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GOE 227 (MVA H.37) AIRFOIL (goe227-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: GOE 227 (MVA H.37) AIRFOIL (goe227-il)
Reynolds number: 1,000,000
Max Cl/Cd: 155.27 at α=4°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe227-il-1000000.txt
Download as CSV file: xf-goe227-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 227 (MVA H.37) 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
  ------ -------- --------- --------- -------- -------- --------
 -12.750  -0.5172   0.04827   0.04548  -0.1293   0.8509   0.0287
 -12.500  -0.5354   0.03916   0.03615  -0.1422   0.8417   0.0288
 -12.250  -0.5211   0.03293   0.02974  -0.1546   0.8354   0.0292
 -12.000  -0.4937   0.02807   0.02470  -0.1658   0.8291   0.0296
 -11.750  -0.4589   0.02432   0.02074  -0.1758   0.8233   0.0302
 -11.500  -0.4197   0.02141   0.01764  -0.1846   0.8183   0.0307
 -11.250  -0.3859   0.01991   0.01598  -0.1889   0.8126   0.0311
 -11.000  -0.3542   0.01894   0.01484  -0.1916   0.8066   0.0314
 -10.750  -0.3209   0.01704   0.01276  -0.1959   0.8011   0.0322
 -10.500  -0.2897   0.01621   0.01185  -0.1979   0.7944   0.0329
 -10.250  -0.2591   0.01566   0.01122  -0.1993   0.7876   0.0335
 -10.000  -0.2282   0.01510   0.01059  -0.2006   0.7796   0.0341
  -9.750  -0.1977   0.01459   0.00996  -0.2018   0.7707   0.0347
  -9.500  -0.1670   0.01410   0.00937  -0.2029   0.7597   0.0353
  -9.250  -0.1366   0.01368   0.00881  -0.2039   0.7465   0.0358
  -9.000  -0.1066   0.01335   0.00835  -0.2046   0.7296   0.0363
  -8.750  -0.0758   0.01271   0.00754  -0.2060   0.7096   0.0373
  -8.500  -0.0457   0.01236   0.00707  -0.2068   0.6920   0.0383
  -8.250  -0.0157   0.01212   0.00673  -0.2075   0.6798   0.0391
  -8.000   0.0145   0.01190   0.00641  -0.2082   0.6711   0.0400
  -7.750   0.0449   0.01167   0.00610  -0.2089   0.6649   0.0409
  -7.500   0.0750   0.01150   0.00583  -0.2095   0.6594   0.0417
  -7.250   0.1062   0.01114   0.00539  -0.2104   0.6552   0.0429
  -7.000   0.1371   0.01088   0.00511  -0.2112   0.6520   0.0445
  -6.750   0.1674   0.01075   0.00495  -0.2117   0.6490   0.0460
  -6.500   0.1976   0.01064   0.00478  -0.2123   0.6462   0.0475
  -6.250   0.2279   0.01051   0.00458  -0.2128   0.6435   0.0487
  -6.000   0.2587   0.01030   0.00434  -0.2135   0.6402   0.0512
  -5.750   0.2890   0.01020   0.00423  -0.2140   0.6380   0.0531
  -5.500   0.3192   0.01012   0.00412  -0.2145   0.6355   0.0549
  -5.250   0.3500   0.00994   0.00391  -0.2151   0.6330   0.0572
  -5.000   0.3801   0.00986   0.00383  -0.2156   0.6304   0.0597
  -4.750   0.4099   0.00984   0.00378  -0.2160   0.6282   0.0620
  -4.500   0.4396   0.00985   0.00374  -0.2163   0.6259   0.0636
  -4.250   0.4703   0.00970   0.00354  -0.2169   0.6235   0.0664
  -4.000   0.5006   0.00961   0.00346  -0.2175   0.6218   0.0688
  -3.750   0.5308   0.00954   0.00339  -0.2179   0.6204   0.0711
  -3.500   0.5607   0.00951   0.00334  -0.2183   0.6187   0.0730
  -3.250   0.5912   0.00940   0.00321  -0.2188   0.6170   0.0753
  -3.000   0.6217   0.00927   0.00308  -0.2194   0.6151   0.0787
  -2.750   0.6518   0.00922   0.00303  -0.2198   0.6133   0.0814
  -2.500   0.6816   0.00920   0.00298  -0.2202   0.6116   0.0838
  -2.250   0.7114   0.00919   0.00294  -0.2206   0.6096   0.0861
  -2.000   0.7415   0.00915   0.00288  -0.2211   0.6069   0.0910
  -1.750   0.7714   0.00914   0.00287  -0.2215   0.6049   0.0951
  -1.500   0.8013   0.00910   0.00282  -0.2219   0.6037   0.0986
  -1.250   0.8315   0.00901   0.00279  -0.2224   0.6024   0.1081
  -1.000   0.8615   0.00894   0.00277  -0.2229   0.6005   0.1231
  -0.750   0.8914   0.00887   0.00275  -0.2233   0.5981   0.1428
  -0.500   0.9215   0.00878   0.00272  -0.2238   0.5958   0.1684
  -0.250   0.9522   0.00858   0.00277  -0.2246   0.5935   0.2670
   0.000   0.9812   0.00862   0.00283  -0.2249   0.5912   0.2943
   0.250   1.0102   0.00872   0.00293  -0.2251   0.5886   0.3085
   0.500   1.0394   0.00873   0.00297  -0.2254   0.5868   0.3186
   0.750   1.0685   0.00873   0.00300  -0.2256   0.5847   0.3271
   1.000   1.0975   0.00873   0.00304  -0.2258   0.5822   0.3361
   1.250   1.1264   0.00876   0.00308  -0.2260   0.5796   0.3446
