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LWK 80-100 (lwk80100-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: LWK 80-100 (lwk80100-il)
Reynolds number: 1,000,000
Max Cl/Cd: 61.39 at α=7.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-lwk80100-il-1000000-n5.txt
Download as CSV file: xf-lwk80100-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: LWK 80-100                                      
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     1.000 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -15.750  -1.1445   0.07063   0.06842  -0.0154   1.0000   0.0036
 -15.500  -1.1827   0.05895   0.05648  -0.0236   1.0000   0.0035
 -15.250  -1.2088   0.05157   0.04889  -0.0275   1.0000   0.0034
 -15.000  -1.2379   0.04498   0.04203  -0.0294   1.0000   0.0034
 -14.750  -1.2291   0.04335   0.04036  -0.0296   1.0000   0.0035
 -14.500  -1.2334   0.04035   0.03723  -0.0296   1.0000   0.0036
 -14.250  -1.2432   0.03700   0.03369  -0.0290   1.0000   0.0036
 -14.000  -1.2389   0.03519   0.03176  -0.0283   1.0000   0.0037
 -13.750  -1.2386   0.03306   0.02949  -0.0271   1.0000   0.0037
 -13.500  -1.2294   0.03183   0.02817  -0.0262   1.0000   0.0039
 -13.250  -1.2304   0.02972   0.02588  -0.0243   1.0000   0.0039
 -13.000  -1.2191   0.02875   0.02483  -0.0231   1.0000   0.0040
 -12.750  -1.2160   0.02710   0.02301  -0.0208   1.0000   0.0040
 -12.500  -1.2017   0.02640   0.02224  -0.0194   1.0000   0.0043
 -12.250  -1.1931   0.02517   0.02087  -0.0173   1.0000   0.0043
 -12.000  -1.1795   0.02408   0.01966  -0.0158   1.0000   0.0044
 -11.750  -1.1637   0.02315   0.01862  -0.0146   1.0000   0.0045
 -11.500  -1.1477   0.02219   0.01754  -0.0133   1.0000   0.0045
 -11.250  -1.1302   0.02136   0.01659  -0.0122   1.0000   0.0045
 -10.750  -1.0953   0.01952   0.01452  -0.0098   1.0000   0.0047
 -10.250  -1.0663   0.01763   0.01244  -0.0058   0.9924   0.0052
 -10.000  -1.0259   0.01674   0.01144  -0.0095   0.9633   0.0054
  -9.750  -0.9815   0.01592   0.01053  -0.0140   0.9515   0.0058
  -9.500  -0.9379   0.01526   0.00976  -0.0182   0.9388   0.0061
  -9.250  -0.8983   0.01464   0.00904  -0.0215   0.9244   0.0064
  -9.000  -0.8660   0.01419   0.00847  -0.0230   0.9091   0.0070
  -8.750  -0.8393   0.01378   0.00796  -0.0232   0.8959   0.0072
  -8.250  -0.7935   0.01284   0.00682  -0.0219   0.8764   0.0077
  -8.000  -0.7708   0.01245   0.00637  -0.0212   0.8691   0.0086
  -7.750  -0.7477   0.01210   0.00597  -0.0205   0.8628   0.0092
  -7.500  -0.7242   0.01182   0.00563  -0.0198   0.8572   0.0099
  -7.250  -0.7005   0.01153   0.00528  -0.0192   0.8525   0.0104
  -7.000  -0.6774   0.01119   0.00493  -0.0184   0.8475   0.0124
  -6.750  -0.6537   0.01092   0.00463  -0.0178   0.8429   0.0145
  -6.500  -0.6295   0.01069   0.00436  -0.0172   0.8388   0.0159
  -6.250  -0.6058   0.01040   0.00408  -0.0165   0.8347   0.0193
  -6.000  -0.5813   0.01019   0.00384  -0.0160   0.8310   0.0214
  -5.500  -0.5323   0.00974   0.00338  -0.0149   0.8240   0.0282
  -5.250  -0.5072   0.00955   0.00317  -0.0144   0.8203   0.0309
  -5.000  -0.4828   0.00932   0.00297  -0.0139   0.8169   0.0382
  -4.750  -0.4577   0.00915   0.00278  -0.0134   0.8139   0.0438
  -4.500  -0.4328   0.00894   0.00261  -0.0129   0.8110   0.0517
  -4.250  -0.4078   0.00873   0.00243  -0.0124   0.8076   0.0623
  -4.000  -0.3826   0.00856   0.00228  -0.0120   0.8043   0.0719
  -3.750  -0.3574   0.00838   0.00213  -0.0115   0.8013   0.0842
  -3.500  -0.3328   0.00817   0.00198  -0.0110   0.7985   0.1053
  -3.250  -0.3080   0.00794   0.00184  -0.0105   0.7955   0.1287
  -3.000  -0.2839   0.00766   0.00170  -0.0098   0.7924   0.1653
  -2.750  -0.2604   0.00736   0.00156  -0.0091   0.7893   0.2113
  -2.500  -0.2373   0.00703   0.00142  -0.0083   0.7863   0.2666
  -2.250  -0.2151   0.00666   0.00127  -0.0073   0.7835   0.3359
  -2.000  -0.1921   0.00633   0.00116  -0.0065   0.7804   0.3970
  -1.750  -0.1713   0.00587   0.00102  -0.0052   0.7772   0.4856
  -1.500  -0.1518   0.00541   0.00091  -0.0036   0.7739   0.5838
  -1.250  -0.1286   0.00521   0.00087  -0.0026   0.7708   0.6368
  -1.000  -0.1034   0.00512   0.00086  -0.0020   0.7675   0.6688
