427 lines
76 KiB
Plaintext
427 lines
76 KiB
Plaintext
22x10E (22x10E.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 0.0771 0.0269 0.011 0.702 0.576 8.305 0.079 2.561 31.441 0.09 44336. 0.6363
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0.43 0.0206 0.0577 0.0757 0.0271 0.011 0.707 0.565 8.369 0.080 2.514 30.630 0.09 44360. 0.6142
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0.86 0.0412 0.1123 0.0742 0.0272 0.011 0.712 0.554 8.424 0.080 2.464 29.823 0.09 44385. 0.5920
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1.29 0.0618 0.1639 0.0726 0.0274 0.011 0.716 0.542 8.471 0.081 2.411 29.020 0.09 44412. 0.5698
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1.72 0.0825 0.2126 0.0709 0.0275 0.011 0.719 0.529 8.506 0.081 2.354 28.224 0.09 44441. 0.5477
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2.15 0.1031 0.2583 0.0691 0.0276 0.011 0.721 0.516 8.529 0.081 2.295 27.433 0.09 44472. 0.5255
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2.58 0.1237 0.3011 0.0672 0.0276 0.011 0.722 0.502 8.538 0.082 2.231 26.650 0.09 44505. 0.5034
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3.01 0.1443 0.3410 0.0652 0.0276 0.011 0.721 0.487 8.532 0.081 2.165 25.872 0.09 44540. 0.4814
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3.44 0.1649 0.3781 0.0631 0.0275 0.011 0.719 0.471 8.509 0.081 2.094 25.100 0.09 44578. 0.4594
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3.87 0.1855 0.4123 0.0608 0.0274 0.011 0.716 0.454 8.467 0.081 2.020 24.333 0.09 44617. 0.4374
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4.29 0.2061 0.4437 0.0585 0.0272 0.011 0.710 0.437 8.404 0.080 1.942 23.569 0.09 44659. 0.4154
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4.72 0.2268 0.4723 0.0560 0.0269 0.011 0.703 0.418 8.319 0.079 1.861 22.807 0.09 44703. 0.3934
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5.15 0.2474 0.4981 0.0535 0.0266 0.011 0.694 0.399 8.211 0.078 1.775 22.045 0.09 44749. 0.3714
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5.58 0.2680 0.5208 0.0508 0.0261 0.011 0.683 0.379 8.080 0.077 1.686 21.280 0.09 44798. 0.3494
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6.01 0.2886 0.5406 0.0480 0.0256 0.011 0.670 0.358 7.926 0.076 1.594 20.508 0.09 44849. 0.3274
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6.44 0.3092 0.5571 0.0451 0.0251 0.010 0.655 0.337 7.748 0.074 1.499 19.725 0.09 44903. 0.3054
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6.87 0.3298 0.5702 0.0422 0.0244 0.010 0.638 0.315 7.547 0.072 1.401 18.928 0.09 44959. 0.2833
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7.30 0.3504 0.5796 0.0392 0.0237 0.010 0.619 0.292 7.322 0.070 1.300 18.109 0.09 45017. 0.2611
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7.73 0.3711 0.5850 0.0361 0.0229 0.009 0.598 0.269 7.073 0.068 1.197 17.262 0.09 45078. 0.2389
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8.16 0.3917 0.5859 0.0329 0.0220 0.009 0.575 0.246 6.801 0.065 1.092 16.379 0.09 45142. 0.2165
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8.59 0.4123 0.5818 0.0297 0.0210 0.009 0.550 0.222 6.505 0.062 0.986 15.449 0.09 45208. 0.1940
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9.02 0.4329 0.5717 0.0264 0.0200 0.008 0.523 0.197 6.187 0.059 0.877 14.459 0.09 45277. 0.1713
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9.45 0.4535 0.5547 0.0231 0.0189 0.008 0.494 0.173 5.845 0.056 0.768 13.392 0.09 45349. 0.1484
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9.88 0.4741 0.5294 0.0198 0.0177 0.007 0.463 0.148 5.482 0.052 0.657 12.224 0.09 45423. 0.1253
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10.31 0.4947 0.4937 0.0164 0.0165 0.007 0.431 0.123 5.097 0.049 0.546 10.925 0.09 45499. 0.1021
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10.74 0.5154 0.4449 0.0131 0.0152 0.006 0.397 0.098 4.693 0.045 0.435 9.452 0.09 45579. 0.0788
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11.17 0.5360 0.3790 0.0098 0.0138 0.006 0.361 0.073 4.270 0.041 0.324 7.743 0.09 45661. 0.0558
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11.60 0.5566 0.2900 0.0065 0.0124 0.005 0.324 0.048 3.831 0.037 0.214 5.705 0.09 45746. 0.0334
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12.03 0.5772 0.1685 0.0032 0.0109 0.005 0.285 0.024 3.378 0.032 0.106 3.197 0.09 45833. 0.0132
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12.45 0.5978 -0.0018 0.0000 0.0094 0.004 0.246 0.000 2.910 0.028 -0.001 -0.033 0.09 45922. 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 0.0775 0.0249 0.083 2.601 2.313 61.558 0.294 10.289 17.045 0.17 88670. 0.6914
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0.87 0.0209 0.0632 0.0760 0.0251 0.083 2.626 2.271 62.128 0.297 10.099 16.576 0.17 88718. 0.6662
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1.74 0.0417 0.1228 0.0745 0.0253 0.084 2.647 2.225 62.634 0.299 9.897 16.113 0.17 88770. 0.6410
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2.61 0.0626 0.1790 0.0729 0.0255 0.085 2.665 2.177 63.061 0.301 9.681 15.655 0.17 88825. 0.6160
