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GOE 493 AIRFOIL (goe493-il) Xfoil prediction polar at RE=100,000 Ncrit=5


Details Polar file
Airfoil: GOE 493 AIRFOIL (goe493-il)
Reynolds number: 100,000
Max Cl/Cd: 51.38 at α=7.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe493-il-100000-n5.txt
Download as CSV file: xf-goe493-il-100000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 493 AIRFOIL                                 
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.100 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -13.250  -0.5868   0.07968   0.07418  -0.0763   1.0000   0.0338
 -13.000  -0.6325   0.06984   0.06418  -0.0814   1.0000   0.0332
 -12.750  -0.6644   0.06356   0.05776  -0.0838   1.0000   0.0330
 -12.500  -0.6911   0.05891   0.05299  -0.0845   1.0000   0.0329
 -12.250  -0.7160   0.05522   0.04922  -0.0841   1.0000   0.0329
 -12.000  -0.7404   0.05222   0.04612  -0.0827   1.0000   0.0330
 -11.750  -0.7650   0.04975   0.04355  -0.0804   1.0000   0.0330
 -11.500  -0.7906   0.04778   0.04150  -0.0770   1.0000   0.0330
 -11.250  -0.7903   0.04499   0.03847  -0.0786   0.9942   0.0338
 -11.000  -0.7852   0.04247   0.03568  -0.0793   0.9874   0.0349
 -10.750  -0.7739   0.04007   0.03293  -0.0802   0.9815   0.0363
 -10.500  -0.7592   0.03826   0.03106  -0.0810   0.9756   0.0381
 -10.250  -0.7427   0.03665   0.02932  -0.0815   0.9701   0.0402
 -10.000  -0.7257   0.03499   0.02741  -0.0817   0.9642   0.0428
  -9.750  -0.7027   0.03337   0.02568  -0.0829   0.9603   0.0454
  -9.500  -0.6895   0.03224   0.02445  -0.0818   0.9531   0.0487
  -9.250  -0.6662   0.03092   0.02297  -0.0825   0.9486   0.0532
  -9.000  -0.6449   0.02989   0.02185  -0.0826   0.9436   0.0584
  -8.750  -0.6265   0.02891   0.02079  -0.0820   0.9373   0.0640
  -8.500  -0.5992   0.02801   0.01973  -0.0829   0.9333   0.0725
  -8.250  -0.5740   0.02728   0.01893  -0.0833   0.9289   0.0812
  -8.000  -0.5557   0.02667   0.01827  -0.0823   0.9221   0.0893
  -7.750  -0.5271   0.02602   0.01751  -0.0832   0.9181   0.1003
  -7.500  -0.4944   0.02538   0.01672  -0.0847   0.9154   0.1121
  -7.250  -0.4797   0.02498   0.01627  -0.0828   0.9074   0.1203
  -7.000  -0.4514   0.02440   0.01562  -0.0834   0.9031   0.1303
  -6.750  -0.4184   0.02384   0.01494  -0.0848   0.9003   0.1418
  -6.500  -0.3994   0.02347   0.01452  -0.0835   0.8935   0.1510
  -6.250  -0.3732   0.02298   0.01400  -0.0835   0.8884   0.1613
  -6.000  -0.3406   0.02246   0.01341  -0.0847   0.8853   0.1735
  -5.750  -0.3052   0.02193   0.01282  -0.0865   0.8830   0.1872
  -5.500  -0.2934   0.02167   0.01257  -0.0837   0.8736   0.1969
  -5.250  -0.2618   0.02119   0.01208  -0.0846   0.8701   0.2121
  -5.000  -0.2270   0.02068   0.01156  -0.0861   0.8675   0.2311
  -4.750  -0.2134   0.02047   0.01138  -0.0836   0.8586   0.2465
  -4.500  -0.1831   0.02004   0.01101  -0.0843   0.8547   0.2706
  -4.250  -0.1494   0.01960   0.01062  -0.0855   0.8519   0.3004
  -4.000  -0.1345   0.01947   0.01055  -0.0832   0.8432   0.3252
