GOE 144 (MVA H.21) AIRFOIL (goe144-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: GOE 144 (MVA H.21) AIRFOIL (goe144-il) Reynolds number: 1,000,000 Max Cl/Cd: 95.41 at α=5.5° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-goe144-il-1000000-n5.txt Download as CSV file: xf-goe144-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: GOE 144 (MVA H.21) AIRFOIL
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 1.000 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-10.000 -0.3930 0.10139 0.09979 -0.0238 1.0000 0.0042
-9.750 -0.4031 0.09569 0.09412 -0.0254 1.0000 0.0045
-9.250 -0.5013 0.04529 0.04331 -0.0794 0.9800 0.0046
-9.000 -0.4917 0.02309 0.02008 -0.1007 0.9669 0.0046
-8.750 -0.4688 0.01765 0.01423 -0.1035 0.9609 0.0048
-8.500 -0.4388 0.01589 0.01226 -0.1051 0.9566 0.0050
-8.250 -0.4058 0.01468 0.01087 -0.1069 0.9532 0.0052
-8.000 -0.3744 0.01368 0.00971 -0.1082 0.9475 0.0055
-7.750 -0.3409 0.01281 0.00868 -0.1098 0.9416 0.0058
-7.500 -0.3084 0.01211 0.00782 -0.1110 0.9350 0.0061
-7.250 -0.2773 0.01150 0.00707 -0.1119 0.9276 0.0064
-7.000 -0.2483 0.01081 0.00623 -0.1123 0.9203 0.0071
-6.750 -0.2199 0.01034 0.00565 -0.1124 0.9121 0.0079
-6.500 -0.1925 0.00996 0.00515 -0.1123 0.9047 0.0087
-6.250 -0.1652 0.00965 0.00473 -0.1122 0.8978 0.0093
-6.000 -0.1384 0.00925 0.00426 -0.1119 0.8908 0.0111
-5.750 -0.1116 0.00897 0.00394 -0.1116 0.8827 0.0128
-5.500 -0.0849 0.00871 0.00364 -0.1112 0.8742 0.0150
-5.250 -0.0581 0.00854 0.00346 -0.1109 0.8652 0.0181
-5.000 -0.0313 0.00844 0.00330 -0.1105 0.8538 0.0201
-4.750 -0.0048 0.00837 0.00315 -0.1101 0.8378 0.0209
-4.500 0.0203 0.00835 0.00299 -0.1093 0.8006 0.0212
-4.250 0.0420 0.00827 0.00259 -0.1078 0.7412 0.0231
-3.750 0.0918 0.00815 0.00217 -0.1062 0.6878 0.0264
-3.500 0.1179 0.00808 0.00200 -0.1057 0.6708 0.0278
-3.250 0.1442 0.00802 0.00184 -0.1053 0.6550 0.0294
-3.000 0.1706 0.00796 0.00169 -0.1048 0.6394 0.0305
-2.750 0.1971 0.00792 0.00155 -0.1044 0.6248 0.0313
-2.500 0.2238 0.00788 0.00143 -0.1040 0.6111 0.0327
-2.250 0.2503 0.00783 0.00132 -0.1036 0.5971 0.0368
-2.000 0.2765 0.00779 0.00124 -0.1031 0.5799 0.0417
-1.750 0.3026 0.00776 0.00122 -0.1027 0.5630 0.0624
-1.500 0.3293 0.00779 0.00118 -0.1023 0.5491 0.0649
-1.250 0.3560 0.00779 0.00114 -0.1020 0.5367 0.0684
-1.000 0.3826 0.00781 0.00111 -0.1016 0.5224 0.0712
-0.750 0.4092 0.00786 0.00109 -0.1012 0.5078 0.0734
-0.500 0.4358 0.00791 0.00107 -0.1009 0.4938 0.0748
-0.250 0.4624 0.00796 0.00106 -0.1005 0.4796 0.0758
0.000 0.4890 0.00801 0.00106 -0.1002 0.4665 0.0778
0.250 0.5156 0.00803 0.00105 -0.0998 0.4560 0.0823
0.500 0.5425 0.00804 0.00105 -0.0995 0.4473 0.0864
0.750 0.5693 0.00807 0.00107 -0.0992 0.4393 0.0884
1.250 0.6225 0.00814 0.00115 -0.0986 0.4177 0.1133
1.500 0.6489 0.00821 0.00121 -0.0982 0.4045 0.1272
1.750 0.6754 0.00829 0.00127 -0.0979 0.3933 0.1347
2.000 0.7019 0.00838 0.00134 -0.0976 0.3826 0.1391
2.250 0.7283 0.00847 0.00141 -0.0972 0.3710 0.1436
2.500 0.7546 0.00857 0.00149 -0.0969 0.3580 0.1475
2.750 0.7806 0.00870 0.00158 -0.0965 0.3427 0.1509
