427 lines
76 KiB
Plaintext
427 lines
76 KiB
Plaintext
20.5x10PN (205x10PN.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 0.0881 0.0340 0.010 0.625 0.496 7.397 0.071 2.205 30.394 0.08 45252. 0.6125
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0.44 0.0227 0.0573 0.0866 0.0344 0.010 0.632 0.488 7.472 0.071 2.169 29.595 0.08 45280. 0.5915
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0.88 0.0455 0.1114 0.0851 0.0347 0.010 0.637 0.479 7.541 0.072 2.130 28.797 0.08 45310. 0.5703
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1.32 0.0682 0.1625 0.0834 0.0350 0.010 0.643 0.469 7.603 0.073 2.088 28.002 0.08 45342. 0.5491
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1.77 0.0909 0.2106 0.0816 0.0352 0.010 0.647 0.459 7.655 0.073 2.043 27.213 0.08 45378. 0.5279
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2.21 0.1137 0.2557 0.0797 0.0354 0.010 0.651 0.448 7.697 0.074 1.995 26.429 0.08 45415. 0.5066
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2.65 0.1364 0.2978 0.0776 0.0356 0.010 0.653 0.437 7.726 0.074 1.944 25.653 0.08 45456. 0.4853
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3.09 0.1591 0.3370 0.0754 0.0356 0.010 0.654 0.425 7.739 0.074 1.889 24.883 0.08 45499. 0.4641
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3.53 0.1819 0.3734 0.0731 0.0356 0.010 0.654 0.411 7.736 0.074 1.830 24.121 0.08 45545. 0.4428
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3.97 0.2046 0.4069 0.0706 0.0355 0.010 0.652 0.397 7.714 0.074 1.768 23.366 0.08 45593. 0.4216
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4.41 0.2273 0.4376 0.0680 0.0353 0.010 0.648 0.383 7.672 0.073 1.702 22.618 0.08 45645. 0.4004
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4.85 0.2501 0.4656 0.0652 0.0350 0.010 0.643 0.367 7.607 0.073 1.632 21.874 0.08 45700. 0.3792
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5.30 0.2728 0.4907 0.0623 0.0346 0.010 0.636 0.350 7.521 0.072 1.559 21.135 0.08 45758. 0.3581
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5.74 0.2956 0.5130 0.0592 0.0341 0.010 0.626 0.333 7.412 0.071 1.483 20.396 0.08 45818. 0.3370
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6.18 0.3183 0.5325 0.0561 0.0335 0.010 0.615 0.316 7.280 0.070 1.403 19.657 0.08 45882. 0.3160
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6.62 0.3410 0.5489 0.0528 0.0328 0.010 0.602 0.297 7.125 0.068 1.321 18.913 0.08 45949. 0.2951
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7.06 0.3638 0.5622 0.0494 0.0320 0.009 0.587 0.278 6.946 0.066 1.237 18.161 0.08 46020. 0.2741
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7.50 0.3865 0.5722 0.0459 0.0310 0.009 0.570 0.259 6.743 0.064 1.150 17.396 0.08 46093. 0.2532
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7.94 0.4092 0.5785 0.0424 0.0300 0.009 0.551 0.239 6.516 0.062 1.061 16.611 0.08 46170. 0.2322
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8.39 0.4320 0.5808 0.0388 0.0288 0.008 0.529 0.218 6.264 0.060 0.970 15.798 0.08 46250. 0.2112
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8.83 0.4547 0.5785 0.0351 0.0276 0.008 0.506 0.197 5.987 0.057 0.878 14.949 0.08 46333. 0.1901
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9.27 0.4774 0.5709 0.0313 0.0262 0.008 0.481 0.176 5.685 0.054 0.783 14.050 0.08 46420. 0.1688
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9.71 0.5002 0.5570 0.0275 0.0247 0.007 0.453 0.155 5.359 0.051 0.688 13.084 0.08 46510. 0.1472
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10.15 0.5229 0.5352 0.0236 0.0230 0.007 0.423 0.133 5.007 0.048 0.591 12.028 0.08 46603. 0.1254
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10.59 0.5456 0.5037 0.0197 0.0213 0.006 0.391 0.111 4.630 0.044 0.493 10.847 0.08 46700. 0.1033
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11.03 0.5684 0.4592 0.0157 0.0195 0.006 0.357 0.089 4.229 0.040 0.394 9.494 0.08 46800. 0.0808
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11.48 0.5911 0.3971 0.0118 0.0175 0.005 0.322 0.066 3.805 0.036 0.295 7.894 0.08 46903. 0.0582
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11.92 0.6138 0.3099 0.0078 0.0155 0.005 0.284 0.044 3.359 0.032 0.195 5.932 0.08 47010. 0.0356
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12.36 0.6366 0.1845 0.0039 0.0133 0.004 0.244 0.022 2.892 0.028 0.097 3.405 0.08 47119. 0.0144
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12.80 0.6593 -0.0046 -0.0001 0.0111 0.003 0.203 0.000 2.404 0.023 -0.002 -0.081 0.08 47229. 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 0.0885 0.0308 0.072 2.261 1.993 53.503 0.255 8.864 16.894 0.16 90501. 0.6826
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0.89 0.0228 0.0638 0.0871 0.0312 0.073 2.289 1.960 54.164 0.259 8.719 16.415 0.16 90558. 0.6578
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1.77 0.0457 0.1239 0.0855 0.0315 0.073 2.315 1.925 54.779 0.262 8.563 15.941 0.16 90619. 0.6331
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2.66 0.0685 0.1804 0.0838 0.0318 0.074 2.338 1.888 55.334 0.264 8.396 15.472 0.16 90684. 0.6084
