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NASA/LANGLEY LS(1)-0413MOD AIRFOIL (ls413mod-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: NASA/LANGLEY LS(1)-0413MOD AIRFOIL (ls413mod-il)
Reynolds number: 1,000,000
Max Cl/Cd: 92.54 at α=6°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-ls413mod-il-1000000-n5.txt
Download as CSV file: xf-ls413mod-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NASA/LANGLEY LS(1)-0413MOD AIRFOIL              
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -16.250  -1.0347   0.06047   0.05757  -0.0561   1.0000   0.0116
 -16.000  -1.0547   0.05324   0.05015  -0.0612   1.0000   0.0116
 -15.750  -1.0665   0.04796   0.04472  -0.0646   1.0000   0.0117
 -15.500  -1.0731   0.04382   0.04044  -0.0670   1.0000   0.0117
 -15.250  -1.0760   0.04043   0.03693  -0.0686   1.0000   0.0118
 -15.000  -1.0756   0.03763   0.03401  -0.0696   1.0000   0.0118
 -14.750  -1.0736   0.03514   0.03141  -0.0703   1.0000   0.0119
 -14.500  -1.0695   0.03300   0.02916  -0.0706   1.0000   0.0119
 -14.250  -1.0641   0.03113   0.02719  -0.0706   1.0000   0.0120
 -14.000  -1.0587   0.02944   0.02540  -0.0701   1.0000   0.0121
 -13.750  -1.0539   0.02802   0.02389  -0.0690   1.0000   0.0122
 -13.500  -1.0463   0.02672   0.02250  -0.0681   1.0000   0.0122
 -13.250  -1.0345   0.02552   0.02121  -0.0676   1.0000   0.0123
 -13.000  -1.0212   0.02454   0.02014  -0.0668   1.0000   0.0124
 -12.750  -1.0069   0.02366   0.01918  -0.0657   1.0000   0.0125
 -12.500  -0.9848   0.02283   0.01826  -0.0660   0.9990   0.0127
 -12.250  -0.9568   0.02192   0.01727  -0.0673   0.9968   0.0128
 -12.000  -0.9278   0.02112   0.01638  -0.0687   0.9946   0.0130
 -11.750  -0.8988   0.02038   0.01557  -0.0700   0.9925   0.0131
 -11.500  -0.8700   0.01979   0.01491  -0.0710   0.9894   0.0132
 -11.250  -0.8418   0.01874   0.01377  -0.0723   0.9858   0.0134
 -11.000  -0.8116   0.01781   0.01278  -0.0739   0.9826   0.0136
 -10.750  -0.7831   0.01713   0.01205  -0.0748   0.9766   0.0138
 -10.500  -0.7527   0.01649   0.01136  -0.0760   0.9711   0.0140
 -10.250  -0.7239   0.01591   0.01073  -0.0769   0.9646   0.0141
 -10.000  -0.6949   0.01536   0.01012  -0.0776   0.9574   0.0142
  -9.750  -0.6668   0.01486   0.00958  -0.0781   0.9489   0.0144
  -9.500  -0.6391   0.01438   0.00904  -0.0785   0.9395   0.0145
  -9.250  -0.6117   0.01394   0.00854  -0.0787   0.9287   0.0147
  -9.000  -0.5843   0.01352   0.00805  -0.0790   0.9189   0.0148
  -8.750  -0.5567   0.01313   0.00759  -0.0792   0.9091   0.0150
  -8.500  -0.5287   0.01274   0.00715  -0.0795   0.8995   0.0152
  -8.250  -0.5007   0.01238   0.00672  -0.0798   0.8901   0.0154
  -8.000  -0.4723   0.01204   0.00632  -0.0801   0.8803   0.0156
  -7.750  -0.4436   0.01173   0.00594  -0.0805   0.8716   0.0158
  -7.500  -0.4148   0.01143   0.00559  -0.0809   0.8624   0.0160
  -7.250  -0.3857   0.01115   0.00525  -0.0813   0.8541   0.0162
  -7.000  -0.3565   0.01090   0.00495  -0.0817   0.8454   0.0164
  -6.750  -0.3270   0.01056   0.00457  -0.0823   0.8375   0.0168
  -6.500  -0.2974   0.01030   0.00427  -0.0828   0.8292   0.0173
  -6.250  -0.2677   0.01008   0.00403  -0.0833   0.8214   0.0178
  -6.000  -0.2380   0.00990   0.00381  -0.0838   0.8131   0.0184
