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AG25 Bubble Dancer DLG by Mark Drela (ag25-il) Xfoil prediction polar at RE=200,000 Ncrit=9


Details Polar file
Airfoil: AG25 Bubble Dancer DLG by Mark Drela (ag25-il)
Reynolds number: 200,000
Max Cl/Cd: 70.85 at α=4°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-ag25-il-200000.txt
Download as CSV file: xf-ag25-il-200000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: AG25 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 =     0.200 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -11.750  -0.4195   0.13738   0.13395  -0.0031   1.0000   0.0291
 -11.500  -0.4179   0.13422   0.13080  -0.0045   1.0000   0.0292
  -7.250  -0.4683   0.07746   0.07427  -0.0220   1.0000   0.0432
  -7.000  -0.4579   0.07417   0.07096  -0.0234   1.0000   0.0446
  -6.750  -0.4461   0.06997   0.06677  -0.0276   1.0000   0.0464
  -6.500  -0.4318   0.06481   0.06159  -0.0338   1.0000   0.0487
  -6.250  -0.4053   0.05657   0.05279  -0.0499   1.0000   0.0536
  -6.000  -0.3980   0.04979   0.04608  -0.0513   1.0000   0.0552
  -5.750  -0.3840   0.04729   0.04365  -0.0505   1.0000   0.0570
  -5.500  -0.3674   0.04426   0.04054  -0.0512   1.0000   0.0600
  -5.250  -0.3464   0.03894   0.03463  -0.0549   1.0000   0.0684
  -5.000  -0.3291   0.03628   0.03202  -0.0544   1.0000   0.0708
  -4.750  -0.2920   0.02427   0.01828  -0.0559   1.0000   0.0306
  -4.250  -0.2423   0.02015   0.01346  -0.0547   1.0000   0.0289
  -4.000  -0.2155   0.01741   0.01034  -0.0547   1.0000   0.0308
  -3.750  -0.1905   0.01618   0.00904  -0.0545   1.0000   0.0348
  -3.500  -0.1635   0.01489   0.00759  -0.0541   1.0000   0.0372
  -3.250  -0.1366   0.01399   0.00657  -0.0538   1.0000   0.0409
  -3.000  -0.1086   0.01295   0.00554  -0.0541   1.0000   0.0530
  -2.750  -0.0780   0.01182   0.00455  -0.0549   1.0000   0.0852
  -2.500  -0.0456   0.01059   0.00410  -0.0567   1.0000   0.2517
  -2.250  -0.0170   0.01012   0.00405  -0.0575   1.0000   0.3796
  -2.000   0.0149   0.00977   0.00407  -0.0588   0.9982   0.4936
  -1.750   0.0570   0.00934   0.00404  -0.0617   0.9917   0.6141
  -1.500   0.0952   0.00888   0.00402  -0.0635   0.9841   0.7464
  -1.250   0.1262   0.00840   0.00389  -0.0629   0.9749   0.9251
  -1.000   0.1752   0.00831   0.00365  -0.0672   0.9666   1.0000
  -0.750   0.2170   0.00827   0.00348  -0.0700   0.9565   1.0000
  -0.500   0.2542   0.00823   0.00332  -0.0716   0.9443   1.0000
  -0.250   0.2885   0.00817   0.00317  -0.0726   0.9306   1.0000
   0.000   0.3195   0.00813   0.00305  -0.0727   0.9156   1.0000
   0.250   0.3481   0.00809   0.00293  -0.0723   0.8996   1.0000
   0.500   0.3742   0.00809   0.00285  -0.0715   0.8802   1.0000
   0.750   0.4003   0.00811   0.00278  -0.0705   0.8611   1.0000
   1.000   0.4261   0.00814   0.00273  -0.0696   0.8407   1.0000
   1.250   0.4519   0.00821   0.00270  -0.0687   0.8190   1.0000
   1.500   0.4778   0.00829   0.00270  -0.0678   0.7960   1.0000
   1.750   0.5038   0.00840   0.00271  -0.0670   0.7724   1.0000
