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LWK 80-100 (lwk80100-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: LWK 80-100 (lwk80100-il)
Reynolds number: 1,000,000
Max Cl/Cd: 60.48 at α=7.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-lwk80100-il-1000000.txt
Download as CSV file: xf-lwk80100-il-1000000.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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -13.750  -0.9745   0.06924   0.06738  -0.0168   1.0000   0.0060
 -13.500  -0.9899   0.06141   0.05942  -0.0230   1.0000   0.0060
 -13.250  -1.0389   0.05044   0.04813  -0.0290   1.0000   0.0059
 -13.000  -1.0376   0.04790   0.04551  -0.0298   1.0000   0.0059
 -12.750  -1.0779   0.04075   0.03800  -0.0299   1.0000   0.0058
 -12.500  -1.0628   0.04024   0.03747  -0.0297   1.0000   0.0062
 -12.250  -1.0802   0.03634   0.03331  -0.0280   1.0000   0.0062
 -12.000  -1.0849   0.03393   0.03070  -0.0260   1.0000   0.0063
 -11.750  -1.0869   0.03184   0.02842  -0.0235   1.0000   0.0064
 -11.500  -1.0820   0.03042   0.02686  -0.0212   1.0000   0.0065
 -11.250  -1.0699   0.02940   0.02572  -0.0196   1.0000   0.0068
 -11.000  -1.0600   0.02781   0.02396  -0.0178   1.0000   0.0069
 -10.750  -1.0505   0.02596   0.02190  -0.0159   1.0000   0.0070
 -10.500  -1.0284   0.02588   0.02176  -0.0153   1.0000   0.0072
 -10.250  -1.0281   0.02222   0.01769  -0.0122   1.0000   0.0075
 -10.000  -1.0126   0.02083   0.01614  -0.0107   1.0000   0.0075
  -9.750  -0.9990   0.01911   0.01424  -0.0089   1.0000   0.0078
  -9.500  -0.9807   0.01814   0.01316  -0.0077   1.0000   0.0081
  -9.250  -0.9614   0.01729   0.01223  -0.0066   1.0000   0.0083
  -9.000  -0.9406   0.01665   0.01154  -0.0057   1.0000   0.0088
  -8.750  -0.9254   0.01608   0.01092  -0.0034   0.9943   0.0092
  -8.500  -0.8885   0.01518   0.00992  -0.0061   0.9748   0.0097
  -8.250  -0.8471   0.01452   0.00917  -0.0096   0.9644   0.0102
  -8.000  -0.8036   0.01396   0.00853  -0.0136   0.9564   0.0107
  -7.750  -0.7648   0.01254   0.00693  -0.0169   0.9441   0.0120
  -7.500  -0.7268   0.01203   0.00635  -0.0196   0.9318   0.0131
  -7.250  -0.6955   0.01161   0.00585  -0.0208   0.9192   0.0142
  -7.000  -0.6676   0.01137   0.00554  -0.0210   0.9087   0.0156
  -6.750  -0.6447   0.01083   0.00492  -0.0203   0.8991   0.0197
  -6.500  -0.6200   0.01064   0.00469  -0.0198   0.8917   0.0216
  -6.250  -0.5970   0.01026   0.00428  -0.0190   0.8853   0.0264
  -6.000  -0.5726   0.01006   0.00406  -0.0185   0.8797   0.0297
  -5.750  -0.5487   0.00979   0.00376  -0.0177   0.8742   0.0341
  -5.500  -0.5244   0.00956   0.00351  -0.0172   0.8693   0.0394
  -5.250  -0.5001   0.00935   0.00329  -0.0165   0.8647   0.0446
  -5.000  -0.4758   0.00914   0.00309  -0.0159   0.8604   0.0529
  -4.750  -0.4514   0.00891   0.00289  -0.0154   0.8564   0.0650
  -4.500  -0.4273   0.00867   0.00270  -0.0147   0.8525   0.0791
  -4.250  -0.4038   0.00839   0.00250  -0.0140   0.8484   0.1016
  -4.000  -0.3802   0.00811   0.00232  -0.0132   0.8447   0.1316
  -3.750  -0.3572   0.00779   0.00215  -0.0124   0.8412   0.1758
  -3.500  -0.3367   0.00730   0.00195  -0.0112   0.8376   0.2485
  -3.250  -0.3165   0.00681   0.00176  -0.0099   0.8338   0.3300
  -3.000  -0.2979   0.00624   0.00156  -0.0082   0.8303   0.4350
  -2.750  -0.2816   0.00561   0.00138  -0.0061   0.8267   0.5598
  -2.500  -0.2617   0.00528   0.00132  -0.0044   0.8234   0.6407
  -2.250  -0.2377   0.00516   0.00132  -0.0035   0.8201   0.6814
  -2.000  -0.2118   0.00512   0.00130  -0.0031   0.8170   0.7007
  -1.750  -0.1853   0.00512   0.00129  -0.0027   0.8142   0.7161
  -1.500  -0.1587   0.00512   0.00130  -0.0024   0.8112   0.7294
  -1.250  -0.1320   0.00512   0.00129  -0.0021   0.8078   0.7393
  -1.000  -0.1052   0.00510   0.00130  -0.0018   0.8043   0.7477
