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GOE 769 AIRFOIL (goe769-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: GOE 769 AIRFOIL (goe769-il)
Reynolds number: 1,000,000
Max Cl/Cd: 105.95 at α=8.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe769-il-1000000-n5.txt
Download as CSV file: xf-goe769-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 769 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
  ------ -------- --------- --------- -------- -------- --------
 -13.500  -0.9447   0.03339   0.03020  -0.0816   1.0000   0.0220
 -13.250  -0.9455   0.03065   0.02729  -0.0811   1.0000   0.0220
 -13.000  -0.9389   0.02874   0.02524  -0.0801   1.0000   0.0220
 -12.750  -0.9291   0.02714   0.02352  -0.0788   1.0000   0.0221
 -12.500  -0.9166   0.02580   0.02207  -0.0775   1.0000   0.0221
 -12.250  -0.8958   0.02449   0.02064  -0.0775   0.9965   0.0222
 -12.000  -0.8690   0.02329   0.01933  -0.0784   0.9841   0.0223
 -11.750  -0.8299   0.02204   0.01796  -0.0816   0.9684   0.0223
 -11.500  -0.7819   0.02051   0.01622  -0.0868   0.9206   0.0225
 -11.250  -0.7633   0.01983   0.01519  -0.0853   0.8404   0.0226
 -11.000  -0.7452   0.01921   0.01433  -0.0837   0.7902   0.0227
 -10.750  -0.7245   0.01864   0.01358  -0.0825   0.7572   0.0228
 -10.500  -0.7024   0.01810   0.01289  -0.0815   0.7321   0.0229
 -10.250  -0.6794   0.01757   0.01224  -0.0806   0.7123   0.0230
 -10.000  -0.6556   0.01709   0.01165  -0.0798   0.6951   0.0232
  -9.750  -0.6311   0.01664   0.01110  -0.0790   0.6800   0.0233
  -9.500  -0.6064   0.01621   0.01057  -0.0783   0.6670   0.0234
  -9.250  -0.5813   0.01580   0.01007  -0.0776   0.6543   0.0236
  -9.000  -0.5559   0.01539   0.00958  -0.0770   0.6446   0.0237
  -8.750  -0.5302   0.01502   0.00912  -0.0763   0.6346   0.0239
  -8.500  -0.5043   0.01464   0.00867  -0.0757   0.6266   0.0240
  -8.250  -0.4780   0.01429   0.00825  -0.0751   0.6178   0.0242
  -8.000  -0.4517   0.01398   0.00787  -0.0745   0.6093   0.0244
  -7.750  -0.4250   0.01366   0.00749  -0.0740   0.6021   0.0246
  -7.500  -0.3982   0.01336   0.00712  -0.0734   0.5944   0.0248
  -7.250  -0.3714   0.01307   0.00676  -0.0729   0.5875   0.0250
  -7.000  -0.3444   0.01278   0.00642  -0.0724   0.5798   0.0252
  -6.750  -0.3174   0.01253   0.00609  -0.0718   0.5707   0.0253
  -6.500  -0.2901   0.01227   0.00578  -0.0713   0.5626   0.0254
  -6.250  -0.2628   0.01206   0.00550  -0.0708   0.5531   0.0256
  -6.000  -0.2358   0.01175   0.00515  -0.0703   0.5450   0.0258
  -5.750  -0.2086   0.01148   0.00483  -0.0698   0.5353   0.0261
  -5.500  -0.1813   0.01126   0.00456  -0.0693   0.5260   0.0264
  -5.250  -0.1538   0.01108   0.00433  -0.0689   0.5145   0.0267
  -5.000  -0.1262   0.01092   0.00411  -0.0684   0.5024   0.0270
  -4.750  -0.0987   0.01079   0.00391  -0.0679   0.4880   0.0273
  -4.500  -0.0713   0.01068   0.00373  -0.0674   0.4721   0.0277
  -4.250  -0.0439   0.01059   0.00356  -0.0670   0.4549   0.0280
  -4.000  -0.0164   0.01051   0.00339  -0.0665   0.4386   0.0284
