612 lines
109 KiB
Plaintext
612 lines
109 KiB
Plaintext
14x7 (14x7.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 0.0958 0.0440 0.002 0.120 0.117 1.420 0.014 0.522 37.458 0.06 24367. 0.5377
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0.30 0.0228 0.0486 0.0942 0.0443 0.002 0.121 0.115 1.429 0.014 0.513 36.585 0.06 24383. 0.5206
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0.61 0.0457 0.0948 0.0924 0.0445 0.002 0.121 0.113 1.437 0.014 0.503 35.705 0.06 24400. 0.5034
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0.91 0.0685 0.1387 0.0905 0.0447 0.002 0.122 0.111 1.444 0.014 0.493 34.821 0.06 24419. 0.4859
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1.21 0.0914 0.1802 0.0885 0.0449 0.002 0.122 0.108 1.449 0.014 0.482 33.933 0.06 24439. 0.4682
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1.51 0.1142 0.2193 0.0864 0.0450 0.002 0.123 0.106 1.452 0.014 0.471 33.042 0.06 24460. 0.4504
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1.82 0.1370 0.2561 0.0842 0.0450 0.002 0.123 0.103 1.454 0.014 0.458 32.148 0.06 24483. 0.4325
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2.12 0.1599 0.2904 0.0818 0.0450 0.002 0.123 0.100 1.453 0.014 0.445 31.252 0.06 24507. 0.4144
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2.42 0.1827 0.3224 0.0792 0.0449 0.002 0.123 0.097 1.449 0.014 0.431 30.354 0.06 24533. 0.3962
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2.73 0.2056 0.3519 0.0765 0.0447 0.002 0.122 0.094 1.443 0.014 0.417 29.451 0.06 24560. 0.3779
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3.03 0.2284 0.3789 0.0737 0.0444 0.002 0.121 0.090 1.434 0.014 0.401 28.544 0.06 24589. 0.3594
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3.33 0.2512 0.4035 0.0707 0.0440 0.002 0.120 0.087 1.421 0.014 0.385 27.630 0.06 24619. 0.3408
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3.63 0.2741 0.4255 0.0676 0.0435 0.002 0.119 0.083 1.405 0.013 0.368 26.707 0.06 24651. 0.3220
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3.94 0.2969 0.4448 0.0643 0.0429 0.002 0.117 0.079 1.386 0.013 0.350 25.773 0.06 24684. 0.3031
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4.24 0.3198 0.4614 0.0609 0.0422 0.002 0.115 0.075 1.363 0.013 0.332 24.824 0.06 24720. 0.2842
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4.54 0.3426 0.4750 0.0574 0.0414 0.002 0.113 0.070 1.336 0.013 0.313 23.856 0.06 24757. 0.2651
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4.85 0.3655 0.4856 0.0538 0.0405 0.002 0.110 0.066 1.306 0.012 0.293 22.864 0.06 24795. 0.2459
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5.15 0.3883 0.4929 0.0501 0.0394 0.002 0.108 0.061 1.273 0.012 0.273 21.841 0.06 24836. 0.2266
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5.45 0.4111 0.4966 0.0462 0.0383 0.002 0.104 0.057 1.236 0.012 0.252 20.781 0.06 24878. 0.2072
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5.75 0.4340 0.4962 0.0423 0.0370 0.002 0.101 0.052 1.195 0.011 0.231 19.673 0.06 24922. 0.1877
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6.06 0.4568 0.4914 0.0383 0.0356 0.002 0.097 0.047 1.150 0.011 0.209 18.506 0.06 24967. 0.1680
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6.36 0.4797 0.4813 0.0343 0.0342 0.001 0.093 0.042 1.102 0.011 0.187 17.266 0.06 25015. 0.1482
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6.66 0.5025 0.4653 0.0301 0.0326 0.001 0.089 0.037 1.051 0.010 0.164 15.932 0.06 25064. 0.1283
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6.96 0.5253 0.4421 0.0260 0.0308 0.001 0.084 0.032 0.995 0.010 0.141 14.480 0.06 25115. 0.1082
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7.27 0.5482 0.4102 0.0217 0.0290 0.001 0.079 0.027 0.937 0.009 0.118 12.876 0.06 25167. 0.0880
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7.57 0.5710 0.3676 0.0174 0.0271 0.001 0.074 0.021 0.874 0.008 0.095 11.075 0.06 25222. 0.0678
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7.87 0.5939 0.3111 0.0131 0.0250 0.001 0.068 0.016 0.808 0.008 0.071 9.014 0.06 25278. 0.0479
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8.18 0.6167 0.2366 0.0088 0.0229 0.001 0.062 0.011 0.738 0.007 0.048 6.602 0.06 25336. 0.0287
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8.48 0.6395 0.1376 0.0044 0.0206 0.001 0.056 0.005 0.666 0.006 0.024 3.702 0.06 25396. 0.0114
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8.78 0.6624 0.0037 0.0001 0.0183 0.001 0.050 0.000 0.590 0.006 0.001 0.097 0.06 25457. 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 0.0963 0.0386 0.013 0.421 0.472 9.955 0.048 2.097 21.484 0.11 48734. 0.6183
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0.61 0.0230 0.0560 0.0946 0.0389 0.013 0.424 0.463 10.041 0.048 2.062 20.938 0.11 48766. 0.5974
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1.22 0.0460 0.1091 0.0929 0.0392 0.014 0.428 0.455 10.117 0.048 2.023 20.393 0.11 48801. 0.5764
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1.83 0.0690 0.1593 0.0910 0.0394 0.014 0.430 0.446 10.184 0.049 1.982 19.849 0.11 48838. 0.5554
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2.44 0.0920 0.2066 0.0890 0.0397 0.014 0.433 0.436 10.238 0.049 1.939 19.309 0.11 48879. 0.5343
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3.05 0.1150 0.2510 0.0869 0.0398 0.014 0.434 0.425 10.278 0.049 1.892 18.773 0.11 48921. 0.5132
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3.66 0.1380 0.2927 0.0846 0.0399 0.014 0.435 0.414 10.302 0.049 1.843 18.240 0.11 48967. 0.4921
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4.27 0.1610 0.3316 0.0822 0.0399 0.014 0.436 0.402 10.307 0.049 1.790 17.712 0.11 49016. 0.4710
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4.88 0.1841 0.3677 0.0796 0.0399 0.014 0.435 0.390 10.291 0.049 1.735 17.188 0.11 49068. 0.4499
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5.49 0.2071 0.4012 0.0769 0.0397 0.014 0.433 0.377 10.252 0.049 1.676 16.668 0.11 49123. 0.4288
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6.10 0.2301 0.4319 0.0741 0.0395 0.014 0.431 0.363 10.187 0.049 1.613 16.151 0.11 49181. 0.4077
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6.71 0.2531 0.4600 0.0711 0.0391 0.014 0.427 0.348 10.095 0.048 1.548 15.636 0.11 49243. 0.3866
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7.32 0.2761 0.4853 0.0679 0.0386 0.013 0.421 0.333 9.973 0.048 1.479 15.123 0.11 49307. 0.3655
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7.93 0.2991 0.5080 0.0646 0.0380 0.013 0.415 0.316 9.822 0.047 1.407 14.610 0.11 49375. 0.3444
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8.54 0.3221 0.5278 0.0612 0.0373 0.013 0.407 0.300 9.640 0.046 1.333 14.096 0.11 49447. 0.3234
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9.15 0.3451 0.5447 0.0576 0.0365 0.013 0.398 0.282 9.428 0.045 1.255 13.578 0.11 49522. 0.3023
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9.76 0.3681 0.5585 0.0540 0.0356 0.012 0.388 0.264 9.185 0.044 1.176 13.053 0.11 49600. 0.2813