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3.55 0.0914 0.2334 0.0820 0.0321 0.075 2.359 1.847 55.815 0.266 8.216 15.011 0.16 90755. 0.5839
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4.43 0.1142 0.2829 0.0801 0.0323 0.075 2.375 1.804 56.208 0.268 8.023 14.556 0.16 90831. 0.5596
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5.32 0.1370 0.3291 0.0781 0.0325 0.076 2.388 1.757 56.495 0.270 7.817 14.109 0.16 90912. 0.5354
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6.21 0.1599 0.3720 0.0759 0.0326 0.076 2.395 1.708 56.661 0.271 7.596 13.670 0.16 90999. 0.5113
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7.09 0.1827 0.4117 0.0735 0.0326 0.076 2.396 1.655 56.688 0.271 7.360 13.240 0.16 91092. 0.4875
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7.98 0.2055 0.4484 0.0710 0.0325 0.076 2.390 1.598 56.560 0.270 7.109 12.817 0.16 91190. 0.4638
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8.87 0.2284 0.4821 0.0683 0.0324 0.075 2.378 1.539 56.263 0.269 6.843 12.403 0.16 91294. 0.4403
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9.75 0.2512 0.5129 0.0655 0.0321 0.075 2.358 1.475 55.786 0.266 6.563 11.996 0.16 91405. 0.4171
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10.64 0.2741 0.5409 0.0626 0.0317 0.074 2.330 1.409 55.124 0.263 6.268 11.595 0.16 91521. 0.3940
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11.53 0.2969 0.5660 0.0595 0.0312 0.073 2.294 1.340 54.272 0.259 5.961 11.200 0.16 91644. 0.3711
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12.41 0.3197 0.5882 0.0563 0.0306 0.071 2.249 1.268 53.226 0.254 5.642 10.809 0.16 91772. 0.3484
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13.30 0.3426 0.6076 0.0530 0.0299 0.070 2.197 1.194 51.984 0.248 5.312 10.420 0.16 91908. 0.3259
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14.19 0.3654 0.6239 0.0496 0.0291 0.068 2.136 1.118 50.540 0.241 4.972 10.031 0.16 92049. 0.3035
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15.07 0.3882 0.6371 0.0462 0.0281 0.066 2.066 1.039 48.893 0.233 4.622 9.640 0.16 92198. 0.2813
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15.96 0.4111 0.6468 0.0426 0.0271 0.063 1.988 0.959 47.039 0.225 4.264 9.244 0.16 92352. 0.2591
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16.85 0.4339 0.6528 0.0389 0.0259 0.060 1.901 0.876 44.974 0.215 3.898 8.839 0.16 92514. 0.2369
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17.73 0.4568 0.6546 0.0352 0.0246 0.057 1.804 0.793 42.697 0.204 3.525 8.420 0.16 92681. 0.2146
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18.62 0.4796 0.6514 0.0314 0.0231 0.054 1.699 0.707 40.206 0.192 3.146 7.979 0.16 92856. 0.1921
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19.51 0.5024 0.6421 0.0276 0.0216 0.050 1.585 0.621 37.499 0.179 2.761 7.508 0.16 93038. 0.1693
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20.39 0.5253 0.6252 0.0237 0.0199 0.046 1.461 0.533 34.578 0.165 2.371 6.993 0.16 93226. 0.1461
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21.28 0.5481 0.5983 0.0197 0.0181 0.042 1.329 0.445 31.444 0.150 1.978 6.413 0.17 93421. 0.1224
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22.17 0.5709 0.5576 0.0158 0.0162 0.038 1.188 0.356 28.104 0.134 1.581 5.738 0.17 93622. 0.0979
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23.05 0.5938 0.4967 0.0118 0.0141 0.033 1.038 0.266 24.564 0.117 1.184 4.914 0.17 93831. 0.0726
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23.94 0.6166 0.4040 0.0079 0.0120 0.028 0.881 0.177 20.835 0.099 0.787 3.850 0.17 94046. 0.0463
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24.83 0.6395 0.2564 0.0039 0.0097 0.023 0.716 0.088 16.931 0.081 0.391 2.356 0.17 94267. 0.0200
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25.71 0.6623 -0.0038 0.0000 0.0074 0.017 0.542 -0.001 12.829 0.061 -0.004 -0.034 0.17 94482. 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 0.0890 0.0296 0.233 4.885 4.509 173.395 0.552 20.056 11.795 0.24 135748. 0.7169
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1.33 0.0229 0.0669 0.0876 0.0300 0.236 4.951 4.436 175.724 0.559 19.730 11.449 0.24 135832. 0.6902
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2.67 0.0458 0.1298 0.0860 0.0303 0.239 5.012 4.357 177.896 0.566 19.379 11.108 0.24 135924. 0.6637
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4.00 0.0687 0.1889 0.0843 0.0307 0.241 5.067 4.272 179.863 0.573 19.001 10.773 0.24 136023. 0.6373
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5.33 0.0916 0.2441 0.0825 0.0310 0.244 5.116 4.181 181.578 0.578 18.596 10.443 0.24 136130. 0.6112
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6.67 0.1145 0.2957 0.0806 0.0312 0.245 5.156 4.083 182.991 0.582 18.160 10.120 0.24 136244. 0.5853
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8.00 0.1373 0.3438 0.0785 0.0314 0.247 5.185 3.978 184.045 0.586 17.694 9.803 0.24 136367. 0.5597
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9.33 0.1602 0.3884 0.0763 0.0315 0.248 5.203 3.866 184.681 0.588 17.195 9.494 0.24 136498. 0.5343
