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AH 93-156 (ah93156-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: AH 93-156 (ah93156-il)
Reynolds number: 1,000,000
Max Cl/Cd: 125.01 at α=6°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-ah93156-il-1000000.txt
Download as CSV file: xf-ah93156-il-1000000.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 =     1.000 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -15.250  -0.6432   0.05389   0.05081  -0.1174   0.8159   0.0111
 -15.000  -0.6689   0.04604   0.04276  -0.1234   0.8118   0.0111
 -14.750  -0.7001   0.03980   0.03627  -0.1261   0.8077   0.0110
 -14.500  -0.7093   0.03689   0.03321  -0.1262   0.8037   0.0111
 -14.250  -0.7139   0.03469   0.03091  -0.1255   0.8007   0.0112
 -14.000  -0.7193   0.03264   0.02875  -0.1242   0.7974   0.0113
 -13.750  -0.7287   0.03042   0.02635  -0.1219   0.7941   0.0113
 -13.500  -0.7244   0.02932   0.02515  -0.1202   0.7910   0.0116
 -13.250  -0.7216   0.02811   0.02382  -0.1182   0.7877   0.0117
 -13.000  -0.7189   0.02688   0.02247  -0.1159   0.7851   0.0118
 -12.750  -0.7169   0.02559   0.02106  -0.1133   0.7823   0.0120
 -12.500  -0.7104   0.02463   0.01999  -0.1110   0.7797   0.0122
 -12.250  -0.7050   0.02358   0.01880  -0.1084   0.7770   0.0123
 -12.000  -0.6964   0.02277   0.01787  -0.1060   0.7744   0.0126
 -11.750  -0.6864   0.02207   0.01706  -0.1037   0.7720   0.0127
 -11.500  -0.6751   0.02147   0.01638  -0.1014   0.7699   0.0129
 -11.250  -0.6611   0.02115   0.01598  -0.0994   0.7676   0.0131
 -11.000  -0.6593   0.01935   0.01398  -0.0959   0.7652   0.0135
 -10.750  -0.6440   0.01864   0.01319  -0.0943   0.7631   0.0138
 -10.500  -0.6263   0.01807   0.01256  -0.0929   0.7611   0.0141
 -10.250  -0.6077   0.01751   0.01192  -0.0917   0.7590   0.0144
 -10.000  -0.5869   0.01714   0.01150  -0.0908   0.7568   0.0148
  -9.750  -0.5664   0.01663   0.01093  -0.0899   0.7553   0.0152
  -9.500  -0.5451   0.01616   0.01039  -0.0890   0.7535   0.0156
  -9.250  -0.5232   0.01572   0.00988  -0.0882   0.7516   0.0160
  -9.000  -0.4999   0.01540   0.00950  -0.0876   0.7497   0.0164
  -8.750  -0.4817   0.01451   0.00852  -0.0863   0.7479   0.0171
  -8.500  -0.4598   0.01403   0.00800  -0.0855   0.7462   0.0177
  -8.250  -0.4359   0.01374   0.00767  -0.0850   0.7445   0.0184
  -8.000  -0.4115   0.01350   0.00738  -0.0846   0.7424   0.0192
  -7.750  -0.3869   0.01324   0.00709  -0.0842   0.7407   0.0199
  -7.500  -0.3618   0.01300   0.00681  -0.0839   0.7392   0.0204
  -7.250  -0.3407   0.01236   0.00613  -0.0829   0.7375   0.0217
  -7.000  -0.3160   0.01207   0.00583  -0.0825   0.7358   0.0227
  -6.750  -0.2906   0.01184   0.00558  -0.0823   0.7341   0.0239
  -6.500  -0.2650   0.01161   0.00532  -0.0820   0.7324   0.0249
  -6.250  -0.2408   0.01126   0.00493  -0.0815   0.7306   0.0264
  -6.000  -0.2155   0.01101   0.00468  -0.0812   0.7289   0.0284
  -5.750  -0.1894   0.01087   0.00450  -0.0811   0.7270   0.0302
  -5.500  -0.1635   0.01068   0.00428  -0.0808   0.7254   0.0318
  -5.250  -0.1385   0.01038   0.00401  -0.0805   0.7239   0.0350
