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NASA SC(2)-0410 AIRFOIL (sc20410-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: NASA SC(2)-0410 AIRFOIL (sc20410-il)
Reynolds number: 1,000,000
Max Cl/Cd: 71.87 at α=6.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-sc20410-il-1000000.txt
Download as CSV file: xf-sc20410-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NASA SC(2)-0410 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
  ------ -------- --------- --------- -------- -------- --------
 -15.750  -1.1006   0.07823   0.07575  -0.0242   1.0000   0.0134
 -15.500  -1.1383   0.06631   0.06358  -0.0325   1.0000   0.0133
 -15.250  -1.1607   0.05879   0.05587  -0.0372   1.0000   0.0133
 -15.000  -1.1764   0.05314   0.05005  -0.0402   1.0000   0.0134
 -14.750  -1.1866   0.04870   0.04546  -0.0421   1.0000   0.0134
 -14.500  -1.1939   0.04491   0.04153  -0.0433   1.0000   0.0135
 -14.250  -1.1978   0.04170   0.03819  -0.0440   1.0000   0.0136
 -14.000  -1.1994   0.03887   0.03522  -0.0444   1.0000   0.0137
 -13.750  -1.1989   0.03637   0.03259  -0.0444   1.0000   0.0138
 -13.500  -1.1964   0.03417   0.03026  -0.0442   1.0000   0.0139
 -13.250  -1.1925   0.03217   0.02814  -0.0438   1.0000   0.0140
 -13.000  -1.1874   0.03043   0.02628  -0.0430   1.0000   0.0142
 -12.750  -1.1811   0.02892   0.02466  -0.0421   1.0000   0.0143
 -12.500  -1.1678   0.02752   0.02314  -0.0421   1.0000   0.0145
 -12.250  -1.1521   0.02621   0.02171  -0.0422   1.0000   0.0147
 -12.000  -1.1351   0.02498   0.02037  -0.0421   1.0000   0.0149
 -11.750  -1.1171   0.02382   0.01909  -0.0419   1.0000   0.0150
 -11.500  -1.0977   0.02279   0.01795  -0.0416   1.0000   0.0151
 -11.250  -1.0773   0.02184   0.01690  -0.0414   1.0000   0.0153
 -11.000  -1.0559   0.02100   0.01597  -0.0412   1.0000   0.0154
 -10.750  -1.0371   0.01952   0.01435  -0.0409   1.0000   0.0156
 -10.500  -1.0166   0.01822   0.01296  -0.0408   1.0000   0.0159
 -10.250  -0.9939   0.01733   0.01201  -0.0407   1.0000   0.0163
 -10.000  -0.9700   0.01664   0.01127  -0.0407   1.0000   0.0166
  -9.750  -0.9454   0.01604   0.01063  -0.0407   1.0000   0.0170
  -9.500  -0.9204   0.01547   0.01003  -0.0407   1.0000   0.0174
  -9.250  -0.8951   0.01494   0.00945  -0.0407   1.0000   0.0178
  -9.000  -0.8695   0.01444   0.00890  -0.0408   1.0000   0.0183
  -8.750  -0.8436   0.01402   0.00844  -0.0408   1.0000   0.0188
  -8.500  -0.8175   0.01355   0.00793  -0.0408   1.0000   0.0192
  -8.250  -0.7910   0.01283   0.00718  -0.0412   1.0000   0.0202
  -8.000  -0.7645   0.01242   0.00676  -0.0413   1.0000   0.0210
  -7.750  -0.7380   0.01208   0.00641  -0.0414   1.0000   0.0220
  -7.500  -0.7114   0.01177   0.00607  -0.0414   1.0000   0.0230
  -7.250  -0.6842   0.01130   0.00561  -0.0416   1.0000   0.0250
