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NASA SC(2)-0010 AIRFOIL (sc20010-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: NASA SC(2)-0010 AIRFOIL (sc20010-il)
Reynolds number: 1,000,000
Max Cl/Cd: 67.71 at α=7.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-sc20010-il-1000000.txt
Download as CSV file: xf-sc20010-il-1000000.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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -15.750  -1.1585   0.08015   0.07779  -0.0061   1.0000   0.0133
 -15.500  -1.2086   0.06522   0.06254  -0.0169   1.0000   0.0132
 -15.250  -1.2335   0.05728   0.05438  -0.0218   1.0000   0.0131
 -15.000  -1.2499   0.05167   0.04860  -0.0245   1.0000   0.0132
 -14.750  -1.2623   0.04713   0.04389  -0.0259   1.0000   0.0132
 -14.500  -1.2707   0.04343   0.04005  -0.0265   1.0000   0.0133
 -14.250  -1.2764   0.04034   0.03681  -0.0264   1.0000   0.0133
 -14.000  -1.2791   0.03779   0.03413  -0.0257   1.0000   0.0134
 -13.750  -1.2808   0.03554   0.03174  -0.0244   1.0000   0.0135
 -13.500  -1.2804   0.03364   0.02971  -0.0227   1.0000   0.0136
 -13.250  -1.2786   0.03199   0.02794  -0.0204   1.0000   0.0137
 -13.000  -1.2754   0.03057   0.02639  -0.0179   1.0000   0.0138
 -12.750  -1.2674   0.02922   0.02492  -0.0158   1.0000   0.0140
 -12.500  -1.2558   0.02791   0.02347  -0.0143   1.0000   0.0141
 -12.250  -1.2422   0.02668   0.02212  -0.0128   1.0000   0.0143
 -12.000  -1.2270   0.02552   0.02084  -0.0116   1.0000   0.0145
 -11.750  -1.2099   0.02448   0.01969  -0.0105   1.0000   0.0147
 -11.500  -1.1913   0.02357   0.01867  -0.0095   1.0000   0.0149
 -11.250  -1.1716   0.02273   0.01772  -0.0086   1.0000   0.0151
 -11.000  -1.1514   0.02189   0.01678  -0.0078   1.0000   0.0153
 -10.750  -1.1305   0.02108   0.01587  -0.0071   1.0000   0.0154
 -10.500  -1.1088   0.02034   0.01505  -0.0064   1.0000   0.0155
 -10.250  -1.0922   0.01872   0.01328  -0.0051   1.0000   0.0158
 -10.000  -1.0721   0.01766   0.01213  -0.0042   1.0000   0.0162
  -9.750  -1.0499   0.01689   0.01131  -0.0035   1.0000   0.0165
  -9.500  -1.0265   0.01627   0.01065  -0.0030   1.0000   0.0168
  -9.250  -1.0026   0.01570   0.01003  -0.0026   1.0000   0.0172
  -9.000  -0.9783   0.01517   0.00945  -0.0021   1.0000   0.0175
  -8.750  -0.9538   0.01466   0.00890  -0.0017   1.0000   0.0180
  -8.500  -0.9289   0.01417   0.00837  -0.0014   1.0000   0.0184
  -8.250  -0.9037   0.01374   0.00788  -0.0010   1.0000   0.0188
  -8.000  -0.8782   0.01334   0.00744  -0.0007   1.0000   0.0192
  -7.750  -0.8543   0.01265   0.00673  -0.0002   1.0000   0.0203
  -7.500  -0.8288   0.01224   0.00632   0.0001   1.0000   0.0211
  -7.250  -0.8029   0.01189   0.00594   0.0003   1.0000   0.0220
  -7.000  -0.7768   0.01157   0.00560   0.0006   1.0000   0.0230
  -6.750  -0.7515   0.01112   0.00515   0.0009   1.0000   0.0249
