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NASA SC(2)-0612 AIRFOIL (sc20612-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: NASA SC(2)-0612 AIRFOIL (sc20612-il)
Reynolds number: 1,000,000
Max Cl/Cd: 79.78 at α=7°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-sc20612-il-1000000-n5.txt
Download as CSV file: xf-sc20612-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NASA SC(2)-0612 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  -1.1290   0.11005   0.10708  -0.0293   1.0000   0.0141
 -19.500  -1.1804   0.09663   0.09345  -0.0366   1.0000   0.0140
 -19.250  -1.2201   0.08554   0.08217  -0.0428   1.0000   0.0140
 -19.000  -1.2492   0.07660   0.07306  -0.0479   1.0000   0.0140
 -18.750  -1.2700   0.06932   0.06562  -0.0520   1.0000   0.0140
 -18.500  -1.2849   0.06332   0.05949  -0.0553   1.0000   0.0141
 -18.250  -1.2949   0.05831   0.05435  -0.0579   1.0000   0.0141
 -18.000  -1.3017   0.05401   0.04995  -0.0600   1.0000   0.0142
 -17.750  -1.3056   0.05031   0.04615  -0.0616   1.0000   0.0143
 -17.500  -1.3071   0.04707   0.04282  -0.0628   1.0000   0.0144
 -17.250  -1.3067   0.04424   0.03990  -0.0637   1.0000   0.0145
 -17.000  -1.3049   0.04170   0.03728  -0.0643   1.0000   0.0146
 -16.750  -1.3018   0.03941   0.03491  -0.0647   1.0000   0.0147
 -16.500  -1.2971   0.03735   0.03276  -0.0650   1.0000   0.0149
 -16.250  -1.2912   0.03546   0.03080  -0.0651   1.0000   0.0150
 -16.000  -1.2842   0.03373   0.02899  -0.0651   1.0000   0.0152
 -15.750  -1.2761   0.03214   0.02734  -0.0649   1.0000   0.0153
 -15.500  -1.2673   0.03068   0.02581  -0.0647   1.0000   0.0155
 -15.250  -1.2581   0.02931   0.02438  -0.0643   1.0000   0.0156
 -15.000  -1.2486   0.02805   0.02305  -0.0637   1.0000   0.0158
 -14.750  -1.2393   0.02690   0.02185  -0.0628   1.0000   0.0159
 -14.500  -1.2316   0.02585   0.02073  -0.0614   1.0000   0.0161
 -14.250  -1.2271   0.02491   0.01974  -0.0593   1.0000   0.0162
 -14.000  -1.2279   0.02407   0.01886  -0.0560   1.0000   0.0163
 -13.750  -1.2208   0.02323   0.01797  -0.0541   1.0000   0.0164
 -13.500  -1.2122   0.02230   0.01699  -0.0526   1.0000   0.0166
 -13.250  -1.1870   0.02127   0.01591  -0.0542   0.9990   0.0170
 -13.000  -1.1594   0.02038   0.01499  -0.0560   0.9978   0.0174
 -12.750  -1.1307   0.01961   0.01418  -0.0578   0.9966   0.0178
 -12.500  -1.1015   0.01890   0.01344  -0.0596   0.9956   0.0182
 -12.250  -1.0714   0.01824   0.01274  -0.0613   0.9947   0.0187
 -12.000  -1.0407   0.01762   0.01207  -0.0632   0.9939   0.0191
 -11.750  -1.0099   0.01704   0.01145  -0.0649   0.9932   0.0195
 -11.500  -0.9809   0.01651   0.01088  -0.0661   0.9917   0.0198
 -11.250  -0.9515   0.01589   0.01024  -0.0675   0.9903   0.0204
 -11.000  -0.9210   0.01535   0.00968  -0.0690   0.9889   0.0211
 -10.750  -0.8897   0.01487   0.00918  -0.0705   0.9876   0.0217
 -10.500  -0.8579   0.01442   0.00872  -0.0720   0.9865   0.0224
 -10.250  -0.8261   0.01401   0.00828  -0.0735   0.9856   0.0231
 -10.000  -0.7940   0.01361   0.00786  -0.0750   0.9849   0.0238
  -9.750  -0.7616   0.01317   0.00743  -0.0766   0.9842   0.0250
  -9.500  -0.7289   0.01279   0.00704  -0.0782   0.9835   0.0262
  -9.250  -0.6961   0.01245   0.00669  -0.0798   0.9829   0.0275
  -9.000  -0.6633   0.01208   0.00634  -0.0814   0.9822   0.0293
  -8.750  -0.6339   0.01177   0.00603  -0.0821   0.9798   0.0312
  -8.500  -0.6029   0.01147   0.00574  -0.0832   0.9778   0.0332
