GOE 456 AIRFOIL (goe456-il) Xfoil prediction polar at RE=500,000 Ncrit=9
| Details | Polar file |
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Airfoil: GOE 456 AIRFOIL (goe456-il) Reynolds number: 500,000 Max Cl/Cd: 117.94 at α=3.5° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-goe456-il-500000.txt Download as CSV file: xf-goe456-il-500000.csv |
XFOIL Version 6.96
Calculated polar for: GOE 456 AIRFOIL
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 0.500 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-9.000 -0.3070 0.10451 0.10233 -0.0329 1.0000 0.0107
-8.750 -0.3089 0.10233 0.10018 -0.0321 1.0000 0.0113
-8.500 -0.3175 0.10117 0.09909 -0.0308 1.0000 0.0118
-8.250 -0.3094 0.09808 0.09601 -0.0332 0.9987 0.0119
-8.000 -0.2912 0.09408 0.09201 -0.0383 0.9960 0.0120
-7.000 -0.2238 0.07386 0.07182 -0.0625 0.9770 0.0130
-6.750 -0.2028 0.07119 0.06914 -0.0654 0.9738 0.0141
-6.500 -0.1752 0.06708 0.06501 -0.0725 0.9709 0.0152
-6.250 -0.1476 0.06244 0.06033 -0.0803 0.9658 0.0160
-6.000 -0.1155 0.05743 0.05527 -0.0892 0.9607 0.0170
-5.750 -0.0761 0.05177 0.04953 -0.0997 0.9567 0.0184
-5.500 -0.0392 0.04742 0.04509 -0.1070 0.9489 0.0198
-5.250 -0.0025 0.04193 0.03945 -0.1144 0.9432 0.0200
-5.000 0.0255 0.03603 0.03331 -0.1191 0.9337 0.0201
-4.750 0.0450 0.02690 0.02365 -0.1242 0.9241 0.0212
-4.500 0.0683 0.02392 0.02047 -0.1252 0.9170 0.0224
-4.250 0.0919 0.02180 0.01814 -0.1255 0.9092 0.0239
-4.000 0.1179 0.01944 0.01542 -0.1257 0.9025 0.0257
-3.750 0.1435 0.01503 0.01019 -0.1243 0.8942 0.0170
-3.500 0.1707 0.01329 0.00805 -0.1239 0.8878 0.0171
-3.250 0.1967 0.01268 0.00726 -0.1233 0.8796 0.0189
-3.000 0.2238 0.01169 0.00606 -0.1228 0.8728 0.0194
-2.750 0.2499 0.01073 0.00493 -0.1222 0.8646 0.0196
-2.500 0.2758 0.00970 0.00374 -0.1216 0.8567 0.0211
-2.250 0.3020 0.00900 0.00292 -0.1211 0.8486 0.0246
-2.000 0.3284 0.00873 0.00258 -0.1206 0.8395 0.0302
-1.750 0.3553 0.00830 0.00203 -0.1202 0.8312 0.0438
-1.500 0.3810 0.00789 0.00194 -0.1198 0.8218 0.1577
-1.250 0.4076 0.00785 0.00187 -0.1195 0.8116 0.1759
-1.000 0.4343 0.00781 0.00180 -0.1192 0.8013 0.1927
-0.750 0.4609 0.00774 0.00173 -0.1189 0.7910 0.2112
-0.500 0.4873 0.00768 0.00166 -0.1185 0.7796 0.2293
-0.250 0.5135 0.00760 0.00160 -0.1181 0.7669 0.2534
0.000 0.5392 0.00750 0.00156 -0.1177 0.7524 0.2969
0.250 0.5644 0.00734 0.00154 -0.1172 0.7363 0.3735
0.500 0.6022 0.00600 0.00159 -0.1196 0.7198 1.0000
0.750 0.6276 0.00611 0.00158 -0.1190 0.7038 1.0000
1.000 0.6530 0.00623 0.00158 -0.1184 0.6891 1.0000
1.250 0.6784 0.00635 0.00161 -0.1179 0.6751 1.0000
1.500 0.7038 0.00649 0.00165 -0.1173 0.6616 1.0000
1.750 0.7291 0.00664 0.00170 -0.1168 0.6473 1.0000
2.000 0.7544 0.00678 0.00177 -0.1162 0.6340 1.0000
2.250 0.7801 0.00692 0.00186 -0.1158 0.6235 1.0000
2.500 0.8058 0.00707 0.00198 -0.1154 0.6147 1.0000
2.750 0.8318 0.00719 0.00209 -0.1150 0.6055 1.0000
3.000 0.8573 0.00733 0.00220 -0.1145 0.5943 1.0000
3.250 0.8815 0.00751 0.00231 -0.1138 0.5752 1.0000
3.500 0.9058 0.00768 0.00245 -0.1131 0.5552 1.0000
3.750 0.9290 0.00790 0.00258 -0.1122 0.5274 1.0000
4.000 0.9522 0.00815 0.00274 -0.1112 0.4968 1.0000
4.250 0.9700 0.00874 0.00297 -0.1094 0.4170 1.0000
4.500 0.9749 0.01059 0.00380 -0.1057 0.2328 1.0000
4.750 0.9770 0.01289 0.00499 -0.1017 0.0300 1.0000
5.000 0.9987 0.01342 0.00559 -0.1005 0.0198 1.0000
5.250 1.0211 0.01387 0.00615 -0.0994 0.0184 1.0000
5.500 1.0422 0.01442 0.00680 -0.0981 0.0165 1.0000
5.750 1.0618 0.01509 0.00756 -0.0967 0.0147 1.0000
6.000 1.0794 0.01592 0.00849 -0.0948 0.0137 1.0000
6.250 1.0939 0.01698 0.00965 -0.0924 0.0129 1.0000
6.500 1.1049 0.01831 0.01107 -0.0895 0.0124 1.0000
6.750 1.1176 0.01951 0.01237 -0.0868 0.0125 1.0000
7.000 1.1327 0.02061 0.01354 -0.0845 0.0128 1.0000
7.250 1.1463 0.02243 0.01538 -0.0823 0.0123 1.0000
7.500 1.1704 0.02492 0.01789 -0.0818 0.0119 1.0000
7.750 1.1936 0.02594 0.01899 -0.0808 0.0124 1.0000
14.750 0.8772 0.15163 0.14985 -0.0804 0.0115 1.0000
15.000 0.8760 0.15656 0.15482 -0.0838 0.0117 1.0000
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Polar data table (+)
Polar graphs
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