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GOE 522 AIRFOIL (goe522-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: GOE 522 AIRFOIL (goe522-il)
Reynolds number: 1,000,000
Max Cl/Cd: 70.7 at α=5.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe522-il-1000000-n5.txt
Download as CSV file: xf-goe522-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 522 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
  ------ -------- --------- --------- -------- -------- --------
 -19.500  -0.6127   0.10641   0.10292  -0.0984   0.9898   0.0241
 -19.250  -0.6075   0.10320   0.09967  -0.1007   0.9882   0.0241
 -19.000  -0.6031   0.09981   0.09624  -0.1031   0.9865   0.0242
 -18.750  -0.5997   0.09620   0.09258  -0.1058   0.9849   0.0243
 -18.500  -0.5924   0.09325   0.08960  -0.1081   0.9832   0.0243
 -18.250  -0.5875   0.08976   0.08607  -0.1108   0.9816   0.0244
 -18.000  -0.5814   0.08639   0.08266  -0.1136   0.9801   0.0245
 -17.750  -0.5749   0.08311   0.07933  -0.1164   0.9788   0.0246
 -17.500  -0.5702   0.07987   0.07605  -0.1188   0.9766   0.0246
 -17.250  -0.5667   0.07693   0.07307  -0.1204   0.9727   0.0247
 -17.000  -0.5617   0.07375   0.06985  -0.1229   0.9696   0.0247
 -16.750  -0.5527   0.07077   0.06683  -0.1257   0.9666   0.0247
 -16.500  -0.5436   0.06751   0.06352  -0.1290   0.9640   0.0248
 -16.250  -0.5359   0.06438   0.06033  -0.1319   0.9604   0.0248
 -16.000  -0.5276   0.06125   0.05715  -0.1350   0.9547   0.0249
 -15.750  -0.5167   0.05814   0.05397  -0.1385   0.9499   0.0249
 -15.500  -0.5039   0.05508   0.05085  -0.1424   0.9446   0.0250
 -15.250  -0.4952   0.05211   0.04781  -0.1456   0.9368   0.0250
 -15.000  -0.4827   0.04915   0.04477  -0.1494   0.9302   0.0250
 -14.750  -0.4728   0.04629   0.04184  -0.1528   0.9238   0.0251
 -14.500  -0.4651   0.04312   0.03859  -0.1566   0.9162   0.0252
 -14.250  -0.4484   0.03981   0.03518  -0.1624   0.9103   0.0252
 -14.000  -0.4362   0.03675   0.03204  -0.1669   0.9018   0.0253
 -13.750  -0.4229   0.03388   0.02905  -0.1712   0.8918   0.0254
 -13.500  -0.4147   0.03127   0.02635  -0.1740   0.8819   0.0255
 -13.250  -0.4075   0.02883   0.02379  -0.1763   0.8709   0.0256
 -13.000  -0.4028   0.02665   0.02153  -0.1775   0.8617   0.0256
 -12.750  -0.3982   0.02471   0.01949  -0.1782   0.8514   0.0257
 -12.500  -0.3941   0.02295   0.01764  -0.1784   0.8417   0.0258
 -12.250  -0.3906   0.02146   0.01603  -0.1779   0.8288   0.0258
 -12.000  -0.3887   0.02003   0.01453  -0.1770   0.8174   0.0259
 -11.750  -0.3873   0.01890   0.01329  -0.1753   0.8063   0.0260
 -11.500  -0.3848   0.01802   0.01233  -0.1731   0.7942   0.0261
 -11.250  -0.3832   0.01730   0.01152  -0.1703   0.7831   0.0261
 -11.000  -0.3807   0.01671   0.01086  -0.1671   0.7731   0.0262
 -10.750  -0.3777   0.01625   0.01032  -0.1635   0.7648   0.0262
 -10.500  -0.3739   0.01588   0.00991  -0.1598   0.7566   0.0264
 -10.250  -0.3649   0.01556   0.00951  -0.1568   0.7481   0.0265
 -10.000  -0.3513   0.01522   0.00912  -0.1546   0.7407   0.0265
  -9.750  -0.3360   0.01492   0.00878  -0.1527   0.7314   0.0267
  -9.500  -0.3204   0.01464   0.00842  -0.1507   0.7231   0.0268
  -9.250  -0.3024   0.01434   0.00809  -0.1491   0.7155   0.0270
  -9.000  -0.2844   0.01408   0.00777  -0.1475   0.7073   0.0271
  -8.750  -0.2652   0.01383   0.00747  -0.1460   0.6999   0.0273
  -8.500  -0.2451   0.01360   0.00720  -0.1447   0.6910   0.0275
  -8.250  -0.2260   0.01340   0.00693  -0.1431   0.6811   0.0277