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10.66 0.1831 0.4298 0.0740 0.0315 0.248 5.208 3.746 184.841 0.588 16.662 9.192 0.24 136637. 0.5092
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12.00 0.2060 0.4679 0.0714 0.0314 0.247 5.197 3.618 184.466 0.587 16.094 8.897 0.24 136786. 0.4844
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13.33 0.2289 0.5031 0.0688 0.0313 0.246 5.170 3.483 183.509 0.584 15.491 8.608 0.24 136943. 0.4598
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14.66 0.2518 0.5353 0.0659 0.0310 0.244 5.126 3.340 181.933 0.579 14.856 8.326 0.24 137109. 0.4355
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16.00 0.2747 0.5646 0.0630 0.0306 0.241 5.063 3.190 179.716 0.572 14.189 8.051 0.24 137284. 0.4116
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17.33 0.2976 0.5911 0.0599 0.0301 0.237 4.982 3.033 176.842 0.563 13.492 7.780 0.25 137469. 0.3878
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18.66 0.3205 0.6148 0.0567 0.0295 0.232 4.882 2.871 173.297 0.552 12.770 7.514 0.25 137664. 0.3644
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20.00 0.3434 0.6356 0.0534 0.0288 0.227 4.763 2.703 169.067 0.538 12.022 7.251 0.25 137867. 0.3412
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21.33 0.3662 0.6536 0.0499 0.0280 0.220 4.625 2.529 164.140 0.522 11.251 6.990 0.25 138081. 0.3182
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22.66 0.3891 0.6685 0.0464 0.0270 0.213 4.466 2.351 158.504 0.505 10.459 6.729 0.25 138304. 0.2953
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24.00 0.4120 0.6803 0.0428 0.0259 0.204 4.287 2.169 152.146 0.484 9.648 6.467 0.25 138537. 0.2726
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25.33 0.4349 0.6884 0.0391 0.0247 0.195 4.087 1.983 145.056 0.462 8.819 6.200 0.25 138780. 0.2499
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26.66 0.4578 0.6926 0.0354 0.0234 0.184 3.866 1.793 137.224 0.437 7.974 5.926 0.25 139033. 0.2271
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28.00 0.4807 0.6922 0.0316 0.0219 0.173 3.624 1.600 128.645 0.409 7.115 5.640 0.25 139297. 0.2042
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29.33 0.5036 0.6860 0.0277 0.0203 0.160 3.362 1.404 119.316 0.380 6.243 5.335 0.25 139570. 0.1809
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30.66 0.5265 0.6726 0.0238 0.0186 0.146 3.078 1.205 109.240 0.348 5.360 5.004 0.25 139853. 0.1572
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31.99 0.5494 0.6494 0.0198 0.0168 0.132 2.773 1.005 98.424 0.313 4.469 4.630 0.25 140147. 0.1328
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33.33 0.5723 0.6125 0.0159 0.0148 0.117 2.448 0.803 86.887 0.277 3.572 4.192 0.25 140451. 0.1075
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34.66 0.5951 0.5547 0.0119 0.0127 0.100 2.103 0.601 74.655 0.238 2.673 3.651 0.25 140765. 0.0810
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35.99 0.6180 0.4622 0.0079 0.0105 0.083 1.740 0.399 61.768 0.197 1.774 2.929 0.25 141089. 0.0529
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37.33 0.6409 0.3042 0.0039 0.0082 0.065 1.360 0.198 48.271 0.154 0.880 1.859 0.25 141421. 0.0237
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38.66 0.6638 -0.0088 -0.0001 0.0058 0.046 0.959 -0.004 34.025 0.108 -0.017 -0.052 0.25 141737. 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 0.0897 0.0290 0.541 8.526 8.073 403.488 0.963 35.910 9.075 0.33 180988. 0.7381
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1.78 0.0229 0.0687 0.0882 0.0294 0.549 8.646 7.943 409.171 0.977 35.331 8.805 0.33 181102. 0.7103
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3.56 0.0459 0.1333 0.0866 0.0298 0.556 8.758 7.803 414.475 0.989 34.706 8.539 0.33 181225. 0.6827
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5.34 0.0688 0.1938 0.0850 0.0302 0.562 8.860 7.651 419.289 1.001 34.033 8.277 0.33 181358. 0.6553
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7.12 0.0917 0.2504 0.0832 0.0305 0.568 8.949 7.489 423.496 1.011 33.309 8.020 0.33 181500. 0.6282
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8.90 0.1146 0.3032 0.0812 0.0307 0.573 9.022 7.314 426.974 1.019 32.532 7.769 0.33 181654. 0.6014
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10.68 0.1376 0.3523 0.0791 0.0309 0.576 9.077 7.127 429.587 1.026 31.699 7.524 0.33 181818. 0.5749
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12.46 0.1605 0.3980 0.0769 0.0310 0.578 9.111 6.926 431.195 1.029 30.807 7.285 0.33 181993. 0.5488
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14.24 0.1834 0.4403 0.0745 0.0310 0.579 9.121 6.712 431.651 1.030 29.854 7.053 0.33 182180. 0.5230
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16.02 0.2063 0.4794 0.0720 0.0310 0.578 9.103 6.483 430.819 1.029 28.838 6.826 0.33 182379. 0.4975
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17.80 0.2293 0.5155 0.0693 0.0308 0.575 9.056 6.241 428.579 1.023 27.759 6.605 0.33 182589. 0.4723
