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NASA NLF1015 (nlf1015-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: NASA NLF1015 (nlf1015-il)
Reynolds number: 1,000,000
Max Cl/Cd: 154.56 at α=3.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-nlf1015-il-1000000-n5.txt
Download as CSV file: xf-nlf1015-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NASA  NLF1015                                   
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -15.500  -0.0628   0.12874   0.12689  -0.1138   0.9436   0.0067
 -15.250  -0.0515   0.12531   0.12343  -0.1174   0.9411   0.0068
 -15.000  -0.1974   0.13909   0.13717  -0.1013   0.9755   0.0065
 -14.500  -0.1938   0.13225   0.13035  -0.1025   0.9641   0.0065
 -14.250  -0.1903   0.12845   0.12655  -0.1038   0.9578   0.0065
 -14.000  -0.1857   0.12341   0.12149  -0.1066   0.9525   0.0065
 -13.000  -0.3581   0.05066   0.04828  -0.1555   0.9333   0.0069
 -12.750  -0.3572   0.03891   0.03609  -0.1749   0.9228   0.0068
 -12.500  -0.3436   0.03347   0.03030  -0.1853   0.9057   0.0069
 -12.250  -0.3401   0.03052   0.02708  -0.1884   0.8860   0.0069
 -12.000  -0.3467   0.02793   0.02423  -0.1884   0.8685   0.0069
 -11.750  -0.3403   0.02685   0.02304  -0.1878   0.8562   0.0070
 -11.500  -0.3398   0.02542   0.02144  -0.1865   0.8448   0.0071
 -11.250  -0.3373   0.02428   0.02016  -0.1850   0.8349   0.0072
 -11.000  -0.3361   0.02309   0.01884  -0.1830   0.8265   0.0072
 -10.750  -0.3367   0.02213   0.01775  -0.1802   0.8189   0.0073
 -10.500  -0.3323   0.02102   0.01649  -0.1782   0.8121   0.0074
 -10.250  -0.3221   0.02006   0.01537  -0.1767   0.8064   0.0074
 -10.000  -0.3086   0.01912   0.01430  -0.1755   0.8016   0.0076
  -9.750  -0.2936   0.01821   0.01325  -0.1745   0.7967   0.0076
  -9.500  -0.2772   0.01738   0.01229  -0.1734   0.7921   0.0077
  -9.250  -0.2579   0.01673   0.01153  -0.1728   0.7881   0.0079
  -9.000  -0.2385   0.01601   0.01071  -0.1721   0.7838   0.0080
  -8.750  -0.2181   0.01538   0.00997  -0.1715   0.7798   0.0082
  -8.250  -0.1740   0.01430   0.00871  -0.1707   0.7733   0.0085
  -8.000  -0.1508   0.01382   0.00816  -0.1705   0.7701   0.0087
  -7.750  -0.1271   0.01339   0.00767  -0.1703   0.7669   0.0088
  -7.500  -0.1029   0.01301   0.00722  -0.1701   0.7639   0.0089
  -7.250  -0.0785   0.01264   0.00677  -0.1699   0.7611   0.0090
  -7.000  -0.0531   0.01228   0.00638  -0.1700   0.7585   0.0091
  -6.750  -0.0292   0.01161   0.00563  -0.1699   0.7556   0.0093
  -6.500  -0.0040   0.01115   0.00512  -0.1700   0.7527   0.0096
  -6.250   0.0221   0.01080   0.00472  -0.1702   0.7500   0.0098
  -6.000   0.0487   0.01050   0.00437  -0.1704   0.7476   0.0101
  -5.750   0.0759   0.01025   0.00410  -0.1707   0.7455   0.0104
  -5.500   0.1035   0.01000   0.00382  -0.1710   0.7434   0.0108
  -5.250   0.1313   0.00978   0.00358  -0.1714   0.7412   0.0113
