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NASA SC(2)-0610 AIRFOIL (sc20610-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: NASA SC(2)-0610 AIRFOIL (sc20610-il)
Reynolds number: 1,000,000
Max Cl/Cd: 77.52 at α=6°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-sc20610-il-1000000-n5.txt
Download as CSV file: xf-sc20610-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NASA SC(2)-0610 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
  ------ -------- --------- --------- -------- -------- --------
 -17.750  -1.0838   0.09460   0.09202  -0.0298   1.0000   0.0103
 -17.500  -1.1531   0.07636   0.07349  -0.0406   1.0000   0.0101
 -17.250  -1.1864   0.06566   0.06258  -0.0475   1.0000   0.0101
 -17.000  -1.2071   0.05807   0.05481  -0.0525   1.0000   0.0101
 -16.750  -1.2202   0.05247   0.04907  -0.0558   1.0000   0.0101
 -16.500  -1.2295   0.04795   0.04441  -0.0581   1.0000   0.0102
 -16.250  -1.2338   0.04438   0.04073  -0.0597   1.0000   0.0103
 -16.000  -1.2357   0.04130   0.03755  -0.0607   1.0000   0.0103
 -15.750  -1.2355   0.03861   0.03475  -0.0614   1.0000   0.0104
 -15.500  -1.2330   0.03629   0.03234  -0.0618   1.0000   0.0105
 -15.250  -1.2293   0.03420   0.03015  -0.0619   1.0000   0.0106
 -15.000  -1.2248   0.03229   0.02815  -0.0618   1.0000   0.0107
 -14.750  -1.2200   0.03057   0.02633  -0.0613   1.0000   0.0107
 -14.500  -1.2157   0.02905   0.02472  -0.0603   1.0000   0.0108
 -14.250  -1.2145   0.02773   0.02333  -0.0583   1.0000   0.0109
 -14.000  -1.2109   0.02649   0.02201  -0.0565   1.0000   0.0110
 -13.750  -1.2007   0.02528   0.02071  -0.0559   1.0000   0.0111
 -13.500  -1.1875   0.02415   0.01950  -0.0555   1.0000   0.0112
 -13.250  -1.1718   0.02311   0.01837  -0.0554   1.0000   0.0113
 -13.000  -1.1542   0.02214   0.01731  -0.0553   1.0000   0.0114
 -12.750  -1.1355   0.02127   0.01637  -0.0551   1.0000   0.0116
 -12.500  -1.1159   0.02048   0.01550  -0.0548   1.0000   0.0117
 -12.250  -1.0954   0.01975   0.01469  -0.0546   1.0000   0.0118
 -12.000  -1.0666   0.01899   0.01386  -0.0560   0.9994   0.0120
 -11.750  -1.0374   0.01829   0.01308  -0.0574   0.9987   0.0121
 -11.500  -1.0079   0.01765   0.01237  -0.0587   0.9980   0.0122
 -11.250  -0.9786   0.01680   0.01145  -0.0602   0.9972   0.0125
 -11.000  -0.9486   0.01610   0.01070  -0.0616   0.9965   0.0128
 -10.750  -0.9180   0.01552   0.01008  -0.0630   0.9958   0.0132
 -10.500  -0.8869   0.01500   0.00953  -0.0644   0.9952   0.0136
 -10.250  -0.8555   0.01453   0.00903  -0.0659   0.9946   0.0140
 -10.000  -0.8238   0.01406   0.00852  -0.0673   0.9941   0.0143
  -9.750  -0.7935   0.01362   0.00804  -0.0684   0.9931   0.0147
  -9.500  -0.7631   0.01320   0.00759  -0.0695   0.9920   0.0150
  -9.250  -0.7322   0.01282   0.00717  -0.0706   0.9909   0.0154
  -9.000  -0.7008   0.01238   0.00670  -0.0719   0.9898   0.0160
  -8.750  -0.6692   0.01199   0.00631  -0.0732   0.9888   0.0168
  -8.500  -0.6373   0.01164   0.00596  -0.0745   0.9879   0.0177
  -8.250  -0.6051   0.01132   0.00562  -0.0758   0.9871   0.0187
  -8.000  -0.5727   0.01100   0.00529  -0.0771   0.9863   0.0199
  -7.750  -0.5402   0.01069   0.00500  -0.0785   0.9856   0.0217
