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WORTMANN FX 082-512 AIRFOIL (fx082512-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: WORTMANN FX 082-512 AIRFOIL (fx082512-il)
Reynolds number: 1,000,000
Max Cl/Cd: 99.08 at α=-0.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-fx082512-il-1000000.txt
Download as CSV file: xf-fx082512-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: WORTMANN FX 082-512 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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -17.500  -0.7967   0.13053   0.12834  -0.0362   1.0000   0.0098
 -17.250  -0.8234   0.12090   0.11858  -0.0408   1.0000   0.0098
 -17.000  -0.8398   0.11379   0.11137  -0.0442   1.0000   0.0098
 -16.750  -0.8560   0.10702   0.10450  -0.0475   1.0000   0.0099
 -16.500  -0.8682   0.10122   0.09861  -0.0502   1.0000   0.0099
 -16.250  -0.8789   0.09593   0.09324  -0.0526   1.0000   0.0099
 -15.750  -0.9045   0.08532   0.08244  -0.0574   1.0000   0.0101
 -15.500  -0.9157   0.08065   0.07769  -0.0592   1.0000   0.0102
 -15.250  -0.9249   0.07643   0.07339  -0.0608   1.0000   0.0103
 -15.000  -0.9352   0.07231   0.06921  -0.0622   1.0000   0.0105
 -14.750  -0.9430   0.06869   0.06554  -0.0632   1.0000   0.0107
 -14.500  -0.9469   0.06572   0.06254  -0.0638   1.0000   0.0109
 -14.250  -0.9538   0.06267   0.05943  -0.0641   1.0000   0.0109
 -14.000  -0.9585   0.06006   0.05679  -0.0641   1.0000   0.0112
 -13.750  -0.9675   0.05725   0.05393  -0.0639   1.0000   0.0112
 -13.500  -0.9611   0.05451   0.05114  -0.0663   0.9992   0.0115
 -13.250  -0.9522   0.05123   0.04777  -0.0704   0.9975   0.0117
 -13.000  -0.9405   0.04848   0.04496  -0.0742   0.9958   0.0120
 -12.750  -0.9315   0.04571   0.04212  -0.0776   0.9936   0.0122
 -12.500  -0.9250   0.04306   0.03940  -0.0805   0.9901   0.0125
 -12.250  -0.9135   0.04049   0.03675  -0.0844   0.9875   0.0127
 -12.000  -0.8975   0.03805   0.03424  -0.0881   0.9846   0.0129
 -11.750  -0.8846   0.03332   0.02941  -0.0961   0.9796   0.0134
 -11.500  -0.8554   0.02908   0.02507  -0.1061   0.9780   0.0141
 -11.250  -0.8209   0.02592   0.02182  -0.1145   0.9773   0.0148
 -11.000  -0.7960   0.02315   0.01896  -0.1196   0.9738   0.0154
 -10.750  -0.7614   0.02058   0.01627  -0.1260   0.9723   0.0162
 -10.500  -0.7245   0.01836   0.01390  -0.1321   0.9713   0.0175
 -10.250  -0.6893   0.01704   0.01251  -0.1360   0.9705   0.0189
 -10.000  -0.6549   0.01616   0.01155  -0.1389   0.9698   0.0202
  -9.750  -0.6192   0.01512   0.01045  -0.1423   0.9693   0.0228
  -9.500  -0.5845   0.01440   0.00969  -0.1448   0.9687   0.0256
  -9.250  -0.5497   0.01370   0.00900  -0.1474   0.9683   0.0315
  -9.000  -0.5157   0.01331   0.00866  -0.1493   0.9678   0.0382
  -8.750  -0.4820   0.01302   0.00841  -0.1510   0.9674   0.0429
  -8.500  -0.4488   0.01292   0.00830  -0.1522   0.9669   0.0462
  -8.250  -0.4255   0.01289   0.00826  -0.1514   0.9637   0.0476
  -8.000  -0.3947   0.01241   0.00775  -0.1526   0.9619   0.0508
  -7.750  -0.3636   0.01223   0.00760  -0.1536   0.9605   0.0532
  -7.500  -0.3312   0.01204   0.00738  -0.1547   0.9594   0.0551
  -7.250  -0.2986   0.01188   0.00720  -0.1559   0.9585   0.0569
