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GOE 255 (MVA CA.6) AIRFOIL (goe255-il) Xfoil prediction polar at RE=100,000 Ncrit=9


Details Polar file
Airfoil: GOE 255 (MVA CA.6) AIRFOIL (goe255-il)
Reynolds number: 100,000
Max Cl/Cd: 41.38 at α=8°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe255-il-100000.txt
Download as CSV file: xf-goe255-il-100000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 255 (MVA CA.6) 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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -11.750  -0.4408   0.10763   0.10349  -0.0542   1.0000   0.0696
 -11.500  -0.6198   0.07171   0.06702  -0.0832   0.9910   0.0590
 -11.250  -0.6374   0.06546   0.06052  -0.0899   0.9825   0.0586
 -11.000  -0.6519   0.06052   0.05526  -0.0931   0.9718   0.0584
 -10.750  -0.6584   0.05591   0.05025  -0.0951   0.9616   0.0585
 -10.500  -0.6533   0.05148   0.04528  -0.0976   0.9544   0.0588
 -10.250  -0.6473   0.04803   0.04148  -0.0977   0.9453   0.0595
 -10.000  -0.6152   0.04542   0.03887  -0.1008   0.9413   0.0623
  -9.750  -0.6031   0.04371   0.03697  -0.0999   0.9317   0.0645
  -9.500  -0.5749   0.04095   0.03373  -0.1022   0.9268   0.0676
  -9.250  -0.5611   0.03890   0.03136  -0.1011   0.9177   0.0697
  -9.000  -0.5267   0.03686   0.02939  -0.1032   0.9130   0.0743
  -8.750  -0.5038   0.03545   0.02762  -0.1033   0.9056   0.0801
  -8.500  -0.4758   0.03371   0.02606  -0.1042   0.8994   0.0881
  -8.250  -0.4373   0.03177   0.02408  -0.1070   0.8960   0.1028
  -8.000  -0.4242   0.03084   0.02312  -0.1051   0.8861   0.1184
  -7.750  -0.3865   0.02958   0.02190  -0.1078   0.8819   0.1481
  -7.500  -0.3664   0.02908   0.02150  -0.1071   0.8731   0.1687
  -7.250  -0.3311   0.02830   0.02062  -0.1089   0.8678   0.1962
  -7.000  -0.2912   0.02745   0.01976  -0.1114   0.8646   0.2270
  -6.750  -0.2748   0.02725   0.01973  -0.1097   0.8540   0.2471
  -6.500  -0.2363   0.02664   0.01911  -0.1115   0.8503   0.2752
  -6.250  -0.2156   0.02680   0.01935  -0.1103   0.8409   0.2932
  -6.000  -0.1796   0.02676   0.01931  -0.1113   0.8360   0.3142
  -5.750  -0.1399   0.02655   0.01893  -0.1129   0.8329   0.3364
  -5.500  -0.1230   0.02704   0.01945  -0.1110   0.8221   0.3495
  -5.250  -0.0863   0.02683   0.01908  -0.1122   0.8182   0.3691
  -5.000  -0.0667   0.02720   0.01946  -0.1108   0.8089   0.3825
  -4.750  -0.0344   0.02705   0.01922  -0.1113   0.8036   0.4011
  -4.500   0.0019   0.02678   0.01883  -0.1123   0.8002   0.4218
  -4.250   0.0155   0.02731   0.01939  -0.1101   0.7896   0.4358
  -4.000   0.0484   0.02705   0.01904  -0.1107   0.7855   0.4545
  -3.750   0.0686   0.02733   0.01935  -0.1096   0.7785   0.4675
  -3.500   0.0912   0.02748   0.01948  -0.1088   0.7719   0.4811
  -3.250   0.1234   0.02727   0.01918  -0.1094   0.7684   0.4964