  -5.000   0.1593   0.00957   0.00334  -0.1718   0.7390   0.0117
  -4.750   0.1873   0.00938   0.00312  -0.1722   0.7368   0.0122
  -4.500   0.2153   0.00923   0.00292  -0.1725   0.7346   0.0125
  -4.250   0.2435   0.00908   0.00274  -0.1729   0.7325   0.0129
  -4.000   0.2721   0.00891   0.00254  -0.1734   0.7306   0.0138
  -3.750   0.3009   0.00877   0.00239  -0.1739   0.7288   0.0149
  -3.500   0.3297   0.00865   0.00227  -0.1744   0.7270   0.0163
  -3.250   0.3589   0.00844   0.00212  -0.1751   0.7251   0.0348
  -3.000   0.3884   0.00818   0.00200  -0.1759   0.7232   0.0742
  -2.750   0.4182   0.00792   0.00190  -0.1768   0.7213   0.1252
  -2.500   0.4482   0.00766   0.00181  -0.1778   0.7194   0.1863
  -2.250   0.4784   0.00745   0.00175  -0.1788   0.7175   0.2444
  -2.000   0.5098   0.00714   0.00169  -0.1802   0.7160   0.3289
  -1.750   0.5444   0.00654   0.00162  -0.1826   0.7146   0.5070
  -1.500   0.5747   0.00643   0.00167  -0.1835   0.7128   0.5706
  -1.250   0.6038   0.00644   0.00169  -0.1839   0.7109   0.5869
  -1.000   0.6327   0.00646   0.00172  -0.1844   0.7090   0.5985
  -0.750   0.6614   0.00649   0.00174  -0.1847   0.7072   0.6064
  -0.500   0.6901   0.00652   0.00177  -0.1851   0.7054   0.6140
  -0.250   0.7187   0.00657   0.00180  -0.1855   0.7034   0.6208
   0.000   0.7474   0.00661   0.00184  -0.1858   0.7015   0.6273
   0.250   0.7757   0.00664   0.00188  -0.1861   0.6994   0.6335
   0.500   0.8037   0.00666   0.00192  -0.1864   0.6965   0.6388
   0.750   0.8313   0.00669   0.00197  -0.1865   0.6932   0.6438
   1.000   0.8586   0.00675   0.00201  -0.1866   0.6896   0.6489
   1.250   0.8859   0.00680   0.00206  -0.1866   0.6862   0.6533
   1.500   0.9133   0.00682   0.00211  -0.1867   0.6825   0.6569
   1.750   0.9402   0.00687   0.00216  -0.1867   0.6782   0.6597
   2.000   0.9665   0.00693   0.00222  -0.1866   0.6740   0.6623
   2.250   0.9934   0.00698   0.00228  -0.1866   0.6699   0.6648
   2.500   1.0199   0.00702   0.00234  -0.1865   0.6650   0.6672
   2.750   1.0454   0.00709   0.00241  -0.1862   0.6599   0.6694
   3.000   1.0712   0.00714   0.00249  -0.1860   0.6543   0.6718
   3.250   1.0959   0.00721   0.00257  -0.1855   0.6469   0.6744
   3.500   1.1201   0.00729   0.00266  -0.1850   0.6394   0.6773
   3.750   1.1422   0.00739   0.00275  -0.1839   0.6301   0.6801
   4.250   1.1818   0.00766   0.00299  -0.1809   0.6018   0.6852
   4.500   1.1933   0.00801   0.00322  -0.1777   0.5710   0.6881
   4.750   1.1949   0.00873   0.00369  -0.1725   0.5168   0.6912
   5.000   1.1979   0.00952   0.00423  -0.1678   0.4678   0.6946
   5.500   1.2072   0.01112   0.00540  -0.1594   0.3771   0.7012
   5.750   1.2134   0.01191   0.00602  -0.1557   0.3372   0.7047
   6.000   1.2182   0.01281   0.00672  -0.1519   0.2963   0.7083
   6.250   1.2228   0.01376   0.00748  -0.1481   0.2569   0.7119
