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NASA/LANGLEY NLF(1)-0215F AIRFOIL (nlf0215f-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: NASA/LANGLEY NLF(1)-0215F AIRFOIL (nlf0215f-il)
Reynolds number: 1,000,000
Max Cl/Cd: 131.78 at α=4.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-nlf0215f-il-1000000-n5.txt
Download as CSV file: xf-nlf0215f-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NASA/LANGLEY NLF(1)-0215F 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 =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -11.750  -0.2473   0.10327   0.10142  -0.0780   0.9452   0.0077
 -11.500  -0.2301   0.09539   0.09350  -0.0873   0.9359   0.0077
 -11.250  -0.4589   0.03102   0.02798  -0.1377   0.9174   0.0077
 -11.000  -0.4246   0.02655   0.02286  -0.1479   0.8660   0.0079
 -10.750  -0.4287   0.02526   0.02124  -0.1449   0.8233   0.0078
 -10.500  -0.4274   0.02456   0.02032  -0.1421   0.7962   0.0079
 -10.250  -0.4256   0.02293   0.01842  -0.1401   0.7763   0.0079
 -10.000  -0.4128   0.02211   0.01742  -0.1388   0.7611   0.0080
  -9.750  -0.4006   0.02092   0.01601  -0.1375   0.7481   0.0080
  -9.500  -0.3881   0.01945   0.01430  -0.1363   0.7371   0.0081
  -9.250  -0.3710   0.01847   0.01315  -0.1354   0.7273   0.0082
  -9.000  -0.3525   0.01750   0.01203  -0.1346   0.7182   0.0083
  -8.750  -0.3320   0.01678   0.01119  -0.1340   0.7103   0.0084
  -8.500  -0.3099   0.01621   0.01052  -0.1336   0.7022   0.0085
  -8.250  -0.2874   0.01566   0.00987  -0.1331   0.6950   0.0086
  -8.000  -0.2642   0.01512   0.00924  -0.1328   0.6879   0.0087
  -7.750  -0.2405   0.01468   0.00872  -0.1325   0.6813   0.0088
  -7.500  -0.2161   0.01419   0.00815  -0.1323   0.6759   0.0089
  -7.250  -0.1914   0.01377   0.00766  -0.1321   0.6704   0.0090
  -6.750  -0.1409   0.01299   0.00677  -0.1319   0.6610   0.0094
  -6.500  -0.1150   0.01264   0.00636  -0.1318   0.6564   0.0096
  -6.250  -0.0891   0.01232   0.00598  -0.1318   0.6517   0.0099
  -6.000  -0.0629   0.01198   0.00558  -0.1318   0.6477   0.0101
  -5.750  -0.0361   0.01163   0.00519  -0.1319   0.6437   0.0103
  -5.500  -0.0090   0.01134   0.00486  -0.1321   0.6395   0.0105
  -5.250   0.0182   0.01109   0.00456  -0.1322   0.6358   0.0107
  -5.000   0.0456   0.01088   0.00430  -0.1324   0.6325   0.0108
  -4.750   0.0737   0.01047   0.00387  -0.1329   0.6296   0.0113
  -4.500   0.1020   0.01022   0.00359  -0.1333   0.6265   0.0117
  -4.250   0.1303   0.01003   0.00338  -0.1336   0.6231   0.0121
  -4.000   0.1587   0.00986   0.00319  -0.1339   0.6198   0.0125
  -3.750   0.1871   0.00972   0.00301  -0.1343   0.6166   0.0130
  -3.500   0.2161   0.00956   0.00285  -0.1347   0.6143   0.0135
  -3.250   0.2451   0.00944   0.00271  -0.1351   0.6117   0.0141
  -3.000   0.2743   0.00928   0.00254  -0.1356   0.6089   0.0154
  -2.750   0.3032   0.00918   0.00242  -0.1360   0.6060   0.0167
