427 lines
76 KiB
Plaintext
427 lines
76 KiB
Plaintext
21x10PN (21x10PN.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 0.0882 0.0337 0.011 0.698 0.546 8.252 0.079 2.430 30.030 0.08 49112. 0.6202
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0.44 0.0220 0.0562 0.0866 0.0340 0.011 0.704 0.537 8.325 0.079 2.388 29.252 0.08 49142. 0.5989
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0.88 0.0441 0.1094 0.0850 0.0342 0.011 0.709 0.527 8.391 0.080 2.343 28.475 0.08 49174. 0.5775
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1.31 0.0661 0.1596 0.0832 0.0345 0.011 0.714 0.516 8.447 0.081 2.295 27.702 0.08 49209. 0.5560
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1.75 0.0881 0.2069 0.0814 0.0347 0.011 0.718 0.504 8.494 0.081 2.243 26.933 0.08 49246. 0.5345
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2.19 0.1101 0.2513 0.0794 0.0348 0.011 0.721 0.492 8.529 0.081 2.189 26.170 0.08 49285. 0.5129
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2.63 0.1322 0.2928 0.0773 0.0349 0.011 0.723 0.479 8.549 0.082 2.130 25.413 0.08 49328. 0.4914
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3.07 0.1542 0.3315 0.0750 0.0349 0.011 0.723 0.465 8.553 0.082 2.069 24.661 0.08 49372. 0.4699
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3.50 0.1762 0.3674 0.0726 0.0348 0.011 0.722 0.450 8.539 0.082 2.003 23.916 0.08 49420. 0.4484
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3.94 0.1983 0.4006 0.0701 0.0347 0.011 0.719 0.435 8.505 0.081 1.933 23.177 0.08 49471. 0.4269
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4.38 0.2203 0.4310 0.0675 0.0345 0.011 0.714 0.418 8.450 0.081 1.860 22.443 0.08 49525. 0.4055
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4.82 0.2423 0.4587 0.0647 0.0342 0.011 0.708 0.401 8.372 0.080 1.783 21.713 0.08 49581. 0.3841
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5.26 0.2643 0.4836 0.0617 0.0337 0.011 0.699 0.383 8.271 0.079 1.702 20.985 0.08 49641. 0.3627
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5.69 0.2864 0.5058 0.0587 0.0332 0.011 0.689 0.364 8.146 0.078 1.618 20.258 0.08 49703. 0.3414
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6.13 0.3084 0.5250 0.0556 0.0326 0.011 0.676 0.344 7.997 0.076 1.532 19.528 0.08 49769. 0.3202
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6.57 0.3304 0.5414 0.0523 0.0319 0.010 0.661 0.324 7.824 0.075 1.442 18.793 0.08 49838. 0.2990
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7.01 0.3524 0.5546 0.0490 0.0311 0.010 0.645 0.303 7.626 0.073 1.350 18.048 0.08 49910. 0.2778
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7.45 0.3745 0.5644 0.0455 0.0302 0.010 0.626 0.282 7.402 0.071 1.255 17.289 0.08 49986. 0.2566
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7.89 0.3965 0.5707 0.0420 0.0292 0.010 0.605 0.260 7.153 0.068 1.158 16.510 0.08 50064. 0.2354
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8.32 0.4185 0.5730 0.0384 0.0281 0.009 0.581 0.238 6.877 0.066 1.059 15.703 0.08 50146. 0.2141
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8.76 0.4406 0.5707 0.0348 0.0268 0.009 0.556 0.215 6.575 0.063 0.958 14.858 0.08 50232. 0.1927
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9.20 0.4626 0.5631 0.0310 0.0255 0.008 0.528 0.192 6.246 0.060 0.855 13.963 0.08 50320. 0.1711
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9.64 0.4846 0.5493 0.0272 0.0240 0.008 0.498 0.169 5.890 0.056 0.751 13.001 0.08 50412. 0.1493
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10.08 0.5066 0.5278 0.0234 0.0225 0.007 0.465 0.145 5.507 0.053 0.645 11.948 0.08 50508. 0.1272
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10.51 0.5287 0.4965 0.0195 0.0208 0.007 0.431 0.121 5.097 0.049 0.538 10.772 0.08 50606. 0.1047
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10.95 0.5507 0.4525 0.0156 0.0190 0.006 0.394 0.097 4.661 0.045 0.431 9.424 0.08 50709. 0.0820
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11.39 0.5727 0.3911 0.0117 0.0171 0.006 0.355 0.073 4.200 0.040 0.323 7.833 0.08 50814. 0.0589
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11.83 0.5948 0.3051 0.0078 0.0152 0.005 0.314 0.048 3.714 0.035 0.214 5.884 0.08 50923. 0.0361
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12.27 0.6168 0.1817 0.0039 0.0131 0.004 0.271 0.024 3.205 0.031 0.106 3.379 0.08 51035. 0.0146
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12.70 0.6388 -0.0035 -0.0001 0.0109 0.004 0.226 0.000 2.673 0.026 -0.002 -0.063 0.09 51148. 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 0.0886 0.0305 0.080 2.529 2.197 59.832 0.286 9.772 16.655 0.17 98222. 0.6898
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0.88 0.0221 0.0625 0.0871 0.0308 0.081 2.556 2.159 60.473 0.289 9.603 16.194 0.17 98282. 0.6648
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1.76 0.0442 0.1214 0.0855 0.0311 0.082 2.580 2.118 61.058 0.292 9.423 15.737 0.17 98347. 0.6400
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2.64 0.0664 0.1769 0.0837 0.0314 0.083 2.602 2.075 61.573 0.294 9.230 15.285 0.17 98416. 0.6152
