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


Details Polar file
Airfoil: NASA/LANGLEY LS(1)-0413 (GA(W)-2) AIRFOIL (ls413-il)
Reynolds number: 1,000,000
Max Cl/Cd: 112.36 at α=2°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-ls413-il-1000000.txt
Download as CSV file: xf-ls413-il-1000000.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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -13.000  -0.4669   0.12244   0.12060  -0.0372   1.0000   0.0217
 -12.750  -0.8453   0.04056   0.03754  -0.0817   1.0000   0.0169
 -12.500  -0.8683   0.03859   0.03547  -0.0779   0.9992   0.0169
 -12.250  -0.8591   0.03454   0.03115  -0.0826   0.9947   0.0169
 -12.000  -0.8412   0.03188   0.02831  -0.0855   0.9916   0.0171
 -11.750  -0.7365   0.04664   0.04411  -0.0805   0.9975   0.0208
 -11.500  -0.7194   0.04401   0.04144  -0.0829   0.9947   0.0196
 -11.250  -0.7235   0.03766   0.03472  -0.0889   0.9876   0.0192
 -11.000  -0.7198   0.03138   0.02794  -0.0925   0.9826   0.0188
 -10.750  -0.7119   0.02662   0.02271  -0.0934   0.9740   0.0184
 -10.500  -0.6918   0.02391   0.01968  -0.0943   0.9689   0.0184
 -10.250  -0.6716   0.02226   0.01783  -0.0942   0.9611   0.0185
 -10.000  -0.6496   0.02052   0.01587  -0.0942   0.9549   0.0185
  -9.750  -0.6271   0.01922   0.01442  -0.0940   0.9474   0.0186
  -9.500  -0.6033   0.01814   0.01320  -0.0939   0.9411   0.0187
  -9.250  -0.5785   0.01720   0.01216  -0.0939   0.9348   0.0189
  -9.000  -0.5533   0.01639   0.01124  -0.0939   0.9288   0.0191
  -8.750  -0.5274   0.01567   0.01042  -0.0940   0.9234   0.0193
  -8.500  -0.5009   0.01501   0.00969  -0.0941   0.9178   0.0195
  -8.250  -0.4742   0.01442   0.00903  -0.0943   0.9123   0.0197
  -8.000  -0.4470   0.01393   0.00846  -0.0945   0.9072   0.0199
  -7.750  -0.4193   0.01345   0.00794  -0.0948   0.9019   0.0201
  -7.500  -0.3918   0.01286   0.00728  -0.0951   0.8968   0.0203
  -7.250  -0.3644   0.01202   0.00637  -0.0956   0.8921   0.0208
  -7.000  -0.3356   0.01152   0.00586  -0.0962   0.8876   0.0213
  -6.750  -0.3066   0.01116   0.00548  -0.0968   0.8830   0.0218
  -6.500  -0.2774   0.01085   0.00514  -0.0973   0.8787   0.0223
  -6.250  -0.2480   0.01056   0.00481  -0.0978   0.8745   0.0230
  -6.000  -0.2182   0.01028   0.00450  -0.0984   0.8702   0.0237
  -5.750  -0.1885   0.01005   0.00425  -0.0990   0.8660   0.0243
  -5.500  -0.1584   0.00965   0.00381  -0.0997   0.8620   0.0260
  -5.250  -0.1284   0.00945   0.00361  -0.1003   0.8581   0.0275
  -5.000  -0.0982   0.00927   0.00342  -0.1009   0.8542   0.0291
  -4.750  -0.0677   0.00897   0.00312  -0.1017   0.8502   0.0321
  -4.500  -0.0377   0.00883   0.00296  -0.1022   0.8463   0.0350
  -4.250  -0.0071   0.00861   0.00274  -0.1030   0.8425   0.0405
  -4.000   0.0236   0.00840   0.00257  -0.1037   0.8386   0.0476
  -3.750   0.0545   0.00816   0.00240  -0.1045   0.8348   0.0659
  -3.500   0.0870   0.00762   0.00219  -0.1061   0.8312   0.1552
