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GOE 12K AIRFOIL (goe12k-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: GOE 12K AIRFOIL (goe12k-il)
Reynolds number: 1,000,000
Max Cl/Cd: 146.69 at α=2.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe12k-il-1000000.txt
Download as CSV file: xf-goe12k-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 12K 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
  ------ -------- --------- --------- -------- -------- --------
 -15.500  -0.9180   0.03786   0.03514  -0.1439   0.9786   0.0153
 -15.250  -0.9273   0.03288   0.02991  -0.1483   0.9765   0.0155
 -15.000  -0.9415   0.03015   0.02700  -0.1456   0.9688   0.0156
 -14.750  -0.9372   0.02797   0.02468  -0.1450   0.9663   0.0160
 -14.500  -0.9395   0.02673   0.02334  -0.1412   0.9595   0.0164
 -14.250  -0.9263   0.02536   0.02185  -0.1403   0.9566   0.0168
 -14.000  -0.9099   0.02389   0.02023  -0.1400   0.9549   0.0173
 -13.750  -0.8891   0.02277   0.01898  -0.1400   0.9539   0.0179
 -13.500  -0.8827   0.02194   0.01802  -0.1367   0.9478   0.0182
 -13.250  -0.8688   0.02056   0.01650  -0.1355   0.9454   0.0189
 -13.000  -0.8485   0.01954   0.01541  -0.1351   0.9440   0.0197
 -12.750  -0.8238   0.01875   0.01454  -0.1354   0.9430   0.0204
 -12.500  -0.7973   0.01800   0.01368  -0.1359   0.9423   0.0212
 -12.250  -0.7693   0.01731   0.01285  -0.1368   0.9416   0.0219
 -12.000  -0.7552   0.01661   0.01210  -0.1346   0.9376   0.0230
 -11.750  -0.7304   0.01618   0.01164  -0.1345   0.9356   0.0242
 -11.500  -0.7035   0.01575   0.01114  -0.1348   0.9342   0.0252
 -11.250  -0.6741   0.01535   0.01065  -0.1356   0.9331   0.0263
 -11.000  -0.6438   0.01498   0.01029  -0.1367   0.9321   0.0279
 -10.750  -0.6101   0.01488   0.01018  -0.1382   0.9314   0.0291
 -10.500  -0.5759   0.01470   0.00994  -0.1399   0.9307   0.0304
 -10.250  -0.5425   0.01431   0.00947  -0.1416   0.9298   0.0315
 -10.000  -0.5067   0.01430   0.00950  -0.1436   0.9291   0.0328
  -9.750  -0.4776   0.01432   0.00951  -0.1441   0.9274   0.0337
  -9.500  -0.4550   0.01435   0.00952  -0.1431   0.9252   0.0346
  -9.250  -0.4287   0.01426   0.00937  -0.1430   0.9231   0.0355
  -9.000  -0.3997   0.01418   0.00922  -0.1435   0.9211   0.0363
  -8.750  -0.3705   0.01358   0.00852  -0.1443   0.9193   0.0375
  -8.500  -0.3352   0.01354   0.00850  -0.1463   0.9179   0.0385
  -8.250  -0.2983   0.01351   0.00846  -0.1486   0.9167   0.0394
  -8.000  -0.2611   0.01345   0.00837  -0.1510   0.9157   0.0405
  -7.750  -0.2242   0.01332   0.00818  -0.1533   0.9147   0.0417
  -7.500  -0.2124   0.01322   0.00804  -0.1499   0.9121   0.0423
  -7.250  -0.1924   0.01319   0.00797  -0.1482   0.9099   0.0429
  -7.000  -0.1683   0.01275   0.00744  -0.1477   0.9080   0.0438
  -6.750  -0.1420   0.01206   0.00673  -0.1478   0.9063   0.0451
  -6.500  -0.1135   0.01185   0.00651  -0.1483   0.9048   0.0460
  -6.250  -0.0842   0.01165   0.00629  -0.1488   0.9035   0.0469
  -6.000  -0.0527   0.01143   0.00603  -0.1499   0.9022   0.0479
  -5.750  -0.0200   0.01121   0.00578  -0.1512   0.9009   0.0489
  -5.500   0.0110   0.01100   0.00553  -0.1521   0.8995   0.0497
  -5.250   0.0210   0.01083   0.00535  -0.1481   0.8972   0.0502
