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DORNIER A-5 AIRFOIL (doa5-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: DORNIER A-5 AIRFOIL (doa5-il)
Reynolds number: 500,000
Max Cl/Cd: 59.01 at α=1.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-doa5-il-500000-n5.txt
Download as CSV file: xf-doa5-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: DORNIER A-5 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
  ------ -------- --------- --------- -------- -------- --------
 -17.500  -0.8171   0.09575   0.09259  -0.0706   1.0000   0.0214
 -17.250  -0.8822   0.08023   0.07672  -0.0794   1.0000   0.0213
 -17.000  -0.9082   0.07336   0.06967  -0.0823   1.0000   0.0214
 -16.750  -0.9305   0.06761   0.06374  -0.0842   1.0000   0.0214
 -16.500  -0.9459   0.06306   0.05903  -0.0853   0.9999   0.0216
 -16.250  -0.9506   0.05866   0.05446  -0.0880   0.9992   0.0218
 -16.000  -0.9522   0.05480   0.05042  -0.0904   0.9982   0.0220
 -15.750  -0.9502   0.05146   0.04690  -0.0925   0.9970   0.0224
 -15.500  -0.9464   0.04854   0.04382  -0.0942   0.9956   0.0225
 -15.250  -0.9414   0.04589   0.04098  -0.0957   0.9942   0.0228
 -15.000  -0.9346   0.04361   0.03855  -0.0968   0.9929   0.0229
 -14.750  -0.9286   0.04143   0.03626  -0.0971   0.9912   0.0231
 -14.500  -0.9197   0.03953   0.03428  -0.0976   0.9894   0.0233
 -14.250  -0.9072   0.03797   0.03265  -0.0982   0.9876   0.0236
 -14.000  -0.8933   0.03645   0.03107  -0.0989   0.9860   0.0238
 -13.750  -0.8767   0.03521   0.02978  -0.0999   0.9846   0.0241
 -13.500  -0.8591   0.03391   0.02841  -0.1008   0.9835   0.0243
 -13.250  -0.8465   0.03273   0.02716  -0.1005   0.9803   0.0246
 -13.000  -0.8305   0.03161   0.02596  -0.1007   0.9778   0.0249
 -12.750  -0.8122   0.03048   0.02475  -0.1012   0.9759   0.0252
 -12.500  -0.7921   0.02937   0.02356  -0.1019   0.9744   0.0255
 -12.250  -0.7703   0.02836   0.02245  -0.1028   0.9732   0.0259
 -12.000  -0.7472   0.02737   0.02138  -0.1037   0.9723   0.0261
 -11.750  -0.7335   0.02655   0.02048  -0.1026   0.9681   0.0265
 -11.500  -0.7120   0.02574   0.01958  -0.1029   0.9657   0.0268
 -11.250  -0.6880   0.02493   0.01869  -0.1037   0.9640   0.0270
 -11.000  -0.6640   0.02396   0.01770  -0.1044   0.9626   0.0274
 -10.750  -0.6381   0.02310   0.01682  -0.1055   0.9615   0.0278
 -10.500  -0.6204   0.02240   0.01610  -0.1048   0.9573   0.0281
 -10.250  -0.6018   0.02174   0.01541  -0.1043   0.9531   0.0284
 -10.000  -0.5773   0.02105   0.01469  -0.1049   0.9508   0.0288
  -9.750  -0.5506   0.02037   0.01398  -0.1059   0.9491   0.0292
  -9.500  -0.5396   0.01984   0.01343  -0.1037   0.9421   0.0295
  -9.250  -0.5176   0.01922   0.01277  -0.1037   0.9384   0.0300
  -9.000  -0.4911   0.01859   0.01210  -0.1046   0.9360   0.0304
  -8.750  -0.4763   0.01808   0.01155  -0.1030   0.9298   0.0310
  -8.500  -0.4520   0.01752   0.01094  -0.1034   0.9262   0.0315
  -8.250  -0.4236   0.01681   0.01021  -0.1048   0.9236   0.0319
  -8.000  -0.3973   0.01613   0.00952  -0.1058   0.9197   0.0326
  -7.750  -0.3760   0.01556   0.00893  -0.1056   0.9136   0.0330
  -7.500  -0.3441   0.01500   0.00834  -0.1074   0.9101   0.0338
  -7.250  -0.3103   0.01449   0.00779  -0.1096   0.9074   0.0347
  -7.000  -0.2957   0.01413   0.00741  -0.1077   0.9000   0.0354
  -6.750  -0.2690   0.01375   0.00698  -0.1081   0.8953   0.0363
