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GOE 222 (MVA H.33) AIRFOIL (goe222-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: GOE 222 (MVA H.33) AIRFOIL (goe222-il)
Reynolds number: 1,000,000
Max Cl/Cd: 115.19 at α=0.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe222-il-1000000.txt
Download as CSV file: xf-goe222-il-1000000.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 =     1.000 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -17.250  -0.4754   0.09161   0.08913  -0.1223   0.9832   0.0221
 -17.000  -0.5018   0.08298   0.08033  -0.1284   0.9807   0.0222
 -16.750  -0.5170   0.07706   0.07428  -0.1321   0.9766   0.0224
 -16.500  -0.5271   0.07199   0.06910  -0.1354   0.9727   0.0226
 -16.250  -0.5332   0.06752   0.06452  -0.1385   0.9690   0.0227
 -16.000  -0.5375   0.06359   0.06050  -0.1411   0.9648   0.0228
 -15.750  -0.5454   0.05945   0.05625  -0.1436   0.9600   0.0230
 -15.500  -0.5523   0.05598   0.05269  -0.1451   0.9553   0.0234
 -15.250  -0.5486   0.05349   0.05016  -0.1466   0.9511   0.0236
 -15.000  -0.5449   0.05095   0.04759  -0.1482   0.9463   0.0238
 -14.750  -0.5409   0.04854   0.04513  -0.1496   0.9414   0.0240
 -14.500  -0.5376   0.04605   0.04257  -0.1513   0.9364   0.0242
 -14.250  -0.5332   0.04367   0.04015  -0.1530   0.9308   0.0244
 -14.000  -0.5292   0.04129   0.03769  -0.1547   0.9249   0.0246
 -13.750  -0.5243   0.03893   0.03525  -0.1565   0.9190   0.0249
 -13.500  -0.5179   0.03666   0.03292  -0.1584   0.9118   0.0251
 -13.250  -0.5103   0.03453   0.03068  -0.1601   0.9048   0.0254
 -13.000  -0.5012   0.03243   0.02852  -0.1621   0.8960   0.0257
 -12.750  -0.4918   0.03041   0.02640  -0.1640   0.8867   0.0260
 -12.500  -0.4780   0.02844   0.02432  -0.1669   0.8755   0.0263
 -12.250  -0.4583   0.02650   0.02226  -0.1706   0.8637   0.0266
 -12.000  -0.4344   0.02468   0.02029  -0.1749   0.8503   0.0268
 -11.750  -0.4160   0.02281   0.01830  -0.1773   0.8343   0.0273
 -11.500  -0.3912   0.02130   0.01669  -0.1804   0.8179   0.0278
 -11.250  -0.3642   0.02010   0.01536  -0.1832   0.8029   0.0281
 -10.750  -0.3111   0.01860   0.01366  -0.1863   0.7809   0.0290
 -10.500  -0.2844   0.01801   0.01296  -0.1875   0.7729   0.0296
 -10.250  -0.2569   0.01741   0.01229  -0.1886   0.7672   0.0301
 -10.000  -0.2295   0.01686   0.01165  -0.1895   0.7616   0.0305
  -9.750  -0.2022   0.01641   0.01109  -0.1903   0.7558   0.0308
  -9.500  -0.1736   0.01597   0.01060  -0.1911   0.7514   0.0311
  -9.250  -0.1466   0.01511   0.00967  -0.1922   0.7469   0.0317
  -9.000  -0.1187   0.01449   0.00901  -0.1932   0.7429   0.0325
  -8.750  -0.0901   0.01411   0.00857  -0.1940   0.7388   0.0331
  -8.500  -0.0608   0.01370   0.00813  -0.1949   0.7361   0.0336
  -8.250  -0.0314   0.01332   0.00772  -0.1957   0.7333   0.0342
  -8.000  -0.0020   0.01297   0.00732  -0.1964   0.7303   0.0348
  -7.750   0.0275   0.01266   0.00696  -0.1971   0.7274   0.0354
  -7.500   0.0568   0.01241   0.00665  -0.1977   0.7243   0.0358
  -7.250   0.0866   0.01210   0.00626  -0.1985   0.7206   0.0365
