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NACA 63 (naca633418-il) Xfoil prediction polar at RE=100,000 Ncrit=9


Details Polar file
Airfoil: NACA 63 (naca633418-il)
Reynolds number: 100,000
Max Cl/Cd: 45.41 at α=9.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-naca633418-il-100000.txt
Download as CSV file: xf-naca633418-il-100000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NACA 63                                         
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.100 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -13.750  -0.6475   0.08257   0.07691  -0.0727   1.0000   0.0845
 -13.500  -0.6710   0.07608   0.07033  -0.0755   1.0000   0.0838
 -13.250  -0.7021   0.06992   0.06404  -0.0781   1.0000   0.0832
 -13.000  -0.7311   0.06477   0.05873  -0.0795   1.0000   0.0828
 -12.750  -0.7575   0.06047   0.05427  -0.0799   1.0000   0.0825
 -12.500  -0.7822   0.05699   0.05062  -0.0792   1.0000   0.0825
 -12.250  -0.8049   0.05422   0.04770  -0.0772   1.0000   0.0825
 -12.000  -0.8294   0.05232   0.04570  -0.0734   1.0000   0.0826
 -11.750  -0.8558   0.05110   0.04441  -0.0680   1.0000   0.0827
 -11.500  -0.8841   0.05036   0.04360  -0.0618   1.0000   0.0827
 -11.250  -0.9084   0.04943   0.04255  -0.0562   1.0000   0.0829
 -11.000  -0.9268   0.04814   0.04107  -0.0515   1.0000   0.0833
 -10.750  -0.9397   0.04666   0.03936  -0.0475   1.0000   0.0839
 -10.500  -0.9329   0.04429   0.03657  -0.0472   0.9962   0.0851
 -10.250  -0.8983   0.04141   0.03369  -0.0500   0.9910   0.0877
 -10.000  -0.8641   0.03954   0.03168  -0.0529   0.9844   0.0914
  -9.750  -0.8347   0.03770   0.02944  -0.0550   0.9771   0.0955
  -9.500  -0.7977   0.03556   0.02732  -0.0576   0.9716   0.1000
  -9.250  -0.7630   0.03418   0.02583  -0.0599   0.9652   0.1060
  -9.000  -0.7286   0.03257   0.02416  -0.0618   0.9586   0.1122
  -8.750  -0.6870   0.03126   0.02280  -0.0651   0.9540   0.1214
  -8.500  -0.6605   0.03008   0.02176  -0.0655   0.9457   0.1299
  -8.250  -0.6228   0.02878   0.02055  -0.0680   0.9403   0.1432
  -8.000  -0.5946   0.02769   0.01958  -0.0690   0.9332   0.1586
  -7.750  -0.5685   0.02656   0.01861  -0.0699   0.9255   0.1805
  -7.500  -0.5349   0.02489   0.01734  -0.0727   0.9208   0.2218
  -7.250  -0.5303   0.02379   0.01664  -0.0703   0.9093   0.2693
  -7.000  -0.5020   0.02269   0.01628  -0.0719   0.9039   0.3763
  -6.750  -0.4882   0.02303   0.01672  -0.0696   0.8935   0.4270
  -6.500  -0.4506   0.02353   0.01712  -0.0709   0.8881   0.4701
  -6.250  -0.4248   0.02434   0.01792  -0.0698   0.8804   0.4933
  -6.000  -0.3951   0.02520   0.01875  -0.0690   0.8732   0.5133
  -5.750  -0.3547   0.02612   0.01962  -0.0696   0.8691   0.5320
  -5.500  -0.3385   0.02684   0.02028  -0.0671   0.8596   0.5460
  -5.250  -0.3059   0.02751   0.02086  -0.0669   0.8538   0.5616
  -5.000  -0.2651   0.02865   0.02198  -0.0666   0.8502   0.5734
  -4.750  -0.2540   0.02947   0.02279  -0.0632   0.8401   0.5832