  -7.500  -0.5076   0.01043   0.00473  -0.0798   0.9850   0.0234
  -7.250  -0.4746   0.01014   0.00447  -0.0813   0.9845   0.0260
  -7.000  -0.4415   0.00990   0.00423  -0.0827   0.9840   0.0284
  -6.750  -0.4081   0.00964   0.00399  -0.0842   0.9835   0.0312
  -6.500  -0.3781   0.00943   0.00379  -0.0849   0.9813   0.0338
  -6.250  -0.3466   0.00921   0.00359  -0.0859   0.9796   0.0365
  -6.000  -0.3147   0.00900   0.00340  -0.0870   0.9782   0.0398
  -5.750  -0.2826   0.00881   0.00322  -0.0881   0.9768   0.0428
  -5.500  -0.2500   0.00860   0.00305  -0.0893   0.9755   0.0477
  -5.250  -0.2175   0.00841   0.00289  -0.0905   0.9743   0.0528
  -5.000  -0.1846   0.00821   0.00273  -0.0917   0.9732   0.0601
  -4.750  -0.1514   0.00801   0.00258  -0.0931   0.9721   0.0681
  -4.500  -0.1191   0.00782   0.00244  -0.0942   0.9704   0.0782
  -4.250  -0.0883   0.00763   0.00232  -0.0950   0.9675   0.0920
  -4.000  -0.0567   0.00744   0.00220  -0.0959   0.9650   0.1096
  -3.750  -0.0240   0.00718   0.00207  -0.0972   0.9626   0.1405
  -3.500   0.0097   0.00690   0.00194  -0.0987   0.9599   0.1799
  -3.250   0.0436   0.00657   0.00181  -0.1003   0.9563   0.2326
  -3.000   0.0766   0.00620   0.00167  -0.1017   0.9497   0.3022
  -2.750   0.1110   0.00577   0.00151  -0.1035   0.9397   0.3876
  -2.500   0.1449   0.00534   0.00136  -0.1051   0.9282   0.4830
  -2.250   0.1772   0.00509   0.00133  -0.1062   0.9185   0.5550
  -2.000   0.2067   0.00504   0.00133  -0.1064   0.9032   0.5938
  -1.750   0.2354   0.00506   0.00134  -0.1063   0.8835   0.6172
  -1.500   0.2632   0.00516   0.00132  -0.1060   0.8521   0.6254
  -1.250   0.2891   0.00541   0.00133  -0.1053   0.7837   0.6332
  -1.000   0.3136   0.00593   0.00140  -0.1045   0.6752   0.6405
  -0.750   0.3374   0.00672   0.00159  -0.1038   0.5221   0.6458
  -0.500   0.3628   0.00737   0.00177  -0.1034   0.3954   0.6518
  -0.250   0.3896   0.00784   0.00190  -0.1033   0.3086   0.6576
   0.000   0.4169   0.00820   0.00204  -0.1033   0.2438   0.6616
   0.250   0.4442   0.00855   0.00217  -0.1032   0.1879   0.6660
   0.500   0.4719   0.00886   0.00230  -0.1032   0.1446   0.6701
   0.750   0.5000   0.00910   0.00242  -0.1032   0.1173   0.6733
   1.000   0.5280   0.00931   0.00255  -0.1032   0.0965   0.6759
   1.250   0.5561   0.00950   0.00269  -0.1032   0.0811   0.6780
   1.500   0.5842   0.00969   0.00283  -0.1032   0.0695   0.6804
   1.750   0.6123   0.00988   0.00297  -0.1032   0.0610   0.6829
   2.000   0.6405   0.01006   0.00312  -0.1032   0.0547   0.6853
   2.250   0.6684   0.01026   0.00328  -0.1031   0.0485   0.6874
   2.500   0.6966   0.01043   0.00343  -0.1031   0.0449   0.6892
   2.750   0.7244   0.01063   0.00360  -0.1031   0.0404   0.6911
   3.000   0.7523   0.01081   0.00378  -0.1030   0.0378   0.6933
   3.250   0.7800   0.01101   0.00398  -0.1029   0.0348   0.6958
   3.500   0.8076   0.01122   0.00418  -0.1028   0.0322   0.6982
   3.750   0.8352   0.01143   0.00438  -0.1027   0.0299   0.7005
   4.000   0.8626   0.01168   0.00461  -0.1025   0.0272   0.7026
   4.250   0.8900   0.01190   0.00484  -0.1023   0.0255   0.7045
   4.500   0.9172   0.01216   0.00508  -0.1022   0.0233   0.7064
