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GOE 228 (MVA H.38) AIRFOIL (goe228-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: GOE 228 (MVA H.38) AIRFOIL (goe228-il)
Reynolds number: 1,000,000
Max Cl/Cd: 109.03 at α=5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe228-il-1000000-n5.txt
Download as CSV file: xf-goe228-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 228 (MVA H.38) 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
  ------ -------- --------- --------- -------- -------- --------
 -17.250  -0.5829   0.09281   0.09026  -0.0960   0.9630   0.0175
 -17.000  -0.6047   0.08585   0.08317  -0.1001   0.9557   0.0177
 -16.750  -0.6237   0.07945   0.07666  -0.1039   0.9478   0.0179
 -16.500  -0.6405   0.07360   0.07068  -0.1074   0.9393   0.0180
 -16.250  -0.6545   0.06811   0.06508  -0.1109   0.9300   0.0181
 -16.000  -0.6663   0.06311   0.05995  -0.1141   0.9209   0.0182
 -15.750  -0.6769   0.05831   0.05504  -0.1173   0.9099   0.0183
 -15.500  -0.6894   0.05337   0.04997  -0.1209   0.8979   0.0185
 -15.250  -0.7002   0.04882   0.04530  -0.1244   0.8855   0.0187
 -15.000  -0.7078   0.04466   0.04101  -0.1277   0.8737   0.0188
 -14.750  -0.7123   0.04074   0.03698  -0.1311   0.8629   0.0190
 -14.500  -0.7136   0.03707   0.03320  -0.1346   0.8535   0.0192
 -14.250  -0.7131   0.03364   0.02966  -0.1380   0.8447   0.0194
 -14.000  -0.7025   0.03045   0.02636  -0.1426   0.8378   0.0196
 -13.750  -0.6850   0.02765   0.02347  -0.1474   0.8315   0.0199
 -13.500  -0.6628   0.02524   0.02094  -0.1522   0.8254   0.0203
 -13.250  -0.6367   0.02320   0.01879  -0.1569   0.8198   0.0207
 -13.000  -0.6078   0.02146   0.01693  -0.1613   0.8132   0.0211
 -12.750  -0.5782   0.02012   0.01545  -0.1648   0.8065   0.0214
 -12.500  -0.5498   0.01924   0.01447  -0.1668   0.8016   0.0217
 -12.250  -0.5216   0.01819   0.01335  -0.1690   0.7972   0.0221
 -12.000  -0.4932   0.01745   0.01255  -0.1704   0.7927   0.0225
 -11.750  -0.4647   0.01688   0.01191  -0.1716   0.7884   0.0229
 -11.500  -0.4358   0.01639   0.01137  -0.1726   0.7847   0.0233
 -11.250  -0.4067   0.01590   0.01084  -0.1735   0.7806   0.0238
 -11.000  -0.3776   0.01543   0.01030  -0.1744   0.7762   0.0242
 -10.750  -0.3486   0.01501   0.00981  -0.1752   0.7715   0.0246
 -10.500  -0.3193   0.01464   0.00937  -0.1760   0.7674   0.0250
 -10.250  -0.2897   0.01429   0.00896  -0.1767   0.7630   0.0253
 -10.000  -0.2603   0.01384   0.00845  -0.1775   0.7579   0.0257
  -9.750  -0.2309   0.01336   0.00791  -0.1784   0.7528   0.0262
  -9.500  -0.2012   0.01299   0.00750  -0.1791   0.7482   0.0267
  -9.250  -0.1713   0.01266   0.00714  -0.1798   0.7427   0.0272
  -9.000  -0.1417   0.01237   0.00679  -0.1804   0.7364   0.0277
  -8.750  -0.1119   0.01209   0.00645  -0.1810   0.7305   0.0281
  -8.500  -0.0820   0.01184   0.00614  -0.1816   0.7234   0.0286
  -8.250  -0.0525   0.01162   0.00585  -0.1821   0.7157   0.0291
