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FX 79-W-151 A (fx79w151a-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: FX 79-W-151 A (fx79w151a-il)
Reynolds number: 200,000
Max Cl/Cd: 71.36 at α=7.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx79w151a-il-200000-n5.txt
Download as CSV file: xf-fx79w151a-il-200000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: FX 79-W-151 A                                   
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.200 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -14.000  -0.5562   0.08884   0.08507  -0.0571   1.0000   0.0177
 -13.750  -0.6021   0.07667   0.07278  -0.0643   1.0000   0.0176
 -13.500  -0.6312   0.06781   0.06382  -0.0699   1.0000   0.0174
 -13.250  -0.6594   0.05879   0.05467  -0.0764   1.0000   0.0172
 -13.000  -0.6842   0.05067   0.04637  -0.0831   1.0000   0.0172
 -12.750  -0.7021   0.04510   0.04064  -0.0872   1.0000   0.0170
 -12.500  -0.7190   0.04102   0.03637  -0.0890   1.0000   0.0173
 -12.250  -0.7176   0.03727   0.03232  -0.0926   0.9725   0.0176
 -12.000  -0.7071   0.03435   0.02917  -0.0955   0.9534   0.0180
 -11.750  -0.6967   0.03231   0.02700  -0.0964   0.9359   0.0187
 -11.500  -0.6883   0.03077   0.02527  -0.0956   0.9202   0.0193
 -11.250  -0.6808   0.02955   0.02387  -0.0937   0.9063   0.0198
 -11.000  -0.6742   0.02838   0.02252  -0.0915   0.8940   0.0206
 -10.750  -0.6648   0.02725   0.02117  -0.0893   0.8835   0.0215
 -10.500  -0.6538   0.02625   0.01996  -0.0872   0.8733   0.0223
 -10.250  -0.6431   0.02528   0.01888  -0.0851   0.8638   0.0238
 -10.000  -0.6287   0.02450   0.01796  -0.0834   0.8556   0.0252
  -9.750  -0.6135   0.02371   0.01701  -0.0817   0.8466   0.0269
  -9.500  -0.5963   0.02295   0.01602  -0.0801   0.8394   0.0288
  -9.250  -0.5815   0.02208   0.01510  -0.0783   0.8307   0.0307
  -9.000  -0.5629   0.02145   0.01432  -0.0770   0.8239   0.0331
  -8.750  -0.5427   0.02088   0.01360  -0.0758   0.8157   0.0360
  -8.500  -0.5243   0.02018   0.01283  -0.0744   0.8090   0.0389
  -8.250  -0.5033   0.01969   0.01222  -0.0734   0.8013   0.0426
  -8.000  -0.4821   0.01915   0.01155  -0.0723   0.7946   0.0463
  -7.750  -0.4607   0.01868   0.01104  -0.0714   0.7873   0.0506
  -7.500  -0.4380   0.01826   0.01046  -0.0705   0.7805   0.0552
  -7.250  -0.4161   0.01781   0.01000  -0.0696   0.7737   0.0603
  -7.000  -0.3927   0.01746   0.00951  -0.0688   0.7667   0.0661
  -6.750  -0.3697   0.01710   0.00911  -0.0680   0.7604   0.0718
  -6.500  -0.3457   0.01681   0.00871  -0.0673   0.7530   0.0781
  -6.250  -0.3220   0.01650   0.00835  -0.0666   0.7473   0.0844
  -6.000  -0.2975   0.01626   0.00800  -0.0660   0.7400   0.0910
  -5.750  -0.2735   0.01597   0.00765  -0.0653   0.7338   0.0971
  -5.500  -0.2488   0.01576   0.00736  -0.0647   0.7271   0.1039
  -5.250  -0.2244   0.01550   0.00704  -0.0641   0.7205   0.1102
