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FX 83-W-108 (fx83w108-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: FX 83-W-108 (fx83w108-il)
Reynolds number: 200,000
Max Cl/Cd: 86.8 at α=4.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx83w108-il-200000-n5.txt
Download as CSV file: xf-fx83w108-il-200000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: FX 83-W-108                                     
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.200 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -10.750  -0.3733   0.10780   0.10398  -0.0474   1.0000   0.0232
 -10.500  -0.3759   0.10451   0.10074  -0.0475   1.0000   0.0230
 -10.250  -0.3869   0.09975   0.09604  -0.0482   1.0000   0.0237
 -10.000  -0.3908   0.09598   0.09231  -0.0490   0.9994   0.0236
  -9.750  -0.3842   0.08980   0.08614  -0.0545   0.9951   0.0235
  -9.500  -0.3817   0.08290   0.07925  -0.0606   0.9899   0.0233
  -9.250  -0.3854   0.07451   0.07088  -0.0682   0.9823   0.0232
  -9.000  -0.4530   0.04149   0.03727  -0.1079   0.9524   0.0222
  -8.750  -0.4419   0.03441   0.02950  -0.1158   0.9433   0.0225
  -8.500  -0.4234   0.03031   0.02483  -0.1189   0.9358   0.0230
  -8.250  -0.3976   0.02719   0.02118  -0.1216   0.9308   0.0236
  -8.000  -0.3670   0.02481   0.01831  -0.1240   0.9275   0.0244
  -7.750  -0.3426   0.02329   0.01662  -0.1246   0.9209   0.0251
  -7.500  -0.3126   0.02239   0.01564  -0.1259   0.9163   0.0263
  -7.250  -0.2801   0.02130   0.01437  -0.1277   0.9131   0.0275
  -7.000  -0.2528   0.02019   0.01304  -0.1282   0.9075   0.0288
  -6.750  -0.2242   0.01914   0.01177  -0.1287   0.9021   0.0299
  -6.500  -0.1929   0.01805   0.01056  -0.1300   0.8982   0.0312
  -6.250  -0.1651   0.01734   0.00981  -0.1304   0.8929   0.0328
  -6.000  -0.1376   0.01680   0.00918  -0.1306   0.8873   0.0351
  -5.750  -0.1067   0.01627   0.00850  -0.1315   0.8831   0.0378
  -5.500  -0.0796   0.01558   0.00780  -0.1317   0.8778   0.0404
  -5.250  -0.0530   0.01515   0.00731  -0.1316   0.8720   0.0433
  -5.000  -0.0231   0.01476   0.00680  -0.1322   0.8678   0.0471
  -4.750   0.0040   0.01423   0.00626  -0.1323   0.8629   0.0516
  -4.500   0.0301   0.01392   0.00588  -0.1320   0.8572   0.0567
  -4.250   0.0586   0.01351   0.00543  -0.1323   0.8528   0.0638
  -4.000   0.0870   0.01318   0.00506  -0.1325   0.8485   0.0729
  -3.750   0.1121   0.01287   0.00478  -0.1321   0.8429   0.0876
  -3.500   0.1395   0.01252   0.00448  -0.1322   0.8382   0.1145
  -3.000   0.1922   0.01179   0.00414  -0.1320   0.8290   0.2275
  -2.750   0.2188   0.01159   0.00406  -0.1319   0.8243   0.2805
  -2.500   0.2473   0.01147   0.00401  -0.1320   0.8205   0.3215
  -2.250   0.2739   0.01143   0.00399  -0.1317   0.8160   0.3510
  -2.000   0.3002   0.01141   0.00398  -0.1313   0.8110   0.3764
  -1.750   0.3277   0.01136   0.00397  -0.1312   0.8069   0.4027
  -1.500   0.3568   0.01133   0.00393  -0.1314   0.8034   0.4270
  -1.250   0.3813   0.01132   0.00397  -0.1306   0.7981   0.4442
  -1.000   0.4080   0.01130   0.00396  -0.1303   0.7936   0.4598
  -0.750   0.4362   0.01127   0.00393  -0.1303   0.7897   0.4747
  -0.500   0.4629   0.01126   0.00394  -0.1300   0.7854   0.4894
  -0.250   0.4884   0.01125   0.00398  -0.1295   0.7804   0.5051
   0.000   0.5155   0.01122   0.00399  -0.1292   0.7760   0.5222
   0.250   0.5439   0.01119   0.00400  -0.1292   0.7724   0.5419
   0.500   0.5678   0.01119   0.00410  -0.1283   0.7666   0.5632
   0.750   0.5938   0.01115   0.00415  -0.1279   0.7618   0.5884
   1.000   0.6215   0.01110   0.00418  -0.1277   0.7579   0.6200
   1.250   0.6455   0.01107   0.00432  -0.1268   0.7527   0.6594
   1.500   0.6695   0.01099   0.00443  -0.1258   0.7477   0.7133
   1.750   0.6966   0.01081   0.00449  -0.1253   0.7434   0.7996
   2.000   0.7433   0.01063   0.00455  -0.1292   0.7389   1.0000
   2.250   0.7685   0.01074   0.00466  -0.1286   0.7325   1.0000
   2.500   0.7967   0.01081   0.00469  -0.1285   0.7271   1.0000
   2.750   0.8206   0.01091   0.00483  -0.1277   0.7186   1.0000
