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SARATOV AIRFOIL (saratov-il) Xfoil prediction polar at RE=100,000 Ncrit=5


Details Polar file
Airfoil: SARATOV AIRFOIL (saratov-il)
Reynolds number: 100,000
Max Cl/Cd: 48.58 at α=8.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-saratov-il-100000-n5.txt
Download as CSV file: xf-saratov-il-100000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: SARATOV AIRFOIL                                 
  
 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
  ------ -------- --------- --------- -------- -------- --------
  -9.250  -0.0296   0.10285   0.09688  -0.0918   0.7284   0.0777
  -9.000  -0.0273   0.10124   0.09513  -0.0932   0.7063   0.0779
  -8.750  -0.0219   0.09894   0.09271  -0.0942   0.6891   0.0780
  -8.500  -0.0151   0.09641   0.09007  -0.0951   0.6755   0.0780
  -8.000   0.0250   0.08882   0.08224  -0.0939   0.6543   0.0820
  -7.500   0.0374   0.08371   0.07698  -0.0963   0.6412   0.0752
  -7.250   0.0452   0.08097   0.07422  -0.0968   0.6358   0.0706
  -6.750   0.0431   0.07432   0.06748  -0.1043   0.6279   0.0630
  -6.500   0.0594   0.07274   0.06587  -0.1028   0.6236   0.0653
  -6.000   0.0883   0.06898   0.06202  -0.1049   0.6161   0.0677
  -5.750   0.1014   0.06595   0.05892  -0.1084   0.6132   0.0668
  -5.500   0.1172   0.06265   0.05553  -0.1125   0.6107   0.0662
  -5.250   0.1356   0.05968   0.05248  -0.1162   0.6080   0.0662
  -5.000   0.1561   0.05689   0.04964  -0.1197   0.6053   0.0665
  -4.750   0.1782   0.05489   0.04757  -0.1223   0.6027   0.0681
  -4.500   0.2024   0.05272   0.04531  -0.1255   0.6002   0.0705
  -4.250   0.2296   0.04960   0.04206  -0.1304   0.5980   0.0718
  -3.750   0.3094   0.03749   0.02934  -0.1513   0.5941   0.0771
  -3.500   0.3386   0.03651   0.02828  -0.1532   0.5919   0.0800
  -3.000   0.4133   0.03053   0.02181  -0.1637   0.5875   0.0915
  -2.750   0.4378   0.03127   0.02258  -0.1627   0.5856   0.0934
  -2.500   0.4650   0.03135   0.02260  -0.1628   0.5839   0.0987
  -2.000   0.5326   0.02894   0.01979  -0.1679   0.5808   0.1253
  -1.750   0.5619   0.02885   0.01956  -0.1686   0.5795   0.1371
  -1.250   0.6197   0.02876   0.01920  -0.1697   0.5772   0.1580
  -0.750   0.6740   0.02886   0.01920  -0.1701   0.5750   0.1743
  -0.500   0.6971   0.02943   0.01985  -0.1690   0.5738   0.1817
  -0.250   0.7266   0.02908   0.01939  -0.1701   0.5727   0.1906
   0.000   0.7519   0.02909   0.01942  -0.1698   0.5716   0.1939
   0.250   0.7799   0.02879   0.01905  -0.1704   0.5706   0.1966
   0.500   0.8089   0.02835   0.01852  -0.1712   0.5696   0.1981
   0.750   0.8379   0.02792   0.01800  -0.1720   0.5687   0.1996
   1.000   0.8675   0.02744   0.01740  -0.1730   0.5676   0.2019
   1.250   0.8970   0.02691   0.01673  -0.1739   0.5666   0.2051
   1.500   0.9233   0.02692   0.01675  -0.1739   0.5655   0.2063
   1.750   0.9501   0.02688   0.01670  -0.1740   0.5645   0.2075
   2.000   0.9770   0.02685   0.01666  -0.1741   0.5637   0.2089
   2.250   1.0039   0.02684   0.01664  -0.1743   0.5630   0.2106
   2.500   1.0310   0.02681   0.01659  -0.1744   0.5624   0.2127
   2.750   1.0584   0.02672   0.01647  -0.1747   0.5618   0.2158
   3.000   1.0862   0.02658   0.01626  -0.1751   0.5613   0.2207