   1.500   1.1552   0.00878   0.00312  -0.2262   0.5768   0.3521
   1.750   1.1835   0.00885   0.00318  -0.2263   0.5736   0.3590
   2.250   1.2407   0.00891   0.00330  -0.2266   0.5670   0.3760
   2.500   1.2693   0.00892   0.00335  -0.2268   0.5631   0.3843
   2.750   1.2976   0.00895   0.00340  -0.2269   0.5587   0.3944
   3.000   1.3251   0.00903   0.00349  -0.2269   0.5537   0.4067
   3.250   1.3538   0.00902   0.00354  -0.2271   0.5477   0.4187
   3.500   1.3810   0.00908   0.00361  -0.2271   0.5387   0.4341
   3.750   1.4087   0.00912   0.00369  -0.2271   0.5270   0.4546
   4.000   1.4347   0.00924   0.00382  -0.2269   0.5085   0.4803
   4.250   1.4569   0.00962   0.00406  -0.2259   0.4748   0.5075
   4.500   1.4774   0.01013   0.00443  -0.2247   0.4454   0.5305
   4.750   1.4995   0.01054   0.00477  -0.2238   0.4284   0.5499
   5.000   1.5231   0.01084   0.00506  -0.2231   0.4172   0.5674
   5.250   1.5463   0.01115   0.00535  -0.2224   0.4078   0.5835
   5.500   1.5700   0.01141   0.00562  -0.2217   0.4000   0.5995
   5.750   1.5929   0.01170   0.00592  -0.2209   0.3921   0.6170
   6.000   1.6160   0.01195   0.00620  -0.2202   0.3834   0.6398
   6.250   1.6384   0.01221   0.00655  -0.2194   0.3752   0.6902
   6.500   1.6575   0.01209   0.00684  -0.2178   0.3684   1.0000
   6.750   1.6774   0.01248   0.00717  -0.2165   0.3604   1.0000
   7.000   1.6997   0.01272   0.00742  -0.2156   0.3543   1.0000
   7.250   1.7175   0.01310   0.00777  -0.2139   0.3469   1.0000
   7.500   1.7365   0.01342   0.00809  -0.2124   0.3404   1.0000
   7.750   1.7540   0.01383   0.00847  -0.2106   0.3323   1.0000
   8.000   1.7714   0.01425   0.00888  -0.2090   0.3247   1.0000
   8.250   1.7882   0.01471   0.00933  -0.2072   0.3163   1.0000
   8.500   1.8046   0.01521   0.00982  -0.2054   0.3088   1.0000
   8.750   1.8193   0.01581   0.01038  -0.2035   0.2990   1.0000
   9.000   1.8333   0.01647   0.01101  -0.2014   0.2872   1.0000
   9.250   1.8433   0.01737   0.01184  -0.1989   0.2714   1.0000
   9.500   1.8485   0.01859   0.01295  -0.1958   0.2514   1.0000
   9.750   1.8488   0.02018   0.01439  -0.1922   0.2250   1.0000
  10.000   1.8401   0.02248   0.01648  -0.1877   0.1923   1.0000
  10.250   1.8226   0.02558   0.01933  -0.1825   0.1511   1.0000
  10.500   1.8078   0.02870   0.02227  -0.1780   0.1196   1.0000
  10.750   1.7983   0.03154   0.02499  -0.1744   0.0977   1.0000
  11.000   1.7745   0.03573   0.02894  -0.1698   0.0556   1.0000
  11.250   1.7585   0.03950   0.03263  -0.1663   0.0332   1.0000
  11.500   1.7581   0.04199   0.03514  -0.1642   0.0273   1.0000
  11.750   1.7614   0.04421   0.03739  -0.1626   0.0245   1.0000
  12.000   1.7640   0.04653   0.03975  -0.1610   0.0226   1.0000
  12.250   1.7668   0.04891   0.04217  -0.1595   0.0211   1.0000
  12.500   1.7719   0.05108   0.04441  -0.1583   0.0202   1.0000
  12.750   1.7754   0.05347   0.04685  -0.1571   0.0193   1.0000
  13.000   1.7770   0.05611   0.04954  -0.1558   0.0185   1.0000
  13.250   1.7759   0.05909   0.05258  -0.1545   0.0177   1.0000
  13.500   1.7796   0.06155   0.05511  -0.1535   0.0173   1.0000
  13.750   1.7824   0.06413   0.05775  -0.1525   0.0168   1.0000
  14.000   1.7837   0.06691   0.06060  -0.1515   0.0163   1.0000
  14.250   1.7843   0.06979   0.06354  -0.1506   0.0158   1.0000
  14.500   1.7830   0.07288   0.06670  -0.1496   0.0154   1.0000
  14.750   1.7781   0.07651   0.07039  -0.1486   0.0149   1.0000
  15.000   1.7728   0.08020   0.07417  -0.1477   0.0145   1.0000
  15.250   1.7729   0.08327   0.07731  -0.1471   0.0143   1.0000
  15.500   1.7718   0.08647   0.08059  -0.1464   0.0140   1.0000
  15.750   1.7695   0.08986   0.08406  -0.1459   0.0138   1.0000
  16.000   1.7662   0.09345   0.08773  -0.1454   0.0135   1.0000
  16.250   1.7636   0.09696   0.09132  -0.1450   0.0132   1.0000
  16.500   1.7591   0.10082   0.09526  -0.1448   0.0130   1.0000
  16.750   1.7545   0.10472   0.09923  -0.1446   0.0128   1.0000
  17.000   1.7486   0.10880   0.10339  -0.1446   0.0126   1.0000
  17.250   1.7408   0.11323   0.10791  -0.1448   0.0124   1.0000
  17.500   1.7306   0.11812   0.11289  -0.1452   0.0121   1.0000
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