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OAF102 AIRFOIL (oaf102-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: OAF102 AIRFOIL (oaf102-il)
Reynolds number: 500,000
Max Cl/Cd: 86.33 at α=3°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-oaf102-il-500000-n5.txt
Download as CSV file: xf-oaf102-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: OAF102 AIRFOIL                                  
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.500 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -13.750  -0.7989   0.10012   0.09750  -0.0113   1.0000   0.0097
 -13.500  -0.8319   0.08909   0.08634  -0.0177   1.0000   0.0096
 -13.250  -0.8579   0.07995   0.07708  -0.0234   1.0000   0.0096
 -13.000  -0.8820   0.07163   0.06865  -0.0290   1.0000   0.0095
 -12.750  -0.9041   0.06379   0.06070  -0.0346   1.0000   0.0095
 -12.500  -0.9255   0.05629   0.05308  -0.0402   1.0000   0.0094
 -12.250  -0.9423   0.04840   0.04507  -0.0481   1.0000   0.0094
 -12.000  -0.9405   0.03921   0.03565  -0.0619   1.0000   0.0095
 -11.750  -0.9161   0.03133   0.02745  -0.0768   1.0000   0.0097
 -11.500  -0.8904   0.02838   0.02430  -0.0819   1.0000   0.0100
 -11.250  -0.8639   0.02635   0.02209  -0.0852   1.0000   0.0102
 -11.000  -0.8365   0.02468   0.02027  -0.0877   1.0000   0.0106
 -10.750  -0.8085   0.02322   0.01865  -0.0899   1.0000   0.0110
 -10.500  -0.7800   0.02192   0.01718  -0.0918   1.0000   0.0114
 -10.250  -0.7509   0.02075   0.01586  -0.0935   1.0000   0.0118
 -10.000  -0.7216   0.01975   0.01472  -0.0950   1.0000   0.0122
  -9.750  -0.6916   0.01855   0.01341  -0.0969   1.0000   0.0128
  -9.500  -0.6604   0.01772   0.01249  -0.0985   0.9877   0.0135
  -9.250  -0.6279   0.01705   0.01172  -0.1002   0.9735   0.0143
  -9.000  -0.5972   0.01645   0.01101  -0.1014   0.9613   0.0152
  -8.750  -0.5681   0.01589   0.01032  -0.1021   0.9500   0.0160
  -8.500  -0.5396   0.01521   0.00955  -0.1028   0.9392   0.0171
  -8.250  -0.5115   0.01474   0.00899  -0.1031   0.9284   0.0182
  -8.000  -0.4830   0.01430   0.00845  -0.1035   0.9183   0.0194
  -7.750  -0.4545   0.01389   0.00793  -0.1039   0.9089   0.0206
  -7.500  -0.4255   0.01342   0.00740  -0.1044   0.8990   0.0226
  -7.250  -0.3965   0.01308   0.00697  -0.1048   0.8893   0.0246
  -7.000  -0.3674   0.01274   0.00652  -0.1052   0.8801   0.0265
  -6.750  -0.3378   0.01236   0.00610  -0.1058   0.8706   0.0295
  -6.500  -0.3084   0.01209   0.00574  -0.1061   0.8614   0.0324
  -6.250  -0.2788   0.01176   0.00535  -0.1067   0.8519   0.0365
  -6.000  -0.2490   0.01151   0.00503  -0.1071   0.8426   0.0407
  -5.750  -0.2192   0.01122   0.00470  -0.1076   0.8340   0.0473
  -5.500  -0.1892   0.01097   0.00441  -0.1081   0.8247   0.0549
  -5.250  -0.1593   0.01072   0.00414  -0.1087   0.8162   0.0651
  -5.000  -0.1293   0.01048   0.00389  -0.1092   0.8075   0.0785
  -4.750  -0.0992   0.01025   0.00367  -0.1097   0.7994   0.0936
