GOE 274 (DAIMLER V) AIRFOIL (goe274-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: GOE 274 (DAIMLER V) AIRFOIL (goe274-il) Reynolds number: 1,000,000 Max Cl/Cd: 115.11 at α=4.25° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-goe274-il-1000000.txt Download as CSV file: xf-goe274-il-1000000.csv |
XFOIL Version 6.96
Calculated polar for: GOE 274 (DAIMLER V) 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
------ -------- --------- --------- -------- -------- --------
-11.500 -0.2713 0.12541 0.12387 -0.0244 1.0000 0.0117
-11.250 -0.2712 0.12322 0.12170 -0.0237 1.0000 0.0120
-11.000 -0.2704 0.12081 0.11929 -0.0233 0.9999 0.0123
-10.750 -0.2618 0.11705 0.11553 -0.0255 0.9994 0.0129
-10.500 -0.2537 0.11292 0.11140 -0.0280 0.9987 0.0136
-10.250 -0.2479 0.10868 0.10716 -0.0308 0.9979 0.0138
-10.000 -0.2430 0.10440 0.10287 -0.0338 0.9971 0.0139
-9.750 -0.2388 0.09993 0.09840 -0.0368 0.9963 0.0139
-9.500 -0.2288 0.09526 0.09373 -0.0380 0.9956 0.0140
-9.250 -0.2176 0.09163 0.09010 -0.0397 0.9950 0.0142
-9.000 -0.2066 0.08805 0.08652 -0.0419 0.9943 0.0144
-8.750 -0.1971 0.08457 0.08304 -0.0438 0.9929 0.0147
-8.500 -0.1877 0.08094 0.07941 -0.0460 0.9911 0.0150
-8.250 -0.1777 0.07715 0.07562 -0.0485 0.9894 0.0156
-8.000 -0.1674 0.07292 0.07140 -0.0518 0.9877 0.0167
-7.750 -0.2697 0.08566 0.08408 -0.0422 0.9909 0.0150
-6.500 -0.1419 0.05999 0.05828 -0.0836 0.9764 0.0174
-6.250 -0.1182 0.05700 0.05526 -0.0870 0.9734 0.0176
-6.000 -0.0925 0.05392 0.05214 -0.0910 0.9702 0.0179
-5.750 -0.0702 0.05101 0.04918 -0.0939 0.9636 0.0184
-5.500 -0.0429 0.04772 0.04581 -0.0977 0.9585 0.0197
-5.250 0.0008 0.04226 0.04010 -0.1048 0.9524 0.0208
-5.000 0.0280 0.03881 0.03649 -0.1070 0.9458 0.0208
-4.750 0.0520 0.03373 0.03124 -0.1097 0.9396 0.0211
-4.500 0.0748 0.03193 0.02939 -0.1104 0.9319 0.0214
-4.250 0.1000 0.03020 0.02758 -0.1112 0.9253 0.0217
-4.000 0.1268 0.02837 0.02564 -0.1121 0.9173 0.0222
-3.750 0.1550 0.02648 0.02361 -0.1130 0.9083 0.0231
-3.500 0.1894 0.02479 0.02159 -0.1130 0.8977 0.0251
-3.250 0.2188 0.02307 0.01964 -0.1134 0.8849 0.0252
-3.000 0.2480 0.02138 0.01769 -0.1138 0.8710 0.0253
-2.750 0.2760 0.01786 0.01393 -0.1152 0.8557 0.0260
-2.500 0.3033 0.01691 0.01284 -0.1154 0.8358 0.0264
-2.250 0.3311 0.01608 0.01184 -0.1156 0.8133 0.0270
-2.000 0.3590 0.01531 0.01086 -0.1157 0.7866 0.0278
-1.750 0.3873 0.01471 0.00999 -0.1156 0.7541 0.0294
-1.500 0.4151 0.01517 0.01009 -0.1148 0.7117 0.0306
-1.250 0.4419 0.01490 0.00943 -0.1145 0.6514 0.0307
-1.000 0.4690 0.01308 0.00712 -0.1148 0.5799 0.0317
-0.750 0.4960 0.01265 0.00649 -0.1148 0.5377 0.0323
-0.500 0.5237 0.01231 0.00600 -0.1149 0.5121 0.0332
-0.250 0.5518 0.01207 0.00561 -0.1150 0.4914 0.0350
0.000 0.5797 0.01277 0.00612 -0.1147 0.4723 0.0375
0.250 0.6084 0.01141 0.00467 -0.1151 0.4577 0.0395
0.500 0.6365 0.01112 0.00435 -0.1152 0.4445 0.0412
0.750 0.6646 0.01100 0.00416 -0.1152 0.4309 0.0434
1.000 0.6927 0.01076 0.00384 -0.1153 0.4174 0.0483
1.250 0.7207 0.01055 0.00362 -0.1155 0.4049 0.0516
