GOE 255 (MVA CA.6) AIRFOIL (goe255-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: GOE 255 (MVA CA.6) AIRFOIL (goe255-il) Reynolds number: 1,000,000 Max Cl/Cd: 127.2 at α=5.25° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-goe255-il-1000000.txt Download as CSV file: xf-goe255-il-1000000.csv |
XFOIL Version 6.96
Calculated polar for: GOE 255 (MVA CA.6) 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 = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.500 -0.6547 0.13828 0.13592 -0.0476 1.0000 0.0099
-19.250 -0.6688 0.13132 0.12887 -0.0515 1.0000 0.0099
-19.000 -0.6796 0.12516 0.12263 -0.0549 1.0000 0.0100
-18.750 -0.6894 0.11933 0.11672 -0.0581 1.0000 0.0100
-18.500 -0.6996 0.11355 0.11086 -0.0613 1.0000 0.0100
-18.250 -0.7086 0.10805 0.10529 -0.0643 1.0000 0.0101
-18.000 -0.7164 0.10287 0.10004 -0.0671 1.0000 0.0101
-17.750 -0.7249 0.09767 0.09476 -0.0699 1.0000 0.0102
-17.500 -0.7331 0.09254 0.08957 -0.0727 1.0000 0.0102
-17.250 -0.7407 0.08759 0.08454 -0.0754 1.0000 0.0103
-17.000 -0.7480 0.08280 0.07968 -0.0780 1.0000 0.0103
-16.750 -0.7550 0.07812 0.07493 -0.0806 1.0000 0.0104
-16.500 -0.7619 0.07359 0.07032 -0.0831 1.0000 0.0105
-16.250 -0.7689 0.06920 0.06587 -0.0854 1.0000 0.0105
-16.000 -0.7767 0.06499 0.06158 -0.0875 1.0000 0.0106
-15.750 -0.7872 0.06104 0.05756 -0.0890 1.0000 0.0106
-15.500 -0.7982 0.05719 0.05364 -0.0904 0.9994 0.0107
-15.250 -0.7984 0.05286 0.04922 -0.0943 0.9970 0.0108
-15.000 -0.7964 0.04867 0.04495 -0.0985 0.9943 0.0109
-14.750 -0.7951 0.04475 0.04094 -0.1021 0.9893 0.0110
-14.500 -0.7918 0.04100 0.03710 -0.1056 0.9834 0.0111
-14.250 -0.7921 0.03760 0.03360 -0.1078 0.9747 0.0112
-14.000 -0.7922 0.03442 0.03032 -0.1095 0.9657 0.0113
-13.750 -0.7919 0.03143 0.02722 -0.1109 0.9556 0.0114
-13.500 -0.7873 0.02862 0.02429 -0.1129 0.9447 0.0115
-13.250 -0.7814 0.02613 0.02168 -0.1147 0.9308 0.0116
-13.000 -0.7754 0.02431 0.01972 -0.1151 0.9080 0.0117
-12.750 -0.7825 0.02257 0.01766 -0.1125 0.8513 0.0119
-12.500 -0.7764 0.02117 0.01601 -0.1113 0.8222 0.0122
-12.250 -0.7616 0.02022 0.01492 -0.1105 0.8069 0.0124
-12.000 -0.7431 0.01948 0.01407 -0.1100 0.7964 0.0127
-11.750 -0.7226 0.01882 0.01334 -0.1096 0.7881 0.0130
-11.500 -0.7010 0.01824 0.01267 -0.1093 0.7813 0.0134
-11.250 -0.6783 0.01768 0.01204 -0.1091 0.7751 0.0138
-11.000 -0.6549 0.01720 0.01147 -0.1088 0.7692 0.0142
-10.750 -0.6305 0.01676 0.01096 -0.1087 0.7642 0.0145
-10.500 -0.6092 0.01594 0.01005 -0.1083 0.7592 0.0150
-10.250 -0.5860 0.01531 0.00936 -0.1080 0.7543 0.0156
-10.000 -0.5611 0.01488 0.00885 -0.1079 0.7495 0.0162
-9.750 -0.5353 0.01444 0.00838 -0.1079 0.7456 0.0168
-9.500 -0.5090 0.01407 0.00794 -0.1078 0.7411 0.0174
-9.250 -0.4833 0.01364 0.00744 -0.1078 0.7365 0.0182
