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AG24 Bubble Dancer DLG by Mark Drela (ag24-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: AG24 Bubble Dancer DLG by Mark Drela (ag24-il)
Reynolds number: 1,000,000
Max Cl/Cd: 107.09 at α=4°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-ag24-il-1000000.txt
Download as CSV file: xf-ag24-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: AG24 Bubble Dancer DLG by Mark Drela            
  
 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
  ------ -------- --------- --------- -------- -------- --------
  -8.500  -0.5211   0.08459   0.08308  -0.0087   1.0000   0.0084
  -8.250  -0.5203   0.07984   0.07835  -0.0121   1.0000   0.0087
  -8.000  -0.5207   0.07459   0.07313  -0.0164   1.0000   0.0088
  -7.750  -0.5156   0.06737   0.06593  -0.0256   1.0000   0.0090
  -7.500  -0.5059   0.05509   0.05357  -0.0421   1.0000   0.0089
  -7.250  -0.5013   0.04260   0.04080  -0.0518   1.0000   0.0089
  -6.250  -0.4284   0.01613   0.01195  -0.0590   0.9957   0.0071
  -6.000  -0.3953   0.01309   0.00853  -0.0610   0.9942   0.0075
  -5.750  -0.3624   0.01177   0.00705  -0.0623   0.9915   0.0078
  -5.500  -0.3283   0.01075   0.00592  -0.0638   0.9887   0.0081
  -5.250  -0.2940   0.01006   0.00516  -0.0653   0.9856   0.0087
  -5.000  -0.2593   0.00953   0.00456  -0.0668   0.9824   0.0098
  -4.750  -0.2294   0.00914   0.00411  -0.0671   0.9752   0.0106
  -4.500  -0.1983   0.00848   0.00332  -0.0678   0.9690   0.0119
  -4.250  -0.1711   0.00806   0.00286  -0.0675   0.9591   0.0141
  -4.000  -0.1441   0.00787   0.00264  -0.0672   0.9491   0.0165
  -3.750  -0.1173   0.00748   0.00220  -0.0667   0.9385   0.0231
  -3.500  -0.0908   0.00720   0.00191  -0.0662   0.9269   0.0355
  -3.250  -0.0640   0.00687   0.00169  -0.0660   0.9144   0.0675
  -3.000  -0.0370   0.00657   0.00150  -0.0658   0.9013   0.1117
  -2.750  -0.0098   0.00629   0.00135  -0.0656   0.8878   0.1602
  -2.500   0.0176   0.00604   0.00121  -0.0655   0.8738   0.2150
  -2.250   0.0451   0.00583   0.00111  -0.0655   0.8593   0.2687
  -2.000   0.0728   0.00565   0.00103  -0.0654   0.8443   0.3220
  -1.750   0.1006   0.00548   0.00097  -0.0654   0.8289   0.3759
  -1.500   0.1285   0.00536   0.00091  -0.0653   0.8126   0.4228
  -1.250   0.1565   0.00526   0.00087  -0.0653   0.7956   0.4675
  -1.000   0.1844   0.00517   0.00085  -0.0653   0.7779   0.5170
  -0.750   0.2123   0.00510   0.00083  -0.0652   0.7595   0.5631
  -0.500   0.2402   0.00503   0.00082  -0.0652   0.7402   0.6101
  -0.250   0.2680   0.00498   0.00082  -0.0651   0.7199   0.6587
   0.000   0.2957   0.00492   0.00084  -0.0650   0.6990   0.7097
   0.250   0.3230   0.00489   0.00087  -0.0647   0.6772   0.7612
   0.500   0.3499   0.00486   0.00091  -0.0644   0.6547   0.8098
   0.750   0.3759   0.00485   0.00095  -0.0638   0.6318   0.8570
   1.000   0.3999   0.00482   0.00097  -0.0627   0.6091   0.9082
   1.250   0.4276   0.00479   0.00096  -0.0624   0.5852   1.0000
   1.500   0.4558   0.00494   0.00100  -0.0625   0.5609   1.0000
   1.750   0.4840   0.00511   0.00105  -0.0625   0.5366   1.0000
   2.000   0.5121   0.00526   0.00111  -0.0626   0.5124   1.0000
   2.250   0.5402   0.00543   0.00119  -0.0627   0.4885   1.0000
   2.500   0.5682   0.00561   0.00127  -0.0627   0.4644   1.0000
   2.750   0.5961   0.00580   0.00136  -0.0627   0.4402   1.0000
   3.000   0.6240   0.00598   0.00146  -0.0628   0.4165   1.0000
   3.250   0.6518   0.00619   0.00158  -0.0628   0.3931   1.0000
