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FX 63-120 AIRFOIL (fx63120-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: FX 63-120 AIRFOIL (fx63120-il)
Reynolds number: 1,000,000
Max Cl/Cd: 129.43 at α=3.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx63120-il-1000000-n5.txt
Download as CSV file: xf-fx63120-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: FX 63-120 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  -0.8201   0.04631   0.04380  -0.0975   0.9960   0.0085
 -13.750  -0.8337   0.03773   0.03500  -0.1087   0.9913   0.0086
 -13.500  -0.8239   0.03178   0.02886  -0.1190   0.9866   0.0087
 -13.250  -0.8054   0.02760   0.02450  -0.1272   0.9813   0.0089
 -13.000  -0.7740   0.02441   0.02113  -0.1357   0.9777   0.0091
 -12.750  -0.7404   0.02241   0.01897  -0.1412   0.9758   0.0094
 -12.500  -0.7198   0.02107   0.01751  -0.1424   0.9685   0.0096
 -12.000  -0.6663   0.01879   0.01498  -0.1458   0.9555   0.0100
 -11.750  -0.6365   0.01776   0.01388  -0.1477   0.9485   0.0105
 -11.500  -0.6018   0.01691   0.01296  -0.1502   0.9422   0.0108
 -11.250  -0.5626   0.01619   0.01217  -0.1534   0.9372   0.0114
 -11.000  -0.5197   0.01547   0.01135  -0.1573   0.9319   0.0119
 -10.750  -0.4736   0.01474   0.01051  -0.1619   0.9267   0.0125
 -10.500  -0.4296   0.01406   0.00972  -0.1660   0.9175   0.0130
 -10.250  -0.3910   0.01365   0.00923  -0.1687   0.9049   0.0136
 -10.000  -0.3586   0.01331   0.00878  -0.1701   0.8923   0.0141
  -9.750  -0.3293   0.01299   0.00836  -0.1707   0.8807   0.0147
  -9.500  -0.3007   0.01265   0.00792  -0.1712   0.8706   0.0152
  -9.000  -0.2441   0.01199   0.00708  -0.1720   0.8521   0.0162
  -8.500  -0.1877   0.01164   0.00664  -0.1724   0.8361   0.0173
  -8.250  -0.1595   0.01144   0.00636  -0.1726   0.8279   0.0179
  -8.000  -0.1309   0.01118   0.00603  -0.1729   0.8205   0.0185
  -7.750  -0.1023   0.01095   0.00572  -0.1731   0.8132   0.0190
  -7.500  -0.0736   0.01075   0.00546  -0.1734   0.8066   0.0194
  -7.250  -0.0445   0.01042   0.00508  -0.1739   0.7991   0.0202
  -7.000  -0.0158   0.01024   0.00485  -0.1741   0.7922   0.0207
  -6.750   0.0133   0.01004   0.00461  -0.1745   0.7854   0.0213
  -6.500   0.0421   0.00988   0.00439  -0.1747   0.7787   0.0220
  -6.250   0.0713   0.00970   0.00416  -0.1750   0.7723   0.0226
  -6.000   0.1005   0.00952   0.00392  -0.1753   0.7653   0.0231
  -5.750   0.1296   0.00937   0.00371  -0.1756   0.7588   0.0235
  -5.500   0.1595   0.00908   0.00337  -0.1762   0.7505   0.0243
  -5.250   0.1888   0.00889   0.00312  -0.1765   0.7410   0.0250
  -5.000   0.2178   0.00876   0.00292  -0.1767   0.7304   0.0256
  -4.750   0.2472   0.00862   0.00273  -0.1771   0.7219   0.0263
  -4.500   0.2765   0.00850   0.00256  -0.1774   0.7146   0.0270
  -4.250   0.3061   0.00839   0.00241  -0.1777   0.7084   0.0278
