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AG24 Bubble Dancer DLG by Mark Drela (ag24-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: AG24 Bubble Dancer DLG by Mark Drela (ag24-il)
Reynolds number: 500,000
Max Cl/Cd: 92.08 at α=4.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-ag24-il-500000.txt
Download as CSV file: xf-ag24-il-500000.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 =     0.500 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
  -9.250  -0.4010   0.08850   0.08642  -0.0157   1.0000   0.0168
  -9.000  -0.4181   0.08031   0.07828  -0.0178   1.0000   0.0174
  -8.750  -0.4206   0.07570   0.07368  -0.0191   1.0000   0.0178
  -8.500  -0.4198   0.07197   0.06997  -0.0201   1.0000   0.0181
  -8.250  -0.4199   0.06808   0.06610  -0.0214   1.0000   0.0185
  -8.000  -0.4225   0.06355   0.06160  -0.0233   1.0000   0.0188
  -7.750  -0.4271   0.05869   0.05676  -0.0258   1.0000   0.0190
  -7.500  -0.4341   0.05320   0.05131  -0.0300   1.0000   0.0192
  -5.500  -0.3869   0.01864   0.01381  -0.0524   0.9994   0.0140
  -5.250  -0.3508   0.01554   0.01024  -0.0542   0.9974   0.0134
  -5.000  -0.3141   0.01392   0.00840  -0.0561   0.9953   0.0140
  -4.750  -0.2773   0.01278   0.00709  -0.0579   0.9929   0.0153
  -4.500  -0.2409   0.01200   0.00620  -0.0597   0.9894   0.0165
  -4.250  -0.2041   0.01070   0.00481  -0.0618   0.9864   0.0199
  -4.000  -0.1653   0.01013   0.00418  -0.0641   0.9838   0.0238
  -3.750  -0.1277   0.00938   0.00337  -0.0662   0.9804   0.0319
  -3.500  -0.0929   0.00878   0.00284  -0.0676   0.9745   0.0595
  -3.250  -0.0574   0.00813   0.00250  -0.0695   0.9696   0.1347
  -3.000  -0.0271   0.00768   0.00230  -0.0702   0.9606   0.2085
  -2.750   0.0030   0.00730   0.00214  -0.0706   0.9517   0.2789
  -2.500   0.0310   0.00699   0.00200  -0.0706   0.9414   0.3433
  -2.250   0.0574   0.00672   0.00189  -0.0701   0.9290   0.4049
  -2.000   0.0836   0.00650   0.00180  -0.0696   0.9161   0.4608
  -1.750   0.1099   0.00631   0.00172  -0.0690   0.9027   0.5133
  -1.500   0.1361   0.00612   0.00165  -0.0685   0.8887   0.5686
  -1.250   0.1623   0.00597   0.00160  -0.0679   0.8740   0.6227
  -1.000   0.1884   0.00582   0.00156  -0.0672   0.8588   0.6777
  -0.750   0.2142   0.00569   0.00154  -0.0665   0.8431   0.7338
  -0.500   0.2395   0.00558   0.00153  -0.0656   0.8262   0.7894
  -0.250   0.2637   0.00548   0.00152  -0.0644   0.8086   0.8429
   0.000   0.2859   0.00539   0.00149  -0.0626   0.7907   0.8973
   0.250   0.3150   0.00528   0.00138  -0.0623   0.7718   0.9861
   0.500   0.3438   0.00536   0.00135  -0.0624   0.7513   1.0000
   0.750   0.3717   0.00547   0.00134  -0.0623   0.7305   1.0000
   1.000   0.3996   0.00559   0.00134  -0.0623   0.7081   1.0000
   1.250   0.4274   0.00572   0.00137  -0.0622   0.6852   1.0000
   1.500   0.4552   0.00587   0.00139  -0.0621   0.6615   1.0000
   1.750   0.4829   0.00602   0.00144  -0.0620   0.6369   1.0000
   2.000   0.5106   0.00619   0.00149  -0.0619   0.6113   1.0000
   2.250   0.5382   0.00637   0.00158  -0.0618   0.5857   1.0000
   2.500   0.5657   0.00656   0.00166  -0.0617   0.5602   1.0000