  -4.500  -0.0692   0.01005   0.00347  -0.1103   0.7912   0.1109
  -4.250  -0.0392   0.00987   0.00329  -0.1108   0.7833   0.1281
  -4.000  -0.0093   0.00971   0.00313  -0.1112   0.7753   0.1468
  -3.750   0.0207   0.00956   0.00301  -0.1117   0.7666   0.1671
  -3.500   0.0504   0.00947   0.00290  -0.1121   0.7585   0.1839
  -3.250   0.0803   0.00937   0.00279  -0.1125   0.7503   0.1985
  -3.000   0.1101   0.00929   0.00270  -0.1129   0.7437   0.2132
  -2.750   0.1400   0.00920   0.00263  -0.1133   0.7368   0.2281
  -2.500   0.1698   0.00913   0.00256  -0.1137   0.7305   0.2427
  -2.250   0.1997   0.00907   0.00251  -0.1141   0.7248   0.2571
  -2.000   0.2295   0.00901   0.00247  -0.1144   0.7188   0.2711
  -1.750   0.2592   0.00898   0.00243  -0.1148   0.7134   0.2853
  -1.500   0.2890   0.00893   0.00241  -0.1151   0.7073   0.2994
  -1.250   0.3186   0.00891   0.00240  -0.1154   0.7013   0.3136
  -1.000   0.3483   0.00889   0.00239  -0.1158   0.6959   0.3276
  -0.750   0.3780   0.00887   0.00240  -0.1161   0.6903   0.3411
  -0.500   0.4075   0.00888   0.00241  -0.1164   0.6847   0.3549
  -0.250   0.4372   0.00887   0.00244  -0.1167   0.6783   0.3693
   0.000   0.4667   0.00887   0.00246  -0.1169   0.6717   0.3826
   0.250   0.4962   0.00888   0.00250  -0.1172   0.6660   0.3937
   0.500   0.5258   0.00889   0.00254  -0.1175   0.6599   0.4038
   1.000   0.5847   0.00893   0.00264  -0.1180   0.6482   0.4249
   1.250   0.6141   0.00896   0.00270  -0.1183   0.6420   0.4354
   1.500   0.6435   0.00899   0.00277  -0.1185   0.6361   0.4472
   1.750   0.6730   0.00902   0.00285  -0.1188   0.6296   0.4598
   2.250   0.7317   0.00908   0.00304  -0.1193   0.6164   0.4849
   2.500   0.7607   0.00914   0.00312  -0.1195   0.6027   0.5009
   2.750   0.7893   0.00925   0.00319  -0.1196   0.5706   0.5205
   3.000   0.8175   0.00947   0.00329  -0.1197   0.5237   0.5414
   3.250   0.8454   0.00980   0.00347  -0.1199   0.4737   0.5640
   3.500   0.8734   0.01014   0.00370  -0.1201   0.4280   0.5895
   3.750   0.9004   0.01074   0.00406  -0.1203   0.3504   0.6235
   4.000   0.9256   0.01174   0.00464  -0.1205   0.2366   0.6756
   4.250   0.9461   0.01226   0.00523  -0.1194   0.1480   0.8674
   4.500   0.9674   0.01274   0.00554  -0.1182   0.0979   1.0000
   4.750   0.9940   0.01329   0.00594  -0.1182   0.0703   1.0000
   5.000   1.0208   0.01375   0.00631  -0.1182   0.0550   1.0000
   5.250   1.0476   0.01417   0.00668  -0.1181   0.0456   1.0000
   5.500   1.0745   0.01455   0.00706  -0.1180   0.0396   1.0000
   5.750   1.1009   0.01498   0.00746  -0.1179   0.0344   1.0000
   6.000   1.1272   0.01539   0.00787  -0.1177   0.0307   1.0000
   6.250   1.1530   0.01587   0.00834  -0.1175   0.0277   1.0000
   6.500   1.1789   0.01628   0.00880  -0.1173   0.0256   1.0000
   6.750   1.2042   0.01676   0.00927  -0.1170   0.0234   1.0000
   7.000   1.2288   0.01732   0.00984  -0.1165   0.0215   1.0000
   7.250   1.2536   0.01781   0.01037  -0.1161   0.0203   1.0000
