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LWK 79-100 (lwk79100-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: LWK 79-100 (lwk79100-il)
Reynolds number: 500,000
Max Cl/Cd: 60.06 at α=7.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-lwk79100-il-500000-n5.txt
Download as CSV file: xf-lwk79100-il-500000-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 =     0.500 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -16.750  -0.9671   0.13502   0.13245   0.0312   1.0000   0.0085
 -16.500  -1.0205   0.11748   0.11469   0.0212   1.0000   0.0083
 -16.250  -1.0577   0.10475   0.10179   0.0138   1.0000   0.0082
 -16.000  -1.0893   0.09376   0.09064   0.0074   1.0000   0.0081
 -15.750  -1.1156   0.08421   0.08095   0.0017   1.0000   0.0081
 -15.500  -1.1405   0.07542   0.07199  -0.0036   1.0000   0.0080
 -15.250  -1.1613   0.06775   0.06417  -0.0082   1.0000   0.0081
 -15.000  -1.1786   0.06106   0.05732  -0.0122   1.0000   0.0080
 -14.750  -1.1940   0.05505   0.05115  -0.0157   1.0000   0.0081
 -14.500  -1.2051   0.05003   0.04599  -0.0185   1.0000   0.0081
 -14.250  -1.2121   0.04588   0.04171  -0.0205   1.0000   0.0082
 -14.000  -1.2168   0.04223   0.03793  -0.0221   1.0000   0.0083
 -13.750  -1.2211   0.03887   0.03441  -0.0233   1.0000   0.0084
 -13.500  -1.2223   0.03608   0.03150  -0.0241   1.0000   0.0085
 -13.250  -1.2242   0.03353   0.02881  -0.0242   1.0000   0.0086
 -13.000  -1.2254   0.03145   0.02660  -0.0235   1.0000   0.0088
 -12.750  -1.2240   0.02990   0.02493  -0.0218   1.0000   0.0090
 -12.500  -1.2212   0.02854   0.02345  -0.0195   1.0000   0.0092
 -12.250  -1.2127   0.02726   0.02204  -0.0179   1.0000   0.0094
 -12.000  -1.2004   0.02610   0.02075  -0.0166   1.0000   0.0097
 -11.750  -1.1863   0.02500   0.01952  -0.0154   1.0000   0.0099
 -11.500  -1.1717   0.02385   0.01826  -0.0142   1.0000   0.0102
 -11.250  -1.1553   0.02281   0.01713  -0.0132   1.0000   0.0107
 -11.000  -1.1363   0.02199   0.01625  -0.0124   1.0000   0.0112
 -10.750  -1.1163   0.02124   0.01542  -0.0116   1.0000   0.0118
 -10.500  -1.0957   0.02051   0.01461  -0.0109   1.0000   0.0124
 -10.250  -1.0749   0.01977   0.01377  -0.0101   1.0000   0.0130
 -10.000  -1.0536   0.01905   0.01295  -0.0094   1.0000   0.0135
  -9.750  -1.0326   0.01825   0.01209  -0.0087   1.0000   0.0144
  -9.500  -1.0100   0.01765   0.01145  -0.0081   1.0000   0.0153
  -9.250  -0.9869   0.01709   0.01083  -0.0075   1.0000   0.0163
  -9.000  -0.9634   0.01656   0.01022  -0.0070   1.0000   0.0172
  -8.750  -0.9402   0.01597   0.00957  -0.0064   1.0000   0.0183
  -8.500  -0.9164   0.01544   0.00904  -0.0059   1.0000   0.0197
  -8.250  -0.8919   0.01502   0.00857  -0.0054   1.0000   0.0213
  -8.000  -0.8672   0.01461   0.00809  -0.0049   1.0000   0.0226
  -7.750  -0.8430   0.01410   0.00754  -0.0044   1.0000   0.0241
  -7.500  -0.8185   0.01363   0.00707  -0.0040   1.0000   0.0260
  -7.250  -0.7935   0.01325   0.00665  -0.0035   1.0000   0.0280