  -8.000  -0.0226   0.01140   0.00557  -0.1826   0.7066   0.0295
  -7.750   0.0070   0.01116   0.00526  -0.1831   0.6970   0.0299
  -7.500   0.0367   0.01092   0.00494  -0.1836   0.6856   0.0306
  -7.250   0.0662   0.01073   0.00469  -0.1841   0.6730   0.0312
  -7.000   0.0954   0.01059   0.00447  -0.1845   0.6593   0.0319
  -6.750   0.1245   0.01049   0.00427  -0.1848   0.6450   0.0327
  -6.500   0.1535   0.01041   0.00410  -0.1851   0.6300   0.0335
  -6.250   0.1824   0.01035   0.00395  -0.1854   0.6145   0.0342
  -6.000   0.2116   0.01026   0.00378  -0.1857   0.6001   0.0353
  -5.750   0.2407   0.01018   0.00363  -0.1860   0.5866   0.0367
  -5.500   0.2697   0.01013   0.00351  -0.1863   0.5741   0.0383
  -5.000   0.3279   0.01003   0.00330  -0.1870   0.5508   0.0443
  -4.750   0.3570   0.00998   0.00322  -0.1873   0.5402   0.0511
  -4.500   0.3861   0.00993   0.00316  -0.1876   0.5302   0.0597
  -4.250   0.4153   0.00990   0.00310  -0.1879   0.5223   0.0663
  -4.000   0.4445   0.00987   0.00304  -0.1883   0.5143   0.0709
  -3.750   0.4734   0.00988   0.00300  -0.1885   0.5064   0.0752
  -3.500   0.5025   0.00988   0.00296  -0.1888   0.4986   0.0786
  -3.000   0.5604   0.00987   0.00289  -0.1893   0.4841   0.0889
  -2.750   0.5896   0.00980   0.00285  -0.1897   0.4775   0.1075
  -2.500   0.6189   0.00965   0.00281  -0.1902   0.4715   0.1520
  -2.250   0.6485   0.00953   0.00277  -0.1908   0.4661   0.1912
  -2.000   0.6776   0.00945   0.00280  -0.1912   0.4599   0.2363
  -1.750   0.7060   0.00950   0.00284  -0.1914   0.4541   0.2524
  -1.500   0.7348   0.00953   0.00289  -0.1916   0.4482   0.2673
  -1.250   0.7625   0.00964   0.00295  -0.1916   0.4402   0.2774
  -1.000   0.7907   0.00972   0.00301  -0.1918   0.4331   0.2855
  -0.750   0.8185   0.00982   0.00307  -0.1918   0.4261   0.2924
  -0.500   0.8462   0.00992   0.00315  -0.1918   0.4206   0.3014
  -0.250   0.8744   0.00999   0.00322  -0.1920   0.4166   0.3082
   0.000   0.9023   0.01009   0.00328  -0.1920   0.4118   0.3128
   0.250   0.9297   0.01019   0.00337  -0.1920   0.4068   0.3183
   0.500   0.9571   0.01030   0.00347  -0.1920   0.4022   0.3247
   1.000   1.0114   0.01052   0.00367  -0.1919   0.3910   0.3403
   1.250   1.0379   0.01067   0.00378  -0.1918   0.3850   0.3471
   1.500   1.0648   0.01078   0.00389  -0.1917   0.3795   0.3541
   1.750   1.0911   0.01092   0.00402  -0.1915   0.3744   0.3610
   2.000   1.1169   0.01109   0.00416  -0.1913   0.3698   0.3666
   2.250   1.1436   0.01119   0.00427  -0.1912   0.3665   0.3724
   2.500   1.1699   0.01131   0.00440  -0.1910   0.3628   0.3805
   3.000   1.2205   0.01163   0.00472  -0.1904   0.3546   0.3973
   3.250   1.2458   0.01177   0.00487  -0.1900   0.3516   0.4063
   3.500   1.2713   0.01190   0.00503  -0.1897   0.3485   0.4175
   3.750   1.2959   0.01204   0.00520  -0.1893   0.3450   0.4302
   4.000   1.3184   0.01221   0.00539  -0.1885   0.3414   0.4466