  -3.750   0.0113   0.01043   0.00325  -0.0660   0.4253   0.0288
  -3.500   0.0390   0.01036   0.00312  -0.0656   0.4146   0.0291
  -3.250   0.0668   0.01022   0.00296  -0.0652   0.4063   0.0297
  -3.000   0.0945   0.01014   0.00284  -0.0648   0.3968   0.0303
  -2.750   0.1226   0.01006   0.00273  -0.0644   0.3889   0.0311
  -2.500   0.1504   0.01002   0.00264  -0.0640   0.3798   0.0319
  -2.250   0.1785   0.00995   0.00255  -0.0636   0.3736   0.0328
  -2.000   0.2064   0.00988   0.00246  -0.0632   0.3658   0.0339
  -1.750   0.2342   0.00984   0.00240  -0.0628   0.3584   0.0354
  -1.500   0.2623   0.00980   0.00233  -0.0625   0.3516   0.0371
  -1.250   0.2901   0.00976   0.00228  -0.0621   0.3447   0.0398
  -1.000   0.3181   0.00972   0.00224  -0.0617   0.3391   0.0437
  -0.750   0.3460   0.00968   0.00221  -0.0614   0.3326   0.0493
  -0.500   0.3737   0.00968   0.00219  -0.0610   0.3252   0.0561
  -0.250   0.4016   0.00965   0.00218  -0.0607   0.3195   0.0641
   0.000   0.4296   0.00964   0.00219  -0.0603   0.3137   0.0719
   0.250   0.4573   0.00967   0.00220  -0.0600   0.3072   0.0789
   0.500   0.4853   0.00968   0.00222  -0.0597   0.3016   0.0852
   0.750   0.5130   0.00971   0.00225  -0.0593   0.2939   0.0916
   1.000   0.5406   0.00977   0.00228  -0.0589   0.2872   0.0975
   1.250   0.5685   0.00980   0.00232  -0.0586   0.2808   0.1041
   1.500   0.5958   0.00986   0.00237  -0.0582   0.2731   0.1139
   1.750   0.6233   0.00989   0.00242  -0.0579   0.2661   0.1251
   2.000   0.6504   0.00998   0.00249  -0.0575   0.2569   0.1375
   2.250   0.6776   0.01003   0.00256  -0.0571   0.2492   0.1556
   2.500   0.7043   0.01009   0.00264  -0.0567   0.2414   0.1832
   2.750   0.7311   0.01008   0.00274  -0.0563   0.2357   0.2354
   3.000   0.7574   0.01010   0.00286  -0.0558   0.2289   0.2892
   3.250   0.7835   0.01009   0.00298  -0.0553   0.2232   0.3572
   3.500   0.8069   0.00973   0.00313  -0.0545   0.2188   0.5708
   4.000   0.8948   0.00922   0.00351  -0.0610   0.2082   1.0000
   4.250   0.9203   0.00936   0.00362  -0.0603   0.2049   1.0000
   4.500   0.9455   0.00953   0.00375  -0.0596   0.2012   1.0000
   4.750   0.9706   0.00972   0.00389  -0.0588   0.1978   1.0000
   5.000   0.9958   0.00990   0.00404  -0.0581   0.1946   1.0000
   5.250   1.0214   0.01004   0.00417  -0.0575   0.1923   1.0000
   5.500   1.0468   0.01021   0.00431  -0.0568   0.1895   1.0000
   5.750   1.0719   0.01040   0.00447  -0.0561   0.1863   1.0000
   6.000   1.0968   0.01060   0.00464  -0.0554   0.1834   1.0000
   6.250   1.1217   0.01081   0.00482  -0.0548   0.1806   1.0000
   6.500   1.1472   0.01097   0.00498  -0.0542   0.1789   1.0000
   6.750   1.1723   0.01115   0.00515  -0.0536   0.1765   1.0000
   7.000   1.1971   0.01135   0.00534  -0.0529   0.1738   1.0000
   7.250   1.2215   0.01158   0.00554  -0.0522   0.1710   1.0000
   7.500   1.2457   0.01183   0.00576  -0.0515   0.1683   1.0000
   7.750   1.2704   0.01203   0.00597  -0.0508   0.1665   1.0000
