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DORNIER A-5 AIRFOIL (doa5-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: DORNIER A-5 AIRFOIL (doa5-il)
Reynolds number: 200,000
Max Cl/Cd: 49.24 at α=3.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-doa5-il-200000-n5.txt
Download as CSV file: xf-doa5-il-200000-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 =     0.200 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -14.000  -0.6821   0.08107   0.07662  -0.0736   1.0000   0.0314
 -13.750  -0.7274   0.07301   0.06837  -0.0762   1.0000   0.0313
 -13.500  -0.7669   0.06690   0.06205  -0.0767   1.0000   0.0313
 -13.250  -0.7974   0.06170   0.05661  -0.0771   0.9993   0.0313
 -13.000  -0.8206   0.05570   0.05021  -0.0799   0.9961   0.0315
 -12.750  -0.8293   0.05164   0.04586  -0.0815   0.9930   0.0317
 -12.500  -0.8265   0.04904   0.04312  -0.0821   0.9895   0.0319
 -12.250  -0.8189   0.04681   0.04076  -0.0830   0.9861   0.0322
 -12.000  -0.8077   0.04470   0.03848  -0.0843   0.9834   0.0325
 -11.750  -0.8015   0.04288   0.03653  -0.0840   0.9783   0.0328
 -11.500  -0.7894   0.04126   0.03477  -0.0845   0.9745   0.0333
 -11.250  -0.7768   0.03964   0.03299  -0.0848   0.9708   0.0338
 -11.000  -0.7681   0.03814   0.03132  -0.0840   0.9650   0.0344
 -10.750  -0.7501   0.03636   0.02928  -0.0845   0.9619   0.0350
 -10.500  -0.7358   0.03476   0.02746  -0.0838   0.9571   0.0355
 -10.250  -0.7179   0.03325   0.02573  -0.0834   0.9526   0.0360
 -10.000  -0.6937   0.03182   0.02405  -0.0839   0.9501   0.0365
  -9.750  -0.6662   0.03054   0.02262  -0.0848   0.9486   0.0370
  -9.500  -0.6537   0.02974   0.02181  -0.0827   0.9421   0.0375
  -9.250  -0.6297   0.02891   0.02097  -0.0829   0.9391   0.0382
  -9.000  -0.6026   0.02807   0.02008  -0.0836   0.9371   0.0390
  -8.750  -0.5739   0.02721   0.01915  -0.0845   0.9356   0.0399
  -8.500  -0.5624   0.02662   0.01849  -0.0820   0.9289   0.0406
  -8.250  -0.5369   0.02585   0.01764  -0.0820   0.9263   0.0413
  -8.000  -0.5094   0.02508   0.01680  -0.0824   0.9244   0.0421
  -7.750  -0.4803   0.02434   0.01599  -0.0832   0.9229   0.0428
  -7.500  -0.4646   0.02368   0.01536  -0.0815   0.9173   0.0435
  -7.250  -0.4435   0.02303   0.01472  -0.0809   0.9130   0.0445
  -7.000  -0.4171   0.02237   0.01406  -0.0813   0.9106   0.0457
  -6.750  -0.3885   0.02171   0.01338  -0.0821   0.9088   0.0475
  -6.500  -0.3590   0.02104   0.01266  -0.0830   0.9074   0.0491
  -6.250  -0.3559   0.02073   0.01236  -0.0789   0.8988   0.0502
  -6.000  -0.3320   0.02017   0.01181  -0.0789   0.8961   0.0519
  -5.750  -0.3045   0.01962   0.01125  -0.0795   0.8941   0.0541
  -5.500  -0.2750   0.01908   0.01067  -0.0804   0.8927   0.0569
  -5.250  -0.2691   0.01884   0.01045  -0.0767   0.8847   0.0589
  -5.000  -0.2441   0.01840   0.01000  -0.0767   0.8812   0.0633
  -4.750  -0.2148   0.01785   0.00946  -0.0775   0.8789   0.0691
  -4.500  -0.1832   0.01733   0.00891  -0.0788   0.8772   0.0769
  -4.250  -0.1744   0.01711   0.00873  -0.0756   0.8698   0.0829
