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NACA 63 (naca633418-il) Xfoil prediction polar at RE=50,000 Ncrit=5


Details Polar file
Airfoil: NACA 63 (naca633418-il)
Reynolds number: 50,000
Max Cl/Cd: 16.59 at α=11.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-naca633418-il-50000-n5.txt
Download as CSV file: xf-naca633418-il-50000-n5.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 =     0.050 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -13.750  -0.5081   0.10500   0.09710  -0.0556   1.0000   0.0809
 -13.500  -0.5741   0.08837   0.08036  -0.0655   1.0000   0.0798
 -13.250  -0.6276   0.07726   0.06903  -0.0720   1.0000   0.0789
 -13.000  -0.6565   0.07084   0.06243  -0.0749   1.0000   0.0792
 -12.750  -0.6754   0.06608   0.05749  -0.0765   1.0000   0.0799
 -12.500  -0.6897   0.06209   0.05330  -0.0773   1.0000   0.0810
 -12.250  -0.7011   0.05863   0.04962  -0.0774   1.0000   0.0822
 -12.000  -0.7104   0.05557   0.04633  -0.0770   1.0000   0.0836
 -11.750  -0.7139   0.05306   0.04365  -0.0761   1.0000   0.0853
 -11.500  -0.7010   0.05170   0.04238  -0.0750   1.0000   0.0880
 -11.250  -0.6975   0.05012   0.04076  -0.0736   1.0000   0.0907
 -11.000  -0.6982   0.04854   0.03908  -0.0716   1.0000   0.0934
 -10.750  -0.7018   0.04717   0.03755  -0.0690   1.0000   0.0958
 -10.500  -0.6982   0.04630   0.03677  -0.0662   1.0000   0.0987
 -10.250  -0.7045   0.04569   0.03621  -0.0625   1.0000   0.1010
 -10.000  -0.7169   0.04515   0.03566  -0.0580   1.0000   0.1031
  -9.750  -0.7078   0.04409   0.03442  -0.0567   0.9960   0.1079
  -9.500  -0.6750   0.04280   0.03319  -0.0586   0.9877   0.1154
  -9.250  -0.6452   0.04145   0.03172  -0.0604   0.9789   0.1246
  -9.000  -0.6187   0.04012   0.03038  -0.0622   0.9698   0.1353
  -8.750  -0.5971   0.03877   0.02910  -0.0634   0.9595   0.1468
  -8.500  -0.5761   0.03733   0.02771  -0.0648   0.9499   0.1616
  -8.250  -0.5568   0.03581   0.02626  -0.0662   0.9401   0.1799
  -8.000  -0.5423   0.03433   0.02492  -0.0667   0.9294   0.2026
  -7.750  -0.5235   0.03273   0.02357  -0.0681   0.9210   0.2363
  -7.500  -0.5154   0.03171   0.02283  -0.0669   0.9094   0.2725
  -7.250  -0.4931   0.03110   0.02258  -0.0670   0.9021   0.3261
  -7.000  -0.4781   0.03110   0.02271  -0.0653   0.8915   0.3700
  -6.750  -0.4463   0.03145   0.02305  -0.0656   0.8855   0.4124
  -6.500  -0.4333   0.03168   0.02317  -0.0634   0.8748   0.4398
  -6.250  -0.4026   0.03222   0.02356  -0.0633   0.8687   0.4672
  -6.000  -0.3884   0.03250   0.02371  -0.0612   0.8588   0.4882
  -5.750  -0.3592   0.03313   0.02419  -0.0605   0.8524   0.5078
  -5.500  -0.3381   0.03361   0.02455  -0.0590   0.8447   0.5247
  -5.250  -0.3102   0.03451   0.02535  -0.0574   0.8374   0.5377
  -5.000  -0.2763   0.03507   0.02576  -0.0570   0.8325   0.5510