   4.750   0.9443   0.01242   0.00535  -0.1019   0.0214   0.7083
   5.000   0.9712   0.01268   0.00562  -0.1017   0.0198   0.7103
   5.250   0.9979   0.01299   0.00593  -0.1014   0.0184   0.7125
   5.500   1.0245   0.01328   0.00625  -0.1011   0.0175   0.7148
   5.750   1.0511   0.01358   0.00658  -0.1008   0.0168   0.7173
   6.000   1.0775   0.01390   0.00691  -0.1005   0.0161   0.7195
   6.250   1.1037   0.01425   0.00727  -0.1001   0.0155   0.7214
   6.500   1.1295   0.01464   0.00769  -0.0997   0.0148   0.7234
   6.750   1.1550   0.01506   0.00815  -0.0992   0.0144   0.7255
   7.000   1.1808   0.01542   0.00856  -0.0988   0.0141   0.7276
   7.250   1.2063   0.01581   0.00900  -0.0983   0.0139   0.7298
   7.500   1.2315   0.01623   0.00947  -0.0977   0.0136   0.7321
   7.750   1.2565   0.01667   0.00995  -0.0972   0.0133   0.7344
   8.000   1.2813   0.01712   0.01045  -0.0966   0.0131   0.7366
   8.250   1.3058   0.01758   0.01096  -0.0960   0.0128   0.7385
   8.500   1.3301   0.01806   0.01149  -0.0953   0.0125   0.7406
   8.750   1.3541   0.01855   0.01204  -0.0947   0.0123   0.7427
   9.000   1.3775   0.01912   0.01265  -0.0939   0.0120   0.7449
   9.250   1.4001   0.01977   0.01337  -0.0930   0.0117   0.7472
   9.500   1.4216   0.02055   0.01425  -0.0919   0.0115   0.7496
   9.750   1.4433   0.02126   0.01503  -0.0909   0.0113   0.7518
  10.000   1.4653   0.02188   0.01573  -0.0899   0.0112   0.7540
  10.250   1.4868   0.02254   0.01647  -0.0888   0.0111   0.7560
  10.500   1.5077   0.02323   0.01726  -0.0877   0.0110   0.7581
  10.750   1.5279   0.02396   0.01810  -0.0865   0.0109   0.7603
  11.000   1.5472   0.02475   0.01899  -0.0851   0.0108   0.7626
  11.250   1.5658   0.02558   0.01992  -0.0837   0.0107   0.7651
  11.500   1.5836   0.02644   0.02088  -0.0821   0.0106   0.7677
  11.750   1.6003   0.02736   0.02190  -0.0804   0.0105   0.7701
  12.000   1.6160   0.02830   0.02296  -0.0786   0.0104   0.7722
  12.250   1.6302   0.02931   0.02409  -0.0766   0.0103   0.7744
  12.500   1.6429   0.03037   0.02527  -0.0744   0.0102   0.7766
  12.750   1.6536   0.03144   0.02646  -0.0719   0.0101   0.7790
  13.000   1.6605   0.03261   0.02775  -0.0689   0.0100   0.7815
  13.250   1.6628   0.03378   0.02904  -0.0651   0.0099   0.7841
  13.500   1.6657   0.03514   0.03051  -0.0617   0.0099   0.7865
  13.750   1.6684   0.03659   0.03208  -0.0586   0.0098   0.7887
  14.000   1.6705   0.03815   0.03376  -0.0557   0.0097   0.7912
  14.250   1.6708   0.03994   0.03568  -0.0530   0.0096   0.7938
  14.500   1.6701   0.04190   0.03777  -0.0505   0.0095   0.7963
  14.750   1.6673   0.04420   0.04020  -0.0482   0.0095   0.7987
  15.000   1.6619   0.04690   0.04302  -0.0463   0.0094   0.8008
  15.250   1.6533   0.05016   0.04642  -0.0449   0.0094   0.8025
  15.500   1.6424   0.05400   0.05042  -0.0442   0.0093   0.8044
  15.750   1.6267   0.05890   0.05550  -0.0447   0.0093   0.8062
  16.000   1.6059   0.06535   0.06214  -0.0469   0.0093   0.8079
  16.250   1.5745   0.07502   0.07205  -0.0525   0.0093   0.8094
  16.500   1.4951   0.09826   0.09571  -0.0686   0.0094   0.8089
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