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3.48 0.0835 0.2318 0.0712 0.0256 0.085 2.679 2.125 63.397 0.303 9.453 15.204 0.17 88884. 0.5911
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4.35 0.1043 0.2813 0.0693 0.0257 0.085 2.689 2.071 63.629 0.304 9.210 14.759 0.17 88947. 0.5664
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5.22 0.1252 0.3276 0.0674 0.0258 0.085 2.694 2.013 63.744 0.304 8.953 14.322 0.17 89015. 0.5419
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6.09 0.1461 0.3707 0.0654 0.0258 0.085 2.693 1.952 63.728 0.304 8.681 13.891 0.17 89086. 0.5176
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6.96 0.1670 0.4107 0.0632 0.0257 0.085 2.686 1.887 63.566 0.304 8.394 13.466 0.17 89162. 0.4934
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7.83 0.1878 0.4476 0.0609 0.0256 0.085 2.673 1.819 63.244 0.302 8.092 13.048 0.17 89242. 0.4694
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8.70 0.2087 0.4816 0.0585 0.0254 0.084 2.652 1.748 62.745 0.300 7.774 12.635 0.17 89327. 0.4455
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9.56 0.2296 0.5127 0.0560 0.0251 0.083 2.623 1.673 62.057 0.296 7.441 12.226 0.17 89417. 0.4218
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10.43 0.2504 0.5408 0.0534 0.0247 0.082 2.585 1.594 61.173 0.292 7.092 11.822 0.18 89512. 0.3981
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11.30 0.2713 0.5659 0.0507 0.0243 0.081 2.539 1.513 60.089 0.287 6.729 11.419 0.18 89611. 0.3746
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12.17 0.2922 0.5880 0.0478 0.0238 0.079 2.485 1.428 58.803 0.281 6.353 11.017 0.18 89716. 0.3512
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13.04 0.3130 0.6069 0.0449 0.0232 0.077 2.422 1.341 57.312 0.274 5.965 10.613 0.18 89825. 0.3278
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13.91 0.3339 0.6224 0.0419 0.0225 0.075 2.350 1.251 55.615 0.266 5.566 10.205 0.18 89940. 0.3044
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14.78 0.3548 0.6344 0.0388 0.0217 0.072 2.270 1.159 53.709 0.256 5.156 9.789 0.18 90060. 0.2811
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15.65 0.3756 0.6424 0.0357 0.0209 0.069 2.180 1.065 51.595 0.246 4.737 9.362 0.18 90184. 0.2577
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16.52 0.3965 0.6460 0.0324 0.0199 0.066 2.082 0.969 49.273 0.235 4.309 8.918 0.18 90315. 0.2341
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17.39 0.4174 0.6445 0.0292 0.0189 0.063 1.975 0.871 46.745 0.223 3.875 8.453 0.18 90450. 0.2104
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18.26 0.4382 0.6371 0.0259 0.0178 0.059 1.860 0.772 44.012 0.210 3.435 7.958 0.18 90591. 0.1865
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19.13 0.4591 0.6224 0.0225 0.0166 0.055 1.736 0.672 41.081 0.196 2.990 7.422 0.18 90737. 0.1623
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20.00 0.4800 0.5988 0.0191 0.0153 0.051 1.604 0.571 37.956 0.181 2.542 6.829 0.18 90888. 0.1377
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20.87 0.5009 0.5634 0.0158 0.0140 0.046 1.464 0.470 34.647 0.165 2.093 6.159 0.18 91045. 0.1127
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21.74 0.5217 0.5125 0.0124 0.0126 0.042 1.317 0.369 31.166 0.149 1.643 5.377 0.18 91208. 0.0872
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22.61 0.5426 0.4394 0.0090 0.0111 0.037 1.163 0.269 27.525 0.131 1.197 4.434 0.18 91376. 0.0613
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23.48 0.5635 0.3336 0.0057 0.0096 0.032 1.003 0.170 23.744 0.113 0.755 3.241 0.18 91549. 0.0356
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24.35 0.5843 0.1751 0.0024 0.0080 0.027 0.838 0.072 19.841 0.095 0.319 1.640 0.18 91728. 0.0117
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25.22 0.6052
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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 0.0779 0.0241 0.270 5.676 5.235 201.450 0.641 23.284 11.786 0.26 133002. 0.7192
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1.29 0.0207 0.0650 0.0765 0.0244 0.273 5.732 5.139 203.446 0.648 22.860 11.458 0.26 133073. 0.6928
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2.59 0.0414 0.1263 0.0750 0.0246 0.275 5.782 5.038 205.223 0.653 22.408 11.134 0.26 133150. 0.6665
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3.88 0.0621 0.1840 0.0734 0.0248 0.277 5.825 4.929 206.738 0.658 21.926 10.815 0.26 133232. 0.6404
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5.17 0.0828 0.2382 0.0717 0.0249 0.279 5.859 4.814 207.949 0.662 21.415 10.501 0.26 133320. 0.6145
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6.47 0.1035 0.2890 0.0698 0.0250 0.280 5.883 4.693 208.810 0.665 20.873 10.193 0.26 133414. 0.5889
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7.76 0.1242 0.3365 0.0679 0.0251 0.281 5.896 4.564 209.276 0.666 20.299 9.891 0.26 133514. 0.5635
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9.05 0.1449 0.3808 0.0659 0.0251 0.281 5.897 4.427 209.302 0.666 19.692 9.594 0.26 133620. 0.5384