-9.000 -0.4577 0.01319 0.00694 -0.1077 0.7320 0.0194
-8.750 -0.4306 0.01283 0.00655 -0.1077 0.7281 0.0206
-8.500 -0.4036 0.01248 0.00616 -0.1078 0.7237 0.0223
-8.250 -0.3768 0.01212 0.00577 -0.1078 0.7193 0.0249
-8.000 -0.3501 0.01174 0.00537 -0.1078 0.7151 0.0299
-7.750 -0.3238 0.01120 0.00493 -0.1079 0.7113 0.0458
-7.500 -0.2968 0.01077 0.00460 -0.1080 0.7069 0.0644
-7.250 -0.2691 0.01051 0.00434 -0.1082 0.7023 0.0758
-7.000 -0.2410 0.01027 0.00411 -0.1084 0.6980 0.0860
-6.750 -0.2128 0.00998 0.00387 -0.1086 0.6936 0.0990
-6.500 -0.1848 0.00970 0.00365 -0.1088 0.6886 0.1180
-6.250 -0.1568 0.00946 0.00346 -0.1090 0.6836 0.1388
-6.000 -0.1280 0.00925 0.00331 -0.1093 0.6786 0.1558
-5.750 -0.0992 0.00909 0.00316 -0.1096 0.6722 0.1698
-5.500 -0.0706 0.00897 0.00303 -0.1098 0.6657 0.1832
-5.250 -0.0415 0.00883 0.00291 -0.1102 0.6587 0.1957
-5.000 -0.0130 0.00871 0.00278 -0.1104 0.6507 0.2090
-4.750 0.0159 0.00855 0.00265 -0.1107 0.6424 0.2247
-4.500 0.0441 0.00841 0.00252 -0.1109 0.6338 0.2437
-4.250 0.0727 0.00821 0.00240 -0.1112 0.6250 0.2707
-4.000 0.1010 0.00809 0.00234 -0.1114 0.6155 0.3045
-3.750 0.1297 0.00806 0.00232 -0.1116 0.6046 0.3261
-3.500 0.1587 0.00808 0.00231 -0.1119 0.5941 0.3401
-3.250 0.1875 0.00813 0.00231 -0.1121 0.5844 0.3517
-3.000 0.2165 0.00816 0.00231 -0.1123 0.5760 0.3602
-2.750 0.2454 0.00823 0.00232 -0.1126 0.5686 0.3666
-2.500 0.2746 0.00828 0.00232 -0.1129 0.5622 0.3720
-2.250 0.3033 0.00833 0.00235 -0.1131 0.5567 0.3793
-2.000 0.3326 0.00840 0.00237 -0.1134 0.5523 0.3846
-1.750 0.3619 0.00844 0.00238 -0.1137 0.5483 0.3875
-1.500 0.3907 0.00845 0.00237 -0.1140 0.5442 0.3918
-1.250 0.4194 0.00850 0.00240 -0.1142 0.5401 0.3953
-1.000 0.4484 0.00855 0.00242 -0.1145 0.5367 0.3990
-0.750 0.4778 0.00858 0.00244 -0.1149 0.5339 0.4022
-0.500 0.5070 0.00863 0.00246 -0.1152 0.5311 0.4045
-0.250 0.5357 0.00864 0.00247 -0.1155 0.5281 0.4082
0.000 0.5641 0.00869 0.00251 -0.1157 0.5248 0.4114
0.250 0.5926 0.00876 0.00256 -0.1159 0.5217 0.4154
0.500 0.6219 0.00879 0.00260 -0.1163 0.5198 0.4189
0.750 0.6510 0.00882 0.00263 -0.1166 0.5175 0.4220
1.000 0.6798 0.00882 0.00266 -0.1169 0.5151 0.4267
1.250 0.7084 0.00886 0.00271 -0.1172 0.5125 0.4305
1.500 0.7367 0.00893 0.00277 -0.1174 0.5097 0.4346
1.750 0.7646 0.00903 0.00285 -0.1176 0.5065 0.4388
2.000 0.7933 0.00903 0.00290 -0.1179 0.5041 0.4443
2.250 0.8221 0.00905 0.00295 -0.1182 0.5014 0.4486
2.500 0.8506 0.00908 0.00300 -0.1184 0.4982 0.4527
2.750 0.8784 0.00915 0.00307 -0.1186 0.4940 0.4572
3.000 0.9053 0.00924 0.00316 -0.1186 0.4891 0.4635
3.250 0.9341 0.00924 0.00322 -0.1189 0.4857 0.4705
3.500 0.9622 0.00926 0.00329 -0.1191 0.4818 0.4802
3.750 0.9895 0.00931 0.00338 -0.1192 0.4774 0.4941
4.000 1.0161 0.00937 0.00350 -0.1192 0.4729 0.5176
