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NASA NLF1015 (nlf1015-il) Xfoil prediction polar at RE=200,000 Ncrit=9


Details Polar file
Airfoil: NASA NLF1015 (nlf1015-il)
Reynolds number: 200,000
Max Cl/Cd: 75.63 at α=7.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-nlf1015-il-200000.txt
Download as CSV file: xf-nlf1015-il-200000.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 =     0.200 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -10.750  -0.0384   0.09372   0.09019  -0.1173   0.9376   0.0612
 -10.500  -0.0302   0.08935   0.08581  -0.1206   0.9366   0.0639
 -10.250  -0.1477   0.09816   0.09455  -0.1157   0.9493   0.0577
 -10.000  -0.1383   0.09648   0.09286  -0.1143   0.9423   0.0599
  -9.750  -0.1256   0.09274   0.08911  -0.1178   0.9396   0.0624
  -9.500  -0.1209   0.08695   0.08333  -0.1256   0.9373   0.0665
  -9.250  -0.1594   0.07792   0.07430  -0.1392   0.9259   0.0681
  -9.000  -0.1828   0.07403   0.07032  -0.1429   0.9173   0.0682
  -8.750  -0.1148   0.07172   0.06813  -0.1386   0.9241   0.0715
  -8.500  -0.0991   0.06723   0.06362  -0.1439   0.9226   0.0741
  -8.250  -0.1217   0.06315   0.05953  -0.1456   0.9116   0.0748
  -8.000  -0.1462   0.05958   0.05591  -0.1466   0.9017   0.0757
  -7.500  -0.1256   0.03667   0.03287  -0.1460   0.8811   0.0858
  -7.250  -0.1106   0.03308   0.02914  -0.1483   0.8794   0.0891
  -7.000  -0.1728   0.03703   0.03110  -0.1499   0.8781   0.0451
  -6.750  -0.1950   0.03680   0.03105  -0.1420   0.8676   0.0467
  -6.500  -0.1657   0.03268   0.02645  -0.1434   0.8664   0.0400
  -6.250  -0.1326   0.02885   0.02185  -0.1451   0.8654   0.0366
  -6.000  -0.1515   0.02943   0.02234  -0.1372   0.8554   0.0364
  -5.750  -0.1207   0.02771   0.02037  -0.1382   0.8538   0.0365
  -5.500  -0.0881   0.02651   0.01908  -0.1396   0.8527   0.0383
  -5.250  -0.0539   0.02535   0.01780  -0.1410   0.8518   0.0398
  -5.000  -0.0193   0.02415   0.01648  -0.1424   0.8510   0.0405
  -4.750  -0.0398   0.02528   0.01760  -0.1345   0.8414   0.0406
  -4.500  -0.0108   0.02449   0.01676  -0.1350   0.8394   0.0420
  -4.250   0.0217   0.02377   0.01597  -0.1361   0.8381   0.0440
  -4.000   0.0578   0.02272   0.01493  -0.1384   0.8372   0.0482
  -3.750   0.0960   0.02199   0.01418  -0.1409   0.8365   0.0589
  -3.500   0.1445   0.01986   0.01314  -0.1472   0.8363   0.2829
  -3.250   0.1871   0.01884   0.01318  -0.1511   0.8359   0.5466
  -3.000   0.1651   0.02072   0.01512  -0.1430   0.8259   0.5714
  -2.750   0.1920   0.02112   0.01553  -0.1426   0.8239   0.6327
  -2.500   0.2210   0.02142   0.01582  -0.1422   0.8224   0.6684
  -2.250   0.2508   0.02164   0.01601  -0.1417   0.8213   0.6940
  -2.000   0.2327   0.02358   0.01799  -0.1345   0.8123   0.7023
  -1.750   0.2548   0.02398   0.01834  -0.1332   0.8095   0.7172
  -1.500   0.2822   0.02419   0.01849  -0.1328   0.8078   0.7308
  -1.250   0.3135   0.02427   0.01849  -0.1331   0.8066   0.7439
  -1.000   0.3014   0.02587   0.02014  -0.1269   0.7985   0.7505
  -0.750   0.3239   0.02624   0.02046  -0.1261   0.7952   0.7609
  -0.500   0.3512   0.02632   0.02051  -0.1257   0.7933   0.7705
  -0.250   0.3810   0.02629   0.02043  -0.1257   0.7919   0.7795
   0.000   0.4170   0.02617   0.02025  -0.1271   0.7910   0.7897
   0.250   0.4491   0.02591   0.01998  -0.1272   0.7902   0.7962
   0.500   0.4315   0.02795   0.02204  -0.1213   0.7787   0.8038
   0.750   0.4634   0.02776   0.02182  -0.1217   0.7772   0.8091
   1.000   0.4995   0.02752   0.02155  -0.1231   0.7762   0.8149
   1.250   0.5412   0.02719   0.02117  -0.1257   0.7756   0.8202
   1.500   0.5785   0.02677   0.02074  -0.1271   0.7750   0.8239
   1.750   0.5608   0.02874   0.02276  -0.1210   0.7624   0.8298
   2.000   0.6027   0.02838   0.02236  -0.1236   0.7615   0.8342
   2.250   0.6422   0.02784   0.02183  -0.1254   0.7608   0.8376
   2.500   0.6830   0.02727   0.02127  -0.1275   0.7604   0.8411
   2.750   0.6707   0.02916   0.02319  -0.1223   0.7476   0.8473
   3.000   0.6749   0.03032   0.02439  -0.1195   0.7384   0.8521
