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GOE 228 (MVA H.38) AIRFOIL (goe228-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: GOE 228 (MVA H.38) AIRFOIL (goe228-il)
Reynolds number: 500,000
Max Cl/Cd: 88.22 at α=3.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe228-il-500000-n5.txt
Download as CSV file: xf-goe228-il-500000-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 =     0.500 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -15.750  -0.4264   0.09326   0.09031  -0.0990   0.9649   0.0219
 -15.500  -0.4625   0.08280   0.07968  -0.1057   0.9575   0.0221
 -15.250  -0.4824   0.07571   0.07246  -0.1102   0.9492   0.0223
 -15.000  -0.4976   0.06968   0.06631  -0.1140   0.9407   0.0224
 -14.750  -0.5083   0.06452   0.06105  -0.1175   0.9310   0.0226
 -14.500  -0.5174   0.05982   0.05622  -0.1206   0.9216   0.0228
 -14.250  -0.5247   0.05546   0.05176  -0.1237   0.9113   0.0230
 -14.000  -0.5307   0.05142   0.04759  -0.1267   0.9015   0.0232
 -13.750  -0.5349   0.04764   0.04368  -0.1296   0.8916   0.0235
 -13.500  -0.5366   0.04405   0.03997  -0.1326   0.8819   0.0237
 -13.250  -0.5364   0.04067   0.03644  -0.1356   0.8732   0.0240
 -13.000  -0.5332   0.03748   0.03312  -0.1388   0.8643   0.0243
 -12.750  -0.5289   0.03451   0.02998  -0.1418   0.8564   0.0247
 -12.500  -0.5189   0.03170   0.02703  -0.1458   0.8485   0.0250
 -12.250  -0.5017   0.02914   0.02426  -0.1503   0.8410   0.0253
 -12.000  -0.4809   0.02678   0.02179  -0.1550   0.8336   0.0257
 -11.750  -0.4558   0.02478   0.01968  -0.1595   0.8267   0.0261
 -11.500  -0.4278   0.02320   0.01798  -0.1634   0.8215   0.0266
 -11.250  -0.4001   0.02207   0.01676  -0.1660   0.8165   0.0271
 -11.000  -0.3727   0.02114   0.01574  -0.1679   0.8115   0.0277
 -10.750  -0.3453   0.02031   0.01478  -0.1695   0.8068   0.0282
 -10.500  -0.3174   0.01954   0.01390  -0.1708   0.8025   0.0287
 -10.250  -0.2893   0.01886   0.01312  -0.1720   0.7977   0.0292
 -10.000  -0.2610   0.01824   0.01238  -0.1730   0.7928   0.0297
  -9.750  -0.2330   0.01746   0.01155  -0.1742   0.7881   0.0303
  -9.500  -0.2042   0.01686   0.01091  -0.1753   0.7836   0.0309
  -9.250  -0.1753   0.01633   0.01032  -0.1762   0.7784   0.0314
  -9.000  -0.1462   0.01586   0.00977  -0.1770   0.7731   0.0321
  -8.750  -0.1171   0.01543   0.00926  -0.1777   0.7683   0.0328
  -8.500  -0.0876   0.01501   0.00878  -0.1785   0.7629   0.0335
  -8.250  -0.0582   0.01461   0.00830  -0.1792   0.7571   0.0340
  -8.000  -0.0287   0.01417   0.00778  -0.1799   0.7514   0.0347
  -7.750   0.0011   0.01373   0.00731  -0.1808   0.7452   0.0354
  -7.500   0.0307   0.01339   0.00691  -0.1814   0.7383   0.0363
  -7.250   0.0603   0.01310   0.00655  -0.1820   0.7315   0.0373
  -7.000   0.0900   0.01282   0.00621  -0.1825   0.7232   0.0384
  -6.750   0.1194   0.01258   0.00588  -0.1830   0.7149   0.0393
  -6.500   0.1492   0.01228   0.00554  -0.1836   0.7052   0.0407
