GOE 619 AIRFOIL (goe619-il) Xfoil prediction polar at RE=100,000 Ncrit=9
| Details | Polar file |
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Airfoil: GOE 619 AIRFOIL (goe619-il) Reynolds number: 100,000 Max Cl/Cd: 52.4 at α=5.5° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-goe619-il-100000.txt Download as CSV file: xf-goe619-il-100000.csv |
XFOIL Version 6.96
Calculated polar for: GOE 619 AIRFOIL
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
------ -------- --------- --------- -------- -------- --------
-8.250 -0.3377 0.10548 0.10099 -0.0234 1.0000 0.1500
-8.000 -0.3684 0.10517 0.10079 -0.0217 1.0000 0.1532
-7.750 -0.4225 0.10469 0.10046 -0.0270 0.9944 0.1549
-7.500 -0.3687 0.09919 0.09491 -0.0244 0.9943 0.1578
-7.250 -0.3421 0.09591 0.09159 -0.0269 0.9891 0.1623
-6.750 -0.4432 0.04861 0.04287 -0.0750 0.9577 0.0971
-6.500 -0.4285 0.04337 0.03698 -0.0775 0.9500 0.0975
-6.250 -0.4023 0.04044 0.03395 -0.0794 0.9441 0.0998
-6.000 -0.3709 0.03923 0.03272 -0.0811 0.9385 0.1033
-5.750 -0.3493 0.03649 0.02949 -0.0818 0.9308 0.1060
-5.500 -0.3147 0.03366 0.02586 -0.0843 0.9263 0.1103
-5.250 -0.2944 0.03224 0.02440 -0.0837 0.9187 0.1143
-5.000 -0.2617 0.03121 0.02311 -0.0850 0.9128 0.1234
-4.750 -0.2210 0.03004 0.02188 -0.0876 0.9091 0.1357
-4.500 -0.2063 0.02945 0.02125 -0.0857 0.8998 0.1455
-4.250 -0.1690 0.02899 0.02074 -0.0875 0.8948 0.1616
-4.000 -0.1448 0.02882 0.02048 -0.0871 0.8874 0.1740
-3.750 -0.1148 0.02866 0.02013 -0.0876 0.8807 0.1865
-3.500 -0.0732 0.02861 0.02010 -0.0900 0.8766 0.2030
-3.250 -0.0593 0.02891 0.02056 -0.0879 0.8670 0.2126
-3.000 -0.0218 0.02857 0.02017 -0.0896 0.8619 0.2254
-2.750 0.0101 0.02823 0.01964 -0.0903 0.8558 0.2367
-2.500 0.0336 0.02806 0.01955 -0.0896 0.8476 0.2454
-2.250 0.0769 0.02746 0.01892 -0.0919 0.8436 0.2608
-2.000 0.0938 0.02752 0.01895 -0.0902 0.8341 0.2744
-1.750 0.1317 0.02708 0.01857 -0.0916 0.8286 0.2969
-1.500 0.1817 0.02635 0.01789 -0.0948 0.8256 0.3282
-1.000 0.2411 0.02597 0.01756 -0.0948 0.8101 0.3775
-0.750 0.2594 0.02608 0.01771 -0.0930 0.7996 0.3956
-0.500 0.3083 0.02530 0.01700 -0.0957 0.7946 0.4219
-0.250 0.3642 0.02419 0.01593 -0.0993 0.7912 0.4515
0.000 0.3804 0.02420 0.01600 -0.0970 0.7787 0.4707
0.250 0.4344 0.02290 0.01480 -0.1001 0.7745 0.5107
0.500 0.4525 0.02272 0.01480 -0.0980 0.7624 0.5404
0.750 0.5035 0.02137 0.01371 -0.1007 0.7576 0.5980
1.000 0.5200 0.02090 0.01386 -0.0980 0.7458 0.7140
1.250 0.6198 0.01944 0.01251 -0.1101 0.7406 1.0000
1.500 0.6386 0.01963 0.01258 -0.1081 0.7282 1.0000
1.750 0.6696 0.01947 0.01226 -0.1080 0.7185 1.0000
2.000 0.7024 0.01921 0.01186 -0.1080 0.7083 1.0000
2.250 0.7249 0.01925 0.01183 -0.1065 0.6957 1.0000
2.500 0.7548 0.01909 0.01155 -0.1062 0.6845 1.0000
2.750 0.7876 0.01885 0.01117 -0.1062 0.6733 1.0000
3.000 0.8104 0.01886 0.01113 -0.1047 0.6589 1.0000
3.250 0.8350 0.01882 0.01101 -0.1035 0.6441 1.0000
3.500 0.8603 0.01875 0.01086 -0.1024 0.6285 1.0000
3.750 0.8853 0.01870 0.01072 -0.1012 0.6119 1.0000
4.000 0.9096 0.01869 0.01061 -0.0999 0.5942 1.0000
4.250 0.9336 0.01871 0.01051 -0.0986 0.5755 1.0000