   3.250   0.7070   0.03005   0.02415  -0.1201   0.7354   0.8560
   3.500   0.7458   0.02952   0.02364  -0.1219   0.7339   0.8607
   3.750   0.7888   0.02880   0.02296  -0.1242   0.7330   0.8652
   4.000   0.8306   0.02786   0.02207  -0.1260   0.7324   0.8691
   4.250   0.8766   0.02681   0.02107  -0.1286   0.7320   0.8733
   4.500   0.9265   0.02572   0.02003  -0.1320   0.7316   0.8779
   4.750   0.9755   0.02458   0.01896  -0.1352   0.7311   0.8822
   5.000   1.0286   0.02338   0.01784  -0.1392   0.7304   0.8866
   5.250   1.0152   0.02455   0.01909  -0.1325   0.7182   0.8956
   5.500   1.0699   0.02306   0.01769  -0.1365   0.7174   0.9002
   5.750   1.1330   0.02154   0.01626  -0.1422   0.7163   0.9046
   6.000   1.1199   0.02224   0.01705  -0.1350   0.7049   0.9169
   6.250   1.1811   0.02069   0.01559  -0.1403   0.7029   0.9227
   6.500   1.1791   0.02089   0.01590  -0.1347   0.6931   0.9380
   6.750   1.2304   0.01948   0.01459  -0.1382   0.6886   0.9479
   7.000   1.2433   0.01926   0.01450  -0.1355   0.6784   1.0000
   7.250   1.3046   0.01790   0.01321  -0.1411   0.6714   1.0000
   7.500   1.3204   0.01795   0.01336  -0.1392   0.6582   1.0000
   7.750   1.3416   0.01774   0.01321  -0.1382   0.6426   1.0000
   8.000   1.3448   0.01817   0.01371  -0.1342   0.6213   1.0000
   8.250   1.3567   0.01831   0.01384  -0.1316   0.5929   1.0000
   8.500   1.3707   0.01850   0.01387  -0.1292   0.5505   1.0000
   8.750   1.3797   0.01919   0.01425  -0.1262   0.5000   1.0000
   9.000   1.3781   0.02057   0.01529  -0.1220   0.4510   1.0000
   9.250   1.3726   0.02229   0.01675  -0.1176   0.4067   1.0000
   9.500   1.3653   0.02426   0.01847  -0.1133   0.3638   1.0000
   9.750   1.3588   0.02634   0.02033  -0.1095   0.3238   1.0000
  10.250   1.3498   0.03072   0.02430  -0.1030   0.2489   1.0000
  10.500   1.3481   0.03291   0.02631  -0.1004   0.2151   1.0000
  10.750   1.3463   0.03523   0.02846  -0.0980   0.1811   1.0000
  11.000   1.3448   0.03763   0.03066  -0.0958   0.1451   1.0000
  11.250   1.3404   0.04039   0.03314  -0.0935   0.1038   1.0000
  11.500   1.3278   0.04408   0.03638  -0.0906   0.0549   1.0000
  11.750   1.3220   0.04732   0.03948  -0.0883   0.0371   1.0000
  12.000   1.3221   0.05008   0.04227  -0.0867   0.0316   1.0000
  12.250   1.3263   0.05247   0.04475  -0.0855   0.0285   1.0000
  12.500   1.3252   0.05546   0.04780  -0.0841   0.0266   1.0000
  12.750   1.3259   0.05835   0.05079  -0.0829   0.0254   1.0000
  13.000   1.3303   0.06089   0.05345  -0.0819   0.0244   1.0000
  13.250   1.3345   0.06349   0.05618  -0.0810   0.0235   1.0000
  13.500   1.3393   0.06607   0.05885  -0.0802   0.0227   1.0000
  13.750   1.3448   0.06859   0.06145  -0.0794   0.0220   1.0000
  14.000   1.3513   0.07103   0.06394  -0.0787   0.0214   1.0000
  14.250   1.3596   0.07329   0.06625  -0.0779   0.0209   1.0000
  14.500   1.3737   0.07505   0.06804  -0.0769   0.0203   1.0000
  14.750   1.3913   0.07667   0.06976  -0.0760   0.0198   1.0000
  15.000   1.3996   0.07911   0.07240  -0.0755   0.0194   1.0000
  15.250   1.4070   0.08170   0.07521  -0.0751   0.0189   1.0000
  15.500   1.4142   0.08443   0.07814  -0.0747   0.0186   1.0000
  15.750   1.4206   0.08740   0.08133  -0.0743   0.0184   1.0000
  16.000   1.4235   0.09082   0.08501  -0.0740   0.0183   1.0000
  16.250   1.4229   0.09471   0.08915  -0.0740   0.0183   1.0000
  16.500   1.4188   0.09906   0.09377  -0.0742   0.0183   1.0000
  16.750   1.4116   0.10386   0.09885  -0.0748   0.0184   1.0000
  17.000   1.4017   0.10909   0.10434  -0.0758   0.0185   1.0000
  17.250   1.3894   0.11477   0.11028  -0.0774   0.0186   1.0000
  17.500   1.3754   0.12084   0.11661  -0.0795   0.0187   1.0000
  17.750   1.3605   0.12726   0.12327  -0.0822   0.0189   1.0000
  18.000   1.3447   0.13408   0.13030  -0.0855   0.0190   1.0000
  18.250   1.3274   0.14149   0.13793  -0.0896   0.0192   1.0000
  18.500   1.3099   0.14927   0.14591  -0.0942   0.0194   1.0000
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