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WORTMANN FX 05-H-126 AIRFOIL (fx05h126-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: WORTMANN FX 05-H-126 AIRFOIL (fx05h126-il)
Reynolds number: 1,000,000
Max Cl/Cd: 158.29 at α=7.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-fx05h126-il-1000000.txt
Download as CSV file: xf-fx05h126-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: WORTMANN FX 05-H-126 AIRFOIL                    
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     1.000 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
  -8.750  -0.3667   0.08525   0.08257   0.0062   0.5773   0.0141
  -8.500  -0.4381   0.08465   0.08182  -0.0008   0.5791   0.0139
  -8.250  -0.4395   0.08122   0.07840  -0.0028   0.5783   0.0140
  -8.000  -0.4459   0.07782   0.07503  -0.0049   0.5775   0.0141
  -7.750  -0.4475   0.07446   0.07166  -0.0072   0.5767   0.0142
  -7.500  -0.4448   0.07043   0.06760  -0.0102   0.5760   0.0143
  -7.250  -0.4391   0.06656   0.06369  -0.0128   0.5753   0.0145
  -6.250  -0.3937   0.04606   0.04258  -0.0201   0.5717   0.0174
  -6.000  -0.3955   0.03606   0.03211  -0.0197   0.5713   0.0177
  -5.750  -0.3778   0.03372   0.02965  -0.0196   0.5708   0.0180
  -5.500  -0.3567   0.03219   0.02803  -0.0194   0.5703   0.0183
  -5.250  -0.3351   0.03044   0.02616  -0.0192   0.5696   0.0186
  -5.000  -0.3128   0.02870   0.02427  -0.0188   0.5689   0.0191
  -4.750  -0.2898   0.02676   0.02214  -0.0183   0.5682   0.0204
  -4.500  -0.2625   0.02567   0.02064  -0.0170   0.5674   0.0221
  -4.250  -0.2472   0.02052   0.01509  -0.0158   0.5667   0.0232
  -4.000  -0.2214   0.01966   0.01418  -0.0156   0.5658   0.0238
  -3.750  -0.1979   0.01580   0.00976  -0.0139   0.5650   0.0195
  -3.500  -0.1715   0.01426   0.00797  -0.0132   0.5641   0.0191
  -3.250  -0.1442   0.01364   0.00728  -0.0130   0.5632   0.0195
  -3.000  -0.1167   0.01309   0.00666  -0.0129   0.5624   0.0201
  -2.750  -0.0894   0.01246   0.00595  -0.0126   0.5616   0.0204
  -2.500  -0.0620   0.01197   0.00541  -0.0124   0.5608   0.0208
  -2.250  -0.0345   0.01158   0.00497  -0.0122   0.5600   0.0212
  -2.000  -0.0071   0.01125   0.00459  -0.0120   0.5592   0.0216
  -1.750   0.0205   0.01098   0.00430  -0.0119   0.5583   0.0218
  -1.500   0.0481   0.01083   0.00411  -0.0118   0.5572   0.0221
  -1.250   0.0742   0.01034   0.00358  -0.0114   0.5564   0.0229
  -1.000   0.1016   0.01005   0.00329  -0.0113   0.5559   0.0242
  -0.750   0.1296   0.00985   0.00310  -0.0112   0.5552   0.0253
  -0.500   0.1577   0.00970   0.00294  -0.0112   0.5544   0.0264
  -0.250   0.1860   0.00959   0.00282  -0.0113   0.5536   0.0275
   0.000   0.2142   0.00946   0.00268  -0.0113   0.5527   0.0294
   0.250   0.2425   0.00933   0.00257  -0.0113   0.5515   0.0340
   0.500   0.2698   0.00905   0.00249  -0.0112   0.5501   0.0914
   0.750   0.2923   0.00820   0.00242  -0.0105   0.5488   0.3674
   1.000   0.3078   0.00708   0.00237  -0.0083   0.5476   0.7113
   1.250   0.3916   0.00646   0.00246  -0.0202   0.5462   0.9792
   1.500   0.4392   0.00657   0.00252  -0.0244   0.5452   0.9920
   1.750   0.4997   0.00665   0.00254  -0.0315   0.5441   1.0000
   2.000   0.5264   0.00673   0.00259  -0.0313   0.5428   1.0000
   2.250   0.5532   0.00683   0.00267  -0.0312   0.5416   1.0000
   2.500   0.5801   0.00685   0.00269  -0.0311   0.5409   1.0000
   2.750   0.6072   0.00687   0.00272  -0.0310   0.5399   1.0000
   3.000   0.6342   0.00688   0.00275  -0.0309   0.5387   1.0000
   3.250   0.6613   0.00691   0.00279  -0.0308   0.5375   1.0000
