GOE 620 AIRFOIL (goe620-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: GOE 620 AIRFOIL (goe620-il) Reynolds number: 1,000,000 Max Cl/Cd: 87.61 at α=5.75° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-goe620-il-1000000-n5.txt Download as CSV file: xf-goe620-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: GOE 620 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
------ -------- --------- --------- -------- -------- --------
-18.500 -0.6320 0.10296 0.10033 -0.0934 0.9956 0.0273
-18.250 -0.6559 0.09478 0.09203 -0.0990 0.9936 0.0276
-18.000 -0.6728 0.08834 0.08549 -0.1032 0.9913 0.0277
-17.750 -0.6877 0.08209 0.07915 -0.1076 0.9892 0.0279
-17.500 -0.6986 0.07639 0.07335 -0.1120 0.9867 0.0281
-17.250 -0.7078 0.07090 0.06778 -0.1165 0.9841 0.0282
-16.750 -0.7321 0.06011 0.05680 -0.1251 0.9760 0.0283
-16.500 -0.7422 0.05482 0.05140 -0.1298 0.9711 0.0285
-16.250 -0.7506 0.04931 0.04578 -0.1355 0.9664 0.0286
-16.000 -0.7598 0.04354 0.03989 -0.1418 0.9582 0.0287
-15.750 -0.7581 0.03800 0.03423 -0.1495 0.9503 0.0289
-15.500 -0.7465 0.03290 0.02899 -0.1581 0.9403 0.0292
-15.250 -0.7188 0.02881 0.02476 -0.1675 0.9324 0.0294
-15.000 -0.6879 0.02541 0.02120 -0.1764 0.9211 0.0297
-14.750 -0.6673 0.02281 0.01842 -0.1820 0.9039 0.0299
-14.500 -0.6586 0.02131 0.01676 -0.1829 0.8846 0.0301
-14.250 -0.6584 0.02022 0.01552 -0.1809 0.8662 0.0302
-14.000 -0.6545 0.01954 0.01473 -0.1782 0.8510 0.0304
-13.750 -0.6521 0.01893 0.01401 -0.1749 0.8375 0.0306
-13.500 -0.6483 0.01846 0.01345 -0.1714 0.8259 0.0308
-13.250 -0.6377 0.01802 0.01292 -0.1690 0.8153 0.0310
-13.000 -0.6246 0.01756 0.01237 -0.1669 0.8065 0.0312
-12.750 -0.6099 0.01715 0.01187 -0.1651 0.7974 0.0315
-12.500 -0.5940 0.01674 0.01138 -0.1634 0.7898 0.0317
-12.250 -0.5764 0.01636 0.01093 -0.1618 0.7824 0.0319
-11.750 -0.5375 0.01570 0.01012 -0.1593 0.7709 0.0324
-11.500 -0.5189 0.01528 0.00965 -0.1579 0.7652 0.0328
-11.250 -0.4997 0.01490 0.00921 -0.1566 0.7594 0.0331
-11.000 -0.4787 0.01457 0.00884 -0.1555 0.7548 0.0335
-10.750 -0.4565 0.01426 0.00849 -0.1546 0.7506 0.0338
-10.500 -0.4340 0.01398 0.00817 -0.1537 0.7460 0.0342
-10.250 -0.4117 0.01372 0.00786 -0.1527 0.7411 0.0345
-10.000 -0.3887 0.01347 0.00756 -0.1519 0.7364 0.0349
-9.750 -0.3650 0.01322 0.00727 -0.1511 0.7317 0.0353
-9.500 -0.3416 0.01298 0.00698 -0.1503 0.7267 0.0357
-9.250 -0.3180 0.01276 0.00671 -0.1495 0.7225 0.0361
-9.000 -0.2939 0.01256 0.00644 -0.1487 0.7189 0.0364
-8.750 -0.2688 0.01234 0.00620 -0.1482 0.7158 0.0367
-8.500 -0.2449 0.01205 0.00589 -0.1475 0.7122 0.0373
-8.250 -0.2203 0.01183 0.00565 -0.1468 0.7088 0.0379
-8.000 -0.1955 0.01165 0.00544 -0.1462 0.7052 0.0385
-7.750 -0.1706 0.01149 0.00524 -0.1455 0.7017 0.0391
-7.500 -0.1450 0.01131 0.00504 -0.1450 0.6988 0.0397
