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TSAGI 12% AIRFOIL (tsagi12-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: TSAGI 12% AIRFOIL (tsagi12-il)
Reynolds number: 1,000,000
Max Cl/Cd: 91.65 at α=5.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-tsagi12-il-1000000.txt
Download as CSV file: xf-tsagi12-il-1000000.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 =     1.000 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -15.250  -0.7414   0.11234   0.11057  -0.0144   1.0000   0.0090
 -15.000  -0.7688   0.10235   0.10054  -0.0192   1.0000   0.0087
 -14.750  -0.9639   0.05614   0.05383  -0.0493   1.0000   0.0080
 -14.500  -0.9611   0.05197   0.04959  -0.0530   1.0000   0.0082
 -14.250  -1.0093   0.04234   0.03964  -0.0583   1.0000   0.0080
 -14.000  -1.0183   0.03924   0.03640  -0.0581   1.0000   0.0081
 -13.750  -1.0297   0.03633   0.03330  -0.0566   1.0000   0.0081
 -13.500  -1.0325   0.03438   0.03121  -0.0547   1.0000   0.0083
 -13.250  -1.0416   0.03209   0.02875  -0.0516   1.0000   0.0083
 -13.000  -1.0447   0.03039   0.02689  -0.0485   1.0000   0.0084
 -12.750  -1.0419   0.02916   0.02553  -0.0455   1.0000   0.0085
 -12.500  -1.0407   0.02788   0.02411  -0.0421   1.0000   0.0085
 -12.250  -1.0377   0.02680   0.02290  -0.0385   1.0000   0.0086
 -12.000  -1.0359   0.02574   0.02170  -0.0345   1.0000   0.0086
 -11.750  -1.0502   0.02318   0.01886  -0.0282   1.0000   0.0091
 -11.500  -1.0423   0.02212   0.01770  -0.0251   1.0000   0.0093
 -11.250  -1.0308   0.02133   0.01682  -0.0225   1.0000   0.0094
 -11.000  -1.0162   0.02080   0.01624  -0.0203   1.0000   0.0098
 -10.750  -1.0040   0.02003   0.01538  -0.0176   1.0000   0.0099
 -10.500  -0.9884   0.01959   0.01489  -0.0154   1.0000   0.0104
 -10.250  -0.9748   0.01897   0.01418  -0.0129   1.0000   0.0106
 -10.000  -0.9600   0.01850   0.01364  -0.0105   1.0000   0.0109
  -9.750  -0.9474   0.01788   0.01293  -0.0077   1.0000   0.0112
  -9.500  -0.9320   0.01760   0.01260  -0.0054   1.0000   0.0114
  -9.250  -0.9051   0.01632   0.01117  -0.0058   0.9980   0.0119
  -9.000  -0.8727   0.01560   0.01041  -0.0073   0.9953   0.0128
  -8.750  -0.8403   0.01512   0.00990  -0.0086   0.9919   0.0135
  -8.500  -0.8083   0.01459   0.00931  -0.0097   0.9878   0.0141
  -8.250  -0.7741   0.01418   0.00885  -0.0113   0.9844   0.0148
  -8.000  -0.7456   0.01335   0.00794  -0.0117   0.9782   0.0157
  -7.750  -0.7121   0.01284   0.00741  -0.0132   0.9723   0.0168
  -7.500  -0.6740   0.01246   0.00702  -0.0156   0.9659   0.0180
  -7.250  -0.6321   0.01220   0.00672  -0.0188   0.9568   0.0192
  -7.000  -0.5928   0.01141   0.00585  -0.0216   0.9403   0.0211
  -6.750  -0.5585   0.01113   0.00551  -0.0231   0.9142   0.0229
  -6.500  -0.5318   0.01095   0.00521  -0.0228   0.8863   0.0242
  -6.250  -0.5094   0.01069   0.00482  -0.0216   0.8621   0.0257
  -6.000  -0.4877   0.01038   0.00443  -0.0203   0.8423   0.0280
  -5.750  -0.4647   0.01021   0.00418  -0.0193   0.8248   0.0297
  -5.500  -0.4410   0.01007   0.00395  -0.0184   0.8097   0.0312
  -5.250  -0.4184   0.00980   0.00360  -0.0172   0.7952   0.0337
  -5.000  -0.3952   0.00959   0.00334  -0.0163   0.7814   0.0366
