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AG26 Bubble Dancer DLG by Mark Drela (ag26-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: AG26 Bubble Dancer DLG by Mark Drela (ag26-il)
Reynolds number: 200,000
Max Cl/Cd: 65.94 at α=4°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-ag26-il-200000-n5.txt
Download as CSV file: xf-ag26-il-200000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: AG26 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 =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
  -6.750  -0.4473   0.07006   0.06676  -0.0224   1.0000   0.0162
  -6.500  -0.4318   0.06291   0.05960  -0.0309   1.0000   0.0147
  -6.250  -0.4036   0.05059   0.04707  -0.0438   1.0000   0.0124
  -6.000  -0.3860   0.04384   0.04011  -0.0490   1.0000   0.0120
  -5.750  -0.3651   0.03713   0.03305  -0.0532   1.0000   0.0117
  -5.500  -0.3425   0.03127   0.02666  -0.0559   1.0000   0.0115
  -5.250  -0.3184   0.02657   0.02138  -0.0573   1.0000   0.0114
  -5.000  -0.2933   0.02299   0.01721  -0.0578   1.0000   0.0115
  -4.750  -0.2677   0.02036   0.01407  -0.0578   1.0000   0.0117
  -4.500  -0.2421   0.01846   0.01176  -0.0575   1.0000   0.0121
  -4.250  -0.2164   0.01656   0.00955  -0.0573   1.0000   0.0128
  -4.000  -0.1917   0.01556   0.00847  -0.0570   1.0000   0.0146
  -3.750  -0.1659   0.01493   0.00774  -0.0568   0.9996   0.0171
  -3.500  -0.1290   0.01380   0.00641  -0.0586   0.9949   0.0188
  -3.250  -0.0928   0.01267   0.00517  -0.0604   0.9896   0.0217
  -3.000  -0.0555   0.01214   0.00456  -0.0624   0.9838   0.0289
  -2.750  -0.0199   0.01148   0.00385  -0.0640   0.9761   0.0420
  -2.500   0.0167   0.01089   0.00339  -0.0660   0.9688   0.0787
  -2.250   0.0502   0.01037   0.00310  -0.0673   0.9580   0.1425
  -2.000   0.0835   0.00988   0.00290  -0.0687   0.9467   0.2308
  -1.750   0.1161   0.00945   0.00276  -0.0697   0.9342   0.3252
  -1.500   0.1473   0.00911   0.00263  -0.0703   0.9200   0.4121
  -1.250   0.1768   0.00879   0.00253  -0.0705   0.9041   0.4948
  -1.000   0.2045   0.00847   0.00244  -0.0701   0.8867   0.5808
  -0.750   0.2292   0.00812   0.00238  -0.0689   0.8673   0.6834
  -0.500   0.2487   0.00765   0.00228  -0.0661   0.8475   0.8455
  -0.250   0.2810   0.00750   0.00210  -0.0664   0.8264   1.0000
   0.000   0.3079   0.00759   0.00202  -0.0658   0.8045   1.0000
   0.250   0.3348   0.00768   0.00196  -0.0653   0.7819   1.0000
   0.500   0.3616   0.00780   0.00192  -0.0648   0.7590   1.0000
   0.750   0.3884   0.00792   0.00190  -0.0643   0.7354   1.0000
   1.000   0.4152   0.00806   0.00190  -0.0639   0.7111   1.0000
   1.250   0.4421   0.00822   0.00191  -0.0634   0.6863   1.0000
   1.500   0.4689   0.00839   0.00196  -0.0630   0.6610   1.0000
   1.750   0.4957   0.00857   0.00201  -0.0626   0.6351   1.0000
   2.000   0.5225   0.00877   0.00208  -0.0622   0.6081   1.0000
   2.250   0.5492   0.00898   0.00217  -0.0619   0.5804   1.0000
   2.500   0.5759   0.00921   0.00228  -0.0615   0.5513   1.0000
