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NASA/LANGLEY LS(1)-0413 (GA(W)-2) AIRFOIL (ls413-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: NASA/LANGLEY LS(1)-0413 (GA(W)-2) AIRFOIL (ls413-il)
Reynolds number: 500,000
Max Cl/Cd: 96.18 at α=3°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-ls413-il-500000.txt
Download as CSV file: xf-ls413-il-500000.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 =     0.500 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -12.750  -0.3482   0.11359   0.11122  -0.0497   1.0000   0.0348
 -12.500  -0.3594   0.10794   0.10559  -0.0520   1.0000   0.0350
 -12.250  -0.3695   0.10254   0.10021  -0.0536   1.0000   0.0351
 -12.000  -0.3789   0.09787   0.09557  -0.0529   1.0000   0.0355
 -11.750  -0.3848   0.09566   0.09340  -0.0512   1.0000   0.0357
 -11.500  -0.3915   0.09314   0.09091  -0.0499   0.9997   0.0359
 -11.250  -0.3854   0.08898   0.08675  -0.0521   0.9985   0.0362
 -11.000  -0.3820   0.08415   0.08192  -0.0549   0.9972   0.0366
 -10.750  -0.3819   0.07834   0.07611  -0.0584   0.9957   0.0370
 -10.500  -0.3882   0.07066   0.06843  -0.0634   0.9943   0.0374
 -10.250  -0.4572   0.05077   0.04837  -0.0792   0.9905   0.0373
 -10.000  -0.4833   0.04319   0.04060  -0.0859   0.9850   0.0374
  -9.750  -0.4905   0.03805   0.03526  -0.0909   0.9787   0.0377
  -9.500  -0.4860   0.03363   0.03063  -0.0940   0.9731   0.0384
  -9.250  -0.4761   0.02946   0.02618  -0.0965   0.9687   0.0398
  -9.000  -0.5268   0.02857   0.02363  -0.0979   0.9688   0.0286
  -8.750  -0.5054   0.02559   0.02038  -0.0983   0.9626   0.0278
  -8.500  -0.4787   0.02307   0.01756  -0.0993   0.9587   0.0274
  -8.250  -0.4505   0.02116   0.01542  -0.1000   0.9555   0.0272
  -8.000  -0.4258   0.01982   0.01391  -0.0999   0.9496   0.0273
  -7.750  -0.3989   0.01865   0.01259  -0.1000   0.9450   0.0275
  -7.500  -0.3715   0.01765   0.01148  -0.1002   0.9412   0.0278
  -7.250  -0.3454   0.01682   0.01057  -0.1001   0.9360   0.0281
  -7.000  -0.3188   0.01608   0.00975  -0.1000   0.9308   0.0285
  -6.750  -0.2916   0.01545   0.00905  -0.1000   0.9266   0.0290
  -6.500  -0.2644   0.01487   0.00840  -0.1001   0.9219   0.0294
  -6.250  -0.2384   0.01389   0.00744  -0.1002   0.9167   0.0305
  -6.000  -0.2104   0.01343   0.00698  -0.1005   0.9124   0.0317
  -5.750  -0.1819   0.01301   0.00653  -0.1009   0.9087   0.0330
  -5.500  -0.1533   0.01261   0.00610  -0.1013   0.9041   0.0343
  -5.250  -0.1241   0.01204   0.00550  -0.1020   0.8997   0.0361
  -5.000  -0.0946   0.01161   0.00508  -0.1026   0.8959   0.0386
  -4.750  -0.0649   0.01134   0.00476  -0.1031   0.8925   0.0417
  -4.500  -0.0346   0.01091   0.00436  -0.1040   0.8884   0.0472
  -4.250  -0.0043   0.01057   0.00405  -0.1048   0.8843   0.0556
  -4.000   0.0266   0.01018   0.00374  -0.1057   0.8806   0.0778
  -3.750   0.0610   0.00901   0.00333  -0.1084   0.8775   0.2679
  -3.500   0.0967   0.00799   0.00307  -0.1113   0.8739   0.4695
