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AG25 Bubble Dancer DLG by Mark Drela (ag25-il) Xfoil prediction polar at RE=100,000 Ncrit=5


Details Polar file
Airfoil: AG25 Bubble Dancer DLG by Mark Drela (ag25-il)
Reynolds number: 100,000
Max Cl/Cd: 53.09 at α=4.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-ag25-il-100000-n5.txt
Download as CSV file: xf-ag25-il-100000-n5.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 =     0.100 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
  -8.250  -0.4832   0.09377   0.08895  -0.0087   1.0000   0.0271
  -8.000  -0.4796   0.08985   0.08508  -0.0104   1.0000   0.0260
  -7.750  -0.4771   0.08572   0.08101  -0.0127   1.0000   0.0250
  -7.500  -0.4747   0.08127   0.07661  -0.0160   1.0000   0.0241
  -7.250  -0.4690   0.07585   0.07125  -0.0215   1.0000   0.0231
  -7.000  -0.4605   0.06893   0.06434  -0.0294   1.0000   0.0219
  -6.500  -0.4299   0.05093   0.04585  -0.0472   1.0000   0.0194
  -6.250  -0.4158   0.04546   0.04011  -0.0506   1.0000   0.0192
  -6.000  -0.3988   0.04035   0.03460  -0.0531   1.0000   0.0191
  -5.750  -0.3792   0.03581   0.02957  -0.0548   1.0000   0.0191
  -5.500  -0.3573   0.03197   0.02517  -0.0558   1.0000   0.0196
  -5.250  -0.3365   0.02887   0.02174  -0.0565   1.0000   0.0214
  -5.000  -0.3135   0.02702   0.01962  -0.0566   1.0000   0.0235
  -4.750  -0.2885   0.02458   0.01671  -0.0564   1.0000   0.0247
  -4.500  -0.2631   0.02241   0.01413  -0.0560   1.0000   0.0257
  -4.250  -0.2376   0.02063   0.01205  -0.0555   1.0000   0.0272
  -4.000  -0.2123   0.01935   0.01051  -0.0549   1.0000   0.0293
  -3.750  -0.1877   0.01809   0.00926  -0.0547   1.0000   0.0350
  -3.500  -0.1621   0.01709   0.00806  -0.0543   1.0000   0.0399
  -3.250  -0.1362   0.01616   0.00711  -0.0542   1.0000   0.0495
  -3.000  -0.1096   0.01534   0.00627  -0.0542   1.0000   0.0678
  -2.750  -0.0825   0.01446   0.00566  -0.0546   1.0000   0.1198
  -2.500  -0.0556   0.01370   0.00535  -0.0551   1.0000   0.2230
  -2.250  -0.0210   0.01311   0.00516  -0.0570   0.9951   0.3485
  -2.000   0.0167   0.01266   0.00503  -0.0592   0.9867   0.4611
  -1.750   0.0543   0.01229   0.00492  -0.0611   0.9783   0.5639
  -1.500   0.0906   0.01191   0.00483  -0.0625   0.9696   0.6684
  -1.250   0.1204   0.01152   0.00470  -0.0620   0.9582   0.7849
  -1.000   0.1572   0.01110   0.00441  -0.0629   0.9452   1.0000
  -0.750   0.1936   0.01112   0.00424  -0.0646   0.9321   1.0000
  -0.500   0.2285   0.01113   0.00408  -0.0659   0.9180   1.0000
  -0.250   0.2621   0.01115   0.00396  -0.0668   0.9028   1.0000
   0.000   0.2944   0.01116   0.00385  -0.0674   0.8869   1.0000
   0.250   0.3246   0.01119   0.00377  -0.0675   0.8690   1.0000
   0.500   0.3539   0.01123   0.00371  -0.0674   0.8501   1.0000
   0.750   0.3829   0.01127   0.00365  -0.0672   0.8311   1.0000
   1.000   0.4105   0.01134   0.00364  -0.0667   0.8098   1.0000
   1.250   0.4381   0.01141   0.00362  -0.0662   0.7885   1.0000
   1.500   0.4651   0.01151   0.00365  -0.0656   0.7651   1.0000
