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WORTMANN FX 08-S-176 AIRFOIL (fx08s176-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: WORTMANN FX 08-S-176 AIRFOIL (fx08s176-il)
Reynolds number: 200,000
Max Cl/Cd: 50.76 at α=6.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx08s176-il-200000-n5.txt
Download as CSV file: xf-fx08s176-il-200000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: WORTMANN FX 08-S-176 AIRFOIL                    
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.200 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -11.250  -0.0931   0.10275   0.09713  -0.0855   0.6051   0.0162
 -11.000  -0.0891   0.09940   0.09380  -0.0868   0.6042   0.0160
 -10.750  -0.0918   0.09437   0.08881  -0.0893   0.6034   0.0164
 -10.500  -0.0877   0.09167   0.08617  -0.0903   0.6024   0.0170
 -10.250  -0.0752   0.09076   0.08526  -0.0905   0.6011   0.0183
 -10.000  -0.0754   0.08687   0.08141  -0.0923   0.6003   0.0183
  -9.750  -0.0738   0.08352   0.07809  -0.0940   0.5994   0.0193
  -9.500  -0.0774   0.07911   0.07373  -0.0963   0.5986   0.0190
  -9.250  -0.0855   0.07386   0.06854  -0.0994   0.5979   0.0185
  -9.000  -0.0988   0.06782   0.06255  -0.1041   0.5971   0.0183
  -8.750  -0.1231   0.06150   0.05621  -0.1070   0.5965   0.0178
  -8.500  -0.1450   0.05737   0.05202  -0.1061   0.5958   0.0177
  -8.250  -0.1691   0.05229   0.04677  -0.1040   0.5951   0.0173
  -8.000  -0.1778   0.04839   0.04268  -0.1021   0.5943   0.0174
  -7.750  -0.1783   0.04535   0.03944  -0.1004   0.5935   0.0177
  -7.500  -0.1764   0.04217   0.03600  -0.0985   0.5927   0.0180
  -7.250  -0.1707   0.03926   0.03280  -0.0966   0.5919   0.0185
  -7.000  -0.1623   0.03633   0.02952  -0.0948   0.5910   0.0193
  -6.750  -0.1517   0.03329   0.02601  -0.0928   0.5902   0.0208
  -6.500  -0.1385   0.03041   0.02262  -0.0909   0.5890   0.0218
  -6.250  -0.1205   0.02846   0.02026  -0.0895   0.5877   0.0224
  -6.000  -0.1009   0.02656   0.01812  -0.0887   0.5866   0.0232
  -5.750  -0.0782   0.02581   0.01730  -0.0883   0.5854   0.0243
  -5.500  -0.0546   0.02518   0.01655  -0.0879   0.5843   0.0258
  -5.250  -0.0303   0.02422   0.01539  -0.0875   0.5831   0.0270
  -5.000  -0.0052   0.02324   0.01421  -0.0870   0.5820   0.0279
  -4.750   0.0202   0.02242   0.01324  -0.0867   0.5810   0.0287
  -4.500   0.0458   0.02183   0.01250  -0.0864   0.5798   0.0296
  -4.250   0.0701   0.02105   0.01169  -0.0860   0.5787   0.0316
  -4.000   0.0951   0.02058   0.01117  -0.0857   0.5777   0.0330
  -3.750   0.1199   0.02012   0.01065  -0.0853   0.5768   0.0342
  -3.500   0.1446   0.01973   0.01019  -0.0849   0.5760   0.0357
  -3.250   0.1687   0.01943   0.00983  -0.0845   0.5751   0.0373
  -3.000   0.1917   0.01920   0.00960  -0.0839   0.5738   0.0391
  -2.750   0.2150   0.01901   0.00945  -0.0834   0.5724   0.0429
  -2.500   0.2392   0.01891   0.00935  -0.0831   0.5710   0.0485
  -2.250   0.2632   0.01873   0.00920  -0.0827   0.5695   0.0571
  -2.000   0.2878   0.01856   0.00904  -0.0824   0.5680   0.0719
  -1.750   0.3127   0.01842   0.00892  -0.0822   0.5667   0.0902
  -1.250   0.3473   0.01635   0.00879  -0.0801   0.5646   0.6072
  -1.000   0.3551   0.01667   0.00979  -0.0741   0.5637   0.7862
  -0.750   0.3777   0.01709   0.01011  -0.0727   0.5628   0.8327
  -0.500   0.3977   0.01753   0.01048  -0.0703   0.5618   0.8556
  -0.250   0.4196   0.01782   0.01067  -0.0686   0.5609   0.8698
   0.000   0.4379   0.01816   0.01102  -0.0668   0.5592   0.8803
   0.250   0.4581   0.01844   0.01129  -0.0655   0.5573   0.8873
   0.500   0.4798   0.01864   0.01146  -0.0647   0.5553   0.8925
   0.750   0.5005   0.01882   0.01162  -0.0633   0.5536   0.8999
   1.000   0.5213   0.01896   0.01172  -0.0619   0.5521   0.9083
