WORTMANN FX 79-K-144/17 AIRFOIL (fx79k144-il) Xfoil prediction polar at RE=200,000 Ncrit=5
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Airfoil: WORTMANN FX 79-K-144/17 AIRFOIL (fx79k144-il) Reynolds number: 200,000 Max Cl/Cd: 64.99 at α=6.25° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-fx79k144-il-200000-n5.txt Download as CSV file: xf-fx79k144-il-200000-n5.csv |
XFOIL Version 6.96
Calculated polar for: WORTMANN FX 79-K-144/17 AIRFOIL
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 0.200 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-11.750 -0.6074 0.06342 0.05919 -0.0713 0.8249 0.0141
-11.500 -0.6330 0.05620 0.05175 -0.0763 0.8241 0.0140
-11.250 -0.6589 0.05041 0.04566 -0.0780 0.8234 0.0140
-11.000 -0.6817 0.04537 0.04023 -0.0775 0.8227 0.0141
-10.750 -0.6845 0.04300 0.03769 -0.0765 0.8220 0.0142
-10.500 -0.6816 0.04151 0.03606 -0.0751 0.8214 0.0145
-10.250 -0.6724 0.04015 0.03456 -0.0743 0.8208 0.0149
-10.000 -0.6627 0.03862 0.03283 -0.0734 0.8200 0.0154
-9.750 -0.6536 0.03663 0.03053 -0.0723 0.8190 0.0162
-9.500 -0.6444 0.03394 0.02738 -0.0711 0.8177 0.0173
-9.250 -0.6316 0.03142 0.02436 -0.0699 0.8163 0.0183
-9.000 -0.6128 0.03020 0.02307 -0.0696 0.8148 0.0190
-8.750 -0.5926 0.02916 0.02188 -0.0692 0.8134 0.0200
-8.500 -0.5719 0.02791 0.02037 -0.0687 0.8122 0.0215
-8.250 -0.5498 0.02669 0.01881 -0.0682 0.8109 0.0230
-8.000 -0.5279 0.02572 0.01781 -0.0679 0.8098 0.0242
-7.750 -0.5046 0.02510 0.01710 -0.0677 0.8085 0.0256
-7.500 -0.4808 0.02457 0.01641 -0.0674 0.8073 0.0275
-7.250 -0.4568 0.02398 0.01564 -0.0672 0.8063 0.0296
-7.000 -0.4322 0.02353 0.01522 -0.0674 0.8051 0.0318
-6.750 -0.4069 0.02306 0.01468 -0.0674 0.8038 0.0339
-6.500 -0.3815 0.02248 0.01398 -0.0674 0.8024 0.0354
-6.250 -0.3562 0.02192 0.01332 -0.0673 0.8010 0.0364
-6.000 -0.3326 0.02111 0.01251 -0.0670 0.7995 0.0375
-5.750 -0.3084 0.02055 0.01192 -0.0668 0.7980 0.0386
-5.500 -0.2840 0.02009 0.01142 -0.0665 0.7964 0.0399
-5.250 -0.2594 0.01969 0.01094 -0.0662 0.7949 0.0414
-5.000 -0.2346 0.01934 0.01052 -0.0660 0.7935 0.0433
-4.750 -0.2094 0.01904 0.01015 -0.0658 0.7923 0.0455
-4.500 -0.1844 0.01865 0.00979 -0.0658 0.7901 0.0499
-4.250 -0.1589 0.01836 0.00950 -0.0658 0.7879 0.0572
-4.000 -0.1339 0.01800 0.00924 -0.0658 0.7855 0.0733
-3.750 -0.1090 0.01763 0.00898 -0.0656 0.7831 0.1024
-3.500 -0.0839 0.01727 0.00874 -0.0654 0.7809 0.1405
-3.250 -0.0587 0.01691 0.00853 -0.0652 0.7791 0.1858
-3.000 -0.0343 0.01652 0.00839 -0.0653 0.7754 0.2453
-2.750 -0.0117 0.01578 0.00818 -0.0652 0.7719 0.3662
-2.500 0.0038 0.01458 0.00823 -0.0632 0.7692 0.6444
-2.000 0.0457 0.01531 0.00929 -0.0582 0.7654 0.7903
-1.750 0.0722 0.01553 0.00941 -0.0579 0.7635 0.8089
-1.500 0.0963 0.01585 0.00971 -0.0573 0.7590 0.8256
-1.250 0.1197 0.01608 0.00990 -0.0560 0.7558 0.8362
-1.000 0.1428 0.01625 0.01002 -0.0545 0.7533 0.8477
-0.750 0.1664 0.01636 0.01008 -0.0531 0.7514 0.8591
-0.250 0.2124 0.01662 0.01031 -0.0511 0.7438 0.8742
0.000 0.2351 0.01667 0.01034 -0.0497 0.7405 0.8813
0.250 0.2614 0.01660 0.01022 -0.0494 0.7382 0.8878
0.500 0.2883 0.01646 0.01004 -0.0491 0.7365 0.8903
0.750 0.3123 0.01656 0.01016 -0.0489 0.7306 0.8929
1.000 0.3392 0.01646 0.01005 -0.0489 0.7265 0.8953
1.250 0.3678 0.01622 0.00977 -0.0491 0.7237 0.8976
1.750 0.4214 0.01608 0.00965 -0.0495 0.7133 0.9029
2.000 0.4485 0.01589 0.00946 -0.0493 0.7104 0.9048
2.250 0.4765 0.01565 0.00923 -0.0493 0.7084 0.9068