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19.58 0.2522 0.5485 0.0665 0.0306 0.570 8.977 5.985 424.843 1.014 26.621 6.390 0.33 182812. 0.4474
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21.36 0.2751 0.5787 0.0635 0.0302 0.563 8.866 5.716 419.558 1.002 25.426 6.180 0.33 183047. 0.4229
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23.14 0.2980 0.6061 0.0604 0.0297 0.553 8.720 5.436 412.681 0.985 24.178 5.974 0.33 183294. 0.3987
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24.92 0.3210 0.6308 0.0571 0.0291 0.542 8.541 5.144 404.177 0.965 22.882 5.773 0.33 183554. 0.3748
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26.70 0.3439 0.6527 0.0538 0.0283 0.528 8.326 4.843 394.014 0.941 21.542 5.575 0.33 183827. 0.3512
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28.48 0.3668 0.6717 0.0503 0.0275 0.512 8.075 4.532 382.162 0.912 20.160 5.379 0.33 184113. 0.3278
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30.26 0.3897 0.6879 0.0468 0.0265 0.494 7.789 4.213 368.590 0.880 18.741 5.185 0.33 184412. 0.3046
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32.04 0.4127 0.7010 0.0432 0.0254 0.474 7.465 3.886 353.267 0.843 17.286 4.990 0.33 184724. 0.2815
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33.82 0.4356 0.7107 0.0394 0.0242 0.451 7.103 3.552 336.168 0.803 15.800 4.793 0.33 185049. 0.2585
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35.60 0.4585 0.7166 0.0357 0.0228 0.425 6.704 3.211 317.270 0.757 14.284 4.591 0.33 185387. 0.2355
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37.39 0.4814 0.7181 0.0318 0.0213 0.398 6.266 2.865 296.559 0.708 12.743 4.382 0.33 185740. 0.2123
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39.17 0.5044 0.7143 0.0279 0.0197 0.367 5.790 2.513 274.027 0.654 11.179 4.160 0.33 186105. 0.1888
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40.95 0.5273 0.7035 0.0240 0.0180 0.335 5.276 2.157 249.683 0.596 9.596 3.919 0.33 186484. 0.1648
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42.73 0.5502 0.6834 0.0200 0.0161 0.300 4.724 1.798 223.546 0.534 7.998 3.648 0.33 186877. 0.1400
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44.51 0.5732 0.6498 0.0160 0.0141 0.262 4.134 1.437 195.659 0.467 6.390 3.330 0.33 187284. 0.1143
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46.29 0.5961 0.5952 0.0119 0.0119 0.223 3.510 1.074 166.090 0.397 4.778 2.933 0.33 187704. 0.0870
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48.07 0.6190 0.5043 0.0079 0.0097 0.181 2.851 0.712 134.935 0.322 3.167 2.393 0.33 188137. 0.0578
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49.85 0.6419 0.3408 0.0039 0.0074 0.137 2.162 0.352 102.303 0.244 1.564 1.559 0.33 188581. 0.0265
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51.63 0.6649 -0.0177 -0.0001 0.0049 0.091 1.430 -0.012 67.673 0.162 -0.052 -0.078 0.33 188988. 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 0.0905 0.0288 1.050 13.240 12.729 783.231 1.496 56.619 7.371 0.41 226221. 0.7528
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2.23 0.0229 0.0698 0.0890 0.0293 1.066 13.432 12.526 794.609 1.518 55.715 7.150 0.41 226364. 0.7243
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4.45 0.0459 0.1353 0.0875 0.0297 1.080 13.612 12.306 805.235 1.538 54.737 6.932 0.41 226518. 0.6960
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6.68 0.0688 0.1967 0.0858 0.0300 1.093 13.775 12.069 814.881 1.556 53.684 6.718 0.41 226685. 0.6680
|
|
8.91 0.0918 0.2541 0.0840 0.0303 1.104 13.918 11.814 823.321 1.572 52.550 6.509 0.41 226864. 0.6403
|
|
11.13 0.1147 0.3077 0.0820 0.0306 1.113 14.036 11.540 830.306 1.586 51.332 6.304 0.41 227056. 0.6130
|
|
13.36 0.1376 0.3576 0.0799 0.0308 1.121 14.125 11.246 835.573 1.596 50.024 6.105 0.41 227262. 0.5860
|
|
15.59 0.1606 0.4039 0.0777 0.0309 1.125 14.180 10.931 838.839 1.602 48.623 5.911 0.41 227483. 0.5594
|
|
17.81 0.1835 0.4468 0.0753 0.0309 1.126 14.197 10.595 839.817 1.604 47.125 5.722 0.41 227717. 0.5331
|
|
20.04 0.2065 0.4866 0.0727 0.0309 1.124 14.170 10.235 838.231 1.601 45.527 5.538 0.41 227966. 0.5072
|
|
22.27 0.2294 0.5232 0.0700 0.0307 1.118 14.096 9.854 833.842 1.593 43.829 5.360 0.41 228230. 0.4816
|
|
24.49 0.2523 0.5569 0.0672 0.0304 1.108 13.971 9.451 826.478 1.578 42.036 5.186 0.41 228510. 0.4564
|
|
26.72 0.2753 0.5878 0.0642 0.0300 1.094 13.794 9.027 816.025 1.558 40.153 5.018 0.41 228804. 0.4315
|
|
28.95 0.2982 0.6158 0.0610 0.0295 1.076 13.564 8.585 802.399 1.532 38.187 4.853 0.41 229114. 0.4070
|
|
31.17 0.3212 0.6412 0.0578 0.0289 1.053 13.279 8.126 785.535 1.500 36.144 4.692 0.41 229440. 0.3828
|
|
33.40 0.3441 0.6639 0.0544 0.0282 1.026 12.938 7.651 765.366 1.462 34.030 4.534 0.41 229783. 0.3589
|
|
35.63 0.3670 0.6838 0.0509 0.0273 0.995 12.540 7.161 741.832 1.417 31.850 4.378 0.41 230141. 0.3353
|
|
37.85 0.3900 0.7009 0.0473 0.0263 0.959 12.085 6.657 714.870 1.365 29.610 4.224 0.41 230515. 0.3119
|
|
40.08 0.4129 0.7151 0.0436 0.0252 0.918 11.570 6.141 684.425 1.307 27.315 4.070 0.41 230906. 0.2887
|
|
