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SOMERS S102 AIRFOIL (SHARP) (s102s-il) Xfoil prediction polar at RE=100,000 Ncrit=5


Details Polar file
Airfoil: SOMERS S102 AIRFOIL (SHARP) (s102s-il)
Reynolds number: 100,000
Max Cl/Cd: 42.21 at α=5.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-s102s-il-100000-n5.txt
Download as CSV file: xf-s102s-il-100000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: SOMERS S102 AIRFOIL (SHARP)                     
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.100 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -11.750  -0.4251   0.10071   0.09545  -0.0560   1.0000   0.0201
 -11.500  -0.4273   0.09653   0.09131  -0.0574   1.0000   0.0199
 -11.250  -0.4346   0.09078   0.08560  -0.0599   1.0000   0.0196
 -11.000  -0.4473   0.08481   0.07963  -0.0628   1.0000   0.0193
 -10.750  -0.4666   0.07891   0.07372  -0.0654   1.0000   0.0192
 -10.500  -0.4871   0.07403   0.06881  -0.0668   1.0000   0.0189
 -10.250  -0.5084   0.06997   0.06471  -0.0672   1.0000   0.0187
 -10.000  -0.5314   0.06651   0.06121  -0.0664   1.0000   0.0186
  -9.750  -0.5558   0.06378   0.05844  -0.0643   1.0000   0.0185
  -9.500  -0.5832   0.06183   0.05647  -0.0607   1.0000   0.0183
  -9.250  -0.5958   0.05849   0.05296  -0.0613   0.9926   0.0182
  -9.000  -0.5908   0.05349   0.04757  -0.0648   0.9807   0.0179
  -8.750  -0.5809   0.04905   0.04270  -0.0672   0.9705   0.0178
  -8.250  -0.5529   0.04188   0.03470  -0.0689   0.9495   0.0178
  -8.000  -0.5286   0.03871   0.03107  -0.0705   0.9435   0.0181
  -7.750  -0.5090   0.03636   0.02836  -0.0703   0.9331   0.0188
  -7.500  -0.4810   0.03382   0.02525  -0.0710   0.9271   0.0200
  -7.250  -0.4569   0.03219   0.02357  -0.0713   0.9184   0.0210
  -7.000  -0.4248   0.03044   0.02163  -0.0725   0.9138   0.0220
  -6.750  -0.3993   0.02890   0.01992  -0.0721   0.9051   0.0227
  -6.500  -0.3671   0.02734   0.01820  -0.0726   0.9003   0.0238
  -6.250  -0.3404   0.02611   0.01687  -0.0723   0.8932   0.0249
  -6.000  -0.3143   0.02502   0.01580  -0.0725   0.8868   0.0266
  -5.750  -0.2872   0.02413   0.01480  -0.0727   0.8811   0.0303
  -5.500  -0.2662   0.02327   0.01397  -0.0720   0.8732   0.0341
  -5.250  -0.2402   0.02234   0.01299  -0.0722   0.8681   0.0393
  -5.000  -0.2210   0.02164   0.01227  -0.0712   0.8598   0.0477
  -4.750  -0.1972   0.02080   0.01142  -0.0710   0.8540   0.0649
  -4.500  -0.1804   0.01960   0.01059  -0.0703   0.8471   0.1214
  -4.250  -0.1777   0.01811   0.01130  -0.0670   0.8398   0.5407
  -4.000  -0.1470   0.01916   0.01208  -0.0664   0.8361   0.6039
  -3.750  -0.1255   0.02072   0.01362  -0.0628   0.8303   0.6360
  -3.500  -0.1028   0.02214   0.01498  -0.0592   0.8254   0.6645
  -3.250  -0.0746   0.02274   0.01548  -0.0573   0.8218   0.6727
  -3.000  -0.0467   0.02241   0.01494  -0.0580   0.8175   0.6764
  -2.750  -0.0223   0.02202   0.01436  -0.0587   0.8118   0.6806
  -2.500   0.0053   0.02185   0.01405  -0.0589   0.8080   0.6821
  -2.250   0.0348   0.02168   0.01373  -0.0595   0.8049   0.6838
  -2.000   0.0617   0.02154   0.01349  -0.0597   0.8012   0.6855
  -1.750   0.0856   0.02145   0.01330  -0.0596   0.7963   0.6874
  -1.500   0.1131   0.02130   0.01304  -0.0600   0.7923   0.6895
  -1.250   0.1429   0.02111   0.01274  -0.0609   0.7893   0.6913
  -1.000   0.1731   0.02094   0.01245  -0.0620   0.7867   0.6932
  -0.750   0.1961   0.02092   0.01238  -0.0621   0.7820   0.6956
  -0.500   0.2224   0.02088   0.01228  -0.0624   0.7781   0.6972
  -0.250   0.2505   0.02083   0.01218  -0.0628   0.7749   0.6982
   0.000   0.2802   0.02076   0.01207  -0.0635   0.7723   0.6992
   0.250   0.3062   0.02082   0.01211  -0.0636   0.7692   0.7006
   0.500   0.3281   0.02098   0.01228  -0.0630   0.7646   0.7024
   0.750   0.3544   0.02103   0.01234  -0.0632   0.7609   0.7041
   1.000   0.3833   0.02105   0.01234  -0.0639   0.7581   0.7055
   1.250   0.4141   0.02103   0.01231  -0.0648   0.7557   0.7069
   1.500   0.4365   0.02123   0.01254  -0.0645   0.7509   0.7086
   1.750   0.4622   0.02127   0.01258  -0.0646   0.7448   0.7102