  -8.000  -0.2050   0.01320   0.00668  -0.1419   0.6707   0.0279
  -7.750  -0.1850   0.01303   0.00645  -0.1404   0.6599   0.0280
  -7.500  -0.1640   0.01285   0.00622  -0.1391   0.6481   0.0282
  -7.250  -0.1436   0.01270   0.00601  -0.1377   0.6353   0.0284
  -7.000  -0.1241   0.01259   0.00581  -0.1361   0.6193   0.0285
  -6.750  -0.1058   0.01245   0.00558  -0.1342   0.6001   0.0287
  -6.500  -0.0880   0.01234   0.00536  -0.1323   0.5790   0.0290
  -6.000  -0.0494   0.01215   0.00501  -0.1289   0.5462   0.0295
  -5.750  -0.0288   0.01205   0.00485  -0.1275   0.5356   0.0297
  -5.500  -0.0071   0.01193   0.00469  -0.1262   0.5270   0.0301
  -5.250   0.0137   0.01185   0.00456  -0.1248   0.5186   0.0304
  -5.000   0.0364   0.01174   0.00442  -0.1237   0.5126   0.0306
  -4.750   0.0585   0.01165   0.00430  -0.1225   0.5063   0.0310
  -4.500   0.0792   0.01158   0.00418  -0.1210   0.4999   0.0314
  -4.250   0.0996   0.01150   0.00407  -0.1194   0.4949   0.0317
  -4.000   0.1212   0.01139   0.00395  -0.1180   0.4914   0.0321
  -3.750   0.1424   0.01128   0.00383  -0.1166   0.4875   0.0328
  -3.500   0.1636   0.01119   0.00372  -0.1152   0.4834   0.0337
  -3.250   0.1846   0.01114   0.00364  -0.1137   0.4789   0.0345
  -3.000   0.2058   0.01108   0.00356  -0.1123   0.4739   0.0358
  -2.500   0.2477   0.01068   0.00330  -0.1096   0.4661   0.0778
  -2.250   0.2693   0.01062   0.00325  -0.1083   0.4618   0.0865
  -2.000   0.2905   0.01055   0.00321  -0.1069   0.4579   0.0975
  -1.750   0.3114   0.01047   0.00319  -0.1056   0.4535   0.1163
  -1.500   0.3348   0.01041   0.00319  -0.1046   0.4509   0.1298
  -1.250   0.3577   0.01037   0.00319  -0.1036   0.4472   0.1416
  -1.000   0.3803   0.01037   0.00321  -0.1025   0.4435   0.1513
  -0.750   0.4020   0.01039   0.00324  -0.1012   0.4388   0.1595
  -0.500   0.4235   0.01043   0.00328  -0.1000   0.4345   0.1687
  -0.250   0.4457   0.01037   0.00329  -0.0989   0.4314   0.1899
   0.000   0.4668   0.01023   0.00333  -0.0976   0.4283   0.2415
   0.250   0.4892   0.01023   0.00340  -0.0966   0.4251   0.2618
   0.500   0.5113   0.01028   0.00348  -0.0954   0.4213   0.2770
   0.750   0.5326   0.01037   0.00357  -0.0941   0.4167   0.2863
   1.000   0.5546   0.01045   0.00366  -0.0930   0.4127   0.2946
   1.250   0.5778   0.01053   0.00374  -0.0921   0.4087   0.3001
   1.500   0.5995   0.01061   0.00383  -0.0909   0.4039   0.3089
   1.750   0.6203   0.01072   0.00395  -0.0895   0.3989   0.3186
   2.000   0.6415   0.01086   0.00407  -0.0883   0.3951   0.3243
   2.250   0.6642   0.01093   0.00417  -0.0874   0.3918   0.3332
   2.500   0.6864   0.01103   0.00428  -0.0863   0.3878   0.3383
   2.750   0.7077   0.01116   0.00441  -0.0851   0.3839   0.3452
   3.000   0.7277   0.01130   0.00457  -0.0837   0.3795   0.3558
   3.250   0.7483   0.01145   0.00472  -0.0825   0.3756   0.3656
   3.500   0.7704   0.01155   0.00486  -0.0815   0.3722   0.3770
   3.750   0.7917   0.01169   0.00502  -0.0803   0.3680   0.3877
   4.000   0.8110   0.01187   0.00522  -0.0789   0.3632   0.3992
   4.250   0.8296   0.01208   0.00543  -0.0774   0.3582   0.4148
   4.500   0.8507   0.01221   0.00562  -0.0763   0.3542   0.4322
   4.750   0.8707   0.01238   0.00583  -0.0750   0.3489   0.4503
   5.000   0.8883   0.01264   0.00610  -0.0734   0.3429   0.4678
   5.250   0.9074   0.01286   0.00635  -0.0720   0.3380   0.4827
   5.500   0.9262   0.01310   0.00661  -0.0706   0.3315   0.4960
   5.750   0.9431   0.01343   0.00692  -0.0690   0.3244   0.5094
