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FX 79-L-100 (fx79l100-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: FX 79-L-100 (fx79l100-il)
Reynolds number: 500,000
Max Cl/Cd: 58.11 at α=7.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx79l100-il-500000-n5.txt
Download as CSV file: xf-fx79l100-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: FX 79-L-100                                     
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.500 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -15.750  -1.0196   0.10691   0.10422   0.0156   1.0000   0.0078
 -15.250  -1.0924   0.08207   0.07904   0.0012   1.0000   0.0076
 -15.000  -1.1178   0.07272   0.06953  -0.0047   1.0000   0.0076
 -14.750  -1.1361   0.06527   0.06188  -0.0095   1.0000   0.0077
 -14.500  -1.1555   0.05826   0.05468  -0.0138   1.0000   0.0077
 -14.250  -1.1666   0.05293   0.04918  -0.0169   1.0000   0.0077
 -14.000  -1.1700   0.04902   0.04512  -0.0190   1.0000   0.0078
 -13.750  -1.1804   0.04436   0.04026  -0.0212   1.0000   0.0078
 -13.500  -1.1904   0.04012   0.03585  -0.0228   1.0000   0.0079
 -13.250  -1.1944   0.03690   0.03246  -0.0235   1.0000   0.0080
 -13.000  -1.1941   0.03444   0.02984  -0.0235   1.0000   0.0080
 -12.750  -1.1946   0.03214   0.02741  -0.0228   1.0000   0.0082
 -12.500  -1.1880   0.03069   0.02584  -0.0216   1.0000   0.0084
 -12.250  -1.1801   0.02941   0.02445  -0.0200   1.0000   0.0086
 -12.000  -1.1714   0.02807   0.02297  -0.0183   1.0000   0.0087
 -11.750  -1.1573   0.02699   0.02179  -0.0172   1.0000   0.0091
 -11.500  -1.1432   0.02584   0.02051  -0.0160   1.0000   0.0092
 -11.250  -1.1288   0.02463   0.01916  -0.0147   1.0000   0.0095
 -11.000  -1.1124   0.02358   0.01799  -0.0136   1.0000   0.0098
 -10.750  -1.0945   0.02266   0.01695  -0.0126   1.0000   0.0101
 -10.500  -1.0752   0.02187   0.01604  -0.0116   1.0000   0.0106
 -10.250  -1.0575   0.02087   0.01494  -0.0105   1.0000   0.0111
 -10.000  -1.0386   0.02000   0.01400  -0.0095   1.0000   0.0116
  -9.750  -1.0175   0.01938   0.01333  -0.0087   1.0000   0.0122
  -9.500  -0.9968   0.01869   0.01256  -0.0079   1.0000   0.0127
  -9.250  -0.9755   0.01806   0.01185  -0.0070   1.0000   0.0134
  -9.000  -0.9543   0.01739   0.01109  -0.0061   1.0000   0.0140
  -8.750  -0.9326   0.01680   0.01041  -0.0052   1.0000   0.0145
  -8.500  -0.9115   0.01611   0.00969  -0.0043   1.0000   0.0156
  -8.250  -0.8892   0.01559   0.00913  -0.0035   1.0000   0.0165
  -8.000  -0.8663   0.01514   0.00864  -0.0027   1.0000   0.0177
  -7.750  -0.8433   0.01470   0.00813  -0.0019   1.0000   0.0186
  -7.500  -0.8208   0.01419   0.00757  -0.0011   1.0000   0.0199
  -7.250  -0.7978   0.01376   0.00715  -0.0003   1.0000   0.0218
  -7.000  -0.7745   0.01337   0.00672   0.0005   1.0000   0.0232
  -6.750  -0.7507   0.01304   0.00635   0.0012   1.0000   0.0249
  -6.500  -0.7280   0.01258   0.00589   0.0021   1.0000   0.0271
  -6.250  -0.7046   0.01222   0.00552   0.0029   1.0000   0.0293
  -6.000  -0.6808   0.01192   0.00519   0.0036   1.0000   0.0317
  -5.750  -0.6575   0.01157   0.00483   0.0045   1.0000   0.0346
  -5.250  -0.6017   0.01095   0.00419   0.0042   0.9828   0.0419
  -5.000  -0.5619   0.01057   0.00385   0.0014   0.9633   0.0495
  -4.750  -0.5137   0.01022   0.00352  -0.0033   0.9407   0.0596
  -4.500  -0.4631   0.00988   0.00317  -0.0085   0.9106   0.0745
  -4.250  -0.4250   0.00963   0.00289  -0.0109   0.8744   0.0936
  -4.000  -0.3976   0.00941   0.00266  -0.0108   0.8433   0.1175
  -3.750  -0.3735   0.00913   0.00242  -0.0101   0.8189   0.1528
  -3.500  -0.3508   0.00878   0.00220  -0.0092   0.7973   0.2043
  -3.250  -0.3287   0.00838   0.00197  -0.0081   0.7787   0.2692
  -3.000  -0.3066   0.00799   0.00177  -0.0071   0.7615   0.3369
  -2.750  -0.2838   0.00767   0.00163  -0.0061   0.7471   0.4023
  -2.250  -0.2350   0.00736   0.00149  -0.0045   0.7218   0.4821
  -2.000  -0.2097   0.00727   0.00143  -0.0039   0.7106   0.5113
  -1.750  -0.1840   0.00722   0.00140  -0.0033   0.7005   0.5350
  -1.500  -0.1586   0.00716   0.00138  -0.0027   0.6904   0.5595
  -1.250  -0.1325   0.00712   0.00136  -0.0022   0.6808   0.5777
  -1.000  -0.1064   0.00711   0.00134  -0.0016   0.6721   0.5949
