GOE 522 AIRFOIL (goe522-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: GOE 522 AIRFOIL (goe522-il) Reynolds number: 1,000,000 Max Cl/Cd: 70.7 at α=5.5° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-goe522-il-1000000-n5.txt Download as CSV file: xf-goe522-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: GOE 522 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
------ -------- --------- --------- -------- -------- --------
-19.500 -0.6127 0.10641 0.10292 -0.0984 0.9898 0.0241
-19.250 -0.6075 0.10320 0.09967 -0.1007 0.9882 0.0241
-19.000 -0.6031 0.09981 0.09624 -0.1031 0.9865 0.0242
-18.750 -0.5997 0.09620 0.09258 -0.1058 0.9849 0.0243
-18.500 -0.5924 0.09325 0.08960 -0.1081 0.9832 0.0243
-18.250 -0.5875 0.08976 0.08607 -0.1108 0.9816 0.0244
-18.000 -0.5814 0.08639 0.08266 -0.1136 0.9801 0.0245
-17.750 -0.5749 0.08311 0.07933 -0.1164 0.9788 0.0246
-17.500 -0.5702 0.07987 0.07605 -0.1188 0.9766 0.0246
-17.250 -0.5667 0.07693 0.07307 -0.1204 0.9727 0.0247
-17.000 -0.5617 0.07375 0.06985 -0.1229 0.9696 0.0247
-16.750 -0.5527 0.07077 0.06683 -0.1257 0.9666 0.0247
-16.500 -0.5436 0.06751 0.06352 -0.1290 0.9640 0.0248
-16.250 -0.5359 0.06438 0.06033 -0.1319 0.9604 0.0248
-16.000 -0.5276 0.06125 0.05715 -0.1350 0.9547 0.0249
-15.750 -0.5167 0.05814 0.05397 -0.1385 0.9499 0.0249
-15.500 -0.5039 0.05508 0.05085 -0.1424 0.9446 0.0250
-15.250 -0.4952 0.05211 0.04781 -0.1456 0.9368 0.0250
-15.000 -0.4827 0.04915 0.04477 -0.1494 0.9302 0.0250
-14.750 -0.4728 0.04629 0.04184 -0.1528 0.9238 0.0251
-14.500 -0.4651 0.04312 0.03859 -0.1566 0.9162 0.0252
-14.250 -0.4484 0.03981 0.03518 -0.1624 0.9103 0.0252
-14.000 -0.4362 0.03675 0.03204 -0.1669 0.9018 0.0253
-13.750 -0.4229 0.03388 0.02905 -0.1712 0.8918 0.0254
-13.500 -0.4147 0.03127 0.02635 -0.1740 0.8819 0.0255
-13.250 -0.4075 0.02883 0.02379 -0.1763 0.8709 0.0256
-13.000 -0.4028 0.02665 0.02153 -0.1775 0.8617 0.0256
-12.750 -0.3982 0.02471 0.01949 -0.1782 0.8514 0.0257
-12.500 -0.3941 0.02295 0.01764 -0.1784 0.8417 0.0258
-12.250 -0.3906 0.02146 0.01603 -0.1779 0.8288 0.0258
-12.000 -0.3887 0.02003 0.01453 -0.1770 0.8174 0.0259
-11.750 -0.3873 0.01890 0.01329 -0.1753 0.8063 0.0260
-11.500 -0.3848 0.01802 0.01233 -0.1731 0.7942 0.0261
-11.250 -0.3832 0.01730 0.01152 -0.1703 0.7831 0.0261
-11.000 -0.3807 0.01671 0.01086 -0.1671 0.7731 0.0262
-10.750 -0.3777 0.01625 0.01032 -0.1635 0.7648 0.0262
-10.500 -0.3739 0.01588 0.00991 -0.1598 0.7566 0.0264
-10.250 -0.3649 0.01556 0.00951 -0.1568 0.7481 0.0265
-10.000 -0.3513 0.01522 0.00912 -0.1546 0.7407 0.0265
-9.750 -0.3360 0.01492 0.00878 -0.1527 0.7314 0.0267
-9.500 -0.3204 0.01464 0.00842 -0.1507 0.7231 0.0268
-9.250 -0.3024 0.01434 0.00809 -0.1491 0.7155 0.0270
-9.000 -0.2844 0.01408 0.00777 -0.1475 0.7073 0.0271
-8.750 -0.2652 0.01383 0.00747 -0.1460 0.6999 0.0273