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10.37 0.3911 0.5691 0.0502 0.0345 0.012 0.377 0.246 8.911 0.043 1.094 12.518 0.11 49682. 0.2602
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10.98 0.4141 0.5761 0.0464 0.0333 0.012 0.364 0.227 8.606 0.041 1.010 11.968 0.11 49767. 0.2390
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11.59 0.4371 0.5792 0.0424 0.0320 0.011 0.349 0.208 8.269 0.039 0.924 11.399 0.11 49856. 0.2178
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12.20 0.4601 0.5778 0.0384 0.0306 0.011 0.334 0.188 7.899 0.038 0.837 10.803 0.11 49948. 0.1964
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12.81 0.4831 0.5712 0.0343 0.0290 0.010 0.317 0.168 7.498 0.036 0.748 10.170 0.11 50044. 0.1748
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13.42 0.5062 0.5583 0.0302 0.0274 0.009 0.299 0.148 7.064 0.034 0.657 9.490 0.11 50143. 0.1529
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14.03 0.5292 0.5378 0.0260 0.0256 0.009 0.279 0.127 6.597 0.031 0.566 8.744 0.11 50246. 0.1307
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14.64 0.5522 0.5076 0.0217 0.0236 0.008 0.258 0.106 6.099 0.029 0.473 7.909 0.11 50353. 0.1081
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15.25 0.5752 0.4646 0.0174 0.0216 0.007 0.235 0.085 5.568 0.027 0.379 6.949 0.11 50464. 0.0851
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15.86 0.5982 0.4041 0.0131 0.0194 0.007 0.212 0.064 5.006 0.024 0.285 5.811 0.11 50578. 0.0617
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16.47 0.6212 0.3183 0.0088 0.0171 0.006 0.187 0.043 4.415 0.021 0.191 4.408 0.11 50695. 0.0383
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17.08 0.6442 0.1940 0.0044 0.0147 0.005 0.160 0.022 3.795 0.018 0.096 2.591 0.11 50816. 0.0160
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17.69 0.6672 0.0055 0.0001 0.0122 0.004 0.133 0.000 3.147 0.015 0.002 0.070 0.11 50939. 0.0001
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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 0.0966 0.0364 0.042 0.892 1.065 31.676 0.101 4.736 15.247 0.17 73099. 0.6594
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0.93 0.0233 0.0603 0.0950 0.0367 0.043 0.901 1.047 31.987 0.102 4.655 14.840 0.17 73149. 0.6363
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1.85 0.0466 0.1173 0.0932 0.0370 0.043 0.909 1.027 32.268 0.103 4.568 14.435 0.17 73202. 0.6131
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2.78 0.0699 0.1711 0.0913 0.0373 0.044 0.916 1.006 32.514 0.103 4.474 14.033 0.17 73259. 0.5899
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3.71 0.0932 0.2217 0.0893 0.0375 0.044 0.922 0.984 32.717 0.104 4.375 13.635 0.17 73320. 0.5668
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4.64 0.1165 0.2691 0.0871 0.0377 0.044 0.926 0.960 32.870 0.105 4.269 13.242 0.17 73386. 0.5437
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5.56 0.1398 0.3134 0.0848 0.0378 0.044 0.929 0.934 32.965 0.105 4.155 12.854 0.17 73456. 0.5207
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6.49 0.1632 0.3548 0.0823 0.0379 0.044 0.930 0.907 32.994 0.105 4.035 12.471 0.17 73530. 0.4978
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7.42 0.1865 0.3932 0.0797 0.0378 0.044 0.928 0.879 32.950 0.105 3.908 12.093 0.17 73610. 0.4751
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8.34 0.2098 0.4287 0.0770 0.0377 0.044 0.925 0.848 32.823 0.104 3.773 11.720 0.17 73694. 0.4524
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9.27 0.2331 0.4613 0.0741 0.0374 0.044 0.919 0.816 32.606 0.104 3.630 11.352 0.17 73783. 0.4298
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10.20 0.2564 0.4912 0.0710 0.0371 0.043 0.910 0.782 32.290 0.103 3.479 10.987 0.17 73877. 0.4073
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11.12 0.2797 0.5182 0.0678 0.0366 0.043 0.898 0.747 31.872 0.101 3.321 10.626 0.17 73976. 0.3848
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12.05 0.3030 0.5425 0.0644 0.0360 0.042 0.883 0.710 31.347 0.100 3.156 10.268 0.17 74080. 0.3625
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12.98 0.3263 0.5639 0.0609 0.0352 0.041 0.865 0.671 30.714 0.098 2.985 9.910 0.17 74190. 0.3403
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13.91 0.3496 0.5823 0.0573 0.0344 0.040 0.844 0.631 29.972 0.095 2.808 9.552 0.17 74305. 0.3181
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14.83 0.3729 0.5977 0.0536 0.0334 0.039 0.820 0.590 29.120 0.093 2.625 9.192 0.17 74425. 0.2960
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15.76 0.3962 0.6098 0.0497 0.0323 0.038 0.793 0.548 28.157 0.090 2.437 8.827 0.17 74550. 0.2738
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16.69 0.4195 0.6184 0.0458 0.0311 0.036 0.763 0.505 27.080 0.086 2.245 8.453 0.17 74681. 0.2517
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17.61 0.4429 0.6230 0.0418 0.0297 0.035 0.729 0.461 25.890 0.082 2.048 8.068 0.17 74817. 0.2295
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18.54 0.4662 0.6231 0.0377 0.0282 0.033 0.693 0.415 24.584 0.078 1.848 7.666 0.17 74959. 0.2071
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19.47 0.4895 0.6178 0.0335 0.0266 0.031 0.653 0.370 23.162 0.074 1.644 7.239 0.17 75106. 0.1845
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20.39 0.5128 0.6060 0.0293 0.0248 0.029 0.609 0.323 21.623 0.069 1.437 6.778 0.17 75259. 0.1615
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21.32 0.5361 0.5860 0.0250 0.0229 0.027 0.563 0.276 19.968 0.064 1.228 6.269 0.17 75417. 0.1380
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22.25 0.5594 0.5552 0.0207 0.0209 0.024 0.513 0.228 18.197 0.058 1.016 5.692 0.17 75581. 0.1140
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23.18 0.5827 0.5095 0.0164 0.0187 0.022 0.460 0.180 16.312 0.052 0.802 5.015 0.17 75751. 0.0893
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24.10 0.6060 0.4422 0.0120 0.0164 0.019 0.403 0.132 14.317 0.046 0.588 4.185 0.17 75926. 0.0638
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25.03 0.6293 0.3413 0.0076 0.0140 0.016 0.344 0.084 12.216 0.039 0.373 3.110 0.17 76107. 0.0377
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25.96 0.6526 0.1829 0.0032 0.0115 0.013 0.282 0.035 10.014 0.032 0.158 1.608 0.17 76292. 0.0127
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26.88 0.6759
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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 0.0970 0.0352 0.097 1.535 1.900 72.637 0.173 8.453 11.867 0.22 97464. 0.6856
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1.23 0.0231 0.0621 0.0954 0.0355 0.098 1.551 1.868 73.394 0.175 8.310 11.545 0.22 97529. 0.6614
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2.45 0.0463 0.1208 0.0936 0.0359 0.099 1.565 1.834 74.084 0.177 8.156 11.226 0.22 97599. 0.6371
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3.68 0.0694 0.1761 0.0917 0.0362 0.100 1.578 1.797 74.690 0.178 7.991 10.910 0.22 97675. 0.6129
