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GOE 243 (MVA PR.3) AIRFOIL (goe243-il) Xfoil prediction polar at RE=100,000 Ncrit=5


Details Polar file
Airfoil: GOE 243 (MVA PR.3) AIRFOIL (goe243-il)
Reynolds number: 100,000
Max Cl/Cd: 49.43 at α=3.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe243-il-100000-n5.txt
Download as CSV file: xf-goe243-il-100000-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 =     0.100 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
  -9.500   0.1723   0.10288   0.09723  -0.1175   0.8558   0.0887
  -9.250   0.1608   0.09981   0.09416  -0.1216   0.8482   0.0902
  -8.750   0.1723   0.08825   0.08248  -0.1249   0.8376   0.0599
  -8.500   0.1847   0.08635   0.08057  -0.1248   0.8309   0.0588
  -8.250   0.1940   0.08355   0.07775  -0.1257   0.8256   0.0577
  -8.000   0.1740   0.07534   0.06949  -0.1311   0.8189   0.0538
  -7.750   0.1782   0.07279   0.06695  -0.1317   0.8113   0.0534
  -7.500   0.1803   0.06897   0.06310  -0.1335   0.8054   0.0529
  -7.250   0.1699   0.06382   0.05792  -0.1362   0.7988   0.0522
  -7.000   0.1356   0.05614   0.05013  -0.1432   0.7882   0.0513
  -6.750   0.1401   0.04559   0.03902  -0.1652   0.7816   0.0511
  -6.500   0.1706   0.04083   0.03381  -0.1782   0.7728   0.0518
  -6.250   0.2131   0.03727   0.02974  -0.1879   0.7665   0.0526
  -6.000   0.2574   0.03455   0.02659  -0.1944   0.7621   0.0530
  -5.750   0.2956   0.03264   0.02434  -0.1984   0.7571   0.0534
  -5.500   0.3232   0.03147   0.02296  -0.1998   0.7492   0.0538
  -5.250   0.3549   0.03035   0.02176  -0.2010   0.7439   0.0543
  -5.000   0.3894   0.02929   0.02061  -0.2024   0.7397   0.0551
  -4.750   0.4150   0.02869   0.01998  -0.2024   0.7330   0.0558
  -4.500   0.4417   0.02811   0.01937  -0.2024   0.7262   0.0569
  -4.250   0.4739   0.02740   0.01854  -0.2031   0.7211   0.0588
  -4.000   0.5060   0.02676   0.01785  -0.2035   0.7168   0.0606
  -3.750   0.5255   0.02666   0.01787  -0.2022   0.7084   0.0621
  -3.500   0.5525   0.02632   0.01754  -0.2016   0.7023   0.0637
  -3.250   0.5830   0.02595   0.01711  -0.2013   0.6976   0.0655
  -3.000   0.6056   0.02592   0.01716  -0.2004   0.6899   0.0672
  -2.750   0.6361   0.02565   0.01690  -0.2011   0.6830   0.0698
  -2.500   0.6751   0.02512   0.01627  -0.2035   0.6776   0.0746
  -2.250   0.7089   0.02478   0.01590  -0.2056   0.6699   0.0806
  -2.000   0.7489   0.02419   0.01523  -0.2091   0.6624   0.0890
  -1.750   0.7985   0.02316   0.01409  -0.2145   0.6568   0.1093
  -1.500   0.8424   0.02236   0.01397  -0.2197   0.6482   0.3055
  -1.250   0.8721   0.02254   0.01405  -0.2200   0.6405   0.3425
  -1.000   0.9012   0.02282   0.01425  -0.2196   0.6344   0.3676
  -0.750   0.9229   0.02333   0.01477  -0.2184   0.6252   0.3870
  -0.500   0.9456   0.02373   0.01522  -0.2166   0.6182   0.3986
  -0.250   0.9735   0.02391   0.01527  -0.2166   0.6105   0.4107
   0.000   0.9942   0.02424   0.01564  -0.2149   0.6019   0.4161
   0.250   1.0252   0.02419   0.01544  -0.2152   0.5954   0.4211
   0.500   1.0490   0.02438   0.01558  -0.2149   0.5859   0.4259
   0.750   1.0809   0.02428   0.01527  -0.2159   0.5781   0.4319
   1.000   1.1049   0.02445   0.01542  -0.2151   0.5698   0.4346
   1.250   1.1281   0.02465   0.01559  -0.2143   0.5606   0.4379
   1.500   1.1545   0.02476   0.01559  -0.2139   0.5524   0.4420
   1.750   1.1765   0.02502   0.01581  -0.2131   0.5424   0.4471