  -5.000   0.0385   0.01068   0.00518  -0.1459   0.8948   0.0507
  -4.750   0.0616   0.01055   0.00502  -0.1449   0.8928   0.0511
  -4.500   0.0882   0.01031   0.00475  -0.1448   0.8907   0.0518
  -4.250   0.1141   0.00965   0.00405  -0.1446   0.8888   0.0533
  -4.000   0.1440   0.00938   0.00377  -0.1452   0.8868   0.0543
  -3.750   0.1776   0.00921   0.00358  -0.1467   0.8846   0.0551
  -3.500   0.1885   0.00910   0.00349  -0.1429   0.8820   0.0559
  -3.250   0.2026   0.00898   0.00336  -0.1398   0.8791   0.0566
  -3.000   0.2241   0.00884   0.00322  -0.1383   0.8767   0.0574
  -2.750   0.2500   0.00869   0.00306  -0.1380   0.8746   0.0584
  -2.500   0.2787   0.00855   0.00291  -0.1382   0.8727   0.0594
  -2.250   0.3096   0.00843   0.00277  -0.1390   0.8707   0.0602
  -2.000   0.3417   0.00837   0.00270  -0.1401   0.8685   0.0610
  -1.750   0.3488   0.00830   0.00265  -0.1352   0.8655   0.0614
  -1.500   0.3637   0.00815   0.00249  -0.1322   0.8624   0.0630
  -1.250   0.3864   0.00801   0.00235  -0.1311   0.8598   0.0655
  -1.000   0.4139   0.00790   0.00225  -0.1310   0.8576   0.0682
  -0.750   0.4437   0.00781   0.00217  -0.1315   0.8556   0.0704
  -0.500   0.4771   0.00776   0.00212  -0.1329   0.8537   0.0740
  -0.250   0.4842   0.00766   0.00210  -0.1280   0.8503   0.0840
   0.000   0.4918   0.00747   0.00207  -0.1234   0.8465   0.1335
   0.250   0.5110   0.00722   0.00202  -0.1214   0.8433   0.1991
   0.500   0.5316   0.00678   0.00200  -0.1201   0.8405   0.3583
   0.750   0.5468   0.00619   0.00205  -0.1175   0.8370   0.5885
   1.000   0.5360   0.00582   0.00214  -0.1085   0.8321   0.7358
   1.250   0.7307   0.00582   0.00276  -0.1472   0.8299   0.9658
   1.500   0.7545   0.00590   0.00281  -0.1459   0.8196   0.9797
   1.750   0.7920   0.00596   0.00284  -0.1479   0.8046   0.9880
   2.000   0.8362   0.00604   0.00286  -0.1516   0.7867   0.9947
   2.250   0.8752   0.00603   0.00279  -0.1542   0.7696   0.9983
   2.500   0.8963   0.00611   0.00277  -0.1527   0.7458   1.0000
   2.750   0.8990   0.00627   0.00283  -0.1470   0.7229   1.0000
   3.000   0.9011   0.00648   0.00292  -0.1412   0.6967   1.0000
   3.250   0.8928   0.00686   0.00310  -0.1331   0.6481   1.0000
   3.500   0.8583   0.00780   0.00356  -0.1193   0.5428   1.0000
   3.750   0.8389   0.00879   0.00411  -0.1093   0.4548   1.0000
   4.000   0.8481   0.00918   0.00437  -0.1054   0.4258   1.0000
   4.250   0.8584   0.00956   0.00464  -0.1018   0.3979   1.0000
   4.500   0.8702   0.00991   0.00489  -0.0986   0.3729   1.0000
   4.750   0.8827   0.01027   0.00514  -0.0955   0.3437   1.0000
   5.000   0.8911   0.01081   0.00546  -0.0917   0.2954   1.0000
   5.250   0.8943   0.01157   0.00591  -0.0870   0.2328   1.0000
   5.500   0.9001   0.01235   0.00639  -0.0829   0.1740   1.0000
   5.750   0.9096   0.01303   0.00683  -0.0795   0.1274   1.0000
   6.000   0.9229   0.01357   0.00721  -0.0769   0.0997   1.0000
   6.250   0.9394   0.01397   0.00754  -0.0749   0.0867   1.0000
   6.500   0.9571   0.01432   0.00786  -0.0731   0.0790   1.0000
   6.750   0.9744   0.01470   0.00820  -0.0713   0.0733   1.0000
   7.000   0.9922   0.01506   0.00855  -0.0695   0.0690   1.0000