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3.52 0.0885 0.2290 0.0818 0.0316 0.083 2.620 2.029 62.005 0.296 9.023 14.840 0.17 98491. 0.5906
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4.40 0.1106 0.2777 0.0798 0.0318 0.084 2.634 1.979 62.338 0.298 8.804 14.401 0.17 98571. 0.5661
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5.28 0.1327 0.3233 0.0777 0.0319 0.084 2.644 1.927 62.556 0.299 8.569 13.969 0.17 98656. 0.5418
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6.16 0.1549 0.3657 0.0755 0.0320 0.084 2.647 1.871 62.642 0.299 8.320 13.544 0.17 98746. 0.5176
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7.04 0.1770 0.4051 0.0731 0.0319 0.084 2.645 1.811 62.579 0.299 8.056 13.127 0.17 98843. 0.4936
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7.92 0.1991 0.4415 0.0705 0.0318 0.084 2.635 1.748 62.352 0.298 7.776 12.717 0.17 98945. 0.4698
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8.80 0.2212 0.4750 0.0678 0.0316 0.083 2.618 1.682 61.947 0.296 7.480 12.313 0.17 99053. 0.4462
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9.68 0.2433 0.5056 0.0650 0.0313 0.082 2.593 1.612 61.355 0.293 7.170 11.916 0.17 99167. 0.4227
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10.56 0.2655 0.5334 0.0621 0.0309 0.081 2.560 1.539 60.569 0.289 6.845 11.524 0.17 99287. 0.3995
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11.44 0.2876 0.5585 0.0590 0.0304 0.080 2.518 1.463 59.584 0.284 6.508 11.137 0.17 99413. 0.3764
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12.32 0.3097 0.5807 0.0558 0.0298 0.078 2.468 1.384 58.397 0.279 6.158 10.753 0.17 99546. 0.3535
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13.20 0.3318 0.6000 0.0526 0.0291 0.076 2.409 1.303 57.003 0.272 5.797 10.371 0.17 99685. 0.3308
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14.08 0.3540 0.6164 0.0492 0.0283 0.074 2.341 1.220 55.397 0.265 5.426 9.987 0.17 99830. 0.3082
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14.96 0.3761 0.6296 0.0457 0.0273 0.072 2.264 1.134 53.576 0.256 5.045 9.601 0.17 99982. 0.2857
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15.84 0.3982 0.6394 0.0422 0.0263 0.069 2.178 1.046 51.535 0.246 4.654 9.209 0.17 100141. 0.2632
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16.72 0.4203 0.6455 0.0386 0.0251 0.066 2.082 0.957 49.271 0.235 4.256 8.808 0.17 100306. 0.2407
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17.60 0.4424 0.6473 0.0349 0.0239 0.063 1.977 0.865 46.780 0.223 3.849 8.391 0.17 100478. 0.2181
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18.48 0.4646 0.6442 0.0312 0.0225 0.059 1.862 0.773 44.060 0.210 3.436 7.953 0.17 100656. 0.1953
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19.36 0.4867 0.6350 0.0274 0.0210 0.055 1.737 0.678 41.110 0.196 3.017 7.483 0.17 100842. 0.1722
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20.24 0.5088 0.6183 0.0235 0.0193 0.051 1.603 0.583 37.930 0.181 2.592 6.969 0.17 101034. 0.1487
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21.12 0.5309 0.5916 0.0196 0.0176 0.046 1.459 0.486 34.522 0.165 2.163 6.390 0.17 101233. 0.1245
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22.00 0.5531 0.5512 0.0157 0.0158 0.041 1.305 0.389 30.889 0.147 1.731 5.716 0.17 101439. 0.0996
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22.88 0.5752 0.4908 0.0118 0.0138 0.036 1.143 0.292 27.039 0.129 1.298 4.894 0.17 101652. 0.0739
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23.76 0.5973 0.3990 0.0078 0.0117 0.031 0.971 0.194 22.982 0.110 0.864 3.832 0.17 101872. 0.0472
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24.64 0.6194 0.2533 0.0039 0.0096 0.025 0.792 0.097 18.730 0.089 0.431 2.346 0.17 102098. 0.0204
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25.52 0.6415 -0.0017 0.0000 0.0073 0.019 0.603 0.000 14.261 0.068 -0.002 -0.015 0.17 102320. 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 0.0891 0.0293 0.260 5.471 4.973 194.199 0.618 22.118 11.614 0.25 147328. 0.7236
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1.32 0.0222 0.0654 0.0876 0.0297 0.263 5.535 4.887 196.454 0.625 21.737 11.283 0.25 147418. 0.6969
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2.65 0.0443 0.1271 0.0860 0.0300 0.266 5.593 4.795 198.519 0.632 21.330 10.956 0.25 147516. 0.6704
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3.97 0.0665 0.1850 0.0842 0.0303 0.269 5.645 4.697 200.348 0.638 20.894 10.634 0.25 147621. 0.6440
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5.29 0.0887 0.2393 0.0823 0.0305 0.271 5.688 4.593 201.890 0.643 20.428 10.318 0.25 147733. 0.6178
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6.61 0.1109 0.2901 0.0803 0.0307 0.272 5.722 4.481 203.094 0.646 19.931 10.007 0.25 147853. 0.5919
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7.94 0.1330 0.3376 0.0782 0.0308 0.273 5.745 4.362 203.903 0.649 19.402 9.703 0.25 147982. 0.5662
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9.26 0.1552 0.3817 0.0759 0.0309 0.274 5.755 4.235 204.260 0.650 18.839 9.405 0.25 148118. 0.5408
