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GOE 612 AIRFOIL (goe612-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: GOE 612 AIRFOIL (goe612-il)
Reynolds number: 1,000,000
Max Cl/Cd: 100.04 at α=5.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe612-il-1000000-n5.txt
Download as CSV file: xf-goe612-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 612 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
  ------ -------- --------- --------- -------- -------- --------
 -17.000  -0.7014   0.09230   0.08977  -0.0760   1.0000   0.0239
 -16.750  -0.7425   0.08226   0.07958  -0.0820   1.0000   0.0240
 -16.500  -0.7751   0.07418   0.07139  -0.0868   1.0000   0.0240
 -16.000  -0.8261   0.05920   0.05616  -0.0980   0.9871   0.0242
 -15.750  -0.8422   0.05178   0.04860  -0.1058   0.9807   0.0243
 -15.500  -0.8528   0.04466   0.04133  -0.1142   0.9743   0.0243
 -15.250  -0.8493   0.03840   0.03491  -0.1234   0.9704   0.0244
 -15.000  -0.8364   0.03267   0.02900  -0.1333   0.9656   0.0245
 -14.750  -0.8169   0.02765   0.02378  -0.1436   0.9584   0.0246
 -14.500  -0.8090   0.02517   0.02113  -0.1466   0.9478   0.0247
 -14.250  -0.8054   0.02380   0.01963  -0.1457   0.9385   0.0247
 -14.000  -0.8046   0.02281   0.01854  -0.1430   0.9294   0.0248
 -13.750  -0.8065   0.02186   0.01749  -0.1395   0.9214   0.0249
 -13.500  -0.8003   0.02095   0.01649  -0.1371   0.9137   0.0250
 -13.250  -0.7896   0.02013   0.01559  -0.1351   0.9075   0.0253
 -13.000  -0.7749   0.01947   0.01488  -0.1336   0.9014   0.0255
 -12.750  -0.7585   0.01886   0.01420  -0.1322   0.8953   0.0257
 -12.500  -0.7409   0.01828   0.01355  -0.1309   0.8895   0.0259
 -12.250  -0.7218   0.01776   0.01296  -0.1297   0.8827   0.0260
 -12.000  -0.7022   0.01726   0.01238  -0.1286   0.8757   0.0262
 -11.750  -0.6816   0.01677   0.01184  -0.1276   0.8686   0.0264
 -11.500  -0.6606   0.01632   0.01131  -0.1266   0.8608   0.0266
 -11.250  -0.6389   0.01589   0.01081  -0.1256   0.8534   0.0268
 -11.000  -0.6170   0.01547   0.01031  -0.1247   0.8443   0.0270
 -10.750  -0.5946   0.01508   0.00984  -0.1239   0.8349   0.0272
 -10.500  -0.5722   0.01471   0.00938  -0.1229   0.8237   0.0275
 -10.250  -0.5491   0.01435   0.00895  -0.1221   0.8117   0.0277
 -10.000  -0.5260   0.01403   0.00853  -0.1213   0.7997   0.0279
  -9.750  -0.5027   0.01373   0.00813  -0.1204   0.7877   0.0281
  -9.500  -0.4788   0.01344   0.00776  -0.1197   0.7759   0.0283
  -9.250  -0.4546   0.01317   0.00740  -0.1190   0.7654   0.0284
  -8.750  -0.4064   0.01258   0.00666  -0.1175   0.7452   0.0290
  -8.500  -0.3824   0.01229   0.00630  -0.1168   0.7361   0.0294
  -8.250  -0.3572   0.01202   0.00599  -0.1162   0.7286   0.0298
  -8.000  -0.3319   0.01179   0.00570  -0.1157   0.7215   0.0302
  -7.750  -0.3062   0.01158   0.00544  -0.1152   0.7156   0.0305
  -7.500  -0.2801   0.01136   0.00519  -0.1147   0.7097   0.0309
  -7.250  -0.2542   0.01117   0.00494  -0.1142   0.7037   0.0313
  -7.000  -0.2281   0.01099   0.00471  -0.1138   0.6984   0.0317
  -6.750  -0.2015   0.01080   0.00449  -0.1134   0.6931   0.0321
  -6.500  -0.1749   0.01063   0.00428  -0.1130   0.6881   0.0325
  -6.250  -0.1485   0.01049   0.00409  -0.1126   0.6834   0.0328
