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GOE 243 (MVA PR.3) AIRFOIL (goe243-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: GOE 243 (MVA PR.3) AIRFOIL (goe243-il)
Reynolds number: 500,000
Max Cl/Cd: 90.27 at α=2.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe243-il-500000-n5.txt
Download as CSV file: xf-goe243-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 243 (MVA PR.3) 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
  ------ -------- --------- --------- -------- -------- --------
 -11.000  -0.1745   0.05057   0.04634  -0.1363   0.7836   0.0264
 -10.750  -0.1915   0.04401   0.03954  -0.1438   0.7771   0.0264
 -10.500  -0.1957   0.03988   0.03527  -0.1485   0.7704   0.0265
 -10.250  -0.1900   0.03671   0.03196  -0.1531   0.7643   0.0266
 -10.000  -0.1747   0.03387   0.02896  -0.1583   0.7589   0.0267
  -9.750  -0.1532   0.03144   0.02643  -0.1634   0.7538   0.0268
  -9.500  -0.1276   0.02939   0.02427  -0.1681   0.7481   0.0270
  -9.000  -0.0688   0.02606   0.02069  -0.1769   0.7378   0.0273
  -8.750  -0.0366   0.02464   0.01918  -0.1810   0.7325   0.0275
  -8.500  -0.0038   0.02339   0.01782  -0.1846   0.7253   0.0277
  -8.250   0.0292   0.02230   0.01659  -0.1879   0.7178   0.0279
  -8.000   0.0629   0.02130   0.01550  -0.1909   0.7110   0.0281
  -7.750   0.0967   0.02041   0.01452  -0.1937   0.7048   0.0283
  -7.500   0.1303   0.01964   0.01364  -0.1961   0.6992   0.0286
  -7.250   0.1641   0.01893   0.01284  -0.1984   0.6940   0.0288
  -7.000   0.1979   0.01828   0.01213  -0.2005   0.6885   0.0291
  -6.750   0.2316   0.01770   0.01148  -0.2025   0.6828   0.0293
  -6.500   0.2651   0.01720   0.01087  -0.2043   0.6771   0.0296
  -6.250   0.2992   0.01670   0.01032  -0.2062   0.6717   0.0299
  -6.000   0.3333   0.01624   0.00980  -0.2081   0.6660   0.0301
  -5.750   0.3674   0.01579   0.00929  -0.2100   0.6601   0.0304
  -5.500   0.4023   0.01532   0.00878  -0.2120   0.6544   0.0308
  -5.250   0.4377   0.01488   0.00833  -0.2142   0.6482   0.0312
  -5.000   0.4725   0.01451   0.00792  -0.2162   0.6417   0.0317
  -4.750   0.5069   0.01419   0.00754  -0.2180   0.6358   0.0323
  -4.500   0.5415   0.01386   0.00717  -0.2197   0.6298   0.0329
  -4.250   0.5754   0.01358   0.00683  -0.2213   0.6225   0.0334
  -4.000   0.6086   0.01336   0.00652  -0.2227   0.6156   0.0339
  -3.750   0.6422   0.01311   0.00623  -0.2241   0.6085   0.0344
  -3.500   0.6755   0.01287   0.00593  -0.2255   0.5992   0.0351
  -3.250   0.7076   0.01272   0.00572  -0.2266   0.5901   0.0359
  -3.000   0.7391   0.01261   0.00554  -0.2274   0.5799   0.0368
  -2.750   0.7701   0.01253   0.00539  -0.2282   0.5715   0.0379
  -2.500   0.8012   0.01245   0.00525  -0.2289   0.5624   0.0390
  -2.250   0.8314   0.01241   0.00515  -0.2295   0.5530   0.0408
  -2.000   0.8613   0.01239   0.00507  -0.2299   0.5417   0.0433
  -1.750   0.8906   0.01241   0.00502  -0.2303   0.5296   0.0470
  -1.250   0.9480   0.01250   0.00500  -0.2308   0.5028   0.0660
  -1.000   0.9765   0.01255   0.00502  -0.2310   0.4921   0.0846
  -0.750   1.0061   0.01251   0.00499  -0.2316   0.4814   0.1196
  -0.500   1.0386   0.01222   0.00500  -0.2331   0.4716   0.2720
  -0.250   1.0654   0.01239   0.00514  -0.2330   0.4613   0.2928
   0.000   1.0918   0.01258   0.00528  -0.2327   0.4522   0.3048
   0.250   1.1179   0.01278   0.00544  -0.2323   0.4430   0.3177
   0.500   1.1436   0.01299   0.00562  -0.2319   0.4353   0.3296
   0.750   1.1698   0.01317   0.00578  -0.2316   0.4281   0.3400
   1.000   1.1948   0.01340   0.00598  -0.2311   0.4205   0.3483
   1.250   1.2200   0.01361   0.00616  -0.2306   0.4141   0.3555