   4.250   1.3394   0.01239   0.00561  -0.1874   0.3379   0.4681
   4.500   1.3626   0.01255   0.00584  -0.1867   0.3351   0.4980
   4.750   1.3865   0.01272   0.00608  -0.1862   0.3325   0.5251
   5.000   1.4098   0.01293   0.00633  -0.1856   0.3295   0.5435
   5.250   1.4325   0.01317   0.00658  -0.1849   0.3262   0.5564
   5.500   1.4545   0.01345   0.00688  -0.1841   0.3228   0.5675
   5.750   1.4761   0.01375   0.00718  -0.1832   0.3195   0.5760
   6.000   1.4989   0.01398   0.00746  -0.1826   0.3169   0.5848
   6.250   1.5209   0.01426   0.00775  -0.1818   0.3137   0.5928
   6.500   1.5421   0.01458   0.00810  -0.1810   0.3099   0.6013
   6.750   1.5622   0.01496   0.00847  -0.1800   0.3061   0.6085
   7.000   1.5826   0.01532   0.00886  -0.1790   0.3030   0.6150
   7.250   1.6042   0.01563   0.00921  -0.1783   0.3004   0.6218
   7.500   1.6247   0.01600   0.00960  -0.1774   0.2968   0.6283
   7.750   1.6436   0.01645   0.01007  -0.1764   0.2921   0.6364
   8.000   1.6621   0.01693   0.01056  -0.1753   0.2883   0.6442
   8.250   1.6822   0.01734   0.01102  -0.1744   0.2854   0.6530
   8.500   1.7007   0.01783   0.01154  -0.1734   0.2799   0.6634
   8.750   1.7158   0.01852   0.01223  -0.1719   0.2720   0.6767
   9.000   1.7306   0.01925   0.01296  -0.1704   0.2613   0.6922
   9.250   1.7394   0.02036   0.01402  -0.1682   0.2442   0.7127
   9.500   1.7269   0.02286   0.01631  -0.1636   0.1955   0.7469
   9.750   1.7179   0.02472   0.01837  -0.1592   0.1705   1.0000
  10.000   1.7248   0.02614   0.01978  -0.1572   0.1623   1.0000
  10.250   1.7362   0.02728   0.02093  -0.1557   0.1587   1.0000
  10.500   1.7462   0.02854   0.02220  -0.1542   0.1552   1.0000
  10.750   1.7549   0.02991   0.02358  -0.1526   0.1510   1.0000
  11.000   1.7666   0.03108   0.02479  -0.1514   0.1485   1.0000
  11.250   1.7789   0.03224   0.02600  -0.1502   0.1471   1.0000
  11.500   1.7902   0.03350   0.02729  -0.1491   0.1451   1.0000
  11.750   1.8001   0.03490   0.02873  -0.1478   0.1431   1.0000
  12.000   1.8084   0.03644   0.03031  -0.1465   0.1405   1.0000
  12.250   1.8144   0.03823   0.03213  -0.1451   0.1378   1.0000
  12.500   1.8212   0.03998   0.03392  -0.1438   0.1351   1.0000
  12.750   1.8298   0.04161   0.03561  -0.1427   0.1334   1.0000
  13.000   1.8388   0.04324   0.03728  -0.1417   0.1311   1.0000
  13.250   1.8444   0.04519   0.03928  -0.1406   0.1275   1.0000
  13.500   1.8458   0.04762   0.04172  -0.1393   0.1234   1.0000
  13.750   1.8474   0.05008   0.04422  -0.1381   0.1192   1.0000
  14.000   1.8462   0.05288   0.04704  -0.1369   0.1116   1.0000
  14.250   1.8250   0.05793   0.05201  -0.1350   0.0931   1.0000
  14.500   1.7918   0.06461   0.05864  -0.1331   0.0744   1.0000
  14.750   1.7592   0.07152   0.06556  -0.1316   0.0598   1.0000
  15.000   1.7284   0.07838   0.07245  -0.1306   0.0465   1.0000
  15.250   1.6991   0.08530   0.07939  -0.1300   0.0351   1.0000
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