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10.58 0.1774 0.4227 0.0735 0.0308 0.274 5.750 4.101 204.105 0.650 18.240 9.113 0.25 148263. 0.5156
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11.90 0.1995 0.4607 0.0710 0.0307 0.273 5.730 3.958 203.383 0.647 17.606 8.827 0.25 148417. 0.4907
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13.23 0.2217 0.4956 0.0683 0.0305 0.271 5.693 3.808 202.048 0.643 16.936 8.548 0.25 148580. 0.4660
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14.55 0.2439 0.5277 0.0654 0.0302 0.268 5.637 3.650 200.068 0.637 16.233 8.274 0.25 148752. 0.4416
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15.87 0.2661 0.5570 0.0625 0.0298 0.265 5.562 3.484 197.418 0.628 15.498 8.005 0.25 148933. 0.4175
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17.20 0.2882 0.5835 0.0594 0.0293 0.260 5.468 3.312 194.081 0.618 14.733 7.741 0.25 149123. 0.3936
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18.52 0.3104 0.6073 0.0562 0.0287 0.255 5.354 3.134 190.041 0.605 13.941 7.480 0.25 149323. 0.3700
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19.84 0.3326 0.6282 0.0529 0.0280 0.248 5.220 2.950 185.282 0.590 13.123 7.222 0.25 149533. 0.3466
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21.16 0.3547 0.6463 0.0495 0.0272 0.241 5.065 2.761 179.788 0.572 12.281 6.966 0.25 149752. 0.3234
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22.49 0.3769 0.6613 0.0460 0.0262 0.233 4.889 2.567 173.544 0.552 11.417 6.708 0.25 149981. 0.3003
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23.81 0.3991 0.6731 0.0425 0.0252 0.223 4.692 2.368 166.536 0.530 10.533 6.449 0.25 150220. 0.2773
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25.13 0.4212 0.6815 0.0388 0.0240 0.213 4.473 2.165 158.752 0.505 9.629 6.185 0.25 150468. 0.2543
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26.45 0.4434 0.6858 0.0351 0.0227 0.201 4.231 1.958 150.178 0.478 8.709 5.913 0.25 150727. 0.2312
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27.78 0.4656 0.6854 0.0313 0.0213 0.189 3.967 1.747 140.808 0.448 7.773 5.629 0.25 150997. 0.2079
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29.10 0.4878 0.6794 0.0275 0.0197 0.175 3.681 1.534 130.636 0.416 6.823 5.326 0.25 151276. 0.1843
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30.42 0.5099 0.6661 0.0236 0.0181 0.160 3.371 1.318 119.662 0.381 5.861 4.995 0.25 151566. 0.1602
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31.74 0.5321 0.6432 0.0197 0.0163 0.145 3.040 1.099 107.894 0.343 4.890 4.621 0.25 151866. 0.1354
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33.07 0.5543 0.6065 0.0158 0.0144 0.128 2.686 0.879 95.346 0.303 3.912 4.184 0.25 152176. 0.1096
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34.39 0.5764 0.5490 0.0118 0.0124 0.110 2.311 0.659 82.042 0.261 2.930 3.642 0.25 152497. 0.0826
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35.71 0.5986 0.4572 0.0079 0.0103 0.091 1.916 0.438 68.019 0.217 1.948 2.920 0.25 152827. 0.0540
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37.04 0.6208 0.3009 0.0039 0.0081 0.072 1.502 0.218 53.319 0.170 0.969 1.853 0.25 153167. 0.0242
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38.36 0.6430 -0.0063 -0.0001 0.0057 0.051 1.065 -0.003 37.808 0.120 -0.014 -0.037 0.26 153496. 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 0.0898 0.0289 0.607 9.562 8.908 452.515 1.080 39.623 8.929 0.33 196427. 0.7446
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1.77 0.0222 0.0671 0.0883 0.0292 0.614 9.678 8.755 458.008 1.093 38.944 8.671 0.33 196548. 0.7169
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3.53 0.0444 0.1303 0.0866 0.0295 0.621 9.784 8.592 463.045 1.105 38.217 8.416 0.33 196679. 0.6893
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5.30 0.0666 0.1897 0.0849 0.0298 0.627 9.879 8.417 467.510 1.116 37.439 8.166 0.33 196820. 0.6620
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7.06 0.0888 0.2453 0.0830 0.0300 0.632 9.959 8.230 471.286 1.125 36.607 7.921 0.33 196970. 0.6349
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8.83 0.1110 0.2973 0.0810 0.0302 0.636 10.021 8.030 474.246 1.132 35.720 7.680 0.33 197131. 0.6081
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10.60 0.1332 0.3459 0.0788 0.0304 0.639 10.064 7.818 476.254 1.137 34.773 7.445 0.33 197303. 0.5817
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12.36 0.1554 0.3911 0.0766 0.0304 0.640 10.083 7.591 477.169 1.139 33.765 7.216 0.33 197486. 0.5555
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14.13 0.1776 0.4331 0.0741 0.0304 0.639 10.076 7.350 476.851 1.138 32.694 6.991 0.33 197681. 0.5296
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15.90 0.1998 0.4719 0.0715 0.0303 0.637 10.041 7.095 475.165 1.134 31.559 6.773 0.33 197887. 0.5041
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17.66 0.2220 0.5078 0.0688 0.0301 0.633 9.974 6.825 471.998 1.127 30.359 6.559 0.33 198105. 0.4788
