686 lines
122 KiB
Plaintext
686 lines
122 KiB
Plaintext
12x10W (12x10W.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 0.1399 0.0808 0.002 0.102 0.092 1.206 0.012 0.411 34.766 0.05 22113. 0.5170
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0.39 0.0342 0.0577 0.1386 0.0821 0.002 0.104 0.092 1.225 0.012 0.407 33.905 0.05 22136. 0.5017
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0.78 0.0683 0.1124 0.1371 0.0833 0.002 0.105 0.091 1.244 0.012 0.403 33.034 0.05 22162. 0.4862
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1.16 0.1025 0.1642 0.1354 0.0845 0.002 0.107 0.089 1.262 0.012 0.398 32.159 0.05 22191. 0.4704
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1.55 0.1367 0.2130 0.1335 0.0857 0.002 0.108 0.088 1.279 0.012 0.393 31.283 0.05 22224. 0.4544
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1.94 0.1708 0.2588 0.1314 0.0868 0.002 0.109 0.087 1.295 0.012 0.386 30.411 0.05 22259. 0.4383
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2.33 0.2050 0.3017 0.1291 0.0877 0.002 0.111 0.085 1.310 0.013 0.379 29.546 0.05 22298. 0.4220
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2.72 0.2391 0.3418 0.1265 0.0885 0.002 0.112 0.084 1.322 0.013 0.372 28.690 0.05 22341. 0.4056
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3.11 0.2733 0.3791 0.1236 0.0891 0.002 0.112 0.082 1.331 0.013 0.363 27.844 0.05 22386. 0.3892
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3.49 0.3075 0.4137 0.1205 0.0895 0.002 0.113 0.080 1.337 0.013 0.354 27.008 0.05 22436. 0.3726
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3.88 0.3416 0.4456 0.1170 0.0897 0.002 0.113 0.077 1.339 0.013 0.344 26.184 0.05 22489. 0.3560
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4.27 0.3758 0.4749 0.1132 0.0896 0.002 0.113 0.075 1.337 0.013 0.333 25.369 0.05 22546. 0.3393
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4.66 0.4100 0.5016 0.1091 0.0891 0.002 0.112 0.072 1.331 0.013 0.321 24.562 0.05 22607. 0.3224
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5.05 0.4441 0.5257 0.1046 0.0883 0.002 0.112 0.069 1.319 0.013 0.307 23.760 0.05 22671. 0.3054
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5.44 0.4783 0.5471 0.0997 0.0872 0.002 0.110 0.066 1.302 0.012 0.293 22.960 0.05 22738. 0.2882
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5.82 0.5125 0.5657 0.0945 0.0856 0.002 0.108 0.062 1.278 0.012 0.278 22.158 0.05 22810. 0.2707
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6.21 0.5466 0.5813 0.0889 0.0836 0.002 0.106 0.059 1.248 0.012 0.261 21.348 0.05 22885. 0.2530
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6.60 0.5808 0.5939 0.0830 0.0812 0.002 0.102 0.055 1.212 0.012 0.244 20.525 0.05 22963. 0.2351
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6.99 0.6149 0.6029 0.0769 0.0784 0.002 0.099 0.051 1.171 0.011 0.226 19.681 0.05 23046. 0.2169
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7.38 0.6491 0.6081 0.0705 0.0752 0.002 0.095 0.047 1.123 0.011 0.207 18.805 0.05 23131. 0.1985
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7.76 0.6833 0.6088 0.0639 0.0717 0.001 0.091 0.042 1.071 0.010 0.188 17.886 0.05 23220. 0.1797
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8.15 0.7174 0.6042 0.0572 0.0679 0.001 0.086 0.038 1.014 0.010 0.168 16.906 0.05 23313. 0.1607
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8.54 0.7516 0.5933 0.0503 0.0638 0.001 0.080 0.033 0.952 0.009 0.148 15.845 0.05 23409. 0.1413
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8.93 0.7858 0.5743 0.0434 0.0593 0.001 0.075 0.029 0.886 0.008 0.127 14.672 0.05 23509. 0.1214
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9.32 0.8199 0.5452 0.0363 0.0546 0.001 0.069 0.024 0.815 0.008 0.107 13.346 0.05 23611. 0.1011
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9.71 0.8541 0.5023 0.0291 0.0495 0.001 0.063 0.019 0.740 0.007 0.086 11.805 0.05 23718. 0.0801
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10.09 0.8882 0.4403 0.0219 0.0442 0.001 0.056 0.014 0.660 0.006 0.064 9.950 0.05 23827. 0.0586
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10.48 0.9224 0.3502 0.0147 0.0386 0.001 0.049 0.010 0.577 0.006 0.043 7.621 0.05 23940. 0.0367
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10.87 0.9566 0.2161 0.0074 0.0328 0.001 0.041 0.005 0.490 0.005 0.022 4.536 0.05 24056. 0.0155
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11.26 0.9907 0.0068 0.0002 0.0268 0.001 0.034 0.000 0.400 0.004 0.001 0.138 0.05 24175. 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 0.1406 0.0726 0.012 0.367 0.372 8.674 0.041 1.653 19.437 0.10 44225. 0.5794
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0.78 0.0345 0.0649 0.1393 0.0740 0.012 0.373 0.368 8.835 0.042 1.638 18.904 0.10 44272. 0.5609
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1.57 0.0689 0.1262 0.1378 0.0753 0.012 0.380 0.364 8.996 0.043 1.621 18.369 0.10 44325. 0.5421
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2.35 0.1034 0.1838 0.1362 0.0766 0.012 0.387 0.360 9.154 0.044 1.601 17.835 0.10 44384. 0.5232
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3.13 0.1379 0.2377 0.1343 0.0779 0.012 0.393 0.355 9.305 0.044 1.579 17.304 0.10 44450. 0.5041
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3.92 0.1724 0.2882 0.1322 0.0791 0.013 0.399 0.349 9.446 0.045 1.554 16.780 0.10 44522. 0.4850
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4.70 0.2068 0.3352 0.1299 0.0801 0.013 0.405 0.343 9.574 0.046 1.527 16.264 0.10 44600. 0.4660
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5.48 0.2413 0.3789 0.1273 0.0811 0.013 0.409 0.336 9.683 0.046 1.496 15.758 0.10 44686. 0.4469
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6.27 0.2758 0.4194 0.1244 0.0818 0.013 0.413 0.329 9.771 0.047 1.463 15.263 0.10 44780. 0.4279
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7.05 0.3102 0.4568 0.1212 0.0823 0.013 0.416 0.320 9.833 0.047 1.425 14.779 0.10 44880. 0.4090
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7.83 0.3447 0.4913 0.1177 0.0826 0.013 0.417 0.311 9.864 0.047 1.384 14.306 0.10 44988. 0.3902
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8.62 0.3792 0.5230 0.1139 0.0826 0.013 0.417 0.301 9.861 0.047 1.339 13.844 0.10 45103. 0.3714
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9.40 0.4137 0.5519 0.1097 0.0822 0.013 0.415 0.290 9.820 0.047 1.290 13.391 0.10 45226. 0.3526
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10.18 0.4481 0.5781 0.1051 0.0815 0.013 0.411 0.278 9.735 0.046 1.236 12.948 0.10 45357. 0.3338
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10.97 0.4826 0.6016 0.1002 0.0804 0.013 0.406 0.265 9.602 0.046 1.178 12.512 0.10 45494. 0.3148
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11.75 0.5171 0.6224 0.0949 0.0788 0.013 0.398 0.251 9.418 0.045 1.116 12.080 0.10 45639. 0.2958
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12.54 0.5515 0.6403 0.0892 0.0769 0.012 0.388 0.236 9.181 0.044 1.049 11.652 0.10 45792. 0.2767
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13.32 0.5860 0.6554 0.0833 0.0744 0.012 0.376 0.220 8.892 0.042 0.979 11.224 0.10 45952. 0.2575
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14.10 0.6205 0.6672 0.0770 0.0716 0.011 0.362 0.204 8.555 0.041 0.905 10.793 0.10 46118. 0.2381
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14.89 0.6550 0.6756 0.0706 0.0684 0.011 0.345 0.187 8.172 0.039 0.830 10.352 0.10 46292. 0.2186
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15.67 0.6894 0.6799 0.0639 0.0648 0.010 0.327 0.169 7.744 0.037 0.752 9.897 0.10 46474. 0.1989
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16.45 0.7239 0.6794 0.0571 0.0609 0.010 0.307 0.151 7.274 0.035 0.672 9.419 0.10 46662. 0.1790
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17.24 0.7584 0.6730 0.0502 0.0566 0.009 0.286 0.133 6.762 0.032 0.591 8.906 0.10 46857. 0.1587
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18.02 0.7928 0.6591 0.0432 0.0520 0.008 0.262 0.114 6.209 0.030 0.508 8.343 0.10 47059. 0.1379
