464 lines
82 KiB
Plaintext
464 lines
82 KiB
Plaintext
19x10E (19x10E.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 0.0863 0.0327 0.007 0.410 0.359 4.852 0.046 1.595 33.511 0.08 33294. 0.6197
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0.41 0.0231 0.0594 0.0850 0.0330 0.007 0.414 0.353 4.903 0.047 1.570 32.647 0.08 33315. 0.5990
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0.83 0.0461 0.1156 0.0835 0.0333 0.007 0.418 0.347 4.950 0.047 1.543 31.784 0.08 33337. 0.5781
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1.24 0.0692 0.1688 0.0820 0.0336 0.007 0.422 0.340 4.993 0.048 1.514 30.925 0.08 33361. 0.5572
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1.66 0.0922 0.2188 0.0803 0.0338 0.007 0.425 0.333 5.029 0.048 1.483 30.072 0.08 33387. 0.5363
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2.07 0.1153 0.2658 0.0785 0.0340 0.007 0.428 0.326 5.059 0.048 1.450 29.225 0.08 33415. 0.5153
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2.49 0.1384 0.3098 0.0766 0.0342 0.007 0.429 0.318 5.080 0.049 1.414 28.388 0.08 33444. 0.4943
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2.90 0.1614 0.3509 0.0745 0.0343 0.007 0.430 0.309 5.092 0.049 1.376 27.558 0.08 33476. 0.4734
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3.32 0.1845 0.3891 0.0723 0.0343 0.007 0.430 0.300 5.093 0.049 1.335 26.738 0.08 33510. 0.4524
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3.73 0.2075 0.4244 0.0699 0.0342 0.007 0.430 0.290 5.082 0.049 1.292 25.927 0.08 33547. 0.4315
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4.15 0.2306 0.4570 0.0675 0.0340 0.007 0.428 0.280 5.058 0.048 1.246 25.122 0.08 33585. 0.4106
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4.56 0.2537 0.4867 0.0648 0.0338 0.007 0.424 0.269 5.020 0.048 1.197 24.323 0.08 33626. 0.3897
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4.98 0.2767 0.5136 0.0620 0.0334 0.007 0.420 0.258 4.967 0.047 1.146 23.528 0.08 33669. 0.3688
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5.39 0.2998 0.5375 0.0591 0.0330 0.007 0.414 0.245 4.898 0.047 1.092 22.733 0.08 33715. 0.3478
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5.81 0.3228 0.5585 0.0560 0.0324 0.006 0.407 0.233 4.811 0.046 1.035 21.934 0.08 33763. 0.3267
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6.22 0.3459 0.5764 0.0528 0.0317 0.006 0.398 0.219 4.708 0.045 0.975 21.126 0.08 33813. 0.3055
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6.64 0.3690 0.5909 0.0494 0.0309 0.006 0.388 0.205 4.586 0.044 0.913 20.304 0.08 33866. 0.2841
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7.05 0.3920 0.6018 0.0459 0.0299 0.006 0.376 0.191 4.447 0.042 0.849 19.461 0.08 33921. 0.2625
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7.47 0.4151 0.6086 0.0424 0.0289 0.006 0.363 0.176 4.292 0.041 0.782 18.589 0.08 33979. 0.2408
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7.88 0.4381 0.6109 0.0387 0.0277 0.006 0.348 0.161 4.121 0.039 0.714 17.678 0.08 34039. 0.2188
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8.30 0.4612 0.6081 0.0349 0.0265 0.005 0.333 0.145 3.935 0.038 0.645 16.715 0.08 34102. 0.1966
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8.71 0.4843 0.5992 0.0311 0.0251 0.005 0.316 0.129 3.733 0.036 0.574 15.687 0.08 34167. 0.1741
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9.13 0.5073 0.5831 0.0272 0.0237 0.005 0.297 0.113 3.517 0.034 0.503 14.571 0.08 34235. 0.1513
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9.54 0.5304 0.5582 0.0233 0.0221 0.004 0.278 0.097 3.287 0.031 0.430 13.343 0.08 34305. 0.1281
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9.96 0.5534 0.5224 0.0193 0.0205 0.004 0.257 0.080 3.044 0.029 0.357 11.966 0.08 34378. 0.1047
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10.37 0.5765 0.4725 0.0154 0.0188 0.004 0.236 0.064 2.789 0.027 0.284 10.390 0.08 34453. 0.0811
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10.79 0.5996 0.4040 0.0114 0.0170 0.003 0.213 0.048 2.522 0.024 0.211 8.543 0.08 34531. 0.0575
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11.20 0.6226 0.3101 0.0075 0.0151 0.003 0.190 0.031 2.247 0.021 0.139 6.313 0.08 34611. 0.0345
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11.62 0.6457 0.1797 0.0037 0.0132 0.003 0.166 0.015 1.963 0.019 0.068 3.528 0.08 34694. 0.0135
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12.03 0.6687 -0.0060 -0.0001 0.0113 0.002 0.141 0.000 1.673 0.016 -0.002 -0.113 0.08 34779. 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 0.0867 0.0302 0.048 1.516 1.440 35.875 0.171 6.403 18.201 0.15 66588. 0.6744
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0.83 0.0231 0.0646 0.0853 0.0306 0.049 1.535 1.417 36.323 0.173 6.304 17.697 0.15 66629. 0.6506
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1.67 0.0463 0.1256 0.0839 0.0309 0.049 1.553 1.393 36.742 0.175 6.197 17.198 0.15 66673. 0.6269
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2.50 0.0694 0.1830 0.0823 0.0312 0.050 1.569 1.367 37.123 0.177 6.081 16.704 0.15 66722. 0.6032
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3.33 0.0926 0.2369 0.0806 0.0315 0.050 1.583 1.339 37.457 0.179 5.957 16.216 0.15 66774. 0.5795
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4.16 0.1157 0.2873 0.0788 0.0317 0.051 1.595 1.309 37.734 0.180 5.823 15.736 0.15 66830. 0.5561
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5.00 0.1389 0.3345 0.0769 0.0319 0.051 1.604 1.277 37.943 0.181 5.680 15.265 0.15 66890. 0.5327
