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TH 25816 HALE AIRFOIL (th25816-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: TH 25816 HALE AIRFOIL (th25816-il)
Reynolds number: 500,000
Max Cl/Cd: 47.87 at α=6.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-th25816-il-500000-n5.txt
Download as CSV file: xf-th25816-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: TH 25816 HALE 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 =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -19.750  -0.3379   0.08237   0.07775  -0.2099   0.9396   0.0130
 -19.500  -0.3439   0.07791   0.07316  -0.2126   0.9391   0.0131
 -19.250  -0.3472   0.07373   0.06882  -0.2154   0.9387   0.0132
 -19.000  -0.3466   0.07008   0.06503  -0.2180   0.9383   0.0132
 -18.750  -0.3452   0.06664   0.06145  -0.2204   0.9379   0.0133
 -18.500  -0.3407   0.06365   0.05834  -0.2226   0.9376   0.0133
 -18.250  -0.3371   0.06060   0.05517  -0.2247   0.9372   0.0135
 -18.000  -0.3875   0.06125   0.05585  -0.2110   0.9297   0.0135
 -17.750  -0.3877   0.05919   0.05370  -0.2106   0.9280   0.0134
 -17.500  -0.3848   0.05687   0.05129  -0.2110   0.9271   0.0136
 -17.250  -0.3763   0.05481   0.04917  -0.2121   0.9263   0.0137
 -17.000  -0.3663   0.05274   0.04705  -0.2134   0.9257   0.0139
 -16.750  -0.3544   0.05083   0.04506  -0.2147   0.9251   0.0139
 -16.500  -0.3403   0.04895   0.04312  -0.2164   0.9247   0.0142
 -16.250  -0.3252   0.04718   0.04129  -0.2181   0.9242   0.0144
 -16.000  -0.3649   0.04723   0.04132  -0.2066   0.9159   0.0143
 -15.750  -0.3569   0.04578   0.03982  -0.2063   0.9141   0.0144
 -15.500  -0.3442   0.04428   0.03826  -0.2068   0.9131   0.0146
 -15.250  -0.3294   0.04278   0.03670  -0.2077   0.9123   0.0148
 -15.000  -0.3128   0.04134   0.03518  -0.2087   0.9116   0.0148
 -14.750  -0.2948   0.03994   0.03373  -0.2099   0.9109   0.0149
 -14.500  -0.2762   0.03856   0.03228  -0.2112   0.9103   0.0152
 -14.250  -0.2559   0.03729   0.03095  -0.2127   0.9097   0.0154
 -13.250  -0.3271   0.03568   0.02922  -0.1841   0.8747   0.0156
 -13.000  -0.3123   0.03460   0.02808  -0.1838   0.8720   0.0159
 -12.750  -0.2944   0.03342   0.02683  -0.1843   0.8702   0.0160
 -12.500  -0.2915   0.03274   0.02609  -0.1814   0.8630   0.0161
 -12.250  -0.2740   0.03169   0.02499  -0.1815   0.8599   0.0163
 -12.000  -0.2519   0.03061   0.02383  -0.1826   0.8575   0.0166
 -11.750  -0.2308   0.02938   0.02255  -0.1837   0.8550   0.0167
 -11.500  -0.2184   0.02835   0.02148  -0.1830   0.8492   0.0171
 -11.250  -0.1952   0.02732   0.02041  -0.1843   0.8454   0.0174
 -11.000  -0.1677   0.02629   0.01931  -0.1864   0.8424   0.0179
 -10.750  -0.1458   0.02550   0.01847  -0.1871   0.8379   0.0182
 -10.500  -0.1272   0.02475   0.01764  -0.1872   0.8326   0.0186
 -10.250  -0.1015   0.02402   0.01684  -0.1887   0.8284   0.0192
 -10.000  -0.0813   0.02335   0.01610  -0.1889   0.8237   0.0196
  -9.750  -0.0701   0.02288   0.01556  -0.1871   0.8174   0.0199
  -9.500  -0.0515   0.02229   0.01490  -0.1870   0.8125   0.0204
  -9.250  -0.0381   0.02179   0.01434  -0.1857   0.8078   0.0208
  -9.000  -0.0334   0.02143   0.01396  -0.1824   0.8025   0.0212
  -8.750  -0.0211   0.02102   0.01349  -0.1807   0.7981   0.0219
  -8.500  -0.0021   0.02059   0.01300  -0.1803   0.7945   0.0226
  -8.250   0.0004   0.02031   0.01269  -0.1765   0.7899   0.0233
  -8.000   0.0055   0.02006   0.01240  -0.1731   0.7853   0.0238
  -7.750   0.0158   0.01970   0.01201  -0.1708   0.7814   0.0251