  -2.500   0.3321   0.00909   0.00232  -0.1364   0.6032   0.0186
  -2.250   0.3612   0.00897   0.00222  -0.1369   0.6006   0.0277
  -2.000   0.3914   0.00875   0.00213  -0.1377   0.5986   0.0626
  -1.750   0.4223   0.00844   0.00204  -0.1388   0.5962   0.1320
  -1.500   0.4554   0.00789   0.00191  -0.1407   0.5936   0.2800
  -1.250   0.4920   0.00704   0.00171  -0.1438   0.5911   0.5074
  -1.000   0.5234   0.00683   0.00189  -0.1448   0.5886   0.6547
  -0.750   0.5516   0.00702   0.00205  -0.1448   0.5860   0.6760
  -0.500   0.5794   0.00724   0.00228  -0.1447   0.5839   0.6887
  -0.250   0.6083   0.00736   0.00238  -0.1449   0.5819   0.6945
   0.000   0.6373   0.00740   0.00239  -0.1452   0.5795   0.6956
   0.250   0.6660   0.00742   0.00239  -0.1455   0.5770   0.6964
   0.500   0.6946   0.00745   0.00240  -0.1457   0.5746   0.6971
   0.750   0.7230   0.00750   0.00242  -0.1459   0.5721   0.6977
   1.000   0.7511   0.00756   0.00245  -0.1461   0.5694   0.6982
   1.250   0.7799   0.00758   0.00248  -0.1464   0.5672   0.6987
   1.500   0.8085   0.00761   0.00252  -0.1466   0.5642   0.6993
   1.750   0.8368   0.00766   0.00256  -0.1468   0.5602   0.6999
   2.000   0.8644   0.00772   0.00260  -0.1469   0.5556   0.7004
   2.250   0.8924   0.00778   0.00264  -0.1470   0.5506   0.7009
   2.500   0.9204   0.00782   0.00268  -0.1471   0.5447   0.7014
   2.750   0.9477   0.00790   0.00274  -0.1472   0.5392   0.7018
   3.000   0.9755   0.00795   0.00279  -0.1473   0.5341   0.7023
   3.250   1.0029   0.00802   0.00285  -0.1473   0.5267   0.7028
   3.500   1.0298   0.00811   0.00293  -0.1473   0.5190   0.7033
   3.750   1.0568   0.00820   0.00300  -0.1472   0.5105   0.7040
   4.000   1.0835   0.00831   0.00309  -0.1471   0.5017   0.7047
   4.250   1.1094   0.00844   0.00320  -0.1469   0.4900   0.7052
   4.500   1.1346   0.00861   0.00332  -0.1465   0.4743   0.7057
   4.750   1.1590   0.00883   0.00346  -0.1461   0.4554   0.7062
   5.000   1.1813   0.00916   0.00368  -0.1452   0.4289   0.7067
   5.250   1.2019   0.00959   0.00395  -0.1440   0.3968   0.7073
   5.500   1.2217   0.01006   0.00427  -0.1427   0.3640   0.7078
   5.750   1.2405   0.01058   0.00462  -0.1412   0.3311   0.7083
   6.000   1.2579   0.01114   0.00502  -0.1395   0.2974   0.7087
   6.250   1.2754   0.01166   0.00540  -0.1379   0.2690   0.7092
   6.500   1.2918   0.01216   0.00578  -0.1359   0.2437   0.7097
   6.750   1.3070   0.01262   0.00613  -0.1338   0.2217   0.7101
   7.000   1.3213   0.01311   0.00653  -0.1315   0.2020   0.7105
   7.250   1.3365   0.01359   0.00693  -0.1294   0.1846   0.7109
   7.500   1.3510   0.01409   0.00737  -0.1272   0.1670   0.7115
   7.750   1.3643   0.01465   0.00785  -0.1248   0.1498   0.7123
   8.000   1.3789   0.01515   0.00832  -0.1228   0.1371   0.7130
   8.250   1.3931   0.01567   0.00881  -0.1207   0.1267   0.7137
