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NACA 64-110 AIRFOIL (n64110-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: NACA 64-110 AIRFOIL (n64110-il)
Reynolds number: 1,000,000
Max Cl/Cd: 68.15 at α=7.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-n64110-il-1000000-n5.txt
Download as CSV file: xf-n64110-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NACA 64-110 AIRFOIL                             
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -15.500  -1.1001   0.06646   0.06441  -0.0235   1.0000   0.0042
 -15.250  -1.1346   0.05664   0.05438  -0.0302   1.0000   0.0042
 -15.000  -1.1592   0.04973   0.04729  -0.0341   1.0000   0.0042
 -14.750  -1.1725   0.04509   0.04249  -0.0361   1.0000   0.0042
 -14.500  -1.1735   0.04231   0.03963  -0.0370   1.0000   0.0043
 -14.250  -1.1887   0.03820   0.03531  -0.0375   1.0000   0.0043
 -14.000  -1.1957   0.03532   0.03227  -0.0372   1.0000   0.0043
 -13.750  -1.1910   0.03374   0.03061  -0.0365   1.0000   0.0045
 -13.500  -1.1928   0.03174   0.02848  -0.0352   1.0000   0.0045
 -13.250  -1.1909   0.03023   0.02685  -0.0335   1.0000   0.0046
 -13.000  -1.1889   0.02886   0.02536  -0.0312   1.0000   0.0047
 -12.750  -1.1817   0.02755   0.02392  -0.0294   1.0000   0.0048
 -12.500  -1.1700   0.02631   0.02254  -0.0281   1.0000   0.0050
 -12.250  -1.1560   0.02516   0.02126  -0.0270   1.0000   0.0051
 -12.000  -1.1399   0.02415   0.02013  -0.0261   1.0000   0.0053
 -11.750  -1.1241   0.02297   0.01881  -0.0252   1.0000   0.0054
 -11.500  -1.1059   0.02201   0.01772  -0.0244   1.0000   0.0056
 -11.250  -1.0867   0.02112   0.01671  -0.0237   1.0000   0.0057
 -11.000  -1.0673   0.02017   0.01565  -0.0230   1.0000   0.0058
 -10.750  -1.0476   0.01922   0.01459  -0.0223   1.0000   0.0061
 -10.500  -1.0249   0.01870   0.01404  -0.0220   1.0000   0.0064
 -10.250  -1.0016   0.01823   0.01352  -0.0217   1.0000   0.0067
 -10.000  -0.9782   0.01775   0.01298  -0.0213   1.0000   0.0069
  -9.750  -0.9549   0.01722   0.01240  -0.0210   1.0000   0.0073
  -9.500  -0.9315   0.01666   0.01177  -0.0206   1.0000   0.0076
  -9.250  -0.9081   0.01608   0.01111  -0.0202   1.0000   0.0079
  -9.000  -0.8844   0.01553   0.01049  -0.0199   1.0000   0.0082
  -8.750  -0.8603   0.01502   0.00991  -0.0195   1.0000   0.0083
  -8.500  -0.8360   0.01457   0.00938  -0.0192   1.0000   0.0085
  -8.250  -0.8053   0.01360   0.00832  -0.0206   0.9786   0.0091
  -7.750  -0.7442   0.01287   0.00751  -0.0225   0.9463   0.0101
  -7.500  -0.7192   0.01253   0.00710  -0.0221   0.9302   0.0106
  -7.250  -0.6949   0.01217   0.00664  -0.0216   0.9156   0.0110
  -7.000  -0.6704   0.01182   0.00620  -0.0211   0.9022   0.0113
  -6.750  -0.6454   0.01150   0.00580  -0.0207   0.8896   0.0117
  -6.250  -0.5947   0.01085   0.00498  -0.0200   0.8659   0.0124