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19.43 0.2442 0.5409 0.0660 0.0298 0.627 9.874 6.542 467.269 1.116 29.099 6.350 0.33 198335. 0.4538
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21.19 0.2664 0.5711 0.0630 0.0294 0.618 9.740 6.246 460.920 1.100 27.782 6.146 0.33 198577. 0.4292
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22.96 0.2886 0.5985 0.0599 0.0289 0.607 9.570 5.938 452.909 1.081 26.411 5.946 0.33 198832. 0.4049
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24.73 0.3108 0.6233 0.0567 0.0283 0.594 9.365 5.618 443.193 1.058 24.990 5.750 0.33 199100. 0.3808
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26.49 0.3330 0.6453 0.0533 0.0275 0.579 9.123 5.288 431.736 1.031 23.523 5.556 0.34 199380. 0.3570
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28.26 0.3552 0.6645 0.0499 0.0267 0.561 8.843 4.949 418.500 0.999 22.014 5.364 0.34 199673. 0.3334
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30.02 0.3774 0.6808 0.0464 0.0257 0.541 8.525 4.601 403.446 0.963 20.464 5.172 0.34 199980. 0.3100
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31.79 0.3996 0.6941 0.0428 0.0246 0.518 8.168 4.244 386.541 0.923 18.878 4.980 0.34 200299. 0.2867
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33.56 0.4219 0.7040 0.0391 0.0234 0.493 7.771 3.880 367.751 0.878 17.257 4.785 0.34 200632. 0.2634
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35.32 0.4441 0.7101 0.0354 0.0221 0.465 7.333 3.509 347.050 0.829 15.606 4.585 0.34 200979. 0.2400
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37.09 0.4663 0.7118 0.0316 0.0207 0.435 6.855 3.131 324.417 0.774 13.927 4.378 0.34 201339. 0.2164
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38.85 0.4885 0.7081 0.0277 0.0191 0.402 6.336 2.748 299.841 0.716 12.223 4.157 0.34 201712. 0.1925
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40.62 0.5107 0.6975 0.0238 0.0174 0.367 5.775 2.360 273.323 0.653 10.498 3.917 0.34 202100. 0.1681
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42.39 0.5329 0.6776 0.0199 0.0156 0.328 5.174 1.969 244.878 0.585 8.756 3.646 0.34 202501. 0.1429
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44.15 0.5551 0.6442 0.0159 0.0137 0.288 4.533 1.574 214.544 0.512 7.002 3.328 0.34 202916. 0.1167
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45.92 0.5773 0.5899 0.0119 0.0116 0.245 3.854 1.178 182.380 0.435 5.241 2.930 0.34 203345. 0.0889
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47.69 0.5995 0.4996 0.0079 0.0095 0.199 3.137 0.782 148.476 0.354 3.480 2.390 0.34 203787. 0.0591
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49.45 0.6217 0.3376 0.0039 0.0072 0.151 2.386 0.388 112.935 0.270 1.725 1.557 0.34 204242. 0.0271
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51.22 0.6439 -0.0136 -0.0001 0.0048 0.101 1.590 -0.010 75.263 0.180 -0.045 -0.061 0.34 204669. 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 0.0907 0.0287 1.180 14.871 14.055 879.699 1.680 62.518 7.247 0.42 245517. 0.7591
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2.21 0.0222 0.0681 0.0892 0.0291 1.194 15.056 13.816 890.667 1.701 61.456 7.036 0.42 245669. 0.7307
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4.42 0.0444 0.1323 0.0875 0.0294 1.208 15.226 13.560 900.727 1.720 60.315 6.828 0.42 245833. 0.7026
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6.63 0.0666 0.1925 0.0857 0.0297 1.220 15.377 13.286 909.644 1.737 59.094 6.624 0.42 246010. 0.6747
|
|
8.84 0.0889 0.2489 0.0838 0.0299 1.230 15.505 12.992 917.187 1.752 57.788 6.425 0.42 246199. 0.6471
|
|
11.04 0.1111 0.3016 0.0818 0.0301 1.238 15.605 12.678 923.105 1.763 56.393 6.230 0.42 246402. 0.6198
|
|
13.25 0.1333 0.3509 0.0797 0.0303 1.243 15.673 12.344 927.127 1.771 54.905 6.039 0.42 246617. 0.5928
|
|
15.46 0.1555 0.3968 0.0774 0.0303 1.246 15.704 11.987 928.976 1.774 53.320 5.853 0.42 246847. 0.5662
|
|
17.67 0.1777 0.4394 0.0749 0.0303 1.245 15.694 11.608 928.370 1.773 51.634 5.671 0.42 247091. 0.5399
|
|
19.88 0.1999 0.4789 0.0723 0.0302 1.241 15.637 11.206 925.041 1.767 49.846 5.495 0.42 247350. 0.5140
|
|
22.09 0.2222 0.5154 0.0696 0.0300 1.232 15.531 10.782 918.764 1.755 47.957 5.323 0.42 247624. 0.4883
|
|
24.30 0.2444 0.5491 0.0667 0.0297 1.219 15.373 10.335 909.376 1.737 45.970 5.155 0.42 247912. 0.4630
|
|
26.51 0.2666 0.5800 0.0637 0.0293 1.203 15.159 9.868 896.761 1.713 43.893 4.991 0.42 248216. 0.4381
|
|
28.72 0.2888 0.6082 0.0605 0.0288 1.181 14.890 9.382 880.832 1.682 41.730 4.831 0.42 248536. 0.4134
|
|
30.93 0.3110 0.6337 0.0573 0.0281 1.155 14.563 8.878 861.510 1.645 39.488 4.674 0.42 248872. 0.3891
|
|
33.13 0.3332 0.6565 0.0539 0.0274 1.125 14.178 8.357 838.718 1.602 37.174 4.520 0.42 249223. 0.3651
|
|
35.34 0.3555 0.6766 0.0505 0.0265 1.089 13.733 7.822 812.384 1.552 34.791 4.367 0.42 249591. 0.3413
|
|
37.55 0.3777 0.6940 0.0469 0.0255 1.049 13.227 7.272 782.432 1.494 32.344 4.215 0.42 249975. 0.3176
|
|
39.76 0.3999 0.7083 0.0433 0.0244 1.004 12.658 6.709 748.795 1.430 29.840 4.064 0.42 250375. 0.2941
|
|
41.97 0.4221 0.7195 0.0396 0.0232 0.954 12.026 6.133 711.407 1.359 27.282 3.910 0.42 250792. 0.2706