  -5.750  -0.2081   0.00973   0.00361  -0.0843   0.8054   0.0190
  -5.500  -0.1782   0.00956   0.00340  -0.0848   0.7970   0.0196
  -5.250  -0.1483   0.00941   0.00322  -0.0853   0.7888   0.0201
  -5.000  -0.1180   0.00921   0.00298  -0.0858   0.7794   0.0212
  -4.750  -0.0879   0.00906   0.00281  -0.0864   0.7698   0.0222
  -4.500  -0.0579   0.00895   0.00265  -0.0868   0.7597   0.0235
  -4.250  -0.0277   0.00884   0.00251  -0.0874   0.7505   0.0246
  -4.000   0.0027   0.00871   0.00236  -0.0879   0.7428   0.0269
  -3.750   0.0331   0.00858   0.00223  -0.0885   0.7353   0.0299
  -3.500   0.0639   0.00840   0.00211  -0.0892   0.7282   0.0441
  -3.250   0.0948   0.00825   0.00200  -0.0900   0.7210   0.0617
  -3.000   0.1258   0.00807   0.00190  -0.0908   0.7128   0.0878
  -2.750   0.1571   0.00786   0.00181  -0.0917   0.7053   0.1261
  -2.500   0.1891   0.00759   0.00171  -0.0928   0.6972   0.1849
  -2.250   0.2217   0.00727   0.00162  -0.0941   0.6885   0.2621
  -2.000   0.2555   0.00685   0.00153  -0.0959   0.6760   0.3793
  -1.750   0.2880   0.00660   0.00147  -0.0972   0.6589   0.4598
  -1.500   0.3204   0.00640   0.00145  -0.0984   0.6414   0.5402
  -1.250   0.3517   0.00632   0.00148  -0.0992   0.6275   0.5965
  -1.000   0.3821   0.00633   0.00154  -0.0997   0.6144   0.6341
  -0.750   0.4118   0.00641   0.00158  -0.1000   0.5991   0.6498
  -0.500   0.4412   0.00652   0.00162  -0.1003   0.5787   0.6594
  -0.250   0.4703   0.00667   0.00167  -0.1005   0.5502   0.6694
   0.000   0.4991   0.00686   0.00174  -0.1007   0.5203   0.6784
   0.250   0.5280   0.00704   0.00181  -0.1009   0.4940   0.6829
   0.500   0.5567   0.00723   0.00189  -0.1011   0.4681   0.6862
   0.750   0.5856   0.00739   0.00197  -0.1014   0.4471   0.6896
   1.000   0.6143   0.00758   0.00206  -0.1016   0.4233   0.6934
   1.250   0.6427   0.00781   0.00216  -0.1017   0.3973   0.6972
   1.500   0.6712   0.00801   0.00228  -0.1019   0.3733   0.7016
   1.750   0.6993   0.00826   0.00242  -0.1020   0.3446   0.7064
   2.000   0.7266   0.00862   0.00259  -0.1020   0.3054   0.7108
   2.250   0.7539   0.00897   0.00277  -0.1020   0.2699   0.7140
   2.500   0.7814   0.00927   0.00295  -0.1021   0.2431   0.7167
   2.750   0.8093   0.00950   0.00311  -0.1022   0.2247   0.7193
   3.000   0.8371   0.00973   0.00327  -0.1022   0.2084   0.7221
   3.250   0.8649   0.00997   0.00344  -0.1023   0.1936   0.7252
   3.500   0.8926   0.01021   0.00362  -0.1023   0.1788   0.7283
   3.750   0.9201   0.01047   0.00381  -0.1023   0.1645   0.7310
   4.250   0.9749   0.01093   0.00421  -0.1023   0.1427   0.7376
   4.500   1.0022   0.01117   0.00441  -0.1023   0.1341   0.7414
   4.750   1.0294   0.01142   0.00462  -0.1023   0.1265   0.7447
   5.000   1.0566   0.01165   0.00483  -0.1022   0.1203   0.7476
   5.250   1.0838   0.01186   0.00506  -0.1022   0.1154   0.7510
   5.500   1.1105   0.01211   0.00530  -0.1020   0.1098   0.7546
   5.750   1.1375   0.01233   0.00553  -0.1019   0.1061   0.7584
   6.000   1.1642   0.01258   0.00577  -0.1018   0.1012   0.7618
   6.250   1.1901   0.01289   0.00605  -0.1016   0.0942   0.7651
   6.500   1.2162   0.01316   0.00632  -0.1014   0.0887   0.7687
   6.750   1.2417   0.01348   0.00662  -0.1011   0.0829   0.7729
   7.000   1.2678   0.01373   0.00689  -0.1008   0.0804   0.7772