-8.500 -0.2451 0.01360 0.00720 -0.1447 0.6910 0.0275
-8.250 -0.2260 0.01340 0.00693 -0.1431 0.6811 0.0277
-8.000 -0.2050 0.01320 0.00668 -0.1419 0.6707 0.0279
-7.750 -0.1850 0.01303 0.00645 -0.1404 0.6599 0.0280
-7.500 -0.1640 0.01285 0.00622 -0.1391 0.6481 0.0282
-7.250 -0.1436 0.01270 0.00601 -0.1377 0.6353 0.0284
-7.000 -0.1241 0.01259 0.00581 -0.1361 0.6193 0.0285
-6.750 -0.1058 0.01245 0.00558 -0.1342 0.6001 0.0287
-6.500 -0.0880 0.01234 0.00536 -0.1323 0.5790 0.0290
-6.000 -0.0494 0.01215 0.00501 -0.1289 0.5462 0.0295
-5.750 -0.0288 0.01205 0.00485 -0.1275 0.5356 0.0297
-5.500 -0.0071 0.01193 0.00469 -0.1262 0.5270 0.0301
-5.250 0.0137 0.01185 0.00456 -0.1248 0.5186 0.0304
-5.000 0.0364 0.01174 0.00442 -0.1237 0.5126 0.0306
-4.750 0.0585 0.01165 0.00430 -0.1225 0.5063 0.0310
-4.500 0.0792 0.01158 0.00418 -0.1210 0.4999 0.0314
-4.250 0.0996 0.01150 0.00407 -0.1194 0.4949 0.0317
-4.000 0.1212 0.01139 0.00395 -0.1180 0.4914 0.0321
-3.750 0.1424 0.01128 0.00383 -0.1166 0.4875 0.0328
-3.500 0.1636 0.01119 0.00372 -0.1152 0.4834 0.0337
-3.250 0.1846 0.01114 0.00364 -0.1137 0.4789 0.0345
-3.000 0.2058 0.01108 0.00356 -0.1123 0.4739 0.0358
-2.500 0.2477 0.01068 0.00330 -0.1096 0.4661 0.0778
-2.250 0.2693 0.01062 0.00325 -0.1083 0.4618 0.0865
-2.000 0.2905 0.01055 0.00321 -0.1069 0.4579 0.0975
-1.750 0.3114 0.01047 0.00319 -0.1056 0.4535 0.1163
-1.500 0.3348 0.01041 0.00319 -0.1046 0.4509 0.1298
-1.250 0.3577 0.01037 0.00319 -0.1036 0.4472 0.1416
-1.000 0.3803 0.01037 0.00321 -0.1025 0.4435 0.1513
-0.750 0.4020 0.01039 0.00324 -0.1012 0.4388 0.1595
-0.500 0.4235 0.01043 0.00328 -0.1000 0.4345 0.1687
-0.250 0.4457 0.01037 0.00329 -0.0989 0.4314 0.1899
0.000 0.4668 0.01023 0.00333 -0.0976 0.4283 0.2415
0.250 0.4892 0.01023 0.00340 -0.0966 0.4251 0.2618
0.500 0.5113 0.01028 0.00348 -0.0954 0.4213 0.2770
0.750 0.5326 0.01037 0.00357 -0.0941 0.4167 0.2863
1.000 0.5546 0.01045 0.00366 -0.0930 0.4127 0.2946
1.250 0.5778 0.01053 0.00374 -0.0921 0.4087 0.3001
1.500 0.5995 0.01061 0.00383 -0.0909 0.4039 0.3089
1.750 0.6203 0.01072 0.00395 -0.0895 0.3989 0.3186
2.000 0.6415 0.01086 0.00407 -0.0883 0.3951 0.3243
2.250 0.6642 0.01093 0.00417 -0.0874 0.3918 0.3332
2.500 0.6864 0.01103 0.00428 -0.0863 0.3878 0.3383
2.750 0.7077 0.01116 0.00441 -0.0851 0.3839 0.3452
3.000 0.7277 0.01130 0.00457 -0.0837 0.3795 0.3558
3.250 0.7483 0.01145 0.00472 -0.0825 0.3756 0.3656
3.500 0.7704 0.01155 0.00486 -0.0815 0.3722 0.3770
3.750 0.7917 0.01169 0.00502 -0.0803 0.3680 0.3877
4.000 0.8110 0.01187 0.00522 -0.0789 0.3632 0.3992
4.250 0.8296 0.01208 0.00543 -0.0774 0.3582 0.4148
4.500 0.8507 0.01221 0.00562 -0.0763 0.3542 0.4322
4.750 0.8707 0.01238 0.00583 -0.0750 0.3489 0.4503
5.000 0.8883 0.01264 0.00610 -0.0734 0.3429 0.4678
5.250 0.9074 0.01286 0.00635 -0.0720 0.3380 0.4827
5.500 0.9262 0.01310 0.00661 -0.0706 0.3315 0.4960