  -3.750  -0.1048   0.01916   0.01031  -0.0836   0.8389   0.3581
  -3.500  -0.0710   0.01884   0.01003  -0.0847   0.8361   0.3924
  -3.250  -0.0555   0.01884   0.01007  -0.0824   0.8273   0.4174
  -3.000  -0.0252   0.01864   0.00989  -0.0827   0.8230   0.4469
  -2.750   0.0091   0.01841   0.00965  -0.0838   0.8201   0.4748
  -2.500   0.0245   0.01848   0.00974  -0.0814   0.8111   0.4962
  -2.250   0.0551   0.01831   0.00959  -0.0818   0.8069   0.5206
  -2.000   0.0899   0.01809   0.00935  -0.0829   0.8040   0.5460
  -1.750   0.1043   0.01820   0.00950  -0.0803   0.7946   0.5647
  -1.500   0.1360   0.01801   0.00933  -0.0808   0.7906   0.5864
  -1.250   0.1639   0.01791   0.00924  -0.0806   0.7855   0.6068
  -1.000   0.1851   0.01792   0.00929  -0.0793   0.7780   0.6257
  -0.750   0.2180   0.01774   0.00911  -0.0800   0.7741   0.6467
  -0.500   0.2403   0.01775   0.00918  -0.0788   0.7673   0.6663
  -0.250   0.2664   0.01768   0.00917  -0.0782   0.7612   0.6876
   0.000   0.3001   0.01749   0.00900  -0.0790   0.7575   0.7106
   0.250   0.3187   0.01760   0.00917  -0.0772   0.7494   0.7320
   0.500   0.3482   0.01749   0.00911  -0.0772   0.7442   0.7551
   0.750   0.3837   0.01728   0.00892  -0.0783   0.7407   0.7804
   1.000   0.4001   0.01744   0.00917  -0.0761   0.7316   0.8062
   1.250   0.4347   0.01728   0.00906  -0.0771   0.7270   0.8347
   1.500   0.4659   0.01726   0.00912  -0.0775   0.7196   0.8668
   1.750   0.5108   0.01709   0.00900  -0.0806   0.7120   0.9000
   2.000   0.5592   0.01702   0.00894  -0.0847   0.7028   0.9341
   2.250   0.6117   0.01687   0.00878  -0.0896   0.6951   0.9673
   2.500   0.6531   0.01701   0.00891  -0.0927   0.6869   1.0000
   2.750   0.6763   0.01703   0.00888  -0.0920   0.6797   1.0000
   3.000   0.6942   0.01718   0.00900  -0.0903   0.6716   1.0000
   3.250   0.7186   0.01725   0.00903  -0.0897   0.6642   1.0000
   3.500   0.7389   0.01742   0.00919  -0.0883   0.6562   1.0000
   3.750   0.7633   0.01753   0.00929  -0.0877   0.6486   1.0000
   4.000   0.7849   0.01771   0.00947  -0.0866   0.6407   1.0000
   4.250   0.8092   0.01784   0.00961  -0.0859   0.6327   1.0000
   4.500   0.8304   0.01805   0.00983  -0.0847   0.6242   1.0000
   4.750   0.8556   0.01818   0.00997  -0.0842   0.6162   1.0000
   5.000   0.8757   0.01844   0.01028  -0.0829   0.6075   1.0000
   5.250   0.9018   0.01858   0.01044  -0.0825   0.5996   1.0000
   5.500   0.9201   0.01888   0.01079  -0.0808   0.5901   1.0000
   5.750   0.9488   0.01899   0.01092  -0.0809   0.5820   1.0000
   6.000   0.9639   0.01934   0.01136  -0.0787   0.5716   1.0000
   6.250   0.9872   0.01956   0.01162  -0.0778   0.5624   1.0000
   6.500   1.0086   0.01977   0.01187  -0.0766   0.5514   1.0000
   6.750   1.0238   0.02005   0.01220  -0.0743   0.5378   1.0000
   7.000   1.0385   0.02025   0.01241  -0.0718   0.5214   1.0000
   7.250   1.0507   0.02045   0.01258  -0.0688   0.5033   1.0000
   7.500   1.0573   0.02078   0.01289  -0.0649   0.4828   1.0000
   7.750   1.0627   0.02119   0.01327  -0.0610   0.4601   1.0000
