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NACA 16-012 (naca16012-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: NACA 16-012 (naca16012-il)
Reynolds number: 1,000,000
Max Cl/Cd: 55.75 at α=8.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-naca16012-il-1000000-n5.txt
Download as CSV file: xf-naca16012-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NACA 16-012                                     
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -16.500  -1.0477   0.06372   0.06124  -0.0644   1.0000   0.0029
 -16.250  -1.0754   0.05635   0.05368  -0.0676   1.0000   0.0029
 -16.000  -1.0972   0.05104   0.04820  -0.0684   1.0000   0.0029
 -15.750  -1.1135   0.04710   0.04410  -0.0677   1.0000   0.0029
 -15.500  -1.1270   0.04391   0.04077  -0.0661   1.0000   0.0029
 -15.250  -1.1381   0.04125   0.03796  -0.0638   1.0000   0.0029
 -15.000  -1.1480   0.03895   0.03551  -0.0610   1.0000   0.0029
 -14.750  -1.1551   0.03708   0.03352  -0.0579   1.0000   0.0030
 -14.500  -1.1626   0.03537   0.03167  -0.0542   1.0000   0.0030
 -14.250  -1.1677   0.03396   0.03015  -0.0504   1.0000   0.0030
 -14.000  -1.1713   0.03226   0.02830  -0.0471   0.9997   0.0030
 -13.750  -1.1696   0.03011   0.02595  -0.0451   0.9986   0.0032
 -13.500  -1.1620   0.02848   0.02417  -0.0435   0.9976   0.0033
 -13.250  -1.1503   0.02713   0.02269  -0.0423   0.9965   0.0033
 -13.000  -1.1357   0.02596   0.02140  -0.0414   0.9957   0.0034
 -12.750  -1.1194   0.02489   0.02022  -0.0406   0.9949   0.0035
 -12.500  -1.1038   0.02391   0.01913  -0.0395   0.9938   0.0036
 -12.250  -1.0875   0.02302   0.01814  -0.0384   0.9922   0.0037
 -12.000  -1.0695   0.02215   0.01715  -0.0376   0.9908   0.0039
 -11.750  -1.0498   0.02132   0.01621  -0.0370   0.9896   0.0040
 -11.500  -1.0291   0.02052   0.01531  -0.0366   0.9885   0.0041
 -11.250  -1.0073   0.01975   0.01445  -0.0364   0.9877   0.0043
 -11.000  -0.9843   0.01903   0.01362  -0.0363   0.9870   0.0044
 -10.750  -0.9601   0.01836   0.01287  -0.0364   0.9863   0.0046
 -10.500  -0.9364   0.01769   0.01212  -0.0364   0.9855   0.0047
 -10.250  -0.9191   0.01697   0.01131  -0.0349   0.9828   0.0050
 -10.000  -0.8970   0.01638   0.01065  -0.0344   0.9811   0.0053
  -9.750  -0.8732   0.01587   0.01009  -0.0343   0.9796   0.0056
  -9.500  -0.8485   0.01538   0.00955  -0.0343   0.9783   0.0060
  -9.250  -0.8233   0.01492   0.00904  -0.0343   0.9772   0.0064
  -9.000  -0.7981   0.01448   0.00854  -0.0344   0.9762   0.0067
  -8.750  -0.7779   0.01404   0.00805  -0.0332   0.9736   0.0071
  -8.500  -0.7573   0.01359   0.00756  -0.0321   0.9708   0.0079
  -8.250  -0.7341   0.01319   0.00714  -0.0316   0.9687   0.0086
  -8.000  -0.7101   0.01283   0.00672  -0.0313   0.9670   0.0093
  -7.750  -0.6855   0.01249   0.00633  -0.0310   0.9654   0.0100
  -7.500  -0.6625   0.01212   0.00597  -0.0304   0.9635   0.0120
  -7.250  -0.6426   0.01185   0.00571  -0.0291   0.9603   0.0138
  -7.000  -0.6204   0.01158   0.00543  -0.0282   0.9576   0.0161
  -6.750  -0.5969   0.01132   0.00519  -0.0276   0.9553   0.0195
