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DORNIER A-5 AIRFOIL (doa5-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: DORNIER A-5 AIRFOIL (doa5-il)
Reynolds number: 500,000
Max Cl/Cd: 75.72 at α=3.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-doa5-il-500000.txt
Download as CSV file: xf-doa5-il-500000.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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -14.250  -0.7250   0.07832   0.07534  -0.0731   1.0000   0.0304
 -14.000  -0.7555   0.07232   0.06925  -0.0743   1.0000   0.0302
 -13.750  -0.7934   0.06644   0.06321  -0.0747   1.0000   0.0302
 -13.500  -0.8244   0.06064   0.05721  -0.0760   0.9993   0.0301
 -13.250  -0.8469   0.05444   0.05072  -0.0794   0.9967   0.0300
 -13.000  -0.8655   0.04948   0.04538  -0.0823   0.9938   0.0303
 -12.750  -0.8752   0.04607   0.04168  -0.0831   0.9892   0.0304
 -12.500  -0.8828   0.04181   0.03708  -0.0844   0.9854   0.0307
 -12.250  -0.8714   0.03853   0.03360  -0.0860   0.9837   0.0310
 -12.000  -0.8639   0.03672   0.03169  -0.0852   0.9780   0.0313
 -11.750  -0.8453   0.03522   0.03010  -0.0861   0.9751   0.0317
 -11.500  -0.8215   0.03389   0.02868  -0.0876   0.9734   0.0320
 -11.250  -0.8044   0.03283   0.02756  -0.0872   0.9689   0.0325
 -11.000  -0.7837   0.03142   0.02602  -0.0877   0.9651   0.0331
 -10.750  -0.7582   0.02996   0.02440  -0.0889   0.9629   0.0338
 -10.500  -0.7305   0.02839   0.02263  -0.0903   0.9615   0.0343
 -10.250  -0.7008   0.02697   0.02103  -0.0918   0.9606   0.0347
 -10.000  -0.6871   0.02607   0.02000  -0.0899   0.9538   0.0351
  -9.750  -0.6603   0.02518   0.01896  -0.0907   0.9512   0.0354
  -9.500  -0.6288   0.02360   0.01733  -0.0917   0.9506   0.0361
  -9.250  -0.5973   0.02271   0.01647  -0.0930   0.9495   0.0369
  -9.000  -0.5652   0.02196   0.01571  -0.0945   0.9486   0.0376
  -8.750  -0.5324   0.02120   0.01491  -0.0960   0.9478   0.0384
  -8.500  -0.5173   0.02064   0.01432  -0.0940   0.9413   0.0388
  -8.250  -0.4891   0.01994   0.01358  -0.0945   0.9387   0.0395
  -8.000  -0.4576   0.01925   0.01285  -0.0956   0.9371   0.0403
  -7.750  -0.4250   0.01860   0.01215  -0.0971   0.9359   0.0410
  -7.500  -0.3947   0.01764   0.01120  -0.0982   0.9348   0.0422
  -7.250  -0.3624   0.01693   0.01051  -0.1000   0.9338   0.0433
  -7.000  -0.3520   0.01655   0.01013  -0.0971   0.9266   0.0442
  -6.750  -0.3237   0.01599   0.00955  -0.0979   0.9241   0.0454
  -6.500  -0.2920   0.01544   0.00897  -0.0993   0.9224   0.0468
  -6.250  -0.2594   0.01475   0.00826  -0.1012   0.9210   0.0484
  -6.000  -0.2254   0.01414   0.00767  -0.1032   0.9196   0.0508
  -5.750  -0.1895   0.01368   0.00721  -0.1054   0.9183   0.0537
  -5.500  -0.1826   0.01345   0.00696  -0.1015   0.9103   0.0558
  -5.250  -0.1516   0.01302   0.00656  -0.1027   0.9078   0.0605
  -5.000  -0.1185   0.01254   0.00610  -0.1043   0.9057   0.0671
  -4.750  -0.0831   0.01202   0.00560  -0.1065   0.9036   0.0782
  -4.500  -0.0696   0.01176   0.00537  -0.1038   0.8967   0.0882
  -4.250  -0.0414   0.01129   0.00499  -0.1043   0.8919   0.1096
