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AH 93-156 (ah93156-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: AH 93-156 (ah93156-il)
Reynolds number: 200,000
Max Cl/Cd: 64.73 at α=7.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-ah93156-il-200000-n5.txt
Download as CSV file: xf-ah93156-il-200000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: AH 93-156                                       
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -12.250  -0.2456   0.08989   0.08546  -0.0990   0.8263   0.0207
 -12.000  -0.3539   0.06140   0.05694  -0.1147   0.8240   0.0203
 -11.750  -0.3829   0.05410   0.04948  -0.1198   0.8207   0.0200
 -11.500  -0.4119   0.04909   0.04428  -0.1209   0.8170   0.0198
 -11.250  -0.4481   0.04440   0.03930  -0.1191   0.8125   0.0200
 -11.000  -0.4714   0.04113   0.03575  -0.1159   0.8086   0.0200
 -10.750  -0.4917   0.03831   0.03256  -0.1117   0.8053   0.0203
 -10.500  -0.5085   0.03596   0.02983  -0.1068   0.8021   0.0205
 -10.250  -0.5082   0.03414   0.02780  -0.1040   0.7990   0.0207
 -10.000  -0.5000   0.03293   0.02649  -0.1020   0.7963   0.0211
  -9.750  -0.4909   0.03159   0.02496  -0.1000   0.7936   0.0214
  -9.500  -0.4790   0.03042   0.02360  -0.0982   0.7912   0.0219
  -9.250  -0.4658   0.02913   0.02208  -0.0966   0.7891   0.0225
  -9.000  -0.4512   0.02785   0.02057  -0.0950   0.7867   0.0233
  -8.750  -0.4347   0.02666   0.01913  -0.0937   0.7842   0.0242
  -8.500  -0.4164   0.02552   0.01769  -0.0925   0.7818   0.0252
  -8.250  -0.3969   0.02460   0.01671  -0.0917   0.7795   0.0262
  -8.000  -0.3761   0.02391   0.01595  -0.0909   0.7773   0.0272
  -7.750  -0.3543   0.02313   0.01503  -0.0902   0.7753   0.0282
  -7.500  -0.3317   0.02231   0.01406  -0.0895   0.7736   0.0295
  -7.250  -0.3088   0.02164   0.01320  -0.0889   0.7717   0.0310
  -7.000  -0.2874   0.02096   0.01252  -0.0882   0.7693   0.0325
  -6.750  -0.2651   0.02052   0.01207  -0.0876   0.7669   0.0344
  -6.500  -0.2423   0.01999   0.01146  -0.0870   0.7646   0.0362
  -6.250  -0.2189   0.01948   0.01083  -0.0863   0.7624   0.0381
  -6.000  -0.1966   0.01893   0.01028  -0.0856   0.7604   0.0406
  -5.750  -0.1728   0.01855   0.00985  -0.0851   0.7588   0.0437
  -5.500  -0.1488   0.01817   0.00937  -0.0846   0.7573   0.0467
  -5.250  -0.1276   0.01777   0.00900  -0.0837   0.7549   0.0504
  -5.000  -0.1050   0.01751   0.00873  -0.0830   0.7522   0.0551
  -4.750  -0.0826   0.01718   0.00839  -0.0823   0.7496   0.0603
  -4.500  -0.0592   0.01691   0.00810  -0.0817   0.7475   0.0672
  -4.250  -0.0357   0.01661   0.00782  -0.0811   0.7456   0.0759
  -4.000  -0.0116   0.01632   0.00753  -0.0806   0.7438   0.0875
  -3.750   0.0129   0.01603   0.00727  -0.0802   0.7422   0.1044
  -3.500   0.0355   0.01582   0.00713  -0.0795   0.7399   0.1270
  -3.250   0.0565   0.01560   0.00706  -0.0786   0.7370   0.1598
  -3.000   0.0776   0.01528   0.00696  -0.0778   0.7343   0.2094
  -2.750   0.0980   0.01487   0.00682  -0.0768   0.7318   0.2829
  -2.500   0.1166   0.01432   0.00667  -0.0755   0.7298   0.3869
  -2.250   0.1319   0.01357   0.00651  -0.0733   0.7279   0.5328
  -2.000   0.1540   0.01354   0.00736  -0.0703   0.7265   0.7454
  -1.750   0.1763   0.01405   0.00792  -0.0686   0.7233   0.7994
  -1.500   0.1946   0.01435   0.00817  -0.0666   0.7199   0.8256
  -1.250   0.2153   0.01460   0.00835  -0.0650   0.7171   0.8445
  -1.000   0.2381   0.01482   0.00849  -0.0637   0.7147   0.8588
  -0.750   0.2653   0.01507   0.00866  -0.0629   0.7128   0.8699
  -0.500   0.2931   0.01532   0.00884  -0.0622   0.7112   0.8839
  -0.250   0.3153   0.01569   0.00923  -0.0605   0.7073   0.8984
   0.000   0.3467   0.01591   0.00942  -0.0607   0.7038   0.9101
   0.250   0.3709   0.01589   0.00935  -0.0599   0.7006   0.9184
   0.500   0.4040   0.01578   0.00916  -0.0610   0.6981   0.9205
   0.750   0.4352   0.01564   0.00894  -0.0618   0.6961   0.9224
   1.000   0.4518   0.01572   0.00905  -0.0600   0.6914   0.9263
   1.250   0.4637   0.01568   0.00900  -0.0571   0.6871   0.9309