  -6.500  -0.7255   0.01082   0.00486   0.0012   1.0000   0.0271
  -6.250  -0.6999   0.01049   0.00455   0.0016   1.0000   0.0303
  -6.000  -0.6742   0.01028   0.00436   0.0019   1.0000   0.0336
  -5.750  -0.6493   0.00999   0.00412   0.0024   0.9999   0.0376
  -5.500  -0.6142   0.00982   0.00394   0.0007   0.9954   0.0407
  -5.250  -0.5805   0.00951   0.00368  -0.0008   0.9881   0.0455
  -5.000  -0.5469   0.00935   0.00351  -0.0021   0.9781   0.0486
  -4.750  -0.5162   0.00910   0.00327  -0.0028   0.9634   0.0528
  -4.500  -0.4892   0.00894   0.00310  -0.0025   0.9440   0.0566
  -4.250  -0.4639   0.00885   0.00295  -0.0018   0.9237   0.0590
  -4.000  -0.4385   0.00865   0.00274  -0.0012   0.9047   0.0655
  -3.750  -0.4120   0.00854   0.00258  -0.0008   0.8879   0.0712
  -3.250  -0.3585   0.00811   0.00225  -0.0004   0.8599   0.1081
  -3.000  -0.3314   0.00787   0.00210  -0.0003   0.8485   0.1393
  -2.750  -0.3048   0.00754   0.00194  -0.0002   0.8387   0.1908
  -2.500  -0.2777   0.00715   0.00178  -0.0002   0.8305   0.2580
  -2.250  -0.2515   0.00666   0.00162  -0.0001   0.8225   0.3558
  -2.000  -0.2257   0.00599   0.00144  -0.0001   0.8142   0.4907
  -1.750  -0.2001   0.00549   0.00135   0.0002   0.8050   0.6178
  -1.500  -0.1719   0.00538   0.00135   0.0003   0.7956   0.6617
  -1.250  -0.1435   0.00538   0.00134   0.0003   0.7886   0.6838
  -1.000  -0.1145   0.00534   0.00134   0.0001   0.7834   0.6982
  -0.750  -0.0857   0.00534   0.00132   0.0000   0.7757   0.7085
  -0.500  -0.0570   0.00535   0.00132   0.0000   0.7655   0.7208
  -0.250  -0.0286   0.00534   0.00132   0.0000   0.7572   0.7346
   0.000   0.0000   0.00531   0.00134   0.0000   0.7493   0.7491
   0.250   0.0285   0.00534   0.00132   0.0000   0.7346   0.7572
   0.500   0.0570   0.00535   0.00132   0.0000   0.7211   0.7653
   0.750   0.0857   0.00534   0.00133   0.0000   0.7087   0.7758
   1.000   0.1145   0.00534   0.00134  -0.0001   0.6983   0.7834
   1.250   0.1435   0.00538   0.00134  -0.0002   0.6837   0.7887
   1.500   0.1719   0.00539   0.00135  -0.0002   0.6614   0.7957
   1.750   0.2001   0.00549   0.00135  -0.0002   0.6176   0.8052
   2.000   0.2257   0.00599   0.00144   0.0001   0.4901   0.8143
   2.250   0.2515   0.00666   0.00162   0.0001   0.3558   0.8225
   2.500   0.2777   0.00715   0.00178   0.0002   0.2581   0.8305
   2.750   0.3048   0.00754   0.00194   0.0002   0.1907   0.8387
   3.000   0.3314   0.00787   0.00210   0.0003   0.1394   0.8485
   3.250   0.3585   0.00811   0.00225   0.0004   0.1081   0.8600
   3.750   0.4120   0.00854   0.00258   0.0008   0.0712   0.8879
   4.000   0.4385   0.00865   0.00274   0.0012   0.0655   0.9048
   4.250   0.4639   0.00885   0.00295   0.0018   0.0590   0.9238
   4.500   0.4892   0.00894   0.00310   0.0025   0.0566   0.9441
   4.750   0.5162   0.00910   0.00327   0.0028   0.0528   0.9635
   5.000   0.5469   0.00935   0.00351   0.0021   0.0486   0.9781
