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GOE 593 AIRFOIL (goe593-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: GOE 593 AIRFOIL (goe593-il)
Reynolds number: 1,000,000
Max Cl/Cd: 117.09 at α=2.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe593-il-1000000.txt
Download as CSV file: xf-goe593-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 593 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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -14.250  -0.9737   0.03640   0.03373  -0.0914   1.0000   0.0126
 -14.000  -1.0030   0.03428   0.03151  -0.0866   1.0000   0.0127
 -13.750  -1.0256   0.03288   0.03002  -0.0805   1.0000   0.0127
 -13.500  -1.0139   0.03130   0.02834  -0.0803   0.9989   0.0129
 -13.250  -0.9885   0.02971   0.02664  -0.0823   0.9968   0.0132
 -13.000  -0.9625   0.02814   0.02494  -0.0842   0.9948   0.0135
 -12.750  -0.9357   0.02707   0.02375  -0.0855   0.9930   0.0139
 -12.500  -0.9130   0.02557   0.02209  -0.0864   0.9900   0.0142
 -12.250  -0.8860   0.02441   0.02077  -0.0876   0.9877   0.0145
 -12.000  -0.8623   0.02248   0.01862  -0.0888   0.9856   0.0149
 -11.750  -0.8337   0.02131   0.01736  -0.0903   0.9844   0.0154
 -11.500  -0.8090   0.02067   0.01666  -0.0902   0.9810   0.0157
 -11.250  -0.7809   0.02020   0.01615  -0.0907   0.9781   0.0161
 -11.000  -0.7509   0.01965   0.01554  -0.0917   0.9761   0.0166
 -10.750  -0.7207   0.01889   0.01468  -0.0927   0.9745   0.0171
 -10.500  -0.6890   0.01828   0.01396  -0.0939   0.9734   0.0176
 -10.250  -0.6580   0.01742   0.01296  -0.0952   0.9723   0.0180
 -10.000  -0.6399   0.01651   0.01199  -0.0937   0.9660   0.0187
  -9.750  -0.6094   0.01612   0.01158  -0.0945   0.9638   0.0192
  -9.500  -0.5773   0.01579   0.01122  -0.0955   0.9622   0.0199
  -9.250  -0.5445   0.01539   0.01076  -0.0967   0.9607   0.0206
  -9.000  -0.5107   0.01496   0.01025  -0.0981   0.9594   0.0213
  -8.750  -0.4879   0.01451   0.00971  -0.0972   0.9527   0.0217
  -8.500  -0.4581   0.01354   0.00867  -0.0981   0.9494   0.0226
  -8.250  -0.4221   0.01319   0.00832  -0.0999   0.9472   0.0234
  -8.000  -0.3896   0.01292   0.00801  -0.1010   0.9432   0.0243
  -7.750  -0.3590   0.01260   0.00762  -0.1016   0.9374   0.0251
  -7.500  -0.3235   0.01231   0.00726  -0.1033   0.9332   0.0258
  -7.250  -0.2961   0.01145   0.00633  -0.1035   0.9264   0.0269
  -7.000  -0.2653   0.01112   0.00597  -0.1042   0.9200   0.0278
  -6.750  -0.2351   0.01086   0.00567  -0.1047   0.9135   0.0288
  -6.500  -0.2075   0.01061   0.00536  -0.1046   0.9056   0.0297
  -6.250  -0.1789   0.01038   0.00506  -0.1047   0.8986   0.0304
  -6.000  -0.1529   0.01022   0.00485  -0.1042   0.8905   0.0309
  -5.750  -0.1292   0.00962   0.00418  -0.1034   0.8828   0.0325
  -5.500  -0.1045   0.00939   0.00393  -0.1027   0.8742   0.0335
  -5.250  -0.0783   0.00921   0.00370  -0.1022   0.8666   0.0346
  -5.000  -0.0535   0.00901   0.00346  -0.1015   0.8576   0.0356
  -4.750  -0.0277   0.00888   0.00327  -0.1009   0.8489   0.0365