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4.91 0.0925 0.2280 0.0897 0.0364 0.101 1.589 1.757 75.197 0.180 7.816 10.599 0.22 97756. 0.5888
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6.13 0.1157 0.2768 0.0876 0.0366 0.101 1.597 1.715 75.587 0.180 7.629 10.292 0.22 97842. 0.5649
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7.36 0.1388 0.3224 0.0853 0.0367 0.102 1.603 1.670 75.842 0.181 7.429 9.989 0.22 97935. 0.5411
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8.59 0.1620 0.3649 0.0828 0.0368 0.102 1.605 1.623 75.942 0.181 7.218 9.692 0.22 98034. 0.5174
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9.82 0.1851 0.4044 0.0803 0.0367 0.102 1.603 1.572 75.870 0.181 6.993 9.399 0.22 98138. 0.4939
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11.04 0.2082 0.4411 0.0775 0.0366 0.101 1.598 1.519 75.604 0.180 6.755 9.111 0.22 98250. 0.4706
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12.27 0.2314 0.4748 0.0746 0.0364 0.101 1.587 1.462 75.125 0.179 6.504 8.828 0.22 98367. 0.4474
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13.50 0.2545 0.5058 0.0716 0.0360 0.100 1.572 1.403 74.417 0.178 6.239 8.549 0.22 98491. 0.4243
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14.72 0.2776 0.5340 0.0684 0.0356 0.099 1.552 1.340 73.465 0.175 5.960 8.273 0.22 98622. 0.4014
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15.95 0.3008 0.5595 0.0651 0.0350 0.097 1.527 1.275 72.261 0.173 5.670 8.001 0.22 98759. 0.3786
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17.18 0.3239 0.5822 0.0616 0.0343 0.095 1.496 1.207 70.801 0.169 5.368 7.731 0.22 98904. 0.3560
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18.40 0.3471 0.6021 0.0580 0.0334 0.093 1.460 1.137 69.082 0.165 5.055 7.462 0.22 99055. 0.3334
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19.63 0.3702 0.6191 0.0543 0.0325 0.090 1.418 1.064 67.101 0.160 4.733 7.193 0.22 99213. 0.3110
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20.86 0.3933 0.6329 0.0505 0.0314 0.087 1.370 0.990 64.855 0.155 4.402 6.922 0.22 99378. 0.2886
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22.09 0.4165 0.6435 0.0466 0.0302 0.084 1.317 0.914 62.340 0.149 4.063 6.646 0.22 99550. 0.2662
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23.31 0.4396 0.6504 0.0427 0.0288 0.080 1.258 0.836 59.553 0.142 3.717 6.364 0.22 99730. 0.2438
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24.54 0.4627 0.6531 0.0386 0.0273 0.076 1.194 0.756 56.491 0.135 3.363 6.071 0.22 99916. 0.2213
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25.77 0.4859 0.6509 0.0345 0.0257 0.071 1.123 0.675 53.152 0.127 3.004 5.763 0.22 100110. 0.1985
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26.99 0.5090 0.6428 0.0303 0.0240 0.066 1.047 0.593 49.534 0.118 2.639 5.432 0.23 100312. 0.1753
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28.22 0.5321 0.6271 0.0260 0.0221 0.061 0.964 0.510 45.637 0.109 2.269 5.069 0.23 100520. 0.1517
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29.45 0.5553 0.6016 0.0217 0.0201 0.056 0.876 0.426 41.463 0.099 1.895 4.660 0.23 100736. 0.1275
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30.67 0.5784 0.5622 0.0174 0.0179 0.050 0.782 0.341 37.017 0.088 1.518 4.181 0.23 100959. 0.1024
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31.90 0.6016 0.5027 0.0131 0.0156 0.043 0.683 0.256 32.304 0.077 1.139 3.594 0.23 101189. 0.0762
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33.13 0.6247 0.4110 0.0087 0.0132 0.037 0.578 0.171 27.335 0.065 0.759 2.830 0.23 101427. 0.0490
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34.35 0.6478 0.2631 0.0044 0.0107 0.030 0.468 0.085 22.124 0.053 0.379 1.747 0.23 101672. 0.0214
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35.58 0.6710 -0.0005 0.0000 0.0081 0.022 0.352 0.000 16.661 0.040 -0.001 -0.003 0.23 101913. 0.0000
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PROP RPM = 5000
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V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
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(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
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0.00 0.0000 0.0000 0.0975 0.0345 0.186 2.351 2.983 139.059 0.266 13.267 9.729 0.28 121826. 0.7042
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1.54 0.0232 0.0637 0.0958 0.0348 0.189 2.376 2.932 140.578 0.268 13.043 9.461 0.28 121908. 0.6790
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3.07 0.0464 0.1239 0.0940 0.0352 0.190 2.400 2.878 141.965 0.271 12.802 9.195 0.28 121996. 0.6538
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4.61 0.0695 0.1805 0.0921 0.0355 0.192 2.420 2.820 143.187 0.273 12.544 8.933 0.28 122091. 0.6288
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6.15 0.0927 0.2338 0.0901 0.0357 0.193 2.438 2.758 144.211 0.275 12.269 8.675 0.28 122192. 0.6039
|
|
7.68 0.1159 0.2836 0.0880 0.0359 0.194 2.451 2.692 145.005 0.277 11.975 8.422 0.28 122301. 0.5791
|
|
9.22 0.1391 0.3303 0.0857 0.0361 0.195 2.460 2.622 145.531 0.278 11.663 8.172 0.28 122417. 0.5546
|
|
10.76 0.1623 0.3738 0.0832 0.0361 0.195 2.464 2.547 145.752 0.278 11.331 7.927 0.28 122541. 0.5303
|
|
12.29 0.1854 0.4142 0.0806 0.0361 0.195 2.462 2.468 145.629 0.278 10.978 7.687 0.28 122673. 0.5061
|
|
13.83 0.2086 0.4517 0.0779 0.0360 0.195 2.453 2.384 145.123 0.277 10.604 7.451 0.28 122812. 0.4822
|
|
15.37 0.2318 0.4863 0.0750 0.0357 0.193 2.438 2.295 144.197 0.275 10.209 7.220 0.28 122960. 0.4584
|
|
16.90 0.2550 0.5181 0.0719 0.0354 0.192 2.414 2.202 142.814 0.273 9.793 6.992 0.28 123115. 0.4348
|
|
18.44 0.2782 0.5471 0.0687 0.0349 0.189 2.383 2.103 140.946 0.269 9.356 6.769 0.28 123279. 0.4114
|
|
19.98 0.3013 0.5734 0.0654 0.0344 0.186 2.343 2.001 138.579 0.265 8.899 6.548 0.28 123452. 0.3882
|
|
21.51 0.3245 0.5970 0.0619 0.0336 0.182 2.294 1.894 135.702 0.259 8.424 6.330 0.28 123633. 0.3651
|
|
23.05 0.3477 0.6178 0.0583 0.0328 0.177 2.237 1.783 132.311 0.253 7.933 6.114 0.28 123823. 0.3422
|
|
24.58 0.3709 0.6357 0.0546 0.0318 0.172 2.171 1.670 128.398 0.245 7.426 5.898 0.28 124021. 0.3194
|
|
26.12 0.3941 0.6506 0.0507 0.0307 0.166 2.095 1.553 123.957 0.237 6.906 5.681 0.28 124229. 0.2967
|
|
27.66 0.4172 0.6623 0.0468 0.0295 0.160 2.011 1.433 118.980 0.227 6.373 5.462 0.28 124445. 0.2740
|
|
29.19 0.4404 0.6704 0.0428 0.0281 0.152 1.918 1.310 113.461 0.217 5.828 5.238 0.28 124670. 0.2513
|
|
30.73 0.4636 0.6745 0.0387 0.0266 0.144 1.815 1.185 107.394 0.205 5.273 5.007 0.28 124904. 0.2285
|
|
32.27 0.4868 0.6738 0.0346 0.0250 0.135 1.704 1.058 100.774 0.192 4.708 4.764 0.28 125147. 0.2054
|
|
33.80 0.5100 0.6674 0.0304 0.0232 0.126 1.582 0.929 93.598 0.179 4.134 4.504 0.28 125400. 0.1820
|
|
35.34 0.5331 0.6536 0.0261 0.0213 0.115 1.452 0.799 85.866 0.164 3.552 4.219 0.28 125661. 0.1580
|
|
36.88 0.5563 0.6300 0.0218 0.0192 0.104 1.311 0.667 77.582 0.148 2.965 3.897 0.28 125932. 0.1333
|
|
38.41 0.5795 0.5925 0.0174 0.0170 0.092 1.162 0.533 68.754 0.131 2.372 3.518 0.28 126212. 0.1077
