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NASA/LANGLEY LS(1)-0413 (GA(W)-2) AIRFOIL (ls413-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: NASA/LANGLEY LS(1)-0413 (GA(W)-2) AIRFOIL (ls413-il)
Reynolds number: 1,000,000
Max Cl/Cd: 86.38 at α=0.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-ls413-il-1000000-n5.txt
Download as CSV file: xf-ls413-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NASA/LANGLEY LS(1)-0413 (GA(W)-2) 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
  ------ -------- --------- --------- -------- -------- --------
 -16.500  -1.0092   0.06295   0.06009  -0.0675   1.0000   0.0116
 -16.250  -1.0322   0.05525   0.05220  -0.0728   1.0000   0.0116
 -16.000  -1.0454   0.04977   0.04657  -0.0763   1.0000   0.0116
 -15.750  -1.0535   0.04546   0.04212  -0.0787   1.0000   0.0117
 -15.500  -1.0575   0.04198   0.03852  -0.0803   1.0000   0.0117
 -15.250  -1.0577   0.03912   0.03555  -0.0814   1.0000   0.0118
 -15.000  -1.0577   0.03645   0.03277  -0.0822   1.0000   0.0118
 -14.750  -1.0546   0.03424   0.03045  -0.0825   1.0000   0.0119
 -14.500  -1.0507   0.03225   0.02837  -0.0826   1.0000   0.0119
 -14.250  -1.0462   0.03054   0.02657  -0.0822   1.0000   0.0120
 -14.000  -1.0440   0.02903   0.02498  -0.0809   1.0000   0.0121
 -13.750  -1.0370   0.02758   0.02343  -0.0804   0.9973   0.0121
 -13.500  -1.0173   0.02611   0.02185  -0.0821   0.9922   0.0122
 -13.250  -0.9955   0.02476   0.02039  -0.0838   0.9866   0.0123
 -13.000  -0.9701   0.02360   0.01913  -0.0857   0.9823   0.0125
 -12.750  -0.9471   0.02262   0.01806  -0.0866   0.9751   0.0126
 -12.500  -0.9219   0.02175   0.01709  -0.0876   0.9690   0.0128
 -12.250  -0.8987   0.02100   0.01626  -0.0880   0.9605   0.0129
 -12.000  -0.8745   0.02035   0.01551  -0.0883   0.9532   0.0131
 -11.750  -0.8506   0.01978   0.01486  -0.0884   0.9449   0.0132
 -11.500  -0.8263   0.01926   0.01426  -0.0885   0.9377   0.0133
 -11.250  -0.8037   0.01839   0.01328  -0.0886   0.9303   0.0135
 -11.000  -0.7808   0.01749   0.01227  -0.0887   0.9239   0.0137
 -10.750  -0.7563   0.01677   0.01148  -0.0889   0.9176   0.0138
 -10.500  -0.7311   0.01615   0.01079  -0.0892   0.9115   0.0139
 -10.250  -0.7052   0.01560   0.01018  -0.0894   0.9061   0.0141
 -10.000  -0.6789   0.01510   0.00961  -0.0897   0.9000   0.0142
  -9.750  -0.6523   0.01464   0.00909  -0.0900   0.8939   0.0144
  -9.500  -0.6251   0.01420   0.00859  -0.0903   0.8884   0.0145
  -9.250  -0.5977   0.01378   0.00812  -0.0907   0.8829   0.0147
  -9.000  -0.5701   0.01338   0.00766  -0.0911   0.8779   0.0149
  -8.750  -0.5421   0.01299   0.00723  -0.0915   0.8735   0.0151
  -8.500  -0.5138   0.01262   0.00681  -0.0920   0.8686   0.0153
  -8.250  -0.4854   0.01226   0.00641  -0.0924   0.8636   0.0155
  -8.000  -0.4569   0.01194   0.00603  -0.0929   0.8590   0.0157
  -7.750  -0.4279   0.01161   0.00567  -0.0934   0.8543   0.0160
  -7.500  -0.3990   0.01132   0.00533  -0.0939   0.8493   0.0162
  -7.250  -0.3699   0.01105   0.00502  -0.0944   0.8449   0.0164
  -7.000  -0.3405   0.01077   0.00470  -0.0950   0.8411   0.0167
  -6.750  -0.3109   0.01045   0.00437  -0.0956   0.8370   0.0173
  -6.500  -0.2813   0.01021   0.00411  -0.0962   0.8331   0.0178
