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NASA SC(2)-0012 AIRFOIL (sc20012-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: NASA SC(2)-0012 AIRFOIL (sc20012-il)
Reynolds number: 500,000
Max Cl/Cd: 58.59 at α=9°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-sc20012-il-500000-n5.txt
Download as CSV file: xf-sc20012-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NASA SC(2)-0012 AIRFOIL                         
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.500 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -18.250  -1.0927   0.12691   0.12365   0.0111   1.0000   0.0157
 -18.000  -1.1348   0.11395   0.11052   0.0038   1.0000   0.0156
 -17.750  -1.1741   0.10192   0.09831  -0.0030   1.0000   0.0156
 -17.500  -1.2078   0.09104   0.08723  -0.0092   1.0000   0.0155
 -17.250  -1.2359   0.08145   0.07745  -0.0149   1.0000   0.0155
 -17.000  -1.2579   0.07332   0.06913  -0.0197   1.0000   0.0155
 -16.750  -1.2753   0.06654   0.06218  -0.0234   1.0000   0.0156
 -16.500  -1.2891   0.06089   0.05636  -0.0262   1.0000   0.0156
 -16.250  -1.2995   0.05613   0.05144  -0.0281   1.0000   0.0156
 -16.000  -1.3072   0.05208   0.04723  -0.0293   1.0000   0.0157
 -15.750  -1.3122   0.04856   0.04356  -0.0299   1.0000   0.0158
 -15.500  -1.3149   0.04548   0.04034  -0.0302   1.0000   0.0158
 -15.250  -1.3177   0.04253   0.03727  -0.0302   1.0000   0.0159
 -15.000  -1.3193   0.03984   0.03447  -0.0299   1.0000   0.0161
 -14.750  -1.3185   0.03750   0.03202  -0.0294   1.0000   0.0162
 -14.500  -1.3154   0.03545   0.02988  -0.0286   1.0000   0.0163
 -14.250  -1.3105   0.03365   0.02799  -0.0277   1.0000   0.0165
 -14.000  -1.3041   0.03205   0.02630  -0.0266   1.0000   0.0167
 -13.750  -1.2964   0.03063   0.02478  -0.0254   1.0000   0.0169
 -13.500  -1.2875   0.02935   0.02341  -0.0241   1.0000   0.0171
 -13.250  -1.2777   0.02817   0.02214  -0.0226   1.0000   0.0173
 -13.000  -1.2672   0.02710   0.02098  -0.0210   1.0000   0.0175
 -12.750  -1.2560   0.02612   0.01991  -0.0193   1.0000   0.0178
 -12.500  -1.2443   0.02522   0.01893  -0.0174   1.0000   0.0181
 -12.250  -1.2318   0.02440   0.01802  -0.0155   1.0000   0.0184
 -12.000  -1.2166   0.02361   0.01714  -0.0140   1.0000   0.0187
 -11.750  -1.1995   0.02287   0.01632  -0.0128   1.0000   0.0190
 -11.500  -1.1826   0.02205   0.01547  -0.0115   1.0000   0.0194
 -11.250  -1.1638   0.02136   0.01474  -0.0105   1.0000   0.0200
 -11.000  -1.1438   0.02073   0.01406  -0.0095   1.0000   0.0206
 -10.750  -1.1233   0.02013   0.01341  -0.0087   1.0000   0.0213
 -10.500  -1.1022   0.01955   0.01276  -0.0079   1.0000   0.0219
 -10.250  -1.0808   0.01897   0.01213  -0.0071   1.0000   0.0226
 -10.000  -1.0591   0.01840   0.01154  -0.0064   1.0000   0.0235
  -9.750  -1.0366   0.01789   0.01102  -0.0057   1.0000   0.0245
  -9.500  -1.0137   0.01742   0.01050  -0.0051   1.0000   0.0256
  -9.250  -0.9906   0.01695   0.01000  -0.0045   1.0000   0.0268
  -9.000  -0.9672   0.01651   0.00956  -0.0039   1.0000   0.0282
  -8.750  -0.9434   0.01611   0.00914  -0.0034   1.0000   0.0297
  -8.500  -0.9195   0.01572   0.00871  -0.0029   1.0000   0.0312
  -8.250  -0.8956   0.01534   0.00835  -0.0024   1.0000   0.0329
  -8.000  -0.8713   0.01501   0.00800  -0.0019   1.0000   0.0347