  -4.750  -0.3713   0.00943   0.00312  -0.0154   0.7689   0.0392
  -4.500  -0.3477   0.00924   0.00289  -0.0145   0.7567   0.0442
  -4.250  -0.3238   0.00904   0.00272  -0.0136   0.7446   0.0540
  -4.000  -0.2994   0.00889   0.00258  -0.0129   0.7328   0.0657
  -3.750  -0.2743   0.00882   0.00247  -0.0123   0.7216   0.0733
  -3.500  -0.2499   0.00870   0.00231  -0.0115   0.7111   0.0801
  -3.250  -0.2249   0.00857   0.00217  -0.0109   0.7009   0.0862
  -3.000  -0.1999   0.00847   0.00204  -0.0103   0.6914   0.0925
  -2.750  -0.1755   0.00835   0.00191  -0.0096   0.6816   0.1021
  -2.500  -0.1519   0.00811   0.00179  -0.0087   0.6724   0.1377
  -2.250  -0.1287   0.00789   0.00169  -0.0078   0.6641   0.1795
  -2.000  -0.1053   0.00767   0.00160  -0.0069   0.6558   0.2239
  -1.750  -0.0831   0.00739   0.00151  -0.0058   0.6479   0.2850
  -1.500  -0.0634   0.00698   0.00140  -0.0043   0.6395   0.3796
  -1.250  -0.0482   0.00640   0.00129  -0.0018   0.6321   0.5192
  -1.000  -0.0420   0.00570   0.00118   0.0029   0.6246   0.6914
  -0.750  -0.0319   0.00524   0.00118   0.0070   0.6175   0.8159
  -0.500  -0.0048   0.00517   0.00122   0.0074   0.6089   0.8654
  -0.250   0.0260   0.00518   0.00125   0.0069   0.6007   0.8880
   0.000   0.0587   0.00524   0.00129   0.0059   0.5917   0.9032
   0.250   0.0906   0.00530   0.00133   0.0051   0.5824   0.9157
   0.500   0.1279   0.00543   0.00143   0.0031   0.5722   0.9268
   0.750   0.1644   0.00557   0.00151   0.0012   0.5610   0.9332
   1.000   0.1988   0.00572   0.00163  -0.0002   0.5490   0.9397
   1.250   0.2288   0.00589   0.00175  -0.0005   0.5364   0.9456
   1.500   0.2778   0.00627   0.00206  -0.0050   0.5208   0.9488
   1.750   0.3219   0.00666   0.00238  -0.0083   0.5056   0.9531
   2.000   0.3461   0.00683   0.00250  -0.0074   0.4920   0.9585
   2.250   0.3855   0.00704   0.00264  -0.0100   0.4780   0.9594
   2.500   0.4223   0.00721   0.00276  -0.0120   0.4657   0.9604
   2.750   0.4545   0.00734   0.00284  -0.0131   0.4549   0.9614
   3.000   0.4863   0.00745   0.00292  -0.0141   0.4446   0.9626
   3.250   0.5172   0.00757   0.00300  -0.0148   0.4336   0.9641
   3.500   0.5466   0.00768   0.00308  -0.0153   0.4253   0.9660
   3.750   0.5711   0.00778   0.00318  -0.0146   0.4180   0.9693
   4.000   0.5963   0.00790   0.00327  -0.0142   0.4106   0.9718
   4.250   0.6298   0.00797   0.00335  -0.0155   0.4025   0.9725
   4.500   0.6627   0.00808   0.00345  -0.0168   0.3937   0.9733
   4.750   0.6952   0.00821   0.00354  -0.0180   0.3808   0.9743
   5.000   0.7272   0.00834   0.00363  -0.0191   0.3653   0.9755
   5.250   0.7580   0.00848   0.00374  -0.0200   0.3494   0.9769
   5.500   0.7871   0.00864   0.00386  -0.0205   0.3328   0.9786
   5.750   0.8129   0.00887   0.00401  -0.0203   0.3100   0.9810
   6.000   0.8341   0.00921   0.00423  -0.0191   0.2798   0.9839
   6.250   0.8629   0.00964   0.00446  -0.0199   0.2346   0.9847
   6.500   0.8896   0.01030   0.00483  -0.0204   0.1771   0.9858
   6.750   0.9130   0.01125   0.00538  -0.0204   0.1050   0.9875
   7.000   0.9363   0.01206   0.00595  -0.0202   0.0586   0.9894
   7.250   0.9589   0.01283   0.00653  -0.0198   0.0287   0.9916