  -7.000  -0.6577   0.01104   0.00536  -0.0416   1.0000   0.0272
  -6.750  -0.6308   0.01071   0.00503  -0.0417   1.0000   0.0301
  -6.500  -0.6044   0.01049   0.00484  -0.0417   1.0000   0.0330
  -6.250  -0.5779   0.01027   0.00461  -0.0416   1.0000   0.0355
  -6.000  -0.5513   0.01003   0.00441  -0.0417   1.0000   0.0387
  -5.750  -0.5254   0.00990   0.00428  -0.0415   1.0000   0.0410
  -5.500  -0.4986   0.00967   0.00406  -0.0415   1.0000   0.0441
  -5.250  -0.4641   0.00944   0.00386  -0.0432   0.9992   0.0476
  -5.000  -0.4296   0.00927   0.00369  -0.0447   0.9982   0.0501
  -4.750  -0.3946   0.00898   0.00343  -0.0465   0.9972   0.0557
  -4.500  -0.3594   0.00879   0.00326  -0.0482   0.9961   0.0602
  -4.250  -0.3237   0.00853   0.00307  -0.0501   0.9951   0.0700
  -4.000  -0.2879   0.00827   0.00289  -0.0521   0.9943   0.0840
  -3.750  -0.2528   0.00796   0.00270  -0.0539   0.9930   0.1082
  -3.500  -0.2174   0.00752   0.00249  -0.0559   0.9915   0.1618
  -3.250  -0.1805   0.00696   0.00228  -0.0584   0.9902   0.2475
  -3.000  -0.1418   0.00629   0.00204  -0.0615   0.9890   0.3628
  -2.750  -0.1011   0.00541   0.00178  -0.0651   0.9881   0.5283
  -2.500  -0.0621   0.00514   0.00174  -0.0676   0.9862   0.6049
  -2.250  -0.0237   0.00505   0.00168  -0.0698   0.9840   0.6269
  -2.000   0.0104   0.00499   0.00164  -0.0710   0.9772   0.6414
  -1.750   0.0457   0.00496   0.00163  -0.0724   0.9709   0.6532
  -1.500   0.0769   0.00495   0.00161  -0.0729   0.9593   0.6602
  -1.250   0.1063   0.00498   0.00163  -0.0729   0.9439   0.6682
  -1.000   0.1342   0.00503   0.00166  -0.0725   0.9264   0.6766
  -0.750   0.1613   0.00513   0.00170  -0.0720   0.9034   0.6829
  -0.250   0.2165   0.00531   0.00173  -0.0713   0.8522   0.6921
   0.000   0.2443   0.00543   0.00175  -0.0710   0.8244   0.6951
   0.250   0.2717   0.00560   0.00178  -0.0706   0.7845   0.6988
   0.500   0.2994   0.00582   0.00183  -0.0704   0.7396   0.7029
   0.750   0.3268   0.00610   0.00188  -0.0702   0.6762   0.7065
   1.000   0.3524   0.00669   0.00198  -0.0697   0.5444   0.7095
   1.250   0.3780   0.00744   0.00217  -0.0695   0.3975   0.7116
   1.500   0.4050   0.00796   0.00233  -0.0695   0.3018   0.7135
   2.000   0.4598   0.00885   0.00264  -0.0696   0.1587   0.7173
   2.250   0.4878   0.00917   0.00279  -0.0697   0.1202   0.7192
   2.500   0.5159   0.00947   0.00295  -0.0698   0.0903   0.7209
   2.750   0.5442   0.00970   0.00309  -0.0699   0.0748   0.7225
   3.000   0.5725   0.00989   0.00325  -0.0699   0.0650   0.7246
   3.250   0.6006   0.01011   0.00343  -0.0699   0.0577   0.7263
   3.500   0.6289   0.01028   0.00361  -0.0700   0.0537   0.7280
   3.750   0.6571   0.01048   0.00379  -0.0700   0.0499   0.7297
   4.000   0.6850   0.01074   0.00404  -0.0700   0.0459   0.7316
   4.250   0.7133   0.01090   0.00421  -0.0700   0.0438   0.7334
