GOE 628 AIRFOIL (goe628-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: GOE 628 AIRFOIL (goe628-il) Reynolds number: 1,000,000 Max Cl/Cd: 111.41 at α=5.75° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-goe628-il-1000000.txt Download as CSV file: xf-goe628-il-1000000.csv |
XFOIL Version 6.96
Calculated polar for: GOE 628 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
------ -------- --------- --------- -------- -------- --------
-19.750 -0.7381 0.12462 0.12230 -0.0545 1.0000 0.0277
-19.500 -0.7865 0.11257 0.11009 -0.0618 1.0000 0.0291
-19.250 -0.8111 0.10497 0.10238 -0.0664 1.0000 0.0300
-19.000 -0.8235 0.09945 0.09685 -0.0697 1.0000 0.0307
-18.750 -0.8330 0.09450 0.09185 -0.0725 1.0000 0.0313
-18.500 -0.8441 0.08936 0.08665 -0.0755 1.0000 0.0320
-18.250 -0.8572 0.08401 0.08121 -0.0787 1.0000 0.0327
-18.000 -0.8703 0.07882 0.07593 -0.0818 1.0000 0.0332
-17.750 -0.8818 0.07389 0.07089 -0.0847 1.0000 0.0337
-17.500 -0.8882 0.06998 0.06698 -0.0868 1.0000 0.0343
-17.250 -0.8972 0.06580 0.06276 -0.0891 1.0000 0.0346
-17.000 -0.9041 0.06201 0.05893 -0.0911 1.0000 0.0349
-16.750 -0.9098 0.05848 0.05537 -0.0930 1.0000 0.0354
-16.500 -0.9212 0.05466 0.05150 -0.0948 1.0000 0.0357
-16.250 -0.9349 0.05082 0.04760 -0.0965 1.0000 0.0360
-16.000 -0.9489 0.04709 0.04381 -0.0979 1.0000 0.0363
-15.750 -0.9662 0.04339 0.04006 -0.0989 1.0000 0.0366
-15.500 -0.9905 0.03965 0.03627 -0.0991 1.0000 0.0368
-15.250 -1.0039 0.03555 0.03207 -0.1018 0.9991 0.0370
-15.000 -0.9818 0.03136 0.02774 -0.1102 0.9962 0.0376
-14.750 -0.9542 0.02768 0.02386 -0.1193 0.9923 0.0380
-14.500 -0.9394 0.02569 0.02179 -0.1213 0.9862 0.0386
-14.250 -0.9098 0.02460 0.02068 -0.1237 0.9832 0.0392
-14.000 -0.8777 0.02382 0.01987 -0.1259 0.9812 0.0397
-13.750 -0.8490 0.02313 0.01915 -0.1273 0.9779 0.0402
-13.500 -0.8220 0.02246 0.01842 -0.1282 0.9731 0.0408
-13.250 -0.7908 0.02177 0.01766 -0.1298 0.9698 0.0414
-13.000 -0.7553 0.02114 0.01695 -0.1322 0.9675 0.0421
-12.750 -0.7239 0.02073 0.01645 -0.1335 0.9625 0.0426
-12.500 -0.6934 0.02020 0.01583 -0.1346 0.9561 0.0430
-12.250 -0.6644 0.01890 0.01449 -0.1362 0.9500 0.0437
-12.000 -0.6396 0.01835 0.01391 -0.1361 0.9397 0.0442
-11.750 -0.6121 0.01793 0.01345 -0.1364 0.9304 0.0447
-11.500 -0.5871 0.01756 0.01302 -0.1361 0.9192 0.0453
-11.250 -0.5642 0.01719 0.01258 -0.1353 0.9072 0.0458
-11.000 -0.5407 0.01684 0.01214 -0.1346 0.8949 0.0463
-10.750 -0.5178 0.01651 0.01171 -0.1337 0.8812 0.0469
-10.500 -0.4945 0.01631 0.01142 -0.1328 0.8661 0.0475
-10.250 -0.4709 0.01613 0.01113 -0.1319 0.8496 0.0479
-10.000 -0.4487 0.01581 0.01068 -0.1309 0.8314 0.0484
-9.750 -0.4302 0.01499 0.00979 -0.1294 0.8118 0.0492
-9.500 -0.4084 0.01462 0.00934 -0.1283 0.7925 0.0498
-9.250 -0.3857 0.01432 0.00895 -0.1273 0.7754 0.0502
-9.000 -0.3626 0.01401 0.00856 -0.1263 0.7614 0.0506
-8.500 -0.3148 0.01340 0.00780 -0.1246 0.7387 0.0514
