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NASA LRN 1015 (NASA TM 102840) (lrn1015-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: NASA LRN 1015 (NASA TM 102840) (lrn1015-il)
Reynolds number: 1,000,000
Max Cl/Cd: 134.37 at α=3.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-lrn1015-il-1000000-n5.txt
Download as CSV file: xf-lrn1015-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NASA LRN 1015 (NASA TM 102840)                  
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -11.500  -0.1234   0.08652   0.08339  -0.1057   0.7222   0.0067
 -11.250  -0.1286   0.08138   0.07825  -0.1079   0.7210   0.0065
 -11.000  -0.1372   0.07592   0.07283  -0.1106   0.7198   0.0067
 -10.750  -0.1534   0.06906   0.06600  -0.1143   0.7184   0.0067
 -10.500  -0.3021   0.04185   0.03859  -0.1297   0.7159   0.0068
 -10.250  -0.2364   0.04723   0.04410  -0.1296   0.7148   0.0069
 -10.000  -0.2956   0.04044   0.03709  -0.1260   0.7124   0.0069
  -9.750  -0.4093   0.02335   0.01879  -0.1153   0.7105   0.0073
  -9.500  -0.3943   0.02196   0.01722  -0.1140   0.7091   0.0074
  -9.250  -0.3800   0.02025   0.01527  -0.1125   0.7077   0.0076
  -9.000  -0.3624   0.01890   0.01371  -0.1114   0.7063   0.0077
  -8.750  -0.3425   0.01779   0.01243  -0.1104   0.7049   0.0078
  -8.500  -0.3213   0.01683   0.01133  -0.1096   0.7035   0.0080
  -8.250  -0.2986   0.01607   0.01043  -0.1090   0.7021   0.0082
  -8.000  -0.2752   0.01541   0.00965  -0.1084   0.7006   0.0084
  -7.750  -0.2508   0.01490   0.00903  -0.1079   0.6991   0.0086
  -7.500  -0.2263   0.01439   0.00843  -0.1075   0.6975   0.0087
  -7.250  -0.2015   0.01388   0.00784  -0.1071   0.6962   0.0088
  -7.000  -0.1783   0.01311   0.00699  -0.1064   0.6951   0.0091
  -6.750  -0.1528   0.01272   0.00657  -0.1061   0.6938   0.0092
  -6.500  -0.1270   0.01234   0.00616  -0.1059   0.6924   0.0094
  -6.250  -0.1008   0.01203   0.00583  -0.1056   0.6909   0.0096
  -6.000  -0.0746   0.01173   0.00550  -0.1054   0.6893   0.0098
  -5.750  -0.0484   0.01142   0.00516  -0.1052   0.6877   0.0101
  -5.500  -0.0221   0.01113   0.00482  -0.1049   0.6863   0.0103
  -5.250   0.0042   0.01083   0.00448  -0.1047   0.6849   0.0105
  -5.000   0.0306   0.01056   0.00417  -0.1045   0.6835   0.0108
  -4.750   0.0573   0.01034   0.00391  -0.1043   0.6819   0.0110
  -4.500   0.0844   0.01012   0.00367  -0.1042   0.6806   0.0112
  -4.250   0.1111   0.00983   0.00338  -0.1040   0.6791   0.0117
  -4.000   0.1385   0.00965   0.00320  -0.1040   0.6777   0.0122
  -3.750   0.1661   0.00949   0.00306  -0.1040   0.6762   0.0129
  -3.500   0.1937   0.00933   0.00288  -0.1039   0.6746   0.0134
  -3.250   0.2213   0.00918   0.00271  -0.1039   0.6729   0.0139
  -3.000   0.2487   0.00900   0.00253  -0.1039   0.6712   0.0147
  -2.750   0.2765   0.00887   0.00240  -0.1039   0.6696   0.0156