  -6.250  -0.2517   0.01001   0.00388  -0.0968   0.8293   0.0184
  -6.000  -0.2219   0.00981   0.00367  -0.0973   0.8259   0.0192
  -5.750  -0.1919   0.00963   0.00348  -0.0979   0.8224   0.0199
  -5.500  -0.1619   0.00943   0.00327  -0.0986   0.8187   0.0211
  -5.250  -0.1319   0.00925   0.00309  -0.0992   0.8152   0.0224
  -5.000  -0.1019   0.00911   0.00293  -0.0997   0.8118   0.0239
  -4.750  -0.0716   0.00894   0.00277  -0.1004   0.8087   0.0258
  -4.500  -0.0413   0.00879   0.00263  -0.1010   0.8052   0.0282
  -4.250  -0.0110   0.00865   0.00250  -0.1016   0.8013   0.0311
  -4.000   0.0191   0.00853   0.00238  -0.1022   0.7976   0.0344
  -3.750   0.0494   0.00840   0.00226  -0.1028   0.7942   0.0392
  -3.500   0.0800   0.00825   0.00216  -0.1035   0.7908   0.0468
  -3.250   0.1107   0.00808   0.00205  -0.1043   0.7871   0.0624
  -3.000   0.1419   0.00783   0.00193  -0.1052   0.7835   0.0999
  -2.750   0.1737   0.00750   0.00180  -0.1064   0.7798   0.1662
  -2.500   0.2067   0.00702   0.00168  -0.1081   0.7758   0.2721
  -2.250   0.2394   0.00663   0.00157  -0.1096   0.7701   0.3615
  -1.750   0.3050   0.00590   0.00146  -0.1124   0.7563   0.5688
  -1.500   0.3353   0.00586   0.00149  -0.1130   0.7490   0.6123
  -1.250   0.3654   0.00587   0.00153  -0.1134   0.7417   0.6347
  -1.000   0.3950   0.00591   0.00154  -0.1137   0.7327   0.6441
  -0.750   0.4246   0.00594   0.00154  -0.1141   0.7224   0.6478
  -0.500   0.4541   0.00599   0.00156  -0.1144   0.7124   0.6516
   0.000   0.5119   0.00617   0.00159  -0.1147   0.6731   0.6603
   0.250   0.5399   0.00636   0.00162  -0.1147   0.6390   0.6635
   0.500   0.5675   0.00657   0.00169  -0.1147   0.5977   0.6668
   0.750   0.5943   0.00690   0.00182  -0.1146   0.5499   0.6714
   1.000   0.6202   0.00734   0.00200  -0.1143   0.4905   0.6765
   1.250   0.6453   0.00788   0.00222  -0.1140   0.4196   0.6807
   1.500   0.6715   0.00827   0.00242  -0.1138   0.3716   0.6846
   1.750   0.6972   0.00870   0.00262  -0.1136   0.3180   0.6880
   2.000   0.7232   0.00909   0.00282  -0.1134   0.2768   0.6906
   2.250   0.7499   0.00940   0.00299  -0.1133   0.2470   0.6930
   2.500   0.7763   0.00972   0.00317  -0.1132   0.2170   0.6952
   2.750   0.8024   0.01006   0.00337  -0.1130   0.1864   0.6976
   3.000   0.8290   0.01034   0.00357  -0.1128   0.1666   0.7001
   3.250   0.8559   0.01058   0.00375  -0.1127   0.1535   0.7027
   3.500   0.8827   0.01082   0.00394  -0.1126   0.1408   0.7054
   3.750   0.9093   0.01107   0.00414  -0.1125   0.1275   0.7082
   4.000   0.9359   0.01131   0.00433  -0.1123   0.1170   0.7108
   4.250   0.9623   0.01156   0.00453  -0.1122   0.1081   0.7133
   4.500   0.9885   0.01181   0.00476  -0.1120   0.1000   0.7160
   4.750   1.0149   0.01204   0.00498  -0.1118   0.0943   0.7189
   5.000   1.0410   0.01228   0.00521  -0.1115   0.0888   0.7218
   5.250   1.0668   0.01255   0.00545  -0.1112   0.0834   0.7246
   5.500   1.0929   0.01277   0.00568  -0.1110   0.0802   0.7274
   5.750   1.1184   0.01304   0.00593  -0.1107   0.0760   0.7301
   6.000   1.1436   0.01332   0.00621  -0.1103   0.0717   0.7331
   6.250   1.1691   0.01355   0.00646  -0.1100   0.0692   0.7364
   6.500   1.1938   0.01385   0.00675  -0.1095   0.0652   0.7397