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18.80 0.8273 0.6351 0.0361 0.0470 0.008 0.237 0.095 5.617 0.027 0.424 7.704 0.10 47268. 0.1164
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19.59 0.8618 0.5969 0.0289 0.0418 0.007 0.211 0.076 4.987 0.024 0.340 6.952 0.10 47484. 0.0940
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20.37 0.8963 0.5376 0.0217 0.0362 0.006 0.183 0.057 4.321 0.021 0.255 6.020 0.10 47707. 0.0705
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21.15 0.9307 0.4439 0.0145 0.0303 0.005 0.153 0.038 3.620 0.017 0.170 4.787 0.10 47936. 0.0458
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21.94 0.9652 0.2883 0.0072 0.0242 0.004 0.122 0.019 2.887 0.014 0.085 2.998 0.10 48172. 0.0202
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22.72 0.9997 0.0013 0.0000 0.0178 0.003 0.090 0.000 2.125 0.010 0.000 0.013 0.10 48413. 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 0.1410 0.0693 0.037 0.787 0.839 27.925 0.089 3.730 13.621 0.14 66337. 0.6099
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1.18 0.0346 0.0684 0.1397 0.0707 0.038 0.803 0.831 28.485 0.091 3.696 13.230 0.14 66408. 0.5897
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2.36 0.0692 0.1327 0.1382 0.0720 0.039 0.818 0.822 29.046 0.092 3.657 12.839 0.14 66487. 0.5692
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3.54 0.1038 0.1931 0.1366 0.0734 0.040 0.834 0.812 29.598 0.094 3.613 12.449 0.14 66576. 0.5487
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4.72 0.1384 0.2495 0.1347 0.0747 0.040 0.849 0.801 30.128 0.096 3.564 12.064 0.14 66675. 0.5281
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5.90 0.1729 0.3020 0.1327 0.0760 0.041 0.863 0.789 30.626 0.097 3.509 11.685 0.14 66783. 0.5075
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7.08 0.2075 0.3509 0.1303 0.0771 0.042 0.876 0.775 31.077 0.099 3.448 11.313 0.14 66902. 0.4870
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8.25 0.2421 0.3962 0.1277 0.0781 0.042 0.887 0.760 31.468 0.100 3.379 10.950 0.14 67032. 0.4667
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9.43 0.2767 0.4382 0.1248 0.0788 0.043 0.896 0.743 31.785 0.101 3.303 10.596 0.14 67172. 0.4464
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10.61 0.3113 0.4769 0.1217 0.0794 0.043 0.902 0.724 32.013 0.102 3.218 10.251 0.14 67324. 0.4264
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11.79 0.3459 0.5126 0.1181 0.0797 0.043 0.905 0.703 32.139 0.102 3.125 9.917 0.14 67487. 0.4065
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12.97 0.3805 0.5454 0.1143 0.0797 0.043 0.906 0.680 32.147 0.102 3.024 9.591 0.14 67661. 0.3867
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14.15 0.4151 0.5753 0.1101 0.0794 0.043 0.902 0.655 32.022 0.102 2.912 9.274 0.14 67847. 0.3670
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15.33 0.4497 0.6025 0.1055 0.0787 0.043 0.894 0.628 31.747 0.101 2.791 8.966 0.14 68043. 0.3473
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16.51 0.4842 0.6270 0.1006 0.0777 0.042 0.882 0.598 31.309 0.100 2.660 8.664 0.14 68251. 0.3276
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17.69 0.5188 0.6489 0.0952 0.0761 0.041 0.865 0.566 30.693 0.098 2.519 8.368 0.14 68470. 0.3079
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18.87 0.5534 0.6680 0.0895 0.0742 0.040 0.842 0.532 29.896 0.095 2.368 8.077 0.14 68700. 0.2881
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20.05 0.5880 0.6844 0.0835 0.0717 0.039 0.815 0.497 28.922 0.092 2.209 7.788 0.15 68941. 0.2683
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21.23 0.6226 0.6978 0.0772 0.0689 0.037 0.783 0.459 27.778 0.088 2.043 7.499 0.15 69193. 0.2485
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22.40 0.6572 0.7080 0.0707 0.0657 0.036 0.746 0.421 26.473 0.084 1.871 7.208 0.15 69456. 0.2286
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23.58 0.6918 0.7144 0.0641 0.0620 0.034 0.705 0.381 25.013 0.080 1.695 6.910 0.15 69729. 0.2086
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24.76 0.7264 0.7164 0.0573 0.0580 0.031 0.659 0.341 23.403 0.074 1.515 6.600 0.15 70013. 0.1883
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25.94 0.7610 0.7130 0.0503 0.0537 0.029 0.610 0.299 21.648 0.069 1.331 6.270 0.15 70308. 0.1677
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27.12 0.7956 0.7027 0.0433 0.0490 0.026 0.556 0.257 19.750 0.063 1.145 5.910 0.15 70613. 0.1466
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28.30 0.8301 0.6828 0.0361 0.0439 0.024 0.499 0.215 17.714 0.056 0.956 5.503 0.15 70929. 0.1247
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29.48 0.8647 0.6491 0.0289 0.0386 0.021 0.438 0.172 15.545 0.049 0.766 5.023 0.15 71254. 0.1019
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30.66 0.8993 0.5942 0.0217 0.0329 0.018 0.373 0.129 13.246 0.042 0.574 4.421 0.15 71591. 0.0777
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31.84 0.9339 0.5029 0.0145 0.0269 0.015 0.305 0.086 10.827 0.034 0.383 3.603 0.15 71937. 0.0517
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33.02 0.9685 0.3401 0.0072 0.0206 0.011 0.234 0.043 8.297 0.026 0.191 2.350 0.15 72293. 0.0238
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34.20 1.0031 0.0028 0.0000 0.0141 0.008 0.160 0.000 5.666 0.018 0.001 0.019 0.15 72656. 0.0000
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PROP RPM = 4000
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V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
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(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
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0.00 0.0000 0.0000 0.1413 0.0674 0.086 1.362 1.494 64.438 0.154 6.646 10.518 0.19 88447. 0.6287
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1.58 0.0347 0.0705 0.1400 0.0688 0.088 1.390 1.481 65.792 0.157 6.586 10.208 0.19 88542. 0.6074
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3.15 0.0693 0.1368 0.1386 0.0703 0.090 1.419 1.465 67.150 0.160 6.518 9.898 0.19 88649. 0.5859
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4.73 0.1040 0.1988 0.1370 0.0717 0.092 1.447 1.448 68.488 0.164 6.441 9.590 0.19 88768. 0.5643
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6.30 0.1387 0.2566 0.1351 0.0730 0.094 1.474 1.429 69.777 0.167 6.354 9.286 0.19 88899. 0.5427
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7.88 0.1733 0.3105 0.1330 0.0743 0.095 1.500 1.407 70.989 0.169 6.257 8.988 0.19 89044. 0.5212
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9.45 0.2080 0.3604 0.1307 0.0754 0.097 1.523 1.382 72.091 0.172 6.148 8.696 0.19 89204. 0.4999
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11.03 0.2427 0.4068 0.1281 0.0764 0.098 1.544 1.355 73.050 0.174 6.026 8.412 0.19 89377. 0.4787
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12.61 0.2773 0.4496 0.1252 0.0773 0.099 1.560 1.324 73.833 0.176 5.890 8.135 0.19 89565. 0.4578
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14.18 0.3120 0.4891 0.1221 0.0779 0.100 1.572 1.291 74.405 0.178 5.740 7.867 0.19 89768. 0.4370
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15.76 0.3467 0.5255 0.1185 0.0782 0.100 1.579 1.253 74.730 0.178 5.575 7.607 0.19 89986. 0.4164
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17.33 0.3813 0.5589 0.1147 0.0782 0.100 1.580 1.213 74.773 0.179 5.393 7.355 0.19 90220. 0.3960
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18.91 0.4160 0.5895 0.1105 0.0780 0.100 1.574 1.168 74.496 0.178 5.195 7.111 0.19 90468. 0.3758
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20.49 0.4507 0.6173 0.1059 0.0773 0.099 1.561 1.119 73.861 0.176 4.979 6.874 0.19 90731. 0.3556
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22.06 0.4853 0.6425 0.1009 0.0762 0.098 1.539 1.067 72.832 0.174 4.744 6.643 0.19 91010. 0.3355
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23.64 0.5200 0.6650 0.0955 0.0747 0.096 1.508 1.010 71.377 0.170 4.492 6.417 0.19 91303. 0.3153
