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DORNIER A-5 AIRFOIL (doa5-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: DORNIER A-5 AIRFOIL (doa5-il)
Reynolds number: 1,000,000
Max Cl/Cd: 87.62 at α=1.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-doa5-il-1000000.txt
Download as CSV file: xf-doa5-il-1000000.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 =     1.000 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -18.000  -0.9165   0.08478   0.08214  -0.0769   1.0000   0.0206
 -17.750  -0.9510   0.07621   0.07337  -0.0810   1.0000   0.0206
 -17.500  -0.9706   0.07062   0.06764  -0.0830   1.0000   0.0207
 -17.250  -0.9898   0.06547   0.06236  -0.0845   1.0000   0.0208
 -17.000  -0.9969   0.06222   0.05903  -0.0850   1.0000   0.0210
 -16.750  -1.0077   0.05877   0.05547  -0.0852   1.0000   0.0212
 -16.500  -1.0219   0.05517   0.05174  -0.0850   1.0000   0.0212
 -16.250  -1.0272   0.05189   0.04833  -0.0858   0.9997   0.0213
 -16.000  -1.0231   0.04894   0.04524  -0.0878   0.9989   0.0216
 -15.750  -1.0162   0.04643   0.04261  -0.0896   0.9978   0.0218
 -15.500  -1.0094   0.04398   0.04003  -0.0912   0.9967   0.0219
 -15.250  -0.9981   0.04212   0.03806  -0.0928   0.9955   0.0221
 -15.000  -0.9969   0.03900   0.03474  -0.0939   0.9945   0.0224
 -14.750  -0.9878   0.03665   0.03227  -0.0948   0.9938   0.0227
 -14.500  -0.9761   0.03511   0.03069  -0.0950   0.9919   0.0229
 -14.250  -0.9606   0.03389   0.02945  -0.0957   0.9901   0.0232
 -14.000  -0.9442   0.03264   0.02815  -0.0965   0.9885   0.0234
 -13.750  -0.9255   0.03156   0.02703  -0.0975   0.9871   0.0238
 -13.500  -0.9062   0.03037   0.02576  -0.0986   0.9860   0.0241
 -13.250  -0.8853   0.02922   0.02454  -0.0997   0.9850   0.0243
 -13.000  -0.8629   0.02816   0.02341  -0.1010   0.9843   0.0246
 -12.750  -0.8396   0.02708   0.02225  -0.1022   0.9837   0.0249
 -12.500  -0.8283   0.02622   0.02133  -0.1008   0.9794   0.0252
 -12.250  -0.8062   0.02532   0.02037  -0.1014   0.9775   0.0255
 -12.000  -0.7816   0.02447   0.01945  -0.1025   0.9760   0.0258
 -11.750  -0.7554   0.02369   0.01859  -0.1038   0.9749   0.0260
 -11.500  -0.7301   0.02255   0.01738  -0.1045   0.9741   0.0265
 -11.250  -0.7038   0.02161   0.01642  -0.1055   0.9734   0.0269
 -11.000  -0.6758   0.02087   0.01568  -0.1069   0.9727   0.0274
 -10.750  -0.6605   0.02025   0.01505  -0.1057   0.9684   0.0277
 -10.500  -0.6359   0.01957   0.01434  -0.1062   0.9663   0.0280
 -10.250  -0.6089   0.01889   0.01364  -0.1072   0.9648   0.0284
 -10.000  -0.5806   0.01822   0.01294  -0.1084   0.9637   0.0288
  -9.750  -0.5507   0.01761   0.01230  -0.1099   0.9626   0.0294
  -9.500  -0.5197   0.01702   0.01168  -0.1116   0.9617   0.0298
  -9.250  -0.4871   0.01647   0.01110  -0.1135   0.9607   0.0302
  -9.000  -0.4734   0.01599   0.01059  -0.1116   0.9542   0.0304
  -8.750  -0.4480   0.01508   0.00965  -0.1126   0.9509   0.0311
  -8.500  -0.4159   0.01429   0.00885  -0.1149   0.9488   0.0318
  -8.250  -0.3811   0.01367   0.00823  -0.1175   0.9470   0.0325
  -8.000  -0.3759   0.01322   0.00775  -0.1139   0.9371   0.0328
  -7.750  -0.3433   0.01271   0.00721  -0.1158   0.9341   0.0337
  -7.500  -0.3220   0.01233   0.00681  -0.1152   0.9277   0.0344
  -7.250  -0.2941   0.01193   0.00637  -0.1159   0.9226   0.0350
  -7.000  -0.2606   0.01148   0.00588  -0.1178   0.9190   0.0359
  -6.750  -0.2437   0.01108   0.00545  -0.1162   0.9116   0.0370
