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NASA SC(2)-0412 AIRFOIL (sc20412-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: NASA SC(2)-0412 AIRFOIL (sc20412-il)
Reynolds number: 1,000,000
Max Cl/Cd: 78.16 at α=8°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-sc20412-il-1000000-n5.txt
Download as CSV file: xf-sc20412-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NASA SC(2)-0412 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
  ------ -------- --------- --------- -------- -------- --------
 -19.750  -1.1477   0.12904   0.12627  -0.0043   1.0000   0.0136
 -19.500  -1.2094   0.11306   0.11008  -0.0133   1.0000   0.0135
 -19.250  -1.2648   0.09872   0.09552  -0.0212   1.0000   0.0134
 -19.000  -1.3053   0.08743   0.08403  -0.0274   1.0000   0.0134
 -18.750  -1.3333   0.07863   0.07505  -0.0323   1.0000   0.0134
 -18.500  -1.3533   0.07152   0.06780  -0.0362   1.0000   0.0135
 -18.250  -1.3673   0.06564   0.06177  -0.0393   1.0000   0.0135
 -18.000  -1.3771   0.06070   0.05671  -0.0416   1.0000   0.0136
 -17.750  -1.3839   0.05639   0.05228  -0.0435   1.0000   0.0136
 -17.500  -1.3878   0.05268   0.04846  -0.0449   1.0000   0.0137
 -17.250  -1.3901   0.04935   0.04503  -0.0460   1.0000   0.0138
 -17.000  -1.3903   0.04641   0.04199  -0.0467   1.0000   0.0139
 -16.750  -1.3893   0.04378   0.03926  -0.0472   1.0000   0.0140
 -16.500  -1.3868   0.04139   0.03679  -0.0475   1.0000   0.0141
 -16.250  -1.3826   0.03925   0.03455  -0.0476   1.0000   0.0142
 -16.000  -1.3770   0.03730   0.03252  -0.0476   1.0000   0.0143
 -15.750  -1.3696   0.03554   0.03068  -0.0476   1.0000   0.0144
 -15.500  -1.3637   0.03368   0.02874  -0.0474   1.0000   0.0145
 -15.250  -1.3570   0.03191   0.02691  -0.0472   1.0000   0.0148
 -15.000  -1.3482   0.03038   0.02531  -0.0469   1.0000   0.0150
 -14.750  -1.3379   0.02899   0.02386  -0.0465   1.0000   0.0152
 -14.500  -1.3264   0.02773   0.02255  -0.0461   1.0000   0.0154
 -14.250  -1.3139   0.02656   0.02134  -0.0457   1.0000   0.0157
 -14.000  -1.3010   0.02547   0.02020  -0.0452   1.0000   0.0159
 -13.750  -1.2875   0.02447   0.01914  -0.0446   1.0000   0.0161
 -13.500  -1.2742   0.02352   0.01814  -0.0438   1.0000   0.0164
 -13.250  -1.2616   0.02264   0.01721  -0.0428   1.0000   0.0166
 -13.000  -1.2468   0.02181   0.01633  -0.0421   1.0000   0.0169
 -12.750  -1.2289   0.02103   0.01550  -0.0419   1.0000   0.0171
 -12.500  -1.2097   0.02030   0.01472  -0.0417   1.0000   0.0174
 -12.250  -1.1903   0.01952   0.01390  -0.0417   1.0000   0.0178
 -12.000  -1.1698   0.01881   0.01317  -0.0416   1.0000   0.0182
 -11.750  -1.1484   0.01818   0.01251  -0.0416   1.0000   0.0187
 -11.500  -1.1263   0.01761   0.01193  -0.0415   1.0000   0.0192
 -11.250  -1.1038   0.01710   0.01138  -0.0413   1.0000   0.0198
 -11.000  -1.0809   0.01662   0.01088  -0.0411   1.0000   0.0203
 -10.750  -1.0577   0.01618   0.01040  -0.0409   1.0000   0.0207
 -10.500  -1.0343   0.01571   0.00991  -0.0407   1.0000   0.0214
 -10.250  -1.0107   0.01527   0.00947  -0.0406   1.0000   0.0222
 -10.000  -0.9851   0.01486   0.00905  -0.0407   0.9998   0.0230
  -9.750  -0.9538   0.01446   0.00864  -0.0420   0.9989   0.0240
  -9.500  -0.9224   0.01408   0.00823  -0.0433   0.9979   0.0248
  -9.250  -0.8909   0.01365   0.00782  -0.0446   0.9967   0.0260
  -9.000  -0.8588   0.01328   0.00745  -0.0460   0.9956   0.0271
  -8.750  -0.8262   0.01294   0.00709  -0.0474   0.9944   0.0283
  -8.500  -0.7933   0.01261   0.00675  -0.0489   0.9935   0.0292