  -4.500  -0.2227   0.02980   0.02300  -0.0630   0.8348   0.5974
  -4.250  -0.1810   0.03096   0.02414  -0.0621   0.8316   0.6046
  -4.000  -0.1792   0.03107   0.02420  -0.0591   0.8205   0.6165
  -3.750  -0.1431   0.03180   0.02489  -0.0582   0.8163   0.6234
  -3.500  -0.1282   0.03166   0.02466  -0.0570   0.8089   0.6349
  -3.250  -0.1072   0.03221   0.02520  -0.0548   0.8015   0.6408
  -3.000  -0.0788   0.03166   0.02450  -0.0558   0.7971   0.6524
  -2.750  -0.0653   0.03231   0.02517  -0.0528   0.7894   0.6574
  -2.500  -0.0477   0.03190   0.02464  -0.0529   0.7822   0.6689
  -2.250  -0.0142   0.03194   0.02464  -0.0524   0.7787   0.6736
  -2.000  -0.0075   0.03240   0.02511  -0.0496   0.7698   0.6800
  -1.750   0.0132   0.03209   0.02471  -0.0499   0.7637   0.6895
  -1.500   0.0455   0.03205   0.02463  -0.0496   0.7605   0.6943
  -1.250   0.0500   0.03246   0.02502  -0.0475   0.7512   0.7022
  -1.000   0.0727   0.03233   0.02484  -0.0473   0.7454   0.7091
  -0.750   0.1045   0.03220   0.02468  -0.0472   0.7423   0.7145
  -0.500   0.1079   0.03276   0.02521  -0.0459   0.7332   0.7233
  -0.250   0.1286   0.03285   0.02530  -0.0448   0.7274   0.7284
   0.000   0.1621   0.03261   0.02503  -0.0451   0.7243   0.7344
   0.250   0.2040   0.03207   0.02438  -0.0479   0.7222   0.7430
   0.500   0.1818   0.03371   0.02613  -0.0423   0.7095   0.7478
   0.750   0.2169   0.03342   0.02581  -0.0430   0.7065   0.7543
   1.000   0.2596   0.03290   0.02522  -0.0453   0.7045   0.7620
   1.250   0.2316   0.03493   0.02736  -0.0396   0.6914   0.7677
   1.500   0.2703   0.03458   0.02698  -0.0410   0.6886   0.7750
   1.750   0.3117   0.03406   0.02644  -0.0424   0.6867   0.7817
   2.000   0.2750   0.03654   0.02900  -0.0363   0.6729   0.7889
   2.250   0.3237   0.03603   0.02845  -0.0393   0.6706   0.7967
   2.500   0.3618   0.03548   0.02794  -0.0394   0.6689   0.8026
   2.750   0.3238   0.03830   0.03081  -0.0341   0.6546   0.8119
   3.000   0.3652   0.03772   0.03025  -0.0350   0.6524   0.8186
   3.250   0.4096   0.03715   0.02971  -0.0363   0.6505   0.8260
   3.500   0.3720   0.04012   0.03273  -0.0312   0.6364   0.8353
   3.750   0.4139   0.03943   0.03207  -0.0319   0.6342   0.8437
   4.000   0.3860   0.04227   0.03497  -0.0280   0.6213   0.8536
   4.250   0.4237   0.04179   0.03452  -0.0285   0.6180   0.8628
   4.500   0.4652   0.04091   0.03369  -0.0287   0.6161   0.8714
   4.750   0.4377   0.04388   0.03672  -0.0253   0.6023   0.8841
   5.000   0.4764   0.04311   0.03599  -0.0252   0.5996   0.8950
   5.250   0.4566   0.04567   0.03862  -0.0223   0.5870   0.9091
   5.500   0.4936   0.04492   0.03794  -0.0222   0.5833   0.9226
   5.750   0.5303   0.04434   0.03743  -0.0223   0.5796   0.9378
   6.000   0.5331   0.04639   0.03960  -0.0226   0.5670   0.9587
   6.250   0.5640   0.04765   0.04098  -0.0259   0.5571   0.9881
   6.500   0.6023   0.04754   0.04092  -0.0280   0.5504   1.0000
   6.750   0.6615   0.04584   0.03929  -0.0304   0.5478   1.0000
