427 lines
76 KiB
Plaintext
427 lines
76 KiB
Plaintext
20x10 (20x10.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 0.0773 0.0298 0.008 0.483 0.394 5.718 0.055 1.753 31.261 0.08 31293. 0.5758
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0.45 0.0235 0.0594 0.0761 0.0302 0.008 0.490 0.388 5.798 0.055 1.727 30.376 0.08 31311. 0.5553
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0.89 0.0471 0.1153 0.0749 0.0306 0.008 0.496 0.382 5.872 0.056 1.698 29.496 0.08 31331. 0.5347
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1.34 0.0706 0.1678 0.0735 0.0309 0.008 0.502 0.375 5.940 0.057 1.667 28.623 0.08 31352. 0.5141
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1.78 0.0941 0.2170 0.0720 0.0312 0.008 0.507 0.367 5.999 0.057 1.633 27.759 0.08 31375. 0.4935
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2.23 0.1177 0.2629 0.0704 0.0315 0.008 0.511 0.359 6.049 0.058 1.596 26.907 0.08 31401. 0.4729
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2.67 0.1412 0.3056 0.0686 0.0317 0.008 0.514 0.350 6.087 0.058 1.556 26.066 0.08 31428. 0.4523
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3.12 0.1647 0.3452 0.0667 0.0318 0.008 0.517 0.340 6.112 0.058 1.513 25.237 0.08 31457. 0.4318
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3.57 0.1883 0.3817 0.0646 0.0319 0.008 0.517 0.330 6.122 0.058 1.466 24.420 0.08 31488. 0.4113
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4.01 0.2118 0.4153 0.0625 0.0319 0.008 0.517 0.318 6.117 0.058 1.417 23.616 0.08 31522. 0.3910
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4.46 0.2353 0.4459 0.0601 0.0317 0.008 0.515 0.307 6.094 0.058 1.364 22.822 0.08 31558. 0.3708
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4.90 0.2589 0.4736 0.0577 0.0315 0.008 0.512 0.294 6.055 0.058 1.308 22.037 0.08 31596. 0.3507
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5.35 0.2824 0.4984 0.0551 0.0312 0.008 0.507 0.281 5.997 0.057 1.250 21.259 0.08 31636. 0.3307
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5.79 0.3059 0.5203 0.0524 0.0308 0.008 0.500 0.267 5.921 0.057 1.190 20.486 0.08 31678. 0.3108
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6.24 0.3295 0.5393 0.0497 0.0303 0.008 0.492 0.253 5.826 0.056 1.126 19.714 0.08 31723. 0.2910
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6.69 0.3530 0.5551 0.0468 0.0297 0.008 0.483 0.239 5.712 0.055 1.061 18.940 0.08 31770. 0.2714
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7.13 0.3765 0.5678 0.0438 0.0290 0.007 0.471 0.223 5.578 0.053 0.993 18.161 0.08 31820. 0.2518
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7.58 0.4000 0.5770 0.0407 0.0282 0.007 0.458 0.208 5.424 0.052 0.924 17.371 0.08 31872. 0.2323
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8.02 0.4236 0.5825 0.0376 0.0273 0.007 0.444 0.192 5.250 0.050 0.853 16.563 0.08 31926. 0.2128
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8.47 0.4471 0.5840 0.0344 0.0263 0.007 0.427 0.175 5.056 0.048 0.780 15.731 0.08 31983. 0.1933
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8.91 0.4706 0.5809 0.0311 0.0252 0.006 0.409 0.159 4.841 0.046 0.706 14.865 0.08 32042. 0.1737
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9.36 0.4942 0.5724 0.0278 0.0240 0.006 0.389 0.142 4.605 0.044 0.630 13.951 0.08 32104. 0.1540
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9.81 0.5177 0.5576 0.0244 0.0226 0.006 0.368 0.124 4.349 0.042 0.553 12.972 0.08 32168. 0.1342
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10.25 0.5412 0.5351 0.0210 0.0212 0.005 0.344 0.107 4.071 0.039 0.475 11.907 0.08 32235. 0.1142
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10.70 0.5648 0.5027 0.0175 0.0197 0.005 0.319 0.089 3.773 0.036 0.397 10.721 0.08 32304. 0.0939
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11.14 0.5883 0.4576 0.0140 0.0180 0.005 0.292 0.071 3.455 0.033 0.317 9.367 0.08 32376. 0.0734
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11.59 0.6118 0.3950 0.0105 0.0162 0.004 0.264 0.053 3.118 0.030 0.238 7.775 0.08 32450. 0.0527
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12.03 0.6354 0.3076 0.0070 0.0144 0.004 0.233 0.036 2.761 0.026 0.158 5.831 0.08 32526. 0.0322
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12.48 0.6589 0.1828 0.0034 0.0124 0.003 0.202 0.018 2.387 0.023 0.078 3.341 0.08 32605. 0.0130
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12.92 0.6824 -0.0045 -0.0001 0.0104 0.003 0.169 0.000 1.994 0.019 -0.002 -0.080 0.08 32684. 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 0.0777 0.0265 0.055 1.722 1.584 40.755 0.195 7.047 17.632 0.16 62585. 0.6511
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0.90 0.0236 0.0671 0.0765 0.0270 0.056 1.752 1.561 41.450 0.198 6.943 17.082 0.16 62621. 0.6261
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1.79 0.0473 0.1299 0.0753 0.0274 0.056 1.780 1.535 42.107 0.201 6.829 16.539 0.16 62661. 0.6012
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2.69 0.0709 0.1886 0.0739 0.0278 0.057 1.805 1.507 42.714 0.204 6.704 16.005 0.16 62704. 0.5765