  -8.250  -0.7619   0.01226   0.00641  -0.0501   0.9916   0.0307
  -8.000  -0.7301   0.01194   0.00610  -0.0513   0.9897   0.0321
  -7.750  -0.6979   0.01166   0.00581  -0.0525   0.9880   0.0334
  -7.500  -0.6653   0.01136   0.00552  -0.0539   0.9864   0.0351
  -7.250  -0.6324   0.01106   0.00525  -0.0553   0.9849   0.0371
  -7.000  -0.5994   0.01081   0.00499  -0.0566   0.9834   0.0388
  -6.750  -0.5666   0.01054   0.00474  -0.0580   0.9816   0.0409
  -6.500  -0.5356   0.01028   0.00451  -0.0589   0.9781   0.0434
  -6.250  -0.5035   0.01007   0.00430  -0.0600   0.9751   0.0455
  -6.000  -0.4706   0.00981   0.00407  -0.0613   0.9723   0.0487
  -5.750  -0.4377   0.00959   0.00386  -0.0625   0.9691   0.0516
  -5.500  -0.4070   0.00938   0.00367  -0.0633   0.9632   0.0547
  -5.250  -0.3753   0.00916   0.00348  -0.0642   0.9578   0.0588
  -5.000  -0.3445   0.00899   0.00331  -0.0649   0.9523   0.0621
  -4.750  -0.3138   0.00878   0.00314  -0.0656   0.9458   0.0678
  -4.500  -0.2831   0.00858   0.00298  -0.0664   0.9398   0.0762
  -4.250  -0.2527   0.00840   0.00283  -0.0670   0.9331   0.0849
  -4.000  -0.2223   0.00824   0.00270  -0.0676   0.9268   0.0946
  -3.750  -0.1917   0.00805   0.00256  -0.0682   0.9196   0.1075
  -3.250  -0.1305   0.00762   0.00229  -0.0696   0.8995   0.1541
  -3.000  -0.0995   0.00738   0.00215  -0.0705   0.8882   0.1894
  -2.500  -0.0355   0.00678   0.00187  -0.0727   0.8655   0.2910
  -2.250  -0.0023   0.00640   0.00172  -0.0742   0.8564   0.3637
  -2.000   0.0320   0.00592   0.00153  -0.0761   0.8405   0.4626
  -1.750   0.0644   0.00567   0.00145  -0.0772   0.8159   0.5396
  -1.500   0.0942   0.00568   0.00144  -0.0775   0.7880   0.5681
  -1.250   0.1240   0.00572   0.00146  -0.0778   0.7650   0.5945
  -1.000   0.1535   0.00580   0.00148  -0.0780   0.7407   0.6109
  -0.750   0.1822   0.00598   0.00152  -0.0780   0.6983   0.6231
  -0.500   0.2107   0.00619   0.00155  -0.0781   0.6459   0.6291
  -0.250   0.2373   0.00675   0.00167  -0.0779   0.5294   0.6366
   0.000   0.2638   0.00744   0.00184  -0.0778   0.3981   0.6434
   0.250   0.2921   0.00776   0.00196  -0.0779   0.3385   0.6482
   0.500   0.3204   0.00808   0.00208  -0.0780   0.2820   0.6524
   0.750   0.3487   0.00841   0.00219  -0.0782   0.2287   0.6561
   1.000   0.3773   0.00869   0.00229  -0.0783   0.1903   0.6588
   1.250   0.4058   0.00893   0.00240  -0.0784   0.1587   0.6610
   1.500   0.4347   0.00910   0.00250  -0.0786   0.1406   0.6627
   1.750   0.4635   0.00928   0.00261  -0.0787   0.1233   0.6642
   2.000   0.4922   0.00946   0.00273  -0.0788   0.1089   0.6658
   2.250   0.5210   0.00963   0.00285  -0.0789   0.0979   0.6674
   2.500   0.5497   0.00982   0.00297  -0.0790   0.0862   0.6690
   2.750   0.5782   0.01001   0.00310  -0.0791   0.0768   0.6707
   3.000   0.6069   0.01018   0.00324  -0.0792   0.0704   0.6724
   3.250   0.6354   0.01037   0.00339  -0.0793   0.0646   0.6740
   3.500   0.6640   0.01054   0.00354  -0.0793   0.0609   0.6755
   3.750   0.6923   0.01074   0.00370  -0.0794   0.0568   0.6770
   4.000   0.7208   0.01090   0.00387  -0.0794   0.0541   0.6790
   4.250   0.7490   0.01109   0.00404  -0.0794   0.0512   0.6808
   4.500   0.7771   0.01130   0.00424  -0.0794   0.0485   0.6825
   4.750   0.8053   0.01148   0.00443  -0.0794   0.0465   0.6842
   5.000   0.8333   0.01169   0.00463  -0.0793   0.0441   0.6859
   5.250   0.8611   0.01192   0.00485  -0.0793   0.0418   0.6876
   5.500   0.8890   0.01212   0.00505  -0.0792   0.0400   0.6893
