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0.66 0.0538 0.1037 0.0957 0.0496 0.001 0.092 0.086 1.085 0.010 0.381 35.863 0.05 16365. 0.4759
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0.99 0.0806 0.1514 0.0942 0.0502 0.001 0.093 0.084 1.097 0.010 0.376 34.918 0.05 16380. 0.4598
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1.32 0.1075 0.1964 0.0926 0.0507 0.001 0.094 0.083 1.108 0.011 0.369 33.973 0.05 16395. 0.4434
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1.65 0.1344 0.2387 0.0908 0.0511 0.001 0.094 0.081 1.118 0.011 0.362 33.029 0.05 16412. 0.4269
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1.98 0.1613 0.2783 0.0888 0.0515 0.002 0.095 0.080 1.125 0.011 0.354 32.090 0.05 16431. 0.4103
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2.31 0.1882 0.3152 0.0867 0.0518 0.002 0.096 0.078 1.131 0.011 0.346 31.155 0.05 16451. 0.3935
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2.64 0.2151 0.3495 0.0844 0.0519 0.002 0.096 0.076 1.134 0.011 0.336 30.226 0.05 16472. 0.3766
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2.97 0.2419 0.3811 0.0818 0.0519 0.002 0.096 0.073 1.135 0.011 0.326 29.301 0.05 16495. 0.3595
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3.30 0.2688 0.4102 0.0791 0.0518 0.002 0.096 0.071 1.133 0.011 0.315 28.381 0.05 16520. 0.3424
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3.63 0.2957 0.4366 0.0761 0.0516 0.002 0.095 0.068 1.127 0.011 0.304 27.463 0.05 16546. 0.3251
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3.96 0.3226 0.4603 0.0730 0.0512 0.001 0.094 0.065 1.118 0.011 0.291 26.544 0.05 16574. 0.3076
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4.29 0.3495 0.4814 0.0697 0.0506 0.001 0.093 0.062 1.105 0.011 0.278 25.621 0.05 16603. 0.2900
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4.62 0.3764 0.4996 0.0661 0.0498 0.001 0.092 0.059 1.088 0.010 0.264 24.691 0.05 16634. 0.2723
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4.94 0.4032 0.5148 0.0624 0.0489 0.001 0.090 0.056 1.068 0.010 0.249 23.750 0.05 16667. 0.2545
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5.27 0.4301 0.5270 0.0585 0.0478 0.001 0.088 0.052 1.044 0.010 0.233 22.790 0.05 16701. 0.2365
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5.60 0.4570 0.5358 0.0545 0.0465 0.001 0.086 0.049 1.017 0.010 0.217 21.807 0.05 16737. 0.2185
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5.93 0.4839 0.5408 0.0504 0.0451 0.001 0.083 0.045 0.986 0.009 0.201 20.790 0.05 16775. 0.2002
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6.26 0.5108 0.5418 0.0462 0.0435 0.001 0.080 0.041 0.951 0.009 0.184 19.732 0.05 16814. 0.1819
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6.59 0.5377 0.5381 0.0419 0.0418 0.001 0.077 0.038 0.914 0.009 0.167 18.618 0.05 16855. 0.1634
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6.92 0.5645 0.5291 0.0374 0.0399 0.001 0.074 0.034 0.873 0.008 0.149 17.434 0.05 16898. 0.1447
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7.25 0.5914 0.5137 0.0329 0.0379 0.001 0.070 0.030 0.828 0.008 0.131 16.158 0.05 16942. 0.1257
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7.58 0.6183 0.4907 0.0283 0.0357 0.001 0.066 0.025 0.780 0.007 0.113 14.763 0.05 16988. 0.1066
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7.91 0.6452 0.4582 0.0237 0.0334 0.001 0.062 0.021 0.729 0.007 0.095 13.212 0.05 17036. 0.0873
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8.24 0.6721 0.4138 0.0190 0.0309 0.001 0.057 0.017 0.675 0.006 0.076 11.452 0.05 17085. 0.0678
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8.57 0.6989 0.3536 0.0143 0.0283 0.001 0.052 0.013 0.618 0.006 0.057 9.411 0.05 17136. 0.0483
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8.90 0.7258 0.2722 0.0096 0.0255 0.001 0.047 0.009 0.558 0.005 0.038 6.975 0.05 17189. 0.0293
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9.23 0.7527 0.1607 0.0048 0.0227 0.001 0.042 0.004 0.495 0.005 0.019 3.972 0.05 17243. 0.0119
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9.56 0.7796 0.0046 0.0001 0.0197 0.001 0.036 0.000 0.430 0.004 0.000 0.111 0.05 17299. 0.0001
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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 0.0987 0.0421 0.010 0.311 0.354 7.362 0.035 1.574 21.801 0.10 32680. 0.5876
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0.66 0.0271 0.0618 0.0975 0.0428 0.010 0.316 0.350 7.483 0.036 1.555 21.189 0.10 32704. 0.5677
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1.33 0.0542 0.1200 0.0962 0.0435 0.010 0.321 0.345 7.601 0.036 1.534 20.578 0.10 32731. 0.5476
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1.99 0.0813 0.1746 0.0947 0.0441 0.010 0.326 0.340 7.713 0.037 1.511 19.971 0.10 32760. 0.5274
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2.66 0.1084 0.2259 0.0931 0.0447 0.010 0.330 0.334 7.816 0.037 1.485 19.371 0.10 32791. 0.5071
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3.32 0.1356 0.2737 0.0913 0.0452 0.011 0.334 0.327 7.907 0.038 1.456 18.778 0.10 32826. 0.4868
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3.99 0.1627 0.3182 0.0894 0.0457 0.011 0.337 0.320 7.985 0.038 1.425 18.195 0.10 32863. 0.4666
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4.65 0.1898 0.3595 0.0872 0.0460 0.011 0.340 0.313 8.046 0.038 1.390 17.621 0.10 32904. 0.4464
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5.32 0.2169 0.3978 0.0848 0.0463 0.011 0.342 0.304 8.087 0.039 1.353 17.058 0.10 32947. 0.4263
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5.98 0.2440 0.4330 0.0823 0.0464 0.011 0.343 0.295 8.106 0.039 1.312 16.505 0.10 32994. 0.4062
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6.65 0.2711 0.4653 0.0795 0.0463 0.011 0.342 0.285 8.100 0.039 1.268 15.962 0.10 33044. 0.3862
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7.31 0.2982 0.4947 0.0765 0.0461 0.011 0.341 0.274 8.067 0.039 1.221 15.428 0.10 33097. 0.3662
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7.98 0.3253 0.5213 0.0734 0.0458 0.011 0.338 0.263 8.004 0.038 1.170 14.902 0.10 33153. 0.3463
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8.64 0.3524 0.5450 0.0700 0.0453 0.011 0.334 0.251 7.911 0.038 1.116 14.382 0.10 33213. 0.3264
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9.31 0.3795 0.5659 0.0664 0.0445 0.010 0.329 0.238 7.785 0.037 1.059 13.866 0.10 33276. 0.3065
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9.97 0.4067 0.5838 0.0626 0.0436 0.010 0.322 0.225 7.628 0.036 0.999 13.352 0.10 33343. 0.2867
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10.64 0.4338 0.5987 0.0587 0.0426 0.010 0.314 0.211 7.440 0.036 0.937 12.836 0.10 33412. 0.2669
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11.30 0.4609 0.6103 0.0547 0.0413 0.010 0.305 0.196 7.221 0.034 0.872 12.316 0.10 33485. 0.2471
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11.97 0.4880 0.6184 0.0505 0.0399 0.009 0.295 0.181 6.971 0.033 0.806 11.786 0.10 33562. 0.2273
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12.63 0.5151 0.6225 0.0463 0.0383 0.009 0.283 0.166 6.691 0.032 0.738 11.241 0.10 33642. 0.2074
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13.30 0.5422 0.6222 0.0419 0.0365 0.009 0.270 0.150 6.381 0.030 0.668 10.673 0.10 33725. 0.1874