|
|
39.95 0.6027 0.5342 0.0131 0.0147 0.080 1.004 0.399 59.397 0.113 1.777 3.050 0.28 126501. 0.0808
|
|
41.49 0.6259 0.4418 0.0087 0.0123 0.066 0.837 0.265 49.531 0.095 1.180 2.429 0.28 126799. 0.0524
|
|
43.02 0.6490 0.2865 0.0043 0.0097 0.053 0.662 0.131 39.182 0.075 0.584 1.519 0.28 127105. 0.0231
|
|
44.56 0.6722 -0.0093 -0.0001 0.0070 0.038 0.479 -0.003 28.312 0.054 -0.013 -0.047 0.28 127404. 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 0.0980 0.0341 0.318 3.345 4.318 237.465 0.378 19.206 8.247 0.33 146185. 0.7183
|
|
1.86 0.0233 0.0652 0.0963 0.0345 0.322 3.383 4.245 240.159 0.382 18.880 8.016 0.33 146284. 0.6922
|
|
3.71 0.0467 0.1267 0.0945 0.0348 0.325 3.418 4.166 242.619 0.386 18.530 7.788 0.33 146391. 0.6662
|
|
5.57 0.0700 0.1846 0.0926 0.0351 0.328 3.448 4.082 244.787 0.390 18.156 7.563 0.33 146506. 0.6404
|
|
7.42 0.0933 0.2390 0.0906 0.0354 0.331 3.474 3.992 246.605 0.392 17.756 7.342 0.33 146629. 0.6148
|
|
9.28 0.1167 0.2899 0.0884 0.0356 0.333 3.494 3.896 248.013 0.395 17.329 7.125 0.33 146761. 0.5894
|
|
11.14 0.1400 0.3374 0.0861 0.0357 0.334 3.507 3.794 248.945 0.396 16.874 6.912 0.33 146902. 0.5642
|
|
12.99 0.1633 0.3818 0.0836 0.0358 0.334 3.512 3.685 249.336 0.397 16.389 6.703 0.33 147053. 0.5393
|
|
14.85 0.1867 0.4230 0.0810 0.0357 0.334 3.509 3.569 249.115 0.396 15.875 6.498 0.33 147212. 0.5145
|
|
16.70 0.2100 0.4612 0.0782 0.0356 0.333 3.497 3.446 248.214 0.395 15.330 6.298 0.33 147381. 0.4900
|
|
18.56 0.2333 0.4965 0.0753 0.0354 0.331 3.473 3.317 246.564 0.392 14.754 6.102 0.33 147561. 0.4657
|
|
20.42 0.2567 0.5289 0.0722 0.0350 0.327 3.439 3.180 244.102 0.388 14.146 5.909 0.33 147750. 0.4417
|
|
22.27 0.2800 0.5585 0.0689 0.0345 0.323 3.392 3.037 240.780 0.383 13.507 5.720 0.33 147949. 0.4178
|
|
24.13 0.3033 0.5854 0.0655 0.0339 0.317 3.333 2.887 236.570 0.377 12.840 5.535 0.33 148158. 0.3941
|
|
25.98 0.3266 0.6096 0.0620 0.0332 0.310 3.261 2.731 231.458 0.368 12.147 5.351 0.33 148378. 0.3706
|
|
27.84 0.3500 0.6310 0.0583 0.0323 0.302 3.176 2.570 225.430 0.359 11.429 5.170 0.34 148609. 0.3473
|
|
29.70 0.3733 0.6495 0.0545 0.0313 0.293 3.078 2.403 218.476 0.348 10.690 4.989 0.34 148850. 0.3242
|
|
31.55 0.3966 0.6651 0.0507 0.0302 0.282 2.966 2.232 210.582 0.335 9.930 4.809 0.34 149101. 0.3011
|
|
33.41 0.4200 0.6775 0.0467 0.0289 0.271 2.842 2.057 201.737 0.321 9.152 4.626 0.34 149364. 0.2781
|
|
35.26 0.4433 0.6863 0.0426 0.0275 0.257 2.704 1.879 191.929 0.305 8.356 4.440 0.34 149637. 0.2550
|
|
37.12 0.4666 0.6912 0.0385 0.0260 0.243 2.552 1.696 181.146 0.288 7.545 4.247 0.34 149922. 0.2319
|
|
38.98 0.4900 0.6913 0.0343 0.0243 0.227 2.386 1.511 169.380 0.270 6.720 4.046 0.34 150217. 0.2084
|
|
40.83 0.5133 0.6856 0.0300 0.0225 0.210 2.206 1.323 156.627 0.249 5.883 3.830 0.34 150524. 0.1846
|
|
42.69 0.5366 0.6724 0.0257 0.0205 0.192 2.013 1.132 142.887 0.227 5.035 3.593 0.34 150841. 0.1602
|
|
44.54 0.5600 0.6490 0.0213 0.0184 0.172 1.806 0.939 128.168 0.204 4.177 3.324 0.34 151170. 0.1350
|
|
46.40 0.5833 0.6110 0.0169 0.0161 0.151 1.585 0.745 112.486 0.179 3.314 3.004 0.34 151510. 0.1087
|
|
48.26 0.6066 0.5503 0.0125 0.0138 0.129 1.351 0.550 95.869 0.153 2.445 2.601 0.34 151861. 0.0808
|
|
50.11 0.6300 0.4506 0.0080 0.0112 0.105 1.104 0.354 78.357 0.125 1.576 2.051 0.34 152223. 0.0512
|
|
51.97 0.6533 0.2742 0.0036 0.0086 0.080 0.845 0.159 59.995 0.095 0.708 1.204 0.34 152595. 0.0201
|
|
53.82 0.6766
|
|
|
|
|
|
|
|
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 0.0986 0.0339 0.503 4.526 5.913 374.809 0.511 26.302 7.156 0.39 170542. 0.7293
|
|
2.16 0.0233 0.0660 0.0969 0.0343 0.508 4.578 5.814 379.162 0.517 25.859 6.954 0.39 170657. 0.7028
|
|
4.33 0.0466 0.1282 0.0951 0.0346 0.514 4.626 5.706 383.137 0.523 25.382 6.756 0.39 170782. 0.6764
|
|
6.49 0.0700 0.1867 0.0932 0.0349 0.518 4.669 5.592 386.642 0.527 24.872 6.560 0.39 170917. 0.6501
|
|
8.66 0.0933 0.2417 0.0912 0.0352 0.522 4.704 5.469 389.586 0.531 24.327 6.367 0.39 171061. 0.6241
|
|
10.82 0.1166 0.2931 0.0890 0.0354 0.526 4.732 5.338 391.869 0.535 23.744 6.179 0.39 171215. 0.5983
|
|
12.99 0.1399 0.3412 0.0867 0.0355 0.528 4.750 5.199 393.390 0.537 23.123 5.994 0.39 171380. 0.5728
|
|
15.15 0.1633 0.3861 0.0842 0.0356 0.528 4.758 5.050 394.042 0.538 22.462 5.813 0.39 171555. 0.5475
|
|
17.31 0.1866 0.4278 0.0816 0.0356 0.528 4.754 4.892 393.713 0.537 21.760 5.636 0.39 171742. 0.5225
|
|
19.48 0.2099 0.4665 0.0788 0.0354 0.526 4.737 4.725 392.293 0.535 21.016 5.463 0.39 171940. 0.4977
|
|
21.64 0.2332 0.5023 0.0758 0.0352 0.523 4.705 4.548 389.672 0.532 20.228 5.293 0.39 172149. 0.4731
|
|
23.81 0.2565 0.5352 0.0727 0.0348 0.517 4.658 4.361 385.748 0.526 19.397 5.128 0.39 172370. 0.4488
|
|
25.97 0.2799 0.5653 0.0694 0.0344 0.510 4.594 4.165 380.443 0.519 18.525 4.965 0.39 172602. 0.4247
|
|
28.14 0.3032 0.5928 0.0660 0.0338 0.501 4.512 3.960 373.714 0.510 17.613 4.806 0.39 172847. 0.4008
|
|
30.30 0.3265 0.6175 0.0625 0.0330 0.490 4.414 3.746 365.532 0.499 16.664 4.649 0.39 173104. 0.3771
|
|
32.46 0.3498 0.6396 0.0588 0.0321 0.477 4.297 3.526 355.881 0.485 15.683 4.494 0.39 173373. 0.3537
|
|
34.63 0.3731 0.6588 0.0550 0.0311 0.462 4.163 3.298 344.741 0.470 14.671 4.340 0.39 173654. 0.3303
|
|
36.79 0.3965 0.6752 0.0511 0.0300 0.445 4.010 3.065 332.092 0.453 13.632 4.186 0.39 173948. 0.3071
|
|
38.96 0.4198 0.6884 0.0471 0.0287 0.426 3.839 2.825 317.914 0.434 12.567 4.031 0.39 174254. 0.2840
|
|
41.12 0.4431 0.6983 0.0430 0.0273 0.405 3.649 2.581 302.187 0.412 11.478 3.873 0.39 174573. 0.2608
|
|
43.29 0.4664 0.7043 0.0389 0.0257 0.382 3.440 2.331 284.894 0.389 10.369 3.711 0.39 174905. 0.2375
|
|
45.45 0.4898 0.7057 0.0346 0.0240 0.357 3.212 2.077 266.022 0.363 9.239 3.542 0.39 175249. 0.2139
|
|
47.62 0.5131 0.7015 0.0303 0.0222 0.329 2.965 1.819 245.563 0.335 8.093 3.361 0.39 175607. 0.1900
|
|
49.78 0.5364 0.6901 0.0260 0.0202 0.300 2.699 1.558 223.518 0.305 6.932 3.162 0.39 175977. 0.1655
|
|
51.94 0.5597 0.6689 0.0216 0.0181 0.268 2.414 1.295 199.899 0.273 5.758 2.937 0.39 176361. 0.1401
|
|
54.11 0.5830 0.6334 0.0171 0.0158 0.234 2.110 1.029 174.732 0.238 4.576 2.670 0.40 176757. 0.1135
|
|
56.27 0.6064 0.5755 0.0127 0.0134 0.199 1.788 0.761 148.060 0.202 3.387 2.333 0.40 177166. 0.0853
|
|
58.44 0.6297 0.4783 0.0082 0.0108 0.161 1.448 0.494 119.948 0.164 2.196 1.867 0.40 177589. 0.0550
|
|
60.60 0.6530 0.3018 0.0038 0.0082 0.121 1.092 0.227 90.471 0.123 1.008 1.136 0.40 178022. 0.0227
|
|
62.77 0.6763
|
|
|
|
|
|
|
|
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 0.0993 0.0338 0.749 5.902 7.779 558.642 0.667 34.600 6.316 0.44 194894. 0.7383
|
|
2.46 0.0232 0.0662 0.0976 0.0342 0.758 5.972 7.649 565.216 0.675 34.023 6.138 0.44 195026. 0.7115
|
|
4.92 0.0464 0.1287 0.0958 0.0346 0.766 6.035 7.510 571.222 0.682 33.404 5.963 0.44 195168. 0.6849
|
|
7.38 0.0696 0.1875 0.0939 0.0349 0.773 6.091 7.361 576.524 0.688 32.740 5.791 0.44 195321. 0.6585
|
|
9.85 0.0928 0.2427 0.0919 0.0352 0.779 6.138 7.201 580.984 0.693 32.030 5.622 0.44 195486. 0.6323