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3.58 0.0946 0.2432 0.0724 0.0282 0.058 1.828 1.477 43.256 0.207 6.568 15.483 0.16 62751. 0.5520
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4.48 0.1182 0.2940 0.0708 0.0285 0.059 1.848 1.443 43.720 0.209 6.419 14.972 0.16 62802. 0.5277
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5.37 0.1419 0.3410 0.0690 0.0287 0.059 1.863 1.407 44.091 0.211 6.258 14.473 0.16 62857. 0.5037
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6.27 0.1655 0.3845 0.0671 0.0289 0.059 1.874 1.368 44.354 0.212 6.084 13.987 0.16 62916. 0.4799
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7.17 0.1892 0.4245 0.0650 0.0290 0.060 1.881 1.326 44.498 0.212 5.897 13.514 0.16 62979. 0.4565
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8.06 0.2128 0.4613 0.0628 0.0290 0.060 1.881 1.281 44.512 0.213 5.697 13.052 0.16 63046. 0.4334
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8.96 0.2365 0.4949 0.0605 0.0289 0.060 1.876 1.233 44.388 0.212 5.486 12.602 0.16 63118. 0.4106
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9.85 0.2601 0.5254 0.0580 0.0287 0.059 1.864 1.183 44.118 0.211 5.262 12.162 0.16 63195. 0.3881
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10.75 0.2838 0.5529 0.0554 0.0284 0.059 1.847 1.130 43.698 0.209 5.028 11.732 0.16 63276. 0.3659
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11.64 0.3074 0.5774 0.0527 0.0281 0.058 1.822 1.075 43.122 0.206 4.783 11.310 0.16 63362. 0.3441
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12.54 0.3311 0.5989 0.0499 0.0276 0.057 1.791 1.018 42.386 0.202 4.528 10.894 0.16 63452. 0.3225
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13.44 0.3547 0.6174 0.0470 0.0270 0.056 1.753 0.959 41.486 0.198 4.264 10.482 0.16 63547. 0.3011
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14.33 0.3784 0.6329 0.0440 0.0263 0.054 1.708 0.898 40.418 0.193 3.992 10.073 0.16 63647. 0.2800
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15.23 0.4020 0.6451 0.0409 0.0255 0.053 1.656 0.835 39.180 0.187 3.713 9.663 0.16 63752. 0.2590
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16.12 0.4257 0.6538 0.0378 0.0246 0.051 1.596 0.770 37.769 0.180 3.426 9.250 0.16 63862. 0.2382
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17.02 0.4493 0.6588 0.0345 0.0236 0.049 1.529 0.704 36.181 0.173 3.133 8.829 0.16 63976. 0.2174
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17.92 0.4730 0.6594 0.0312 0.0224 0.046 1.454 0.637 34.416 0.164 2.834 8.396 0.16 64096. 0.1966
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18.81 0.4966 0.6550 0.0279 0.0211 0.044 1.372 0.569 32.471 0.155 2.529 7.943 0.16 64221. 0.1757
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19.71 0.5203 0.6446 0.0245 0.0198 0.041 1.282 0.499 30.346 0.145 2.220 7.461 0.16 64350. 0.1547
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20.60 0.5439 0.6265 0.0210 0.0183 0.038 1.185 0.429 28.042 0.134 1.908 6.937 0.16 64485. 0.1333
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21.50 0.5676 0.5984 0.0175 0.0166 0.034 1.080 0.358 25.560 0.122 1.592 6.349 0.16 64624. 0.1114
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22.39 0.5912 0.5565 0.0140 0.0149 0.031 0.968 0.286 22.904 0.109 1.273 5.669 0.16 64769. 0.0890
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23.29 0.6148 0.4945 0.0105 0.0131 0.027 0.849 0.214 20.080 0.096 0.954 4.843 0.16 64919. 0.0658
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24.19 0.6385 0.4009 0.0070 0.0111 0.023 0.722 0.143 17.093 0.082 0.634 3.782 0.16 65073. 0.0419
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25.08 0.6621 0.2530 0.0035 0.0091 0.019 0.590 0.071 13.952 0.067 0.315 2.301 0.16 65232. 0.0180
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25.98 0.6858 -0.0066 -0.0001 0.0069 0.014 0.449 -0.001 10.626 0.051 -0.006 -0.058 0.16 65389. 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 0.0781 0.0253 0.176 3.692 3.583 131.049 0.417 15.938 12.402 0.24 93875. 0.6887
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1.35 0.0237 0.0708 0.0769 0.0257 0.179 3.761 3.531 133.497 0.425 15.706 11.997 0.24 93930. 0.6614
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2.69 0.0474 0.1370 0.0757 0.0262 0.182 3.827 3.473 135.822 0.432 15.450 11.599 0.24 93990. 0.6342
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4.04 0.0711 0.1986 0.0743 0.0266 0.185 3.887 3.410 137.977 0.439 15.169 11.210 0.24 94055. 0.6074
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5.39 0.0948 0.2558 0.0728 0.0270 0.188 3.942 3.341 139.915 0.445 14.862 10.831 0.24 94125. 0.5809
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6.73 0.1185 0.3089 0.0712 0.0273 0.190 3.989 3.266 141.586 0.451 14.527 10.462 0.24 94202. 0.5547
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8.08 0.1422 0.3580 0.0694 0.0276 0.192 4.027 3.184 142.940 0.455 14.163 10.104 0.24 94285. 0.5290