|
|
44.18 0.4443 0.7271 0.0358 0.0219 0.899 11.330 5.547 670.214 1.280 24.674 3.754 0.42 251226. 0.2471
|
|
46.39 0.4665 0.7305 0.0320 0.0204 0.838 10.568 4.951 625.177 1.194 22.022 3.592 0.42 251677. 0.2233
|
|
48.60 0.4888 0.7288 0.0280 0.0188 0.773 9.742 4.346 576.271 1.101 19.331 3.421 0.42 252145. 0.1992
|
|
50.81 0.5110 0.7205 0.0241 0.0171 0.702 8.849 3.733 523.499 1.000 16.606 3.235 0.42 252630. 0.1746
|
|
53.02 0.5332 0.7032 0.0201 0.0152 0.626 7.893 3.115 466.894 0.892 13.854 3.026 0.42 253133. 0.1492
|
|
55.22 0.5554 0.6730 0.0161 0.0133 0.545 6.872 2.491 406.528 0.776 11.082 2.780 0.42 253652. 0.1226
|
|
57.43 0.5776 0.6221 0.0120 0.0112 0.459 5.790 1.866 342.521 0.654 8.300 2.471 0.42 254189. 0.0943
|
|
59.64 0.5998 0.5348 0.0080 0.0090 0.369 4.650 1.240 275.051 0.525 5.517 2.045 0.42 254743. 0.0636
|
|
61.85 0.6220 0.3713 0.0040 0.0067 0.274 3.454 0.617 204.329 0.390 2.744 1.369 0.42 255311. 0.0300
|
|
64.06 0.6443 -0.0133 -0.0001 0.0042 0.173 2.184 -0.013 129.168 0.247 -0.060 -0.047 0.43 255837. 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 0.0918 0.0288 2.047 21.507 20.488 1526.752 2.430 91.132 6.087 0.50 294594. 0.7698
|
|
2.67 0.0224 0.0692 0.0903 0.0292 2.074 21.782 20.141 1546.266 2.461 89.585 5.908 0.50 294779. 0.7408
|
|
5.34 0.0448 0.1343 0.0886 0.0295 2.098 22.034 19.767 1564.130 2.489 87.923 5.732 0.50 294979. 0.7121
|
|
8.02 0.0672 0.1954 0.0868 0.0298 2.119 22.257 19.366 1579.927 2.515 86.140 5.560 0.50 295194. 0.6836
|
|
10.69 0.0896 0.2526 0.0849 0.0301 2.137 22.444 18.937 1593.239 2.536 84.231 5.391 0.50 295425. 0.6555
|
|
13.36 0.1120 0.3061 0.0828 0.0303 2.150 22.590 18.478 1603.608 2.552 82.189 5.226 0.50 295671. 0.6277
|
|
16.03 0.1344 0.3560 0.0806 0.0304 2.160 22.688 17.987 1610.559 2.563 80.008 5.066 0.50 295935. 0.6003
|
|
18.70 0.1568 0.4025 0.0783 0.0305 2.164 22.731 17.464 1613.587 2.568 77.681 4.909 0.50 296215. 0.5732
|
|
21.38 0.1792 0.4458 0.0758 0.0305 2.162 22.711 16.908 1612.184 2.566 75.205 4.757 0.50 296512. 0.5465
|
|
24.05 0.2015 0.4859 0.0731 0.0303 2.154 22.622 16.316 1605.872 2.556 72.576 4.609 0.50 296828. 0.5201
|
|
26.72 0.2239 0.5230 0.0703 0.0301 2.138 22.458 15.692 1594.245 2.537 69.796 4.464 0.50 297162. 0.4941
|
|
29.39 0.2463 0.5572 0.0674 0.0298 2.115 22.216 15.034 1577.019 2.510 66.871 4.324 0.50 297514. 0.4685
|
|
32.06 0.2687 0.5886 0.0643 0.0294 2.084 21.891 14.346 1553.989 2.473 63.811 4.187 0.50 297884. 0.4431
|
|
34.74 0.2911 0.6173 0.0611 0.0288 2.045 21.483 13.630 1525.003 2.427 60.625 4.054 0.50 298274. 0.4182
|
|
37.41 0.3135 0.6434 0.0578 0.0281 1.998 20.989 12.887 1489.922 2.371 57.321 3.923 0.50 298683. 0.3935
|
|
40.08 0.3359 0.6668 0.0543 0.0274 1.943 20.407 12.120 1448.615 2.306 53.909 3.795 0.50 299112. 0.3691
|
|
42.75 0.3583 0.6875 0.0508 0.0265 1.879 19.735 11.330 1400.951 2.230 50.396 3.668 0.50 299560. 0.3450
|
|
45.42 0.3807 0.7055 0.0471 0.0254 1.806 18.972 10.519 1346.799 2.143 46.790 3.543 0.50 300028. 0.3210
|
|
48.10 0.4031 0.7205 0.0434 0.0243 1.725 18.117 9.689 1286.039 2.047 43.097 3.417 0.50 300516. 0.2972
|
|
50.77 0.4255 0.7324 0.0396 0.0230 1.634 17.166 8.841 1218.557 1.939 39.325 3.291 0.50 301024. 0.2734
|
|
53.44 0.4479 0.7408 0.0358 0.0216 1.534 16.119 7.977 1144.261 1.821 35.480 3.162 0.50 301553. 0.2495
|
|
56.11 0.4703 0.7449 0.0318 0.0201 1.426 14.976 7.098 1063.082 1.692 31.570 3.028 0.51 302103. 0.2254
|
|
58.78 0.4927 0.7440 0.0278 0.0184 1.307 13.735 6.206 974.984 1.552 27.603 2.887 0.51 302673. 0.2009
|
|
61.46 0.5151 0.7364 0.0238 0.0166 1.180 12.396 5.303 879.979 1.401 23.586 2.733 0.51 303264. 0.1759
|
|
64.13 0.5375 0.7195 0.0197 0.0147 1.043 10.962 4.391 778.136 1.238 19.530 2.559 0.51 303876. 0.1498
|
|
66.80 0.5599 0.6889 0.0156 0.0126 0.898 9.433 3.473 669.600 1.066 15.447 2.352 0.51 304509. 0.1225
|
|
69.47 0.5822 0.6356 0.0114 0.0105 0.744 7.813 2.552 554.609 0.883 11.350 2.087 0.51 305163. 0.0931
|
|
72.14 0.6046 0.5397 0.0073 0.0082 0.581 6.107 1.631 433.504 0.690 7.254 1.706 0.51 305837. 0.0609
|
|
74.82 0.6270 0.3463 0.0032 0.0058 0.411 4.320 0.714 306.645 0.488 3.175 1.056 0.51 306528. 0.0249
|
|
77.49 0.6494
|
|
|
|
|
|
|
|
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 0.0932 0.0292 3.291 29.631 28.309 2454.028 3.348 125.919 5.232 0.58 343653. 0.7779
|
|
3.09 0.0222 0.0689 0.0917 0.0296 3.333 30.012 27.838 2485.552 3.391 123.825 5.080 0.58 343869. 0.7489
|
|
6.19 0.0445 0.1338 0.0900 0.0299 3.372 30.360 27.332 2514.393 3.430 121.572 4.930 0.58 344103. 0.7202
|
|
9.28 0.0667 0.1947 0.0882 0.0302 3.406 30.668 26.788 2539.885 3.465 119.154 4.784 0.58 344353. 0.6918
|
|
12.38 0.0889 0.2518 0.0863 0.0305 3.435 30.928 26.206 2561.367 3.494 116.563 4.641 0.58 344621. 0.6638
|
|
15.47 0.1112 0.3053 0.0842 0.0307 3.457 31.130 25.582 2578.131 3.517 113.789 4.501 0.58 344908. 0.6360
|
|
18.57 0.1334 0.3553 0.0820 0.0308 3.472 31.266 24.916 2589.413 3.532 110.825 4.364 0.58 345214. 0.6087
|
|
21.66 0.1556 0.4019 0.0797 0.0309 3.479 31.327 24.204 2594.416 3.539 107.661 4.232 0.58 345540. 0.5817