   1.500   0.4936   0.01557   0.00885  -0.0577   0.6842   0.9323
   1.750   0.5246   0.01543   0.00866  -0.0585   0.6818   0.9335
   2.000   0.5484   0.01545   0.00869  -0.0581   0.6778   0.9358
   2.250   0.5673   0.01548   0.00873  -0.0567   0.6729   0.9385
   2.500   0.5898   0.01538   0.00862  -0.0558   0.6693   0.9410
   2.750   0.6135   0.01521   0.00841  -0.0551   0.6664   0.9434
   3.000   0.6316   0.01528   0.00853  -0.0537   0.6611   0.9455
   3.250   0.6566   0.01526   0.00854  -0.0535   0.6562   0.9472
   3.500   0.6858   0.01514   0.00841  -0.0539   0.6527   0.9486
   3.750   0.7085   0.01512   0.00841  -0.0532   0.6480   0.9504
   4.000   0.7250   0.01517   0.00851  -0.0514   0.6419   0.9531
   4.250   0.7496   0.01504   0.00838  -0.0510   0.6376   0.9552
   4.500   0.7652   0.01506   0.00845  -0.0489   0.6314   0.9577
   4.750   0.7895   0.01505   0.00847  -0.0486   0.6250   0.9590
   5.000   0.8174   0.01496   0.00839  -0.0489   0.6192   0.9601
   5.250   0.8373   0.01506   0.00856  -0.0479   0.6109   0.9624
   5.500   0.8647   0.01498   0.00849  -0.0480   0.6046   0.9639
   5.750   0.8813   0.01507   0.00863  -0.0464   0.5955   0.9664
   6.000   0.8999   0.01509   0.00869  -0.0449   0.5869   0.9687
   6.250   0.9223   0.01509   0.00869  -0.0442   0.5776   0.9706
   6.500   0.9446   0.01525   0.00890  -0.0438   0.5661   0.9727
   6.750   0.9683   0.01539   0.00907  -0.0436   0.5549   0.9747
   7.000   0.9914   0.01553   0.00922  -0.0433   0.5429   0.9765
   7.250   1.0136   0.01572   0.00941  -0.0428   0.5299   0.9786
   7.500   1.0344   0.01598   0.00966  -0.0422   0.5159   0.9810
   7.750   1.0552   0.01633   0.01001  -0.0418   0.5011   0.9835
   8.000   1.0763   0.01675   0.01042  -0.0416   0.4858   0.9867
   8.250   1.0942   0.01725   0.01092  -0.0410   0.4694   0.9923
   8.500   1.1058   0.01784   0.01148  -0.0391   0.4544   1.0000
   8.750   1.1078   0.01839   0.01201  -0.0355   0.4406   1.0000
   9.000   1.1137   0.01904   0.01264  -0.0328   0.4262   1.0000
   9.250   1.1213   0.01976   0.01334  -0.0304   0.4116   1.0000
   9.500   1.1289   0.02057   0.01413  -0.0283   0.3962   1.0000
   9.750   1.1356   0.02149   0.01501  -0.0261   0.3794   1.0000
  10.000   1.1415   0.02252   0.01601  -0.0240   0.3613   1.0000
  10.250   1.1466   0.02365   0.01710  -0.0220   0.3415   1.0000
  10.500   1.1502   0.02491   0.01830  -0.0199   0.3208   1.0000
  10.750   1.1536   0.02626   0.01957  -0.0179   0.3002   1.0000
  11.000   1.1567   0.02769   0.02094  -0.0160   0.2783   1.0000
  11.250   1.1577   0.02930   0.02246  -0.0141   0.2564   1.0000
  11.500   1.1601   0.03092   0.02402  -0.0124   0.2344   1.0000
  11.750   1.1608   0.03275   0.02574  -0.0107   0.2127   1.0000
  12.000   1.1626   0.03457   0.02749  -0.0092   0.1903   1.0000
  12.250   1.1637   0.03653   0.02936  -0.0079   0.1702   1.0000
  12.500   1.1656   0.03850   0.03126  -0.0066   0.1492   1.0000
  13.000   1.1668   0.04288   0.03547  -0.0044   0.1096   1.0000
  13.250   1.1663   0.04527   0.03777  -0.0034   0.0910   1.0000
  13.500   1.1665   0.04768   0.04012  -0.0026   0.0752   1.0000
  13.750   1.1667   0.05016   0.04256  -0.0019   0.0613   1.0000
  14.000   1.1675   0.05267   0.04505  -0.0013   0.0510   1.0000
  14.250   1.1681   0.05527   0.04764  -0.0008   0.0425   1.0000
  14.500   1.1685   0.05795   0.05033  -0.0005   0.0362   1.0000
  14.750   1.1695   0.06065   0.05308  -0.0002   0.0312   1.0000
  15.000   1.1704   0.06344   0.05594  -0.0001   0.0276   1.0000
  15.250   1.1704   0.06640   0.05895  -0.0001   0.0247   1.0000
  15.500   1.1706   0.06941   0.06204  -0.0002   0.0229   1.0000
  15.750   1.1710   0.07247   0.06521  -0.0005   0.0207   1.0000
  16.000   1.1696   0.07582   0.06864  -0.0009   0.0195   1.0000
  16.250   1.1680   0.07929   0.07221  -0.0014   0.0181   1.0000
  16.500   1.1682   0.08256   0.07560  -0.0020   0.0168   1.0000
  16.750   1.1659   0.08623   0.07936  -0.0028   0.0158   1.0000
  17.000   1.1620   0.09022   0.08343  -0.0037   0.0152   1.0000
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