   6.000   0.9614   0.01369   0.00721  -0.0676   0.3176   0.5243
   6.250   0.9767   0.01408   0.00759  -0.0657   0.3093   0.5382
   6.500   0.9930   0.01443   0.00796  -0.0641   0.3003   0.5567
   6.750   1.0073   0.01487   0.00839  -0.0622   0.2905   0.5718
   7.000   1.0215   0.01532   0.00884  -0.0603   0.2810   0.5882
   7.250   1.0347   0.01583   0.00935  -0.0583   0.2712   0.6071
   7.500   1.0483   0.01633   0.00986  -0.0565   0.2624   0.6276
   7.750   1.0608   0.01687   0.01043  -0.0545   0.2539   0.6524
   8.000   1.0721   0.01746   0.01106  -0.0524   0.2453   0.6831
   8.250   1.0866   0.01786   0.01160  -0.0507   0.2407   0.7308
   8.500   1.2169   0.01871   0.01291  -0.0733   0.2270   0.9962
   8.750   1.2422   0.01931   0.01350  -0.0737   0.2245   1.0000
   9.000   1.2599   0.01992   0.01411  -0.0728   0.2216   1.0000
   9.250   1.2757   0.02064   0.01482  -0.0718   0.2181   1.0000
   9.500   1.2923   0.02134   0.01551  -0.0709   0.2154   1.0000
   9.750   1.3081   0.02210   0.01626  -0.0699   0.2123   1.0000
  10.000   1.3254   0.02279   0.01697  -0.0691   0.2104   1.0000
  10.250   1.3428   0.02348   0.01767  -0.0684   0.2088   1.0000
  10.500   1.3593   0.02424   0.01844  -0.0676   0.2071   1.0000
  10.750   1.3744   0.02510   0.01930  -0.0667   0.2054   1.0000
  11.000   1.3901   0.02593   0.02015  -0.0659   0.2040   1.0000
  11.250   1.4040   0.02689   0.02113  -0.0650   0.2024   1.0000
  11.500   1.4175   0.02791   0.02215  -0.0642   0.2007   1.0000
  11.750   1.4318   0.02888   0.02314  -0.0634   0.1994   1.0000
  12.000   1.4437   0.03004   0.02433  -0.0625   0.1979   1.0000
  12.250   1.4592   0.03095   0.02527  -0.0618   0.1974   1.0000
  12.500   1.4738   0.03194   0.02629  -0.0612   0.1967   1.0000
  12.750   1.4874   0.03303   0.02742  -0.0605   0.1960   1.0000
  13.000   1.5014   0.03408   0.02851  -0.0599   0.1952   1.0000
  13.250   1.5134   0.03531   0.02977  -0.0592   0.1936   1.0000
  13.500   1.5255   0.03654   0.03104  -0.0585   0.1928   1.0000
  13.750   1.5370   0.03783   0.03235  -0.0579   0.1915   1.0000
  14.000   1.5460   0.03935   0.03391  -0.0571   0.1902   1.0000
  14.250   1.5557   0.04081   0.03540  -0.0564   0.1889   1.0000
  14.500   1.5633   0.04250   0.03713  -0.0557   0.1879   1.0000
  14.750   1.5714   0.04414   0.03881  -0.0551   0.1867   1.0000
  15.000   1.5768   0.04608   0.04078  -0.0544   0.1854   1.0000
  15.250   1.5831   0.04792   0.04266  -0.0538   0.1842   1.0000
  15.500   1.5903   0.04971   0.04450  -0.0532   0.1836   1.0000
  15.750   1.6002   0.05127   0.04611  -0.0529   0.1831   1.0000
  16.000   1.6089   0.05296   0.04786  -0.0525   0.1825   1.0000
  16.250   1.6168   0.05474   0.04970  -0.0521   0.1817   1.0000
  16.500   1.6251   0.05647   0.05148  -0.0518   0.1806   1.0000
  16.750   1.6304   0.05853   0.05359  -0.0515   0.1793   1.0000
  17.000   1.6365   0.06049   0.05560  -0.0512   0.1776   1.0000
  17.250   1.6391   0.06286   0.05801  -0.0509   0.1762   1.0000
  17.500   1.6434   0.06503   0.06022  -0.0506   0.1749   1.0000
  17.750   1.6424   0.06783   0.06306  -0.0503   0.1730   1.0000
  18.000   1.6422   0.07049   0.06576  -0.0501   0.1711   1.0000
  18.250   1.6470   0.07266   0.06800  -0.0500   0.1697   1.0000
  18.500   1.6530   0.07468   0.07006  -0.0499   0.1679   1.0000
  18.750   1.6549   0.07718   0.07261  -0.0499   0.1648   1.0000
  19.000   1.6548   0.07992   0.07538  -0.0498   0.1623   1.0000
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