   6.750   1.2181   0.01417   0.00705  -0.1090   0.0612   0.7429
   7.250   1.2668   0.01474   0.00765  -0.1079   0.0560   0.7488
   7.500   1.2901   0.01509   0.00799  -0.1072   0.0528   0.7521
   7.750   1.3138   0.01539   0.00833  -0.1066   0.0509   0.7555
   8.000   1.3370   0.01571   0.00867  -0.1059   0.0488   0.7590
   8.500   1.3809   0.01648   0.00945  -0.1041   0.0438   0.7658
   8.750   1.4029   0.01682   0.00983  -0.1032   0.0423   0.7698
   9.000   1.4237   0.01720   0.01024  -0.1021   0.0402   0.7741
   9.250   1.4431   0.01765   0.01069  -0.1007   0.0379   0.7780
   9.500   1.4621   0.01807   0.01115  -0.0993   0.0363   0.7821
   9.750   1.4785   0.01848   0.01161  -0.0974   0.0349   0.7865
  10.000   1.4955   0.01896   0.01211  -0.0956   0.0334   0.7909
  10.250   1.5122   0.01951   0.01268  -0.0939   0.0317   0.7949
  10.500   1.5291   0.02005   0.01328  -0.0923   0.0305   0.7992
  10.750   1.5463   0.02059   0.01387  -0.0908   0.0294   0.8039
  11.000   1.5628   0.02118   0.01450  -0.0892   0.0283   0.8085
  11.250   1.5784   0.02185   0.01519  -0.0876   0.0269   0.8129
  11.500   1.5933   0.02257   0.01596  -0.0859   0.0256   0.8179
  11.750   1.6091   0.02323   0.01668  -0.0843   0.0247   0.8231
  12.000   1.6240   0.02395   0.01747  -0.0828   0.0237   0.8282
  12.250   1.6382   0.02475   0.01831  -0.0812   0.0227   0.8344
  12.500   1.6513   0.02563   0.01924  -0.0795   0.0218   0.8409
  12.750   1.6643   0.02652   0.02020  -0.0778   0.0211   0.8480
  13.000   1.6779   0.02739   0.02115  -0.0763   0.0206   0.8561
  13.250   1.6905   0.02832   0.02217  -0.0747   0.0201   0.8648
  13.500   1.7024   0.02932   0.02324  -0.0731   0.0195   0.8745
  13.750   1.7133   0.03039   0.02439  -0.0715   0.0189   0.8862
  14.000   1.7230   0.03154   0.02563  -0.0698   0.0183   0.9018
  14.250   1.7269   0.03261   0.02686  -0.0670   0.0177   1.0000
  14.500   1.7367   0.03390   0.02821  -0.0656   0.0173   1.0000
  14.750   1.7463   0.03522   0.02961  -0.0642   0.0169   1.0000
  15.000   1.7550   0.03665   0.03110  -0.0629   0.0166   1.0000
  15.250   1.7630   0.03816   0.03269  -0.0616   0.0163   1.0000
  15.500   1.7698   0.03979   0.03439  -0.0603   0.0159   1.0000
  15.750   1.7755   0.04155   0.03621  -0.0590   0.0156   1.0000
  16.000   1.7805   0.04343   0.03817  -0.0578   0.0153   1.0000
  16.250   1.7843   0.04547   0.04028  -0.0567   0.0150   1.0000
  16.500   1.7870   0.04768   0.04257  -0.0556   0.0146   1.0000
  16.750   1.7881   0.05012   0.04509  -0.0546   0.0143   1.0000
  17.000   1.7895   0.05262   0.04769  -0.0539   0.0141   1.0000
  17.250   1.7913   0.05514   0.05030  -0.0533   0.0139   1.0000
  17.500   1.7921   0.05786   0.05312  -0.0529   0.0137   1.0000
  17.750   1.7913   0.06084   0.05620  -0.0526   0.0134   1.0000
  18.000   1.7889   0.06408   0.05954  -0.0524   0.0131   1.0000
  18.250   1.7851   0.06764   0.06320  -0.0526   0.0129   1.0000
  18.500   1.7794   0.07158   0.06725  -0.0530   0.0127   1.0000
  18.750   1.7721   0.07586   0.07164  -0.0536   0.0124   1.0000
  19.000   1.7623   0.08063   0.07653  -0.0547   0.0122   1.0000
  19.250   1.7500   0.08592   0.08194  -0.0561   0.0120   1.0000
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