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WORTMANN FX 76-120 (fx76120-il) Xfoil prediction polar at RE=200,000 Ncrit=9


Details Polar file
Airfoil: WORTMANN FX 76-120 (fx76120-il)
Reynolds number: 200,000
Max Cl/Cd: 49.29 at α=6.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-fx76120-il-200000.txt
Download as CSV file: xf-fx76120-il-200000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: WORTMANN FX 76-120                              
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.200 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -15.250  -0.8257   0.10872   0.10456  -0.0190   1.0000   0.0443
 -15.000  -0.8777   0.09393   0.08966  -0.0279   1.0000   0.0434
 -14.750  -0.9248   0.08151   0.07704  -0.0364   1.0000   0.0426
 -14.500  -0.9638   0.07185   0.06715  -0.0431   1.0000   0.0422
 -14.250  -0.9934   0.06474   0.05981  -0.0473   1.0000   0.0420
 -14.000  -1.0189   0.05891   0.05374  -0.0498   1.0000   0.0418
 -13.750  -1.0386   0.05443   0.04903  -0.0507   1.0000   0.0419
 -13.500  -1.0555   0.05063   0.04499  -0.0505   1.0000   0.0421
 -13.250  -1.0705   0.04759   0.04170  -0.0493   1.0000   0.0427
 -13.000  -1.0817   0.04506   0.03892  -0.0472   1.0000   0.0432
 -12.750  -1.0920   0.04288   0.03648  -0.0443   1.0000   0.0437
 -12.500  -1.1019   0.04145   0.03478  -0.0404   1.0000   0.0442
 -12.250  -1.0949   0.03846   0.03175  -0.0391   1.0000   0.0457
 -12.000  -1.0869   0.03716   0.03044  -0.0369   1.0000   0.0469
 -11.750  -1.0807   0.03573   0.02889  -0.0344   1.0000   0.0479
 -11.500  -1.0728   0.03431   0.02732  -0.0320   1.0000   0.0494
 -11.250  -1.0641   0.03295   0.02574  -0.0296   1.0000   0.0508
 -11.000  -1.0561   0.03197   0.02450  -0.0268   1.0000   0.0523
 -10.750  -1.0402   0.02980   0.02234  -0.0258   1.0000   0.0544
 -10.500  -1.0254   0.02877   0.02130  -0.0241   1.0000   0.0564
 -10.250  -1.0106   0.02770   0.02012  -0.0222   1.0000   0.0585
 -10.000  -0.9960   0.02678   0.01902  -0.0201   1.0000   0.0608
  -9.750  -0.9801   0.02530   0.01750  -0.0185   1.0000   0.0634
  -9.500  -0.9644   0.02438   0.01662  -0.0167   1.0000   0.0663
  -9.250  -0.9482   0.02356   0.01573  -0.0148   1.0000   0.0696
  -9.000  -0.9318   0.02267   0.01472  -0.0129   1.0000   0.0728
  -8.750  -0.9170   0.02161   0.01374  -0.0109   1.0000   0.0767
  -8.500  -0.9006   0.02092   0.01300  -0.0089   1.0000   0.0813
  -8.250  -0.8859   0.01999   0.01208  -0.0067   1.0000   0.0863
  -8.000  -0.8703   0.01933   0.01143  -0.0046   1.0000   0.0925
  -7.750  -0.8558   0.01853   0.01066  -0.0023   1.0000   0.0999
  -7.500  -0.8392   0.01798   0.01006  -0.0002   1.0000   0.1091
  -7.250  -0.8248   0.01729   0.00946   0.0021   1.0000   0.1212
  -7.000  -0.8093   0.01672   0.00895   0.0043   1.0000   0.1361
  -6.750  -0.7936   0.01621   0.00850   0.0065   1.0000   0.1529
