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CAST 10-2/DOA 2 AIRFOIL (cast102-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: CAST 10-2/DOA 2 AIRFOIL (cast102-il)
Reynolds number: 1,000,000
Max Cl/Cd: 75.62 at α=6.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-cast102-il-1000000-n5.txt
Download as CSV file: xf-cast102-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: CAST 10-2/DOA 2 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
  ------ -------- --------- --------- -------- -------- --------
 -11.000  -0.5478   0.07736   0.07561  -0.0619   0.9758   0.0067
 -10.750  -0.5855   0.06593   0.06404  -0.0709   0.9612   0.0067
 -10.500  -0.6129   0.05989   0.05784  -0.0732   0.9486   0.0067
 -10.250  -0.6338   0.05567   0.05346  -0.0726   0.9381   0.0067
 -10.000  -0.6443   0.05178   0.04939  -0.0714   0.9306   0.0067
  -9.750  -0.6473   0.04792   0.04534  -0.0705   0.9253   0.0068
  -9.500  -0.6471   0.04391   0.04111  -0.0694   0.9202   0.0069
  -9.250  -0.6432   0.04008   0.03704  -0.0681   0.9159   0.0070
  -8.750  -0.6623   0.02054   0.01581  -0.0609   0.9062   0.0083
  -8.500  -0.6417   0.01866   0.01365  -0.0602   0.9034   0.0086
  -8.250  -0.6186   0.01758   0.01240  -0.0599   0.9009   0.0087
  -8.000  -0.5959   0.01638   0.01102  -0.0594   0.8985   0.0089
  -7.750  -0.5716   0.01557   0.01012  -0.0592   0.8962   0.0091
  -7.500  -0.5462   0.01502   0.00952  -0.0592   0.8936   0.0092
  -7.250  -0.5205   0.01457   0.00902  -0.0591   0.8911   0.0094
  -7.000  -0.4947   0.01411   0.00851  -0.0591   0.8887   0.0096
  -6.750  -0.4688   0.01365   0.00799  -0.0590   0.8865   0.0098
  -6.500  -0.4431   0.01315   0.00743  -0.0589   0.8843   0.0100
  -6.250  -0.4173   0.01267   0.00689  -0.0588   0.8822   0.0103
  -6.000  -0.3911   0.01219   0.00637  -0.0588   0.8799   0.0106
  -5.750  -0.3649   0.01175   0.00588  -0.0588   0.8776   0.0109
  -5.500  -0.3384   0.01136   0.00545  -0.0588   0.8754   0.0112
  -5.250  -0.3113   0.01107   0.00512  -0.0589   0.8733   0.0114
  -5.000  -0.2852   0.01061   0.00462  -0.0589   0.8712   0.0119
  -4.750  -0.2583   0.01029   0.00428  -0.0590   0.8691   0.0123
  -4.500  -0.2308   0.01003   0.00400  -0.0591   0.8671   0.0127
  -4.250  -0.2031   0.00976   0.00373  -0.0594   0.8651   0.0131
  -4.000  -0.1753   0.00952   0.00347  -0.0596   0.8631   0.0135
  -3.750  -0.1474   0.00928   0.00322  -0.0598   0.8611   0.0140
  -3.500  -0.1193   0.00907   0.00299  -0.0601   0.8590   0.0145
  -3.250  -0.0910   0.00889   0.00279  -0.0603   0.8569   0.0148
  -3.000  -0.0630   0.00865   0.00255  -0.0606   0.8549   0.0159
  -2.750  -0.0345   0.00851   0.00240  -0.0609   0.8531   0.0169
  -2.500  -0.0059   0.00836   0.00226  -0.0612   0.8513   0.0177
  -2.250   0.0229   0.00823   0.00213  -0.0616   0.8494   0.0186
  -2.000   0.0516   0.00808   0.00200  -0.0620   0.8473   0.0200
  -1.750   0.0803   0.00796   0.00189  -0.0623   0.8438   0.0223
  -1.500   0.1087   0.00785   0.00177  -0.0625   0.8388   0.0264
  -1.250   0.1372   0.00772   0.00167  -0.0627   0.8322   0.0342
  -1.000   0.1600   0.00570   0.00124  -0.0633   0.8257   0.5518
  -0.750   0.1884   0.00556   0.00123  -0.0636   0.8188   0.6003
  -0.500   0.2169   0.00553   0.00119  -0.0637   0.8087   0.6195
  -0.250   0.2452   0.00550   0.00117  -0.0639   0.7955   0.6370
   0.000   0.2736   0.00549   0.00116  -0.0640   0.7814   0.6523
   0.250   0.3017   0.00552   0.00115  -0.0641   0.7644   0.6598
   0.500   0.3297   0.00559   0.00114  -0.0642   0.7428   0.6657
   0.750   0.3564   0.00571   0.00115  -0.0640   0.7077   0.6713
   1.000   0.3809   0.00603   0.00122  -0.0634   0.6452   0.6747
   1.250   0.4026   0.00660   0.00140  -0.0624   0.5508   0.6780
   1.500   0.4257   0.00710   0.00158  -0.0617   0.4741   0.6809
   1.750   0.4487   0.00759   0.00176  -0.0610   0.3976   0.6840
   2.000   0.4724   0.00802   0.00194  -0.0605   0.3331   0.6876
   2.250   0.4979   0.00831   0.00207  -0.0602   0.2933   0.6913
   2.500   0.5243   0.00852   0.00219  -0.0601   0.2680   0.6950
   2.750   0.5505   0.00874   0.00231  -0.0600   0.2449   0.6985
   3.000   0.5765   0.00896   0.00245  -0.0599   0.2195   0.7022