  -4.000  -0.1489   0.01667   0.00833  -0.0756   0.8662   0.0936
  -3.750  -0.1183   0.01614   0.00787  -0.0767   0.8639   0.1146
  -3.500  -0.0854   0.01541   0.00735  -0.0784   0.8619   0.1651
  -3.250  -0.0776   0.01410   0.00675  -0.0761   0.8547   0.3249
  -3.000  -0.0555   0.01317   0.00668  -0.0757   0.8510   0.5335
  -2.750  -0.0226   0.01305   0.00666  -0.0765   0.8487   0.5744
  -2.500   0.0136   0.01301   0.00667  -0.0779   0.8469   0.6015
  -2.250   0.0412   0.01305   0.00670  -0.0777   0.8429   0.6199
  -2.000   0.0652   0.01315   0.00682  -0.0766   0.8374   0.6316
  -1.750   0.1013   0.01306   0.00665  -0.0782   0.8340   0.6413
  -1.500   0.1418   0.01306   0.00665  -0.0803   0.8312   0.6481
  -1.250   0.1767   0.01299   0.00653  -0.0816   0.8264   0.6550
  -1.000   0.2017   0.01303   0.00655  -0.0809   0.8193   0.6603
  -0.750   0.2436   0.01298   0.00646  -0.0834   0.8139   0.6663
  -0.500   0.2738   0.01294   0.00634  -0.0839   0.8073   0.6741
  -0.250   0.2981   0.01307   0.00650  -0.0829   0.7995   0.6779
   0.000   0.3360   0.01308   0.00647  -0.0847   0.7943   0.6821
   0.250   0.3549   0.01312   0.00651  -0.0829   0.7865   0.6870
   0.500   0.3809   0.01309   0.00645  -0.0826   0.7796   0.6912
   0.750   0.4101   0.01310   0.00646  -0.0827   0.7719   0.6933
   1.000   0.4272   0.01315   0.00654  -0.0804   0.7617   0.6959
   1.250   0.4504   0.01316   0.00655  -0.0793   0.7525   0.6990
   1.500   0.4731   0.01312   0.00649  -0.0782   0.7416   0.7027
   1.750   0.4935   0.01307   0.00642  -0.0767   0.7300   0.7072
   2.000   0.5209   0.01307   0.00642  -0.0764   0.7196   0.7092
   2.250   0.5448   0.01310   0.00644  -0.0755   0.7075   0.7116
   2.500   0.5659   0.01313   0.00647  -0.0740   0.6918   0.7146
   2.750   0.5920   0.01313   0.00641  -0.0735   0.6721   0.7182
   3.000   0.6205   0.01315   0.00627  -0.0736   0.6473   0.7230
   3.250   0.6412   0.01329   0.00632  -0.0720   0.6175   0.7256
   3.500   0.6600   0.01349   0.00640  -0.0700   0.5853   0.7281
   3.750   0.6770   0.01375   0.00651  -0.0678   0.5546   0.7310
   4.000   0.6912   0.01406   0.00667  -0.0651   0.5167   0.7345
   4.250   0.7010   0.01452   0.00688  -0.0617   0.4704   0.7389
   4.500   0.7080   0.01507   0.00720  -0.0579   0.4260   0.7421
   4.750   0.7161   0.01563   0.00758  -0.0542   0.3983   0.7450
   5.000   0.7303   0.01605   0.00794  -0.0518   0.3801   0.7486
   5.250   0.7465   0.01645   0.00826  -0.0499   0.3626   0.7525
   5.500   0.7637   0.01685   0.00857  -0.0483   0.3461   0.7565
   5.750   0.7787   0.01724   0.00892  -0.0461   0.3300   0.7585
   6.000   0.7940   0.01765   0.00929  -0.0441   0.3130   0.7609
   6.250   0.8101   0.01804   0.00964  -0.0422   0.2928   0.7637
   6.500   0.8261   0.01846   0.01000  -0.0405   0.2710   0.7668
   6.750   0.8407   0.01897   0.01039  -0.0386   0.2385   0.7701
   7.000   0.8519   0.01963   0.01086  -0.0362   0.2100   0.7730
   7.250   0.8646   0.02021   0.01137  -0.0340   0.1951   0.7753