  -2.500   0.3043   0.00877   0.00228  -0.1039   0.6680   0.0168
  -2.250   0.3320   0.00867   0.00217  -0.1039   0.6663   0.0182
  -2.000   0.3601   0.00856   0.00208  -0.1040   0.6648   0.0204
  -1.750   0.3882   0.00846   0.00201  -0.1041   0.6632   0.0240
  -1.500   0.4162   0.00835   0.00194  -0.1041   0.6613   0.0308
  -1.250   0.4435   0.00815   0.00187  -0.1041   0.6594   0.0697
  -1.000   0.4691   0.00772   0.00179  -0.1040   0.6574   0.1911
  -0.750   0.4929   0.00707   0.00171  -0.1037   0.6553   0.3875
  -0.500   0.5149   0.00635   0.00166  -0.1031   0.6532   0.6152
  -0.250   0.5398   0.00613   0.00174  -0.1025   0.6510   0.7205
   0.000   0.5674   0.00611   0.00181  -0.1024   0.6489   0.7560
   0.250   0.5956   0.00613   0.00186  -0.1024   0.6458   0.7727
   0.500   0.6239   0.00615   0.00185  -0.1025   0.6411   0.7803
   0.750   0.6514   0.00618   0.00185  -0.1024   0.6354   0.7858
   1.000   0.6796   0.00620   0.00187  -0.1025   0.6295   0.7915
   1.250   0.7075   0.00624   0.00188  -0.1026   0.6239   0.7967
   1.500   0.7352   0.00629   0.00191  -0.1026   0.6192   0.8010
   1.750   0.7631   0.00632   0.00195  -0.1027   0.6129   0.8053
   2.000   0.7900   0.00639   0.00198  -0.1025   0.6057   0.8096
   2.250   0.8178   0.00645   0.00203  -0.1026   0.5981   0.8133
   2.500   0.8444   0.00653   0.00208  -0.1025   0.5905   0.8166
   2.750   0.8713   0.00660   0.00214  -0.1024   0.5809   0.8196
   3.000   0.8972   0.00670   0.00222  -0.1021   0.5699   0.8228
   3.250   0.9218   0.00686   0.00232  -0.1016   0.5534   0.8261
   3.500   0.9450   0.00708   0.00245  -0.1008   0.5331   0.8294
   3.750   0.9667   0.00736   0.00263  -0.0998   0.5099   0.8324
   4.000   0.9867   0.00768   0.00285  -0.0984   0.4847   0.8358
   4.250   1.0050   0.00806   0.00312  -0.0968   0.4566   0.8394
   4.500   1.0206   0.00853   0.00344  -0.0947   0.4243   0.8434
   4.750   1.0359   0.00899   0.00377  -0.0926   0.3956   0.8471
   5.000   1.0495   0.00946   0.00412  -0.0902   0.3684   0.8507
   5.250   1.0585   0.00999   0.00452  -0.0869   0.3379   0.8550
   5.500   1.0619   0.01051   0.00492  -0.0825   0.3104   0.8602
   6.000   1.0764   0.01150   0.00578  -0.0755   0.2740   0.8707
   6.250   1.0842   0.01202   0.00627  -0.0723   0.2599   0.8773
   6.500   1.0902   0.01266   0.00688  -0.0691   0.2457   0.8844
   6.750   1.0961   0.01340   0.00761  -0.0661   0.2318   0.8942
   7.000   1.1051   0.01408   0.00830  -0.0637   0.2206   0.9072
   7.250   1.1166   0.01474   0.00900  -0.0618   0.2104   0.9294
   7.500   1.1492   0.01551   0.00976  -0.0646   0.1960   0.9643
   7.750   1.1639   0.01626   0.01048  -0.0635   0.1868   1.0000
   8.000   1.1773   0.01702   0.01121  -0.0621   0.1775   1.0000
   8.250   1.1890   0.01788   0.01202  -0.0606   0.1672   1.0000
   8.500   1.2024   0.01866   0.01277  -0.0593   0.1594   1.0000
