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LWK 80-080 (lwk80080-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: LWK 80-080 (lwk80080-il)
Reynolds number: 1,000,000
Max Cl/Cd: 57.22 at α=7°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-lwk80080-il-1000000-n5.txt
Download as CSV file: xf-lwk80080-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: LWK 80-080                                      
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -12.000  -0.9267   0.06640   0.06497  -0.0151   1.0000   0.0022
 -11.500  -1.0397   0.04233   0.04025  -0.0190   1.0000   0.0019
 -11.250  -1.0427   0.03876   0.03646  -0.0174   1.0000   0.0019
 -11.000  -1.0739   0.03038   0.02736  -0.0135   1.0000   0.0020
 -10.750  -1.0715   0.02687   0.02346  -0.0114   1.0000   0.0022
 -10.500  -1.0578   0.02505   0.02142  -0.0101   1.0000   0.0022
 -10.250  -1.0333   0.02508   0.02149  -0.0099   1.0000   0.0024
 -10.000  -1.0145   0.02404   0.02033  -0.0091   1.0000   0.0025
  -9.750  -1.0001   0.02205   0.01807  -0.0077   1.0000   0.0026
  -9.500  -0.9804   0.02102   0.01689  -0.0068   1.0000   0.0027
  -9.250  -0.9598   0.02012   0.01585  -0.0060   1.0000   0.0028
  -9.000  -0.9396   0.01912   0.01470  -0.0051   1.0000   0.0030
  -8.750  -0.9183   0.01827   0.01373  -0.0043   1.0000   0.0032
  -8.500  -0.8974   0.01734   0.01266  -0.0034   1.0000   0.0034
  -8.250  -0.8774   0.01618   0.01133  -0.0022   1.0000   0.0036
  -8.000  -0.8560   0.01536   0.01038  -0.0013   1.0000   0.0037
  -7.750  -0.8384   0.01505   0.01004   0.0006   0.9963   0.0039
  -7.500  -0.8059   0.01417   0.00903  -0.0009   0.9792   0.0040
  -7.250  -0.7691   0.01350   0.00822  -0.0033   0.9650   0.0041
  -7.000  -0.7302   0.01247   0.00707  -0.0064   0.9557   0.0053
  -6.750  -0.6889   0.01207   0.00664  -0.0099   0.9459   0.0059
  -6.500  -0.6495   0.01139   0.00584  -0.0129   0.9345   0.0062
  -6.250  -0.6135   0.01086   0.00517  -0.0151   0.9215   0.0064
  -6.000  -0.5818   0.01051   0.00473  -0.0163   0.9086   0.0068
  -5.750  -0.5536   0.01019   0.00429  -0.0166   0.8974   0.0072
  -5.500  -0.5273   0.00989   0.00390  -0.0164   0.8878   0.0075
  -5.250  -0.5019   0.00959   0.00352  -0.0160   0.8794   0.0076
  -4.750  -0.4522   0.00900   0.00285  -0.0149   0.8656   0.0130
  -4.500  -0.4270   0.00879   0.00261  -0.0144   0.8598   0.0169
  -4.250  -0.4016   0.00861   0.00242  -0.0140   0.8546   0.0205
  -4.000  -0.3764   0.00841   0.00221  -0.0135   0.8491   0.0274
  -3.500  -0.3257   0.00807   0.00189  -0.0127   0.8399   0.0447
  -3.250  -0.3012   0.00783   0.00174  -0.0121   0.8352   0.0666
  -3.000  -0.2755   0.00770   0.00159  -0.0117   0.8310   0.0773
  -2.750  -0.2519   0.00737   0.00144  -0.0110   0.8270   0.1245
  -2.500  -0.2280   0.00709   0.00132  -0.0103   0.8227   0.1691
  -2.250  -0.2049   0.00676   0.00118  -0.0094   0.8184   0.2326
  -2.000  -0.1834   0.00632   0.00105  -0.0083   0.8143   0.3221
  -1.750  -0.1625   0.00586   0.00092  -0.0071   0.8098   0.4204
  -1.500  -0.1412   0.00547   0.00080  -0.0058   0.8055   0.5073
  -1.250  -0.1215   0.00506   0.00072  -0.0042   0.8015   0.6079
  -1.000  -0.0982   0.00487   0.00071  -0.0032   0.7968   0.6608