|
|
24.76 0.1779 0.4453 0.0772 0.0308 3.476 31.302 23.447 2592.345 3.536 104.292 4.102 0.58 345885. 0.5550
|
|
27.85 0.2001 0.4856 0.0746 0.0307 3.463 31.182 22.642 2582.429 3.523 100.713 3.977 0.58 346252. 0.5287
|
|
30.95 0.2223 0.5230 0.0718 0.0305 3.438 30.960 21.791 2564.017 3.498 96.925 3.855 0.58 346638. 0.5028
|
|
34.04 0.2446 0.5576 0.0688 0.0302 3.402 30.629 20.894 2536.631 3.460 92.938 3.736 0.58 347046. 0.4772
|
|
37.14 0.2668 0.5895 0.0657 0.0297 3.352 30.186 19.955 2499.953 3.410 88.762 3.621 0.59 347476. 0.4519
|
|
40.23 0.2890 0.6187 0.0625 0.0292 3.291 29.628 18.977 2453.737 3.347 84.411 3.508 0.59 347927. 0.4270
|
|
43.33 0.3113 0.6454 0.0591 0.0285 3.215 28.952 17.963 2397.775 3.271 79.897 3.398 0.59 348400. 0.4024
|
|
46.42 0.3335 0.6695 0.0557 0.0277 3.127 28.156 16.914 2331.865 3.181 75.233 3.290 0.59 348896. 0.3781
|
|
49.52 0.3557 0.6911 0.0521 0.0268 3.025 27.238 15.834 2255.807 3.077 70.429 3.184 0.59 349414. 0.3540
|
|
52.61 0.3779 0.7101 0.0485 0.0258 2.909 26.195 14.724 2169.403 2.959 65.495 3.079 0.59 349955. 0.3301
|
|
55.71 0.4002 0.7263 0.0447 0.0247 2.779 25.024 13.588 2072.466 2.827 60.440 2.974 0.59 350519. 0.3063
|
|
58.80 0.4224 0.7395 0.0409 0.0234 2.635 23.724 12.427 1964.817 2.680 55.275 2.869 0.59 351106. 0.2826
|
|
61.90 0.4446 0.7495 0.0370 0.0220 2.476 22.293 11.243 1846.305 2.519 50.008 2.762 0.59 351716. 0.2588
|
|
64.99 0.4669 0.7556 0.0331 0.0204 2.302 20.730 10.038 1716.817 2.342 44.650 2.652 0.59 352350. 0.2348
|
|
68.09 0.4891 0.7571 0.0290 0.0188 2.114 19.033 8.815 1576.289 2.150 39.209 2.536 0.59 353008. 0.2104
|
|
71.18 0.5113 0.7526 0.0249 0.0169 1.911 17.203 7.576 1424.725 1.944 33.699 2.412 0.59 353689. 0.1855
|
|
74.28 0.5336 0.7400 0.0208 0.0150 1.693 15.241 6.324 1262.214 1.722 28.131 2.273 0.59 354395. 0.1597
|
|
77.37 0.5558 0.7153 0.0167 0.0130 1.460 13.149 5.063 1088.967 1.486 22.521 2.109 0.59 355124. 0.1326
|
|
80.47 0.5780 0.6710 0.0125 0.0108 1.214 10.932 3.796 905.328 1.235 16.887 1.902 0.59 355877. 0.1036
|
|
83.56 0.6003 0.5903 0.0083 0.0085 0.955 8.595 2.529 711.812 0.971 11.249 1.612 0.59 356654. 0.0716
|
|
86.66 0.6225 0.4284 0.0042 0.0061 0.683 6.146 1.266 509.029 0.694 5.630 1.128 0.59 357452. 0.0355
|
|
89.75 0.6447 -0.0101 -0.0001 0.0035 0.393 3.535 -0.017 292.748 0.399 -0.074 -0.026 0.60 358169. 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 0.0949 0.0298 5.011 39.479 37.660 3736.640 4.460 167.511 4.571 0.67 392689. 0.7838
|
|
3.54 0.0223 0.0689 0.0934 0.0302 5.076 39.991 37.044 3785.128 4.518 164.771 4.439 0.67 392939. 0.7549
|
|
7.08 0.0445 0.1338 0.0917 0.0305 5.135 40.459 36.379 3829.404 4.571 161.816 4.309 0.67 393208. 0.7262
|
|
10.62 0.0668 0.1948 0.0899 0.0308 5.188 40.871 35.665 3868.431 4.618 158.638 4.182 0.67 393497. 0.6978
|
|
14.17 0.0890 0.2520 0.0880 0.0311 5.232 41.217 34.898 3901.191 4.657 155.225 4.057 0.67 393807. 0.6697
|
|
17.71 0.1113 0.3055 0.0859 0.0313 5.266 41.486 34.075 3926.591 4.687 151.567 3.936 0.67 394138. 0.6420
|
|
21.25 0.1336 0.3556 0.0837 0.0314 5.288 41.664 33.195 3943.465 4.707 147.650 3.818 0.67 394491. 0.6146
|
|
24.79 0.1558 0.4024 0.0813 0.0315 5.298 41.739 32.254 3950.608 4.716 143.465 3.703 0.67 394866. 0.5876
|
|
28.33 0.1781 0.4460 0.0788 0.0315 5.293 41.699 31.251 3946.795 4.711 139.003 3.591 0.67 395265. 0.5610
|
|
31.87 0.2003 0.4866 0.0761 0.0313 5.271 41.531 30.184 3930.855 4.692 134.256 3.483 0.67 395686. 0.5346
|
|
35.41 0.2226 0.5243 0.0732 0.0311 5.232 41.223 29.053 3901.776 4.657 129.228 3.377 0.67 396132. 0.5086
|
|
38.95 0.2449 0.5593 0.0702 0.0308 5.175 40.770 27.862 3858.830 4.606 123.929 3.275 0.67 396602. 0.4830
|
|
42.50 0.2671 0.5915 0.0671 0.0303 5.098 40.164 26.613 3801.528 4.538 118.374 3.175 0.67 397097. 0.4577
|
|
46.04 0.2894 0.6212 0.0638 0.0297 5.001 39.403 25.311 3729.509 4.452 112.582 3.078 0.67 397616. 0.4327
|
|
49.58 0.3116 0.6484 0.0604 0.0290 4.885 38.484 23.959 3642.485 4.348 106.570 2.983 0.67 398161. 0.4080
|
|
53.12 0.3339 0.6731 0.0569 0.0282 4.747 37.403 22.562 3540.160 4.226 100.354 2.891 0.67 398730. 0.3836
|
|
56.66 0.3562 0.6953 0.0532 0.0273 4.589 36.157 21.121 3422.252 4.085 93.948 2.799 0.67 399326. 0.3595
|
|
60.20 0.3784 0.7150 0.0495 0.0262 4.410 34.744 19.642 3288.473 3.925 87.368 2.709 0.67 399948. 0.3355
|
|
63.74 0.4007 0.7320 0.0457 0.0250 4.209 33.160 18.126 3138.539 3.746 80.624 2.619 0.67 400595. 0.3116
|
|
67.28 0.4229 0.7462 0.0418 0.0237 3.986 31.402 16.576 2972.196 3.548 73.731 2.530 0.67 401269. 0.2878
|
|
70.83 0.4452 0.7571 0.0378 0.0222 3.740 29.469 14.995 2789.217 3.329 66.699 2.438 0.67 401970. 0.2638
|
|
74.37 0.4674 0.7645 0.0337 0.0206 3.472 27.358 13.387 2589.435 3.091 59.543 2.345 0.67 402698. 0.2397
|
|
77.91 0.4897 0.7673 0.0296 0.0189 3.182 25.069 11.753 2372.752 2.832 52.276 2.247 0.67 403453. 0.2152
|
|
81.45 0.5120 0.7645 0.0255 0.0170 2.869 22.601 10.097 2139.176 2.553 44.912 2.141 0.68 404234. 0.1901
|
|
84.99 0.5342 0.7537 0.0212 0.0151 2.533 19.956 8.424 1888.851 2.255 37.470 2.023 0.68 405043. 0.1640
|
|