  -6.500  -0.5721   0.01111   0.00495  -0.0273   0.9534   0.0217
  -6.250  -0.5461   0.01093   0.00474  -0.0273   0.9518   0.0228
  -6.000  -0.5235   0.01070   0.00449  -0.0264   0.9492   0.0245
  -5.750  -0.5010   0.01047   0.00425  -0.0255   0.9462   0.0267
  -5.500  -0.4772   0.01026   0.00404  -0.0250   0.9436   0.0288
  -5.250  -0.4526   0.01007   0.00383  -0.0246   0.9413   0.0305
  -5.000  -0.4268   0.00989   0.00362  -0.0244   0.9393   0.0319
  -4.750  -0.4008   0.00970   0.00341  -0.0243   0.9374   0.0343
  -4.500  -0.3780   0.00951   0.00323  -0.0235   0.9345   0.0385
  -4.250  -0.3542   0.00934   0.00307  -0.0228   0.9315   0.0417
  -4.000  -0.3299   0.00916   0.00291  -0.0223   0.9288   0.0494
  -3.750  -0.3057   0.00892   0.00274  -0.0218   0.9263   0.0677
  -3.500  -0.2809   0.00866   0.00256  -0.0214   0.9241   0.0915
  -3.250  -0.2575   0.00841   0.00242  -0.0208   0.9214   0.1212
  -3.000  -0.2358   0.00815   0.00229  -0.0197   0.9180   0.1585
  -2.750  -0.2143   0.00784   0.00215  -0.0187   0.9147   0.2071
  -2.500  -0.1951   0.00735   0.00197  -0.0172   0.9115   0.2918
  -2.250  -0.1754   0.00687   0.00179  -0.0158   0.9087   0.3792
  -2.000  -0.1581   0.00648   0.00167  -0.0138   0.9049   0.4538
  -1.750  -0.1426   0.00603   0.00153  -0.0113   0.9007   0.5385
  -1.500  -0.1343   0.00538   0.00134  -0.0072   0.8964   0.6634
  -1.250  -0.1245   0.00493   0.00128  -0.0031   0.8922   0.7639
  -1.000  -0.1072   0.00476   0.00136  -0.0006   0.8881   0.8279
  -0.750  -0.0828   0.00475   0.00141   0.0002   0.8848   0.8534
  -0.500  -0.0549   0.00475   0.00143   0.0001   0.8820   0.8641
  -0.250  -0.0264   0.00475   0.00144  -0.0002   0.8792   0.8701
   0.000   0.0000   0.00476   0.00147   0.0000   0.8751   0.8751
   0.250   0.0264   0.00475   0.00144   0.0002   0.8700   0.8792
   0.500   0.0549   0.00475   0.00143  -0.0001   0.8641   0.8820
   0.750   0.0829   0.00475   0.00141  -0.0002   0.8534   0.8848
   1.000   0.1071   0.00476   0.00136   0.0006   0.8271   0.8881
   1.250   0.1246   0.00493   0.00128   0.0031   0.7639   0.8923
   1.500   0.1344   0.00538   0.00134   0.0072   0.6635   0.8964
   1.750   0.1427   0.00603   0.00153   0.0113   0.5391   0.9007
   2.000   0.1583   0.00648   0.00167   0.0137   0.4548   0.9049
   2.250   0.1755   0.00687   0.00179   0.0157   0.3796   0.9087
   2.500   0.1950   0.00736   0.00197   0.0172   0.2911   0.9115
   2.750   0.2143   0.00784   0.00215   0.0186   0.2070   0.9147
   3.000   0.2359   0.00815   0.00229   0.0197   0.1585   0.9180
   3.250   0.2576   0.00841   0.00242   0.0207   0.1209   0.9214
   3.500   0.2810   0.00866   0.00256   0.0214   0.0917   0.9240
   3.750   0.3058   0.00892   0.00274   0.0218   0.0675   0.9263
   4.000   0.3301   0.00915   0.00291   0.0223   0.0495   0.9287
   4.250   0.3543   0.00934   0.00307   0.0228   0.0417   0.9315
   4.500   0.3781   0.00951   0.00323   0.0234   0.0385   0.9345
   4.750   0.4010   0.00970   0.00341   0.0242   0.0343   0.9374
   5.000   0.4270   0.00989   0.00362   0.0244   0.0319   0.9392
