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NASA SC(2)-0010 AIRFOIL (sc20010-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: NASA SC(2)-0010 AIRFOIL (sc20010-il)
Reynolds number: 1,000,000
Max Cl/Cd: 70.12 at α=8.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-sc20010-il-1000000-n5.txt
Download as CSV file: xf-sc20010-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NASA SC(2)-0010 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  -1.0395   0.14316   0.14108   0.0300   1.0000   0.0101
 -17.500  -1.1403   0.11693   0.11459   0.0154   1.0000   0.0099
 -17.250  -1.2108   0.09840   0.09585   0.0054   1.0000   0.0097
 -17.000  -1.2677   0.08210   0.07932  -0.0040   1.0000   0.0096
 -16.750  -1.3150   0.06778   0.06474  -0.0135   1.0000   0.0096
 -16.500  -1.3408   0.05908   0.05584  -0.0191   1.0000   0.0096
 -16.250  -1.3582   0.05293   0.04952  -0.0224   1.0000   0.0096
 -16.000  -1.3692   0.04828   0.04472  -0.0242   1.0000   0.0096
 -15.750  -1.3764   0.04449   0.04078  -0.0252   1.0000   0.0097
 -15.500  -1.3860   0.04069   0.03683  -0.0256   1.0000   0.0097
 -15.250  -1.3933   0.03745   0.03343  -0.0253   1.0000   0.0098
 -15.000  -1.3975   0.03478   0.03063  -0.0245   1.0000   0.0099
 -14.750  -1.3985   0.03261   0.02833  -0.0232   1.0000   0.0100
 -14.500  -1.3970   0.03080   0.02640  -0.0215   1.0000   0.0100
 -14.250  -1.3933   0.02930   0.02479  -0.0195   1.0000   0.0101
 -14.000  -1.3879   0.02803   0.02343  -0.0172   1.0000   0.0102
 -13.750  -1.3803   0.02694   0.02224  -0.0149   1.0000   0.0103
 -13.500  -1.3677   0.02592   0.02113  -0.0134   1.0000   0.0104
 -13.250  -1.3526   0.02500   0.02013  -0.0121   1.0000   0.0106
 -13.000  -1.3360   0.02415   0.01919  -0.0110   1.0000   0.0107
 -12.750  -1.3182   0.02334   0.01831  -0.0099   1.0000   0.0109
 -12.500  -1.2997   0.02255   0.01744  -0.0090   1.0000   0.0110
 -12.250  -1.2805   0.02177   0.01658  -0.0081   1.0000   0.0111
 -12.000  -1.2607   0.02101   0.01574  -0.0072   1.0000   0.0113
 -11.750  -1.2401   0.02030   0.01495  -0.0065   1.0000   0.0114
 -11.500  -1.2189   0.01961   0.01419  -0.0057   1.0000   0.0115
 -11.250  -1.1971   0.01896   0.01347  -0.0051   1.0000   0.0117
 -11.000  -1.1748   0.01834   0.01278  -0.0045   1.0000   0.0118
 -10.750  -1.1520   0.01775   0.01212  -0.0039   1.0000   0.0120
 -10.500  -1.1288   0.01720   0.01150  -0.0034   1.0000   0.0121
 -10.250  -1.1051   0.01668   0.01093  -0.0030   1.0000   0.0123
 -10.000  -1.0811   0.01618   0.01037  -0.0026   1.0000   0.0124
  -9.750  -1.0577   0.01556   0.00970  -0.0021   1.0000   0.0126
  -9.500  -1.0337   0.01501   0.00911  -0.0016   1.0000   0.0130
  -9.250  -1.0091   0.01453   0.00860  -0.0013   1.0000   0.0133
  -9.000  -0.9842   0.01409   0.00813  -0.0010   1.0000   0.0136
  -8.750  -0.9589   0.01369   0.00770  -0.0007   1.0000   0.0140
  -8.500  -0.9333   0.01332   0.00730  -0.0004   1.0000   0.0144
  -8.250  -0.9076   0.01296   0.00692  -0.0002   1.0000   0.0149
  -8.000  -0.8818   0.01262   0.00655   0.0000   1.0000   0.0152
  -7.750  -0.8558   0.01228   0.00619   0.0003   1.0000   0.0156
  -7.500  -0.8301   0.01190   0.00580   0.0005   1.0000   0.0164