88.53 0.5565 0.7312 0.0170 0.0129 2.175 17.138 6.738 1622.096 1.936 29.970 1.884 0.68 405880. 0.1366
|
|
92.07 0.5787 0.6894 0.0127 0.0107 1.796 14.152 5.044 1339.461 1.599 22.435 1.708 0.68 406743. 0.1072
|
|
95.61 0.6010 0.6111 0.0084 0.0083 1.397 11.007 3.348 1041.772 1.244 14.893 1.458 0.68 407633. 0.0745
|
|
99.16 0.6233 0.4478 0.0042 0.0058 0.979 7.713 1.658 730.025 0.871 7.374 1.030 0.68 408547. 0.0371
|
|
102.70 0.6455 -0.0476 -0.0002 0.0031 0.524 4.132 -0.091 391.093 0.467 -0.405 -0.106 0.68 409242. 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 0.0971 0.0309 7.415 51.929 48.736 5529.471 5.867 216.778 3.998 0.75 441693. 0.7798
|
|
4.02 0.0224 0.0685 0.0955 0.0313 7.499 52.516 47.954 5591.951 5.933 213.298 3.890 0.75 441978. 0.7526
|
|
8.03 0.0449 0.1332 0.0938 0.0316 7.575 53.050 47.106 5648.790 5.994 209.528 3.782 0.75 442287. 0.7254
|
|
12.05 0.0673 0.1941 0.0920 0.0319 7.642 53.517 46.191 5698.530 6.046 205.458 3.677 0.75 442618. 0.6982
|
|
16.06 0.0897 0.2515 0.0900 0.0321 7.697 53.904 45.205 5739.689 6.090 201.073 3.572 0.75 442974. 0.6711
|
|
20.08 0.1122 0.3054 0.0879 0.0323 7.739 54.194 44.145 5770.638 6.123 196.357 3.470 0.75 443353. 0.6441
|
|
24.09 0.1346 0.3558 0.0857 0.0324 7.764 54.373 43.007 5789.641 6.143 191.295 3.369 0.75 443759. 0.6174
|
|
28.11 0.1570 0.4030 0.0832 0.0324 7.771 54.421 41.788 5794.820 6.148 185.872 3.271 0.75 444190. 0.5908
|
|
32.12 0.1795 0.4470 0.0806 0.0324 7.757 54.322 40.485 5784.274 6.137 180.076 3.175 0.75 444647. 0.5644
|
|
36.14 0.2019 0.4881 0.0779 0.0322 7.719 54.058 39.096 5756.154 6.107 173.900 3.081 0.75 445131. 0.5382
|
|
40.15 0.2243 0.5262 0.0749 0.0320 7.656 53.614 37.623 5708.850 6.057 167.347 2.989 0.75 445643. 0.5123
|
|
44.17 0.2468 0.5615 0.0718 0.0316 7.565 52.978 36.068 5641.123 5.985 160.430 2.900 0.75 446182. 0.4866
|
|
48.18 0.2692 0.5942 0.0686 0.0311 7.446 52.142 34.436 5552.146 5.891 153.172 2.813 0.75 446750. 0.4613
|
|
52.20 0.2916 0.6244 0.0652 0.0305 7.297 51.101 32.733 5441.277 5.773 145.597 2.729 0.75 447345. 0.4362
|
|
56.21 0.3141 0.6520 0.0617 0.0297 7.118 49.849 30.964 5307.989 5.632 137.728 2.646 0.75 447969. 0.4114
|
|
60.23 0.3365 0.6772 0.0580 0.0288 6.909 48.383 29.134 5151.827 5.466 129.587 2.565 0.75 448622. 0.3868
|
|
64.24 0.3589 0.7000 0.0543 0.0278 6.668 46.697 27.247 4972.366 5.276 121.195 2.485 0.75 449304. 0.3625
|
|
68.26 0.3814 0.7202 0.0504 0.0267 6.396 44.790 25.308 4769.244 5.060 112.570 2.407 0.76 450016. 0.3383
|
|
72.27 0.4038 0.7378 0.0465 0.0254 6.091 42.657 23.320 4542.092 4.819 103.728 2.329 0.76 450758. 0.3142
|
|
76.29 0.4262 0.7526 0.0424 0.0240 5.754 40.295 21.287 4290.596 4.552 94.687 2.250 0.76 451529. 0.2901
|
|
80.30 0.4487 0.7642 0.0383 0.0225 5.384 37.702 19.214 4014.520 4.260 85.462 2.171 0.76 452331. 0.2659
|
|
84.32 0.4711 0.7721 0.0341 0.0208 4.980 34.877 17.102 3713.743 3.940 76.071 2.089 0.76 453163. 0.2414
|
|
88.33 0.4936 0.7754 0.0298 0.0190 4.544 31.821 14.958 3388.304 3.595 66.532 2.002 0.76 454026. 0.2164
|
|
92.35 0.5160 0.7726 0.0255 0.0170 4.075 28.536 12.784 3038.490 3.224 56.864 1.908 0.76 454920. 0.1907
|
|
96.37 0.5384 0.7613 0.0211 0.0149 3.574 25.027 10.587 2664.875 2.828 47.092 1.802 0.76 455844. 0.1638
|
|
100.38 0.5609 0.7367 0.0167 0.0127 3.042 21.304 8.373 2268.427 2.407 37.242 1.674 0.76 456800. 0.1354
|
|
104.40 0.5833 0.6896 0.0122 0.0104 2.482 17.380 6.148 1850.582 1.964 27.347 1.507 0.76 457786. 0.1044
|
|
108.41 0.6057 0.5982 0.0078 0.0079 1.895 13.273 3.922 1413.302 1.500 17.443 1.259 0.76 458802. 0.0696
|
|
112.43 0.6282 0.3967 0.0034 0.0054 1.286 9.004 1.701 958.753 1.017 7.568 0.805 0.76 459843. 0.0293
|
|
116.44 0.6506
|
|
|
|
|
|
|
|
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 0.0997 0.0348 11.446 72.140 61.767 8534.961 8.150 274.740 3.282 0.83 490649. 0.7208
|
|
4.46 0.0224 0.0629 0.0981 0.0350 11.494 72.447 60.819 8571.350 8.185 270.524 3.218 0.83 490970. 0.7013
|
|
8.91 0.0448 0.1232 0.0965 0.0351 11.531 72.679 59.787 8598.825 8.211 265.931 3.154 0.83 491316. 0.6813
|
|
13.37 0.0672 0.1810 0.0947 0.0352 11.554 72.824 58.666 8615.917 8.228 260.946 3.088 0.83 491688. 0.6609
|
|
17.83 0.0896 0.2362 0.0927 0.0352 11.561 72.868 57.453 8621.099 8.233 255.549 3.023 0.83 492087. 0.6402
|
|
22.28 0.1120 0.2888 0.0906 0.0351 11.550 72.797 56.142 8612.708 8.225 249.718 2.957 0.83 492513. 0.6190
|
|
26.74 0.1345 0.3388 0.0883 0.0350 11.518 72.596 54.729 8588.915 8.202 243.436 2.890 0.83 492968. 0.5974
|
|
31.20 0.1569 0.3861 0.0859 0.0349 11.463 72.247 53.211 8547.712 8.162 236.683 2.824 0.83 493452. 0.5755
|
|
35.65 0.1793 0.4309 0.0832 0.0346 11.381 71.734 51.584 8486.926 8.104 229.445 2.757 0.83 493965. 0.5532
|
|
40.11 0.2017 0.4730 0.0804 0.0343 11.270 71.036 49.845 8404.363 8.026 221.710 2.690 0.83 494509. 0.5307
|
|
44.56 0.2241 0.5125 0.0774 0.0339 11.128 70.137 47.995 8298.080 7.924 213.481 2.623 0.84 495082. 0.5078
|
|
49.02 0.2465 0.5495 0.0743 0.0333 10.952 69.026 46.038 8166.582 7.799 204.777 2.557 0.84 495686. 0.4848
|
|
53.48 0.2689 0.5839 0.0710 0.0327 10.740 67.693 43.980 8008.836 7.648 195.625 2.491 0.84 496321. 0.4615
|