  -0.750  -0.0800   0.00708   0.00132  -0.0012   0.6629   0.6079
  -0.500  -0.0535   0.00707   0.00131  -0.0008   0.6548   0.6190
  -0.250  -0.0267   0.00707   0.00130  -0.0004   0.6460   0.6286
   0.000   0.0000   0.00706   0.00130   0.0000   0.6378   0.6380
   0.250   0.0267   0.00706   0.00130   0.0004   0.6290   0.6461
   0.500   0.0535   0.00707   0.00131   0.0007   0.6192   0.6548
   0.750   0.0799   0.00708   0.00132   0.0012   0.6082   0.6631
   1.000   0.1064   0.00711   0.00134   0.0016   0.5953   0.6722
   1.250   0.1324   0.00712   0.00136   0.0021   0.5781   0.6809
   1.500   0.1584   0.00716   0.00137   0.0027   0.5577   0.6900
   1.750   0.1840   0.00722   0.00140   0.0033   0.5354   0.7003
   2.000   0.2096   0.00727   0.00143   0.0039   0.5106   0.7106
   2.250   0.2349   0.00736   0.00148   0.0045   0.4820   0.7219
   2.750   0.2841   0.00764   0.00163   0.0060   0.4071   0.7475
   3.000   0.3066   0.00798   0.00178   0.0071   0.3389   0.7620
   3.250   0.3283   0.00841   0.00198   0.0082   0.2638   0.7785
   3.500   0.3505   0.00880   0.00220   0.0092   0.2011   0.7968
   3.750   0.3736   0.00911   0.00242   0.0101   0.1558   0.8186
   4.000   0.3976   0.00940   0.00265   0.0108   0.1193   0.8438
   4.250   0.4251   0.00963   0.00289   0.0108   0.0937   0.8753
   4.500   0.4630   0.00989   0.00317   0.0085   0.0737   0.9106
   4.750   0.5132   0.01022   0.00351   0.0034   0.0600   0.9402
   5.000   0.5617   0.01057   0.00385  -0.0013   0.0501   0.9631
   5.250   0.6017   0.01094   0.00419  -0.0042   0.0422   0.9828
   5.750   0.6575   0.01157   0.00484  -0.0045   0.0353   1.0000
   6.000   0.6807   0.01193   0.00520  -0.0036   0.0320   1.0000
   6.250   0.7046   0.01222   0.00552  -0.0029   0.0295   1.0000
   6.500   0.7280   0.01257   0.00586  -0.0021   0.0268   1.0000
   6.750   0.7510   0.01299   0.00630  -0.0013   0.0246   1.0000
   7.000   0.7746   0.01335   0.00670  -0.0005   0.0230   1.0000
   7.250   0.7979   0.01373   0.00712   0.0003   0.0216   1.0000
   7.500   0.8208   0.01418   0.00756   0.0010   0.0200   1.0000
   7.750   0.8435   0.01466   0.00810   0.0019   0.0185   1.0000
   8.000   0.8665   0.01509   0.00858   0.0026   0.0173   1.0000
   8.250   0.8893   0.01556   0.00909   0.0034   0.0163   1.0000
   8.500   0.9114   0.01610   0.00966   0.0042   0.0153   1.0000
   8.750   0.9322   0.01682   0.01042   0.0052   0.0143   1.0000
   9.000   0.9540   0.01741   0.01112   0.0061   0.0137   1.0000
   9.250   0.9756   0.01802   0.01181   0.0070   0.0131   1.0000
   9.500   0.9969   0.01864   0.01250   0.0078   0.0124   1.0000
   9.750   1.0175   0.01935   0.01329   0.0087   0.0120   1.0000
  10.000   1.0379   0.02007   0.01407   0.0096   0.0114   1.0000
  10.250   1.0567   0.02096   0.01502   0.0106   0.0110   1.0000
  10.500   1.0738   0.02202   0.01620   0.0118   0.0106   1.0000
  10.750   1.0917   0.02299   0.01730   0.0129   0.0103   1.0000
  11.000   1.1108   0.02375   0.01818   0.0138   0.0099   1.0000
  11.250   1.1277   0.02473   0.01928   0.0148   0.0095   1.0000
  11.500   1.1426   0.02589   0.02056   0.0160   0.0092   1.0000
  11.750   1.1572   0.02699   0.02178   0.0172   0.0090   1.0000
  12.000   1.1697   0.02825   0.02317   0.0185   0.0088   1.0000
  12.250   1.1789   0.02952   0.02458   0.0201   0.0087   1.0000
  12.500   1.1859   0.03089   0.02607   0.0217   0.0085   1.0000
  12.750   1.1910   0.03252   0.02783   0.0229   0.0083   1.0000
  13.000   1.1937   0.03452   0.02996   0.0235   0.0082   1.0000
  13.250   1.1927   0.03713   0.03272   0.0234   0.0081   1.0000
  13.500   1.1924   0.03993   0.03566   0.0228   0.0080   1.0000
  13.750   1.1838   0.04401   0.03991   0.0212   0.0077   1.0000
  14.000   1.1737   0.04858   0.04466   0.0191   0.0078   1.0000
  14.250   1.1667   0.05300   0.04925   0.0168   0.0079   1.0000
  14.500   1.1494   0.05929   0.05572   0.0131   0.0077   1.0000
  14.750   1.1350   0.06552   0.06213   0.0092   0.0078   1.0000
  15.000   1.1139   0.07343   0.07021   0.0041   0.0078   1.0000
  15.250   1.0868   0.08319   0.08016  -0.0021   0.0078   1.0000
  15.500   1.0577   0.09403   0.09119  -0.0086   0.0079   1.0000
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