|
|
12.31 0.1160 0.2944 0.0897 0.0354 0.784 6.175 7.030 584.457 0.698 31.271 5.456 0.44 195661. 0.6063
|
|
14.77 0.1392 0.3427 0.0874 0.0355 0.787 6.200 6.849 586.791 0.700 30.462 5.294 0.44 195849. 0.5806
|
|
17.23 0.1625 0.3879 0.0849 0.0356 0.788 6.211 6.655 587.826 0.702 29.601 5.135 0.44 196049. 0.5552
|
|
19.69 0.1857 0.4299 0.0823 0.0355 0.788 6.206 6.449 587.399 0.701 28.686 4.980 0.45 196261. 0.5300
|
|
22.15 0.2089 0.4689 0.0795 0.0354 0.785 6.184 6.231 585.344 0.699 27.716 4.828 0.45 196486. 0.5052
|
|
24.61 0.2321 0.5051 0.0766 0.0352 0.780 6.144 6.000 581.498 0.694 26.690 4.680 0.45 196724. 0.4805
|
|
27.08 0.2553 0.5384 0.0735 0.0348 0.772 6.083 5.757 575.710 0.687 25.607 4.536 0.45 196975. 0.4561
|
|
29.54 0.2785 0.5690 0.0702 0.0344 0.762 6.000 5.501 567.860 0.678 24.469 4.394 0.45 197239. 0.4319
|
|
32.00 0.3017 0.5969 0.0668 0.0338 0.748 5.894 5.234 557.877 0.666 23.279 4.255 0.45 197517. 0.4080
|
|
34.46 0.3249 0.6222 0.0632 0.0330 0.732 5.766 4.955 545.722 0.651 22.041 4.119 0.45 197808. 0.3843
|
|
36.92 0.3481 0.6449 0.0596 0.0322 0.713 5.614 4.667 531.367 0.634 20.760 3.984 0.45 198114. 0.3607
|
|
39.38 0.3713 0.6648 0.0558 0.0312 0.690 5.439 4.370 514.785 0.614 19.439 3.851 0.45 198433. 0.3374
|
|
41.84 0.3945 0.6820 0.0519 0.0300 0.665 5.240 4.065 495.945 0.592 18.082 3.718 0.45 198766. 0.3142
|
|
44.31 0.4177 0.6962 0.0479 0.0287 0.637 5.017 3.752 474.818 0.567 16.690 3.584 0.45 199114. 0.2910
|
|
46.77 0.4410 0.7072 0.0438 0.0273 0.605 4.769 3.432 451.375 0.539 15.268 3.449 0.45 199476. 0.2678
|
|
49.23 0.4642 0.7145 0.0396 0.0258 0.571 4.496 3.106 425.591 0.508 13.817 3.311 0.45 199852. 0.2445
|
|
51.69 0.4874 0.7175 0.0354 0.0241 0.533 4.199 2.774 397.444 0.474 12.341 3.166 0.45 200243. 0.2210
|
|
54.15 0.5106 0.7153 0.0311 0.0222 0.492 3.877 2.437 366.921 0.438 10.842 3.013 0.45 200648. 0.1971
|
|
56.61 0.5338 0.7064 0.0268 0.0202 0.448 3.529 2.096 334.024 0.399 9.323 2.846 0.45 201068. 0.1727
|
|
59.07 0.5570 0.6883 0.0223 0.0181 0.401 3.157 1.751 298.767 0.357 7.787 2.658 0.45 201502. 0.1474
|
|
61.54 0.5802 0.6571 0.0179 0.0158 0.350 2.760 1.403 261.187 0.312 6.239 2.436 0.45 201952. 0.1209
|
|
64.00 0.6034 0.6052 0.0134 0.0134 0.297 2.339 1.053 221.344 0.264 4.683 2.157 0.45 202416. 0.0928
|
|
66.46 0.6266 0.5173 0.0090 0.0109 0.240 1.895 0.702 179.329 0.214 3.122 1.776 0.45 202894. 0.0623
|
|
68.92 0.6498 0.3564 0.0045 0.0082 0.181 1.429 0.352 135.259 0.161 1.565 1.179 0.45 203385. 0.0293
|
|
71.38 0.6730 0.0006 0.0000 0.0054 0.119 0.939 0.000 88.877 0.106 0.002 0.002 0.45 203857. 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 0.1001 0.0339 1.069 7.488 9.926 797.296 0.846 44.152 5.647 0.50 219241. 0.7457
|
|
2.77 0.0232 0.0667 0.0984 0.0343 1.082 7.577 9.762 806.820 0.856 43.421 5.488 0.50 219390. 0.7186
|
|
5.54 0.0465 0.1295 0.0967 0.0347 1.094 7.659 9.585 815.518 0.865 42.635 5.331 0.50 219551. 0.6917
|
|
8.31 0.0697 0.1887 0.0947 0.0350 1.104 7.731 9.396 823.190 0.873 41.792 5.177 0.50 219724. 0.6651
|
|
11.09 0.0929 0.2442 0.0927 0.0353 1.113 7.791 9.193 829.637 0.880 40.889 5.026 0.50 219910. 0.6386
|
|
13.86 0.1161 0.2963 0.0905 0.0355 1.119 7.839 8.976 834.650 0.886 39.925 4.878 0.50 220108. 0.6125
|
|
16.63 0.1394 0.3450 0.0882 0.0356 1.124 7.870 8.744 838.010 0.889 38.895 4.733 0.50 220320. 0.5866
|
|
19.40 0.1626 0.3905 0.0857 0.0357 1.126 7.884 8.498 839.487 0.891 37.799 4.591 0.50 220546. 0.5610
|
|
22.17 0.1858 0.4328 0.0831 0.0357 1.125 7.878 8.236 838.844 0.890 36.634 4.453 0.50 220786. 0.5356
|
|
24.94 0.2090 0.4722 0.0803 0.0355 1.121 7.850 7.958 835.844 0.887 35.397 4.318 0.50 221040. 0.5106
|
|
27.71 0.2323 0.5087 0.0773 0.0353 1.113 7.797 7.664 830.255 0.881 34.088 4.187 0.50 221308. 0.4858
|
|
30.49 0.2555 0.5424 0.0742 0.0349 1.102 7.718 7.353 821.853 0.872 32.707 4.058 0.50 221592. 0.4612
|
|
33.26 0.2787 0.5733 0.0709 0.0344 1.087 7.611 7.027 810.468 0.860 31.255 3.932 0.50 221890. 0.4369
|
|
36.03 0.3020 0.6017 0.0674 0.0338 1.067 7.475 6.685 795.995 0.845 29.736 3.809 0.50 222204. 0.4128
|
|
38.80 0.3252 0.6274 0.0638 0.0331 1.044 7.310 6.330 778.380 0.826 28.156 3.689 0.50 222533. 0.3889
|
|
41.57 0.3484 0.6505 0.0601 0.0322 1.016 7.115 5.962 757.582 0.804 26.519 3.570 0.50 222878. 0.3653
|
|
44.34 0.3716 0.6710 0.0563 0.0312 0.984 6.889 5.583 733.562 0.778 24.832 3.452 0.50 223238. 0.3418
|
|
47.11 0.3949 0.6888 0.0524 0.0300 0.947 6.633 5.193 706.279 0.749 23.097 3.335 0.50 223614. 0.3185
|
|
49.89 0.4181 0.7036 0.0483 0.0287 0.906 6.346 4.793 675.691 0.717 21.319 3.217 0.50 224006. 0.2952
|
|
52.66 0.4413 0.7153 0.0442 0.0273 0.861 6.027 4.384 641.756 0.681 19.501 3.099 0.50 224414. 0.2719
|
|
55.43 0.4645 0.7234 0.0400 0.0257 0.811 5.676 3.967 604.437 0.641 17.647 2.977 0.51 224838. 0.2485
|
|
58.20 0.4878 0.7274 0.0357 0.0240 0.756 5.294 3.543 563.705 0.598 15.760 2.851 0.51 225279. 0.2249
|
|
60.97 0.5110 0.7262 0.0314 0.0221 0.697 4.879 3.112 519.541 0.551 13.843 2.717 0.51 225736. 0.2009
|
|
63.74 0.5342 0.7186 0.0270 0.0201 0.633 4.432 2.676 471.946 0.501 11.901 2.571 0.51 226209. 0.1763
|
|
66.51 0.5574 0.7020 0.0225 0.0179 0.564 3.953 2.234 420.943 0.447 9.938 2.407 0.51 226699. 0.1508
|
|
69.29 0.5807 0.6724 0.0180 0.0156 0.492 3.443 1.789 366.584 0.389 7.958 2.214 0.51 227206. 0.1241
|
|
72.06 0.6039 0.6222 0.0135 0.0131 0.414 2.902 1.342 308.957 0.328 5.968 1.970 0.51 227728. 0.0956
|
|
74.83 0.6271 0.5354 0.0090 0.0105 0.333 2.331 0.893 248.197 0.263 3.972 1.632 0.51 228267. 0.0646
|
|
77.60 0.6504 0.3723 0.0045 0.0078 0.247 1.732 0.445 184.470 0.196 1.980 1.094 0.51 228821. 0.0306
|
|
80.37 0.6736 -0.0070 -0.0001 0.0050 0.157 1.101 -0.005 117.285 0.124 -0.023 -0.020 0.51 229344. 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 0.1010 0.0341 1.475 9.299 12.370 1100.145 1.051 55.024 5.100 0.56 243582. 0.7518
|
|
3.08 0.0232 0.0669 0.0994 0.0345 1.493 9.411 12.167 1113.452 1.063 54.121 4.956 0.56 243748. 0.7246
|
|
6.16 0.0465 0.1301 0.0976 0.0349 1.509 9.514 11.949 1125.591 1.075 53.148 4.815 0.56 243928. 0.6976
|
|
9.24 0.0697 0.1895 0.0957 0.0352 1.524 9.604 11.714 1136.288 1.085 52.104 4.676 0.56 244121. 0.6707
|
|
12.32 0.0929 0.2452 0.0936 0.0355 1.536 9.680 11.463 1145.264 1.094 50.986 4.540 0.56 244328. 0.6442
|
|
15.40 0.1162 0.2976 0.0914 0.0357 1.545 9.739 11.194 1152.229 1.100 49.789 4.406 0.56 244550. 0.6179
|
|
18.48 0.1394 0.3465 0.0891 0.0358 1.551 9.778 10.906 1156.876 1.105 48.512 4.276 0.56 244787. 0.5919
|
|
21.56 0.1627 0.3922 0.0866 0.0359 1.554 9.795 10.600 1158.887 1.107 47.150 4.149 0.56 245038. 0.5661
|
|
24.65 0.1859 0.4348 0.0839 0.0359 1.553 9.787 10.275 1157.936 1.106 45.701 4.025 0.56 245306. 0.5407
|
|
27.73 0.2091 0.4745 0.0811 0.0357 1.547 9.751 9.929 1153.693 1.102 44.163 3.903 0.56 245589. 0.5155
|
|
30.81 0.2324 0.5112 0.0781 0.0355 1.537 9.685 9.563 1145.834 1.094 42.535 3.785 0.56 245889. 0.4906
|
|
33.89 0.2556 0.5452 0.0750 0.0351 1.521 9.585 9.176 1134.053 1.083 40.815 3.670 0.56 246205. 0.4659
|
|