  -7.750  -0.8421   0.01465   0.00762  -0.0025   0.9910   0.0366
  -7.500  -0.8109   0.01430   0.00728  -0.0035   0.9777   0.0388
  -7.250  -0.7799   0.01401   0.00695  -0.0044   0.9629   0.0410
  -7.000  -0.7509   0.01366   0.00659  -0.0048   0.9459   0.0430
  -6.750  -0.7242   0.01339   0.00629  -0.0047   0.9273   0.0450
  -6.500  -0.6990   0.01317   0.00600  -0.0041   0.9088   0.0470
  -6.250  -0.6744   0.01292   0.00570  -0.0035   0.8916   0.0491
  -6.000  -0.6494   0.01268   0.00543  -0.0029   0.8765   0.0519
  -5.500  -0.5978   0.01224   0.00490  -0.0021   0.8523   0.0577
  -5.250  -0.5717   0.01202   0.00465  -0.0018   0.8428   0.0607
  -5.000  -0.5448   0.01182   0.00441  -0.0016   0.8340   0.0635
  -4.500  -0.4913   0.01138   0.00395  -0.0013   0.8198   0.0725
  -4.250  -0.4643   0.01116   0.00374  -0.0012   0.8134   0.0790
  -4.000  -0.4372   0.01095   0.00355  -0.0011   0.8079   0.0879
  -3.750  -0.4099   0.01073   0.00337  -0.0010   0.8030   0.1003
  -3.500  -0.3824   0.01050   0.00320  -0.0010   0.7982   0.1151
  -3.250  -0.3551   0.01028   0.00304  -0.0010   0.7938   0.1329
  -3.000  -0.3280   0.01002   0.00288  -0.0009   0.7896   0.1595
  -2.750  -0.3009   0.00972   0.00272  -0.0009   0.7853   0.1951
  -2.500  -0.2738   0.00940   0.00257  -0.0009   0.7807   0.2387
  -2.250  -0.2472   0.00901   0.00241  -0.0009   0.7766   0.2967
  -2.000  -0.2211   0.00853   0.00224  -0.0008   0.7731   0.3775
  -1.750  -0.1953   0.00804   0.00207  -0.0006   0.7699   0.4661
  -1.500  -0.1700   0.00750   0.00198  -0.0003   0.7664   0.5738
  -1.250  -0.1428   0.00733   0.00204  -0.0001   0.7613   0.6419
  -1.000  -0.1144   0.00731   0.00205   0.0000   0.7545   0.6670
  -0.750  -0.0860   0.00731   0.00206   0.0000   0.7477   0.6877
  -0.500  -0.0574   0.00729   0.00208   0.0000   0.7400   0.7038
  -0.250  -0.0287   0.00732   0.00206   0.0000   0.7321   0.7139
   0.000   0.0000   0.00729   0.00207   0.0000   0.7234   0.7234
   0.250   0.0287   0.00732   0.00206   0.0000   0.7138   0.7322
   0.500   0.0574   0.00729   0.00208   0.0000   0.7037   0.7401
   0.750   0.0860   0.00731   0.00206   0.0000   0.6883   0.7478
   1.000   0.1144   0.00731   0.00205   0.0000   0.6672   0.7547
   1.250   0.1427   0.00733   0.00204   0.0001   0.6414   0.7615
   1.500   0.1700   0.00750   0.00198   0.0003   0.5739   0.7664
   1.750   0.1953   0.00804   0.00207   0.0006   0.4663   0.7699
   2.000   0.2211   0.00853   0.00224   0.0008   0.3778   0.7731
   2.250   0.2472   0.00901   0.00241   0.0009   0.2969   0.7766
   2.500   0.2738   0.00940   0.00257   0.0009   0.2389   0.7807
   2.750   0.3009   0.00972   0.00272   0.0009   0.1950   0.7853
   3.000   0.3280   0.01002   0.00288   0.0009   0.1596   0.7896
   3.250   0.3551   0.01028   0.00304   0.0010   0.1326   0.7938
   3.500   0.3825   0.01050   0.00320   0.0010   0.1151   0.7982
   3.750   0.4099   0.01073   0.00337   0.0010   0.1002   0.8030
   4.000   0.4372   0.01096   0.00355   0.0011   0.0879   0.8079
   4.250   0.4643   0.01115   0.00374   0.0012   0.0790   0.8134
   4.500   0.4913   0.01138   0.00395   0.0013   0.0725   0.8198
   5.000   0.5449   0.01182   0.00441   0.0016   0.0635   0.8340
   5.250   0.5717   0.01202   0.00465   0.0018   0.0607   0.8428