42.31 0.4359 0.7260 0.0399 0.0240 0.872 10.995 5.614 650.441 1.242 24.969 3.915 0.41 231313. 0.2655
|
|
44.53 0.4588 0.7334 0.0361 0.0226 0.822 10.360 5.076 612.877 1.171 22.578 3.757 0.41 231738. 0.2422
|
|
46.76 0.4817 0.7366 0.0322 0.0211 0.767 9.664 4.529 571.700 1.092 20.145 3.593 0.41 232179. 0.2189
|
|
48.99 0.5047 0.7346 0.0282 0.0194 0.707 8.907 3.974 526.900 1.006 17.676 3.421 0.41 232636. 0.1952
|
|
51.21 0.5276 0.7261 0.0242 0.0176 0.642 8.089 3.412 478.487 0.914 15.176 3.234 0.41 233111. 0.1710
|
|
53.44 0.5506 0.7087 0.0202 0.0157 0.572 7.210 2.845 426.506 0.815 12.653 3.025 0.41 233603. 0.1460
|
|
55.67 0.5735 0.6783 0.0162 0.0137 0.498 6.272 2.274 371.041 0.709 10.114 2.779 0.41 234112. 0.1200
|
|
57.89 0.5964 0.6272 0.0121 0.0115 0.419 5.278 1.701 312.226 0.596 7.567 2.471 0.41 234637. 0.0923
|
|
60.12 0.6194 0.5394 0.0080 0.0092 0.336 4.230 1.129 250.254 0.478 5.023 2.047 0.41 235180. 0.0623
|
|
62.35 0.6423 0.3747 0.0040 0.0068 0.249 3.133 0.560 185.347 0.354 2.492 1.371 0.41 235736. 0.0294
|
|
64.57 0.6653 -0.0169 -0.0001 0.0043 0.156 1.965 -0.015 116.265 0.222 -0.068 -0.060 0.42 236234. 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 0.0915 0.0289 1.820 19.115 18.537 1356.949 2.160 82.453 6.196 0.49 271444. 0.7636
|
|
2.69 0.0231 0.0708 0.0900 0.0293 1.847 19.401 18.243 1377.226 2.192 81.145 6.008 0.49 271616. 0.7345
|
|
5.38 0.0462 0.1372 0.0885 0.0298 1.872 19.668 17.924 1396.145 2.222 79.728 5.823 0.49 271804. 0.7057
|
|
8.06 0.0692 0.1995 0.0868 0.0301 1.895 19.909 17.581 1413.306 2.249 78.199 5.642 0.49 272006. 0.6771
|
|
10.75 0.0923 0.2576 0.0849 0.0304 1.915 20.120 17.210 1428.294 2.273 76.550 5.465 0.49 272224. 0.6489
|
|
13.44 0.1154 0.3118 0.0830 0.0307 1.932 20.295 16.811 1440.669 2.293 74.775 5.293 0.49 272457. 0.6211
|
|
16.13 0.1385 0.3623 0.0809 0.0309 1.944 20.426 16.382 1449.957 2.308 72.868 5.125 0.49 272708. 0.5937
|
|
18.82 0.1615 0.4092 0.0786 0.0310 1.952 20.506 15.922 1455.653 2.317 70.822 4.961 0.49 272975. 0.5666
|
|
21.50 0.1846 0.4527 0.0762 0.0311 1.954 20.528 15.430 1457.245 2.319 68.631 4.802 0.49 273260. 0.5400
|
|
24.19 0.2077 0.4930 0.0736 0.0310 1.950 20.486 14.904 1454.237 2.314 66.292 4.648 0.49 273563. 0.5136
|
|
26.88 0.2308 0.5301 0.0708 0.0308 1.939 20.373 14.345 1446.208 2.302 63.805 4.499 0.49 273884. 0.4877
|
|
29.57 0.2538 0.5643 0.0679 0.0305 1.921 20.185 13.754 1432.849 2.280 61.176 4.354 0.49 274223. 0.4621
|
|
32.25 0.2769 0.5957 0.0648 0.0301 1.896 19.919 13.133 1413.961 2.250 58.413 4.213 0.49 274581. 0.4370
|
|
34.94 0.3000 0.6243 0.0616 0.0296 1.863 19.573 12.484 1389.401 2.211 55.528 4.075 0.49 274958. 0.4121
|
|
37.63 0.3231 0.6502 0.0583 0.0290 1.823 19.145 11.809 1359.050 2.163 52.528 3.941 0.49 275354. 0.3877
|
|
40.32 0.3461 0.6734 0.0548 0.0282 1.774 18.634 11.111 1322.798 2.105 49.424 3.810 0.49 275770. 0.3635
|
|
43.01 0.3692 0.6940 0.0513 0.0273 1.717 18.039 10.392 1280.534 2.038 46.222 3.681 0.49 276205. 0.3396
|
|
45.69 0.3923 0.7117 0.0476 0.0263 1.652 17.357 9.652 1232.154 1.961 42.932 3.553 0.49 276659. 0.3159
|
|
48.38 0.4154 0.7266 0.0439 0.0251 1.579 16.588 8.894 1177.554 1.874 39.560 3.426 0.49 277134. 0.2924
|
|
51.07 0.4385 0.7384 0.0401 0.0238 1.497 15.730 8.119 1116.645 1.777 36.114 3.298 0.49 277629. 0.2690
|
|
53.76 0.4615 0.7466 0.0362 0.0224 1.407 14.782 7.329 1049.347 1.670 32.599 3.168 0.49 278144. 0.2455
|
|
56.45 0.4846 0.7507 0.0322 0.0208 1.308 13.744 6.525 975.613 1.553 29.024 3.034 0.49 278679. 0.2218
|
|
59.13 0.5077 0.7498 0.0282 0.0191 1.201 12.614 5.710 895.424 1.425 25.396 2.892 0.49 279235. 0.1978
|
|
61.82 0.5308 0.7423 0.0241 0.0172 1.085 11.394 4.884 808.806 1.287 21.724 2.739 0.49 279811. 0.1732
|
|
64.51 0.5538 0.7258 0.0200 0.0153 0.960 10.084 4.051 715.845 1.139 18.017 2.567 0.50 280408. 0.1478
|
|
67.20 0.5769 0.6959 0.0159 0.0131 0.827 8.688 3.212 616.704 0.982 14.287 2.362 0.50 281026. 0.1212
|
|
69.88 0.6000 0.6441 0.0117 0.0109 0.686 7.207 2.371 511.639 0.814 10.548 2.102 0.50 281664. 0.0927
|
|
72.57 0.6231 0.5513 0.0076 0.0085 0.538 5.649 1.532 401.009 0.638 6.815 1.733 0.50 282321. 0.0614
|
|
75.26 0.6461 0.3659 0.0034 0.0061 0.382 4.018 0.697 285.199 0.454 3.102 1.109 0.50 282995. 0.0265
|
|
77.95 0.6692
|
|
|
|
|
|
|
|
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 0.0928 0.0292 2.918 26.278 25.579 2176.320 2.969 113.777 5.331 0.57 316652. 0.7717
|
|
3.12 0.0230 0.0707 0.0913 0.0296 2.963 26.677 25.182 2209.302 3.014 112.012 5.170 0.57 316854. 0.7426
|
|
6.24 0.0459 0.1371 0.0898 0.0301 3.004 27.048 24.752 2240.075 3.056 110.097 5.012 0.57 317072. 0.7137
|
|
9.36 0.0689 0.1993 0.0881 0.0304 3.041 27.385 24.287 2267.985 3.094 108.026 4.857 0.57 317308. 0.6851
|
|
12.48 0.0919 0.2575 0.0862 0.0308 3.074 27.680 23.784 2292.381 3.127 105.791 4.706 0.57 317562. 0.6569
|
|
15.60 0.1148 0.3118 0.0843 0.0310 3.101 27.923 23.242 2312.554 3.155 103.382 4.559 0.57 317834. 0.6290
|
|
18.72 0.1378 0.3624 0.0822 0.0312 3.122 28.107 22.660 2327.750 3.175 100.790 4.415 0.57 318126. 0.6016
|
|
21.84 0.1608 0.4095 0.0799 0.0314 3.134 28.220 22.034 2337.169 3.188 98.006 4.276 0.57 318437. 0.5745