4.500 0.9578 0.01876 0.01043 -0.0974 0.5560 1.0000
4.750 0.9776 0.01895 0.01052 -0.0955 0.5344 1.0000
5.000 0.9972 0.01919 0.01064 -0.0936 0.5126 1.0000
5.250 1.0185 0.01948 0.01077 -0.0921 0.4922 1.0000
5.500 1.0406 0.01986 0.01097 -0.0908 0.4736 1.0000
5.750 1.0626 0.02035 0.01130 -0.0896 0.4567 1.0000
6.000 1.0842 0.02090 0.01176 -0.0884 0.4414 1.0000
6.250 1.1058 0.02151 0.01229 -0.0873 0.4277 1.0000
6.500 1.1282 0.02214 0.01285 -0.0863 0.4156 1.0000
6.750 1.1537 0.02277 0.01332 -0.0859 0.4049 1.0000
7.000 1.1739 0.02340 0.01397 -0.0847 0.3942 1.0000
7.250 1.1963 0.02408 0.01462 -0.0838 0.3849 1.0000
7.500 1.2199 0.02469 0.01515 -0.0831 0.3757 1.0000
7.750 1.2390 0.02538 0.01591 -0.0818 0.3671 1.0000
8.000 1.2634 0.02600 0.01645 -0.0813 0.3589 1.0000
8.250 1.2822 0.02675 0.01728 -0.0799 0.3518 1.0000
8.500 1.3036 0.02744 0.01801 -0.0790 0.3450 1.0000
8.750 1.3291 0.02820 0.01871 -0.0788 0.3386 1.0000
9.000 1.3428 0.02892 0.01962 -0.0766 0.3319 1.0000
9.250 1.3695 0.02956 0.02016 -0.0766 0.3253 1.0000
9.500 1.3840 0.03040 0.02118 -0.0747 0.3196 1.0000
9.750 1.3999 0.03112 0.02200 -0.0729 0.3134 1.0000
10.000 1.4280 0.03179 0.02255 -0.0732 0.3068 1.0000
10.250 1.4324 0.03257 0.02360 -0.0697 0.3006 1.0000
10.500 1.4529 0.03312 0.02415 -0.0687 0.2939 1.0000
10.750 1.4666 0.03392 0.02504 -0.0668 0.2878 1.0000
11.000 1.4736 0.03469 0.02598 -0.0639 0.2818 1.0000
11.250 1.5003 0.03514 0.02628 -0.0638 0.2744 1.0000
11.500 1.4924 0.03599 0.02743 -0.0587 0.2687 1.0000
11.750 1.5043 0.03638 0.02778 -0.0564 0.2613 1.0000
12.000 1.5059 0.03721 0.02874 -0.0530 0.2551 1.0000
12.250 1.5036 0.03799 0.02964 -0.0491 0.2484 1.0000
12.500 1.5142 0.03855 0.03016 -0.0471 0.2412 1.0000
12.750 1.5042 0.03984 0.03170 -0.0430 0.2351 1.0000
13.000 1.5181 0.04021 0.03193 -0.0415 0.2272 1.0000
13.250 1.5009 0.04208 0.03412 -0.0374 0.2212 1.0000
13.500 1.5025 0.04312 0.03518 -0.0351 0.2139 1.0000
13.750 1.4934 0.04501 0.03725 -0.0325 0.2070 1.0000
14.000 1.4889 0.04671 0.03903 -0.0304 0.1995 1.0000
14.250 1.4798 0.04897 0.04142 -0.0285 0.1921 1.0000
14.500 1.4725 0.05121 0.04374 -0.0270 0.1843 1.0000
14.750 1.4615 0.05411 0.04678 -0.0258 0.1767 1.0000
15.000 1.4546 0.05673 0.04946 -0.0249 0.1693 1.0000
15.250 1.4427 0.06025 0.05312 -0.0243 0.1621 1.0000
15.500 1.4361 0.06331 0.05622 -0.0241 0.1557 1.0000
15.750 1.4267 0.06702 0.06003 -0.0241 0.1498 1.0000
16.000 1.4181 0.07079 0.06390 -0.0244 0.1444 1.0000
16.250 1.4169 0.07364 0.06670 -0.0245 0.1400 1.0000
16.500 1.4034 0.07853 0.07180 -0.0254 0.1357 1.0000
16.750 1.3963 0.08258 0.07595 -0.0262 0.1319 1.0000
17.000 1.3982 0.08524 0.07857 -0.0266 0.1283 1.0000
17.250 1.3865 0.09027 0.08377 -0.0280 0.1255 1.0000
17.500 1.3719 0.09592 0.08962 -0.0298 0.1228 1.0000
17.750 1.3617 0.10095 0.09478 -0.0316 0.1201 1.0000
18.000 1.3642 0.10376 0.09758 -0.0325 0.1169 1.0000
18.250 1.3582 0.10816 0.10206 -0.0341 0.1142 1.0000
18.500 1.3328 0.11629 0.11043 -0.0378 0.1127 1.0000
18.750 1.2908 0.12798 0.12238 -0.0437 0.1121 1.0000
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