  -6.500  -0.2386   0.01334   0.00653  -0.1094   0.8919   0.0373
  -6.250  -0.2275   0.01304   0.00624  -0.1065   0.8833   0.0385
  -6.000  -0.2023   0.01271   0.00590  -0.1065   0.8782   0.0402
  -5.750  -0.1808   0.01244   0.00561  -0.1056   0.8724   0.0420
  -5.500  -0.1590   0.01215   0.00532  -0.1048   0.8659   0.0442
  -5.250  -0.1316   0.01185   0.00501  -0.1051   0.8608   0.0475
  -5.000  -0.1079   0.01159   0.00476  -0.1046   0.8541   0.0517
  -4.750  -0.0788   0.01133   0.00449  -0.1052   0.8472   0.0586
  -4.500  -0.0517   0.01114   0.00428  -0.1053   0.8410   0.0660
  -4.250  -0.0242   0.01092   0.00404  -0.1055   0.8341   0.0730
  -4.000   0.0055   0.01073   0.00381  -0.1062   0.8285   0.0801
  -3.750   0.0291   0.01053   0.00366  -0.1056   0.8236   0.0892
  -3.500   0.0542   0.01029   0.00348  -0.1054   0.8192   0.1105
  -3.250   0.0803   0.00997   0.00329  -0.1055   0.8144   0.1508
  -3.000   0.1065   0.00974   0.00312  -0.1055   0.8097   0.1811
  -2.750   0.1152   0.00811   0.00248  -0.1034   0.8032   0.4582
  -2.500   0.1402   0.00787   0.00240  -0.1030   0.7972   0.5158
  -2.250   0.1662   0.00777   0.00238  -0.1027   0.7908   0.5469
  -2.000   0.1899   0.00771   0.00237  -0.1018   0.7839   0.5690
  -1.750   0.2161   0.00769   0.00236  -0.1014   0.7765   0.5845
  -1.500   0.2403   0.00767   0.00235  -0.1006   0.7687   0.5940
  -1.250   0.2653   0.00767   0.00233  -0.1000   0.7606   0.6006
  -1.000   0.2909   0.00767   0.00231  -0.0994   0.7534   0.6081
  -0.750   0.3154   0.00766   0.00231  -0.0987   0.7442   0.6158
  -0.500   0.3402   0.00768   0.00227  -0.0980   0.7339   0.6218
  -0.250   0.3640   0.00770   0.00226  -0.0970   0.7220   0.6269
   0.000   0.3877   0.00773   0.00227  -0.0961   0.7099   0.6324
   0.250   0.4108   0.00778   0.00227  -0.0950   0.6954   0.6379
   0.500   0.4317   0.00786   0.00229  -0.0935   0.6751   0.6427
   0.750   0.4516   0.00798   0.00235  -0.0917   0.6567   0.6492
   1.000   0.4704   0.00812   0.00240  -0.0898   0.6378   0.6561
   1.250   0.4875   0.00827   0.00248  -0.0874   0.6138   0.6610
   1.500   0.5016   0.00850   0.00258  -0.0845   0.5819   0.6654
   1.750   0.5140   0.00879   0.00270  -0.0813   0.5484   0.6695
   2.000   0.5241   0.00918   0.00286  -0.0777   0.4987   0.6739
   2.250   0.5300   0.00974   0.00315  -0.0733   0.4369   0.6768
   2.500   0.5431   0.01018   0.00342  -0.0705   0.3968   0.6808
   2.750   0.5618   0.01047   0.00362  -0.0687   0.3780   0.6855
   3.000   0.5814   0.01073   0.00380  -0.0672   0.3601   0.6902
   3.250   0.6002   0.01102   0.00403  -0.0655   0.3422   0.6932
   3.500   0.6194   0.01131   0.00426  -0.0639   0.3265   0.6966
   3.750   0.6394   0.01156   0.00447  -0.0625   0.3157   0.6998
   4.000   0.6609   0.01176   0.00464  -0.0614   0.3037   0.7031
   4.250   0.6820   0.01198   0.00482  -0.0602   0.2933   0.7064
   4.500   0.7014   0.01226   0.00505  -0.0587   0.2783   0.7089
   4.750   0.7195   0.01259   0.00531  -0.0570   0.2518   0.7113
   5.000   0.7328   0.01315   0.00564  -0.0545   0.2071   0.7141
   5.250   0.7502   0.01355   0.00595  -0.0528   0.1889   0.7172
   5.500   0.7686   0.01392   0.00626  -0.0512   0.1762   0.7207
   5.750   0.7876   0.01426   0.00654  -0.0498   0.1666   0.7239
   6.000   0.8066   0.01458   0.00687  -0.0484   0.1603   0.7260
   6.250   0.8257   0.01492   0.00720  -0.0470   0.1550   0.7282
   6.500   0.8446   0.01526   0.00754  -0.0456   0.1508   0.7306
