LWK 80-150/K25 (lwk80150k25-il) Xfoil prediction polar at RE=50,000 Ncrit=5
| Details | Polar file |
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Airfoil: LWK 80-150/K25 (lwk80150k25-il) Reynolds number: 50,000 Max Cl/Cd: 23.37 at α=6° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-lwk80150k25-il-50000-n5.txt Download as CSV file: xf-lwk80150k25-il-50000-n5.csv |
XFOIL Version 6.96
Calculated polar for: LWK 80-150/K25
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 0.050 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-13.750 -0.6577 0.10552 0.09763 -0.0394 1.0000 0.0704
-13.500 -0.6992 0.09348 0.08552 -0.0466 1.0000 0.0695
-13.250 -0.7409 0.08392 0.07581 -0.0517 1.0000 0.0686
-13.000 -0.7765 0.07674 0.06843 -0.0543 1.0000 0.0683
-12.750 -0.8036 0.07134 0.06282 -0.0552 1.0000 0.0684
-12.500 -0.8261 0.06679 0.05802 -0.0551 1.0000 0.0687
-12.250 -0.8429 0.06303 0.05402 -0.0542 1.0000 0.0692
-12.000 -0.8582 0.05959 0.05029 -0.0526 1.0000 0.0702
-11.750 -0.8696 0.05646 0.04684 -0.0507 1.0000 0.0713
-11.500 -0.8777 0.05356 0.04357 -0.0485 1.0000 0.0724
-11.250 -0.8664 0.05164 0.04169 -0.0476 1.0000 0.0747
-11.000 -0.8586 0.04976 0.03970 -0.0462 1.0000 0.0771
-10.750 -0.8534 0.04784 0.03758 -0.0444 1.0000 0.0800
-10.500 -0.8463 0.04577 0.03516 -0.0425 1.0000 0.0829
-10.250 -0.8281 0.04402 0.03338 -0.0419 1.0000 0.0863
-10.000 -0.8142 0.04266 0.03197 -0.0405 1.0000 0.0903
-9.750 -0.8001 0.04119 0.03021 -0.0390 1.0000 0.0954
-9.500 -0.7800 0.03992 0.02903 -0.0383 1.0000 0.1007
-9.250 -0.7663 0.03891 0.02791 -0.0365 1.0000 0.1068
-9.000 -0.7471 0.03787 0.02687 -0.0353 1.0000 0.1137
-8.750 -0.7357 0.03712 0.02604 -0.0330 1.0000 0.1213
-8.500 -0.7233 0.03640 0.02534 -0.0307 1.0000 0.1291
-8.250 -0.7166 0.03580 0.02466 -0.0277 1.0000 0.1381
-8.000 -0.7130 0.03519 0.02414 -0.0243 1.0000 0.1461
-7.750 -0.7092 0.03460 0.02352 -0.0209 1.0000 0.1564
-7.500 -0.7094 0.03399 0.02296 -0.0170 1.0000 0.1667
-7.250 -0.7106 0.03336 0.02239 -0.0129 1.0000 0.1779
-7.000 -0.6982 0.03238 0.02151 -0.0115 0.9960 0.1982
-6.750 -0.6841 0.03131 0.02063 -0.0105 0.9903 0.2250
-6.500 -0.6720 0.03021 0.01978 -0.0093 0.9846 0.2610
-6.250 -0.6622 0.02907 0.01898 -0.0076 0.9791 0.3104
-6.000 -0.6555 0.02806 0.01844 -0.0049 0.9737 0.3763
-5.750 -0.6303 0.02807 0.01926 -0.0031 0.9707 0.4823
-5.500 -0.5815 0.02994 0.02137 -0.0031 0.9695 0.5717
-5.250 -0.5584 0.03073 0.02201 -0.0015 0.9652 0.6158
-5.000 -0.5435 0.03130 0.02241 0.0011 0.9599 0.6479
-4.750 -0.5259 0.03185 0.02278 0.0031 0.9556 0.6766
-4.500 -0.4957 0.03299 0.02373 0.0041 0.9525 0.6985
-4.250 -0.4715 0.03384 0.02441 0.0058 0.9484 0.7194
-4.000 -0.4439 0.03455 0.02497 0.0066 0.9449 0.7390
-3.750 -0.4067 0.03531 0.02553 0.0059 0.9426 0.7555
-3.500 -0.3647 0.03592 0.02598 0.0041 0.9409 0.7697
-3.250 -0.3413 0.03616 0.02609 0.0050 0.9368 0.7828
-3.000 -0.3222 0.03623 0.02604 0.0062 0.9324 0.7962
-2.750 -0.2787 0.03638 0.02605 0.0033 0.9302 0.8050
-2.500 -0.2490 0.03634 0.02589 0.0024 0.9272 0.8151
-2.250 -0.2202 0.03633 0.02578 0.0017 0.9237 0.8238
-2.000 -0.2015 0.03625 0.02564 0.0027 0.9189 0.8325
-1.750 -0.1705 0.03621 0.02551 0.0015 0.9154 0.8401