  -4.000  -0.0088   0.01057   0.00452  -0.1060   0.8882   0.1727
  -3.750  -0.0085   0.00877   0.00375  -0.1025   0.8805   0.4383
  -3.500   0.0165   0.00829   0.00357  -0.1022   0.8755   0.5307
  -3.250   0.0503   0.00810   0.00343  -0.1034   0.8718   0.5680
  -3.000   0.0735   0.00806   0.00342  -0.1024   0.8664   0.5868
  -2.750   0.1002   0.00802   0.00339  -0.1020   0.8617   0.6018
  -2.500   0.1316   0.00799   0.00335  -0.1027   0.8578   0.6163
  -2.250   0.1648   0.00799   0.00334  -0.1037   0.8540   0.6304
  -2.000   0.1885   0.00803   0.00336  -0.1027   0.8484   0.6415
  -1.750   0.2184   0.00804   0.00338  -0.1030   0.8436   0.6477
  -1.500   0.2542   0.00805   0.00334  -0.1046   0.8396   0.6545
  -1.250   0.2795   0.00810   0.00339  -0.1040   0.8342   0.6604
  -1.000   0.3074   0.00815   0.00343  -0.1039   0.8285   0.6647
  -0.750   0.3428   0.00819   0.00341  -0.1054   0.8227   0.6693
  -0.500   0.3659   0.00823   0.00341  -0.1043   0.8154   0.6747
  -0.250   0.3944   0.00829   0.00347  -0.1043   0.8082   0.6786
   0.000   0.4229   0.00839   0.00357  -0.1043   0.8018   0.6830
   0.250   0.4463   0.00844   0.00363  -0.1032   0.7944   0.6881
   0.500   0.4764   0.00851   0.00365  -0.1036   0.7880   0.6931
   0.750   0.4974   0.00858   0.00377  -0.1020   0.7799   0.6964
   1.000   0.5231   0.00863   0.00382  -0.1013   0.7717   0.6998
   1.250   0.5453   0.00866   0.00386  -0.1000   0.7629   0.7034
   1.500   0.5700   0.00866   0.00382  -0.0993   0.7542   0.7074
   1.750   0.5913   0.00866   0.00385  -0.0978   0.7436   0.7101
   2.000   0.6126   0.00870   0.00388  -0.0963   0.7299   0.7124
   2.250   0.6340   0.00877   0.00392  -0.0947   0.7154   0.7149
   2.500   0.6546   0.00885   0.00396  -0.0931   0.6993   0.7179
   2.750   0.6718   0.00894   0.00398  -0.0907   0.6760   0.7215
   3.000   0.6869   0.00909   0.00398  -0.0880   0.6519   0.7253
   3.250   0.7012   0.00926   0.00408  -0.0850   0.6252   0.7273
   3.500   0.7123   0.00952   0.00423  -0.0814   0.5908   0.7296
   3.750   0.7204   0.00989   0.00443  -0.0773   0.5546   0.7323
   4.000   0.7287   0.01032   0.00469  -0.0733   0.5108   0.7355
   4.250   0.7297   0.01099   0.00502  -0.0681   0.4470   0.7394
   4.500   0.7367   0.01157   0.00537  -0.0642   0.4037   0.7425
   4.750   0.7508   0.01198   0.00568  -0.0616   0.3823   0.7446
   5.000   0.7674   0.01233   0.00598  -0.0595   0.3636   0.7470
   5.250   0.7847   0.01266   0.00626  -0.0576   0.3470   0.7498
   5.500   0.8023   0.01300   0.00653  -0.0558   0.3323   0.7532
   5.750   0.8202   0.01336   0.00682  -0.0542   0.3170   0.7569
   6.000   0.8379   0.01364   0.00708  -0.0524   0.3008   0.7595
   6.250   0.8548   0.01397   0.00736  -0.0505   0.2801   0.7619
   6.750   0.8810   0.01504   0.00810  -0.0457   0.2091   0.7679
   7.000   0.8951   0.01558   0.00853  -0.0436   0.1916   0.7710
   7.250   0.9110   0.01605   0.00894  -0.0418   0.1802   0.7737
   7.500   0.9260   0.01648   0.00934  -0.0398   0.1707   0.7758
   7.750   0.9429   0.01686   0.00974  -0.0381   0.1638   0.7780