  -6.500  -0.7773   0.01577   0.00815   0.0086   1.0000   0.1699
  -6.250  -0.7602   0.01542   0.00784   0.0105   1.0000   0.1866
  -6.000  -0.7426   0.01511   0.00755   0.0124   1.0000   0.2023
  -5.750  -0.7246   0.01483   0.00727   0.0142   1.0000   0.2173
  -5.500  -0.7062   0.01457   0.00702   0.0159   1.0000   0.2317
  -5.250  -0.6876   0.01434   0.00680   0.0176   1.0000   0.2463
  -5.000  -0.6689   0.01411   0.00659   0.0192   1.0000   0.2606
  -4.750  -0.6503   0.01387   0.00639   0.0209   1.0000   0.2755
  -4.500  -0.6317   0.01363   0.00621   0.0225   1.0000   0.2910
  -4.250  -0.6131   0.01341   0.00605   0.0241   1.0000   0.3075
  -4.000  -0.5945   0.01319   0.00589   0.0257   1.0000   0.3252
  -3.750  -0.5762   0.01297   0.00576   0.0273   1.0000   0.3443
  -3.500  -0.5583   0.01274   0.00565   0.0290   1.0000   0.3654
  -3.250  -0.5405   0.01255   0.00557   0.0306   1.0000   0.3898
  -3.000  -0.4994   0.01238   0.00558   0.0276   0.9940   0.4277
  -2.750  -0.4586   0.01216   0.00560   0.0247   0.9877   0.4711
  -2.500  -0.4202   0.01190   0.00560   0.0224   0.9804   0.5206
  -2.250  -0.3831   0.01165   0.00558   0.0206   0.9725   0.5738
  -2.000  -0.3448   0.01138   0.00556   0.0186   0.9643   0.6280
  -1.750  -0.3011   0.01111   0.00554   0.0158   0.9573   0.6810
  -1.500  -0.2643   0.01087   0.00549   0.0145   0.9474   0.7285
  -1.250  -0.2177   0.01068   0.00547   0.0114   0.9415   0.7710
  -1.000  -0.1778   0.01055   0.00545   0.0098   0.9323   0.8054
  -0.750  -0.1251   0.01044   0.00541   0.0056   0.9278   0.8346
  -0.500  -0.0874   0.01037   0.00539   0.0045   0.9160   0.8590
  -0.250  -0.0459   0.01031   0.00535   0.0027   0.9047   0.8787
   0.000  -0.0005   0.01028   0.00533   0.0001   0.8937   0.8943
   0.250   0.0457   0.01032   0.00536  -0.0026   0.8789   0.9049
   0.500   0.0874   0.01037   0.00539  -0.0045   0.8592   0.9160
   0.750   0.1254   0.01044   0.00542  -0.0056   0.8346   0.9279
   1.000   0.1780   0.01055   0.00545  -0.0098   0.8055   0.9323
   1.250   0.2178   0.01068   0.00547  -0.0115   0.7709   0.9413
   1.750   0.3010   0.01111   0.00553  -0.0158   0.6809   0.9573
   2.000   0.3446   0.01138   0.00556  -0.0186   0.6279   0.9642
   2.250   0.3830   0.01164   0.00558  -0.0205   0.5736   0.9724
   2.500   0.4203   0.01190   0.00559  -0.0224   0.5205   0.9804
   2.750   0.4586   0.01216   0.00560  -0.0247   0.4710   0.9877
   3.000   0.4990   0.01238   0.00558  -0.0275   0.4279   0.9939
   3.250   0.5405   0.01255   0.00557  -0.0306   0.3899   1.0000
   3.500   0.5583   0.01274   0.00565  -0.0290   0.3655   1.0000
   3.750   0.5762   0.01297   0.00576  -0.0273   0.3449   1.0000
   4.000   0.5945   0.01319   0.00589  -0.0257   0.3254   1.0000
   4.250   0.6130   0.01340   0.00604  -0.0241   0.3073   1.0000
   4.500   0.6317   0.01363   0.00621  -0.0225   0.2910   1.0000
