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NACA 63-212 AIRFOIL (n63212-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: NACA 63-212 AIRFOIL (n63212-il)
Reynolds number: 500,000
Max Cl/Cd: 69.12 at α=3.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-n63212-il-500000-n5.txt
Download as CSV file: xf-n63212-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NACA 63-212 AIRFOIL                             
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -13.750  -0.8010   0.08046   0.07779  -0.0267   1.0000   0.0104
 -13.500  -0.8382   0.06827   0.06538  -0.0355   1.0000   0.0103
 -13.250  -0.8668   0.05966   0.05656  -0.0415   1.0000   0.0103
 -13.000  -0.8882   0.05322   0.04991  -0.0455   1.0000   0.0104
 -12.750  -0.9054   0.04801   0.04451  -0.0480   1.0000   0.0103
 -12.500  -0.9186   0.04381   0.04010  -0.0494   1.0000   0.0103
 -12.250  -0.9276   0.04043   0.03653  -0.0499   1.0000   0.0104
 -12.000  -0.9352   0.03745   0.03335  -0.0497   1.0000   0.0105
 -11.750  -0.9393   0.03505   0.03076  -0.0488   1.0000   0.0106
 -11.500  -0.9412   0.03307   0.02860  -0.0473   1.0000   0.0107
 -11.250  -0.9406   0.03142   0.02676  -0.0452   1.0000   0.0109
 -11.000  -0.9335   0.02969   0.02483  -0.0439   1.0000   0.0110
 -10.750  -0.9223   0.02818   0.02314  -0.0427   1.0000   0.0111
 -10.500  -0.9085   0.02686   0.02162  -0.0417   1.0000   0.0112
 -10.250  -0.8932   0.02553   0.02013  -0.0408   1.0000   0.0113
 -10.000  -0.8773   0.02413   0.01857  -0.0398   1.0000   0.0114
  -9.750  -0.8616   0.02257   0.01688  -0.0388   1.0000   0.0116
  -9.500  -0.8436   0.02142   0.01562  -0.0380   1.0000   0.0117
  -9.250  -0.8252   0.02037   0.01450  -0.0371   1.0000   0.0118
  -9.000  -0.7980   0.01936   0.01340  -0.0379   0.9858   0.0120
  -8.750  -0.7661   0.01840   0.01235  -0.0397   0.9690   0.0122
  -8.500  -0.7347   0.01755   0.01142  -0.0412   0.9540   0.0124
  -8.250  -0.7066   0.01680   0.01058  -0.0419   0.9380   0.0126
  -8.000  -0.6819   0.01619   0.00987  -0.0418   0.9223   0.0129
  -7.750  -0.6585   0.01566   0.00925  -0.0413   0.9080   0.0132
  -7.500  -0.6355   0.01511   0.00861  -0.0407   0.8950   0.0134
  -7.250  -0.6121   0.01458   0.00798  -0.0401   0.8833   0.0136
  -7.000  -0.5884   0.01409   0.00739  -0.0396   0.8722   0.0138
  -6.750  -0.5639   0.01362   0.00684  -0.0392   0.8616   0.0141
  -6.500  -0.5390   0.01320   0.00633  -0.0389   0.8519   0.0143
  -6.250  -0.5138   0.01282   0.00586  -0.0385   0.8423   0.0145
  -6.000  -0.4882   0.01241   0.00538  -0.0383   0.8330   0.0150
  -5.750  -0.4623   0.01207   0.00498  -0.0381   0.8244   0.0155
  -5.500  -0.4359   0.01177   0.00464  -0.0380   0.8154   0.0162
  -5.250  -0.4092   0.01151   0.00432  -0.0379   0.8073   0.0171
  -5.000  -0.3823   0.01126   0.00401  -0.0378   0.7987   0.0183
