LWK 80-150/K25 (lwk80150k25-il) Xfoil prediction polar at RE=100,000 Ncrit=9
| Details | Polar file |
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Airfoil: LWK 80-150/K25 (lwk80150k25-il) Reynolds number: 100,000 Max Cl/Cd: 38.12 at α=5° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-lwk80150k25-il-100000.txt Download as CSV file: xf-lwk80150k25-il-100000.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 = 0.100 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-13.500 -0.7319 0.09471 0.08921 -0.0487 1.0000 0.0838
-13.250 -0.7250 0.08981 0.08433 -0.0492 1.0000 0.0827
-13.000 -0.7495 0.08270 0.07715 -0.0520 1.0000 0.0817
-12.750 -0.7781 0.07621 0.07055 -0.0540 1.0000 0.0802
-12.500 -0.8141 0.07017 0.06433 -0.0548 1.0000 0.0792
-12.250 -0.8463 0.06507 0.05901 -0.0541 1.0000 0.0777
-12.000 -0.8768 0.06070 0.05439 -0.0521 1.0000 0.0770
-11.750 -0.9034 0.05698 0.05040 -0.0490 1.0000 0.0763
-11.500 -0.9236 0.05395 0.04711 -0.0452 1.0000 0.0761
-11.250 -0.9371 0.05135 0.04427 -0.0413 1.0000 0.0763
-11.000 -0.9444 0.04895 0.04166 -0.0377 1.0000 0.0767
-10.750 -0.9504 0.04728 0.03983 -0.0338 1.0000 0.0779
-10.500 -0.9634 0.04599 0.03837 -0.0284 1.0000 0.0785
-10.250 -0.9781 0.04491 0.03712 -0.0224 1.0000 0.0793
-10.000 -0.9889 0.04370 0.03569 -0.0170 1.0000 0.0805
-9.750 -0.9958 0.04223 0.03393 -0.0121 1.0000 0.0817
-9.500 -0.9996 0.04082 0.03216 -0.0075 1.0000 0.0830
-9.250 -0.9973 0.03914 0.03017 -0.0039 1.0000 0.0841
-9.000 -0.9797 0.03707 0.02816 -0.0029 1.0000 0.0871
-8.750 -0.9696 0.03598 0.02699 -0.0005 1.0000 0.0904
-8.500 -0.9602 0.03486 0.02564 0.0022 1.0000 0.0941
-8.250 -0.9444 0.03330 0.02390 0.0039 1.0000 0.0979
-8.000 -0.9278 0.03220 0.02288 0.0053 1.0000 0.1027
-7.750 -0.9158 0.03133 0.02181 0.0077 1.0000 0.1085
-7.500 -0.8957 0.02997 0.02056 0.0086 1.0000 0.1149
-7.250 -0.8821 0.02916 0.01964 0.0107 1.0000 0.1224
-7.000 -0.8656 0.02807 0.01868 0.0122 1.0000 0.1310
-6.750 -0.8520 0.02717 0.01777 0.0143 1.0000 0.1419
-6.500 -0.8395 0.02640 0.01703 0.0165 1.0000 0.1535
-6.250 -0.8218 0.02549 0.01623 0.0176 0.9987 0.1698
-6.000 -0.8031 0.02448 0.01548 0.0185 0.9965 0.1914
-5.750 -0.7859 0.02351 0.01477 0.0195 0.9937 0.2232
-5.500 -0.7740 0.02230 0.01405 0.0215 0.9907 0.2746
-5.250 -0.7703 0.02079 0.01338 0.0248 0.9879 0.3780
-5.000 -0.7671 0.02011 0.01406 0.0302 0.9857 0.5627
-4.750 -0.7470 0.02130 0.01546 0.0334 0.9828 0.6604
-4.500 -0.7226 0.02263 0.01669 0.0355 0.9798 0.7003
-4.250 -0.6987 0.02394 0.01786 0.0375 0.9775 0.7275
-4.000 -0.6747 0.02528 0.01911 0.0399 0.9752 0.7464
-3.750 -0.6473 0.02655 0.02027 0.0415 0.9722 0.7636
-3.500 -0.6165 0.02779 0.02139 0.0424 0.9695 0.7801
-3.250 -0.5830 0.02895 0.02243 0.0426 0.9672 0.7960
-3.000 -0.5608 0.02965 0.02303 0.0444 0.9644 0.8112
-2.750 -0.4898 0.03158 0.02483 0.0390 0.9620 0.8229
-2.500 -0.4001 0.03333 0.02641 0.0297 0.9606 0.8370
-2.250 -0.3371 0.03405 0.02702 0.0237 0.9586 0.8499
-2.000 -0.2983 0.03435 0.02722 0.0214 0.9559 0.8632
-1.750 -0.2229 0.03473 0.02750 0.0125 0.9541 0.8707
-1.500 -0.2088 0.03462 0.02735 0.0141 0.9499 0.8815
-1.250 -0.1678 0.03464 0.02731 0.0109 0.9464 0.8895