  -5.000  -0.1120   0.01023   0.00386  -0.0804   0.7222   0.0377
  -4.750  -0.0864   0.00998   0.00362  -0.0801   0.7204   0.0419
  -4.500  -0.0599   0.00982   0.00346  -0.0800   0.7187   0.0459
  -4.250  -0.0338   0.00961   0.00327  -0.0798   0.7169   0.0521
  -4.000  -0.0072   0.00946   0.00312  -0.0798   0.7151   0.0593
  -3.750   0.0192   0.00930   0.00299  -0.0797   0.7134   0.0692
  -3.500   0.0455   0.00914   0.00288  -0.0796   0.7113   0.0856
  -3.250   0.0713   0.00894   0.00278  -0.0794   0.7097   0.1077
  -3.000   0.0971   0.00872   0.00267  -0.0792   0.7079   0.1364
  -2.750   0.1224   0.00846   0.00257  -0.0790   0.7059   0.1771
  -2.500   0.1471   0.00816   0.00246  -0.0787   0.7037   0.2343
  -2.250   0.1710   0.00780   0.00235  -0.0782   0.7017   0.3124
  -2.000   0.1938   0.00737   0.00225  -0.0776   0.6995   0.4105
  -1.750   0.2141   0.00681   0.00212  -0.0765   0.6968   0.5482
  -1.500   0.2286   0.00605   0.00208  -0.0740   0.6943   0.7529
  -1.250   0.2540   0.00608   0.00227  -0.0733   0.6918   0.8109
  -1.000   0.2821   0.00616   0.00234  -0.0734   0.6894   0.8289
  -0.750   0.3103   0.00627   0.00243  -0.0734   0.6869   0.8384
  -0.500   0.3386   0.00638   0.00252  -0.0734   0.6845   0.8465
  -0.250   0.3668   0.00656   0.00266  -0.0734   0.6820   0.8532
   0.000   0.3951   0.00668   0.00275  -0.0736   0.6795   0.8592
   0.250   0.4224   0.00680   0.00290  -0.0734   0.6770   0.8630
   0.500   0.4495   0.00698   0.00308  -0.0731   0.6741   0.8688
   0.750   0.4765   0.00713   0.00323  -0.0728   0.6714   0.8753
   1.000   0.5021   0.00731   0.00341  -0.0721   0.6687   0.8797
   1.250   0.5287   0.00751   0.00358  -0.0717   0.6657   0.8853
   1.500   0.5551   0.00758   0.00367  -0.0714   0.6629   0.8899
   1.750   0.5805   0.00759   0.00370  -0.0709   0.6596   0.8923
   2.000   0.6077   0.00758   0.00369  -0.0708   0.6562   0.8938
   2.250   0.6353   0.00759   0.00367  -0.0710   0.6528   0.8950
   2.500   0.6628   0.00760   0.00367  -0.0711   0.6490   0.8964
   2.750   0.6902   0.00758   0.00367  -0.0712   0.6447   0.8978
   3.000   0.7178   0.00757   0.00366  -0.0714   0.6400   0.8991
   3.250   0.7454   0.00760   0.00365  -0.0716   0.6356   0.9003
   3.500   0.7733   0.00760   0.00369  -0.0719   0.6307   0.9016
   3.750   0.8010   0.00763   0.00371  -0.0722   0.6247   0.9026
   4.000   0.8275   0.00763   0.00370  -0.0722   0.6188   0.9035
   4.250   0.8528   0.00760   0.00368  -0.0719   0.6116   0.9046
   4.500   0.8777   0.00762   0.00369  -0.0715   0.6046   0.9057
   4.750   0.9031   0.00765   0.00373  -0.0712   0.5961   0.9066
   5.000   0.9278   0.00771   0.00377  -0.0709   0.5873   0.9075
   5.250   0.9512   0.00779   0.00384  -0.0702   0.5769   0.9087
   5.500   0.9750   0.00788   0.00392  -0.0697   0.5653   0.9099
   5.750   0.9977   0.00800   0.00402  -0.0690   0.5527   0.9110
   6.000   1.0188   0.00815   0.00414  -0.0680   0.5379   0.9122
   6.250   1.0386   0.00834   0.00428  -0.0667   0.5221   0.9133
   6.500   1.0559   0.00858   0.00446  -0.0650   0.5046   0.9147
   6.750   1.0722   0.00883   0.00466  -0.0631   0.4884   0.9160
   7.000   1.0835   0.00908   0.00486  -0.0602   0.4722   0.9172