36.97 0.2788 0.5765 0.0716 0.0346 1.499 9.451 8.769 1118.109 1.068 39.006 3.557 0.56 246538. 0.4415
|
|
40.05 0.3021 0.6052 0.0682 0.0340 1.472 9.279 8.344 1097.857 1.048 37.114 3.447 0.56 246888. 0.4173
|
|
43.13 0.3253 0.6314 0.0645 0.0333 1.439 9.071 7.901 1073.222 1.025 35.144 3.339 0.56 247254. 0.3934
|
|
46.21 0.3486 0.6549 0.0608 0.0324 1.400 8.825 7.442 1044.148 0.997 33.104 3.233 0.56 247638. 0.3697
|
|
49.29 0.3718 0.6759 0.0569 0.0313 1.355 8.542 6.969 1010.584 0.965 30.999 3.128 0.56 248040. 0.3461
|
|
52.37 0.3950 0.6942 0.0530 0.0301 1.304 8.220 6.483 972.474 0.929 28.836 3.024 0.56 248459. 0.3227
|
|
55.45 0.4183 0.7097 0.0489 0.0288 1.247 7.859 5.984 929.762 0.888 26.617 2.919 0.56 248895. 0.2993
|
|
58.53 0.4415 0.7220 0.0447 0.0273 1.183 7.458 5.474 882.391 0.843 24.349 2.814 0.56 249350. 0.2759
|
|
61.61 0.4647 0.7310 0.0405 0.0257 1.113 7.018 4.954 830.311 0.793 22.035 2.706 0.56 249822. 0.2524
|
|
64.69 0.4880 0.7358 0.0361 0.0240 1.037 6.538 4.424 773.478 0.739 19.679 2.594 0.56 250312. 0.2287
|
|
67.78 0.5112 0.7358 0.0317 0.0221 0.955 6.017 3.886 711.872 0.680 17.287 2.476 0.56 250821. 0.2046
|
|
70.86 0.5345 0.7293 0.0273 0.0200 0.866 5.456 3.341 645.491 0.616 14.862 2.348 0.56 251348. 0.1799
|
|
73.94 0.5577 0.7142 0.0228 0.0178 0.770 4.855 2.790 574.366 0.548 12.411 2.203 0.56 251893. 0.1543
|
|
77.02 0.5809 0.6863 0.0183 0.0154 0.669 4.214 2.234 498.571 0.476 9.938 2.033 0.56 252456. 0.1273
|
|
80.10 0.6042 0.6380 0.0137 0.0130 0.561 3.535 1.675 418.230 0.399 7.452 1.817 0.57 253038. 0.0986
|
|
83.18 0.6274 0.5529 0.0091 0.0103 0.447 2.819 1.115 333.530 0.318 4.959 1.516 0.57 253637. 0.0671
|
|
86.26 0.6506 0.3892 0.0045 0.0076 0.328 2.068 0.555 244.706 0.234 2.470 1.029 0.57 254253. 0.0321
|
|
89.34 0.6739 -0.0094 -0.0001 0.0047 0.202 1.276 -0.008 150.953 0.144 -0.036 -0.024 0.57 254828. 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 0.1021 0.0344 1.982 11.356 15.130 1477.960 1.283 67.297 4.643 0.61 267915. 0.7570
|
|
3.39 0.0232 0.0671 0.1005 0.0348 2.006 11.495 14.884 1496.033 1.299 66.205 4.513 0.61 268099. 0.7297
|
|
6.78 0.0465 0.1303 0.0987 0.0352 2.028 11.622 14.619 1512.505 1.313 65.026 4.384 0.61 268298. 0.7025
|
|
10.17 0.0697 0.1898 0.0968 0.0355 2.048 11.733 14.334 1526.999 1.326 63.760 4.258 0.61 268512. 0.6756
|
|
13.56 0.0930 0.2458 0.0947 0.0358 2.064 11.826 14.029 1539.132 1.336 62.401 4.134 0.61 268741. 0.6490
|
|
16.95 0.1162 0.2982 0.0925 0.0360 2.077 11.899 13.702 1548.516 1.344 60.946 4.013 0.61 268986. 0.6226
|
|
20.34 0.1395 0.3473 0.0901 0.0362 2.085 11.946 13.352 1554.743 1.350 59.391 3.895 0.61 269247. 0.5966
|
|
23.73 0.1627 0.3932 0.0876 0.0363 2.088 11.967 12.979 1557.379 1.352 57.732 3.780 0.61 269526. 0.5708
|
|
27.12 0.1860 0.4361 0.0849 0.0362 2.087 11.956 12.582 1555.984 1.351 55.965 3.668 0.61 269821. 0.5453
|
|
30.51 0.2092 0.4759 0.0821 0.0361 2.079 11.911 12.160 1550.115 1.346 54.089 3.558 0.61 270135. 0.5200
|
|
33.90 0.2325 0.5129 0.0791 0.0358 2.064 11.828 11.713 1539.339 1.336 52.101 3.451 0.61 270466. 0.4951
|
|
37.29 0.2557 0.5472 0.0759 0.0355 2.043 11.704 11.241 1523.243 1.322 50.001 3.347 0.61 270815. 0.4704
|
|
40.68 0.2790 0.5788 0.0725 0.0350 2.014 11.537 10.744 1501.497 1.303 47.790 3.246 0.61 271182. 0.4459
|
|
44.07 0.3022 0.6079 0.0690 0.0343 1.977 11.325 10.224 1473.911 1.280 45.476 3.146 0.61 271568. 0.4216
|
|
47.46 0.3254 0.6344 0.0654 0.0335 1.932 11.068 9.682 1440.379 1.250 43.067 3.049 0.61 271973. 0.3976
|
|
50.85 0.3487 0.6584 0.0616 0.0326 1.879 10.764 9.121 1400.833 1.216 40.571 2.953 0.61 272397. 0.3738
|
|
54.24 0.3719 0.6798 0.0577 0.0315 1.817 10.413 8.542 1355.206 1.176 37.995 2.859 0.62 272839. 0.3502
|
|
57.63 0.3952 0.6986 0.0536 0.0303 1.748 10.015 7.946 1303.429 1.132 35.346 2.765 0.62 273301. 0.3267
|
|
61.02 0.4184 0.7147 0.0495 0.0290 1.670 9.570 7.336 1245.427 1.081 32.629 2.672 0.62 273783. 0.3033
|
|
64.41 0.4417 0.7277 0.0453 0.0275 1.584 9.076 6.711 1181.126 1.025 29.851 2.577 0.62 274284. 0.2798
|
|
67.80 0.4649 0.7374 0.0410 0.0259 1.489 8.533 6.074 1110.457 0.964 27.016 2.481 0.62 274804. 0.2562
|
|
71.19 0.4882 0.7431 0.0366 0.0241 1.386 7.940 5.425 1033.366 0.897 24.130 2.381 0.62 275345. 0.2324
|
|
74.58 0.5114 0.7441 0.0322 0.0221 1.274 7.298 4.766 949.824 0.825 21.198 2.276 0.62 275905. 0.2082
|
|
77.97 0.5347 0.7388 0.0277 0.0200 1.153 6.607 4.098 859.829 0.746 18.226 2.162 0.62 276486. 0.1834
|
|
81.36 0.5579 0.7251 0.0231 0.0178 1.024 5.866 3.422 763.423 0.663 15.220 2.033 0.62 277086. 0.1576
|
|
84.75 0.5811 0.6989 0.0185 0.0154 0.886 5.077 2.740 660.706 0.574 12.188 1.881 0.62 277707. 0.1305
|
|
88.14 0.6044 0.6525 0.0139 0.0128 0.740 4.240 2.055 551.846 0.479 9.139 1.689 0.62 278347. 0.1014
|
|
91.53 0.6276 0.5693 0.0092 0.0102 0.586 3.359 1.367 437.097 0.379 6.081 1.419 0.62 279007. 0.0695
|
|
94.92 0.6509 0.4054 0.0046 0.0074 0.425 2.434 0.680 316.779 0.275 3.027 0.974 0.62 279685. 0.0337
|
|
98.31 0.6741 -0.0119 -0.0001 0.0044 0.254 1.457 -0.012 189.638 0.165 -0.051 -0.028 0.62 280311. 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 0.0349 2.606 13.690 18.227 1943.616 1.547 81.074 4.254 0.67 292239. 0.7611
|
|
3.70 0.0233 0.0671 0.1017 0.0353 2.639 13.859 17.935 1967.557 1.566 79.775 4.134 0.67 292441. 0.7339
|
|
7.40 0.0465 0.1303 0.0999 0.0357 2.668 14.012 17.620 1989.372 1.583 78.372 4.017 0.67 292659. 0.7067
|
|
11.10 0.0698 0.1899 0.0980 0.0360 2.694 14.147 17.280 2008.550 1.598 76.862 3.902 0.67 292894. 0.6799
|
|
14.80 0.0930 0.2458 0.0959 0.0363 2.715 14.260 16.915 2024.575 1.611 75.238 3.790 0.67 293145. 0.6532
|
|
18.50 0.1163 0.2984 0.0937 0.0365 2.732 14.347 16.524 2036.921 1.621 73.498 3.679 0.67 293414. 0.6269
|
|
22.20 0.1395 0.3476 0.0914 0.0367 2.742 14.404 16.105 2045.043 1.627 71.635 3.572 0.67 293701. 0.6008
|
|
25.90 0.1628 0.3936 0.0888 0.0367 2.747 14.428 15.658 2048.378 1.630 69.646 3.467 0.67 294006. 0.5750
|
|
29.60 0.1860 0.4366 0.0861 0.0367 2.744 14.414 15.181 2046.347 1.628 67.526 3.365 0.67 294331. 0.5495
|
|
33.30 0.2093 0.4766 0.0832 0.0366 2.733 14.357 14.675 2038.367 1.622 65.273 3.265 0.67 294674. 0.5243
|
|
36.99 0.2325 0.5139 0.0802 0.0363 2.714 14.255 14.138 2023.871 1.611 62.884 3.168 0.67 295037. 0.4993
|
|
40.69 0.2558 0.5484 0.0770 0.0359 2.685 14.103 13.570 2002.320 1.593 60.357 3.074 0.67 295420. 0.4746
|
|
44.39 0.2790 0.5803 0.0736 0.0354 2.646 13.899 12.971 1973.279 1.570 57.697 2.982 0.67 295822. 0.4501
|
|
48.09 0.3023 0.6096 0.0700 0.0347 2.597 13.640 12.345 1936.488 1.541 54.910 2.891 0.67 296245. 0.4258
|
|
51.79 0.3256 0.6365 0.0663 0.0339 2.537 13.325 11.692 1891.816 1.505 52.008 2.803 0.67 296688. 0.4018
|
|
55.49 0.3488 0.6609 0.0625 0.0330 2.466 12.954 11.016 1839.177 1.464 48.999 2.717 0.67 297152. 0.3779
|
|
59.19 0.3721 0.6828 0.0585 0.0319 2.385 12.527 10.318 1778.493 1.415 45.893 2.631 0.67 297637. 0.3542
|
|
62.89 0.3953 0.7021 0.0545 0.0307 2.293 12.042 9.599 1709.676 1.361 42.697 2.547 0.67 298142. 0.3307
|
|
66.59 0.4186 0.7188 0.0503 0.0293 2.189 11.500 8.862 1632.635 1.299 39.420 2.462 0.67 298669. 0.3072