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25.21 0.5547 0.6849 0.0898 0.0727 0.093 1.468 0.949 69.485 0.166 4.222 6.196 0.19 91611. 0.2952
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26.79 0.5894 0.7022 0.0837 0.0703 0.090 1.419 0.885 67.165 0.160 3.938 5.979 0.19 91934. 0.2751
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28.36 0.6240 0.7166 0.0774 0.0674 0.086 1.362 0.819 64.436 0.154 3.642 5.763 0.19 92271. 0.2550
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29.94 0.6587 0.7280 0.0709 0.0642 0.082 1.296 0.750 61.318 0.146 3.335 5.546 0.19 92623. 0.2348
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31.52 0.6934 0.7358 0.0642 0.0605 0.078 1.222 0.679 57.824 0.138 3.020 5.326 0.19 92989. 0.2146
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33.09 0.7280 0.7396 0.0574 0.0565 0.072 1.140 0.607 53.967 0.129 2.698 5.098 0.20 93369. 0.1942
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34.67 0.7627 0.7383 0.0504 0.0521 0.067 1.051 0.533 49.756 0.119 2.370 4.858 0.20 93764. 0.1734
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36.24 0.7974 0.7304 0.0433 0.0473 0.061 0.955 0.458 45.199 0.108 2.038 4.597 0.20 94172. 0.1521
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37.82 0.8320 0.7135 0.0362 0.0422 0.054 0.852 0.382 40.307 0.096 1.701 4.304 0.20 94595. 0.1301
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39.40 0.8667 0.6835 0.0290 0.0367 0.047 0.741 0.306 35.088 0.084 1.362 3.957 0.20 95031. 0.1071
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40.97 0.9014 0.6323 0.0217 0.0309 0.040 0.625 0.229 29.558 0.071 1.020 3.521 0.20 95481. 0.0825
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42.55 0.9360 0.5439 0.0144 0.0248 0.032 0.502 0.153 23.735 0.057 0.679 2.916 0.20 95944. 0.0557
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44.12 0.9707 0.3778 0.0072 0.0185 0.024 0.373 0.076 17.642 0.042 0.338 1.953 0.20 96421. 0.0263
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45.70 1.0054 -0.0012 0.0000 0.0118 0.015 0.239 0.000 11.304 0.027 -0.001 -0.006 0.20 96905. 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 0.1417 0.0663 0.166 2.092 2.340 123.753 0.236 10.409 8.577 0.24 110556. 0.6416
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1.97 0.0347 0.0719 0.1404 0.0677 0.170 2.137 2.319 126.439 0.241 10.316 8.320 0.24 110675. 0.6195
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3.94 0.0694 0.1394 0.1390 0.0692 0.173 2.183 2.296 129.137 0.247 10.211 8.063 0.24 110808. 0.5973
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5.92 0.1041 0.2026 0.1373 0.0706 0.177 2.228 2.269 131.798 0.252 10.092 7.808 0.24 110957. 0.5751
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7.89 0.1389 0.2614 0.1355 0.0720 0.180 2.271 2.239 134.366 0.257 9.957 7.557 0.24 111122. 0.5529
|
|
9.86 0.1736 0.3161 0.1334 0.0733 0.183 2.312 2.205 136.783 0.261 9.806 7.310 0.24 111304. 0.5308
|
|
11.83 0.2083 0.3668 0.1311 0.0745 0.186 2.349 2.166 138.986 0.265 9.636 7.070 0.24 111503. 0.5088
|
|
13.81 0.2430 0.4138 0.1286 0.0755 0.189 2.382 2.124 140.910 0.269 9.446 6.836 0.24 111721. 0.4871
|
|
15.78 0.2777 0.4572 0.1257 0.0763 0.191 2.409 2.076 142.487 0.272 9.235 6.609 0.24 111957. 0.4656
|
|
17.75 0.3124 0.4972 0.1225 0.0770 0.193 2.428 2.023 143.649 0.274 9.001 6.389 0.24 112211. 0.4444
|
|
19.72 0.3472 0.5341 0.1190 0.0773 0.194 2.440 1.965 144.324 0.276 8.742 6.177 0.24 112485. 0.4234
|
|
21.70 0.3819 0.5680 0.1151 0.0774 0.194 2.442 1.902 144.443 0.276 8.458 5.971 0.24 112777. 0.4026
|
|
23.67 0.4166 0.5990 0.1109 0.0771 0.193 2.433 1.832 143.930 0.275 8.147 5.772 0.24 113088. 0.3820
|
|
25.64 0.4513 0.6272 0.1063 0.0765 0.191 2.412 1.756 142.711 0.273 7.809 5.580 0.24 113418. 0.3615
|
|
27.61 0.4860 0.6528 0.1013 0.0754 0.189 2.379 1.673 140.712 0.269 7.441 5.393 0.24 113767. 0.3411
|
|
29.59 0.5207 0.6759 0.0959 0.0739 0.185 2.331 1.584 137.873 0.263 7.045 5.211 0.24 114135. 0.3207
|
|
31.56 0.5554 0.6964 0.0901 0.0719 0.180 2.268 1.489 134.169 0.256 6.622 5.033 0.24 114521. 0.3003
|
|
33.53 0.5902 0.7143 0.0840 0.0694 0.174 2.191 1.389 129.619 0.248 6.176 4.859 0.24 114925. 0.2800
|
|
35.50 0.6249 0.7295 0.0777 0.0666 0.167 2.101 1.284 124.259 0.237 5.711 4.687 0.24 115348. 0.2597
|
|
37.48 0.6596 0.7417 0.0712 0.0633 0.158 1.997 1.176 118.124 0.226 5.230 4.515 0.24 115789. 0.2394
|
|
39.45 0.6943 0.7507 0.0644 0.0596 0.149 1.881 1.065 111.245 0.212 4.736 4.341 0.24 116248. 0.2190
|
|
41.42 0.7290 0.7558 0.0576 0.0555 0.139 1.752 0.951 103.643 0.198 4.230 4.162 0.24 116725. 0.1985
|
|
43.39 0.7637 0.7561 0.0506 0.0511 0.128 1.612 0.835 95.338 0.182 3.716 3.975 0.24 117219. 0.1776
|
|
45.37 0.7985 0.7502 0.0435 0.0463 0.116 1.460 0.718 86.346 0.165 3.194 3.772 0.25 117731. 0.1563
|
|
47.34 0.8332 0.7358 0.0363 0.0411 0.103 1.296 0.599 76.685 0.146 2.666 3.546 0.25 118261. 0.1342
|
|
49.31 0.8679 0.7087 0.0290 0.0356 0.089 1.122 0.480 66.376 0.127 2.134 3.278 0.25 118807. 0.1110
|
|
51.28 0.9026 0.6611 0.0218 0.0297 0.074 0.937 0.359 55.447 0.106 1.599 2.941 0.25 119371. 0.0862
|
|
53.26 0.9373 0.5761 0.0145 0.0235 0.059 0.743 0.239 43.936 0.084 1.063 2.468 0.25 119952. 0.0590
|
|
55.23 0.9720 0.4095 0.0072 0.0171 0.043 0.539 0.119 31.890 0.061 0.529 1.691 0.25 120549. 0.0285
|
|
57.20 1.0067 -0.0022 0.0000 0.0104 0.026 0.327 0.000 19.354 0.037 -0.002 -0.009 0.25 121155. 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 0.1420 0.0656 0.284 2.980 3.378 211.534 0.337 15.026 7.243 0.29 132664. 0.6510
|
|
2.37 0.0347 0.0729 0.1408 0.0670 0.290 3.046 3.349 216.243 0.344 14.894 7.024 0.29 132806. 0.6284
|
|
4.74 0.0695 0.1413 0.1393 0.0685 0.296 3.113 3.315 220.978 0.352 14.745 6.804 0.29 132966. 0.6057
|
|
7.11 0.1042 0.2052 0.1377 0.0700 0.303 3.179 3.277 225.650 0.359 14.575 6.587 0.29 133145. 0.5830
|
|
9.48 0.1390 0.2647 0.1359 0.0714 0.309 3.242 3.234 230.166 0.366 14.384 6.373 0.29 133343. 0.5603
|
|
11.84 0.1737 0.3200 0.1339 0.0727 0.314 3.302 3.185 234.423 0.373 14.168 6.163 0.29 133562. 0.5378
|
|
14.21 0.2085 0.3713 0.1316 0.0739 0.320 3.357 3.131 238.309 0.379 13.924 5.958 0.29 133801. 0.5155
|
|
16.58 0.2432 0.4187 0.1290 0.0749 0.324 3.405 3.069 241.710 0.385 13.652 5.760 0.29 134063. 0.4934
|
|
18.95 0.2780 0.4625 0.1261 0.0758 0.328 3.444 3.001 244.508 0.389 13.349 5.567 0.29 134346. 0.4716
|
|
21.32 0.3127 0.5029 0.1230 0.0765 0.331 3.474 2.925 246.582 0.392 13.012 5.381 0.29 134652. 0.4500
|
|
23.69 0.3474 0.5402 0.1194 0.0768 0.332 3.491 2.842 247.809 0.394 12.640 5.201 0.29 134981. 0.4287
|
|
26.06 0.3822 0.5743 0.1156 0.0769 0.333 3.494 2.750 248.064 0.395 12.231 5.028 0.29 135332. 0.4076
|
|
28.43 0.4169 0.6057 0.1113 0.0767 0.332 3.483 2.649 247.219 0.393 11.783 4.860 0.29 135707. 0.3868
|
|
30.80 0.4517 0.6343 0.1067 0.0760 0.329 3.453 2.539 245.140 0.390 11.294 4.698 0.29 136104. 0.3660
|
|
33.17 0.4864 0.6602 0.1017 0.0749 0.324 3.405 2.420 241.701 0.385 10.764 4.541 0.29 136523. 0.3454
|
|
35.53 0.5212 0.6837 0.0963 0.0734 0.318 3.336 2.291 236.793 0.377 10.191 4.389 0.29 136965. 0.3248
|
|
37.90 0.5559 0.7046 0.0905 0.0714 0.309 3.245 2.154 230.375 0.367 9.580 4.240 0.29 137430. 0.3043
|
|
40.27 0.5907 0.7230 0.0844 0.0690 0.298 3.134 2.009 222.476 0.354 8.935 4.095 0.29 137916. 0.2838
|
|
42.64 0.6254 0.7389 0.0781 0.0661 0.286 3.003 1.858 213.159 0.339 8.262 3.953 0.29 138424. 0.2634
|
|
45.01 0.6601 0.7519 0.0715 0.0628 0.272 2.852 1.701 202.486 0.322 7.566 3.810 0.29 138954. 0.2430
|
|
47.38 0.6949 0.7617 0.0647 0.0591 0.255 2.684 1.540 190.506 0.303 6.852 3.667 0.29 139506. 0.2226
|
|
49.75 0.7296 0.7679 0.0578 0.0550 0.238 2.497 1.376 177.261 0.282 6.121 3.521 0.29 140079. 0.2020
|
|
52.12 0.7644 0.7696 0.0508 0.0505 0.218 2.293 1.209 162.782 0.259 5.377 3.368 0.29 140674. 0.1811
|
|
54.49 0.7991 0.7653 0.0437 0.0456 0.197 2.072 1.039 147.098 0.234 4.622 3.204 0.29 141289. 0.1597
|
|
56.85 0.8339 0.7530 0.0365 0.0404 0.175 1.835 0.867 130.241 0.207 3.859 3.021 0.30 141925. 0.1376
|
|
