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DORNIER A-5 AIRFOIL (doa5-il) Xfoil prediction polar at RE=100,000 Ncrit=5


Details Polar file
Airfoil: DORNIER A-5 AIRFOIL (doa5-il)
Reynolds number: 100,000
Max Cl/Cd: 35.43 at α=6.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-doa5-il-100000-n5.txt
Download as CSV file: xf-doa5-il-100000-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 =     0.100 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -12.250  -0.5409   0.09755   0.09197  -0.0604   1.0000   0.0478
 -12.000  -0.5846   0.08759   0.08195  -0.0646   1.0000   0.0472
 -11.750  -0.6295   0.08016   0.07444  -0.0663   1.0000   0.0467
 -11.500  -0.6689   0.07496   0.06912  -0.0658   1.0000   0.0465
 -11.250  -0.7057   0.07092   0.06498  -0.0637   1.0000   0.0463
 -11.000  -0.7373   0.06746   0.06138  -0.0615   0.9993   0.0462
 -10.750  -0.7540   0.06307   0.05670  -0.0631   0.9937   0.0463
 -10.500  -0.7687   0.05962   0.05298  -0.0629   0.9868   0.0464
 -10.250  -0.7729   0.05608   0.04910  -0.0630   0.9812   0.0466
 -10.000  -0.7731   0.05284   0.04552  -0.0624   0.9756   0.0469
  -9.750  -0.7660   0.04970   0.04200  -0.0624   0.9715   0.0473
  -9.500  -0.7609   0.04714   0.03910  -0.0610   0.9661   0.0478
  -9.250  -0.7483   0.04447   0.03594  -0.0608   0.9623   0.0489
  -9.000  -0.7325   0.04245   0.03361  -0.0604   0.9585   0.0497
  -8.750  -0.7151   0.04111   0.03221  -0.0598   0.9542   0.0505
  -8.500  -0.6932   0.03970   0.03066  -0.0599   0.9512   0.0513
  -8.250  -0.6669   0.03822   0.02898  -0.0606   0.9488   0.0521
  -8.000  -0.6498   0.03698   0.02760  -0.0593   0.9438   0.0529
  -7.750  -0.6263   0.03574   0.02618  -0.0591   0.9402   0.0538
  -7.500  -0.5992   0.03455   0.02482  -0.0595   0.9376   0.0551
  -7.250  -0.5697   0.03351   0.02351  -0.0602   0.9356   0.0570
  -7.000  -0.5542   0.03275   0.02281  -0.0585   0.9305   0.0581
  -6.750  -0.5306   0.03201   0.02207  -0.0582   0.9270   0.0597
  -6.500  -0.5036   0.03124   0.02125  -0.0583   0.9246   0.0613
  -6.250  -0.4748   0.03050   0.02044  -0.0587   0.9227   0.0633
  -6.000  -0.4567   0.02996   0.01982  -0.0572   0.9185   0.0650
  -5.750  -0.4379   0.02933   0.01926  -0.0559   0.9140   0.0670
  -5.500  -0.4129   0.02872   0.01870  -0.0559   0.9108   0.0702
  -5.250  -0.3847   0.02816   0.01810  -0.0564   0.9084   0.0743
  -5.000  -0.3690   0.02765   0.01763  -0.0546   0.9039   0.0773
  -4.750  -0.3534   0.02718   0.01720  -0.0530   0.8988   0.0809
  -4.500  -0.3280   0.02666   0.01664  -0.0531   0.8953   0.0870
  -4.250  -0.2984   0.02599   0.01604  -0.0541   0.8926   0.0963
  -4.000  -0.2854   0.02554   0.01563  -0.0520   0.8852   0.1051
  -3.750  -0.2606   0.02494   0.01510  -0.0521   0.8808   0.1229
  -3.500  -0.2315   0.02418   0.01452  -0.0532   0.8779   0.1628
  -3.250  -0.2220   0.02222   0.01370  -0.0522   0.8722   0.3573
  -3.000  -0.2087   0.02228   0.01466  -0.0488   0.8671   0.5591
  -2.750  -0.1807   0.02267   0.01507  -0.0482   0.8640   0.6063
  -2.500  -0.1507   0.02325   0.01564  -0.0476   0.8616   0.6330
  -2.250  -0.1382   0.02386   0.01622  -0.0444   0.8547   0.6473
  -2.000  -0.1125   0.02430   0.01660  -0.0436   0.8507   0.6611
  -1.750  -0.0806   0.02450   0.01670  -0.0441   0.8477   0.6743
  -1.500  -0.0559   0.02504   0.01723  -0.0425   0.8436   0.6819
  -1.250  -0.0371   0.02530   0.01743  -0.0410   0.8365   0.6919
  -1.000  -0.0085   0.02559   0.01770  -0.0402   0.8328   0.6983
  -0.750   0.0279   0.02545   0.01746  -0.0419   0.8302   0.7075
  -0.500   0.0418   0.02575   0.01777  -0.0391   0.8216   0.7115
  -0.250   0.0743   0.02553   0.01750  -0.0396   0.8164   0.7158
   0.000   0.1159   0.02497   0.01685  -0.0421   0.8132   0.7197
   0.500   0.1653   0.02470   0.01651  -0.0413   0.7986   0.7268
   0.750   0.2001   0.02439   0.01619  -0.0424   0.7957   0.7297
   1.000   0.2394   0.02396   0.01572  -0.0443   0.7934   0.7330
   1.250   0.2497   0.02419   0.01594  -0.0417   0.7809   0.7382
   1.500   0.2885   0.02367   0.01540  -0.0435   0.7770   0.7417