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5.83 0.1620 0.3784 0.0748 0.0320 0.051 1.609 1.242 38.075 0.182 5.527 14.801 0.15 66954. 0.5095
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6.66 0.1852 0.4191 0.0726 0.0321 0.051 1.611 1.206 38.119 0.182 5.363 14.347 0.15 67022. 0.4865
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7.50 0.2083 0.4569 0.0702 0.0320 0.051 1.609 1.167 38.064 0.182 5.189 13.900 0.15 67095. 0.4636
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8.33 0.2315 0.4916 0.0677 0.0319 0.051 1.602 1.125 37.901 0.181 5.004 13.462 0.15 67173. 0.4409
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9.16 0.2546 0.5235 0.0651 0.0316 0.050 1.590 1.081 37.620 0.180 4.808 13.031 0.15 67255. 0.4184
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10.00 0.2778 0.5524 0.0623 0.0313 0.050 1.573 1.034 37.214 0.178 4.600 12.606 0.15 67342. 0.3959
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10.83 0.3009 0.5785 0.0593 0.0309 0.049 1.550 0.985 36.673 0.175 4.382 12.186 0.15 67434. 0.3735
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11.66 0.3241 0.6016 0.0562 0.0303 0.048 1.521 0.934 35.988 0.172 4.153 11.768 0.15 67531. 0.3512
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12.49 0.3472 0.6217 0.0530 0.0296 0.047 1.486 0.880 35.152 0.168 3.913 11.350 0.15 67632. 0.3288
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13.33 0.3704 0.6387 0.0496 0.0287 0.046 1.444 0.823 34.167 0.163 3.663 10.931 0.15 67738. 0.3063
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14.16 0.3935 0.6522 0.0461 0.0278 0.044 1.396 0.765 33.036 0.158 3.403 10.506 0.15 67850. 0.2838
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14.99 0.4167 0.6620 0.0424 0.0267 0.043 1.342 0.705 31.762 0.152 3.137 10.070 0.15 67966. 0.2612
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15.83 0.4398 0.6675 0.0387 0.0255 0.041 1.283 0.644 30.349 0.145 2.863 9.620 0.15 68087. 0.2384
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16.66 0.4630 0.6682 0.0350 0.0242 0.039 1.217 0.581 28.800 0.138 2.584 9.149 0.15 68214. 0.2154
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17.49 0.4861 0.6632 0.0311 0.0228 0.036 1.146 0.517 27.119 0.129 2.300 8.649 0.15 68345. 0.1921
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18.33 0.5093 0.6513 0.0272 0.0213 0.034 1.070 0.452 25.310 0.121 2.012 8.107 0.15 68481. 0.1684
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19.16 0.5324 0.6308 0.0233 0.0197 0.031 0.988 0.387 23.379 0.112 1.722 7.510 0.15 68623. 0.1443
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19.99 0.5556 0.5990 0.0194 0.0179 0.029 0.902 0.321 21.333 0.102 1.430 6.835 0.15 68769. 0.1197
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20.82 0.5787 0.5522 0.0154 0.0161 0.026 0.811 0.256 19.179 0.092 1.138 6.049 0.15 68921. 0.0945
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21.66 0.6019 0.4843 0.0115 0.0142 0.023 0.715 0.190 16.927 0.081 0.847 5.100 0.15 69078. 0.0687
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22.49 0.6250 0.3848 0.0076 0.0123 0.020 0.617 0.126 14.592 0.070 0.559 3.903 0.15 69240. 0.0427
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23.32 0.6482 0.2353 0.0037 0.0103 0.016 0.515 0.062 12.187 0.058 0.275 2.301 0.15 69406. 0.0177
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24.16 0.6713 -0.0031 0.0000 0.0082 0.013 0.411 -0.001 9.724 0.046 -0.003 -0.029 0.15 69576. 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 0.0870 0.0292 0.157 3.298 3.253 117.069 0.373 14.468 12.602 0.23 99879. 0.7019
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1.25 0.0232 0.0672 0.0857 0.0296 0.159 3.343 3.203 118.647 0.378 14.245 12.243 0.23 99941. 0.6766
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2.50 0.0464 0.1305 0.0842 0.0299 0.161 3.385 3.148 120.129 0.382 14.003 11.887 0.23 100008. 0.6513
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3.76 0.0696 0.1900 0.0827 0.0303 0.163 3.423 3.090 121.482 0.387 13.743 11.536 0.23 100081. 0.6262
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5.01 0.0928 0.2457 0.0810 0.0306 0.165 3.456 3.027 122.674 0.390 13.462 11.190 0.23 100159. 0.6012
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6.26 0.1160 0.2979 0.0792 0.0308 0.166 3.484 2.959 123.671 0.394 13.161 10.851 0.23 100244. 0.5764
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7.51 0.1392 0.3465 0.0772 0.0310 0.167 3.506 2.886 124.439 0.396 12.837 10.519 0.23 100334. 0.5519
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8.77 0.1624 0.3918 0.0751 0.0311 0.168 3.520 2.808 124.939 0.398 12.491 10.195 0.23 100431. 0.5276
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10.02 0.1856 0.4338 0.0729 0.0312 0.168 3.526 2.725 125.137 0.398 12.121 9.877 0.23 100534. 0.5035
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11.27 0.2088 0.4727 0.0705 0.0312 0.168 3.522 2.636 124.996 0.398 11.727 9.567 0.23 100644. 0.4797
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12.52 0.2320 0.5085 0.0680 0.0310 0.167 3.507 2.542 124.480 0.396 11.308 9.263 0.23 100761. 0.4561
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13.77 0.2552 0.5414 0.0653 0.0308 0.166 3.481 2.442 123.559 0.393 10.864 8.966 0.23 100885. 0.4327
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15.03 0.2784 0.5715 0.0625 0.0305 0.164 3.443 2.337 122.200 0.389 10.395 8.675 0.23 101016. 0.4095