   8.750   1.2159   0.01944   0.01353  -0.0581   0.1524   1.0000
   9.000   1.2300   0.02020   0.01427  -0.0569   0.1458   1.0000
   9.250   1.2429   0.02104   0.01509  -0.0556   0.1394   1.0000
   9.500   1.2570   0.02181   0.01585  -0.0545   0.1337   1.0000
   9.750   1.2694   0.02270   0.01672  -0.0533   0.1271   1.0000
  10.000   1.2836   0.02349   0.01752  -0.0523   0.1226   1.0000
  10.250   1.2965   0.02436   0.01838  -0.0511   0.1172   1.0000
  10.500   1.3094   0.02524   0.01925  -0.0501   0.1119   1.0000
  10.750   1.3222   0.02616   0.02017  -0.0490   0.1071   1.0000
  11.000   1.3339   0.02715   0.02114  -0.0479   0.1017   1.0000
  11.250   1.3479   0.02800   0.02202  -0.0470   0.0984   1.0000
  11.500   1.3605   0.02899   0.02302  -0.0461   0.0946   1.0000
  11.750   1.3722   0.03007   0.02408  -0.0451   0.0898   1.0000
  12.000   1.3860   0.03101   0.02504  -0.0443   0.0871   1.0000
  12.250   1.3976   0.03213   0.02617  -0.0434   0.0829   1.0000
  12.500   1.4086   0.03330   0.02733  -0.0425   0.0788   1.0000
  12.750   1.4214   0.03436   0.02842  -0.0417   0.0758   1.0000
  13.000   1.4328   0.03555   0.02963  -0.0410   0.0728   1.0000
  13.250   1.4433   0.03684   0.03091  -0.0402   0.0695   1.0000
  13.500   1.4547   0.03805   0.03214  -0.0394   0.0666   1.0000
  13.750   1.4660   0.03930   0.03343  -0.0388   0.0644   1.0000
  14.000   1.4775   0.04054   0.03471  -0.0381   0.0629   1.0000
  14.250   1.4871   0.04195   0.03613  -0.0374   0.0602   1.0000
  14.500   1.4960   0.04347   0.03766  -0.0368   0.0573   1.0000
  14.750   1.5071   0.04480   0.03904  -0.0362   0.0556   1.0000
  15.000   1.5174   0.04621   0.04049  -0.0357   0.0540   1.0000
  15.250   1.5259   0.04781   0.04212  -0.0352   0.0522   1.0000
  15.500   1.5332   0.04952   0.04384  -0.0346   0.0493   1.0000
  15.750   1.5420   0.05114   0.04551  -0.0341   0.0474   1.0000
  16.000   1.5497   0.05289   0.04729  -0.0337   0.0450   1.0000
  16.250   1.5565   0.05473   0.04916  -0.0333   0.0430   1.0000
  16.500   1.5621   0.05674   0.05121  -0.0329   0.0407   1.0000
  16.750   1.5687   0.05864   0.05315  -0.0326   0.0381   1.0000
  17.000   1.5704   0.06112   0.05564  -0.0322   0.0343   1.0000
  17.250   1.5736   0.06347   0.05802  -0.0320   0.0307   1.0000
  17.500   1.5720   0.06641   0.06096  -0.0317   0.0261   1.0000
  17.750   1.5689   0.06958   0.06415  -0.0316   0.0221   1.0000
  18.000   1.5651   0.07291   0.06751  -0.0316   0.0188   1.0000
  18.250   1.5624   0.07621   0.07086  -0.0318   0.0168   1.0000
  18.500   1.5585   0.07975   0.07446  -0.0321   0.0143   1.0000
  18.750   1.5554   0.08325   0.07803  -0.0326   0.0125   1.0000
  19.000   1.5495   0.08719   0.08203  -0.0332   0.0100   1.0000
  19.250   1.5375   0.09209   0.08698  -0.0342   0.0068   1.0000
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