|
57.93 0.2913 0.6159 0.0675 0.0319 10.492 66.131 41.830 7824.022 7.471 186.059 2.425 0.84 496987. 0.4382
|
|
62.39 0.3137 0.6453 0.0639 0.0311 10.207 64.333 39.593 7611.342 7.268 176.108 2.359 0.84 497685. 0.4148
|
|
66.85 0.3361 0.6723 0.0601 0.0301 9.883 62.292 37.276 7369.920 7.038 165.802 2.294 0.84 498415. 0.3913
|
|
71.30 0.3586 0.6966 0.0563 0.0290 9.521 60.010 34.884 7099.907 6.780 155.165 2.229 0.84 499177. 0.3678
|
|
75.76 0.3810 0.7181 0.0523 0.0278 9.121 57.490 32.424 6801.759 6.495 144.220 2.162 0.84 499971. 0.3440
|
|
80.22 0.4034 0.7367 0.0482 0.0264 8.681 54.717 29.899 6473.646 6.182 132.991 2.095 0.84 500798. 0.3201
|
|
84.67 0.4258 0.7518 0.0441 0.0250 8.203 51.703 27.315 6117.105 5.841 121.499 2.025 0.84 501657. 0.2958
|
|
89.13 0.4482 0.7629 0.0398 0.0234 7.687 48.452 24.677 5732.483 5.474 109.762 1.952 0.84 502550. 0.2710
|
|
93.59 0.4706 0.7696 0.0355 0.0217 7.130 44.941 21.989 5317.092 5.077 97.806 1.876 0.84 503477. 0.2458
|
|
98.04 0.4930 0.7705 0.0311 0.0199 6.534 41.182 19.256 4872.342 4.653 85.652 1.793 0.84 504437. 0.2198
|
|
102.50 0.5154 0.7637 0.0266 0.0180 5.900 37.186 16.485 4399.593 4.201 73.326 1.700 0.84 505430. 0.1928
|
|
106.96 0.5378 0.7459 0.0221 0.0159 5.231 32.972 13.681 3901.012 3.725 60.854 1.591 0.85 506458. 0.1644
|
|
111.41 0.5602 0.7114 0.0175 0.0138 4.532 28.564 10.852 3379.446 3.227 48.272 1.457 0.85 507520. 0.1341
|
|
115.87 0.5827 0.6500 0.0129 0.0116 3.806 23.990 8.008 2838.356 2.710 35.618 1.280 0.85 508615. 0.1012
|
|
120.32 0.6051 0.5408 0.0083 0.0093 3.060 19.288 5.158 2281.948 2.179 22.942 1.025 0.85 509744. 0.0651
|
|
124.78 0.6275 0.3348 0.0037 0.0070 2.299 14.493 2.314 1714.638 1.637 10.290 0.612 0.85 510900. 0.0260
|
|
129.24 0.6499
|
|
|
|
|
|
|
|
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 0.1015 0.0434 18.981 108.758 76.147 14154.142 12.287 338.704 2.440 0.92 539610. 0.5950
|
|
4.90 0.0224 0.0517 0.1002 0.0434 18.976 108.731 75.128 14150.572 12.284 334.169 2.408 0.92 539956. 0.5832
|
|
9.79 0.0448 0.1020 0.0987 0.0433 18.938 108.511 73.997 14121.957 12.260 329.140 2.377 0.92 540332. 0.5712
|
|
14.69 0.0671 0.1510 0.0970 0.0431 18.863 108.082 72.749 14066.077 12.211 323.588 2.346 0.92 540738. 0.5591
|
|
19.58 0.0895 0.1988 0.0952 0.0429 18.749 107.430 71.376 13981.241 12.137 317.480 2.316 0.92 541175. 0.5466
|
|
24.48 0.1119 0.2452 0.0932 0.0425 18.595 106.547 69.872 13866.285 12.038 310.789 2.286 0.92 541644. 0.5338
|
|
29.37 0.1343 0.2904 0.0910 0.0421 18.399 105.425 68.230 13720.363 11.911 303.488 2.256 0.92 542145. 0.5206
|
|
34.27 0.1566 0.3343 0.0886 0.0415 18.161 104.060 66.446 13542.690 11.757 295.553 2.225 0.92 542679. 0.5069
|
|
39.16 0.1790 0.3768 0.0860 0.0409 17.879 102.446 64.516 13332.581 11.574 286.965 2.195 0.92 543247. 0.4926
|
|
44.06 0.2014 0.4179 0.0833 0.0401 17.553 100.576 62.435 13089.279 11.363 277.712 2.164 0.92 543848. 0.4777
|
|
48.95 0.2238 0.4574 0.0803 0.0393 17.182 98.448 60.206 12812.252 11.123 267.798 2.131 0.92 544483. 0.4621
|
|
53.85 0.2462 0.4953 0.0771 0.0383 16.764 96.058 57.833 12501.236 10.853 257.241 2.098 0.92 545152. 0.4459
|
|
58.74 0.2685 0.5316 0.0738 0.0373 16.302 93.410 55.324 12156.639 10.553 246.081 2.064 0.92 545856. 0.4290
|
|
63.64 0.2909 0.5660 0.0703 0.0361 15.796 90.506 52.689 11778.779 10.225 234.360 2.029 0.92 546594. 0.4115
|
|
68.53 0.3133 0.5986 0.0666 0.0348 15.245 87.349 49.937 11367.870 9.869 222.121 1.992 0.92 547366. 0.3934
|
|
73.43 0.3357 0.6292 0.0628 0.0335 14.650 83.940 47.078 10924.147 9.483 209.404 1.955 0.92 548174. 0.3747
|
|
78.32 0.3580 0.6577 0.0588 0.0320 14.011 80.278 44.121 10447.642 9.070 196.248 1.915 0.92 549017. 0.3555
|
|
83.22 0.3804 0.6837 0.0548 0.0305 13.330 76.376 41.072 9939.845 8.629 182.686 1.874 0.92 549895. 0.3356
|
|
88.11 0.4028 0.7061 0.0506 0.0289 12.624 72.333 37.937 9413.566 8.172 168.743 1.828 0.92 550808. 0.3146
|
|
93.01 0.4252 0.7246 0.0463 0.0272 11.885 68.099 34.724 8862.587 7.694 154.453 1.777 0.92 551758. 0.2926
|
|
97.90 0.4476 0.7370 0.0419 0.0255 11.136 63.808 31.437 8304.202 7.209 139.834 1.717 0.93 552743. 0.2690
|
|
102.80 0.4699 0.7358 0.0374 0.0239 10.458 59.925 28.073 7798.758 6.770 124.871 1.633 0.93 553765. 0.2417
|
|
107.69 0.4923 0.7259 0.0329 0.0223 9.752 55.880 24.651 7272.354 6.313 109.646 1.537 0.93 554823. 0.2133
|
|
112.59 0.5147 0.7048 0.0282 0.0206 9.021 51.689 21.177 6726.899 5.840 94.197 1.428 0.93 555917. 0.1836
|
|
117.48 0.5371 0.6691 0.0236 0.0189 8.270 47.387 17.664 6167.028 5.354 78.568 1.299 0.93 557048. 0.1526
|
|
122.38 0.5594 0.6139 0.0188 0.0172 7.507 43.012 14.121 5597.730 4.859 62.811 1.144 0.93 558216. 0.1201
|
|
127.27 0.5818 0.5321 0.0141 0.0154 6.739 38.611 10.565 5024.950 4.362 46.994 0.954 0.93 559420. 0.0866
|
|
132.17 0.6042 0.4137 0.0094 0.0137 5.974 34.228 7.013 4454.570 3.867 31.193 0.714 0.93 560661. 0.0528
|
|
137.06 0.6266 0.2440 0.0046 0.0119 5.218 29.899 3.483 3891.199 3.378 15.495 0.406 0.93 561936. 0.0212
|
|
141.96 0.6490 -0.0052 -0.0001 0.0101 4.437 25.423 -0.060 3308.672 2.872 -0.269 -0.008 0.94 563180. 0.0000
|
|
|
|
|
|
|