  -3.250   0.1206   0.00700   0.00201  -0.1081   0.8276   0.2878
  -3.000   0.1545   0.00643   0.00186  -0.1100   0.8243   0.4082
  -2.750   0.1887   0.00588   0.00177  -0.1119   0.8206   0.5470
  -2.500   0.2196   0.00578   0.00179  -0.1126   0.8164   0.6012
  -2.250   0.2496   0.00582   0.00182  -0.1130   0.8113   0.6238
  -2.000   0.2797   0.00580   0.00183  -0.1134   0.8058   0.6395
  -1.750   0.3094   0.00582   0.00184  -0.1137   0.8000   0.6531
  -1.500   0.3390   0.00589   0.00188  -0.1140   0.7945   0.6669
  -1.250   0.3689   0.00593   0.00193  -0.1143   0.7886   0.6784
  -1.000   0.3983   0.00593   0.00193  -0.1145   0.7822   0.6843
  -0.750   0.4279   0.00595   0.00193  -0.1148   0.7755   0.6877
  -0.500   0.4576   0.00597   0.00193  -0.1151   0.7688   0.6912
  -0.250   0.4871   0.00603   0.00193  -0.1154   0.7616   0.6947
   0.000   0.5163   0.00603   0.00192  -0.1156   0.7500   0.6984
   0.250   0.5456   0.00605   0.00193  -0.1159   0.7392   0.7016
   0.500   0.5748   0.00611   0.00195  -0.1161   0.7304   0.7046
   0.750   0.6044   0.00614   0.00199  -0.1164   0.7220   0.7084
   1.000   0.6337   0.00622   0.00203  -0.1166   0.7115   0.7124
   1.250   0.6624   0.00626   0.00206  -0.1168   0.6977   0.7168
   1.500   0.6910   0.00635   0.00212  -0.1169   0.6826   0.7205
   1.750   0.7195   0.00646   0.00218  -0.1170   0.6613   0.7235
   2.000   0.7472   0.00665   0.00225  -0.1169   0.6300   0.7262
   2.250   0.7729   0.00703   0.00237  -0.1166   0.5725   0.7286
   2.500   0.7962   0.00763   0.00262  -0.1159   0.4917   0.7312
   2.750   0.8187   0.00835   0.00295  -0.1151   0.4046   0.7337
   3.000   0.8426   0.00892   0.00324  -0.1145   0.3413   0.7363
   3.250   0.8667   0.00945   0.00351  -0.1140   0.2867   0.7391
   3.500   0.8916   0.00990   0.00377  -0.1137   0.2461   0.7418
   3.750   0.9164   0.01035   0.00403  -0.1133   0.2068   0.7445
   4.000   0.9416   0.01073   0.00427  -0.1129   0.1790   0.7473
   4.250   0.9670   0.01106   0.00452  -0.1126   0.1596   0.7501
   4.500   0.9926   0.01137   0.00477  -0.1123   0.1436   0.7529
   4.750   1.0183   0.01167   0.00501  -0.1120   0.1295   0.7560
   5.000   1.0438   0.01198   0.00526  -0.1116   0.1173   0.7591
   5.250   1.0693   0.01229   0.00552  -0.1113   0.1079   0.7618
   5.500   1.0945   0.01258   0.00578  -0.1109   0.1006   0.7650
   5.750   1.1199   0.01284   0.00606  -0.1106   0.0948   0.7680
   6.000   1.1450   0.01313   0.00633  -0.1102   0.0898   0.7712
   6.250   1.1692   0.01349   0.00667  -0.1096   0.0838   0.7748
   6.500   1.1949   0.01372   0.00692  -0.1093   0.0808   0.7781
   6.750   1.2191   0.01402   0.00722  -0.1088   0.0767   0.7817
   7.000   1.2423   0.01441   0.00760  -0.1080   0.0719   0.7852
   7.250   1.2672   0.01464   0.00787  -0.1076   0.0698   0.7890
   7.500   1.2910   0.01496   0.00819  -0.1070   0.0667   0.7928
   7.750   1.3135   0.01535   0.00857  -0.1062   0.0629   0.7965
   8.000   1.3363   0.01569   0.00896  -0.1054   0.0605   0.8003