  -6.500  -0.2163   0.01075   0.00511  -0.1167   0.9066   0.0384
  -6.250  -0.1843   0.01047   0.00479  -0.1181   0.9023   0.0399
  -6.000  -0.1688   0.01028   0.00458  -0.1158   0.8943   0.0409
  -5.750  -0.1425   0.00995   0.00422  -0.1159   0.8878   0.0436
  -5.500  -0.1247   0.00973   0.00401  -0.1140   0.8785   0.0460
  -5.250  -0.0993   0.00949   0.00374  -0.1138   0.8707   0.0501
  -5.000  -0.0777   0.00927   0.00356  -0.1127   0.8642   0.0563
  -4.750  -0.0530   0.00905   0.00336  -0.1123   0.8578   0.0665
  -4.500  -0.0270   0.00889   0.00319  -0.1122   0.8528   0.0745
  -4.250  -0.0027   0.00868   0.00301  -0.1117   0.8470   0.0838
  -4.000   0.0235   0.00849   0.00283  -0.1116   0.8414   0.0974
  -3.750   0.0483   0.00821   0.00266  -0.1113   0.8367   0.1302
  -3.500   0.0713   0.00788   0.00249  -0.1107   0.8319   0.1798
  -3.250   0.0821   0.00631   0.00186  -0.1089   0.8264   0.4550
  -3.000   0.1096   0.00607   0.00177  -0.1091   0.8216   0.5140
  -2.750   0.1343   0.00597   0.00174  -0.1084   0.8177   0.5385
  -2.500   0.1604   0.00591   0.00172  -0.1081   0.8135   0.5569
  -2.250   0.1882   0.00589   0.00171  -0.1081   0.8089   0.5750
  -2.000   0.2158   0.00590   0.00171  -0.1080   0.8027   0.5903
  -1.750   0.2400   0.00587   0.00171  -0.1072   0.7967   0.6039
  -1.500   0.2666   0.00587   0.00171  -0.1069   0.7906   0.6133
  -1.250   0.2937   0.00589   0.00171  -0.1066   0.7850   0.6204
  -1.000   0.3189   0.00588   0.00169  -0.1060   0.7794   0.6255
  -0.750   0.3449   0.00587   0.00169  -0.1056   0.7734   0.6316
  -0.500   0.3713   0.00588   0.00169  -0.1052   0.7677   0.6377
  -0.250   0.3962   0.00587   0.00168  -0.1045   0.7598   0.6423
   0.000   0.4210   0.00588   0.00168  -0.1038   0.7520   0.6472
   0.250   0.4455   0.00588   0.00169  -0.1031   0.7425   0.6518
   0.500   0.4688   0.00592   0.00168  -0.1020   0.7307   0.6571
   0.750   0.4901   0.00598   0.00171  -0.1005   0.7162   0.6625
   1.000   0.5115   0.00606   0.00175  -0.0991   0.7008   0.6676
   1.250   0.5323   0.00616   0.00178  -0.0975   0.6822   0.6733
   1.500   0.5493   0.00627   0.00182  -0.0951   0.6613   0.6774
   1.750   0.5643   0.00644   0.00191  -0.0922   0.6365   0.6817
   2.000   0.5802   0.00665   0.00201  -0.0896   0.6058   0.6858
   2.250   0.5941   0.00692   0.00212  -0.0867   0.5720   0.6898
   2.500   0.6073   0.00724   0.00229  -0.0836   0.5349   0.6938
   2.750   0.6135   0.00779   0.00256  -0.0792   0.4659   0.6975
   3.000   0.6226   0.00836   0.00286  -0.0756   0.4053   0.7008
   3.250   0.6403   0.00869   0.00307  -0.0736   0.3797   0.7042
   3.500   0.6588   0.00899   0.00326  -0.0718   0.3567   0.7073
   3.750   0.6784   0.00923   0.00343  -0.0702   0.3398   0.7103
   4.000   0.6998   0.00942   0.00361  -0.0690   0.3285   0.7130
   4.250   0.7204   0.00966   0.00380  -0.0676   0.3164   0.7157
   4.500   0.7419   0.00986   0.00397  -0.0664   0.3049   0.7186
   4.750   0.7627   0.01008   0.00416  -0.0651   0.2920   0.7216
   5.000   0.7827   0.01035   0.00434  -0.0637   0.2750   0.7243
   5.250   0.7995   0.01071   0.00457  -0.0618   0.2441   0.7268
   5.500   0.8106   0.01130   0.00494  -0.0588   0.2003   0.7291
   5.750   0.8273   0.01169   0.00527  -0.0568   0.1819   0.7314
   6.000   0.8459   0.01203   0.00555  -0.0553   0.1705   0.7338
   6.250   0.8658   0.01232   0.00582  -0.0539   0.1637   0.7362
