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GOE 222 (MVA H.33) AIRFOIL (goe222-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: GOE 222 (MVA H.33) AIRFOIL (goe222-il)
Reynolds number: 200,000
Max Cl/Cd: 67.16 at α=2.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe222-il-200000-n5.txt
Download as CSV file: xf-goe222-il-200000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 222 (MVA H.33) AIRFOIL                      
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.200 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -13.250  -0.2784   0.06777   0.06307  -0.1446   0.9416   0.0343
 -13.000  -0.3088   0.06053   0.05562  -0.1500   0.9321   0.0344
 -12.750  -0.3256   0.05449   0.04933  -0.1557   0.9252   0.0346
 -12.500  -0.3410   0.05003   0.04468  -0.1590   0.9141   0.0348
 -12.250  -0.3507   0.04579   0.04020  -0.1629   0.9048   0.0350
 -12.000  -0.3590   0.04217   0.03634  -0.1661   0.8937   0.0353
 -11.750  -0.3580   0.04005   0.03415  -0.1666   0.8830   0.0357
 -11.500  -0.3440   0.03813   0.03215  -0.1685   0.8764   0.0362
 -11.250  -0.3333   0.03624   0.03018  -0.1704   0.8660   0.0366
 -11.000  -0.3137   0.03415   0.02793  -0.1738   0.8595   0.0372
 -10.750  -0.2976   0.03245   0.02609  -0.1757   0.8498   0.0377
 -10.500  -0.2751   0.03086   0.02432  -0.1778   0.8442   0.0383
 -10.250  -0.2557   0.02959   0.02290  -0.1788   0.8363   0.0390
 -10.000  -0.2317   0.02833   0.02145  -0.1803   0.8305   0.0398
  -9.750  -0.2072   0.02722   0.02014  -0.1816   0.8250   0.0406
  -9.500  -0.1838   0.02624   0.01905  -0.1822   0.8190   0.0412
  -9.250  -0.1588   0.02530   0.01810  -0.1827   0.8144   0.0418
  -9.000  -0.1327   0.02445   0.01721  -0.1834   0.8103   0.0425
  -8.750  -0.1086   0.02372   0.01644  -0.1838   0.8049   0.0432
  -8.500  -0.0822   0.02298   0.01563  -0.1846   0.8002   0.0440
  -8.250  -0.0539   0.02227   0.01482  -0.1856   0.7965   0.0451
  -8.000  -0.0263   0.02165   0.01410  -0.1865   0.7929   0.0462
  -7.750   0.0004   0.02111   0.01348  -0.1872   0.7889   0.0471
  -7.500   0.0277   0.02042   0.01277  -0.1881   0.7854   0.0480
  -7.250   0.0568   0.01973   0.01204  -0.1894   0.7820   0.0490
  -7.000   0.0879   0.01911   0.01133  -0.1909   0.7786   0.0503
  -6.750   0.1157   0.01862   0.01077  -0.1917   0.7736   0.0517
  -6.500   0.1444   0.01817   0.01023  -0.1925   0.7685   0.0535
  -6.250   0.1752   0.01767   0.00962  -0.1938   0.7642   0.0555
  -6.000   0.2074   0.01715   0.00897  -0.1953   0.7605   0.0583
  -5.750   0.2351   0.01680   0.00856  -0.1958   0.7554   0.0612
  -5.500   0.2645   0.01640   0.00811  -0.1966   0.7505   0.0661
  -5.250   0.2960   0.01584   0.00759  -0.1980   0.7459   0.0852
  -5.000   0.3277   0.01517   0.00707  -0.1996   0.7415   0.1435
  -4.750   0.3562   0.01472   0.00689  -0.2005   0.7365   0.2121
  -4.500   0.3852   0.01467   0.00688  -0.2009   0.7326   0.2452
  -4.250   0.4150   0.01469   0.00685  -0.2014   0.7294   0.2642