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10.35 0.1656 0.4220 0.0638 0.0250 0.280 5.884 4.283 208.838 0.665 19.052 9.303 0.26 133733. 0.5135
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11.64 0.1863 0.4602 0.0615 0.0249 0.279 5.856 4.132 207.835 0.662 18.378 9.017 0.26 133852. 0.4888
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12.94 0.2070 0.4954 0.0591 0.0247 0.277 5.811 3.972 206.236 0.656 17.668 8.736 0.26 133978. 0.4644
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14.23 0.2277 0.5277 0.0566 0.0244 0.274 5.747 3.805 203.999 0.649 16.923 8.459 0.26 134112. 0.4401
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15.52 0.2484 0.5571 0.0540 0.0241 0.270 5.666 3.630 201.096 0.640 16.144 8.186 0.26 134252. 0.4160
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16.82 0.2691 0.5836 0.0513 0.0237 0.265 5.565 3.447 197.513 0.629 15.334 7.917 0.26 134399. 0.3920
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18.11 0.2898 0.6072 0.0485 0.0231 0.259 5.444 3.259 193.239 0.615 14.494 7.649 0.26 134554. 0.3682
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19.40 0.3105 0.6278 0.0456 0.0225 0.252 5.304 3.064 188.264 0.599 13.627 7.381 0.26 134716. 0.3446
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20.70 0.3311 0.6453 0.0426 0.0219 0.245 5.144 2.863 182.582 0.581 12.734 7.112 0.26 134886. 0.3210
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21.99 0.3518 0.6594 0.0395 0.0211 0.236 4.964 2.657 176.186 0.561 11.818 6.840 0.26 135063. 0.2974
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23.28 0.3725 0.6699 0.0364 0.0202 0.227 4.764 2.446 169.074 0.538 10.881 6.563 0.26 135248. 0.2738
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24.58 0.3932 0.6763 0.0332 0.0193 0.216 4.543 2.232 161.245 0.513 9.926 6.277 0.26 135440. 0.2501
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25.87 0.4139 0.6782 0.0300 0.0183 0.205 4.302 2.013 152.704 0.486 8.954 5.979 0.26 135640. 0.2263
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27.16 0.4346 0.6746 0.0267 0.0172 0.192 4.042 1.792 143.458 0.457 7.969 5.664 0.26 135849. 0.2022
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28.46 0.4553 0.6644 0.0233 0.0160 0.179 3.762 1.568 133.522 0.425 6.973 5.325 0.26 136065. 0.1778
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29.75 0.4760 0.6460 0.0200 0.0147 0.165 3.463 1.342 122.916 0.391 5.970 4.953 0.26 136289. 0.1530
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31.05 0.4967 0.6168 0.0166 0.0134 0.150 3.146 1.116 111.667 0.355 4.963 4.532 0.27 136521. 0.1277
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32.34 0.5174 0.5730 0.0132 0.0120 0.134 2.812 0.889 99.814 0.318 3.956 4.042 0.27 136761. 0.1017
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33.63 0.5381 0.5081 0.0099 0.0105 0.117 2.462 0.664 87.402 0.278 2.954 3.446 0.27 137009. 0.0749
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34.93 0.5588 0.4110 0.0066 0.0089 0.100 2.099 0.441 74.491 0.237 1.961 2.684 0.27 137265. 0.0475
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36.22 0.5795 0.2600 0.0033 0.0073 0.082 1.723 0.221 61.146 0.195 0.982 1.637 0.27 137529. 0.0205
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37.51 0.6002 0.0057 0.0001 0.0057 0.064 1.334 0.004 47.355 0.151 0.016 0.035 0.27 137793. 0.0001
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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 0.0785 0.0238 0.632 9.960 9.378 471.346 1.125 41.713 9.024 0.35 177328. 0.7371
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1.73 0.0207 0.0664 0.0771 0.0241 0.639 10.063 9.208 476.212 1.137 40.955 8.770 0.35 177424. 0.7098
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3.45 0.0415 0.1290 0.0756 0.0243 0.644 10.154 9.026 480.552 1.147 40.147 8.519 0.35 177527. 0.6826
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5.18 0.0622 0.1879 0.0739 0.0245 0.649 10.233 8.832 484.256 1.156 39.286 8.273 0.35 177637. 0.6557
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6.91 0.0829 0.2432 0.0722 0.0246 0.653 10.295 8.627 487.223 1.163 38.371 8.031 0.35 177755. 0.6291
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8.64 0.1036 0.2951 0.0704 0.0247 0.656 10.340 8.408 489.344 1.168 37.401 7.794 0.35 177881. 0.6028
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10.36 0.1244 0.3435 0.0685 0.0248 0.658 10.365 8.177 490.508 1.171 36.373 7.562 0.35 178015. 0.5767
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12.09 0.1451 0.3887 0.0664 0.0248 0.658 10.367 7.933 490.604 1.171 35.286 7.334 0.35 178157. 0.5510
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13.82 0.1658 0.4308 0.0643 0.0247 0.656 10.344 7.675 489.515 1.169 34.139 7.112 0.35 178308. 0.5255
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15.54 0.1865 0.4698 0.0620 0.0246 0.653 10.293 7.403 487.117 1.163 32.931 6.894 0.35 178468. 0.5003
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17.27 0.2073 0.5058 0.0596 0.0244 0.648 10.212 7.117 483.278 1.154 31.658 6.680 0.35 178637. 0.4753