  -5.000  -0.1996   0.01529   0.00676  -0.0635   0.7145   0.1171
  -4.750  -0.1750   0.01507   0.00646  -0.0630   0.7075   0.1235
  -4.500  -0.1503   0.01484   0.00618  -0.0624   0.7019   0.1306
  -4.250  -0.1254   0.01465   0.00594  -0.0618   0.6950   0.1378
  -4.000  -0.1009   0.01443   0.00569  -0.0612   0.6889   0.1459
  -3.750  -0.0760   0.01424   0.00545  -0.0607   0.6828   0.1535
  -3.500  -0.0514   0.01404   0.00524  -0.0601   0.6763   0.1622
  -3.250  -0.0265   0.01386   0.00501  -0.0595   0.6710   0.1726
  -3.000  -0.0019   0.01368   0.00484  -0.0589   0.6641   0.1849
  -2.750   0.0227   0.01350   0.00465  -0.0584   0.6581   0.1996
  -2.500   0.0471   0.01332   0.00451  -0.0577   0.6522   0.2192
  -2.250   0.0713   0.01313   0.00437  -0.0571   0.6460   0.2453
  -1.750   0.1187   0.01271   0.00414  -0.0557   0.6345   0.3170
  -1.500   0.1411   0.01245   0.00404  -0.0547   0.6287   0.3721
  -1.250   0.1621   0.01215   0.00397  -0.0534   0.6233   0.4449
  -1.000   0.1823   0.01186   0.00396  -0.0519   0.6173   0.5234
  -0.750   0.2029   0.01159   0.00392  -0.0503   0.6121   0.6009
  -0.500   0.2250   0.01134   0.00395  -0.0490   0.6064   0.6830
  -0.250   0.2553   0.01114   0.00402  -0.0492   0.6005   0.7692
   0.000   0.3079   0.01114   0.00410  -0.0541   0.5952   0.8440
   0.250   0.3646   0.01125   0.00424  -0.0600   0.5883   0.8874
   0.500   0.4141   0.01139   0.00431  -0.0644   0.5825   0.9139
   0.750   0.4539   0.01156   0.00443  -0.0668   0.5766   0.9370
   1.000   0.4944   0.01176   0.00457  -0.0693   0.5704   0.9533
   1.250   0.5347   0.01194   0.00465  -0.0719   0.5653   0.9673
   1.500   0.5789   0.01208   0.00477  -0.0754   0.5587   0.9795
   1.750   0.6210   0.01218   0.00481  -0.0785   0.5528   0.9879
   2.000   0.6604   0.01225   0.00483  -0.0813   0.5473   0.9933
   2.250   0.6991   0.01233   0.00489  -0.0838   0.5414   0.9987
   2.500   0.7262   0.01241   0.00491  -0.0840   0.5363   1.0000
   2.750   0.7477   0.01251   0.00499  -0.0830   0.5308   1.0000
   3.000   0.7694   0.01260   0.00509  -0.0820   0.5253   1.0000
   3.250   0.7912   0.01272   0.00516  -0.0811   0.5205   1.0000
   3.500   0.8128   0.01285   0.00530  -0.0801   0.5152   1.0000
   3.750   0.8345   0.01298   0.00544  -0.0791   0.5100   1.0000
   4.000   0.8563   0.01313   0.00556  -0.0781   0.5054   1.0000
   4.250   0.8778   0.01329   0.00574  -0.0770   0.4998   1.0000
   4.500   0.8992   0.01345   0.00591  -0.0760   0.4944   1.0000
   4.750   0.9210   0.01363   0.00606  -0.0750   0.4900   1.0000
   5.000   0.9424   0.01381   0.00630  -0.0740   0.4849   1.0000
   5.250   0.9636   0.01400   0.00651  -0.0729   0.4798   1.0000
   5.500   0.9852   0.01420   0.00670  -0.0718   0.4754   1.0000
   5.750   1.0061   0.01441   0.00697  -0.0707   0.4702   1.0000
   6.000   1.0269   0.01462   0.00723  -0.0696   0.4651   1.0000
