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NACA 63 (naca633418-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: NACA 63 (naca633418-il)
Reynolds number: 1,000,000
Max Cl/Cd: 120.54 at α=6.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-naca633418-il-1000000.txt
Download as CSV file: xf-naca633418-il-1000000.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 =     1.000 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -19.750  -1.0444   0.09303   0.08947  -0.0509   1.0000   0.0179
 -19.500  -1.0512   0.08859   0.08496  -0.0530   1.0000   0.0181
 -19.250  -1.0557   0.08443   0.08075  -0.0551   1.0000   0.0184
 -19.000  -1.0629   0.08014   0.07638  -0.0569   1.0000   0.0184
 -18.750  -1.0651   0.07646   0.07264  -0.0587   1.0000   0.0186
 -18.500  -1.0689   0.07266   0.06877  -0.0603   1.0000   0.0187
 -18.250  -1.0674   0.06952   0.06557  -0.0618   1.0000   0.0191
 -18.000  -1.0669   0.06637   0.06236  -0.0631   1.0000   0.0193
 -17.750  -1.0692   0.06300   0.05891  -0.0644   1.0000   0.0194
 -17.500  -1.0690   0.05993   0.05577  -0.0655   1.0000   0.0195
 -17.250  -1.0620   0.05762   0.05339  -0.0665   1.0000   0.0201
 -17.000  -1.0580   0.05508   0.05078  -0.0674   1.0000   0.0203
 -16.750  -1.0593   0.05209   0.04772  -0.0682   1.0000   0.0203
 -16.500  -1.0510   0.05006   0.04562  -0.0690   1.0000   0.0206
 -16.250  -1.0539   0.04704   0.04254  -0.0697   1.0000   0.0208
 -16.000  -1.0550   0.04426   0.03971  -0.0703   1.0000   0.0210
 -15.750  -1.0528   0.04185   0.03727  -0.0708   1.0000   0.0214
 -15.500  -1.0498   0.03961   0.03496  -0.0711   1.0000   0.0216
 -15.250  -1.0437   0.03772   0.03304  -0.0713   1.0000   0.0219
 -15.000  -1.0372   0.03596   0.03124  -0.0714   1.0000   0.0222
 -14.750  -1.0299   0.03430   0.02953  -0.0714   1.0000   0.0225
 -14.500  -1.0229   0.03265   0.02783  -0.0712   1.0000   0.0229
 -14.250  -1.0142   0.03118   0.02633  -0.0711   1.0000   0.0233
 -14.000  -1.0055   0.02976   0.02485  -0.0708   1.0000   0.0236
 -13.750  -0.9928   0.02868   0.02373  -0.0705   1.0000   0.0240
 -13.500  -0.9893   0.02696   0.02196  -0.0699   1.0000   0.0243
 -13.250  -0.9863   0.02528   0.02026  -0.0691   1.0000   0.0249
 -13.000  -0.9666   0.02387   0.01883  -0.0706   0.9745   0.0256
 -12.750  -0.9177   0.02258   0.01749  -0.0775   0.9589   0.0265
 -12.500  -0.8677   0.02146   0.01628  -0.0842   0.9382   0.0275
 -12.250  -0.8429   0.02051   0.01515  -0.0859   0.9025   0.0282
 -12.000  -0.8377   0.01943   0.01395  -0.0843   0.8781   0.0292
 -11.750  -0.8281   0.01862   0.01306  -0.0828   0.8621   0.0300
 -11.500  -0.8170   0.01793   0.01228  -0.0814   0.8488   0.0308
 -11.250  -0.8049   0.01726   0.01154  -0.0800   0.8374   0.0316
 -11.000  -0.7918   0.01670   0.01090  -0.0786   0.8278   0.0324
 -10.750  -0.7878   0.01586   0.01000  -0.0760   0.8176   0.0335
 -10.500  -0.7811   0.01530   0.00939  -0.0735   0.8089   0.0346
 -10.250  -0.7639   0.01488   0.00892  -0.0724   0.8010   0.0359
 -10.000  -0.7441   0.01455   0.00853  -0.0716   0.7936   0.0372
  -9.750  -0.7259   0.01403   0.00800  -0.0706   0.7866   0.0393
  -9.500  -0.7048   0.01367   0.00759  -0.0699   0.7799   0.0412
  -9.250  -0.6816   0.01338   0.00726  -0.0695   0.7738   0.0430
  -9.000  -0.6599   0.01293   0.00681  -0.0690   0.7671   0.0459
  -8.750  -0.6361   0.01265   0.00648  -0.0686   0.7606   0.0486
  -8.500  -0.6123   0.01229   0.00612  -0.0683   0.7548   0.0522
  -8.250  -0.5872   0.01200   0.00582  -0.0681   0.7486   0.0562