  -7.000   0.1168   0.01159   0.00571  -0.1995   0.7186   0.0376
  -6.750   0.1467   0.01129   0.00540  -0.2003   0.7161   0.0384
  -6.500   0.1767   0.01104   0.00512  -0.2009   0.7133   0.0393
  -6.250   0.2065   0.01083   0.00487  -0.2015   0.7104   0.0403
  -6.000   0.2363   0.01067   0.00466  -0.2020   0.7075   0.0412
  -5.750   0.2664   0.01049   0.00442  -0.2027   0.7044   0.0422
  -5.500   0.2969   0.01024   0.00413  -0.2035   0.7020   0.0442
  -5.250   0.3270   0.01005   0.00393  -0.2041   0.7004   0.0461
  -5.000   0.3571   0.00991   0.00377  -0.2046   0.6984   0.0479
  -4.750   0.3875   0.00967   0.00353  -0.2053   0.6962   0.0520
  -4.500   0.4178   0.00946   0.00333  -0.2059   0.6938   0.0598
  -4.250   0.4491   0.00877   0.00294  -0.2074   0.6912   0.1451
  -4.000   0.4797   0.00831   0.00275  -0.2085   0.6884   0.2292
  -3.750   0.5098   0.00828   0.00275  -0.2090   0.6851   0.2550
  -3.500   0.5395   0.00823   0.00274  -0.2094   0.6831   0.2691
  -3.250   0.5692   0.00820   0.00272  -0.2098   0.6809   0.2781
  -3.000   0.5987   0.00818   0.00272  -0.2102   0.6782   0.2863
  -2.750   0.6282   0.00818   0.00270  -0.2105   0.6754   0.2929
  -2.500   0.6574   0.00819   0.00271  -0.2108   0.6723   0.2999
  -2.250   0.6865   0.00825   0.00273  -0.2110   0.6689   0.3062
  -2.000   0.7158   0.00827   0.00274  -0.2114   0.6657   0.3120
  -1.750   0.7449   0.00825   0.00276  -0.2116   0.6626   0.3182
  -1.500   0.7738   0.00827   0.00278  -0.2118   0.6587   0.3239
  -1.250   0.8021   0.00829   0.00278  -0.2119   0.6539   0.3292
  -1.000   0.8301   0.00832   0.00279  -0.2120   0.6485   0.3333
  -0.750   0.8588   0.00831   0.00281  -0.2122   0.6429   0.3373
  -0.500   0.8864   0.00835   0.00282  -0.2122   0.6361   0.3407
  -0.250   0.9138   0.00841   0.00283  -0.2121   0.6289   0.3433
   0.000   0.9408   0.00843   0.00284  -0.2120   0.6187   0.3477
   0.250   0.9672   0.00848   0.00288  -0.2118   0.6062   0.3517
   0.500   0.9918   0.00861   0.00294  -0.2112   0.5892   0.3550
   0.750   1.0137   0.00883   0.00304  -0.2100   0.5671   0.3582
   1.000   1.0347   0.00912   0.00320  -0.2088   0.5434   0.3610
   1.250   1.0554   0.00942   0.00338  -0.2075   0.5226   0.3637
   1.500   1.0770   0.00967   0.00357  -0.2064   0.5063   0.3679
   1.750   1.0982   0.00991   0.00376  -0.2052   0.4936   0.3715
   2.250   1.1386   0.01036   0.00411  -0.2024   0.4734   0.3780
   2.750   1.1827   0.01080   0.00450  -0.2004   0.4573   0.3855
   3.000   1.2052   0.01105   0.00473  -0.1996   0.4506   0.3900
   3.250   1.2280   0.01128   0.00496  -0.1988   0.4451   0.3942
   3.500   1.2524   0.01146   0.00514  -0.1983   0.4410   0.3979
   3.750   1.2758   0.01167   0.00536  -0.1977   0.4366   0.4020
   4.000   1.2976   0.01194   0.00562  -0.1968   0.4318   0.4071
   4.250   1.3203   0.01218   0.00588  -0.1960   0.4277   0.4120
   4.500   1.3445   0.01236   0.00608  -0.1956   0.4247   0.4168
   4.750   1.3677   0.01258   0.00633  -0.1949   0.4211   0.4228
   5.000   1.3893   0.01286   0.00662  -0.1941   0.4170   0.4292