  -4.750  -0.3554   0.01100   0.00373  -0.0377   0.7908   0.0212
  -4.500  -0.3283   0.01076   0.00347  -0.0377   0.7826   0.0266
  -4.250  -0.3010   0.01052   0.00321  -0.0377   0.7750   0.0345
  -4.000  -0.2738   0.01027   0.00298  -0.0377   0.7670   0.0459
  -3.750  -0.2467   0.00995   0.00274  -0.0378   0.7595   0.0711
  -3.500  -0.2194   0.00965   0.00252  -0.0379   0.7516   0.1004
  -3.250  -0.1923   0.00930   0.00230  -0.0380   0.7444   0.1441
  -3.000  -0.1652   0.00889   0.00208  -0.0382   0.7366   0.2019
  -2.750  -0.1390   0.00822   0.00181  -0.0384   0.7295   0.3135
  -2.500  -0.1123   0.00767   0.00165  -0.0387   0.7219   0.4224
  -2.250  -0.0846   0.00745   0.00158  -0.0388   0.7148   0.4770
  -2.000  -0.0565   0.00731   0.00155  -0.0389   0.7072   0.5209
  -1.750  -0.0285   0.00721   0.00152  -0.0389   0.7002   0.5560
  -1.500  -0.0002   0.00714   0.00151  -0.0390   0.6926   0.5814
  -1.250   0.0282   0.00712   0.00148  -0.0391   0.6857   0.5966
  -1.000   0.0568   0.00710   0.00147  -0.0392   0.6782   0.6068
  -0.750   0.0854   0.00710   0.00144  -0.0393   0.6710   0.6162
  -0.500   0.1141   0.00709   0.00144  -0.0394   0.6637   0.6252
  -0.250   0.1426   0.00711   0.00143  -0.0395   0.6564   0.6332
   0.000   0.1714   0.00711   0.00144  -0.0397   0.6490   0.6418
   0.250   0.1999   0.00713   0.00145  -0.0398   0.6417   0.6495
   0.500   0.2286   0.00715   0.00147  -0.0399   0.6343   0.6578
   0.750   0.2570   0.00717   0.00150  -0.0400   0.6266   0.6655
   1.000   0.2857   0.00720   0.00154  -0.0402   0.6188   0.6739
   1.250   0.3140   0.00724   0.00158  -0.0402   0.6106   0.6814
   1.500   0.3426   0.00727   0.00163  -0.0403   0.6019   0.6899
   1.750   0.3708   0.00733   0.00169  -0.0404   0.5930   0.6975
   2.000   0.3992   0.00737   0.00176  -0.0405   0.5829   0.7057
   2.250   0.4273   0.00743   0.00183  -0.0405   0.5713   0.7135
   2.500   0.4553   0.00752   0.00190  -0.0405   0.5551   0.7217
   2.750   0.4829   0.00761   0.00199  -0.0405   0.5374   0.7293
   3.000   0.5103   0.00774   0.00208  -0.0404   0.5146   0.7377
   3.250   0.5369   0.00794   0.00218  -0.0402   0.4791   0.7455
   3.500   0.5631   0.00822   0.00233  -0.0400   0.4365   0.7539
   3.750   0.5889   0.00852   0.00251  -0.0397   0.3936   0.7619
   4.000   0.6136   0.00902   0.00276  -0.0394   0.3307   0.7704
   4.250   0.6371   0.00963   0.00312  -0.0390   0.2619   0.7789
   4.500   0.6601   0.01034   0.00353  -0.0385   0.1893   0.7876
   4.750   0.6831   0.01100   0.00394  -0.0380   0.1303   0.7969
   5.000   0.7067   0.01158   0.00433  -0.0376   0.0879   0.8060
   5.250   0.7310   0.01204   0.00470  -0.0372   0.0623   0.8158
   5.500   0.7557   0.01241   0.00505  -0.0368   0.0484   0.8251
   5.750   0.7804   0.01276   0.00540  -0.0364   0.0394   0.8349
   6.000   0.8048   0.01312   0.00577  -0.0359   0.0332   0.8453
