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S9033 (7.5%) (s9033-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: S9033 (7.5%) (s9033-il)
Reynolds number: 1,000,000
Max Cl/Cd: 70.67 at α=6.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-s9033-il-1000000.txt
Download as CSV file: xf-s9033-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: S9033 (7.5%)                                    
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -16.250  -0.9810   0.13549   0.13368   0.0366   1.0000   0.0064
 -16.000  -1.0357   0.11786   0.11591   0.0262   1.0000   0.0061
 -15.750  -1.0961   0.10091   0.09881   0.0159   1.0000   0.0056
 -15.500  -1.1974   0.07765   0.07527   0.0015   1.0000   0.0046
 -15.250  -1.2215   0.06909   0.06660  -0.0035   1.0000   0.0043
 -15.000  -1.2912   0.05029   0.04751  -0.0173   1.0000   0.0040
 -14.750  -1.3184   0.04157   0.03857  -0.0247   1.0000   0.0040
 -14.500  -1.3315   0.03738   0.03422  -0.0268   1.0000   0.0041
 -14.250  -1.3485   0.03420   0.03088  -0.0258   1.0000   0.0041
 -14.000  -1.3529   0.03245   0.02901  -0.0233   1.0000   0.0042
 -13.750  -1.3574   0.03001   0.02636  -0.0211   1.0000   0.0043
 -13.500  -1.3548   0.02771   0.02388  -0.0195   1.0000   0.0048
 -13.250  -1.3410   0.02641   0.02249  -0.0185   1.0000   0.0052
 -13.000  -1.3238   0.02541   0.02143  -0.0177   1.0000   0.0056
 -12.750  -1.3044   0.02464   0.02057  -0.0170   1.0000   0.0060
 -12.500  -1.2843   0.02389   0.01973  -0.0163   1.0000   0.0064
 -12.250  -1.2684   0.02250   0.01822  -0.0154   1.0000   0.0072
 -12.000  -1.2456   0.02204   0.01776  -0.0149   1.0000   0.0078
 -11.750  -1.2220   0.02168   0.01739  -0.0145   1.0000   0.0084
 -11.500  -1.1987   0.02125   0.01690  -0.0141   1.0000   0.0090
 -11.250  -1.1746   0.02091   0.01651  -0.0137   1.0000   0.0094
 -11.000  -1.1494   0.02074   0.01631  -0.0134   1.0000   0.0097
 -10.750  -1.1335   0.01898   0.01434  -0.0123   1.0000   0.0106
 -10.500  -1.1110   0.01828   0.01359  -0.0118   1.0000   0.0112
 -10.250  -1.0868   0.01786   0.01314  -0.0114   1.0000   0.0118
 -10.000  -1.0627   0.01739   0.01262  -0.0109   1.0000   0.0123
  -9.750  -1.0385   0.01690   0.01207  -0.0105   1.0000   0.0129
  -9.500  -1.0141   0.01643   0.01153  -0.0100   1.0000   0.0134
  -9.250  -0.9889   0.01609   0.01115  -0.0097   1.0000   0.0138
  -9.000  -0.9628   0.01593   0.01094  -0.0094   1.0000   0.0141
  -8.750  -0.9432   0.01439   0.00921  -0.0084   1.0000   0.0155
  -8.500  -0.9184   0.01392   0.00873  -0.0080   1.0000   0.0167
  -8.250  -0.8931   0.01353   0.00832  -0.0076   1.0000   0.0175
  -8.000  -0.8679   0.01309   0.00783  -0.0072   1.0000   0.0183
  -7.750  -0.8428   0.01261   0.00729  -0.0067   1.0000   0.0189
  -7.500  -0.8173   0.01221   0.00682  -0.0062   1.0000   0.0195
  -7.250  -0.7917   0.01181   0.00636  -0.0058   1.0000   0.0198
  -7.000  -0.7662   0.01140   0.00590  -0.0053   1.0000   0.0201
