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NACA 6412 (naca6412-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: NACA 6412 (naca6412-il)
Reynolds number: 1,000,000
Max Cl/Cd: 136.61 at α=5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-naca6412-il-1000000-n5.txt
Download as CSV file: xf-naca6412-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NACA 6412                                       
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -14.500  -0.3133   0.14165   0.13978  -0.0534   0.9966   0.0099
 -14.250  -0.3023   0.13860   0.13673  -0.0557   0.9958   0.0100
 -13.250  -0.7265   0.02680   0.02365  -0.1446   0.9505   0.0142
 -13.000  -0.7102   0.02449   0.02114  -0.1458   0.9447   0.0144
 -12.750  -0.6912   0.02284   0.01932  -0.1464   0.9398   0.0145
 -12.500  -0.6710   0.02151   0.01785  -0.1467   0.9342   0.0147
 -12.250  -0.6492   0.02043   0.01662  -0.1467   0.9291   0.0148
 -12.000  -0.6266   0.01946   0.01552  -0.1468   0.9245   0.0150
 -11.750  -0.6051   0.01832   0.01426  -0.1468   0.9189   0.0153
 -11.500  -0.5819   0.01745   0.01328  -0.1466   0.9135   0.0156
 -11.250  -0.5575   0.01678   0.01251  -0.1465   0.9086   0.0159
 -11.000  -0.5327   0.01619   0.01185  -0.1464   0.9031   0.0162
 -10.750  -0.5076   0.01564   0.01121  -0.1462   0.8976   0.0165
 -10.500  -0.4822   0.01512   0.01059  -0.1461   0.8924   0.0168
 -10.250  -0.4568   0.01458   0.00996  -0.1459   0.8861   0.0171
 -10.000  -0.4314   0.01411   0.00937  -0.1456   0.8787   0.0174
  -9.750  -0.4056   0.01367   0.00883  -0.1454   0.8705   0.0177
  -9.500  -0.3799   0.01329   0.00833  -0.1451   0.8613   0.0179
  -9.250  -0.3540   0.01284   0.00779  -0.1449   0.8529   0.0182
  -9.000  -0.3283   0.01238   0.00725  -0.1446   0.8454   0.0187
  -8.750  -0.3019   0.01201   0.00681  -0.1444   0.8388   0.0191
  -8.500  -0.2754   0.01170   0.00642  -0.1442   0.8313   0.0195
  -8.250  -0.2487   0.01141   0.00607  -0.1440   0.8246   0.0200
  -8.000  -0.2217   0.01115   0.00574  -0.1438   0.8173   0.0206
  -7.750  -0.1950   0.01090   0.00540  -0.1435   0.8101   0.0210
  -7.500  -0.1679   0.01066   0.00509  -0.1433   0.8023   0.0214
  -7.250  -0.1416   0.01037   0.00473  -0.1430   0.7939   0.0222
  -7.000  -0.1146   0.01012   0.00443  -0.1428   0.7860   0.0228
  -6.750  -0.0877   0.00993   0.00418  -0.1426   0.7781   0.0236
  -6.500  -0.0604   0.00974   0.00393  -0.1424   0.7705   0.0244
  -6.250  -0.0335   0.00959   0.00371  -0.1421   0.7616   0.0252
  -6.000  -0.0065   0.00939   0.00347  -0.1419   0.7525   0.0265
  -5.750   0.0202   0.00925   0.00328  -0.1416   0.7433   0.0277
  -5.500   0.0475   0.00912   0.00309  -0.1414   0.7340   0.0290
  -5.250   0.0743   0.00899   0.00291  -0.1411   0.7246   0.0305
  -5.000   0.1012   0.00888   0.00275  -0.1408   0.7142   0.0324
  -4.750   0.1282   0.00880   0.00261  -0.1405   0.7041   0.0341
