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WB-135/35 13.5% smoothed (wb13535sm-il) Xfoil prediction polar at RE=200,000 Ncrit=9


Details Polar file
Airfoil: WB-135/35 13.5% smoothed (wb13535sm-il)
Reynolds number: 200,000
Max Cl/Cd: 73.79 at α=4.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-wb13535sm-il-200000.txt
Download as CSV file: xf-wb13535sm-il-200000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: WB-135/35  13.5%  smoothed                      
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -11.000  -0.5255   0.06691   0.06329  -0.0744   1.0000   0.0358
 -10.750  -0.5339   0.06248   0.05889  -0.0744   1.0000   0.0349
 -10.500  -0.5598   0.05709   0.05350  -0.0760   1.0000   0.0337
 -10.250  -0.5934   0.05417   0.05059  -0.0760   1.0000   0.0339
 -10.000  -0.6295   0.05297   0.04943  -0.0705   1.0000   0.0330
  -9.750  -0.6580   0.05145   0.04784  -0.0667   0.9991   0.0333
  -9.500  -0.6486   0.04479   0.04065  -0.0742   0.9890   0.0331
  -9.250  -0.6326   0.03947   0.03478  -0.0785   0.9814   0.0323
  -9.000  -0.6137   0.03511   0.02986  -0.0808   0.9732   0.0317
  -8.750  -0.5890   0.03180   0.02608  -0.0826   0.9667   0.0315
  -8.500  -0.5611   0.02926   0.02319  -0.0840   0.9602   0.0318
  -8.250  -0.5263   0.02704   0.02068  -0.0863   0.9568   0.0325
  -8.000  -0.4994   0.02543   0.01886  -0.0867   0.9490   0.0337
  -7.750  -0.4629   0.02417   0.01734  -0.0887   0.9448   0.0354
  -7.500  -0.4278   0.02181   0.01496  -0.0910   0.9422   0.0378
  -7.250  -0.4016   0.02061   0.01374  -0.0911   0.9342   0.0400
  -7.000  -0.3677   0.01946   0.01250  -0.0926   0.9297   0.0427
  -6.750  -0.3368   0.01823   0.01120  -0.0936   0.9246   0.0473
  -6.500  -0.3108   0.01735   0.01021  -0.0935   0.9164   0.0539
  -6.250  -0.2796   0.01598   0.00887  -0.0944   0.9119   0.0739
  -6.000  -0.2599   0.01510   0.00848  -0.0934   0.9021   0.1785
  -5.750  -0.2254   0.01506   0.00829  -0.0946   0.8974   0.2051
  -5.500  -0.2004   0.01505   0.00819  -0.0940   0.8889   0.2206
  -5.250  -0.1699   0.01497   0.00804  -0.0944   0.8831   0.2364
  -5.000  -0.1445   0.01499   0.00799  -0.0939   0.8754   0.2509
  -4.750  -0.1167   0.01498   0.00792  -0.0937   0.8690   0.2659
  -4.500  -0.0895   0.01498   0.00780  -0.0935   0.8628   0.2784
  -4.250  -0.0635   0.01478   0.00763  -0.0931   0.8557   0.2871
  -4.000  -0.0331   0.01454   0.00729  -0.0934   0.8510   0.2968
  -3.750  -0.0096   0.01445   0.00717  -0.0925   0.8431   0.3060
  -3.500   0.0187   0.01425   0.00695  -0.0924   0.8380   0.3164
  -3.250   0.0449   0.01413   0.00679  -0.0920   0.8319   0.3278
  -3.000   0.0710   0.01402   0.00663  -0.0916   0.8256   0.3402
  -2.750   0.1006   0.01382   0.00640  -0.0917   0.8209   0.3539
  -2.500   0.1238   0.01371   0.00634  -0.0907   0.8123   0.3675
  -2.250   0.1532   0.01348   0.00606  -0.0906   0.8058   0.3833
  -2.000   0.1767   0.01337   0.00598  -0.0896   0.7966   0.3981
  -1.750   0.2058   0.01320   0.00577  -0.0895   0.7907   0.4148
  -1.500   0.2293   0.01315   0.00576  -0.0886   0.7824   0.4312
  -1.250   0.2577   0.01301   0.00561  -0.0884   0.7763   0.4490
  -1.000   0.2816   0.01295   0.00561  -0.0875   0.7680   0.4659
  -0.750   0.3095   0.01282   0.00548  -0.0872   0.7616   0.4841
  -0.500   0.3339   0.01279   0.00552  -0.0864   0.7544   0.5034
  -0.250   0.3606   0.01273   0.00547  -0.0860   0.7483   0.5253
   0.000   0.3865   0.01265   0.00546  -0.0854   0.7421   0.5471
   0.250   0.4112   0.01257   0.00546  -0.0847   0.7350   0.5724
   0.500   0.4386   0.01243   0.00538  -0.0843   0.7293   0.6013
   0.750   0.4610   0.01230   0.00544  -0.0832   0.7217   0.6344
   1.000   0.4874   0.01204   0.00536  -0.0826   0.7157   0.6824
   1.250   0.5380   0.01146   0.00544  -0.0869   0.7073   0.8569
   1.500   0.6348   0.01131   0.00525  -0.1013   0.6984   1.0000
   1.750   0.6576   0.01139   0.00529  -0.1003   0.6894   1.0000
   2.000   0.6823   0.01146   0.00528  -0.0995   0.6814   1.0000
   2.250   0.7063   0.01151   0.00528  -0.0986   0.6721   1.0000
   2.500   0.7293   0.01157   0.00532  -0.0975   0.6618   1.0000
   2.750   0.7535   0.01161   0.00531  -0.0965   0.6515   1.0000