  -7.250  -0.8040   0.01158   0.00547   0.0007   1.0000   0.0172
  -7.000  -0.7732   0.01127   0.00516  -0.0001   0.9886   0.0183
  -6.750  -0.7421   0.01098   0.00486  -0.0010   0.9752   0.0195
  -6.500  -0.7127   0.01069   0.00457  -0.0014   0.9580   0.0215
  -6.250  -0.6863   0.01049   0.00432  -0.0011   0.9367   0.0235
  -6.000  -0.6614   0.01028   0.00409  -0.0005   0.9142   0.0263
  -5.750  -0.6359   0.01012   0.00387   0.0001   0.8938   0.0289
  -5.500  -0.6098   0.00995   0.00366   0.0004   0.8764   0.0322
  -5.250  -0.5830   0.00980   0.00347   0.0006   0.8614   0.0351
  -5.000  -0.5560   0.00963   0.00329   0.0008   0.8484   0.0385
  -4.750  -0.5286   0.00951   0.00311   0.0009   0.8369   0.0407
  -4.500  -0.5011   0.00935   0.00294   0.0009   0.8264   0.0440
  -4.250  -0.4734   0.00920   0.00278   0.0010   0.8176   0.0471
  -4.000  -0.4455   0.00908   0.00263   0.0009   0.8093   0.0496
  -3.750  -0.4177   0.00892   0.00248   0.0009   0.8023   0.0551
  -3.500  -0.3896   0.00878   0.00234   0.0009   0.7956   0.0609
  -3.000  -0.3336   0.00847   0.00208   0.0008   0.7830   0.0783
  -2.750  -0.3055   0.00831   0.00197   0.0007   0.7766   0.0927
  -2.500  -0.2775   0.00815   0.00186   0.0006   0.7714   0.1108
  -2.250  -0.2493   0.00796   0.00175   0.0005   0.7665   0.1326
  -2.000  -0.2214   0.00775   0.00164   0.0004   0.7591   0.1664
  -1.750  -0.1936   0.00752   0.00154   0.0004   0.7503   0.2074
  -1.500  -0.1658   0.00729   0.00144   0.0003   0.7406   0.2527
  -1.250  -0.1382   0.00696   0.00134   0.0002   0.7344   0.3206
  -1.000  -0.1104   0.00661   0.00125   0.0000   0.7296   0.3948
  -0.500  -0.0563   0.00581   0.00107   0.0000   0.7088   0.5868
  -0.250  -0.0285   0.00563   0.00110   0.0000   0.6992   0.6589
   0.000   0.0000   0.00560   0.00111   0.0000   0.6879   0.6876
   0.250   0.0285   0.00563   0.00110   0.0000   0.6588   0.6993
   0.500   0.0563   0.00579   0.00107   0.0000   0.5905   0.7084
   1.000   0.1104   0.00661   0.00125   0.0000   0.3954   0.7296
   1.250   0.1381   0.00696   0.00134  -0.0002   0.3198   0.7345
   1.500   0.1657   0.00729   0.00144  -0.0003   0.2519   0.7406
   1.750   0.1935   0.00752   0.00154  -0.0003   0.2073   0.7505
   2.000   0.2213   0.00775   0.00164  -0.0004   0.1664   0.7593
   2.250   0.2492   0.00796   0.00175  -0.0005   0.1326   0.7664
   2.500   0.2774   0.00815   0.00186  -0.0006   0.1108   0.7714
   2.750   0.3055   0.00831   0.00197  -0.0007   0.0927   0.7766
   3.000   0.3335   0.00847   0.00208  -0.0008   0.0784   0.7829
   3.500   0.3896   0.00878   0.00234  -0.0009   0.0609   0.7955
   3.750   0.4177   0.00892   0.00248  -0.0009   0.0551   0.8023
   4.000   0.4455   0.00908   0.00263  -0.0009   0.0496   0.8092
   4.250   0.4734   0.00920   0.00278  -0.0010   0.0471   0.8176
   4.500   0.5011   0.00934   0.00294  -0.0009   0.0440   0.8264
   4.750   0.5286   0.00951   0.00311  -0.0009   0.0407   0.8369
   5.000   0.5560   0.00963   0.00329  -0.0008   0.0385   0.8484
   5.250   0.5830   0.00980   0.00347  -0.0006   0.0350   0.8614
   5.500   0.6097   0.00995   0.00366  -0.0004   0.0321   0.8764
