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GOE 626 AIRFOIL (goe626-il) Xfoil prediction polar at RE=100,000 Ncrit=5


Details Polar file
Airfoil: GOE 626 AIRFOIL (goe626-il)
Reynolds number: 100,000
Max Cl/Cd: 51.59 at α=8°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe626-il-100000-n5.txt
Download as CSV file: xf-goe626-il-100000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 626 AIRFOIL                                 
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.100 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -12.750  -0.4087   0.10621   0.10035  -0.0549   1.0000   0.0561
 -12.500  -0.5244   0.08243   0.07626  -0.0660   1.0000   0.0568
 -12.250  -0.5445   0.07750   0.07126  -0.0671   1.0000   0.0571
 -12.000  -0.5601   0.07372   0.06742  -0.0673   1.0000   0.0577
 -11.750  -0.5738   0.07066   0.06432  -0.0668   1.0000   0.0582
 -11.500  -0.5871   0.06804   0.06167  -0.0658   1.0000   0.0587
 -11.250  -0.5998   0.06579   0.05940  -0.0645   1.0000   0.0591
 -11.000  -0.6136   0.06369   0.05728  -0.0628   1.0000   0.0596
 -10.750  -0.6271   0.06189   0.05550  -0.0607   1.0000   0.0600
 -10.500  -0.6258   0.05996   0.05361  -0.0613   0.9975   0.0608
 -10.250  -0.6100   0.05748   0.05111  -0.0651   0.9912   0.0622
 -10.000  -0.5988   0.05489   0.04849  -0.0686   0.9834   0.0638
  -9.750  -0.5903   0.05229   0.04583  -0.0717   0.9756   0.0654
  -9.500  -0.5750   0.04927   0.04277  -0.0764   0.9685   0.0678
  -9.250  -0.5644   0.04607   0.03956  -0.0807   0.9596   0.0704
  -9.000  -0.5420   0.04249   0.03588  -0.0873   0.9535   0.0753
  -8.750  -0.5288   0.03872   0.03205  -0.0925   0.9442   0.0802
  -8.500  -0.4999   0.03444   0.02765  -0.1007   0.9387   0.0889
  -8.250  -0.4779   0.03129   0.02439  -0.1052   0.9308   0.0988
  -8.000  -0.4473   0.02890   0.02190  -0.1096   0.9250   0.1125
  -7.750  -0.4104   0.02720   0.02013  -0.1138   0.9213   0.1287
  -7.500  -0.3871   0.02626   0.01919  -0.1144   0.9127   0.1429
  -7.250  -0.3523   0.02570   0.01868  -0.1164   0.9074   0.1611
  -7.000  -0.3121   0.02541   0.01838  -0.1189   0.9039   0.1790
  -6.750  -0.2877   0.02549   0.01848  -0.1181   0.8945   0.1893
  -6.500  -0.2503   0.02541   0.01831  -0.1196   0.8892   0.2010
  -6.250  -0.2082   0.02511   0.01785  -0.1222   0.8856   0.2126
  -6.000  -0.1840   0.02500   0.01760  -0.1215   0.8747   0.2212
  -5.750  -0.1436   0.02512   0.01766  -0.1232   0.8693   0.2295
  -5.500  -0.1130   0.02459   0.01686  -0.1241   0.8602   0.2398
  -5.250  -0.0783   0.02517   0.01753  -0.1242   0.8522   0.2450
  -5.000  -0.0431   0.02461   0.01667  -0.1259   0.8445   0.2554
  -4.750  -0.0140   0.02491   0.01705  -0.1252   0.8340   0.2590
  -4.500   0.0208   0.02479   0.01686  -0.1260   0.8258   0.2648
  -4.250   0.0502   0.02423   0.01606  -0.1266   0.8143   0.2725
  -4.000   0.0805   0.02438   0.01626  -0.1262   0.8036   0.2765
  -3.750   0.1135   0.02422   0.01602  -0.1268   0.7930   0.2827
  -3.500   0.1416   0.02364   0.01518  -0.1272   0.7796   0.2894
  -3.250   0.1730   0.02341   0.01495  -0.1274   0.7681   0.2922
  -3.000   0.2039   0.02312   0.01457  -0.1276   0.7554   0.2957
  -2.750   0.2320   0.02278   0.01411  -0.1276   0.7411   0.2995
  -2.500   0.2625   0.02230   0.01342  -0.1281   0.7278   0.3038
  -2.250   0.2943   0.02185   0.01274  -0.1288   0.7150   0.3075
  -2.000   0.3236   0.02161   0.01244  -0.1288   0.7014   0.3100
  -1.750   0.3524   0.02139   0.01214  -0.1288   0.6882   0.3125
  -1.500   0.3825   0.02117   0.01179  -0.1290   0.6760   0.3155
  -1.250   0.4126   0.02097   0.01142  -0.1292   0.6641   0.3190
  -1.000   0.4410   0.02080   0.01107  -0.1293   0.6521   0.3225
  -0.750   0.4715   0.02063   0.01065  -0.1297   0.6416   0.3253
  -0.500   0.4983   0.02052   0.01051  -0.1293   0.6303   0.3274
  -0.250   0.5267   0.02048   0.01040  -0.1292   0.6203   0.3298
   0.000   0.5536   0.02046   0.01034  -0.1289   0.6100   0.3326
   0.250   0.5818   0.02046   0.01023  -0.1289   0.6008   0.3355
   0.500   0.6083   0.02045   0.01015  -0.1285   0.5908   0.3382