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13.96 0.5693 0.6167 0.0374 0.0346 0.008 0.255 0.134 6.040 0.029 0.597 10.075 0.10 33812. 0.1672
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14.63 0.5964 0.6049 0.0329 0.0324 0.008 0.240 0.118 5.670 0.027 0.524 9.433 0.10 33902. 0.1468
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15.29 0.6235 0.5853 0.0283 0.0301 0.007 0.223 0.101 5.270 0.025 0.451 8.730 0.10 33995. 0.1260
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15.96 0.6507 0.5555 0.0236 0.0277 0.006 0.205 0.085 4.841 0.023 0.377 7.941 0.10 34092. 0.1047
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16.62 0.6778 0.5122 0.0189 0.0251 0.006 0.185 0.068 4.383 0.021 0.302 7.029 0.11 34192. 0.0830
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17.29 0.7049 0.4497 0.0142 0.0223 0.005 0.165 0.051 3.898 0.019 0.227 5.934 0.11 34295. 0.0607
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17.95 0.7320 0.3587 0.0095 0.0194 0.005 0.143 0.034 3.387 0.016 0.151 4.557 0.11 34402. 0.0381
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18.62 0.7591 0.2219 0.0048 0.0163 0.004 0.120 0.017 2.851 0.014 0.076 2.719 0.11 34512. 0.0161
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19.28 0.7862 0.0037 0.0001 0.0131 0.003 0.097 0.000 2.292 0.011 0.001 0.044 0.11 34625. 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 0.0990 0.0395 0.031 0.657 0.799 23.327 0.074 3.553 15.530 0.15 49019. 0.6289
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1.01 0.0276 0.0670 0.0978 0.0403 0.032 0.669 0.789 23.762 0.076 3.510 15.062 0.15 49056. 0.6062
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2.03 0.0551 0.1298 0.0965 0.0410 0.032 0.681 0.778 24.184 0.077 3.462 14.597 0.15 49097. 0.5835
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3.04 0.0827 0.1886 0.0950 0.0417 0.033 0.693 0.766 24.586 0.078 3.408 14.137 0.15 49141. 0.5607
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4.06 0.1103 0.2434 0.0934 0.0423 0.033 0.703 0.753 24.958 0.079 3.349 13.684 0.15 49190. 0.5381
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5.07 0.1379 0.2944 0.0915 0.0429 0.034 0.713 0.738 25.291 0.081 3.284 13.240 0.15 49243. 0.5155
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6.09 0.1654 0.3417 0.0895 0.0433 0.034 0.721 0.722 25.575 0.081 3.212 12.806 0.15 49301. 0.4930
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7.10 0.1930 0.3854 0.0873 0.0437 0.035 0.727 0.704 25.799 0.082 3.132 12.381 0.15 49363. 0.4708
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8.11 0.2206 0.4257 0.0849 0.0440 0.035 0.731 0.685 25.955 0.083 3.046 11.967 0.15 49430. 0.4487
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9.13 0.2482 0.4628 0.0823 0.0441 0.035 0.733 0.664 26.031 0.083 2.952 11.563 0.15 49502. 0.4268
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10.14 0.2757 0.4967 0.0794 0.0441 0.035 0.733 0.641 26.018 0.083 2.850 11.169 0.15 49579. 0.4051
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11.16 0.3033 0.5275 0.0764 0.0439 0.035 0.730 0.616 25.908 0.082 2.740 10.784 0.15 49661. 0.3835
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12.17 0.3309 0.5554 0.0731 0.0435 0.034 0.724 0.590 25.693 0.082 2.622 10.408 0.15 49748. 0.3621
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13.19 0.3584 0.5803 0.0696 0.0430 0.034 0.715 0.561 25.366 0.081 2.497 10.039 0.16 49840. 0.3408
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14.20 0.3860 0.6023 0.0659 0.0422 0.033 0.702 0.532 24.926 0.079 2.365 9.675 0.16 49937. 0.3197
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15.22 0.4136 0.6214 0.0621 0.0413 0.033 0.687 0.501 24.374 0.078 2.227 9.315 0.16 50040. 0.2986
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16.23 0.4412 0.6373 0.0581 0.0402 0.032 0.668 0.468 23.709 0.075 2.083 8.958 0.16 50148. 0.2777
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17.24 0.4687 0.6500 0.0539 0.0389 0.031 0.646 0.435 22.934 0.073 1.934 8.599 0.16 50261. 0.2569
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18.26 0.4963 0.6592 0.0496 0.0374 0.030 0.621 0.400 22.048 0.070 1.781 8.236 0.16 50379. 0.2361
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19.27 0.5239 0.6645 0.0453 0.0357 0.028 0.593 0.365 21.052 0.067 1.624 7.864 0.16 50502. 0.2153
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20.29 0.5515 0.6652 0.0408 0.0338 0.027 0.562 0.329 19.946 0.063 1.463 7.479 0.16 50631. 0.1944
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21.30 0.5790 0.6606 0.0362 0.0317 0.025 0.528 0.292 18.732 0.060 1.299 7.073 0.16 50765. 0.1732
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22.32 0.6066 0.6493 0.0316 0.0295 0.023 0.490 0.255 17.408 0.055 1.133 6.637 0.16 50904. 0.1518
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23.33 0.6342 0.6297 0.0269 0.0271 0.021 0.450 0.217 15.978 0.051 0.965 6.156 0.16 51049. 0.1299
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24.34 0.6617 0.5986 0.0221 0.0245 0.019 0.407 0.179 14.442 0.046 0.794 5.609 0.16 51198. 0.1074
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25.36 0.6893 0.5515 0.0174 0.0217 0.017 0.361 0.140 12.804 0.041 0.623 4.961 0.16 51353. 0.0841
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26.37 0.7169 0.4802 0.0126 0.0188 0.015 0.312 0.101 11.067 0.035 0.451 4.153 0.16 51513. 0.0599
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27.39 0.7445 0.3691 0.0078 0.0157 0.012 0.260 0.063 9.237 0.029 0.278 3.074 0.16 51679. 0.0349
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28.40 0.7720 0.1854 0.0030 0.0124 0.010 0.206 0.024 7.321 0.023 0.107 1.489 0.16 51849. 0.0105
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29.42 0.7996
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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 0.0993 0.0381 0.071 1.127 1.424 53.312 0.127 6.335 12.117 0.21 65358. 0.6552
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1.35 0.0276 0.0696 0.0981 0.0389 0.073 1.149 1.407 54.369 0.130 6.259 11.740 0.21 65407. 0.6310
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2.70 0.0551 0.1347 0.0968 0.0396 0.074 1.171 1.388 55.399 0.132 6.175 11.366 0.21 65461. 0.6068
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4.06 0.0827 0.1955 0.0953 0.0403 0.076 1.191 1.367 56.381 0.135 6.081 10.997 0.21 65520. 0.5826
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5.41 0.1102 0.2521 0.0937 0.0410 0.077 1.211 1.344 57.294 0.137 5.976 10.636 0.21 65585. 0.5586
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6.76 0.1378 0.3047 0.0919 0.0416 0.078 1.228 1.318 58.116 0.139 5.860 10.283 0.21 65656. 0.5348
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8.11 0.1653 0.3533 0.0899 0.0421 0.079 1.243 1.289 58.822 0.140 5.733 9.938 0.21 65733. 0.5112
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9.46 0.1929 0.3983 0.0877 0.0425 0.080 1.255 1.257 59.388 0.142 5.592 9.602 0.21 65816. 0.4878
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10.81 0.2205 0.4397 0.0853 0.0428 0.080 1.263 1.223 59.790 0.143 5.439 9.276 0.21 65905. 0.4647
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12.17 0.2480 0.4778 0.0827 0.0429 0.080 1.268 1.185 60.003 0.143 5.272 8.959 0.21 66001. 0.4419
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13.52 0.2756 0.5127 0.0798 0.0429 0.080 1.268 1.144 60.005 0.143 5.091 8.651 0.21 66104. 0.4193
