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GOE 613 AIRFOIL (goe613-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: GOE 613 AIRFOIL (goe613-il)
Reynolds number: 1,000,000
Max Cl/Cd: 106.04 at α=4.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe613-il-1000000-n5.txt
Download as CSV file: xf-goe613-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 613 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
  ------ -------- --------- --------- -------- -------- --------
 -12.000  -0.3918   0.11760   0.11592  -0.0323   1.0000   0.0069
 -11.750  -0.3894   0.11468   0.11301  -0.0328   1.0000   0.0071
 -10.750  -0.6560   0.02321   0.02017  -0.0995   0.9646   0.0121
 -10.500  -0.6304   0.02209   0.01899  -0.1000   0.9610   0.0130
 -10.250  -0.6084   0.01978   0.01645  -0.1006   0.9562   0.0142
 -10.000  -0.5836   0.01761   0.01396  -0.1015   0.9525   0.0152
  -9.750  -0.5563   0.01644   0.01259  -0.1022   0.9482   0.0159
  -9.500  -0.5234   0.01689   0.01313  -0.1030   0.9441   0.0165
  -9.250  -0.4888   0.01751   0.01383  -0.1041   0.9406   0.0169
  -9.000  -0.4543   0.01793   0.01430  -0.1054   0.9371   0.0173
  -8.750  -0.4251   0.01784   0.01417  -0.1058   0.9310   0.0178
  -8.500  -0.3959   0.01753   0.01379  -0.1063   0.9242   0.0184
  -8.250  -0.3711   0.01661   0.01268  -0.1062   0.9164   0.0191
  -8.000  -0.3461   0.01588   0.01178  -0.1059   0.9089   0.0198
  -7.750  -0.3216   0.01525   0.01099  -0.1055   0.9020   0.0202
  -7.500  -0.2954   0.01503   0.01069  -0.1052   0.8955   0.0204
  -7.250  -0.2727   0.01408   0.00955  -0.1046   0.8892   0.0209
  -7.000  -0.2473   0.01390   0.00933  -0.1041   0.8824   0.0215
  -6.750  -0.2216   0.01364   0.00899  -0.1038   0.8761   0.0218
  -6.500  -0.1954   0.01362   0.00896  -0.1034   0.8694   0.0221
  -6.250  -0.1697   0.01342   0.00868  -0.1030   0.8624   0.0225
  -6.000  -0.1445   0.01311   0.00830  -0.1025   0.8543   0.0229
  -5.750  -0.1197   0.01265   0.00772  -0.1019   0.8466   0.0233
  -5.500  -0.0949   0.01217   0.00713  -0.1013   0.8378   0.0238
  -5.250  -0.0697   0.01181   0.00668  -0.1008   0.8281   0.0243
  -5.000  -0.0449   0.01148   0.00623  -0.1001   0.8152   0.0248
  -4.750  -0.0209   0.01110   0.00573  -0.0993   0.7971   0.0251
  -4.500   0.0027   0.01076   0.00524  -0.0983   0.7772   0.0254
  -4.250   0.0263   0.01049   0.00483  -0.0974   0.7578   0.0257
  -4.000   0.0507   0.01024   0.00447  -0.0966   0.7422   0.0259
  -3.750   0.0755   0.00997   0.00411  -0.0959   0.7305   0.0261
  -3.500   0.1007   0.00972   0.00378  -0.0953   0.7199   0.0262
  -3.250   0.1258   0.00949   0.00348  -0.0947   0.7093   0.0264
  -3.000   0.1507   0.00931   0.00323  -0.0940   0.6975   0.0265
  -2.750   0.1758   0.00914   0.00299  -0.0934   0.6845   0.0266
  -2.500   0.2007   0.00900   0.00278  -0.0927   0.6694   0.0267
  -2.250   0.2238   0.00865   0.00233  -0.0917   0.6514   0.0278
  -2.000   0.2477   0.00852   0.00210  -0.0909   0.6279   0.0284
  -1.750   0.2708   0.00851   0.00196  -0.0898   0.5946   0.0291
  -1.500   0.2935   0.00858   0.00186  -0.0887   0.5595   0.0296
  -1.250   0.3171   0.00864   0.00181  -0.0878   0.5331   0.0303
  -1.000   0.3419   0.00867   0.00176  -0.0871   0.5151   0.0310
  -0.750   0.3671   0.00867   0.00170  -0.0866   0.5013   0.0316
  -0.500   0.3925   0.00867   0.00164  -0.0860   0.4888   0.0322
  -0.250   0.4181   0.00867   0.00160  -0.0855   0.4767   0.0329
   0.000   0.4436   0.00869   0.00156  -0.0850   0.4634   0.0335
   0.250   0.4689   0.00873   0.00154  -0.0845   0.4485   0.0342
   0.500   0.4942   0.00878   0.00153  -0.0839   0.4333   0.0347
   0.750   0.5193   0.00882   0.00151  -0.0834   0.4187   0.0369
   1.000   0.5443   0.00887   0.00153  -0.0828   0.4030   0.0410
   1.250   0.5693   0.00896   0.00155  -0.0822   0.3871   0.0448
   1.500   0.5941   0.00903   0.00159  -0.0816   0.3720   0.0529
   1.750   0.6185   0.00905   0.00165  -0.0809   0.3583   0.0959
   2.000   0.6277   0.00773   0.00183  -0.0777   0.3484   0.6997