   1.750   0.4919   0.01163   0.00369  -0.0650   0.7410   1.0000
   2.000   0.5185   0.01177   0.00374  -0.0644   0.7160   1.0000
   2.250   0.5450   0.01194   0.00381  -0.0637   0.6898   1.0000
   2.500   0.5713   0.01213   0.00395  -0.0631   0.6624   1.0000
   2.750   0.5975   0.01234   0.00408  -0.0624   0.6339   1.0000
   3.000   0.6236   0.01259   0.00423  -0.0618   0.6045   1.0000
   3.250   0.6495   0.01286   0.00442  -0.0612   0.5744   1.0000
   3.500   0.6753   0.01316   0.00463  -0.0606   0.5439   1.0000
   3.750   0.7010   0.01349   0.00492  -0.0600   0.5132   1.0000
   4.000   0.7265   0.01385   0.00520  -0.0595   0.4820   1.0000
   4.250   0.7520   0.01423   0.00553  -0.0590   0.4506   1.0000
   4.500   0.7772   0.01465   0.00588  -0.0584   0.4194   1.0000
   4.750   0.8022   0.01511   0.00631  -0.0579   0.3884   1.0000
   5.000   0.8272   0.01559   0.00675  -0.0574   0.3573   1.0000
   5.250   0.8520   0.01610   0.00723  -0.0569   0.3263   1.0000
   5.500   0.8764   0.01666   0.00775  -0.0564   0.2954   1.0000
   5.750   0.9006   0.01726   0.00831  -0.0559   0.2651   1.0000
   6.000   0.9246   0.01791   0.00897  -0.0554   0.2354   1.0000
   6.250   0.9483   0.01860   0.00965  -0.0549   0.2054   1.0000
   6.500   0.9716   0.01936   0.01040  -0.0544   0.1765   1.0000
   6.750   0.9944   0.02020   0.01122  -0.0538   0.1486   1.0000
   7.000   1.0167   0.02114   0.01213  -0.0532   0.1216   1.0000
   7.250   1.0382   0.02220   0.01316  -0.0526   0.0971   1.0000
   7.500   1.0586   0.02344   0.01439  -0.0518   0.0758   1.0000
   7.750   1.0787   0.02473   0.01573  -0.0509   0.0575   1.0000
   8.000   1.0971   0.02625   0.01732  -0.0499   0.0452   1.0000
   8.250   1.1145   0.02789   0.01905  -0.0487   0.0361   1.0000
   8.500   1.1297   0.02976   0.02102  -0.0474   0.0306   1.0000
   8.750   1.1462   0.03149   0.02299  -0.0460   0.0258   1.0000
   9.000   1.1610   0.03332   0.02498  -0.0447   0.0227   1.0000
   9.250   1.1713   0.03589   0.02768  -0.0430   0.0208   1.0000
   9.500   1.1836   0.03846   0.03053  -0.0414   0.0195   1.0000
   9.750   1.1954   0.04084   0.03326  -0.0398   0.0178   1.0000
  10.000   1.2044   0.04316   0.03595  -0.0383   0.0162   1.0000
  10.250   1.2102   0.04554   0.03857  -0.0368   0.0150   1.0000
  10.500   1.2113   0.04831   0.04158  -0.0349   0.0145   1.0000
  10.750   1.2075   0.05133   0.04485  -0.0330   0.0141   1.0000
  11.000   1.2001   0.05475   0.04852  -0.0315   0.0138   1.0000
  11.250   1.1900   0.05865   0.05267  -0.0309   0.0137   1.0000
  11.500   1.1774   0.06313   0.05740  -0.0313   0.0136   1.0000
  11.750   1.1633   0.06823   0.06276  -0.0328   0.0135   1.0000
  12.000   1.1478   0.07406   0.06883  -0.0356   0.0135   1.0000
  12.250   1.1312   0.08072   0.07572  -0.0396   0.0136   1.0000
  12.500   1.1128   0.08848   0.08372  -0.0447   0.0137   1.0000
  12.750   1.0903   0.09806   0.09353  -0.0514   0.0140   1.0000
  13.000   1.0569   0.11171   0.10742  -0.0607   0.0146   1.0000
  13.250   1.0086   0.13159   0.12733  -0.0722   0.0166   1.0000
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