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9.43 0.1659 0.4033 0.0675 0.0278 0.193 4.055 3.096 143.926 0.458 13.771 9.756 0.24 94373. 0.5036
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10.78 0.1896 0.4450 0.0654 0.0279 0.194 4.071 3.001 144.502 0.460 13.348 9.419 0.24 94469. 0.4787
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12.12 0.2133 0.4832 0.0632 0.0279 0.194 4.075 2.899 144.630 0.460 12.897 9.093 0.24 94570. 0.4543
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13.47 0.2371 0.5182 0.0608 0.0278 0.193 4.065 2.792 144.281 0.459 12.418 8.776 0.24 94679. 0.4302
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14.82 0.2608 0.5501 0.0584 0.0277 0.192 4.041 2.678 143.430 0.457 11.912 8.469 0.24 94794. 0.4066
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16.16 0.2845 0.5789 0.0558 0.0274 0.190 4.002 2.559 142.056 0.452 11.381 8.169 0.24 94916. 0.3834
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17.51 0.3082 0.6047 0.0530 0.0270 0.188 3.948 2.434 140.142 0.446 10.826 7.877 0.24 95046. 0.3606
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18.86 0.3319 0.6276 0.0502 0.0266 0.185 3.879 2.304 137.671 0.438 10.249 7.592 0.24 95182. 0.3381
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20.20 0.3556 0.6475 0.0473 0.0260 0.181 3.793 2.170 134.629 0.429 9.652 7.311 0.24 95325. 0.3160
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21.55 0.3793 0.6645 0.0443 0.0253 0.176 3.691 2.031 131.004 0.417 9.036 7.033 0.24 95476. 0.2941
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22.90 0.4030 0.6784 0.0412 0.0245 0.170 3.572 1.889 126.783 0.404 8.402 6.758 0.24 95634. 0.2725
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24.24 0.4267 0.6889 0.0380 0.0235 0.164 3.436 1.743 121.957 0.388 7.752 6.482 0.24 95800. 0.2511
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25.59 0.4504 0.6959 0.0347 0.0225 0.156 3.283 1.594 116.514 0.371 7.088 6.203 0.24 95972. 0.2297
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26.94 0.4741 0.6989 0.0314 0.0213 0.148 3.112 1.441 110.449 0.352 6.410 5.918 0.24 96153. 0.2084
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28.28 0.4978 0.6972 0.0280 0.0200 0.139 2.923 1.286 103.757 0.330 5.721 5.622 0.24 96340. 0.1871
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29.63 0.5215 0.6897 0.0246 0.0186 0.129 2.717 1.129 96.435 0.307 5.021 5.309 0.24 96536. 0.1655
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30.98 0.5452 0.6749 0.0211 0.0171 0.119 2.493 0.970 88.486 0.282 4.312 4.970 0.24 96739. 0.1436
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32.33 0.5689 0.6504 0.0176 0.0154 0.107 2.252 0.809 79.915 0.254 3.597 4.590 0.24 96949. 0.1211
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33.67 0.5926 0.6121 0.0141 0.0136 0.095 1.993 0.647 70.736 0.225 2.876 4.147 0.24 97167. 0.0978
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35.02 0.6163 0.5529 0.0105 0.0118 0.082 1.718 0.484 60.965 0.194 2.153 3.602 0.24 97392. 0.0735
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36.37 0.6400 0.4590 0.0070 0.0098 0.068 1.426 0.321 50.628 0.161 1.430 2.879 0.24 97625. 0.0479
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37.71 0.6637 0.3002 0.0035 0.0077 0.053 1.120 0.159 39.752 0.127 0.708 1.816 0.24 97864. 0.0212
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39.06 0.6874 -0.0135 -0.0001 0.0054 0.038 0.793 -0.005 28.160 0.090 -0.022 -0.079 0.24 98094. 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 0.0786 0.0247 0.407 6.408 6.411 303.246 0.724 28.517 9.589 0.32 125163. 0.7123
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1.80 0.0238 0.0731 0.0775 0.0252 0.415 6.534 6.319 309.239 0.738 28.106 9.268 0.32 125236. 0.6835
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3.60 0.0475 0.1413 0.0762 0.0256 0.422 6.655 6.217 314.945 0.752 27.653 8.953 0.32 125316. 0.6549
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5.40 0.0713 0.2046 0.0748 0.0261 0.429 6.767 6.105 320.245 0.765 27.155 8.647 0.32 125403. 0.6268
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7.20 0.0950 0.2634 0.0733 0.0264 0.436 6.868 5.982 325.025 0.776 26.609 8.348 0.32 125498. 0.5990
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9.00 0.1188 0.3179 0.0717 0.0268 0.441 6.955 5.848 329.165 0.786 26.014 8.059 0.32 125600. 0.5718
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10.80 0.1425 0.3682 0.0699 0.0271 0.446 7.027 5.703 332.540 0.794 25.366 7.778 0.32 125711. 0.5450
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12.60 0.1663 0.4146 0.0680 0.0273 0.449 7.079 5.545 335.030 0.800 24.665 7.507 0.32 125830. 0.5187
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14.40 0.1900 0.4573 0.0659 0.0274 0.451 7.111 5.376 336.527 0.803 23.911 7.245 0.32 125957. 0.4928
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16.20 0.2138 0.4965 0.0637 0.0274 0.452 7.120 5.194 336.940 0.804 23.104 6.992 0.32 126094. 0.4675
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18.00 0.2375 0.5323 0.0613 0.0274 0.451 7.104 5.001 336.196 0.803 22.247 6.748 0.32 126239. 0.4427