  -8.000  -0.5628   0.01167   0.00547  -0.0679   0.7424   0.0615
  -7.750  -0.5371   0.01137   0.00518  -0.0678   0.7366   0.0676
  -7.500  -0.5112   0.01107   0.00490  -0.0678   0.7306   0.0751
  -7.250  -0.4855   0.01076   0.00460  -0.0677   0.7247   0.0854
  -7.000  -0.4595   0.01042   0.00432  -0.0677   0.7191   0.0991
  -6.750  -0.4333   0.01005   0.00403  -0.0678   0.7131   0.1171
  -6.500  -0.4070   0.00972   0.00375  -0.0679   0.7072   0.1387
  -6.250  -0.3805   0.00933   0.00347  -0.0680   0.7019   0.1672
  -6.000  -0.3540   0.00887   0.00318  -0.0683   0.6962   0.2051
  -5.750  -0.3273   0.00843   0.00289  -0.0685   0.6903   0.2496
  -5.500  -0.3005   0.00798   0.00262  -0.0688   0.6849   0.2998
  -5.250  -0.2726   0.00759   0.00241  -0.0692   0.6798   0.3466
  -5.000  -0.2441   0.00735   0.00227  -0.0695   0.6743   0.3828
  -4.750  -0.2154   0.00723   0.00217  -0.0698   0.6685   0.4070
  -4.500  -0.1859   0.00711   0.00209  -0.0702   0.6637   0.4255
  -4.250  -0.1565   0.00704   0.00203  -0.0706   0.6582   0.4404
  -4.000  -0.1272   0.00701   0.00197  -0.0709   0.6530   0.4526
  -3.750  -0.0977   0.00696   0.00193  -0.0712   0.6483   0.4641
  -3.500  -0.0680   0.00693   0.00189  -0.0716   0.6434   0.4737
  -3.250  -0.0385   0.00690   0.00185  -0.0719   0.6381   0.4829
  -3.000  -0.0092   0.00692   0.00183  -0.0722   0.6328   0.4914
  -2.750   0.0206   0.00687   0.00181  -0.0726   0.6283   0.5003
  -2.500   0.0504   0.00689   0.00179  -0.0729   0.6233   0.5078
  -2.250   0.0797   0.00688   0.00178  -0.0732   0.6185   0.5157
  -2.000   0.1093   0.00691   0.00177  -0.0736   0.6140   0.5225
  -1.750   0.1391   0.00688   0.00176  -0.0740   0.6095   0.5284
  -1.500   0.1686   0.00688   0.00176  -0.0743   0.6045   0.5344
  -1.250   0.1979   0.00693   0.00176  -0.0746   0.5994   0.5397
  -1.000   0.2277   0.00693   0.00176  -0.0750   0.5954   0.5447
  -0.750   0.2573   0.00692   0.00177  -0.0753   0.5911   0.5501
  -0.500   0.2868   0.00694   0.00178  -0.0756   0.5864   0.5551
  -0.250   0.3160   0.00702   0.00179  -0.0759   0.5813   0.5594
   0.000   0.3457   0.00700   0.00181  -0.0763   0.5774   0.5647
   0.250   0.3753   0.00700   0.00183  -0.0766   0.5731   0.5695
   0.500   0.4046   0.00704   0.00186  -0.0769   0.5685   0.5743
   0.750   0.4336   0.00713   0.00189  -0.0772   0.5634   0.5786
   1.000   0.4633   0.00711   0.00193  -0.0776   0.5596   0.5838
   1.250   0.4927   0.00713   0.00197  -0.0779   0.5551   0.5887
   1.500   0.5218   0.00719   0.00200  -0.0782   0.5501   0.5935
   1.750   0.5507   0.00726   0.00206  -0.0784   0.5452   0.5983
   2.000   0.5802   0.00726   0.00211  -0.0788   0.5409   0.6033
   2.250   0.6094   0.00730   0.00216  -0.0790   0.5361   0.6083
   2.500   0.6381   0.00739   0.00223  -0.0792   0.5310   0.6130
   2.750   0.6671   0.00743   0.00229  -0.0795   0.5265   0.6183
   3.000   0.6963   0.00746   0.00237  -0.0798   0.5216   0.6235
   3.250   0.7250   0.00753   0.00244  -0.0800   0.5165   0.6285
   3.500   0.7534   0.00764   0.00252  -0.0802   0.5108   0.6330
   3.750   0.7824   0.00765   0.00260  -0.0805   0.5048   0.6385
   4.000   0.8105   0.00774   0.00268  -0.0806   0.4980   0.6441
   4.250   0.8390   0.00783   0.00278  -0.0808   0.4922   0.6492
   4.500   0.8676   0.00789   0.00287  -0.0810   0.4860   0.6544
   5.000   0.9233   0.00808   0.00308  -0.0811   0.4683   0.6650
   5.250   0.9505   0.00822   0.00319  -0.0811   0.4574   0.6700
   5.500   0.9778   0.00833   0.00333  -0.0811   0.4480   0.6759
   5.750   1.0052   0.00845   0.00347  -0.0811   0.4395   0.6815