|
|
70.29 0.4418 0.7325 0.0460 0.0277 2.075 10.898 8.109 1547.274 1.231 36.067 2.377 0.67 299217. 0.2837
|
|
73.99 0.4651 0.7429 0.0416 0.0261 1.949 10.238 7.339 1453.507 1.157 32.645 2.290 0.67 299786. 0.2600
|
|
77.69 0.4883 0.7495 0.0372 0.0242 1.812 9.518 6.556 1351.263 1.075 29.161 2.201 0.67 300377. 0.2362
|
|
81.39 0.5116 0.7514 0.0327 0.0222 1.664 8.738 5.760 1240.504 0.987 25.620 2.106 0.68 300989. 0.2118
|
|
85.09 0.5348 0.7474 0.0281 0.0201 1.504 7.897 4.953 1121.229 0.892 22.030 2.004 0.68 301624. 0.1869
|
|
88.79 0.5581 0.7350 0.0235 0.0178 1.332 6.998 4.136 993.494 0.791 18.399 1.888 0.68 302280. 0.1610
|
|
92.49 0.5813 0.7105 0.0188 0.0154 1.150 6.039 3.313 857.428 0.682 14.734 1.752 0.68 302957. 0.1337
|
|
96.19 0.6046 0.6660 0.0141 0.0128 0.957 5.024 2.484 713.263 0.568 11.048 1.579 0.68 303657. 0.1043
|
|
99.89 0.6279 0.5847 0.0094 0.0101 0.753 3.954 1.653 561.352 0.447 7.351 1.335 0.68 304378. 0.0719
|
|
103.59 0.6511 0.4211 0.0047 0.0072 0.539 2.833 0.822 402.156 0.320 3.657 0.927 0.68 305118. 0.0352
|
|
107.28 0.6744 -0.0146 -0.0001 0.0042 0.314 1.647 -0.016 233.841 0.186 -0.071 -0.031 0.68 305792. 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 0.1048 0.0356 3.383 16.403 21.690 2522.913 1.853 96.477 3.899 0.72 316552. 0.7611
|
|
4.01 0.0233 0.0667 0.1032 0.0360 3.422 16.593 21.349 2552.030 1.875 94.959 3.794 0.72 316772. 0.7348
|
|
8.02 0.0465 0.1297 0.1014 0.0364 3.458 16.765 20.979 2578.555 1.894 93.315 3.690 0.72 317010. 0.7084
|
|
12.03 0.0698 0.1892 0.0995 0.0367 3.489 16.916 20.580 2601.844 1.911 91.541 3.588 0.72 317266. 0.6821
|
|
16.04 0.0930 0.2451 0.0974 0.0370 3.515 17.043 20.151 2621.243 1.925 89.631 3.487 0.72 317540. 0.6560
|
|
20.04 0.1163 0.2977 0.0952 0.0372 3.535 17.139 19.689 2636.077 1.936 87.578 3.388 0.72 317833. 0.6300
|
|
24.05 0.1396 0.3470 0.0928 0.0373 3.548 17.201 19.195 2645.621 1.943 85.379 3.291 0.72 318146. 0.6043
|
|
28.06 0.1628 0.3932 0.0902 0.0374 3.553 17.224 18.666 2649.118 1.946 83.026 3.196 0.72 318479. 0.5787
|
|
32.07 0.1861 0.4363 0.0875 0.0373 3.548 17.202 18.102 2645.795 1.943 80.516 3.103 0.72 318832. 0.5533
|
|
36.08 0.2093 0.4765 0.0846 0.0372 3.533 17.131 17.501 2634.857 1.935 77.845 3.013 0.72 319206. 0.5282
|
|
40.09 0.2326 0.5139 0.0815 0.0369 3.507 17.005 16.864 2615.525 1.921 75.009 2.924 0.72 319601. 0.5033
|
|
44.10 0.2559 0.5487 0.0782 0.0365 3.469 16.820 16.189 2587.073 1.900 72.009 2.838 0.72 320018. 0.4786
|
|
48.11 0.2791 0.5809 0.0748 0.0359 3.418 16.572 15.478 2548.897 1.872 68.847 2.754 0.72 320456. 0.4542
|
|
52.11 0.3024 0.6105 0.0712 0.0353 3.353 16.258 14.733 2500.638 1.837 65.533 2.672 0.73 320916. 0.4299
|
|
56.12 0.3256 0.6378 0.0675 0.0344 3.275 15.878 13.957 2442.123 1.794 62.079 2.592 0.73 321399. 0.4059
|
|
60.13 0.3489 0.6626 0.0636 0.0335 3.183 15.430 13.151 2373.251 1.743 58.496 2.513 0.73 321903. 0.3820
|
|
64.14 0.3722 0.6849 0.0595 0.0324 3.076 14.914 12.319 2293.927 1.685 54.796 2.436 0.73 322430. 0.3583
|
|
68.15 0.3954 0.7048 0.0554 0.0311 2.956 14.330 11.463 2204.056 1.619 50.988 2.359 0.73 322979. 0.3347
|
|
72.16 0.4187 0.7220 0.0512 0.0297 2.821 13.677 10.585 2103.522 1.545 47.081 2.282 0.73 323552. 0.3112
|
|
76.17 0.4419 0.7363 0.0468 0.0281 2.672 12.953 9.686 1992.210 1.463 43.083 2.205 0.73 324147. 0.2876
|
|
80.18 0.4652 0.7475 0.0424 0.0264 2.508 12.158 8.768 1870.014 1.374 39.001 2.127 0.73 324765. 0.2639
|
|
84.18 0.4885 0.7550 0.0379 0.0245 2.329 11.293 7.834 1736.857 1.276 34.844 2.046 0.73 325407. 0.2400
|
|
88.19 0.5117 0.7579 0.0333 0.0225 2.136 10.355 6.884 1592.709 1.170 30.618 1.960 0.73 326072. 0.2156
|
|
92.20 0.5350 0.7550 0.0286 0.0203 1.928 9.347 5.920 1437.609 1.056 26.332 1.868 0.73 326760. 0.1905
|
|
96.21 0.5582 0.7439 0.0239 0.0179 1.705 8.268 4.945 1271.699 0.934 21.995 1.764 0.73 327472. 0.1644
|
|
100.22 0.5815 0.7207 0.0191 0.0154 1.469 7.121 3.961 1095.242 0.805 17.618 1.640 0.73 328207. 0.1368
|
|
104.23 0.6048 0.6775 0.0144 0.0128 1.219 5.908 2.970 908.675 0.667 13.212 1.483 0.74 328966. 0.1071
|
|
108.24 0.6280 0.5970 0.0096 0.0101 0.956 4.633 1.977 712.621 0.523 8.792 1.258 0.74 329747. 0.0741
|
|
112.25 0.6513 0.4321 0.0048 0.0072 0.681 3.302 0.983 507.875 0.373 4.373 0.878 0.74 330550. 0.0365
|
|
116.25 0.6745 -0.0166 -0.0001 0.0041 0.392 1.899 -0.021 292.001 0.214 -0.093 -0.032 0.74 331271. 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 0.1065 0.0372 4.415 19.877 25.549 3292.344 2.246 113.643 3.520 0.78 340851. 0.7457
|
|
4.32 0.0233 0.0650 0.1048 0.0375 4.454 20.053 25.157 3321.500 2.266 111.899 3.435 0.78 341089. 0.7222
|
|
8.63 0.0465 0.1268 0.1031 0.0378 4.489 20.209 24.731 3347.391 2.283 110.004 3.351 0.78 341347. 0.6985
|
|
12.95 0.0698 0.1855 0.1011 0.0380 4.518 20.342 24.270 3369.307 2.298 107.952 3.267 0.78 341624. 0.6746
|
|
17.27 0.0930 0.2410 0.0991 0.0382 4.541 20.445 23.772 3386.513 2.310 105.737 3.184 0.78 341921. 0.6506
|
|
21.59 0.1163 0.2935 0.0968 0.0384 4.557 20.516 23.235 3398.242 2.318 103.351 3.101 0.78 342239. 0.6265
|
|
25.90 0.1396 0.3429 0.0944 0.0384 4.564 20.549 22.659 3403.649 2.322 100.787 3.020 0.78 342578. 0.6024
|
|
30.22 0.1628 0.3893 0.0919 0.0384 4.562 20.538 22.041 3401.857 2.320 98.040 2.939 0.78 342939. 0.5783
|
|
34.54 0.1861 0.4329 0.0891 0.0383 4.549 20.478 21.381 3391.950 2.314 95.104 2.859 0.78 343322. 0.5541
|
|
38.85 0.2093 0.4736 0.0862 0.0381 4.523 20.364 20.678 3372.965 2.301 91.974 2.781 0.78 343728. 0.5299
|
|
43.17 0.2326 0.5116 0.0831 0.0378 4.484 20.188 19.930 3343.932 2.281 88.648 2.703 0.78 344156. 0.5058
|
|
47.49 0.2559 0.5470 0.0798 0.0373 4.431 19.947 19.138 3303.921 2.254 85.124 2.627 0.78 344607. 0.4817
|
|
51.81 0.2791 0.5797 0.0763 0.0367 4.361 19.634 18.302 3252.128 2.218 81.406 2.553 0.78 345082. 0.4577
|
|
56.12 0.3024 0.6100 0.0726 0.0360 4.275 19.247 17.425 3188.027 2.175 77.506 2.479 0.78 345580. 0.4337
|
|
60.44 0.3256 0.6378 0.0688 0.0351 4.172 18.784 16.510 3111.311 2.122 73.438 2.407 0.78 346102. 0.4099
|
|
64.76 0.3489 0.6631 0.0648 0.0341 4.052 18.243 15.561 3021.742 2.061 69.215 2.336 0.78 346647. 0.3862
|
|
69.08 0.3722 0.6860 0.0608 0.0330 3.915 17.624 14.580 2919.103 1.991 64.851 2.265 0.78 347217. 0.3625
|
|
73.39 0.3954 0.7064 0.0566 0.0317 3.759 16.924 13.570 2803.221 1.912 60.358 2.196 0.78 347811. 0.3390
|
|
77.71 0.4187 0.7242 0.0522 0.0302 3.586 16.143 12.533 2673.928 1.824 55.745 2.126 0.78 348429. 0.3154
|
|
82.03 0.4419 0.7392 0.0478 0.0286 3.394 15.281 11.471 2531.076 1.726 51.024 2.056 0.79 349072. 0.2918
|
|
86.34 0.4652 0.7510 0.0433 0.0268 3.184 14.336 10.387 2374.589 1.620 46.201 1.984 0.79 349739. 0.2680
|
|
90.66 0.4885 0.7591 0.0387 0.0249 2.956 13.309 9.282 2204.511 1.504 41.288 1.910 0.79 350432. 0.2439
|
|
94.98 0.5117 0.7624 0.0340 0.0228 2.710 12.201 8.159 2020.995 1.379 36.291 1.831 0.79 351149. 0.2192
|
|
99.30 0.5350 0.7597 0.0293 0.0206 2.446 11.014 7.019 1824.310 1.244 31.220 1.745 0.79 351891. 0.1938
|
|
103.61 0.5582 0.7482 0.0244 0.0182 2.166 9.750 5.865 1614.900 1.102 26.087 1.647 0.79 352659. 0.1672
