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WORTMANN FX 05-H-126 AIRFOIL (fx05h126-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: WORTMANN FX 05-H-126 AIRFOIL (fx05h126-il)
Reynolds number: 500,000
Max Cl/Cd: 116.29 at α=7°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx05h126-il-500000-n5.txt
Download as CSV file: xf-fx05h126-il-500000-n5.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 =     0.500 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
  -7.750  -0.4367   0.07595   0.07241  -0.0065   0.5730   0.0129
  -7.500  -0.4392   0.07070   0.06715  -0.0107   0.5723   0.0129
  -7.250  -0.4385   0.06515   0.06154  -0.0145   0.5716   0.0129
  -7.000  -0.4338   0.05971   0.05600  -0.0174   0.5708   0.0130
  -6.750  -0.4263   0.05422   0.05036  -0.0195   0.5700   0.0131
  -6.500  -0.4165   0.04867   0.04461  -0.0208   0.5693   0.0132
  -6.250  -0.4044   0.04312   0.03880  -0.0214   0.5686   0.0134
  -6.000  -0.3930   0.03603   0.03128  -0.0209   0.5679   0.0140
  -5.750  -0.3844   0.02752   0.02201  -0.0190   0.5672   0.0144
  -5.500  -0.3654   0.02401   0.01795  -0.0179   0.5664   0.0147
  -5.250  -0.3421   0.02219   0.01578  -0.0172   0.5656   0.0149
  -5.000  -0.3178   0.02072   0.01401  -0.0166   0.5647   0.0151
  -4.750  -0.2941   0.01889   0.01191  -0.0161   0.5639   0.0154
  -4.500  -0.2682   0.01798   0.01089  -0.0159   0.5631   0.0158
  -4.250  -0.2416   0.01736   0.01017  -0.0157   0.5623   0.0162
  -4.000  -0.2148   0.01671   0.00941  -0.0155   0.5615   0.0167
  -3.750  -0.1879   0.01599   0.00854  -0.0153   0.5608   0.0170
  -3.500  -0.1608   0.01532   0.00777  -0.0151   0.5600   0.0173
  -3.250  -0.1337   0.01475   0.00710  -0.0149   0.5592   0.0177
  -3.000  -0.1065   0.01424   0.00650  -0.0147   0.5583   0.0181
  -2.750  -0.0791   0.01377   0.00598  -0.0145   0.5575   0.0185
  -2.500  -0.0517   0.01337   0.00554  -0.0144   0.5566   0.0190
  -2.250  -0.0243   0.01302   0.00516  -0.0142   0.5558   0.0193
  -2.000   0.0032   0.01272   0.00483  -0.0141   0.5549   0.0197
  -1.750   0.0302   0.01234   0.00443  -0.0140   0.5541   0.0204
  -1.500   0.0572   0.01200   0.00408  -0.0138   0.5532   0.0214
  -1.250   0.0848   0.01176   0.00384  -0.0137   0.5523   0.0221
  -1.000   0.1125   0.01157   0.00363  -0.0137   0.5515   0.0229
  -0.750   0.1404   0.01142   0.00346  -0.0136   0.5506   0.0238
  -0.500   0.1684   0.01129   0.00331  -0.0136   0.5498   0.0248
  -0.250   0.1965   0.01119   0.00318  -0.0137   0.5489   0.0258
   0.000   0.2245   0.01107   0.00305  -0.0137   0.5479   0.0281
   0.250   0.2526   0.01097   0.00297  -0.0137   0.5470   0.0336
   0.500   0.2801   0.01081   0.00293  -0.0137   0.5463   0.0690
   0.750   0.3070   0.01055   0.00290  -0.0136   0.5455   0.1503
   1.000   0.3301   0.00984   0.00287  -0.0131   0.5445   0.3898
   1.250   0.3432   0.00866   0.00288  -0.0103   0.5433   0.7449
   1.500   0.4502   0.00827   0.00305  -0.0269   0.5412   0.9895
   1.750   0.5020   0.00831   0.00306  -0.0322   0.5394   1.0000
   2.000   0.5288   0.00834   0.00308  -0.0320   0.5378   1.0000
   2.250   0.5557   0.00839   0.00311  -0.0319   0.5365   1.0000
   2.500   0.5826   0.00844   0.00314  -0.0318   0.5353   1.0000
   2.750   0.6095   0.00848   0.00317  -0.0317   0.5340   1.0000
   3.000   0.6365   0.00853   0.00320  -0.0316   0.5328   1.0000
   3.250   0.6635   0.00859   0.00325  -0.0315   0.5318   1.0000
   3.500   0.6905   0.00866   0.00330  -0.0314   0.5306   1.0000