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14.87 0.3031 0.5444 0.0768 0.0427 0.080 1.263 1.101 59.775 0.143 4.896 8.352 0.21 66213. 0.3970
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16.22 0.3307 0.5732 0.0735 0.0424 0.080 1.253 1.054 59.292 0.142 4.687 8.060 0.21 66329. 0.3749
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17.57 0.3583 0.5990 0.0700 0.0419 0.079 1.237 1.004 58.543 0.140 4.464 7.775 0.21 66452. 0.3529
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18.92 0.3858 0.6220 0.0663 0.0411 0.077 1.215 0.951 57.523 0.137 4.229 7.497 0.21 66582. 0.3312
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20.28 0.4134 0.6420 0.0624 0.0402 0.075 1.188 0.895 56.230 0.134 3.983 7.223 0.21 66718. 0.3097
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21.63 0.4409 0.6591 0.0584 0.0391 0.073 1.155 0.838 54.667 0.131 3.727 6.952 0.21 66862. 0.2883
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22.98 0.4685 0.6731 0.0543 0.0378 0.071 1.116 0.778 52.836 0.126 3.462 6.681 0.21 67013. 0.2671
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24.33 0.4960 0.6837 0.0500 0.0363 0.068 1.072 0.717 50.738 0.121 3.189 6.410 0.21 67170. 0.2459
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25.68 0.5236 0.6906 0.0456 0.0346 0.065 1.022 0.654 48.373 0.115 2.910 6.134 0.21 67335. 0.2248
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27.04 0.5512 0.6933 0.0411 0.0327 0.061 0.967 0.590 45.743 0.109 2.624 5.850 0.21 67506. 0.2036
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28.39 0.5787 0.6909 0.0366 0.0306 0.057 0.905 0.524 42.847 0.102 2.333 5.552 0.21 67684. 0.1822
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29.74 0.6063 0.6824 0.0319 0.0284 0.053 0.839 0.458 39.689 0.095 2.037 5.234 0.21 67870. 0.1605
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31.09 0.6338 0.6658 0.0272 0.0259 0.049 0.766 0.391 36.269 0.087 1.737 4.885 0.21 68062. 0.1383
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32.44 0.6614 0.6384 0.0225 0.0233 0.044 0.689 0.323 32.593 0.078 1.435 4.489 0.21 68262. 0.1155
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33.79 0.6889 0.5953 0.0177 0.0205 0.038 0.606 0.254 28.668 0.068 1.130 4.018 0.21 68468. 0.0918
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35.15 0.7165 0.5280 0.0129 0.0175 0.033 0.518 0.185 24.504 0.058 0.823 3.427 0.21 68681. 0.0668
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36.50 0.7441 0.4195 0.0081 0.0144 0.027 0.425 0.116 20.113 0.048 0.517 2.622 0.21 68901. 0.0405
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37.85 0.7716 0.2313 0.0033 0.0111 0.021 0.328 0.048 15.512 0.037 0.212 1.394 0.21 69128. 0.0138
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39.20 0.7992
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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 0.0996 0.0372 0.136 1.720 2.233 101.740 0.194 9.930 9.953 0.26 81696. 0.6738
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1.67 0.0273 0.0707 0.0985 0.0380 0.139 1.755 2.206 103.828 0.198 9.814 9.639 0.26 81757. 0.6488
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3.35 0.0546 0.1369 0.0972 0.0388 0.142 1.790 2.177 105.867 0.202 9.685 9.329 0.26 81823. 0.6237
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5.02 0.0819 0.1987 0.0957 0.0395 0.145 1.823 2.145 107.817 0.206 9.541 9.023 0.26 81897. 0.5988
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6.70 0.1092 0.2561 0.0941 0.0401 0.147 1.853 2.109 109.637 0.209 9.380 8.724 0.26 81977. 0.5741
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8.37 0.1365 0.3094 0.0923 0.0407 0.149 1.881 2.069 111.283 0.213 9.202 8.432 0.26 82064. 0.5496
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|
10.04 0.1638 0.3588 0.0904 0.0413 0.151 1.905 2.025 112.711 0.215 9.006 8.148 0.26 82159. 0.5254
|
|
11.72 0.1911 0.4044 0.0882 0.0417 0.153 1.925 1.976 113.871 0.217 8.791 7.872 0.26 82261. 0.5015
|
|
13.39 0.2184 0.4465 0.0858 0.0420 0.154 1.939 1.923 114.719 0.219 8.555 7.604 0.26 82372. 0.4779
|
|
15.07 0.2457 0.4851 0.0833 0.0422 0.154 1.947 1.866 115.206 0.220 8.298 7.345 0.26 82490. 0.4546
|
|
16.74 0.2730 0.5206 0.0805 0.0422 0.155 1.949 1.803 115.288 0.220 8.020 7.093 0.26 82616. 0.4316
|
|
18.42 0.3003 0.5530 0.0775 0.0421 0.154 1.943 1.736 114.925 0.219 7.720 6.850 0.26 82751. 0.4089
|
|
20.09 0.3276 0.5824 0.0742 0.0418 0.153 1.928 1.663 114.077 0.218 7.398 6.613 0.26 82894. 0.3864
|
|
21.76 0.3549 0.6090 0.0708 0.0413 0.151 1.905 1.586 112.715 0.215 7.055 6.383 0.26 83045. 0.3642
|
|
23.44 0.3822 0.6328 0.0672 0.0406 0.149 1.873 1.505 110.826 0.212 6.693 6.158 0.26 83205. 0.3423
|
|
25.11 0.4096 0.6538 0.0634 0.0397 0.145 1.833 1.419 108.408 0.207 6.313 5.938 0.26 83373. 0.3206
|
|
26.79 0.4369 0.6719 0.0594 0.0386 0.141 1.783 1.330 105.464 0.201 5.918 5.722 0.26 83550. 0.2991
|
|
28.46 0.4642 0.6872 0.0553 0.0373 0.137 1.724 1.239 101.997 0.195 5.509 5.507 0.26 83735. 0.2777
|
|
30.13 0.4915 0.6993 0.0511 0.0359 0.131 1.657 1.144 98.009 0.187 5.087 5.293 0.26 83929. 0.2565
|
|
31.81 0.5188 0.7080 0.0467 0.0342 0.125 1.581 1.047 93.500 0.179 4.655 5.077 0.26 84131. 0.2353
|
|
33.48 0.5461 0.7128 0.0423 0.0324 0.119 1.496 0.947 88.472 0.169 4.213 4.856 0.26 84342. 0.2142
|
|
35.16 0.5734 0.7131 0.0378 0.0304 0.111 1.402 0.846 82.927 0.158 3.763 4.627 0.26 84561. 0.1928
|
|
36.83 0.6007 0.7079 0.0332 0.0281 0.103 1.299 0.743 76.867 0.147 3.305 4.384 0.26 84789. 0.1712
|
|
38.50 0.6280 0.6956 0.0285 0.0257 0.094 1.188 0.639 70.296 0.134 2.841 4.121 0.26 85026. 0.1492
|
|
40.18 0.6553 0.6738 0.0238 0.0231 0.085 1.069 0.533 63.222 0.121 2.372 3.825 0.26 85271. 0.1266
|
|
41.85 0.6826 0.6383 0.0191 0.0204 0.075 0.941 0.427 55.657 0.106 1.899 3.479 0.26 85525. 0.1030
|
|
43.53 0.7099 0.5818 0.0143 0.0174 0.064 0.805 0.320 47.619 0.091 1.424 3.049 0.26 85787. 0.0782
|
|
45.20 0.7372 0.4896 0.0095 0.0143 0.052 0.661 0.213 39.131 0.075 0.948 2.471 0.26 86057. 0.0517
|
|
46.87 0.7645 0.3286 0.0048 0.0111 0.041 0.511 0.107 30.225 0.058 0.474 1.599 0.26 86336. 0.0237
|
|
48.55 0.7918 0.0016 0.0000 0.0077 0.028 0.353 0.000 20.901 0.040 0.002 0.007 0.26 86617. 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 0.1000 0.0367 0.232 2.439 3.227 173.169 0.276 14.352 8.451 0.31 98033. 0.6879
|
|
2.01 0.0273 0.0721 0.0989 0.0375 0.237 2.491 3.189 176.850 0.281 14.187 8.180 0.31 98105. 0.6619
|
|
4.02 0.0547 0.1396 0.0976 0.0382 0.242 2.542 3.148 180.447 0.287 14.002 7.912 0.31 98186. 0.6361
|
|
6.03 0.0820 0.2024 0.0961 0.0390 0.247 2.590 3.101 183.892 0.293 13.795 7.650 0.31 98274. 0.6104
|
|
8.05 0.1094 0.2608 0.0945 0.0396 0.251 2.636 3.050 187.113 0.298 13.565 7.393 0.31 98370. 0.5850
|
|
10.06 0.1367 0.3149 0.0928 0.0403 0.255 2.677 2.992 190.033 0.302 13.310 7.142 0.31 98475. 0.5598
|
|
12.07 0.1640 0.3650 0.0908 0.0408 0.258 2.713 2.929 192.571 0.306 13.028 6.899 0.31 98589. 0.5350
|
|
14.08 0.1914 0.4113 0.0886 0.0412 0.261 2.742 2.859 194.645 0.310 12.718 6.663 0.31 98713. 0.5105
|
|
16.09 0.2187 0.4539 0.0863 0.0416 0.263 2.763 2.783 196.171 0.312 12.378 6.434 0.31 98845. 0.4863
|
|
18.10 0.2461 0.4931 0.0837 0.0418 0.264 2.776 2.699 197.066 0.314 12.007 6.213 0.31 98988. 0.4625
|
|
20.12 0.2734 0.5291 0.0809 0.0418 0.265 2.779 2.609 197.253 0.314 11.605 5.999 0.31 99140. 0.4391
|
|
22.13 0.3007 0.5620 0.0779 0.0417 0.264 2.770 2.512 196.659 0.313 11.172 5.793 0.31 99302. 0.4160