5.750 0.9431 0.01343 0.00692 -0.0690 0.3244 0.5094
6.000 0.9614 0.01369 0.00721 -0.0676 0.3176 0.5243
6.250 0.9767 0.01408 0.00759 -0.0657 0.3093 0.5382
6.500 0.9930 0.01443 0.00796 -0.0641 0.3003 0.5567
6.750 1.0073 0.01487 0.00839 -0.0622 0.2905 0.5718
7.000 1.0215 0.01532 0.00884 -0.0603 0.2810 0.5882
7.250 1.0347 0.01583 0.00935 -0.0583 0.2712 0.6071
7.500 1.0483 0.01633 0.00986 -0.0565 0.2624 0.6276
7.750 1.0608 0.01687 0.01043 -0.0545 0.2539 0.6524
8.000 1.0721 0.01746 0.01106 -0.0524 0.2453 0.6831
8.250 1.0866 0.01786 0.01160 -0.0507 0.2407 0.7308
8.500 1.2169 0.01871 0.01291 -0.0733 0.2270 0.9962
8.750 1.2422 0.01931 0.01350 -0.0737 0.2245 1.0000
9.000 1.2599 0.01992 0.01411 -0.0728 0.2216 1.0000
9.250 1.2757 0.02064 0.01482 -0.0718 0.2181 1.0000
9.500 1.2923 0.02134 0.01551 -0.0709 0.2154 1.0000
9.750 1.3081 0.02210 0.01626 -0.0699 0.2123 1.0000
10.000 1.3254 0.02279 0.01697 -0.0691 0.2104 1.0000
10.250 1.3428 0.02348 0.01767 -0.0684 0.2088 1.0000
10.500 1.3593 0.02424 0.01844 -0.0676 0.2071 1.0000
10.750 1.3744 0.02510 0.01930 -0.0667 0.2054 1.0000
11.000 1.3901 0.02593 0.02015 -0.0659 0.2040 1.0000
11.250 1.4040 0.02689 0.02113 -0.0650 0.2024 1.0000
11.500 1.4175 0.02791 0.02215 -0.0642 0.2007 1.0000
11.750 1.4318 0.02888 0.02314 -0.0634 0.1994 1.0000
12.000 1.4437 0.03004 0.02433 -0.0625 0.1979 1.0000
12.250 1.4592 0.03095 0.02527 -0.0618 0.1974 1.0000
12.500 1.4738 0.03194 0.02629 -0.0612 0.1967 1.0000
12.750 1.4874 0.03303 0.02742 -0.0605 0.1960 1.0000
13.000 1.5014 0.03408 0.02851 -0.0599 0.1952 1.0000
13.250 1.5134 0.03531 0.02977 -0.0592 0.1936 1.0000
13.500 1.5255 0.03654 0.03104 -0.0585 0.1928 1.0000
13.750 1.5370 0.03783 0.03235 -0.0579 0.1915 1.0000
14.000 1.5460 0.03935 0.03391 -0.0571 0.1902 1.0000
14.250 1.5557 0.04081 0.03540 -0.0564 0.1889 1.0000
14.500 1.5633 0.04250 0.03713 -0.0557 0.1879 1.0000
14.750 1.5714 0.04414 0.03881 -0.0551 0.1867 1.0000
15.000 1.5768 0.04608 0.04078 -0.0544 0.1854 1.0000
15.250 1.5831 0.04792 0.04266 -0.0538 0.1842 1.0000
15.500 1.5903 0.04971 0.04450 -0.0532 0.1836 1.0000
15.750 1.6002 0.05127 0.04611 -0.0529 0.1831 1.0000
16.000 1.6089 0.05296 0.04786 -0.0525 0.1825 1.0000
16.250 1.6168 0.05474 0.04970 -0.0521 0.1817 1.0000
16.500 1.6251 0.05647 0.05148 -0.0518 0.1806 1.0000
16.750 1.6304 0.05853 0.05359 -0.0515 0.1793 1.0000
17.000 1.6365 0.06049 0.05560 -0.0512 0.1776 1.0000
17.250 1.6391 0.06286 0.05801 -0.0509 0.1762 1.0000
17.500 1.6434 0.06503 0.06022 -0.0506 0.1749 1.0000
17.750 1.6424 0.06783 0.06306 -0.0503 0.1730 1.0000
18.000 1.6422 0.07049 0.06576 -0.0501 0.1711 1.0000
18.250 1.6470 0.07266 0.06800 -0.0500 0.1697 1.0000
18.500 1.6530 0.07468 0.07006 -0.0499 0.1679 1.0000
18.750 1.6549 0.07718 0.07261 -0.0499 0.1648 1.0000
19.000 1.6548 0.07992 0.07538 -0.0498 0.1623 1.0000
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