   6.000   1.0318   0.00863   0.00362  -0.0810   0.4289   0.6867
   6.250   1.0583   0.00878   0.00378  -0.0809   0.4159   0.6920
   6.500   1.0835   0.00901   0.00397  -0.0805   0.3987   0.6978
   6.750   1.1079   0.00929   0.00419  -0.0801   0.3799   0.7036
   7.000   1.1310   0.00962   0.00445  -0.0795   0.3565   0.7091
   7.250   1.1513   0.01009   0.00481  -0.0784   0.3260   0.7150
   7.500   1.1697   0.01066   0.00523  -0.0771   0.2941   0.7209
   7.750   1.1864   0.01128   0.00570  -0.0755   0.2618   0.7265
   8.000   1.2010   0.01194   0.00622  -0.0735   0.2297   0.7330
   8.250   1.2139   0.01262   0.00676  -0.0713   0.2009   0.7395
   8.500   1.2246   0.01325   0.00728  -0.0687   0.1758   0.7458
   9.000   1.2371   0.01460   0.00847  -0.0621   0.1374   0.7601
   9.250   1.2433   0.01535   0.00917  -0.0590   0.1208   0.7679
   9.500   1.2498   0.01617   0.00995  -0.0563   0.1066   0.7763
   9.750   1.2561   0.01705   0.01080  -0.0537   0.0943   0.7847
  10.000   1.2633   0.01798   0.01171  -0.0514   0.0840   0.7941
  10.250   1.2701   0.01897   0.01271  -0.0492   0.0748   0.8042
  10.500   1.2769   0.02004   0.01378  -0.0472   0.0672   0.8155
  10.750   1.2849   0.02108   0.01486  -0.0454   0.0615   0.8283
  11.000   1.2936   0.02211   0.01594  -0.0437   0.0569   0.8432
  11.250   1.2999   0.02329   0.01717  -0.0419   0.0526   0.8629
  11.500   1.3070   0.02432   0.01832  -0.0400   0.0495   0.8938
  11.750   1.3157   0.02545   0.01960  -0.0389   0.0464   1.0000
  12.000   1.3254   0.02676   0.02092  -0.0379   0.0437   1.0000
  12.250   1.3347   0.02811   0.02229  -0.0370   0.0413   1.0000
  12.500   1.3404   0.02978   0.02395  -0.0360   0.0388   1.0000
  12.750   1.3509   0.03111   0.02533  -0.0353   0.0372   1.0000
  13.000   1.3589   0.03267   0.02691  -0.0346   0.0355   1.0000
  13.250   1.3640   0.03451   0.02876  -0.0338   0.0337   1.0000
  13.500   1.3726   0.03612   0.03042  -0.0332   0.0326   1.0000
  13.750   1.3810   0.03778   0.03211  -0.0327   0.0314   1.0000
  14.000   1.3875   0.03965   0.03401  -0.0323   0.0302   1.0000
  14.250   1.3899   0.04198   0.03637  -0.0318   0.0289   1.0000
  14.500   1.3981   0.04382   0.03826  -0.0315   0.0282   1.0000
  14.750   1.4058   0.04572   0.04022  -0.0313   0.0274   1.0000
  15.000   1.4120   0.04783   0.04236  -0.0312   0.0267   1.0000
  15.250   1.4164   0.05017   0.04474  -0.0311   0.0258   1.0000
  15.500   1.4181   0.05286   0.04747  -0.0311   0.0250   1.0000
  15.750   1.4211   0.05547   0.05014  -0.0312   0.0244   1.0000
  16.000   1.4279   0.05768   0.05241  -0.0313   0.0240   1.0000
  16.250   1.4333   0.06012   0.05492  -0.0316   0.0234   1.0000
  16.500   1.4379   0.06268   0.05753  -0.0319   0.0228   1.0000
  16.750   1.4405   0.06554   0.06043  -0.0324   0.0223   1.0000
  17.000   1.4409   0.06872   0.06367  -0.0329   0.0218   1.0000
  17.250   1.4383   0.07235   0.06736  -0.0336   0.0212   1.0000
  17.500   1.4391   0.07564   0.07072  -0.0344   0.0208   1.0000
  17.750   1.4422   0.07864   0.07380  -0.0352   0.0206   1.0000
  18.000   1.4448   0.08175   0.07698  -0.0360   0.0202   1.0000
  18.250   1.4464   0.08503   0.08033  -0.0370   0.0198   1.0000
  18.500   1.4480   0.08838   0.08374  -0.0380   0.0195   1.0000
  18.750   1.4472   0.09214   0.08758  -0.0393   0.0192   1.0000
  19.000   1.4467   0.09586   0.09136  -0.0406   0.0188   1.0000
  19.250   1.4443   0.09992   0.09549  -0.0421   0.0185   1.0000
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