|
|
24.14 0.3281 0.5919 0.0746 0.0414 0.262 2.750 2.407 195.217 0.311 10.707 5.593 0.31 99474. 0.3932
|
|
26.15 0.3554 0.6189 0.0712 0.0409 0.259 2.717 2.296 192.873 0.307 10.211 5.398 0.31 99656. 0.3706
|
|
28.16 0.3828 0.6432 0.0675 0.0402 0.254 2.671 2.178 189.605 0.302 9.686 5.209 0.31 99848. 0.3483
|
|
30.17 0.4101 0.6647 0.0637 0.0393 0.249 2.612 2.054 185.408 0.295 9.137 5.025 0.31 100051. 0.3263
|
|
32.19 0.4375 0.6835 0.0597 0.0382 0.242 2.540 1.925 180.287 0.287 8.564 4.844 0.31 100264. 0.3046
|
|
34.20 0.4648 0.6994 0.0556 0.0369 0.234 2.455 1.792 174.246 0.277 7.972 4.665 0.31 100487. 0.2830
|
|
36.21 0.4921 0.7123 0.0513 0.0354 0.224 2.357 1.655 167.289 0.266 7.361 4.487 0.31 100720. 0.2616
|
|
38.22 0.5195 0.7219 0.0469 0.0338 0.214 2.246 1.514 159.417 0.254 6.735 4.308 0.31 100963. 0.2402
|
|
40.23 0.5468 0.7277 0.0425 0.0319 0.202 2.122 1.370 150.632 0.240 6.095 4.126 0.31 101217. 0.2188
|
|
42.24 0.5742 0.7293 0.0379 0.0299 0.189 1.985 1.224 140.936 0.224 5.442 3.938 0.31 101481. 0.1974
|
|
44.26 0.6015 0.7255 0.0333 0.0276 0.175 1.836 1.074 130.334 0.207 4.779 3.739 0.31 101755. 0.1756
|
|
46.27 0.6288 0.7148 0.0286 0.0252 0.159 1.674 0.923 118.833 0.189 4.107 3.524 0.31 102040. 0.1534
|
|
48.28 0.6562 0.6949 0.0239 0.0226 0.143 1.500 0.771 106.448 0.169 3.427 3.283 0.31 102335. 0.1306
|
|
50.29 0.6835 0.6615 0.0191 0.0197 0.125 1.313 0.617 93.199 0.148 2.742 3.000 0.32 102640. 0.1068
|
|
52.30 0.7109 0.6071 0.0143 0.0168 0.106 1.115 0.462 79.117 0.126 2.054 2.648 0.32 102955. 0.0815
|
|
54.31 0.7382 0.5161 0.0095 0.0136 0.086 0.905 0.307 64.245 0.102 1.366 2.167 0.32 103281. 0.0544
|
|
56.33 0.7655 0.3515 0.0047 0.0103 0.065 0.685 0.153 48.640 0.077 0.679 1.424 0.32 103616. 0.0252
|
|
58.34 0.7929 -0.0044 0.0000 0.0068 0.043 0.455 -0.001 32.283 0.051 -0.006 -0.017 0.32 103953. 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 0.1004 0.0363 0.365 3.289 4.410 272.357 0.372 19.616 7.344 0.36 114368. 0.6988
|
|
2.35 0.0274 0.0732 0.0993 0.0371 0.373 3.361 4.360 278.311 0.380 19.393 7.106 0.36 114453. 0.6723
|
|
4.70 0.0547 0.1415 0.0980 0.0379 0.381 3.431 4.304 284.137 0.388 19.144 6.870 0.36 114547. 0.6458
|
|
7.05 0.0821 0.2051 0.0966 0.0387 0.389 3.498 4.241 289.723 0.395 18.865 6.640 0.36 114650. 0.6196
|
|
9.40 0.1095 0.2642 0.0950 0.0394 0.396 3.561 4.171 294.953 0.402 18.554 6.415 0.36 114762. 0.5936
|
|
11.74 0.1368 0.3190 0.0932 0.0400 0.402 3.619 4.094 299.702 0.409 18.208 6.195 0.36 114885. 0.5680
|
|
14.09 0.1642 0.3696 0.0913 0.0405 0.407 3.669 4.008 303.841 0.414 17.826 5.982 0.36 115019. 0.5427
|
|
16.44 0.1915 0.4164 0.0891 0.0410 0.412 3.710 3.913 307.233 0.419 17.404 5.776 0.36 115163. 0.5177
|
|
18.79 0.2189 0.4595 0.0867 0.0413 0.415 3.740 3.809 309.746 0.423 16.941 5.577 0.36 115318. 0.4932
|
|
21.14 0.2463 0.4991 0.0842 0.0415 0.417 3.758 3.695 311.244 0.425 16.436 5.385 0.36 115484. 0.4690
|
|
23.49 0.2736 0.5354 0.0813 0.0416 0.418 3.763 3.572 311.604 0.425 15.888 5.199 0.36 115662. 0.4453
|
|
25.84 0.3010 0.5687 0.0783 0.0415 0.417 3.752 3.439 310.706 0.424 15.296 5.020 0.36 115852. 0.4218
|
|
28.19 0.3284 0.5989 0.0751 0.0412 0.414 3.724 3.296 308.442 0.421 14.661 4.847 0.36 116053. 0.3987
|
|
30.54 0.3557 0.6264 0.0716 0.0407 0.409 3.679 3.144 304.726 0.416 13.983 4.679 0.36 116266. 0.3759
|
|
32.89 0.3831 0.6511 0.0679 0.0400 0.402 3.617 2.982 299.520 0.409 13.266 4.516 0.36 116491. 0.3534
|
|
35.23 0.4105 0.6731 0.0641 0.0391 0.393 3.536 2.813 292.818 0.399 12.513 4.358 0.36 116728. 0.3312
|
|
37.58 0.4378 0.6924 0.0601 0.0380 0.382 3.437 2.637 284.626 0.388 11.730 4.202 0.36 116976. 0.3092
|
|
39.93 0.4652 0.7089 0.0559 0.0367 0.369 3.320 2.455 274.950 0.375 10.918 4.049 0.36 117237. 0.2875
|
|
42.28 0.4926 0.7224 0.0516 0.0352 0.354 3.185 2.267 263.797 0.360 10.083 3.897 0.36 117510. 0.2659
|
|
44.63 0.5199 0.7328 0.0472 0.0335 0.337 3.033 2.074 251.168 0.343 9.225 3.745 0.36 117794. 0.2444
|
|
46.98 0.5473 0.7396 0.0427 0.0316 0.318 2.862 1.877 237.066 0.323 8.348 3.591 0.36 118091. 0.2229
|
|
49.33 0.5746 0.7421 0.0382 0.0296 0.297 2.674 1.676 221.495 0.302 7.454 3.432 0.37 118399. 0.2013
|
|
51.68 0.6020 0.7396 0.0335 0.0273 0.274 2.469 1.472 204.461 0.279 6.546 3.265 0.37 118720. 0.1794
|
|
54.03 0.6294 0.7304 0.0288 0.0248 0.249 2.246 1.265 185.978 0.254 5.625 3.084 0.37 119053. 0.1571
|
|
56.37 0.6567 0.7123 0.0240 0.0222 0.223 2.005 1.055 166.067 0.227 4.694 2.882 0.37 119398. 0.1341
|
|
58.72 0.6841 0.6810 0.0192 0.0193 0.194 1.748 0.844 144.762 0.197 3.755 2.645 0.37 119754. 0.1101
|
|
61.07 0.7115 0.6288 0.0144 0.0163 0.164 1.474 0.632 122.114 0.167 2.812 2.348 0.37 120123. 0.0846
|
|
63.42 0.7388 0.5396 0.0096 0.0131 0.132 1.186 0.420 98.193 0.134 1.869 1.941 0.37 120503. 0.0570
|
|
65.77 0.7662 0.3734 0.0048 0.0098 0.098 0.883 0.209 73.089 0.100 0.928 1.295 0.37 120895. 0.0268
|
|
68.12 0.7936 -0.0067 -0.0001 0.0062 0.063 0.565 -0.002 46.752 0.064 -0.010 -0.022 0.37 121287. 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 0.1009 0.0361 0.542 4.272 5.787 404.323 0.483 25.740 6.492 0.41 130701. 0.7076
|
|
2.69 0.0274 0.0739 0.0998 0.0369 0.554 4.367 5.723 413.381 0.493 25.454 6.279 0.41 130798. 0.6806
|
|
5.37 0.0548 0.1430 0.0985 0.0377 0.566 4.461 5.650 422.252 0.504 25.133 6.069 0.41 130906. 0.6537
|
|
8.06 0.0821 0.2072 0.0971 0.0385 0.578 4.551 5.569 430.768 0.514 24.772 5.864 0.41 131024. 0.6271
|
|
10.75 0.1095 0.2668 0.0955 0.0392 0.588 4.636 5.479 438.751 0.524 24.369 5.664 0.41 131153. 0.6007
|
|
13.43 0.1369 0.3220 0.0938 0.0399 0.598 4.712 5.378 446.012 0.532 23.920 5.469 0.41 131293. 0.5747
|
|
16.12 0.1643 0.3731 0.0918 0.0404 0.607 4.779 5.266 452.350 0.540 23.422 5.280 0.41 131446. 0.5490
|
|
18.80 0.1917 0.4202 0.0897 0.0409 0.614 4.834 5.142 457.562 0.546 22.873 5.097 0.41 131611. 0.5238
|
|
21.49 0.2191 0.4636 0.0873 0.0412 0.619 4.875 5.006 461.442 0.551 22.269 4.921 0.41 131789. 0.4989
|
|
24.18 0.2464 0.5036 0.0847 0.0415 0.622 4.900 4.858 463.788 0.554 21.609 4.751 0.41 131979. 0.4745
|
|
26.86 0.2738 0.5402 0.0819 0.0415 0.623 4.907 4.697 464.409 0.554 20.891 4.587 0.41 132183. 0.4505
|
|
29.55 0.3012 0.5738 0.0789 0.0414 0.621 4.893 4.522 463.124 0.553 20.116 4.429 0.41 132400. 0.4268
|
|
32.24 0.3286 0.6044 0.0756 0.0411 0.617 4.858 4.335 459.769 0.549 19.283 4.277 0.41 132631. 0.4035
|
|
34.92 0.3560 0.6322 0.0721 0.0406 0.609 4.799 4.135 454.216 0.542 18.393 4.129 0.41 132875. 0.3805
|
|
37.61 0.3834 0.6573 0.0684 0.0399 0.599 4.716 3.923 446.404 0.533 17.451 3.986 0.41 133133. 0.3578
|
|
40.30 0.4107 0.6797 0.0645 0.0390 0.585 4.610 3.701 436.323 0.521 16.463 3.847 0.41 133404. 0.3354
|
|
42.98 0.4381 0.6994 0.0605 0.0379 0.569 4.480 3.470 423.983 0.506 15.433 3.712 0.41 133689. 0.3133
|
|
45.67 0.4655 0.7164 0.0563 0.0366 0.549 4.325 3.230 409.395 0.489 14.366 3.578 0.42 133987. 0.2914
|
|
48.35 0.4929 0.7306 0.0520 0.0351 0.526 4.148 2.983 392.567 0.469 13.267 3.446 0.42 134299. 0.2697
|
|
51.04 0.5203 0.7416 0.0476 0.0334 0.501 3.946 2.729 373.502 0.446 12.139 3.314 0.42 134625. 0.2481
|
|
53.73 0.5477 0.7492 0.0431 0.0315 0.472 3.721 2.470 352.206 0.420 10.986 3.181 0.42 134965. 0.2265
|
|
56.41 0.5750 0.7527 0.0385 0.0294 0.441 3.473 2.205 328.681 0.392 9.810 3.043 0.42 135318. 0.2048
|
|
59.10 0.6024 0.7512 0.0338 0.0271 0.406 3.201 1.937 302.941 0.362 8.614 2.900 0.42 135685. 0.1828
|
|