  -3.250   0.1287   0.00766   0.00315  -0.1124   0.8696   0.5924
  -3.000   0.1586   0.00769   0.00321  -0.1128   0.8656   0.6269
  -2.750   0.1885   0.00775   0.00324  -0.1130   0.8622   0.6469
  -2.500   0.2182   0.00785   0.00331  -0.1133   0.8589   0.6636
  -2.250   0.2475   0.00796   0.00343  -0.1135   0.8547   0.6796
  -2.000   0.2761   0.00809   0.00359  -0.1133   0.8504   0.6953
  -1.750   0.3038   0.00823   0.00376  -0.1129   0.8465   0.7078
  -1.500   0.3332   0.00831   0.00379  -0.1131   0.8424   0.7146
  -1.250   0.3618   0.00831   0.00380  -0.1132   0.8366   0.7182
  -1.000   0.3908   0.00830   0.00375  -0.1132   0.8306   0.7220
  -0.750   0.4202   0.00834   0.00374  -0.1134   0.8244   0.7267
  -0.500   0.4494   0.00833   0.00371  -0.1136   0.8177   0.7308
  -0.250   0.4779   0.00834   0.00369  -0.1135   0.8114   0.7341
   0.000   0.5063   0.00833   0.00370  -0.1134   0.8028   0.7381
   0.250   0.5355   0.00835   0.00367  -0.1136   0.7957   0.7430
   0.500   0.5640   0.00833   0.00366  -0.1135   0.7856   0.7475
   0.750   0.5916   0.00833   0.00365  -0.1132   0.7753   0.7512
   1.000   0.6202   0.00833   0.00364  -0.1132   0.7659   0.7548
   1.250   0.6494   0.00834   0.00365  -0.1135   0.7569   0.7579
   1.500   0.6789   0.00837   0.00364  -0.1138   0.7481   0.7607
   1.750   0.7076   0.00836   0.00365  -0.1139   0.7367   0.7634
   2.000   0.7357   0.00838   0.00368  -0.1138   0.7239   0.7658
   2.250   0.7637   0.00841   0.00370  -0.1138   0.7093   0.7683
   2.500   0.7915   0.00847   0.00373  -0.1137   0.6891   0.7711
   2.750   0.8189   0.00858   0.00377  -0.1135   0.6633   0.7743
   3.000   0.8454   0.00879   0.00383  -0.1132   0.6238   0.7774
   3.250   0.8669   0.00930   0.00398  -0.1119   0.5449   0.7799
   3.500   0.8846   0.01019   0.00438  -0.1102   0.4453   0.7826
   3.750   0.9040   0.01100   0.00482  -0.1088   0.3679   0.7857
   4.000   0.9246   0.01175   0.00522  -0.1078   0.3001   0.7889
   4.250   0.9469   0.01238   0.00560  -0.1070   0.2510   0.7922
   4.500   0.9693   0.01296   0.00596  -0.1063   0.2087   0.7953
   4.750   0.9917   0.01346   0.00632  -0.1054   0.1795   0.7982
   5.000   1.0146   0.01392   0.00668  -0.1047   0.1590   0.8014
   5.250   1.0380   0.01436   0.00705  -0.1041   0.1430   0.8048
   5.500   1.0621   0.01475   0.00740  -0.1035   0.1306   0.8084
   5.750   1.0855   0.01515   0.00776  -0.1029   0.1208   0.8116
   6.000   1.1077   0.01558   0.00815  -0.1020   0.1123   0.8150
   6.250   1.1309   0.01594   0.00855  -0.1012   0.1064   0.8189
   6.500   1.1535   0.01638   0.00896  -0.1004   0.1004   0.8230
   6.750   1.1752   0.01685   0.00945  -0.0995   0.0952   0.8268
   7.000   1.1977   0.01718   0.00983  -0.0986   0.0911   0.8305
   7.250   1.2181   0.01767   0.01032  -0.0975   0.0864   0.8347
   7.500   1.2385   0.01818   0.01085  -0.0963   0.0825   0.8394
   7.750   1.2604   0.01852   0.01125  -0.0954   0.0792   0.8437
   8.000   1.2797   0.01897   0.01172  -0.0941   0.0757   0.8482