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16.28 0.3016 0.5986 0.0596 0.0300 0.161 3.391 2.226 120.375 0.383 9.901 8.388 0.23 101154. 0.3865
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17.53 0.3248 0.6229 0.0564 0.0294 0.158 3.326 2.109 118.051 0.376 9.382 8.104 0.23 101300. 0.3635
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18.78 0.3480 0.6442 0.0532 0.0287 0.154 3.246 1.987 115.203 0.367 8.838 7.823 0.23 101453. 0.3405
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20.04 0.3712 0.6624 0.0497 0.0279 0.150 3.151 1.859 111.833 0.356 8.271 7.541 0.23 101613. 0.3176
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21.29 0.3944 0.6774 0.0462 0.0269 0.145 3.041 1.728 107.952 0.344 7.684 7.258 0.23 101781. 0.2946
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22.54 0.4176 0.6888 0.0426 0.0258 0.139 2.918 1.592 103.571 0.330 7.080 6.971 0.23 101956. 0.2716
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23.79 0.4408 0.6962 0.0389 0.0246 0.132 2.781 1.453 98.700 0.314 6.461 6.675 0.23 102138. 0.2484
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25.04 0.4640 0.6991 0.0351 0.0233 0.125 2.630 1.310 93.352 0.297 5.829 6.367 0.23 102329. 0.2251
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26.30 0.4872 0.6965 0.0312 0.0218 0.117 2.466 1.166 87.537 0.279 5.186 6.041 0.23 102526. 0.2015
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27.55 0.5104 0.6873 0.0273 0.0203 0.109 2.290 1.020 81.271 0.259 4.535 5.690 0.23 102732. 0.1774
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28.80 0.5336 0.6696 0.0233 0.0186 0.100 2.101 0.872 74.573 0.237 3.878 5.303 0.23 102945. 0.1529
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30.05 0.5568 0.6409 0.0194 0.0168 0.090 1.901 0.724 67.467 0.215 3.218 4.865 0.23 103166. 0.1278
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31.31 0.5800 0.5969 0.0154 0.0150 0.080 1.690 0.575 59.981 0.191 2.558 4.349 0.23 103394. 0.1019
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32.56 0.6032 0.5306 0.0114 0.0130 0.070 1.469 0.427 52.154 0.166 1.901 3.718 0.23 103630. 0.0751
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33.81 0.6264 0.4296 0.0075 0.0110 0.059 1.241 0.281 44.030 0.140 1.251 2.898 0.23 103874. 0.0475
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35.06 0.6496 0.2691 0.0037 0.0089 0.048 1.005 0.138 35.664 0.114 0.612 1.750 0.23 104125. 0.0201
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36.31 0.6728 -0.0085 -0.0001 0.0068 0.036 0.763 -0.003 27.082 0.086 -0.014 -0.054 0.23 104379. 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 0.0875 0.0287 0.366 5.767 5.814 272.915 0.652 25.859 9.662 0.30 133168. 0.7195
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1.67 0.0232 0.0687 0.0861 0.0291 0.371 5.848 5.724 276.759 0.661 25.462 9.382 0.30 133251. 0.6932
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3.34 0.0464 0.1333 0.0847 0.0295 0.376 5.924 5.628 280.374 0.669 25.033 9.105 0.30 133341. 0.6670
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5.01 0.0696 0.1939 0.0831 0.0298 0.380 5.994 5.524 283.682 0.677 24.570 8.832 0.30 133437. 0.6410
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6.68 0.0928 0.2507 0.0814 0.0301 0.384 6.056 5.412 286.607 0.684 24.071 8.564 0.30 133542. 0.6153
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8.35 0.1160 0.3038 0.0796 0.0304 0.388 6.108 5.291 289.067 0.690 23.535 8.302 0.30 133655. 0.5898
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10.02 0.1392 0.3533 0.0777 0.0306 0.390 6.148 5.162 290.974 0.695 22.959 8.046 0.30 133775. 0.5645
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11.69 0.1624 0.3994 0.0756 0.0307 0.392 6.175 5.023 292.243 0.698 22.342 7.796 0.30 133905. 0.5396
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13.36 0.1856 0.4422 0.0734 0.0308 0.393 6.187 4.875 292.783 0.699 21.682 7.552 0.30 134043. 0.5149
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15.03 0.2088 0.4818 0.0710 0.0308 0.392 6.181 4.717 292.508 0.698 20.979 7.314 0.30 134189. 0.4905
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16.70 0.2320 0.5183 0.0685 0.0306 0.391 6.156 4.549 291.334 0.696 20.232 7.082 0.30 134346. 0.4664
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18.37 0.2552 0.5519 0.0658 0.0304 0.388 6.111 4.371 289.181 0.690 19.440 6.855 0.30 134511. 0.4426
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20.03 0.2784 0.5826 0.0629 0.0301 0.384 6.043 4.182 285.976 0.683 18.603 6.633 0.30 134686. 0.4190
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21.70 0.3016 0.6105 0.0600 0.0296 0.378 5.951 3.984 281.645 0.672 17.721 6.416 0.30 134870. 0.3955
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23.37 0.3248 0.6355 0.0568 0.0290 0.370 5.834 3.776 276.110 0.659 16.794 6.202 0.30 135065. 0.3722
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25.04 0.3480 0.6577 0.0535 0.0283 0.361 5.691 3.557 269.309 0.643 15.821 5.991 0.30 135269. 0.3489
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26.71 0.3712 0.6769 0.0501 0.0275 0.350 5.520 3.329 261.242 0.624 14.808 5.780 0.30 135483. 0.3257
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28.38 0.3944 0.6930 0.0466 0.0265 0.338 5.324 3.093 251.936 0.601 13.760 5.569 0.30 135706. 0.3025
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30.05 0.4176 0.7056 0.0429 0.0254 0.324 5.101 2.851 241.415 0.576 12.680 5.356 0.30 135940. 0.2793