  -4.500  -0.0036   0.00861   0.00293  -0.1000   0.8386   0.0379
  -4.250   0.0203   0.00839   0.00268  -0.0990   0.8266   0.0396
  -4.000   0.0446   0.00826   0.00249  -0.0981   0.8130   0.0412
  -3.750   0.0691   0.00815   0.00231  -0.0972   0.7991   0.0429
  -3.500   0.0934   0.00802   0.00212  -0.0963   0.7864   0.0455
  -3.250   0.1178   0.00789   0.00196  -0.0954   0.7744   0.0496
  -3.000   0.1423   0.00775   0.00181  -0.0946   0.7624   0.0570
  -2.750   0.1661   0.00756   0.00169  -0.0937   0.7505   0.0823
  -2.500   0.1905   0.00746   0.00163  -0.0928   0.7394   0.1057
  -2.250   0.2152   0.00742   0.00157  -0.0921   0.7274   0.1195
  -2.000   0.2404   0.00738   0.00152  -0.0914   0.7157   0.1308
  -1.750   0.2654   0.00734   0.00147  -0.0907   0.7047   0.1428
  -1.500   0.2900   0.00730   0.00142  -0.0899   0.6942   0.1581
  -1.250   0.3150   0.00720   0.00138  -0.0892   0.6838   0.1833
  -1.000   0.3388   0.00705   0.00137  -0.0884   0.6741   0.2376
  -0.750   0.3625   0.00690   0.00135  -0.0875   0.6646   0.2957
  -0.500   0.3842   0.00657   0.00134  -0.0863   0.6558   0.4085
  -0.250   0.4016   0.00612   0.00136  -0.0842   0.6464   0.5859
   0.000   0.4188   0.00574   0.00140  -0.0818   0.6370   0.7260
   0.250   0.4357   0.00547   0.00147  -0.0791   0.6274   0.8434
   0.500   0.4654   0.00543   0.00156  -0.0793   0.6167   0.9125
   0.750   0.5138   0.00554   0.00166  -0.0837   0.6052   0.9480
   1.000   0.5595   0.00569   0.00175  -0.0876   0.5929   0.9628
   1.250   0.5966   0.00584   0.00183  -0.0895   0.5799   0.9729
   1.500   0.6315   0.00601   0.00192  -0.0910   0.5649   0.9805
   1.750   0.6701   0.00618   0.00200  -0.0933   0.5459   0.9855
   2.000   0.7091   0.00637   0.00209  -0.0958   0.5254   0.9900
   2.250   0.7481   0.00660   0.00220  -0.0983   0.5022   0.9946
   2.500   0.7953   0.00684   0.00230  -0.1027   0.4738   0.9988
   2.750   0.8243   0.00704   0.00238  -0.1031   0.4498   1.0000
   3.000   0.8420   0.00722   0.00246  -0.1010   0.4290   1.0000
   3.500   0.8777   0.00761   0.00267  -0.0970   0.3917   1.0000
   3.750   0.8962   0.00780   0.00279  -0.0950   0.3761   1.0000
   4.000   0.9148   0.00799   0.00291  -0.0931   0.3620   1.0000
   4.500   0.9524   0.00838   0.00318  -0.0895   0.3336   1.0000
   4.750   0.9721   0.00856   0.00331  -0.0878   0.3231   1.0000
   5.000   0.9911   0.00876   0.00347  -0.0860   0.3116   1.0000
   5.250   1.0103   0.00896   0.00362  -0.0842   0.3012   1.0000
   5.500   1.0305   0.00913   0.00377  -0.0827   0.2930   1.0000
   5.750   1.0496   0.00934   0.00394  -0.0809   0.2844   1.0000
   6.000   1.0703   0.00949   0.00409  -0.0795   0.2776   1.0000
   6.500   1.1099   0.00988   0.00444  -0.0763   0.2620   1.0000
   6.750   1.1284   0.01014   0.00465  -0.0745   0.2528   1.0000
   7.000   1.1489   0.01031   0.00483  -0.0731   0.2458   1.0000
   7.250   1.1661   0.01056   0.00504  -0.0711   0.2385   1.0000
   7.500   1.1850   0.01072   0.00522  -0.0693   0.2335   1.0000
   7.750   1.2024   0.01094   0.00544  -0.0673   0.2265   1.0000