   5.750   0.9166   0.01235   0.00527  -0.0791   0.0379   0.6909
   6.000   0.9441   0.01260   0.00551  -0.0790   0.0360   0.6924
   6.250   0.9716   0.01283   0.00575  -0.0789   0.0345   0.6938
   6.500   0.9989   0.01308   0.00600  -0.0787   0.0326   0.6953
   6.750   1.0259   0.01336   0.00627  -0.0786   0.0309   0.6971
   7.000   1.0530   0.01361   0.00655  -0.0784   0.0294   0.6991
   7.250   1.0797   0.01390   0.00685  -0.0781   0.0277   0.7011
   7.500   1.1062   0.01422   0.00717  -0.0779   0.0264   0.7032
   7.750   1.1328   0.01451   0.00749  -0.0776   0.0254   0.7054
   8.000   1.1591   0.01483   0.00783  -0.0773   0.0243   0.7075
   8.250   1.1850   0.01519   0.00819  -0.0769   0.0233   0.7094
   8.500   1.2107   0.01557   0.00858  -0.0765   0.0225   0.7111
   8.750   1.2365   0.01591   0.00895  -0.0762   0.0219   0.7125
   9.000   1.2620   0.01626   0.00934  -0.0757   0.0212   0.7145
   9.250   1.2872   0.01665   0.00976  -0.0753   0.0205   0.7165
   9.500   1.3120   0.01706   0.01021  -0.0748   0.0199   0.7188
   9.750   1.3363   0.01753   0.01071  -0.0742   0.0193   0.7211
  10.000   1.3605   0.01799   0.01120  -0.0736   0.0189   0.7233
  10.250   1.3848   0.01841   0.01168  -0.0730   0.0185   0.7255
  10.500   1.4086   0.01885   0.01217  -0.0723   0.0181   0.7276
  10.750   1.4321   0.01932   0.01268  -0.0716   0.0177   0.7295
  11.250   1.4778   0.02032   0.01377  -0.0700   0.0168   0.7335
  11.500   1.4997   0.02088   0.01438  -0.0691   0.0165   0.7359
  11.750   1.5208   0.02150   0.01505  -0.0681   0.0161   0.7383
  12.000   1.5407   0.02220   0.01581  -0.0669   0.0158   0.7407
  12.250   1.5613   0.02279   0.01647  -0.0658   0.0156   0.7432
  12.500   1.5812   0.02340   0.01715  -0.0646   0.0155   0.7457
  12.750   1.6002   0.02405   0.01787  -0.0633   0.0153   0.7479
  13.000   1.6183   0.02472   0.01862  -0.0619   0.0151   0.7503
  13.250   1.6354   0.02543   0.01941  -0.0604   0.0149   0.7529
  13.500   1.6511   0.02617   0.02024  -0.0586   0.0147   0.7557
  13.750   1.6648   0.02695   0.02109  -0.0566   0.0146   0.7587
  14.000   1.6754   0.02775   0.02198  -0.0540   0.0144   0.7618
  14.250   1.6836   0.02863   0.02293  -0.0512   0.0143   0.7648
  14.500   1.6924   0.02961   0.02400  -0.0486   0.0141   0.7677
  14.750   1.7004   0.03069   0.02518  -0.0462   0.0140   0.7710
  15.000   1.7077   0.03189   0.02647  -0.0439   0.0138   0.7743
  15.250   1.7136   0.03323   0.02790  -0.0416   0.0137   0.7776
  15.500   1.7184   0.03472   0.02949  -0.0395   0.0136   0.7806
  15.750   1.7216   0.03641   0.03128  -0.0375   0.0135   0.7836
  16.000   1.7232   0.03834   0.03332  -0.0357   0.0134   0.7869
  16.250   1.7223   0.04058   0.03569  -0.0341   0.0132   0.7906
  16.500   1.7193   0.04320   0.03842  -0.0328   0.0131   0.7943
  16.750   1.7136   0.04626   0.04161  -0.0319   0.0130   0.7979
  17.000   1.7053   0.04982   0.04532  -0.0315   0.0129   0.8014
  17.250   1.6965   0.05373   0.04938  -0.0316   0.0129   0.8052
  17.500   1.6861   0.05811   0.05391  -0.0324   0.0129   0.8090
  17.750   1.6727   0.06328   0.05923  -0.0340   0.0128   0.8123
  18.000   1.6529   0.06997   0.06610  -0.0369   0.0128   0.8150
  18.250   1.6249   0.07877   0.07510  -0.0417   0.0128   0.8172
  18.500   1.5772   0.09229   0.08888  -0.0498   0.0129   0.8182
  18.750   1.4947   0.11308   0.11000  -0.0620   0.0129   0.8169
  19.000   1.4090   0.13471   0.13192  -0.0748   0.0131   0.8151
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