  -6.000  -0.5692   0.01044   0.00447  -0.0197   0.8550   0.0131
  -5.750  -0.5432   0.01014   0.00412  -0.0195   0.8446   0.0137
  -5.250  -0.4900   0.00966   0.00353  -0.0192   0.8242   0.0152
  -5.000  -0.4631   0.00946   0.00327  -0.0192   0.8149   0.0161
  -4.500  -0.4089   0.00903   0.00275  -0.0191   0.7963   0.0189
  -4.250  -0.3816   0.00884   0.00254  -0.0191   0.7876   0.0213
  -4.000  -0.3541   0.00869   0.00235  -0.0191   0.7781   0.0234
  -3.750  -0.3265   0.00855   0.00216  -0.0191   0.7690   0.0256
  -3.500  -0.2990   0.00839   0.00199  -0.0191   0.7602   0.0300
  -3.250  -0.2712   0.00826   0.00184  -0.0192   0.7514   0.0335
  -3.000  -0.2435   0.00811   0.00168  -0.0192   0.7432   0.0421
  -2.750  -0.2161   0.00789   0.00153  -0.0193   0.7346   0.0659
  -2.500  -0.1891   0.00751   0.00136  -0.0194   0.7262   0.1263
  -2.250  -0.1624   0.00709   0.00118  -0.0195   0.7175   0.2061
  -2.000  -0.1361   0.00650   0.00097  -0.0196   0.7089   0.3235
  -1.750  -0.1096   0.00600   0.00083  -0.0198   0.7011   0.4335
  -1.500  -0.0819   0.00579   0.00077  -0.0199   0.6932   0.4875
  -1.250  -0.0544   0.00560   0.00074  -0.0199   0.6860   0.5449
  -1.000  -0.0267   0.00544   0.00073  -0.0200   0.6783   0.5928
  -0.750   0.0015   0.00538   0.00072  -0.0201   0.6709   0.6188
  -0.500   0.0299   0.00537   0.00071  -0.0202   0.6629   0.6302
  -0.250   0.0583   0.00536   0.00071  -0.0203   0.6557   0.6398
   0.000   0.0869   0.00537   0.00071  -0.0205   0.6484   0.6474
   0.250   0.1154   0.00537   0.00071  -0.0206   0.6416   0.6547
   0.500   0.1438   0.00539   0.00073  -0.0207   0.6327   0.6621
   0.750   0.1722   0.00541   0.00075  -0.0209   0.6226   0.6704
   1.000   0.2004   0.00545   0.00077  -0.0209   0.6068   0.6782
   1.250   0.2283   0.00554   0.00080  -0.0210   0.5821   0.6863
   1.500   0.2556   0.00569   0.00084  -0.0209   0.5444   0.6938
   1.750   0.2830   0.00587   0.00089  -0.0209   0.5018   0.7020
   2.000   0.3098   0.00613   0.00098  -0.0209   0.4454   0.7100
   2.500   0.3597   0.00735   0.00142  -0.0206   0.2277   0.7277
   2.750   0.3850   0.00792   0.00167  -0.0204   0.1363   0.7363
   3.000   0.4113   0.00831   0.00189  -0.0204   0.0823   0.7452
   3.250   0.4379   0.00861   0.00208  -0.0203   0.0501   0.7536
   3.750   0.4924   0.00898   0.00243  -0.0203   0.0324   0.7718
   4.000   0.5194   0.00917   0.00264  -0.0202   0.0272   0.7811
   4.250   0.5467   0.00932   0.00283  -0.0202   0.0248   0.7908
   4.500   0.5737   0.00949   0.00303  -0.0201   0.0220   0.8002
   4.750   0.6003   0.00973   0.00328  -0.0200   0.0185   0.8095
   5.000   0.6271   0.00992   0.00353  -0.0199   0.0172   0.8198
   5.250   0.6536   0.01013   0.00378  -0.0197   0.0158   0.8299
   5.500   0.6798   0.01038   0.00406  -0.0195   0.0145   0.8403