1.500 0.7487 0.01051 0.00354 -0.1155 0.3940 0.0547
1.750 0.7786 0.01001 0.00291 -0.1155 0.3847 0.0338
2.000 0.8068 0.00997 0.00283 -0.1156 0.3749 0.0346
2.250 0.8349 0.00996 0.00278 -0.1157 0.3647 0.0354
2.500 0.8631 0.00996 0.00276 -0.1158 0.3553 0.0361
2.750 0.8909 0.01002 0.00278 -0.1158 0.3451 0.0369
3.000 0.9186 0.01009 0.00281 -0.1158 0.3341 0.0379
3.250 0.9465 0.01011 0.00279 -0.1159 0.3236 0.0399
3.500 0.9740 0.01021 0.00286 -0.1159 0.3126 0.0431
3.750 1.0013 0.01035 0.00294 -0.1158 0.3004 0.0472
4.000 1.0229 0.00889 0.00326 -0.1151 0.2880 1.0000
4.250 1.0498 0.00912 0.00339 -0.1150 0.2728 1.0000
4.500 1.0763 0.00938 0.00356 -0.1148 0.2544 1.0000
4.750 1.1019 0.00975 0.00377 -0.1146 0.2289 1.0000
5.000 1.1276 0.01009 0.00399 -0.1143 0.2079 1.0000
5.250 1.1535 0.01040 0.00422 -0.1141 0.1942 1.0000
5.500 1.1795 0.01069 0.00445 -0.1138 0.1840 1.0000
5.750 1.2058 0.01093 0.00465 -0.1137 0.1781 1.0000
6.000 1.2317 0.01121 0.00489 -0.1134 0.1702 1.0000
6.250 1.2579 0.01144 0.00511 -0.1133 0.1647 1.0000
6.500 1.2833 0.01175 0.00538 -0.1130 0.1573 1.0000
6.750 1.3095 0.01195 0.00559 -0.1128 0.1521 1.0000
7.000 1.3345 0.01228 0.00588 -0.1124 0.1426 1.0000
7.250 1.3582 0.01275 0.00620 -0.1119 0.1180 1.0000
7.500 1.3753 0.01395 0.00706 -0.1104 0.0685 1.0000
7.750 1.3905 0.01535 0.00817 -0.1084 0.0197 1.0000
8.000 1.4128 0.01590 0.00874 -0.1075 0.0167 1.0000
8.250 1.4356 0.01637 0.00926 -0.1067 0.0156 1.0000
8.500 1.4579 0.01684 0.00978 -0.1059 0.0146 1.0000
8.750 1.4793 0.01739 0.01037 -0.1050 0.0136 1.0000
9.000 1.4984 0.01814 0.01119 -0.1036 0.0126 1.0000
9.250 1.5178 0.01881 0.01194 -0.1023 0.0121 1.0000
9.500 1.5379 0.01936 0.01255 -0.1011 0.0117 1.0000
9.750 1.5567 0.01998 0.01322 -0.0997 0.0112 1.0000
10.000 1.5742 0.02064 0.01394 -0.0982 0.0107 1.0000
10.250 1.5901 0.02136 0.01473 -0.0963 0.0103 1.0000
10.500 1.6039 0.02216 0.01559 -0.0942 0.0100 1.0000
10.750 1.6115 0.02323 0.01675 -0.0910 0.0096 1.0000
11.000 1.6066 0.02490 0.01857 -0.0858 0.0092 1.0000
11.250 1.6194 0.02560 0.01933 -0.0837 0.0090 1.0000
11.500 1.6286 0.02655 0.02036 -0.0811 0.0088 1.0000
11.750 1.6360 0.02768 0.02157 -0.0785 0.0086 1.0000
12.000 1.6418 0.02895 0.02293 -0.0758 0.0084 1.0000
12.250 1.6463 0.03039 0.02445 -0.0732 0.0082 1.0000
12.500 1.6496 0.03198 0.02614 -0.0707 0.0080 1.0000
12.750 1.6521 0.03374 0.02799 -0.0684 0.0078 1.0000
13.000 1.6530 0.03574 0.03009 -0.0663 0.0077 1.0000
13.250 1.6531 0.03795 0.03239 -0.0645 0.0075 1.0000
13.500 1.6511 0.04053 0.03507 -0.0629 0.0074 1.0000
13.750 1.6479 0.04341 0.03805 -0.0617 0.0073 1.0000
14.000 1.6415 0.04690 0.04165 -0.0609 0.0072 1.0000
14.250 1.6325 0.05099 0.04586 -0.0606 0.0071 1.0000
14.500 1.6207 0.05575 0.05075 -0.0610 0.0070 1.0000
14.750 1.6065 0.06123 0.05636 -0.0619 0.0070 1.0000
15.000 1.5910 0.06722 0.06249 -0.0634 0.0069 1.0000
15.250 1.5755 0.07330 0.06869 -0.0651 0.0069 1.0000
15.500 1.5573 0.07971 0.07522 -0.0667 0.0068 1.0000
15.750 1.5386 0.08602 0.08164 -0.0681 0.0067 1.0000
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