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NACA 63(2)A-015 (naca632a015-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: NACA 63(2)A-015 (naca632a015-il)
Reynolds number: 1,000,000
Max Cl/Cd: 93.12 at α=8.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-naca632a015-il-1000000.txt
Download as CSV file: xf-naca632a015-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NACA 63(2)A-015                                 
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -15.250  -0.3655   0.14060   0.13894  -0.0203   1.0000   0.0134
 -15.000  -0.3661   0.13754   0.13587  -0.0221   1.0000   0.0134
 -14.250  -0.8795   0.05357   0.05078  -0.0563   1.0000   0.0087
 -13.750  -0.8996   0.04632   0.04327  -0.0575   1.0000   0.0088
 -13.500  -0.9170   0.04222   0.03898  -0.0571   1.0000   0.0089
 -13.250  -0.9255   0.03932   0.03594  -0.0563   1.0000   0.0089
 -13.000  -0.9400   0.03573   0.03207  -0.0545   1.0000   0.0089
 -12.750  -0.9396   0.03399   0.03024  -0.0530   1.0000   0.0090
 -12.500  -0.9432   0.03173   0.02778  -0.0508   1.0000   0.0090
 -12.250  -0.9444   0.02970   0.02558  -0.0484   1.0000   0.0090
 -12.000  -0.9389   0.02862   0.02443  -0.0462   1.0000   0.0092
 -11.750  -0.9315   0.02790   0.02367  -0.0439   1.0000   0.0094
 -11.500  -0.9277   0.02656   0.02220  -0.0411   1.0000   0.0095
 -11.250  -0.9245   0.02491   0.02036  -0.0379   1.0000   0.0094
 -11.000  -0.9185   0.02413   0.01951  -0.0347   1.0000   0.0096
 -10.750  -0.9141   0.02322   0.01850  -0.0311   1.0000   0.0097
 -10.500  -0.9110   0.02265   0.01787  -0.0269   1.0000   0.0100
 -10.250  -0.9071   0.02175   0.01687  -0.0230   1.0000   0.0099
 -10.000  -0.8867   0.02090   0.01594  -0.0223   0.9991   0.0102
  -9.750  -0.8551   0.01967   0.01459  -0.0239   0.9961   0.0103
  -9.500  -0.8245   0.01884   0.01366  -0.0251   0.9912   0.0105
  -9.250  -0.7926   0.01817   0.01292  -0.0265   0.9855   0.0107
  -9.000  -0.7640   0.01729   0.01196  -0.0272   0.9771   0.0108
  -8.750  -0.7354   0.01575   0.01033  -0.0284   0.9684   0.0114
  -8.500  -0.6972   0.01489   0.00942  -0.0313   0.9594   0.0116
  -8.250  -0.6547   0.01418   0.00868  -0.0350   0.9478   0.0121
  -8.000  -0.6122   0.01356   0.00799  -0.0386   0.9300   0.0126
  -7.750  -0.5829   0.01308   0.00737  -0.0393   0.9036   0.0131
  -7.500  -0.5629   0.01276   0.00692  -0.0378   0.8775   0.0134
  -7.250  -0.5479   0.01231   0.00635  -0.0354   0.8553   0.0139
  -7.000  -0.5300   0.01200   0.00596  -0.0335   0.8369   0.0144
  -6.750  -0.5102   0.01176   0.00565  -0.0320   0.8214   0.0153
  -6.500  -0.4899   0.01152   0.00533  -0.0305   0.8085   0.0159
  -6.250  -0.4696   0.01122   0.00497  -0.0290   0.7974   0.0168
  -6.000  -0.4480   0.01100   0.00472  -0.0278   0.7873   0.0181
  -5.750  -0.4251   0.01081   0.00448  -0.0268   0.7776   0.0193
  -5.500  -0.4029   0.01059   0.00423  -0.0258   0.7689   0.0210
  -5.250  -0.3786   0.01046   0.00407  -0.0250   0.7602   0.0235
  -5.000  -0.3547   0.01030   0.00391  -0.0242   0.7522   0.0270