59.22 0.8686 0.7285 0.0292 0.0348 0.151 1.581 0.694 112.247 0.179 3.089 2.806 0.30 142583. 0.1143
|
|
61.59 0.9034 0.6841 0.0219 0.0289 0.125 1.312 0.520 93.166 0.148 2.315 2.534 0.30 143260. 0.0894
|
|
63.96 0.9381 0.6027 0.0146 0.0227 0.098 1.029 0.346 73.064 0.116 1.540 2.149 0.30 143959. 0.0618
|
|
66.33 0.9728 0.4375 0.0073 0.0161 0.070 0.733 0.173 52.024 0.083 0.768 1.504 0.30 144676. 0.0306
|
|
68.70 1.0076 0.0003 0.0000 0.0093 0.040 0.424 0.000 30.123 0.048 0.000 0.001 0.30 145402. 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 0.1424 0.0651 0.447 4.028 4.611 333.629 0.455 20.508 6.268 0.33 154769. 0.6581
|
|
2.77 0.0348 0.0737 0.1412 0.0666 0.458 4.120 4.571 341.214 0.465 20.332 6.076 0.33 154935. 0.6352
|
|
5.53 0.0696 0.1427 0.1398 0.0681 0.468 4.212 4.526 348.849 0.476 20.131 5.885 0.33 155122. 0.6121
|
|
8.30 0.1043 0.2072 0.1382 0.0696 0.478 4.303 4.475 356.392 0.486 19.904 5.695 0.33 155330. 0.5891
|
|
11.07 0.1391 0.2672 0.1364 0.0710 0.488 4.391 4.417 363.688 0.496 19.646 5.508 0.33 155562. 0.5661
|
|
13.83 0.1739 0.3229 0.1344 0.0724 0.497 4.475 4.351 370.573 0.506 19.355 5.326 0.33 155817. 0.5432
|
|
16.60 0.2087 0.3746 0.1321 0.0736 0.505 4.551 4.277 376.868 0.514 19.026 5.148 0.33 156097. 0.5206
|
|
19.36 0.2434 0.4224 0.1295 0.0747 0.513 4.617 4.194 382.387 0.522 18.657 4.975 0.33 156403. 0.4982
|
|
22.13 0.2782 0.4665 0.1267 0.0756 0.519 4.672 4.102 386.940 0.528 18.245 4.808 0.33 156734. 0.4762
|
|
24.90 0.3130 0.5072 0.1235 0.0762 0.523 4.713 3.999 390.331 0.532 17.788 4.647 0.33 157092. 0.4544
|
|
27.66 0.3478 0.5447 0.1200 0.0766 0.526 4.738 3.885 392.362 0.535 17.281 4.491 0.34 157476. 0.4329
|
|
30.43 0.3825 0.5791 0.1161 0.0767 0.527 4.743 3.760 392.834 0.536 16.724 4.341 0.34 157887. 0.4116
|
|
33.20 0.4173 0.6107 0.1119 0.0764 0.525 4.728 3.623 391.539 0.534 16.114 4.197 0.34 158325. 0.3906
|
|
35.96 0.4521 0.6396 0.1073 0.0758 0.521 4.688 3.473 388.264 0.530 15.447 4.057 0.34 158789. 0.3697
|
|
38.73 0.4869 0.6659 0.1022 0.0747 0.513 4.622 3.310 382.802 0.522 14.723 3.922 0.34 159280. 0.3489
|
|
41.49 0.5216 0.6896 0.0968 0.0732 0.503 4.528 3.134 374.983 0.512 13.941 3.791 0.34 159797. 0.3282
|
|
44.26 0.5564 0.7109 0.0910 0.0712 0.489 4.404 2.946 364.737 0.498 13.105 3.664 0.34 160340. 0.3075
|
|
47.03 0.5912 0.7298 0.0849 0.0687 0.472 4.252 2.748 352.109 0.480 12.223 3.540 0.34 160909. 0.2869
|
|
49.79 0.6260 0.7461 0.0785 0.0658 0.452 4.072 2.541 337.199 0.460 11.303 3.418 0.34 161503. 0.2664
|
|
52.56 0.6607 0.7597 0.0719 0.0625 0.429 3.865 2.327 320.107 0.437 10.351 3.297 0.34 162123. 0.2459
|
|
55.33 0.6955 0.7703 0.0651 0.0588 0.404 3.633 2.107 300.913 0.411 9.372 3.176 0.34 162768. 0.2254
|
|
58.09 0.7303 0.7774 0.0581 0.0546 0.375 3.377 1.882 279.681 0.382 8.372 3.053 0.34 163438. 0.2048
|
|
60.86 0.7651 0.7801 0.0511 0.0501 0.344 3.097 1.653 256.461 0.350 7.354 2.924 0.34 164132. 0.1838
|
|
63.62 0.7998 0.7773 0.0439 0.0452 0.310 2.793 1.421 231.301 0.316 6.321 2.787 0.34 164852. 0.1624
|
|
66.39 0.8346 0.7666 0.0366 0.0399 0.274 2.466 1.186 204.251 0.279 5.276 2.634 0.34 165596. 0.1403
|
|
69.16 0.8694 0.7443 0.0293 0.0342 0.235 2.118 0.949 175.371 0.239 4.222 2.455 0.35 166364. 0.1169
|
|
71.92 0.9042 0.7026 0.0220 0.0283 0.194 1.748 0.711 144.741 0.197 3.163 2.228 0.35 167156. 0.0919
|
|
74.69 0.9389 0.6241 0.0146 0.0220 0.151 1.358 0.473 112.466 0.153 2.102 1.906 0.35 167972. 0.0641
|
|
77.46 0.9737 0.4598 0.0073 0.0154 0.106 0.950 0.235 78.684 0.107 1.045 1.354 0.35 168810. 0.0321
|
|
80.22 1.0085 -0.0045 0.0000 0.0085 0.058 0.525 -0.001 43.509 0.059 -0.005 -0.013 0.35 169657. 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 0.1428 0.0649 0.665 5.242 6.040 496.114 0.592 26.866 5.522 0.38 176871. 0.6636
|
|
3.16 0.0348 0.0742 0.1416 0.0664 0.681 5.363 5.989 507.602 0.606 26.641 5.352 0.38 177061. 0.6405
|
|
6.32 0.0696 0.1437 0.1403 0.0679 0.696 5.485 5.932 519.177 0.620 26.385 5.182 0.38 177274. 0.6172
|
|
9.49 0.1044 0.2086 0.1387 0.0694 0.712 5.606 5.866 530.623 0.633 26.093 5.014 0.38 177513. 0.5938
|
|
12.65 0.1391 0.2689 0.1369 0.0709 0.726 5.723 5.792 541.707 0.647 25.761 4.849 0.38 177777. 0.5706
|
|
15.81 0.1739 0.3250 0.1349 0.0722 0.740 5.834 5.707 552.177 0.659 25.384 4.688 0.38 178069. 0.5476
|
|
18.97 0.2087 0.3769 0.1327 0.0735 0.753 5.935 5.611 561.764 0.671 24.959 4.531 0.38 178390. 0.5248
|
|
22.14 0.2435 0.4249 0.1301 0.0746 0.765 6.024 5.504 570.184 0.681 24.481 4.378 0.38 178739. 0.5022
|
|
25.30 0.2783 0.4692 0.1273 0.0755 0.774 6.098 5.383 577.148 0.689 23.945 4.231 0.38 179118. 0.4800
|
|
28.46 0.3131 0.5102 0.1241 0.0762 0.781 6.153 5.250 582.361 0.695 23.350 4.089 0.38 179528. 0.4580
|
|
31.62 0.3479 0.5478 0.1206 0.0766 0.785 6.186 5.101 585.524 0.699 22.690 3.952 0.38 179968. 0.4364
|
|
34.79 0.3827 0.5825 0.1168 0.0767 0.786 6.195 4.938 586.333 0.700 21.963 3.820 0.38 180438. 0.4150
|
|
37.95 0.4174 0.6143 0.1125 0.0765 0.784 6.175 4.758 584.477 0.698 21.165 3.693 0.38 180939. 0.3939
|
|
41.11 0.4522 0.6434 0.1079 0.0758 0.777 6.124 4.562 579.635 0.692 20.293 3.570 0.38 181470. 0.3729
|
|
44.27 0.4870 0.6700 0.1028 0.0748 0.766 6.038 4.349 571.496 0.682 19.345 3.452 0.39 182032. 0.3520
|
|
47.44 0.5218 0.6940 0.0974 0.0732 0.751 5.914 4.119 559.801 0.668 18.320 3.337 0.39 182624. 0.3312
|
|
50.60 0.5566 0.7156 0.0916 0.0712 0.730 5.752 3.872 544.439 0.650 17.225 3.226 0.39 183245. 0.3104
|
|
53.76 0.5914 0.7349 0.0854 0.0687 0.705 5.552 3.612 525.478 0.627 16.068 3.118 0.39 183896. 0.2898
|
|
56.92 0.6262 0.7517 0.0790 0.0658 0.675 5.315 3.341 503.066 0.600 14.860 3.012 0.39 184576. 0.2692
|
|
60.09 0.6609 0.7659 0.0723 0.0624 0.640 5.043 3.060 477.354 0.570 13.610 2.907 0.39 185285. 0.2487
|
|
63.25 0.6957 0.7771 0.0655 0.0587 0.601 4.738 2.771 448.464 0.535 12.326 2.803 0.39 186023. 0.2281
|
|
66.41 0.7305 0.7850 0.0585 0.0545 0.559 4.400 2.476 416.491 0.497 11.012 2.696 0.39 186789. 0.2074
|
|
69.57 0.7653 0.7887 0.0514 0.0499 0.512 4.031 2.175 381.515 0.455 9.675 2.586 0.39 187584. 0.1865
|
|
72.74 0.8001 0.7871 0.0442 0.0449 0.461 3.630 1.870 343.604 0.410 8.318 2.468 0.39 188407. 0.1650
|
|
75.90 0.8349 0.7780 0.0369 0.0396 0.406 3.200 1.561 302.834 0.361 6.944 2.338 0.39 189258. 0.1429
|
|
79.06 0.8697 0.7578 0.0296 0.0339 0.348 2.740 1.250 259.297 0.310 5.559 2.186 0.40 190136. 0.1195
|
|
82.22 0.9045 0.7188 0.0222 0.0279 0.286 2.252 0.937 213.112 0.254 4.167 1.994 0.40 191042. 0.0944
|
|
85.39 0.9392 0.6438 0.0147 0.0215 0.221 1.737 0.624 164.440 0.196 2.773 1.720 0.40 191975. 0.0664
|
|
88.55 0.9740 0.4826 0.0074 0.0148 0.152 1.199 0.311 113.490 0.135 1.384 1.243 0.40 192934. 0.0339
|
|
91.71 1.0088 0.0019 0.0000 0.0079 0.081 0.638 0.001 60.426 0.072 0.003 0.005 0.40 193901. 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 0.1433 0.0648 0.946 6.624 7.670 705.361 0.748 34.115 4.932 0.43 198971. 0.6679
|
|
3.56 0.0348 0.0746 0.1421 0.0663 0.968 6.780 7.607 721.977 0.766 33.838 4.779 0.43 199184. 0.6445
|
|
7.12 0.0696 0.1444 0.1408 0.0679 0.991 6.938 7.536 738.739 0.784 33.521 4.627 0.43 199424. 0.6211
|
|
10.68 0.1044 0.2096 0.1393 0.0694 1.013 7.094 7.455 755.332 0.801 33.158 4.476 0.43 199692. 0.5976
|
|
14.24 0.1392 0.2702 0.1375 0.0709 1.034 7.245 7.362 771.418 0.819 32.745 4.328 0.43 199990. 0.5743
|
|
17.80 0.1740 0.3265 0.1356 0.0723 1.055 7.388 7.256 786.630 0.835 32.275 4.184 0.43 200319. 0.5511
|
|
21.36 0.2089 0.3786 0.1333 0.0735 1.074 7.518 7.136 800.573 0.849 31.742 4.043 0.43 200679. 0.5281
|
|
24.92 0.2437 0.4268 0.1308 0.0747 1.090 7.634 7.001 812.839 0.862 31.141 3.907 0.43 201073. 0.5055
|
|
28.48 0.2785 0.4713 0.1280 0.0756 1.104 7.729 6.850 823.008 0.873 30.468 3.775 0.43 201501. 0.4831
|
|
32.04 0.3133 0.5124 0.1248 0.0763 1.114 7.801 6.681 830.651 0.881 29.717 3.648 0.43 201962. 0.4611
|
|
35.60 0.3481 0.5503 0.1213 0.0767 1.120 7.845 6.494 835.336 0.886 28.883 3.526 0.43 202458. 0.4393
|
|
39.16 0.3829 0.5851 0.1174 0.0769 1.122 7.857 6.287 836.625 0.888 27.963 3.408 0.43 202988. 0.4179
|
|
42.72 0.4177 0.6171 0.1132 0.0766 1.119 7.833 6.059 834.068 0.885 26.952 3.295 0.43 203553. 0.3966