-7.250 -0.1192 0.01113 0.00484 -0.1445 0.6958 0.0403
-7.000 -0.0933 0.01097 0.00465 -0.1441 0.6924 0.0408
-6.750 -0.0676 0.01083 0.00448 -0.1435 0.6888 0.0413
-6.500 -0.0425 0.01066 0.00427 -0.1429 0.6853 0.0420
-6.250 -0.0175 0.01050 0.00409 -0.1423 0.6818 0.0427
-6.000 0.0088 0.01034 0.00393 -0.1419 0.6791 0.0435
-5.750 0.0350 0.01019 0.00378 -0.1414 0.6755 0.0444
-5.500 0.0611 0.01007 0.00364 -0.1410 0.6717 0.0453
-5.250 0.0869 0.00997 0.00351 -0.1404 0.6678 0.0461
-5.000 0.1123 0.00989 0.00338 -0.1398 0.6637 0.0468
-4.750 0.1385 0.00973 0.00322 -0.1394 0.6604 0.0480
-4.500 0.1646 0.00960 0.00309 -0.1389 0.6564 0.0491
-4.250 0.1904 0.00950 0.00298 -0.1383 0.6518 0.0503
-4.000 0.2155 0.00943 0.00287 -0.1377 0.6469 0.0514
-3.750 0.2417 0.00935 0.00278 -0.1372 0.6428 0.0526
-3.500 0.2675 0.00923 0.00267 -0.1367 0.6379 0.0547
-3.250 0.2925 0.00915 0.00257 -0.1360 0.6321 0.0567
-3.000 0.3173 0.00909 0.00249 -0.1352 0.6264 0.0589
-2.750 0.3428 0.00899 0.00241 -0.1346 0.6206 0.0631
-2.500 0.3667 0.00889 0.00233 -0.1337 0.6137 0.0729
-2.250 0.3898 0.00874 0.00225 -0.1327 0.6065 0.0974
-2.000 0.4129 0.00868 0.00220 -0.1316 0.5965 0.1105
-1.750 0.4352 0.00865 0.00216 -0.1304 0.5851 0.1224
-1.500 0.4556 0.00865 0.00214 -0.1288 0.5708 0.1357
-1.250 0.4750 0.00867 0.00215 -0.1270 0.5554 0.1531
-1.000 0.4951 0.00865 0.00216 -0.1253 0.5432 0.1739
-0.750 0.5157 0.00866 0.00216 -0.1237 0.5348 0.1867
-0.500 0.5350 0.00869 0.00218 -0.1219 0.5249 0.1980
-0.250 0.5557 0.00873 0.00220 -0.1203 0.5161 0.2068
0.000 0.5746 0.00880 0.00225 -0.1184 0.5056 0.2182
0.250 0.5955 0.00883 0.00230 -0.1169 0.4962 0.2304
0.500 0.6139 0.00895 0.00237 -0.1150 0.4857 0.2397
0.750 0.6351 0.00901 0.00244 -0.1136 0.4767 0.2511
1.000 0.6543 0.00914 0.00254 -0.1118 0.4672 0.2620
1.250 0.6754 0.00922 0.00263 -0.1104 0.4583 0.2753
1.500 0.6940 0.00934 0.00275 -0.1085 0.4492 0.2925
1.750 0.7149 0.00941 0.00286 -0.1071 0.4420 0.3132
2.000 0.7344 0.00952 0.00299 -0.1055 0.4343 0.3322
2.250 0.7549 0.00962 0.00311 -0.1040 0.4276 0.3512
2.500 0.7735 0.00976 0.00326 -0.1022 0.4180 0.3673
2.750 0.7922 0.00991 0.00341 -0.1004 0.4092 0.3837
3.000 0.8111 0.01005 0.00357 -0.0987 0.4007 0.4025
3.250 0.8299 0.01022 0.00373 -0.0970 0.3932 0.4179
3.500 0.8479 0.01039 0.00391 -0.0952 0.3842 0.4352
3.750 0.8655 0.01057 0.00411 -0.0933 0.3760 0.4555
4.000 0.8830 0.01075 0.00433 -0.0914 0.3666 0.4827
4.250 0.8995 0.01094 0.00457 -0.0894 0.3586 0.5145
4.500 0.9158 0.01116 0.00482 -0.0874 0.3488 0.5453
4.750 0.9315 0.01141 0.00510 -0.0853 0.3386 0.5758
5.000 0.9460 0.01168 0.00540 -0.0830 0.3294 0.6078
5.250 0.9612 0.01190 0.00570 -0.0808 0.3196 0.6497
5.750 1.1012 0.01257 0.00688 -0.1006 0.2809 1.0000
6.000 1.1190 0.01297 0.00724 -0.0991 0.2724 1.0000