   7.500   0.8800   0.02072   0.01186  -0.0323   0.1837   0.7778
   7.750   0.8953   0.02125   0.01239  -0.0306   0.1749   0.7807
   8.000   0.9108   0.02181   0.01294  -0.0290   0.1672   0.7841
   8.250   0.9264   0.02241   0.01352  -0.0275   0.1606   0.7875
   8.500   0.9411   0.02294   0.01409  -0.0258   0.1547   0.7900
   8.750   0.9538   0.02362   0.01475  -0.0239   0.1490   0.7926
   9.000   0.9705   0.02413   0.01534  -0.0225   0.1436   0.7951
   9.250   0.9858   0.02474   0.01598  -0.0211   0.1378   0.7977
   9.500   0.9994   0.02548   0.01671  -0.0195   0.1333   0.8002
   9.750   1.0174   0.02600   0.01732  -0.0186   0.1282   0.8028
  10.000   1.0324   0.02662   0.01799  -0.0172   0.1227   0.8052
  10.250   1.0467   0.02726   0.01868  -0.0157   0.1178   0.8078
  10.500   1.0619   0.02788   0.01936  -0.0144   0.1127   0.8107
  10.750   1.0755   0.02864   0.02012  -0.0131   0.1081   0.8134
  11.000   1.0902   0.02940   0.02093  -0.0120   0.1043   0.8159
  11.250   1.1036   0.03026   0.02181  -0.0108   0.1008   0.8181
  11.500   1.1145   0.03127   0.02281  -0.0094   0.0977   0.8203
  11.750   1.1276   0.03216   0.02378  -0.0081   0.0948   0.8225
  12.000   1.1403   0.03312   0.02484  -0.0070   0.0920   0.8247
  12.250   1.1516   0.03421   0.02597  -0.0059   0.0893   0.8270
  12.500   1.1610   0.03550   0.02726  -0.0047   0.0870   0.8291
  12.750   1.1744   0.03654   0.02842  -0.0038   0.0847   0.8312
  13.000   1.1875   0.03763   0.02962  -0.0030   0.0822   0.8332
  13.500   1.2089   0.04017   0.03232  -0.0014   0.0776   0.8371
  13.750   1.2190   0.04155   0.03378  -0.0006   0.0756   0.8391
  14.000   1.2307   0.04284   0.03521   0.0000   0.0734   0.8412
  14.250   1.2407   0.04426   0.03675   0.0006   0.0711   0.8434
  14.500   1.2492   0.04584   0.03840   0.0012   0.0692   0.8459
  14.750   1.2552   0.04767   0.04026   0.0017   0.0674   0.8487
  15.000   1.2643   0.04932   0.04207   0.0021   0.0655   0.8517
  15.250   1.2722   0.05111   0.04400   0.0024   0.0634   0.8549
  15.500   1.2781   0.05313   0.04611   0.0026   0.0615   0.8583
  15.750   1.2819   0.05541   0.04846   0.0027   0.0599   0.8616
  16.000   1.2854   0.05782   0.05094   0.0027   0.0583   0.8649
  16.250   1.2907   0.06015   0.05345   0.0025   0.0565   0.8682
  16.500   1.2944   0.06273   0.05618   0.0022   0.0548   0.8715
  16.750   1.2967   0.06554   0.05911   0.0016   0.0533   0.8751
  17.000   1.2968   0.06868   0.06233   0.0009   0.0520   0.8790
  17.500   1.2972   0.07533   0.06930  -0.0011   0.0492   0.8884
  17.750   1.2970   0.07892   0.07307  -0.0024   0.0478   0.8949
  18.000   1.2959   0.08283   0.07717  -0.0043   0.0464   0.9041
  18.250   1.2933   0.08711   0.08162  -0.0068   0.0453   0.9320
  18.500   1.2829   0.09102   0.08560  -0.0074   0.0445   1.0000
  18.750   1.2769   0.09561   0.09030  -0.0094   0.0435   1.0000
  19.000   1.2701   0.10048   0.09536  -0.0118   0.0423   1.0000
  19.250   1.2621   0.10560   0.10064  -0.0143   0.0414   1.0000
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