-1.500 -0.1440 0.03612 0.02535 0.0009 0.9120 0.8479
-1.250 -0.1104 0.03607 0.02525 -0.0009 0.9085 0.8536
-1.000 -0.1089 0.03600 0.02514 0.0030 0.9019 0.8629
-0.750 -0.0686 0.03596 0.02506 -0.0001 0.8986 0.8670
-0.500 -0.0336 0.03591 0.02499 -0.0022 0.8954 0.8720
-0.250 -0.0340 0.03590 0.02497 0.0020 0.8882 0.8799
0.000 0.0001 0.03589 0.02495 0.0000 0.8837 0.8838
0.250 0.0343 0.03589 0.02496 -0.0020 0.8799 0.8883
0.500 0.0335 0.03591 0.02499 0.0023 0.8720 0.8954
0.750 0.0695 0.03595 0.02506 -0.0001 0.8669 0.8987
1.000 0.1097 0.03599 0.02514 -0.0031 0.8628 0.9019
1.250 0.1108 0.03607 0.02524 0.0008 0.8535 0.9085
1.500 0.1433 0.03612 0.02535 -0.0008 0.8479 0.9120
1.750 0.1703 0.03621 0.02551 -0.0015 0.8404 0.9155
2.000 0.2008 0.03627 0.02565 -0.0026 0.8326 0.9191
2.250 0.2203 0.03633 0.02578 -0.0018 0.8240 0.9238
2.500 0.2496 0.03634 0.02589 -0.0025 0.8151 0.9273
2.750 0.2793 0.03637 0.02604 -0.0034 0.8050 0.9303
3.000 0.3229 0.03620 0.02602 -0.0063 0.7962 0.9324
3.250 0.3417 0.03614 0.02607 -0.0050 0.7828 0.9368
3.500 0.3650 0.03589 0.02595 -0.0041 0.7695 0.9409
3.750 0.4070 0.03529 0.02552 -0.0059 0.7555 0.9427
4.000 0.4445 0.03454 0.02496 -0.0067 0.7392 0.9449
4.250 0.4719 0.03383 0.02441 -0.0059 0.7197 0.9485
4.500 0.4953 0.03303 0.02376 -0.0041 0.6990 0.9526
5.000 0.5436 0.03130 0.02242 -0.0012 0.6482 0.9600
5.250 0.5587 0.03071 0.02199 0.0015 0.6155 0.9653
5.500 0.5819 0.02993 0.02137 0.0031 0.5719 0.9695
5.750 0.6307 0.02805 0.01923 0.0031 0.4818 0.9707
6.000 0.6556 0.02805 0.01843 0.0049 0.3764 0.9737
6.250 0.6626 0.02905 0.01896 0.0075 0.3111 0.9791
6.500 0.6723 0.03020 0.01977 0.0092 0.2611 0.9847
6.750 0.6843 0.03130 0.02062 0.0104 0.2253 0.9903
7.000 0.6986 0.03236 0.02150 0.0114 0.1985 0.9960
7.250 0.7112 0.03333 0.02237 0.0128 0.1786 1.0000
7.500 0.7100 0.03398 0.02295 0.0169 0.1672 1.0000
7.750 0.7100 0.03458 0.02351 0.0208 0.1566 1.0000
8.000 0.7132 0.03516 0.02411 0.0243 0.1465 1.0000
8.250 0.7175 0.03579 0.02464 0.0276 0.1385 1.0000
8.500 0.7245 0.03638 0.02533 0.0306 0.1295 1.0000
8.750 0.7374 0.03712 0.02603 0.0328 0.1216 1.0000
9.000 0.7469 0.03785 0.02684 0.0353 0.1138 1.0000
9.250 0.7649 0.03884 0.02783 0.0366 0.1072 1.0000
9.500 0.7792 0.03987 0.02898 0.0384 0.1008 1.0000
9.750 0.8007 0.04117 0.03018 0.0389 0.0956 1.0000
10.000 0.8152 0.04267 0.03198 0.0404 0.0904 1.0000
10.250 0.8284 0.04401 0.03337 0.0418 0.0863 1.0000
10.500 0.8455 0.04576 0.03517 0.0426 0.0827 1.0000
10.750 0.8520 0.04777 0.03750 0.0445 0.0796 1.0000
11.000 0.8584 0.04970 0.03963 0.0462 0.0767 1.0000
11.250 0.8670 0.05148 0.04148 0.0475 0.0743 1.0000
11.500 0.8771 0.05357 0.04359 0.0485 0.0723 1.0000
11.750 0.8687 0.05646 0.04686 0.0507 0.0711 1.0000
12.000 0.8585 0.05959 0.05029 0.0526 0.0701 1.0000
12.250 0.8436 0.06300 0.05399 0.0541 0.0691 1.0000
12.500 0.8256 0.06682 0.05806 0.0550 0.0681 1.0000
12.750 0.8044 0.07126 0.06273 0.0551 0.0679 1.0000
13.000 0.7767 0.07674 0.06843 0.0542 0.0678 1.0000
13.250 0.7408 0.08403 0.07592 0.0515 0.0683 1.0000
13.500 0.6972 0.09398 0.08601 0.0461 0.0692 1.0000
13.750 0.6562 0.10610 0.09820 0.0388 0.0702 1.0000
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