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FX 79-L-100 (fx79l100-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: FX 79-L-100 (fx79l100-il)
Reynolds number: 1,000,000
Max Cl/Cd: 70.55 at α=7.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-fx79l100-il-1000000.txt
Download as CSV file: xf-fx79l100-il-1000000.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 =     1.000 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -16.250  -1.0237   0.11818   0.11630   0.0241   1.0000   0.0082
 -16.000  -1.0338   0.11105   0.10909   0.0205   1.0000   0.0079
 -15.750  -1.0523   0.10222   0.10017   0.0158   1.0000   0.0078
 -15.500  -1.0928   0.08853   0.08631   0.0077   1.0000   0.0078
 -15.250  -1.1298   0.07684   0.07446   0.0005   1.0000   0.0076
 -15.000  -1.1580   0.06743   0.06488  -0.0055   1.0000   0.0076
 -14.750  -1.1715   0.06107   0.05836  -0.0096   1.0000   0.0077
 -14.250  -1.1900   0.05091   0.04792  -0.0156   1.0000   0.0077
 -14.000  -1.2113   0.04466   0.04144  -0.0188   1.0000   0.0079
 -13.750  -1.2136   0.04129   0.03795  -0.0202   1.0000   0.0078
 -13.500  -1.2404   0.03539   0.03174  -0.0216   1.0000   0.0080
 -13.250  -1.2440   0.03263   0.02880  -0.0213   1.0000   0.0080
 -13.000  -1.2468   0.03031   0.02632  -0.0201   1.0000   0.0081
 -12.750  -1.2464   0.02850   0.02440  -0.0180   1.0000   0.0085
 -12.500  -1.2357   0.02753   0.02337  -0.0164   1.0000   0.0087
 -12.250  -1.2208   0.02658   0.02235  -0.0154   1.0000   0.0089
 -12.000  -1.2084   0.02523   0.02087  -0.0141   1.0000   0.0090
 -11.750  -1.1913   0.02436   0.01991  -0.0131   1.0000   0.0093
 -11.500  -1.1744   0.02337   0.01882  -0.0121   1.0000   0.0095
 -11.250  -1.1598   0.02197   0.01728  -0.0108   1.0000   0.0096
 -11.000  -1.1412   0.02106   0.01626  -0.0098   1.0000   0.0099
 -10.750  -1.1220   0.02018   0.01529  -0.0089   1.0000   0.0101
 -10.500  -1.1009   0.01950   0.01452  -0.0081   1.0000   0.0105
 -10.250  -1.0794   0.01887   0.01380  -0.0074   1.0000   0.0106
 -10.000  -1.0626   0.01756   0.01235  -0.0060   1.0000   0.0110
  -9.750  -1.0444   0.01648   0.01120  -0.0049   1.0000   0.0118
  -9.500  -1.0219   0.01592   0.01060  -0.0041   1.0000   0.0123
  -9.250  -0.9988   0.01545   0.01009  -0.0035   1.0000   0.0130
  -9.000  -0.9755   0.01498   0.00958  -0.0029   1.0000   0.0136
  -8.750  -0.9514   0.01463   0.00918  -0.0023   1.0000   0.0142
  -8.500  -0.9312   0.01375   0.00821  -0.0012   1.0000   0.0154
  -8.250  -0.9084   0.01323   0.00768  -0.0004   1.0000   0.0165
  -8.000  -0.8841   0.01290   0.00733   0.0002   1.0000   0.0176
  -7.750  -0.8600   0.01254   0.00694   0.0008   1.0000   0.0185
  -7.500  -0.8353   0.01227   0.00662   0.0014   1.0000   0.0190
  -7.250  -0.8140   0.01157   0.00590   0.0025   1.0000   0.0214
  -7.000  -0.7900   0.01124   0.00556   0.0032   1.0000   0.0227
  -6.750  -0.7655   0.01097   0.00527   0.0038   1.0000   0.0242