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31.72 0.4408 0.7145 0.0392 0.0242 0.308 4.854 2.602 229.702 0.548 11.573 5.138 0.30 136184. 0.2559
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33.39 0.4640 0.7190 0.0353 0.0228 0.291 4.582 2.348 216.825 0.518 10.443 4.911 0.30 136437. 0.2324
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35.06 0.4872 0.7183 0.0314 0.0213 0.272 4.286 2.090 202.811 0.484 9.295 4.673 0.31 136701. 0.2086
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36.73 0.5104 0.7113 0.0275 0.0197 0.252 3.966 1.828 187.697 0.448 8.131 4.417 0.31 136975. 0.1844
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38.40 0.5336 0.6963 0.0235 0.0180 0.230 3.624 1.564 171.528 0.409 6.957 4.136 0.31 137259. 0.1597
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40.07 0.5568 0.6705 0.0195 0.0162 0.207 3.262 1.299 154.361 0.369 5.778 3.817 0.31 137554. 0.1343
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41.74 0.5800 0.6296 0.0156 0.0143 0.183 2.879 1.034 136.268 0.325 4.598 3.441 0.31 137858. 0.1080
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43.41 0.6032 0.5663 0.0116 0.0123 0.157 2.479 0.770 117.339 0.280 3.424 2.976 0.31 138173. 0.0806
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45.08 0.6263 0.4668 0.0077 0.0103 0.131 2.064 0.509 97.687 0.233 2.263 2.362 0.31 138498. 0.0520
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46.75 0.6495 0.3026 0.0038 0.0081 0.104 1.636 0.252 77.443 0.185 1.121 1.476 0.31 138833. 0.0229
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48.42 0.6727 0.0009 0.0000 0.0060 0.076 1.197 0.001 56.670 0.135 0.002 0.004 0.31 139171. 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 0.0881 0.0285 0.710 8.947 9.145 529.272 1.011 40.677 7.837 0.38 166453. 0.7319
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2.10 0.0234 0.0702 0.0867 0.0289 0.720 9.078 9.005 537.013 1.026 40.053 7.605 0.38 166558. 0.7048
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4.21 0.0468 0.1361 0.0853 0.0293 0.730 9.201 8.853 544.294 1.040 39.376 7.377 0.38 166671. 0.6778
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6.31 0.0702 0.1979 0.0837 0.0297 0.739 9.314 8.688 550.958 1.052 38.645 7.153 0.38 166794. 0.6511
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8.42 0.0936 0.2558 0.0820 0.0300 0.747 9.413 8.511 556.847 1.063 37.857 6.933 0.38 166926. 0.6246
|
|
10.52 0.1170 0.3098 0.0801 0.0302 0.753 9.497 8.320 561.792 1.073 37.008 6.717 0.38 167069. 0.5984
|
|
12.63 0.1403 0.3602 0.0782 0.0305 0.759 9.562 8.115 565.621 1.080 36.095 6.507 0.38 167222. 0.5725
|
|
14.73 0.1637 0.4070 0.0760 0.0306 0.762 9.604 7.895 568.151 1.085 35.117 6.303 0.38 167385. 0.5469
|
|
16.83 0.1871 0.4504 0.0738 0.0306 0.763 9.622 7.660 569.204 1.087 34.070 6.104 0.38 167560. 0.5217
|
|
18.94 0.2105 0.4906 0.0714 0.0306 0.763 9.612 7.408 568.601 1.086 32.953 5.910 0.38 167747. 0.4967
|
|
21.04 0.2339 0.5278 0.0688 0.0305 0.759 9.571 7.141 566.170 1.081 31.764 5.721 0.38 167945. 0.4721
|
|
23.15 0.2573 0.5619 0.0661 0.0302 0.753 9.496 6.858 561.751 1.073 30.504 5.537 0.38 168155. 0.4478
|
|
25.25 0.2807 0.5931 0.0632 0.0299 0.745 9.385 6.558 555.192 1.060 29.171 5.358 0.38 168377. 0.4237
|
|
27.36 0.3041 0.6215 0.0601 0.0294 0.733 9.236 6.242 546.344 1.043 27.765 5.182 0.38 168611. 0.3998
|
|
29.46 0.3275 0.6470 0.0569 0.0288 0.718 9.045 5.910 535.047 1.022 26.286 5.010 0.38 168857. 0.3761
|
|
31.56 0.3509 0.6697 0.0536 0.0281 0.699 8.810 5.561 521.182 0.995 24.735 4.840 0.38 169116. 0.3524
|
|
33.67 0.3742 0.6894 0.0501 0.0272 0.677 8.533 5.198 504.758 0.964 23.120 4.671 0.38 169388. 0.3288
|
|
35.77 0.3976 0.7060 0.0464 0.0262 0.652 8.213 4.822 485.826 0.928 21.448 4.502 0.38 169672. 0.3053
|
|
37.88 0.4210 0.7192 0.0427 0.0250 0.623 7.851 4.435 464.434 0.887 19.727 4.331 0.38 169968. 0.2817
|
|
39.98 0.4444 0.7287 0.0389 0.0237 0.591 7.449 4.039 440.630 0.842 17.964 4.157 0.38 170278. 0.2580
|
|
42.08 0.4678 0.7338 0.0350 0.0223 0.556 7.006 3.634 414.467 0.792 16.165 3.977 0.38 170600. 0.2341
|
|
44.19 0.4912 0.7337 0.0310 0.0208 0.518 6.525 3.223 386.004 0.737 14.336 3.787 0.38 170935. 0.2100
|
|
46.29 0.5146 0.7272 0.0270 0.0191 0.476 6.006 2.807 355.317 0.679 12.485 3.583 0.38 171282. 0.1854
|
|
48.40 0.5380 0.7123 0.0230 0.0174 0.432 5.452 2.387 322.503 0.616 10.618 3.357 0.38 171643. 0.1602
|
|
50.50 0.5614 0.6862 0.0189 0.0155 0.386 4.863 1.966 287.683 0.549 8.744 3.099 0.38 172017. 0.1342
|
|
52.61 0.5848 0.6438 0.0149 0.0135 0.337 4.243 1.545 251.013 0.479 6.871 2.791 0.38 172403. 0.1071
|
|
54.71 0.6081 0.5762 0.0108 0.0115 0.285 3.595 1.126 212.687 0.406 5.010 2.402 0.38 172803. 0.0787
|
|
56.81 0.6315 0.4658 0.0069 0.0093 0.232 2.924 0.713 172.946 0.330 3.172 1.870 0.38 173216. 0.0488
|
|
58.92 0.6549 0.2729 0.0030 0.0071 0.177 2.232 0.308 132.064 0.252 1.368 1.056 0.38 173640. 0.0181
|
|
61.02 0.6783
|
|
|
|
|
|
|
|
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 0.0888 0.0285 1.226 12.879 13.278 914.258 1.455 59.062 6.587 0.45 199733. 0.7413
|
|
2.51 0.0232 0.0702 0.0875 0.0289 1.244 13.070 13.078 927.824 1.477 58.172 6.393 0.45 199858. 0.7140
|
|
5.01 0.0464 0.1363 0.0860 0.0293 1.261 13.250 12.861 940.596 1.497 57.207 6.202 0.45 199993. 0.6869
|
|
7.52 0.0696 0.1982 0.0845 0.0297 1.277 13.415 12.627 952.307 1.516 56.164 6.014 0.45 200139. 0.6600
|
|
10.02 0.0928 0.2562 0.0828 0.0300 1.291 13.561 12.374 962.681 1.532 55.038 5.830 0.45 200297. 0.6333
|
|