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19.79 0.2613 0.5650 0.0588 0.0272 0.448 7.063 4.798 334.233 0.798 21.341 6.511 0.32 126393. 0.4184
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21.59 0.2850 0.5946 0.0562 0.0269 0.444 6.994 4.584 331.002 0.790 20.390 6.281 0.32 126557. 0.3946
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23.39 0.3088 0.6213 0.0534 0.0266 0.438 6.898 4.361 326.458 0.779 19.396 6.058 0.32 126730. 0.3712
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25.19 0.3325 0.6451 0.0506 0.0261 0.430 6.774 4.128 320.561 0.765 18.362 5.841 0.32 126913. 0.3482
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26.99 0.3563 0.6660 0.0476 0.0255 0.420 6.620 3.887 313.278 0.748 17.291 5.628 0.32 127105. 0.3256
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28.79 0.3801 0.6840 0.0446 0.0248 0.408 6.436 3.639 304.574 0.727 16.186 5.419 0.32 127307. 0.3033
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30.59 0.4038 0.6990 0.0415 0.0240 0.395 6.221 3.383 294.423 0.703 15.049 5.212 0.32 127518. 0.2813
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32.39 0.4276 0.7109 0.0383 0.0230 0.379 5.976 3.121 282.795 0.675 13.883 5.006 0.32 127740. 0.2595
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34.19 0.4513 0.7193 0.0350 0.0219 0.362 5.698 2.853 269.669 0.644 12.691 4.799 0.32 127971. 0.2378
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35.99 0.4751 0.7239 0.0316 0.0208 0.342 5.389 2.580 255.029 0.609 11.475 4.588 0.32 128213. 0.2162
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37.79 0.4988 0.7241 0.0282 0.0194 0.320 5.047 2.302 238.861 0.570 10.238 4.370 0.32 128464. 0.1945
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39.59 0.5226 0.7187 0.0248 0.0180 0.297 4.673 2.019 221.161 0.528 8.982 4.141 0.32 128726. 0.1726
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41.39 0.5463 0.7065 0.0212 0.0164 0.271 4.267 1.733 201.933 0.482 7.710 3.894 0.32 128997. 0.1504
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43.19 0.5701 0.6848 0.0177 0.0147 0.243 3.829 1.445 181.193 0.433 6.427 3.617 0.32 129279. 0.1275
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44.99 0.5938 0.6495 0.0141 0.0129 0.213 3.359 1.154 158.970 0.380 5.134 3.293 0.32 129571. 0.1038
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46.79 0.6176 0.5930 0.0106 0.0110 0.181 2.859 0.863 135.310 0.323 3.836 2.891 0.32 129872. 0.0788
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48.59 0.6413 0.5000 0.0070 0.0090 0.148 2.330 0.571 110.275 0.263 2.538 2.347 0.32 130184. 0.0520
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50.39 0.6651 0.3339 0.0034 0.0068 0.113 1.773 0.280 83.928 0.200 1.244 1.511 0.32 130504. 0.0235
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52.19 0.6888 -0.0328 -0.0002 0.0045 0.074 1.173 -0.018 55.523 0.133 -0.078 -0.143 0.32 130796. 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 0.0792 0.0244 0.786 9.903 10.098 585.850 1.119 44.915 7.818 0.40 156446. 0.7288
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2.25 0.0238 0.0745 0.0781 0.0249 0.802 10.107 9.955 597.901 1.142 44.280 7.552 0.40 156538. 0.6991
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4.50 0.0475 0.1439 0.0769 0.0254 0.817 10.301 9.797 609.390 1.164 43.578 7.292 0.40 156638. 0.6696
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6.75 0.0713 0.2083 0.0755 0.0258 0.832 10.482 9.623 620.082 1.184 42.805 7.039 0.40 156747. 0.6407
|
|
9.00 0.0950 0.2680 0.0740 0.0262 0.845 10.646 9.433 629.747 1.203 41.956 6.794 0.40 156866. 0.6122
|
|
11.25 0.1188 0.3233 0.0724 0.0266 0.856 10.787 9.224 638.143 1.219 41.028 6.556 0.40 156994. 0.5842
|
|
13.50 0.1426 0.3744 0.0706 0.0269 0.865 10.904 8.997 645.024 1.232 40.017 6.326 0.40 157133. 0.5567
|
|
15.75 0.1663 0.4215 0.0686 0.0271 0.872 10.990 8.750 650.145 1.242 38.921 6.104 0.40 157282. 0.5298
|
|
18.00 0.1901 0.4648 0.0666 0.0272 0.876 11.044 8.485 653.288 1.248 37.739 5.891 0.40 157442. 0.5034
|
|
20.25 0.2138 0.5046 0.0643 0.0273 0.877 11.060 8.200 654.271 1.250 36.474 5.685 0.40 157613. 0.4776
|
|
22.50 0.2376 0.5411 0.0620 0.0272 0.876 11.038 7.897 652.945 1.247 35.127 5.486 0.40 157795. 0.4523
|
|
24.75 0.2614 0.5744 0.0594 0.0270 0.871 10.974 7.577 649.188 1.240 33.704 5.294 0.40 157988. 0.4275
|
|
27.00 0.2851 0.6047 0.0568 0.0268 0.862 10.868 7.241 642.900 1.228 32.208 5.109 0.40 158193. 0.4033
|
|
29.25 0.3089 0.6320 0.0540 0.0264 0.850 10.717 6.889 633.992 1.211 30.643 4.929 0.40 158410. 0.3795
|
|
31.50 0.3326 0.6565 0.0512 0.0259 0.835 10.521 6.523 622.388 1.189 29.015 4.754 0.40 158639. 0.3562
|
|
33.75 0.3564 0.6781 0.0482 0.0253 0.815 10.278 6.144 608.017 1.161 27.328 4.583 0.40 158880. 0.3333
|
|
36.00 0.3801 0.6969 0.0451 0.0246 0.792 9.987 5.752 590.815 1.128 25.587 4.416 0.40 159132. 0.3107
|
|
38.25 0.4039 0.7129 0.0420 0.0238 0.765 9.648 5.350 570.725 1.090 23.795 4.251 0.40 159397. 0.2885
|
|
40.50 0.4277 0.7258 0.0387 0.0228 0.734 9.258 4.936 547.693 1.046 21.957 4.088 0.40 159675. 0.2665