  -7.000  -0.7680   0.01292   0.00627  -0.0031   1.0000   0.0297
  -6.750  -0.7433   0.01246   0.00582  -0.0026   1.0000   0.0328
  -6.500  -0.7180   0.01210   0.00545  -0.0022   1.0000   0.0357
  -6.250  -0.6923   0.01179   0.00509  -0.0018   1.0000   0.0382
  -6.000  -0.6672   0.01140   0.00473  -0.0013   1.0000   0.0433
  -5.750  -0.6415   0.01109   0.00442  -0.0009   1.0000   0.0481
  -5.500  -0.6162   0.01074   0.00411  -0.0004   1.0000   0.0560
  -5.250  -0.5902   0.01041   0.00381  -0.0001   0.9991   0.0663
  -5.000  -0.5495   0.01004   0.00350  -0.0031   0.9500   0.0838
  -4.750  -0.5103   0.00987   0.00319  -0.0053   0.8404   0.1040
  -4.500  -0.4863   0.00978   0.00297  -0.0045   0.7935   0.1226
  -4.250  -0.4610   0.00958   0.00275  -0.0039   0.7669   0.1452
  -4.000  -0.4351   0.00939   0.00255  -0.0035   0.7477   0.1691
  -3.750  -0.4089   0.00917   0.00236  -0.0032   0.7321   0.1960
  -3.500  -0.3826   0.00892   0.00217  -0.0029   0.7186   0.2274
  -3.250  -0.3564   0.00863   0.00200  -0.0026   0.7069   0.2694
  -3.000  -0.3304   0.00831   0.00184  -0.0024   0.6966   0.3210
  -2.750  -0.3037   0.00809   0.00171  -0.0021   0.6872   0.3608
  -2.500  -0.2767   0.00790   0.00161  -0.0019   0.6787   0.3953
  -2.000  -0.2223   0.00762   0.00147  -0.0015   0.6629   0.4550
  -1.500  -0.1671   0.00746   0.00140  -0.0011   0.6483   0.5037
  -1.250  -0.1394   0.00742   0.00137  -0.0009   0.6412   0.5224
  -1.000  -0.1116   0.00738   0.00136  -0.0007   0.6336   0.5401
  -0.750  -0.0838   0.00736   0.00135  -0.0005   0.6259   0.5559
  -0.500  -0.0558   0.00735   0.00133  -0.0004   0.6150   0.5684
  -0.250  -0.0278   0.00735   0.00132  -0.0002   0.6031   0.5805
   0.000   0.0000   0.00734   0.00132   0.0000   0.5923   0.5923
   0.500   0.0558   0.00735   0.00133   0.0004   0.5684   0.6151
   0.750   0.0838   0.00736   0.00135   0.0005   0.5559   0.6258
   1.000   0.1116   0.00738   0.00136   0.0007   0.5401   0.6336
   1.250   0.1394   0.00742   0.00137   0.0009   0.5224   0.6412
   1.500   0.1671   0.00746   0.00140   0.0011   0.5036   0.6483
   2.000   0.2223   0.00762   0.00147   0.0015   0.4550   0.6630
   2.500   0.2767   0.00790   0.00161   0.0019   0.3953   0.6787
   2.750   0.3037   0.00809   0.00171   0.0021   0.3607   0.6872
   3.000   0.3304   0.00831   0.00184   0.0024   0.3209   0.6967
   3.250   0.3564   0.00863   0.00200   0.0026   0.2693   0.7068
   3.500   0.3826   0.00892   0.00217   0.0029   0.2274   0.7185
   3.750   0.4089   0.00917   0.00236   0.0032   0.1958   0.7321
   4.000   0.4351   0.00939   0.00255   0.0035   0.1690   0.7477
   4.250   0.4610   0.00958   0.00275   0.0039   0.1449   0.7669
   4.500   0.4863   0.00978   0.00297   0.0045   0.1226   0.7934
   4.750   0.5104   0.00987   0.00319   0.0053   0.1040   0.8403
   5.000   0.5496   0.01004   0.00350   0.0030   0.0839   0.9501
   5.250   0.5902   0.01041   0.00381   0.0001   0.0663   0.9992