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19.00 0.2280 0.5389 0.0571 0.0241 0.641 10.098 6.817 477.887 1.141 30.322 6.470 0.35 178815. 0.4506
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20.73 0.2487 0.5691 0.0544 0.0238 0.631 9.950 6.503 470.879 1.124 28.925 6.264 0.35 179003. 0.4260
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22.45 0.2694 0.5965 0.0517 0.0234 0.620 9.767 6.176 462.216 1.103 27.471 6.061 0.35 179200. 0.4017
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24.18 0.2902 0.6211 0.0489 0.0228 0.606 9.548 5.837 451.871 1.079 25.964 5.859 0.35 179407. 0.3776
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25.91 0.3109 0.6427 0.0459 0.0222 0.590 9.294 5.487 439.820 1.050 24.407 5.659 0.35 179624. 0.3535
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27.63 0.3316 0.6612 0.0429 0.0215 0.571 9.003 5.127 426.042 1.017 22.804 5.458 0.35 179851. 0.3296
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29.36 0.3523 0.6765 0.0398 0.0207 0.551 8.675 4.757 410.525 0.980 21.160 5.256 0.35 180088. 0.3058
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31.09 0.3731 0.6883 0.0367 0.0199 0.527 8.310 4.379 393.260 0.939 19.478 5.051 0.35 180335. 0.2819
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32.82 0.3938 0.6962 0.0334 0.0189 0.502 7.908 3.993 374.246 0.893 17.762 4.840 0.35 180593. 0.2579
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34.54 0.4145 0.6997 0.0301 0.0179 0.474 7.470 3.601 353.493 0.844 16.017 4.620 0.35 180861. 0.2339
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36.27 0.4352 0.6979 0.0268 0.0167 0.444 6.995 3.203 331.020 0.790 14.248 4.389 0.35 181139. 0.2095
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38.00 0.4560 0.6897 0.0235 0.0155 0.412 6.484 2.801 306.861 0.733 12.461 4.141 0.35 181428. 0.1848
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39.72 0.4767 0.6735 0.0201 0.0142 0.377 5.939 2.397 281.067 0.671 10.660 3.867 0.35 181728. 0.1597
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41.45 0.4974 0.6465 0.0167 0.0128 0.340 5.361 1.990 253.707 0.606 8.852 3.558 0.35 182038. 0.1339
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43.18 0.5181 0.6047 0.0133 0.0114 0.302 4.752 1.584 224.871 0.537 7.045 3.195 0.35 182359. 0.1072
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44.91 0.5389 0.5410 0.0099 0.0098 0.261 4.114 1.180 194.678 0.465 5.247 2.748 0.35 182691. 0.0796
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46.63 0.5596 0.4425 0.0065 0.0082 0.219 3.450 0.779 163.272 0.390 3.465 2.164 0.35 183033. 0.0510
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48.36 0.5803 0.2826 0.0032 0.0066 0.175 2.764 0.384 130.817 0.312 1.710 1.333 0.35 183386. 0.0220
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50.09 0.6010 -0.0059 0.0000 0.0049 0.130 2.054 -0.006 97.192 0.232 -0.025 -0.027 0.36 183734. 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 0.0793 0.0238 1.232 15.526 14.799 918.476 1.754 65.828 7.308 0.44 221648. 0.7499
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2.16 0.0207 0.0672 0.0779 0.0240 1.245 15.690 14.532 928.176 1.773 64.639 7.101 0.44 221768. 0.7220
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4.32 0.0414 0.1305 0.0763 0.0242 1.256 15.837 14.247 936.822 1.789 63.370 6.898 0.44 221897. 0.6944
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6.47 0.0621 0.1901 0.0747 0.0244 1.266 15.961 13.943 944.201 1.803 62.019 6.698 0.44 222035. 0.6670
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8.63 0.0829 0.2460 0.0730 0.0246 1.274 16.061 13.620 950.110 1.815 60.581 6.502 0.44 222183. 0.6400
|
|
10.79 0.1036 0.2984 0.0711 0.0247 1.280 16.133 13.277 954.333 1.823 59.056 6.310 0.44 222341. 0.6132
|
|
12.95 0.1243 0.3475 0.0692 0.0247 1.283 16.172 12.914 956.652 1.827 57.440 6.123 0.44 222509. 0.5868
|
|
15.10 0.1450 0.3933 0.0671 0.0248 1.283 16.175 12.529 956.839 1.827 55.730 5.939 0.44 222687. 0.5607
|
|
17.26 0.1657 0.4359 0.0650 0.0247 1.280 16.138 12.123 954.667 1.823 53.925 5.760 0.44 222876. 0.5349
|
|
19.42 0.1864 0.4754 0.0627 0.0246 1.274 16.057 11.696 949.891 1.814 52.022 5.585 0.44 223077. 0.5094
|
|
21.58 0.2071 0.5120 0.0603 0.0244 1.264 15.928 11.245 942.249 1.800 50.018 5.413 0.44 223288. 0.4841
|
|
23.73 0.2278 0.5457 0.0577 0.0241 1.249 15.747 10.772 931.514 1.779 47.913 5.245 0.44 223512. 0.4591
|
|
25.89 0.2486 0.5766 0.0551 0.0237 1.230 15.511 10.277 917.554 1.752 45.711 5.080 0.44 223747. 0.4344
|
|
28.05 0.2693 0.6047 0.0523 0.0233 1.207 15.219 9.761 900.291 1.719 43.419 4.918 0.44 223994. 0.4098
|
|
30.21 0.2900 0.6300 0.0494 0.0228 1.180 14.870 9.227 879.667 1.680 41.041 4.758 0.44 224253. 0.3854
|
|
32.36 0.3107 0.6524 0.0465 0.0221 1.147 14.464 8.675 855.636 1.634 38.585 4.598 0.44 224524. 0.3612
|
|
34.52 0.3314 0.6719 0.0434 0.0214 1.111 14.000 8.106 828.159 1.582 36.056 4.440 0.44 224808. 0.3371
|
|
36.68 0.3521 0.6882 0.0403 0.0206 1.069 13.476 7.523 797.206 1.523 33.460 4.280 0.44 225105. 0.3131
|
|
38.84 0.3728 0.7012 0.0371 0.0197 1.023 12.894 6.925 762.761 1.457 30.804 4.118 0.44 225414. 0.2890
|
|
