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TSAGI 12% AIRFOIL (tsagi12-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: TSAGI 12% AIRFOIL (tsagi12-il)
Reynolds number: 500,000
Max Cl/Cd: 88.47 at α=6°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-tsagi12-il-500000.txt
Download as CSV file: xf-tsagi12-il-500000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: TSAGI 12% 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
  ------ -------- --------- --------- -------- -------- --------
 -12.000  -0.7297   0.05526   0.05270  -0.0537   1.0000   0.0144
 -11.750  -0.7672   0.04838   0.04552  -0.0561   1.0000   0.0147
 -11.500  -0.7955   0.04411   0.04106  -0.0541   1.0000   0.0145
 -11.250  -0.8161   0.04106   0.03780  -0.0504   1.0000   0.0145
 -11.000  -0.8375   0.03834   0.03480  -0.0450   1.0000   0.0147
 -10.750  -0.8572   0.03578   0.03201  -0.0388   1.0000   0.0146
 -10.500  -0.8576   0.03463   0.03059  -0.0347   1.0000   0.0150
 -10.250  -0.8751   0.03091   0.02650  -0.0288   1.0000   0.0153
 -10.000  -0.8755   0.02874   0.02413  -0.0248   1.0000   0.0156
  -9.750  -0.8691   0.02731   0.02257  -0.0215   1.0000   0.0159
  -9.500  -0.8588   0.02645   0.02161  -0.0187   1.0000   0.0163
  -9.250  -0.8504   0.02521   0.02021  -0.0155   1.0000   0.0165
  -9.000  -0.8390   0.02458   0.01950  -0.0127   1.0000   0.0172
  -8.750  -0.8304   0.02349   0.01825  -0.0093   1.0000   0.0178
  -8.500  -0.8222   0.02246   0.01707  -0.0058   1.0000   0.0182
  -8.250  -0.8010   0.02155   0.01597  -0.0048   0.9986   0.0190
  -8.000  -0.7693   0.01966   0.01385  -0.0063   0.9949   0.0201
  -7.750  -0.7358   0.01878   0.01294  -0.0081   0.9904   0.0213
  -7.500  -0.7005   0.01811   0.01220  -0.0100   0.9859   0.0227
  -7.250  -0.6646   0.01733   0.01130  -0.0118   0.9817   0.0242
  -7.000  -0.6334   0.01604   0.00987  -0.0128   0.9750   0.0256
  -6.750  -0.5973   0.01517   0.00899  -0.0149   0.9703   0.0279
  -6.500  -0.5618   0.01462   0.00838  -0.0167   0.9611   0.0302
  -6.250  -0.5239   0.01377   0.00744  -0.0190   0.9518   0.0324
  -6.000  -0.4870   0.01295   0.00659  -0.0212   0.9382   0.0358
  -5.750  -0.4523   0.01251   0.00607  -0.0227   0.9206   0.0388
  -5.500  -0.4240   0.01193   0.00540  -0.0228   0.9007   0.0421
  -5.250  -0.3977   0.01160   0.00501  -0.0224   0.8812   0.0459
  -5.000  -0.3724   0.01144   0.00473  -0.0218   0.8628   0.0495
  -4.750  -0.3500   0.01109   0.00436  -0.0206   0.8452   0.0558
  -4.500  -0.3264   0.01090   0.00409  -0.0196   0.8295   0.0631
  -4.250  -0.3026   0.01073   0.00387  -0.0187   0.8150   0.0736
  -4.000  -0.2804   0.01044   0.00354  -0.0175   0.8012   0.0857
  -3.750  -0.2574   0.01022   0.00329  -0.0164   0.7883   0.0960
  -3.500  -0.2341   0.01002   0.00308  -0.0155   0.7760   0.1074
  -3.250  -0.2109   0.00979   0.00290  -0.0145   0.7643   0.1277
  -3.000  -0.1886   0.00951   0.00273  -0.0134   0.7534   0.1681
  -2.750  -0.1671   0.00919   0.00257  -0.0122   0.7428   0.2226
  -2.500  -0.1465   0.00880   0.00241  -0.0108   0.7320   0.2943
  -2.250  -0.1291   0.00828   0.00225  -0.0088   0.7225   0.3981
  -2.000  -0.1191   0.00756   0.00208  -0.0052   0.7132   0.5503
  -1.750  -0.1160   0.00673   0.00202   0.0003   0.7038   0.7423
  -1.500  -0.0733   0.00659   0.00222  -0.0024   0.6948   0.8616
  -1.250  -0.0306   0.00674   0.00234  -0.0053   0.6852   0.8904
  -1.000   0.0074   0.00690   0.00244  -0.0073   0.6760   0.9043
  -0.750   0.0357   0.00707   0.00251  -0.0071   0.6670   0.9158
  -0.500   0.0793   0.00731   0.00268  -0.0103   0.6566   0.9208
  -0.250   0.1058   0.00751   0.00282  -0.0097   0.6476   0.9302
   0.000   0.1501   0.00784   0.00305  -0.0129   0.6374   0.9330
   0.250   0.1941   0.00820   0.00335  -0.0161   0.6262   0.9384
   0.500   0.2312   0.00852   0.00361  -0.0178   0.6160   0.9457
   0.750   0.2895   0.00902   0.00403  -0.0239   0.6036   0.9517
   1.000   0.3310   0.00933   0.00427  -0.0265   0.5917   0.9595
   1.250   0.3759   0.00944   0.00434  -0.0301   0.5783   0.9625
   1.500   0.4079   0.00947   0.00432  -0.0311   0.5654   0.9653