   4.500   0.7413   0.01111   0.00440  -0.0700   0.0409   0.7353
   4.750   0.7690   0.01140   0.00468  -0.0699   0.0378   0.7371
   5.000   0.7971   0.01158   0.00486  -0.0700   0.0354   0.7386
   5.250   0.8243   0.01191   0.00518  -0.0698   0.0316   0.7411
   5.500   0.8521   0.01207   0.00537  -0.0698   0.0294   0.7433
   5.750   0.8789   0.01246   0.00575  -0.0696   0.0260   0.7454
   6.000   0.9065   0.01268   0.00599  -0.0695   0.0244   0.7475
   6.250   0.9336   0.01299   0.00630  -0.0693   0.0228   0.7497
   6.500   0.9597   0.01351   0.00684  -0.0690   0.0213   0.7520
   6.750   0.9867   0.01384   0.00721  -0.0688   0.0206   0.7540
   7.000   1.0134   0.01421   0.00761  -0.0686   0.0199   0.7561
   7.250   1.0397   0.01458   0.00803  -0.0683   0.0192   0.7586
   7.500   1.0657   0.01500   0.00850  -0.0679   0.0186   0.7610
   7.750   1.0909   0.01557   0.00911  -0.0675   0.0181   0.7634
   8.000   1.1141   0.01650   0.01013  -0.0667   0.0174   0.7660
   8.250   1.1391   0.01706   0.01076  -0.0662   0.0172   0.7686
   8.500   1.1642   0.01761   0.01137  -0.0658   0.0170   0.7710
   8.750   1.1888   0.01817   0.01201  -0.0652   0.0168   0.7737
   9.000   1.2132   0.01873   0.01266  -0.0647   0.0164   0.7764
   9.250   1.2374   0.01931   0.01332  -0.0641   0.0160   0.7793
   9.500   1.2609   0.01999   0.01408  -0.0634   0.0157   0.7823
   9.750   1.2841   0.02069   0.01485  -0.0627   0.0155   0.7854
  10.000   1.3067   0.02141   0.01566  -0.0620   0.0152   0.7885
  10.250   1.3286   0.02219   0.01653  -0.0611   0.0150   0.7918
  10.500   1.3495   0.02309   0.01753  -0.0602   0.0147   0.7952
  10.750   1.3685   0.02424   0.01878  -0.0590   0.0145   0.7989
  11.000   1.3844   0.02585   0.02054  -0.0574   0.0143   0.8022
  11.250   1.3938   0.02835   0.02332  -0.0551   0.0140   0.8057
  11.500   1.4070   0.03004   0.02522  -0.0532   0.0139   0.8094
  11.750   1.4222   0.03127   0.02660  -0.0517   0.0138   0.8134
  12.000   1.4353   0.03266   0.02815  -0.0499   0.0138   0.8173
  12.250   1.4457   0.03418   0.02985  -0.0478   0.0137   0.8213
  12.500   1.4531   0.03585   0.03171  -0.0454   0.0136   0.8257
  12.750   1.4554   0.03774   0.03378  -0.0425   0.0135   0.8303
  13.000   1.4491   0.03962   0.03585  -0.0383   0.0135   0.8350
  13.250   1.4412   0.04192   0.03834  -0.0348   0.0134   0.8403
  13.500   1.4327   0.04455   0.04114  -0.0321   0.0134   0.8457
  13.750   1.4207   0.04781   0.04462  -0.0303   0.0133   0.8506
  14.000   1.4062   0.05184   0.04884  -0.0296   0.0133   0.8559
  14.250   1.3895   0.05678   0.05398  -0.0305   0.0132   0.8610
  14.500   1.3647   0.06393   0.06137  -0.0338   0.0132   0.8655
  14.750   1.3273   0.07550   0.07321  -0.0421   0.0133   0.8696
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