  -7.000  -0.2655   0.01174   0.00705  -0.1571   0.9578   0.0580
  -6.750  -0.2304   0.01128   0.00652  -0.1591   0.9572   0.0598
  -6.500  -0.1947   0.01075   0.00595  -0.1614   0.9568   0.0630
  -6.250  -0.1602   0.01048   0.00569  -0.1630   0.9563   0.0657
  -6.000  -0.1254   0.01020   0.00538  -0.1647   0.9558   0.0677
  -5.750  -0.0903   0.00990   0.00504  -0.1665   0.9554   0.0691
  -5.500  -0.0628   0.00969   0.00480  -0.1665   0.9525   0.0700
  -5.250  -0.0332   0.00948   0.00456  -0.1670   0.9501   0.0707
  -5.000  -0.0004   0.00920   0.00425  -0.1682   0.9488   0.0718
  -4.750   0.0339   0.00882   0.00381  -0.1698   0.9478   0.0755
  -4.500   0.0681   0.00852   0.00349  -0.1712   0.9469   0.0787
  -4.250   0.1027   0.00825   0.00322  -0.1728   0.9460   0.0814
  -4.000   0.1377   0.00802   0.00297  -0.1743   0.9452   0.0840
  -3.750   0.1748   0.00772   0.00267  -0.1763   0.9441   0.0893
  -3.500   0.2188   0.00648   0.00196  -0.1809   0.9432   0.2580
  -3.250   0.2576   0.00632   0.00187  -0.1833   0.9421   0.2861
  -3.000   0.2835   0.00631   0.00189  -0.1827   0.9371   0.2947
  -2.750   0.3193   0.00622   0.00178  -0.1843   0.9332   0.3003
  -2.500   0.3607   0.00612   0.00170  -0.1871   0.9306   0.3058
  -2.250   0.4066   0.00607   0.00164  -0.1910   0.9276   0.3100
  -2.000   0.4306   0.00610   0.00166  -0.1899   0.9196   0.3127
  -1.750   0.4754   0.00604   0.00160  -0.1936   0.9147   0.3163
  -1.500   0.5040   0.00604   0.00161  -0.1936   0.9052   0.3194
  -1.250   0.5395   0.00605   0.00160  -0.1951   0.8949   0.3220
  -1.000   0.5693   0.00607   0.00158  -0.1953   0.8798   0.3240
  -0.750   0.5967   0.00613   0.00155  -0.1949   0.8539   0.3258
  -0.500   0.6212   0.00627   0.00154  -0.1939   0.8176   0.3273
  -0.250   0.6403   0.00657   0.00159  -0.1917   0.7647   0.3284
   0.000   0.6559   0.00696   0.00168  -0.1888   0.6997   0.3305
   0.250   0.6682   0.00761   0.00190  -0.1853   0.6011   0.3331
   0.500   0.6775   0.00889   0.00237  -0.1816   0.4173   0.3353
   0.750   0.6900   0.01026   0.00289  -0.1787   0.2256   0.3372
   1.000   0.7082   0.01119   0.00332  -0.1769   0.0914   0.3389
   1.250   0.7342   0.01137   0.00347  -0.1764   0.0853   0.3403
   1.500   0.7600   0.01157   0.00366  -0.1759   0.0797   0.3416
   1.750   0.7862   0.01173   0.00382  -0.1754   0.0779   0.3427
   2.000   0.8124   0.01188   0.00398  -0.1750   0.0767   0.3437
   2.250   0.8385   0.01202   0.00415  -0.1745   0.0752   0.3451
   2.500   0.8648   0.01216   0.00433  -0.1742   0.0735   0.3476
   2.750   0.8905   0.01234   0.00454  -0.1736   0.0714   0.3496
   3.000   0.9157   0.01258   0.00479  -0.1730   0.0686   0.3513
   3.250   0.9394   0.01297   0.00521  -0.1721   0.0647   0.3530
   3.500   0.9656   0.01306   0.00532  -0.1717   0.0639   0.3547
   3.750   0.9914   0.01321   0.00549  -0.1712   0.0626   0.3564
   4.000   1.0169   0.01337   0.00566  -0.1706   0.0607   0.3580
   4.250   1.0423   0.01354   0.00583  -0.1700   0.0586   0.3593
   4.500   1.0674   0.01373   0.00602  -0.1694   0.0563   0.3612
   4.750   1.0906   0.01412   0.00646  -0.1684   0.0528   0.3637
   5.000   1.1173   0.01414   0.00650  -0.1681   0.0516   0.3660