   8.250   1.2942   0.01971   0.01248  -0.0919   0.0719   0.8538
   8.500   1.3132   0.02002   0.01287  -0.0904   0.0697   0.8592
   8.750   1.3309   0.02041   0.01333  -0.0888   0.0669   0.8648
   9.000   1.3480   0.02099   0.01393  -0.0872   0.0641   0.8710
   9.250   1.3601   0.02187   0.01485  -0.0849   0.0611   0.8771
   9.500   1.3791   0.02231   0.01538  -0.0836   0.0592   0.8840
   9.750   1.3964   0.02283   0.01598  -0.0821   0.0569   0.8911
  10.000   1.4119   0.02347   0.01666  -0.0804   0.0546   0.8995
  10.250   1.4202   0.02461   0.01784  -0.0778   0.0519   0.9092
  10.500   1.4368   0.02508   0.01843  -0.0762   0.0504   0.9215
  10.750   1.4494   0.02562   0.01908  -0.0740   0.0486   0.9442
  11.000   1.4618   0.02628   0.01980  -0.0721   0.0468   1.0000
  11.250   1.4750   0.02742   0.02095  -0.0707   0.0449   1.0000
  11.500   1.4854   0.02879   0.02238  -0.0690   0.0433   1.0000
  11.750   1.5011   0.02972   0.02339  -0.0680   0.0420   1.0000
  12.000   1.5150   0.03076   0.02451  -0.0667   0.0407   1.0000
  12.250   1.5277   0.03189   0.02568  -0.0655   0.0395   1.0000
  12.500   1.5379   0.03323   0.02707  -0.0640   0.0383   1.0000
  12.750   1.5420   0.03513   0.02901  -0.0620   0.0371   1.0000
  13.000   1.5498   0.03675   0.03072  -0.0604   0.0363   1.0000
  13.250   1.5604   0.03811   0.03220  -0.0592   0.0356   1.0000
  13.500   1.5703   0.03954   0.03373  -0.0580   0.0346   1.0000
  13.750   1.5788   0.04109   0.03535  -0.0569   0.0337   1.0000
  14.000   1.5870   0.04269   0.03702  -0.0558   0.0329   1.0000
  14.250   1.5921   0.04461   0.03900  -0.0546   0.0321   1.0000
  14.500   1.5929   0.04700   0.04145  -0.0533   0.0314   1.0000
  14.750   1.5892   0.04989   0.04443  -0.0517   0.0307   1.0000
  15.000   1.5940   0.05201   0.04668  -0.0509   0.0303   1.0000
  15.250   1.5977   0.05432   0.04913  -0.0502   0.0299   1.0000
  15.500   1.6002   0.05682   0.05176  -0.0497   0.0293   1.0000
  15.750   1.6012   0.05955   0.05460  -0.0493   0.0288   1.0000
  16.000   1.6014   0.06247   0.05763  -0.0490   0.0283   1.0000
  16.250   1.6006   0.06560   0.06088  -0.0490   0.0278   1.0000
  16.500   1.5987   0.06899   0.06437  -0.0491   0.0275   1.0000
  16.750   1.5953   0.07265   0.06814  -0.0495   0.0271   1.0000
  17.000   1.5901   0.07667   0.07225  -0.0502   0.0268   1.0000
  17.250   1.5830   0.08105   0.07673  -0.0510   0.0264   1.0000
  17.500   1.5733   0.08587   0.08164  -0.0521   0.0260   1.0000
  17.750   1.5592   0.09145   0.08736  -0.0535   0.0256   1.0000
  18.000   1.5513   0.09657   0.09263  -0.0556   0.0254   1.0000
  18.250   1.5415   0.10209   0.09832  -0.0580   0.0252   1.0000
  18.500   1.5301   0.10808   0.10448  -0.0608   0.0250   1.0000
  18.750   1.5173   0.11444   0.11100  -0.0640   0.0248   1.0000
  19.000   1.5036   0.12109   0.11781  -0.0676   0.0246   1.0000
  19.250   1.4888   0.12806   0.12493  -0.0715   0.0243   1.0000
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