   2.250   0.6759   0.00736   0.00208  -0.0822   0.3323   0.9631
   2.500   0.7366   0.00761   0.00223  -0.0897   0.3187   0.9938
   2.750   0.7795   0.00780   0.00234  -0.0933   0.3088   1.0000
   3.000   0.8021   0.00791   0.00242  -0.0922   0.3024   1.0000
   3.250   0.8244   0.00804   0.00251  -0.0910   0.2956   1.0000
   3.500   0.8470   0.00817   0.00261  -0.0900   0.2895   1.0000
   3.750   0.8691   0.00833   0.00272  -0.0888   0.2802   1.0000
   4.000   0.8915   0.00848   0.00283  -0.0877   0.2719   1.0000
   4.250   0.9131   0.00868   0.00297  -0.0865   0.2602   1.0000
   4.500   0.9354   0.00885   0.00309  -0.0854   0.2515   1.0000
   4.750   0.9575   0.00903   0.00323  -0.0843   0.2421   1.0000
   5.000   0.9791   0.00925   0.00339  -0.0831   0.2305   1.0000
   5.250   1.0009   0.00946   0.00355  -0.0820   0.2203   1.0000
   5.500   1.0222   0.00970   0.00372  -0.0808   0.2080   1.0000
   5.750   1.0438   0.00992   0.00391  -0.0796   0.1978   1.0000
   6.000   1.0632   0.01027   0.00414  -0.0781   0.1781   1.0000
   6.250   1.0768   0.01097   0.00457  -0.0756   0.1335   1.0000
   6.500   1.0897   0.01172   0.00509  -0.0729   0.0945   1.0000
   6.750   1.0932   0.01311   0.00607  -0.0687   0.0180   1.0000
   7.000   1.1134   0.01341   0.00638  -0.0673   0.0142   1.0000
   7.250   1.1335   0.01370   0.00670  -0.0660   0.0128   1.0000
   7.500   1.1523   0.01404   0.00705  -0.0644   0.0114   1.0000
   7.750   1.1697   0.01438   0.00742  -0.0625   0.0102   1.0000
   8.000   1.1876   0.01469   0.00775  -0.0608   0.0098   1.0000
   8.250   1.2050   0.01502   0.00811  -0.0590   0.0092   1.0000
   8.500   1.2221   0.01538   0.00850  -0.0572   0.0085   1.0000
   8.750   1.2385   0.01580   0.00894  -0.0553   0.0080   1.0000
   9.000   1.2541   0.01628   0.00945  -0.0533   0.0073   1.0000
   9.250   1.2708   0.01669   0.00990  -0.0516   0.0070   1.0000
   9.500   1.2869   0.01715   0.01040  -0.0498   0.0067   1.0000
   9.750   1.3029   0.01762   0.01091  -0.0481   0.0063   1.0000
  10.000   1.3179   0.01814   0.01147  -0.0462   0.0061   1.0000
  10.250   1.3328   0.01869   0.01205  -0.0445   0.0058   1.0000
  10.500   1.3467   0.01930   0.01270  -0.0426   0.0056   1.0000
  10.750   1.3581   0.02007   0.01353  -0.0404   0.0053   1.0000
  11.000   1.3700   0.02083   0.01434  -0.0385   0.0051   1.0000
  11.250   1.3825   0.02157   0.01513  -0.0367   0.0049   1.0000
  11.500   1.3946   0.02234   0.01598  -0.0349   0.0048   1.0000
  11.750   1.4059   0.02319   0.01689  -0.0332   0.0046   1.0000
  12.000   1.4160   0.02416   0.01791  -0.0314   0.0045   1.0000
  12.250   1.4257   0.02517   0.01899  -0.0297   0.0043   1.0000
  12.500   1.4347   0.02627   0.02015  -0.0280   0.0042   1.0000
  12.750   1.4426   0.02749   0.02143  -0.0264   0.0040   1.0000
  13.000   1.4507   0.02874   0.02274  -0.0250   0.0039   1.0000
  13.250   1.4561   0.03026   0.02434  -0.0235   0.0039   1.0000
  13.500   1.4604   0.03195   0.02611  -0.0221   0.0037   1.0000
  13.750   1.4626   0.03389   0.02813  -0.0208   0.0036   1.0000
  14.000   1.4601   0.03640   0.03074  -0.0196   0.0035   1.0000
  14.250   1.4571   0.03908   0.03354  -0.0186   0.0035   1.0000
  14.500   1.4587   0.04142   0.03597  -0.0181   0.0034   1.0000
  14.750   1.4538   0.04461   0.03928  -0.0177   0.0034   1.0000
  15.000   1.4558   0.04714   0.04189  -0.0175   0.0033   1.0000
  15.250   1.4470   0.05110   0.04597  -0.0177   0.0034   1.0000
  15.500   1.4431   0.05468   0.04966  -0.0182   0.0033   1.0000
  15.750   1.4346   0.05903   0.05413  -0.0190   0.0033   1.0000
  16.000   1.4215   0.06415   0.05938  -0.0202   0.0033   1.0000
  16.250   1.4122   0.06886   0.06420  -0.0214   0.0032   1.0000
  16.500   1.4006   0.07399   0.06945  -0.0229   0.0032   1.0000
  16.750   1.3878   0.07933   0.07490  -0.0244   0.0032   1.0000
  17.000   1.3731   0.08505   0.08073  -0.0262   0.0032   1.0000
  17.250   1.3580   0.09095   0.08675  -0.0281   0.0031   1.0000
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