|
|
46.28 0.4525 0.6464 0.1086 0.0760 1.109 7.769 5.811 827.206 0.878 25.846 3.186 0.43 204152. 0.3755
|
|
49.84 0.4873 0.6732 0.1035 0.0749 1.094 7.659 5.540 815.588 0.865 24.642 3.081 0.43 204786. 0.3546
|
|
53.40 0.5221 0.6975 0.0980 0.0734 1.071 7.502 5.247 798.843 0.848 23.340 2.979 0.43 205453. 0.3337
|
|
56.96 0.5569 0.7194 0.0922 0.0714 1.042 7.295 4.934 776.807 0.824 21.947 2.881 0.44 206153. 0.3129
|
|
60.52 0.5918 0.7390 0.0860 0.0689 1.005 7.040 4.603 749.573 0.795 20.475 2.785 0.44 206887. 0.2922
|
|
64.08 0.6266 0.7562 0.0795 0.0659 0.962 6.737 4.257 717.357 0.761 18.937 2.692 0.44 207653. 0.2716
|
|
67.64 0.6614 0.7709 0.0729 0.0625 0.912 6.390 3.899 680.375 0.722 17.345 2.600 0.44 208452. 0.2510
|
|
71.20 0.6962 0.7827 0.0660 0.0587 0.857 5.999 3.532 638.806 0.678 15.708 2.507 0.44 209284. 0.2304
|
|
74.76 0.7310 0.7912 0.0589 0.0545 0.795 5.567 3.155 592.787 0.629 14.035 2.414 0.44 210148. 0.2097
|
|
78.32 0.7658 0.7958 0.0518 0.0498 0.727 5.094 2.772 542.431 0.576 12.330 2.318 0.44 211043. 0.1887
|
|
81.88 0.8006 0.7953 0.0445 0.0448 0.654 4.581 2.383 487.840 0.518 10.599 2.216 0.44 211971. 0.1672
|
|
85.44 0.8354 0.7876 0.0372 0.0394 0.575 4.030 1.989 429.123 0.455 8.848 2.103 0.44 212929. 0.1450
|
|
89.00 0.8702 0.7690 0.0297 0.0337 0.491 3.441 1.592 366.411 0.389 7.082 1.971 0.44 213919. 0.1216
|
|
92.56 0.9050 0.7322 0.0223 0.0275 0.402 2.816 1.193 299.879 0.318 5.307 1.804 0.45 214940. 0.0964
|
|
96.12 0.9398 0.6599 0.0148 0.0211 0.308 2.158 0.793 229.755 0.244 3.528 1.566 0.45 215990. 0.0682
|
|
99.68 0.9746 0.5003 0.0074 0.0144 0.210 1.468 0.395 156.346 0.166 1.756 1.145 0.45 217070. 0.0352
|
|
103.24 1.0095 -0.0039 0.0000 0.0073 0.107 0.750 -0.002 79.867 0.085 -0.007 -0.009 0.45 218156. 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 0.1438 0.0648 1.298 8.182 9.503 968.075 0.924 42.269 4.452 0.48 221066. 0.6711
|
|
3.96 0.0348 0.0748 0.1427 0.0664 1.329 8.378 9.429 991.262 0.947 41.938 4.314 0.48 221303. 0.6477
|
|
7.91 0.0696 0.1449 0.1414 0.0680 1.361 8.576 9.343 1014.682 0.969 41.558 4.176 0.48 221569. 0.6242
|
|
11.87 0.1045 0.2103 0.1399 0.0695 1.392 8.773 9.245 1037.895 0.991 41.121 4.040 0.48 221867. 0.6007
|
|
15.83 0.1393 0.2711 0.1382 0.0710 1.422 8.963 9.132 1060.421 1.013 40.621 3.906 0.48 222198. 0.5772
|
|
19.79 0.1741 0.3275 0.1363 0.0724 1.451 9.143 9.004 1081.748 1.033 40.050 3.775 0.48 222564. 0.5539
|
|
23.74 0.2089 0.3797 0.1340 0.0738 1.477 9.309 8.858 1101.324 1.052 39.401 3.648 0.48 222965. 0.5309
|
|
27.70 0.2438 0.4281 0.1316 0.0749 1.500 9.454 8.693 1118.571 1.068 38.667 3.525 0.48 223403. 0.5082
|
|
31.66 0.2786 0.4727 0.1287 0.0759 1.519 9.576 8.508 1132.903 1.082 37.841 3.406 0.48 223879. 0.4858
|
|
35.62 0.3134 0.5139 0.1256 0.0766 1.534 9.667 8.300 1143.719 1.092 36.919 3.292 0.48 224392. 0.4637
|
|
39.57 0.3482 0.5519 0.1221 0.0770 1.543 9.724 8.069 1150.420 1.099 35.892 3.181 0.48 224944. 0.4419
|
|
43.53 0.3831 0.5869 0.1182 0.0772 1.545 9.740 7.814 1152.394 1.100 34.757 3.076 0.48 225535. 0.4204
|
|
47.49 0.4179 0.6191 0.1140 0.0770 1.541 9.712 7.533 1149.018 1.097 33.508 2.974 0.48 226164. 0.3991
|
|
51.44 0.4527 0.6486 0.1093 0.0763 1.528 9.633 7.226 1139.654 1.088 32.140 2.876 0.48 226831. 0.3780
|
|
55.40 0.4875 0.6755 0.1043 0.0753 1.507 9.498 6.891 1123.679 1.073 30.650 2.781 0.48 227536. 0.3570
|
|
59.36 0.5224 0.7001 0.0988 0.0737 1.476 9.302 6.528 1100.575 1.051 29.036 2.690 0.48 228278. 0.3361
|
|
63.32 0.5572 0.7223 0.0929 0.0717 1.435 9.045 6.139 1070.107 1.022 27.307 2.602 0.48 229058. 0.3153
|
|
67.27 0.5920 0.7422 0.0867 0.0691 1.384 8.726 5.728 1032.403 0.986 25.479 2.517 0.48 229875. 0.2945
|
|
71.23 0.6268 0.7598 0.0802 0.0662 1.325 8.349 5.299 987.761 0.943 23.568 2.433 0.49 230728. 0.2739
|
|
75.19 0.6616 0.7749 0.0734 0.0627 1.256 7.915 4.854 936.484 0.894 21.589 2.351 0.49 231617. 0.2532
|
|
79.14 0.6965 0.7872 0.0665 0.0589 1.179 7.428 4.396 878.823 0.839 19.554 2.269 0.49 232543. 0.2326
|
|
83.10 0.7313 0.7965 0.0594 0.0546 1.093 6.888 3.928 814.972 0.778 17.472 2.186 0.49 233504. 0.2119
|
|
87.06 0.7661 0.8018 0.0522 0.0499 0.999 6.298 3.451 745.088 0.712 15.351 2.101 0.49 234500. 0.1908
|
|
91.02 0.8009 0.8023 0.0449 0.0448 0.898 5.657 2.967 669.313 0.639 13.197 2.011 0.49 235532. 0.1693
|
|
94.97 0.8358 0.7958 0.0375 0.0394 0.788 4.968 2.477 587.798 0.561 11.017 1.911 0.49 236598. 0.1471
|
|
98.93 0.8706 0.7789 0.0300 0.0335 0.671 4.232 1.983 500.726 0.478 8.818 1.796 0.49 237699. 0.1236
|
|
102.89 0.9054 0.7442 0.0225 0.0273 0.548 3.451 1.485 408.336 0.390 6.607 1.650 0.50 238834. 0.0983
|
|
106.85 0.9402 0.6746 0.0149 0.0208 0.417 2.628 0.987 310.952 0.297 4.392 1.440 0.50 240003. 0.0700
|
|
110.80 0.9751 0.5174 0.0074 0.0140 0.280 1.766 0.491 208.997 0.200 2.183 1.065 0.50 241204. 0.0365
|
|
114.76 1.0099 -0.0065 0.0000 0.0069 0.138 0.868 -0.003 102.750 0.098 -0.013 -0.013 0.50 242408. 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 0.1444 0.0650 1.732 9.923 11.544 1291.390 1.121 51.347 4.054 0.52 243158. 0.6736
|
|
4.35 0.0348 0.0750 0.1433 0.0666 1.774 10.164 11.457 1322.832 1.148 50.961 3.928 0.52 243418. 0.6502
|
|
8.71 0.0697 0.1452 0.1420 0.0682 1.817 10.409 11.357 1354.642 1.176 50.517 3.803 0.52 243711. 0.6266
|
|
13.06 0.1045 0.2107 0.1406 0.0697 1.859 10.651 11.242 1386.210 1.203 50.004 3.678 0.52 244038. 0.6030
|
|
17.42 0.1393 0.2716 0.1389 0.0713 1.900 10.887 11.109 1416.892 1.230 49.413 3.556 0.52 244402. 0.5796
|
|
21.77 0.1742 0.3281 0.1370 0.0728 1.939 11.111 10.957 1445.975 1.255 48.736 3.437 0.52 244804. 0.5563
|
|
26.13 0.2090 0.3804 0.1349 0.0741 1.975 11.316 10.783 1472.707 1.278 47.963 3.321 0.52 245246. 0.5332
|
|
30.48 0.2439 0.4288 0.1324 0.0753 2.007 11.497 10.586 1496.297 1.299 47.086 3.209 0.53 245728. 0.5105
|
|
34.84 0.2787 0.4735 0.1296 0.0763 2.033 11.648 10.363 1515.948 1.316 46.097 3.101 0.53 246252. 0.4881
|
|
39.19 0.3135 0.5149 0.1265 0.0770 2.053 11.763 10.114 1530.847 1.329 44.987 2.997 0.53 246818. 0.4660
|
|
43.55 0.3484 0.5530 0.1230 0.0775 2.065 11.834 9.836 1540.174 1.337 43.750 2.897 0.53 247427. 0.4442
|
|
47.90 0.3832 0.5881 0.1192 0.0776 2.069 11.857 9.528 1543.107 1.340 42.379 2.800 0.53 248078. 0.4227
|
|
52.25 0.4180 0.6204 0.1149 0.0774 2.064 11.824 9.188 1538.804 1.336 40.867 2.708 0.53 248771. 0.4014
|
|
56.61 0.4529 0.6500 0.1102 0.0768 2.047 11.729 8.815 1526.408 1.325 39.209 2.619 0.53 249506. 0.3803
|
|
60.96 0.4877 0.6772 0.1052 0.0757 2.018 11.565 8.408 1505.081 1.307 37.400 2.534 0.53 250283. 0.3593
|
|
65.32 0.5225 0.7020 0.0996 0.0742 1.977 11.327 7.967 1474.120 1.280 35.438 2.451 0.53 251101. 0.3383
|
|
69.67 0.5574 0.7244 0.0937 0.0721 1.922 11.013 7.494 1433.203 1.244 33.335 2.372 0.53 251961. 0.3175
|
|
74.03 0.5922 0.7447 0.0875 0.0696 1.854 10.623 6.994 1382.496 1.200 31.109 2.295 0.53 252861. 0.2967
|
|
78.38 0.6270 0.7626 0.0809 0.0665 1.773 10.161 6.470 1322.403 1.148 28.781 2.219 0.53 253801. 0.2760
|
|
82.74 0.6619 0.7781 0.0741 0.0631 1.681 9.630 5.928 1253.337 1.088 26.368 2.145 0.54 254781. 0.2554
|
|
87.09 0.6967 0.7910 0.0672 0.0592 1.577 9.033 5.370 1175.641 1.021 23.885 2.072 0.54 255800. 0.2347
|
|
91.44 0.7316 0.8008 0.0600 0.0548 1.461 8.372 4.799 1089.581 0.946 21.344 1.998 0.54 256859. 0.2140
|
|
95.80 0.7664 0.8069 0.0527 0.0501 1.335 7.648 4.216 995.371 0.864 18.755 1.921 0.54 257956. 0.1929
|
|
100.15 0.8012 0.8083 0.0453 0.0449 1.198 6.863 3.625 893.206 0.775 16.125 1.841 0.54 259092. 0.1714
|
|
104.51 0.8361 0.8030 0.0379 0.0394 1.050 6.019 3.027 783.286 0.680 13.463 1.753 0.54 260267. 0.1491
|
|
108.86 0.8709 0.7876 0.0303 0.0335 0.893 5.116 2.423 665.857 0.578 10.776 1.650 0.54 261479. 0.1256
|
|
113.22 0.9057 0.7549 0.0227 0.0272 0.726 4.159 1.815 541.244 0.470 8.073 1.521 0.54 262729. 0.1002
|
|
117.57 0.9406 0.6880 0.0151 0.0206 0.550 3.149 1.206 409.881 0.356 5.365 1.335 0.55 264015. 0.0717
|
|
121.93 0.9754 0.5333 0.0075 0.0137 0.365 2.093 0.599 272.344 0.236 2.665 0.998 0.55 265337. 0.0378
|
|
