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SIKORSKY SC2110 AIRFOIL (sc2110-il) Xfoil prediction polar at RE=100,000 Ncrit=9


Details Polar file
Airfoil: SIKORSKY SC2110 AIRFOIL (sc2110-il)
Reynolds number: 100,000
Max Cl/Cd: 34.71 at α=2.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-sc2110-il-100000.txt
Download as CSV file: xf-sc2110-il-100000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: SIKORSKY SC2110 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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
  -9.000  -0.5123   0.10427   0.09969  -0.0055   1.0000   0.0854
  -8.750  -0.5278   0.09930   0.09478  -0.0168   1.0000   0.0866
  -8.500  -0.5460   0.09551   0.09088  -0.0244   1.0000   0.0870
  -8.250  -0.5043   0.09078   0.08633  -0.0138   1.0000   0.0908
  -8.000  -0.4981   0.08705   0.08262  -0.0155   1.0000   0.0940
  -7.750  -0.3985   0.07275   0.06859  -0.0247   1.0000   0.1076
  -7.500  -0.4071   0.06850   0.06437  -0.0271   1.0000   0.1102
  -7.250  -0.4252   0.06488   0.06077  -0.0280   1.0000   0.1122
  -7.000  -0.4478   0.06205   0.05792  -0.0269   1.0000   0.1143
  -6.750  -0.4805   0.06039   0.05607  -0.0249   1.0000   0.1164
  -6.500  -0.4958   0.05671   0.05229  -0.0230   1.0000   0.1182
  -6.250  -0.5147   0.06238   0.05755  -0.0239   1.0000   0.1200
  -6.000  -0.5083   0.05982   0.05505  -0.0217   1.0000   0.1246
  -5.750  -0.5128   0.05782   0.05269  -0.0205   1.0000   0.1346
  -5.500  -0.5028   0.05460   0.04964  -0.0184   1.0000   0.1393
  -5.250  -0.4986   0.05224   0.04705  -0.0172   1.0000   0.1517
  -4.750  -0.4788   0.04731   0.04207  -0.0141   1.0000   0.1756
  -4.500  -0.4703   0.04500   0.03960  -0.0130   1.0000   0.2001
  -4.250  -0.4585   0.04245   0.03717  -0.0112   1.0000   0.2210
  -3.750  -0.4369   0.03814   0.03291  -0.0077   1.0000   0.2962
  -3.500  -0.4221   0.03579   0.03063  -0.0060   1.0000   0.3283
  -3.250  -0.3403   0.03104   0.02318  -0.0094   1.0000   0.0995
  -3.000  -0.3110   0.02809   0.01979  -0.0085   1.0000   0.0812
  -2.750  -0.2823   0.02674   0.01785  -0.0072   1.0000   0.0724
  -2.500  -0.2549   0.02489   0.01585  -0.0069   1.0000   0.0709
  -2.250  -0.2287   0.02392   0.01465  -0.0063   1.0000   0.0723
  -2.000  -0.2026   0.02300   0.01359  -0.0057   1.0000   0.0733
  -1.750  -0.1756   0.02158   0.01219  -0.0054   1.0000   0.0744
  -1.500  -0.1498   0.02057   0.01131  -0.0051   1.0000   0.0778
  -1.250  -0.1249   0.02003   0.01080  -0.0048   1.0000   0.0851
  -1.000  -0.0989   0.01931   0.01018  -0.0047   1.0000   0.0927
  -0.750  -0.0407   0.01852   0.00955  -0.0106   0.9904   0.1358
  -0.500   0.0187   0.01637   0.01023  -0.0111   0.9847   1.0000
  -0.250   0.0838   0.01669   0.01026  -0.0185   0.9712   1.0000
   0.000   0.1449   0.01690   0.01029  -0.0251   0.9587   1.0000
   0.250   0.2114   0.01697   0.01024  -0.0323   0.9459   1.0000
   0.500   0.2745   0.01688   0.01007  -0.0386   0.9316   1.0000
   0.750   0.3207   0.01669   0.00986  -0.0414   0.9148   1.0000