   3.250   1.1119   0.02694   0.01670  -0.1748   0.5604   0.2227
   3.500   1.1358   0.02730   0.01716  -0.1743   0.5588   0.2251
   3.750   1.1573   0.02763   0.01764  -0.1735   0.5565   0.2278
   4.000   1.1798   0.02784   0.01792  -0.1729   0.5539   0.2316
   4.250   1.2037   0.02796   0.01809  -0.1724   0.5512   0.2359
   4.500   1.2278   0.02827   0.01852  -0.1718   0.5485   0.2381
   4.750   1.2537   0.02848   0.01879  -0.1714   0.5460   0.2413
   5.000   1.2816   0.02860   0.01893  -0.1713   0.5439   0.2478
   5.250   1.3057   0.02901   0.01946  -0.1707   0.5419   0.2526
   5.500   1.3226   0.02974   0.02043  -0.1693   0.5394   0.2565
   5.750   1.3417   0.03032   0.02117  -0.1681   0.5367   0.2634
   6.000   1.3625   0.03076   0.02178  -0.1671   0.5335   0.2681
   6.250   1.3889   0.03080   0.02189  -0.1666   0.5297   0.2750
   6.500   1.4192   0.03071   0.02183  -0.1666   0.5267   0.2837
   6.750   1.4381   0.03130   0.02258  -0.1653   0.5240   0.2945
   7.000   1.4494   0.03219   0.02376  -0.1631   0.5203   0.3013
   7.250   1.4673   0.03264   0.02438  -0.1615   0.5160   0.3114
   7.750   1.5172   0.03247   0.02440  -0.1598   0.5061   0.3336
   8.000   1.5246   0.03332   0.02550  -0.1569   0.5010   0.3411
   8.250   1.5504   0.03292   0.02524  -0.1560   0.4947   0.3525
   8.500   1.5595   0.03316   0.02568  -0.1529   0.4865   0.3601
   8.750   1.5753   0.03243   0.02503  -0.1502   0.4735   0.3694
   9.000   1.5603   0.03369   0.02655  -0.1441   0.4644   0.3732
   9.250   1.5456   0.03512   0.02817  -0.1384   0.4541   0.3770
   9.500   1.5241   0.03749   0.03072  -0.1331   0.4432   0.3787
   9.750   1.4811   0.04325   0.03670  -0.1284   0.4414   0.3771
  10.000   1.4149   0.05387   0.04750  -0.1260   0.4390   0.3698
  10.250   1.3646   0.06302   0.05675  -0.1249   0.4230   0.3662
  10.750   1.2977   0.07645   0.07039  -0.1232   0.3714   0.3642
  11.000   1.3742   0.06455   0.05658  -0.1175   0.1961   0.3859
  11.250   1.3632   0.06853   0.06042  -0.1164   0.1809   0.3888
  11.500   1.3585   0.07178   0.06356  -0.1154   0.1668   0.3935
  11.750   1.3586   0.07450   0.06619  -0.1145   0.1540   0.3991
  12.000   1.3629   0.07680   0.06848  -0.1137   0.1422   0.4055
  12.250   1.3707   0.07877   0.07057  -0.1131   0.1310   0.4119
  12.500   1.3778   0.08090   0.07275  -0.1125   0.1187   0.4178
  12.750   1.3851   0.08305   0.07496  -0.1121   0.1036   0.4224
  13.000   1.3904   0.08551   0.07733  -0.1116   0.0828   0.4259
  13.250   1.3956   0.08779   0.07937  -0.1109   0.0592   0.4284
  13.500   1.4028   0.08969   0.08107  -0.1099   0.0463   0.4303
  13.750   1.4109   0.09158   0.08293  -0.1090   0.0401   0.4323
  14.000   1.4181   0.09368   0.08506  -0.1083   0.0363   0.4345
  14.250   1.4254   0.09587   0.08732  -0.1077   0.0333   0.4367
  14.500   1.4301   0.09844   0.08990  -0.1072   0.0310   0.4382
  14.750   1.4366   0.10079   0.09236  -0.1067   0.0295   0.4395
  15.000   1.4432   0.10317   0.09486  -0.1062   0.0282   0.4403
  15.250   1.4493   0.10561   0.09741  -0.1058   0.0271   0.4411
  15.500   1.4550   0.10814   0.10002  -0.1056   0.0260   0.4421
  15.750   1.4597   0.11079   0.10275  -0.1055   0.0250   0.4435
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