   2.000   0.5299   0.00853   0.00272  -0.0662   0.7475   1.0000
   2.250   0.5560   0.00868   0.00278  -0.0655   0.7208   1.0000
   2.500   0.5822   0.00885   0.00287  -0.0649   0.6930   1.0000
   2.750   0.6084   0.00905   0.00296  -0.0643   0.6642   1.0000
   3.000   0.6345   0.00927   0.00307  -0.0637   0.6336   1.0000
   3.250   0.6606   0.00951   0.00321  -0.0632   0.6021   1.0000
   3.500   0.6866   0.00979   0.00340  -0.0626   0.5700   1.0000
   3.750   0.7125   0.01009   0.00359  -0.0621   0.5373   1.0000
   4.000   0.7383   0.01042   0.00382  -0.0616   0.5037   1.0000
   4.250   0.7639   0.01079   0.00406  -0.0612   0.4704   1.0000
   4.500   0.7896   0.01115   0.00434  -0.0607   0.4362   1.0000
   4.750   0.8150   0.01157   0.00468  -0.0603   0.4027   1.0000
   5.000   0.8404   0.01199   0.00503  -0.0599   0.3685   1.0000
   5.250   0.8655   0.01246   0.00540  -0.0595   0.3350   1.0000
   5.500   0.8905   0.01296   0.00582  -0.0591   0.3015   1.0000
   5.750   0.9153   0.01348   0.00627  -0.0587   0.2678   1.0000
   6.000   0.9397   0.01408   0.00680  -0.0582   0.2352   1.0000
   6.250   0.9641   0.01469   0.00735  -0.0578   0.2019   1.0000
   6.500   0.9878   0.01542   0.00796  -0.0574   0.1698   1.0000
   6.750   1.0112   0.01619   0.00865  -0.0569   0.1372   1.0000
   7.000   1.0339   0.01711   0.00945  -0.0563   0.1060   1.0000
   7.250   1.0553   0.01826   0.01047  -0.0556   0.0783   1.0000
   7.500   1.0760   0.01956   0.01177  -0.0546   0.0557   1.0000
   7.750   1.0931   0.02142   0.01356  -0.0533   0.0405   1.0000
   8.000   1.1137   0.02273   0.01501  -0.0522   0.0325   1.0000
   8.250   1.1307   0.02474   0.01713  -0.0506   0.0272   1.0000
   8.500   1.1501   0.02615   0.01865  -0.0495   0.0233   1.0000
   8.750   1.1645   0.02908   0.02168  -0.0479   0.0211   1.0000
   9.000   1.1800   0.03240   0.02531  -0.0462   0.0201   1.0000
   9.250   1.1963   0.03501   0.02826  -0.0446   0.0195   1.0000
   9.500   1.2090   0.03821   0.03186  -0.0429   0.0191   1.0000
   9.750   1.2183   0.04138   0.03544  -0.0410   0.0185   1.0000
  10.000   1.2249   0.04424   0.03872  -0.0391   0.0176   1.0000
  10.250   1.2280   0.04712   0.04191  -0.0372   0.0167   1.0000
  10.500   1.2263   0.05022   0.04531  -0.0352   0.0161   1.0000
  10.750   1.2135   0.05397   0.04938  -0.0325   0.0162   1.0000
  11.000   1.1957   0.05808   0.05380  -0.0307   0.0163   1.0000
  11.250   1.1760   0.06286   0.05885  -0.0307   0.0165   1.0000
  11.500   1.1551   0.06851   0.06475  -0.0326   0.0167   1.0000
  11.750   1.1337   0.07519   0.07165  -0.0363   0.0169   1.0000
  12.000   1.1113   0.08310   0.07975  -0.0417   0.0172   1.0000
  12.250   1.0863   0.09275   0.08952  -0.0488   0.0177   1.0000
  12.500   1.0585   0.10403   0.10092  -0.0566   0.0189   1.0000
  12.750   1.0314   0.11547   0.11240  -0.0635   0.0199   1.0000
  13.000   0.9716   0.14482   0.14177  -0.0792   0.0260   1.0000
  13.250   0.9644   0.15234   0.14925  -0.0825   0.0275   1.0000
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