   6.750   0.8642   0.01557   0.00787  -0.0443   0.1470   0.7334
   7.000   0.8844   0.01586   0.00818  -0.0432   0.1436   0.7362
   7.250   0.9035   0.01621   0.00852  -0.0419   0.1391   0.7388
   7.500   0.9216   0.01661   0.00890  -0.0405   0.1345   0.7411
   7.750   0.9414   0.01690   0.00925  -0.0393   0.1308   0.7429
   8.000   0.9605   0.01724   0.00962  -0.0380   0.1256   0.7447
   8.250   0.9785   0.01764   0.01001  -0.0367   0.1195   0.7466
   8.500   0.9973   0.01800   0.01038  -0.0354   0.1129   0.7489
   8.750   1.0145   0.01847   0.01081  -0.0340   0.1058   0.7513
   9.000   1.0308   0.01898   0.01126  -0.0325   0.0999   0.7534
   9.250   1.0477   0.01947   0.01175  -0.0311   0.0960   0.7553
   9.500   1.0647   0.01995   0.01226  -0.0298   0.0933   0.7569
   9.750   1.0805   0.02047   0.01281  -0.0283   0.0908   0.7583
  10.000   1.0950   0.02108   0.01343  -0.0266   0.0877   0.7598
  10.250   1.1111   0.02161   0.01400  -0.0252   0.0855   0.7614
  10.500   1.1281   0.02210   0.01456  -0.0240   0.0835   0.7632
  10.750   1.1441   0.02265   0.01516  -0.0226   0.0809   0.7653
  11.000   1.1590   0.02328   0.01582  -0.0212   0.0785   0.7675
  11.250   1.1731   0.02397   0.01653  -0.0198   0.0762   0.7697
  11.500   1.1892   0.02456   0.01716  -0.0186   0.0736   0.7716
  11.750   1.2038   0.02522   0.01786  -0.0173   0.0713   0.7733
  12.000   1.2177   0.02593   0.01860  -0.0159   0.0690   0.7749
  12.250   1.2307   0.02670   0.01941  -0.0145   0.0669   0.7764
  12.500   1.2447   0.02745   0.02022  -0.0132   0.0652   0.7780
  12.750   1.2577   0.02827   0.02108  -0.0120   0.0632   0.7795
  13.000   1.2698   0.02917   0.02200  -0.0107   0.0611   0.7810
  13.250   1.2803   0.03020   0.02305  -0.0093   0.0588   0.7823
  13.500   1.2934   0.03107   0.02400  -0.0082   0.0573   0.7837
  13.750   1.3054   0.03204   0.02503  -0.0070   0.0554   0.7849
  14.000   1.3158   0.03314   0.02617  -0.0058   0.0535   0.7861
  14.250   1.3251   0.03436   0.02742  -0.0046   0.0519   0.7873
  14.500   1.3346   0.03558   0.02870  -0.0035   0.0503   0.7885
  14.750   1.3459   0.03667   0.02989  -0.0026   0.0488   0.7899
  15.000   1.3555   0.03792   0.03122  -0.0016   0.0469   0.7913
  15.250   1.3641   0.03930   0.03265  -0.0007   0.0452   0.7927
  15.500   1.3710   0.04085   0.03425   0.0003   0.0436   0.7941
  15.750   1.3797   0.04230   0.03579   0.0010   0.0422   0.7954
  16.000   1.3869   0.04391   0.03747   0.0017   0.0405   0.7966
  16.250   1.3929   0.04569   0.03931   0.0024   0.0391   0.7978
  16.500   1.3976   0.04765   0.04132   0.0029   0.0377   0.7989
  16.750   1.4029   0.04961   0.04336   0.0034   0.0364   0.8000
  17.000   1.4070   0.05175   0.04558   0.0037   0.0350   0.8010
  17.250   1.4098   0.05409   0.04798   0.0039   0.0339   0.8021
  17.500   1.4102   0.05675   0.05071   0.0040   0.0328   0.8032
  17.750   1.4121   0.05934   0.05340   0.0039   0.0319   0.8043
  18.000   1.4131   0.06211   0.05628   0.0036   0.0309   0.8055
  18.250   1.4125   0.06515   0.05943   0.0032   0.0301   0.8070
  18.500   1.4102   0.06849   0.06286   0.0026   0.0292   0.8083
  18.750   1.4058   0.07223   0.06670   0.0016   0.0284   0.8095
  19.000   1.4002   0.07629   0.07086   0.0004   0.0276   0.8105
  19.250   1.3962   0.08026   0.07496  -0.0010   0.0271   0.8116
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