   2.750   0.5932   0.00676   0.00176  -0.0617   0.5342   1.0000
   3.000   0.6206   0.00698   0.00187  -0.0616   0.5080   1.0000
   3.250   0.6480   0.00720   0.00202  -0.0615   0.4816   1.0000
   3.500   0.6753   0.00744   0.00216  -0.0614   0.4553   1.0000
   3.750   0.7025   0.00768   0.00232  -0.0613   0.4289   1.0000
   4.000   0.7297   0.00794   0.00249  -0.0613   0.4025   1.0000
   4.250   0.7567   0.00822   0.00270  -0.0612   0.3754   1.0000
   4.500   0.7836   0.00851   0.00291  -0.0611   0.3480   1.0000
   4.750   0.8103   0.00883   0.00313  -0.0610   0.3200   1.0000
   5.000   0.8369   0.00917   0.00338  -0.0608   0.2918   1.0000
   5.250   0.8633   0.00954   0.00365  -0.0607   0.2626   1.0000
   5.500   0.8894   0.00995   0.00397  -0.0605   0.2331   1.0000
   5.750   0.9153   0.01038   0.00429  -0.0604   0.2048   1.0000
   6.000   0.9409   0.01086   0.00465  -0.0601   0.1738   1.0000
   6.250   0.9663   0.01137   0.00504  -0.0599   0.1450   1.0000
   6.500   0.9914   0.01192   0.00548  -0.0597   0.1167   1.0000
   6.750   1.0160   0.01254   0.00598  -0.0594   0.0888   1.0000
   7.000   1.0401   0.01322   0.00654  -0.0590   0.0634   1.0000
   7.250   1.0638   0.01397   0.00718  -0.0585   0.0421   1.0000
   7.500   1.0865   0.01492   0.00803  -0.0579   0.0254   1.0000
   7.750   1.1086   0.01595   0.00910  -0.0571   0.0173   1.0000
   8.000   1.1321   0.01668   0.00991  -0.0565   0.0141   1.0000
   8.250   1.1493   0.01845   0.01184  -0.0550   0.0114   1.0000
   8.500   1.1714   0.01931   0.01283  -0.0542   0.0106   1.0000
   8.750   1.1917   0.02039   0.01404  -0.0531   0.0098   1.0000
   9.000   1.2123   0.02135   0.01508  -0.0523   0.0089   1.0000
   9.250   1.2317   0.02240   0.01620  -0.0514   0.0081   1.0000
   9.500   1.2442   0.02445   0.01840  -0.0496   0.0075   1.0000
   9.750   1.2505   0.02763   0.02184  -0.0470   0.0072   1.0000
  10.000   1.2672   0.02892   0.02330  -0.0457   0.0070   1.0000
  10.250   1.2810   0.03057   0.02514  -0.0442   0.0069   1.0000
  10.500   1.2920   0.03246   0.02724  -0.0424   0.0067   1.0000
  10.750   1.2997   0.03461   0.02961  -0.0404   0.0065   1.0000
  11.000   1.3020   0.03694   0.03220  -0.0378   0.0063   1.0000
  11.250   1.2990   0.03948   0.03498  -0.0350   0.0062   1.0000
  11.500   1.2927   0.04237   0.03810  -0.0327   0.0061   1.0000
  11.750   1.2832   0.04580   0.04177  -0.0310   0.0061   1.0000
  12.000   1.2713   0.04979   0.04600  -0.0304   0.0061   1.0000
  12.250   1.2576   0.05442   0.05086  -0.0308   0.0061   1.0000
  12.500   1.2420   0.05981   0.05648  -0.0325   0.0061   1.0000
  12.750   1.2248   0.06602   0.06290  -0.0354   0.0061   1.0000
  13.000   1.2066   0.07297   0.07005  -0.0392   0.0062   1.0000
  13.250   1.1875   0.08067   0.07793  -0.0439   0.0062   1.0000
  13.500   1.1676   0.08902   0.08645  -0.0491   0.0063   1.0000
  13.750   1.1467   0.09803   0.09561  -0.0547   0.0064   1.0000
  14.000   1.1256   0.10752   0.10522  -0.0605   0.0064   1.0000
  14.250   1.1042   0.11768   0.11547  -0.0665   0.0065   1.0000
  14.500   1.0811   0.12876   0.12665  -0.0729   0.0067   1.0000
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