61.79 0.6298 0.7434 0.0290 0.0246 0.369 2.905 1.664 275.003 0.328 7.402 2.745 0.42 136066. 0.1604
|
|
64.47 0.6572 0.7269 0.0242 0.0219 0.328 2.587 1.389 244.901 0.292 6.176 2.572 0.42 136461. 0.1373
|
|
67.16 0.6846 0.6975 0.0194 0.0190 0.285 2.247 1.111 212.687 0.254 4.941 2.369 0.42 136869. 0.1131
|
|
69.85 0.7120 0.6475 0.0145 0.0159 0.239 1.885 0.832 178.437 0.213 3.700 2.115 0.42 137291. 0.0874
|
|
72.53 0.7393 0.5603 0.0096 0.0127 0.191 1.503 0.553 142.260 0.170 2.458 1.762 0.42 137726. 0.0593
|
|
75.22 0.7667 0.3933 0.0048 0.0093 0.140 1.102 0.274 104.291 0.124 1.220 1.193 0.42 138174. 0.0283
|
|
77.91 0.7941 -0.0090 -0.0001 0.0058 0.086 0.681 -0.004 64.420 0.077 -0.017 -0.026 0.42 138621. 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 0.1014 0.0361 0.770 5.395 7.363 574.421 0.609 32.749 5.814 0.46 147032. 0.7148
|
|
3.02 0.0274 0.0745 0.1003 0.0369 0.788 5.518 7.283 587.578 0.623 32.394 5.622 0.46 147142. 0.6874
|
|
6.05 0.0548 0.1440 0.0991 0.0377 0.805 5.639 7.193 600.479 0.637 31.993 5.433 0.46 147263. 0.6602
|
|
9.07 0.0822 0.2087 0.0977 0.0385 0.822 5.756 7.091 612.875 0.650 31.542 5.248 0.46 147396. 0.6332
|
|
12.10 0.1096 0.2687 0.0961 0.0392 0.837 5.865 6.978 624.511 0.663 31.037 5.068 0.46 147541. 0.6066
|
|
15.12 0.1370 0.3243 0.0944 0.0399 0.852 5.965 6.851 635.109 0.674 30.474 4.893 0.46 147700. 0.5803
|
|
18.14 0.1644 0.3757 0.0924 0.0405 0.864 6.052 6.710 644.378 0.684 29.847 4.723 0.46 147872. 0.5544
|
|
21.17 0.1918 0.4231 0.0903 0.0409 0.874 6.123 6.554 652.020 0.692 29.153 4.559 0.46 148058. 0.5289
|
|
24.19 0.2192 0.4668 0.0879 0.0413 0.882 6.177 6.383 657.736 0.698 28.390 4.401 0.46 148258. 0.5039
|
|
27.22 0.2466 0.5070 0.0853 0.0415 0.887 6.210 6.195 661.232 0.702 27.554 4.249 0.46 148473. 0.4792
|
|
30.24 0.2740 0.5439 0.0825 0.0416 0.888 6.219 5.990 662.230 0.703 26.645 4.103 0.46 148703. 0.4550
|
|
33.26 0.3014 0.5777 0.0795 0.0415 0.886 6.203 5.769 660.472 0.701 25.660 3.962 0.46 148948. 0.4312
|
|
36.29 0.3288 0.6086 0.0762 0.0412 0.879 6.158 5.531 655.719 0.696 24.601 3.826 0.46 149208. 0.4077
|
|
39.31 0.3562 0.6367 0.0727 0.0407 0.869 6.084 5.276 647.784 0.687 23.469 3.694 0.47 149483. 0.3845
|
|
42.34 0.3836 0.6621 0.0690 0.0400 0.854 5.978 5.007 636.578 0.675 22.271 3.567 0.47 149774. 0.3617
|
|
45.36 0.4110 0.6849 0.0651 0.0391 0.834 5.842 4.724 622.088 0.660 21.011 3.444 0.47 150079. 0.3392
|
|
48.38 0.4384 0.7050 0.0610 0.0379 0.810 5.675 4.429 604.328 0.641 19.699 3.324 0.47 150400. 0.3170
|
|
51.41 0.4658 0.7225 0.0568 0.0366 0.782 5.478 4.123 583.316 0.619 18.339 3.206 0.47 150737. 0.2950
|
|
54.43 0.4932 0.7372 0.0525 0.0351 0.750 5.250 3.808 559.064 0.593 16.937 3.089 0.47 151089. 0.2732
|
|
57.46 0.5206 0.7489 0.0480 0.0334 0.713 4.992 3.484 531.579 0.564 15.498 2.973 0.47 151456. 0.2515
|
|
60.48 0.5480 0.7571 0.0434 0.0314 0.672 4.704 3.153 500.865 0.531 14.026 2.856 0.47 151839. 0.2298
|
|
63.50 0.5754 0.7615 0.0388 0.0293 0.626 4.385 2.816 466.932 0.495 12.525 2.735 0.47 152237. 0.2080
|
|
66.53 0.6028 0.7611 0.0341 0.0270 0.576 4.036 2.473 429.794 0.456 10.999 2.610 0.47 152651. 0.1859
|
|
69.55 0.6302 0.7545 0.0293 0.0244 0.522 3.658 2.125 389.479 0.413 9.452 2.475 0.47 153080. 0.1634
|
|
72.58 0.6576 0.7395 0.0244 0.0217 0.464 3.250 1.773 346.035 0.367 7.887 2.324 0.47 153524. 0.1402
|
|
75.60 0.6850 0.7119 0.0195 0.0188 0.402 2.813 1.418 299.539 0.318 6.309 2.148 0.47 153984. 0.1159
|
|
78.62 0.7124 0.6639 0.0146 0.0157 0.335 2.349 1.062 250.099 0.265 4.724 1.926 0.47 154459. 0.0900
|
|
81.65 0.7398 0.5788 0.0097 0.0124 0.265 1.858 0.705 197.874 0.210 3.138 1.617 0.47 154950. 0.0615
|
|
84.67 0.7672 0.4117 0.0048 0.0090 0.192 1.344 0.350 143.061 0.152 1.556 1.109 0.48 155455. 0.0297
|
|
87.70 0.7946 -0.0114 -0.0001 0.0054 0.115 0.802 -0.006 85.448 0.091 -0.025 -0.030 0.48 155955. 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 0.1020 0.0361 1.057 6.664 9.143 788.422 0.753 40.667 5.260 0.51 163361. 0.7206
|
|
3.36 0.0274 0.0749 0.1009 0.0369 1.082 6.820 9.046 806.864 0.770 40.239 5.085 0.51 163483. 0.6931
|
|
6.72 0.0548 0.1448 0.0997 0.0378 1.106 6.973 8.937 824.970 0.788 39.754 4.914 0.51 163617. 0.6656
|
|
10.09 0.0822 0.2098 0.0984 0.0386 1.130 7.120 8.814 842.391 0.804 39.206 4.746 0.51 163765. 0.6384
|
|
13.45 0.1097 0.2701 0.0968 0.0393 1.152 7.258 8.676 858.762 0.820 38.591 4.582 0.51 163927. 0.6116
|
|
16.81 0.1371 0.3260 0.0951 0.0400 1.172 7.385 8.521 873.694 0.834 37.902 4.424 0.51 164103. 0.5851
|
|
20.17 0.1645 0.3776 0.0932 0.0406 1.189 7.495 8.348 886.777 0.847 37.133 4.270 0.51 164295. 0.5590
|
|
23.53 0.1919 0.4252 0.0910 0.0411 1.204 7.587 8.157 897.592 0.857 36.281 4.122 0.51 164502. 0.5334
|
|
26.89 0.2193 0.4691 0.0887 0.0414 1.215 7.655 7.945 905.718 0.865 35.341 3.979 0.51 164725. 0.5082
|
|
30.26 0.2467 0.5095 0.0861 0.0417 1.221 7.698 7.713 910.743 0.870 34.309 3.841 0.52 164965. 0.4834
|
|
33.62 0.2741 0.5467 0.0832 0.0417 1.223 7.711 7.460 912.277 0.871 33.184 3.709 0.52 165221. 0.4591
|
|
36.98 0.3016 0.5807 0.0802 0.0416 1.220 7.691 7.186 909.958 0.869 31.965 3.582 0.52 165494. 0.4351
|
|
40.34 0.3290 0.6118 0.0769 0.0413 1.212 7.636 6.891 903.458 0.863 30.652 3.460 0.52 165783. 0.4115
|
|
43.70 0.3564 0.6402 0.0734 0.0408 1.197 7.544 6.575 892.511 0.852 29.247 3.342 0.52 166090. 0.3882
|
|
47.06 0.3838 0.6659 0.0696 0.0401 1.176 7.413 6.240 876.995 0.837 27.757 3.227 0.52 166413. 0.3653
|
|
50.43 0.4112 0.6890 0.0657 0.0392 1.149 7.243 5.888 856.891 0.818 26.191 3.117 0.52 166754. 0.3427
|
|
53.79 0.4386 0.7096 0.0616 0.0381 1.116 7.034 5.521 832.223 0.795 24.558 3.009 0.52 167112. 0.3204
|
|
57.15 0.4660 0.7275 0.0574 0.0367 1.077 6.787 5.141 803.015 0.767 22.865 2.904 0.52 167486. 0.2983
|
|
60.51 0.4935 0.7427 0.0530 0.0352 1.032 6.502 4.748 769.290 0.735 21.120 2.799 0.52 167878. 0.2764
|
|
63.87 0.5209 0.7549 0.0485 0.0335 0.980 6.179 4.345 731.057 0.698 19.327 2.696 0.52 168287. 0.2546
|
|
67.24 0.5483 0.7639 0.0439 0.0315 0.923 5.818 3.933 688.324 0.657 17.493 2.591 0.52 168713. 0.2329
|
|
70.60 0.5757 0.7690 0.0392 0.0293 0.860 5.419 3.512 641.103 0.612 15.622 2.485 0.52 169156. 0.2110
|
|
73.96 0.6031 0.7696 0.0344 0.0270 0.790 4.982 3.084 589.416 0.563 13.719 2.373 0.52 169616. 0.1889
|
|
77.32 0.6305 0.7641 0.0296 0.0244 0.715 4.508 2.651 533.302 0.509 11.790 2.254 0.52 170094. 0.1663
|
|
80.68 0.6579 0.7505 0.0247 0.0216 0.634 3.996 2.212 472.828 0.452 9.838 2.122 0.52 170588. 0.1430
|
|
84.04 0.6854 0.7246 0.0197 0.0187 0.547 3.449 1.769 408.098 0.390 7.870 1.967 0.53 171100. 0.1185
|
|
87.41 0.7128 0.6787 0.0148 0.0155 0.455 2.868 1.325 339.269 0.324 5.893 1.771 0.53 171629. 0.0924
|
|
90.77 0.7402 0.5956 0.0098 0.0122 0.357 2.253 0.880 266.557 0.255 3.913 1.497 0.53 172174. 0.0636
|
|
94.13 0.7676 0.4289 0.0049 0.0087 0.255 1.608 0.436 190.244 0.182 1.939 1.039 0.53 172736. 0.0311
|
|
97.49 0.7950 -0.0143 -0.0001 0.0050 0.147 0.929 -0.008 109.951 0.105 -0.036 -0.034 0.53 173290. 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 0.1027 0.0362 1.412 8.088 11.134 1052.607 0.914 49.525 4.798 0.57 179687. 0.7254
|
|
3.70 0.0274 0.0752 0.1016 0.0371 1.445 8.281 11.021 1077.749 0.936 49.022 4.638 0.57 179821. 0.6977
|
|
7.40 0.0549 0.1454 0.1005 0.0379 1.478 8.471 10.892 1102.468 0.957 48.449 4.481 0.57 179969. 0.6701
|
|
11.10 0.0823 0.2106 0.0991 0.0387 1.510 8.654 10.747 1126.284 0.978 47.801 4.328 0.57 180132. 0.6428