   7.250   1.0113   0.01535   0.00886  -0.0680   0.0669   1.0000
   7.500   1.0298   0.01568   0.00920  -0.0665   0.0647   1.0000
   7.750   1.0472   0.01609   0.00958  -0.0647   0.0609   1.0000
   8.000   1.0642   0.01651   0.01002  -0.0630   0.0583   1.0000
   8.250   1.0835   0.01681   0.01035  -0.0616   0.0570   1.0000
   8.500   1.1024   0.01713   0.01068  -0.0602   0.0549   1.0000
   8.750   1.1203   0.01752   0.01107  -0.0587   0.0526   1.0000
   9.000   1.1359   0.01805   0.01158  -0.0568   0.0488   1.0000
   9.250   1.1553   0.01836   0.01192  -0.0555   0.0477   1.0000
   9.500   1.1741   0.01869   0.01227  -0.0542   0.0453   1.0000
   9.750   1.1911   0.01914   0.01270  -0.0527   0.0424   1.0000
  10.000   1.2081   0.01960   0.01317  -0.0511   0.0399   1.0000
  10.250   1.2258   0.02001   0.01360  -0.0496   0.0373   1.0000
  10.500   1.2417   0.02056   0.01412  -0.0479   0.0341   1.0000
  10.750   1.2586   0.02102   0.01461  -0.0464   0.0319   1.0000
  11.000   1.2739   0.02160   0.01516  -0.0448   0.0293   1.0000
  11.250   1.2886   0.02223   0.01581  -0.0429   0.0272   1.0000
  11.500   1.3041   0.02279   0.01640  -0.0413   0.0257   1.0000
  11.750   1.3178   0.02349   0.01711  -0.0394   0.0241   1.0000
  12.000   1.3311   0.02421   0.01786  -0.0376   0.0228   1.0000
  12.250   1.3455   0.02487   0.01857  -0.0358   0.0218   1.0000
  12.500   1.3594   0.02556   0.01929  -0.0341   0.0208   1.0000
  12.750   1.3708   0.02643   0.02019  -0.0321   0.0198   1.0000
  13.000   1.3805   0.02742   0.02123  -0.0299   0.0189   1.0000
  13.250   1.3942   0.02813   0.02200  -0.0283   0.0182   1.0000
  13.500   1.4060   0.02898   0.02291  -0.0265   0.0177   1.0000
  13.750   1.4175   0.02986   0.02385  -0.0247   0.0172   1.0000
  14.000   1.4277   0.03086   0.02488  -0.0228   0.0165   1.0000
  14.250   1.4337   0.03217   0.02625  -0.0205   0.0159   1.0000
  14.500   1.4387   0.03357   0.02773  -0.0182   0.0154   1.0000
  14.750   1.4492   0.03458   0.02881  -0.0165   0.0151   1.0000
  15.000   1.4596   0.03561   0.02991  -0.0149   0.0147   1.0000
  15.250   1.4659   0.03697   0.03136  -0.0130   0.0145   1.0000
  15.500   1.4758   0.03808   0.03252  -0.0115   0.0139   1.0000
  15.750   1.4818   0.03950   0.03401  -0.0097   0.0137   1.0000
  16.000   1.4878   0.04098   0.03554  -0.0080   0.0133   1.0000
  16.250   1.4888   0.04291   0.03755  -0.0061   0.0130   1.0000
  16.500   1.4848   0.04537   0.04011  -0.0040   0.0127   1.0000
  16.750   1.4799   0.04799   0.04284  -0.0020   0.0125   1.0000
  17.000   1.4878   0.04946   0.04439  -0.0010   0.0122   1.0000
  17.250   1.4893   0.05161   0.04664   0.0003   0.0121   1.0000
  17.500   1.4909   0.05380   0.04894   0.0014   0.0119   1.0000
  17.750   1.4884   0.05650   0.05174   0.0025   0.0118   1.0000
  18.000   1.4877   0.05909   0.05444   0.0033   0.0116   1.0000
  18.250   1.4842   0.06206   0.05751   0.0040   0.0114   1.0000
  18.500   1.4838   0.06478   0.06032   0.0044   0.0112   1.0000
  18.750   1.4769   0.06843   0.06408   0.0046   0.0110   1.0000
  19.000   1.4694   0.07229   0.06804   0.0044   0.0109   1.0000
  19.250   1.4599   0.07661   0.07249   0.0039   0.0109   1.0000
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