  -4.500  -0.2417   0.03505   0.02547  -0.0543   0.8166   0.5774
  -4.250  -0.2099   0.03554   0.02585  -0.0536   0.8114   0.5848
  -4.000  -0.2010   0.03527   0.02546  -0.0518   0.8019   0.5970
  -3.750  -0.1688   0.03552   0.02561  -0.0514   0.7971   0.6037
  -3.500  -0.1583   0.03522   0.02518  -0.0500   0.7888   0.6151
  -3.250  -0.1338   0.03543   0.02533  -0.0488   0.7823   0.6210
  -3.000  -0.1082   0.03494   0.02466  -0.0493   0.7776   0.6317
  -2.750  -0.0958   0.03524   0.02494  -0.0469   0.7689   0.6373
  -2.500  -0.0728   0.03515   0.02476  -0.0463   0.7629   0.6451
  -2.250  -0.0443   0.03478   0.02424  -0.0469   0.7589   0.6534
  -2.000  -0.0361   0.03511   0.02457  -0.0442   0.7496   0.6593
  -1.750  -0.0129   0.03480   0.02413  -0.0445   0.7441   0.6684
  -1.500   0.0178   0.03468   0.02395  -0.0446   0.7405   0.6739
  -1.250   0.0232   0.03505   0.02431  -0.0420   0.7310   0.6805
  -1.000   0.0481   0.03481   0.02397  -0.0424   0.7259   0.6888
  -0.750   0.0785   0.03473   0.02384  -0.0424   0.7225   0.6940
  -0.500   0.0824   0.03519   0.02430  -0.0399   0.7128   0.7012
  -0.250   0.1081   0.03509   0.02414  -0.0402   0.7080   0.7084
   0.000   0.1382   0.03500   0.02401  -0.0403   0.7047   0.7142
   0.250   0.1412   0.03560   0.02462  -0.0381   0.6951   0.7221
   0.500   0.1665   0.03563   0.02462  -0.0379   0.6903   0.7282
   0.750   0.1965   0.03554   0.02450  -0.0381   0.6871   0.7346
   1.000   0.1990   0.03632   0.02528  -0.0363   0.6774   0.7432
   1.250   0.2222   0.03646   0.02543  -0.0355   0.6727   0.7489
   1.500   0.2535   0.03636   0.02531  -0.0361   0.6695   0.7562
   1.750   0.2532   0.03738   0.02637  -0.0337   0.6597   0.7638
   2.000   0.2766   0.03756   0.02657  -0.0332   0.6550   0.7708
   2.250   0.3100   0.03747   0.02646  -0.0343   0.6519   0.7791
   2.500   0.3026   0.03875   0.02781  -0.0307   0.6415   0.7863
   2.750   0.3294   0.03892   0.02799  -0.0310   0.6370   0.7951
   3.000   0.3607   0.03882   0.02793  -0.0311   0.6342   0.8022
   3.250   0.3521   0.04043   0.02959  -0.0284   0.6229   0.8119
   3.500   0.3780   0.04052   0.02973  -0.0280   0.6188   0.8200
   3.750   0.4117   0.04035   0.02959  -0.0285   0.6161   0.8292
   4.000   0.4004   0.04225   0.03158  -0.0255   0.6041   0.8393
   4.250   0.4299   0.04226   0.03164  -0.0257   0.6004   0.8494
   4.750   0.4504   0.04409   0.03364  -0.0230   0.5852   0.8722
   5.000   0.4818   0.04391   0.03354  -0.0231   0.5819   0.8841
   5.250   0.4777   0.04576   0.03548  -0.0213   0.5706   0.8996
   5.500   0.5065   0.04580   0.03562  -0.0215   0.5661   0.9151
   5.750   0.5456   0.04539   0.03532  -0.0225   0.5633   0.9313
   6.250   0.5950   0.04719   0.03738  -0.0257   0.5468   1.0000
   6.500   0.5953   0.04959   0.03983  -0.0261   0.5340   1.0000