126.28 1.0102 -0.0096 -0.0001 0.0065 0.173 0.991 -0.005 128.973 0.112 -0.022 -0.017 0.55 266659. 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 0.1450 0.0652 2.257 11.854 13.796 1682.919 1.339 61.365 3.718 0.57 265246. 0.6753
|
|
4.77 0.0350 0.0754 0.1439 0.0668 2.313 12.148 13.697 1724.767 1.373 60.926 3.602 0.57 265530. 0.6519
|
|
9.54 0.0700 0.1459 0.1427 0.0685 2.370 12.447 13.583 1767.182 1.406 60.416 3.486 0.57 265850. 0.6282
|
|
14.32 0.1050 0.2116 0.1413 0.0701 2.426 12.744 13.450 1809.343 1.440 59.824 3.372 0.57 266208. 0.6046
|
|
19.09 0.1400 0.2727 0.1397 0.0717 2.481 13.033 13.295 1850.367 1.472 59.138 3.259 0.57 266607. 0.5811
|
|
23.86 0.1750 0.3294 0.1378 0.0732 2.534 13.307 13.117 1889.286 1.503 58.346 3.149 0.57 267049. 0.5577
|
|
28.63 0.2100 0.3819 0.1357 0.0746 2.582 13.559 12.913 1925.072 1.532 57.438 3.043 0.57 267534. 0.5346
|
|
33.41 0.2450 0.4305 0.1333 0.0758 2.624 13.782 12.680 1956.657 1.557 56.402 2.939 0.57 268065. 0.5118
|
|
38.18 0.2800 0.4753 0.1305 0.0769 2.659 13.967 12.416 1982.956 1.578 55.228 2.840 0.57 268641. 0.4893
|
|
42.95 0.3150 0.5168 0.1274 0.0776 2.686 14.107 12.119 2002.877 1.594 53.906 2.744 0.57 269264. 0.4672
|
|
47.72 0.3500 0.5550 0.1239 0.0781 2.703 14.195 11.787 2015.325 1.604 52.428 2.653 0.57 269934. 0.4453
|
|
52.50 0.3850 0.5903 0.1200 0.0783 2.708 14.222 11.418 2019.194 1.607 50.786 2.565 0.58 270651. 0.4238
|
|
57.27 0.4200 0.6227 0.1157 0.0780 2.700 14.181 11.010 2013.361 1.602 48.971 2.480 0.58 271414. 0.4024
|
|
62.04 0.4550 0.6525 0.1110 0.0774 2.678 14.064 10.561 1996.685 1.589 46.976 2.399 0.58 272224. 0.3812
|
|
66.81 0.4900 0.6798 0.1058 0.0763 2.639 13.862 10.071 1968.057 1.566 44.795 2.321 0.58 273080. 0.3602
|
|
71.59 0.5250 0.7048 0.1002 0.0747 2.584 13.570 9.539 1926.557 1.533 42.429 2.246 0.58 273981. 0.3392
|
|
76.36 0.5600 0.7275 0.0942 0.0725 2.510 13.184 8.968 1871.783 1.490 39.890 2.173 0.58 274927. 0.3182
|
|
81.13 0.5950 0.7479 0.0879 0.0699 2.419 12.706 8.364 1803.987 1.436 37.201 2.103 0.58 275918. 0.2974
|
|
85.90 0.6300 0.7661 0.0812 0.0668 2.312 12.141 7.731 1723.722 1.372 34.387 2.034 0.58 276953. 0.2766
|
|
90.68 0.6650 0.7819 0.0744 0.0632 2.188 11.492 7.075 1631.540 1.298 31.471 1.967 0.58 278032. 0.2558
|
|
95.45 0.6999 0.7951 0.0673 0.0592 2.049 10.762 6.401 1527.898 1.216 28.471 1.900 0.59 279155. 0.2351
|
|
100.22 0.7349 0.8052 0.0600 0.0548 1.895 9.954 5.710 1413.152 1.125 25.399 1.833 0.59 280320. 0.2142
|
|
104.99 0.7699 0.8117 0.0526 0.0499 1.727 9.069 5.006 1287.587 1.025 22.268 1.764 0.59 281528. 0.1929
|
|
109.76 0.8049 0.8134 0.0451 0.0446 1.544 8.110 4.291 1151.459 0.916 19.088 1.690 0.59 282778. 0.1712
|
|
114.54 0.8399 0.8084 0.0375 0.0390 1.348 7.079 3.568 1005.045 0.800 15.868 1.610 0.59 284070. 0.1487
|
|
119.31 0.8749 0.7930 0.0298 0.0329 1.138 5.978 2.837 848.677 0.675 12.619 1.516 0.59 285404. 0.1249
|
|
124.08 0.9099 0.7596 0.0221 0.0265 0.916 4.809 2.102 682.800 0.543 9.350 1.396 0.59 286779. 0.0990
|
|
128.85 0.9449 0.6889 0.0144 0.0197 0.681 3.578 1.366 508.014 0.404 6.076 1.220 0.60 288194. 0.0697
|
|
133.63 0.9799 0.5165 0.0066 0.0126 0.436 2.290 0.632 325.113 0.259 2.811 0.882 0.60 289648. 0.0343
|
|
138.40 1.0149
|
|
|
|
|
|
|
|
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 0.1456 0.0656 2.885 13.987 16.264 2151.288 1.580 72.344 3.429 0.62 287329. 0.6762
|
|
5.15 0.0348 0.0750 0.1447 0.0672 2.957 14.338 16.156 2205.317 1.620 71.860 3.323 0.62 287634. 0.6530
|
|
10.29 0.0697 0.1451 0.1435 0.0689 3.031 14.695 16.029 2260.232 1.660 71.295 3.217 0.62 287977. 0.6297
|
|
15.44 0.1045 0.2106 0.1422 0.0706 3.104 15.051 15.880 2314.977 1.700 70.636 3.111 0.62 288362. 0.6063
|
|
20.59 0.1393 0.2715 0.1406 0.0722 3.176 15.399 15.707 2368.402 1.740 69.866 3.008 0.62 288791. 0.5829
|
|
25.73 0.1742 0.3280 0.1388 0.0737 3.244 15.729 15.506 2419.235 1.777 68.973 2.907 0.62 289266. 0.5598
|
|
30.88 0.2090 0.3803 0.1368 0.0752 3.307 16.034 15.275 2466.134 1.812 67.942 2.809 0.62 289788. 0.5369
|
|
36.03 0.2439 0.4287 0.1344 0.0764 3.363 16.304 15.009 2507.702 1.842 66.759 2.715 0.62 290359. 0.5142
|
|
41.17 0.2787 0.4735 0.1317 0.0775 3.410 16.531 14.706 2542.526 1.868 65.413 2.623 0.62 290979. 0.4919
|
|
46.32 0.3135 0.5149 0.1286 0.0783 3.445 16.704 14.364 2569.202 1.887 63.892 2.536 0.62 291650. 0.4700
|
|
51.46 0.3484 0.5532 0.1252 0.0788 3.468 16.816 13.981 2586.324 1.900 62.186 2.452 0.62 292371. 0.4483
|
|
56.61 0.3832 0.5885 0.1214 0.0790 3.477 16.856 13.553 2592.485 1.904 60.284 2.371 0.62 293143. 0.4268
|
|
61.76 0.4180 0.6210 0.1171 0.0788 3.468 16.815 13.080 2586.253 1.900 58.178 2.294 0.62 293965. 0.4056
|
|
66.90 0.4529 0.6510 0.1124 0.0782 3.441 16.685 12.558 2566.178 1.885 55.858 2.220 0.63 294837. 0.3846
|
|
72.05 0.4877 0.6785 0.1073 0.0771 3.394 16.455 11.987 2530.850 1.859 53.317 2.148 0.63 295759. 0.3637
|
|
77.20 0.5226 0.7038 0.1018 0.0756 3.324 16.118 11.366 2479.075 1.821 50.555 2.079 0.63 296729. 0.3428
|
|
82.34 0.5574 0.7267 0.0958 0.0735 3.232 15.671 10.698 2410.264 1.770 47.585 2.013 0.63 297748. 0.3220
|
|
87.49 0.5922 0.7476 0.0894 0.0709 3.117 15.114 9.989 2324.673 1.708 44.433 1.949 0.63 298815. 0.3012
|
|
92.64 0.6271 0.7662 0.0828 0.0678 2.981 14.453 9.247 2223.004 1.633 41.130 1.887 0.63 299929. 0.2805
|
|
97.78 0.6619 0.7826 0.0759 0.0642 2.824 13.693 8.476 2105.986 1.547 37.702 1.826 0.63 301090. 0.2599
|
|
102.93 0.6967 0.7964 0.0688 0.0602 2.647 12.836 7.682 1974.221 1.450 34.171 1.765 0.63 302298. 0.2392
|
|
108.08 0.7316 0.8074 0.0615 0.0557 2.452 11.886 6.869 1828.185 1.343 30.552 1.704 0.64 303551. 0.2184
|
|
113.22 0.7664 0.8150 0.0541 0.0509 2.237 10.847 6.039 1668.252 1.225 26.862 1.642 0.64 304851. 0.1973
|
|
118.37 0.8013 0.8181 0.0465 0.0456 2.004 9.718 5.196 1494.753 1.098 23.110 1.577 0.64 306195. 0.1757
|
|
123.51 0.8361 0.8151 0.0389 0.0399 1.754 8.504 4.341 1308.033 0.961 19.309 1.505 0.64 307585. 0.1534
|
|
128.66 0.8709 0.8027 0.0311 0.0338 1.487 7.207 3.478 1108.503 0.814 15.470 1.423 0.64 309019. 0.1298
|
|
133.81 0.9058 0.7741 0.0234 0.0273 1.203 5.830 2.609 896.705 0.659 11.605 1.320 0.64 310497. 0.1042
|
|
138.95 0.9406 0.7131 0.0156 0.0205 0.903 4.378 1.738 673.377 0.495 7.730 1.171 0.65 312019. 0.0755
|
|
144.10 0.9754 0.5660 0.0078 0.0134 0.589 2.858 0.868 439.499 0.323 3.862 0.896 0.65 313581. 0.0408
|
|
149.25 1.0103 0.0036 0.0000 0.0060 0.262 1.272 0.002 195.648 0.144 0.011 0.006 0.65 315141. 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 0.1463 0.0662 3.638 16.376 18.952 2712.490 1.850 84.297 3.169 0.67 309407. 0.6746
|
|
5.54 0.0348 0.0747 0.1454 0.0679 3.729 16.788 18.835 2780.666 1.897 83.776 3.072 0.67 309733. 0.6519
|
|
11.09 0.0697 0.1446 0.1444 0.0696 3.822 17.207 18.697 2850.132 1.944 83.162 2.975 0.67 310102. 0.6291
|
|
16.63 0.1045 0.2100 0.1431 0.0713 3.915 17.626 18.534 2919.552 1.991 82.440 2.879 0.67 310516. 0.6061
|
|
22.18 0.1394 0.2708 0.1416 0.0729 4.006 18.036 18.343 2987.466 2.038 81.589 2.785 0.67 310977. 0.5832
|
|
27.72 0.1742 0.3272 0.1399 0.0745 4.093 18.427 18.119 3052.266 2.082 80.594 2.693 0.67 311487. 0.5604
|
|
33.27 0.2091 0.3796 0.1379 0.0760 4.174 18.790 17.859 3112.239 2.123 79.435 2.603 0.67 312050. 0.5378
|
|
38.81 0.2439 0.4280 0.1356 0.0773 4.245 19.112 17.558 3165.601 2.159 78.096 2.516 0.67 312665. 0.5154
|
|
44.35 0.2788 0.4729 0.1329 0.0784 4.305 19.383 17.213 3210.531 2.190 76.563 2.432 0.67 313334. 0.4933
|
|
49.90 0.3136 0.5143 0.1299 0.0792 4.352 19.592 16.821 3245.195 2.214 74.822 2.351 0.67 314058. 0.4715
|
|
55.44 0.3485 0.5526 0.1265 0.0798 4.382 19.729 16.380 3267.764 2.229 72.859 2.274 0.67 314836. 0.4499
|
|
60.99 0.3833 0.5880 0.1227 0.0800 4.394 19.781 15.887 3276.396 2.235 70.664 2.199 0.67 315669. 0.4286
|
|
66.53 0.4182 0.6207 0.1184 0.0798 4.384 19.737 15.338 3269.219 2.230 68.224 2.128 0.67 316557. 0.4075
|
|
72.08 0.4530 0.6508 0.1137 0.0792 4.351 19.587 14.733 3244.357 2.213 65.530 2.060 0.67 317499. 0.3866
|
|
77.62 0.4879 0.6785 0.1086 0.0781 4.291 19.320 14.068 3200.020 2.183 62.574 1.994 0.67 318494. 0.3657
|
|