   7.250   1.0913   0.00929   0.00503  -0.0566   0.4566   0.9189
   7.500   1.0991   0.00963   0.00533  -0.0531   0.4409   0.9205
   7.750   1.1046   0.01005   0.00570  -0.0493   0.4244   0.9225
   8.000   1.1107   0.01053   0.00614  -0.0458   0.4079   0.9244
   8.250   1.1156   0.01113   0.00667  -0.0424   0.3886   0.9262
   8.500   1.1215   0.01178   0.00727  -0.0393   0.3706   0.9278
   8.750   1.1249   0.01258   0.00799  -0.0359   0.3502   0.9294
   9.000   1.1294   0.01341   0.00873  -0.0329   0.3300   0.9309
   9.250   1.1356   0.01416   0.00942  -0.0301   0.3116   0.9327
   9.500   1.1364   0.01519   0.01034  -0.0268   0.2870   0.9345
   9.750   1.1384   0.01625   0.01129  -0.0237   0.2610   0.9363
  10.000   1.1460   0.01712   0.01210  -0.0215   0.2449   0.9377
  10.250   1.1486   0.01826   0.01312  -0.0188   0.2201   0.9393
  10.750   1.1582   0.02045   0.01514  -0.0142   0.1805   0.9426
  11.000   1.1632   0.02160   0.01619  -0.0120   0.1608   0.9440
  11.250   1.1677   0.02288   0.01738  -0.0101   0.1405   0.9457
  11.500   1.1745   0.02409   0.01851  -0.0085   0.1222   0.9474
  11.750   1.1781   0.02555   0.01987  -0.0066   0.1026   0.9492
  12.000   1.1844   0.02692   0.02117  -0.0052   0.0854   0.9510
  12.250   1.1892   0.02846   0.02263  -0.0038   0.0689   0.9529
  12.500   1.1937   0.03012   0.02420  -0.0025   0.0528   0.9548
  12.750   1.2020   0.03164   0.02568  -0.0018   0.0426   0.9568
  13.000   1.2115   0.03326   0.02728  -0.0015   0.0335   0.9592
  13.250   1.2222   0.03499   0.02899  -0.0016   0.0260   0.9616
  13.500   1.2340   0.03681   0.03079  -0.0020   0.0201   0.9638
  13.750   1.2471   0.03866   0.03266  -0.0028   0.0160   0.9656
  14.000   1.2608   0.04054   0.03457  -0.0037   0.0132   0.9671
  14.250   1.2738   0.04253   0.03660  -0.0047   0.0114   0.9685
  14.500   1.2873   0.04451   0.03864  -0.0057   0.0101   0.9698
  14.750   1.2981   0.04685   0.04103  -0.0067   0.0088   0.9734
  15.000   1.3097   0.04890   0.04314  -0.0074   0.0082   0.9980
  15.250   1.3161   0.05093   0.04522  -0.0071   0.0077   1.0000
  15.500   1.3212   0.05306   0.04740  -0.0067   0.0075   1.0000
  15.750   1.3178   0.05608   0.05051  -0.0061   0.0069   1.0000
  16.000   1.3241   0.05815   0.05263  -0.0059   0.0067   1.0000
  16.250   1.3265   0.06064   0.05520  -0.0057   0.0066   1.0000
  16.500   1.3302   0.06304   0.05768  -0.0056   0.0063   1.0000
  16.750   1.3301   0.06592   0.06064  -0.0055   0.0062   1.0000
  17.000   1.3306   0.06878   0.06358  -0.0055   0.0061   1.0000
  17.250   1.3324   0.07151   0.06639  -0.0056   0.0060   1.0000
  17.500   1.3314   0.07460   0.06954  -0.0058   0.0057   1.0000
  17.750   1.3303   0.07778   0.07281  -0.0060   0.0058   1.0000
  18.000   1.3270   0.08129   0.07639  -0.0064   0.0056   1.0000
  18.250   1.3229   0.08498   0.08017  -0.0070   0.0055   1.0000
  18.500   1.3200   0.08855   0.08383  -0.0076   0.0055   1.0000
  18.750   1.3099   0.09314   0.08850  -0.0085   0.0053   1.0000
  19.000   1.3049   0.09716   0.09261  -0.0095   0.0053   1.0000
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