|
|
42.75 0.4514 0.7355 0.0354 0.0217 0.700 8.819 4.514 521.676 0.996 20.076 3.924 0.40 159964. 0.2446
|
|
45.00 0.4752 0.7415 0.0320 0.0205 0.661 8.328 4.082 492.637 0.941 18.158 3.759 0.40 160266. 0.2228
|
|
47.25 0.4989 0.7433 0.0286 0.0192 0.618 7.785 3.643 460.552 0.880 16.206 3.588 0.40 160581. 0.2009
|
|
49.50 0.5227 0.7399 0.0251 0.0177 0.570 7.191 3.198 425.411 0.812 14.224 3.410 0.40 160908. 0.1789
|
|
51.75 0.5465 0.7299 0.0215 0.0161 0.519 6.546 2.747 387.223 0.740 12.218 3.217 0.40 161248. 0.1564
|
|
54.00 0.5702 0.7110 0.0180 0.0144 0.464 5.849 2.291 346.018 0.661 10.191 3.003 0.40 161600. 0.1334
|
|
56.25 0.5940 0.6790 0.0144 0.0126 0.405 5.103 1.832 301.855 0.577 8.151 2.753 0.40 161965. 0.1094
|
|
58.50 0.6177 0.6262 0.0108 0.0106 0.342 4.308 1.372 254.824 0.487 6.102 2.442 0.40 162343. 0.0839
|
|
60.75 0.6415 0.5367 0.0071 0.0085 0.275 3.466 0.911 205.049 0.392 4.052 2.015 0.40 162732. 0.0564
|
|
63.00 0.6653 0.3705 0.0035 0.0064 0.205 2.581 0.452 152.661 0.292 2.008 1.341 0.41 163133. 0.0264
|
|
65.25 0.6890 -0.0250 -0.0001 0.0040 0.129 1.625 -0.018 96.100 0.184 -0.082 -0.087 0.41 163496. 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 0.0800 0.0244 1.355 14.233 14.684 1010.341 1.608 65.314 6.592 0.48 187725. 0.7411
|
|
2.71 0.0238 0.0756 0.0789 0.0249 1.384 14.536 14.481 1031.884 1.642 64.410 6.365 0.48 187835. 0.7106
|
|
5.42 0.0477 0.1459 0.0777 0.0254 1.411 14.826 14.255 1052.444 1.675 63.408 6.144 0.48 187956. 0.6805
|
|
8.13 0.0715 0.2112 0.0763 0.0258 1.437 15.096 14.006 1071.604 1.706 62.301 5.928 0.48 188088. 0.6509
|
|
10.84 0.0953 0.2717 0.0748 0.0263 1.460 15.340 13.732 1088.944 1.733 61.081 5.720 0.48 188231. 0.6219
|
|
13.54 0.1192 0.3276 0.0732 0.0266 1.481 15.553 13.432 1104.030 1.757 59.744 5.518 0.48 188386. 0.5933
|
|
16.25 0.1430 0.3793 0.0714 0.0269 1.497 15.727 13.103 1116.418 1.777 58.284 5.324 0.48 188554. 0.5654
|
|
18.96 0.1669 0.4269 0.0694 0.0271 1.510 15.857 12.747 1125.669 1.792 56.697 5.136 0.48 188734. 0.5380
|
|
21.67 0.1907 0.4708 0.0673 0.0273 1.517 15.938 12.361 1131.391 1.801 54.982 4.956 0.48 188927. 0.5112
|
|
24.38 0.2145 0.5111 0.0651 0.0273 1.520 15.964 11.948 1133.253 1.804 53.143 4.782 0.48 189134. 0.4849
|
|
27.09 0.2384 0.5480 0.0627 0.0273 1.517 15.932 11.507 1130.990 1.800 51.184 4.615 0.48 189354. 0.4593
|
|
29.80 0.2622 0.5818 0.0601 0.0271 1.508 15.839 11.041 1124.390 1.790 49.109 4.454 0.48 189588. 0.4342
|
|
32.51 0.2860 0.6125 0.0575 0.0268 1.493 15.683 10.550 1113.270 1.772 46.927 4.298 0.48 189836. 0.4096
|
|
35.21 0.3099 0.6403 0.0547 0.0265 1.472 15.460 10.037 1097.481 1.747 44.643 4.148 0.48 190099. 0.3855
|
|
37.92 0.3337 0.6654 0.0518 0.0260 1.444 15.170 9.502 1076.887 1.714 42.265 4.002 0.48 190375. 0.3619
|
|
40.63 0.3576 0.6876 0.0487 0.0253 1.410 14.811 8.948 1051.367 1.673 39.799 3.860 0.48 190666. 0.3388
|
|
43.34 0.3814 0.7070 0.0456 0.0246 1.369 14.380 8.375 1020.812 1.625 37.252 3.721 0.48 190972. 0.3159
|
|
46.05 0.4052 0.7237 0.0424 0.0238 1.321 13.877 7.786 985.118 1.568 34.631 3.585 0.48 191292. 0.2935
|
|
48.76 0.4291 0.7374 0.0391 0.0228 1.266 13.301 7.181 944.198 1.503 31.942 3.450 0.48 191627. 0.2712
|
|
51.47 0.4529 0.7479 0.0358 0.0216 1.204 12.650 6.562 897.971 1.429 29.190 3.315 0.48 191977. 0.2491
|
|
54.18 0.4767 0.7549 0.0323 0.0204 1.135 11.923 5.931 846.375 1.347 26.382 3.178 0.48 192342. 0.2271
|
|
56.88 0.5006 0.7578 0.0288 0.0190 1.059 11.120 5.289 789.370 1.256 23.524 3.039 0.48 192722. 0.2050
|
|
59.59 0.5244 0.7557 0.0253 0.0175 0.975 10.240 4.636 726.937 1.157 20.622 2.893 0.48 193117. 0.1827
|
|
62.30 0.5483 0.7472 0.0217 0.0159 0.884 9.285 3.975 659.094 1.049 17.683 2.736 0.48 193528. 0.1600
|
|
65.01 0.5721 0.7299 0.0180 0.0141 0.786 8.254 3.308 585.898 0.932 14.715 2.561 0.48 193953. 0.1367
|
|
67.72 0.5959 0.6995 0.0144 0.0122 0.681 7.149 2.636 507.456 0.808 11.726 2.356 0.48 194394. 0.1122
|
|
70.43 0.6198 0.6480 0.0107 0.0102 0.569 5.972 1.962 423.933 0.675 8.725 2.099 0.49 194850. 0.0862
|
|
73.14 0.6436 0.5577 0.0070 0.0081 0.450 4.727 1.287 335.559 0.534 5.723 1.739 0.49 195320. 0.0579
|
|
75.85 0.6674 0.3816 0.0033 0.0058 0.325 3.417 0.614 242.552 0.386 2.730 1.148 0.49 195803. 0.0264
|
|
78.55 0.6913
|
|
|
|
|
|
|
|
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 0.0809 0.0245 2.162 19.471 20.222 1612.541 2.200 89.947 5.688 0.56 218997. 0.7504
|
|
3.15 0.0238 0.0759 0.0799 0.0250 2.210 19.898 19.952 1647.917 2.248 88.747 5.492 0.56 219125. 0.7197
|
|
6.31 0.0476 0.1466 0.0787 0.0255 2.255 20.306 19.652 1681.736 2.294 87.410 5.300 0.56 219266. 0.6893
|
|
9.46 0.0714 0.2122 0.0773 0.0260 2.298 20.688 19.318 1713.307 2.337 85.928 5.114 0.56 219420. 0.6595
|
|
12.62 0.0952 0.2729 0.0758 0.0264 2.336 21.033 18.950 1741.945 2.376 84.289 4.934 0.56 219587. 0.6302
|
|
15.77 0.1190 0.3291 0.0742 0.0268 2.370 21.335 18.544 1766.938 2.410 82.485 4.760 0.56 219768. 0.6014
|
|
18.93 0.1428 0.3811 0.0724 0.0271 2.397 21.584 18.100 1787.553 2.439 80.510 4.593 0.56 219964. 0.5733