3.000 0.8062 0.00888 0.00170 -0.0960 0.3221 0.1534
3.250 0.8318 0.00905 0.00182 -0.0956 0.3032 0.1569
3.500 0.8571 0.00925 0.00196 -0.0951 0.2841 0.1619
3.750 0.8823 0.00945 0.00212 -0.0946 0.2656 0.1665
4.000 0.9064 0.00977 0.00232 -0.0939 0.2381 0.1727
4.250 0.9296 0.01017 0.00258 -0.0932 0.2025 0.1819
4.500 0.9536 0.01046 0.00282 -0.0925 0.1767 0.2110
4.750 0.9726 0.01123 0.00333 -0.0911 0.1061 0.2615
5.000 0.9961 0.01152 0.00364 -0.0904 0.0890 0.3141
5.500 1.0495 0.01100 0.00434 -0.0907 0.0616 1.0000
5.750 1.0690 0.01178 0.00491 -0.0893 0.0174 1.0000
6.000 1.0933 0.01204 0.00520 -0.0886 0.0130 1.0000
6.250 1.1172 0.01235 0.00552 -0.0879 0.0111 1.0000
6.500 1.1404 0.01272 0.00591 -0.0871 0.0093 1.0000
6.750 1.1639 0.01305 0.00628 -0.0863 0.0083 1.0000
7.000 1.1872 0.01337 0.00663 -0.0855 0.0075 1.0000
7.250 1.2100 0.01374 0.00701 -0.0847 0.0068 1.0000
7.500 1.2318 0.01419 0.00748 -0.0837 0.0061 1.0000
7.750 1.2534 0.01466 0.00800 -0.0826 0.0056 1.0000
8.000 1.2752 0.01507 0.00845 -0.0816 0.0053 1.0000
8.250 1.2966 0.01551 0.00895 -0.0806 0.0049 1.0000
8.500 1.3176 0.01596 0.00942 -0.0795 0.0046 1.0000
8.750 1.3383 0.01641 0.00990 -0.0784 0.0042 1.0000
9.000 1.3571 0.01700 0.01053 -0.0770 0.0039 1.0000
9.250 1.3744 0.01769 0.01129 -0.0753 0.0037 1.0000
9.500 1.3924 0.01828 0.01195 -0.0738 0.0036 1.0000
9.750 1.4096 0.01889 0.01262 -0.0721 0.0034 1.0000
10.000 1.4253 0.01956 0.01336 -0.0703 0.0033 1.0000
10.250 1.4396 0.02021 0.01408 -0.0682 0.0031 1.0000
10.500 1.4506 0.02092 0.01488 -0.0655 0.0030 1.0000
10.750 1.4605 0.02168 0.01571 -0.0627 0.0029 1.0000
11.000 1.4697 0.02249 0.01658 -0.0600 0.0028 1.0000
11.250 1.4787 0.02332 0.01749 -0.0574 0.0027 1.0000
11.500 1.4867 0.02425 0.01848 -0.0548 0.0027 1.0000
11.750 1.4937 0.02527 0.01958 -0.0523 0.0026 1.0000
12.000 1.4971 0.02658 0.02097 -0.0496 0.0024 1.0000
12.250 1.4976 0.02818 0.02267 -0.0468 0.0024 1.0000
12.500 1.4914 0.03042 0.02504 -0.0439 0.0023 1.0000
12.750 1.4902 0.03245 0.02719 -0.0418 0.0023 1.0000
13.000 1.4948 0.03412 0.02895 -0.0404 0.0022 1.0000
13.250 1.4917 0.03667 0.03163 -0.0390 0.0022 1.0000
13.500 1.4938 0.03890 0.03395 -0.0383 0.0022 1.0000
13.750 1.4879 0.04220 0.03739 -0.0378 0.0022 1.0000
14.000 1.4867 0.04519 0.04050 -0.0377 0.0021 1.0000
14.250 1.4809 0.04889 0.04433 -0.0380 0.0021 1.0000
14.500 1.4771 0.05248 0.04806 -0.0385 0.0020 1.0000
14.750 1.4658 0.05724 0.05296 -0.0394 0.0020 1.0000
15.000 1.4681 0.06027 0.05607 -0.0401 0.0019 1.0000
15.250 1.4591 0.06497 0.06089 -0.0414 0.0019 1.0000
15.500 1.4469 0.07033 0.06639 -0.0430 0.0019 1.0000
15.750 1.4397 0.07508 0.07126 -0.0446 0.0019 1.0000
16.000 1.4285 0.08062 0.07692 -0.0466 0.0018 1.0000
16.250 1.4162 0.08653 0.08296 -0.0489 0.0019 1.0000
16.500 1.4061 0.09226 0.08881 -0.0513 0.0018 1.0000
16.750 1.3941 0.09848 0.09515 -0.0540 0.0018 1.0000
17.000 1.3818 0.10496 0.10176 -0.0569 0.0018 1.0000
17.250 1.3711 0.11129 0.10821 -0.0599 0.0018 1.0000
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Polar data table (+)
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