|
|
24.97 0.1837 0.4532 0.0775 0.0314 3.138 28.254 21.363 2339.988 3.192 95.023 4.141 0.57 318769. 0.5478
|
|
28.09 0.2067 0.4937 0.0749 0.0313 3.132 28.199 20.646 2335.418 3.186 91.834 4.010 0.57 319121. 0.5215
|
|
31.21 0.2296 0.5312 0.0721 0.0312 3.115 28.047 19.883 2322.767 3.169 88.441 3.883 0.57 319494. 0.4955
|
|
34.33 0.2526 0.5658 0.0692 0.0309 3.086 27.790 19.076 2301.537 3.140 84.850 3.759 0.57 319889. 0.4700
|
|
37.45 0.2756 0.5975 0.0661 0.0305 3.046 27.426 18.227 2271.402 3.099 81.074 3.640 0.57 320305. 0.4448
|
|
40.57 0.2985 0.6266 0.0629 0.0300 2.993 26.952 17.339 2232.132 3.045 77.126 3.523 0.57 320742. 0.4199
|
|
43.69 0.3215 0.6531 0.0595 0.0293 2.928 26.366 16.416 2183.552 2.979 73.019 3.410 0.57 321202. 0.3955
|
|
46.81 0.3445 0.6770 0.0561 0.0285 2.850 25.664 15.460 2125.485 2.900 68.766 3.299 0.57 321685. 0.3713
|
|
49.93 0.3674 0.6983 0.0525 0.0276 2.760 24.847 14.473 2057.769 2.807 64.378 3.190 0.57 322189. 0.3474
|
|
53.05 0.3904 0.7170 0.0488 0.0266 2.656 23.911 13.459 1980.238 2.701 59.866 3.083 0.57 322717. 0.3237
|
|
56.17 0.4134 0.7329 0.0450 0.0254 2.538 22.854 12.419 1892.731 2.582 55.240 2.976 0.57 323267. 0.3002
|
|
59.29 0.4363 0.7458 0.0412 0.0241 2.407 21.675 11.356 1795.105 2.449 50.510 2.869 0.57 323840. 0.2767
|
|
62.41 0.4593 0.7555 0.0372 0.0226 2.263 20.373 10.271 1687.240 2.302 45.684 2.761 0.58 324437. 0.2533
|
|
65.53 0.4823 0.7613 0.0332 0.0211 2.104 18.946 9.167 1569.052 2.140 40.774 2.650 0.58 325057. 0.2296
|
|
68.66 0.5052 0.7625 0.0292 0.0193 1.932 17.394 8.046 1440.504 1.965 35.788 2.533 0.58 325701. 0.2057
|
|
71.78 0.5282 0.7577 0.0251 0.0175 1.746 15.717 6.911 1301.630 1.776 30.739 2.408 0.58 326368. 0.1812
|
|
74.90 0.5512 0.7448 0.0209 0.0155 1.546 13.917 5.764 1152.554 1.572 25.639 2.268 0.58 327059. 0.1559
|
|
78.02 0.5741 0.7198 0.0167 0.0133 1.332 11.996 4.610 993.519 1.355 20.504 2.105 0.58 327774. 0.1293
|
|
81.14 0.5971 0.6751 0.0125 0.0111 1.106 9.961 3.452 824.914 1.125 15.353 1.898 0.58 328512. 0.1009
|
|
84.26 0.6201 0.5939 0.0083 0.0087 0.868 7.816 2.294 647.294 0.883 10.205 1.608 0.58 329273. 0.0697
|
|
87.38 0.6430 0.4304 0.0041 0.0062 0.619 5.570 1.143 461.306 0.629 5.083 1.124 0.58 330053. 0.0344
|
|
90.50 0.6660 -0.0207 -0.0001 0.0035 0.351 3.164 -0.030 262.053 0.357 -0.134 -0.052 0.58 330714. 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 0.0943 0.0297 4.431 34.912 33.968 3304.409 3.944 151.089 4.663 0.65 361841. 0.7778
|
|
3.57 0.0230 0.0708 0.0929 0.0302 4.500 35.451 33.453 3355.407 4.005 148.797 4.522 0.65 362073. 0.7486
|
|
7.14 0.0460 0.1373 0.0913 0.0306 4.563 35.953 32.892 3402.971 4.062 146.304 4.384 0.65 362325. 0.7197
|
|
10.71 0.0690 0.1996 0.0896 0.0310 4.621 36.409 32.284 3446.074 4.113 143.599 4.249 0.65 362596. 0.6911
|
|
14.28 0.0920 0.2578 0.0878 0.0313 4.672 36.806 31.626 3483.693 4.158 140.672 4.118 0.65 362889. 0.6628
|
|
17.85 0.1150 0.3123 0.0858 0.0316 4.713 37.134 30.915 3514.732 4.195 137.510 3.990 0.65 363203. 0.6349
|
|
21.43 0.1380 0.3630 0.0837 0.0318 4.745 37.380 30.148 3538.037 4.223 134.100 3.865 0.65 363539. 0.6074
|
|
25.00 0.1610 0.4103 0.0814 0.0319 4.764 37.532 29.323 3552.380 4.240 130.431 3.744 0.65 363897. 0.5803
|
|
28.57 0.1839 0.4542 0.0789 0.0320 4.769 37.576 28.438 3556.508 4.245 126.492 3.627 0.65 364279. 0.5536
|
|
32.14 0.2069 0.4950 0.0763 0.0319 4.760 37.498 27.490 3549.204 4.237 122.275 3.513 0.65 364685. 0.5272
|
|
35.71 0.2299 0.5327 0.0735 0.0317 4.733 37.289 26.480 3529.411 4.213 117.782 3.403 0.65 365115. 0.5012
|
|
39.28 0.2529 0.5676 0.0705 0.0314 4.689 36.940 25.409 3496.357 4.173 113.020 3.296 0.65 365569. 0.4756
|
|
42.85 0.2759 0.5998 0.0674 0.0310 4.626 36.446 24.282 3449.551 4.118 108.007 3.193 0.65 366047. 0.4503
|
|
46.42 0.2989 0.6293 0.0641 0.0305 4.544 35.802 23.103 3388.659 4.045 102.760 3.092 0.65 366551. 0.4254
|
|
49.99 0.3219 0.6563 0.0607 0.0298 4.443 35.007 21.875 3313.425 3.955 97.299 2.994 0.65 367080. 0.4009
|
|
53.56 0.3449 0.6807 0.0572 0.0290 4.323 34.058 20.603 3223.604 3.848 91.640 2.899 0.65 367634. 0.3766
|
|
57.13 0.3679 0.7026 0.0536 0.0280 4.183 32.953 19.289 3118.963 3.723 85.799 2.805 0.65 368214. 0.3526
|
|
60.70 0.3909 0.7219 0.0498 0.0270 4.022 31.688 17.938 2999.255 3.580 79.790 2.713 0.66 368820. 0.3289
|
|
64.28 0.4139 0.7386 0.0460 0.0257 3.841 30.262 16.553 2864.251 3.419 73.626 2.621 0.66 369452. 0.3052
|
|
67.85 0.4369 0.7524 0.0420 0.0244 3.639 28.671 15.135 2713.739 3.239 67.321 2.530 0.66 370110. 0.2817
|
|
71.42 0.4599 0.7630 0.0380 0.0229 3.416 26.916 13.689 2547.542 3.041 60.887 2.437 0.66 370795. 0.2581
|
|
74.99 0.4829 0.7700 0.0339 0.0213 3.172 24.993 12.216 2365.536 2.824 54.336 2.342 0.66 371506. 0.2343
|
|
78.56 0.5058 0.7725 0.0298 0.0195 2.907 22.902 10.720 2167.667 2.587 47.684 2.243 0.66 372245. 0.2102
|
|
82.13 0.5288 0.7693 0.0256 0.0176 2.620 20.645 9.205 1953.991 2.332 40.945 2.137 0.66 373010. 0.1856
|
|
85.70 0.5518 0.7583 0.0213 0.0155 2.313 18.222 7.674 1724.698 2.059 34.136 2.018 0.66 373802. 0.1600
|
|