   6.750   0.6354   0.04928   0.03960  -0.0275   0.5301   1.0000
   7.000   0.6382   0.05162   0.04197  -0.0278   0.5175   1.0000
   7.250   0.6774   0.05123   0.04167  -0.0289   0.5132   1.0000
   7.500   0.6806   0.05354   0.04403  -0.0291   0.5004   1.0000
   7.750   0.7205   0.05287   0.04345  -0.0298   0.4960   1.0000
   8.000   0.7233   0.05517   0.04581  -0.0297   0.4826   1.0000
   8.250   0.7650   0.05407   0.04483  -0.0300   0.4784   1.0000
   8.500   0.7671   0.05637   0.04720  -0.0298   0.4644   1.0000
   9.000   0.8137   0.05688   0.04792  -0.0294   0.4460   1.0000
   9.250   0.8188   0.05888   0.05000  -0.0291   0.4322   1.0000
   9.500   0.8608   0.05684   0.04809  -0.0284   0.4269   1.0000
   9.750   0.8693   0.05825   0.04960  -0.0279   0.4128   1.0000
  10.000   0.8775   0.05972   0.05118  -0.0274   0.3983   1.0000
  10.500   0.9094   0.06062   0.05229  -0.0260   0.3708   1.0000
  10.750   0.9335   0.05994   0.05173  -0.0250   0.3571   1.0000
  11.000   0.9521   0.05990   0.05177  -0.0242   0.3411   1.0000
  11.250   0.9672   0.06032   0.05225  -0.0234   0.3232   1.0000
  11.500   0.9835   0.06062   0.05258  -0.0226   0.3039   1.0000
  11.750   1.0031   0.06046   0.05239  -0.0215   0.2831   1.0000
  12.000   1.0158   0.06130   0.05314  -0.0208   0.2614   1.0000
  12.250   1.0217   0.06315   0.05491  -0.0203   0.2398   1.0000
  12.500   1.0280   0.06496   0.05658  -0.0199   0.2195   1.0000
  12.750   1.0322   0.06715   0.05862  -0.0196   0.2012   1.0000
  13.000   1.0343   0.06979   0.06112  -0.0195   0.1847   1.0000
  13.250   1.0363   0.07255   0.06380  -0.0196   0.1702   1.0000
  13.500   1.0378   0.07555   0.06678  -0.0199   0.1572   1.0000
  13.750   1.0403   0.07853   0.06974  -0.0202   0.1458   1.0000
  14.000   1.0442   0.08133   0.07250  -0.0205   0.1361   1.0000
  14.250   1.0492   0.08398   0.07510  -0.0208   0.1276   1.0000
  14.500   1.0528   0.08712   0.07835  -0.0214   0.1199   1.0000
  14.750   1.0607   0.08937   0.08048  -0.0216   0.1133   1.0000
  15.000   1.0627   0.09294   0.08426  -0.0224   0.1075   1.0000
  15.250   1.0701   0.09545   0.08676  -0.0228   0.1022   1.0000
  15.500   1.0740   0.09872   0.09015  -0.0236   0.0977   1.0000
  15.750   1.0749   0.10257   0.09420  -0.0248   0.0936   1.0000
  16.000   1.0847   0.10476   0.09637  -0.0252   0.0898   1.0000
  16.250   1.0844   0.10891   0.10068  -0.0266   0.0868   1.0000
  16.500   1.0747   0.11484   0.10691  -0.0293   0.0843   1.0000
  16.750   1.0672   0.12046   0.11273  -0.0319   0.0820   1.0000
  17.000   1.0689   0.12431   0.11665  -0.0335   0.0796   1.0000
  17.250   1.0732   0.12766   0.12003  -0.0349   0.0774   1.0000
  17.500   1.0370   0.13977   0.13249  -0.0420   0.0768   1.0000
  17.750   0.9660   0.16258   0.15558  -0.0559   0.0765   1.0000
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