  -6.500  -0.7413   0.01069   0.00496   0.0045   1.0000   0.0255
  -6.250  -0.7185   0.01025   0.00452   0.0055   1.0000   0.0286
  -6.000  -0.6943   0.01002   0.00430   0.0062   1.0000   0.0312
  -5.750  -0.6701   0.00979   0.00406   0.0069   1.0000   0.0330
  -5.500  -0.6478   0.00940   0.00368   0.0080   1.0000   0.0380
  -5.250  -0.6241   0.00919   0.00347   0.0089   1.0000   0.0412
  -5.000  -0.5923   0.00883   0.00315   0.0079   0.9914   0.0480
  -4.750  -0.5550   0.00858   0.00291   0.0058   0.9818   0.0550
  -4.500  -0.5152   0.00827   0.00266   0.0031   0.9657   0.0674
  -4.250  -0.4633   0.00789   0.00238  -0.0025   0.9487   0.0934
  -4.000  -0.4089   0.00740   0.00207  -0.0088   0.9172   0.1456
  -3.750  -0.3761   0.00702   0.00181  -0.0102   0.8747   0.2099
  -3.500  -0.3538   0.00666   0.00160  -0.0091   0.8408   0.2795
  -3.000  -0.3111   0.00598   0.00129  -0.0065   0.7925   0.4270
  -2.750  -0.2873   0.00583   0.00121  -0.0056   0.7739   0.4697
  -2.500  -0.2624   0.00576   0.00116  -0.0048   0.7573   0.4986
  -2.250  -0.2368   0.00572   0.00111  -0.0042   0.7428   0.5193
  -2.000  -0.2111   0.00569   0.00107  -0.0036   0.7296   0.5385
  -1.750  -0.1850   0.00568   0.00104  -0.0031   0.7176   0.5531
  -1.500  -0.1588   0.00565   0.00101  -0.0026   0.7062   0.5694
  -1.250  -0.1323   0.00563   0.00099  -0.0022   0.6956   0.5830
  -1.000  -0.1061   0.00562   0.00098  -0.0017   0.6856   0.5984
  -0.750  -0.0795   0.00562   0.00097  -0.0013   0.6759   0.6120
  -0.500  -0.0530   0.00560   0.00097  -0.0009   0.6667   0.6230
  -0.250  -0.0268   0.00560   0.00097  -0.0004   0.6570   0.6359
   0.000   0.0000   0.00559   0.00096   0.0000   0.6467   0.6466
   0.250   0.0268   0.00560   0.00097   0.0004   0.6364   0.6567
   0.500   0.0530   0.00560   0.00097   0.0009   0.6248   0.6665
   0.750   0.0794   0.00562   0.00097   0.0013   0.6116   0.6759
   1.000   0.1058   0.00563   0.00098   0.0017   0.5973   0.6859
   1.250   0.1322   0.00563   0.00099   0.0022   0.5829   0.6956
   1.500   0.1587   0.00565   0.00101   0.0026   0.5688   0.7061
   1.750   0.1849   0.00568   0.00103   0.0031   0.5526   0.7175
   2.000   0.2110   0.00569   0.00107   0.0036   0.5382   0.7298
   2.250   0.2367   0.00572   0.00111   0.0042   0.5197   0.7428
   2.500   0.2623   0.00576   0.00116   0.0048   0.4974   0.7573
   2.750   0.2872   0.00584   0.00121   0.0056   0.4688   0.7738
   3.000   0.3110   0.00598   0.00129   0.0065   0.4272   0.7925
   3.250   0.3335   0.00621   0.00141   0.0076   0.3703   0.8145
   3.500   0.3539   0.00664   0.00160   0.0091   0.2835   0.8412
   3.750   0.3759   0.00703   0.00181   0.0102   0.2090   0.8749
   4.000   0.4086   0.00742   0.00207   0.0088   0.1435   0.9170
   4.250   0.4628   0.00788   0.00238   0.0026   0.0942   0.9485
   4.500   0.5149   0.00827   0.00265  -0.0030   0.0676   0.9655
   4.750   0.5550   0.00857   0.00290  -0.0058   0.0557   0.9818
   5.000   0.5924   0.00884   0.00315  -0.0080   0.0482   0.9916
