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TSAGI 12% AIRFOIL (tsagi12-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: TSAGI 12% AIRFOIL (tsagi12-il)
Reynolds number: 500,000
Max Cl/Cd: 76.53 at α=5.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-tsagi12-il-500000-n5.txt
Download as CSV file: xf-tsagi12-il-500000-n5.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 =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -14.500  -0.7633   0.09342   0.09089  -0.0263   1.0000   0.0070
 -14.250  -0.8555   0.07124   0.06861  -0.0389   1.0000   0.0066
 -14.000  -0.9230   0.05014   0.04712  -0.0560   1.0000   0.0062
 -13.750  -0.9506   0.04385   0.04059  -0.0588   1.0000   0.0061
 -13.500  -0.9609   0.04065   0.03723  -0.0584   1.0000   0.0063
 -13.250  -0.9765   0.03748   0.03385  -0.0566   1.0000   0.0063
 -13.000  -0.9818   0.03538   0.03159  -0.0543   1.0000   0.0065
 -12.750  -0.9872   0.03344   0.02947  -0.0513   1.0000   0.0065
 -12.500  -0.9932   0.03155   0.02740  -0.0476   1.0000   0.0066
 -12.250  -0.9941   0.03009   0.02577  -0.0441   1.0000   0.0067
 -12.000  -0.9957   0.02868   0.02418  -0.0401   1.0000   0.0068
 -11.750  -0.9940   0.02755   0.02289  -0.0362   1.0000   0.0069
 -11.500  -0.9870   0.02656   0.02175  -0.0331   1.0000   0.0071
 -11.250  -0.9805   0.02540   0.02044  -0.0299   1.0000   0.0072
 -11.000  -0.9741   0.02421   0.01911  -0.0266   1.0000   0.0074
 -10.750  -0.9637   0.02329   0.01810  -0.0239   1.0000   0.0077
 -10.500  -0.9517   0.02247   0.01718  -0.0214   1.0000   0.0080
 -10.250  -0.9378   0.02181   0.01644  -0.0191   1.0000   0.0084
 -10.000  -0.9250   0.02105   0.01558  -0.0166   1.0000   0.0086
  -9.750  -0.9115   0.02037   0.01479  -0.0141   1.0000   0.0089
  -9.500  -0.8927   0.01961   0.01391  -0.0127   0.9989   0.0093
  -9.250  -0.8645   0.01878   0.01295  -0.0133   0.9932   0.0097
  -9.000  -0.8363   0.01795   0.01200  -0.0139   0.9869   0.0101
  -8.750  -0.8090   0.01706   0.01102  -0.0143   0.9795   0.0109
  -8.500  -0.7773   0.01644   0.01035  -0.0155   0.9731   0.0119
  -8.250  -0.7450   0.01588   0.00971  -0.0168   0.9655   0.0130
  -8.000  -0.7111   0.01530   0.00902  -0.0184   0.9572   0.0138
  -7.750  -0.6753   0.01463   0.00833  -0.0204   0.9476   0.0157
  -7.500  -0.6388   0.01414   0.00778  -0.0226   0.9344   0.0175
  -7.000  -0.5728   0.01327   0.00677  -0.0252   0.8981   0.0219
  -6.750  -0.5450   0.01300   0.00636  -0.0252   0.8744   0.0242
  -6.500  -0.5203   0.01280   0.00601  -0.0245   0.8499   0.0259
  -6.250  -0.4979   0.01251   0.00560  -0.0234   0.8278   0.0284
  -6.000  -0.4754   0.01226   0.00526  -0.0223   0.8073   0.0308
  -5.750  -0.4524   0.01205   0.00494  -0.0213   0.7906   0.0327
  -5.500  -0.4288   0.01187   0.00463  -0.0204   0.7764   0.0345
  -5.250  -0.4057   0.01161   0.00432  -0.0194   0.7638   0.0378
  -5.000  -0.3822   0.01140   0.00406  -0.0186   0.7517   0.0415
  -4.750  -0.3584   0.01121   0.00382  -0.0177   0.7397   0.0454
  -4.500  -0.3343   0.01101   0.00362  -0.0170   0.7287   0.0531