   8.250   1.3594   0.01598   0.00929  -0.1046   0.0584   0.8045
   8.500   1.3814   0.01637   0.00967  -0.1037   0.0557   0.8087
   8.750   1.4009   0.01688   0.01018  -0.1024   0.0521   0.8130
   9.000   1.4227   0.01717   0.01053  -0.1015   0.0506   0.8175
   9.250   1.4432   0.01754   0.01093  -0.1003   0.0485   0.8225
   9.500   1.4616   0.01800   0.01140  -0.0988   0.0461   0.8273
   9.750   1.4752   0.01855   0.01199  -0.0964   0.0436   0.8325
  10.000   1.4937   0.01894   0.01244  -0.0949   0.0424   0.8379
  10.250   1.5114   0.01942   0.01296  -0.0933   0.0406   0.8433
  10.500   1.5275   0.02000   0.01357  -0.0916   0.0387   0.8490
  10.750   1.5416   0.02076   0.01436  -0.0896   0.0366   0.8554
  11.000   1.5591   0.02126   0.01494  -0.0881   0.0356   0.8617
  11.250   1.5755   0.02185   0.01558  -0.0866   0.0342   0.8690
  11.500   1.5903   0.02256   0.01632  -0.0849   0.0326   0.8765
  11.750   1.6012   0.02355   0.01736  -0.0827   0.0307   0.8858
  12.000   1.6171   0.02414   0.01805  -0.0812   0.0301   0.8964
  12.250   1.6314   0.02481   0.01882  -0.0795   0.0291   0.9115
  12.500   1.6388   0.02541   0.01956  -0.0765   0.0283   1.0000
  12.750   1.6520   0.02639   0.02056  -0.0750   0.0273   1.0000
  13.000   1.6623   0.02760   0.02180  -0.0733   0.0263   1.0000
  13.250   1.6718   0.02886   0.02313  -0.0715   0.0255   1.0000
  13.500   1.6850   0.02985   0.02419  -0.0701   0.0251   1.0000
  13.750   1.6973   0.03091   0.02531  -0.0688   0.0245   1.0000
  14.000   1.7090   0.03204   0.02650  -0.0674   0.0239   1.0000
  14.250   1.7193   0.03329   0.02780  -0.0660   0.0233   1.0000
  14.500   1.7279   0.03470   0.02925  -0.0646   0.0227   1.0000
  14.750   1.7343   0.03633   0.03094  -0.0630   0.0221   1.0000
  15.000   1.7366   0.03836   0.03305  -0.0613   0.0215   1.0000
  15.250   1.7400   0.04032   0.03511  -0.0598   0.0212   1.0000
  15.500   1.7478   0.04191   0.03678  -0.0586   0.0209   1.0000
  15.750   1.7537   0.04372   0.03868  -0.0575   0.0207   1.0000
  16.000   1.7586   0.04569   0.04073  -0.0564   0.0204   1.0000
  16.250   1.7630   0.04774   0.04287  -0.0555   0.0200   1.0000
  16.500   1.7665   0.04994   0.04515  -0.0546   0.0197   1.0000
  16.750   1.7691   0.05231   0.04761  -0.0539   0.0194   1.0000
  17.000   1.7703   0.05491   0.05030  -0.0533   0.0190   1.0000
  17.250   1.7699   0.05779   0.05326  -0.0529   0.0187   1.0000
  17.500   1.7668   0.06107   0.05662  -0.0526   0.0183   1.0000
  17.750   1.7598   0.06496   0.06062  -0.0526   0.0180   1.0000
  18.000   1.7498   0.06942   0.06519  -0.0529   0.0178   1.0000
  18.250   1.7359   0.07465   0.07055  -0.0537   0.0175   1.0000
  18.500   1.7290   0.07903   0.07505  -0.0546   0.0174   1.0000
  18.750   1.7212   0.08365   0.07980  -0.0558   0.0172   1.0000
  19.000   1.7116   0.08869   0.08497  -0.0573   0.0171   1.0000
  19.250   1.6990   0.09436   0.09077  -0.0593   0.0170   1.0000
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