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TSAGI 12% AIRFOIL (tsagi12-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: TSAGI 12% AIRFOIL (tsagi12-il)
Reynolds number: 1,000,000
Max Cl/Cd: 86.5 at α=5.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-tsagi12-il-1000000-n5.txt
Download as CSV file: xf-tsagi12-il-1000000-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 =     1.000 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -16.250  -0.7589   0.12417   0.12222  -0.0093   1.0000   0.0049
 -16.000  -0.8092   0.10995   0.10794  -0.0167   1.0000   0.0048
 -15.750  -1.0820   0.05065   0.04798  -0.0549   1.0000   0.0041
 -15.500  -1.1217   0.04226   0.03931  -0.0595   1.0000   0.0040
 -15.250  -1.1427   0.03794   0.03479  -0.0594   1.0000   0.0039
 -15.000  -1.1396   0.03624   0.03302  -0.0585   1.0000   0.0040
 -14.750  -1.1471   0.03383   0.03046  -0.0566   1.0000   0.0041
 -14.500  -1.1510   0.03190   0.02840  -0.0542   1.0000   0.0041
 -14.250  -1.1522   0.03026   0.02663  -0.0516   1.0000   0.0042
 -14.000  -1.1498   0.02895   0.02520  -0.0490   1.0000   0.0042
 -13.750  -1.1484   0.02761   0.02373  -0.0459   1.0000   0.0042
 -13.500  -1.1409   0.02669   0.02272  -0.0433   1.0000   0.0044
 -13.250  -1.1376   0.02560   0.02150  -0.0399   1.0000   0.0044
 -13.000  -1.1309   0.02475   0.02056  -0.0367   1.0000   0.0046
 -12.750  -1.1248   0.02392   0.01963  -0.0333   1.0000   0.0046
 -12.500  -1.1168   0.02300   0.01861  -0.0303   1.0000   0.0047
 -12.250  -1.1052   0.02222   0.01772  -0.0278   1.0000   0.0048
 -12.000  -1.0938   0.02139   0.01678  -0.0252   1.0000   0.0049
 -11.750  -1.0803   0.02070   0.01601  -0.0229   1.0000   0.0050
 -11.500  -1.0647   0.02018   0.01541  -0.0208   1.0000   0.0050
 -11.250  -1.0530   0.01935   0.01447  -0.0181   1.0000   0.0051
 -11.000  -1.0403   0.01859   0.01362  -0.0155   1.0000   0.0054
 -10.500  -0.9948   0.01724   0.01215  -0.0144   0.9968   0.0059
 -10.250  -0.9694   0.01663   0.01147  -0.0144   0.9911   0.0061
 -10.000  -0.9413   0.01603   0.01079  -0.0148   0.9858   0.0064
  -9.750  -0.9130   0.01547   0.01017  -0.0153   0.9792   0.0066
  -9.500  -0.8803   0.01495   0.00958  -0.0167   0.9734   0.0070
  -9.250  -0.8458   0.01443   0.00899  -0.0185   0.9665   0.0072
  -9.000  -0.8089   0.01373   0.00823  -0.0209   0.9584   0.0080
  -8.750  -0.7691   0.01316   0.00760  -0.0239   0.9462   0.0087
  -8.500  -0.7317   0.01270   0.00706  -0.0262   0.9261   0.0095
  -8.250  -0.7022   0.01238   0.00660  -0.0267   0.8988   0.0099
  -8.000  -0.6790   0.01208   0.00618  -0.0258   0.8720   0.0107
  -7.750  -0.6574   0.01182   0.00582  -0.0246   0.8473   0.0119
  -7.500  -0.6358   0.01161   0.00550  -0.0233   0.8238   0.0131
  -7.250  -0.6136   0.01141   0.00520  -0.0222   0.8031   0.0143
  -7.000  -0.5913   0.01119   0.00493  -0.0211   0.7853   0.0165
  -6.750  -0.5683   0.01101   0.00467  -0.0201   0.7681   0.0185
  -6.500  -0.5449   0.01083   0.00441  -0.0192   0.7517   0.0201
  -6.250  -0.5215   0.01064   0.00418  -0.0183   0.7371   0.0222
  -6.000  -0.4973   0.01047   0.00396  -0.0176   0.7251   0.0243
  -5.750  -0.4726   0.01035   0.00378  -0.0169   0.7130   0.0258
  -5.500  -0.4480   0.01021   0.00357  -0.0162   0.7023   0.0270