40.99 0.3935 0.7104 0.0338 0.0188 0.972 12.253 6.316 724.821 1.384 28.095 3.953 0.44 225736. 0.2649
|
|
43.15 0.4143 0.7153 0.0305 0.0177 0.916 11.553 5.697 683.404 1.305 25.340 3.781 0.44 226071. 0.2407
|
|
45.31 0.4350 0.7152 0.0272 0.0165 0.856 10.794 5.069 638.552 1.220 22.546 3.600 0.44 226418. 0.2162
|
|
47.47 0.4557 0.7089 0.0238 0.0153 0.792 9.979 4.434 590.328 1.127 19.721 3.407 0.44 226779. 0.1913
|
|
49.63 0.4764 0.6948 0.0203 0.0139 0.723 9.109 3.794 538.834 1.029 16.876 3.194 0.44 227154. 0.1659
|
|
51.78 0.4971 0.6703 0.0169 0.0125 0.649 8.185 3.152 484.208 0.925 14.020 2.953 0.44 227541. 0.1398
|
|
53.94 0.5178 0.6310 0.0134 0.0110 0.572 7.212 2.510 426.633 0.815 11.165 2.669 0.44 227942. 0.1128
|
|
56.10 0.5385 0.5697 0.0100 0.0095 0.491 6.193 1.871 366.344 0.700 8.322 2.316 0.44 228357. 0.0845
|
|
58.26 0.5593 0.4723 0.0066 0.0079 0.407 5.133 1.238 303.632 0.580 5.507 1.849 0.44 228785. 0.0549
|
|
60.41 0.5800 0.3090 0.0033 0.0062 0.320 4.037 0.614 238.829 0.456 2.733 1.167 0.44 229225. 0.0244
|
|
62.57 0.6007 -0.0018 0.0000 0.0044 0.230 2.902 -0.003 171.665 0.328 -0.011 -0.007 0.44 229659. 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 0.0803 0.0239 2.141 22.490 21.580 1596.494 2.541 95.990 6.131 0.52 265958. 0.7596
|
|
2.59 0.0207 0.0676 0.0789 0.0242 2.164 22.731 21.194 1613.576 2.568 94.269 5.957 0.52 266103. 0.7315
|
|
5.18 0.0414 0.1314 0.0773 0.0244 2.184 22.945 20.780 1628.782 2.592 92.430 5.787 0.52 266259. 0.7036
|
|
7.77 0.0622 0.1914 0.0757 0.0246 2.202 23.127 20.339 1641.740 2.613 90.470 5.619 0.52 266426. 0.6759
|
|
10.36 0.0829 0.2477 0.0739 0.0247 2.215 23.273 19.870 1652.080 2.629 88.384 5.455 0.52 266604. 0.6486
|
|
12.95 0.1036 0.3006 0.0721 0.0248 2.225 23.376 19.372 1659.422 2.641 86.168 5.295 0.52 266794. 0.6216
|
|
15.54 0.1243 0.3500 0.0701 0.0249 2.231 23.432 18.844 1663.382 2.647 83.818 5.138 0.52 266997. 0.5949
|
|
18.13 0.1450 0.3962 0.0680 0.0249 2.231 23.435 18.285 1663.563 2.648 81.332 4.985 0.52 267212. 0.5686
|
|
20.72 0.1657 0.4392 0.0658 0.0248 2.226 23.378 17.694 1659.560 2.641 78.705 4.836 0.52 267440. 0.5426
|
|
23.31 0.1865 0.4792 0.0635 0.0247 2.214 23.257 17.071 1650.947 2.628 75.934 4.690 0.52 267681. 0.5168
|
|
25.90 0.2072 0.5163 0.0611 0.0245 2.196 23.064 16.415 1637.263 2.606 73.015 4.547 0.52 267936. 0.4914
|
|
28.49 0.2279 0.5505 0.0585 0.0242 2.170 22.794 15.725 1618.102 2.575 69.946 4.408 0.52 268206. 0.4662
|
|
31.08 0.2486 0.5819 0.0558 0.0239 2.137 22.444 15.003 1593.220 2.536 66.735 4.271 0.53 268489. 0.4413
|
|
33.67 0.2693 0.6106 0.0530 0.0234 2.095 22.011 14.251 1562.479 2.487 63.390 4.137 0.53 268786. 0.4165
|
|
36.26 0.2900 0.6365 0.0501 0.0228 2.046 21.494 13.471 1525.779 2.428 59.919 4.005 0.53 269098. 0.3920
|
|
38.84 0.3108 0.6596 0.0471 0.0222 1.989 20.892 12.665 1483.038 2.360 56.333 3.873 0.53 269425. 0.3676
|
|
41.43 0.3315 0.6798 0.0440 0.0215 1.923 20.204 11.834 1434.188 2.283 52.638 3.743 0.53 269766. 0.3434
|
|
44.02 0.3522 0.6970 0.0409 0.0206 1.850 19.429 10.982 1379.181 2.195 48.846 3.611 0.53 270123. 0.3192
|
|
46.61 0.3729 0.7109 0.0376 0.0197 1.767 18.567 10.109 1317.986 2.098 44.964 3.479 0.53 270495. 0.2950
|
|
49.20 0.3936 0.7212 0.0343 0.0187 1.677 17.617 9.218 1250.600 1.990 41.004 3.343 0.53 270882. 0.2707
|
|
51.79 0.4143 0.7273 0.0309 0.0176 1.578 16.581 8.313 1177.056 1.873 36.975 3.203 0.53 271284. 0.2463
|
|
54.38 0.4351 0.7286 0.0275 0.0164 1.472 15.460 7.394 1097.427 1.747 32.889 3.056 0.53 271702. 0.2216
|
|
56.97 0.4558 0.7239 0.0241 0.0151 1.357 14.254 6.465 1011.828 1.610 28.757 2.898 0.53 272136. 0.1965
|
|
59.56 0.4765 0.7115 0.0206 0.0138 1.234 12.966 5.529 920.441 1.465 24.595 2.725 0.53 272586. 0.1709
|
|
62.15 0.4972 0.6888 0.0171 0.0123 1.104 11.601 4.590 823.510 1.311 20.416 2.528 0.53 273051. 0.1445
|
|
64.74 0.5179 0.6515 0.0136 0.0108 0.967 10.162 3.651 721.365 1.148 16.238 2.295 0.53 273533. 0.1170
|
|
67.33 0.5386 0.5917 0.0101 0.0092 0.824 8.655 2.716 614.427 0.978 12.079 2.005 0.53 274031. 0.0881
|
|
69.92 0.5594 0.4944 0.0067 0.0075 0.675 7.089 1.789 503.216 0.801 7.959 1.613 0.53 274544. 0.0575
|
|
72.51 0.5801 0.3256 0.0033 0.0058 0.521 5.470 0.877 388.329 0.618 3.900 1.024 0.53 275073. 0.0256
|
|
75.10 0.6008 -0.0158 -0.0001 0.0040 0.361 3.788 -0.028 268.901 0.428 -0.127 -0.048 0.53 275585. 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 0.0816 0.0242 3.445 31.022 29.836 2569.216 3.505 132.712 5.267 0.61 310255. 0.7674
|
|
3.02 0.0207 0.0677 0.0801 0.0245 3.482 31.356 29.308 2596.839 3.543 130.361 5.119 0.61 310425. 0.7391
|
|
6.03 0.0414 0.1315 0.0786 0.0247 3.515 31.652 28.742 2621.381 3.576 127.846 4.973 0.61 310608. 0.7111
|
|
9.05 0.0620 0.1915 0.0769 0.0249 3.543 31.904 28.139 2642.235 3.604 125.162 4.830 0.61 310803. 0.6834
|
|
12.06 0.0827 0.2480 0.0752 0.0251 3.566 32.104 27.496 2658.804 3.627 122.304 4.691 0.61 311012. 0.6560
|
|
15.08 0.1034 0.3010 0.0733 0.0252 3.581 32.245 26.813 2670.473 3.643 119.265 4.554 0.61 311235. 0.6290
|
|
18.09 0.1241 0.3506 0.0713 0.0252 3.589 32.319 26.088 2676.619 3.651 116.040 4.421 0.61 311472. 0.6022
|
|
