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FX 63-137 13.7% smoothed (fx63137sm-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: FX 63-137 13.7% smoothed (fx63137sm-il)
Reynolds number: 200,000
Max Cl/Cd: 88.87 at α=4.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx63137sm-il-200000-n5.txt
Download as CSV file: xf-fx63137sm-il-200000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: FX 63-137 13.7% 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 =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -10.750  -0.1616   0.11682   0.11309  -0.0676   0.9777   0.0308
 -10.500  -0.1506   0.11288   0.10916  -0.0708   0.9725   0.0313
 -10.250  -0.1531   0.10483   0.10110  -0.0762   0.9654   0.0238
 -10.000  -0.1380   0.10248   0.09875  -0.0772   0.9583   0.0226
  -9.500  -0.1207   0.09377   0.09005  -0.0833   0.9434   0.0213
  -9.250  -0.1146   0.08750   0.08377  -0.0885   0.9377   0.0204
  -9.000  -0.1048   0.08340   0.07967  -0.0919   0.9294   0.0207
  -8.750  -0.0935   0.07797   0.07424  -0.0975   0.9238   0.0207
  -8.250  -0.1454   0.03782   0.03326  -0.1486   0.8915   0.0197
  -8.000  -0.1219   0.03140   0.02614  -0.1605   0.8804   0.0198
  -7.750  -0.0851   0.02832   0.02271  -0.1668   0.8751   0.0201
  -7.500  -0.0548   0.02623   0.02036  -0.1702   0.8674   0.0206
  -7.250  -0.0197   0.02429   0.01810  -0.1738   0.8611   0.0211
  -7.000   0.0160   0.02249   0.01598  -0.1771   0.8554   0.0217
  -6.750   0.0466   0.02108   0.01428  -0.1788   0.8478   0.0225
  -6.500   0.0819   0.01983   0.01267  -0.1811   0.8419   0.0237
  -6.250   0.1117   0.01904   0.01185  -0.1821   0.8351   0.0247
  -6.000   0.1425   0.01824   0.01094  -0.1832   0.8283   0.0257
  -5.500   0.2043   0.01676   0.00919  -0.1851   0.8155   0.0277
  -5.250   0.2363   0.01610   0.00849  -0.1864   0.8092   0.0289
  -5.000   0.2686   0.01561   0.00794  -0.1876   0.8033   0.0308
  -4.750   0.2990   0.01516   0.00743  -0.1885   0.7964   0.0334
  -4.500   0.3323   0.01472   0.00694  -0.1899   0.7905   0.0362
  -4.250   0.3647   0.01430   0.00645  -0.1911   0.7843   0.0396
  -4.000   0.3964   0.01397   0.00607  -0.1922   0.7776   0.0454
  -3.750   0.4306   0.01361   0.00568  -0.1937   0.7720   0.0558
  -3.500   0.4625   0.01326   0.00540  -0.1949   0.7654   0.0779
  -3.250   0.4960   0.01287   0.00513  -0.1965   0.7589   0.1248
  -3.000   0.5328   0.01233   0.00488  -0.1990   0.7536   0.2271
  -2.750   0.5653   0.01202   0.00492  -0.2004   0.7465   0.3398
  -2.500   0.5961   0.01199   0.00495  -0.2010   0.7402   0.3977
  -2.250   0.6258   0.01203   0.00498  -0.2013   0.7341   0.4310
  -2.000   0.6545   0.01209   0.00500  -0.2013   0.7271   0.4518
  -1.750   0.6841   0.01215   0.00498  -0.2015   0.7211   0.4689
  -1.500   0.7123   0.01222   0.00505  -0.2014   0.7141   0.4891
  -1.250   0.7408   0.01231   0.00510  -0.2014   0.7074   0.5075
  -1.000   0.7694   0.01237   0.00512  -0.2014   0.7011   0.5176
  -0.750   0.7976   0.01244   0.00514  -0.2014   0.6938   0.5277
  -0.500   0.8261   0.01250   0.00516  -0.2014   0.6874   0.5356
  -0.250   0.8542   0.01258   0.00519  -0.2014   0.6802   0.5451
   0.000   0.8820   0.01264   0.00525  -0.2013   0.6730   0.5526
   0.250   0.9102   0.01273   0.00529  -0.2013   0.6662   0.5619
   0.500   0.9374   0.01281   0.00538  -0.2010   0.6584   0.5695
   0.750   0.9656   0.01292   0.00542  -0.2010   0.6518   0.5786
   1.000   0.9924   0.01301   0.00554  -0.2007   0.6435   0.5866
   1.250   1.0203   0.01313   0.00561  -0.2007   0.6364   0.5958
   1.500   1.0469   0.01323   0.00575  -0.2004   0.6281   0.6040