  -4.750  -0.3305   0.01014   0.00375  -0.0235   0.7443   0.0305
  -4.500  -0.3057   0.01004   0.00360  -0.0229   0.7368   0.0334
  -4.250  -0.2813   0.00986   0.00343  -0.0223   0.7289   0.0361
  -4.000  -0.2562   0.00978   0.00329  -0.0217   0.7213   0.0381
  -3.750  -0.2317   0.00957   0.00308  -0.0210   0.7141   0.0405
  -3.500  -0.2069   0.00945   0.00293  -0.0204   0.7066   0.0429
  -3.250  -0.1811   0.00934   0.00280  -0.0200   0.6994   0.0451
  -3.000  -0.1565   0.00917   0.00262  -0.0193   0.6916   0.0486
  -2.750  -0.1312   0.00905   0.00248  -0.0188   0.6846   0.0521
  -2.500  -0.1060   0.00890   0.00234  -0.0182   0.6773   0.0592
  -2.250  -0.0821   0.00869   0.00220  -0.0174   0.6702   0.0841
  -2.000  -0.0805   0.00694   0.00165  -0.0130   0.6632   0.4204
  -1.750  -0.0612   0.00654   0.00154  -0.0113   0.6551   0.5160
  -1.500  -0.0371   0.00638   0.00148  -0.0105   0.6448   0.5546
  -1.250  -0.0122   0.00631   0.00144  -0.0099   0.6329   0.5797
  -0.750   0.0395   0.00624   0.00139  -0.0089   0.6127   0.6172
  -0.500   0.0654   0.00624   0.00138  -0.0085   0.6044   0.6338
  -0.250   0.0917   0.00620   0.00139  -0.0081   0.5963   0.6518
   0.000   0.1179   0.00623   0.00139  -0.0077   0.5882   0.6666
   0.250   0.1444   0.00620   0.00141  -0.0074   0.5803   0.6805
   1.000   0.2240   0.00627   0.00145  -0.0064   0.5540   0.7094
   1.250   0.2514   0.00630   0.00146  -0.0063   0.5455   0.7166
   1.500   0.2778   0.00634   0.00149  -0.0060   0.5370   0.7235
   1.750   0.3047   0.00637   0.00151  -0.0058   0.5275   0.7310
   2.000   0.3313   0.00642   0.00155  -0.0055   0.5181   0.7379
   2.250   0.3574   0.00647   0.00159  -0.0052   0.5078   0.7452
   2.750   0.4102   0.00658   0.00168  -0.0046   0.4880   0.7597
   3.000   0.4366   0.00664   0.00173  -0.0043   0.4764   0.7676
   3.250   0.4623   0.00670   0.00179  -0.0039   0.4631   0.7756
   3.500   0.4878   0.00679   0.00186  -0.0035   0.4472   0.7841
   3.750   0.5126   0.00689   0.00194  -0.0029   0.4296   0.7926
   4.000   0.5366   0.00705   0.00204  -0.0022   0.4086   0.8023
   4.250   0.5593   0.00723   0.00216  -0.0013   0.3792   0.8129
   4.500   0.5807   0.00751   0.00231  -0.0001   0.3446   0.8243
   4.750   0.6017   0.00779   0.00249   0.0011   0.3137   0.8377
   5.000   0.6235   0.00800   0.00267   0.0022   0.2901   0.8523
   5.250   0.6453   0.00821   0.00285   0.0033   0.2705   0.8691
   5.500   0.6677   0.00839   0.00303   0.0043   0.2546   0.8880
   5.750   0.6921   0.00856   0.00323   0.0048   0.2425   0.9085
   6.000   0.7207   0.00876   0.00344   0.0045   0.2321   0.9286
   6.250   0.7549   0.00900   0.00368   0.0028   0.2222   0.9445
   6.500   0.7912   0.00925   0.00392   0.0007   0.2126   0.9565
   6.750   0.8299   0.00957   0.00420  -0.0021   0.2028   0.9632
   7.000   0.8647   0.00979   0.00442  -0.0039   0.1963   0.9708
   7.250   0.9009   0.01010   0.00470  -0.0060   0.1879   0.9749
   7.500   0.9327   0.01032   0.00493  -0.0072   0.1821   0.9810
   7.750   0.9649   0.01064   0.00520  -0.0085   0.1739   0.9852