   7.500   0.9836   0.01330   0.00699  -0.0196   0.0229   0.9936
   7.750   1.0105   0.01380   0.00750  -0.0199   0.0190   0.9949
   8.000   1.0394   0.01414   0.00788  -0.0207   0.0177   0.9959
   8.250   1.0670   0.01456   0.00831  -0.0212   0.0161   0.9972
   8.500   1.0922   0.01523   0.00904  -0.0213   0.0145   0.9987
   8.750   1.1202   0.01566   0.00952  -0.0219   0.0140   0.9999
   9.000   1.1365   0.01606   0.00995  -0.0201   0.0133   1.0000
   9.250   1.1498   0.01648   0.01041  -0.0177   0.0125   1.0000
   9.500   1.1605   0.01700   0.01097  -0.0148   0.0121   1.0000
   9.750   1.1671   0.01768   0.01169  -0.0113   0.0116   1.0000
  10.000   1.1640   0.01869   0.01280  -0.0061   0.0111   1.0000
  10.250   1.1717   0.01912   0.01329  -0.0027   0.0109   1.0000
  10.500   1.1701   0.01953   0.01374   0.0024   0.0107   1.0000
  10.750   1.1693   0.02000   0.01427   0.0072   0.0104   1.0000
  11.000   1.1686   0.02067   0.01500   0.0116   0.0102   1.0000
  11.250   1.1688   0.02148   0.01588   0.0155   0.0101   1.0000
  11.500   1.1716   0.02234   0.01680   0.0187   0.0097   1.0000
  11.750   1.1718   0.02348   0.01801   0.0217   0.0096   1.0000
  12.000   1.1795   0.02433   0.01890   0.0237   0.0092   1.0000
  12.250   1.1816   0.02566   0.02028   0.0259   0.0090   1.0000
  12.500   1.1803   0.02737   0.02206   0.0281   0.0087   1.0000
  12.750   1.1798   0.02920   0.02396   0.0298   0.0086   1.0000
  13.000   1.1743   0.03158   0.02643   0.0315   0.0084   1.0000
  13.250   1.1680   0.03420   0.02915   0.0330   0.0083   1.0000
  13.500   1.1628   0.03684   0.03189   0.0341   0.0082   1.0000
  13.750   1.1701   0.03845   0.03359   0.0345   0.0080   1.0000
  14.000   1.1650   0.04125   0.03648   0.0354   0.0080   1.0000
  14.250   1.1731   0.04290   0.03820   0.0355   0.0078   1.0000
  14.500   1.1755   0.04513   0.04051   0.0356   0.0077   1.0000
  14.750   1.1771   0.04753   0.04299   0.0357   0.0074   1.0000
  15.000   1.1739   0.05043   0.04599   0.0359   0.0075   1.0000
  15.250   1.1749   0.05304   0.04868   0.0356   0.0073   1.0000
  15.500   1.1732   0.05607   0.05180   0.0352   0.0070   1.0000
  15.750   1.1715   0.05913   0.05494   0.0348   0.0070   1.0000
  16.000   1.1683   0.06249   0.05839   0.0342   0.0069   1.0000
  16.250   1.1651   0.06592   0.06190   0.0334   0.0068   1.0000
  16.500   1.1628   0.06938   0.06544   0.0324   0.0067   1.0000
  16.750   1.1566   0.07333   0.06950   0.0315   0.0067   1.0000
  17.000   1.1535   0.07708   0.07333   0.0302   0.0066   1.0000
  17.250   1.1514   0.08083   0.07712   0.0286   0.0063   1.0000
  17.500   1.1425   0.08538   0.08179   0.0273   0.0064   1.0000
  17.750   1.1307   0.09040   0.08696   0.0259   0.0065   1.0000
  18.000   1.1254   0.09481   0.09142   0.0240   0.0063   1.0000
  18.250   1.1164   0.09976   0.09645   0.0221   0.0062   1.0000
  18.500   1.1096   0.10448   0.10126   0.0201   0.0063   1.0000
  18.750   1.0937   0.11069   0.10758   0.0175   0.0061   1.0000
  19.000   1.0858   0.11588   0.11289   0.0152   0.0062   1.0000
  19.250   1.0751   0.12163   0.11875   0.0126   0.0062   1.0000
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