   3.500   0.6795   0.00641   0.00170  -0.0628   0.3688   1.0000
   3.750   0.7071   0.00663   0.00183  -0.0628   0.3444   1.0000
   4.000   0.7346   0.00686   0.00198  -0.0628   0.3198   1.0000
   4.250   0.7619   0.00712   0.00216  -0.0628   0.2944   1.0000
   4.500   0.7892   0.00740   0.00233  -0.0627   0.2696   1.0000
   4.750   0.8162   0.00770   0.00253  -0.0627   0.2434   1.0000
   5.000   0.8430   0.00802   0.00275  -0.0626   0.2165   1.0000
   5.250   0.8699   0.00834   0.00298  -0.0626   0.1928   1.0000
   5.500   0.8962   0.00875   0.00326  -0.0624   0.1632   1.0000
   5.750   0.9226   0.00912   0.00354  -0.0623   0.1392   1.0000
   6.000   0.9486   0.00956   0.00386  -0.0621   0.1131   1.0000
   6.250   0.9743   0.01003   0.00420  -0.0620   0.0886   1.0000
   6.500   0.9999   0.01052   0.00458  -0.0617   0.0667   1.0000
   6.750   1.0251   0.01106   0.00502  -0.0615   0.0469   1.0000
   7.000   1.0506   0.01155   0.00545  -0.0612   0.0337   1.0000
   7.250   1.0756   0.01208   0.00593  -0.0609   0.0225   1.0000
   7.500   1.1003   0.01268   0.00648  -0.0605   0.0145   1.0000
   7.750   1.1249   0.01330   0.00714  -0.0600   0.0102   1.0000
   8.000   1.1479   0.01420   0.00810  -0.0593   0.0073   1.0000
   8.250   1.1729   0.01466   0.00862  -0.0590   0.0066   1.0000
   8.500   1.1971   0.01521   0.00923  -0.0585   0.0058   1.0000
   8.750   1.2206   0.01587   0.00995  -0.0580   0.0053   1.0000
   9.000   1.2422   0.01682   0.01100  -0.0572   0.0048   1.0000
   9.250   1.2583   0.01858   0.01297  -0.0556   0.0044   1.0000
   9.500   1.2800   0.01935   0.01383  -0.0549   0.0043   1.0000
   9.750   1.3012   0.02016   0.01474  -0.0541   0.0041   1.0000
  10.000   1.3212   0.02109   0.01576  -0.0531   0.0040   1.0000
  10.250   1.3398   0.02213   0.01694  -0.0521   0.0038   1.0000
  10.500   1.3575   0.02324   0.01816  -0.0509   0.0036   1.0000
  10.750   1.3742   0.02437   0.01940  -0.0497   0.0034   1.0000
  11.000   1.3896   0.02557   0.02072  -0.0483   0.0032   1.0000
  11.250   1.4030   0.02689   0.02215  -0.0468   0.0030   1.0000
  11.500   1.4139   0.02833   0.02371  -0.0450   0.0029   1.0000
  11.750   1.4195   0.03000   0.02553  -0.0427   0.0028   1.0000
  12.000   1.4184   0.03192   0.02759  -0.0397   0.0028   1.0000
  12.250   1.4143   0.03421   0.03005  -0.0370   0.0027   1.0000
  12.500   1.4071   0.03706   0.03308  -0.0350   0.0027   1.0000
  12.750   1.3987   0.04038   0.03658  -0.0339   0.0027   1.0000
  13.000   1.3893   0.04420   0.04059  -0.0337   0.0027   1.0000
  13.250   1.3790   0.04858   0.04515  -0.0344   0.0027   1.0000
  13.500   1.3655   0.05385   0.05061  -0.0361   0.0026   1.0000
  13.750   1.3535   0.05935   0.05627  -0.0385   0.0027   1.0000
  14.000   1.3380   0.06581   0.06290  -0.0417   0.0027   1.0000
  14.250   1.3217   0.07271   0.06997  -0.0453   0.0027   1.0000
  14.500   1.3057   0.07987   0.07728  -0.0491   0.0027   1.0000
  14.750   1.2869   0.08771   0.08527  -0.0533   0.0027   1.0000
  15.000   1.2675   0.09596   0.09365  -0.0577   0.0027   1.0000
  15.250   1.2472   0.10466   0.10248  -0.0623   0.0027   1.0000
  15.500   1.2250   0.11400   0.11195  -0.0671   0.0028   1.0000
  15.750   1.2008   0.12422   0.12231  -0.0725   0.0028   1.0000
  16.000   1.1728   0.13573   0.13397  -0.0785   0.0029   1.0000
  16.250   1.1383   0.14978   0.14818  -0.0859   0.0030   1.0000
  16.500   1.0757   0.17447   0.17308  -0.0988   0.0033   1.0000
  16.750   0.8740   0.14894   0.14750  -0.0634   0.0035   1.0000
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