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NACA 64(1)-212 MOD A (n64212ma-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: NACA 64(1)-212 MOD A (n64212ma-il)
Reynolds number: 500,000
Max Cl/Cd: 68.49 at α=9.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-n64212ma-il-500000.txt
Download as CSV file: xf-n64212ma-il-500000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NACA 64(1)-212 MOD A                            
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.500 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -10.500  -0.3892   0.10533   0.10287  -0.0252   1.0000   0.0259
 -10.250  -0.3865   0.10169   0.09926  -0.0268   1.0000   0.0265
 -10.000  -0.4133   0.09111   0.08870  -0.0369   1.0000   0.0278
  -9.750  -0.4040   0.08929   0.08691  -0.0355   1.0000   0.0280
  -9.500  -0.3974   0.08684   0.08448  -0.0356   1.0000   0.0282
  -9.250  -0.3930   0.08402   0.08169  -0.0363   1.0000   0.0284
  -9.000  -0.3893   0.08121   0.07891  -0.0372   1.0000   0.0288
  -8.750  -0.3910   0.07738   0.07512  -0.0394   1.0000   0.0293
  -8.500  -0.4017   0.07208   0.06985  -0.0440   1.0000   0.0295
  -8.250  -0.4200   0.06739   0.06518  -0.0477   0.9919   0.0297
  -8.000  -0.4262   0.05477   0.05197  -0.0625   0.9563   0.0319
  -7.750  -0.4066   0.05210   0.04926  -0.0643   0.9387   0.0321
  -7.500  -0.3938   0.04996   0.04704  -0.0643   0.9192   0.0323
  -7.250  -0.3832   0.04791   0.04487  -0.0635   0.9017   0.0326
  -7.000  -0.3720   0.04579   0.04262  -0.0627   0.8866   0.0332
  -6.750  -0.3696   0.04065   0.03685  -0.0609   0.8725   0.0362
  -6.500  -0.3526   0.03879   0.03496  -0.0604   0.8598   0.0364
  -6.250  -0.3350   0.03710   0.03319  -0.0599   0.8479   0.0368
  -6.000  -0.3166   0.03547   0.03144  -0.0593   0.8363   0.0374
  -5.750  -0.3004   0.03229   0.02761  -0.0575   0.8260   0.0408
  -5.500  -0.2792   0.03042   0.02574  -0.0572   0.8144   0.0411
  -5.250  -0.2572   0.02899   0.02425  -0.0569   0.8030   0.0416
  -5.000  -0.2348   0.02768   0.02281  -0.0564   0.7905   0.0425
  -4.750  -0.2121   0.02570   0.02033  -0.0552   0.7794   0.0460
  -4.500  -0.1883   0.02435   0.01895  -0.0549   0.7658   0.0467
  -4.250  -0.1621   0.02491   0.01900  -0.0537   0.7523   0.0509
  -4.000  -0.1388   0.02196   0.01608  -0.0537   0.7382   0.0518
  -3.750  -0.1135   0.02081   0.01489  -0.0535   0.7227   0.0527
  -3.500  -0.0874   0.01999   0.01393  -0.0530   0.7058   0.0551
  -3.250  -0.0585   0.01630   0.00947  -0.0511   0.6935   0.0402
  -3.000  -0.0318   0.01528   0.00834  -0.0506   0.6774   0.0400
  -2.750  -0.0048   0.01453   0.00745  -0.0502   0.6604   0.0402
  -2.500   0.0217   0.01376   0.00657  -0.0497   0.6398   0.0401
  -2.250   0.0478   0.01324   0.00589  -0.0490   0.6118   0.0402
  -2.000   0.0741   0.01288   0.00538  -0.0485   0.5831   0.0405
  -1.750   0.0993   0.01232   0.00472  -0.0479   0.5505   0.0409
  -1.500   0.1241   0.01208   0.00432  -0.0473   0.5019   0.0415
  -1.250   0.1437   0.01272   0.00427  -0.0462   0.3189   0.0423
  -1.000   0.1669   0.01306   0.00423  -0.0456   0.2198   0.0436
  -0.750   0.1930   0.01303   0.00405  -0.0452   0.1887   0.0448
  -0.500   0.2195   0.01293   0.00384  -0.0449   0.1678   0.0457
  -0.250   0.2452   0.01287   0.00364  -0.0447   0.1283   0.0471
   0.000   0.2723   0.01282   0.00353  -0.0445   0.1209   0.0490
   0.250   0.2997   0.01278   0.00344  -0.0443   0.1180   0.0511
   0.500   0.3271   0.01268   0.00335  -0.0442   0.1166   0.0548
   0.750   0.3546   0.01263   0.00330  -0.0441   0.1154   0.0605
   1.000   0.3822   0.01256   0.00325  -0.0439   0.1145   0.0739
   1.250   0.4060   0.01080   0.00326  -0.0443   0.1139   0.6744
   1.500   0.4319   0.01084   0.00344  -0.0437   0.1133   0.7290
   1.750   0.4583   0.01097   0.00360  -0.0432   0.1128   0.7580
   2.000   0.4843   0.01112   0.00379  -0.0427   0.1122   0.7794
   2.250   0.5101   0.01126   0.00396  -0.0421   0.1114   0.7988
   2.500   0.5352   0.01142   0.00417  -0.0413   0.1102   0.8201
   2.750   0.5599   0.01159   0.00437  -0.0404   0.1090   0.8378