  -4.000   0.3355   0.00829   0.00227  -0.1780   0.7016   0.0284
  -3.750   0.3649   0.00820   0.00213  -0.1782   0.6954   0.0289
  -3.500   0.3949   0.00806   0.00197  -0.1787   0.6891   0.0302
  -3.250   0.4242   0.00798   0.00185  -0.1789   0.6823   0.0314
  -3.000   0.4538   0.00791   0.00176  -0.1792   0.6763   0.0327
  -2.750   0.4831   0.00786   0.00168  -0.1795   0.6699   0.0343
  -2.500   0.5123   0.00781   0.00161  -0.1797   0.6637   0.0378
  -2.250   0.5421   0.00772   0.00155  -0.1801   0.6571   0.0491
  -2.000   0.5717   0.00763   0.00151  -0.1804   0.6503   0.0717
  -1.750   0.6017   0.00753   0.00146  -0.1809   0.6445   0.0994
  -1.500   0.6324   0.00734   0.00142  -0.1816   0.6373   0.1621
  -1.250   0.6641   0.00706   0.00138  -0.1827   0.6304   0.2660
  -1.000   0.6948   0.00690   0.00143  -0.1834   0.6234   0.3525
  -0.500   0.7521   0.00697   0.00149  -0.1836   0.6084   0.3825
  -0.250   0.7804   0.00703   0.00153  -0.1836   0.6001   0.3950
   0.000   0.8091   0.00706   0.00157  -0.1837   0.5917   0.4095
   0.500   0.8651   0.00722   0.00169  -0.1837   0.5642   0.4368
   1.000   0.9199   0.00750   0.00184  -0.1834   0.5280   0.4488
   1.250   0.9474   0.00763   0.00192  -0.1833   0.5131   0.4557
   1.500   0.9748   0.00777   0.00202  -0.1832   0.4974   0.4646
   2.000   1.0294   0.00806   0.00226  -0.1830   0.4673   0.4940
   2.250   1.0565   0.00823   0.00241  -0.1828   0.4510   0.5147
   2.500   1.0833   0.00842   0.00257  -0.1826   0.4340   0.5358
   2.750   1.1101   0.00862   0.00273  -0.1824   0.4192   0.5538
   3.000   1.1369   0.00880   0.00290  -0.1822   0.4067   0.5688
   3.250   1.1636   0.00899   0.00306  -0.1820   0.3933   0.5815
   3.500   1.1897   0.00923   0.00325  -0.1817   0.3763   0.5929
   3.750   1.2155   0.00949   0.00345  -0.1814   0.3576   0.6035
   4.000   1.2407   0.00980   0.00367  -0.1809   0.3337   0.6127
   4.250   1.2650   0.01019   0.00394  -0.1803   0.3066   0.6222
   4.500   1.2896   0.01054   0.00421  -0.1798   0.2837   0.6313
   4.750   1.3140   0.01090   0.00449  -0.1792   0.2637   0.6409
   5.000   1.3377   0.01132   0.00482  -0.1785   0.2396   0.6498
   5.250   1.3609   0.01178   0.00516  -0.1778   0.2170   0.6584
   5.500   1.3849   0.01215   0.00548  -0.1771   0.2006   0.6670
   6.000   1.4320   0.01293   0.00616  -0.1758   0.1694   0.6846
   6.250   1.4549   0.01336   0.00653  -0.1750   0.1529   0.6946
   6.500   1.4775   0.01381   0.00692  -0.1741   0.1371   0.7060
   6.750   1.4991   0.01431   0.00736  -0.1732   0.1202   0.7163
   7.000   1.5201   0.01485   0.00783  -0.1721   0.1043   0.7283
   7.500   1.5632   0.01576   0.00872  -0.1701   0.0852   0.7543
   7.750   1.5844   0.01621   0.00918  -0.1690   0.0786   0.7683
   8.000   1.6060   0.01659   0.00961  -0.1681   0.0743   0.7854
   8.250   1.6259   0.01707   0.01011  -0.1668   0.0687   0.8052
   8.500   1.6464   0.01744   0.01056  -0.1656   0.0651   0.8338