|
|
14.80 0.1097 0.2711 0.0976 0.0395 1.540 8.826 10.582 1148.697 0.997 47.068 4.178 0.57 180310. 0.6159
|
|
18.50 0.1371 0.3271 0.0959 0.0402 1.568 8.984 10.397 1169.169 1.015 46.245 4.033 0.57 180504. 0.5893
|
|
22.20 0.1646 0.3789 0.0940 0.0408 1.592 9.122 10.190 1187.140 1.031 45.324 3.893 0.57 180716. 0.5631
|
|
25.90 0.1920 0.4267 0.0918 0.0413 1.612 9.236 9.959 1202.035 1.044 44.298 3.758 0.57 180944. 0.5374
|
|
29.60 0.2194 0.4707 0.0895 0.0417 1.627 9.323 9.704 1213.279 1.053 43.164 3.628 0.57 181190. 0.5121
|
|
33.30 0.2468 0.5113 0.0869 0.0420 1.636 9.377 9.424 1220.309 1.059 41.917 3.503 0.57 181454. 0.4872
|
|
37.00 0.2743 0.5486 0.0841 0.0420 1.640 9.394 9.117 1222.592 1.061 40.554 3.382 0.57 181737. 0.4628
|
|
40.70 0.3017 0.5829 0.0810 0.0419 1.636 9.372 8.785 1219.638 1.059 39.074 3.267 0.57 182038. 0.4387
|
|
44.40 0.3291 0.6142 0.0777 0.0416 1.624 9.305 8.426 1211.002 1.051 37.478 3.156 0.57 182357. 0.4151
|
|
48.10 0.3566 0.6428 0.0742 0.0411 1.604 9.192 8.041 1196.328 1.039 35.768 3.049 0.57 182695. 0.3917
|
|
51.80 0.3840 0.6688 0.0704 0.0404 1.576 9.032 7.633 1175.445 1.020 33.952 2.945 0.57 183052. 0.3687
|
|
55.50 0.4114 0.6923 0.0664 0.0395 1.540 8.824 7.204 1148.331 0.997 32.043 2.845 0.57 183427. 0.3460
|
|
59.20 0.4388 0.7132 0.0623 0.0383 1.495 8.568 6.756 1115.022 0.968 30.049 2.748 0.57 183822. 0.3236
|
|
62.90 0.4663 0.7315 0.0580 0.0370 1.442 8.264 6.291 1075.559 0.934 27.982 2.653 0.57 184235. 0.3015
|
|
66.60 0.4937 0.7472 0.0536 0.0354 1.381 7.914 5.811 1029.972 0.894 25.849 2.559 0.57 184666. 0.2795
|
|
70.30 0.5211 0.7599 0.0490 0.0336 1.312 7.517 5.319 978.282 0.849 23.658 2.466 0.57 185117. 0.2577
|
|
74.00 0.5486 0.7696 0.0444 0.0316 1.234 7.073 4.814 920.499 0.799 21.415 2.372 0.57 185586. 0.2359
|
|
77.69 0.5760 0.7755 0.0397 0.0295 1.149 6.582 4.300 856.642 0.744 19.126 2.277 0.57 186075. 0.2139
|
|
81.39 0.6034 0.7769 0.0348 0.0270 1.055 6.045 3.777 786.738 0.683 16.798 2.177 0.58 186582. 0.1917
|
|
85.09 0.6308 0.7726 0.0299 0.0244 0.953 5.462 3.246 710.843 0.617 14.437 2.071 0.58 187108. 0.1691
|
|
88.79 0.6583 0.7602 0.0250 0.0216 0.844 4.833 2.709 629.046 0.546 12.048 1.953 0.58 187653. 0.1456
|
|
92.49 0.6857 0.7360 0.0200 0.0186 0.726 4.161 2.167 541.490 0.470 9.638 1.815 0.58 188216. 0.1211
|
|
96.19 0.7131 0.6921 0.0150 0.0154 0.601 3.445 1.622 448.386 0.389 7.216 1.641 0.58 188799. 0.0947
|
|
99.89 0.7405 0.6112 0.0099 0.0120 0.469 2.690 1.077 350.028 0.304 4.791 1.396 0.58 189399. 0.0656
|
|
103.59 0.7680 0.4452 0.0049 0.0085 0.331 1.896 0.533 246.799 0.214 2.373 0.980 0.58 190018. 0.0324
|
|
107.29 0.7954 -0.0175 -0.0001 0.0047 0.185 1.061 -0.011 138.073 0.120 -0.050 -0.037 0.58 190625. 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 0.1034 0.0364 1.842 9.677 13.345 1373.952 1.093 59.357 4.405 0.62 196010. 0.7292
|
|
4.04 0.0274 0.0754 0.1024 0.0373 1.887 9.914 13.215 1407.470 1.120 58.779 4.259 0.62 196156. 0.7015
|
|
8.08 0.0549 0.1457 0.1013 0.0381 1.932 10.146 13.066 1440.483 1.146 58.119 4.114 0.62 196317. 0.6739
|
|
12.11 0.0823 0.2110 0.0999 0.0390 1.974 10.371 12.897 1472.344 1.172 57.367 3.973 0.62 196495. 0.6465
|
|
16.15 0.1098 0.2716 0.0985 0.0398 2.015 10.582 12.706 1502.378 1.196 56.514 3.836 0.62 196689. 0.6195
|
|
20.19 0.1372 0.3277 0.0968 0.0405 2.052 10.776 12.489 1529.860 1.217 55.550 3.703 0.62 196902. 0.5929
|
|
24.23 0.1646 0.3796 0.0949 0.0412 2.084 10.946 12.245 1554.035 1.237 54.467 3.574 0.62 197133. 0.5667
|
|
28.27 0.1921 0.4275 0.0928 0.0417 2.111 11.087 11.973 1574.130 1.253 53.257 3.450 0.62 197383. 0.5409
|
|
32.30 0.2195 0.4717 0.0904 0.0421 2.131 11.195 11.671 1589.373 1.265 51.914 3.331 0.62 197652. 0.5156
|
|
36.34 0.2470 0.5124 0.0879 0.0423 2.144 11.263 11.338 1599.013 1.272 50.432 3.216 0.62 197941. 0.4907
|
|
40.38 0.2744 0.5499 0.0850 0.0424 2.149 11.286 10.973 1602.339 1.275 48.809 3.106 0.62 198250. 0.4662
|
|
44.42 0.3018 0.5843 0.0820 0.0423 2.144 11.260 10.576 1598.699 1.272 47.043 3.001 0.62 198579. 0.4422
|
|
48.46 0.3293 0.6159 0.0786 0.0420 2.129 11.182 10.147 1587.508 1.263 45.134 2.899 0.62 198929. 0.4185
|
|
52.49 0.3567 0.6447 0.0751 0.0415 2.103 11.046 9.687 1568.293 1.248 43.086 2.801 0.62 199298. 0.3951
|
|
56.53 0.3842 0.6710 0.0713 0.0408 2.066 10.853 9.197 1540.828 1.226 40.909 2.707 0.62 199689. 0.3720
|
|
60.57 0.4116 0.6947 0.0673 0.0399 2.018 10.601 8.682 1505.089 1.198 38.616 2.616 0.62 200099. 0.3493
|
|
64.61 0.4390 0.7160 0.0631 0.0387 1.959 10.292 8.143 1461.130 1.163 36.220 2.528 0.62 200531. 0.3268
|
|
68.65 0.4665 0.7347 0.0588 0.0373 1.890 9.924 7.584 1409.015 1.121 33.734 2.441 0.62 200982. 0.3046
|
|
72.68 0.4939 0.7508 0.0543 0.0357 1.809 9.500 7.007 1348.791 1.073 31.167 2.356 0.62 201454. 0.2826
|
|
76.72 0.5214 0.7641 0.0497 0.0339 1.717 9.019 6.414 1280.491 1.019 28.529 2.272 0.62 201947. 0.2607
|
|
80.76 0.5488 0.7744 0.0450 0.0319 1.615 8.481 5.807 1204.134 0.958 25.828 2.187 0.63 202460. 0.2388
|
|
84.80 0.5762 0.7811 0.0402 0.0297 1.502 7.887 5.187 1119.744 0.891 23.071 2.101 0.63 202994. 0.2168
|
|
88.84 0.6037 0.7834 0.0353 0.0272 1.378 7.236 4.556 1027.362 0.818 20.266 2.011 0.63 203548. 0.1945
|
|
92.87 0.6311 0.7801 0.0303 0.0246 1.243 6.530 3.916 927.059 0.738 17.418 1.916 0.63 204123. 0.1718
|
|
96.91 0.6586 0.7690 0.0253 0.0217 1.098 5.768 3.268 818.955 0.652 14.537 1.810 0.63 204718. 0.1483
|
|
100.95 0.6860 0.7463 0.0203 0.0186 0.943 4.953 2.615 703.238 0.560 11.630 1.686 0.63 205333. 0.1236
|
|
104.99 0.7134 0.7044 0.0152 0.0154 0.778 4.087 1.958 580.185 0.462 8.708 1.530 0.63 205969. 0.0970
|
|
109.02 0.7409 0.6258 0.0101 0.0119 0.604 3.171 1.300 450.190 0.358 5.780 1.309 0.63 206626. 0.0676
|
|
113.06 0.7683 0.4609 0.0050 0.0083 0.421 2.210 0.643 313.759 0.250 2.861 0.930 0.63 207301. 0.0338
|
|
117.10 0.7958 -0.0211 -0.0001 0.0045 0.228 1.197 -0.015 169.896 0.135 -0.068 -0.041 0.64 207959. 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 0.1042 0.0367 2.364 11.462 15.782 1762.971 1.295 70.197 4.060 0.67 212329. 0.7309
|
|
4.38 0.0275 0.0753 0.1032 0.0376 2.422 11.744 15.636 1806.241 1.327 69.551 3.927 0.67 212487. 0.7035
|
|
8.75 0.0549 0.1456 0.1021 0.0385 2.480 12.022 15.469 1849.014 1.358 68.807 3.795 0.67 212662. 0.6763
|
|
13.13 0.0824 0.2110 0.1009 0.0394 2.535 12.291 15.278 1890.448 1.389 67.955 3.666 0.67 212854. 0.6492
|
|
17.51 0.1098 0.2716 0.0994 0.0402 2.588 12.546 15.059 1929.665 1.417 66.981 3.540 0.67 213065. 0.6224
|
|
21.88 0.1373 0.3278 0.0978 0.0409 2.636 12.780 14.810 1965.694 1.444 65.874 3.417 0.67 213296. 0.5959
|
|
26.26 0.1647 0.3798 0.0959 0.0416 2.679 12.987 14.529 1997.529 1.467 64.623 3.299 0.67 213546. 0.5698
|
|
30.64 0.1922 0.4277 0.0938 0.0422 2.714 13.160 14.213 2024.125 1.487 63.219 3.185 0.67 213818. 0.5441
|
|
35.01 0.2196 0.4720 0.0915 0.0426 2.742 13.292 13.861 2044.441 1.502 61.654 3.075 0.67 214110. 0.5188
|
|
39.39 0.2471 0.5128 0.0890 0.0429 2.759 13.377 13.472 2057.458 1.511 59.922 2.970 0.67 214424. 0.4939
|
|
43.76 0.2745 0.5504 0.0861 0.0430 2.765 13.408 13.043 2062.230 1.515 58.017 2.869 0.67 214760. 0.4695
|
|
48.14 0.3020 0.5850 0.0830 0.0429 2.760 13.380 12.576 2057.897 1.512 55.939 2.772 0.67 215118. 0.4454
|
|
52.52 0.3294 0.6167 0.0797 0.0426 2.741 13.288 12.070 2043.700 1.501 53.688 2.679 0.67 215497. 0.4217
|
|
56.89 0.3569 0.6458 0.0761 0.0421 2.708 13.127 11.526 2019.028 1.483 51.268 2.589 0.67 215899. 0.3983
