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LWK 79-100 (lwk79100-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: LWK 79-100 (lwk79100-il)
Reynolds number: 1,000,000
Max Cl/Cd: 74.23 at α=8.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-lwk79100-il-1000000-n5.txt
Download as CSV file: xf-lwk79100-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: LWK 79-100                                      
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -17.750  -1.1066   0.12069   0.11826   0.0214   1.0000   0.0055
 -17.500  -1.1482   0.10757   0.10499   0.0138   1.0000   0.0054
 -17.250  -1.1849   0.09596   0.09322   0.0071   1.0000   0.0053
 -17.000  -1.2167   0.08562   0.08273   0.0011   1.0000   0.0052
 -16.750  -1.2531   0.07483   0.07177  -0.0053   1.0000   0.0053
 -16.500  -1.2808   0.06616   0.06293  -0.0104   1.0000   0.0052
 -16.250  -1.2975   0.05972   0.05635  -0.0142   1.0000   0.0051
 -16.000  -1.3173   0.05316   0.04963  -0.0180   1.0000   0.0051
 -15.750  -1.3320   0.04773   0.04407  -0.0209   1.0000   0.0052
 -15.500  -1.3427   0.04318   0.03939  -0.0230   1.0000   0.0052
 -15.250  -1.3541   0.03882   0.03489  -0.0249   1.0000   0.0053
 -15.000  -1.3578   0.03564   0.03159  -0.0259   1.0000   0.0054
 -14.750  -1.3628   0.03259   0.02841  -0.0265   1.0000   0.0054
 -14.500  -1.3656   0.03017   0.02588  -0.0264   1.0000   0.0055
 -14.250  -1.3672   0.02831   0.02391  -0.0251   1.0000   0.0056
 -14.000  -1.3651   0.02699   0.02251  -0.0231   1.0000   0.0058
 -13.750  -1.3609   0.02592   0.02137  -0.0207   1.0000   0.0059
 -13.500  -1.3524   0.02482   0.02017  -0.0188   1.0000   0.0060
 -13.250  -1.3386   0.02391   0.01919  -0.0175   1.0000   0.0062
 -13.000  -1.3238   0.02299   0.01819  -0.0163   1.0000   0.0064
 -12.750  -1.3072   0.02216   0.01727  -0.0152   1.0000   0.0066
 -12.500  -1.2897   0.02135   0.01637  -0.0142   1.0000   0.0068
 -12.250  -1.2711   0.02058   0.01552  -0.0133   1.0000   0.0069
 -12.000  -1.2516   0.01985   0.01472  -0.0124   1.0000   0.0071
 -11.750  -1.2312   0.01918   0.01397  -0.0116   1.0000   0.0073
 -11.500  -1.2109   0.01846   0.01317  -0.0108   1.0000   0.0075
 -11.250  -1.1902   0.01773   0.01239  -0.0101   1.0000   0.0079
 -11.000  -1.1684   0.01710   0.01171  -0.0094   1.0000   0.0083
 -10.750  -1.1459   0.01653   0.01110  -0.0088   1.0000   0.0087
 -10.500  -1.1230   0.01601   0.01053  -0.0082   1.0000   0.0091
 -10.250  -1.0996   0.01551   0.00998  -0.0076   1.0000   0.0096
 -10.000  -1.0758   0.01506   0.00947  -0.0071   1.0000   0.0100
  -9.750  -1.0523   0.01454   0.00892  -0.0066   1.0000   0.0108
  -9.500  -1.0283   0.01409   0.00845  -0.0061   1.0000   0.0118
  -9.250  -1.0037   0.01368   0.00802  -0.0056   1.0000   0.0127
  -9.000  -0.9789   0.01331   0.00760  -0.0052   1.0000   0.0133
  -8.750  -0.9543   0.01289   0.00716  -0.0047   1.0000   0.0144
  -8.500  -0.9293   0.01252   0.00678  -0.0043   1.0000   0.0156
  -8.250  -0.9040   0.01218   0.00643  -0.0039   1.0000   0.0167
  -8.000  -0.8785   0.01189   0.00609  -0.0035   1.0000   0.0175
  -7.750  -0.8532   0.01153   0.00573  -0.0031   1.0000   0.0190
  -7.500  -0.8278   0.01121   0.00541  -0.0027   1.0000   0.0206