|
|
22.08 0.1665 0.4290 0.0705 0.0274 2.418 21.771 17.616 1803.074 2.460 78.357 4.431 0.56 220174. 0.5457
|
|
25.23 0.1903 0.4731 0.0684 0.0275 2.431 21.890 17.092 1812.851 2.473 76.026 4.276 0.56 220400. 0.5187
|
|
28.39 0.2141 0.5137 0.0662 0.0276 2.436 21.932 16.528 1816.339 2.478 73.519 4.127 0.56 220641. 0.4923
|
|
31.54 0.2379 0.5510 0.0637 0.0275 2.431 21.893 15.927 1813.105 2.473 70.842 3.984 0.56 220898. 0.4665
|
|
34.70 0.2617 0.5851 0.0612 0.0274 2.418 21.768 15.289 1802.801 2.459 68.004 3.846 0.56 221171. 0.4412
|
|
37.85 0.2855 0.6163 0.0585 0.0271 2.394 21.555 14.616 1785.142 2.435 65.013 3.714 0.56 221461. 0.4165
|
|
41.01 0.3093 0.6446 0.0557 0.0267 2.360 21.250 13.912 1759.889 2.401 61.880 3.585 0.56 221766. 0.3924
|
|
44.16 0.3331 0.6701 0.0527 0.0262 2.316 20.851 13.178 1726.834 2.356 58.615 3.461 0.56 222089. 0.3686
|
|
47.31 0.3569 0.6929 0.0497 0.0256 2.261 20.355 12.416 1685.786 2.300 55.226 3.341 0.56 222428. 0.3453
|
|
50.47 0.3807 0.7131 0.0465 0.0248 2.195 19.761 11.629 1636.574 2.233 51.724 3.223 0.56 222784. 0.3224
|
|
53.62 0.4045 0.7305 0.0433 0.0240 2.118 19.066 10.818 1579.044 2.154 48.116 3.107 0.56 223157. 0.2998
|
|
56.78 0.4283 0.7450 0.0400 0.0230 2.029 18.270 9.985 1513.052 2.064 44.413 2.993 0.56 223547. 0.2775
|
|
59.93 0.4521 0.7566 0.0366 0.0218 1.929 17.369 9.133 1438.478 1.962 40.623 2.880 0.56 223955. 0.2553
|
|
63.09 0.4758 0.7648 0.0331 0.0206 1.817 16.364 8.263 1355.217 1.849 36.753 2.765 0.56 224380. 0.2332
|
|
66.24 0.4996 0.7692 0.0295 0.0192 1.694 15.253 7.377 1263.202 1.723 32.812 2.649 0.56 224822. 0.2111
|
|
69.39 0.5234 0.7688 0.0259 0.0176 1.559 14.036 6.477 1162.406 1.586 28.809 2.527 0.56 225282. 0.1887
|
|
72.55 0.5472 0.7625 0.0223 0.0160 1.412 12.713 5.565 1052.849 1.436 24.753 2.397 0.56 225760. 0.1659
|
|
75.70 0.5710 0.7479 0.0186 0.0142 1.253 11.285 4.644 934.621 1.275 20.655 2.254 0.56 226255. 0.1425
|
|
78.86 0.5948 0.7211 0.0149 0.0123 1.083 9.755 3.715 807.889 1.102 16.526 2.086 0.57 226768. 0.1180
|
|
82.01 0.6186 0.6745 0.0111 0.0102 0.902 8.125 2.783 672.916 0.918 12.379 1.876 0.57 227298. 0.0918
|
|
85.17 0.6424 0.5911 0.0074 0.0080 0.711 6.400 1.850 530.068 0.723 8.229 1.583 0.57 227845. 0.0632
|
|
88.32 0.6662 0.4252 0.0037 0.0058 0.509 4.585 0.919 379.715 0.518 4.089 1.098 0.57 228407. 0.0309
|
|
91.47 0.6900
|
|
|
|
|
|
|
|
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 0.0821 0.0248 3.265 25.724 26.780 2434.785 2.906 119.117 4.989 0.63 250260. 0.7574
|
|
3.61 0.0238 0.0763 0.0810 0.0253 3.339 26.307 26.438 2489.917 2.972 117.598 4.816 0.63 250407. 0.7265
|
|
7.22 0.0477 0.1472 0.0798 0.0259 3.410 26.865 26.055 2542.737 3.035 115.894 4.648 0.63 250569. 0.6960
|
|
10.83 0.0715 0.2130 0.0785 0.0264 3.476 27.387 25.628 2592.149 3.094 113.994 4.484 0.63 250746. 0.6660
|
|
14.45 0.0953 0.2740 0.0771 0.0268 3.536 27.861 25.153 2637.061 3.148 111.882 4.326 0.63 250938. 0.6366
|
|
18.06 0.1192 0.3304 0.0755 0.0272 3.589 28.276 24.628 2676.345 3.195 109.546 4.174 0.64 251146. 0.6077
|
|
21.67 0.1430 0.3825 0.0737 0.0276 3.633 28.620 24.050 2708.848 3.233 106.977 4.027 0.64 251371. 0.5794
|
|
25.28 0.1668 0.4307 0.0718 0.0278 3.666 28.880 23.418 2733.431 3.263 104.164 3.886 0.64 251613. 0.5517
|
|
28.89 0.1907 0.4750 0.0697 0.0280 3.687 29.045 22.731 2749.072 3.281 101.108 3.750 0.64 251873. 0.5246
|
|
32.50 0.2145 0.5159 0.0674 0.0280 3.694 29.107 21.990 2754.914 3.288 97.810 3.620 0.64 252150. 0.4981
|
|
36.11 0.2384 0.5534 0.0650 0.0280 3.688 29.057 21.196 2750.276 3.283 94.279 3.496 0.64 252446. 0.4721
|
|
39.73 0.2622 0.5879 0.0624 0.0278 3.667 28.892 20.352 2734.634 3.264 90.527 3.376 0.64 252760. 0.4468
|
|
43.34 0.2860 0.6194 0.0596 0.0275 3.631 28.606 19.462 2707.560 3.232 86.566 3.260 0.64 253093. 0.4220
|
|
46.95 0.3099 0.6481 0.0568 0.0271 3.579 28.196 18.527 2668.703 3.186 82.410 3.149 0.64 253445. 0.3976
|
|
50.56 0.3337 0.6741 0.0538 0.0266 3.510 27.657 17.552 2617.758 3.125 78.072 3.041 0.64 253815. 0.3738
|
|
54.17 0.3575 0.6974 0.0507 0.0260 3.426 26.989 16.539 2554.458 3.049 73.566 2.937 0.64 254205. 0.3504
|
|
57.78 0.3814 0.7181 0.0475 0.0252 3.324 26.187 15.491 2478.554 2.959 68.905 2.835 0.64 254614. 0.3273
|
|
61.39 0.4052 0.7362 0.0442 0.0243 3.205 25.249 14.411 2389.824 2.853 64.101 2.735 0.64 255043. 0.3046
|
|
65.01 0.4290 0.7515 0.0408 0.0233 3.068 24.174 13.302 2288.063 2.731 59.166 2.637 0.64 255492. 0.2821
|
|
68.62 0.4529 0.7638 0.0373 0.0221 2.914 22.959 12.165 2173.098 2.594 54.112 2.539 0.64 255960. 0.2598
|
|
72.23 0.4767 0.7730 0.0337 0.0208 2.742 21.604 11.005 2044.767 2.441 48.949 2.441 0.64 256448. 0.2376
|
|
75.84 0.5005 0.7784 0.0301 0.0194 2.552 20.106 9.822 1902.977 2.272 43.690 2.341 0.64 256956. 0.2153
|
|
79.45 0.5244 0.7793 0.0264 0.0178 2.344 18.465 8.621 1747.686 2.086 38.345 2.237 0.64 257484. 0.1927
|
|
83.06 0.5482 0.7744 0.0227 0.0161 2.117 16.682 7.403 1578.928 1.885 32.928 2.127 0.64 258032. 0.1698
|
|
86.68 0.5721 0.7615 0.0189 0.0142 1.873 14.758 6.172 1396.844 1.667 27.453 2.004 0.65 258601. 0.1461