83.16 0.5227 0.7039 0.1030 0.0765 4.204 18.925 13.344 3134.692 2.138 59.354 1.931 0.68 319542. 0.3449
|
|
88.71 0.5576 0.7272 0.0970 0.0744 4.087 18.399 12.564 3047.608 2.079 55.884 1.870 0.68 320642. 0.3241
|
|
94.25 0.5924 0.7483 0.0906 0.0717 3.941 17.744 11.735 2939.083 2.005 52.197 1.811 0.68 321794. 0.3033
|
|
99.80 0.6273 0.7673 0.0839 0.0686 3.768 16.965 10.865 2810.031 1.917 48.329 1.754 0.68 322996. 0.2827
|
|
105.34 0.6621 0.7840 0.0769 0.0650 3.569 16.068 9.962 2661.400 1.815 44.311 1.698 0.68 324249. 0.2620
|
|
110.89 0.6970 0.7984 0.0697 0.0609 3.344 15.057 9.031 2493.969 1.701 40.168 1.642 0.68 325552. 0.2413
|
|
116.43 0.7318 0.8099 0.0624 0.0563 3.096 13.936 8.076 2308.353 1.575 35.921 1.587 0.68 326905. 0.2205
|
|
121.97 0.7667 0.8182 0.0548 0.0514 2.823 12.709 7.101 2105.044 1.436 31.586 1.530 0.69 328306. 0.1994
|
|
127.52 0.8015 0.8221 0.0472 0.0460 2.527 11.377 6.110 1884.465 1.285 27.177 1.471 0.69 329757. 0.1777
|
|
133.06 0.8364 0.8201 0.0394 0.0402 2.209 9.944 5.105 1647.053 1.123 22.708 1.406 0.69 331255. 0.1553
|
|
138.61 0.8712 0.8090 0.0316 0.0340 1.868 8.412 4.090 1393.329 0.950 18.192 1.331 0.69 332801. 0.1317
|
|
144.15 0.9061 0.7822 0.0237 0.0274 1.507 6.786 3.067 1124.005 0.767 13.643 1.238 0.69 334395. 0.1060
|
|
149.70 0.9409 0.7233 0.0158 0.0205 1.127 5.072 2.041 840.118 0.573 9.080 1.102 0.70 336035. 0.0770
|
|
155.24 0.9758 0.5780 0.0079 0.0133 0.728 3.279 1.017 543.113 0.370 4.523 0.849 0.70 337720. 0.0419
|
|
160.78 1.0106 -0.0057 0.0000 0.0057 0.314 1.412 -0.004 233.897 0.160 -0.018 -0.008 0.70 339393. 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 0.1470 0.0675 4.562 19.171 21.858 3402.156 2.166 97.226 2.914 0.71 331480. 0.6662
|
|
5.94 0.0349 0.0737 0.1462 0.0692 4.674 19.642 21.736 3485.735 2.219 96.681 2.828 0.71 331827. 0.6448
|
|
11.88 0.0697 0.1428 0.1452 0.0709 4.789 20.121 21.590 3570.905 2.273 96.033 2.742 0.71 332220. 0.6231
|
|
17.82 0.1046 0.2076 0.1440 0.0725 4.903 20.601 21.417 3655.978 2.327 95.263 2.657 0.71 332661. 0.6013
|
|
23.76 0.1394 0.2680 0.1427 0.0742 5.014 21.069 21.211 3739.098 2.380 94.347 2.573 0.71 333153. 0.5794
|
|
29.70 0.1743 0.3243 0.1410 0.0758 5.120 21.515 20.967 3818.277 2.431 93.262 2.491 0.72 333699. 0.5577
|
|
35.64 0.2091 0.3766 0.1391 0.0772 5.218 21.927 20.681 3891.403 2.477 91.988 2.410 0.72 334301. 0.5360
|
|
41.58 0.2440 0.4252 0.1368 0.0785 5.306 22.293 20.347 3956.320 2.519 90.502 2.333 0.72 334960. 0.5145
|
|
47.52 0.2788 0.4703 0.1342 0.0796 5.379 22.600 19.961 4010.839 2.553 88.786 2.257 0.72 335677. 0.4931
|
|
53.46 0.3137 0.5120 0.1313 0.0804 5.435 22.837 19.520 4052.764 2.580 86.823 2.185 0.72 336454. 0.4719
|
|
59.40 0.3485 0.5506 0.1279 0.0810 5.471 22.990 19.019 4079.894 2.597 84.598 2.114 0.72 337289. 0.4509
|
|
65.34 0.3834 0.5864 0.1241 0.0812 5.485 23.046 18.457 4089.984 2.604 82.098 2.047 0.72 338184. 0.4300
|
|
71.28 0.4182 0.6193 0.1199 0.0810 5.472 22.994 17.830 4080.713 2.598 79.308 1.982 0.72 339137. 0.4092
|
|
77.22 0.4531 0.6497 0.1152 0.0804 5.431 22.819 17.135 4049.674 2.578 76.217 1.919 0.72 340149. 0.3885
|
|
83.17 0.4879 0.6777 0.1101 0.0793 5.357 22.508 16.370 3994.499 2.543 72.815 1.859 0.72 341218. 0.3677
|
|
89.11 0.5228 0.7034 0.1045 0.0777 5.248 22.050 15.535 3913.159 2.491 69.101 1.801 0.72 342343. 0.3470
|
|
95.05 0.5576 0.7269 0.0984 0.0755 5.102 21.438 14.634 3804.547 2.422 65.090 1.745 0.73 343525. 0.3263
|
|
100.99 0.5925 0.7484 0.0920 0.0728 4.920 20.674 13.674 3668.942 2.336 60.820 1.690 0.73 344761. 0.3056
|
|
106.93 0.6273 0.7677 0.0852 0.0696 4.704 19.764 12.665 3507.479 2.233 56.333 1.638 0.73 346052. 0.2850
|
|
112.87 0.6622 0.7849 0.0781 0.0659 4.454 18.715 11.616 3321.373 2.114 51.668 1.586 0.73 347397. 0.2644
|
|
118.81 0.6970 0.7997 0.0708 0.0617 4.173 17.534 10.534 3111.636 1.981 46.854 1.535 0.73 348796. 0.2437
|
|
124.75 0.7319 0.8119 0.0634 0.0571 3.861 16.223 9.423 2879.042 1.833 41.914 1.485 0.73 350247. 0.2228
|
|
130.69 0.7667 0.8208 0.0557 0.0521 3.519 14.787 8.289 2624.225 1.671 36.869 1.433 0.73 351750. 0.2017
|
|
136.63 0.8016 0.8256 0.0480 0.0466 3.148 13.229 7.135 2347.756 1.495 31.735 1.378 0.74 353306. 0.1800
|
|
142.57 0.8364 0.8246 0.0401 0.0407 2.749 11.553 5.964 2050.286 1.305 26.527 1.319 0.74 354913. 0.1575
|
|
148.51 0.8713 0.8146 0.0321 0.0344 2.324 9.763 4.780 1732.683 1.103 21.260 1.251 0.74 356571. 0.1338
|
|
154.45 0.9061 0.7888 0.0241 0.0277 1.872 7.867 3.586 1396.179 0.889 15.951 1.165 0.74 358279. 0.1079
|
|
160.39 0.9410 0.7304 0.0161 0.0207 1.398 5.874 2.388 1042.503 0.664 10.620 1.039 0.75 360037. 0.0785
|
|
166.33 0.9758 0.5837 0.0080 0.0134 0.904 3.798 1.189 673.986 0.429 5.291 0.800 0.75 361843. 0.0427
|
|
172.27 1.0107 -0.0074 0.0000 0.0058 0.392 1.647 -0.006 292.318 0.186 -0.028 -0.010 0.75 363633. 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 0.1477 0.0701 5.749 22.647 24.980 4287.135 2.559 111.111 2.643 0.76 353546. 0.6459
|
|
6.33 0.0348 0.0714 0.1469 0.0717 5.883 23.177 24.855 4387.324 2.618 110.557 2.570 0.76 353914. 0.6264
|
|
12.67 0.0697 0.1386 0.1460 0.0734 6.020 23.715 24.706 4489.146 2.679 109.894 2.496 0.76 354330. 0.6067
|
|
19.00 0.1045 0.2019 0.1450 0.0751 6.156 24.249 24.527 4590.357 2.740 109.098 2.424 0.76 354797. 0.5869
|
|
25.34 0.1394 0.2613 0.1437 0.0767 6.287 24.768 24.312 4688.544 2.798 108.139 2.352 0.76 355320. 0.5670
|
|
31.67 0.1742 0.3168 0.1422 0.0782 6.412 25.257 24.053 4781.122 2.854 106.990 2.282 0.76 355900. 0.5472
|
|
38.01 0.2090 0.3688 0.1404 0.0796 6.525 25.703 23.746 4865.490 2.904 105.621 2.214 0.76 356540. 0.5274
|
|
44.34 0.2439 0.4174 0.1382 0.0808 6.623 26.091 23.383 4939.087 2.948 104.006 2.147 0.76 357242. 0.5077
|
|
50.68 0.2787 0.4628 0.1357 0.0817 6.704 26.410 22.959 4999.403 2.984 102.123 2.083 0.76 358007. 0.4880
|
|
57.01 0.3136 0.5050 0.1328 0.0825 6.764 26.646 22.470 5044.007 3.010 99.949 2.021 0.77 358836. 0.4683
|
|
63.34 0.3484 0.5443 0.1295 0.0829 6.800 26.785 21.912 5070.460 3.026 97.466 1.960 0.77 359728. 0.4487
|
|
69.68 0.3832 0.5808 0.1258 0.0830 6.807 26.816 21.281 5076.313 3.030 94.657 1.901 0.77 360684. 0.4289
|
|
76.01 0.4181 0.6147 0.1216 0.0827 6.784 26.725 20.573 5058.985 3.019 91.508 1.844 0.77 361704. 0.4091
|
|
82.35 0.4529 0.6459 0.1170 0.0820 6.726 26.496 19.785 5015.681 2.994 88.005 1.789 0.77 362785. 0.3891
|
|
88.68 0.4878 0.6747 0.1118 0.0808 6.629 26.115 18.915 4943.522 2.950 84.134 1.735 0.77 363928. 0.3691
|
|
95.02 0.5226 0.7012 0.1062 0.0791 6.490 25.568 17.962 4839.950 2.889 79.893 1.683 0.77 365131. 0.3488
|
|
101.35 0.5574 0.7254 0.1001 0.0769 6.308 24.847 16.929 4703.523 2.807 75.301 1.633 0.77 366394. 0.3284
|
|
107.69 0.5923 0.7474 0.0936 0.0741 6.081 23.954 15.827 4534.413 2.706 70.400 1.583 0.78 367715. 0.3080
|
|
114.02 0.6271 0.7673 0.0867 0.0709 5.812 22.894 14.667 4333.830 2.587 65.241 1.535 0.78 369095. 0.2875
|
|
120.35 0.6619 0.7850 0.0796 0.0671 5.502 21.675 13.460 4103.098 2.449 59.868 1.488 0.78 370532. 0.2669
|
|
126.69 0.6968 0.8004 0.0722 0.0628 5.154 20.303 12.212 3843.291 2.294 54.318 1.441 0.78 372026. 0.2463
|
|
133.02 0.7316 0.8132 0.0646 0.0581 4.768 18.782 10.930 3555.326 2.122 48.617 1.394 0.78 373575. 0.2254
|
|
139.36 0.7665 0.8227 0.0569 0.0530 4.345 17.116 9.620 3240.098 1.934 42.789 1.347 0.78 375181. 0.2042
|
|
145.69 0.8013 0.8280 0.0490 0.0474 3.887 15.313 8.285 2898.693 1.730 36.853 1.296 0.79 376841. 0.1825
|
|
152.03 0.8361 0.8272 0.0410 0.0414 3.396 13.378 6.930 2532.417 1.511 30.825 1.241 0.79 378556. 0.1598
|
|
158.36 0.8710 0.8167 0.0329 0.0350 2.874 11.321 5.558 2142.969 1.279 24.722 1.176 0.79 380325. 0.1356
|
|
164.70 0.9058 0.7888 0.0247 0.0283 2.323 9.153 4.173 1732.582 1.034 18.563 1.093 0.79 382148. 0.1091
|
|
171.03 0.9407 0.7251 0.0164 0.0213 1.749 6.890 2.781 1304.211 0.778 12.369 0.967 0.80 384023. 0.0789
|
|
177.36 0.9755 0.5675 0.0082 0.0141 1.155 4.552 1.386 861.597 0.514 6.166 0.730 0.80 385948. 0.0420
|
|
183.70 1.0103 -0.0068 0.0000 0.0067 0.547 2.155 -0.008 407.910 0.243 -0.034 -0.008 0.80 387861. 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 0.1482 0.0747 7.345 27.234 28.305 5477.481 3.077 125.901 2.344 0.81 375608. 0.6097