  -4.000   0.4457   0.01473   0.00680  -0.2020   0.7264   0.2789
  -3.750   0.4750   0.01480   0.00680  -0.2023   0.7231   0.2906
  -3.500   0.5022   0.01488   0.00688  -0.2022   0.7190   0.2997
  -3.250   0.5304   0.01496   0.00686  -0.2023   0.7149   0.3105
  -3.000   0.5591   0.01509   0.00699  -0.2025   0.7110   0.3205
  -2.750   0.5896   0.01522   0.00703  -0.2030   0.7076   0.3317
  -2.500   0.6173   0.01537   0.00718  -0.2030   0.7039   0.3404
  -2.250   0.6441   0.01543   0.00718  -0.2029   0.6996   0.3466
  -2.000   0.6714   0.01546   0.00722  -0.2028   0.6953   0.3505
  -1.750   0.7003   0.01548   0.00720  -0.2031   0.6913   0.3545
  -1.500   0.7303   0.01550   0.00712  -0.2035   0.6874   0.3587
  -1.250   0.7550   0.01554   0.00715  -0.2030   0.6820   0.3624
  -1.000   0.7815   0.01554   0.00713  -0.2029   0.6765   0.3654
  -0.750   0.8099   0.01553   0.00709  -0.2030   0.6717   0.3684
  -0.500   0.8358   0.01558   0.00715  -0.2027   0.6662   0.3721
  -0.250   0.8606   0.01562   0.00720  -0.2022   0.6599   0.3762
   0.000   0.8880   0.01564   0.00715  -0.2022   0.6542   0.3802
   0.250   0.9130   0.01568   0.00720  -0.2017   0.6478   0.3835
   0.500   0.9373   0.01571   0.00727  -0.2011   0.6404   0.3866
   0.750   0.9630   0.01574   0.00728  -0.2008   0.6336   0.3903
   1.000   0.9853   0.01583   0.00739  -0.1998   0.6246   0.3945
   1.250   1.0094   0.01589   0.00741  -0.1991   0.6160   0.3991
   1.500   1.0311   0.01596   0.00750  -0.1981   0.6048   0.4029
   1.750   1.0523   0.01605   0.00758  -0.1968   0.5920   0.4067
   2.000   1.0729   0.01616   0.00765  -0.1955   0.5783   0.4108
   2.250   1.0919   0.01631   0.00772  -0.1939   0.5642   0.4152
   2.500   1.1091   0.01652   0.00783  -0.1919   0.5507   0.4195
   2.750   1.1263   0.01677   0.00803  -0.1901   0.5380   0.4237
   3.000   1.1452   0.01707   0.00829  -0.1886   0.5267   0.4288
   3.250   1.1648   0.01741   0.00856  -0.1873   0.5170   0.4344
   3.500   1.1849   0.01775   0.00887  -0.1861   0.5081   0.4395
   3.750   1.2053   0.01810   0.00920  -0.1850   0.5006   0.4446
   4.000   1.2256   0.01846   0.00956  -0.1839   0.4928   0.4506
   4.500   1.2658   0.01923   0.01033  -0.1817   0.4788   0.4638
   4.750   1.2863   0.01962   0.01073  -0.1807   0.4728   0.4720
   5.000   1.3076   0.02001   0.01111  -0.1799   0.4682   0.4800
   5.250   1.3285   0.02038   0.01155  -0.1790   0.4635   0.4890
   5.500   1.3488   0.02078   0.01200  -0.1780   0.4584   0.4984
   5.750   1.3685   0.02122   0.01246  -0.1770   0.4533   0.5096
   6.000   1.3885   0.02166   0.01293  -0.1760   0.4485   0.5220
   6.250   1.4069   0.02212   0.01349  -0.1748   0.4430   0.5358
   6.500   1.4250   0.02262   0.01404  -0.1736   0.4374   0.5510
   6.750   1.4438   0.02312   0.01455  -0.1725   0.4328   0.5669
   7.000   1.4627   0.02360   0.01513  -0.1714   0.4287   0.5840
   7.500   1.4992   0.02458   0.01633  -0.1692   0.4203   0.6267