12.53 0.1161 0.3103 0.0809 0.0303 1.303 13.685 12.101 971.432 1.546 53.825 5.650 0.45 200467. 0.6070
|
|
15.04 0.1393 0.3609 0.0790 0.0305 1.312 13.781 11.808 978.261 1.557 52.521 5.475 0.45 200649. 0.5810
|
|
17.54 0.1625 0.4079 0.0769 0.0306 1.318 13.846 11.493 982.854 1.564 51.122 5.304 0.45 200844. 0.5553
|
|
20.05 0.1857 0.4515 0.0746 0.0307 1.321 13.874 11.157 984.902 1.568 49.624 5.138 0.45 201052. 0.5300
|
|
22.55 0.2089 0.4920 0.0722 0.0307 1.320 13.863 10.797 984.098 1.566 48.026 4.976 0.45 201274. 0.5050
|
|
25.06 0.2321 0.5294 0.0697 0.0305 1.314 13.807 10.415 980.145 1.560 46.324 4.819 0.45 201509. 0.4803
|
|
27.56 0.2553 0.5639 0.0669 0.0303 1.304 13.703 10.009 972.764 1.548 44.518 4.667 0.45 201759. 0.4559
|
|
30.07 0.2785 0.5956 0.0641 0.0300 1.290 13.547 9.579 961.693 1.531 42.608 4.518 0.45 202022. 0.4318
|
|
32.58 0.3018 0.6245 0.0610 0.0295 1.270 13.336 9.126 946.679 1.507 40.594 4.373 0.45 202300. 0.4079
|
|
35.08 0.3250 0.6506 0.0579 0.0289 1.244 13.065 8.650 927.447 1.476 38.473 4.230 0.45 202593. 0.3842
|
|
37.59 0.3482 0.6740 0.0545 0.0282 1.212 12.731 8.149 903.770 1.438 36.248 4.090 0.45 202900. 0.3606
|
|
40.09 0.3714 0.6945 0.0510 0.0273 1.174 12.335 7.628 875.639 1.394 33.929 3.951 0.46 203222. 0.3370
|
|
42.60 0.3946 0.7121 0.0474 0.0263 1.131 11.877 7.088 843.136 1.342 31.527 3.813 0.46 203559. 0.3135
|
|
45.11 0.4178 0.7265 0.0437 0.0251 1.081 11.359 6.532 806.343 1.283 29.053 3.674 0.46 203910. 0.2900
|
|
47.61 0.4410 0.7374 0.0399 0.0238 1.026 10.781 5.961 765.343 1.218 26.515 3.533 0.46 204277. 0.2664
|
|
50.12 0.4642 0.7442 0.0360 0.0224 0.966 10.146 5.379 720.223 1.146 23.924 3.387 0.46 204659. 0.2426
|
|
52.62 0.4875 0.7463 0.0320 0.0209 0.900 9.454 4.786 671.083 1.068 21.290 3.235 0.46 205055. 0.2186
|
|
55.13 0.5107 0.7425 0.0280 0.0193 0.829 8.706 4.186 618.048 0.984 18.620 3.072 0.46 205467. 0.1941
|
|
57.64 0.5339 0.7311 0.0239 0.0175 0.753 7.907 3.581 561.278 0.893 15.927 2.894 0.46 205894. 0.1691
|
|
60.14 0.5571 0.7095 0.0199 0.0156 0.672 7.057 2.972 500.975 0.797 13.220 2.691 0.46 206337. 0.1433
|
|
62.65 0.5803 0.6731 0.0158 0.0136 0.587 6.162 2.364 437.398 0.696 10.513 2.451 0.46 206794. 0.1164
|
|
65.15 0.6035 0.6141 0.0118 0.0116 0.497 5.224 1.758 370.870 0.590 7.820 2.150 0.46 207267. 0.0880
|
|
67.66 0.6267 0.5167 0.0078 0.0094 0.405 4.251 1.159 301.792 0.480 5.156 1.742 0.46 207756. 0.0579
|
|
70.16 0.6499 0.3452 0.0038 0.0072 0.309 3.249 0.571 230.639 0.367 2.538 1.122 0.46 208259. 0.0262
|
|
72.67 0.6732 -0.0062 0.0000 0.0049 0.211 2.219 -0.007 157.535 0.251 -0.030 -0.019 0.46 208763. 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 0.0897 0.0286 1.957 17.621 18.255 1459.341 1.991 81.199 5.674 0.53 233006. 0.7487
|
|
2.94 0.0233 0.0709 0.0884 0.0291 1.987 17.888 17.982 1481.484 2.021 79.986 5.505 0.53 233152. 0.7210
|
|
5.88 0.0467 0.1376 0.0869 0.0295 2.015 18.140 17.686 1502.326 2.049 78.667 5.340 0.53 233312. 0.6935
|
|
8.81 0.0700 0.2001 0.0853 0.0299 2.040 18.371 17.365 1521.421 2.076 77.240 5.177 0.53 233484. 0.6662
|
|
11.75 0.0933 0.2585 0.0836 0.0302 2.063 18.575 17.018 1538.322 2.099 75.696 5.018 0.53 233670. 0.6393
|
|
14.69 0.1166 0.3132 0.0818 0.0305 2.082 18.747 16.644 1552.553 2.118 74.031 4.862 0.53 233870. 0.6126
|
|
17.63 0.1400 0.3641 0.0798 0.0307 2.097 18.880 16.240 1563.615 2.133 72.237 4.711 0.53 234085. 0.5863
|
|
20.57 0.1633 0.4115 0.0777 0.0308 2.107 18.969 15.807 1570.999 2.143 70.309 4.564 0.53 234315. 0.5603
|
|
23.51 0.1866 0.4555 0.0754 0.0309 2.111 19.008 15.343 1574.191 2.147 68.244 4.421 0.53 234560. 0.5347
|
|
26.44 0.2100 0.4964 0.0730 0.0309 2.109 18.990 14.846 1572.684 2.145 66.036 4.282 0.53 234822. 0.5095
|
|
29.38 0.2333 0.5342 0.0704 0.0307 2.100 18.909 14.317 1565.995 2.136 63.684 4.147 0.53 235099. 0.4846
|
|
32.32 0.2566 0.5690 0.0676 0.0305 2.083 18.760 13.756 1553.661 2.119 61.186 4.016 0.53 235393. 0.4600
|
|
35.26 0.2799 0.6010 0.0647 0.0301 2.059 18.538 13.161 1535.256 2.094 58.541 3.888 0.53 235704. 0.4356
|
|
38.20 0.3033 0.6303 0.0616 0.0296 2.025 18.237 12.533 1510.367 2.060 55.749 3.764 0.53 236032. 0.4115
|
|
41.13 0.3266 0.6568 0.0583 0.0290 1.983 17.853 11.872 1478.543 2.017 52.808 3.642 0.53 236377. 0.3875
|
|
44.07 0.3499 0.6806 0.0549 0.0282 1.930 17.381 11.178 1439.424 1.964 49.721 3.522 0.53 236739. 0.3637
|
|
47.01 0.3733 0.7016 0.0514 0.0273 1.868 16.820 10.455 1393.004 1.900 46.502 3.404 0.53 237119. 0.3399
|
|
49.95 0.3966 0.7197 0.0477 0.0263 1.796 16.173 9.705 1339.419 1.827 43.168 3.286 0.53 237516. 0.3162
|
|
52.89 0.4199 0.7346 0.0439 0.0251 1.715 15.441 8.933 1278.804 1.745 39.733 3.168 0.53 237930. 0.2924
|
|
55.83 0.4432 0.7460 0.0400 0.0238 1.624 14.626 8.141 1211.296 1.652 36.211 3.048 0.53 238362. 0.2686
|
|
58.76 0.4666 0.7535 0.0360 0.0223 1.525 13.729 7.332 1137.037 1.551 32.614 2.925 0.53 238812. 0.2446
|
|
61.70 0.4899 0.7562 0.0320 0.0207 1.416 12.753 6.510 1056.201 1.441 28.956 2.796 0.53 239279. 0.2203
|
|
64.64 0.5132 0.7530 0.0279 0.0190 1.299 11.700 5.677 968.996 1.322 25.250 2.657 0.53 239765. 0.1955
|
|
67.58 0.5366 0.7421 0.0238 0.0172 1.174 10.574 4.836 875.694 1.195 21.512 2.505 0.54 240268. 0.1701
|
|
70.52 0.5599 0.7208 0.0196 0.0152 1.041 9.378 3.992 776.638 1.059 17.757 2.331 0.54 240789. 0.1439
|
|
73.45 0.5832 0.6840 0.0155 0.0132 0.902 8.117 3.148 672.269 0.917 14.003 2.124 0.54 241328. 0.1164
|
|
76.39 0.6065 0.6229 0.0113 0.0110 0.755 6.800 2.309 563.140 0.768 10.271 1.860 0.54 241885. 0.0873
|
|