  -6.250   0.1785   0.01206   0.00525  -0.1841   0.6948   0.0423
  -6.000   0.2076   0.01189   0.00499  -0.1844   0.6828   0.0442
  -5.750   0.2368   0.01171   0.00476  -0.1848   0.6700   0.0468
  -5.500   0.2656   0.01158   0.00456  -0.1851   0.6568   0.0508
  -5.250   0.2941   0.01148   0.00440  -0.1853   0.6428   0.0565
  -5.000   0.3225   0.01141   0.00426  -0.1855   0.6287   0.0630
  -4.750   0.3507   0.01138   0.00413  -0.1857   0.6147   0.0689
  -4.500   0.3792   0.01133   0.00401  -0.1859   0.6013   0.0747
  -4.250   0.4075   0.01131   0.00391  -0.1860   0.5892   0.0797
  -4.000   0.4357   0.01128   0.00381  -0.1862   0.5775   0.0856
  -3.750   0.4641   0.01124   0.00371  -0.1864   0.5659   0.0934
  -3.500   0.4926   0.01116   0.00363  -0.1867   0.5554   0.1093
  -3.250   0.5211   0.01105   0.00356  -0.1871   0.5452   0.1433
  -3.000   0.5500   0.01092   0.00349  -0.1876   0.5368   0.1783
  -2.750   0.5785   0.01083   0.00350  -0.1879   0.5281   0.2260
  -2.500   0.6068   0.01085   0.00354  -0.1881   0.5203   0.2558
  -2.250   0.6346   0.01092   0.00359  -0.1882   0.5119   0.2750
  -2.000   0.6623   0.01101   0.00365  -0.1882   0.5045   0.2879
  -1.750   0.6902   0.01110   0.00369  -0.1882   0.4969   0.2953
  -1.250   0.7455   0.01129   0.00380  -0.1882   0.4843   0.3109
  -1.000   0.7730   0.01138   0.00387  -0.1882   0.4780   0.3174
  -0.750   0.7999   0.01151   0.00395  -0.1881   0.4722   0.3247
  -0.500   0.8276   0.01160   0.00401  -0.1881   0.4666   0.3310
  -0.250   0.8546   0.01171   0.00410  -0.1881   0.4603   0.3375
   0.000   0.8809   0.01185   0.00421  -0.1879   0.4538   0.3453
   0.250   0.9079   0.01196   0.00430  -0.1878   0.4468   0.3536
   0.500   0.9337   0.01212   0.00442  -0.1875   0.4397   0.3612
   0.750   0.9602   0.01226   0.00453  -0.1873   0.4343   0.3683
   1.000   0.9868   0.01236   0.00465  -0.1872   0.4292   0.3754
   1.250   1.0125   0.01252   0.00478  -0.1869   0.4242   0.3820
   1.750   1.0644   0.01279   0.00505  -0.1865   0.4156   0.3962
   2.000   1.0897   0.01295   0.00520  -0.1861   0.4104   0.4052
   2.250   1.1136   0.01315   0.00539  -0.1856   0.4047   0.4148
   2.750   1.1633   0.01346   0.00574  -0.1848   0.3942   0.4385
   3.000   1.1861   0.01366   0.00596  -0.1840   0.3894   0.4540
   3.250   1.2081   0.01385   0.00618  -0.1831   0.3855   0.4736
   3.500   1.2310   0.01400   0.00641  -0.1823   0.3817   0.4978
   3.750   1.2536   0.01421   0.00667  -0.1815   0.3776   0.5225
   4.000   1.2759   0.01447   0.00695  -0.1807   0.3738   0.5433
   4.250   1.2975   0.01477   0.00726  -0.1798   0.3702   0.5592
   4.500   1.3211   0.01499   0.00752  -0.1793   0.3673   0.5727
   4.750   1.3441   0.01524   0.00781  -0.1787   0.3640   0.5841
   5.000   1.3663   0.01552   0.00811  -0.1779   0.3606   0.5941
   5.250   1.3876   0.01585   0.00846  -0.1771   0.3573   0.6043
   5.500   1.4082   0.01621   0.00883  -0.1761   0.3541   0.6139
   5.750   1.4300   0.01652   0.00917  -0.1753   0.3515   0.6237