|
|
107.93 0.5815 0.7238 0.0196 0.0157 1.869 8.412 4.699 1393.411 0.950 20.903 1.530 0.79 353452. 0.1390
|
|
112.25 0.6048 0.6779 0.0147 0.0131 1.557 7.008 3.525 1160.724 0.792 15.681 1.378 0.79 354270. 0.1084
|
|
116.56 0.6280 0.5925 0.0098 0.0104 1.231 5.542 2.347 917.994 0.626 10.439 1.160 0.79 355112. 0.0744
|
|
120.88 0.6513 0.4210 0.0049 0.0075 0.894 4.025 1.168 666.609 0.455 5.194 0.794 0.79 355976. 0.0360
|
|
125.20 0.6745 -0.0152 -0.0001 0.0046 0.541 2.437 -0.025 403.738 0.275 -0.109 -0.028 0.80 356756. 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 0.1083 0.0406 5.933 24.929 29.833 4424.042 2.816 132.698 3.059 0.83 365131. 0.7002
|
|
4.63 0.0233 0.0609 0.1067 0.0408 5.957 25.030 29.390 4441.942 2.828 130.729 3.001 0.83 365388. 0.6819
|
|
9.26 0.0465 0.1194 0.1049 0.0409 5.974 25.104 28.907 4455.071 2.836 128.580 2.943 0.83 365666. 0.6632
|
|
13.88 0.0698 0.1756 0.1030 0.0410 5.985 25.147 28.382 4462.768 2.841 126.244 2.885 0.83 365965. 0.6441
|
|
18.51 0.0931 0.2293 0.1010 0.0410 5.987 25.156 27.813 4464.334 2.842 123.712 2.826 0.83 366286. 0.6246
|
|
23.14 0.1164 0.2807 0.0987 0.0409 5.980 25.126 27.198 4458.981 2.839 120.975 2.767 0.83 366630. 0.6047
|
|
27.77 0.1396 0.3295 0.0963 0.0408 5.962 25.052 26.534 4445.892 2.830 118.025 2.707 0.83 366996. 0.5844
|
|
32.40 0.1629 0.3760 0.0937 0.0406 5.933 24.930 25.822 4424.189 2.817 114.856 2.647 0.83 367386. 0.5638
|
|
37.02 0.1862 0.4199 0.0910 0.0403 5.891 24.753 25.058 4392.944 2.797 111.459 2.587 0.83 367800. 0.5428
|
|
41.65 0.2094 0.4614 0.0880 0.0399 5.835 24.518 24.242 4351.160 2.770 107.830 2.527 0.83 368238. 0.5215
|
|
46.28 0.2327 0.5005 0.0849 0.0395 5.763 24.218 23.374 4297.828 2.736 103.967 2.467 0.84 368701. 0.4998
|
|
50.91 0.2560 0.5370 0.0815 0.0389 5.675 23.846 22.452 4231.919 2.694 99.867 2.406 0.84 369188. 0.4779
|
|
55.54 0.2793 0.5712 0.0780 0.0381 5.569 23.399 21.478 4152.535 2.644 95.535 2.346 0.84 369700. 0.4557
|
|
60.16 0.3025 0.6029 0.0743 0.0373 5.443 22.872 20.455 4059.071 2.584 90.984 2.286 0.84 370237. 0.4333
|
|
64.79 0.3258 0.6321 0.0704 0.0363 5.299 22.264 19.387 3951.180 2.515 86.232 2.225 0.84 370800. 0.4107
|
|
69.42 0.3491 0.6590 0.0664 0.0351 5.134 21.573 18.277 3828.589 2.437 81.295 2.165 0.84 371388. 0.3880
|
|
74.05 0.3724 0.6833 0.0622 0.0339 4.950 20.798 17.129 3690.990 2.350 76.190 2.105 0.84 372002. 0.3651
|
|
78.68 0.3956 0.7051 0.0579 0.0325 4.745 19.936 15.946 3538.064 2.252 70.930 2.044 0.84 372641. 0.3421
|
|
83.30 0.4189 0.7240 0.0535 0.0309 4.520 18.991 14.732 3370.218 2.146 65.526 1.983 0.84 373307. 0.3189
|
|
87.93 0.4422 0.7397 0.0490 0.0293 4.275 17.964 13.487 3187.981 2.030 59.991 1.919 0.84 373999. 0.2954
|
|
92.56 0.4654 0.7512 0.0443 0.0275 4.013 16.863 12.215 2992.715 1.905 54.332 1.851 0.84 374717. 0.2712
|
|
97.19 0.4887 0.7584 0.0396 0.0255 3.731 15.677 10.918 2782.191 1.771 48.564 1.780 0.84 375461. 0.2465
|
|
101.82 0.5120 0.7600 0.0348 0.0235 3.429 14.408 9.599 2556.904 1.628 42.695 1.703 0.84 376232. 0.2211
|
|
106.44 0.5353 0.7542 0.0300 0.0213 3.108 13.060 8.259 2317.662 1.475 36.736 1.616 0.85 377030. 0.1947
|
|
111.07 0.5585 0.7380 0.0251 0.0190 2.770 11.639 6.902 2065.465 1.315 30.701 1.516 0.85 377855. 0.1669
|
|
115.70 0.5818 0.7063 0.0201 0.0165 2.416 10.152 5.531 1801.652 1.147 24.602 1.392 0.85 378706. 0.1373
|
|
120.33 0.6051 0.6498 0.0151 0.0140 2.049 8.609 4.150 1527.850 0.973 18.457 1.232 0.85 379584. 0.1052
|
|
124.96 0.6283 0.5508 0.0100 0.0114 1.671 7.021 2.762 1245.993 0.793 12.285 1.005 0.85 380488. 0.0700
|
|
129.58 0.6516 0.3692 0.0050 0.0088 1.285 5.400 1.373 958.263 0.610 6.108 0.650 0.85 381416. 0.0319
|
|
134.21 0.6749 -0.0111 -0.0001 0.0061 0.887 3.728 -0.028 661.531 0.421 -0.122 -0.019 0.85 382276. 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 0.1098 0.0463 8.215 32.363 34.414 6126.257 3.656 153.072 2.548 0.89 389411. 0.6264
|
|
4.95 0.0233 0.0545 0.1083 0.0464 8.220 32.380 33.939 6129.482 3.658 150.961 2.511 0.89 389684. 0.6132
|
|
9.90 0.0467 0.1074 0.1066 0.0463 8.211 32.346 33.415 6123.059 3.654 148.630 2.475 0.89 389980. 0.5997
|
|
14.85 0.0700 0.1588 0.1048 0.0462 8.189 32.258 32.840 6106.351 3.644 146.070 2.439 0.89 390300. 0.5859
|
|
19.80 0.0933 0.2086 0.1028 0.0460 8.152 32.112 32.210 6078.685 3.628 143.269 2.403 0.89 390644. 0.5717
|
|
24.75 0.1167 0.2568 0.1006 0.0457 8.100 31.906 31.524 6039.858 3.605 140.218 2.367 0.89 391013. 0.5571
|
|
29.70 0.1400 0.3034 0.0982 0.0453 8.032 31.640 30.779 5989.423 3.575 136.906 2.331 0.89 391407. 0.5420
|
|
34.64 0.1633 0.3484 0.0956 0.0448 7.948 31.310 29.975 5926.902 3.537 133.327 2.294 0.89 391827. 0.5264
|
|
39.59 0.1867 0.3916 0.0929 0.0443 7.847 30.913 29.108 5851.733 3.492 129.473 2.256 0.89 392273. 0.5102
|
|
44.54 0.2100 0.4330 0.0899 0.0436 7.729 30.445 28.178 5763.238 3.440 125.337 2.218 0.89 392745. 0.4934
|
|
49.49 0.2333 0.4726 0.0867 0.0428 7.591 29.903 27.184 5660.624 3.378 120.917 2.178 0.89 393243. 0.4760
|
|
54.44 0.2567 0.5102 0.0834 0.0419 7.433 29.282 26.126 5542.989 3.308 116.209 2.138 0.89 393769. 0.4580
|
|
59.39 0.2800 0.5459 0.0798 0.0409 7.254 28.577 25.004 5409.549 3.229 111.219 2.097 0.89 394321. 0.4394
|
|
64.34 0.3033 0.5794 0.0760 0.0398 7.054 27.786 23.822 5259.892 3.139 105.962 2.054 0.89 394900. 0.4202
|
|
69.29 0.3266 0.6109 0.0721 0.0385 6.831 26.910 22.585 5093.992 3.040 100.460 2.011 0.89 395506. 0.4006
|
|
74.24 0.3500 0.6401 0.0680 0.0372 6.587 25.948 21.298 4911.858 2.932 94.734 1.967 0.89 396140. 0.3804
|
|
79.19 0.3733 0.6670 0.0637 0.0357 6.321 24.899 19.965 4713.374 2.813 88.804 1.921 0.89 396801. 0.3598
|
|
84.14 0.3966 0.6914 0.0593 0.0340 6.032 23.763 18.590 4498.300 2.685 82.688 1.874 0.90 397489. 0.3387
|
|
89.09 0.4200 0.7131 0.0548 0.0323 5.722 22.540 17.177 4266.779 2.547 76.402 1.826 0.90 398206. 0.3172
|
|
94.03 0.4433 0.7312 0.0502 0.0304 5.393 21.246 15.728 4021.833 2.400 69.956 1.774 0.90 398950. 0.2948
|
|
98.98 0.4666 0.7430 0.0454 0.0285 5.060 19.933 14.244 3773.388 2.252 63.359 1.712 0.90 399722. 0.2708
|
|
103.93 0.4900 0.7461 0.0406 0.0267 4.728 18.625 12.728 3525.770 2.104 56.616 1.637 0.90 400522. 0.2448
|
|
108.88 0.5133 0.7419 0.0357 0.0247 4.377 17.244 11.185 3264.240 1.948 49.752 1.554 0.90 401350. 0.2179
|
|
113.83 0.5366 0.7279 0.0307 0.0226 4.011 15.800 9.618 2990.900 1.785 42.782 1.459 0.90 402207. 0.1896
|
|
118.78 0.5600 0.7006 0.0256 0.0205 3.631 14.303 8.031 2707.509 1.616 35.722 1.345 0.90 403093. 0.1598
|
|
123.73 0.5833 0.6545 0.0205 0.0183 3.240 12.764 6.427 2416.254 1.442 28.589 1.207 0.90 404006. 0.1282
|
|
128.68 0.6066 0.5810 0.0154 0.0160 2.843 11.198 4.813 2119.725 1.265 21.408 1.030 0.90 404948. 0.0947
|
|
133.63 0.6300 0.4661 0.0102 0.0138 2.441 9.618 3.194 1820.605 1.087 14.205 0.796 0.91 405918. 0.0596
|
|
138.58 0.6533 0.2856 0.0050 0.0115 2.040 8.038 1.577 1521.580 0.908 7.016 0.470 0.91 406914. 0.0247
|
|
143.53 0.6766 -0.0106 -0.0001 0.0092 1.632 6.430 -0.045 1217.269 0.727 -0.201 -0.017 0.91 407866. 0.0000
|
|
|
|
|
|
|