   5.250   0.4528   0.01007   0.00383   0.0245   0.0305   0.9413
   5.500   0.4775   0.01026   0.00404   0.0249   0.0287   0.9435
   5.750   0.5013   0.01047   0.00425   0.0255   0.0266   0.9461
   6.000   0.5238   0.01070   0.00449   0.0263   0.0245   0.9492
   6.250   0.5463   0.01093   0.00474   0.0272   0.0228   0.9518
   6.500   0.5724   0.01111   0.00495   0.0272   0.0217   0.9534
   6.750   0.5972   0.01133   0.00519   0.0275   0.0195   0.9553
   7.000   0.6207   0.01158   0.00543   0.0281   0.0161   0.9576
   7.250   0.6429   0.01185   0.00571   0.0290   0.0139   0.9602
   7.500   0.6629   0.01212   0.00597   0.0303   0.0119   0.9634
   7.750   0.6859   0.01249   0.00633   0.0309   0.0100   0.9654
   8.000   0.7105   0.01282   0.00672   0.0312   0.0094   0.9670
   8.250   0.7345   0.01319   0.00713   0.0315   0.0086   0.9687
   8.500   0.7576   0.01359   0.00756   0.0321   0.0079   0.9708
   8.750   0.7784   0.01403   0.00804   0.0331   0.0072   0.9736
   9.000   0.7985   0.01448   0.00854   0.0343   0.0068   0.9762
   9.250   0.8238   0.01492   0.00904   0.0342   0.0064   0.9772
   9.500   0.8489   0.01538   0.00955   0.0342   0.0060   0.9783
   9.750   0.8736   0.01587   0.01009   0.0342   0.0056   0.9796
  10.000   0.8975   0.01638   0.01064   0.0343   0.0053   0.9811
  10.250   0.9196   0.01697   0.01131   0.0348   0.0050   0.9828
  10.500   0.9367   0.01769   0.01211   0.0363   0.0047   0.9856
  10.750   0.9609   0.01835   0.01286   0.0363   0.0046   0.9864
  11.000   0.9850   0.01903   0.01363   0.0361   0.0044   0.9870
  11.250   1.0081   0.01974   0.01444   0.0362   0.0043   0.9877
  11.500   1.0299   0.02051   0.01530   0.0365   0.0041   0.9886
  11.750   1.0505   0.02131   0.01621   0.0369   0.0040   0.9896
  12.000   1.0701   0.02216   0.01716   0.0375   0.0039   0.9909
  12.250   1.0883   0.02302   0.01814   0.0382   0.0037   0.9923
  12.500   1.1044   0.02393   0.01915   0.0394   0.0036   0.9939
  12.750   1.1204   0.02490   0.02023   0.0404   0.0035   0.9950
  13.000   1.1367   0.02597   0.02142   0.0412   0.0034   0.9957
  13.250   1.1515   0.02713   0.02270   0.0420   0.0033   0.9966
  13.500   1.1632   0.02849   0.02418   0.0432   0.0032   0.9976
  13.750   1.1708   0.03012   0.02596   0.0448   0.0031   0.9987
  14.000   1.1725   0.03227   0.02831   0.0469   0.0030   0.9997
  14.250   1.1692   0.03386   0.03004   0.0503   0.0030   1.0000
  14.500   1.1629   0.03534   0.03165   0.0542   0.0030   1.0000
  14.750   1.1568   0.03696   0.03339   0.0577   0.0029   1.0000
  15.000   1.1483   0.03895   0.03551   0.0610   0.0029   1.0000
  15.250   1.1398   0.04114   0.03785   0.0637   0.0029   1.0000
  15.500   1.1288   0.04380   0.04065   0.0659   0.0029   1.0000
  15.750   1.1147   0.04706   0.04407   0.0676   0.0029   1.0000
  16.000   1.0984   0.05103   0.04819   0.0682   0.0029   1.0000
  16.250   1.0776   0.05623   0.05356   0.0674   0.0029   1.0000
  16.500   1.0482   0.06393   0.06146   0.0640   0.0029   1.0000
  16.750   0.9318   0.09520   0.09317   0.0454   0.0030   1.0000
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