6.250 1.1341 0.01349 0.00769 -0.0972 0.2619 1.0000
6.500 1.1510 0.01395 0.00811 -0.0957 0.2526 1.0000
6.750 1.1670 0.01447 0.00859 -0.0941 0.2447 1.0000
7.000 1.1850 0.01492 0.00901 -0.0928 0.2391 1.0000
7.250 1.2020 0.01543 0.00949 -0.0914 0.2328 1.0000
7.500 1.2184 0.01598 0.01001 -0.0900 0.2270 1.0000
7.750 1.2367 0.01645 0.01048 -0.0889 0.2230 1.0000
8.000 1.2540 0.01698 0.01099 -0.0877 0.2184 1.0000
8.250 1.2697 0.01760 0.01160 -0.0863 0.2137 1.0000
8.500 1.2874 0.01815 0.01214 -0.0852 0.2101 1.0000
8.750 1.3040 0.01875 0.01274 -0.0841 0.2054 1.0000
9.000 1.3203 0.01939 0.01337 -0.0829 0.2013 1.0000
9.250 1.3346 0.02016 0.01412 -0.0815 0.1960 1.0000
9.500 1.3504 0.02085 0.01481 -0.0804 0.1901 1.0000
9.750 1.3628 0.02177 0.01568 -0.0789 0.1824 1.0000
10.000 1.3721 0.02290 0.01675 -0.0772 0.1682 1.0000
10.250 1.3653 0.02509 0.01874 -0.0740 0.1350 1.0000
10.500 1.3735 0.02638 0.02000 -0.0723 0.1275 1.0000
10.750 1.3856 0.02744 0.02106 -0.0711 0.1240 1.0000
11.000 1.3954 0.02868 0.02230 -0.0698 0.1197 1.0000
11.250 1.4088 0.02969 0.02332 -0.0688 0.1178 1.0000
11.500 1.4218 0.03073 0.02440 -0.0678 0.1168 1.0000
11.750 1.4339 0.03186 0.02555 -0.0668 0.1153 1.0000
12.000 1.4447 0.03310 0.02681 -0.0658 0.1134 1.0000
12.250 1.4546 0.03445 0.02816 -0.0647 0.1115 1.0000
12.500 1.4650 0.03575 0.02949 -0.0637 0.1098 1.0000
12.750 1.4744 0.03716 0.03093 -0.0627 0.1081 1.0000
13.000 1.4843 0.03855 0.03234 -0.0617 0.1063 1.0000
13.250 1.4960 0.03982 0.03366 -0.0610 0.1059 1.0000
13.500 1.5077 0.04109 0.03498 -0.0602 0.1053 1.0000
13.750 1.5190 0.04240 0.03633 -0.0595 0.1045 1.0000
14.000 1.5287 0.04388 0.03786 -0.0588 0.1038 1.0000
14.250 1.5385 0.04534 0.03935 -0.0580 0.1027 1.0000
14.500 1.5473 0.04694 0.04099 -0.0573 0.1021 1.0000
14.750 1.5555 0.04859 0.04269 -0.0566 0.1010 1.0000
15.000 1.5624 0.05039 0.04452 -0.0559 0.0998 1.0000
15.250 1.5688 0.05227 0.04644 -0.0552 0.0985 1.0000
15.500 1.5742 0.05426 0.04847 -0.0545 0.0974 1.0000
15.750 1.5780 0.05642 0.05068 -0.0538 0.0956 1.0000
16.000 1.5844 0.05836 0.05267 -0.0533 0.0948 1.0000
16.250 1.5933 0.06007 0.05443 -0.0529 0.0941 1.0000
16.500 1.6009 0.06190 0.05631 -0.0525 0.0933 1.0000
16.750 1.6070 0.06393 0.05840 -0.0522 0.0920 1.0000
17.000 1.6128 0.06597 0.06048 -0.0518 0.0900 1.0000
17.250 1.6159 0.06833 0.06289 -0.0515 0.0885 1.0000
17.500 1.6183 0.07077 0.06536 -0.0511 0.0864 1.0000
17.750 1.6193 0.07343 0.06807 -0.0509 0.0848 1.0000
18.000 1.6239 0.07567 0.07037 -0.0507 0.0830 1.0000
18.250 1.6250 0.07836 0.07309 -0.0505 0.0791 1.0000
18.500 1.6213 0.08158 0.07631 -0.0504 0.0736 1.0000
18.750 1.6105 0.08569 0.08038 -0.0504 0.0649 1.0000
19.000 1.5998 0.08988 0.08458 -0.0505 0.0597 1.0000
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