   3.000   0.7771   0.01165   0.00529  -0.0955   0.6401   1.0000
   3.250   0.7991   0.01171   0.00534  -0.0942   0.6269   1.0000
   3.500   0.8213   0.01176   0.00538  -0.0928   0.6125   1.0000
   3.750   0.8432   0.01182   0.00538  -0.0914   0.5959   1.0000
   4.000   0.8636   0.01190   0.00543  -0.0897   0.5751   1.0000
   4.250   0.8832   0.01202   0.00546  -0.0879   0.5507   1.0000
   4.500   0.9010   0.01221   0.00555  -0.0857   0.5203   1.0000
   4.750   0.9176   0.01252   0.00569  -0.0834   0.4869   1.0000
   5.000   0.9338   0.01295   0.00591  -0.0811   0.4580   1.0000
   5.250   0.9509   0.01341   0.00621  -0.0791   0.4353   1.0000
   5.500   0.9692   0.01389   0.00657  -0.0774   0.4183   1.0000
   5.750   0.9886   0.01435   0.00694  -0.0759   0.4046   1.0000
   6.000   1.0085   0.01480   0.00734  -0.0745   0.3924   1.0000
   6.250   1.0280   0.01526   0.00774  -0.0730   0.3803   1.0000
   6.500   1.0465   0.01572   0.00814  -0.0714   0.3675   1.0000
   6.750   1.0646   0.01619   0.00854  -0.0697   0.3550   1.0000
   7.000   1.0832   0.01657   0.00895  -0.0681   0.3445   1.0000
   7.250   1.1027   0.01699   0.00939  -0.0667   0.3358   1.0000
   7.500   1.1211   0.01746   0.00982  -0.0652   0.3263   1.0000
   7.750   1.1349   0.01778   0.01020  -0.0628   0.3137   1.0000
   8.000   1.1509   0.01815   0.01063  -0.0608   0.3039   1.0000
   8.250   1.1646   0.01857   0.01105  -0.0584   0.2940   1.0000
   8.500   1.1760   0.01892   0.01146  -0.0556   0.2836   1.0000
   8.750   1.1840   0.01931   0.01190  -0.0523   0.2690   1.0000
   9.000   1.1932   0.01977   0.01238  -0.0493   0.2536   1.0000
   9.250   1.2021   0.02030   0.01294  -0.0465   0.2325   1.0000
   9.500   1.2070   0.02114   0.01365  -0.0434   0.1966   1.0000
   9.750   1.2026   0.02273   0.01487  -0.0396   0.1438   1.0000
  10.000   1.1797   0.02587   0.01733  -0.0344   0.0592   1.0000
  10.250   1.1762   0.02791   0.01923  -0.0315   0.0394   1.0000
  10.500   1.1811   0.02944   0.02082  -0.0295   0.0346   1.0000
  10.750   1.1840   0.03118   0.02263  -0.0275   0.0312   1.0000
  11.000   1.1859   0.03306   0.02462  -0.0256   0.0294   1.0000
  11.250   1.1896   0.03487   0.02657  -0.0241   0.0282   1.0000
  11.500   1.1916   0.03688   0.02873  -0.0226   0.0275   1.0000
  11.750   1.1915   0.03915   0.03113  -0.0213   0.0267   1.0000
  12.000   1.1905   0.04158   0.03369  -0.0202   0.0263   1.0000
  12.250   1.1865   0.04441   0.03663  -0.0192   0.0257   1.0000
  12.500   1.1820   0.04738   0.03971  -0.0184   0.0253   1.0000
  12.750   1.1790   0.05031   0.04274  -0.0178   0.0251   1.0000
  13.000   1.1747   0.05346   0.04599  -0.0173   0.0249   1.0000
  13.250   1.1702   0.05673   0.04933  -0.0169   0.0245   1.0000
  13.500   1.1665   0.05994   0.05260  -0.0165   0.0241   1.0000
  13.750   1.1643   0.06294   0.05565  -0.0158   0.0237   1.0000
  14.000   1.1666   0.06529   0.05800  -0.0146   0.0230   1.0000
  14.250   1.1720   0.06760   0.06041  -0.0143   0.0227   1.0000
  14.500   1.1789   0.06970   0.06260  -0.0136   0.0224   1.0000
  14.750   1.1866   0.07174   0.06472  -0.0129   0.0221   1.0000
  15.000   1.1968   0.07349   0.06656  -0.0119   0.0219   1.0000
  15.250   1.2070   0.07538   0.06855  -0.0110   0.0218   1.0000
  15.500   1.2166   0.07746   0.07076  -0.0100   0.0217   1.0000
  15.750   1.2241   0.07991   0.07336  -0.0094   0.0218   1.0000
  16.000   1.2298   0.08271   0.07635  -0.0089   0.0219   1.0000
  16.250   1.2329   0.08591   0.07972  -0.0087   0.0221   1.0000
  16.500   1.2335   0.08955   0.08354  -0.0088   0.0223   1.0000
  16.750   1.2325   0.09354   0.08771  -0.0091   0.0226   1.0000
  17.000   1.2312   0.09796   0.09231  -0.0093   0.0229   1.0000
  17.250   1.2323   0.10206   0.09658  -0.0097   0.0232   1.0000
  17.500   1.2232   0.10610   0.10078  -0.0118   0.0235   1.0000
  17.750   1.2091   0.11158   0.10647  -0.0145   0.0237   1.0000
  18.000   1.1941   0.11764   0.11272  -0.0175   0.0237   1.0000
  18.250   1.1724   0.12516   0.12054  -0.0222   0.0243   1.0000
  18.500   1.1269   0.13840   0.13421  -0.0312   0.0253   1.0000
  18.750   1.0918   0.15066   0.14675  -0.0393   0.0262   1.0000
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