   5.250   1.4094   0.01321   0.00697  -0.1929   0.4125   0.4352
   5.500   1.4329   0.01342   0.00722  -0.1924   0.4097   0.4425
   5.750   1.4564   0.01363   0.00749  -0.1919   0.4069   0.4509
   6.000   1.4786   0.01390   0.00780  -0.1912   0.4036   0.4600
   6.250   1.4997   0.01422   0.00815  -0.1903   0.4000   0.4717
   6.500   1.5192   0.01461   0.00857  -0.1891   0.3959   0.4859
   6.750   1.5406   0.01492   0.00894  -0.1884   0.3929   0.5031
   7.000   1.5637   0.01516   0.00927  -0.1878   0.3903   0.5227
   7.250   1.5854   0.01546   0.00964  -0.1871   0.3869   0.5427
   7.500   1.6054   0.01585   0.01007  -0.1862   0.3825   0.5617
   7.750   1.6216   0.01642   0.01065  -0.1846   0.3770   0.5798
   8.000   1.6445   0.01667   0.01099  -0.1842   0.3728   0.6001
   8.250   1.6641   0.01710   0.01147  -0.1832   0.3663   0.6219
   8.500   1.6809   0.01767   0.01209  -0.1819   0.3584   0.6512
   8.750   1.6962   0.01772   0.01269  -0.1801   0.3493   0.9892
   9.000   1.7117   0.01841   0.01334  -0.1786   0.3393   1.0000
   9.250   1.7237   0.01929   0.01417  -0.1767   0.3266   1.0000
   9.500   1.7344   0.02028   0.01509  -0.1746   0.3095   1.0000
   9.750   1.7363   0.02182   0.01648  -0.1714   0.2832   1.0000
  10.000   1.7356   0.02358   0.01810  -0.1680   0.2602   1.0000
  10.250   1.7396   0.02513   0.01957  -0.1654   0.2452   1.0000
  10.500   1.7457   0.02660   0.02099  -0.1631   0.2345   1.0000
  10.750   1.7558   0.02783   0.02222  -0.1614   0.2277   1.0000
  11.000   1.7640   0.02922   0.02359  -0.1596   0.2210   1.0000
  11.250   1.7744   0.03049   0.02488  -0.1580   0.2159   1.0000
  11.500   1.7855   0.03174   0.02614  -0.1566   0.2114   1.0000
  11.750   1.7936   0.03325   0.02765  -0.1550   0.2064   1.0000
  12.000   1.8030   0.03468   0.02909  -0.1535   0.2018   1.0000
  12.250   1.8152   0.03588   0.03033  -0.1524   0.1985   1.0000
  12.500   1.8243   0.03737   0.03184  -0.1510   0.1942   1.0000
  12.750   1.8310   0.03907   0.03355  -0.1495   0.1894   1.0000
  13.000   1.8411   0.04052   0.03503  -0.1483   0.1857   1.0000
  13.250   1.8514   0.04195   0.03649  -0.1472   0.1811   1.0000
  13.500   1.8561   0.04389   0.03843  -0.1457   0.1755   1.0000
  13.750   1.8638   0.04556   0.04012  -0.1444   0.1698   1.0000
  14.000   1.8671   0.04766   0.04222  -0.1429   0.1620   1.0000
  14.250   1.8692   0.04989   0.04442  -0.1413   0.1520   1.0000
  14.500   1.8633   0.05294   0.04741  -0.1394   0.1384   1.0000
  14.750   1.8518   0.05657   0.05096  -0.1372   0.1236   1.0000
  15.000   1.8370   0.06064   0.05496  -0.1349   0.1094   1.0000
  15.250   1.8221   0.06486   0.05914  -0.1329   0.0950   1.0000
  15.500   1.7938   0.07066   0.06483  -0.1306   0.0701   1.0000
  15.750   1.7679   0.07641   0.07053  -0.1287   0.0544   1.0000
  16.000   1.7528   0.08113   0.07527  -0.1275   0.0468   1.0000
  16.250   1.7424   0.08537   0.07956  -0.1267   0.0409   1.0000
  16.500   1.7320   0.08964   0.08386  -0.1260   0.0347   1.0000
  16.750   1.7187   0.09438   0.08860  -0.1254   0.0262   1.0000
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