GOE 256 (JUNKERS E) AIRFOIL (goe256-il) Xfoil prediction polar at RE=100,000 Ncrit=5
| Details | Polar file |
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Airfoil: GOE 256 (JUNKERS E) AIRFOIL (goe256-il) Reynolds number: 100,000 Max Cl/Cd: 48.27 at α=6.75° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-goe256-il-100000-n5.txt Download as CSV file: xf-goe256-il-100000-n5.csv |
XFOIL Version 6.96
Calculated polar for: GOE 256 (JUNKERS E) 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 = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-11.500 -0.0855 0.11486 0.10964 -0.0820 0.9538 0.0822
-11.250 -0.0789 0.11171 0.10649 -0.0835 0.9488 0.0839
-11.000 -0.2171 0.11321 0.10776 -0.0759 0.9705 0.0685
-10.750 -0.2007 0.10980 0.10433 -0.0776 0.9662 0.0677
-10.500 -0.1893 0.10598 0.10049 -0.0802 0.9612 0.0669
-10.000 -0.1994 0.09205 0.08651 -0.0918 0.9486 0.0605
-9.750 -0.1892 0.08805 0.08250 -0.0949 0.9434 0.0602
-9.500 -0.1841 0.08367 0.07810 -0.0983 0.9370 0.0599
-9.250 -0.1845 0.07869 0.07311 -0.1022 0.9291 0.0597
-9.000 -0.1961 0.07157 0.06596 -0.1091 0.9200 0.0598
-8.750 -0.2201 0.06415 0.05839 -0.1141 0.9092 0.0598
-8.500 -0.2446 0.05846 0.05245 -0.1147 0.8980 0.0599
-8.250 -0.2598 0.05267 0.04625 -0.1150 0.8908 0.0601
-8.000 -0.2730 0.04894 0.04216 -0.1123 0.8811 0.0603
-7.750 -0.2748 0.04501 0.03774 -0.1107 0.8753 0.0606
-7.500 -0.2583 0.04275 0.03528 -0.1105 0.8721 0.0611
-7.250 -0.2528 0.04165 0.03408 -0.1076 0.8638 0.0616
-7.000 -0.2358 0.04014 0.03241 -0.1068 0.8592 0.0623
-6.750 -0.2152 0.03865 0.03072 -0.1065 0.8561 0.0636
-6.500 -0.2039 0.03734 0.02918 -0.1044 0.8502 0.0649
-6.250 -0.1917 0.03580 0.02732 -0.1024 0.8443 0.0663
-6.000 -0.1725 0.03392 0.02499 -0.1014 0.8405 0.0677
-5.750 -0.1486 0.03214 0.02274 -0.1010 0.8378 0.0690
-5.500 -0.1354 0.03148 0.02204 -0.0988 0.8307 0.0699
-5.250 -0.1127 0.03072 0.02122 -0.0981 0.8258 0.0714
-5.000 -0.0843 0.02982 0.02017 -0.0983 0.8223 0.0737
-4.750 -0.0560 0.02878 0.01888 -0.0983 0.8186 0.0764
-4.500 -0.0407 0.02820 0.01805 -0.0960 0.8103 0.0781
-4.250 -0.0112 0.02716 0.01697 -0.0962 0.8060 0.0800
-4.000 0.0219 0.02631 0.01608 -0.0971 0.8028 0.0830
-3.750 0.0372 0.02604 0.01575 -0.0948 0.7943 0.0857
-3.500 0.0661 0.02536 0.01489 -0.0948 0.7896 0.0889
-3.250 0.0982 0.02449 0.01404 -0.0954 0.7863 0.0920
-3.000 0.1166 0.02426 0.01384 -0.0938 0.7791 0.0952
-2.750 0.1428 0.02380 0.01332 -0.0934 0.7736 0.0992
-2.500 0.1741 0.02314 0.01261 -0.0937 0.7698 0.1032
-2.250 0.1958 0.02282 0.01236 -0.0926 0.7635 0.1074
-2.000 0.2193 0.02251 0.01204 -0.0917 0.7570 0.1122
-1.750 0.2497 0.02197 0.01147 -0.0919 0.7527 0.1175
-1.500 0.2721 0.02170 0.01125 -0.0909 0.7461 0.1236
-1.250 0.2957 0.02147 0.01098 -0.0899 0.7391 0.1306
-1.000 0.3267 0.02094 0.01047 -0.0902 0.7345 0.1404
-0.750 0.3470 0.02079 0.01039 -0.0888 0.7266 0.1526
-0.500 0.3735 0.02039 0.01009 -0.0884 0.7198 0.1770
-0.250 0.4066 0.01940 0.00972 -0.0894 0.7152 0.3275
0.000 0.4186 0.01883 0.00995 -0.0866 0.7054 0.5281
0.500 0.6202 0.01807 0.00993 -0.1137 0.6921 1.0000
0.750 0.6415 0.01808 0.00983 -0.1124 0.6830 1.0000
1.000 0.6605 0.01816 0.00982 -0.1107 0.6733 1.0000
1.250 0.6826 0.01815 0.00970 -0.1095 0.6641 1.0000
1.500 0.6991 0.01830 0.00979 -0.1074 0.6529 1.0000
1.750 0.7216 0.01828 0.00966 -0.1062 0.6434 1.0000
2.000 0.7381 0.01841 0.00973 -0.1040 0.6311 1.0000
2.250 0.7552 0.01854 0.00979 -0.1020 0.6189 1.0000