   3.500   0.6885   0.00695   0.00283  -0.0308   0.5362   1.0000
   3.750   0.7157   0.00698   0.00286  -0.0307   0.5348   1.0000
   4.000   0.7428   0.00698   0.00286  -0.0306   0.5332   1.0000
   4.250   0.7700   0.00696   0.00282  -0.0305   0.5312   1.0000
   4.500   0.7971   0.00698   0.00281  -0.0304   0.5280   1.0000
   4.750   0.8246   0.00691   0.00279  -0.0304   0.5249   1.0000
   5.000   0.8521   0.00685   0.00275  -0.0304   0.5214   1.0000
   5.250   0.8796   0.00683   0.00275  -0.0304   0.5186   1.0000
   5.500   0.9070   0.00680   0.00272  -0.0304   0.5152   1.0000
   5.750   0.9345   0.00680   0.00274  -0.0304   0.5109   1.0000
   6.000   0.9622   0.00678   0.00278  -0.0305   0.5067   1.0000
   6.250   0.9897   0.00677   0.00279  -0.0306   0.5018   1.0000
   6.500   1.0173   0.00679   0.00284  -0.0307   0.4959   1.0000
   6.750   1.0449   0.00682   0.00291  -0.0308   0.4897   1.0000
   7.000   1.0724   0.00687   0.00298  -0.0309   0.4819   1.0000
   7.250   1.0998   0.00696   0.00307  -0.0311   0.4696   1.0000
   7.500   1.1270   0.00712   0.00321  -0.0313   0.4486   1.0000
   7.750   1.1531   0.00763   0.00355  -0.0316   0.4096   1.0000
   8.000   1.1776   0.00850   0.00421  -0.0321   0.3637   1.0000
   8.250   1.1996   0.00975   0.00516  -0.0326   0.3009   1.0000
   8.500   1.2167   0.01159   0.00657  -0.0331   0.2216   1.0000
   8.750   1.2314   0.01331   0.00798  -0.0332   0.1663   1.0000
   9.000   1.2458   0.01479   0.00931  -0.0333   0.1329   1.0000
   9.250   1.2540   0.01747   0.01182  -0.0350   0.0970   1.0000
   9.500   1.2573   0.01964   0.01395  -0.0347   0.0843   1.0000
   9.750   1.2561   0.02142   0.01572  -0.0328   0.0772   1.0000
  10.000   1.2621   0.02292   0.01723  -0.0317   0.0725   1.0000
  10.250   1.2659   0.02465   0.01894  -0.0307   0.0658   1.0000
  10.500   1.2760   0.02592   0.02025  -0.0300   0.0628   1.0000
  10.750   1.2837   0.02740   0.02173  -0.0293   0.0589   1.0000
  11.000   1.2900   0.02898   0.02331  -0.0285   0.0541   1.0000
  11.250   1.3004   0.03026   0.02463  -0.0279   0.0516   1.0000
  11.500   1.3082   0.03174   0.02610  -0.0272   0.0478   1.0000
  11.750   1.3151   0.03332   0.02768  -0.0266   0.0434   1.0000
  12.000   1.3236   0.03476   0.02915  -0.0260   0.0398   1.0000
  12.250   1.3279   0.03658   0.03092  -0.0253   0.0326   1.0000
  12.500   1.3299   0.03868   0.03297  -0.0246   0.0240   1.0000
  12.750   1.3296   0.04105   0.03526  -0.0239   0.0156   1.0000
  13.000   1.3319   0.04326   0.03746  -0.0234   0.0121   1.0000
  13.250   1.3358   0.04534   0.03957  -0.0229   0.0102   1.0000
  13.500   1.3426   0.04721   0.04149  -0.0225   0.0096   1.0000
  13.750   1.3490   0.04913   0.04346  -0.0222   0.0090   1.0000
  14.000   1.3554   0.05106   0.04544  -0.0219   0.0086   1.0000
  14.250   1.3572   0.05352   0.04795  -0.0216   0.0080   1.0000
  14.500   1.3610   0.05578   0.05028  -0.0213   0.0076   1.0000
  14.750   1.3666   0.05792   0.05248  -0.0212   0.0074   1.0000
  15.000   1.3707   0.06024   0.05487  -0.0211   0.0073   1.0000
  15.250   1.3762   0.06241   0.05711  -0.0210   0.0070   1.0000
  15.500   1.3792   0.06492   0.05968  -0.0210   0.0067   1.0000
  15.750   1.3811   0.06759   0.06242  -0.0210   0.0066   1.0000
  16.000   1.3837   0.07023   0.06513  -0.0211   0.0065   1.0000
  16.250   1.3840   0.07316   0.06813  -0.0212   0.0062   1.0000
  16.500   1.3840   0.07618   0.07122  -0.0215   0.0061   1.0000
  16.750   1.3821   0.07951   0.07464  -0.0218   0.0060   1.0000
  17.000   1.3782   0.08317   0.07838  -0.0223   0.0059   1.0000
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