   3.000   0.5854   0.01178   0.00456  -0.0399   0.1082   0.8504
   3.250   0.6102   0.01197   0.00475  -0.0392   0.1075   0.8602
   3.500   0.6353   0.01220   0.00497  -0.0386   0.1068   0.8703
   3.750   0.6587   0.01246   0.00523  -0.0377   0.1060   0.8810
   4.000   0.6824   0.01269   0.00546  -0.0369   0.1053   0.8918
   4.250   0.7063   0.01286   0.00565  -0.0360   0.1047   0.9038
   4.500   0.7286   0.01301   0.00584  -0.0348   0.1040   0.9162
   4.750   0.7500   0.01317   0.00603  -0.0334   0.1032   0.9310
   5.000   0.7706   0.01333   0.00621  -0.0319   0.1026   0.9500
   5.250   0.7985   0.01355   0.00644  -0.0320   0.1018   0.9725
   5.500   0.8306   0.01389   0.00675  -0.0332   0.1008   1.0000
   5.750   0.8564   0.01433   0.00713  -0.0332   0.1000   1.0000
   6.000   0.8824   0.01468   0.00746  -0.0332   0.0990   1.0000
   6.250   0.9091   0.01492   0.00771  -0.0332   0.0982   1.0000
   6.500   0.9350   0.01519   0.00800  -0.0331   0.0971   1.0000
   6.750   0.9602   0.01551   0.00831  -0.0328   0.0960   1.0000
   7.000   0.9844   0.01589   0.00866  -0.0325   0.0948   1.0000
   7.250   1.0074   0.01641   0.00914  -0.0320   0.0937   1.0000
   7.500   1.0334   0.01653   0.00933  -0.0318   0.0924   1.0000
   7.750   1.0583   0.01675   0.00958  -0.0314   0.0906   1.0000
   8.000   1.0817   0.01707   0.00988  -0.0309   0.0890   1.0000
   8.250   1.1068   0.01724   0.01012  -0.0306   0.0872   1.0000
   8.500   1.1327   0.01730   0.01023  -0.0304   0.0846   1.0000
   8.750   1.1598   0.01729   0.01028  -0.0303   0.0810   1.0000
   9.000   1.1864   0.01733   0.01042  -0.0301   0.0615   1.0000
   9.250   1.2096   0.01766   0.01045  -0.0297   0.0534   1.0000
   9.500   1.2265   0.01840   0.01123  -0.0283   0.0508   1.0000
   9.750   1.2417   0.01911   0.01198  -0.0266   0.0490   1.0000
  10.000   1.2560   0.01979   0.01269  -0.0247   0.0475   1.0000
  10.250   1.2681   0.02058   0.01350  -0.0227   0.0465   1.0000
  10.500   1.2835   0.02117   0.01415  -0.0212   0.0454   1.0000
  10.750   1.2970   0.02189   0.01491  -0.0195   0.0445   1.0000
  11.000   1.3091   0.02271   0.01577  -0.0178   0.0438   1.0000
  11.250   1.3223   0.02350   0.01661  -0.0163   0.0430   1.0000
  11.500   1.3360   0.02428   0.01745  -0.0150   0.0423   1.0000
  11.750   1.3492   0.02512   0.01835  -0.0137   0.0415   1.0000
  12.000   1.3618   0.02603   0.01930  -0.0125   0.0409   1.0000
  12.250   1.3732   0.02705   0.02036  -0.0113   0.0403   1.0000
  12.500   1.3849   0.02807   0.02146  -0.0102   0.0398   1.0000
  12.750   1.3949   0.02925   0.02270  -0.0090   0.0394   1.0000
  13.000   1.4052   0.03045   0.02396  -0.0080   0.0389   1.0000
  13.250   1.4158   0.03165   0.02523  -0.0072   0.0384   1.0000
  13.500   1.4255   0.03296   0.02659  -0.0063   0.0379   1.0000
  13.750   1.4326   0.03453   0.02822  -0.0056   0.0375   1.0000
  14.000   1.4380   0.03631   0.03007  -0.0048   0.0372   1.0000
  14.250   1.4435   0.03814   0.03199  -0.0042   0.0369   1.0000
  14.500   1.4480   0.04013   0.03406  -0.0037   0.0366   1.0000
  14.750   1.4517   0.04226   0.03627  -0.0034   0.0363   1.0000
  15.000   1.4547   0.04453   0.03863  -0.0032   0.0360   1.0000
  15.250   1.4567   0.04699   0.04117  -0.0032   0.0358   1.0000
  15.500   1.4577   0.04962   0.04389  -0.0034   0.0355   1.0000
  15.750   1.4579   0.05247   0.04682  -0.0037   0.0352   1.0000
  16.000   1.4568   0.05558   0.05001  -0.0043   0.0350   1.0000
  16.250   1.4544   0.05896   0.05347  -0.0050   0.0348   1.0000
  16.500   1.4509   0.06260   0.05717  -0.0060   0.0346   1.0000
  16.750   1.4473   0.06639   0.06105  -0.0072   0.0344   1.0000
  17.000   1.4444   0.07024   0.06501  -0.0086   0.0342   1.0000
  17.250   1.4404   0.07438   0.06927  -0.0102   0.0340   1.0000
  17.500   1.4360   0.07874   0.07375  -0.0121   0.0338   1.0000
  17.750   1.4310   0.08329   0.07841  -0.0141   0.0336   1.0000
  18.000   1.4255   0.08806   0.08330  -0.0164   0.0333   1.0000
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