   2.000   0.3369   0.02336   0.01512  -0.0418   0.7601   0.7488
   2.250   0.3582   0.02329   0.01505  -0.0408   0.7497   0.7538
   2.500   0.3913   0.02285   0.01461  -0.0415   0.7422   0.7576
   2.750   0.4084   0.02286   0.01467  -0.0395   0.7312   0.7609
   3.250   0.4604   0.02254   0.01442  -0.0387   0.7139   0.7701
   3.500   0.4935   0.02212   0.01403  -0.0393   0.7061   0.7739
   3.750   0.5087   0.02218   0.01415  -0.0370   0.6917   0.7775
   4.000   0.5329   0.02195   0.01395  -0.0361   0.6764   0.7816
   4.250   0.5646   0.02153   0.01351  -0.0364   0.6591   0.7860
   4.500   0.5960   0.02109   0.01305  -0.0365   0.6386   0.7894
   4.750   0.6237   0.02083   0.01277  -0.0361   0.6155   0.7927
   5.000   0.6499   0.02068   0.01258  -0.0355   0.5869   0.7963
   5.250   0.6827   0.02048   0.01223  -0.0361   0.5539   0.7998
   5.500   0.7076   0.02059   0.01221  -0.0356   0.5157   0.8037
   5.750   0.7279   0.02075   0.01220  -0.0341   0.4770   0.8065
   6.000   0.7457   0.02107   0.01232  -0.0324   0.4427   0.8098
   6.250   0.7618   0.02150   0.01259  -0.0306   0.4125   0.8139
   6.500   0.7789   0.02202   0.01291  -0.0291   0.3891   0.8185
   6.750   0.7943   0.02245   0.01330  -0.0272   0.3672   0.8222
   7.000   0.8097   0.02290   0.01371  -0.0254   0.3470   0.8261
   7.250   0.8252   0.02342   0.01418  -0.0237   0.3269   0.8306
   7.500   0.8408   0.02399   0.01470  -0.0222   0.3050   0.8350
   7.750   0.8531   0.02455   0.01521  -0.0201   0.2813   0.8384
   8.000   0.8666   0.02512   0.01575  -0.0183   0.2551   0.8421
   8.250   0.8790   0.02584   0.01635  -0.0165   0.2287   0.8458
   8.500   0.8915   0.02664   0.01700  -0.0149   0.2118   0.8493
   8.750   0.9048   0.02745   0.01771  -0.0133   0.1986   0.8527
   9.000   0.9195   0.02817   0.01843  -0.0119   0.1882   0.8563
   9.500   0.9501   0.02977   0.02005  -0.0096   0.1715   0.8646
   9.750   0.9642   0.03068   0.02092  -0.0084   0.1647   0.8686
  10.000   0.9805   0.03146   0.02177  -0.0074   0.1581   0.8726
  10.250   0.9957   0.03237   0.02270  -0.0064   0.1517   0.8765
  10.500   1.0121   0.03334   0.02365  -0.0056   0.1463   0.8802
  10.750   1.0295   0.03420   0.02464  -0.0050   0.1406   0.8840
  11.000   1.0454   0.03513   0.02560  -0.0042   0.1359   0.8881
  11.250   1.0619   0.03609   0.02663  -0.0035   0.1311   0.8926
  11.500   1.0775   0.03705   0.02774  -0.0028   0.1259   0.8972
  11.750   1.0918   0.03805   0.02879  -0.0020   0.1217   0.9015
  12.000   1.1069   0.03909   0.02997  -0.0014   0.1175   0.9063
  12.250   1.1215   0.04018   0.03122  -0.0008   0.1132   0.9118
  12.500   1.1353   0.04132   0.03245  -0.0004   0.1098   0.9187
  13.000   1.1587   0.04358   0.03499   0.0010   0.1034   1.0000
  13.250   1.1703   0.04500   0.03647   0.0015   0.1004   1.0000
  13.500   1.1823   0.04643   0.03789   0.0018   0.0979   1.0000
  13.750   1.1937   0.04808   0.03968   0.0023   0.0950   1.0000
  14.000   1.2033   0.04983   0.04158   0.0027   0.0921   1.0000
  14.250   1.2127   0.05156   0.04339   0.0031   0.0896   1.0000
  14.500   1.2237   0.05322   0.04505   0.0034   0.0874   1.0000
  14.750   1.2298   0.05537   0.04737   0.0038   0.0850   1.0000
  15.000   1.2315   0.05785   0.05011   0.0042   0.0825   1.0000
  15.250   1.2342   0.06027   0.05268   0.0044   0.0803   1.0000
  15.500   1.2383   0.06256   0.05505   0.0045   0.0783   1.0000
  15.750   1.2456   0.06463   0.05709   0.0045   0.0765   1.0000
  16.000   1.2371   0.06836   0.06117   0.0044   0.0746   1.0000
  16.250   1.2303   0.07209   0.06515   0.0040   0.0729   1.0000
  16.500   1.2238   0.07584   0.06910   0.0033   0.0712   1.0000
  16.750   1.2197   0.07940   0.07279   0.0024   0.0697   1.0000
  17.000   1.2197   0.08248   0.07592   0.0014   0.0682   1.0000
  17.250   1.2144   0.08644   0.07998   0.0001   0.0669   1.0000
  17.500   1.1921   0.09313   0.08699  -0.0026   0.0659   1.0000
  17.750   1.1664   0.10077   0.09493  -0.0062   0.0649   1.0000
  18.000   1.1327   0.11035   0.10480  -0.0115   0.0642   1.0000
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