   5.750   0.7055   0.01069   0.00442  -0.0192   0.0133   0.8513
   6.000   0.7309   0.01100   0.00482  -0.0189   0.0128   0.8632
   6.250   0.7562   0.01128   0.00517  -0.0185   0.0124   0.8755
   6.500   0.7810   0.01157   0.00554  -0.0180   0.0120   0.8888
   6.750   0.8054   0.01186   0.00591  -0.0175   0.0116   0.9028
   7.000   0.8292   0.01218   0.00631  -0.0168   0.0111   0.9182
   7.250   0.8523   0.01251   0.00671  -0.0160   0.0107   0.9354
   7.500   0.8757   0.01285   0.00713  -0.0153   0.0104   0.9578
   7.750   0.9059   0.01334   0.00767  -0.0162   0.0100   1.0000
   8.000   0.9297   0.01392   0.00830  -0.0158   0.0095   1.0000
   8.250   0.9519   0.01474   0.00920  -0.0152   0.0090   1.0000
   8.500   0.9760   0.01524   0.00977  -0.0149   0.0089   1.0000
   8.750   1.0000   0.01575   0.01033  -0.0145   0.0088   1.0000
   9.000   1.0234   0.01631   0.01096  -0.0141   0.0086   1.0000
   9.250   1.0465   0.01689   0.01161  -0.0136   0.0083   1.0000
   9.500   1.0693   0.01749   0.01228  -0.0131   0.0081   1.0000
   9.750   1.0922   0.01802   0.01287  -0.0127   0.0078   1.0000
  10.000   1.1151   0.01851   0.01343  -0.0122   0.0074   1.0000
  10.250   1.1374   0.01906   0.01403  -0.0117   0.0072   1.0000
  10.500   1.1595   0.01959   0.01461  -0.0112   0.0069   1.0000
  10.750   1.1807   0.02019   0.01525  -0.0106   0.0067   1.0000
  11.000   1.1998   0.02103   0.01617  -0.0098   0.0064   1.0000
  11.250   1.2149   0.02230   0.01757  -0.0085   0.0061   1.0000
  11.500   1.2332   0.02309   0.01846  -0.0076   0.0061   1.0000
  11.750   1.2509   0.02387   0.01934  -0.0066   0.0059   1.0000
  12.000   1.2661   0.02486   0.02046  -0.0053   0.0058   1.0000
  12.250   1.2789   0.02593   0.02166  -0.0038   0.0057   1.0000
  12.500   1.2894   0.02684   0.02267  -0.0019   0.0055   1.0000
  12.750   1.2959   0.02799   0.02394   0.0004   0.0054   1.0000
  13.000   1.3028   0.02913   0.02519   0.0023   0.0052   1.0000
  13.250   1.3098   0.03032   0.02647   0.0040   0.0051   1.0000
  13.500   1.3142   0.03179   0.02806   0.0056   0.0050   1.0000
  13.750   1.3205   0.03318   0.02954   0.0067   0.0048   1.0000
  14.000   1.3240   0.03490   0.03137   0.0078   0.0048   1.0000
  14.250   1.3254   0.03694   0.03352   0.0086   0.0047   1.0000
  14.500   1.3380   0.03790   0.03449   0.0089   0.0045   1.0000
  14.750   1.3342   0.04067   0.03741   0.0093   0.0044   1.0000
  15.000   1.3342   0.04319   0.04003   0.0093   0.0044   1.0000
  15.250   1.3334   0.04595   0.04289   0.0089   0.0042   1.0000
  15.500   1.3222   0.05020   0.04730   0.0079   0.0042   1.0000
  15.750   1.3118   0.05466   0.05190   0.0063   0.0041   1.0000
  16.000   1.2928   0.06074   0.05816   0.0035   0.0041   1.0000
  16.250   1.2722   0.06768   0.06527  -0.0002   0.0041   1.0000
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