   8.000   0.9582   0.01734   0.01019  -0.0363   0.1565   0.7805
   8.250   0.9748   0.01778   0.01065  -0.0347   0.1504   0.7831
   8.500   0.9920   0.01821   0.01109  -0.0332   0.1441   0.7858
   8.750   1.0057   0.01886   0.01168  -0.0313   0.1369   0.7884
   9.000   1.0255   0.01908   0.01197  -0.0302   0.1313   0.7907
   9.250   1.0411   0.01954   0.01242  -0.0286   0.1246   0.7933
   9.500   1.0581   0.01996   0.01289  -0.0271   0.1195   0.7960
   9.750   1.0756   0.02038   0.01331  -0.0258   0.1137   0.7990
  10.000   1.0904   0.02097   0.01387  -0.0242   0.1084   0.8016
  10.250   1.1067   0.02151   0.01442  -0.0229   0.1045   0.8036
  10.500   1.1204   0.02213   0.01503  -0.0212   0.1003   0.8056
  10.750   1.1310   0.02291   0.01582  -0.0192   0.0965   0.8076
  11.000   1.1468   0.02345   0.01644  -0.0179   0.0937   0.8097
  11.250   1.1603   0.02414   0.01717  -0.0163   0.0908   0.8120
  11.500   1.1712   0.02501   0.01805  -0.0145   0.0877   0.8145
  11.750   1.1795   0.02609   0.01914  -0.0125   0.0848   0.8170
  12.000   1.1968   0.02663   0.01976  -0.0116   0.0827   0.8192
  12.250   1.2115   0.02729   0.02048  -0.0104   0.0802   0.8212
  12.500   1.2248   0.02804   0.02129  -0.0092   0.0778   0.8232
  12.750   1.2335   0.02915   0.02240  -0.0075   0.0752   0.8251
  13.000   1.2465   0.02999   0.02332  -0.0063   0.0730   0.8271
  13.250   1.2616   0.03070   0.02411  -0.0054   0.0708   0.8290
  13.500   1.2746   0.03157   0.02501  -0.0043   0.0683   0.8312
  13.750   1.2834   0.03278   0.02621  -0.0030   0.0658   0.8333
  14.000   1.2934   0.03394   0.02745  -0.0018   0.0638   0.8352
  14.250   1.3059   0.03492   0.02850  -0.0009   0.0616   0.8373
  14.500   1.3156   0.03612   0.02975   0.0001   0.0594   0.8392
  14.750   1.3200   0.03778   0.03143   0.0014   0.0572   0.8411
  15.000   1.3289   0.03915   0.03290   0.0023   0.0554   0.8431
  15.250   1.3388   0.04048   0.03432   0.0031   0.0535   0.8452
  15.500   1.3465   0.04204   0.03594   0.0038   0.0518   0.8472
  15.750   1.3501   0.04399   0.03791   0.0046   0.0500   0.8492
  16.000   1.3542   0.04598   0.03998   0.0053   0.0483   0.8513
  16.250   1.3628   0.04760   0.04172   0.0057   0.0467   0.8536
  16.500   1.3688   0.04951   0.04372   0.0061   0.0451   0.8563
  16.750   1.3728   0.05176   0.04602   0.0062   0.0437   0.8592
  17.000   1.3707   0.05469   0.04901   0.0063   0.0423   0.8623
  17.250   1.3770   0.05684   0.05130   0.0062   0.0411   0.8654
  17.500   1.3821   0.05922   0.05377   0.0059   0.0397   0.8680
  17.750   1.3842   0.06206   0.05671   0.0053   0.0385   0.8708
  18.000   1.3821   0.06550   0.06020   0.0045   0.0373   0.8738
  18.250   1.3780   0.06928   0.06408   0.0035   0.0363   0.8768
  18.500   1.3792   0.07260   0.06755   0.0023   0.0353   0.8804
  18.750   1.3781   0.07636   0.07144   0.0008   0.0344   0.8842
  19.000   1.3764   0.08049   0.07569  -0.0012   0.0334   0.8888
  19.250   1.3715   0.08519   0.08049  -0.0036   0.0327   0.8942
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