   7.500   1.2778   0.01833   0.01094  -0.1156   0.0191   1.0000
   7.750   1.3013   0.01891   0.01154  -0.1151   0.0180   1.0000
   8.000   1.3232   0.01967   0.01232  -0.1142   0.0169   1.0000
   8.250   1.3462   0.02023   0.01294  -0.1136   0.0161   1.0000
   8.500   1.3684   0.02085   0.01363  -0.1128   0.0153   1.0000
   8.750   1.3898   0.02151   0.01434  -0.1119   0.0146   1.0000
   9.000   1.4104   0.02221   0.01508  -0.1109   0.0140   1.0000
   9.250   1.4295   0.02302   0.01593  -0.1097   0.0135   1.0000
   9.500   1.4453   0.02408   0.01705  -0.1080   0.0129   1.0000
   9.750   1.4626   0.02490   0.01796  -0.1066   0.0126   1.0000
  10.000   1.4783   0.02580   0.01896  -0.1048   0.0122   1.0000
  10.250   1.4927   0.02673   0.01998  -0.1030   0.0119   1.0000
  10.500   1.5059   0.02768   0.02102  -0.1010   0.0115   1.0000
  10.750   1.5165   0.02864   0.02205  -0.0986   0.0111   1.0000
  11.000   1.5259   0.02971   0.02319  -0.0962   0.0108   1.0000
  11.250   1.5354   0.03088   0.02444  -0.0941   0.0105   1.0000
  11.500   1.5433   0.03227   0.02591  -0.0920   0.0102   1.0000
  11.750   1.5491   0.03395   0.02769  -0.0899   0.0100   1.0000
  12.000   1.5525   0.03594   0.02978  -0.0878   0.0097   1.0000
  12.250   1.5596   0.03766   0.03163  -0.0862   0.0096   1.0000
  12.500   1.5657   0.03953   0.03363  -0.0846   0.0094   1.0000
  12.750   1.5708   0.04154   0.03578  -0.0832   0.0093   1.0000
  13.000   1.5750   0.04372   0.03810  -0.0818   0.0091   1.0000
  13.250   1.5779   0.04606   0.04058  -0.0805   0.0089   1.0000
  13.500   1.5801   0.04856   0.04322  -0.0794   0.0088   1.0000
  13.750   1.5812   0.05123   0.04603  -0.0785   0.0086   1.0000
  14.000   1.5812   0.05407   0.04901  -0.0776   0.0085   1.0000
  14.250   1.5801   0.05712   0.05221  -0.0770   0.0083   1.0000
  14.500   1.5783   0.06033   0.05557  -0.0766   0.0082   1.0000
  14.750   1.5754   0.06374   0.05911  -0.0763   0.0081   1.0000
  15.000   1.5715   0.06736   0.06286  -0.0763   0.0080   1.0000
  15.250   1.5668   0.07124   0.06687  -0.0765   0.0079   1.0000
  15.500   1.5615   0.07537   0.07114  -0.0771   0.0078   1.0000
  15.750   1.5546   0.07987   0.07577  -0.0779   0.0077   1.0000
  16.000   1.5465   0.08474   0.08077  -0.0791   0.0076   1.0000
  16.250   1.5367   0.09008   0.08626  -0.0807   0.0075   1.0000
  16.500   1.5255   0.09587   0.09219  -0.0827   0.0075   1.0000
  16.750   1.5125   0.10216   0.09863  -0.0851   0.0074   1.0000
  17.000   1.4974   0.10908   0.10571  -0.0881   0.0074   1.0000
  17.250   1.4808   0.11660   0.11338  -0.0917   0.0073   1.0000
  17.500   1.4630   0.12470   0.12165  -0.0959   0.0073   1.0000
  17.750   1.4431   0.13361   0.13074  -0.1008   0.0073   1.0000
  18.000   1.4218   0.14335   0.14066  -0.1066   0.0073   1.0000
  18.250   1.3973   0.15457   0.15208  -0.1137   0.0073   1.0000
  18.500   1.3609   0.17014   0.16791  -0.1238   0.0074   1.0000
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