   5.250   0.5805   0.00951   0.00368   0.0008   0.0454   0.9881
   5.500   0.6142   0.00982   0.00394  -0.0007   0.0407   0.9954
   5.750   0.6494   0.00999   0.00412  -0.0024   0.0375   0.9999
   6.000   0.6742   0.01028   0.00436  -0.0019   0.0336   1.0000
   6.250   0.6999   0.01049   0.00455  -0.0016   0.0304   1.0000
   6.500   0.7255   0.01083   0.00487  -0.0012   0.0272   1.0000
   6.750   0.7515   0.01112   0.00515  -0.0009   0.0249   1.0000
   7.000   0.7768   0.01157   0.00560  -0.0006   0.0230   1.0000
   7.250   0.8029   0.01189   0.00594  -0.0003   0.0221   1.0000
   7.500   0.8288   0.01224   0.00632  -0.0001   0.0211   1.0000
   7.750   0.8544   0.01265   0.00673   0.0002   0.0203   1.0000
   8.000   0.8782   0.01333   0.00744   0.0007   0.0192   1.0000
   8.250   0.9037   0.01374   0.00789   0.0010   0.0188   1.0000
   8.500   0.9290   0.01417   0.00837   0.0014   0.0184   1.0000
   8.750   0.9538   0.01465   0.00890   0.0017   0.0180   1.0000
   9.000   0.9784   0.01516   0.00945   0.0021   0.0175   1.0000
   9.250   1.0027   0.01570   0.01003   0.0026   0.0171   1.0000
   9.500   1.0266   0.01627   0.01064   0.0030   0.0168   1.0000
   9.750   1.0499   0.01689   0.01131   0.0035   0.0165   1.0000
  10.000   1.0721   0.01766   0.01214   0.0042   0.0162   1.0000
  10.250   1.0922   0.01872   0.01328   0.0051   0.0158   1.0000
  10.500   1.1088   0.02035   0.01506   0.0064   0.0155   1.0000
  10.750   1.1306   0.02108   0.01588   0.0071   0.0154   1.0000
  11.000   1.1515   0.02189   0.01678   0.0078   0.0153   1.0000
  11.250   1.1717   0.02272   0.01771   0.0086   0.0151   1.0000
  11.500   1.1915   0.02356   0.01866   0.0095   0.0149   1.0000
  11.750   1.2101   0.02448   0.01968   0.0104   0.0147   1.0000
  12.000   1.2270   0.02553   0.02085   0.0116   0.0145   1.0000
  12.250   1.2424   0.02668   0.02212   0.0128   0.0143   1.0000
  12.500   1.2560   0.02791   0.02347   0.0142   0.0141   1.0000
  12.750   1.2677   0.02921   0.02491   0.0158   0.0140   1.0000
  13.000   1.2758   0.03056   0.02638   0.0178   0.0138   1.0000
  13.250   1.2791   0.03199   0.02793   0.0204   0.0137   1.0000
  13.500   1.2810   0.03362   0.02970   0.0226   0.0136   1.0000
  13.750   1.2817   0.03550   0.03170   0.0243   0.0135   1.0000
  14.000   1.2804   0.03772   0.03406   0.0255   0.0134   1.0000
  14.250   1.2774   0.04030   0.03677   0.0262   0.0133   1.0000
  14.500   1.2722   0.04334   0.03996   0.0264   0.0133   1.0000
  14.750   1.2636   0.04707   0.04384   0.0258   0.0132   1.0000
  15.000   1.2520   0.05151   0.04843   0.0244   0.0132   1.0000
  15.250   1.2347   0.05726   0.05436   0.0217   0.0131   1.0000
  15.500   1.2103   0.06514   0.06245   0.0167   0.0132   1.0000
  15.750   1.1617   0.07975   0.07738   0.0062   0.0133   1.0000
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