89.27 0.5748 0.7355 0.0170 0.0133 1.985 15.638 6.133 1480.163 1.767 27.278 1.879 0.66 374622. 0.1332
|
|
92.84 0.5978 0.6933 0.0127 0.0110 1.637 12.900 4.585 1220.989 1.457 20.396 1.703 0.66 375468. 0.1044
|
|
96.41 0.6208 0.6146 0.0084 0.0085 1.271 10.016 3.039 948.039 1.132 13.518 1.454 0.66 376340. 0.0725
|
|
99.98 0.6438 0.4502 0.0042 0.0060 0.888 6.998 1.500 662.322 0.791 6.671 1.027 0.66 377234. 0.0360
|
|
103.56 0.6668 -0.0940 -0.0004 0.0030 0.453 3.569 -0.154 337.819 0.403 -0.686 -0.207 0.67 377187. 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 0.0962 0.0307 6.525 45.695 43.851 4865.658 5.163 195.050 4.088 0.73 407006. 0.7748
|
|
4.04 0.0231 0.0704 0.0948 0.0312 6.617 46.343 43.204 4934.651 5.236 192.173 3.971 0.73 407270. 0.7471
|
|
8.09 0.0463 0.1367 0.0932 0.0316 6.704 46.947 42.497 4998.952 5.304 189.027 3.856 0.73 407557. 0.7195
|
|
12.13 0.0694 0.1990 0.0915 0.0319 6.782 47.493 41.726 5057.123 5.366 185.599 3.742 0.73 407867. 0.6919
|
|
16.17 0.0926 0.2574 0.0897 0.0322 6.850 47.968 40.889 5107.696 5.419 181.873 3.631 0.73 408201. 0.6646
|
|
20.21 0.1157 0.3121 0.0877 0.0325 6.905 48.357 39.980 5149.062 5.463 177.832 3.522 0.73 408560. 0.6374
|
|
24.26 0.1388 0.3632 0.0855 0.0327 6.946 48.642 38.997 5179.477 5.496 173.459 3.415 0.73 408944. 0.6104
|
|
28.30 0.1620 0.4108 0.0832 0.0328 6.969 48.808 37.936 5197.089 5.514 168.739 3.311 0.73 409354. 0.5837
|
|
32.34 0.1851 0.4550 0.0807 0.0328 6.973 48.835 36.793 5199.955 5.517 163.656 3.209 0.73 409791. 0.5572
|
|
36.38 0.2083 0.4962 0.0780 0.0327 6.955 48.706 35.567 5186.206 5.503 158.203 3.111 0.73 410255. 0.5310
|
|
40.43 0.2314 0.5343 0.0751 0.0325 6.912 48.405 34.257 5154.164 5.469 152.377 3.015 0.73 410746. 0.5050
|
|
44.47 0.2545 0.5696 0.0721 0.0322 6.843 47.920 32.867 5102.586 5.414 146.193 2.922 0.73 411266. 0.4794
|
|
48.51 0.2777 0.6021 0.0689 0.0318 6.746 47.245 31.401 5030.655 5.338 139.673 2.831 0.73 411813. 0.4541
|
|
52.56 0.3008 0.6321 0.0655 0.0312 6.622 46.373 29.865 4937.793 5.239 132.841 2.743 0.74 412388. 0.4291
|
|
56.60 0.3239 0.6595 0.0620 0.0305 6.469 45.300 28.265 4823.577 5.118 125.724 2.658 0.74 412993. 0.4044
|
|
60.64 0.3471 0.6844 0.0584 0.0296 6.286 44.023 26.606 4687.630 4.974 118.344 2.574 0.74 413626. 0.3801
|
|
64.68 0.3702 0.7068 0.0546 0.0286 6.074 42.539 24.892 4529.612 4.806 110.721 2.493 0.74 414288. 0.3560
|
|
68.73 0.3934 0.7267 0.0507 0.0275 5.832 40.845 23.129 4349.201 4.615 102.876 2.412 0.74 414980. 0.3320
|
|
72.77 0.4165 0.7440 0.0468 0.0262 5.560 38.937 21.319 4146.061 4.399 94.826 2.332 0.74 415701. 0.3082
|
|
76.81 0.4396 0.7585 0.0427 0.0247 5.257 36.813 19.467 3919.888 4.159 86.587 2.252 0.74 416452. 0.2845
|
|
80.86 0.4628 0.7699 0.0386 0.0232 4.922 34.471 17.576 3670.455 3.894 78.177 2.172 0.74 417234. 0.2606
|
|
84.90 0.4859 0.7776 0.0343 0.0215 4.556 31.908 15.650 3397.635 3.605 69.612 2.089 0.74 418045. 0.2366
|
|
88.94 0.5091 0.7809 0.0300 0.0196 4.159 29.127 13.694 3101.440 3.291 60.911 2.003 0.74 418887. 0.2121
|
|
92.98 0.5322 0.7784 0.0257 0.0176 3.731 26.127 11.712 2782.065 2.952 52.095 1.909 0.74 419759. 0.1870
|
|
97.03 0.5553 0.7677 0.0213 0.0154 3.272 22.915 9.709 2439.974 2.589 43.186 1.805 0.74 420662. 0.1610
|
|
101.07 0.5785 0.7446 0.0169 0.0131 2.784 19.496 7.692 2075.992 2.203 34.212 1.680 0.74 421595. 0.1334
|
|
105.11 0.6016 0.7003 0.0124 0.0107 2.268 15.885 5.667 1691.402 1.795 25.206 1.520 0.75 422559. 0.1035
|
|
109.15 0.6248 0.6139 0.0080 0.0081 1.727 12.096 3.643 1287.997 1.367 16.205 1.283 0.75 423552. 0.0701
|
|
113.20 0.6479 0.4225 0.0036 0.0055 1.164 8.150 1.629 867.774 0.921 7.245 0.851 0.75 424567. 0.0311
|
|
117.24 0.6710
|
|
|
|
|
|
|
|
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 0.0984 0.0340 9.901 62.403 55.397 7383.069 7.050 246.408 3.403 0.81 452135. 0.7250
|
|
4.48 0.0231 0.0654 0.0971 0.0343 9.984 62.929 54.626 7445.230 7.110 242.977 3.328 0.81 452430. 0.7040
|
|
8.96 0.0462 0.1278 0.0955 0.0345 10.057 63.387 53.776 7499.400 7.161 239.197 3.252 0.81 452750. 0.6827
|
|
13.45 0.0693 0.1873 0.0939 0.0347 10.117 63.764 52.844 7544.062 7.204 235.050 3.177 0.81 453096. 0.6611
|
|
17.93 0.0924 0.2438 0.0921 0.0349 10.162 64.049 51.825 7577.727 7.236 230.516 3.102 0.81 453469. 0.6392
|
|
22.41 0.1154 0.2974 0.0901 0.0350 10.190 64.226 50.713 7598.668 7.256 225.572 3.027 0.81 453870. 0.6170
|
|
26.89 0.1385 0.3481 0.0880 0.0350 10.198 64.279 49.505 7605.008 7.262 220.198 2.953 0.81 454300. 0.5946
|
|
31.37 0.1616 0.3959 0.0856 0.0350 10.185 64.192 48.195 7594.647 7.252 214.372 2.878 0.81 454758. 0.5719
|
|
35.86 0.1847 0.4409 0.0831 0.0348 10.145 63.944 46.780 7565.280 7.224 208.076 2.805 0.81 455247. 0.5491
|
|
40.34 0.2078 0.4831 0.0804 0.0346 10.077 63.515 45.255 7514.627 7.176 201.296 2.732 0.81 455765. 0.5260
|
|
44.82 0.2309 0.5225 0.0775 0.0342 9.978 62.890 43.622 7440.630 7.105 194.030 2.659 0.82 456314. 0.5027
|
|
49.30 0.2540 0.5593 0.0744 0.0338 9.845 62.055 41.883 7341.786 7.011 186.294 2.587 0.82 456893. 0.4793
|
|
53.79 0.2771 0.5934 0.0711 0.0332 9.678 61.001 40.044 7217.101 6.892 178.115 2.517 0.82 457504. 0.4558