  -7.000  -0.7760   0.01068   0.00485  -0.0019   1.0000   0.0230
  -6.750  -0.7505   0.01036   0.00453  -0.0015   1.0000   0.0253
  -6.500  -0.7247   0.01008   0.00426  -0.0011   1.0000   0.0275
  -6.250  -0.6909   0.00983   0.00400  -0.0024   0.9773   0.0296
  -6.000  -0.6518   0.00986   0.00367  -0.0047   0.8177   0.0340
  -5.500  -0.6008   0.00962   0.00321  -0.0037   0.7498   0.0424
  -5.250  -0.5743   0.00946   0.00299  -0.0034   0.7313   0.0481
  -5.000  -0.5477   0.00926   0.00278  -0.0031   0.7164   0.0569
  -4.750  -0.5210   0.00906   0.00258  -0.0029   0.7038   0.0676
  -4.500  -0.4942   0.00885   0.00239  -0.0027   0.6927   0.0818
  -4.250  -0.4672   0.00865   0.00220  -0.0025   0.6825   0.0966
  -3.750  -0.4130   0.00826   0.00188  -0.0021   0.6645   0.1307
  -3.500  -0.3859   0.00806   0.00173  -0.0019   0.6567   0.1533
  -3.250  -0.3586   0.00786   0.00160  -0.0018   0.6499   0.1743
  -3.000  -0.3314   0.00765   0.00147  -0.0016   0.6429   0.2017
  -2.750  -0.3042   0.00741   0.00134  -0.0015   0.6367   0.2363
  -2.500  -0.2773   0.00714   0.00121  -0.0013   0.6300   0.2800
  -2.250  -0.2501   0.00692   0.00111  -0.0011   0.6242   0.3185
  -2.000  -0.2226   0.00674   0.00104  -0.0010   0.6178   0.3529
  -1.750  -0.1951   0.00660   0.00096  -0.0009   0.6112   0.3826
  -1.500  -0.1673   0.00647   0.00091  -0.0008   0.6046   0.4088
  -1.250  -0.1396   0.00637   0.00086  -0.0006   0.5954   0.4348
  -1.000  -0.1118   0.00628   0.00082  -0.0005   0.5832   0.4592
  -0.750  -0.0839   0.00622   0.00079  -0.0004   0.5718   0.4806
  -0.500  -0.0560   0.00617   0.00078  -0.0002   0.5604   0.5013
  -0.250  -0.0281   0.00615   0.00077  -0.0001   0.5477   0.5205
   0.000   0.0000   0.00614   0.00076   0.0000   0.5354   0.5356
   0.250   0.0281   0.00615   0.00076   0.0001   0.5205   0.5476
   0.500   0.0560   0.00617   0.00078   0.0002   0.5013   0.5602
   0.750   0.0839   0.00622   0.00079   0.0004   0.4805   0.5718
   1.000   0.1118   0.00629   0.00082   0.0005   0.4591   0.5832
   1.250   0.1396   0.00637   0.00086   0.0006   0.4346   0.5955
   1.500   0.1673   0.00647   0.00091   0.0008   0.4086   0.6046
   1.750   0.1951   0.00660   0.00096   0.0009   0.3829   0.6112
   2.000   0.2226   0.00674   0.00104   0.0010   0.3533   0.6178
   2.250   0.2501   0.00692   0.00111   0.0011   0.3188   0.6242
   2.500   0.2773   0.00714   0.00121   0.0013   0.2797   0.6301
   2.750   0.3043   0.00741   0.00134   0.0015   0.2364   0.6368
   3.000   0.3313   0.00766   0.00147   0.0016   0.2009   0.6429
   3.250   0.3586   0.00786   0.00160   0.0018   0.1744   0.6498
   3.500   0.3859   0.00806   0.00173   0.0019   0.1529   0.6567
   3.750   0.4130   0.00826   0.00188   0.0021   0.1308   0.6646
   4.000   0.4401   0.00847   0.00204   0.0023   0.1117   0.6727
   4.250   0.4672   0.00866   0.00220   0.0025   0.0965   0.6824
   4.500   0.4942   0.00885   0.00239   0.0027   0.0820   0.6927
   4.750   0.5210   0.00906   0.00258   0.0029   0.0676   0.7039
   5.000   0.5478   0.00926   0.00278   0.0031   0.0569   0.7164
   5.250   0.5743   0.00946   0.00299   0.0034   0.0481   0.7314
   5.500   0.6008   0.00962   0.00321   0.0037   0.0424   0.7499