   2.000   0.4974   0.02086   0.01213  -0.0656   0.7366   0.7120
   2.250   0.5272   0.02044   0.01168  -0.0653   0.7239   0.7135
   2.500   0.5534   0.02008   0.01131  -0.0645   0.7091   0.7149
   2.750   0.5791   0.01978   0.01102  -0.0637   0.6947   0.7164
   3.000   0.6047   0.01957   0.01084  -0.0631   0.6815   0.7179
   3.250   0.6322   0.01941   0.01069  -0.0629   0.6710   0.7195
   3.500   0.6583   0.01930   0.01063  -0.0626   0.6603   0.7213
   3.750   0.6817   0.01927   0.01069  -0.0619   0.6483   0.7231
   4.000   0.7063   0.01920   0.01067  -0.0613   0.6350   0.7251
   4.250   0.7299   0.01912   0.01065  -0.0606   0.6188   0.7273
   4.500   0.7518   0.01905   0.01066  -0.0595   0.5989   0.7293
   4.750   0.7702   0.01904   0.01074  -0.0577   0.5727   0.7313
   5.000   0.7889   0.01902   0.01074  -0.0559   0.5294   0.7335
   5.250   0.8062   0.01910   0.01022  -0.0534   0.4304   0.7358
   5.500   0.8107   0.02005   0.01063  -0.0497   0.3499   0.7382
   5.750   0.8176   0.02101   0.01125  -0.0468   0.2995   0.7407
   6.000   0.8273   0.02181   0.01185  -0.0443   0.2669   0.7433
   6.250   0.8385   0.02249   0.01243  -0.0420   0.2447   0.7456
   6.500   0.8519   0.02313   0.01304  -0.0401   0.2291   0.7480
   6.750   0.8673   0.02379   0.01367  -0.0386   0.2173   0.7507
   7.000   0.8835   0.02449   0.01431  -0.0372   0.2073   0.7537
   7.250   0.9024   0.02510   0.01494  -0.0363   0.1985   0.7572
   7.500   0.9198   0.02583   0.01562  -0.0353   0.1912   0.7607
   7.750   0.9393   0.02639   0.01628  -0.0344   0.1844   0.7640
   8.000   0.9584   0.02705   0.01697  -0.0335   0.1789   0.7679
   8.250   0.9789   0.02777   0.01769  -0.0329   0.1742   0.7721
   8.500   1.0005   0.02841   0.01844  -0.0324   0.1689   0.7763
   8.750   1.0203   0.02909   0.01918  -0.0317   0.1641   0.7803
   9.000   1.0418   0.02987   0.01994  -0.0312   0.1599   0.7851
   9.250   1.0643   0.03057   0.02081  -0.0309   0.1558   0.7906
   9.500   1.0849   0.03128   0.02166  -0.0303   0.1517   0.7959
   9.750   1.1055   0.03205   0.02249  -0.0298   0.1477   0.8025
  10.000   1.1274   0.03289   0.02342  -0.0294   0.1441   0.8098
  10.250   1.1463   0.03368   0.02446  -0.0286   0.1402   0.8186
  10.500   1.1644   0.03448   0.02543  -0.0277   0.1364   0.8292
  10.750   1.1820   0.03528   0.02632  -0.0268   0.1329   0.8426
  11.000   1.1995   0.03616   0.02735  -0.0258   0.1296   0.8616
  11.250   1.2105   0.03692   0.02849  -0.0238   0.1261   0.9021
  11.500   1.2238   0.03781   0.02955  -0.0228   0.1223   1.0000
  11.750   1.2407   0.03889   0.03066  -0.0224   0.1188   1.0000
  12.000   1.2570   0.04016   0.03200  -0.0220   0.1155   1.0000
  12.250   1.2664   0.04155   0.03368  -0.0209   0.1116   1.0000
  12.500   1.2767   0.04288   0.03516  -0.0200   0.1079   1.0000
  12.750   1.2875   0.04409   0.03641  -0.0192   0.1047   1.0000
  13.000   1.2954   0.04569   0.03817  -0.0183   0.1015   1.0000
  13.250   1.2993   0.04753   0.04030  -0.0172   0.0978   1.0000
  13.500   1.3037   0.04919   0.04210  -0.0163   0.0943   1.0000
  13.750   1.3095   0.05069   0.04363  -0.0156   0.0915   1.0000
  14.000   1.3103   0.05297   0.04616  -0.0148   0.0883   1.0000
  14.250   1.3091   0.05544   0.04890  -0.0141   0.0848   1.0000
  14.500   1.3093   0.05762   0.05123  -0.0137   0.0817   1.0000
  14.750   1.3109   0.05967   0.05330  -0.0135   0.0792   1.0000
  15.000   1.3043   0.06313   0.05707  -0.0134   0.0761   1.0000
  15.250   1.2980   0.06655   0.06075  -0.0136   0.0731   1.0000
  15.500   1.2937   0.06969   0.06401  -0.0141   0.0705   1.0000
  15.750   1.2913   0.07265   0.06700  -0.0147   0.0683   1.0000
  16.000   1.2768   0.07787   0.07253  -0.0160   0.0660   1.0000
  16.250   1.2615   0.08339   0.07832  -0.0178   0.0638   1.0000
  16.500   1.2469   0.08908   0.08420  -0.0201   0.0620   1.0000
  16.750   1.2341   0.09472   0.08997  -0.0228   0.0603   1.0000
  17.000   1.2265   0.09963   0.09491  -0.0253   0.0586   1.0000
  17.250   1.1978   0.10910   0.10463  -0.0305   0.0579   1.0000
  17.500   1.1576   0.12179   0.11756  -0.0381   0.0579   1.0000
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