   6.000   1.4521   0.01682   0.00952  -0.1747   0.3488   0.6324
   6.250   1.4734   0.01715   0.00990  -0.1739   0.3458   0.6411
   6.500   1.4941   0.01752   0.01031  -0.1730   0.3428   0.6494
   6.750   1.5137   0.01794   0.01076  -0.1720   0.3399   0.6593
   7.000   1.5328   0.01840   0.01125  -0.1710   0.3371   0.6697
   7.250   1.5534   0.01879   0.01170  -0.1702   0.3349   0.6810
   7.500   1.5740   0.01917   0.01216  -0.1694   0.3324   0.6935
   7.750   1.5939   0.01958   0.01265  -0.1686   0.3295   0.7092
   8.000   1.6126   0.02006   0.01322  -0.1676   0.3255   0.7359
   8.250   1.6241   0.02029   0.01378  -0.1652   0.3221   1.0000
   8.500   1.6415   0.02090   0.01441  -0.1641   0.3191   1.0000
   8.750   1.6608   0.02142   0.01497  -0.1633   0.3164   1.0000
   9.000   1.6793   0.02199   0.01558  -0.1624   0.3135   1.0000
   9.250   1.6967   0.02263   0.01626  -0.1614   0.3104   1.0000
   9.500   1.7126   0.02338   0.01702  -0.1603   0.3070   1.0000
   9.750   1.7266   0.02424   0.01789  -0.1589   0.3031   1.0000
  10.000   1.7436   0.02494   0.01863  -0.1580   0.2982   1.0000
  10.250   1.7568   0.02589   0.01960  -0.1567   0.2917   1.0000
  10.500   1.7688   0.02695   0.02066  -0.1552   0.2859   1.0000
  10.750   1.7829   0.02787   0.02162  -0.1541   0.2795   1.0000
  11.000   1.7916   0.02919   0.02293  -0.1525   0.2721   1.0000
  11.250   1.8007   0.03052   0.02427  -0.1509   0.2611   1.0000
  11.500   1.8042   0.03232   0.02602  -0.1490   0.2460   1.0000
  11.750   1.7903   0.03562   0.02915  -0.1457   0.2114   1.0000
  12.000   1.7645   0.04015   0.03348  -0.1418   0.1782   1.0000
  12.250   1.7603   0.04295   0.03629  -0.1399   0.1701   1.0000
  12.500   1.7571   0.04575   0.03912  -0.1381   0.1639   1.0000
  12.750   1.7581   0.04824   0.04166  -0.1368   0.1603   1.0000
  13.000   1.7577   0.05094   0.04442  -0.1356   0.1569   1.0000
  13.250   1.7557   0.05387   0.04741  -0.1343   0.1538   1.0000
  13.500   1.7531   0.05694   0.05054  -0.1332   0.1510   1.0000
  13.750   1.7524   0.05985   0.05353  -0.1323   0.1486   1.0000
  14.000   1.7548   0.06247   0.05624  -0.1316   0.1464   1.0000
  14.250   1.7545   0.06543   0.05929  -0.1308   0.1439   1.0000
  14.500   1.7524   0.06865   0.06260  -0.1302   0.1416   1.0000
  14.750   1.7466   0.07233   0.06635  -0.1295   0.1389   1.0000
  15.000   1.7382   0.07639   0.07048  -0.1288   0.1361   1.0000
  15.250   1.7328   0.08013   0.07430  -0.1284   0.1335   1.0000
  15.500   1.7330   0.08318   0.07745  -0.1280   0.1309   1.0000
  15.750   1.7286   0.08686   0.08120  -0.1277   0.1267   1.0000
  16.000   1.7176   0.09139   0.08579  -0.1275   0.1220   1.0000
  16.250   1.7107   0.09544   0.08991  -0.1274   0.1167   1.0000
  16.500   1.6974   0.10041   0.09489  -0.1274   0.1070   1.0000
  16.750   1.6681   0.10767   0.10208  -0.1278   0.0872   1.0000
  17.000   1.6372   0.11523   0.10956  -0.1285   0.0706   1.0000
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