   1.000   0.3552   0.01641   0.00956  -0.0415   0.8964   1.0000
   1.250   0.3809   0.01604   0.00918  -0.0397   0.8777   1.0000
   1.500   0.3972   0.01566   0.00880  -0.0364   0.8547   1.0000
   1.750   0.4143   0.01509   0.00821  -0.0326   0.8319   1.0000
   2.000   0.4295   0.01451   0.00762  -0.0285   0.8025   1.0000
   2.250   0.4447   0.01389   0.00697  -0.0244   0.7601   1.0000
   2.500   0.4592   0.01327   0.00613  -0.0197   0.6748   1.0000
   2.750   0.4714   0.01358   0.00541  -0.0149   0.5107   1.0000
   3.000   0.4898   0.01454   0.00564  -0.0131   0.4299   1.0000
   3.250   0.5110   0.01535   0.00599  -0.0120   0.3911   1.0000
   3.500   0.5341   0.01603   0.00642  -0.0113   0.3630   1.0000
   3.750   0.5578   0.01673   0.00687  -0.0107   0.3414   1.0000
   4.000   0.5825   0.01738   0.00737  -0.0103   0.3231   1.0000
   4.250   0.6076   0.01805   0.00792  -0.0099   0.3076   1.0000
   4.500   0.6329   0.01874   0.00846  -0.0096   0.2937   1.0000
   4.750   0.6585   0.01939   0.00903  -0.0094   0.2809   1.0000
   5.000   0.6845   0.02007   0.00973  -0.0092   0.2694   1.0000
   5.250   0.7105   0.02084   0.01045  -0.0091   0.2594   1.0000
   5.500   0.7365   0.02154   0.01108  -0.0090   0.2496   1.0000
   5.750   0.7625   0.02233   0.01196  -0.0088   0.2403   1.0000
   6.000   0.7887   0.02319   0.01272  -0.0088   0.2330   1.0000
   6.250   0.8144   0.02406   0.01377  -0.0086   0.2249   1.0000
   6.500   0.8404   0.02489   0.01452  -0.0086   0.2178   1.0000
   6.750   0.8655   0.02591   0.01574  -0.0084   0.2107   1.0000
   7.000   0.8911   0.02685   0.01676  -0.0083   0.2047   1.0000
   7.250   0.9162   0.02808   0.01804  -0.0082   0.1992   1.0000
   7.500   0.9402   0.02915   0.01937  -0.0080   0.1927   1.0000
   7.750   0.9654   0.03015   0.02035  -0.0079   0.1875   1.0000
   8.000   0.9879   0.03184   0.02233  -0.0076   0.1831   1.0000
   8.250   1.0098   0.03337   0.02417  -0.0073   0.1780   1.0000
   8.500   1.0341   0.03444   0.02526  -0.0071   0.1734   1.0000
   8.750   1.0545   0.03635   0.02737  -0.0068   0.1692   1.0000
   9.000   1.0704   0.03868   0.03020  -0.0060   0.1650   1.0000
   9.250   1.0889   0.04065   0.03240  -0.0055   0.1614   1.0000
   9.500   1.1128   0.04186   0.03359  -0.0054   0.1579   1.0000
   9.750   1.1242   0.04483   0.03692  -0.0046   0.1546   1.0000
  10.000   1.1249   0.04872   0.04140  -0.0032   0.1514   1.0000
  10.250   1.1240   0.05284   0.04595  -0.0020   0.1492   1.0000
  10.500   1.1203   0.05703   0.05047  -0.0009   0.1474   1.0000
  10.750   1.1308   0.05929   0.05285  -0.0002   0.1449   1.0000
  11.000   1.1628   0.06012   0.05351  -0.0003   0.1415   1.0000
  11.250   1.1320   0.06635   0.06020   0.0013   0.1409   1.0000
  11.500   1.0954   0.07275   0.06684   0.0023   0.1410   1.0000
  11.750   1.0583   0.08000   0.07424   0.0015   0.1415   1.0000
  12.000   0.8372   0.13724   0.13147  -0.0362   0.2014   1.0000
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