   4.750   0.6503   0.01386   0.00639  -0.0208   0.2755   1.0000
   5.000   0.6688   0.01412   0.00659  -0.0192   0.2609   1.0000
   5.250   0.6875   0.01434   0.00679  -0.0176   0.2463   1.0000
   5.500   0.7062   0.01457   0.00702  -0.0159   0.2318   1.0000
   5.750   0.7246   0.01482   0.00727  -0.0142   0.2174   1.0000
   6.000   0.7425   0.01511   0.00755  -0.0124   0.2023   1.0000
   6.250   0.7601   0.01542   0.00783  -0.0105   0.1865   1.0000
   6.500   0.7773   0.01577   0.00814  -0.0086   0.1700   1.0000
   6.750   0.7935   0.01621   0.00851  -0.0065   0.1529   1.0000
   7.000   0.8092   0.01673   0.00895  -0.0043   0.1362   1.0000
   7.250   0.8247   0.01730   0.00947  -0.0021   0.1213   1.0000
   7.500   0.8394   0.01796   0.01005   0.0002   0.1094   1.0000
   7.750   0.8558   0.01853   0.01065   0.0023   0.0998   1.0000
   8.000   0.8704   0.01931   0.01141   0.0046   0.0925   1.0000
   8.250   0.8859   0.01998   0.01207   0.0067   0.0863   1.0000
   8.500   0.9006   0.02092   0.01300   0.0089   0.0813   1.0000
   8.750   0.9170   0.02161   0.01374   0.0109   0.0767   1.0000
   9.000   0.9316   0.02271   0.01475   0.0129   0.0726   1.0000
   9.250   0.9481   0.02355   0.01572   0.0148   0.0694   1.0000
   9.500   0.9644   0.02438   0.01662   0.0167   0.0663   1.0000
   9.750   0.9802   0.02531   0.01751   0.0185   0.0634   1.0000
  10.000   0.9961   0.02678   0.01903   0.0201   0.0608   1.0000
  10.250   1.0108   0.02771   0.02013   0.0221   0.0585   1.0000
  10.500   1.0252   0.02873   0.02125   0.0241   0.0562   1.0000
  10.750   1.0403   0.02981   0.02235   0.0257   0.0544   1.0000
  11.000   1.0561   0.03196   0.02450   0.0269   0.0522   1.0000
  11.250   1.0647   0.03299   0.02578   0.0295   0.0509   1.0000
  11.500   1.0729   0.03434   0.02735   0.0320   0.0493   1.0000
  11.750   1.0812   0.03578   0.02895   0.0343   0.0481   1.0000
  12.000   1.0874   0.03710   0.03036   0.0369   0.0468   1.0000
  12.250   1.0968   0.03840   0.03164   0.0388   0.0454   1.0000
  12.500   1.1024   0.04152   0.03487   0.0403   0.0443   1.0000
  12.750   1.0923   0.04289   0.03650   0.0443   0.0437   1.0000
  13.000   1.0832   0.04525   0.03911   0.0470   0.0434   1.0000
  13.250   1.0705   0.04766   0.04178   0.0492   0.0427   1.0000
  13.500   1.0563   0.05070   0.04505   0.0504   0.0422   1.0000
  13.750   1.0397   0.05438   0.04898   0.0506   0.0418   1.0000
  14.000   1.0199   0.05890   0.05373   0.0496   0.0418   1.0000
  14.250   0.9952   0.06459   0.05965   0.0471   0.0418   1.0000
  14.500   0.9644   0.07190   0.06721   0.0427   0.0419   1.0000
  14.750   0.9240   0.08187   0.07742   0.0358   0.0423   1.0000
  15.000   0.8773   0.09431   0.09005   0.0274   0.0433   1.0000
  15.250   0.8305   0.10800   0.10385   0.0192   0.0442   1.0000
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