   1.750   1.0743   0.01336   0.00584  -0.2002   0.6203   0.6136
   2.000   1.1007   0.01348   0.00600  -0.1999   0.6118   0.6221
   2.250   1.1277   0.01363   0.00611  -0.1996   0.6036   0.6318
   2.500   1.1538   0.01376   0.00630  -0.1992   0.5949   0.6408
   3.000   1.2059   0.01408   0.00663  -0.1985   0.5771   0.6604
   3.250   1.2320   0.01427   0.00679  -0.1981   0.5684   0.6708
   3.500   1.2572   0.01444   0.00702  -0.1976   0.5586   0.6814
   3.750   1.2825   0.01464   0.00723  -0.1970   0.5494   0.6918
   4.000   1.3076   0.01485   0.00746  -0.1965   0.5395   0.7033
   4.250   1.3321   0.01506   0.00772  -0.1958   0.5297   0.7145
   4.500   1.3562   0.01530   0.00796  -0.1951   0.5198   0.7262
   4.750   1.3802   0.01553   0.00824  -0.1944   0.5092   0.7387
   5.000   1.4030   0.01580   0.00853  -0.1934   0.4972   0.7517
   5.250   1.4240   0.01610   0.00882  -0.1921   0.4820   0.7650
   5.500   1.4435   0.01645   0.00914  -0.1906   0.4640   0.7790
   5.750   1.4616   0.01683   0.00948  -0.1887   0.4442   0.7943
   6.000   1.4790   0.01724   0.00987  -0.1868   0.4261   0.8110
   6.250   1.4963   0.01764   0.01026  -0.1849   0.4107   0.8297
   6.500   1.5125   0.01803   0.01067  -0.1828   0.3967   0.8522
   6.750   1.5252   0.01840   0.01106  -0.1800   0.3832   0.8837
   7.000   1.5321   0.01872   0.01141  -0.1760   0.3701   1.0000
   7.500   1.5627   0.02000   0.01260  -0.1722   0.3394   1.0000
   7.750   1.5769   0.02071   0.01328  -0.1701   0.3244   1.0000
   8.000   1.5899   0.02149   0.01403  -0.1680   0.3092   1.0000
   8.250   1.6013   0.02237   0.01487  -0.1656   0.2933   1.0000
   8.500   1.6114   0.02335   0.01581  -0.1632   0.2770   1.0000
   8.750   1.6204   0.02443   0.01686  -0.1607   0.2605   1.0000
   9.000   1.6284   0.02563   0.01801  -0.1583   0.2442   1.0000
   9.250   1.6357   0.02692   0.01927  -0.1559   0.2283   1.0000
   9.500   1.6421   0.02835   0.02066  -0.1535   0.2124   1.0000
   9.750   1.6476   0.02992   0.02219  -0.1512   0.1962   1.0000
  10.000   1.6521   0.03164   0.02388  -0.1490   0.1800   1.0000
  10.250   1.6557   0.03352   0.02572  -0.1468   0.1645   1.0000
  10.500   1.6586   0.03553   0.02770  -0.1448   0.1506   1.0000
  10.750   1.6611   0.03768   0.02983  -0.1429   0.1390   1.0000
  11.000   1.6653   0.03976   0.03192  -0.1413   0.1294   1.0000
  11.250   1.6685   0.04199   0.03419  -0.1398   0.1221   1.0000
  11.500   1.6721   0.04426   0.03650  -0.1384   0.1160   1.0000
  11.750   1.6744   0.04674   0.03902  -0.1371   0.1111   1.0000
  12.000   1.6791   0.04904   0.04140  -0.1360   0.1066   1.0000
  12.250   1.6814   0.05165   0.04407  -0.1349   0.1027   1.0000
  12.500   1.6814   0.05461   0.04706  -0.1339   0.0995   1.0000
  12.750   1.6868   0.05702   0.04961  -0.1332   0.0965   1.0000
  13.000   1.6903   0.05971   0.05239  -0.1325   0.0938   1.0000
  13.250   1.6924   0.06263   0.05539  -0.1319   0.0914   1.0000
  13.500   1.6931   0.06579   0.05862  -0.1314   0.0893   1.0000
  13.750   1.6924   0.06920   0.06207  -0.1310   0.0874   1.0000
  14.000   1.6972   0.07194   0.06496  -0.1307   0.0857   1.0000
  14.250   1.7011   0.07485   0.06799  -0.1305   0.0838   1.0000
  14.500   1.7045   0.07786   0.07112  -0.1304   0.0820   1.0000
  14.750   1.7066   0.08109   0.07445  -0.1304   0.0802   1.0000
  15.000   1.7081   0.08445   0.07788  -0.1305   0.0787   1.0000
  15.250   1.7090   0.08788   0.08137  -0.1306   0.0773   1.0000
  15.500   1.7108   0.09118   0.08472  -0.1307   0.0760   1.0000
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