  -4.250  -0.3102   0.01084   0.00343  -0.0162   0.7180   0.0612
  -4.000  -0.2854   0.01075   0.00326  -0.0155   0.7076   0.0674
  -3.750  -0.2611   0.01058   0.00306  -0.0148   0.6971   0.0735
  -3.500  -0.2364   0.01046   0.00288  -0.0141   0.6872   0.0791
  -3.000  -0.1870   0.01021   0.00255  -0.0128   0.6693   0.0902
  -2.750  -0.1623   0.01009   0.00240  -0.0122   0.6605   0.0978
  -2.500  -0.1384   0.00990   0.00227  -0.0114   0.6514   0.1192
  -2.250  -0.1146   0.00970   0.00216  -0.0106   0.6435   0.1528
  -2.000  -0.0907   0.00952   0.00205  -0.0099   0.6353   0.1841
  -1.750  -0.0668   0.00934   0.00196  -0.0091   0.6276   0.2178
  -1.500  -0.0443   0.00909   0.00186  -0.0081   0.6194   0.2719
  -1.250  -0.0247   0.00864   0.00175  -0.0066   0.6115   0.3686
  -1.000  -0.0080   0.00815   0.00164  -0.0044   0.6033   0.4861
  -0.750   0.0016   0.00749   0.00154  -0.0006   0.5960   0.6355
  -0.500   0.0163   0.00711   0.00150   0.0024   0.5881   0.7343
  -0.250   0.0429   0.00688   0.00157   0.0029   0.5792   0.8203
   0.000   0.0806   0.00691   0.00165   0.0009   0.5691   0.8628
   0.250   0.1233   0.00702   0.00175  -0.0023   0.5583   0.8890
   0.500   0.1626   0.00715   0.00186  -0.0047   0.5467   0.9063
   0.750   0.2060   0.00735   0.00201  -0.0080   0.5342   0.9179
   1.000   0.2458   0.00767   0.00228  -0.0104   0.5219   0.9302
   1.250   0.2789   0.00796   0.00251  -0.0112   0.5094   0.9390
   1.500   0.3153   0.00819   0.00267  -0.0130   0.4966   0.9424
   1.750   0.3448   0.00835   0.00277  -0.0134   0.4850   0.9469
   2.000   0.3681   0.00845   0.00283  -0.0124   0.4740   0.9511
   2.250   0.4001   0.00856   0.00289  -0.0134   0.4639   0.9522
   2.750   0.4619   0.00880   0.00305  -0.0150   0.4445   0.9550
   3.000   0.4912   0.00892   0.00314  -0.0155   0.4364   0.9570
   3.250   0.5186   0.00903   0.00324  -0.0155   0.4282   0.9598
   3.500   0.5407   0.00915   0.00335  -0.0143   0.4213   0.9638
   3.750   0.5730   0.00927   0.00346  -0.0154   0.4130   0.9648
   4.000   0.6044   0.00940   0.00358  -0.0164   0.4031   0.9661
   4.250   0.6343   0.00955   0.00370  -0.0170   0.3924   0.9676
   4.500   0.6637   0.00966   0.00383  -0.0175   0.3833   0.9694
   4.750   0.6909   0.00979   0.00397  -0.0176   0.3761   0.9717
   5.000   0.7132   0.00992   0.00412  -0.0165   0.3686   0.9751
   5.250   0.7440   0.01005   0.00426  -0.0174   0.3594   0.9760
   5.500   0.7736   0.01022   0.00441  -0.0180   0.3407   0.9771
   5.750   0.8020   0.01048   0.00458  -0.0185   0.3132   0.9785
   6.000   0.8277   0.01088   0.00482  -0.0185   0.2741   0.9805
   6.250   0.8492   0.01150   0.00518  -0.0178   0.2220   0.9829
   6.500   0.8691   0.01215   0.00563  -0.0168   0.1772   0.9856
   6.750   0.8934   0.01297   0.00617  -0.0170   0.1220   0.9871
   7.250   0.9397   0.01445   0.00729  -0.0167   0.0520   0.9908
   7.500   0.9613   0.01520   0.00791  -0.0162   0.0299   0.9930
   7.750   0.9855   0.01575   0.00847  -0.0161   0.0223   0.9948