|
|
90.29 0.5959 0.7367 0.0151 0.0122 1.611 12.696 4.931 1201.693 1.434 21.934 1.861 0.65 259189. 0.1213
|
|
93.90 0.6197 0.6922 0.0113 0.0101 1.333 10.501 3.685 993.889 1.186 16.389 1.682 0.65 259797. 0.0947
|
|
97.51 0.6436 0.6105 0.0075 0.0079 1.038 8.178 2.437 773.999 0.924 10.839 1.428 0.65 260425. 0.0654
|
|
101.12 0.6674 0.4417 0.0037 0.0055 0.728 5.733 1.192 542.589 0.648 5.301 0.996 0.65 261069. 0.0319
|
|
104.73 0.6912
|
|
|
|
|
|
|
|
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 0.0834 0.0255 4.787 33.522 34.437 3569.455 3.787 153.176 4.376 0.71 281512. 0.7534
|
|
4.08 0.0239 0.0757 0.0824 0.0261 4.890 34.249 34.025 3646.808 3.869 151.343 4.232 0.71 281679. 0.7242
|
|
8.16 0.0479 0.1464 0.0813 0.0266 4.990 34.945 33.558 3721.000 3.948 149.267 4.091 0.71 281862. 0.6952
|
|
12.24 0.0718 0.2121 0.0800 0.0271 5.083 35.598 33.033 3790.487 4.022 146.930 3.953 0.71 282062. 0.6665
|
|
16.32 0.0958 0.2732 0.0786 0.0275 5.168 36.192 32.444 3853.706 4.089 144.312 3.819 0.71 282280. 0.6381
|
|
20.40 0.1197 0.3299 0.0770 0.0279 5.242 36.711 31.789 3909.029 4.148 141.395 3.688 0.71 282517. 0.6101
|
|
24.48 0.1436 0.3824 0.0752 0.0283 5.303 37.141 31.062 3954.774 4.196 138.164 3.562 0.71 282772. 0.5825
|
|
28.56 0.1676 0.4309 0.0733 0.0285 5.350 37.465 30.262 3989.248 4.233 134.607 3.441 0.72 283048. 0.5553
|
|
32.64 0.1915 0.4756 0.0712 0.0287 5.379 37.668 29.388 4010.865 4.256 130.719 3.323 0.72 283343. 0.5286
|
|
36.73 0.2155 0.5169 0.0689 0.0287 5.389 37.737 28.441 4018.282 4.264 126.505 3.210 0.72 283659. 0.5023
|
|
40.81 0.2394 0.5548 0.0664 0.0286 5.378 37.663 27.423 4010.410 4.255 121.976 3.101 0.72 283995. 0.4765
|
|
44.89 0.2633 0.5897 0.0638 0.0285 5.346 37.438 26.337 3986.382 4.230 117.146 2.997 0.72 284353. 0.4512
|
|
48.97 0.2873 0.6216 0.0610 0.0282 5.291 37.054 25.188 3945.487 4.186 112.034 2.896 0.72 284732. 0.4263
|
|
53.05 0.3112 0.6507 0.0581 0.0278 5.213 36.506 23.979 3887.137 4.124 106.658 2.798 0.72 285132. 0.4020
|
|
57.13 0.3352 0.6771 0.0550 0.0272 5.110 35.789 22.715 3810.826 4.043 101.038 2.704 0.72 285554. 0.3780
|
|
61.21 0.3591 0.7009 0.0518 0.0265 4.983 34.899 21.401 3716.114 3.943 95.192 2.612 0.72 285997. 0.3545
|
|
65.29 0.3830 0.7221 0.0485 0.0257 4.831 33.834 20.040 3602.637 3.823 89.137 2.523 0.72 286462. 0.3314
|
|
69.37 0.4070 0.7408 0.0451 0.0248 4.653 32.589 18.636 3470.088 3.682 82.891 2.436 0.72 286950. 0.3085
|
|
73.45 0.4309 0.7567 0.0416 0.0237 4.450 31.162 17.192 3318.191 3.521 76.470 2.350 0.72 287460. 0.2859
|
|
77.53 0.4548 0.7698 0.0380 0.0225 4.220 29.552 15.712 3146.710 3.339 69.889 2.265 0.72 287992. 0.2634
|
|
81.61 0.4788 0.7797 0.0344 0.0211 3.963 27.756 14.200 2955.445 3.136 63.164 2.179 0.72 288546. 0.2409
|
|
85.69 0.5027 0.7860 0.0307 0.0196 3.680 25.772 12.659 2744.247 2.912 56.308 2.092 0.72 289124. 0.2184
|
|
89.77 0.5267 0.7879 0.0269 0.0180 3.370 23.601 11.092 2513.065 2.666 49.339 2.002 0.72 289723. 0.1956
|
|
93.85 0.5506 0.7841 0.0230 0.0162 3.033 21.243 9.504 2261.951 2.400 42.272 1.906 0.72 290346. 0.1724
|
|
97.93 0.5745 0.7723 0.0191 0.0142 2.670 18.699 7.897 1991.126 2.113 35.125 1.799 0.73 290991. 0.1483
|
|
102.01 0.5985 0.7485 0.0152 0.0122 2.281 15.975 6.277 1700.998 1.805 27.920 1.674 0.73 291659. 0.1230
|
|
106.09 0.6224 0.7045 0.0113 0.0099 1.867 13.075 4.649 1392.224 1.477 20.679 1.515 0.73 292349. 0.0958
|
|
110.18 0.6464 0.6206 0.0073 0.0076 1.429 10.009 3.019 1065.801 1.131 13.430 1.285 0.73 293061. 0.0655
|
|
114.26 0.6703 0.4378 0.0034 0.0052 0.969 6.788 1.393 722.757 0.767 6.195 0.874 0.73 293791. 0.0303
|
|
118.34 0.6942
|
|
|
|
|
|
|
|
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 0.0848 0.0281 7.237 45.617 43.260 5396.993 5.154 192.423 3.636 0.79 312751. 0.7016
|
|
4.52 0.0239 0.0700 0.0839 0.0286 7.359 46.383 42.795 5487.666 5.240 190.350 3.537 0.79 312936. 0.6788
|
|
9.03 0.0477 0.1362 0.0829 0.0290 7.473 47.098 42.261 5572.275 5.321 187.975 3.440 0.79 313138. 0.6561
|
|
13.55 0.0716 0.1987 0.0817 0.0294 7.575 47.745 41.652 5648.766 5.394 185.270 3.344 0.79 313359. 0.6333
|
|
18.07 0.0954 0.2575 0.0803 0.0298 7.664 48.306 40.963 5715.154 5.458 182.204 3.251 0.79 313601. 0.6104
|
|
22.59 0.1193 0.3128 0.0788 0.0300 7.737 48.765 40.187 5769.458 5.509 178.752 3.159 0.79 313863. 0.5876
|
|
27.10 0.1431 0.3647 0.0771 0.0303 7.791 49.105 39.319 5809.712 5.548 174.892 3.070 0.79 314147. 0.5647
|
|
31.62 0.1670 0.4134 0.0752 0.0304 7.824 49.311 38.356 5834.030 5.571 170.606 2.982 0.79 314452. 0.5418
|
|
36.14 0.1908 0.4588 0.0731 0.0304 7.832 49.367 37.294 5840.680 5.577 165.886 2.896 0.79 314780. 0.5189
|
|
40.66 0.2147 0.5012 0.0709 0.0304 7.816 49.262 36.136 5828.225 5.566 160.735 2.812 0.80 315131. 0.4960
|
|
45.17 0.2385 0.5407 0.0684 0.0302 7.772 48.985 34.884 5795.550 5.534 155.165 2.730 0.80 315505. 0.4731
|
|
49.69 0.2624 0.5772 0.0658 0.0299 7.700 48.531 33.542 5741.798 5.483 149.195 2.650 0.80 315902. 0.4502
|
|
54.21 0.2862 0.6109 0.0630 0.0295 7.599 47.893 32.115 5666.272 5.411 142.848 2.571 0.80 316322. 0.4274