  -6.750  -0.7420   0.01062   0.00499  -0.0046   1.0000   0.0217
  -6.500  -0.7167   0.01014   0.00448  -0.0040   1.0000   0.0240
  -6.250  -0.6908   0.00980   0.00413  -0.0036   1.0000   0.0262
  -6.000  -0.6649   0.00947   0.00377  -0.0031   1.0000   0.0295
  -5.750  -0.6393   0.00911   0.00346  -0.0026   1.0000   0.0370
  -5.500  -0.6136   0.00878   0.00317  -0.0021   1.0000   0.0458
  -5.250  -0.5875   0.00857   0.00296  -0.0016   1.0000   0.0509
  -5.000  -0.5618   0.00830   0.00272  -0.0011   1.0000   0.0586
  -4.750  -0.5360   0.00809   0.00252  -0.0006   1.0000   0.0654
  -4.500  -0.5103   0.00787   0.00233   0.0000   1.0000   0.0738
  -4.250  -0.4848   0.00763   0.00215   0.0005   1.0000   0.0857
  -4.000  -0.4593   0.00741   0.00199   0.0011   1.0000   0.0989
  -3.750  -0.4338   0.00720   0.00183   0.0017   1.0000   0.1134
  -3.500  -0.4087   0.00695   0.00169   0.0023   1.0000   0.1355
  -3.250  -0.3835   0.00671   0.00156   0.0030   1.0000   0.1605
  -3.000  -0.3583   0.00651   0.00145   0.0036   1.0000   0.1839
  -2.750  -0.3332   0.00631   0.00134   0.0042   1.0000   0.2065
  -2.500  -0.3082   0.00612   0.00126   0.0049   1.0000   0.2311
  -2.250  -0.2776   0.00594   0.00118   0.0043   0.9985   0.2599
  -2.000  -0.2381   0.00574   0.00112   0.0018   0.9939   0.2963
  -1.750  -0.1996   0.00551   0.00106  -0.0005   0.9858   0.3394
  -1.500  -0.1630   0.00527   0.00100  -0.0023   0.9723   0.3855
  -1.250  -0.1271   0.00504   0.00093  -0.0039   0.9450   0.4391
  -1.000  -0.0994   0.00489   0.00086  -0.0035   0.8928   0.4920
  -0.750  -0.0754   0.00488   0.00081  -0.0023   0.8374   0.5366
  -0.500  -0.0508   0.00493   0.00078  -0.0014   0.7780   0.5769
  -0.250  -0.0256   0.00499   0.00076  -0.0006   0.7178   0.6196
   0.000   0.0000   0.00500   0.00075   0.0000   0.6678   0.6679
   0.250   0.0256   0.00499   0.00076   0.0006   0.6195   0.7176
   0.500   0.0507   0.00493   0.00078   0.0014   0.5768   0.7775
   0.750   0.0753   0.00488   0.00081   0.0024   0.5365   0.8375
   1.000   0.0993   0.00489   0.00086   0.0035   0.4919   0.8929
   1.250   0.1271   0.00504   0.00093   0.0039   0.4391   0.9451
   1.500   0.1630   0.00527   0.00100   0.0023   0.3854   0.9723
   1.750   0.1995   0.00551   0.00106   0.0005   0.3395   0.9857
   2.000   0.2379   0.00574   0.00112  -0.0018   0.2963   0.9938
   2.250   0.2775   0.00594   0.00118  -0.0043   0.2601   0.9984
   2.500   0.3083   0.00612   0.00126  -0.0049   0.2310   1.0000
   2.750   0.3334   0.00631   0.00134  -0.0043   0.2066   1.0000
   3.000   0.3585   0.00651   0.00145  -0.0036   0.1838   1.0000
   3.250   0.3837   0.00671   0.00156  -0.0030   0.1604   1.0000
   3.500   0.4088   0.00694   0.00169  -0.0024   0.1356   1.0000
   3.750   0.4340   0.00720   0.00183  -0.0018   0.1135   1.0000
   4.000   0.4595   0.00741   0.00199  -0.0012   0.0989   1.0000
   4.250   0.4850   0.00763   0.00215  -0.0006   0.0857   1.0000