   5.500   0.6162   0.01074   0.00411   0.0004   0.0559   1.0000
   5.750   0.6415   0.01109   0.00442   0.0009   0.0481   1.0000
   6.000   0.6672   0.01140   0.00473   0.0013   0.0432   1.0000
   6.250   0.6923   0.01179   0.00509   0.0018   0.0382   1.0000
   6.500   0.7180   0.01210   0.00545   0.0022   0.0357   1.0000
   6.750   0.7433   0.01246   0.00582   0.0026   0.0328   1.0000
   7.000   0.7680   0.01293   0.00628   0.0031   0.0297   1.0000
   7.250   0.7935   0.01326   0.00665   0.0035   0.0280   1.0000
   7.500   0.8186   0.01363   0.00707   0.0039   0.0260   1.0000
   7.750   0.8431   0.01410   0.00754   0.0044   0.0241   1.0000
   8.000   0.8673   0.01461   0.00809   0.0049   0.0226   1.0000
   8.250   0.8921   0.01501   0.00856   0.0054   0.0213   1.0000
   8.500   0.9165   0.01545   0.00904   0.0058   0.0198   1.0000
   8.750   0.9403   0.01597   0.00958   0.0063   0.0182   1.0000
   9.000   0.9635   0.01656   0.01022   0.0069   0.0172   1.0000
   9.250   0.9870   0.01710   0.01083   0.0075   0.0163   1.0000
   9.500   1.0102   0.01764   0.01144   0.0080   0.0153   1.0000
   9.750   1.0329   0.01825   0.01209   0.0086   0.0144   1.0000
  10.000   1.0540   0.01904   0.01294   0.0093   0.0135   1.0000
  10.250   1.0752   0.01977   0.01377   0.0101   0.0130   1.0000
  10.500   1.0963   0.02050   0.01459   0.0108   0.0124   1.0000
  10.750   1.1168   0.02123   0.01541   0.0115   0.0117   1.0000
  11.000   1.1369   0.02198   0.01624   0.0123   0.0112   1.0000
  11.250   1.1558   0.02281   0.01713   0.0131   0.0107   1.0000
  11.500   1.1725   0.02383   0.01824   0.0141   0.0102   1.0000
  11.750   1.1870   0.02500   0.01952   0.0153   0.0099   1.0000
  12.000   1.2014   0.02609   0.02074   0.0164   0.0096   1.0000
  12.250   1.2137   0.02725   0.02203   0.0177   0.0093   1.0000
  12.500   1.2224   0.02854   0.02345   0.0193   0.0092   1.0000
  12.750   1.2258   0.02987   0.02489   0.0215   0.0090   1.0000
  13.000   1.2262   0.03149   0.02665   0.0233   0.0088   1.0000
  13.250   1.2259   0.03349   0.02877   0.0240   0.0086   1.0000
  13.500   1.2241   0.03603   0.03145   0.0239   0.0085   1.0000
  13.750   1.2221   0.03891   0.03446   0.0231   0.0084   1.0000
  14.000   1.2182   0.04224   0.03792   0.0219   0.0083   1.0000
  14.250   1.2126   0.04600   0.04184   0.0203   0.0083   1.0000
  14.500   1.2059   0.05015   0.04612   0.0182   0.0081   1.0000
  14.750   1.1945   0.05521   0.05132   0.0154   0.0081   1.0000
  15.000   1.1819   0.06083   0.05708   0.0121   0.0080   1.0000
  15.250   1.1649   0.06746   0.06387   0.0081   0.0080   1.0000
  15.500   1.1438   0.07517   0.07174   0.0035   0.0080   1.0000
  15.750   1.1178   0.08415   0.08089  -0.0019   0.0081   1.0000
  16.000   1.0896   0.09408   0.09095  -0.0078   0.0081   1.0000
  16.250   1.0561   0.10546   0.10252  -0.0145   0.0082   1.0000
  16.500   1.0212   0.11777   0.11499  -0.0216   0.0083   1.0000
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