   1.250   0.5438   0.01906   0.01177  -0.0609   0.5507   0.9158
   1.500   0.5689   0.01905   0.01169  -0.0606   0.5494   0.9199
   1.750   0.5976   0.01893   0.01148  -0.0610   0.5479   0.9219
   2.000   0.6273   0.01879   0.01124  -0.0615   0.5466   0.9240
   2.250   0.6418   0.01907   0.01161  -0.0597   0.5427   0.9282
   2.500   0.6613   0.01919   0.01174  -0.0586   0.5397   0.9322
   2.750   0.6856   0.01924   0.01178  -0.0583   0.5378   0.9350
   3.000   0.7112   0.01928   0.01180  -0.0582   0.5363   0.9378
   3.250   0.7375   0.01926   0.01176  -0.0583   0.5349   0.9407
   3.500   0.7638   0.01923   0.01168  -0.0583   0.5337   0.9439
   3.750   0.7912   0.01917   0.01158  -0.0586   0.5326   0.9466
   4.000   0.8078   0.01957   0.01209  -0.0573   0.5295   0.9497
   4.250   0.8245   0.01993   0.01254  -0.0561   0.5263   0.9533
   4.500   0.8460   0.02010   0.01274  -0.0556   0.5241   0.9563
   4.750   0.8700   0.02016   0.01281  -0.0554   0.5223   0.9584
   5.000   0.8961   0.02016   0.01282  -0.0556   0.5208   0.9601
   5.250   0.9257   0.02011   0.01277  -0.0564   0.5196   0.9614
   5.500   0.9568   0.02003   0.01268  -0.0574   0.5185   0.9628
   5.750   0.9597   0.02095   0.01381  -0.0545   0.5132   0.9676
   6.000   0.9782   0.02122   0.01414  -0.0538   0.5101   0.9705
   6.500   1.0335   0.02114   0.01413  -0.0548   0.5064   0.9744
   6.750   1.0660   0.02100   0.01402  -0.0561   0.5051   0.9759
   7.000   1.0617   0.02231   0.01553  -0.0528   0.4990   0.9835
   7.250   1.0809   0.02275   0.01606  -0.0527   0.4956   0.9881
   7.500   1.1083   0.02276   0.01612  -0.0534   0.4935   0.9928
   7.750   1.1383   0.02257   0.01599  -0.0542   0.4920   1.0000
   8.250   1.1150   0.02615   0.01978  -0.0480   0.4794   1.0000
   8.500   1.1478   0.02573   0.01941  -0.0488   0.4781   1.0000
   8.750   1.0870   0.03271   0.02648  -0.0456   0.4606   1.0000
   9.250   1.1303   0.03334   0.02721  -0.0461   0.4510   1.0000
   9.750   1.1405   0.03666   0.03056  -0.0451   0.4262   1.0000
  10.000   1.1698   0.03622   0.03016  -0.0455   0.4197   1.0000
  10.250   1.1831   0.03722   0.03119  -0.0453   0.4109   1.0000
  10.500   1.2117   0.03659   0.03045  -0.0454   0.3938   1.0000
  10.750   1.2152   0.03823   0.03197  -0.0445   0.3721   1.0000
  11.000   1.2221   0.03957   0.03320  -0.0438   0.3541   1.0000
  11.250   1.2216   0.04160   0.03511  -0.0427   0.3349   1.0000
  11.500   1.2255   0.04349   0.03702  -0.0422   0.3234   1.0000
  11.750   1.2210   0.04621   0.03967  -0.0413   0.3021   1.0000
  12.000   1.2154   0.04914   0.04251  -0.0406   0.2769   1.0000
  12.250   1.1942   0.05363   0.04669  -0.0395   0.2295   1.0000
  12.500   1.1606   0.05965   0.05233  -0.0383   0.1794   1.0000
  12.750   1.1377   0.06490   0.05733  -0.0377   0.1357   1.0000
  13.000   1.1139   0.07047   0.06261  -0.0374   0.0888   1.0000
  13.250   1.0920   0.07606   0.06792  -0.0373   0.0449   1.0000
  13.500   1.0844   0.08016   0.07190  -0.0375   0.0182   1.0000
  13.750   1.0836   0.08354   0.07529  -0.0379   0.0135   1.0000
  14.000   1.0863   0.08655   0.07836  -0.0383   0.0117   1.0000
  14.250   1.0905   0.08941   0.08132  -0.0388   0.0110   1.0000
  14.500   1.0941   0.09235   0.08437  -0.0393   0.0103   1.0000
  14.750   1.0972   0.09543   0.08756  -0.0399   0.0098   1.0000
  15.000   1.1002   0.09853   0.09079  -0.0405   0.0095   1.0000
  15.250   1.1033   0.10167   0.09406  -0.0413   0.0093   1.0000
  15.500   1.1067   0.10478   0.09729  -0.0420   0.0091   1.0000
  15.750   1.1092   0.10804   0.10067  -0.0429   0.0089   1.0000
  16.000   1.1117   0.11132   0.10407  -0.0438   0.0088   1.0000
  16.250   1.1137   0.11471   0.10757  -0.0447   0.0086   1.0000
  16.500   1.1157   0.11811   0.11108  -0.0458   0.0084   1.0000
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