  -0.750  -0.0789   0.00512   0.00131  -0.0013   0.8003   0.7592
  -0.500  -0.0525   0.00515   0.00132  -0.0009   0.7952   0.7679
  -0.250  -0.0264   0.00512   0.00132  -0.0004   0.7887   0.7756
   0.000  -0.0001   0.00516   0.00132   0.0000   0.7823   0.7829
   0.250   0.0263   0.00512   0.00132   0.0005   0.7750   0.7889
   0.500   0.0527   0.00515   0.00132   0.0009   0.7682   0.7949
   0.750   0.0789   0.00512   0.00130   0.0014   0.7588   0.8000
   1.000   0.1052   0.00510   0.00129   0.0018   0.7474   0.8043
   1.250   0.1320   0.00512   0.00129   0.0021   0.7390   0.8078
   1.500   0.1588   0.00512   0.00130   0.0024   0.7292   0.8112
   1.750   0.1851   0.00512   0.00128   0.0028   0.7142   0.8142
   2.000   0.2117   0.00513   0.00129   0.0031   0.6999   0.8171
   2.250   0.2378   0.00516   0.00131   0.0035   0.6821   0.8201
   2.500   0.2628   0.00524   0.00133   0.0042   0.6515   0.8234
   2.750   0.2818   0.00561   0.00138   0.0061   0.5604   0.8267
   3.000   0.2972   0.00629   0.00157   0.0084   0.4252   0.8303
   3.250   0.3164   0.00682   0.00176   0.0099   0.3290   0.8338
   3.500   0.3365   0.00732   0.00196   0.0112   0.2449   0.8375
   3.750   0.3573   0.00779   0.00215   0.0125   0.1758   0.8412
   4.000   0.3802   0.00811   0.00232   0.0132   0.1313   0.8447
   4.250   0.4039   0.00839   0.00250   0.0140   0.1025   0.8484
   4.500   0.4275   0.00866   0.00270   0.0147   0.0811   0.8525
   4.750   0.4515   0.00890   0.00288   0.0154   0.0654   0.8564
   5.000   0.4759   0.00912   0.00308   0.0159   0.0534   0.8604
   5.250   0.5006   0.00931   0.00326   0.0165   0.0464   0.8647
   5.500   0.5246   0.00955   0.00350   0.0172   0.0397   0.8694
   5.750   0.5488   0.00979   0.00374   0.0177   0.0334   0.8742
   6.000   0.5730   0.01002   0.00402   0.0184   0.0295   0.8796
   6.250   0.5971   0.01025   0.00424   0.0190   0.0256   0.8853
   6.500   0.6209   0.01056   0.00460   0.0197   0.0209   0.8915
   7.000   0.6683   0.01130   0.00545   0.0209   0.0148   0.9085
   7.250   0.6955   0.01161   0.00584   0.0208   0.0139   0.9192
   7.500   0.7270   0.01202   0.00632   0.0196   0.0124   0.9319
   7.750   0.7638   0.01283   0.00723   0.0170   0.0112   0.9449
   8.000   0.8035   0.01405   0.00863   0.0136   0.0105   0.9566
   8.250   0.8464   0.01474   0.00943   0.0097   0.0101   0.9647
   8.500   0.8877   0.01542   0.01019   0.0062   0.0093   0.9754
   8.750   0.9249   0.01626   0.01112   0.0035   0.0089   0.9953
   9.000   0.9399   0.01676   0.01164   0.0058   0.0085   1.0000
   9.250   0.9596   0.01756   0.01252   0.0069   0.0083   1.0000
   9.500   0.9785   0.01847   0.01351   0.0081   0.0080   1.0000
   9.750   0.9964   0.01954   0.01471   0.0094   0.0078   1.0000
  10.000   1.0107   0.02114   0.01648   0.0110   0.0075   1.0000
  10.250   1.0201   0.02354   0.01915   0.0132   0.0074   1.0000
  10.500   1.0275   0.02606   0.02196   0.0155   0.0073   1.0000
  10.750   1.0347   0.02830   0.02446   0.0176   0.0071   1.0000
  11.000   1.0545   0.02857   0.02479   0.0184   0.0070   1.0000
  11.250   1.0594   0.03077   0.02722   0.0206   0.0069   1.0000
  11.500   1.0573   0.03303   0.02971   0.0237   0.0068   1.0000
  11.750   1.0638   0.03421   0.03101   0.0256   0.0067   1.0000
  12.000   1.0759   0.03486   0.03172   0.0267   0.0064   1.0000
  12.250   1.0748   0.03692   0.03393   0.0283   0.0062   1.0000
  12.500   1.0522   0.04144   0.03874   0.0299   0.0064   1.0000
  12.750   1.0487   0.04413   0.04156   0.0302   0.0060   1.0000
  13.000   1.0322   0.04868   0.04632   0.0295   0.0060   1.0000
  13.250   1.0058   0.05532   0.05318   0.0268   0.0059   1.0000
  13.750   0.9615   0.07279   0.07100   0.0138   0.0062   1.0000
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