  -3.000   0.1397   0.02782   0.01966  -0.1081   0.7615   0.5089
  -2.750   0.1592   0.02823   0.02007  -0.1071   0.7554   0.5202
  -2.500   0.1907   0.02809   0.01988  -0.1076   0.7522   0.5324
  -2.250   0.2252   0.02786   0.01954  -0.1086   0.7497   0.5452
  -2.000   0.2206   0.02950   0.02125  -0.1049   0.7395   0.5521
  -1.750   0.2489   0.02961   0.02129  -0.1052   0.7363   0.5629
  -1.500   0.2848   0.02934   0.02092  -0.1064   0.7340   0.5749
  -1.250   0.2745   0.03147   0.02314  -0.1022   0.7247   0.5801
  -1.000   0.3006   0.03166   0.02329  -0.1022   0.7205   0.5907
  -0.750   0.3394   0.03111   0.02270  -0.1035   0.7180   0.6016
  -0.500   0.3317   0.03321   0.02482  -0.0998   0.7089   0.6087
  -0.250   0.3561   0.03343   0.02508  -0.0995   0.7043   0.6197
   0.000   0.3937   0.03295   0.02459  -0.1005   0.7018   0.6342
   0.250   0.4352   0.03231   0.02391  -0.1020   0.7000   0.6486
   0.500   0.3840   0.03701   0.02876  -0.0942   0.6876   0.6515
   0.750   0.4331   0.03591   0.02763  -0.0965   0.6856   0.6656
   1.000   0.4804   0.03492   0.02662  -0.0987   0.6839   0.6803
   1.750   0.5021   0.03866   0.03062  -0.0925   0.6635   0.7242
   2.000   0.5855   0.03497   0.02702  -0.0974   0.6660   0.7668
   2.250   0.5368   0.03967   0.03198  -0.0899   0.6525   0.7955
   2.500   0.5195   0.04231   0.03507  -0.0854   0.6423   0.9612
   2.750   0.5606   0.04213   0.03465  -0.0881   0.6380   1.0000
   3.000   0.6107   0.04104   0.03339  -0.0904   0.6360   1.0000
   3.250   0.6642   0.03952   0.03174  -0.0927   0.6347   1.0000
   3.500   0.6414   0.04313   0.03535  -0.0887   0.6210   1.0000
   3.750   0.6931   0.04149   0.03362  -0.0904   0.6194   1.0000
   4.000   0.7502   0.03944   0.03148  -0.0926   0.6186   1.0000
   4.250   0.7335   0.04243   0.03449  -0.0887   0.6043   1.0000
   4.500   0.7686   0.04178   0.03381  -0.0889   0.5999   1.0000
   4.750   0.8362   0.03894   0.03090  -0.0921   0.6012   1.0000
   5.000   0.8308   0.04085   0.03284  -0.0887   0.5885   1.0000
   5.250   0.8886   0.03866   0.03062  -0.0910   0.5877   1.0000
   5.500   0.9522   0.03647   0.02839  -0.0946   0.5867   1.0000
   5.750   0.9007   0.04090   0.03290  -0.0861   0.5653   1.0000
   6.000   0.9790   0.03733   0.02929  -0.0904   0.5678   1.0000
   6.250   1.0007   0.03725   0.02923  -0.0892   0.5586   1.0000
   6.500   1.0706   0.03475   0.02672  -0.0937   0.5567   1.0000
   6.750   1.1441   0.03248   0.02439  -0.0992   0.5544   1.0000
   7.000   1.1400   0.03363   0.02561  -0.0947   0.5412   1.0000
   7.250   1.1448   0.03442   0.02644  -0.0914   0.5296   1.0000
   7.500   1.2147   0.03230   0.02426  -0.0964   0.5244   1.0000
   7.750   1.2176   0.03310   0.02510  -0.0928   0.5123   1.0000
   8.000   1.2887   0.03114   0.02300  -0.0983   0.5062   1.0000
   8.250   1.2795   0.03244   0.02442  -0.0931   0.4938   1.0000
