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WORTMANN FX 60-126 AIRFOIL (fx60126-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: WORTMANN FX 60-126 AIRFOIL (fx60126-il)
Reynolds number: 200,000
Max Cl/Cd: 75.22 at α=5.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx60126-il-200000-n5.txt
Download as CSV file: xf-fx60126-il-200000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: WORTMANN FX 60-126 AIRFOIL                      
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.200 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -11.750  -0.5348   0.07369   0.06966  -0.0576   1.0000   0.0122
 -11.500  -0.5795   0.06183   0.05755  -0.0660   1.0000   0.0118
 -11.250  -0.6037   0.05515   0.05069  -0.0705   1.0000   0.0117
 -11.000  -0.6227   0.05014   0.04556  -0.0733   1.0000   0.0117
 -10.750  -0.6399   0.04628   0.04159  -0.0746   1.0000   0.0116
 -10.500  -0.6616   0.04349   0.03873  -0.0736   1.0000   0.0116
 -10.250  -0.6853   0.04118   0.03636  -0.0718   1.0000   0.0116
 -10.000  -0.6707   0.03713   0.03201  -0.0787   0.9944   0.0117
  -9.750  -0.6474   0.03393   0.02853  -0.0838   0.9877   0.0119
  -9.500  -0.6196   0.03133   0.02566  -0.0880   0.9831   0.0121
  -9.250  -0.5943   0.02923   0.02334  -0.0905   0.9772   0.0124
  -9.000  -0.5652   0.02729   0.02117  -0.0931   0.9728   0.0127
  -8.750  -0.5331   0.02556   0.01925  -0.0959   0.9698   0.0131
  -8.500  -0.5060   0.02410   0.01761  -0.0973   0.9639   0.0135
  -8.250  -0.4741   0.02274   0.01609  -0.0995   0.9595   0.0139
  -8.000  -0.4404   0.02143   0.01466  -0.1020   0.9562   0.0147
  -7.750  -0.4113   0.02043   0.01359  -0.1034   0.9505   0.0156
  -7.500  -0.3801   0.01949   0.01254  -0.1049   0.9451   0.0167
  -7.250  -0.3458   0.01854   0.01143  -0.1069   0.9410   0.0179
  -7.000  -0.3168   0.01760   0.01043  -0.1079   0.9342   0.0191
  -6.750  -0.2854   0.01682   0.00956  -0.1092   0.9286   0.0210
  -6.500  -0.2523   0.01604   0.00871  -0.1107   0.9246   0.0244
  -6.250  -0.2245   0.01541   0.00804  -0.1111   0.9172   0.0319
  -6.000  -0.1933   0.01472   0.00736  -0.1121   0.9114   0.0462
  -5.750  -0.1637   0.01418   0.00685  -0.1127   0.9046   0.0662
  -5.500  -0.1345   0.01361   0.00638  -0.1134   0.8974   0.0908
  -5.250  -0.1043   0.01295   0.00591  -0.1143   0.8916   0.1375
  -5.000  -0.0760   0.01244   0.00555  -0.1148   0.8841   0.1804
  -4.750  -0.0457   0.01206   0.00520  -0.1153   0.8785   0.2139
  -4.500  -0.0174   0.01179   0.00498  -0.1155   0.8711   0.2474
  -4.250   0.0119   0.01156   0.00476  -0.1157   0.8642   0.2755
  -4.000   0.0405   0.01140   0.00458  -0.1157   0.8560   0.3033
  -3.750   0.0694   0.01125   0.00444  -0.1158   0.8480   0.3290
  -3.500   0.0977   0.01116   0.00435  -0.1157   0.8392   0.3539
  -3.250   0.1267   0.01108   0.00423  -0.1157   0.8316   0.3754
  -3.000   0.1549   0.01104   0.00416  -0.1155   0.8226   0.3909
  -2.750   0.1838   0.01099   0.00404  -0.1155   0.8151   0.4035
  -2.500   0.2120   0.01096   0.00397  -0.1153   0.8056   0.4160
  -2.250   0.2404   0.01093   0.00390  -0.1152   0.7962   0.4308
  -2.000   0.2687   0.01092   0.00382  -0.1150   0.7855   0.4446
  -1.750   0.2966   0.01089   0.00378  -0.1148   0.7741   0.4556
  -1.500   0.3248   0.01088   0.00372  -0.1146   0.7633   0.4650
  -1.250   0.3532   0.01088   0.00365  -0.1145   0.7527   0.4751
  -1.000   0.3811   0.01087   0.00364  -0.1143   0.7415   0.4842
  -0.750   0.4093   0.01089   0.00360  -0.1141   0.7298   0.4936
  -0.500   0.4372   0.01090   0.00358  -0.1139   0.7173   0.5021
  -0.250   0.4650   0.01093   0.00355  -0.1136   0.7035   0.5103
   0.000   0.4928   0.01096   0.00354  -0.1134   0.6896   0.5184
   0.250   0.5205   0.01101   0.00354  -0.1132   0.6757   0.5264
   0.500   0.5481   0.01107   0.00357  -0.1129   0.6621   0.5351
   0.750   0.5757   0.01114   0.00362  -0.1127   0.6485   0.5438
   1.000   0.6032   0.01123   0.00366  -0.1125   0.6346   0.5533
   1.250   0.6305   0.01132   0.00374  -0.1122   0.6212   0.5619
   1.500   0.6578   0.01144   0.00380  -0.1120   0.6067   0.5711
   1.750   0.6845   0.01155   0.00389  -0.1116   0.5898   0.5789