-8.250 -0.2907 0.01314 0.00745 -0.1238 0.7290 0.0518
-8.000 -0.2654 0.01284 0.00710 -0.1232 0.7213 0.0522
-7.750 -0.2405 0.01258 0.00678 -0.1225 0.7132 0.0526
-7.500 -0.2150 0.01233 0.00648 -0.1219 0.7059 0.0530
-7.250 -0.1893 0.01210 0.00619 -0.1213 0.6979 0.0534
-7.000 -0.1637 0.01192 0.00594 -0.1207 0.6893 0.0537
-6.750 -0.1372 0.01174 0.00571 -0.1202 0.6809 0.0540
-6.500 -0.1132 0.01138 0.00527 -0.1193 0.6724 0.0545
-6.250 -0.0878 0.01100 0.00487 -0.1187 0.6660 0.0552
-6.000 -0.0619 0.01073 0.00456 -0.1182 0.6595 0.0559
-5.750 -0.0360 0.01055 0.00432 -0.1176 0.6526 0.0565
-5.500 -0.0089 0.01034 0.00409 -0.1173 0.6466 0.0571
-5.250 0.0179 0.01017 0.00389 -0.1168 0.6402 0.0578
-5.000 0.0444 0.01004 0.00370 -0.1163 0.6337 0.0585
-4.750 0.0719 0.00989 0.00352 -0.1160 0.6278 0.0592
-4.500 0.0991 0.00976 0.00335 -0.1156 0.6208 0.0599
-4.250 0.1259 0.00969 0.00321 -0.1151 0.6136 0.0604
-4.000 0.1532 0.00949 0.00300 -0.1148 0.6075 0.0620
-3.750 0.1801 0.00935 0.00283 -0.1144 0.6007 0.0636
-3.500 0.2070 0.00925 0.00270 -0.1139 0.5939 0.0651
-3.250 0.2346 0.00915 0.00258 -0.1136 0.5868 0.0668
-3.000 0.2613 0.00907 0.00246 -0.1131 0.5790 0.0698
-2.500 0.3137 0.00860 0.00219 -0.1122 0.5644 0.1272
-2.250 0.3390 0.00836 0.00210 -0.1116 0.5571 0.1752
-2.000 0.3661 0.00824 0.00207 -0.1113 0.5498 0.2034
-1.750 0.3925 0.00822 0.00206 -0.1108 0.5414 0.2225
-1.500 0.4199 0.00820 0.00206 -0.1105 0.5335 0.2361
-1.250 0.4464 0.00822 0.00208 -0.1100 0.5243 0.2499
-1.000 0.4736 0.00823 0.00209 -0.1096 0.5162 0.2600
-0.750 0.5003 0.00828 0.00211 -0.1092 0.5071 0.2686
-0.500 0.5272 0.00831 0.00213 -0.1088 0.4987 0.2766
-0.250 0.5537 0.00836 0.00216 -0.1083 0.4890 0.2845
0.000 0.5804 0.00843 0.00219 -0.1078 0.4796 0.2908
0.250 0.6060 0.00851 0.00224 -0.1072 0.4683 0.2995
0.500 0.6326 0.00858 0.00229 -0.1068 0.4577 0.3073
0.750 0.6581 0.00867 0.00235 -0.1061 0.4464 0.3159
1.000 0.6837 0.00877 0.00243 -0.1055 0.4347 0.3245
1.250 0.7093 0.00887 0.00249 -0.1049 0.4236 0.3321
1.500 0.7341 0.00899 0.00258 -0.1042 0.4118 0.3400
1.750 0.7591 0.00913 0.00267 -0.1035 0.3998 0.3466
2.000 0.7838 0.00924 0.00277 -0.1028 0.3885 0.3557
2.250 0.8077 0.00941 0.00288 -0.1019 0.3776 0.3641
2.500 0.8325 0.00952 0.00298 -0.1012 0.3684 0.3717
2.750 0.8562 0.00967 0.00310 -0.1003 0.3596 0.3795
3.000 0.8811 0.00979 0.00320 -0.0996 0.3527 0.3861
3.250 0.9041 0.00994 0.00334 -0.0986 0.3453 0.3954
3.500 0.9285 0.01005 0.00345 -0.0978 0.3399 0.4045
3.750 0.9521 0.01016 0.00358 -0.0969 0.3343 0.4150
4.250 0.9977 0.01043 0.00387 -0.0948 0.3241 0.4384
4.500 1.0211 0.01051 0.00400 -0.0939 0.3204 0.4547
4.750 1.0423 0.01062 0.00415 -0.0926 0.3165 0.4753
5.000 1.0611 0.01073 0.00431 -0.0908 0.3123 0.5039
5.250 1.0785 0.01077 0.00451 -0.0888 0.3085 0.5695
5.500 1.1488 0.01032 0.00497 -0.0980 0.3044 1.0000
5.750 1.1687 0.01049 0.00512 -0.0964 0.3013 1.0000