|
|
6.73 0.0348 0.0674 0.1476 0.0763 7.505 27.825 28.182 5596.430 3.144 125.354 2.284 0.81 375995. 0.5929
|
|
13.46 0.0697 0.1312 0.1468 0.0779 7.666 28.424 28.035 5716.825 3.211 124.698 2.224 0.81 376433. 0.5759
|
|
20.19 0.1045 0.1916 0.1459 0.0795 7.826 29.014 27.855 5835.523 3.278 123.901 2.165 0.81 376925. 0.5587
|
|
26.92 0.1393 0.2487 0.1447 0.0811 7.978 29.578 27.637 5949.075 3.342 122.929 2.107 0.81 377477. 0.5416
|
|
33.65 0.1742 0.3025 0.1433 0.0825 8.118 30.099 27.371 6053.914 3.401 121.746 2.051 0.81 378090. 0.5246
|
|
40.38 0.2090 0.3533 0.1416 0.0838 8.243 30.560 27.049 6146.529 3.453 120.316 1.996 0.81 378767. 0.5076
|
|
47.11 0.2438 0.4013 0.1396 0.0848 8.346 30.944 26.665 6223.725 3.496 118.604 1.943 0.81 379512. 0.4907
|
|
53.84 0.2787 0.4466 0.1372 0.0856 8.425 31.237 26.209 6282.638 3.529 116.580 1.892 0.81 380324. 0.4737
|
|
60.57 0.3135 0.4893 0.1345 0.0862 8.476 31.426 25.678 6320.716 3.550 114.216 1.843 0.81 381205. 0.4566
|
|
67.30 0.3484 0.5294 0.1312 0.0864 8.496 31.500 25.065 6335.583 3.559 111.489 1.794 0.81 382155. 0.4393
|
|
74.03 0.3832 0.5670 0.1276 0.0862 8.482 31.447 24.366 6324.899 3.553 108.380 1.747 0.82 383173. 0.4217
|
|
80.75 0.4180 0.6023 0.1235 0.0857 8.430 31.254 23.577 6286.180 3.531 104.870 1.701 0.82 384259. 0.4039
|
|
87.48 0.4529 0.6350 0.1188 0.0847 8.337 30.909 22.694 6216.644 3.492 100.943 1.656 0.82 385411. 0.3857
|
|
94.21 0.4877 0.6654 0.1137 0.0833 8.198 30.394 21.714 6113.190 3.434 96.585 1.611 0.82 386629. 0.3671
|
|
100.94 0.5225 0.6935 0.1081 0.0814 8.010 29.697 20.636 5972.880 3.355 91.791 1.567 0.82 387911. 0.3481
|
|
107.67 0.5574 0.7193 0.1019 0.0790 7.770 28.807 19.465 5794.029 3.255 86.580 1.524 0.82 389257. 0.3287
|
|
114.40 0.5922 0.7428 0.0954 0.0760 7.479 27.728 18.210 5576.921 3.133 81.000 1.481 0.82 390665. 0.3090
|
|
121.13 0.6270 0.7641 0.0884 0.0726 7.138 26.466 16.887 5323.056 2.990 75.112 1.439 0.83 392135. 0.2891
|
|
127.86 0.6619 0.7831 0.0812 0.0686 6.751 25.029 15.505 5034.040 2.828 68.968 1.397 0.83 393665. 0.2690
|
|
134.59 0.6967 0.7997 0.0737 0.0642 6.318 23.423 14.076 4711.073 2.646 62.612 1.355 0.83 395255. 0.2486
|
|
141.32 0.7315 0.8132 0.0660 0.0594 5.842 21.659 12.607 4356.252 2.447 56.076 1.313 0.83 396905. 0.2279
|
|
148.05 0.7664 0.8228 0.0581 0.0541 5.327 19.750 11.102 3972.405 2.231 49.382 1.268 0.83 398614. 0.2065
|
|
154.78 0.8012 0.8273 0.0501 0.0485 4.773 17.697 9.567 3559.328 1.999 42.555 1.219 0.84 400380. 0.1844
|
|
161.51 0.8361 0.8244 0.0419 0.0425 4.183 15.508 8.007 3119.200 1.752 35.615 1.164 0.84 402204. 0.1611
|
|
168.24 0.8709 0.8095 0.0336 0.0362 3.561 13.202 6.425 2655.338 1.492 28.580 1.098 0.84 404086. 0.1360
|
|
174.97 0.9057 0.7734 0.0253 0.0296 2.912 10.797 4.827 2171.556 1.220 21.470 1.008 0.84 406023. 0.1083
|
|
181.70 0.9406 0.6950 0.0168 0.0228 2.243 8.316 3.218 1672.669 0.940 14.312 0.872 0.84 408017. 0.0765
|
|
188.43 0.9754 0.5161 0.0084 0.0159 1.562 5.789 1.604 1164.439 0.654 7.135 0.625 0.85 410063. 0.0387
|
|
195.16 1.0102 -0.0050 0.0000 0.0089 0.874 3.242 -0.008 652.084 0.366 -0.038 -0.006 0.85 412111. 0.0000
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PROP RPM = 18000
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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 0.1484 0.0815 9.517 33.323 31.776 7096.505 3.765 141.340 2.031 0.86 397676. 0.5598
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7.13 0.0349 0.0620 0.1479 0.0831 9.707 33.990 31.657 7238.510 3.840 140.811 1.984 0.86 398081. 0.5457
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14.26 0.0697 0.1211 0.1472 0.0848 9.900 34.665 31.515 7382.357 3.916 140.178 1.936 0.86 398540. 0.5315
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21.39 0.1046 0.1772 0.1464 0.0864 10.089 35.328 31.342 7523.580 3.991 139.407 1.889 0.86 399057. 0.5172
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28.53 0.1395 0.2306 0.1454 0.0879 10.268 35.955 31.128 7657.101 4.062 138.458 1.844 0.86 399635. 0.5030
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35.66 0.1743 0.2814 0.1442 0.0893 10.430 36.521 30.864 7777.511 4.126 137.284 1.800 0.86 400280. 0.4890
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42.79 0.2092 0.3298 0.1426 0.0905 10.567 37.000 30.540 7879.556 4.180 135.841 1.758 0.86 400993. 0.4750
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49.92 0.2441 0.3760 0.1408 0.0914 10.673 37.371 30.144 7958.601 4.222 134.083 1.718 0.86 401779. 0.4612
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57.05 0.2789 0.4202 0.1386 0.0920 10.743 37.616 29.669 8010.795 4.250 131.969 1.680 0.86 402637. 0.4474
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64.18 0.3138 0.4624 0.1359 0.0922 10.773 37.721 29.106 8033.077 4.262 129.463 1.643 0.86 403571. 0.4335
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71.32 0.3487 0.5028 0.1329 0.0921 10.759 37.672 28.446 8022.663 4.256 126.530 1.608 0.86 404578. 0.4194
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78.45 0.3835 0.5413 0.1293 0.0916 10.699 37.462 27.686 7977.921 4.232 123.147 1.574 0.86 405660. 0.4050
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85.58 0.4184 0.5779 0.1253 0.0907 10.590 37.083 26.819 7897.213 4.190 119.291 1.540 0.86 406814. 0.3900
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92.71 0.4533 0.6124 0.1207 0.0893 10.431 36.525 25.842 7778.514 4.127 114.945 1.507 0.87 408040. 0.3746
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99.84 0.4881 0.6449 0.1156 0.0875 10.218 35.778 24.751 7619.417 4.042 110.092 1.473 0.87 409336. 0.3584
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106.97 0.5230 0.6752 0.1100 0.0852 9.947 34.830 23.545 7417.464 3.935 104.728 1.440 0.87 410700. 0.3416
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114.11 0.5579 0.7033 0.1038 0.0823 9.617 33.673 22.229 7171.114 3.804 98.873 1.406 0.87 412132. 0.3241
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121.24 0.5927 0.7292 0.0972 0.0790 9.227 32.310 20.813 6880.735 3.650 92.578 1.372 0.87 413630. 0.3061
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128.37 0.6276 0.7529 0.0902 0.0752 8.781 30.748 19.315 6548.195 3.474 85.911 1.338 0.87 415193. 0.2875
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135.50 0.6624 0.7742 0.0829 0.0709 8.282 28.999 17.746 6175.688 3.276 78.936 1.303 0.88 416821. 0.2685
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142.63 0.6973 0.7931 0.0753 0.0662 7.731 27.071 16.121 5765.007 3.058 71.705 1.268 0.88 418512. 0.2490
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149.76 0.7322 0.8088 0.0675 0.0611 7.133 24.976 14.447 5318.836 2.822 64.258 1.232 0.88 420265. 0.2290
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156.90 0.7670 0.8183 0.0594 0.0557 6.507 22.784 12.728 4852.145 2.574 56.613 1.190 0.88 422081. 0.2075
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164.03 0.8019 0.8194 0.0512 0.0501 5.855 20.503 10.970 4366.250 2.316 48.793 1.140 0.88 423957. 0.1845
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171.16 0.8368 0.8105 0.0429 0.0443 5.169 18.101 9.180 3854.729 2.045 40.833 1.080 0.89 425895. 0.1600
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178.29 0.8716 0.7856 0.0344 0.0382 4.456 15.605 7.364 3323.164 1.763 32.754 1.005 0.89 427892. 0.1334
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185.42 0.9065 0.7337 0.0258 0.0319 3.725 13.044 5.527 2777.772 1.474 24.586 0.903 0.89 429949. 0.1038
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192.55 0.9414 0.6328 0.0172 0.0256 2.985 10.451 3.678 2225.757 1.181 16.362 0.750 0.89 432064. 0.0703
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199.69 0.9762 0.4333 0.0085 0.0192 2.246 7.866 1.828 1675.084 0.889 8.131 0.495 0.90 434236. 0.0327
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206.82 1.0111 -0.0045 -0.0001 0.0130 1.518 5.316 -0.012 1132.205 0.601 -0.056 -0.005 0.90 436429. 0.0000
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