   6.250   0.8291   0.01343   0.00614  -0.0354   0.0295   0.8555
   6.500   0.8528   0.01380   0.00654  -0.0348   0.0263   0.8664
   6.750   0.8761   0.01416   0.00697  -0.0341   0.0241   0.8788
   7.500   0.9397   0.01534   0.00833  -0.0308   0.0193   0.9275
   7.750   0.9618   0.01571   0.00881  -0.0299   0.0185   0.9552
   8.000   0.9885   0.01621   0.00936  -0.0302   0.0175   1.0000
   8.250   1.0114   0.01675   0.00994  -0.0297   0.0167   1.0000
   8.500   1.0336   0.01733   0.01055  -0.0292   0.0162   1.0000
   8.750   1.0545   0.01800   0.01125  -0.0285   0.0154   1.0000
   9.000   1.0736   0.01879   0.01209  -0.0276   0.0148   1.0000
   9.250   1.0938   0.01944   0.01280  -0.0268   0.0145   1.0000
   9.500   1.1127   0.02016   0.01359  -0.0258   0.0141   1.0000
   9.750   1.1305   0.02092   0.01442  -0.0247   0.0138   1.0000
  10.000   1.1470   0.02173   0.01531  -0.0235   0.0135   1.0000
  10.250   1.1611   0.02253   0.01618  -0.0218   0.0132   1.0000
  10.500   1.1735   0.02340   0.01711  -0.0200   0.0130   1.0000
  10.750   1.1852   0.02432   0.01810  -0.0183   0.0127   1.0000
  11.000   1.1965   0.02532   0.01917  -0.0167   0.0126   1.0000
  11.250   1.2074   0.02637   0.02030  -0.0152   0.0123   1.0000
  11.500   1.2178   0.02750   0.02150  -0.0138   0.0121   1.0000
  11.750   1.2269   0.02879   0.02286  -0.0125   0.0118   1.0000
  12.000   1.2340   0.03032   0.02447  -0.0112   0.0117   1.0000
  12.250   1.2380   0.03229   0.02654  -0.0099   0.0114   1.0000
  12.500   1.2469   0.03373   0.02810  -0.0090   0.0113   1.0000
  12.750   1.2543   0.03540   0.02989  -0.0082   0.0111   1.0000
  13.000   1.2605   0.03724   0.03186  -0.0074   0.0110   1.0000
  13.250   1.2647   0.03937   0.03412  -0.0068   0.0109   1.0000
  13.500   1.2686   0.04154   0.03644  -0.0063   0.0108   1.0000
  13.750   1.2709   0.04398   0.03902  -0.0061   0.0106   1.0000
  14.000   1.2722   0.04659   0.04178  -0.0060   0.0105   1.0000
  14.250   1.2709   0.04963   0.04497  -0.0061   0.0103   1.0000
  14.500   1.2699   0.05269   0.04819  -0.0066   0.0102   1.0000
  14.750   1.2665   0.05620   0.05185  -0.0073   0.0101   1.0000
  15.000   1.2611   0.06009   0.05590  -0.0083   0.0100   1.0000
  15.250   1.2546   0.06433   0.06030  -0.0097   0.0100   1.0000
  15.500   1.2479   0.06882   0.06494  -0.0116   0.0099   1.0000
  15.750   1.2382   0.07403   0.07031  -0.0139   0.0098   1.0000
  16.000   1.2286   0.07950   0.07593  -0.0166   0.0097   1.0000
  16.250   1.2170   0.08564   0.08222  -0.0199   0.0096   1.0000
  16.500   1.2003   0.09306   0.08983  -0.0241   0.0096   1.0000
  16.750   1.1857   0.10050   0.09742  -0.0285   0.0095   1.0000
  17.000   1.1639   0.10992   0.10704  -0.0342   0.0096   1.0000
  17.250   1.1297   0.12293   0.12030  -0.0424   0.0096   1.0000
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