21.11 0.1447 0.3970 0.0692 0.0252 3.589 32.319 25.320 2676.594 3.651 112.624 4.291 0.61 311724. 0.5758
|
|
24.12 0.1654 0.4403 0.0670 0.0252 3.580 32.236 24.508 2669.758 3.642 109.013 4.164 0.61 311991. 0.5498
|
|
27.14 0.1861 0.4806 0.0647 0.0250 3.561 32.063 23.651 2655.431 3.622 105.201 4.040 0.61 312273. 0.5240
|
|
30.15 0.2068 0.5180 0.0622 0.0248 3.531 31.791 22.748 2632.876 3.592 101.184 3.919 0.61 312571. 0.4985
|
|
33.17 0.2274 0.5526 0.0596 0.0245 3.489 31.411 21.798 2601.413 3.549 96.958 3.801 0.61 312886. 0.4733
|
|
36.18 0.2481 0.5845 0.0569 0.0241 3.434 30.919 20.803 2560.635 3.493 92.533 3.685 0.61 313216. 0.4483
|
|
39.20 0.2688 0.6137 0.0540 0.0237 3.366 30.311 19.766 2510.312 3.425 87.919 3.571 0.61 313564. 0.4235
|
|
42.21 0.2895 0.6402 0.0511 0.0231 3.286 29.586 18.689 2450.288 3.343 83.130 3.460 0.61 313928. 0.3989
|
|
45.23 0.3101 0.6640 0.0480 0.0224 3.192 28.743 17.576 2380.436 3.247 78.177 3.349 0.61 314309. 0.3745
|
|
48.24 0.3308 0.6850 0.0449 0.0217 3.085 27.780 16.429 2300.651 3.139 73.074 3.239 0.61 314707. 0.3501
|
|
51.26 0.3515 0.7030 0.0417 0.0208 2.965 26.695 15.250 2210.857 3.016 67.833 3.129 0.61 315123. 0.3259
|
|
54.27 0.3722 0.7179 0.0384 0.0199 2.831 25.490 14.044 2111.010 2.880 62.466 3.017 0.62 315556. 0.3016
|
|
57.29 0.3928 0.7293 0.0350 0.0189 2.684 24.163 12.812 2001.108 2.730 56.988 2.904 0.62 316007. 0.2772
|
|
60.30 0.4135 0.7368 0.0316 0.0177 2.523 22.715 11.559 1881.201 2.566 51.413 2.787 0.62 316476. 0.2527
|
|
63.32 0.4342 0.7395 0.0281 0.0165 2.349 21.148 10.287 1751.407 2.389 45.757 2.664 0.62 316962. 0.2279
|
|
66.33 0.4549 0.7365 0.0246 0.0152 2.162 19.463 9.001 1611.916 2.199 40.036 2.533 0.62 317467. 0.2027
|
|
69.35 0.4755 0.7262 0.0211 0.0138 1.962 17.665 7.705 1463.017 1.996 34.270 2.389 0.62 317990. 0.1768
|
|
72.36 0.4962 0.7059 0.0175 0.0123 1.750 15.759 6.403 1305.109 1.780 28.479 2.225 0.62 318532. 0.1502
|
|
75.38 0.5169 0.6713 0.0139 0.0107 1.527 13.750 5.100 1138.720 1.553 22.686 2.032 0.62 319092. 0.1224
|
|
78.39 0.5376 0.6147 0.0104 0.0091 1.293 11.646 3.803 964.533 1.316 16.918 1.789 0.62 319671. 0.0930
|
|
81.41 0.5582 0.5204 0.0069 0.0074 1.051 9.459 2.518 783.398 1.069 11.202 1.458 0.62 320268. 0.0617
|
|
84.42 0.5789 0.3525 0.0034 0.0056 0.800 7.200 1.252 596.293 0.813 5.569 0.952 0.62 320883. 0.0284
|
|
87.44 0.5996 -0.0010 0.0000 0.0038 0.539 4.857 -0.002 402.210 0.549 -0.010 -0.002 0.62 321484. 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 0.0832 0.0247 5.253 41.389 39.732 3917.427 4.676 176.726 4.600 0.70 354534. 0.7734
|
|
3.44 0.0207 0.0675 0.0817 0.0250 5.310 41.834 39.038 3959.533 4.726 173.642 4.472 0.70 354730. 0.7452
|
|
6.89 0.0413 0.1312 0.0802 0.0252 5.360 42.228 38.295 3996.856 4.771 170.336 4.346 0.70 354940. 0.7173
|
|
10.33 0.0620 0.1912 0.0785 0.0254 5.402 42.562 37.501 4028.434 4.809 166.803 4.222 0.70 355166. 0.6896
|
|
13.77 0.0826 0.2476 0.0767 0.0256 5.436 42.825 36.654 4053.342 4.838 163.035 4.102 0.70 355406. 0.6623
|
|
17.21 0.1033 0.3006 0.0748 0.0257 5.459 43.008 35.752 4070.637 4.859 159.023 3.984 0.70 355663. 0.6353
|
|
20.66 0.1239 0.3503 0.0728 0.0258 5.471 43.100 34.793 4079.356 4.869 154.760 3.869 0.70 355935. 0.6086
|
|
24.10 0.1446 0.3969 0.0707 0.0258 5.469 43.091 33.777 4078.522 4.868 150.239 3.756 0.70 356225. 0.5823
|
|
27.54 0.1653 0.4403 0.0684 0.0257 5.454 42.971 32.701 4067.140 4.855 145.454 3.647 0.70 356532. 0.5562
|
|
30.99 0.1859 0.4809 0.0661 0.0255 5.423 42.728 31.565 4044.194 4.827 140.400 3.540 0.70 356856. 0.5305
|
|
34.43 0.2066 0.5186 0.0636 0.0253 5.376 42.352 30.366 4008.578 4.785 135.069 3.436 0.70 357199. 0.5050
|
|
37.87 0.2272 0.5536 0.0609 0.0250 5.309 41.830 29.104 3959.228 4.726 129.456 3.334 0.70 357559. 0.4797
|
|
41.31 0.2479 0.5859 0.0581 0.0246 5.224 41.157 27.781 3895.485 4.650 123.571 3.235 0.70 357939. 0.4547
|
|
44.76 0.2685 0.6155 0.0553 0.0241 5.119 40.328 26.401 3817.003 4.556 117.431 3.137 0.70 358337. 0.4299
|
|
48.20 0.2892 0.6426 0.0523 0.0235 4.993 39.341 24.967 3723.557 4.445 111.052 3.041 0.70 358755. 0.4053
|
|
51.64 0.3099 0.6670 0.0491 0.0228 4.848 38.193 23.483 3614.958 4.315 104.451 2.946 0.70 359192. 0.3808
|
|
55.08 0.3305 0.6888 0.0459 0.0220 4.682 36.884 21.953 3491.070 4.167 97.645 2.852 0.70 359648. 0.3564
|
|
58.53 0.3512 0.7076 0.0427 0.0212 4.495 35.413 20.380 3351.781 4.001 90.651 2.758 0.70 360124. 0.3321
|
|
61.97 0.3718 0.7234 0.0393 0.0202 4.287 33.778 18.769 3197.038 3.816 83.486 2.663 0.70 360620. 0.3077
|
|
65.41 0.3925 0.7359 0.0358 0.0191 4.059 31.980 17.124 3026.844 3.613 76.169 2.566 0.70 361135. 0.2832
|
|
68.86 0.4131 0.7445 0.0323 0.0179 3.810 30.019 15.449 2841.286 3.392 68.718 2.466 0.70 361672. 0.2585
|
|
72.30 0.4338 0.7485 0.0288 0.0167 3.541 27.898 13.749 2640.543 3.152 61.156 2.362 0.70 362228. 0.2336
|
|
75.74 0.4544 0.7471 0.0252 0.0153 3.252 25.620 12.029 2424.937 2.895 53.504 2.250 0.71 362805. 0.2081
|
|
79.18 0.4751 0.7384 0.0215 0.0139 2.943 23.190 10.294 2194.942 2.620 45.788 2.127 0.71 363403. 0.1820
|
|
82.63 0.4958 0.7200 0.0179 0.0123 2.617 20.615 8.551 1951.231 2.329 38.036 1.988 0.71 364022. 0.1550