   8.000   1.2205   0.01116   0.00565  -0.0654   0.2204   1.0000
   8.250   1.2379   0.01142   0.00589  -0.0635   0.2118   1.0000
   8.500   1.2559   0.01168   0.00614  -0.0617   0.2024   1.0000
   8.750   1.2726   0.01202   0.00643  -0.0598   0.1901   1.0000
   9.000   1.2875   0.01244   0.00677  -0.0576   0.1717   1.0000
   9.250   1.2980   0.01310   0.00726  -0.0547   0.1432   1.0000
   9.500   1.3029   0.01407   0.00800  -0.0510   0.1075   1.0000
   9.750   1.3082   0.01506   0.00881  -0.0475   0.0800   1.0000
  10.000   1.3197   0.01577   0.00945  -0.0451   0.0685   1.0000
  10.250   1.3342   0.01633   0.01001  -0.0432   0.0626   1.0000
  10.500   1.3480   0.01694   0.01061  -0.0413   0.0583   1.0000
  10.750   1.3632   0.01748   0.01118  -0.0396   0.0550   1.0000
  11.000   1.3784   0.01804   0.01177  -0.0380   0.0524   1.0000
  11.250   1.3915   0.01873   0.01246  -0.0362   0.0493   1.0000
  11.500   1.4050   0.01941   0.01317  -0.0345   0.0468   1.0000
  11.750   1.4206   0.01999   0.01379  -0.0331   0.0447   1.0000
  12.000   1.4338   0.02072   0.01455  -0.0316   0.0424   1.0000
  12.250   1.4444   0.02164   0.01548  -0.0297   0.0394   1.0000
  12.500   1.4593   0.02230   0.01619  -0.0285   0.0377   1.0000
  12.750   1.4713   0.02318   0.01709  -0.0270   0.0351   1.0000
  13.000   1.4810   0.02422   0.01815  -0.0254   0.0323   1.0000
  13.250   1.4923   0.02519   0.01915  -0.0241   0.0296   1.0000
  13.500   1.4999   0.02645   0.02042  -0.0225   0.0269   1.0000
  13.750   1.5080   0.02772   0.02171  -0.0211   0.0238   1.0000
  14.000   1.5142   0.02918   0.02320  -0.0196   0.0217   1.0000
  14.250   1.5200   0.03072   0.02478  -0.0183   0.0199   1.0000
  14.500   1.5221   0.03263   0.02673  -0.0169   0.0183   1.0000
  14.750   1.5277   0.03430   0.02849  -0.0159   0.0174   1.0000
  15.000   1.5310   0.03626   0.03049  -0.0149   0.0165   1.0000
  15.250   1.5322   0.03848   0.03278  -0.0140   0.0157   1.0000
  15.500   1.5296   0.04116   0.03554  -0.0131   0.0149   1.0000
  15.750   1.5324   0.04340   0.03786  -0.0126   0.0144   1.0000
  16.000   1.5335   0.04589   0.04044  -0.0123   0.0140   1.0000
  16.250   1.5326   0.04865   0.04327  -0.0120   0.0135   1.0000
  16.500   1.5294   0.05176   0.04647  -0.0119   0.0131   1.0000
  16.750   1.5208   0.05563   0.05042  -0.0120   0.0126   1.0000
  17.000   1.5112   0.05976   0.05466  -0.0123   0.0123   1.0000
  17.250   1.5003   0.06416   0.05918  -0.0129   0.0120   1.0000
  17.500   1.4937   0.06814   0.06326  -0.0136   0.0119   1.0000
  17.750   1.4873   0.07219   0.06742  -0.0144   0.0118   1.0000
  18.000   1.4789   0.07658   0.07191  -0.0155   0.0116   1.0000
  18.250   1.4678   0.08142   0.07687  -0.0167   0.0114   1.0000
  18.500   1.4573   0.08628   0.08183  -0.0180   0.0112   1.0000
  18.750   1.4462   0.09129   0.08694  -0.0195   0.0111   1.0000
  19.000   1.4310   0.09696   0.09273  -0.0213   0.0110   1.0000
  19.250   1.4198   0.10207   0.09792  -0.0230   0.0108   1.0000
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