   3.750   0.7174   0.00874   0.00336  -0.0313   0.5294   1.0000
   4.000   0.7448   0.00882   0.00350  -0.0314   0.5279   1.0000
   4.250   0.7721   0.00890   0.00362  -0.0314   0.5262   1.0000
   4.500   0.7993   0.00898   0.00374  -0.0315   0.5243   1.0000
   4.750   0.8266   0.00902   0.00382  -0.0315   0.5218   1.0000
   5.000   0.8538   0.00902   0.00383  -0.0314   0.5191   1.0000
   5.250   0.8810   0.00895   0.00373  -0.0313   0.5149   1.0000
   5.500   0.9086   0.00894   0.00382  -0.0315   0.5082   1.0000
   5.750   0.9359   0.00893   0.00383  -0.0315   0.5036   1.0000
   6.000   0.9633   0.00897   0.00391  -0.0315   0.4989   1.0000
   6.250   0.9907   0.00900   0.00399  -0.0316   0.4913   1.0000
   6.500   1.0180   0.00904   0.00408  -0.0317   0.4829   1.0000
   6.750   1.0453   0.00909   0.00414  -0.0318   0.4688   1.0000
   7.000   1.0722   0.00922   0.00423  -0.0319   0.4480   1.0000
   7.250   1.0984   0.00951   0.00445  -0.0321   0.4219   1.0000
   7.500   1.1227   0.01020   0.00495  -0.0324   0.3848   1.0000
   7.750   1.1454   0.01115   0.00573  -0.0328   0.3460   1.0000
   8.000   1.1661   0.01229   0.00668  -0.0331   0.3005   1.0000
   8.250   1.1829   0.01380   0.00796  -0.0333   0.2512   1.0000
   8.500   1.1929   0.01588   0.00979  -0.0336   0.1984   1.0000
   9.000   1.1924   0.02131   0.01498  -0.0338   0.1399   1.0000
   9.250   1.1875   0.02339   0.01699  -0.0317   0.1227   1.0000
   9.500   1.1809   0.02580   0.01926  -0.0301   0.0986   1.0000
   9.750   1.1834   0.02762   0.02103  -0.0289   0.0873   1.0000
  10.000   1.1880   0.02930   0.02268  -0.0280   0.0793   1.0000
  10.250   1.1939   0.03090   0.02428  -0.0271   0.0732   1.0000
  10.500   1.2009   0.03243   0.02583  -0.0263   0.0681   1.0000
  10.750   1.2090   0.03390   0.02732  -0.0257   0.0633   1.0000
  11.000   1.2154   0.03550   0.02891  -0.0249   0.0586   1.0000
  11.250   1.2241   0.03695   0.03039  -0.0243   0.0550   1.0000
  11.500   1.2329   0.03841   0.03188  -0.0238   0.0516   1.0000
  11.750   1.2405   0.04003   0.03350  -0.0233   0.0471   1.0000
  12.000   1.2493   0.04159   0.03510  -0.0228   0.0435   1.0000
  12.250   1.2568   0.04329   0.03680  -0.0224   0.0386   1.0000
  12.500   1.2653   0.04491   0.03844  -0.0220   0.0351   1.0000
  12.750   1.2710   0.04686   0.04036  -0.0216   0.0294   1.0000
  13.000   1.2757   0.04890   0.04238  -0.0212   0.0224   1.0000
  13.250   1.2793   0.05109   0.04453  -0.0209   0.0159   1.0000
  13.500   1.2817   0.05346   0.04690  -0.0205   0.0119   1.0000
  13.750   1.2865   0.05559   0.04906  -0.0202   0.0102   1.0000
  14.000   1.2924   0.05766   0.05120  -0.0200   0.0093   1.0000
  14.250   1.2970   0.05991   0.05351  -0.0199   0.0085   1.0000
  14.500   1.3014   0.06219   0.05585  -0.0197   0.0079   1.0000
  14.750   1.3055   0.06457   0.05829  -0.0196   0.0074   1.0000
  15.000   1.3110   0.06679   0.06060  -0.0196   0.0073   1.0000
  15.250   1.3153   0.06921   0.06310  -0.0196   0.0070   1.0000
  15.500   1.3188   0.07174   0.06572  -0.0197   0.0068   1.0000
  15.750   1.3220   0.07432   0.06838  -0.0198   0.0064   1.0000
  16.000   1.3239   0.07713   0.07126  -0.0201   0.0061   1.0000
  16.250   1.3253   0.08002   0.07426  -0.0203   0.0060   1.0000
  16.500   1.3251   0.08321   0.07752  -0.0207   0.0058   1.0000
  16.750   1.3233   0.08661   0.08101  -0.0212   0.0056   1.0000
  17.000   1.3203   0.09027   0.08476  -0.0218   0.0054   1.0000
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