   5.750   0.6359   0.01012   0.00387  -0.0001   0.0289   0.8938
   6.000   0.6614   0.01028   0.00409   0.0005   0.0263   0.9142
   6.250   0.6863   0.01048   0.00432   0.0011   0.0236   0.9368
   6.500   0.7127   0.01069   0.00457   0.0014   0.0216   0.9581
   6.750   0.7422   0.01098   0.00485   0.0010   0.0195   0.9753
   7.000   0.7732   0.01127   0.00516   0.0001   0.0183   0.9887
   7.250   0.8040   0.01157   0.00547  -0.0007   0.0172   1.0000
   7.500   0.8301   0.01190   0.00580  -0.0005   0.0164   1.0000
   7.750   0.8558   0.01228   0.00619  -0.0003   0.0156   1.0000
   8.000   0.8818   0.01262   0.00655   0.0000   0.0152   1.0000
   8.250   0.9076   0.01296   0.00692   0.0002   0.0149   1.0000
   8.500   0.9333   0.01331   0.00730   0.0004   0.0144   1.0000
   8.750   0.9589   0.01369   0.00770   0.0007   0.0140   1.0000
   9.000   0.9841   0.01409   0.00813   0.0010   0.0136   1.0000
   9.250   1.0091   0.01453   0.00860   0.0013   0.0133   1.0000
   9.500   1.0337   0.01501   0.00911   0.0016   0.0130   1.0000
   9.750   1.0577   0.01556   0.00970   0.0021   0.0126   1.0000
  10.000   1.0811   0.01618   0.01037   0.0026   0.0124   1.0000
  10.250   1.1051   0.01667   0.01092   0.0030   0.0123   1.0000
  10.500   1.1288   0.01720   0.01150   0.0034   0.0121   1.0000
  10.750   1.1521   0.01775   0.01212   0.0039   0.0120   1.0000
  11.000   1.1748   0.01834   0.01277   0.0045   0.0118   1.0000
  11.250   1.1972   0.01896   0.01347   0.0051   0.0117   1.0000
  11.500   1.2189   0.01961   0.01419   0.0057   0.0115   1.0000
  11.750   1.2401   0.02030   0.01495   0.0064   0.0114   1.0000
  12.000   1.2607   0.02102   0.01574   0.0072   0.0113   1.0000
  12.250   1.2806   0.02177   0.01657   0.0080   0.0111   1.0000
  12.500   1.2998   0.02254   0.01744   0.0089   0.0110   1.0000
  12.750   1.3185   0.02333   0.01830   0.0099   0.0108   1.0000
  13.000   1.3363   0.02414   0.01919   0.0109   0.0107   1.0000
  13.250   1.3530   0.02499   0.02011   0.0120   0.0106   1.0000
  13.500   1.3681   0.02592   0.02112   0.0133   0.0104   1.0000
  13.750   1.3808   0.02693   0.02223   0.0149   0.0103   1.0000
  14.000   1.3886   0.02803   0.02342   0.0171   0.0102   1.0000
  14.250   1.3940   0.02930   0.02479   0.0194   0.0101   1.0000
  14.500   1.3979   0.03080   0.02640   0.0214   0.0100   1.0000
  14.750   1.3993   0.03261   0.02832   0.0230   0.0099   1.0000
  15.000   1.3980   0.03481   0.03066   0.0244   0.0099   1.0000
  15.250   1.3941   0.03747   0.03345   0.0252   0.0098   1.0000
  15.500   1.3864   0.04076   0.03690   0.0254   0.0097   1.0000
  15.750   1.3780   0.04443   0.04073   0.0250   0.0097   1.0000
  16.000   1.3712   0.04819   0.04462   0.0240   0.0096   1.0000
  16.250   1.3598   0.05290   0.04949   0.0222   0.0096   1.0000
  16.500   1.3430   0.05897   0.05573   0.0189   0.0096   1.0000
  16.750   1.3177   0.06756   0.06452   0.0134   0.0096   1.0000
  17.000   1.2710   0.08180   0.07902   0.0038   0.0096   1.0000
  17.250   1.2120   0.09854   0.09599  -0.0058   0.0097   1.0000
  17.500   1.1416   0.11706   0.11473  -0.0158   0.0099   1.0000
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