79.33 0.6299 0.5188 0.0073 0.0088 0.603 5.433 1.480 449.935 0.614 6.582 1.492 0.54 242460. 0.0560
|
|
82.27 0.6532 0.3266 0.0033 0.0065 0.447 4.026 0.666 333.453 0.455 2.961 0.905 0.54 243052. 0.0228
|
|
85.21 0.6765
|
|
|
|
|
|
|
|
PROP RPM = 8000
|
|
|
|
V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
|
|
(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
|
|
0.00 0.0000 0.0000 0.0908 0.0289 2.951 23.253 24.132 2200.878 2.627 107.338 4.973 0.60 266270. 0.7545
|
|
3.34 0.0232 0.0706 0.0895 0.0294 2.997 23.609 23.779 2234.580 2.667 105.771 4.827 0.60 266437. 0.7269
|
|
6.67 0.0464 0.1370 0.0880 0.0298 3.039 23.944 23.396 2266.324 2.705 104.067 4.682 0.60 266619. 0.6995
|
|
10.01 0.0695 0.1993 0.0865 0.0302 3.078 24.252 22.981 2295.426 2.740 102.220 4.541 0.60 266815. 0.6723
|
|
13.35 0.0927 0.2576 0.0848 0.0305 3.113 24.524 22.531 2321.221 2.771 100.219 4.403 0.60 267027. 0.6454
|
|
16.68 0.1159 0.3121 0.0829 0.0308 3.142 24.754 22.045 2342.986 2.797 98.058 4.268 0.60 267255. 0.6188
|
|
20.02 0.1391 0.3630 0.0810 0.0310 3.165 24.934 21.521 2359.976 2.817 95.727 4.136 0.60 267499. 0.5926
|
|
23.36 0.1623 0.4104 0.0788 0.0312 3.180 25.055 20.958 2371.427 2.831 93.220 4.008 0.60 267760. 0.5667
|
|
26.69 0.1855 0.4546 0.0766 0.0312 3.187 25.109 20.353 2376.566 2.837 90.530 3.884 0.60 268039. 0.5412
|
|
30.03 0.2086 0.4955 0.0741 0.0312 3.184 25.089 19.706 2374.630 2.835 87.653 3.764 0.60 268336. 0.5160
|
|
33.37 0.2318 0.5335 0.0715 0.0311 3.171 24.986 19.016 2364.886 2.823 84.584 3.647 0.60 268652. 0.4912
|
|
36.70 0.2550 0.5686 0.0688 0.0308 3.147 24.793 18.283 2346.649 2.801 81.322 3.534 0.60 268986. 0.4666
|
|
40.04 0.2782 0.6009 0.0659 0.0305 3.110 24.504 17.506 2319.273 2.768 77.865 3.423 0.61 269338. 0.4424
|
|
43.38 0.3014 0.6306 0.0628 0.0300 3.060 24.112 16.685 2282.147 2.724 74.213 3.316 0.61 269710. 0.4183
|
|
46.71 0.3245 0.6576 0.0595 0.0294 2.997 23.609 15.820 2234.617 2.667 70.366 3.211 0.61 270101. 0.3944
|
|
50.05 0.3477 0.6819 0.0561 0.0286 2.918 22.991 14.911 2176.096 2.598 66.324 3.108 0.61 270512. 0.3706
|
|
53.39 0.3709 0.7036 0.0525 0.0277 2.825 22.256 13.962 2106.518 2.514 62.104 3.006 0.61 270942. 0.3469
|
|
56.72 0.3941 0.7225 0.0488 0.0266 2.717 21.406 12.978 2026.080 2.418 57.728 2.905 0.61 271392. 0.3232
|
|
60.06 0.4173 0.7384 0.0450 0.0254 2.595 20.444 11.964 1934.990 2.310 53.216 2.804 0.61 271861. 0.2996
|
|
63.40 0.4404 0.7510 0.0411 0.0241 2.459 19.371 10.923 1833.458 2.189 48.586 2.702 0.61 272350. 0.2758
|
|
66.73 0.4636 0.7599 0.0371 0.0226 2.309 18.190 9.859 1721.695 2.055 43.854 2.597 0.61 272859. 0.2519
|
|
70.07 0.4868 0.7643 0.0330 0.0210 2.146 16.904 8.776 1599.955 1.910 39.037 2.488 0.61 273388. 0.2276
|
|
73.41 0.5100 0.7632 0.0289 0.0193 1.969 15.516 7.679 1468.547 1.753 34.155 2.372 0.61 273937. 0.2030
|
|
76.74 0.5332 0.7551 0.0247 0.0175 1.781 14.029 6.570 1327.865 1.585 29.225 2.244 0.61 274506. 0.1777
|
|
80.08 0.5564 0.7373 0.0205 0.0155 1.580 12.450 5.456 1178.411 1.407 24.269 2.100 0.61 275095. 0.1515
|
|
83.42 0.5795 0.7054 0.0163 0.0134 1.369 10.785 4.341 1020.827 1.219 19.310 1.929 0.61 275704. 0.1241
|
|
86.75 0.6027 0.6513 0.0122 0.0113 1.148 9.043 3.231 855.920 1.022 14.373 1.712 0.61 276334. 0.0951
|
|
90.09 0.6259 0.5581 0.0080 0.0090 0.918 7.234 2.133 684.696 0.817 9.488 1.413 0.61 276983. 0.0637
|
|
93.43 0.6491 0.3851 0.0040 0.0067 0.682 5.371 1.054 508.348 0.607 4.687 0.940 0.62 277653. 0.0298
|
|
96.76 0.6723 -0.0034 0.0000 0.0043 0.439 3.456 -0.006 327.118 0.390 -0.026 -0.008 0.62 278322. 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 0.0921 0.0294 4.268 29.891 30.981 3182.841 3.377 137.805 4.415 0.68 299523. 0.7589
|
|
3.75 0.0232 0.0705 0.0908 0.0298 4.334 30.355 30.540 3232.220 3.429 135.842 4.286 0.68 299712. 0.7314
|
|
7.50 0.0463 0.1368 0.0894 0.0303 4.397 30.792 30.059 3278.748 3.479 133.700 4.158 0.68 299917. 0.7040
|
|
11.25 0.0695 0.1990 0.0878 0.0307 4.454 31.193 29.535 3321.411 3.524 131.372 4.033 0.68 300139. 0.6769
|
|
15.01 0.0927 0.2573 0.0861 0.0310 4.505 31.548 28.967 3359.214 3.564 128.845 3.911 0.68 300378. 0.6501
|
|
18.76 0.1158 0.3118 0.0843 0.0313 4.548 31.847 28.352 3391.102 3.598 126.108 3.792 0.68 300635. 0.6236
|
|
22.51 0.1390 0.3628 0.0823 0.0315 4.581 32.081 27.687 3415.973 3.624 123.151 3.676 0.68 300911. 0.5974
|
|
26.26 0.1622 0.4103 0.0802 0.0317 4.603 32.238 26.970 3432.702 3.642 119.964 3.564 0.68 301206. 0.5715
|
|
30.01 0.1853 0.4545 0.0779 0.0318 4.613 32.308 26.200 3440.160 3.650 116.539 3.454 0.68 301522. 0.5461
|
|
33.76 0.2085 0.4956 0.0754 0.0317 4.609 32.280 25.375 3437.234 3.647 112.869 3.348 0.68 301857. 0.5209
|
|
37.51 0.2317 0.5338 0.0728 0.0316 4.590 32.145 24.494 3422.851 3.632 108.948 3.246 0.68 302213. 0.4961
|
|
41.27 0.2548 0.5691 0.0700 0.0314 4.554 31.893 23.555 3396.004 3.603 104.775 3.146 0.68 302590. 0.4715
|
|
45.02 0.2780 0.6018 0.0671 0.0310 4.500 31.515 22.560 3355.764 3.561 100.347 3.049 0.68 302988. 0.4473
|
|
48.77 0.3012 0.6318 0.0639 0.0305 4.427 31.003 21.508 3301.247 3.503 95.665 2.955 0.68 303407. 0.4232
|
|
52.52 0.3243 0.6592 0.0606 0.0298 4.334 30.348 20.397 3231.522 3.429 90.728 2.863 0.68 303848. 0.3993
|
|
56.27 0.3475 0.6840 0.0572 0.0290 4.218 29.543 19.230 3145.729 3.338 85.536 2.773 0.68 304311. 0.3755
|
|
60.02 0.3707 0.7062 0.0535 0.0281 4.082 28.585 18.010 3043.728 3.229 80.110 2.684 0.68 304796. 0.3517
|
|
63.77 0.3938 0.7257 0.0498 0.0270 3.924 27.477 16.745 2925.812 3.104 74.480 2.596 0.68 305302. 0.3280
|
|