   5.500   0.5978   0.01224   0.00490   0.0021   0.0576   0.8523
   6.000   0.6494   0.01268   0.00543   0.0029   0.0519   0.8765
   6.250   0.6744   0.01292   0.00570   0.0034   0.0491   0.8916
   6.500   0.6991   0.01316   0.00600   0.0041   0.0469   0.9087
   6.750   0.7243   0.01339   0.00629   0.0047   0.0450   0.9273
   7.000   0.7510   0.01366   0.00659   0.0048   0.0430   0.9459
   7.250   0.7799   0.01400   0.00694   0.0044   0.0409   0.9630
   7.500   0.8110   0.01430   0.00728   0.0035   0.0388   0.9778
   7.750   0.8422   0.01465   0.00762   0.0025   0.0366   0.9911
   8.000   0.8714   0.01501   0.00800   0.0019   0.0347   1.0000
   8.250   0.8956   0.01534   0.00835   0.0024   0.0329   1.0000
   8.500   0.9196   0.01572   0.00871   0.0029   0.0312   1.0000
   8.750   0.9435   0.01611   0.00914   0.0034   0.0297   1.0000
   9.000   0.9673   0.01651   0.00956   0.0039   0.0282   1.0000
   9.250   0.9907   0.01695   0.00999   0.0045   0.0268   1.0000
   9.500   1.0138   0.01742   0.01050   0.0051   0.0256   1.0000
   9.750   1.0367   0.01789   0.01102   0.0057   0.0245   1.0000
  10.000   1.0593   0.01840   0.01154   0.0063   0.0235   1.0000
  10.250   1.0809   0.01897   0.01213   0.0071   0.0226   1.0000
  10.500   1.1024   0.01955   0.01276   0.0078   0.0219   1.0000
  10.750   1.1234   0.02013   0.01341   0.0087   0.0212   1.0000
  11.000   1.1440   0.02073   0.01406   0.0095   0.0206   1.0000
  11.250   1.1640   0.02136   0.01474   0.0104   0.0200   1.0000
  11.500   1.1829   0.02205   0.01546   0.0114   0.0194   1.0000
  11.750   1.1998   0.02287   0.01632   0.0127   0.0190   1.0000
  12.000   1.2169   0.02361   0.01714   0.0139   0.0187   1.0000
  12.250   1.2323   0.02440   0.01802   0.0154   0.0183   1.0000
  12.500   1.2448   0.02522   0.01893   0.0173   0.0181   1.0000
  12.750   1.2566   0.02612   0.01991   0.0192   0.0178   1.0000
  13.000   1.2678   0.02710   0.02098   0.0209   0.0175   1.0000
  13.250   1.2784   0.02817   0.02214   0.0225   0.0173   1.0000
  13.500   1.2882   0.02934   0.02340   0.0239   0.0171   1.0000
  13.750   1.2972   0.03062   0.02477   0.0253   0.0169   1.0000
  14.000   1.3050   0.03204   0.02629   0.0265   0.0167   1.0000
  14.250   1.3115   0.03364   0.02798   0.0275   0.0165   1.0000
  14.500   1.3164   0.03543   0.02986   0.0285   0.0163   1.0000
  14.750   1.3195   0.03748   0.03201   0.0292   0.0162   1.0000
  15.000   1.3205   0.03981   0.03445   0.0297   0.0161   1.0000
  15.250   1.3190   0.04250   0.03724   0.0300   0.0159   1.0000
  15.500   1.3163   0.04544   0.04030   0.0300   0.0158   1.0000
  15.750   1.3137   0.04851   0.04352   0.0297   0.0158   1.0000
  16.000   1.3089   0.05202   0.04718   0.0290   0.0157   1.0000
  16.250   1.3013   0.05607   0.05137   0.0279   0.0156   1.0000
  16.500   1.2909   0.06083   0.05630   0.0260   0.0156   1.0000
  16.750   1.2772   0.06647   0.06211   0.0232   0.0156   1.0000
  17.000   1.2599   0.07324   0.06905   0.0194   0.0155   1.0000
  17.250   1.2379   0.08139   0.07739   0.0146   0.0155   1.0000
  17.500   1.2099   0.09097   0.08716   0.0090   0.0155   1.0000
  17.750   1.1761   0.10189   0.09828   0.0027   0.0156   1.0000
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