   6.500   1.2272   0.01477   0.00831  -0.1445   0.2173   0.7153
   6.750   1.2307   0.01590   0.00924  -0.1408   0.1771   0.7191
   7.000   1.2367   0.01696   0.01015  -0.1377   0.1452   0.7233
   7.250   1.2454   0.01794   0.01102  -0.1351   0.1196   0.7276
   7.500   1.2535   0.01900   0.01196  -0.1325   0.0937   0.7318
   7.750   1.2631   0.02003   0.01291  -0.1302   0.0723   0.7365
   8.000   1.2702   0.02125   0.01401  -0.1276   0.0484   0.7412
   8.250   1.2784   0.02245   0.01511  -0.1253   0.0294   0.7456
   8.500   1.2860   0.02374   0.01633  -0.1230   0.0119   0.7504
   8.750   1.2988   0.02471   0.01731  -0.1214   0.0078   0.7556
   9.000   1.3138   0.02556   0.01819  -0.1201   0.0068   0.7606
   9.250   1.3288   0.02640   0.01910  -0.1188   0.0062   0.7662
   9.500   1.3440   0.02726   0.02001  -0.1177   0.0059   0.7724
   9.750   1.3584   0.02818   0.02099  -0.1164   0.0056   0.7786
  10.000   1.3729   0.02911   0.02198  -0.1153   0.0054   0.7857
  10.250   1.3865   0.03014   0.02307  -0.1140   0.0052   0.7925
  10.500   1.3994   0.03123   0.02423  -0.1127   0.0049   0.7999
  10.750   1.4117   0.03239   0.02545  -0.1114   0.0046   0.8072
  11.000   1.4224   0.03372   0.02686  -0.1100   0.0043   0.8155
  11.250   1.4355   0.03484   0.02806  -0.1089   0.0043   0.8242
  11.500   1.4480   0.03605   0.02934  -0.1078   0.0042   0.8341
  11.750   1.4601   0.03728   0.03066  -0.1066   0.0041   0.8450
  12.000   1.4713   0.03861   0.03207  -0.1054   0.0040   0.8581
  12.250   1.4821   0.03995   0.03353  -0.1042   0.0039   0.8745
  12.500   1.4911   0.04135   0.03504  -0.1027   0.0038   0.8986
  12.750   1.4955   0.04254   0.03639  -0.1004   0.0037   1.0000
  13.000   1.5052   0.04417   0.03808  -0.0993   0.0037   1.0000
  13.250   1.5146   0.04585   0.03983  -0.0984   0.0036   1.0000
  13.500   1.5232   0.04765   0.04168  -0.0974   0.0035   1.0000
  13.750   1.5318   0.04947   0.04357  -0.0965   0.0034   1.0000
  14.000   1.5391   0.05147   0.04564  -0.0956   0.0034   1.0000
  14.250   1.5465   0.05349   0.04774  -0.0947   0.0033   1.0000
  14.500   1.5531   0.05562   0.04994  -0.0940   0.0032   1.0000
  14.750   1.5594   0.05782   0.05221  -0.0932   0.0032   1.0000
  15.000   1.5642   0.06024   0.05471  -0.0925   0.0031   1.0000
  15.250   1.5693   0.06268   0.05722  -0.0919   0.0031   1.0000
  15.500   1.5726   0.06538   0.06001  -0.0913   0.0030   1.0000
  15.750   1.5751   0.06825   0.06296  -0.0909   0.0030   1.0000
  16.000   1.5765   0.07129   0.06609  -0.0905   0.0029   1.0000
  16.250   1.5762   0.07463   0.06953  -0.0902   0.0029   1.0000
  16.500   1.5740   0.07831   0.07331  -0.0900   0.0028   1.0000
  16.750   1.5701   0.08233   0.07745  -0.0900   0.0028   1.0000
  17.000   1.5638   0.08680   0.08205  -0.0903   0.0027   1.0000
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