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SELIG 3002-099-83 (s3002-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: SELIG 3002-099-83 (s3002-il)
Reynolds number: 1,000,000
Max Cl/Cd: 112.46 at α=5.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-s3002-il-1000000.txt
Download as CSV file: xf-s3002-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: SELIG 3002-099-83                               
  
 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
  ------ -------- --------- --------- -------- -------- --------
  -9.750  -0.2890   0.08672   0.08517  -0.0355   1.0000   0.0119
  -9.500  -0.3839   0.09111   0.08945  -0.0342   1.0000   0.0116
  -9.250  -0.3820   0.08789   0.08625  -0.0352   1.0000   0.0117
  -9.000  -0.3796   0.08495   0.08334  -0.0361   1.0000   0.0118
  -8.750  -0.3787   0.08186   0.08027  -0.0371   1.0000   0.0119
  -8.500  -0.3790   0.07890   0.07734  -0.0378   1.0000   0.0120
  -8.250  -0.3829   0.07589   0.07435  -0.0382   1.0000   0.0121
  -8.000  -0.3911   0.07277   0.07129  -0.0385   0.9996   0.0122
  -7.750  -0.4292   0.02028   0.01678  -0.0884   0.9655   0.0090
  -7.500  -0.4035   0.01835   0.01458  -0.0891   0.9570   0.0092
  -7.250  -0.3791   0.01745   0.01354  -0.0889   0.9460   0.0095
  -7.000  -0.3548   0.01637   0.01228  -0.0886   0.9354   0.0098
  -6.750  -0.3305   0.01520   0.01088  -0.0882   0.9254   0.0101
  -6.500  -0.3056   0.01420   0.00967  -0.0877   0.9153   0.0106
  -6.250  -0.2800   0.01329   0.00857  -0.0874   0.9063   0.0109
  -6.000  -0.2539   0.01262   0.00773  -0.0870   0.8977   0.0112
  -5.750  -0.2275   0.01190   0.00689  -0.0868   0.8893   0.0114
  -5.500  -0.2020   0.01090   0.00576  -0.0865   0.8814   0.0120
  -5.250  -0.1747   0.01053   0.00535  -0.0864   0.8736   0.0125
  -5.000  -0.1474   0.01027   0.00503  -0.0862   0.8660   0.0133
  -4.750  -0.1196   0.01000   0.00470  -0.0861   0.8583   0.0142
  -4.500  -0.0927   0.00943   0.00403  -0.0860   0.8507   0.0151
  -4.250  -0.0649   0.00910   0.00369  -0.0859   0.8429   0.0161
  -4.000  -0.0372   0.00888   0.00341  -0.0858   0.8353   0.0173
  -3.750  -0.0089   0.00871   0.00320  -0.0857   0.8275   0.0183
  -3.500   0.0187   0.00826   0.00269  -0.0857   0.8196   0.0204
  -3.250   0.0470   0.00811   0.00252  -0.0857   0.8115   0.0224
  -3.000   0.0750   0.00783   0.00218  -0.0856   0.8036   0.0249
  -2.750   0.1035   0.00765   0.00198  -0.0857   0.7955   0.0274
  -2.250   0.1603   0.00731   0.00159  -0.0857   0.7792   0.0367
  -2.000   0.1885   0.00700   0.00142  -0.0858   0.7709   0.0804
  -1.750   0.2169   0.00667   0.00131  -0.0860   0.7617   0.1535
  -1.500   0.2451   0.00633   0.00122  -0.0862   0.7526   0.2437
  -1.250   0.2732   0.00587   0.00114  -0.0866   0.7427   0.3812
  -1.000   0.3014   0.00538   0.00109  -0.0869   0.7324   0.5409
  -0.750   0.3291   0.00514   0.00112  -0.0868   0.7217   0.6533
  -0.500   0.3570   0.00514   0.00116  -0.0866   0.7100   0.7014
  -0.250   0.3850   0.00518   0.00119  -0.0865   0.6971   0.7246
   0.000   0.4130   0.00524   0.00123  -0.0863   0.6835   0.7436
   0.250   0.4409   0.00531   0.00125  -0.0861   0.6686   0.7549
   0.500   0.4689   0.00541   0.00127  -0.0860   0.6519   0.7633
   1.000   0.5242   0.00560   0.00134  -0.0856   0.6155   0.7811
   1.250   0.5515   0.00571   0.00140  -0.0854   0.5947   0.7912
   1.500   0.5785   0.00585   0.00146  -0.0851   0.5730   0.7993
   1.750   0.6058   0.00599   0.00153  -0.0849   0.5498   0.8070
   2.000   0.6328   0.00615   0.00159  -0.0847   0.5256   0.8129
   2.250   0.6598   0.00632   0.00167  -0.0845   0.4996   0.8177
   2.500   0.6869   0.00652   0.00176  -0.0843   0.4734   0.8223
   2.750   0.7138   0.00672   0.00186  -0.0841   0.4475   0.8265
   3.000   0.7404   0.00691   0.00197  -0.0839   0.4228   0.8308
   3.250   0.7673   0.00711   0.00209  -0.0837   0.3996   0.8354
   3.500   0.7942   0.00733   0.00221  -0.0836   0.3771   0.8399
   3.750   0.8207   0.00752   0.00234  -0.0833   0.3562   0.8446
   4.000   0.8473   0.00772   0.00248  -0.0831   0.3360   0.8499