   1.500   1.2451   0.01383   0.00634  -0.2301   0.4073   0.3608
   1.750   1.2683   0.01412   0.00655  -0.2292   0.3998   0.3644
   2.000   1.2926   0.01433   0.00676  -0.2286   0.3929   0.3693
   2.250   1.3161   0.01458   0.00699  -0.2278   0.3861   0.3740
   2.500   1.3381   0.01487   0.00724  -0.2268   0.3802   0.3787
   2.750   1.3596   0.01511   0.00746  -0.2257   0.3758   0.3833
   3.000   1.3802   0.01534   0.00770  -0.2243   0.3709   0.3877
   3.250   1.4009   0.01563   0.00799  -0.2231   0.3657   0.3932
   3.500   1.4212   0.01600   0.00834  -0.2219   0.3605   0.3990
   3.750   1.4433   0.01630   0.00864  -0.2210   0.3560   0.4050
   4.000   1.4648   0.01664   0.00898  -0.2200   0.3505   0.4108
   4.250   1.4846   0.01706   0.00940  -0.2188   0.3443   0.4181
   4.500   1.5038   0.01751   0.00983  -0.2175   0.3383   0.4257
   5.000   1.5422   0.01843   0.01076  -0.2151   0.3254   0.4399
   5.250   1.5607   0.01895   0.01127  -0.2138   0.3201   0.4477
   5.750   1.5951   0.02014   0.01245  -0.2109   0.3058   0.4625
   6.000   1.6122   0.02076   0.01308  -0.2095   0.2979   0.4707
   6.250   1.6260   0.02159   0.01387  -0.2077   0.2885   0.4781
   6.500   1.6415   0.02233   0.01462  -0.2062   0.2803   0.4862
   6.750   1.6535   0.02332   0.01558  -0.2043   0.2703   0.4942
   7.000   1.6659   0.02430   0.01652  -0.2026   0.2586   0.5009
   7.250   1.6750   0.02555   0.01773  -0.2005   0.2451   0.5068
   7.500   1.6810   0.02704   0.01915  -0.1981   0.2284   0.5126
   7.750   1.6840   0.02881   0.02081  -0.1956   0.2102   0.5179
   8.000   1.6873   0.03061   0.02254  -0.1932   0.1953   0.5223
   8.250   1.6937   0.03223   0.02414  -0.1912   0.1865   0.5269
   8.500   1.7006   0.03383   0.02574  -0.1894   0.1803   0.5320
   8.750   1.7100   0.03527   0.02720  -0.1878   0.1769   0.5374
   9.000   1.7197   0.03673   0.02867  -0.1864   0.1741   0.5422
   9.250   1.7280   0.03834   0.03032  -0.1849   0.1714   0.5461
   9.500   1.7363   0.03997   0.03198  -0.1834   0.1690   0.5499
   9.750   1.7434   0.04175   0.03380  -0.1820   0.1667   0.5538
  10.000   1.7533   0.04331   0.03540  -0.1808   0.1654   0.5579
  10.250   1.7623   0.04498   0.03712  -0.1796   0.1644   0.5618
  10.500   1.7715   0.04663   0.03884  -0.1784   0.1633   0.5653
  10.750   1.7794   0.04846   0.04073  -0.1773   0.1623   0.5688
  11.000   1.7873   0.05028   0.04262  -0.1761   0.1614   0.5725
  11.250   1.7941   0.05225   0.04464  -0.1750   0.1606   0.5762
  11.500   1.8007   0.05427   0.04671  -0.1739   0.1598   0.5797
  11.750   1.8064   0.05642   0.04891  -0.1728   0.1590   0.5827
  12.000   1.8117   0.05862   0.05119  -0.1718   0.1582   0.5857
  12.250   1.8162   0.06092   0.05356  -0.1708   0.1575   0.5888
  12.500   1.8202   0.06330   0.05601  -0.1698   0.1568   0.5919
  12.750   1.8237   0.06576   0.05853  -0.1689   0.1561   0.5949
  13.000   1.8266   0.06832   0.06115  -0.1680   0.1554   0.5979
  13.250   1.8294   0.07091   0.06380  -0.1671   0.1547   0.6005
  13.500   1.8316   0.07359   0.06656  -0.1663   0.1541   0.6030
  13.750   1.8338   0.07624   0.06928  -0.1655   0.1535   0.6055
  14.000   1.8352   0.07904   0.07214  -0.1647   0.1528   0.6080
  14.250   1.8379   0.08164   0.07482  -0.1641   0.1523   0.6109
  14.500   1.8417   0.08418   0.07744  -0.1635   0.1520   0.6138
  14.750   1.8466   0.08658   0.07991  -0.1630   0.1518   0.6168
  15.000   1.8510   0.08903   0.08243  -0.1625   0.1515   0.6196
  15.250   1.8547   0.09156   0.08506  -0.1620   0.1513   0.6223
  15.500   1.8596   0.09394   0.08752  -0.1616   0.1510   0.6253
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