   8.000   0.9997   0.01087   0.00544  -0.0104   0.1675   0.9884
   8.250   1.0318   0.01121   0.00573  -0.0118   0.1584   0.9924
   8.500   1.0655   0.01148   0.00599  -0.0135   0.1505   0.9954
   8.750   1.0998   0.01181   0.00630  -0.0154   0.1412   0.9980
   9.000   1.1335   0.01220   0.00663  -0.0172   0.1299   0.9999
   9.250   1.1450   0.01253   0.00690  -0.0144   0.1199   1.0000
   9.500   1.1557   0.01286   0.00720  -0.0114   0.1103   1.0000
   9.750   1.1658   0.01325   0.00755  -0.0083   0.1011   1.0000
  10.000   1.1748   0.01368   0.00794  -0.0050   0.0921   1.0000
  10.250   1.1799   0.01408   0.00830  -0.0010   0.0855   1.0000
  10.500   1.1870   0.01445   0.00867   0.0026   0.0790   1.0000
  10.750   1.1941   0.01495   0.00914   0.0060   0.0721   1.0000
  11.000   1.2040   0.01545   0.00962   0.0087   0.0663   1.0000
  11.250   1.2146   0.01599   0.01016   0.0112   0.0615   1.0000
  11.500   1.2251   0.01659   0.01075   0.0135   0.0573   1.0000
  11.750   1.2362   0.01722   0.01140   0.0155   0.0539   1.0000
  12.000   1.2483   0.01786   0.01206   0.0173   0.0514   1.0000
  12.250   1.2587   0.01864   0.01285   0.0192   0.0489   1.0000
  12.500   1.2693   0.01946   0.01370   0.0208   0.0465   1.0000
  12.750   1.2822   0.02020   0.01449   0.0221   0.0449   1.0000
  13.000   1.2920   0.02118   0.01549   0.0235   0.0425   1.0000
  13.250   1.2986   0.02244   0.01677   0.0250   0.0400   1.0000
  13.500   1.3122   0.02327   0.01767   0.0259   0.0386   1.0000
  13.750   1.3227   0.02435   0.01880   0.0268   0.0369   1.0000
  14.000   1.3301   0.02572   0.02019   0.0278   0.0353   1.0000
  14.250   1.3356   0.02729   0.02181   0.0288   0.0337   1.0000
  14.500   1.3467   0.02846   0.02304   0.0294   0.0326   1.0000
  14.750   1.3556   0.02984   0.02447   0.0299   0.0315   1.0000
  15.000   1.3620   0.03147   0.02614   0.0305   0.0304   1.0000
  15.250   1.3658   0.03336   0.02807   0.0310   0.0296   1.0000
  15.500   1.3667   0.03559   0.03037   0.0315   0.0287   1.0000
  15.750   1.3736   0.03731   0.03216   0.0317   0.0281   1.0000
  16.000   1.3772   0.03938   0.03431   0.0319   0.0277   1.0000
  16.250   1.3807   0.04154   0.03655   0.0319   0.0271   1.0000
  16.500   1.3823   0.04396   0.03905   0.0318   0.0267   1.0000
  16.750   1.3826   0.04657   0.04172   0.0316   0.0262   1.0000
  17.000   1.3812   0.04945   0.04467   0.0312   0.0257   1.0000
  17.250   1.3770   0.05277   0.04807   0.0307   0.0253   1.0000
  17.500   1.3703   0.05644   0.05182   0.0299   0.0247   1.0000
  17.750   1.3608   0.06058   0.05606   0.0289   0.0244   1.0000
  18.000   1.3557   0.06430   0.05986   0.0278   0.0240   1.0000
  18.250   1.3515   0.06794   0.06360   0.0268   0.0238   1.0000
  18.500   1.3456   0.07187   0.06763   0.0255   0.0236   1.0000
  18.750   1.3360   0.07640   0.07226   0.0240   0.0234   1.0000
  19.000   1.3266   0.08099   0.07696   0.0223   0.0232   1.0000
  19.250   1.3176   0.08558   0.08164   0.0206   0.0228   1.0000
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