   5.250   1.1431   0.01422   0.00661  -0.1677   0.0492   0.3683
   5.500   1.1682   0.01436   0.00671  -0.1670   0.0458   0.3707
   5.750   1.1922   0.01456   0.00692  -0.1662   0.0418   0.3731
   6.000   1.2158   0.01477   0.00706  -0.1653   0.0356   0.3750
   6.250   1.2384   0.01507   0.00733  -0.1642   0.0297   0.3776
   6.500   1.2602   0.01544   0.00772  -0.1630   0.0258   0.3806
   6.750   1.2806   0.01595   0.00823  -0.1614   0.0225   0.3833
   7.000   1.3022   0.01631   0.00865  -0.1601   0.0212   0.3862
   7.250   1.3228   0.01675   0.00911  -0.1587   0.0197   0.3889
   7.500   1.3407   0.01744   0.00982  -0.1567   0.0179   0.3911
   7.750   1.3620   0.01780   0.01026  -0.1554   0.0173   0.3952
   8.000   1.3821   0.01826   0.01079  -0.1539   0.0165   0.3991
   8.250   1.4017   0.01876   0.01134  -0.1523   0.0157   0.4030
   8.500   1.4199   0.01938   0.01200  -0.1505   0.0150   0.4067
   8.750   1.4341   0.02041   0.01312  -0.1480   0.0141   0.4121
   9.000   1.4535   0.02090   0.01369  -0.1465   0.0138   0.4182
   9.250   1.4719   0.02148   0.01436  -0.1448   0.0134   0.4248
   9.500   1.4901   0.02209   0.01506  -0.1431   0.0130   0.4335
   9.750   1.5082   0.02272   0.01576  -0.1414   0.0125   0.4448
  10.000   1.5259   0.02337   0.01651  -0.1398   0.0120   0.4625
  10.250   1.5424   0.02416   0.01741  -0.1380   0.0116   0.4952
  10.500   1.5543   0.02557   0.01906  -0.1357   0.0111   0.5636
  10.750   1.5727   0.02656   0.02044  -0.1345   0.0108   0.7153
  11.000   1.5827   0.02694   0.02129  -0.1314   0.0107   1.0000
  11.250   1.5974   0.02783   0.02226  -0.1294   0.0104   1.0000
  11.500   1.6106   0.02886   0.02337  -0.1273   0.0102   1.0000
  11.750   1.6234   0.02993   0.02452  -0.1252   0.0100   1.0000
  12.000   1.6357   0.03103   0.02570  -0.1231   0.0097   1.0000
  12.250   1.6464   0.03227   0.02702  -0.1208   0.0095   1.0000
  12.500   1.6571   0.03351   0.02834  -0.1187   0.0093   1.0000
  12.750   1.6667   0.03484   0.02975  -0.1165   0.0091   1.0000
  13.000   1.6752   0.03629   0.03127  -0.1143   0.0089   1.0000
  13.250   1.6805   0.03811   0.03318  -0.1119   0.0087   1.0000
  13.500   1.6821   0.04037   0.03557  -0.1093   0.0086   1.0000
  13.750   1.6727   0.04402   0.03944  -0.1061   0.0083   1.0000
  14.000   1.6696   0.04700   0.04260  -0.1037   0.0082   1.0000
  14.250   1.6721   0.04928   0.04500  -0.1019   0.0082   1.0000
  14.500   1.6726   0.05187   0.04772  -0.1002   0.0081   1.0000
  14.750   1.6746   0.05431   0.05028  -0.0988   0.0080   1.0000
  15.000   1.6720   0.05746   0.05360  -0.0975   0.0080   1.0000
  15.250   1.6666   0.06112   0.05741  -0.0966   0.0079   1.0000
  15.500   1.6669   0.06408   0.06048  -0.0960   0.0078   1.0000
  15.750   1.6597   0.06829   0.06484  -0.0957   0.0077   1.0000
  16.000   1.6552   0.07226   0.06895  -0.0958   0.0076   1.0000
  16.250   1.6429   0.07772   0.07457  -0.0966   0.0075   1.0000
  16.500   1.6306   0.08345   0.08047  -0.0980   0.0075   1.0000
  16.750   1.6181   0.08954   0.08672  -0.1000   0.0074   1.0000
  17.000   1.5985   0.09739   0.09476  -0.1033   0.0074   1.0000
  17.250   1.5794   0.10562   0.10318  -0.1074   0.0074   1.0000
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