2.500 0.4998 0.01582 0.00945 -0.0491 0.7004 0.9093
2.750 0.5278 0.01565 0.00931 -0.0493 0.6970 0.9112
3.000 0.5569 0.01543 0.00911 -0.0496 0.6946 0.9130
3.250 0.5816 0.01561 0.00935 -0.0497 0.6866 0.9153
3.500 0.6108 0.01544 0.00921 -0.0502 0.6825 0.9171
3.750 0.6356 0.01532 0.00916 -0.0497 0.6766 0.9193
4.000 0.6610 0.01518 0.00908 -0.0493 0.6698 0.9219
4.250 0.6895 0.01491 0.00884 -0.0493 0.6645 0.9237
4.500 0.7173 0.01475 0.00873 -0.0495 0.6571 0.9253
4.750 0.7483 0.01439 0.00839 -0.0499 0.6518 0.9264
5.000 0.7773 0.01420 0.00824 -0.0502 0.6431 0.9274
5.250 0.8079 0.01391 0.00794 -0.0505 0.6331 0.9283
5.500 0.8374 0.01371 0.00771 -0.0508 0.6196 0.9293
5.750 0.8635 0.01373 0.00771 -0.0506 0.6001 0.9308
6.000 0.8884 0.01383 0.00776 -0.0502 0.5756 0.9320
6.250 0.9099 0.01400 0.00786 -0.0493 0.5433 0.9332
6.500 0.9290 0.01432 0.00802 -0.0480 0.5075 0.9346
6.750 0.9453 0.01479 0.00835 -0.0464 0.4677 0.9363
7.000 0.9547 0.01556 0.00884 -0.0439 0.4118 0.9387
7.250 0.9579 0.01661 0.00959 -0.0408 0.3516 0.9416
7.500 0.9565 0.01807 0.01071 -0.0376 0.2856 0.9456
7.750 0.9539 0.01997 0.01219 -0.0350 0.2097 0.9492
8.000 0.9592 0.02148 0.01347 -0.0332 0.1633 0.9523
8.250 0.9660 0.02293 0.01469 -0.0317 0.1203 0.9555
8.500 0.9751 0.02425 0.01587 -0.0304 0.0899 0.9586
8.750 0.9848 0.02548 0.01700 -0.0291 0.0668 0.9619
9.000 0.9958 0.02664 0.01812 -0.0279 0.0521 0.9657
9.250 1.0083 0.02775 0.01924 -0.0269 0.0442 0.9701
9.500 1.0203 0.02892 0.02042 -0.0260 0.0388 0.9752
9.750 1.0334 0.03001 0.02156 -0.0253 0.0337 0.9823
10.000 1.0440 0.03114 0.02274 -0.0243 0.0300 1.0000
10.250 1.0579 0.03238 0.02408 -0.0239 0.0270 1.0000
10.500 1.0686 0.03388 0.02562 -0.0232 0.0245 1.0000
10.750 1.0811 0.03526 0.02711 -0.0227 0.0221 1.0000
11.000 1.0912 0.03685 0.02877 -0.0221 0.0202 1.0000
11.250 1.0990 0.03864 0.03063 -0.0213 0.0187 1.0000
11.500 1.1081 0.04034 0.03246 -0.0206 0.0175 1.0000
11.750 1.1166 0.04212 0.03433 -0.0199 0.0164 1.0000
12.000 1.1245 0.04396 0.03626 -0.0193 0.0157 1.0000
12.250 1.1315 0.04593 0.03830 -0.0186 0.0151 1.0000
12.500 1.1377 0.04801 0.04046 -0.0180 0.0146 1.0000
12.750 1.1457 0.04999 0.04257 -0.0174 0.0141 1.0000
13.000 1.1537 0.05197 0.04467 -0.0169 0.0136 1.0000
13.250 1.1619 0.05398 0.04679 -0.0165 0.0130 1.0000
13.500 1.1698 0.05605 0.04896 -0.0162 0.0125 1.0000
13.750 1.1772 0.05820 0.05122 -0.0161 0.0120 1.0000
14.000 1.1836 0.06049 0.05360 -0.0160 0.0117 1.0000
14.250 1.1885 0.06294 0.05613 -0.0158 0.0115 1.0000
14.500 1.1933 0.06545 0.05876 -0.0155 0.0113 1.0000
14.750 1.1978 0.06803 0.06150 -0.0152 0.0111 1.0000
15.000 1.2014 0.07076 0.06439 -0.0149 0.0109 1.0000
15.250 1.2038 0.07369 0.06750 -0.0148 0.0107 1.0000
15.500 1.2048 0.07687 0.07086 -0.0148 0.0106 1.0000
15.750 1.2043 0.08031 0.07449 -0.0149 0.0105 1.0000
16.000 1.2020 0.08408 0.07846 -0.0154 0.0104 1.0000
16.250 1.1978 0.08822 0.08282 -0.0161 0.0103 1.0000
16.500 1.1917 0.09273 0.08754 -0.0171 0.0102 1.0000
16.750 1.1836 0.09769 0.09272 -0.0185 0.0101 1.0000
17.000 1.1737 0.10312 0.09837 -0.0204 0.0101 1.0000
17.250 1.1617 0.10911 0.10458 -0.0228 0.0100 1.0000
17.500 1.1479 0.11567 0.11137 -0.0258 0.0100 1.0000
17.750 1.1319 0.12297 0.11889 -0.0295 0.0100 1.0000
18.000 1.1133 0.13128 0.12743 -0.0341 0.0100 1.0000
18.250 1.0916 0.14090 0.13729 -0.0399 0.0101 1.0000
18.500 1.0644 0.15279 0.14942 -0.0475 0.0102 1.0000
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