   8.500   1.2992   0.03263   0.02462  -0.0918   0.4846   1.0000
   8.750   1.3258   0.03258   0.02457  -0.0915   0.4759   1.0000
   9.000   1.3228   0.03386   0.02594  -0.0874   0.4669   1.0000
   9.250   1.3537   0.03375   0.02583  -0.0878   0.4597   1.0000
   9.500   1.3476   0.03530   0.02749  -0.0836   0.4513   1.0000
   9.750   1.3745   0.03526   0.02746  -0.0835   0.4442   1.0000
  10.000   1.3718   0.03676   0.02906  -0.0801   0.4364   1.0000
  10.250   1.3921   0.03700   0.02935  -0.0792   0.4291   1.0000
  10.500   1.3957   0.03821   0.03065  -0.0767   0.4215   1.0000
  10.750   1.4219   0.03783   0.03026  -0.0762   0.4131   1.0000
  11.000   1.4132   0.03978   0.03233  -0.0728   0.4046   1.0000
  11.250   1.4472   0.03855   0.03100  -0.0727   0.3939   1.0000
  11.500   1.4546   0.03928   0.03176  -0.0707   0.3834   1.0000
  11.750   1.4551   0.04075   0.03328  -0.0683   0.3737   1.0000
  12.000   1.4782   0.04065   0.03310  -0.0676   0.3628   1.0000
  12.250   1.5036   0.04050   0.03278  -0.0671   0.3503   1.0000
  12.500   1.4935   0.04287   0.03529  -0.0642   0.3407   1.0000
  12.750   1.5040   0.04393   0.03633  -0.0628   0.3300   1.0000
  13.000   1.5254   0.04428   0.03655  -0.0622   0.3183   1.0000
  13.250   1.5124   0.04703   0.03947  -0.0596   0.3095   1.0000
  13.500   1.5184   0.04845   0.04089  -0.0581   0.2993   1.0000
  13.750   1.5177   0.05039   0.04288  -0.0565   0.2900   1.0000
  14.000   1.5128   0.05283   0.04545  -0.0548   0.2821   1.0000
  14.250   1.5113   0.05496   0.04765  -0.0535   0.2738   1.0000
  14.500   1.5035   0.05780   0.05065  -0.0521   0.2663   1.0000
  14.750   1.4959   0.06066   0.05361  -0.0509   0.2582   1.0000
  15.000   1.4835   0.06419   0.05728  -0.0500   0.2504   1.0000
  15.250   1.4744   0.06748   0.06067  -0.0493   0.2421   1.0000
  15.500   1.4609   0.07162   0.06498  -0.0489   0.2347   1.0000
  15.750   1.4533   0.07514   0.06858  -0.0487   0.2268   1.0000
  16.000   1.4390   0.07978   0.07340  -0.0488   0.2194   1.0000
  16.250   1.4330   0.08333   0.07700  -0.0490   0.2114   1.0000
  16.500   1.4150   0.08884   0.08269  -0.0496   0.2037   1.0000
  16.750   1.4118   0.09222   0.08608  -0.0500   0.1960   1.0000
  17.000   1.3950   0.09781   0.09186  -0.0509   0.1891   1.0000
  17.250   1.3913   0.10141   0.09545  -0.0515   0.1813   1.0000
  17.500   1.3755   0.10701   0.10118  -0.0528   0.1738   1.0000
  17.750   1.3677   0.11140   0.10558  -0.0538   0.1658   1.0000
  18.000   1.3561   0.11652   0.11080  -0.0552   0.1586   1.0000
  18.250   1.3449   0.12166   0.11601  -0.0568   0.1510   1.0000
  18.500   1.3353   0.12657   0.12090  -0.0585   0.1418   1.0000
  18.750   1.3181   0.13315   0.12768  -0.0610   0.1347   1.0000
  19.000   1.3043   0.13919   0.13378  -0.0636   0.1248   1.0000
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