4.250 1.0443 0.00931 0.00359 -0.1195 0.4684 0.5599
4.500 1.0710 0.00926 0.00372 -0.1195 0.4618 0.6238
4.750 1.0967 0.00920 0.00387 -0.1194 0.4545 0.7046
5.000 1.1204 0.00910 0.00403 -0.1187 0.4429 0.8077
5.250 1.1435 0.00899 0.00421 -0.1177 0.4253 1.0000
5.500 1.1597 0.00954 0.00452 -0.1158 0.3774 1.0000
5.750 1.1721 0.01026 0.00500 -0.1132 0.3417 1.0000
6.000 1.1895 0.01070 0.00536 -0.1116 0.3276 1.0000
6.250 1.2061 0.01110 0.00571 -0.1097 0.3177 1.0000
6.500 1.2251 0.01144 0.00601 -0.1083 0.3108 1.0000
6.750 1.2421 0.01187 0.00640 -0.1067 0.3031 1.0000
7.000 1.2640 0.01212 0.00667 -0.1059 0.2987 1.0000
7.250 1.2833 0.01249 0.00702 -0.1047 0.2929 1.0000
7.500 1.3007 0.01295 0.00745 -0.1032 0.2868 1.0000
7.750 1.3235 0.01319 0.00771 -0.1027 0.2834 1.0000
8.000 1.3436 0.01355 0.00807 -0.1017 0.2782 1.0000
8.250 1.3613 0.01402 0.00852 -0.1004 0.2728 1.0000
8.500 1.3821 0.01437 0.00888 -0.0996 0.2681 1.0000
8.750 1.4015 0.01478 0.00930 -0.0987 0.2617 1.0000
9.000 1.4178 0.01535 0.00984 -0.0973 0.2546 1.0000
9.250 1.4369 0.01580 0.01029 -0.0964 0.2466 1.0000
9.500 1.4516 0.01649 0.01093 -0.0949 0.2346 1.0000
9.750 1.4583 0.01762 0.01193 -0.0924 0.2109 1.0000
10.000 1.4514 0.01964 0.01372 -0.0885 0.1739 1.0000
10.250 1.4474 0.02167 0.01562 -0.0854 0.1517 1.0000
10.500 1.4476 0.02359 0.01746 -0.0830 0.1341 1.0000
10.750 1.4426 0.02598 0.01971 -0.0804 0.1104 1.0000
11.000 1.4263 0.02935 0.02287 -0.0771 0.0777 1.0000
11.250 1.4130 0.03263 0.02602 -0.0743 0.0530 1.0000
11.500 1.3900 0.03691 0.03017 -0.0711 0.0184 1.0000
11.750 1.3945 0.03892 0.03221 -0.0700 0.0154 1.0000
12.000 1.4014 0.04077 0.03411 -0.0691 0.0145 1.0000
12.250 1.4070 0.04276 0.03616 -0.0682 0.0137 1.0000
12.500 1.4111 0.04493 0.03839 -0.0673 0.0129 1.0000
12.750 1.4171 0.04696 0.04047 -0.0666 0.0124 1.0000
13.000 1.4231 0.04902 0.04259 -0.0659 0.0120 1.0000
13.250 1.4282 0.05119 0.04482 -0.0652 0.0116 1.0000
13.500 1.4319 0.05357 0.04725 -0.0646 0.0112 1.0000
13.750 1.4345 0.05609 0.04984 -0.0640 0.0109 1.0000
14.000 1.4346 0.05892 0.05274 -0.0634 0.0105 1.0000
14.250 1.4327 0.06201 0.05591 -0.0628 0.0102 1.0000
14.500 1.4364 0.06455 0.05851 -0.0625 0.0101 1.0000
14.750 1.4394 0.06717 0.06119 -0.0622 0.0099 1.0000
15.000 1.4414 0.06994 0.06404 -0.0620 0.0097 1.0000
15.250 1.4420 0.07290 0.06707 -0.0618 0.0095 1.0000
15.500 1.4423 0.07591 0.07014 -0.0616 0.0093 1.0000
15.750 1.4419 0.07903 0.07334 -0.0615 0.0091 1.0000
16.000 1.4403 0.08235 0.07672 -0.0615 0.0088 1.0000
16.250 1.4387 0.08570 0.08014 -0.0615 0.0087 1.0000
16.500 1.4339 0.08948 0.08400 -0.0616 0.0085 1.0000
16.750 1.4262 0.09367 0.08828 -0.0619 0.0083 1.0000
17.000 1.4146 0.09849 0.09321 -0.0622 0.0082 1.0000
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