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NACA 64(1)-112 (naca641112-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: NACA 64(1)-112 (naca641112-il)
Reynolds number: 500,000
Max Cl/Cd: 56.01 at α=3.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-naca641112-il-500000-n5.txt
Download as CSV file: xf-naca641112-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NACA 64(1)-112                                  
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.500 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -14.750  -0.9048   0.08288   0.08025  -0.0194   1.0000   0.0102
 -14.500  -0.9684   0.06652   0.06352  -0.0302   1.0000   0.0100
 -14.250  -0.9946   0.05901   0.05579  -0.0345   1.0000   0.0099
 -14.000  -1.0029   0.05473   0.05137  -0.0367   1.0000   0.0101
 -13.750  -1.0198   0.04959   0.04602  -0.0387   1.0000   0.0101
 -13.500  -1.0255   0.04624   0.04253  -0.0396   1.0000   0.0103
 -13.250  -1.0320   0.04298   0.03909  -0.0401   1.0000   0.0104
 -13.000  -1.0355   0.04020   0.03615  -0.0401   1.0000   0.0106
 -12.750  -1.0401   0.03742   0.03317  -0.0396   1.0000   0.0107
 -12.500  -1.0419   0.03501   0.03057  -0.0387   1.0000   0.0109
 -12.250  -1.0406   0.03301   0.02839  -0.0376   1.0000   0.0111
 -12.000  -1.0372   0.03129   0.02649  -0.0362   1.0000   0.0113
 -11.750  -1.0329   0.02963   0.02465  -0.0345   1.0000   0.0114
 -11.500  -1.0263   0.02827   0.02314  -0.0327   1.0000   0.0116
 -11.250  -1.0175   0.02708   0.02179  -0.0308   1.0000   0.0118
 -11.000  -1.0069   0.02565   0.02021  -0.0293   1.0000   0.0121
 -10.750  -0.9929   0.02448   0.01894  -0.0282   1.0000   0.0123
 -10.500  -0.9756   0.02372   0.01813  -0.0273   1.0000   0.0127
 -10.250  -0.9569   0.02305   0.01741  -0.0265   1.0000   0.0130
 -10.000  -0.9382   0.02221   0.01649  -0.0257   1.0000   0.0133
  -9.750  -0.9190   0.02135   0.01554  -0.0249   1.0000   0.0136
  -9.500  -0.8992   0.02053   0.01463  -0.0242   1.0000   0.0140
  -9.250  -0.8791   0.01971   0.01371  -0.0234   1.0000   0.0143
  -9.000  -0.8587   0.01893   0.01285  -0.0227   1.0000   0.0147
  -8.750  -0.8335   0.01822   0.01205  -0.0229   0.9862   0.0151
  -8.500  -0.8007   0.01753   0.01126  -0.0246   0.9664   0.0156
  -8.250  -0.7724   0.01655   0.01021  -0.0256   0.9493   0.0162
  -8.000  -0.7476   0.01597   0.00956  -0.0255   0.9326   0.0167
  -7.750  -0.7250   0.01548   0.00900  -0.0248   0.9171   0.0172
  -7.500  -0.7027   0.01502   0.00846  -0.0240   0.9030   0.0178
  -7.250  -0.6800   0.01458   0.00792  -0.0233   0.8902   0.0184
  -7.000  -0.6568   0.01415   0.00741  -0.0226   0.8783   0.0191
  -6.750  -0.6331   0.01376   0.00692  -0.0221   0.8673   0.0198
  -6.500  -0.6096   0.01331   0.00639  -0.0215   0.8569   0.0208
  -6.250  -0.5853   0.01290   0.00594  -0.0210   0.8466   0.0222
  -6.000  -0.5602   0.01258   0.00557  -0.0207   0.8370   0.0236