   4.500   0.5104   0.00787   0.00233   0.0000   0.0738   1.0000
   4.750   0.5361   0.00809   0.00252   0.0006   0.0654   1.0000
   5.000   0.5619   0.00830   0.00272   0.0011   0.0587   1.0000
   5.250   0.5876   0.00857   0.00296   0.0016   0.0509   1.0000
   5.500   0.6137   0.00878   0.00317   0.0021   0.0457   1.0000
   5.750   0.6393   0.00911   0.00346   0.0026   0.0370   1.0000
   6.000   0.6650   0.00947   0.00377   0.0031   0.0295   1.0000
   6.250   0.6908   0.00979   0.00413   0.0036   0.0263   1.0000
   6.500   0.7166   0.01014   0.00448   0.0040   0.0240   1.0000
   6.750   0.7420   0.01060   0.00498   0.0046   0.0219   1.0000
   7.000   0.7661   0.01140   0.00590   0.0053   0.0201   1.0000
   7.250   0.7916   0.01181   0.00636   0.0058   0.0198   1.0000
   7.500   0.8172   0.01220   0.00680   0.0062   0.0195   1.0000
   7.750   0.8427   0.01260   0.00727   0.0067   0.0189   1.0000
   8.000   0.8678   0.01308   0.00782   0.0072   0.0183   1.0000
   8.250   0.8929   0.01354   0.00833   0.0077   0.0175   1.0000
   8.500   0.9183   0.01391   0.00873   0.0080   0.0166   1.0000
   8.750   0.9430   0.01438   0.00921   0.0084   0.0155   1.0000
   9.000   0.9631   0.01583   0.01083   0.0094   0.0141   1.0000
   9.250   0.9888   0.01607   0.01112   0.0097   0.0138   1.0000
   9.500   1.0138   0.01644   0.01154   0.0101   0.0134   1.0000
   9.750   1.0382   0.01691   0.01208   0.0105   0.0129   1.0000
  10.000   1.0623   0.01740   0.01264   0.0110   0.0123   1.0000
  10.250   1.0864   0.01787   0.01316   0.0114   0.0118   1.0000
  10.500   1.1106   0.01829   0.01360   0.0118   0.0112   1.0000
  10.750   1.1330   0.01898   0.01434   0.0124   0.0105   1.0000
  11.000   1.1490   0.02072   0.01629   0.0135   0.0097   1.0000
  11.250   1.1737   0.02097   0.01658   0.0138   0.0095   1.0000
  11.500   1.1981   0.02124   0.01690   0.0142   0.0090   1.0000
  11.750   1.2215   0.02166   0.01736   0.0146   0.0084   1.0000
  12.000   1.2449   0.02204   0.01777   0.0151   0.0078   1.0000
  12.250   1.2677   0.02250   0.01822   0.0155   0.0072   1.0000
  12.500   1.2836   0.02388   0.01973   0.0165   0.0064   1.0000
  12.750   1.3039   0.02459   0.02052   0.0171   0.0060   1.0000
  13.000   1.3230   0.02541   0.02143   0.0178   0.0055   1.0000
  13.250   1.3410   0.02631   0.02237   0.0186   0.0051   1.0000
  13.500   1.3537   0.02773   0.02389   0.0197   0.0047   1.0000
  13.750   1.3582   0.02983   0.02617   0.0212   0.0044   1.0000
  14.000   1.3499   0.03256   0.02912   0.0236   0.0042   1.0000
  14.250   1.3442   0.03442   0.03111   0.0261   0.0041   1.0000
  14.500   1.3353   0.03695   0.03378   0.0270   0.0041   1.0000
  14.750   1.3062   0.04329   0.04033   0.0233   0.0042   1.0000
  15.000   1.2719   0.05431   0.05159   0.0138   0.0042   1.0000
  15.250   1.2267   0.06801   0.06551   0.0042   0.0043   1.0000
  15.500   1.1983   0.07740   0.07503  -0.0013   0.0048   1.0000
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