|
|
61.27 0.3843 0.6723 0.0723 0.0413 2.660 12.897 10.947 1983.584 1.457 48.691 2.503 0.67 216323. 0.3753
|
|
65.65 0.4118 0.6964 0.0682 0.0404 2.598 12.596 10.336 1937.345 1.423 45.973 2.420 0.67 216770. 0.3525
|
|
70.02 0.4392 0.7180 0.0640 0.0392 2.522 12.226 9.697 1880.398 1.381 43.131 2.339 0.67 217238. 0.3300
|
|
74.40 0.4667 0.7371 0.0596 0.0378 2.431 11.787 9.033 1812.835 1.332 40.179 2.260 0.68 217728. 0.3078
|
|
78.78 0.4941 0.7537 0.0551 0.0361 2.326 11.279 8.347 1734.737 1.274 37.129 2.183 0.68 218241. 0.2857
|
|
83.15 0.5216 0.7676 0.0505 0.0343 2.208 10.703 7.642 1646.154 1.209 33.993 2.106 0.68 218776. 0.2638
|
|
87.53 0.5491 0.7785 0.0457 0.0322 2.075 10.059 6.920 1547.119 1.136 30.780 2.029 0.68 219333. 0.2418
|
|
91.91 0.5765 0.7859 0.0408 0.0299 1.928 9.347 6.182 1437.663 1.056 27.499 1.950 0.68 219912. 0.2197
|
|
96.28 0.6040 0.7890 0.0359 0.0275 1.767 8.568 5.431 1317.840 0.968 24.158 1.869 0.68 220514. 0.1974
|
|
100.66 0.6314 0.7868 0.0308 0.0247 1.593 7.722 4.669 1187.744 0.872 20.767 1.783 0.68 221138. 0.1746
|
|
105.03 0.6589 0.7770 0.0257 0.0218 1.405 6.811 3.897 1047.533 0.769 17.334 1.687 0.68 221783. 0.1509
|
|
109.41 0.6863 0.7559 0.0206 0.0187 1.203 5.835 3.118 897.449 0.659 13.869 1.576 0.68 222451. 0.1261
|
|
113.79 0.7138 0.7159 0.0154 0.0154 0.989 4.797 2.335 737.851 0.542 10.384 1.435 0.68 223141. 0.0994
|
|
118.16 0.7412 0.6396 0.0102 0.0119 0.763 3.701 1.550 569.253 0.418 6.893 1.235 0.69 223853. 0.0696
|
|
122.54 0.7687 0.4760 0.0051 0.0082 0.526 2.551 0.766 392.326 0.288 3.409 0.886 0.69 224585. 0.0352
|
|
126.92 0.7961 -0.0252 -0.0001 0.0043 0.276 1.337 -0.021 205.566 0.151 -0.091 -0.045 0.69 225294. 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 0.1050 0.0375 3.019 13.592 18.451 2251.272 1.536 82.072 3.717 0.72 228644. 0.7235
|
|
4.72 0.0275 0.0744 0.1041 0.0384 3.090 13.912 18.293 2304.284 1.572 81.369 3.601 0.72 228814. 0.6978
|
|
9.43 0.0549 0.1441 0.1031 0.0393 3.160 14.228 18.110 2356.679 1.607 80.553 3.485 0.72 229001. 0.6721
|
|
14.15 0.0824 0.2091 0.1019 0.0401 3.228 14.534 17.898 2407.414 1.642 79.609 3.372 0.72 229209. 0.6464
|
|
18.86 0.1099 0.2696 0.1005 0.0409 3.293 14.824 17.653 2455.400 1.675 78.522 3.261 0.72 229436. 0.6208
|
|
23.58 0.1373 0.3258 0.0989 0.0417 3.352 15.090 17.373 2499.463 1.705 77.276 3.153 0.72 229685. 0.5954
|
|
28.29 0.1648 0.3780 0.0971 0.0423 3.404 15.325 17.055 2538.363 1.731 75.859 3.047 0.72 229955. 0.5702
|
|
33.01 0.1922 0.4262 0.0950 0.0429 3.448 15.521 16.695 2570.826 1.754 74.258 2.945 0.72 230248. 0.5453
|
|
37.72 0.2197 0.4708 0.0927 0.0433 3.481 15.670 16.291 2595.574 1.770 72.463 2.847 0.72 230564. 0.5207
|
|
42.44 0.2472 0.5119 0.0902 0.0436 3.502 15.766 15.842 2611.343 1.781 70.466 2.752 0.72 230903. 0.4963
|
|
47.15 0.2746 0.5498 0.0874 0.0436 3.509 15.799 15.347 2616.918 1.785 68.262 2.660 0.72 231266. 0.4722
|
|
51.87 0.3021 0.5847 0.0843 0.0435 3.502 15.764 14.804 2611.158 1.781 65.849 2.572 0.72 231652. 0.4483
|
|
56.58 0.3296 0.6168 0.0809 0.0432 3.477 15.655 14.215 2593.013 1.769 63.227 2.486 0.72 232063. 0.4248
|
|
61.30 0.3570 0.6461 0.0773 0.0427 3.435 15.465 13.579 2561.613 1.747 60.401 2.404 0.72 232497. 0.4015
|
|
66.01 0.3845 0.6729 0.0735 0.0420 3.375 15.193 12.901 2516.485 1.716 57.385 2.325 0.72 232955. 0.3785
|
|
70.73 0.4120 0.6973 0.0694 0.0410 3.296 14.837 12.185 2457.534 1.676 54.199 2.249 0.73 233437. 0.3557
|
|
75.44 0.4394 0.7193 0.0651 0.0398 3.198 14.398 11.435 2384.847 1.627 50.863 2.175 0.73 233943. 0.3332
|
|
80.16 0.4669 0.7388 0.0607 0.0383 3.082 13.877 10.655 2298.555 1.568 47.394 2.103 0.73 234473. 0.3110
|
|
84.87 0.4944 0.7559 0.0561 0.0367 2.949 13.275 9.849 2198.781 1.500 43.807 2.032 0.73 235026. 0.2889
|
|
89.59 0.5218 0.7703 0.0513 0.0348 2.797 12.591 9.019 2085.607 1.423 40.116 1.961 0.73 235604. 0.2669
|
|
94.30 0.5493 0.7818 0.0465 0.0327 2.627 11.828 8.168 1959.087 1.336 36.333 1.891 0.73 236205. 0.2449
|
|
99.02 0.5767 0.7900 0.0416 0.0303 2.440 10.983 7.299 1819.268 1.241 32.467 1.820 0.73 236830. 0.2228
|
|
103.73 0.6042 0.7940 0.0365 0.0278 2.234 10.059 6.414 1666.213 1.137 28.530 1.746 0.73 237479. 0.2004
|
|
108.45 0.6317 0.7928 0.0314 0.0250 2.012 9.056 5.515 1500.045 1.023 24.530 1.668 0.73 238152. 0.1774
|
|
113.16 0.6591 0.7842 0.0262 0.0220 1.771 7.975 4.604 1320.987 0.901 20.479 1.581 0.73 238849. 0.1537
|
|
117.88 0.6866 0.7647 0.0210 0.0188 1.515 6.819 3.684 1129.406 0.770 16.389 1.480 0.74 239569. 0.1287
|
|
122.59 0.7141 0.7264 0.0157 0.0154 1.242 5.590 2.759 925.863 0.632 12.272 1.352 0.74 240313. 0.1017
|
|
127.31 0.7415 0.6519 0.0104 0.0119 0.954 4.294 1.831 711.190 0.485 8.146 1.168 0.74 241080. 0.0716
|
|
132.02 0.7690 0.4886 0.0052 0.0081 0.652 2.937 0.905 486.505 0.332 4.027 0.844 0.74 241869. 0.0364
|
|
136.74 0.7965 -0.0292 -0.0002 0.0042 0.335 1.508 -0.027 249.772 0.170 -0.119 -0.049 0.74 242628. 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 0.1059 0.0394 3.901 16.391 21.356 2908.815 1.852 94.990 3.330 0.77 244954. 0.6973
|
|
5.05 0.0275 0.0717 0.1051 0.0403 3.984 16.739 21.189 2970.651 1.891 94.247 3.235 0.77 245135. 0.6748
|
|
10.11 0.0549 0.1392 0.1041 0.0411 4.065 17.081 20.993 3031.297 1.930 93.377 3.141 0.77 245336. 0.6521
|
|
15.16 0.0824 0.2026 0.1030 0.0419 4.143 17.408 20.764 3089.420 1.967 92.360 3.048 0.77 245558. 0.6294
|
|
20.21 0.1099 0.2621 0.1017 0.0426 4.216 17.714 20.498 3143.658 2.001 91.176 2.958 0.77 245801. 0.6067
|
|
25.27 0.1374 0.3177 0.1001 0.0433 4.281 17.990 20.190 3192.584 2.032 89.807 2.868 0.77 246067. 0.5840
|
|
30.32 0.1648 0.3697 0.0984 0.0439 4.338 18.227 19.837 3234.729 2.059 88.235 2.782 0.77 246357. 0.5613
|
|
35.37 0.1923 0.4182 0.0964 0.0443 4.383 18.418 19.434 3268.638 2.081 86.443 2.697 0.77 246672. 0.5387
|
|
40.42 0.2198 0.4633 0.0941 0.0446 4.416 18.555 18.979 3292.861 2.096 84.419 2.614 0.77 247011. 0.5161
|
|
45.48 0.2472 0.5052 0.0916 0.0448 4.433 18.629 18.470 3306.005 2.105 82.154 2.534 0.77 247375. 0.4934
|
|
50.53 0.2747 0.5440 0.0888 0.0448 4.434 18.633 17.905 3306.738 2.105 79.639 2.456 0.77 247765. 0.4709
|
|
55.58 0.3022 0.5799 0.0857 0.0447 4.417 18.560 17.283 3293.800 2.097 76.874 2.380 0.77 248181. 0.4483
|
|
60.64 0.3297 0.6130 0.0823 0.0443 4.380 18.403 16.605 3266.010 2.079 73.857 2.306 0.77 248622. 0.4258
|
|
65.69 0.3571 0.6434 0.0787 0.0437 4.321 18.157 15.871 3222.335 2.051 70.595 2.234 0.78 249089. 0.4033
|
|
70.74 0.3846 0.6711 0.0748 0.0429 4.241 17.818 15.086 3162.179 2.013 67.104 2.164 0.78 249582. 0.3808
|
|
75.80 0.4121 0.6963 0.0707 0.0418 4.138 17.386 14.255 3085.404 1.964 63.407 2.096 0.78 250100. 0.3585
|
|
80.85 0.4395 0.7191 0.0664 0.0406 4.012 16.860 13.383 2992.022 1.905 59.528 2.029 0.78 250644. 0.3363
|
|
85.90 0.4670 0.7394 0.0619 0.0391 3.865 16.240 12.475 2882.075 1.835 55.489 1.963 0.78 251213. 0.3142
|
|
90.96 0.4945 0.7571 0.0572 0.0374 3.695 15.527 11.535 2755.562 1.754 51.308 1.899 0.78 251808. 0.2922
|
|
96.01 0.5219 0.7722 0.0524 0.0354 3.503 14.721 10.567 2612.448 1.663 47.001 1.835 0.78 252428. 0.2702
|
|
101.06 0.5494 0.7844 0.0475 0.0333 3.289 13.821 9.573 2452.722 1.561 42.582 1.770 0.78 253074. 0.2482
|
|
106.12 0.5769 0.7932 0.0424 0.0309 3.053 12.827 8.558 2276.427 1.449 38.065 1.705 0.78 253745. 0.2260
|
|
111.17 0.6044 0.7981 0.0373 0.0283 2.794 11.741 7.523 2083.672 1.327 33.461 1.638 0.78 254442. 0.2035