|
|
86.07 0.5164 0.6874 0.0142 0.0107 2.273 17.905 6.807 1694.703 2.023 30.278 1.822 0.71 364661. 0.1268
|
|
89.51 0.5371 0.6326 0.0106 0.0090 1.913 15.072 5.070 1426.520 1.703 22.550 1.612 0.71 365322. 0.0968
|
|
92.96 0.5577 0.5389 0.0070 0.0073 1.540 12.130 3.348 1148.144 1.370 14.891 1.322 0.71 366004. 0.0645
|
|
96.40 0.5784 0.3673 0.0035 0.0054 1.155 9.100 1.650 861.283 1.028 7.340 0.869 0.71 366706. 0.0298
|
|
99.84 0.5990 -0.0124 -0.0001 0.0036 0.756 5.957 -0.035 563.828 0.673 -0.156 -0.028 0.71 367382. 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 0.0852 0.0259 7.840 54.905 51.503 5846.342 6.203 229.084 3.996 0.79 398788. 0.7648
|
|
3.86 0.0206 0.0660 0.0837 0.0261 7.903 55.345 50.625 5893.193 6.253 225.181 3.896 0.79 399010. 0.7394
|
|
7.73 0.0412 0.1287 0.0822 0.0263 7.958 55.728 49.682 5933.936 6.296 220.986 3.798 0.79 399249. 0.7139
|
|
11.59 0.0618 0.1880 0.0805 0.0265 8.002 56.041 48.672 5967.314 6.332 216.492 3.699 0.79 399504. 0.6884
|
|
15.46 0.0824 0.2441 0.0787 0.0266 8.035 56.274 47.592 5992.060 6.358 211.688 3.602 0.79 399777. 0.6628
|
|
19.32 0.1030 0.2970 0.0768 0.0266 8.055 56.412 46.439 6006.824 6.373 206.561 3.507 0.79 400067. 0.6373
|
|
23.19 0.1237 0.3468 0.0748 0.0267 8.060 56.444 45.212 6010.200 6.377 201.104 3.412 0.79 400376. 0.6119
|
|
27.05 0.1443 0.3936 0.0726 0.0266 8.047 56.355 43.909 6000.738 6.367 195.305 3.319 0.79 400704. 0.5866
|
|
30.91 0.1649 0.4374 0.0703 0.0265 8.015 56.132 42.527 5976.938 6.342 189.159 3.227 0.79 401051. 0.5613
|
|
34.78 0.1855 0.4783 0.0679 0.0263 7.962 55.759 41.065 5937.213 6.300 182.658 3.137 0.79 401418. 0.5362
|
|
38.64 0.2061 0.5165 0.0654 0.0261 7.885 55.220 39.521 5879.870 6.239 175.791 3.049 0.79 401805. 0.5112
|
|
42.51 0.2267 0.5519 0.0627 0.0257 7.782 54.500 37.894 5803.156 6.157 168.553 2.962 0.79 402213. 0.4863
|
|
46.37 0.2473 0.5848 0.0598 0.0253 7.652 53.586 36.185 5705.875 6.054 160.953 2.876 0.79 402641. 0.4615
|
|
50.24 0.2679 0.6150 0.0569 0.0248 7.493 52.473 34.400 5587.326 5.928 153.012 2.793 0.79 403091. 0.4368
|
|
54.10 0.2885 0.6427 0.0538 0.0242 7.305 51.157 32.543 5447.248 5.780 144.753 2.710 0.79 403562. 0.4123
|
|
57.96 0.3091 0.6678 0.0506 0.0234 7.088 49.636 30.620 5285.267 5.608 136.198 2.628 0.79 404054. 0.3878
|
|
61.83 0.3298 0.6901 0.0474 0.0226 6.841 47.906 28.635 5101.103 5.412 127.370 2.546 0.79 404568. 0.3634
|
|
65.69 0.3504 0.7097 0.0440 0.0217 6.564 45.968 26.594 4894.746 5.193 118.290 2.464 0.79 405104. 0.3389
|
|
69.56 0.3710 0.7262 0.0405 0.0207 6.258 43.823 24.501 4666.332 4.951 108.981 2.382 0.79 405662. 0.3144
|
|
73.42 0.3916 0.7393 0.0370 0.0196 5.922 41.473 22.362 4416.093 4.686 99.467 2.297 0.79 406242. 0.2897
|
|
77.29 0.4122 0.7484 0.0334 0.0184 5.558 38.922 20.183 4144.461 4.397 89.773 2.209 0.79 406845. 0.2647
|
|
81.15 0.4328 0.7527 0.0297 0.0171 5.166 36.177 17.969 3852.146 4.087 79.925 2.116 0.79 407470. 0.2392
|
|
85.02 0.4534 0.7510 0.0260 0.0157 4.747 33.246 15.727 3540.054 3.756 69.952 2.015 0.79 408118. 0.2131
|
|
88.88 0.4740 0.7414 0.0223 0.0142 4.304 30.141 13.464 3209.422 3.405 59.887 1.903 0.79 408789. 0.1862
|
|
92.74 0.4946 0.7210 0.0185 0.0127 3.838 26.877 11.188 2861.863 3.037 49.765 1.773 0.80 409483. 0.1582
|
|
96.61 0.5152 0.6847 0.0147 0.0111 3.352 23.473 8.909 2499.381 2.652 39.627 1.617 0.80 410201. 0.1287
|
|
100.47 0.5359 0.6241 0.0110 0.0094 2.849 19.951 6.636 2124.427 2.254 29.517 1.417 0.80 410942. 0.0973
|
|
104.34 0.5565 0.5224 0.0072 0.0077 2.333 16.340 4.381 1739.867 1.846 19.487 1.142 0.80 411707. 0.0638
|
|
108.20 0.5771 0.3438 0.0036 0.0060 1.809 12.668 2.156 1348.904 1.431 9.588 0.725 0.80 412493. 0.0284
|
|
112.07 0.5977 -0.0126 -0.0001 0.0042 1.272 8.906 -0.054 948.354 1.006 -0.238 -0.026 0.80 413255. 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 0.0876 0.0302 12.513 78.866 65.361 9330.792 8.910 290.724 3.177 0.87 443008. 0.6851
|
|
4.32 0.0207 0.0591 0.0861 0.0302 12.509 78.843 64.287 9328.073 8.908 285.947 3.126 0.87 443259. 0.6685
|
|
8.63 0.0414 0.1163 0.0846 0.0301 12.492 78.734 63.126 9315.176 8.895 280.785 3.074 0.87 443529. 0.6513
|
|
12.95 0.0622 0.1715 0.0829 0.0300 12.459 78.529 61.877 9290.885 8.872 275.229 3.021 0.87 443818. 0.6338
|
|
17.26 0.0829 0.2246 0.0811 0.0299 12.410 78.217 60.535 9253.966 8.837 269.260 2.967 0.87 444126. 0.6157
|
|
21.58 0.1036 0.2755 0.0792 0.0298 12.342 77.787 59.097 9203.111 8.788 262.864 2.913 0.87 444454. 0.5972
|
|
25.90 0.1243 0.3244 0.0771 0.0295 12.253 77.228 57.560 9137.012 8.725 256.027 2.857 0.87 444804. 0.5782
|
|
30.21 0.1450 0.3710 0.0749 0.0293 12.142 76.529 55.921 9054.307 8.646 248.738 2.801 0.87 445175. 0.5587
|
|
34.53 0.1657 0.4154 0.0726 0.0290 12.007 75.677 54.179 8953.535 8.550 240.987 2.745 0.87 445568. 0.5388
|
|
38.84 0.1865 0.4576 0.0701 0.0286 11.845 74.660 52.330 8833.132 8.435 232.765 2.687 0.87 445983. 0.5184
|
|
43.16 0.2072 0.4974 0.0675 0.0281 11.655 73.461 50.373 8691.263 8.300 224.060 2.629 0.87 446421. 0.4976
|
|
47.48 0.2279 0.5349 0.0647 0.0276 11.433 72.063 48.306 8525.919 8.142 214.863 2.570 0.87 446882. 0.4764
|
|