  -8.250  -0.5712   0.01117   0.00547  -0.0844   0.9759   0.0359
  -8.000  -0.5390   0.01090   0.00520  -0.0856   0.9740   0.0383
  -7.750  -0.5066   0.01063   0.00496  -0.0870   0.9723   0.0415
  -7.500  -0.4739   0.01041   0.00474  -0.0882   0.9709   0.0437
  -7.250  -0.4410   0.01014   0.00449  -0.0896   0.9695   0.0463
  -7.000  -0.4110   0.00993   0.00430  -0.0903   0.9665   0.0487
  -6.750  -0.3804   0.00975   0.00411  -0.0911   0.9635   0.0506
  -6.500  -0.3487   0.00952   0.00389  -0.0921   0.9609   0.0533
  -6.250  -0.3169   0.00931   0.00371  -0.0932   0.9587   0.0558
  -6.000  -0.2850   0.00913   0.00353  -0.0942   0.9565   0.0582
  -5.750  -0.2539   0.00894   0.00336  -0.0950   0.9536   0.0619
  -5.500  -0.2232   0.00876   0.00321  -0.0958   0.9500   0.0659
  -5.250  -0.1921   0.00859   0.00306  -0.0966   0.9468   0.0707
  -5.000  -0.1606   0.00839   0.00291  -0.0975   0.9439   0.0795
  -4.500  -0.0976   0.00800   0.00265  -0.0994   0.9375   0.1033
  -4.250  -0.0662   0.00782   0.00252  -0.1003   0.9335   0.1187
  -4.000  -0.0343   0.00759   0.00239  -0.1013   0.9296   0.1405
  -3.750  -0.0021   0.00735   0.00226  -0.1024   0.9250   0.1710
  -3.500   0.0304   0.00706   0.00213  -0.1037   0.9179   0.2138
  -3.250   0.0635   0.00675   0.00199  -0.1050   0.9113   0.2667
  -3.000   0.0969   0.00644   0.00187  -0.1065   0.9047   0.3242
  -2.500   0.1635   0.00580   0.00159  -0.1093   0.8775   0.4560
  -2.250   0.1961   0.00556   0.00151  -0.1105   0.8547   0.5316
  -2.000   0.2261   0.00555   0.00151  -0.1108   0.8318   0.5682
  -1.750   0.2546   0.00566   0.00152  -0.1107   0.7958   0.5882
  -1.500   0.2822   0.00588   0.00155  -0.1105   0.7445   0.5995
  -1.250   0.3094   0.00619   0.00162  -0.1102   0.6792   0.6118
  -0.750   0.3598   0.00748   0.00198  -0.1093   0.4397   0.6283
  -0.500   0.3868   0.00792   0.00212  -0.1092   0.3627   0.6324
  -0.250   0.4142   0.00831   0.00224  -0.1091   0.2974   0.6364
   0.000   0.4418   0.00866   0.00237  -0.1091   0.2419   0.6399
   0.250   0.4698   0.00894   0.00250  -0.1091   0.2024   0.6428
   0.500   0.4978   0.00921   0.00263  -0.1091   0.1664   0.6452
   0.750   0.5258   0.00947   0.00276  -0.1091   0.1365   0.6477
   1.000   0.5541   0.00969   0.00288  -0.1091   0.1177   0.6499
   1.250   0.5825   0.00988   0.00301  -0.1092   0.1032   0.6518
   1.500   0.6108   0.01010   0.00314  -0.1092   0.0891   0.6538
   1.750   0.6390   0.01030   0.00328  -0.1092   0.0779   0.6560
   2.000   0.6672   0.01049   0.00343  -0.1092   0.0698   0.6584
   2.250   0.6953   0.01068   0.00359  -0.1091   0.0642   0.6606
   2.500   0.7236   0.01085   0.00375  -0.1091   0.0609   0.6626
   2.750   0.7518   0.01102   0.00391  -0.1091   0.0580   0.6645
   3.000   0.7797   0.01123   0.00408  -0.1090   0.0547   0.6663
   3.250   0.8078   0.01141   0.00425  -0.1089   0.0526   0.6681
   3.500   0.8358   0.01159   0.00443  -0.1089   0.0507   0.6697
   3.750   0.8635   0.01180   0.00461  -0.1087   0.0484   0.6711
   4.000   0.8911   0.01201   0.00482  -0.1086   0.0460   0.6731
   4.250   0.9189   0.01219   0.00502  -0.1085   0.0440   0.6750
   4.500   0.9463   0.01241   0.00523  -0.1083   0.0414   0.6769
   4.750   0.9736   0.01264   0.00545  -0.1081   0.0392   0.6790
   5.000   1.0008   0.01286   0.00568  -0.1079   0.0368   0.6812
   5.250   1.0277   0.01313   0.00592  -0.1076   0.0340   0.6833