  -4.250   0.1820   0.00861   0.00235  -0.1399   0.6840   0.0391
  -4.000   0.2088   0.00854   0.00223  -0.1396   0.6742   0.0417
  -3.750   0.2357   0.00847   0.00214  -0.1393   0.6638   0.0446
  -3.500   0.2625   0.00843   0.00204  -0.1390   0.6533   0.0474
  -3.250   0.2890   0.00839   0.00197  -0.1387   0.6421   0.0511
  -3.000   0.3159   0.00836   0.00189  -0.1384   0.6307   0.0548
  -2.750   0.3425   0.00832   0.00183  -0.1380   0.6204   0.0595
  -2.500   0.3690   0.00831   0.00178  -0.1377   0.6099   0.0637
  -2.250   0.3958   0.00828   0.00174  -0.1374   0.5996   0.0699
  -2.000   0.4222   0.00828   0.00171  -0.1370   0.5888   0.0768
  -1.500   0.4754   0.00826   0.00166  -0.1364   0.5697   0.0927
  -1.250   0.5019   0.00828   0.00165  -0.1360   0.5602   0.1001
  -1.000   0.5286   0.00828   0.00165  -0.1358   0.5515   0.1084
  -0.750   0.5549   0.00831   0.00166  -0.1354   0.5423   0.1176
  -0.500   0.5817   0.00832   0.00167  -0.1351   0.5347   0.1270
  -0.250   0.6081   0.00834   0.00169  -0.1348   0.5268   0.1386
   0.000   0.6347   0.00836   0.00172  -0.1345   0.5198   0.1513
   0.250   0.6612   0.00838   0.00175  -0.1342   0.5125   0.1663
   0.500   0.6874   0.00842   0.00179  -0.1338   0.5062   0.1809
   0.750   0.7142   0.00843   0.00184  -0.1336   0.5004   0.1966
   1.000   0.7403   0.00847   0.00189  -0.1332   0.4938   0.2159
   1.250   0.7667   0.00851   0.00195  -0.1329   0.4883   0.2334
   1.500   0.7932   0.00853   0.00201  -0.1326   0.4829   0.2532
   1.750   0.8194   0.00857   0.00209  -0.1323   0.4777   0.2761
   2.000   0.8453   0.00861   0.00217  -0.1319   0.4729   0.3031
   2.250   0.8717   0.00862   0.00225  -0.1316   0.4685   0.3319
   2.500   0.8977   0.00863   0.00234  -0.1313   0.4637   0.3687
   2.750   0.9190   0.00822   0.00254  -0.1302   0.4590   0.6379
   3.000   0.9909   0.00776   0.00282  -0.1405   0.4530   0.9999
   3.250   1.0178   0.00787   0.00291  -0.1403   0.4486   0.9999
   3.500   1.0442   0.00800   0.00301  -0.1400   0.4439   0.9999
   3.750   1.0703   0.00814   0.00313  -0.1397   0.4390   0.9999
   4.000   1.0973   0.00825   0.00323  -0.1396   0.4344   0.9999
   4.250   1.1238   0.00837   0.00334  -0.1394   0.4301   0.9999
   4.500   1.1499   0.00852   0.00347  -0.1391   0.4257   0.9999
   4.750   1.1760   0.00866   0.00360  -0.1389   0.4208   0.9999
   5.000   1.2022   0.00880   0.00373  -0.1386   0.4142   0.9999
   5.250   1.2271   0.00900   0.00390  -0.1381   0.4066   0.9999
   5.500   1.2526   0.00917   0.00405  -0.1378   0.3960   0.9999
   5.750   1.2768   0.00941   0.00423  -0.1372   0.3832   0.9999
   6.000   1.3004   0.00967   0.00444  -0.1365   0.3690   0.9999
   6.250   1.3228   0.01001   0.00468  -0.1357   0.3497   0.9999
   6.500   1.3451   0.01034   0.00493  -0.1348   0.3327   0.9999
   6.750   1.3660   0.01075   0.00524  -0.1337   0.3133   0.9999