  -5.250  -0.4240   0.01002   0.00332  -0.0155   0.6923   0.0293
  -5.000  -0.3994   0.00985   0.00312  -0.0148   0.6823   0.0313
  -4.750  -0.3746   0.00971   0.00294  -0.0142   0.6726   0.0331
  -4.500  -0.3498   0.00959   0.00276  -0.0135   0.6630   0.0345
  -4.250  -0.3248   0.00943   0.00259  -0.0129   0.6548   0.0393
  -4.000  -0.3002   0.00928   0.00244  -0.0123   0.6471   0.0462
  -3.750  -0.2752   0.00912   0.00231  -0.0117   0.6389   0.0565
  -3.500  -0.2501   0.00902   0.00220  -0.0111   0.6310   0.0645
  -3.250  -0.2242   0.00895   0.00210  -0.0107   0.6233   0.0674
  -3.000  -0.1987   0.00886   0.00198  -0.0102   0.6164   0.0717
  -2.750  -0.1731   0.00876   0.00187  -0.0097   0.6095   0.0765
  -2.500  -0.1475   0.00870   0.00178  -0.0093   0.6021   0.0800
  -2.250  -0.1214   0.00863   0.00169  -0.0089   0.5940   0.0830
  -2.000  -0.0959   0.00856   0.00160  -0.0084   0.5865   0.0883
  -1.750  -0.0707   0.00843   0.00151  -0.0079   0.5791   0.1027
  -1.500  -0.0467   0.00826   0.00144  -0.0071   0.5715   0.1397
  -1.250  -0.0217   0.00813   0.00137  -0.0066   0.5622   0.1657
  -1.000   0.0032   0.00803   0.00132  -0.0060   0.5533   0.1885
  -0.750   0.0272   0.00789   0.00127  -0.0052   0.5431   0.2268
  -0.500   0.0485   0.00756   0.00120  -0.0040   0.5328   0.3124
  -0.250   0.0687   0.00723   0.00114  -0.0025   0.5215   0.4070
   0.000   0.0895   0.00698   0.00110  -0.0012   0.5103   0.4847
   0.250   0.1073   0.00664   0.00104   0.0009   0.4988   0.5809
   0.500   0.1208   0.00624   0.00100   0.0040   0.4877   0.6952
   0.750   0.1348   0.00595   0.00100   0.0071   0.4768   0.7817
   1.000   0.1558   0.00582   0.00106   0.0087   0.4665   0.8485
   1.250   0.1862   0.00583   0.00114   0.0082   0.4558   0.8854
   1.500   0.2241   0.00591   0.00125   0.0060   0.4459   0.9094
   1.750   0.2712   0.00609   0.00142   0.0017   0.4360   0.9278
   2.000   0.3114   0.00628   0.00158  -0.0011   0.4274   0.9398
   2.250   0.3435   0.00641   0.00168  -0.0020   0.4199   0.9431
   2.500   0.3707   0.00651   0.00176  -0.0019   0.4129   0.9468
   2.750   0.3968   0.00664   0.00187  -0.0015   0.4067   0.9516
   3.000   0.4312   0.00678   0.00199  -0.0031   0.3994   0.9531
   3.250   0.4623   0.00691   0.00209  -0.0039   0.3926   0.9543
   3.500   0.4926   0.00703   0.00219  -0.0045   0.3833   0.9556
   3.750   0.5221   0.00717   0.00230  -0.0050   0.3722   0.9575
   4.000   0.5479   0.00731   0.00241  -0.0046   0.3641   0.9608
   4.250   0.5716   0.00740   0.00251  -0.0037   0.3589   0.9640
   4.500   0.6027   0.00753   0.00262  -0.0046   0.3503   0.9647
   4.750   0.6337   0.00764   0.00274  -0.0055   0.3433   0.9654
   5.000   0.6639   0.00780   0.00287  -0.0062   0.3310   0.9662
   5.250   0.6929   0.00801   0.00302  -0.0067   0.3101   0.9673
   5.500   0.7199   0.00833   0.00321  -0.0068   0.2792   0.9687
   5.750   0.7431   0.00882   0.00349  -0.0063   0.2348   0.9709
   6.000   0.7574   0.00940   0.00384  -0.0039   0.1879   0.9753
   6.250   0.7841   0.00996   0.00420  -0.0042   0.1476   0.9761
   6.500   0.8087   0.01066   0.00466  -0.0042   0.0980   0.9772
   6.750   0.8347   0.01115   0.00504  -0.0044   0.0743   0.9784
   7.000   0.8589   0.01174   0.00548  -0.0042   0.0456   0.9800