   7.000   0.6649   0.04837   0.04186  -0.0315   0.5338   1.0000
   7.250   0.7254   0.04620   0.03978  -0.0334   0.5313   1.0000
   7.500   0.7940   0.04293   0.03660  -0.0352   0.5303   1.0000
   7.750   0.8747   0.03861   0.03239  -0.0375   0.5303   1.0000
   8.000   0.9832   0.03305   0.02691  -0.0429   0.5293   1.0000
   8.250   0.9872   0.03405   0.02800  -0.0414   0.5152   1.0000
   8.500   1.0341   0.03223   0.02626  -0.0426   0.5041   1.0000
   8.750   1.1154   0.02838   0.02236  -0.0467   0.4931   1.0000
   9.000   1.1515   0.02736   0.02135  -0.0473   0.4786   1.0000
   9.250   1.1724   0.02710   0.02115  -0.0464   0.4628   1.0000
   9.500   1.1926   0.02681   0.02089  -0.0452   0.4458   1.0000
   9.750   1.2083   0.02661   0.02068  -0.0433   0.4275   1.0000
  10.000   1.2079   0.02725   0.02136  -0.0401   0.4081   1.0000
  10.250   1.2065   0.02814   0.02226  -0.0371   0.3860   1.0000
  10.500   1.2091   0.02894   0.02296  -0.0346   0.3600   1.0000
  10.750   1.2043   0.03045   0.02435  -0.0320   0.3312   1.0000
  11.000   1.1972   0.03238   0.02609  -0.0296   0.3000   1.0000
  11.250   1.1878   0.03477   0.02823  -0.0274   0.2683   1.0000
  11.500   1.1775   0.03749   0.03071  -0.0255   0.2385   1.0000
  11.750   1.1681   0.04036   0.03330  -0.0239   0.2122   1.0000
  12.000   1.1614   0.04321   0.03593  -0.0226   0.1893   1.0000
  12.250   1.1595   0.04576   0.03820  -0.0215   0.1704   1.0000
  12.500   1.1620   0.04807   0.04032  -0.0206   0.1542   1.0000
  12.750   1.1687   0.05013   0.04223  -0.0199   0.1408   1.0000
  13.000   1.1752   0.05228   0.04441  -0.0193   0.1300   1.0000
  13.250   1.1870   0.05407   0.04615  -0.0187   0.1207   1.0000
  13.500   1.2065   0.05534   0.04721  -0.0181   0.1122   1.0000
  13.750   1.2144   0.05752   0.04955  -0.0177   0.1060   1.0000
  14.000   1.2400   0.05861   0.05046  -0.0172   0.0994   1.0000
  14.250   1.2467   0.06100   0.05307  -0.0169   0.0951   1.0000
  14.500   1.2680   0.06239   0.05435  -0.0166   0.0903   1.0000
  14.750   1.2849   0.06456   0.05663  -0.0163   0.0866   1.0000
  15.000   1.2909   0.06725   0.05954  -0.0161   0.0838   1.0000
  15.250   1.3009   0.06964   0.06204  -0.0160   0.0810   1.0000
  15.500   1.3307   0.07142   0.06370  -0.0159   0.0774   1.0000
  15.750   1.3199   0.07529   0.06791  -0.0159   0.0763   1.0000
  16.000   1.3102   0.07944   0.07237  -0.0162   0.0752   1.0000
  16.250   1.2996   0.08389   0.07710  -0.0168   0.0742   1.0000
  16.500   1.2867   0.08872   0.08220  -0.0178   0.0734   1.0000
  16.750   1.2713   0.09401   0.08775  -0.0192   0.0726   1.0000
  17.000   1.2515   0.10003   0.09403  -0.0213   0.0722   1.0000
  17.250   1.2210   0.10782   0.10214  -0.0246   0.0722   1.0000
  17.500   1.1718   0.11917   0.11387  -0.0306   0.0733   1.0000
  17.750   1.1064   0.13511   0.13016  -0.0401   0.0753   1.0000
  18.000   1.0428   0.15377   0.14899  -0.0516   0.0773   1.0000
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