51.79 0.2486 0.5699 0.0618 0.0270 11.178 70.455 46.130 8335.642 7.960 205.186 2.510 0.88 447366. 0.4547
|
|
56.11 0.2693 0.6025 0.0587 0.0263 10.889 68.629 43.852 8119.658 7.754 195.056 2.450 0.88 447874. 0.4327
|
|
60.42 0.2900 0.6327 0.0556 0.0255 10.564 66.581 41.480 7877.298 7.522 184.501 2.388 0.88 448406. 0.4103
|
|
64.74 0.3108 0.6598 0.0523 0.0246 10.209 64.345 39.018 7612.780 7.270 173.551 2.325 0.88 448961. 0.3873
|
|
69.06 0.3315 0.6833 0.0489 0.0237 9.830 61.954 36.474 7329.887 7.000 162.234 2.257 0.88 449541. 0.3635
|
|
73.37 0.3522 0.7028 0.0453 0.0227 9.425 59.402 33.853 7027.942 6.711 150.579 2.185 0.88 450145. 0.3390
|
|
77.69 0.3729 0.7175 0.0417 0.0217 8.997 56.706 31.164 6709.037 6.407 138.616 2.107 0.88 450774. 0.3137
|
|
82.00 0.3936 0.7270 0.0381 0.0206 8.546 53.866 28.412 6372.939 6.086 126.377 2.022 0.88 451427. 0.2875
|
|
86.32 0.4143 0.7309 0.0343 0.0194 8.064 50.827 25.607 6013.487 5.742 113.900 1.931 0.88 452106. 0.2607
|
|
90.64 0.4351 0.7281 0.0305 0.0182 7.554 47.611 22.757 5632.993 5.379 101.221 1.832 0.88 452809. 0.2331
|
|
94.95 0.4558 0.7167 0.0266 0.0169 7.020 44.244 19.869 5234.552 4.999 88.379 1.722 0.88 453538. 0.2047
|
|
99.27 0.4765 0.6942 0.0227 0.0156 6.465 40.750 16.956 4821.209 4.604 75.419 1.595 0.88 454292. 0.1752
|
|
103.58 0.4972 0.6571 0.0188 0.0142 5.896 37.159 14.026 4396.400 4.198 62.388 1.447 0.88 455072. 0.1445
|
|
107.90 0.5179 0.6004 0.0149 0.0128 5.316 33.507 11.094 3964.261 3.786 49.346 1.269 0.88 455878. 0.1128
|
|
112.22 0.5386 0.5167 0.0109 0.0114 4.733 29.830 8.173 3529.215 3.370 36.353 1.050 0.89 456711. 0.0801
|
|
116.53 0.5594 0.3951 0.0071 0.0100 4.152 26.167 5.278 3095.840 2.956 23.478 0.773 0.89 457569. 0.0474
|
|
120.85 0.5801 0.2185 0.0033 0.0086 3.578 22.554 2.427 2668.401 2.548 10.794 0.412 0.89 458451. 0.0171
|
|
125.16 0.6008
|
|
|
|
|
|
|
|
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 0.0883 0.0380 20.955 120.071 79.801 15626.360 13.566 354.955 2.316 0.96 487270. 0.5519
|
|
4.91 0.0214 0.0493 0.0870 0.0379 20.909 119.807 78.630 15592.014 13.536 349.748 2.287 0.96 487550. 0.5410
|
|
9.82 0.0429 0.0973 0.0856 0.0377 20.825 119.323 77.341 15529.098 13.481 344.014 2.259 0.96 487852. 0.5299
|
|
14.74 0.0643 0.1441 0.0841 0.0375 20.699 118.600 75.928 15434.908 13.399 337.728 2.231 0.96 488178. 0.5185
|
|
19.65 0.0857 0.1898 0.0823 0.0372 20.527 117.618 74.383 15307.202 13.288 330.857 2.204 0.96 488528. 0.5070
|
|
24.56 0.1072 0.2344 0.0805 0.0368 20.309 116.365 72.701 15144.111 13.147 323.372 2.177 0.96 488903. 0.4952
|
|
29.47 0.1286 0.2779 0.0785 0.0363 20.041 114.830 70.874 14944.264 12.973 315.249 2.151 0.96 489304. 0.4830
|
|
34.38 0.1500 0.3203 0.0763 0.0357 19.722 113.004 68.900 14706.650 12.767 306.466 2.125 0.96 489731. 0.4704
|
|
39.30 0.1715 0.3616 0.0739 0.0351 19.352 110.883 66.773 14430.636 12.527 297.008 2.099 0.96 490185. 0.4574
|
|
44.21 0.1929 0.4016 0.0714 0.0343 18.929 108.460 64.490 14115.320 12.254 286.853 2.072 0.96 490666. 0.4439
|
|
49.12 0.2143 0.4404 0.0687 0.0334 18.454 105.738 62.049 13761.070 11.946 275.993 2.045 0.96 491175. 0.4297
|
|
54.03 0.2358 0.4778 0.0658 0.0325 17.926 102.715 59.447 13367.624 11.605 264.420 2.017 0.96 491712. 0.4148
|
|
58.94 0.2572 0.5136 0.0628 0.0314 17.347 99.397 56.691 12935.805 11.230 252.160 1.988 0.96 492277. 0.3992
|
|
63.86 0.2786 0.5478 0.0595 0.0303 16.719 95.797 53.790 12467.370 10.823 239.258 1.957 0.96 492870. 0.3828
|
|
68.77 0.3001 0.5801 0.0562 0.0291 16.044 91.929 50.756 11963.905 10.386 225.762 1.924 0.96 493492. 0.3656
|
|
73.68 0.3215 0.6103 0.0527 0.0278 15.323 87.801 47.598 11426.620 9.920 211.718 1.889 0.96 494142. 0.3477
|
|
78.59 0.3429 0.6370 0.0491 0.0264 14.583 83.559 44.326 10874.556 9.440 197.164 1.849 0.97 494820. 0.3283
|
|
83.50 0.3644 0.6580 0.0453 0.0251 13.856 79.395 40.948 10332.664 8.970 182.138 1.797 0.97 495527. 0.3068
|
|
88.41 0.3858 0.6717 0.0415 0.0238 13.153 75.363 37.475 9807.954 8.514 166.690 1.733 0.97 496263. 0.2830
|
|
93.33 0.4072 0.6700 0.0375 0.0228 12.594 72.160 33.908 9391.055 8.153 150.823 1.638 0.97 497029. 0.2543
|
|
98.24 0.4287 0.6570 0.0335 0.0219 12.069 69.156 30.272 9000.182 7.813 134.650 1.526 0.97 497823. 0.2239
|
|
103.15 0.4501 0.6340 0.0294 0.0209 11.534 66.090 26.587 8601.202 7.467 118.260 1.402 0.97 498646. 0.1928
|
|
108.06 0.4715 0.5994 0.0253 0.0199 10.995 63.002 22.871 8199.321 7.118 101.730 1.265 0.97 499500. 0.1614
|
|
112.97 0.4930 0.5514 0.0212 0.0189 10.459 59.930 19.143 7799.513 6.771 85.149 1.113 0.97 500383. 0.1299
|
|
117.89 0.5144 0.4881 0.0171 0.0180 9.934 56.921 15.426 7407.835 6.431 68.617 0.945 0.97 501296. 0.0989
|
|
122.80 0.5358 0.4082 0.0130 0.0171 9.422 53.989 11.747 7026.297 6.100 52.249 0.758 0.97 502240. 0.0693
|
|
127.71 0.5573 0.3101 0.0090 0.0162 8.928 51.157 8.131 6657.710 5.780 36.165 0.554 0.97 503216. 0.0421
|
|
132.62 0.5787 0.1925 0.0051 0.0153 8.453 48.432 4.602 6303.040 5.472 20.468 0.331 0.98 504226. 0.0189
|
|
137.53 0.6001 0.0528 0.0013 0.0145 7.978 45.714 1.150 5949.406 5.165 5.114 0.088 0.98 505288. 0.0025
|
|
142.45 0.6216
|
|
|
|
|
|
|