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WORTMANN FX 08-S-176 AIRFOIL (fx08s176-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: WORTMANN FX 08-S-176 AIRFOIL (fx08s176-il)
Reynolds number: 1,000,000
Max Cl/Cd: 139.29 at α=6°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx08s176-il-1000000-n5.txt
Download as CSV file: xf-fx08s176-il-1000000-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 =     1.000 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -14.000  -0.6743   0.03540   0.03133  -0.1177   0.5681   0.0049
 -13.750  -0.6893   0.03246   0.02820  -0.1155   0.5674   0.0049
 -13.500  -0.6986   0.03011   0.02566  -0.1128   0.5667   0.0049
 -13.250  -0.6984   0.02849   0.02391  -0.1105   0.5659   0.0050
 -13.000  -0.6985   0.02690   0.02216  -0.1078   0.5650   0.0052
 -12.750  -0.6948   0.02571   0.02083  -0.1051   0.5642   0.0053
 -12.500  -0.6911   0.02466   0.01965  -0.1021   0.5634   0.0053
 -12.250  -0.6819   0.02360   0.01845  -0.0999   0.5625   0.0054
 -12.000  -0.6686   0.02270   0.01740  -0.0982   0.5616   0.0055
 -11.750  -0.6543   0.02178   0.01635  -0.0967   0.5607   0.0056
 -11.500  -0.6385   0.02088   0.01534  -0.0953   0.5602   0.0058
 -11.250  -0.6205   0.02014   0.01449  -0.0942   0.5596   0.0060
 -11.000  -0.6006   0.01951   0.01380  -0.0933   0.5590   0.0063
 -10.750  -0.5790   0.01905   0.01330  -0.0926   0.5581   0.0066
 -10.500  -0.5568   0.01862   0.01282  -0.0919   0.5573   0.0069
 -10.250  -0.5342   0.01821   0.01236  -0.0913   0.5564   0.0073
 -10.000  -0.5125   0.01766   0.01171  -0.0906   0.5555   0.0075
  -9.750  -0.4894   0.01725   0.01122  -0.0901   0.5547   0.0079
  -9.500  -0.4664   0.01679   0.01068  -0.0895   0.5539   0.0081
  -9.250  -0.4435   0.01629   0.01010  -0.0889   0.5531   0.0084
  -9.000  -0.4195   0.01591   0.00968  -0.0885   0.5522   0.0088
  -8.750  -0.3947   0.01564   0.00938  -0.0882   0.5514   0.0092
  -8.500  -0.3692   0.01545   0.00915  -0.0880   0.5506   0.0096
  -8.250  -0.3443   0.01516   0.00881  -0.0876   0.5498   0.0099
  -8.000  -0.3190   0.01491   0.00852  -0.0874   0.5490   0.0104
  -7.750  -0.2938   0.01463   0.00817  -0.0871   0.5480   0.0108
  -7.500  -0.2684   0.01438   0.00786  -0.0869   0.5470   0.0113
  -7.250  -0.2425   0.01417   0.00759  -0.0867   0.5461   0.0116
  -7.000  -0.2159   0.01401   0.00740  -0.0866   0.5455   0.0118
  -6.750  -0.1920   0.01344   0.00678  -0.0862   0.5449   0.0125
  -6.500  -0.1660   0.01319   0.00652  -0.0860   0.5442   0.0129
  -6.250  -0.1396   0.01297   0.00628  -0.0860   0.5435   0.0134
  -6.000  -0.1131   0.01278   0.00606  -0.0859   0.5428   0.0139
  -5.750  -0.0866   0.01257   0.00582  -0.0858   0.5421   0.0145
  -5.500  -0.0599   0.01237   0.00559  -0.0858   0.5413   0.0152
  -5.250  -0.0336   0.01213   0.00531  -0.0857   0.5405   0.0156
  -5.000  -0.0069   0.01192   0.00507  -0.0856   0.5397   0.0160
  -4.750   0.0201   0.01176   0.00488  -0.0856   0.5389   0.0163
  -4.500   0.0468   0.01156   0.00465  -0.0856   0.5380   0.0165
  -4.250   0.0721   0.01116   0.00419  -0.0854   0.5370   0.0172
  -4.000   0.0984   0.01089   0.00389  -0.0853   0.5361   0.0179
  -3.750   0.1254   0.01071   0.00368  -0.0853   0.5353   0.0185
  -3.500   0.1525   0.01055   0.00350  -0.0853   0.5345   0.0192
  -3.250   0.1798   0.01042   0.00335  -0.0854   0.5336   0.0200
  -3.000   0.2073   0.01031   0.00321  -0.0856   0.5327   0.0208
  -2.750   0.2350   0.01021   0.00308  -0.0857   0.5319   0.0215
  -2.500   0.2630   0.01010   0.00296  -0.0860   0.5313   0.0220
  -2.250   0.2910   0.00999   0.00285  -0.0862   0.5306   0.0227
  -2.000   0.3191   0.00988   0.00273  -0.0864   0.5297   0.0245
  -1.750   0.3472   0.00978   0.00265  -0.0867   0.5288   0.0273
  -1.500   0.3753   0.00967   0.00258  -0.0870   0.5278   0.0360
  -1.250   0.4034   0.00953   0.00253  -0.0873   0.5267   0.0582
  -1.000   0.4317   0.00946   0.00247  -0.0877   0.5253   0.0681
  -0.750   0.4601   0.00938   0.00241  -0.0880   0.5238   0.0789
  -0.500   0.4883   0.00927   0.00236  -0.0884   0.5224   0.0990
  -0.250   0.5159   0.00900   0.00231  -0.0888   0.5209   0.1842
   0.000   0.5419   0.00767   0.00219  -0.0899   0.5195   0.6048