|
|
58.27 0.3001 0.6250 0.0677 0.0325 9.476 59.723 38.113 7065.891 6.747 169.528 2.447 0.82 458146. 0.4323
|
|
62.75 0.3232 0.6540 0.0641 0.0317 9.236 58.215 36.098 6887.532 6.577 160.566 2.377 0.82 458820. 0.4088
|
|
67.23 0.3463 0.6804 0.0604 0.0308 8.960 56.473 34.006 6681.378 6.380 151.259 2.309 0.82 459525. 0.3853
|
|
71.71 0.3694 0.7043 0.0566 0.0297 8.645 54.489 31.842 6446.713 6.156 141.635 2.240 0.82 460263. 0.3618
|
|
76.20 0.3925 0.7257 0.0526 0.0285 8.291 52.259 29.613 6182.830 5.904 131.720 2.172 0.82 461032. 0.3384
|
|
80.68 0.4156 0.7442 0.0485 0.0271 7.899 49.784 27.324 5890.026 5.625 121.537 2.104 0.82 461835. 0.3148
|
|
85.16 0.4387 0.7597 0.0444 0.0256 7.466 47.058 24.979 5567.476 5.317 111.106 2.035 0.82 462670. 0.2911
|
|
89.64 0.4618 0.7719 0.0401 0.0240 6.993 44.076 22.583 5214.665 4.980 100.448 1.964 0.82 463538. 0.2672
|
|
94.12 0.4849 0.7801 0.0358 0.0222 6.480 40.842 20.140 4832.100 4.614 89.584 1.890 0.82 464439. 0.2428
|
|
98.61 0.5079 0.7834 0.0314 0.0203 5.926 37.352 17.657 4419.238 4.220 78.539 1.812 0.82 465373. 0.2180
|
|
103.09 0.5310 0.7802 0.0269 0.0183 5.334 33.618 15.138 3977.347 3.798 67.336 1.726 0.82 466341. 0.1923
|
|
107.57 0.5541 0.7677 0.0224 0.0161 4.705 29.652 12.591 3508.197 3.350 56.004 1.628 0.83 467342. 0.1653
|
|
112.05 0.5772 0.7408 0.0178 0.0139 4.042 25.476 10.022 3014.102 2.878 44.577 1.508 0.83 468377. 0.1367
|
|
116.54 0.6003 0.6901 0.0132 0.0115 3.350 21.115 7.440 2498.187 2.386 33.094 1.351 0.83 469445. 0.1055
|
|
121.02 0.6234 0.5950 0.0086 0.0090 2.634 16.603 4.857 1964.346 1.876 21.603 1.121 0.83 470545. 0.0707
|
|
125.50 0.6465 0.4019 0.0041 0.0065 1.900 11.975 2.282 1416.821 1.353 10.150 0.730 0.83 471671. 0.0316
|
|
129.98 0.6696
|
|
|
|
|
|
|
|
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 0.1003 0.0414 16.071 92.083 68.281 11983.891 10.403 303.714 2.584 0.89 497254. 0.6112
|
|
4.93 0.0231 0.0550 0.0990 0.0416 16.125 92.395 67.443 12024.598 10.439 299.988 2.544 0.89 497574. 0.5980
|
|
9.85 0.0461 0.1082 0.0977 0.0417 16.153 92.554 66.506 12045.272 10.457 295.820 2.504 0.89 497924. 0.5846
|
|
14.78 0.0692 0.1598 0.0961 0.0416 16.150 92.540 65.463 12043.428 10.455 291.177 2.465 0.89 498303. 0.5709
|
|
19.71 0.0923 0.2097 0.0944 0.0416 16.115 92.337 64.305 12017.026 10.432 286.027 2.427 0.89 498713. 0.5571
|
|
24.64 0.1154 0.2581 0.0925 0.0414 16.044 91.932 63.025 11964.342 10.386 280.337 2.389 0.90 499154. 0.5429
|
|
29.56 0.1384 0.3048 0.0905 0.0411 15.936 91.313 61.618 11883.766 10.317 274.076 2.352 0.90 499628. 0.5284
|
|
34.49 0.1615 0.3500 0.0882 0.0407 15.789 90.468 60.076 11773.790 10.221 267.217 2.314 0.90 500135. 0.5134
|
|
39.42 0.1846 0.3935 0.0857 0.0402 15.600 89.386 58.394 11632.984 10.099 259.734 2.277 0.90 500675. 0.4980
|
|
44.35 0.2077 0.4353 0.0831 0.0396 15.368 88.058 56.567 11460.112 9.949 251.611 2.239 0.90 501250. 0.4820
|
|
49.27 0.2307 0.4753 0.0802 0.0389 15.092 86.476 54.596 11254.250 9.770 242.843 2.200 0.90 501858. 0.4654
|
|
54.20 0.2538 0.5135 0.0771 0.0381 14.771 84.638 52.484 11015.063 9.562 233.451 2.161 0.90 502500. 0.4481
|
|
59.13 0.2769 0.5499 0.0738 0.0372 14.406 82.546 50.241 10742.798 9.326 223.470 2.121 0.90 503177. 0.4303
|
|
64.06 0.3000 0.5842 0.0703 0.0361 13.998 80.204 47.874 10437.970 9.061 212.946 2.080 0.90 503889. 0.4120
|
|
68.98 0.3230 0.6165 0.0667 0.0349 13.546 77.614 45.396 10100.916 8.769 201.921 2.038 0.90 504635. 0.3931
|
|
73.91 0.3461 0.6466 0.0629 0.0337 13.050 74.776 42.814 9731.601 8.448 190.438 1.995 0.90 505416. 0.3737
|
|
78.84 0.3692 0.6744 0.0589 0.0323 12.511 71.686 40.137 9329.443 8.099 178.531 1.951 0.90 506232. 0.3539
|
|
83.77 0.3923 0.6999 0.0549 0.0308 11.927 68.340 37.373 8893.906 7.721 166.233 1.906 0.90 507083. 0.3335
|
|
88.69 0.4153 0.7228 0.0507 0.0291 11.297 64.732 34.528 8424.447 7.313 153.579 1.859 0.90 507970. 0.3127
|
|
93.62 0.4384 0.7422 0.0464 0.0274 10.632 60.921 31.608 7928.478 6.883 140.594 1.808 0.90 508893. 0.2910
|
|
98.55 0.4615 0.7570 0.0420 0.0256 9.935 56.925 28.621 7408.375 6.431 127.307 1.752 0.90 509852. 0.2683
|
|
103.48 0.4846 0.7654 0.0375 0.0238 9.219 52.821 25.571 6874.298 5.968 113.739 1.687 0.91 510846. 0.2442
|
|
108.40 0.5076 0.7622 0.0330 0.0220 8.518 48.806 22.460 6351.758 5.514 99.902 1.604 0.91 511877. 0.2176
|
|
113.33 0.5307 0.7496 0.0283 0.0201 7.782 44.590 19.302 5803.024 5.038 85.857 1.509 0.91 512944. 0.1897
|
|
118.26 0.5538 0.7238 0.0236 0.0181 7.017 40.208 16.106 5232.791 4.543 71.640 1.396 0.91 514047. 0.1604
|
|
123.18 0.5769 0.6790 0.0189 0.0161 6.231 35.706 12.882 4646.822 4.034 57.298 1.257 0.91 515186. 0.1292
|
|
128.11 0.5999 0.6064 0.0142 0.0140 5.432 31.124 9.642 4050.591 3.516 42.888 1.080 0.91 516362. 0.0960
|
|
133.04 0.6230 0.4909 0.0094 0.0119 4.628 26.516 6.403 3450.812 2.996 28.481 0.842 0.91 517573. 0.0610
|
|
137.97 0.6461 0.3058 0.0047 0.0099 3.827 21.928 3.181 2853.725 2.477 14.149 0.506 0.91 518816. 0.0258
|
|
142.89 0.6692 -0.0092 -0.0001 0.0077 2.997 17.175 -0.072 2235.161 1.940 -0.322 -0.015 0.91 519962. 0.0000
|
|
|
|
|
|
|