   6.500   0.8848   0.01263   0.00610  -0.0524   0.1575   0.7386
   6.750   0.9045   0.01293   0.00638  -0.0511   0.1520   0.7408
   7.000   0.9253   0.01315   0.00662  -0.0499   0.1488   0.7432
   7.250   0.9447   0.01344   0.00692  -0.0486   0.1440   0.7453
   7.500   0.9626   0.01380   0.00728  -0.0470   0.1381   0.7474
   7.750   0.9836   0.01403   0.00754  -0.0459   0.1347   0.7497
   8.000   1.0031   0.01433   0.00783  -0.0446   0.1271   0.7519
   8.250   1.0222   0.01466   0.00814  -0.0433   0.1203   0.7540
   8.500   1.0404   0.01504   0.00846  -0.0419   0.1109   0.7559
   8.750   1.0583   0.01544   0.00882  -0.0404   0.1052   0.7574
   9.000   1.0752   0.01583   0.00918  -0.0388   0.1000   0.7593
   9.250   1.0921   0.01622   0.00960  -0.0373   0.0960   0.7611
   9.500   1.1098   0.01660   0.01001  -0.0358   0.0935   0.7629
   9.750   1.1264   0.01705   0.01046  -0.0343   0.0903   0.7647
  10.000   1.1407   0.01762   0.01103  -0.0324   0.0860   0.7668
  10.250   1.1585   0.01802   0.01147  -0.0311   0.0841   0.7687
  10.500   1.1768   0.01840   0.01188  -0.0299   0.0818   0.7706
  10.750   1.1940   0.01886   0.01235  -0.0286   0.0792   0.7722
  11.000   1.2087   0.01943   0.01292  -0.0269   0.0758   0.7736
  11.250   1.2245   0.01990   0.01342  -0.0255   0.0735   0.7755
  11.500   1.2419   0.02033   0.01388  -0.0243   0.0713   0.7770
  11.750   1.2574   0.02086   0.01443  -0.0229   0.0689   0.7786
  12.000   1.2709   0.02152   0.01508  -0.0212   0.0656   0.7804
  12.250   1.2862   0.02209   0.01570  -0.0199   0.0639   0.7822
  12.500   1.3012   0.02269   0.01633  -0.0185   0.0622   0.7840
  12.750   1.3149   0.02339   0.01703  -0.0171   0.0599   0.7856
  13.000   1.3261   0.02425   0.01789  -0.0154   0.0572   0.7869
  13.250   1.3404   0.02494   0.01863  -0.0141   0.0557   0.7880
  13.500   1.3548   0.02562   0.01936  -0.0129   0.0540   0.7891
  13.750   1.3676   0.02640   0.02016  -0.0116   0.0519   0.7908
  14.000   1.3774   0.02740   0.02118  -0.0100   0.0496   0.7923
  14.250   1.3904   0.02821   0.02205  -0.0088   0.0481   0.7938
  14.500   1.4034   0.02904   0.02293  -0.0077   0.0462   0.7954
  14.750   1.4138   0.03006   0.02397  -0.0064   0.0442   0.7969
  15.000   1.4231   0.03120   0.02514  -0.0050   0.0422   0.7982
  15.250   1.4346   0.03220   0.02619  -0.0039   0.0406   0.7995
  15.500   1.4447   0.03333   0.02735  -0.0028   0.0389   0.8007
  15.750   1.4512   0.03477   0.02879  -0.0015   0.0369   0.8019
  16.000   1.4602   0.03604   0.03012  -0.0005   0.0357   0.8030
  16.250   1.4680   0.03744   0.03157   0.0006   0.0344   0.8040
  16.500   1.4741   0.03903   0.03320   0.0016   0.0331   0.8057
  16.750   1.4771   0.04093   0.03515   0.0026   0.0316   0.8073
  17.000   1.4843   0.04251   0.03681   0.0033   0.0308   0.8087
  17.250   1.4901   0.04426   0.03863   0.0040   0.0297   0.8100
  17.500   1.4936   0.04629   0.04073   0.0046   0.0288   0.8112
  17.750   1.4942   0.04866   0.04315   0.0052   0.0276   0.8126
  18.000   1.4948   0.05113   0.04569   0.0056   0.0267   0.8140
  18.250   1.4990   0.05329   0.04794   0.0058   0.0260   0.8152
  18.500   1.5005   0.05580   0.05053   0.0059   0.0253   0.8166
  18.750   1.4994   0.05868   0.05348   0.0058   0.0246   0.8178
  19.000   1.4951   0.06205   0.05692   0.0055   0.0238   0.8187
  19.250   1.4887   0.06580   0.06076   0.0049   0.0232   0.8195
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