   0.750   0.6365   0.02046   0.01003  -0.1284   0.5820   0.3409
   1.000   0.6622   0.02050   0.00999  -0.1280   0.5722   0.3437
   1.250   0.6904   0.02052   0.00994  -0.1279   0.5644   0.3464
   1.500   0.7146   0.02057   0.01007  -0.1271   0.5552   0.3490
   1.750   0.7414   0.02063   0.01010  -0.1268   0.5473   0.3518
   2.000   0.7668   0.02072   0.01018  -0.1262   0.5388   0.3545
   2.250   0.7924   0.02080   0.01024  -0.1257   0.5306   0.3574
   2.500   0.8190   0.02090   0.01028  -0.1253   0.5234   0.3604
   2.750   0.8436   0.02103   0.01040  -0.1246   0.5148   0.3635
   3.000   0.8697   0.02111   0.01045  -0.1242   0.5075   0.3667
   3.250   0.8924   0.02123   0.01067  -0.1231   0.4982   0.3700
   3.500   0.9172   0.02134   0.01074  -0.1224   0.4902   0.3738
   3.750   0.9404   0.02151   0.01094  -0.1215   0.4818   0.3776
   4.000   0.9646   0.02166   0.01108  -0.1207   0.4744   0.3813
   4.250   0.9896   0.02184   0.01125  -0.1201   0.4682   0.3849
   4.500   1.0121   0.02203   0.01154  -0.1191   0.4607   0.3886
   4.750   1.0367   0.02221   0.01171  -0.1184   0.4539   0.3933
   5.000   1.0595   0.02245   0.01199  -0.1174   0.4465   0.3989
   5.250   1.0826   0.02269   0.01227  -0.1165   0.4396   0.4046
   5.500   1.1072   0.02290   0.01247  -0.1158   0.4333   0.4110
   5.750   1.1272   0.02318   0.01287  -0.1145   0.4251   0.4181
   6.000   1.1497   0.02341   0.01312  -0.1134   0.4179   0.4256
   6.250   1.1712   0.02370   0.01350  -0.1123   0.4113   0.4343
   6.500   1.1920   0.02401   0.01391  -0.1111   0.4046   0.4445
   6.750   1.2146   0.02427   0.01420  -0.1102   0.3985   0.4586
   7.000   1.2332   0.02459   0.01470  -0.1087   0.3912   0.4767
   7.250   1.2516   0.02486   0.01511  -0.1071   0.3835   0.5034
   7.500   1.2703   0.02508   0.01552  -0.1056   0.3761   0.5522
   8.000   1.2975   0.02515   0.01622  -0.1006   0.3606   1.0000
   8.250   1.3087   0.02568   0.01685  -0.0980   0.3517   1.0000
   8.500   1.3223   0.02617   0.01726  -0.0957   0.3435   1.0000
   8.750   1.3335   0.02678   0.01795  -0.0933   0.3347   1.0000
   9.000   1.3453   0.02737   0.01851  -0.0910   0.3264   1.0000
   9.250   1.3560   0.02807   0.01928  -0.0887   0.3176   1.0000
   9.500   1.3659   0.02879   0.01999  -0.0863   0.3090   1.0000
   9.750   1.3744   0.02965   0.02091  -0.0840   0.2995   1.0000
  10.000   1.3822   0.03054   0.02178  -0.0816   0.2904   1.0000
  10.250   1.3892   0.03158   0.02291  -0.0794   0.2804   1.0000
  10.500   1.3953   0.03270   0.02402  -0.0771   0.2714   1.0000
  10.750   1.4011   0.03394   0.02532  -0.0751   0.2619   1.0000
  11.000   1.4056   0.03530   0.02671  -0.0730   0.2529   1.0000
  11.250   1.4086   0.03684   0.02827  -0.0710   0.2436   1.0000
  11.500   1.4110   0.03854   0.03001  -0.0692   0.2343   1.0000
  11.750   1.4112   0.04044   0.03189  -0.0675   0.2261   1.0000
  12.000   1.4128   0.04243   0.03394  -0.0660   0.2179   1.0000
  12.250   1.4112   0.04470   0.03621  -0.0646   0.2107   1.0000
  12.500   1.4110   0.04705   0.03864  -0.0635   0.2034   1.0000
  12.750   1.4081   0.04971   0.04130  -0.0626   0.1969   1.0000
  13.000   1.4068   0.05241   0.04407  -0.0619   0.1908   1.0000
  13.250   1.4042   0.05533   0.04702  -0.0613   0.1850   1.0000
  13.500   1.4018   0.05831   0.05000  -0.0609   0.1802   1.0000
  13.750   1.4002   0.06139   0.05321  -0.0608   0.1749   1.0000
  14.000   1.3970   0.06469   0.05655  -0.0608   0.1697   1.0000
  14.250   1.3943   0.06796   0.05983  -0.0608   0.1650   1.0000
  14.500   1.3913   0.07151   0.06353  -0.0611   0.1597   1.0000
  14.750   1.3869   0.07524   0.06732  -0.0615   0.1544   1.0000
  15.000   1.3840   0.07877   0.07085  -0.0619   0.1496   1.0000
  15.250   1.3782   0.08302   0.07528  -0.0628   0.1437   1.0000
  15.500   1.3733   0.08706   0.07938  -0.0637   0.1384   1.0000
  15.750   1.3682   0.09128   0.08370  -0.0647   0.1329   1.0000
  16.000   1.3616   0.09587   0.08843  -0.0660   0.1270   1.0000
  16.250   1.3567   0.10014   0.09273  -0.0672   0.1219   1.0000
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