-1.000 -0.1301 0.03463 0.02726 0.0080 0.9426 0.8976
-0.750 -0.0863 0.03467 0.02726 0.0040 0.9393 0.9044
-0.500 -0.0758 0.03458 0.02716 0.0060 0.9336 0.9126
-0.250 -0.0264 0.03456 0.02713 0.0010 0.9294 0.9178
0.000 -0.0001 0.03465 0.02721 0.0000 0.9242 0.9242
0.250 0.0279 0.03456 0.02713 -0.0012 0.9179 0.9296
0.500 0.0751 0.03458 0.02717 -0.0059 0.9127 0.9338
0.750 0.0851 0.03468 0.02728 -0.0039 0.9047 0.9394
1.000 0.1302 0.03463 0.02727 -0.0080 0.8977 0.9428
1.250 0.1680 0.03465 0.02733 -0.0109 0.8898 0.9465
1.500 0.2090 0.03461 0.02734 -0.0142 0.8815 0.9500
1.750 0.2232 0.03472 0.02749 -0.0125 0.8706 0.9541
2.000 0.2974 0.03436 0.02723 -0.0212 0.8633 0.9560
2.250 0.3399 0.03400 0.02697 -0.0242 0.8498 0.9587
2.500 0.4064 0.03319 0.02628 -0.0307 0.8366 0.9605
2.750 0.4909 0.03155 0.02480 -0.0392 0.8229 0.9623
3.000 0.5565 0.02975 0.02313 -0.0438 0.8103 0.9645
3.250 0.5855 0.02881 0.02229 -0.0428 0.7957 0.9673
3.500 0.6181 0.02765 0.02124 -0.0425 0.7796 0.9695
3.750 0.6478 0.02648 0.02020 -0.0415 0.7634 0.9722
4.000 0.6750 0.02522 0.01904 -0.0399 0.7461 0.9751
4.250 0.6988 0.02391 0.01783 -0.0375 0.7274 0.9776
4.500 0.7229 0.02262 0.01669 -0.0356 0.7004 0.9799
4.750 0.7473 0.02127 0.01543 -0.0335 0.6601 0.9829
5.000 0.7670 0.02012 0.01408 -0.0302 0.5643 0.9858
5.250 0.7701 0.02079 0.01337 -0.0248 0.3768 0.9880
5.500 0.7738 0.02229 0.01404 -0.0214 0.2750 0.9906
5.750 0.7858 0.02349 0.01476 -0.0195 0.2233 0.9937
6.000 0.8032 0.02447 0.01547 -0.0185 0.1920 0.9965
6.250 0.8221 0.02550 0.01622 -0.0177 0.1706 0.9988
6.500 0.8395 0.02639 0.01701 -0.0165 0.1539 1.0000
6.750 0.8519 0.02714 0.01775 -0.0143 0.1420 1.0000
7.000 0.8660 0.02806 0.01867 -0.0123 0.1317 1.0000
7.250 0.8830 0.02918 0.01964 -0.0109 0.1230 1.0000
7.500 0.8955 0.02994 0.02054 -0.0086 0.1151 1.0000
7.750 0.9154 0.03129 0.02177 -0.0076 0.1086 1.0000
8.000 0.9270 0.03212 0.02280 -0.0052 0.1028 1.0000
8.250 0.9441 0.03327 0.02387 -0.0039 0.0979 1.0000
8.500 0.9599 0.03482 0.02561 -0.0022 0.0941 1.0000
8.750 0.9688 0.03590 0.02690 0.0006 0.0902 1.0000
9.000 0.9792 0.03700 0.02807 0.0030 0.0868 1.0000
9.250 0.9982 0.03932 0.03033 0.0037 0.0839 1.0000
9.500 0.9980 0.04074 0.03210 0.0078 0.0827 1.0000
9.750 0.9960 0.04225 0.03393 0.0121 0.0818 1.0000
10.000 0.9892 0.04374 0.03572 0.0169 0.0806 1.0000
10.250 0.9782 0.04498 0.03720 0.0224 0.0795 1.0000
10.500 0.9629 0.04608 0.03848 0.0284 0.0787 1.0000
10.750 0.9506 0.04722 0.03976 0.0338 0.0775 1.0000
11.000 0.9455 0.04892 0.04160 0.0376 0.0763 1.0000
11.250 0.9397 0.05126 0.04415 0.0410 0.0759 1.0000
11.500 0.9255 0.05391 0.04705 0.0450 0.0759 1.0000
11.750 0.9031 0.05705 0.05047 0.0490 0.0764 1.0000
12.000 0.8768 0.06078 0.05447 0.0520 0.0771 1.0000
12.250 0.8467 0.06515 0.05909 0.0540 0.0779 1.0000
12.500 0.8122 0.07039 0.06456 0.0547 0.0789 1.0000
12.750 0.7781 0.07635 0.07069 0.0538 0.0802 1.0000
13.000 0.7437 0.08345 0.07792 0.0514 0.0815 1.0000
13.250 0.7234 0.09024 0.08476 0.0487 0.0827 1.0000
13.500 0.7284 0.09530 0.08980 0.0481 0.0837 1.0000
13.750 0.4083 0.13023 0.12535 0.0258 0.1564 1.0000
14.000 0.4055 0.13381 0.12893 0.0244 0.1539 1.0000
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