   1.750   0.4345   0.00955   0.00436  -0.0310   0.5529   0.9692
   2.000   0.4634   0.00959   0.00435  -0.0313   0.5401   0.9721
   2.250   0.4974   0.00959   0.00429  -0.0328   0.5264   0.9736
   2.500   0.5306   0.00961   0.00427  -0.0341   0.5131   0.9755
   2.750   0.5617   0.00966   0.00427  -0.0350   0.5010   0.9778
   3.000   0.5907   0.00973   0.00431  -0.0354   0.4891   0.9808
   3.250   0.6177   0.00984   0.00440  -0.0354   0.4785   0.9839
   3.500   0.6513   0.00983   0.00436  -0.0369   0.4673   0.9853
   3.750   0.6836   0.00986   0.00435  -0.0381   0.4558   0.9870
   4.000   0.7154   0.00989   0.00439  -0.0391   0.4458   0.9891
   4.250   0.7459   0.00995   0.00445  -0.0399   0.4370   0.9915
   4.500   0.7749   0.01007   0.00455  -0.0404   0.4266   0.9938
   4.750   0.8071   0.01008   0.00455  -0.0416   0.4131   0.9955
   5.000   0.8389   0.01010   0.00456  -0.0427   0.3948   0.9975
   5.250   0.8708   0.01013   0.00458  -0.0439   0.3780   0.9994
   5.500   0.8965   0.01023   0.00469  -0.0437   0.3627   1.0000
   5.750   0.9177   0.01038   0.00482  -0.0426   0.3453   1.0000
   6.000   0.9378   0.01060   0.00498  -0.0413   0.3202   1.0000
   6.250   0.9568   0.01092   0.00518  -0.0399   0.2865   1.0000
   6.500   0.9729   0.01147   0.00551  -0.0380   0.2393   1.0000
   6.750   0.9850   0.01233   0.00604  -0.0355   0.1753   1.0000
   7.000   0.9915   0.01362   0.00684  -0.0323   0.0937   1.0000
   7.500   1.0105   0.01556   0.00840  -0.0262   0.0314   1.0000
   7.750   1.0246   0.01611   0.00900  -0.0239   0.0279   1.0000
   8.000   1.0340   0.01692   0.00986  -0.0208   0.0252   1.0000
   8.250   1.0467   0.01745   0.01047  -0.0182   0.0238   1.0000
   8.500   1.0585   0.01799   0.01107  -0.0155   0.0224   1.0000
   8.750   1.0681   0.01860   0.01172  -0.0125   0.0212   1.0000
   9.000   1.0732   0.01937   0.01253  -0.0087   0.0201   1.0000
   9.250   1.0684   0.02051   0.01375  -0.0034   0.0190   1.0000
   9.500   1.0695   0.02113   0.01444   0.0011   0.0187   1.0000
   9.750   1.0659   0.02172   0.01509   0.0065   0.0184   1.0000
  10.000   1.0631   0.02246   0.01591   0.0113   0.0180   1.0000
  10.250   1.0619   0.02336   0.01688   0.0154   0.0175   1.0000
  10.500   1.0625   0.02435   0.01795   0.0189   0.0171   1.0000
  10.750   1.0642   0.02545   0.01910   0.0219   0.0164   1.0000
  11.000   1.0662   0.02668   0.02038   0.0244   0.0160   1.0000
  11.250   1.0680   0.02807   0.02181   0.0267   0.0156   1.0000
  11.500   1.0646   0.03003   0.02382   0.0292   0.0150   1.0000
  11.750   1.0620   0.03223   0.02608   0.0317   0.0147   1.0000
  12.000   1.0699   0.03342   0.02738   0.0328   0.0143   1.0000
  12.250   1.0751   0.03501   0.02907   0.0342   0.0140   1.0000
  12.500   1.0797   0.03673   0.03089   0.0355   0.0136   1.0000
  12.750   1.0846   0.03847   0.03273   0.0368   0.0134   1.0000
  13.000   1.0892   0.04030   0.03464   0.0379   0.0131   1.0000
  13.250   1.0935   0.04222   0.03666   0.0389   0.0129   1.0000
  13.500   1.0973   0.04418   0.03872   0.0397   0.0127   1.0000
  13.750   1.0999   0.04629   0.04091   0.0403   0.0123   1.0000
  14.000   1.1025   0.04863   0.04338   0.0414   0.0123   1.0000
  14.250   1.1034   0.05089   0.04569   0.0414   0.0120   1.0000
  14.500   1.1038   0.05345   0.04838   0.0418   0.0119   1.0000
  14.750   1.1035   0.05610   0.05109   0.0421   0.0115   1.0000
  15.000   1.1005   0.05924   0.05440   0.0422   0.0116   1.0000
  15.250   1.0975   0.06240   0.05765   0.0421   0.0114   1.0000
  15.500   1.0831   0.06748   0.06294   0.0423   0.0111   1.0000
  15.750   1.0747   0.07152   0.06713   0.0414   0.0111   1.0000
  16.000   1.0613   0.07650   0.07229   0.0400   0.0111   1.0000
  16.250   1.0505   0.08120   0.07713   0.0383   0.0111   1.0000
  16.500   1.0289   0.08792   0.08406   0.0358   0.0111   1.0000
  16.750   1.0210   0.09258   0.08883   0.0335   0.0111   1.0000
  17.000   0.9971   0.10023   0.09667   0.0299   0.0111   1.0000
  17.250   0.9810   0.10727   0.10390   0.0250   0.0108   1.0000
  17.500   0.7540   0.11530   0.11257   0.0268   0.0129   1.0000
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