   8.000   1.0683   0.02168   0.01369  -0.0573   0.4349   1.0000
   8.250   1.0743   0.02227   0.01419  -0.0539   0.4090   1.0000
   8.500   1.0805   0.02298   0.01482  -0.0507   0.3835   1.0000
   8.750   1.0879   0.02375   0.01550  -0.0478   0.3612   1.0000
   9.000   1.0943   0.02463   0.01633  -0.0450   0.3380   1.0000
   9.250   1.0989   0.02566   0.01729  -0.0421   0.3143   1.0000
   9.500   1.1022   0.02684   0.01840  -0.0392   0.2862   1.0000
   9.750   1.1026   0.02825   0.01970  -0.0362   0.2499   1.0000
  10.000   1.0961   0.03017   0.02135  -0.0329   0.1964   1.0000
  10.250   1.0861   0.03256   0.02339  -0.0296   0.1574   1.0000
  10.500   1.0821   0.03475   0.02542  -0.0271   0.1294   1.0000
  10.750   1.0797   0.03693   0.02749  -0.0249   0.1070   1.0000
  11.000   1.0780   0.03915   0.02963  -0.0230   0.0921   1.0000
  11.250   1.0761   0.04147   0.03192  -0.0213   0.0833   1.0000
  11.500   1.0771   0.04362   0.03414  -0.0199   0.0765   1.0000
  11.750   1.0760   0.04603   0.03656  -0.0186   0.0720   1.0000
  12.000   1.0771   0.04833   0.03892  -0.0174   0.0681   1.0000
  12.250   1.0795   0.05056   0.04126  -0.0164   0.0650   1.0000
  12.500   1.0813   0.05291   0.04368  -0.0156   0.0624   1.0000
  12.750   1.0822   0.05538   0.04618  -0.0148   0.0603   1.0000
  13.000   1.0869   0.05751   0.04841  -0.0140   0.0580   1.0000
  13.250   1.0929   0.05956   0.05056  -0.0134   0.0556   1.0000
  13.500   1.0987   0.06164   0.05271  -0.0128   0.0535   1.0000
  13.750   1.1047   0.06373   0.05483  -0.0123   0.0518   1.0000
  14.000   1.1116   0.06569   0.05677  -0.0117   0.0501   1.0000
  14.250   1.1213   0.06749   0.05872  -0.0111   0.0483   1.0000
  14.500   1.1299   0.06942   0.06077  -0.0106   0.0465   1.0000
  14.750   1.1380   0.07143   0.06288  -0.0103   0.0448   1.0000
  15.000   1.1461   0.07344   0.06492  -0.0099   0.0434   1.0000
  15.250   1.1570   0.07513   0.06655  -0.0094   0.0418   1.0000
  15.500   1.1625   0.07765   0.06931  -0.0092   0.0405   1.0000
  15.750   1.1684   0.08015   0.07201  -0.0091   0.0392   1.0000
  16.000   1.1730   0.08282   0.07484  -0.0091   0.0380   1.0000
  16.250   1.1763   0.08561   0.07775  -0.0093   0.0369   1.0000
  16.500   1.1804   0.08829   0.08051  -0.0096   0.0358   1.0000
  16.750   1.1892   0.09043   0.08262  -0.0095   0.0347   1.0000
  17.000   1.1847   0.09447   0.08693  -0.0103   0.0340   1.0000
  17.250   1.1785   0.09888   0.09162  -0.0115   0.0334   1.0000
  17.500   1.1704   0.10365   0.09666  -0.0130   0.0327   1.0000
  17.750   1.1612   0.10869   0.10193  -0.0148   0.0322   1.0000
  18.000   1.1502   0.11412   0.10759  -0.0171   0.0317   1.0000
  18.250   1.1377   0.11998   0.11367  -0.0198   0.0312   1.0000
  18.500   1.1231   0.12642   0.12032  -0.0232   0.0308   1.0000
  18.750   1.1063   0.13358   0.12769  -0.0272   0.0305   1.0000
  19.000   1.0824   0.14267   0.13701  -0.0327   0.0304   1.0000
  19.250   1.0178   0.16304   0.15775  -0.0457   0.0315   1.0000
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