   2.000   0.7111   0.01170   0.00396  -0.1112   0.5710   0.5876
   2.250   0.7373   0.01185   0.00407  -0.1108   0.5529   0.5961
   2.500   0.7637   0.01202   0.00420  -0.1104   0.5360   0.6057
   2.750   0.7902   0.01217   0.00434  -0.1100   0.5213   0.6162
   3.000   0.8167   0.01231   0.00451  -0.1097   0.5081   0.6268
   3.250   0.8431   0.01246   0.00469  -0.1094   0.4955   0.6384
   3.500   0.8694   0.01264   0.00487  -0.1090   0.4825   0.6506
   3.750   0.8952   0.01282   0.00506  -0.1086   0.4683   0.6625
   4.000   0.9207   0.01301   0.00527  -0.1081   0.4513   0.6755
   4.250   0.9458   0.01321   0.00550  -0.1075   0.4326   0.6900
   4.500   0.9703   0.01344   0.00573  -0.1069   0.4139   0.7059
   4.750   0.9945   0.01369   0.00598  -0.1062   0.3957   0.7238
   5.000   1.0187   0.01392   0.00625  -0.1055   0.3787   0.7451
   5.250   1.0420   0.01415   0.00653  -0.1046   0.3620   0.7726
   5.500   1.0635   0.01435   0.00680  -0.1034   0.3464   0.8137
   5.750   1.0816   0.01438   0.00700  -0.1012   0.3298   1.0000
   6.000   1.1057   0.01481   0.00735  -0.1007   0.3082   1.0000
   6.250   1.1285   0.01531   0.00775  -0.1001   0.2873   1.0000
   6.500   1.1515   0.01580   0.00818  -0.0994   0.2669   1.0000
   6.750   1.1739   0.01632   0.00863  -0.0987   0.2454   1.0000
   7.000   1.1951   0.01692   0.00914  -0.0978   0.2268   1.0000
   7.250   1.2166   0.01749   0.00967  -0.0970   0.2081   1.0000
   7.500   1.2373   0.01810   0.01023  -0.0961   0.1900   1.0000
   7.750   1.2568   0.01879   0.01085  -0.0950   0.1741   1.0000
   8.000   1.2758   0.01948   0.01149  -0.0938   0.1575   1.0000
   8.250   1.2936   0.02024   0.01218  -0.0925   0.1420   1.0000
   8.500   1.3109   0.02099   0.01290  -0.0912   0.1308   1.0000
   8.750   1.3275   0.02174   0.01365  -0.0897   0.1220   1.0000
   9.000   1.3437   0.02244   0.01438  -0.0882   0.1128   1.0000
   9.250   1.3583   0.02317   0.01514  -0.0864   0.1050   1.0000
   9.500   1.3706   0.02404   0.01599  -0.0844   0.0979   1.0000
   9.750   1.3835   0.02489   0.01690  -0.0825   0.0921   1.0000
  10.000   1.3933   0.02594   0.01795  -0.0804   0.0870   1.0000
  10.250   1.4058   0.02686   0.01896  -0.0787   0.0827   1.0000
  10.500   1.4176   0.02785   0.02005  -0.0770   0.0779   1.0000
  10.750   1.4262   0.02909   0.02132  -0.0752   0.0739   1.0000
  11.000   1.4373   0.03021   0.02254  -0.0736   0.0704   1.0000
  11.250   1.4466   0.03149   0.02391  -0.0721   0.0669   1.0000
  11.500   1.4536   0.03299   0.02545  -0.0705   0.0640   1.0000
  11.750   1.4604   0.03458   0.02711  -0.0691   0.0616   1.0000
  12.000   1.4675   0.03621   0.02885  -0.0678   0.0593   1.0000
  12.250   1.4728   0.03805   0.03078  -0.0666   0.0571   1.0000
  12.500   1.4763   0.04013   0.03292  -0.0655   0.0552   1.0000
  12.750   1.4771   0.04256   0.03541  -0.0644   0.0535   1.0000
  13.000   1.4789   0.04500   0.03794  -0.0636   0.0521   1.0000
  13.250   1.4843   0.04716   0.04028  -0.0629   0.0509   1.0000
  13.500   1.4882   0.04952   0.04279  -0.0624   0.0494   1.0000
  13.750   1.4913   0.05205   0.04546  -0.0621   0.0478   1.0000
  14.000   1.4933   0.05478   0.04831  -0.0620   0.0463   1.0000
  14.250   1.4935   0.05781   0.05144  -0.0621   0.0447   1.0000
  14.500   1.4910   0.06127   0.05497  -0.0624   0.0434   1.0000
  14.750   1.4919   0.06444   0.05827  -0.0628   0.0420   1.0000
  15.000   1.4945   0.06751   0.06152  -0.0634   0.0403   1.0000
  15.250   1.4952   0.07091   0.06507  -0.0642   0.0387   1.0000
  15.500   1.4943   0.07464   0.06893  -0.0653   0.0372   1.0000
  15.750   1.4910   0.07883   0.07322  -0.0666   0.0360   1.0000
  16.000   1.4854   0.08348   0.07796  -0.0683   0.0350   1.0000
  16.250   1.4834   0.08766   0.08231  -0.0697   0.0340   1.0000
  16.500   1.4806   0.09206   0.08688  -0.0713   0.0328   1.0000
  16.750   1.4765   0.09681   0.09179  -0.0733   0.0317   1.0000
  17.000   1.4709   0.10192   0.09704  -0.0756   0.0307   1.0000
  17.250   1.4637   0.10743   0.10266  -0.0782   0.0297   1.0000
  17.500   1.4552   0.11325   0.10859  -0.0811   0.0289   1.0000
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