   8.000   1.0119   0.01625   0.00900  -0.0164   0.0180   0.9962
   8.250   1.0371   0.01678   0.00955  -0.0166   0.0156   0.9978
   8.500   1.0615   0.01739   0.01021  -0.0166   0.0137   0.9993
   8.750   1.0816   0.01788   0.01077  -0.0157   0.0126   1.0000
   9.000   1.0930   0.01838   0.01132  -0.0130   0.0117   1.0000
   9.250   1.1025   0.01894   0.01193  -0.0100   0.0112   1.0000
   9.500   1.1091   0.01958   0.01263  -0.0065   0.0106   1.0000
   9.750   1.1097   0.02038   0.01349  -0.0020   0.0099   1.0000
  10.000   1.1099   0.02085   0.01403   0.0027   0.0097   1.0000
  10.250   1.1108   0.02138   0.01462   0.0071   0.0093   1.0000
  10.500   1.1122   0.02205   0.01536   0.0111   0.0090   1.0000
  10.750   1.1139   0.02286   0.01624   0.0146   0.0087   1.0000
  11.000   1.1160   0.02380   0.01725   0.0178   0.0084   1.0000
  11.250   1.1194   0.02482   0.01833   0.0205   0.0081   1.0000
  11.500   1.1217   0.02603   0.01961   0.0229   0.0078   1.0000
  11.750   1.1234   0.02745   0.02109   0.0251   0.0075   1.0000
  12.000   1.1249   0.02901   0.02272   0.0269   0.0074   1.0000
  12.250   1.1213   0.03114   0.02496   0.0287   0.0071   1.0000
  12.500   1.1220   0.03306   0.02697   0.0300   0.0070   1.0000
  12.750   1.1245   0.03494   0.02895   0.0310   0.0068   1.0000
  13.000   1.1261   0.03699   0.03109   0.0318   0.0067   1.0000
  13.250   1.1263   0.03926   0.03347   0.0325   0.0065   1.0000
  13.500   1.1265   0.04162   0.03592   0.0331   0.0063   1.0000
  13.750   1.1259   0.04412   0.03851   0.0334   0.0061   1.0000
  14.000   1.1242   0.04680   0.04130   0.0337   0.0060   1.0000
  14.250   1.1228   0.04954   0.04413   0.0338   0.0060   1.0000
  14.500   1.1234   0.05214   0.04681   0.0337   0.0059   1.0000
  14.750   1.1209   0.05518   0.04995   0.0334   0.0058   1.0000
  15.000   1.1173   0.05844   0.05331   0.0331   0.0057   1.0000
  15.250   1.1143   0.06176   0.05672   0.0325   0.0056   1.0000
  15.500   1.1143   0.06486   0.05990   0.0317   0.0054   1.0000
  15.750   1.1106   0.06844   0.06358   0.0308   0.0053   1.0000
  16.000   1.1040   0.07237   0.06765   0.0301   0.0055   1.0000
  16.250   1.1016   0.07610   0.07142   0.0287   0.0052   1.0000
  16.500   1.0956   0.08024   0.07565   0.0274   0.0051   1.0000
  16.750   1.0904   0.08433   0.07984   0.0261   0.0051   1.0000
  17.000   1.0811   0.08910   0.08471   0.0246   0.0050   1.0000
  17.250   1.0740   0.09366   0.08938   0.0230   0.0050   1.0000
  17.500   1.0674   0.09834   0.09417   0.0212   0.0049   1.0000
  17.750   1.0597   0.10323   0.09919   0.0192   0.0048   1.0000
  18.000   1.0512   0.10841   0.10450   0.0171   0.0048   1.0000
  18.250   1.0410   0.11392   0.11013   0.0148   0.0048   1.0000
  18.500   1.0323   0.11937   0.11569   0.0124   0.0047   1.0000
  18.750   1.0205   0.12549   0.12194   0.0096   0.0047   1.0000
  19.000   1.0104   0.13141   0.12798   0.0068   0.0047   1.0000
  19.250   0.9981   0.13799   0.13469   0.0036   0.0047   1.0000
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