   7.250   0.8824   0.01225   0.00590  -0.0038   0.0292   0.9821
   7.500   0.9014   0.01264   0.00628  -0.0023   0.0218   0.9851
   7.750   0.9282   0.01303   0.00665  -0.0026   0.0167   0.9860
   8.000   0.9557   0.01341   0.00704  -0.0031   0.0135   0.9867
   8.250   0.9831   0.01377   0.00742  -0.0035   0.0121   0.9877
   8.500   1.0094   0.01421   0.00786  -0.0038   0.0106   0.9889
   8.750   1.0349   0.01463   0.00831  -0.0039   0.0097   0.9902
   9.000   1.0597   0.01502   0.00873  -0.0038   0.0089   0.9916
   9.250   1.0827   0.01547   0.00922  -0.0034   0.0085   0.9932
   9.500   1.1050   0.01597   0.00974  -0.0030   0.0076   0.9946
   9.750   1.1298   0.01658   0.01039  -0.0032   0.0070   0.9957
  10.000   1.1548   0.01704   0.01090  -0.0034   0.0067   0.9969
  10.250   1.1784   0.01755   0.01145  -0.0034   0.0063   0.9981
  10.500   1.2009   0.01813   0.01207  -0.0033   0.0061   0.9992
  10.750   1.2177   0.01866   0.01265  -0.0020   0.0058   1.0000
  11.000   1.2153   0.01911   0.01315   0.0033   0.0057   1.0000
  11.250   1.2159   0.01965   0.01374   0.0077   0.0055   1.0000
  11.500   1.2170   0.02034   0.01448   0.0116   0.0053   1.0000
  11.750   1.2162   0.02128   0.01549   0.0155   0.0050   1.0000
  12.000   1.2193   0.02219   0.01645   0.0184   0.0049   1.0000
  12.250   1.2238   0.02315   0.01749   0.0209   0.0049   1.0000
  12.500   1.2285   0.02423   0.01863   0.0231   0.0047   1.0000
  12.750   1.2323   0.02548   0.01996   0.0251   0.0046   1.0000
  13.000   1.2415   0.02645   0.02097   0.0265   0.0044   1.0000
  13.250   1.2421   0.02818   0.02279   0.0282   0.0043   1.0000
  13.500   1.2461   0.02974   0.02442   0.0294   0.0042   1.0000
  13.750   1.2497   0.03145   0.02621   0.0305   0.0040   1.0000
  14.000   1.2503   0.03351   0.02835   0.0314   0.0040   1.0000
  14.250   1.2568   0.03511   0.03000   0.0320   0.0039   1.0000
  14.500   1.2593   0.03714   0.03211   0.0325   0.0038   1.0000
  14.750   1.2590   0.03955   0.03460   0.0330   0.0038   1.0000
  15.000   1.2581   0.04207   0.03720   0.0332   0.0037   1.0000
  15.250   1.2548   0.04494   0.04015   0.0334   0.0036   1.0000
  15.500   1.2514   0.04791   0.04319   0.0333   0.0035   1.0000
  15.750   1.2449   0.05135   0.04674   0.0330   0.0034   1.0000
  16.000   1.2437   0.05430   0.04979   0.0326   0.0036   1.0000
  16.250   1.2319   0.05869   0.05427   0.0318   0.0033   1.0000
  16.500   1.2249   0.06260   0.05829   0.0309   0.0033   1.0000
  16.750   1.2190   0.06648   0.06225   0.0299   0.0033   1.0000
  17.000   1.2118   0.07062   0.06650   0.0287   0.0033   1.0000
  17.250   1.2037   0.07496   0.07093   0.0274   0.0033   1.0000
  17.500   1.2007   0.07868   0.07474   0.0262   0.0033   1.0000
  17.750   1.1919   0.08330   0.07946   0.0247   0.0032   1.0000
  18.000   1.1846   0.08775   0.08402   0.0232   0.0032   1.0000
  18.250   1.1714   0.09321   0.08958   0.0212   0.0032   1.0000
  18.500   1.1643   0.09783   0.09430   0.0194   0.0032   1.0000
  18.750   1.1514   0.10345   0.10003   0.0172   0.0031   1.0000
  19.000   1.1409   0.10878   0.10545   0.0150   0.0031   1.0000
  19.250   1.1290   0.11448   0.11125   0.0126   0.0031   1.0000
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