  -6.000  -0.1218   0.01029   0.00387  -0.1122   0.6794   0.0334
  -5.750  -0.0950   0.01011   0.00367  -0.1119   0.6748   0.0341
  -5.500  -0.0684   0.00996   0.00350  -0.1115   0.6693   0.0349
  -5.250  -0.0419   0.00985   0.00335  -0.1111   0.6638   0.0358
  -5.000  -0.0146   0.00972   0.00320  -0.1108   0.6582   0.0367
  -4.750   0.0124   0.00961   0.00306  -0.1105   0.6523   0.0376
  -4.250   0.0662   0.00937   0.00279  -0.1098   0.6428   0.0407
  -4.000   0.0935   0.00926   0.00267  -0.1095   0.6375   0.0423
  -3.750   0.1202   0.00917   0.00255  -0.1091   0.6316   0.0445
  -3.500   0.1471   0.00908   0.00245  -0.1088   0.6271   0.0474
  -3.250   0.1746   0.00897   0.00235  -0.1085   0.6224   0.0508
  -3.000   0.2015   0.00888   0.00226  -0.1082   0.6164   0.0552
  -2.750   0.2278   0.00880   0.00217  -0.1077   0.6104   0.0622
  -2.500   0.2547   0.00864   0.00209  -0.1074   0.6057   0.0780
  -2.250   0.2815   0.00854   0.00203  -0.1071   0.5997   0.0929
  -2.000   0.3079   0.00851   0.00199  -0.1066   0.5928   0.1013
  -1.750   0.3352   0.00845   0.00194  -0.1064   0.5866   0.1081
  -1.500   0.3620   0.00842   0.00191  -0.1060   0.5799   0.1143
  -1.250   0.3886   0.00839   0.00188  -0.1056   0.5746   0.1216
  -0.750   0.4421   0.00827   0.00183  -0.1049   0.5626   0.1489
  -0.500   0.4678   0.00818   0.00181  -0.1044   0.5556   0.1782
  -0.250   0.4934   0.00808   0.00181  -0.1038   0.5470   0.2150
   0.000   0.5187   0.00804   0.00183  -0.1033   0.5386   0.2442
   0.250   0.5445   0.00802   0.00185  -0.1027   0.5292   0.2689
   0.500   0.5700   0.00805   0.00188  -0.1021   0.5190   0.2867
   0.750   0.5946   0.00812   0.00193  -0.1014   0.5048   0.3004
   1.000   0.6186   0.00821   0.00198  -0.1005   0.4870   0.3128
   1.250   0.6415   0.00837   0.00206  -0.0995   0.4644   0.3247
   1.500   0.6630   0.00857   0.00218  -0.0982   0.4395   0.3371
   1.750   0.6838   0.00880   0.00231  -0.0967   0.4112   0.3496
   2.000   0.7037   0.00907   0.00247  -0.0952   0.3833   0.3638
   2.250   0.7245   0.00928   0.00262  -0.0938   0.3626   0.3800
   2.500   0.7460   0.00945   0.00276  -0.0925   0.3479   0.3978
   2.750   0.7673   0.00961   0.00290  -0.0912   0.3355   0.4147
   3.000   0.7892   0.00974   0.00303  -0.0900   0.3253   0.4323
   3.250   0.8101   0.00988   0.00317  -0.0886   0.3159   0.4524
   3.500   0.8298   0.00999   0.00330  -0.0869   0.3073   0.4731
   3.750   0.8482   0.01010   0.00343  -0.0850   0.2991   0.4962
   4.000   0.8672   0.01018   0.00357  -0.0833   0.2920   0.5315
   4.250   0.8815   0.01014   0.00378  -0.0806   0.2847   0.6363
   4.750   1.0117   0.01015   0.00448  -0.0971   0.2701   1.0000
   5.000   1.0290   0.01032   0.00462  -0.0950   0.2655   1.0000
   5.250   1.0474   0.01047   0.00477  -0.0931   0.2614   1.0000
   5.500   1.0656   0.01066   0.00493  -0.0912   0.2571   1.0000
   5.750   1.0833   0.01088   0.00512  -0.0893   0.2524   1.0000
   6.000   1.1026   0.01108   0.00531  -0.0877   0.2488   1.0000
   6.250   1.1224   0.01127   0.00550  -0.0862   0.2450   1.0000
   6.500   1.1417   0.01151   0.00571  -0.0847   0.2404   1.0000
   6.750   1.1600   0.01179   0.00597  -0.0831   0.2354   1.0000