   8.500   1.4069   0.01623   0.00933  -0.1186   0.1166   0.7142
   8.750   1.4205   0.01680   0.00988  -0.1165   0.1072   0.7148
   9.000   1.4336   0.01740   0.01048  -0.1144   0.0989   0.7154
   9.250   1.4456   0.01808   0.01114  -0.1122   0.0912   0.7160
   9.500   1.4590   0.01871   0.01178  -0.1103   0.0856   0.7165
   9.750   1.4698   0.01949   0.01255  -0.1081   0.0790   0.7171
  10.000   1.4818   0.02025   0.01332  -0.1062   0.0736   0.7177
  10.250   1.4902   0.02124   0.01430  -0.1039   0.0662   0.7183
  10.500   1.5009   0.02215   0.01522  -0.1020   0.0613   0.7190
  10.750   1.5096   0.02323   0.01630  -0.1000   0.0564   0.7196
  11.000   1.5204   0.02423   0.01734  -0.0984   0.0527   0.7202
  11.250   1.5289   0.02544   0.01855  -0.0966   0.0487   0.7209
  11.500   1.5380   0.02665   0.01979  -0.0951   0.0452   0.7215
  11.750   1.5470   0.02793   0.02110  -0.0936   0.0419   0.7221
  12.000   1.5541   0.02941   0.02258  -0.0921   0.0385   0.7227
  12.250   1.5636   0.03074   0.02396  -0.0909   0.0362   0.7233
  12.500   1.5718   0.03223   0.02548  -0.0896   0.0339   0.7239
  12.750   1.5786   0.03389   0.02716  -0.0884   0.0314   0.7245
  13.000   1.5874   0.03541   0.02873  -0.0874   0.0298   0.7250
  13.250   1.5946   0.03711   0.03047  -0.0864   0.0277   0.7255
  13.500   1.6008   0.03896   0.03235  -0.0854   0.0258   0.7260
  13.750   1.6086   0.04069   0.03413  -0.0846   0.0245   0.7265
  14.000   1.6159   0.04251   0.03600  -0.0839   0.0231   0.7271
  14.250   1.6214   0.04454   0.03808  -0.0831   0.0214   0.7279
  14.500   1.6273   0.04658   0.04017  -0.0824   0.0202   0.7286
  14.750   1.6341   0.04858   0.04223  -0.0819   0.0189   0.7295
  15.000   1.6389   0.05083   0.04453  -0.0814   0.0174   0.7302
  15.250   1.6433   0.05316   0.04691  -0.0809   0.0161   0.7310
  15.500   1.6485   0.05544   0.04925  -0.0805   0.0147   0.7318
  15.750   1.6512   0.05807   0.05194  -0.0802   0.0132   0.7325
  16.000   1.6550   0.06062   0.05454  -0.0800   0.0119   0.7332
  16.250   1.6576   0.06337   0.05735  -0.0798   0.0106   0.7339
  16.500   1.6594   0.06625   0.06029  -0.0798   0.0095   0.7345
  16.750   1.6612   0.06920   0.06330  -0.0798   0.0084   0.7352
  17.000   1.6620   0.07235   0.06652  -0.0800   0.0076   0.7359
  17.250   1.6633   0.07548   0.06972  -0.0802   0.0070   0.7366
  17.500   1.6642   0.07872   0.07304  -0.0805   0.0064   0.7372
  17.750   1.6632   0.08226   0.07666  -0.0810   0.0060   0.7379
  18.000   1.6635   0.08569   0.08017  -0.0815   0.0057   0.7385
  18.250   1.6639   0.08915   0.08372  -0.0822   0.0054   0.7392
  18.500   1.6630   0.09288   0.08754  -0.0830   0.0052   0.7398
  18.750   1.6616   0.09671   0.09146  -0.0839   0.0050   0.7404
  19.000   1.6595   0.10067   0.09551  -0.0850   0.0048   0.7409
  19.250   1.6563   0.10488   0.09981  -0.0862   0.0047   0.7415
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