|
|
58.72 0.3101 0.6419 0.0600 0.0290 7.467 47.065 30.609 5568.366 5.317 136.150 2.493 0.80 316767. 0.4047
|
|
63.24 0.3339 0.6701 0.0569 0.0284 7.305 46.044 29.030 5447.493 5.202 129.125 2.417 0.80 317235. 0.3821
|
|
67.76 0.3578 0.6957 0.0537 0.0276 7.111 44.823 27.383 5303.032 5.064 121.799 2.342 0.80 317727. 0.3596
|
|
72.28 0.3816 0.7186 0.0504 0.0267 6.885 43.397 25.674 5134.327 4.903 114.196 2.268 0.80 318243. 0.3372
|
|
76.79 0.4055 0.7389 0.0469 0.0257 6.626 41.760 23.907 4940.694 4.718 106.339 2.195 0.80 318783. 0.3148
|
|
81.31 0.4293 0.7564 0.0433 0.0246 6.332 39.907 22.088 4721.449 4.509 98.249 2.122 0.80 319348. 0.2926
|
|
85.83 0.4532 0.7710 0.0397 0.0233 6.002 37.832 20.222 4475.934 4.274 89.946 2.049 0.80 319937. 0.2703
|
|
90.35 0.4770 0.7826 0.0359 0.0219 5.637 35.530 18.312 4203.564 4.014 81.452 1.976 0.80 320551. 0.2481
|
|
94.86 0.5009 0.7907 0.0321 0.0203 5.235 32.996 16.363 3903.852 3.728 72.784 1.901 0.80 321190. 0.2256
|
|
99.38 0.5247 0.7944 0.0282 0.0186 4.797 30.236 14.380 3577.218 3.416 63.962 1.823 0.80 321853. 0.2028
|
|
103.90 0.5486 0.7924 0.0243 0.0168 4.324 27.251 12.367 3224.081 3.079 55.007 1.740 0.81 322542. 0.1795
|
|
108.41 0.5724 0.7827 0.0203 0.0148 3.815 24.044 10.328 2844.657 2.716 45.940 1.647 0.81 323255. 0.1553
|
|
112.93 0.5963 0.7610 0.0162 0.0127 3.273 20.628 8.270 2440.486 2.330 36.786 1.537 0.81 323993. 0.1297
|
|
117.45 0.6201 0.7191 0.0122 0.0105 2.700 17.018 6.199 2013.487 1.923 27.575 1.397 0.81 324755. 0.1020
|
|
121.97 0.6440 0.6384 0.0081 0.0082 2.100 13.239 4.123 1566.316 1.496 18.338 1.194 0.81 325542. 0.0711
|
|
126.48 0.6678 0.4672 0.0040 0.0057 1.478 9.313 2.047 1101.817 1.052 9.104 0.843 0.81 326349. 0.0354
|
|
131.00 0.6917
|
|
|
|
|
|
|
|
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 0.0860 0.0341 11.704 67.060 53.056 8727.339 7.576 235.992 2.757 0.87 343990. 0.5892
|
|
4.98 0.0239 0.0589 0.0852 0.0346 11.847 67.883 52.573 8834.467 7.669 233.845 2.699 0.87 344190. 0.5742
|
|
9.96 0.0478 0.1153 0.0843 0.0349 11.972 68.600 52.009 8927.813 7.750 231.337 2.642 0.87 344411. 0.5591
|
|
14.93 0.0717 0.1694 0.0832 0.0352 12.074 69.182 51.355 9003.576 7.816 228.426 2.587 0.87 344653. 0.5439
|
|
19.91 0.0956 0.2212 0.0820 0.0354 12.147 69.601 50.599 9058.030 7.863 225.066 2.534 0.87 344918. 0.5288
|
|
24.89 0.1195 0.2708 0.0806 0.0356 12.187 69.829 49.733 9087.797 7.889 221.213 2.482 0.87 345206. 0.5136
|
|
29.87 0.1434 0.3185 0.0790 0.0356 12.190 69.846 48.748 9090.021 7.891 216.830 2.432 0.87 345518. 0.4982
|
|
34.84 0.1673 0.3642 0.0772 0.0355 12.153 69.635 47.637 9062.496 7.867 211.888 2.384 0.87 345855. 0.4828
|
|
39.82 0.1911 0.4080 0.0752 0.0352 12.074 69.183 46.396 9003.740 7.816 206.368 2.337 0.87 346218. 0.4671
|
|
44.80 0.2150 0.4500 0.0730 0.0349 11.953 68.487 45.025 8913.139 7.738 200.271 2.291 0.87 346606. 0.4511
|
|
49.78 0.2389 0.4901 0.0706 0.0344 11.789 67.548 43.527 8790.890 7.632 193.610 2.246 0.88 347020. 0.4347
|
|
54.76 0.2628 0.5283 0.0679 0.0338 11.583 66.371 41.908 8637.694 7.499 186.409 2.201 0.88 347461. 0.4180
|
|
59.73 0.2867 0.5644 0.0651 0.0331 11.338 64.963 40.175 8454.456 7.339 178.699 2.155 0.88 347927. 0.4008
|
|
64.71 0.3106 0.5985 0.0621 0.0322 11.053 63.331 38.335 8242.069 7.155 170.514 2.110 0.88 348420. 0.3832
|
|
69.69 0.3345 0.6303 0.0590 0.0313 10.730 61.480 36.396 8001.158 6.946 161.889 2.063 0.88 348939. 0.3652
|
|
74.67 0.3584 0.6599 0.0557 0.0303 10.369 59.412 34.365 7732.040 6.712 152.857 2.016 0.88 349485. 0.3467
|
|
79.65 0.3823 0.6870 0.0523 0.0291 9.970 57.127 32.251 7434.626 6.454 143.450 1.968 0.88 350057. 0.3278
|
|
84.62 0.4062 0.7115 0.0487 0.0278 9.533 54.620 30.058 7108.391 6.171 133.699 1.918 0.88 350656. 0.3085
|
|
89.60 0.4301 0.7334 0.0451 0.0264 9.055 51.886 27.795 6752.580 5.862 123.630 1.867 0.88 351282. 0.2888
|
|
94.58 0.4540 0.7523 0.0413 0.0249 8.537 48.918 25.466 6366.374 5.527 113.272 1.814 0.88 351935. 0.2686
|
|
99.56 0.4779 0.7680 0.0374 0.0233 7.978 45.712 23.079 5949.043 5.164 102.653 1.760 0.88 352615. 0.2480
|
|
104.53 0.5018 0.7800 0.0335 0.0215 7.375 42.259 20.639 5499.769 4.774 91.801 1.702 0.88 353322. 0.2269
|
|
109.51 0.5257 0.7877 0.0294 0.0196 6.730 38.559 18.153 5018.202 4.356 80.743 1.641 0.88 354056. 0.2051
|
|
114.49 0.5496 0.7841 0.0253 0.0177 6.082 34.851 15.621 4535.656 3.937 69.482 1.562 0.89 354818. 0.1811
|
|
119.47 0.5734 0.7677 0.0212 0.0158 5.416 31.036 13.053 4039.073 3.506 58.059 1.466 0.89 355606. 0.1554
|
|
124.45 0.5973 0.7351 0.0169 0.0138 4.721 27.049 10.457 3520.288 3.056 46.515 1.347 0.89 356422. 0.1278
|
|
129.42 0.6212 0.6762 0.0127 0.0117 4.003 22.937 7.843 2985.074 2.591 34.885 1.192 0.89 357265. 0.0979
|
|
134.40 0.6451 0.5721 0.0085 0.0095 3.269 18.733 5.219 2437.955 2.116 23.212 0.971 0.89 358134. 0.0651
|
|
139.38 0.6690 0.3813 0.0042 0.0074 2.527 14.481 2.593 1884.647 1.636 11.535 0.624 0.89 359026. 0.0295
|
|
144.36 0.6929 -0.0589 -0.0004 0.0047 1.625 9.310 -0.248 1211.652 1.052 -1.105 -0.093 0.89 359560. 0.0000
|
|
|
|
|
|
|