   3.000   0.8474   0.01095   0.00482  -0.1272   0.7096   1.0000
   3.250   0.8715   0.01100   0.00485  -0.1262   0.6975   1.0000
   3.500   0.8950   0.01104   0.00489  -0.1251   0.6829   1.0000
   3.750   0.9185   0.01109   0.00491  -0.1239   0.6663   1.0000
   4.000   0.9415   0.01117   0.00496  -0.1227   0.6492   1.0000
   4.250   0.9643   0.01129   0.00507  -0.1215   0.6318   1.0000
   4.500   0.9866   0.01143   0.00520  -0.1202   0.6114   1.0000
   4.750   1.0078   0.01161   0.00530  -0.1187   0.5846   1.0000
   5.000   1.0270   0.01187   0.00543  -0.1168   0.5493   1.0000
   5.250   1.0429   0.01229   0.00563  -0.1143   0.5025   1.0000
   5.500   1.0528   0.01297   0.00597  -0.1107   0.4403   1.0000
   5.750   1.0592   0.01384   0.00647  -0.1068   0.3744   1.0000
   6.000   1.0647   0.01480   0.00708  -0.1028   0.3120   1.0000
   6.250   1.0709   0.01571   0.00771  -0.0991   0.2601   1.0000
   6.500   1.0779   0.01661   0.00836  -0.0955   0.2151   1.0000
   6.750   1.0870   0.01748   0.00904  -0.0925   0.1789   1.0000
   7.000   1.0983   0.01827   0.00970  -0.0899   0.1511   1.0000
   7.250   1.1103   0.01907   0.01038  -0.0874   0.1287   1.0000
   7.500   1.1224   0.01987   0.01110  -0.0850   0.1097   1.0000
   7.750   1.1350   0.02068   0.01184  -0.0828   0.0952   1.0000
   8.000   1.1480   0.02148   0.01262  -0.0808   0.0837   1.0000
   8.250   1.1611   0.02230   0.01343  -0.0787   0.0743   1.0000
   8.500   1.1730   0.02322   0.01430  -0.0766   0.0661   1.0000
   8.750   1.1868   0.02402   0.01516  -0.0748   0.0603   1.0000
   9.000   1.1977   0.02506   0.01616  -0.0728   0.0550   1.0000
   9.250   1.2113   0.02592   0.01712  -0.0711   0.0512   1.0000
   9.500   1.2234   0.02691   0.01816  -0.0693   0.0477   1.0000
   9.750   1.2331   0.02811   0.01937  -0.0673   0.0449   1.0000
  10.000   1.2450   0.02918   0.02052  -0.0656   0.0426   1.0000
  10.250   1.2571   0.03025   0.02167  -0.0640   0.0400   1.0000
  10.500   1.2678   0.03145   0.02294  -0.0624   0.0382   1.0000
  10.750   1.2765   0.03284   0.02436  -0.0607   0.0363   1.0000
  11.000   1.2861   0.03421   0.02581  -0.0591   0.0348   1.0000
  11.250   1.2960   0.03558   0.02729  -0.0575   0.0334   1.0000
  11.500   1.3056   0.03700   0.02880  -0.0561   0.0322   1.0000
  11.750   1.3147   0.03849   0.03037  -0.0546   0.0311   1.0000
  12.000   1.3229   0.04006   0.03202  -0.0532   0.0301   1.0000
  12.250   1.3300   0.04179   0.03382  -0.0518   0.0293   1.0000
  12.500   1.3359   0.04373   0.03582  -0.0504   0.0283   1.0000
  12.750   1.3453   0.04531   0.03755  -0.0492   0.0274   1.0000
  13.000   1.3532   0.04711   0.03949  -0.0480   0.0266   1.0000
  13.250   1.3605   0.04896   0.04148  -0.0469   0.0258   1.0000
  13.500   1.3670   0.05093   0.04357  -0.0458   0.0252   1.0000
  13.750   1.3726   0.05300   0.04576  -0.0448   0.0246   1.0000
  14.000   1.3775   0.05516   0.04803  -0.0439   0.0241   1.0000
  14.250   1.3815   0.05746   0.05045  -0.0431   0.0236   1.0000
  14.500   1.3849   0.05988   0.05297  -0.0423   0.0232   1.0000
  14.750   1.3871   0.06255   0.05573  -0.0416   0.0228   1.0000
  15.000   1.3879   0.06546   0.05880  -0.0410   0.0223   1.0000
  15.250   1.3875   0.06849   0.06205  -0.0407   0.0220   1.0000
  15.500   1.3848   0.07192   0.06570  -0.0406   0.0215   1.0000
  15.750   1.3810   0.07560   0.06960  -0.0407   0.0212   1.0000
  16.000   1.3756   0.07958   0.07379  -0.0411   0.0208   1.0000
  16.250   1.3682   0.08396   0.07839  -0.0418   0.0204   1.0000
  16.500   1.3602   0.08859   0.08323  -0.0429   0.0202   1.0000
  16.750   1.3503   0.09371   0.08855  -0.0445   0.0199   1.0000
  17.000   1.3390   0.09926   0.09430  -0.0465   0.0197   1.0000
  17.250   1.3265   0.10521   0.10047  -0.0490   0.0195   1.0000
  17.500   1.3127   0.11168   0.10713  -0.0522   0.0193   1.0000
  17.750   1.2963   0.11899   0.11464  -0.0561   0.0192   1.0000
  18.000   1.2787   0.12695   0.12280  -0.0607   0.0191   1.0000
  18.250   1.2524   0.13745   0.13353  -0.0673   0.0191   1.0000
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