   7.000   1.3848   0.01128   0.00563  -0.1322   0.2865   0.9999
   7.250   1.4025   0.01181   0.00604  -0.1305   0.2641   0.9999
   7.500   1.4173   0.01244   0.00651  -0.1284   0.2361   0.9999
   7.750   1.4314   0.01312   0.00705  -0.1261   0.2085   0.9999
   8.000   1.4447   0.01387   0.00764  -0.1238   0.1813   0.9999
   8.250   1.4575   0.01464   0.00828  -0.1215   0.1568   0.9999
   8.500   1.4687   0.01553   0.00901  -0.1190   0.1310   0.9999
   8.750   1.4813   0.01634   0.00972  -0.1168   0.1108   0.9999
   9.000   1.4924   0.01725   0.01052  -0.1145   0.0917   0.9999
   9.250   1.5057   0.01805   0.01126  -0.1125   0.0788   0.9999
   9.500   1.5189   0.01887   0.01203  -0.1106   0.0686   0.9999
   9.750   1.5321   0.01971   0.01284  -0.1088   0.0603   0.9999
  10.000   1.5459   0.02052   0.01364  -0.1071   0.0534   0.9999
  10.250   1.5590   0.02140   0.01451  -0.1054   0.0477   0.9999
  10.500   1.5716   0.02233   0.01543  -0.1038   0.0430   0.9999
  10.750   1.5841   0.02328   0.01639  -0.1021   0.0388   0.9999
  11.000   1.5963   0.02428   0.01741  -0.1005   0.0355   0.9999
  11.250   1.6075   0.02538   0.01851  -0.0989   0.0322   0.9999
  11.500   1.6192   0.02646   0.01962  -0.0974   0.0298   0.9999
  11.750   1.6294   0.02768   0.02086  -0.0959   0.0273   0.9999
  12.000   1.6398   0.02893   0.02214  -0.0944   0.0255   0.9999
  12.250   1.6492   0.03028   0.02352  -0.0930   0.0235   0.9999
  12.500   1.6573   0.03177   0.02504  -0.0915   0.0219   0.9999
  12.750   1.6661   0.03324   0.02655  -0.0902   0.0205   0.9999
  13.000   1.6733   0.03488   0.02824  -0.0889   0.0191   0.9999
  13.250   1.6802   0.03662   0.03002  -0.0876   0.0181   0.9999
  13.500   1.6874   0.03836   0.03181  -0.0865   0.0172   0.9999
  13.750   1.6930   0.04029   0.03379  -0.0853   0.0163   0.9999
  14.000   1.6974   0.04241   0.03596  -0.0842   0.0155   0.9999
  14.250   1.7021   0.04456   0.03818  -0.0833   0.0148   0.9999
  14.500   1.7069   0.04675   0.04043  -0.0824   0.0143   0.9999
  14.750   1.7106   0.04908   0.04283  -0.0816   0.0138   0.9999
  15.000   1.7131   0.05158   0.04539  -0.0809   0.0132   0.9999
  15.250   1.7144   0.05429   0.04816  -0.0802   0.0127   0.9999
  15.500   1.7146   0.05717   0.05111  -0.0796   0.0123   0.9999
  15.750   1.7164   0.05992   0.05394  -0.0792   0.0120   0.9999
  16.000   1.7170   0.06283   0.05693  -0.0788   0.0117   0.9999
  16.250   1.7168   0.06587   0.06005  -0.0784   0.0114   0.9999
  16.500   1.7159   0.06906   0.06331  -0.0782   0.0111   0.9999
  16.750   1.7145   0.07235   0.06667  -0.0780   0.0109   0.9999
  17.000   1.7122   0.07578   0.07017  -0.0780   0.0106   0.9999
  17.250   1.7091   0.07931   0.07378  -0.0780   0.0103   0.9999
  17.500   1.7048   0.08306   0.07761  -0.0780   0.0101   0.9999
  17.750   1.6996   0.08699   0.08162  -0.0782   0.0099   0.9999
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