  -0.750  -0.0747   0.00477   0.00071  -0.0022   0.7907   0.7035
  -0.500  -0.0501   0.00471   0.00071  -0.0014   0.7822   0.7283
  -0.250  -0.0254   0.00469   0.00071  -0.0006   0.7712   0.7485
   0.000   0.0000   0.00469   0.00070   0.0000   0.7608   0.7603
   0.250   0.0252   0.00470   0.00070   0.0007   0.7465   0.7715
   0.500   0.0501   0.00471   0.00071   0.0014   0.7278   0.7822
   0.750   0.0745   0.00477   0.00071   0.0022   0.7011   0.7909
   1.000   0.0985   0.00486   0.00071   0.0031   0.6649   0.7968
   1.250   0.1204   0.00511   0.00072   0.0044   0.5952   0.8015
   1.500   0.1405   0.00552   0.00081   0.0060   0.4972   0.8056
   1.750   0.1608   0.00598   0.00094   0.0074   0.3933   0.8099
   2.000   0.1814   0.00647   0.00108   0.0087   0.2891   0.8145
   2.250   0.2042   0.00682   0.00119   0.0096   0.2194   0.8183
   2.500   0.2276   0.00713   0.00132   0.0104   0.1616   0.8225
   2.750   0.2518   0.00738   0.00145   0.0110   0.1216   0.8269
   3.000   0.2752   0.00772   0.00161   0.0117   0.0736   0.8312
   3.250   0.2999   0.00794   0.00175   0.0123   0.0494   0.8356
   3.500   0.3252   0.00811   0.00190   0.0127   0.0382   0.8401
   4.000   0.3759   0.00847   0.00222   0.0136   0.0219   0.8489
   4.250   0.4015   0.00862   0.00242   0.0140   0.0194   0.8544
   4.500   0.4266   0.00883   0.00263   0.0145   0.0144   0.8597
   4.750   0.4516   0.00906   0.00287   0.0150   0.0098   0.8659
   5.250   0.5017   0.00962   0.00356   0.0161   0.0075   0.8799
   5.500   0.5270   0.00993   0.00396   0.0165   0.0072   0.8879
   5.750   0.5537   0.01017   0.00427   0.0165   0.0071   0.8972
   6.000   0.5814   0.01056   0.00479   0.0163   0.0065   0.9081
   6.250   0.6126   0.01096   0.00530   0.0153   0.0063   0.9208
   6.500   0.6489   0.01145   0.00590   0.0131   0.0060   0.9340
   6.750   0.6886   0.01211   0.00667   0.0100   0.0057   0.9457
   7.000   0.7295   0.01275   0.00742   0.0066   0.0053   0.9558
   7.250   0.7695   0.01347   0.00823   0.0033   0.0047   0.9650
   7.500   0.8040   0.01484   0.00980   0.0012   0.0041   0.9810
   8.000   0.8526   0.01605   0.01117   0.0019   0.0040   1.0000
   8.250   0.8762   0.01644   0.01162   0.0024   0.0038   1.0000
   8.500   0.8971   0.01742   0.01275   0.0034   0.0035   1.0000
   8.750   0.9175   0.01848   0.01398   0.0044   0.0034   1.0000
   9.000   0.9359   0.01994   0.01565   0.0056   0.0032   1.0000
   9.250   0.9556   0.02108   0.01695   0.0066   0.0030   1.0000
   9.500   0.9792   0.02131   0.01724   0.0069   0.0028   1.0000
   9.750   0.9940   0.02333   0.01954   0.0084   0.0027   1.0000
  10.000   1.0158   0.02383   0.02009   0.0089   0.0025   1.0000
  10.250   1.0348   0.02485   0.02123   0.0097   0.0024   1.0000
  10.500   1.0400   0.02827   0.02509   0.0119   0.0024   1.0000
  10.750   1.0723   0.02678   0.02336   0.0113   0.0022   1.0000
  11.000   1.0796   0.02954   0.02645   0.0130   0.0022   1.0000
  11.250   1.0835   0.03260   0.02982   0.0149   0.0022   1.0000
  11.500   1.0753   0.03720   0.03479   0.0171   0.0019   1.0000
  11.750   1.0516   0.04306   0.04103   0.0200   0.0020   1.0000
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