   2.750   0.6024   0.00946   0.00244  -0.0612   0.5199   1.0000
   3.000   0.6288   0.00975   0.00258  -0.0608   0.4865   1.0000
   3.250   0.6550   0.01006   0.00275  -0.0605   0.4516   1.0000
   3.500   0.6811   0.01040   0.00295  -0.0602   0.4165   1.0000
   3.750   0.7073   0.01075   0.00321  -0.0599   0.3820   1.0000
   4.000   0.7333   0.01112   0.00347  -0.0596   0.3493   1.0000
   4.250   0.7593   0.01152   0.00376  -0.0594   0.3180   1.0000
   4.500   0.7853   0.01192   0.00407  -0.0591   0.2883   1.0000
   4.750   0.8112   0.01233   0.00444  -0.0589   0.2606   1.0000
   5.000   0.8369   0.01278   0.00482  -0.0586   0.2331   1.0000
   5.250   0.8625   0.01324   0.00522  -0.0583   0.2071   1.0000
   5.500   0.8879   0.01373   0.00565  -0.0580   0.1817   1.0000
   5.750   0.9131   0.01426   0.00612  -0.0577   0.1570   1.0000
   6.000   0.9383   0.01479   0.00666  -0.0574   0.1348   1.0000
   6.250   0.9629   0.01541   0.00722  -0.0571   0.1144   1.0000
   6.500   0.9877   0.01600   0.00782  -0.0567   0.0976   1.0000
   6.750   1.0120   0.01665   0.00846  -0.0563   0.0818   1.0000
   7.000   1.0361   0.01732   0.00916  -0.0559   0.0684   1.0000
   7.250   1.0599   0.01805   0.00990  -0.0554   0.0554   1.0000
   7.500   1.0832   0.01882   0.01074  -0.0549   0.0440   1.0000
   7.750   1.1061   0.01968   0.01165  -0.0543   0.0343   1.0000
   8.000   1.1282   0.02066   0.01269  -0.0536   0.0266   1.0000
   8.250   1.1486   0.02191   0.01398  -0.0528   0.0205   1.0000
   8.500   1.1696   0.02301   0.01528  -0.0519   0.0172   1.0000
   8.750   1.1888   0.02432   0.01669  -0.0510   0.0140   1.0000
   9.000   1.2072   0.02574   0.01829  -0.0500   0.0121   1.0000
   9.250   1.2246   0.02726   0.02002  -0.0488   0.0108   1.0000
   9.500   1.2409   0.02885   0.02180  -0.0475   0.0099   1.0000
   9.750   1.2553   0.03060   0.02379  -0.0462   0.0091   1.0000
  10.000   1.2657   0.03283   0.02622  -0.0446   0.0086   1.0000
  10.250   1.2706   0.03585   0.02949  -0.0425   0.0081   1.0000
  10.500   1.2805   0.03785   0.03177  -0.0409   0.0077   1.0000
  10.750   1.2875   0.03995   0.03415  -0.0393   0.0072   1.0000
  11.000   1.2895   0.04212   0.03658  -0.0372   0.0067   1.0000
  11.250   1.2872   0.04461   0.03930  -0.0353   0.0063   1.0000
  11.500   1.2823   0.04749   0.04241  -0.0341   0.0061   1.0000
  11.750   1.2741   0.05110   0.04627  -0.0337   0.0060   1.0000
  12.000   1.2637   0.05543   0.05084  -0.0345   0.0059   1.0000
  12.250   1.2515   0.06053   0.05618  -0.0365   0.0058   1.0000
  12.500   1.2371   0.06662   0.06250  -0.0397   0.0058   1.0000
  12.750   1.2206   0.07373   0.06983  -0.0440   0.0058   1.0000
  13.000   1.2016   0.08191   0.07822  -0.0492   0.0059   1.0000
  13.250   1.1802   0.09116   0.08766  -0.0551   0.0060   1.0000
  13.500   1.1566   0.10134   0.09802  -0.0613   0.0061   1.0000
  13.750   1.1291   0.11287   0.10969  -0.0680   0.0064   1.0000
  14.000   1.0972   0.12596   0.12289  -0.0750   0.0070   1.0000
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