   6.000   0.6519   0.00987   0.00367   0.0047   0.0341   0.8169
   6.250   0.6905   0.00983   0.00399   0.0025   0.0297   0.9761
   6.500   0.7247   0.01008   0.00426   0.0011   0.0275   1.0000
   6.750   0.7505   0.01036   0.00453   0.0015   0.0253   1.0000
   7.000   0.7761   0.01068   0.00485   0.0019   0.0230   1.0000
   7.250   0.8021   0.01093   0.00512   0.0023   0.0221   1.0000
   7.500   0.8278   0.01121   0.00541   0.0027   0.0205   1.0000
   7.750   0.8533   0.01153   0.00573   0.0031   0.0189   1.0000
   8.000   0.8786   0.01189   0.00609   0.0035   0.0175   1.0000
   8.250   0.9041   0.01218   0.00642   0.0039   0.0167   1.0000
   8.500   0.9294   0.01252   0.00679   0.0043   0.0156   1.0000
   8.750   0.9544   0.01289   0.00717   0.0047   0.0144   1.0000
   9.000   0.9790   0.01332   0.00760   0.0052   0.0133   1.0000
   9.250   1.0039   0.01369   0.00802   0.0056   0.0126   1.0000
   9.500   1.0284   0.01409   0.00845   0.0060   0.0118   1.0000
   9.750   1.0525   0.01454   0.00893   0.0065   0.0109   1.0000
  10.000   1.0760   0.01507   0.00948   0.0071   0.0100   1.0000
  10.250   1.0999   0.01552   0.00998   0.0076   0.0096   1.0000
  10.500   1.1233   0.01601   0.01052   0.0081   0.0092   1.0000
  10.750   1.1462   0.01654   0.01110   0.0087   0.0087   1.0000
  11.000   1.1687   0.01710   0.01170   0.0093   0.0083   1.0000
  11.250   1.1906   0.01772   0.01238   0.0100   0.0079   1.0000
  11.500   1.2114   0.01844   0.01315   0.0107   0.0075   1.0000
  11.750   1.2317   0.01918   0.01397   0.0116   0.0072   1.0000
  12.000   1.2521   0.01985   0.01471   0.0123   0.0071   1.0000
  12.250   1.2716   0.02057   0.01551   0.0132   0.0069   1.0000
  12.500   1.2903   0.02133   0.01636   0.0141   0.0068   1.0000
  12.750   1.3079   0.02215   0.01725   0.0151   0.0066   1.0000
  13.000   1.3244   0.02300   0.01819   0.0162   0.0064   1.0000
  13.250   1.3396   0.02388   0.01916   0.0174   0.0062   1.0000
  13.500   1.3527   0.02485   0.02020   0.0187   0.0060   1.0000
  13.750   1.3633   0.02584   0.02127   0.0204   0.0059   1.0000
  14.000   1.3667   0.02696   0.02247   0.0229   0.0058   1.0000
  14.250   1.3682   0.02830   0.02391   0.0250   0.0057   1.0000
  14.500   1.3669   0.03014   0.02584   0.0262   0.0055   1.0000
  14.750   1.3646   0.03251   0.02833   0.0264   0.0055   1.0000
  15.000   1.3592   0.03560   0.03154   0.0258   0.0053   1.0000
  15.250   1.3552   0.03883   0.03489   0.0247   0.0053   1.0000
  15.500   1.3460   0.04291   0.03911   0.0230   0.0052   1.0000
  15.750   1.3353   0.04746   0.04379   0.0208   0.0052   1.0000
  16.000   1.3176   0.05333   0.04981   0.0176   0.0052   1.0000
  16.250   1.3018   0.05928   0.05591   0.0142   0.0052   1.0000
  16.500   1.2803   0.06652   0.06330   0.0099   0.0052   1.0000
  16.750   1.2492   0.07585   0.07280   0.0044   0.0052   1.0000
  17.000   1.2188   0.08555   0.08266  -0.0013   0.0052   1.0000
  17.250   1.1904   0.09519   0.09245  -0.0069   0.0054   1.0000
  17.500   1.1481   0.10794   0.10536  -0.0142   0.0054   1.0000
  17.750   1.1067   0.12099   0.11858  -0.0218   0.0055   1.0000
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