67.53 0.4170 0.7424 0.0459 0.0258 3.745 26.224 15.438 2792.301 2.963 68.669 2.508 0.68 305831. 0.3043
|
|
71.28 0.4402 0.7558 0.0419 0.0244 3.545 24.826 14.097 2643.495 2.805 62.702 2.419 0.68 306382. 0.2804
|
|
75.03 0.4633 0.7656 0.0378 0.0229 3.325 23.288 12.725 2479.724 2.631 56.601 2.328 0.69 306955. 0.2564
|
|
78.78 0.4865 0.7711 0.0337 0.0212 3.086 21.613 11.328 2301.357 2.442 50.389 2.233 0.69 307550. 0.2321
|
|
82.53 0.5097 0.7713 0.0295 0.0195 2.828 19.805 9.912 2108.849 2.238 44.087 2.132 0.69 308168. 0.2073
|
|
86.28 0.5328 0.7647 0.0252 0.0176 2.552 17.870 8.481 1902.778 2.019 37.722 2.022 0.69 308808. 0.1818
|
|
90.03 0.5560 0.7486 0.0209 0.0155 2.258 15.814 7.041 1683.886 1.787 31.320 1.897 0.69 309470. 0.1554
|
|
93.79 0.5792 0.7187 0.0166 0.0134 1.949 13.647 5.600 1453.130 1.542 24.911 1.748 0.69 310155. 0.1278
|
|
97.54 0.6023 0.6667 0.0124 0.0112 1.625 11.380 4.166 1211.747 1.286 18.529 1.559 0.69 310863. 0.0983
|
|
101.29 0.6255 0.5752 0.0082 0.0089 1.289 9.028 2.746 961.285 1.020 12.212 1.295 0.69 311594. 0.0663
|
|
105.04 0.6487 0.4006 0.0040 0.0065 0.944 6.608 1.349 703.609 0.747 6.002 0.870 0.69 312346. 0.0312
|
|
108.79 0.6718 -0.0110 -0.0001 0.0041 0.589 4.123 -0.022 439.002 0.466 -0.099 -0.023 0.69 313094. 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 0.0937 0.0303 6.043 38.090 38.900 4506.492 4.303 173.026 3.915 0.75 332760. 0.7541
|
|
4.16 0.0231 0.0695 0.0924 0.0308 6.127 38.619 38.364 4569.120 4.363 170.644 3.808 0.75 332971. 0.7285
|
|
8.33 0.0463 0.1351 0.0910 0.0311 6.207 39.119 37.778 4628.210 4.420 168.037 3.702 0.75 333200. 0.7028
|
|
12.49 0.0694 0.1969 0.0894 0.0315 6.279 39.577 37.138 4682.460 4.471 165.192 3.597 0.75 333447. 0.6770
|
|
16.65 0.0925 0.2550 0.0877 0.0318 6.344 39.984 36.442 4730.524 4.517 162.093 3.494 0.75 333714. 0.6514
|
|
20.81 0.1157 0.3095 0.0859 0.0321 6.398 40.325 35.685 4770.957 4.556 158.725 3.393 0.75 334001. 0.6259
|
|
24.98 0.1388 0.3605 0.0839 0.0323 6.440 40.590 34.864 4802.222 4.586 155.076 3.293 0.75 334309. 0.6005
|
|
29.14 0.1619 0.4082 0.0818 0.0325 6.467 40.763 33.977 4822.712 4.605 151.132 3.196 0.75 334639. 0.5752
|
|
33.30 0.1851 0.4526 0.0795 0.0325 6.478 40.831 33.022 4830.787 4.613 146.882 3.100 0.75 334990. 0.5502
|
|
37.46 0.2082 0.4940 0.0770 0.0325 6.470 40.780 31.996 4824.796 4.607 142.317 3.008 0.76 335364. 0.5254
|
|
41.63 0.2314 0.5324 0.0744 0.0323 6.441 40.597 30.897 4803.122 4.587 137.432 2.918 0.76 335761. 0.5009
|
|
45.79 0.2545 0.5681 0.0716 0.0321 6.389 40.268 29.726 4764.210 4.549 132.221 2.830 0.76 336181. 0.4765
|
|
49.95 0.2776 0.6010 0.0686 0.0317 6.312 39.781 28.481 4706.618 4.494 126.684 2.745 0.76 336624. 0.4524
|
|
54.11 0.3008 0.6314 0.0654 0.0312 6.208 39.125 27.163 4628.983 4.420 120.821 2.662 0.76 337092. 0.4284
|
|
58.28 0.3239 0.6592 0.0621 0.0305 6.075 38.288 25.771 4529.919 4.326 114.630 2.580 0.76 337583. 0.4045
|
|
62.44 0.3470 0.6846 0.0585 0.0297 5.911 37.259 24.306 4408.148 4.209 108.111 2.501 0.76 338098. 0.3808
|
|
66.60 0.3702 0.7074 0.0548 0.0287 5.717 36.035 22.772 4263.416 4.071 101.292 2.423 0.76 338637. 0.3570
|
|
70.76 0.3933 0.7275 0.0510 0.0276 5.493 34.622 21.179 4096.151 3.912 94.206 2.345 0.76 339201. 0.3333
|
|
74.93 0.4164 0.7449 0.0470 0.0263 5.239 33.022 19.534 3906.857 3.731 86.887 2.268 0.76 339788. 0.3095
|
|
79.09 0.4396 0.7592 0.0430 0.0249 4.956 31.240 17.843 3696.062 3.529 79.364 2.190 0.76 340401. 0.2856
|
|
83.25 0.4627 0.7699 0.0388 0.0233 4.646 29.281 16.112 3464.332 3.308 71.665 2.109 0.76 341037. 0.2615
|
|
87.41 0.4858 0.7764 0.0345 0.0216 4.308 27.152 14.348 3212.346 3.068 63.820 2.026 0.76 341698. 0.2370
|
|
91.58 0.5090 0.7775 0.0302 0.0198 3.944 24.858 12.558 2940.944 2.808 55.857 1.937 0.76 342384. 0.2119
|
|
95.74 0.5321 0.7718 0.0259 0.0178 3.555 22.409 10.748 2651.208 2.532 47.806 1.839 0.76 343094. 0.1862
|
|
99.90 0.5552 0.7563 0.0215 0.0158 3.144 19.817 8.926 2344.531 2.239 39.703 1.727 0.77 343829. 0.1593
|
|
104.06 0.5784 0.7265 0.0171 0.0136 2.712 17.096 7.101 2022.685 1.932 31.585 1.592 0.77 344589. 0.1310
|
|
108.23 0.6015 0.6735 0.0127 0.0114 2.264 14.266 5.282 1687.895 1.612 23.495 1.419 0.77 345375. 0.1007
|
|
112.39 0.6246 0.5792 0.0084 0.0090 1.801 11.350 3.480 1342.893 1.282 15.480 1.175 0.77 346185. 0.0677
|
|
116.55 0.6478 0.3993 0.0041 0.0067 1.329 8.375 1.707 990.893 0.946 7.594 0.781 0.77 347019. 0.0315
|
|
120.71 0.6709 -0.0137 -0.0001 0.0043 0.848 5.346 -0.036 632.533 0.604 -0.160 -0.026 0.77 347848. 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 0.0955 0.0333 8.842 50.663 47.989 6593.433 5.724 213.455 3.301 0.83 365978. 0.7062
|
|
4.59 0.0232 0.0651 0.0942 0.0336 8.916 51.087 47.359 6648.559 5.772 210.651 3.231 0.83 366212. 0.6866
|
|
9.19 0.0464 0.1273 0.0929 0.0339 8.982 51.465 46.664 6697.817 5.814 207.562 3.160 0.83 366466. 0.6666
|
|
13.78 0.0696 0.1866 0.0913 0.0341 9.038 51.787 45.902 6739.706 5.851 204.171 3.089 0.83 366740. 0.6463
|
|
18.37 0.0928 0.2431 0.0897 0.0342 9.082 52.040 45.067 6772.700 5.880 200.458 3.018 0.83 367037. 0.6257
|
|
22.97 0.1161 0.2968 0.0879 0.0344 9.113 52.213 44.155 6795.218 5.899 196.401 2.947 0.83 367356. 0.6048
|
|
27.56 0.1393 0.3476 0.0859 0.0344 9.126 52.293 43.162 6805.561 5.908 191.984 2.877 0.83 367699. 0.5836
|
|
32.16 0.1625 0.3956 0.0837 0.0344 9.122 52.265 42.084 6801.951 5.905 187.190 2.806 0.83 368065. 0.5622
|
|
36.75 0.1857 0.4408 0.0814 0.0343 9.096 52.116 40.918 6782.557 5.888 182.002 2.736 0.83 368457. 0.5405