   0.250   0.5711   0.00729   0.00219  -0.0907   0.5180   0.7249
   0.500   0.5985   0.00725   0.00238  -0.0906   0.5169   0.7991
   0.750   0.6270   0.00734   0.00249  -0.0909   0.5154   0.8210
   1.000   0.6566   0.00741   0.00255  -0.0914   0.5137   0.8317
   1.250   0.6847   0.00748   0.00262  -0.0916   0.5120   0.8366
   1.500   0.7136   0.00755   0.00268  -0.0921   0.5105   0.8411
   1.750   0.7429   0.00761   0.00272  -0.0926   0.5091   0.8452
   2.000   0.7719   0.00766   0.00274  -0.0931   0.5077   0.8471
   2.250   0.7999   0.00773   0.00280  -0.0934   0.5062   0.8494
   2.500   0.8273   0.00783   0.00290  -0.0935   0.5045   0.8535
   2.750   0.8563   0.00788   0.00296  -0.0940   0.5032   0.8555
   3.000   0.8854   0.00793   0.00302  -0.0946   0.5017   0.8570
   3.250   0.9145   0.00799   0.00308  -0.0952   0.5001   0.8588
   3.500   0.9436   0.00804   0.00314  -0.0958   0.4983   0.8602
   3.750   0.9726   0.00810   0.00319  -0.0964   0.4965   0.8611
   4.000   1.0009   0.00814   0.00325  -0.0969   0.4946   0.8620
   4.250   1.0290   0.00820   0.00331  -0.0973   0.4927   0.8629
   4.500   1.0566   0.00828   0.00338  -0.0976   0.4908   0.8641
   4.750   1.0849   0.00834   0.00348  -0.0981   0.4890   0.8652
   5.000   1.1131   0.00840   0.00358  -0.0986   0.4868   0.8662
   5.250   1.1411   0.00846   0.00366  -0.0990   0.4831   0.8672
   5.500   1.1678   0.00855   0.00374  -0.0992   0.4766   0.8682
   5.750   1.1954   0.00863   0.00384  -0.0996   0.4701   0.8692
   6.000   1.2216   0.00877   0.00395  -0.0997   0.4634   0.8704
   6.250   1.2456   0.00900   0.00412  -0.0995   0.4434   0.8717
   6.500   1.2615   0.00965   0.00456  -0.0979   0.4050   0.8733
   6.750   1.2766   0.01035   0.00510  -0.0963   0.3738   0.8746
   7.000   1.2895   0.01111   0.00571  -0.0943   0.3454   0.8759
   7.250   1.2997   0.01185   0.00634  -0.0918   0.3209   0.8775
   7.500   1.3032   0.01275   0.00709  -0.0882   0.2911   0.8792
   7.750   1.2817   0.01410   0.00824  -0.0803   0.2477   0.8820
   8.000   1.2465   0.01625   0.01024  -0.0715   0.2099   0.8851
   8.250   1.2173   0.01927   0.01322  -0.0662   0.1861   0.8881
   8.500   1.1876   0.02346   0.01735  -0.0626   0.1582   0.8904
   8.750   1.1668   0.02697   0.02079  -0.0596   0.1341   0.8923
   9.000   1.1339   0.03124   0.02495  -0.0558   0.0985   0.8943
   9.250   1.1196   0.03425   0.02788  -0.0534   0.0752   0.8958
   9.500   1.0974   0.03792   0.03143  -0.0507   0.0399   0.8975
   9.750   1.0896   0.04071   0.03415  -0.0492   0.0174   0.8988
  10.000   1.0913   0.04290   0.03633  -0.0483   0.0077   0.8998
  10.250   1.1001   0.04453   0.03800  -0.0479   0.0066   0.9006
  10.500   1.1100   0.04609   0.03960  -0.0476   0.0059   0.9015
  10.750   1.1192   0.04776   0.04130  -0.0474   0.0056   0.9023
  11.000   1.1283   0.04947   0.04306  -0.0471   0.0054   0.9031
  11.250   1.1375   0.05120   0.04482  -0.0469   0.0050   0.9038
  11.500   1.1467   0.05295   0.04662  -0.0468   0.0048   0.9045
  12.000   1.1615   0.05688   0.05065  -0.0464   0.0042   0.9061
  12.250   1.1688   0.05889   0.05271  -0.0463   0.0041   0.9070
  12.500   1.1721   0.06139   0.05528  -0.0461   0.0037   0.9078
  12.750   1.1817   0.06322   0.05715  -0.0462   0.0036   0.9087
  13.000   1.1890   0.06534   0.05932  -0.0462   0.0035   0.9097
  13.250   1.1954   0.06759   0.06163  -0.0463   0.0033   0.9107
  13.500   1.2024   0.06980   0.06389  -0.0464   0.0033   0.9117
  13.750   1.2086   0.07215   0.06630  -0.0466   0.0031   0.9126
  14.000   1.2136   0.07472   0.06894  -0.0468   0.0030   0.9135
  14.250   1.2205   0.07706   0.07132  -0.0471   0.0029   0.9143
  14.500   1.2252   0.07972   0.07404  -0.0475   0.0028   0.9151
  14.750   1.2298   0.08242   0.07680  -0.0479   0.0027   0.9159
  15.000   1.2352   0.08505   0.07949  -0.0484   0.0027   0.9167
  15.250   1.2395   0.08790   0.08239  -0.0489   0.0026   0.9174
  15.500   1.2445   0.09064   0.08518  -0.0495   0.0025   0.9181
  16.000   1.2494   0.09694   0.09161  -0.0509   0.0024   0.9196
  16.250   1.2476   0.10076   0.09552  -0.0517   0.0023   0.9203
  16.500   1.2467   0.10447   0.09932  -0.0526   0.0022   0.9211
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