   5.500   1.0546   0.01338   0.00617  -0.1074   0.0318   0.6853
   5.750   1.0811   0.01368   0.00644  -0.1070   0.0295   0.6870
   6.000   1.1077   0.01395   0.00672  -0.1067   0.0281   0.6886
   6.250   1.1340   0.01424   0.00702  -0.1063   0.0268   0.6906
   6.500   1.1600   0.01457   0.00735  -0.1059   0.0254   0.6927
   6.750   1.1860   0.01488   0.00769  -0.1055   0.0245   0.6947
   7.000   1.2118   0.01519   0.00804  -0.1050   0.0238   0.6966
   7.250   1.2374   0.01553   0.00839  -0.1045   0.0230   0.6986
   7.500   1.2626   0.01590   0.00877  -0.1040   0.0222   0.7006
   7.750   1.2874   0.01631   0.00920  -0.1034   0.0214   0.7026
   8.000   1.3123   0.01669   0.00960  -0.1028   0.0208   0.7044
   8.250   1.3371   0.01705   0.00999  -0.1022   0.0203   0.7061
   8.750   1.3858   0.01784   0.01086  -0.1008   0.0194   0.7098
   9.000   1.4095   0.01826   0.01133  -0.1000   0.0189   0.7119
   9.250   1.4329   0.01872   0.01182  -0.0992   0.0185   0.7142
   9.500   1.4556   0.01923   0.01236  -0.0983   0.0180   0.7166
   9.750   1.4774   0.01981   0.01299  -0.0972   0.0176   0.7190
  10.000   1.5000   0.02028   0.01351  -0.0962   0.0174   0.7214
  10.250   1.5220   0.02076   0.01405  -0.0952   0.0171   0.7236
  10.500   1.5435   0.02128   0.01462  -0.0941   0.0169   0.7257
  10.750   1.5645   0.02181   0.01521  -0.0929   0.0166   0.7280
  11.000   1.5848   0.02236   0.01583  -0.0916   0.0164   0.7303
  11.250   1.6045   0.02294   0.01647  -0.0902   0.0161   0.7327
  11.500   1.6235   0.02355   0.01714  -0.0887   0.0159   0.7351
  11.750   1.6415   0.02418   0.01783  -0.0871   0.0156   0.7376
  12.000   1.6581   0.02484   0.01856  -0.0853   0.0154   0.7400
  12.250   1.6732   0.02555   0.01932  -0.0832   0.0152   0.7424
  12.500   1.6865   0.02631   0.02014  -0.0809   0.0150   0.7445
  12.750   1.6953   0.02712   0.02104  -0.0777   0.0148   0.7469
  13.000   1.7036   0.02813   0.02213  -0.0748   0.0145   0.7494
  13.250   1.7137   0.02906   0.02314  -0.0721   0.0144   0.7520
  13.500   1.7242   0.02998   0.02415  -0.0697   0.0143   0.7548
  13.750   1.7337   0.03099   0.02526  -0.0673   0.0142   0.7575
  14.000   1.7422   0.03210   0.02647  -0.0648   0.0141   0.7600
  14.250   1.7499   0.03331   0.02776  -0.0624   0.0140   0.7623
  14.500   1.7566   0.03462   0.02917  -0.0601   0.0139   0.7646
  14.750   1.7622   0.03605   0.03072  -0.0578   0.0138   0.7671
  15.000   1.7666   0.03763   0.03240  -0.0556   0.0137   0.7697
  15.250   1.7701   0.03935   0.03423  -0.0535   0.0136   0.7724
  15.500   1.7724   0.04124   0.03623  -0.0516   0.0135   0.7751
  15.750   1.7732   0.04335   0.03844  -0.0498   0.0134   0.7776
  16.000   1.7727   0.04569   0.04090  -0.0482   0.0133   0.7799
  16.250   1.7707   0.04831   0.04365  -0.0469   0.0132   0.7823
  16.500   1.7666   0.05128   0.04674  -0.0460   0.0131   0.7849
  16.750   1.7605   0.05466   0.05026  -0.0454   0.0130   0.7875
  17.000   1.7525   0.05851   0.05424  -0.0453   0.0130   0.7901
  17.250   1.7415   0.06304   0.05892  -0.0459   0.0129   0.7924
  17.500   1.7268   0.06850   0.06454  -0.0474   0.0129   0.7945
  17.750   1.7077   0.07522   0.07142  -0.0502   0.0128   0.7963
  18.250   1.6394   0.09612   0.09277  -0.0617   0.0128   0.7985
  18.500   1.5687   0.11482   0.11178  -0.0730   0.0129   0.7978
  18.750   1.4601   0.14186   0.13918  -0.0899   0.0131   0.7953
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