   7.250   1.2934   0.01401   0.00718  -0.1006   0.0773   0.7809
   7.500   1.3184   0.01434   0.00751  -0.1002   0.0737   0.7847
   7.750   1.3435   0.01464   0.00783  -0.0998   0.0707   0.7888
   8.000   1.3683   0.01495   0.00815  -0.0994   0.0675   0.7931
   8.250   1.3924   0.01532   0.00852  -0.0989   0.0640   0.7971
   8.500   1.4162   0.01567   0.00889  -0.0983   0.0611   0.8013
   8.750   1.4403   0.01599   0.00925  -0.0978   0.0592   0.8057
   9.000   1.4637   0.01635   0.00963  -0.0971   0.0565   0.8100
   9.250   1.4859   0.01679   0.01007  -0.0963   0.0531   0.8138
   9.500   1.5085   0.01717   0.01048  -0.0956   0.0506   0.8178
   9.750   1.5299   0.01762   0.01095  -0.0947   0.0463   0.8224
  10.000   1.5498   0.01816   0.01147  -0.0935   0.0408   0.8269
  10.250   1.5671   0.01886   0.01213  -0.0920   0.0335   0.8310
  10.500   1.5839   0.01953   0.01281  -0.0904   0.0292   0.8353
  10.750   1.5992   0.02023   0.01352  -0.0885   0.0263   0.8399
  11.000   1.6146   0.02084   0.01416  -0.0867   0.0245   0.8442
  11.250   1.6255   0.02150   0.01487  -0.0840   0.0230   0.8485
  11.500   1.6374   0.02226   0.01568  -0.0817   0.0217   0.8533
  11.750   1.6512   0.02295   0.01643  -0.0798   0.0210   0.8581
  12.000   1.6642   0.02371   0.01725  -0.0779   0.0203   0.8626
  12.250   1.6764   0.02455   0.01816  -0.0760   0.0196   0.8679
  12.500   1.6878   0.02548   0.01915  -0.0741   0.0190   0.8733
  12.750   1.6983   0.02651   0.02025  -0.0722   0.0184   0.8784
  13.000   1.7078   0.02764   0.02145  -0.0704   0.0177   0.8840
  13.250   1.7188   0.02870   0.02259  -0.0688   0.0173   0.8898
  13.500   1.7287   0.02986   0.02384  -0.0673   0.0169   0.8960
  13.750   1.7376   0.03114   0.02520  -0.0658   0.0164   0.9033
  14.000   1.7454   0.03253   0.02668  -0.0642   0.0160   0.9115
  14.250   1.7521   0.03406   0.02829  -0.0628   0.0156   0.9219
  14.500   1.7570   0.03566   0.03000  -0.0612   0.0152   0.9386
  14.750   1.7587   0.03741   0.03185  -0.0594   0.0149   1.0000
  15.000   1.7625   0.03949   0.03400  -0.0584   0.0145   1.0000
  15.250   1.7678   0.04148   0.03608  -0.0576   0.0142   1.0000
  15.500   1.7722   0.04360   0.03828  -0.0568   0.0140   1.0000
  15.750   1.7751   0.04592   0.04068  -0.0562   0.0138   1.0000
  16.000   1.7767   0.04844   0.04330  -0.0557   0.0135   1.0000
  16.250   1.7771   0.05120   0.04614  -0.0554   0.0132   1.0000
  16.500   1.7763   0.05416   0.04919  -0.0552   0.0130   1.0000
  16.750   1.7740   0.05740   0.05252  -0.0552   0.0127   1.0000
  17.000   1.7702   0.06095   0.05618  -0.0554   0.0125   1.0000
  17.250   1.7650   0.06480   0.06013  -0.0559   0.0122   1.0000
  17.500   1.7576   0.06904   0.06447  -0.0566   0.0120   1.0000
  17.750   1.7483   0.07368   0.06921  -0.0576   0.0118   1.0000
  18.000   1.7369   0.07878   0.07443  -0.0589   0.0116   1.0000
  18.250   1.7255   0.08400   0.07977  -0.0604   0.0115   1.0000
  18.500   1.7124   0.08957   0.08547  -0.0622   0.0114   1.0000
  18.750   1.6974   0.09557   0.09161  -0.0644   0.0113   1.0000
  19.000   1.6800   0.10209   0.09826  -0.0669   0.0112   1.0000
  19.250   1.6598   0.10921   0.10552  -0.0699   0.0111   1.0000
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