|
|
116.22 0.6318 0.7976 0.0321 0.0254 2.514 10.564 6.470 1874.764 1.194 28.781 1.565 0.79 255164. 0.1804
|
|
121.27 0.6593 0.7897 0.0268 0.0224 2.213 9.299 5.404 1650.201 1.051 24.037 1.485 0.79 255912. 0.1565
|
|
126.33 0.6868 0.7703 0.0215 0.0191 1.892 7.949 4.326 1410.768 0.898 19.244 1.391 0.79 256684. 0.1311
|
|
131.38 0.7142 0.7314 0.0161 0.0157 1.552 6.523 3.241 1157.586 0.737 14.416 1.270 0.79 257482. 0.1036
|
|
136.43 0.7417 0.6543 0.0107 0.0121 1.196 5.027 2.152 892.179 0.568 9.571 1.094 0.79 258305. 0.0727
|
|
141.49 0.7692 0.4854 0.0053 0.0084 0.827 3.474 1.064 616.488 0.392 4.731 0.783 0.79 259151. 0.0366
|
|
146.54 0.7967 -0.0299 -0.0002 0.0044 0.440 1.848 -0.034 327.913 0.209 -0.150 -0.047 0.79 259964. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 16000
|
|
|
|
V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
|
|
(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
|
|
0.00 0.0000 0.0000 0.1067 0.0431 5.176 20.389 24.488 3859.548 2.303 108.923 2.878 0.82 261260. 0.6453
|
|
5.40 0.0275 0.0664 0.1060 0.0439 5.269 20.758 24.317 3929.415 2.345 108.164 2.807 0.82 261452. 0.6272
|
|
10.79 0.0550 0.1295 0.1051 0.0447 5.360 21.114 24.115 3996.769 2.385 107.265 2.737 0.82 261665. 0.6090
|
|
16.19 0.0825 0.1893 0.1041 0.0454 5.444 21.446 23.876 4059.741 2.423 106.201 2.668 0.82 261901. 0.5906
|
|
21.58 0.1100 0.2460 0.1028 0.0460 5.520 21.746 23.595 4116.464 2.457 104.948 2.600 0.82 262160. 0.5722
|
|
26.98 0.1375 0.2996 0.1014 0.0465 5.585 22.003 23.265 4165.053 2.486 103.481 2.533 0.82 262444. 0.5537
|
|
32.37 0.1650 0.3503 0.0997 0.0470 5.637 22.207 22.881 4203.706 2.509 101.775 2.469 0.82 262754. 0.5351
|
|
37.77 0.1925 0.3983 0.0978 0.0473 5.674 22.349 22.439 4230.735 2.525 99.810 2.406 0.82 263090. 0.5164
|
|
43.16 0.2200 0.4435 0.0956 0.0474 5.692 22.423 21.935 4244.600 2.533 97.568 2.344 0.82 263453. 0.4974
|
|
48.56 0.2475 0.4861 0.0931 0.0474 5.691 22.419 21.366 4243.926 2.533 95.037 2.284 0.82 263843. 0.4783
|
|
53.95 0.2750 0.5260 0.0904 0.0472 5.669 22.332 20.730 4227.494 2.523 92.207 2.224 0.83 264261. 0.4588
|
|
59.35 0.3025 0.5634 0.0873 0.0469 5.625 22.157 20.026 4194.205 2.503 89.076 2.166 0.83 264707. 0.4391
|
|
64.74 0.3300 0.5983 0.0839 0.0463 5.556 21.886 19.254 4143.053 2.473 85.643 2.108 0.83 265180. 0.4191
|
|
70.14 0.3575 0.6306 0.0803 0.0455 5.462 21.517 18.416 4073.136 2.431 81.916 2.051 0.83 265681. 0.3988
|
|
75.53 0.3850 0.6603 0.0764 0.0445 5.343 21.046 17.516 3983.971 2.378 77.913 1.994 0.83 266209. 0.3782
|
|
80.93 0.4125 0.6876 0.0722 0.0433 5.197 20.473 16.560 3875.504 2.313 73.661 1.938 0.83 266764. 0.3574
|
|
86.32 0.4399 0.7124 0.0678 0.0419 5.026 19.799 15.555 3747.903 2.237 69.188 1.882 0.83 267347. 0.3364
|
|
91.72 0.4674 0.7346 0.0632 0.0402 4.829 19.024 14.505 3601.316 2.149 64.520 1.827 0.83 267957. 0.3153
|
|
97.11 0.4949 0.7541 0.0585 0.0384 4.607 18.150 13.417 3435.762 2.051 59.681 1.771 0.83 268594. 0.2940
|
|
102.51 0.5224 0.7708 0.0536 0.0363 4.360 17.175 12.295 3251.121 1.940 54.690 1.715 0.83 269259. 0.2725
|
|
107.90 0.5499 0.7845 0.0486 0.0340 4.087 16.098 11.143 3047.313 1.819 49.563 1.659 0.83 269950. 0.2509
|
|
113.30 0.5774 0.7943 0.0434 0.0316 3.789 14.927 9.963 2825.626 1.686 44.316 1.599 0.84 270669. 0.2287
|
|
118.69 0.6049 0.7992 0.0382 0.0289 3.469 13.664 8.759 2586.669 1.544 38.962 1.536 0.84 271415. 0.2060
|
|
124.09 0.6324 0.7979 0.0328 0.0260 3.124 12.308 7.535 2329.861 1.391 33.515 1.467 0.84 272187. 0.1824
|
|
129.48 0.6599 0.7881 0.0274 0.0230 2.757 10.860 6.292 2055.814 1.227 27.989 1.388 0.84 272987. 0.1578
|
|
134.88 0.6874 0.7648 0.0220 0.0197 2.368 9.329 5.036 1766.027 1.054 22.400 1.293 0.84 273814. 0.1315
|
|
140.27 0.7149 0.7187 0.0164 0.0163 1.962 7.727 3.769 1462.755 0.873 16.765 1.169 0.84 274667. 0.1028
|
|
145.67 0.7424 0.6296 0.0109 0.0128 1.540 6.068 2.497 1148.589 0.686 11.105 0.986 0.84 275546. 0.0706
|
|
151.06 0.7699 0.4448 0.0053 0.0092 1.109 4.367 1.224 826.700 0.493 5.445 0.672 0.85 276451. 0.0337
|
|
156.46 0.7974 -0.0395 -0.0003 0.0055 0.660 2.602 -0.062 492.485 0.294 -0.278 -0.058 0.85 277315. 0.0000
|
|
|
|
|
|
|
|
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 0.1072 0.0486 7.001 25.956 27.756 5220.484 2.932 123.459 2.412 0.87 277573. 0.5757
|
|
5.73 0.0275 0.0593 0.1065 0.0494 7.113 26.373 27.592 5304.341 2.980 122.727 2.359 0.87 277774. 0.5615
|
|
11.46 0.0550 0.1159 0.1058 0.0501 7.220 26.768 27.394 5383.810 3.024 121.849 2.308 0.87 277998. 0.5473
|
|
17.19 0.0825 0.1701 0.1049 0.0508 7.317 27.127 27.157 5456.058 3.065 120.796 2.258 0.87 278246. 0.5331
|
|
22.92 0.1099 0.2220 0.1038 0.0514 7.400 27.435 26.874 5517.916 3.100 119.534 2.209 0.87 278519. 0.5189
|
|
28.65 0.1374 0.2716 0.1025 0.0519 7.465 27.677 26.536 5566.656 3.127 118.031 2.162 0.87 278819. 0.5047
|
|
34.38 0.1649 0.3191 0.1009 0.0522 7.509 27.842 26.137 5599.774 3.146 116.257 2.117 0.87 279146. 0.4904
|
|
40.11 0.1924 0.3646 0.0991 0.0523 7.530 27.917 25.671 5614.957 3.154 114.183 2.074 0.87 279502. 0.4761
|
|
45.84 0.2199 0.4083 0.0970 0.0523 7.524 27.894 25.131 5610.298 3.151 111.784 2.032 0.88 279887. 0.4615
|
|
51.57 0.2474 0.4501 0.0947 0.0520 7.489 27.765 24.514 5584.311 3.137 109.040 1.991 0.88 280301. 0.4467
|
|
57.30 0.2749 0.4902 0.0920 0.0516 7.424 27.524 23.817 5535.917 3.110 105.939 1.951 0.88 280746. 0.4315
|
|
63.03 0.3023 0.5284 0.0890 0.0509 7.328 27.169 23.038 5464.476 3.070 102.475 1.912 0.88 281220. 0.4159
|
|
68.76 0.3298 0.5647 0.0856 0.0500 7.201 26.698 22.178 5369.709 3.016 98.647 1.873 0.88 281724. 0.3997
|
|
74.49 0.3573 0.5990 0.0820 0.0489 7.042 26.110 21.237 5251.534 2.950 94.464 1.834 0.88 282257. 0.3830
|
|
80.22 0.3848 0.6312 0.0781 0.0476 6.853 25.408 20.222 5110.300 2.871 89.947 1.795 0.88 282820. 0.3657
|
|
85.95 0.4123 0.6612 0.0739 0.0461 6.634 24.595 19.139 4946.833 2.779 85.129 1.755 0.88 283412. 0.3479
|
|
91.68 0.4398 0.6889 0.0695 0.0444 6.386 23.676 17.996 4761.959 2.675 80.045 1.714 0.88 284033. 0.3295
|
|
97.41 0.4672 0.7142 0.0649 0.0424 6.110 22.653 16.800 4556.227 2.559 74.725 1.672 0.88 284682. 0.3106
|
|
103.14 0.4947 0.7368 0.0601 0.0403 5.806 21.527 15.556 4329.737 2.432 69.195 1.630 0.88 285361. 0.2912
|
|
108.87 0.5222 0.7567 0.0551 0.0380 5.475 20.297 14.271 4082.406 2.293 63.478 1.586 0.89 286069. 0.2714
|
|
114.60 0.5497 0.7736 0.0500 0.0355 5.115 18.963 12.948 3814.068 2.142 57.595 1.540 0.89 286805. 0.2511
|
|
120.33 0.5772 0.7865 0.0448 0.0329 4.730 17.535 11.593 3526.793 1.981 51.564 1.491 0.89 287569. 0.2300
|
|
126.06 0.6047 0.7930 0.0394 0.0300 4.326 16.040 10.206 3226.054 1.812 45.398 1.435 0.89 288363. 0.2077
|
|
131.79 0.6322 0.7886 0.0339 0.0272 3.918 14.526 8.792 2921.690 1.641 39.107 1.365 0.89 289185. 0.1834
|
|
137.52 0.6596 0.7730 0.0284 0.0242 3.489 12.937 7.356 2602.078 1.462 32.719 1.282 0.89 290035. 0.1576
|
|
143.25 0.6871 0.7409 0.0228 0.0211 3.043 11.281 5.902 2268.948 1.275 26.251 1.180 0.89 290913. 0.1299
|
|
148.98 0.7146 0.6822 0.0171 0.0179 2.583 9.575 4.435 1925.771 1.082 19.725 1.044 0.90 291820. 0.0997
|
|
154.71 0.7421 0.5775 0.0114 0.0147 2.115 7.840 2.960 1576.852 0.886 13.168 0.852 0.90 292755. 0.0664
|
|
160.44 0.7696 0.3865 0.0057 0.0114 1.645 6.098 1.486 1226.582 0.689 6.609 0.549 0.90 293716. 0.0303
|
|
166.16 0.7971 0.0027 0.0000 0.0081 1.171 4.340 0.007 872.969 0.490 0.031 0.004 0.90 294672. 0.0000
|
|
|
|
|
|
|