   3.250   0.6024   0.00920   0.00260  -0.0597   0.1966   0.7060
   3.500   0.6286   0.00941   0.00274  -0.0596   0.1793   0.7100
   3.750   0.6546   0.00963   0.00290  -0.0594   0.1621   0.7140
   4.000   0.6807   0.00983   0.00307  -0.0592   0.1477   0.7184
   4.250   0.7069   0.01002   0.00323  -0.0591   0.1378   0.7231
   4.500   0.7330   0.01022   0.00339  -0.0590   0.1283   0.7274
   4.750   0.7592   0.01041   0.00358  -0.0588   0.1192   0.7317
   5.000   0.7849   0.01062   0.00377  -0.0586   0.1095   0.7366
   5.250   0.8103   0.01086   0.00397  -0.0584   0.0984   0.7419
   5.500   0.8354   0.01112   0.00419  -0.0581   0.0867   0.7471
   5.750   0.8601   0.01141   0.00444  -0.0577   0.0742   0.7529
   6.000   0.8847   0.01171   0.00470  -0.0573   0.0638   0.7586
   6.250   0.9090   0.01202   0.00498  -0.0569   0.0520   0.7642
   6.500   0.9312   0.01253   0.00538  -0.0561   0.0317   0.7707
   6.750   0.9548   0.01291   0.00574  -0.0556   0.0250   0.7772
   7.000   0.9789   0.01321   0.00608  -0.0551   0.0221   0.7849
   7.250   1.0031   0.01350   0.00640  -0.0546   0.0207   0.7925
   7.500   1.0269   0.01382   0.00677  -0.0541   0.0194   0.8011
   7.750   1.0501   0.01418   0.00717  -0.0535   0.0181   0.8095
   8.000   1.0738   0.01448   0.00753  -0.0529   0.0175   0.8195
   8.250   1.0971   0.01477   0.00790  -0.0523   0.0169   0.8311
   8.500   1.1199   0.01508   0.00829  -0.0516   0.0162   0.8450
   8.750   1.1419   0.01541   0.00870  -0.0508   0.0154   0.8622
   9.000   1.1628   0.01577   0.00915  -0.0497   0.0147   0.8845
   9.250   1.1806   0.01617   0.00968  -0.0480   0.0139   0.9179
   9.500   1.1991   0.01640   0.01003  -0.0463   0.0136   1.0000
   9.750   1.2204   0.01681   0.01049  -0.0454   0.0133   1.0000
  10.000   1.2403   0.01724   0.01096  -0.0443   0.0129   1.0000
  10.250   1.2597   0.01770   0.01146  -0.0431   0.0125   1.0000
  10.500   1.2789   0.01818   0.01199  -0.0419   0.0121   1.0000
  10.750   1.2976   0.01870   0.01254  -0.0406   0.0118   1.0000
  11.000   1.3158   0.01925   0.01313  -0.0393   0.0114   1.0000
  11.250   1.3330   0.01989   0.01380  -0.0379   0.0111   1.0000
  11.500   1.3482   0.02066   0.01465  -0.0362   0.0107   1.0000
  11.750   1.3648   0.02130   0.01535  -0.0348   0.0105   1.0000
  12.000   1.3815   0.02193   0.01604  -0.0335   0.0103   1.0000
  12.250   1.3974   0.02260   0.01678  -0.0320   0.0101   1.0000
  12.500   1.4125   0.02333   0.01758  -0.0305   0.0099   1.0000
  12.750   1.4265   0.02413   0.01845  -0.0289   0.0097   1.0000
  13.000   1.4402   0.02495   0.01935  -0.0273   0.0095   1.0000
  13.250   1.4531   0.02584   0.02031  -0.0257   0.0094   1.0000
  13.500   1.4653   0.02677   0.02131  -0.0241   0.0092   1.0000
  13.750   1.4769   0.02775   0.02237  -0.0224   0.0090   1.0000
  14.000   1.4873   0.02882   0.02352  -0.0208   0.0089   1.0000
  14.250   1.4967   0.02998   0.02475  -0.0190   0.0087   1.0000
  14.500   1.5048   0.03126   0.02611  -0.0173   0.0086   1.0000
  14.750   1.5112   0.03270   0.02763  -0.0155   0.0084   1.0000
  15.000   1.5150   0.03436   0.02939  -0.0136   0.0083   1.0000
  15.250   1.5152   0.03638   0.03152  -0.0116   0.0081   1.0000
  15.500   1.5157   0.03844   0.03370  -0.0099   0.0080   1.0000
  15.750   1.5195   0.04027   0.03563  -0.0086   0.0079   1.0000
  16.000   1.5216   0.04232   0.03779  -0.0074   0.0078   1.0000
  16.250   1.5220   0.04463   0.04022  -0.0063   0.0078   1.0000
  16.500   1.5201   0.04726   0.04296  -0.0054   0.0077   1.0000
  16.750   1.5162   0.05028   0.04611  -0.0048   0.0076   1.0000
  17.000   1.5106   0.05374   0.04970  -0.0046   0.0076   1.0000
  17.250   1.5031   0.05768   0.05378  -0.0050   0.0075   1.0000
  17.500   1.4928   0.06230   0.05854  -0.0059   0.0075   1.0000
  17.750   1.4793   0.06781   0.06420  -0.0078   0.0074   1.0000
  18.000   1.4622   0.07443   0.07098  -0.0106   0.0074   1.0000
  18.250   1.4393   0.08256   0.07929  -0.0147   0.0074   1.0000
  18.500   1.4097   0.09232   0.08923  -0.0198   0.0074   1.0000
  18.750   1.3746   0.10328   0.10038  -0.0255   0.0074   1.0000
  19.000   1.3350   0.11494   0.11220  -0.0314   0.0075   1.0000
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