  -7.500   0.0310   0.01932   0.01159  -0.1695   0.7783   0.0271
  -7.250   0.0356   0.01906   0.01132  -0.1660   0.7749   0.0291
  -7.000   0.0367   0.01880   0.01108  -0.1618   0.7712   0.0326
  -6.750   0.0378   0.01844   0.01075  -0.1576   0.7674   0.0435
  -6.500   0.0427   0.01802   0.01038  -0.1544   0.7640   0.0605
  -6.250   0.0492   0.01748   0.00992  -0.1515   0.7610   0.0873
  -6.000   0.0428   0.01719   0.00970  -0.1457   0.7576   0.1035
  -5.750   0.0349   0.01681   0.00943  -0.1398   0.7540   0.1285
  -5.500   0.0298   0.01642   0.00912  -0.1343   0.7507   0.1546
  -5.250   0.0223   0.01585   0.00870  -0.1286   0.7476   0.1945
  -5.000   0.0177   0.01524   0.00822  -0.1234   0.7448   0.2379
  -4.750  -0.0036   0.01478   0.00790  -0.1147   0.7412   0.2737
  -4.500  -0.0282   0.01443   0.00766  -0.1050   0.7371   0.2998
  -4.250  -0.0593   0.01397   0.00730  -0.0941   0.7333   0.3310
  -4.000  -0.0747   0.01347   0.00687  -0.0862   0.7303   0.3627
  -3.750  -0.0878   0.01240   0.00615  -0.0792   0.7277   0.4510
  -3.500  -0.0942   0.01175   0.00584  -0.0733   0.7249   0.5282
  -3.250  -0.0904   0.01141   0.00579  -0.0691   0.7220   0.5983
  -3.000  -0.0758   0.01131   0.00585  -0.0669   0.7193   0.6438
  -2.750  -0.0547   0.01132   0.00589  -0.0660   0.7168   0.6687
  -2.500  -0.0293   0.01134   0.00589  -0.0660   0.7147   0.6811
  -2.250  -0.0008   0.01133   0.00583  -0.0666   0.7129   0.6865
  -2.000   0.0296   0.01132   0.00580  -0.0676   0.7113   0.6918
  -1.750   0.0534   0.01138   0.00582  -0.0674   0.7093   0.6980
  -1.500   0.0716   0.01148   0.00590  -0.0660   0.7070   0.7028
  -1.250   0.0918   0.01157   0.00600  -0.0650   0.7044   0.7052
  -1.000   0.1132   0.01166   0.00608  -0.0643   0.7020   0.7079
  -0.750   0.1368   0.01171   0.00611  -0.0640   0.6996   0.7109
  -0.500   0.1637   0.01173   0.00608  -0.0644   0.6975   0.7138
  -0.250   0.1930   0.01173   0.00602  -0.0653   0.6959   0.7165
   0.000   0.2247   0.01172   0.00594  -0.0667   0.6943   0.7190
   0.250   0.2439   0.01185   0.00609  -0.0655   0.6922   0.7216
   0.500   0.2606   0.01202   0.00630  -0.0639   0.6896   0.7245
   0.750   0.2800   0.01216   0.00645  -0.0628   0.6869   0.7276
   1.000   0.3018   0.01227   0.00655  -0.0622   0.6844   0.7306
   1.250   0.3266   0.01234   0.00659  -0.0623   0.6822   0.7335
   1.500   0.3543   0.01237   0.00658  -0.0629   0.6804   0.7363
   1.750   0.3837   0.01239   0.00659  -0.0638   0.6787   0.7387
   2.000   0.4140   0.01242   0.00660  -0.0649   0.6771   0.7414
   2.250   0.4247   0.01272   0.00696  -0.0621   0.6742   0.7449
   2.500   0.4404   0.01295   0.00722  -0.0604   0.6712   0.7485
   2.750   0.4604   0.01313   0.00739  -0.0596   0.6685   0.7519
   3.000   0.4835   0.01325   0.00751  -0.0593   0.6663   0.7549
   3.250   0.5094   0.01333   0.00760  -0.0596   0.6644   0.7574
   3.500   0.5381   0.01337   0.00764  -0.0604   0.6625   0.7602
   3.750   0.5686   0.01339   0.00765  -0.0615   0.6606   0.7632
   4.000   0.5769   0.01380   0.00811  -0.0585   0.6574   0.7674
   4.250   0.5915   0.01411   0.00844  -0.0567   0.6542   0.7714
   4.500   0.6094   0.01436   0.00873  -0.0554   0.6511   0.7741
   4.750   0.6327   0.01450   0.00889  -0.0552   0.6486   0.7770
   5.000   0.6603   0.01455   0.00894  -0.0559   0.6463   0.7800
   5.250   0.6899   0.01457   0.00895  -0.0569   0.6441   0.7831
   5.500   0.6935   0.01516   0.00960  -0.0531   0.6398   0.7873
   5.750   0.7063   0.01556   0.01005  -0.0510   0.6359   0.7904
   6.000   0.7263   0.01579   0.01030  -0.0503   0.6324   0.7933