   6.250   1.0482   0.01485   0.00746  -0.0685   0.4609   1.0000
   6.500   1.0690   0.01509   0.00775  -0.0674   0.4563   1.0000
   6.750   1.0892   0.01533   0.00808  -0.0662   0.4512   1.0000
   7.000   1.1099   0.01558   0.00835  -0.0650   0.4467   1.0000
   7.250   1.1304   0.01585   0.00866  -0.0638   0.4424   1.0000
   7.500   1.1496   0.01612   0.00903  -0.0625   0.4371   1.0000
   7.750   1.1696   0.01639   0.00936  -0.0612   0.4326   1.0000
   8.000   1.1902   0.01669   0.00969  -0.0601   0.4285   1.0000
   8.250   1.2077   0.01699   0.01012  -0.0585   0.4227   1.0000
   8.500   1.2257   0.01728   0.01044  -0.0569   0.4166   1.0000
   8.750   1.2407   0.01759   0.01084  -0.0548   0.4086   1.0000
   9.000   1.2507   0.01792   0.01118  -0.0519   0.3959   1.0000
   9.250   1.2542   0.01833   0.01158  -0.0478   0.3795   1.0000
   9.500   1.2520   0.01884   0.01205  -0.0430   0.3609   1.0000
   9.750   1.2498   0.01961   0.01273  -0.0387   0.3400   1.0000
  10.000   1.2512   0.02051   0.01360  -0.0354   0.3174   1.0000
  10.250   1.2534   0.02157   0.01461  -0.0325   0.2971   1.0000
  10.500   1.2536   0.02289   0.01586  -0.0297   0.2709   1.0000
  10.750   1.2507   0.02455   0.01742  -0.0270   0.2425   1.0000
  11.000   1.2386   0.02703   0.01969  -0.0240   0.2057   1.0000
  11.250   1.2299   0.02953   0.02206  -0.0217   0.1779   1.0000
  11.500   1.2167   0.03258   0.02496  -0.0194   0.1472   1.0000
  11.750   1.2045   0.03576   0.02802  -0.0176   0.1195   1.0000
  12.000   1.1933   0.03902   0.03116  -0.0162   0.0953   1.0000
  12.250   1.1836   0.04231   0.03437  -0.0151   0.0754   1.0000
  12.500   1.1741   0.04574   0.03771  -0.0142   0.0567   1.0000
  12.750   1.1639   0.04940   0.04130  -0.0136   0.0412   1.0000
  13.000   1.1591   0.05262   0.04452  -0.0131   0.0332   1.0000
  13.250   1.1560   0.05575   0.04766  -0.0129   0.0279   1.0000
  13.500   1.1542   0.05882   0.05081  -0.0127   0.0247   1.0000
  13.750   1.1511   0.06211   0.05414  -0.0126   0.0220   1.0000
  14.000   1.1485   0.06541   0.05750  -0.0126   0.0197   1.0000
  14.250   1.1491   0.06839   0.06059  -0.0127   0.0191   1.0000
  14.500   1.1478   0.07163   0.06392  -0.0129   0.0176   1.0000
  14.750   1.1455   0.07506   0.06742  -0.0132   0.0166   1.0000
  15.000   1.1414   0.07880   0.07122  -0.0136   0.0158   1.0000
  15.250   1.1408   0.08213   0.07470  -0.0140   0.0153   1.0000
  15.500   1.1403   0.08545   0.07813  -0.0144   0.0149   1.0000
  15.750   1.1397   0.08884   0.08161  -0.0149   0.0143   1.0000
  16.000   1.1380   0.09239   0.08526  -0.0155   0.0138   1.0000
  16.250   1.1370   0.09589   0.08884  -0.0161   0.0136   1.0000
  16.500   1.1357   0.09947   0.09251  -0.0168   0.0131   1.0000
  16.750   1.1336   0.10313   0.09623  -0.0176   0.0126   1.0000
  17.000   1.1315   0.10679   0.09995  -0.0184   0.0123   1.0000
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