2.500 0.7751 0.01859 0.00976 -0.1003 0.6075 1.0000
2.750 0.7950 0.01866 0.00973 -0.0987 0.5960 1.0000
3.000 0.8121 0.01881 0.00981 -0.0967 0.5838 1.0000
3.250 0.8315 0.01893 0.00983 -0.0950 0.5723 1.0000
3.750 0.8700 0.01923 0.00992 -0.0916 0.5500 1.0000
4.000 0.8892 0.01942 0.01002 -0.0900 0.5398 1.0000
4.250 0.9092 0.01963 0.01012 -0.0885 0.5303 1.0000
4.500 0.9271 0.01991 0.01034 -0.0867 0.5213 1.0000
4.750 0.9477 0.02016 0.01050 -0.0854 0.5131 1.0000
5.000 0.9654 0.02047 0.01077 -0.0836 0.5049 1.0000
5.250 0.9847 0.02077 0.01100 -0.0821 0.4972 1.0000
5.500 1.0044 0.02109 0.01126 -0.0807 0.4901 1.0000
5.750 1.0214 0.02145 0.01161 -0.0789 0.4828 1.0000
6.000 1.0451 0.02176 0.01183 -0.0782 0.4770 1.0000
6.250 1.0620 0.02216 0.01226 -0.0765 0.4709 1.0000
6.500 1.0806 0.02255 0.01265 -0.0750 0.4649 1.0000
6.750 1.1048 0.02289 0.01293 -0.0745 0.4597 1.0000
7.000 1.1218 0.02334 0.01341 -0.0728 0.4541 1.0000
7.250 1.1386 0.02378 0.01389 -0.0711 0.4482 1.0000
7.500 1.1612 0.02415 0.01421 -0.0704 0.4426 1.0000
7.750 1.1749 0.02462 0.01472 -0.0682 0.4363 1.0000
8.000 1.1876 0.02508 0.01522 -0.0658 0.4294 1.0000
8.250 1.2089 0.02544 0.01550 -0.0648 0.4228 1.0000
8.500 1.2147 0.02604 0.01621 -0.0615 0.4156 1.0000
8.750 1.2308 0.02649 0.01667 -0.0598 0.4091 1.0000
9.000 1.2470 0.02701 0.01721 -0.0582 0.4033 1.0000
9.250 1.2559 0.02767 0.01797 -0.0557 0.3966 1.0000
9.500 1.2730 0.02813 0.01842 -0.0543 0.3903 1.0000
9.750 1.2828 0.02886 0.01924 -0.0520 0.3841 1.0000
10.000 1.2934 0.02959 0.02007 -0.0500 0.3780 1.0000
10.250 1.3113 0.03009 0.02057 -0.0488 0.3727 1.0000
10.500 1.3193 0.03099 0.02161 -0.0466 0.3668 1.0000
10.750 1.3284 0.03187 0.02259 -0.0446 0.3608 1.0000
11.000 1.3446 0.03244 0.02319 -0.0434 0.3553 1.0000
11.250 1.3487 0.03362 0.02452 -0.0411 0.3489 1.0000
11.500 1.3558 0.03465 0.02565 -0.0391 0.3422 1.0000
11.750 1.3673 0.03548 0.02651 -0.0376 0.3360 1.0000
12.000 1.3674 0.03702 0.02823 -0.0352 0.3286 1.0000
12.250 1.3771 0.03796 0.02920 -0.0337 0.3218 1.0000
12.500 1.3764 0.03971 0.03113 -0.0316 0.3142 1.0000
12.750 1.3810 0.04109 0.03258 -0.0299 0.3067 1.0000
13.000 1.3808 0.04296 0.03458 -0.0282 0.2985 1.0000
13.250 1.3826 0.04465 0.03635 -0.0266 0.2901 1.0000
13.500 1.3785 0.04700 0.03884 -0.0249 0.2807 1.0000
13.750 1.3796 0.04889 0.04077 -0.0236 0.2717 1.0000
14.000 1.3726 0.05177 0.04379 -0.0222 0.2611 1.0000
14.250 1.3679 0.05452 0.04662 -0.0211 0.2510 1.0000
14.500 1.3655 0.05708 0.04919 -0.0202 0.2412 1.0000
14.750 1.3581 0.06039 0.05258 -0.0194 0.2309 1.0000
15.000 1.3525 0.06359 0.05582 -0.0188 0.2214 1.0000
15.250 1.3492 0.06653 0.05874 -0.0183 0.2125 1.0000
15.500 1.3415 0.07023 0.06251 -0.0180 0.2038 1.0000
15.750 1.3371 0.07348 0.06575 -0.0178 0.1960 1.0000
16.000 1.3307 0.07714 0.06944 -0.0178 0.1883 1.0000
16.250 1.3264 0.08056 0.07284 -0.0178 0.1813 1.0000
16.500 1.3203 0.08431 0.07664 -0.0181 0.1745 1.0000
16.750 1.3190 0.08734 0.07963 -0.0182 0.1685 1.0000
17.000 1.3132 0.09126 0.08367 -0.0187 0.1629 1.0000
17.500 1.3124 0.09736 0.08985 -0.0194 0.1531 1.0000
17.750 1.3073 0.10131 0.09393 -0.0202 0.1483 1.0000
18.000 1.3075 0.10429 0.09692 -0.0208 0.1434 1.0000
18.250 1.3034 0.10811 0.10084 -0.0217 0.1388 1.0000
18.500 1.2956 0.11265 0.10554 -0.0232 0.1339 1.0000
18.750 1.2953 0.11583 0.10872 -0.0241 0.1289 1.0000
19.000 1.2871 0.12058 0.11362 -0.0258 0.1243 1.0000
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