6.000 1.1874 0.01069 0.00529 -0.0946 0.2981 1.0000
6.250 1.2051 0.01093 0.00550 -0.0927 0.2945 1.0000
6.500 1.2235 0.01117 0.00573 -0.0909 0.2915 1.0000
6.750 1.2454 0.01131 0.00589 -0.0898 0.2897 1.0000
7.000 1.2668 0.01148 0.00607 -0.0886 0.2873 1.0000
7.250 1.2871 0.01169 0.00628 -0.0873 0.2846 1.0000
7.500 1.3066 0.01194 0.00651 -0.0858 0.2818 1.0000
7.750 1.3248 0.01224 0.00680 -0.0842 0.2786 1.0000
8.000 1.3421 0.01259 0.00714 -0.0825 0.2751 1.0000
8.250 1.3651 0.01274 0.00732 -0.0818 0.2727 1.0000
8.500 1.3863 0.01296 0.00755 -0.0808 0.2698 1.0000
8.750 1.4060 0.01324 0.00783 -0.0795 0.2666 1.0000
9.000 1.4247 0.01358 0.00817 -0.0782 0.2640 1.0000
9.250 1.4414 0.01401 0.00859 -0.0767 0.2608 1.0000
9.500 1.4601 0.01438 0.00897 -0.0754 0.2585 1.0000
9.750 1.4812 0.01464 0.00928 -0.0746 0.2566 1.0000
10.000 1.5015 0.01496 0.00962 -0.0736 0.2545 1.0000
10.250 1.5208 0.01533 0.01001 -0.0726 0.2519 1.0000
10.500 1.5386 0.01578 0.01047 -0.0715 0.2492 1.0000
10.750 1.5551 0.01631 0.01100 -0.0702 0.2463 1.0000
11.000 1.5696 0.01696 0.01166 -0.0687 0.2432 1.0000
11.250 1.5902 0.01732 0.01207 -0.0680 0.2416 1.0000
11.500 1.6096 0.01775 0.01254 -0.0672 0.2393 1.0000
11.750 1.6273 0.01827 0.01309 -0.0663 0.2366 1.0000
12.000 1.6435 0.01889 0.01373 -0.0653 0.2337 1.0000
12.250 1.6565 0.01973 0.01455 -0.0640 0.2298 1.0000
12.500 1.6732 0.02036 0.01523 -0.0631 0.2263 1.0000
12.750 1.6907 0.02095 0.01585 -0.0623 0.2222 1.0000
13.000 1.7044 0.02180 0.01671 -0.0613 0.2181 1.0000
13.250 1.7143 0.02292 0.01782 -0.0600 0.2136 1.0000
13.500 1.7306 0.02365 0.01860 -0.0593 0.2107 1.0000
13.750 1.7448 0.02453 0.01952 -0.0584 0.2069 1.0000
14.000 1.7539 0.02579 0.02077 -0.0573 0.2015 1.0000
14.250 1.7639 0.02702 0.02204 -0.0563 0.1979 1.0000
14.500 1.7767 0.02807 0.02313 -0.0556 0.1939 1.0000
14.750 1.7850 0.02950 0.02457 -0.0546 0.1889 1.0000
15.000 1.7905 0.03117 0.02625 -0.0536 0.1836 1.0000
15.250 1.7996 0.03258 0.02770 -0.0528 0.1792 1.0000
15.500 1.8010 0.03467 0.02978 -0.0518 0.1726 1.0000
15.750 1.8070 0.03640 0.03154 -0.0510 0.1675 1.0000
16.000 1.8081 0.03858 0.03374 -0.0501 0.1616 1.0000
16.250 1.8081 0.04092 0.03610 -0.0493 0.1561 1.0000
16.500 1.8097 0.04315 0.03836 -0.0486 0.1511 1.0000
16.750 1.8041 0.04612 0.04133 -0.0478 0.1448 1.0000
17.000 1.8037 0.04861 0.04386 -0.0473 0.1399 1.0000
17.250 1.7952 0.05200 0.04727 -0.0467 0.1343 1.0000
17.500 1.7903 0.05512 0.05042 -0.0463 0.1290 1.0000
17.750 1.7810 0.05872 0.05405 -0.0460 0.1242 1.0000
18.000 1.7734 0.06222 0.05761 -0.0458 0.1207 1.0000
18.250 1.7682 0.06552 0.06095 -0.0457 0.1170 1.0000
18.500 1.7558 0.06968 0.06515 -0.0457 0.1130 1.0000
18.750 1.7451 0.07370 0.06924 -0.0458 0.1099 1.0000
19.000 1.7365 0.07755 0.07315 -0.0461 0.1068 1.0000
19.250 1.7224 0.08211 0.07777 -0.0465 0.1034 1.0000
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