   8.750   1.6561   0.01763   0.01096  -0.1622   0.0613   1.0000
   9.000   1.6713   0.01821   0.01152  -0.1601   0.0556   1.0000
   9.250   1.6857   0.01883   0.01211  -0.1579   0.0495   1.0000
   9.500   1.6999   0.01948   0.01274  -0.1558   0.0445   1.0000
   9.750   1.7127   0.02022   0.01347  -0.1535   0.0398   1.0000
  10.000   1.7271   0.02089   0.01415  -0.1515   0.0373   1.0000
  10.250   1.7408   0.02161   0.01490  -0.1495   0.0353   1.0000
  10.500   1.7531   0.02244   0.01574  -0.1473   0.0332   1.0000
  10.750   1.7663   0.02324   0.01658  -0.1454   0.0318   1.0000
  11.000   1.7795   0.02406   0.01745  -0.1435   0.0308   1.0000
  11.250   1.7918   0.02497   0.01840  -0.1417   0.0297   1.0000
  11.500   1.8025   0.02602   0.01949  -0.1397   0.0283   1.0000
  11.750   1.8121   0.02720   0.02070  -0.1377   0.0268   1.0000
  12.000   1.8235   0.02828   0.02184  -0.1360   0.0260   1.0000
  12.250   1.8343   0.02943   0.02305  -0.1344   0.0249   1.0000
  12.500   1.8439   0.03074   0.02440  -0.1328   0.0235   1.0000
  12.750   1.8516   0.03226   0.02595  -0.1311   0.0220   1.0000
  13.000   1.8603   0.03372   0.02747  -0.1295   0.0207   1.0000
  13.250   1.8674   0.03539   0.02918  -0.1280   0.0187   1.0000
  13.500   1.8730   0.03726   0.03108  -0.1265   0.0167   1.0000
  13.750   1.8772   0.03933   0.03319  -0.1251   0.0146   1.0000
  14.000   1.8808   0.04152   0.03544  -0.1238   0.0130   1.0000
  14.250   1.8837   0.04388   0.03785  -0.1226   0.0117   1.0000
  14.500   1.8861   0.04636   0.04040  -0.1215   0.0107   1.0000
  14.750   1.8889   0.04887   0.04299  -0.1206   0.0100   1.0000
  15.000   1.8902   0.05166   0.04584  -0.1197   0.0093   1.0000
  15.250   1.8910   0.05459   0.04885  -0.1191   0.0088   1.0000
  15.500   1.8920   0.05759   0.05194  -0.1186   0.0084   1.0000
  15.750   1.8927   0.06069   0.05513  -0.1182   0.0080   1.0000
  16.000   1.8925   0.06402   0.05855  -0.1180   0.0076   1.0000
  16.250   1.8913   0.06758   0.06221  -0.1180   0.0073   1.0000
  16.500   1.8892   0.07136   0.06608  -0.1181   0.0071   1.0000
  16.750   1.8857   0.07545   0.07027  -0.1184   0.0068   1.0000
  17.000   1.8804   0.07990   0.07482  -0.1189   0.0064   1.0000
  17.250   1.8772   0.08414   0.07917  -0.1196   0.0063   1.0000
  17.500   1.8734   0.08856   0.08370  -0.1205   0.0061   1.0000
  17.750   1.8682   0.09329   0.08854  -0.1215   0.0059   1.0000
  18.000   1.8628   0.09812   0.09347  -0.1228   0.0058   1.0000
  18.250   1.8558   0.10331   0.09878  -0.1243   0.0056   1.0000
  18.500   1.8484   0.10866   0.10424  -0.1260   0.0055   1.0000
  18.750   1.8404   0.11416   0.10985  -0.1280   0.0053   1.0000
  19.000   1.8311   0.11996   0.11575  -0.1303   0.0051   1.0000
  19.250   1.8223   0.12571   0.12162  -0.1327   0.0050   1.0000
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