|
|
41.34 0.2089 0.4833 0.0789 0.0341 9.046 51.832 39.661 6745.514 5.856 176.411 2.667 0.83 368873. 0.5187
|
|
45.94 0.2321 0.5232 0.0762 0.0338 8.970 51.397 38.311 6688.938 5.807 170.407 2.598 0.83 369314. 0.4966
|
|
50.53 0.2553 0.5603 0.0734 0.0334 8.866 50.798 36.867 6611.004 5.739 163.984 2.529 0.83 369782. 0.4743
|
|
55.12 0.2785 0.5948 0.0703 0.0329 8.730 50.021 35.329 6509.917 5.651 157.141 2.461 0.83 370275. 0.4518
|
|
59.72 0.3017 0.6268 0.0671 0.0323 8.561 49.053 33.696 6383.867 5.542 149.879 2.394 0.83 370795. 0.4292
|
|
64.31 0.3249 0.6561 0.0636 0.0315 8.356 47.878 31.969 6230.966 5.409 142.197 2.327 0.83 371341. 0.4063
|
|
68.90 0.3482 0.6828 0.0600 0.0306 8.112 46.481 30.147 6049.224 5.251 134.094 2.260 0.83 371914. 0.3833
|
|
73.50 0.3714 0.7068 0.0562 0.0295 7.830 44.865 28.238 5838.851 5.069 125.602 2.194 0.83 372513. 0.3600
|
|
78.09 0.3946 0.7277 0.0522 0.0283 7.512 43.044 26.251 5601.928 4.863 116.766 2.125 0.84 373139. 0.3363
|
|
82.69 0.4178 0.7452 0.0482 0.0270 7.159 41.020 24.197 5338.512 4.634 107.628 2.056 0.84 373792. 0.3123
|
|
87.28 0.4410 0.7591 0.0439 0.0255 6.771 38.796 22.083 5049.054 4.383 98.226 1.984 0.84 374471. 0.2879
|
|
91.87 0.4642 0.7687 0.0396 0.0239 6.348 36.374 19.918 4733.799 4.109 88.597 1.908 0.84 375177. 0.2630
|
|
96.47 0.4874 0.7732 0.0352 0.0222 5.892 33.762 17.711 4393.823 3.814 78.777 1.828 0.84 375911. 0.2376
|
|
101.06 0.5106 0.7711 0.0308 0.0204 5.406 30.976 15.468 4031.257 3.500 68.802 1.740 0.84 376671. 0.2114
|
|
105.65 0.5338 0.7600 0.0263 0.0184 4.893 28.036 13.200 3648.709 3.168 58.712 1.641 0.84 377458. 0.1841
|
|
110.25 0.5570 0.7365 0.0217 0.0164 4.357 24.965 10.915 3249.062 2.821 48.550 1.524 0.84 378273. 0.1555
|
|
114.84 0.5803 0.6945 0.0172 0.0143 3.803 21.791 8.625 2835.956 2.462 38.366 1.380 0.84 379115. 0.1251
|
|
119.44 0.6035 0.6241 0.0126 0.0122 3.237 18.546 6.343 2413.574 2.095 28.214 1.192 0.84 379984. 0.0927
|
|
124.03 0.6267 0.5067 0.0081 0.0100 2.664 15.265 4.082 1986.591 1.725 18.155 0.932 0.85 380881. 0.0581
|
|
128.62 0.6499 0.3044 0.0037 0.0079 2.092 11.988 1.857 1560.138 1.354 8.259 0.540 0.85 381804. 0.0227
|
|
133.22 0.6731
|
|
|
|
|
|
|
|
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 0.0969 0.0398 13.712 72.018 57.955 10224.697 8.137 257.783 2.571 0.90 399196. 0.6044
|
|
5.01 0.0232 0.0556 0.0958 0.0399 13.752 72.233 57.267 10255.159 8.161 254.723 2.533 0.90 399448. 0.5919
|
|
10.02 0.0464 0.1096 0.0945 0.0400 13.774 72.348 56.500 10271.536 8.174 251.314 2.495 0.90 399724. 0.5792
|
|
15.03 0.0696 0.1619 0.0931 0.0400 13.775 72.351 55.650 10271.952 8.174 247.530 2.457 0.90 400023. 0.5661
|
|
20.04 0.0928 0.2125 0.0915 0.0399 13.752 72.229 54.709 10254.669 8.160 243.344 2.420 0.90 400346. 0.5527
|
|
25.04 0.1160 0.2616 0.0897 0.0398 13.703 71.971 53.671 10218.035 8.131 238.728 2.382 0.91 400695. 0.5390
|
|
30.05 0.1392 0.3090 0.0878 0.0396 13.625 71.566 52.531 10160.507 8.085 233.657 2.345 0.91 401069. 0.5249
|
|
35.06 0.1624 0.3547 0.0858 0.0393 13.518 71.003 51.283 10080.633 8.022 228.109 2.307 0.91 401470. 0.5103
|
|
40.07 0.1856 0.3987 0.0835 0.0389 13.379 70.273 49.924 9977.013 7.939 222.063 2.270 0.91 401898. 0.4952
|
|
45.08 0.2088 0.4410 0.0810 0.0384 13.207 69.366 48.449 9848.246 7.837 215.503 2.231 0.91 402354. 0.4797
|
|
50.09 0.2320 0.4815 0.0783 0.0378 12.998 68.272 46.856 9692.870 7.713 208.415 2.193 0.91 402838. 0.4635
|
|
55.10 0.2552 0.5201 0.0755 0.0370 12.752 66.980 45.142 9509.419 7.567 200.790 2.153 0.91 403351. 0.4468
|
|
60.11 0.2784 0.5567 0.0724 0.0362 12.467 65.484 43.307 9296.999 7.398 192.628 2.113 0.91 403892. 0.4294
|
|
65.12 0.3016 0.5913 0.0691 0.0353 12.142 63.775 41.351 9054.388 7.205 183.931 2.071 0.91 404462. 0.4114
|
|
70.12 0.3248 0.6237 0.0657 0.0342 11.774 61.843 39.276 8780.176 6.987 174.700 2.029 0.91 405060. 0.3927
|
|
75.13 0.3480 0.6538 0.0620 0.0330 11.362 59.677 37.081 8472.607 6.742 164.935 1.985 0.91 405688. 0.3733
|
|
80.14 0.3712 0.6815 0.0581 0.0317 10.904 57.273 34.774 8131.324 6.471 154.675 1.940 0.91 406344. 0.3532
|
|
85.15 0.3944 0.7062 0.0541 0.0302 10.408 54.665 32.368 7761.060 6.176 143.975 1.892 0.91 407030. 0.3324
|
|
90.16 0.4176 0.7262 0.0500 0.0287 9.890 51.947 29.874 7375.152 5.869 132.881 1.837 0.91 407745. 0.3101
|
|
95.17 0.4408 0.7408 0.0457 0.0272 9.353 49.124 27.303 6974.292 5.550 121.443 1.776 0.91 408488. 0.2865
|
|
100.18 0.4640 0.7473 0.0412 0.0256 8.815 46.301 24.662 6573.572 5.231 109.697 1.702 0.91 409260. 0.2610
|
|
105.19 0.4872 0.7450 0.0367 0.0240 8.270 43.435 21.964 6166.665 4.907 97.695 1.615 0.92 410062. 0.2338
|
|
110.19 0.5104 0.7337 0.0321 0.0224 7.698 40.432 19.222 5740.340 4.568 85.498 1.519 0.92 410893. 0.2056
|
|
115.20 0.5336 0.7110 0.0275 0.0206 7.107 37.327 16.448 5299.441 4.217 73.159 1.408 0.92 411753. 0.1763
|
|
120.21 0.5568 0.6730 0.0228 0.0189 6.504 34.162 13.655 4850.098 3.860 60.735 1.277 0.92 412642. 0.1457
|
|
125.22 0.5800 0.6148 0.0182 0.0171 5.897 30.971 10.857 4397.065 3.499 48.293 1.120 0.92 413561. 0.1140
|
|
130.23 0.6032 0.5297 0.0135 0.0154 5.292 27.796 8.073 3946.263 3.140 35.907 0.928 0.92 414509. 0.0814
|
|
135.24 0.6264 0.4084 0.0089 0.0136 4.699 24.680 5.322 3503.890 2.788 23.671 0.689 0.92 415487. 0.0491
|
|
140.25 0.6496 0.2381 0.0044 0.0120 4.124 21.661 2.625 3075.270 2.447 11.677 0.387 0.92 416495. 0.0194
|
|
145.26 0.6728 -0.0019 0.0000 0.0103 3.558 18.688 -0.018 2653.225 2.111 -0.080 -0.003 0.92 417521. 0.0000
|
|
|
|
|
|
|