   4.250   0.8739   0.00794   0.00263  -0.0829   0.3170   0.8553
   4.500   0.9000   0.00816   0.00279  -0.0826   0.2981   0.8614
   4.750   0.9264   0.00837   0.00295  -0.0824   0.2801   0.8684
   5.000   0.9521   0.00857   0.00312  -0.0821   0.2622   0.8767
   5.250   0.9776   0.00880   0.00330  -0.0817   0.2443   0.8872
   5.500   1.0019   0.00901   0.00350  -0.0810   0.2266   0.9039
   5.750   1.0256   0.00912   0.00366  -0.0801   0.2103   1.0000
   6.000   1.0521   0.00943   0.00389  -0.0801   0.1947   1.0000
   6.250   1.0783   0.00974   0.00413  -0.0799   0.1792   1.0000
   6.500   1.1043   0.01006   0.00438  -0.0798   0.1655   1.0000
   6.750   1.1299   0.01039   0.00466  -0.0795   0.1522   1.0000
   7.000   1.1553   0.01073   0.00493  -0.0793   0.1393   1.0000
   7.250   1.1806   0.01107   0.00522  -0.0790   0.1274   1.0000
   7.500   1.2057   0.01141   0.00553  -0.0786   0.1168   1.0000
   7.750   1.2305   0.01178   0.00586  -0.0783   0.1065   1.0000
   8.000   1.2548   0.01218   0.00621  -0.0778   0.0961   1.0000
   8.250   1.2786   0.01262   0.00659  -0.0773   0.0862   1.0000
   8.500   1.3029   0.01300   0.00695  -0.0769   0.0789   1.0000
   8.750   1.3265   0.01342   0.00735  -0.0763   0.0712   1.0000
   9.000   1.3492   0.01392   0.00780  -0.0757   0.0635   1.0000
   9.250   1.3727   0.01431   0.00822  -0.0751   0.0587   1.0000
   9.500   1.3943   0.01488   0.00874  -0.0743   0.0522   1.0000
   9.750   1.4175   0.01526   0.00915  -0.0737   0.0494   1.0000
  10.000   1.4387   0.01581   0.00968  -0.0729   0.0453   1.0000
  10.250   1.4600   0.01632   0.01023  -0.0720   0.0422   1.0000
  10.500   1.4816   0.01676   0.01071  -0.0712   0.0400   1.0000
  10.750   1.5014   0.01734   0.01129  -0.0702   0.0375   1.0000
  11.000   1.5193   0.01805   0.01203  -0.0689   0.0348   1.0000
  11.250   1.5398   0.01847   0.01251  -0.0679   0.0336   1.0000
  11.500   1.5585   0.01901   0.01309  -0.0668   0.0321   1.0000
  11.750   1.5747   0.01965   0.01376  -0.0652   0.0305   1.0000
  12.000   1.5842   0.02052   0.01466  -0.0626   0.0284   1.0000
  12.250   1.5980   0.02110   0.01530  -0.0606   0.0276   1.0000
  12.500   1.6120   0.02167   0.01594  -0.0588   0.0266   1.0000
  12.750   1.6248   0.02234   0.01665  -0.0570   0.0254   1.0000
  13.000   1.6349   0.02320   0.01754  -0.0549   0.0239   1.0000
  13.250   1.6398   0.02445   0.01884  -0.0524   0.0223   1.0000
  13.500   1.6538   0.02513   0.01959  -0.0511   0.0217   1.0000
  13.750   1.6646   0.02607   0.02060  -0.0495   0.0209   1.0000
  14.000   1.6738   0.02717   0.02175  -0.0479   0.0199   1.0000
  14.250   1.6805   0.02850   0.02313  -0.0463   0.0191   1.0000
  14.500   1.6825   0.03028   0.02498  -0.0445   0.0180   1.0000
  14.750   1.6888   0.03180   0.02659  -0.0432   0.0174   1.0000
  15.000   1.6967   0.03324   0.02812  -0.0422   0.0169   1.0000
  15.250   1.7024   0.03492   0.02988  -0.0412   0.0163   1.0000
  15.500   1.7063   0.03686   0.03190  -0.0403   0.0157   1.0000
  15.750   1.7081   0.03910   0.03421  -0.0395   0.0150   1.0000
  16.000   1.7057   0.04189   0.03708  -0.0390   0.0144   1.0000
  16.250   1.7005   0.04515   0.04045  -0.0387   0.0138   1.0000
  16.500   1.7029   0.04769   0.04309  -0.0387   0.0135   1.0000
  16.750   1.7021   0.05071   0.04622  -0.0389   0.0131   1.0000
  17.000   1.6998   0.05408   0.04969  -0.0394   0.0127   1.0000
  17.250   1.6952   0.05793   0.05364  -0.0403   0.0123   1.0000
  17.500   1.6880   0.06232   0.05814  -0.0415   0.0119   1.0000
  17.750   1.6779   0.06739   0.06333  -0.0433   0.0115   1.0000
  18.000   1.6633   0.07342   0.06949  -0.0457   0.0112   1.0000
  18.250   1.6458   0.08022   0.07642  -0.0487   0.0109   1.0000
  18.500   1.6267   0.08762   0.08397  -0.0522   0.0107   1.0000
  18.750   1.6117   0.09443   0.09093  -0.0556   0.0106   1.0000
  19.000   1.5935   0.10203   0.09868  -0.0595   0.0105   1.0000
  19.250   1.5746   0.10996   0.10675  -0.0637   0.0104   1.0000
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