   6.250   0.7531   0.01585   0.01036  -0.0507   0.6296   0.7963
   6.500   0.7721   0.01613   0.01066  -0.0499   0.6262   0.7997
   6.750   0.7767   0.01681   0.01139  -0.0465   0.6209   0.8036
   7.000   0.7934   0.01716   0.01175  -0.0452   0.6167   0.8065
   7.250   0.8174   0.01728   0.01189  -0.0452   0.6133   0.8087
   7.500   0.8325   0.01770   0.01234  -0.0437   0.6090   0.8114
   7.750   0.8381   0.01844   0.01315  -0.0406   0.6030   0.8148
   8.000   0.8561   0.01877   0.01347  -0.0396   0.5979   0.8180
   8.250   0.8732   0.01915   0.01386  -0.0386   0.5927   0.8213
   8.500   0.8795   0.01994   0.01470  -0.0358   0.5859   0.8241
   8.750   0.8966   0.02031   0.01508  -0.0347   0.5801   0.8262
   9.000   0.9049   0.02106   0.01588  -0.0323   0.5732   0.8286
   9.250   0.9154   0.02173   0.01658  -0.0302   0.5652   0.8312
   9.500   0.9244   0.02250   0.01736  -0.0280   0.5564   0.8341
   9.750   0.9354   0.02319   0.01804  -0.0262   0.5469   0.8370
  10.000   0.9418   0.02414   0.01900  -0.0237   0.5361   0.8399
  10.250   0.9497   0.02499   0.01983  -0.0215   0.5235   0.8420
  10.500   0.9527   0.02607   0.02089  -0.0185   0.5082   0.8440
  10.750   0.9565   0.02716   0.02194  -0.0158   0.4920   0.8461
  11.000   0.9567   0.02847   0.02320  -0.0127   0.4740   0.8484
  11.250   0.9557   0.02988   0.02453  -0.0095   0.4538   0.8509
  11.500   0.9561   0.03130   0.02590  -0.0066   0.4367   0.8534
  11.750   0.9555   0.03281   0.02734  -0.0037   0.4179   0.8558
  12.000   0.9558   0.03435   0.02881  -0.0011   0.4004   0.8578
  12.250   0.9542   0.03598   0.03038   0.0017   0.3819   0.8594
  12.500   0.9573   0.03738   0.03176   0.0039   0.3676   0.8610
  12.750   0.9570   0.03904   0.03337   0.0064   0.3495   0.8627
  13.000   0.9592   0.04059   0.03489   0.0084   0.3348   0.8646
  13.250   0.9622   0.04213   0.03638   0.0103   0.3193   0.8665
  13.500   0.9616   0.04395   0.03814   0.0125   0.3010   0.8684
  13.750   0.9670   0.04542   0.03958   0.0139   0.2884   0.8700
  14.000   0.9699   0.04712   0.04123   0.0155   0.2738   0.8718
  14.250   0.9728   0.04884   0.04289   0.0170   0.2577   0.8734
  14.500   0.9789   0.05039   0.04441   0.0181   0.2444   0.8748
  14.750   0.9822   0.05208   0.04607   0.0195   0.2298   0.8763
  15.000   0.9865   0.05371   0.04766   0.0207   0.2159   0.8776
  15.250   0.9919   0.05533   0.04927   0.0218   0.2056   0.8790
  15.500   0.9958   0.05707   0.05099   0.0229   0.1930   0.8804
  15.750   1.0028   0.05862   0.05252   0.0237   0.1814   0.8819
  16.000   1.0083   0.06032   0.05422   0.0245   0.1715   0.8834
  16.250   1.0134   0.06208   0.05594   0.0252   0.1613   0.8850
  16.500   1.0175   0.06395   0.05777   0.0260   0.1488   0.8864
  16.750   1.0253   0.06556   0.05941   0.0264   0.1421   0.8880
  17.000   1.0302   0.06744   0.06125   0.0269   0.1328   0.8893
  17.250   1.0349   0.06938   0.06316   0.0274   0.1223   0.8904
  17.500   1.0420   0.07108   0.06489   0.0277   0.1174   0.8916
  17.750   1.0484   0.07282   0.06665   0.0281   0.1104   0.8929
  18.000   1.0526   0.07481   0.06864   0.0285   0.1035   0.8940
  18.250   1.0587   0.07665   0.07051   0.0288   0.0980   0.8951
  18.500   1.0639   0.07860   0.07246   0.0290   0.0929   0.8961
  18.750   1.0703   0.08046   0.07437   0.0290   0.0881   0.8972
  19.000   1.0764   0.08239   0.07632   0.0290   0.0846   0.8983
  19.250   1.0815   0.08442   0.07837   0.0290   0.0804   0.8996
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