  -0.750  -0.0783   0.00504   0.00088  -0.0013   0.7627   0.6993
  -0.500  -0.0524   0.00502   0.00087  -0.0009   0.7565   0.7151
  -0.250  -0.0262   0.00500   0.00087  -0.0004   0.7479   0.7287
   0.000  -0.0001   0.00501   0.00086   0.0000   0.7384   0.7396
   0.250   0.0260   0.00500   0.00087   0.0005   0.7274   0.7482
   0.500   0.0526   0.00502   0.00087   0.0008   0.7159   0.7560
   0.750   0.0783   0.00504   0.00087   0.0014   0.6981   0.7623
   1.000   0.1034   0.00512   0.00086   0.0020   0.6681   0.7675
   1.250   0.1285   0.00522   0.00087   0.0026   0.6344   0.7707
   1.500   0.1518   0.00542   0.00091   0.0036   0.5823   0.7739
   1.750   0.1700   0.00596   0.00104   0.0055   0.4680   0.7773
   2.000   0.1917   0.00636   0.00117   0.0066   0.3905   0.7806
   2.250   0.2150   0.00667   0.00128   0.0074   0.3336   0.7835
   2.500   0.2382   0.00698   0.00141   0.0082   0.2780   0.7863
   2.750   0.2607   0.00734   0.00155   0.0091   0.2157   0.7893
   3.000   0.2834   0.00770   0.00170   0.0099   0.1576   0.7924
   3.250   0.3081   0.00794   0.00183   0.0105   0.1292   0.7955
   3.750   0.3575   0.00838   0.00213   0.0115   0.0846   0.8013
   4.000   0.3826   0.00855   0.00228   0.0120   0.0723   0.8043
   4.250   0.4080   0.00873   0.00243   0.0124   0.0635   0.8077
   4.500   0.4329   0.00894   0.00261   0.0129   0.0528   0.8110
   4.750   0.4577   0.00915   0.00278   0.0134   0.0431   0.8139
   5.000   0.4827   0.00933   0.00296   0.0139   0.0369   0.8169
   5.250   0.5072   0.00955   0.00316   0.0144   0.0304   0.8204
   5.500   0.5323   0.00974   0.00337   0.0149   0.0278   0.8241
   6.000   0.5813   0.01018   0.00384   0.0160   0.0211   0.8309
   6.250   0.6056   0.01042   0.00408   0.0166   0.0181   0.8347
   6.500   0.6294   0.01069   0.00436   0.0172   0.0150   0.8388
   6.750   0.6534   0.01095   0.00464   0.0178   0.0129   0.8429
   7.000   0.6767   0.01126   0.00498   0.0186   0.0107   0.8475
   7.250   0.7005   0.01153   0.00529   0.0192   0.0102   0.8524
   7.500   0.7240   0.01184   0.00564   0.0199   0.0091   0.8573
   7.750   0.7471   0.01217   0.00602   0.0206   0.0085   0.8628
   8.000   0.7698   0.01255   0.00645   0.0214   0.0079   0.8691
   8.250   0.7920   0.01301   0.00701   0.0222   0.0073   0.8765
   8.750   0.8393   0.01379   0.00797   0.0233   0.0069   0.8961
   9.000   0.8659   0.01420   0.00848   0.0231   0.0066   0.9092
   9.250   0.8977   0.01476   0.00917   0.0216   0.0064   0.9248
   9.500   0.9377   0.01539   0.00991   0.0182   0.0059   0.9394
   9.750   0.9816   0.01607   0.01070   0.0139   0.0057   0.9522
  10.000   1.0263   0.01686   0.01157   0.0094   0.0053   0.9641
  10.250   1.0583   0.01781   0.01262   0.0076   0.0051   1.0000
  10.500   1.0761   0.01876   0.01368   0.0088   0.0049   1.0000
  10.750   1.0926   0.01985   0.01490   0.0102   0.0047   1.0000
  11.000   1.1090   0.02089   0.01606   0.0115   0.0046   1.0000
  11.250   1.1273   0.02167   0.01695   0.0126   0.0046   1.0000
  11.500   1.1443   0.02259   0.01799   0.0138   0.0045   1.0000
  11.750   1.1594   0.02363   0.01915   0.0151   0.0045   1.0000
  12.000   1.1763   0.02443   0.02004   0.0162   0.0044   1.0000
  12.250   1.1921   0.02524   0.02095   0.0174   0.0043   1.0000
  12.500   1.1987   0.02665   0.02251   0.0198   0.0042   1.0000
  12.750   1.2078   0.02779   0.02378   0.0217   0.0041   1.0000
  13.000   1.2158   0.02904   0.02515   0.0234   0.0041   1.0000
  13.250   1.2212   0.03055   0.02679   0.0251   0.0039   1.0000
  13.500   1.2164   0.03302   0.02947   0.0270   0.0040   1.0000
  13.750   1.2360   0.03332   0.02976   0.0273   0.0038   1.0000
  14.000   1.2345   0.03563   0.03224   0.0284   0.0037   1.0000
  14.250   1.2316   0.03820   0.03498   0.0292   0.0037   1.0000
  14.500   1.2202   0.04183   0.03881   0.0296   0.0036   1.0000
  14.750   1.2211   0.04431   0.04139   0.0294   0.0036   1.0000
  15.000   1.2021   0.04948   0.04676   0.0281   0.0036   1.0000
  15.250   1.1865   0.05487   0.05232   0.0257   0.0036   1.0000
  15.500   1.1279   0.06976   0.06756   0.0157   0.0037   1.0000
  15.750   1.1382   0.07235   0.07017   0.0140   0.0036   1.0000
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