   2.000   1.2064   0.02505   0.01562  -0.2136   0.5344   0.4546
   2.250   1.2244   0.02547   0.01611  -0.2120   0.5251   0.4582
   2.500   1.2483   0.02570   0.01628  -0.2112   0.5175   0.4629
   2.750   1.2691   0.02608   0.01663  -0.2101   0.5095   0.4686
   3.000   1.2925   0.02638   0.01684  -0.2096   0.5017   0.4761
   3.250   1.3169   0.02664   0.01702  -0.2090   0.4953   0.4809
   3.500   1.3323   0.02718   0.01762  -0.2071   0.4873   0.4855
   3.750   1.3524   0.02755   0.01794  -0.2059   0.4803   0.4922
   4.000   1.3740   0.02793   0.01822  -0.2050   0.4738   0.5006
   4.250   1.3871   0.02854   0.01890  -0.2028   0.4664   0.5052
   4.500   1.4068   0.02899   0.01929  -0.2015   0.4598   0.5118
   4.750   1.4278   0.02950   0.01972  -0.2008   0.4536   0.5211
   5.000   1.4423   0.03020   0.02050  -0.1990   0.4472   0.5256
   5.250   1.4610   0.03076   0.02104  -0.1977   0.4416   0.5320
   5.500   1.4840   0.03122   0.02137  -0.1972   0.4364   0.5421
   5.750   1.4944   0.03212   0.02241  -0.1950   0.4298   0.5468
   6.000   1.5088   0.03287   0.02317  -0.1933   0.4235   0.5537
   6.250   1.5303   0.03337   0.02354  -0.1926   0.4181   0.5628
   6.500   1.5397   0.03440   0.02469  -0.1904   0.4120   0.5677
   6.750   1.5506   0.03538   0.02572  -0.1885   0.4056   0.5745
   7.000   1.5678   0.03607   0.02634  -0.1874   0.3999   0.5829
   7.250   1.5794   0.03706   0.02739  -0.1856   0.3946   0.5884
   7.500   1.5879   0.03831   0.02873  -0.1837   0.3887   0.5954
   7.750   1.6001   0.03933   0.02976  -0.1821   0.3832   0.6026
   8.000   1.6158   0.04007   0.03047  -0.1808   0.3782   0.6088
   8.250   1.6189   0.04178   0.03233  -0.1787   0.3719   0.6155
   8.500   1.6260   0.04323   0.03383  -0.1769   0.3657   0.6218
   8.750   1.6383   0.04421   0.03478  -0.1754   0.3603   0.6277
   9.000   1.6404   0.04615   0.03686  -0.1735   0.3538   0.6339
   9.250   1.6440   0.04800   0.03878  -0.1717   0.3472   0.6401
   9.500   1.6529   0.04928   0.04004  -0.1702   0.3413   0.6457
   9.750   1.6514   0.05171   0.04261  -0.1684   0.3343   0.6513
  10.000   1.6532   0.05388   0.04484  -0.1668   0.3273   0.6573
  10.250   1.6588   0.05560   0.04657  -0.1653   0.3211   0.6623
  10.500   1.6537   0.05863   0.04977  -0.1638   0.3131   0.6673
  10.750   1.6564   0.06083   0.05196  -0.1625   0.3060   0.6734
  11.000   1.6521   0.06397   0.05521  -0.1612   0.2980   0.6778
  11.250   1.6508   0.06675   0.05804  -0.1600   0.2901   0.6825
  11.500   1.6474   0.06992   0.06127  -0.1589   0.2822   0.6875
  11.750   1.6439   0.07317   0.06455  -0.1580   0.2740   0.6928
  12.000   1.6415   0.07631   0.06775  -0.1571   0.2665   0.6973
  12.250   1.6375   0.07974   0.07123  -0.1564   0.2589   0.7020
  12.500   1.6384   0.08255   0.07402  -0.1557   0.2527   0.7074
  12.750   1.6343   0.08617   0.07771  -0.1552   0.2461   0.7122
  13.000   1.6367   0.08876   0.08029  -0.1546   0.2410   0.7176
  13.250   1.6383   0.09160   0.08317  -0.1541   0.2365   0.7234
  13.500   1.6372   0.09491   0.08655  -0.1538   0.2319   0.7287
  13.750   1.6407   0.09747   0.08914  -0.1534   0.2283   0.7343
  14.000   1.6496   0.09921   0.09085  -0.1530   0.2254   0.7415
  14.250   1.6551   0.10152   0.09319  -0.1527   0.2225   0.7480
  14.500   1.6543   0.10485   0.09666  -0.1526   0.2194   0.7541
  14.750   1.6565   0.10774   0.09963  -0.1526   0.2166   0.7608
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