   7.000   1.1800   0.01203   0.00621  -0.0817   0.2317   1.0000
   7.250   1.1997   0.01229   0.00646  -0.0804   0.2273   1.0000
   7.500   1.2183   0.01260   0.00675  -0.0789   0.2220   1.0000
   7.750   1.2369   0.01293   0.00706  -0.0775   0.2171   1.0000
   8.000   1.2560   0.01325   0.00737  -0.0762   0.2119   1.0000
   8.250   1.2736   0.01365   0.00774  -0.0747   0.2056   1.0000
   8.500   1.2918   0.01404   0.00811  -0.0734   0.2001   1.0000
   8.750   1.3096   0.01445   0.00851  -0.0720   0.1939   1.0000
   9.000   1.3262   0.01494   0.00897  -0.0705   0.1878   1.0000
   9.250   1.3440   0.01538   0.00940  -0.0692   0.1825   1.0000
   9.500   1.3601   0.01592   0.00992  -0.0677   0.1763   1.0000
   9.750   1.3764   0.01645   0.01044  -0.0663   0.1708   1.0000
  10.000   1.3910   0.01710   0.01106  -0.0647   0.1629   1.0000
  10.250   1.4055   0.01778   0.01171  -0.0632   0.1557   1.0000
  10.500   1.4189   0.01853   0.01242  -0.0616   0.1483   1.0000
  10.750   1.4330   0.01926   0.01314  -0.0602   0.1420   1.0000
  11.000   1.4478   0.01997   0.01385  -0.0589   0.1377   1.0000
  11.250   1.4614   0.02078   0.01465  -0.0575   0.1336   1.0000
  11.500   1.4765   0.02150   0.01539  -0.0563   0.1302   1.0000
  11.750   1.4907   0.02230   0.01620  -0.0551   0.1269   1.0000
  12.000   1.5031   0.02323   0.01712  -0.0538   0.1227   1.0000
  12.250   1.5159   0.02416   0.01807  -0.0526   0.1192   1.0000
  12.500   1.5301   0.02501   0.01894  -0.0516   0.1170   1.0000
  12.750   1.5420   0.02604   0.01998  -0.0504   0.1136   1.0000
  13.000   1.5539   0.02710   0.02105  -0.0493   0.1110   1.0000
  13.250   1.5652   0.02823   0.02220  -0.0482   0.1080   1.0000
  13.500   1.5780   0.02926   0.02327  -0.0473   0.1061   1.0000
  13.750   1.5899   0.03037   0.02442  -0.0463   0.1037   1.0000
  14.000   1.5999   0.03167   0.02573  -0.0453   0.1010   1.0000
  14.250   1.6088   0.03307   0.02714  -0.0443   0.0979   1.0000
  14.500   1.6194   0.03436   0.02848  -0.0435   0.0960   1.0000
  14.750   1.6293   0.03572   0.02987  -0.0426   0.0926   1.0000
  15.000   1.6338   0.03755   0.03168  -0.0416   0.0870   1.0000
  15.250   1.6425   0.03907   0.03324  -0.0408   0.0848   1.0000
  15.500   1.6490   0.04080   0.03498  -0.0400   0.0800   1.0000
  15.750   1.6476   0.04327   0.03742  -0.0389   0.0708   1.0000
  16.250   1.6084   0.05206   0.04603  -0.0362   0.0382   1.0000
  16.500   1.5874   0.05692   0.05087  -0.0353   0.0257   1.0000
  16.750   1.5743   0.06112   0.05509  -0.0348   0.0191   1.0000
  17.000   1.5694   0.06451   0.05854  -0.0346   0.0170   1.0000
  17.250   1.5656   0.06782   0.06191  -0.0345   0.0156   1.0000
  17.500   1.5615   0.07124   0.06540  -0.0346   0.0146   1.0000
  17.750   1.5571   0.07476   0.06899  -0.0348   0.0137   1.0000
  18.000   1.5532   0.07830   0.07261  -0.0351   0.0133   1.0000
  18.250   1.5469   0.08216   0.07655  -0.0355   0.0129   1.0000
  18.500   1.5396   0.08625   0.08072  -0.0360   0.0125   1.0000
  18.750   1.5317   0.09047   0.08504  -0.0367   0.0122   1.0000
  19.000   1.5245   0.09468   0.08934  -0.0375   0.0119   1.0000
  19.250   1.5163   0.09904   0.09379  -0.0385   0.0117   1.0000
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