   8.000   1.2949   0.01223   0.00617  -0.0502   0.1649   1.0000
   8.250   1.3191   0.01245   0.00638  -0.0495   0.1627   1.0000
   8.500   1.3429   0.01269   0.00662  -0.0488   0.1604   1.0000
   8.750   1.3660   0.01296   0.00687  -0.0480   0.1578   1.0000
   9.000   1.3886   0.01325   0.00715  -0.0471   0.1551   1.0000
   9.250   1.4120   0.01348   0.00739  -0.0463   0.1538   1.0000
   9.500   1.4350   0.01372   0.00765  -0.0455   0.1522   1.0000
   9.750   1.4575   0.01398   0.00792  -0.0446   0.1504   1.0000
  10.000   1.4792   0.01427   0.00821  -0.0437   0.1485   1.0000
  10.250   1.5001   0.01459   0.00852  -0.0426   0.1463   1.0000
  10.500   1.5200   0.01494   0.00887  -0.0414   0.1441   1.0000
  10.750   1.5401   0.01525   0.00920  -0.0402   0.1424   1.0000
  11.000   1.5598   0.01555   0.00952  -0.0390   0.1410   1.0000
  11.250   1.5768   0.01586   0.00986  -0.0373   0.1395   1.0000
  11.500   1.5923   0.01621   0.01023  -0.0353   0.1379   1.0000
  11.750   1.6071   0.01661   0.01064  -0.0334   0.1363   1.0000
  12.000   1.6211   0.01706   0.01111  -0.0315   0.1347   1.0000
  12.250   1.6344   0.01758   0.01164  -0.0296   0.1329   1.0000
  12.500   1.6482   0.01810   0.01219  -0.0278   0.1315   1.0000
  12.750   1.6627   0.01862   0.01276  -0.0263   0.1303   1.0000
  13.000   1.6765   0.01921   0.01339  -0.0249   0.1292   1.0000
  13.250   1.6893   0.01990   0.01411  -0.0234   0.1276   1.0000
  13.500   1.7009   0.02072   0.01495  -0.0221   0.1258   1.0000
  13.750   1.7114   0.02167   0.01593  -0.0208   0.1241   1.0000
  14.000   1.7211   0.02277   0.01706  -0.0197   0.1224   1.0000
  14.250   1.7314   0.02390   0.01824  -0.0189   0.1208   1.0000
  14.500   1.7427   0.02503   0.01942  -0.0182   0.1194   1.0000
  14.750   1.7528   0.02633   0.02077  -0.0176   0.1181   1.0000
  15.000   1.7612   0.02783   0.02231  -0.0172   0.1163   1.0000
  15.250   1.7683   0.02951   0.02404  -0.0168   0.1148   1.0000
  15.500   1.7736   0.03142   0.02600  -0.0166   0.1133   1.0000
  15.750   1.7767   0.03358   0.02821  -0.0164   0.1115   1.0000
  16.000   1.7830   0.03547   0.03017  -0.0163   0.1108   1.0000
  16.250   1.7876   0.03752   0.03229  -0.0163   0.1096   1.0000
  16.500   1.7903   0.03978   0.03462  -0.0162   0.1085   1.0000
  16.750   1.7908   0.04228   0.03718  -0.0163   0.1073   1.0000
  17.000   1.7890   0.04504   0.04000  -0.0164   0.1061   1.0000
  17.250   1.7850   0.04809   0.04311  -0.0166   0.1049   1.0000
  17.500   1.7789   0.05146   0.04655  -0.0170   0.1036   1.0000
  17.750   1.7713   0.05506   0.05023  -0.0175   0.1025   1.0000
  18.000   1.7683   0.05821   0.05345  -0.0180   0.1013   1.0000
  18.250   1.7639   0.06155   0.05688  -0.0186   0.1006   1.0000
  18.500   1.7570   0.06523   0.06063  -0.0193   0.0992   1.0000
  18.750   1.7488   0.06913   0.06461  -0.0201   0.0982   1.0000
  19.000   1.7378   0.07344   0.06900  -0.0212   0.0970   1.0000
  19.250   1.7249   0.07803   0.07366  -0.0223   0.0958   1.0000
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