   5.250   0.6240   0.00921   0.00349  -0.0089   0.0413   1.0000
   5.500   0.6477   0.00940   0.00368  -0.0081   0.0379   1.0000
   5.750   0.6700   0.00980   0.00406  -0.0070   0.0326   1.0000
   6.000   0.6944   0.01000   0.00428  -0.0062   0.0313   1.0000
   6.250   0.7186   0.01023   0.00451  -0.0055   0.0290   1.0000
   6.500   0.7417   0.01064   0.00491  -0.0046   0.0259   1.0000
   6.750   0.7655   0.01096   0.00527  -0.0039   0.0243   1.0000
   7.000   0.7901   0.01121   0.00553  -0.0032   0.0226   1.0000
   7.250   0.8142   0.01154   0.00585  -0.0026   0.0212   1.0000
   7.500   0.8357   0.01220   0.00655  -0.0015   0.0190   1.0000
   7.750   0.8606   0.01245   0.00684  -0.0009   0.0182   1.0000
   8.000   0.8847   0.01280   0.00721  -0.0003   0.0170   1.0000
   8.250   0.9086   0.01318   0.00761   0.0003   0.0160   1.0000
   8.500   0.9277   0.01419   0.00868   0.0017   0.0145   1.0000
   8.750   0.9513   0.01462   0.00916   0.0023   0.0141   1.0000
   9.000   0.9746   0.01509   0.00970   0.0030   0.0135   1.0000
   9.250   0.9983   0.01549   0.01013   0.0036   0.0128   1.0000
   9.500   1.0219   0.01590   0.01057   0.0041   0.0121   1.0000
   9.750   1.0438   0.01653   0.01125   0.0049   0.0117   1.0000
  10.000   1.0619   0.01764   0.01244   0.0061   0.0110   1.0000
  10.250   1.0786   0.01895   0.01389   0.0075   0.0106   1.0000
  10.500   1.0995   0.01967   0.01471   0.0083   0.0105   1.0000
  10.750   1.1186   0.02062   0.01576   0.0093   0.0103   1.0000
  11.000   1.1389   0.02133   0.01656   0.0101   0.0100   1.0000
  11.250   1.1578   0.02222   0.01755   0.0110   0.0097   1.0000
  11.500   1.1742   0.02336   0.01882   0.0122   0.0095   1.0000
  11.750   1.1911   0.02435   0.01990   0.0132   0.0093   1.0000
  12.000   1.2058   0.02555   0.02123   0.0143   0.0091   1.0000
  12.250   1.2200   0.02666   0.02245   0.0155   0.0090   1.0000
  12.500   1.2373   0.02735   0.02316   0.0163   0.0087   1.0000
  12.750   1.2424   0.02888   0.02483   0.0184   0.0086   1.0000
  13.000   1.2481   0.03024   0.02628   0.0200   0.0084   1.0000
  13.250   1.2465   0.03246   0.02865   0.0213   0.0083   1.0000
  13.500   1.2438   0.03505   0.03137   0.0215   0.0081   1.0000
  13.750   1.2096   0.04188   0.03856   0.0199   0.0077   1.0000
  14.000   1.2083   0.04512   0.04192   0.0185   0.0078   1.0000
  14.250   1.2094   0.04823   0.04513   0.0169   0.0079   1.0000
  14.500   1.1817   0.05577   0.05292   0.0127   0.0078   1.0000
  14.750   1.1729   0.06087   0.05814   0.0096   0.0078   1.0000
  15.000   1.1555   0.06778   0.06520   0.0053   0.0079   1.0000
  15.250   1.1325   0.07619   0.07378  -0.0001   0.0079   1.0000
  15.500   1.1174   0.08367   0.08137  -0.0048   0.0079   1.0000
  15.750   1.0838   0.09543   0.09329  -0.0119   0.0079   1.0000
  16.000   1.0674   0.10383   0.10179  -0.0166   0.0081   1.0000
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