   7.750   1.5172   0.02508   0.01693  -0.1680   0.4163   0.6593
   8.000   1.5315   0.02526   0.01750  -0.1659   0.4126   0.8165
   8.250   1.5425   0.02573   0.01810  -0.1636   0.4084   1.0000
   8.500   1.5585   0.02642   0.01883  -0.1623   0.4038   1.0000
   8.750   1.5740   0.02715   0.01956  -0.1609   0.3993   1.0000
   9.000   1.5895   0.02789   0.02031  -0.1596   0.3947   1.0000
   9.250   1.6026   0.02875   0.02127  -0.1580   0.3892   1.0000
   9.500   1.6151   0.02964   0.02220  -0.1564   0.3835   1.0000
   9.750   1.6279   0.03055   0.02310  -0.1549   0.3785   1.0000
  10.000   1.6396   0.03155   0.02423  -0.1533   0.3725   1.0000
  10.250   1.6500   0.03264   0.02537  -0.1516   0.3663   1.0000
  10.500   1.6599   0.03378   0.02654  -0.1499   0.3601   1.0000
  10.750   1.6685   0.03507   0.02794  -0.1482   0.3522   1.0000
  11.000   1.6751   0.03651   0.02939  -0.1464   0.3444   1.0000
  11.250   1.6813   0.03809   0.03105  -0.1447   0.3341   1.0000
  11.500   1.6857   0.03985   0.03284  -0.1428   0.3230   1.0000
  11.750   1.6871   0.04190   0.03489  -0.1409   0.3097   1.0000
  12.000   1.6859   0.04425   0.03722  -0.1389   0.2949   1.0000
  12.250   1.6829   0.04684   0.03976  -0.1369   0.2809   1.0000
  12.750   1.6775   0.05218   0.04503  -0.1332   0.2580   1.0000
  13.000   1.6756   0.05484   0.04767  -0.1316   0.2494   1.0000
  13.250   1.6753   0.05741   0.05025  -0.1301   0.2416   1.0000
  13.500   1.6742   0.06009   0.05292  -0.1286   0.2354   1.0000
  13.750   1.6779   0.06233   0.05524  -0.1275   0.2298   1.0000
  14.000   1.6786   0.06488   0.05782  -0.1264   0.2243   1.0000
  14.250   1.6781   0.06758   0.06052  -0.1252   0.2194   1.0000
  14.500   1.6821   0.06991   0.06294  -0.1243   0.2144   1.0000
  14.750   1.6833   0.07254   0.06563  -0.1234   0.2094   1.0000
  15.000   1.6830   0.07535   0.06847  -0.1225   0.2050   1.0000
  15.250   1.6858   0.07785   0.07106  -0.1218   0.2010   1.0000
  15.500   1.6879   0.08050   0.07382  -0.1212   0.1963   1.0000
  15.750   1.6870   0.08353   0.07690  -0.1206   0.1912   1.0000
  16.000   1.6852   0.08667   0.08008  -0.1200   0.1867   1.0000
  16.250   1.6872   0.08948   0.08302  -0.1197   0.1817   1.0000
  16.500   1.6861   0.09266   0.08629  -0.1195   0.1765   1.0000
  16.750   1.6828   0.09613   0.08983  -0.1192   0.1715   1.0000
  17.000   1.6816   0.09943   0.09324  -0.1192   0.1646   1.0000
  17.250   1.6756   0.10337   0.09723  -0.1193   0.1576   1.0000
  17.500   1.6717   0.10707   0.10101  -0.1195   0.1489   1.0000
  17.750   1.6639   0.11134   0.10532  -0.1199   0.1393   1.0000
  18.000   1.6537   0.11599   0.10999  -0.1205   0.1290   1.0000
  18.250   1.6412   0.12101   0.11499  -0.1213   0.1177   1.0000
  18.500   1.6277   0.12620   0.12016  -0.1223   0.1054   1.0000
  18.750   1.6096   0.13216   0.12607  -0.1238   0.0852   1.0000
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