  -5.500  -0.5091   0.01199   0.00483  -0.0201   0.8184   0.0266
  -5.250  -0.4837   0.01163   0.00443  -0.0199   0.8098   0.0294
  -5.000  -0.4574   0.01138   0.00413  -0.0197   0.8008   0.0321
  -4.750  -0.4309   0.01114   0.00384  -0.0196   0.7928   0.0351
  -4.500  -0.4045   0.01087   0.00356  -0.0194   0.7842   0.0410
  -4.250  -0.3779   0.01061   0.00330  -0.0194   0.7759   0.0500
  -4.000  -0.3516   0.01031   0.00304  -0.0193   0.7675   0.0691
  -3.750  -0.3256   0.00991   0.00278  -0.0192   0.7595   0.1066
  -3.500  -0.3004   0.00936   0.00247  -0.0191   0.7518   0.1749
  -3.250  -0.2756   0.00866   0.00215  -0.0191   0.7442   0.2738
  -3.000  -0.2512   0.00793   0.00184  -0.0190   0.7367   0.3914
  -2.750  -0.2248   0.00757   0.00173  -0.0190   0.7290   0.4707
  -2.500  -0.1973   0.00744   0.00165  -0.0190   0.7213   0.5044
  -2.250  -0.1696   0.00731   0.00160  -0.0190   0.7137   0.5390
  -2.000  -0.1424   0.00720   0.00160  -0.0189   0.7064   0.5797
  -1.750  -0.1144   0.00715   0.00158  -0.0189   0.6996   0.6027
  -1.500  -0.0860   0.00713   0.00154  -0.0190   0.6926   0.6120
  -1.250  -0.0575   0.00711   0.00150  -0.0191   0.6861   0.6199
  -1.000  -0.0290   0.00710   0.00147  -0.0193   0.6793   0.6272
  -0.750  -0.0004   0.00710   0.00144  -0.0194   0.6728   0.6334
  -0.500   0.0281   0.00709   0.00143  -0.0196   0.6657   0.6397
  -0.250   0.0567   0.00711   0.00141  -0.0197   0.6594   0.6459
   0.000   0.0853   0.00710   0.00142  -0.0199   0.6531   0.6517
   0.250   0.1139   0.00711   0.00142  -0.0200   0.6471   0.6582
   0.500   0.1424   0.00712   0.00144  -0.0202   0.6415   0.6644
   0.750   0.1710   0.00713   0.00147  -0.0203   0.6354   0.6715
   1.250   0.2280   0.00717   0.00155  -0.0206   0.6229   0.6854
   1.500   0.2564   0.00722   0.00159  -0.0207   0.6156   0.6924
   1.750   0.2848   0.00723   0.00165  -0.0208   0.6076   0.6993
   2.000   0.3131   0.00729   0.00171  -0.0209   0.5997   0.7067
   2.250   0.3408   0.00734   0.00176  -0.0208   0.5826   0.7137
   2.500   0.3679   0.00746   0.00179  -0.0207   0.5493   0.7217
   2.750   0.3948   0.00759   0.00187  -0.0206   0.5172   0.7294
   3.000   0.4215   0.00780   0.00195  -0.0204   0.4785   0.7376
   3.250   0.4481   0.00800   0.00208  -0.0203   0.4392   0.7451
   3.500   0.4718   0.00861   0.00233  -0.0199   0.3451   0.7532
   3.750   0.4939   0.00943   0.00274  -0.0194   0.2386   0.7609
   4.000   0.5170   0.01015   0.00312  -0.0190   0.1558   0.7693
   4.250   0.5410   0.01069   0.00347  -0.0186   0.1028   0.7778
   4.500   0.5655   0.01117   0.00381  -0.0183   0.0659   0.7866
   4.750   0.5905   0.01154   0.00412  -0.0180   0.0475   0.7956
   5.000   0.6161   0.01183   0.00442  -0.0177   0.0395   0.8042
   5.250   0.6416   0.01213   0.00474  -0.0174   0.0346   0.8135
   5.500   0.6668   0.01240   0.00507  -0.0170   0.0311   0.8228
   5.750   0.6912   0.01277   0.00546  -0.0166   0.0275   0.8325
   6.000   0.7162   0.01304   0.00580  -0.0162   0.0258   0.8430
   6.250   0.7404   0.01335   0.00619  -0.0157   0.0239   0.8533
   6.500   0.7638   0.01373   0.00660  -0.0150   0.0222   0.8643
   6.750   0.7862   0.01417   0.00712  -0.0142   0.0208   0.8765
   7.000   0.8087   0.01453   0.00756  -0.0134   0.0198   0.8896
   7.250   0.8302   0.01492   0.00804  -0.0123   0.0189   0.9042
   7.750   0.8716   0.01573   0.00900  -0.0101   0.0173   0.9414
   8.000   0.8976   0.01635   0.00968  -0.0103   0.0166   0.9690
   8.250   0.9220   0.01710   0.01049  -0.0104   0.0160   1.0000
   8.500   0.9441   0.01767   0.01111  -0.0098   0.0155   1.0000
   8.750   0.9652   0.01830   0.01181  -0.0091   0.0151   1.0000
   9.000   0.9857   0.01899   0.01255  -0.0083   0.0147   1.0000
   9.250   1.0055   0.01969   0.01331  -0.0075   0.0143   1.0000
   9.500   1.0246   0.02044   0.01414  -0.0066   0.0140   1.0000
   9.750   1.0429   0.02121   0.01497  -0.0056   0.0136   1.0000
  10.000   1.0607   0.02199   0.01581  -0.0046   0.0134   1.0000
  10.250   1.0768   0.02280   0.01668  -0.0033   0.0131   1.0000
  10.500   1.0906   0.02364   0.01757  -0.0017   0.0128   1.0000
  10.750   1.1017   0.02473   0.01873   0.0001   0.0126   1.0000
  11.000   1.1119   0.02599   0.02010   0.0018   0.0123   1.0000
  11.250   1.1240   0.02702   0.02124   0.0033   0.0121   1.0000
  11.500   1.1354   0.02815   0.02250   0.0047   0.0119   1.0000
  11.750   1.1451   0.02948   0.02396   0.0061   0.0117   1.0000
  12.000   1.1538   0.03091   0.02554   0.0074   0.0115   1.0000
  12.250   1.1614   0.03247   0.02723   0.0086   0.0114   1.0000
  12.500   1.1673   0.03420   0.02912   0.0097   0.0112   1.0000
  12.750   1.1730   0.03594   0.03099   0.0107   0.0109   1.0000
  13.000   1.1762   0.03800   0.03320   0.0116   0.0108   1.0000
  13.250   1.1788   0.04011   0.03547   0.0122   0.0106   1.0000
  13.500   1.1807   0.04235   0.03785   0.0126   0.0105   1.0000
  13.750   1.1821   0.04469   0.04031   0.0127   0.0103   1.0000
  14.000   1.1821   0.04730   0.04304   0.0126   0.0102   1.0000
  14.250   1.1814   0.05009   0.04595   0.0122   0.0100   1.0000
  14.500   1.1796   0.05312   0.04909   0.0116   0.0099   1.0000
  14.750   1.1723   0.05706   0.05319   0.0105   0.0099   1.0000
  15.000   1.1710   0.06028   0.05648   0.0093   0.0097   1.0000
  15.250   1.1579   0.06547   0.06186   0.0072   0.0097   1.0000
  15.500   1.1493   0.07025   0.06676   0.0048   0.0096   1.0000
  15.750   1.1336   0.07664   0.07331   0.0015   0.0095   1.0000
  16.000   1.1151   0.08404   0.08090  -0.0028   0.0096   1.0000
  16.250   1.0937   0.09273   0.08978  -0.0081   0.0095   1.0000
  16.500   1.0510   0.10734   0.10469  -0.0174   0.0096   1.0000
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