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N-12 (n12-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: N-12 (n12-il)
Reynolds number: 1,000,000
Max Cl/Cd: 64.36 at α=7.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-n12-il-1000000.txt
Download as CSV file: xf-n12-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: N-12                                            
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -16.500  -1.0260   0.09020   0.08797  -0.0208   1.0000   0.0108
 -16.250  -1.0806   0.07601   0.07356  -0.0294   1.0000   0.0106
 -16.000  -1.1177   0.06570   0.06304  -0.0357   1.0000   0.0105
 -15.750  -1.1416   0.05805   0.05520  -0.0403   1.0000   0.0105
 -15.500  -1.1567   0.05235   0.04933  -0.0435   1.0000   0.0106
 -15.250  -1.1690   0.04757   0.04440  -0.0456   1.0000   0.0108
 -15.000  -1.1791   0.04355   0.04021  -0.0467   1.0000   0.0109
 -14.750  -1.1788   0.04107   0.03763  -0.0470   1.0000   0.0109
 -14.500  -1.1856   0.03805   0.03444  -0.0468   1.0000   0.0110
 -14.250  -1.1986   0.03474   0.03093  -0.0456   1.0000   0.0112
 -14.000  -1.2082   0.03208   0.02812  -0.0436   1.0000   0.0115
 -13.750  -1.2063   0.03058   0.02652  -0.0417   1.0000   0.0116
 -13.500  -1.1966   0.02990   0.02581  -0.0402   1.0000   0.0119
 -13.250  -1.1867   0.02929   0.02516  -0.0384   1.0000   0.0121
 -13.000  -1.1786   0.02859   0.02442  -0.0362   1.0000   0.0123
 -12.750  -1.1715   0.02786   0.02362  -0.0336   1.0000   0.0124
 -12.500  -1.1623   0.02745   0.02317  -0.0311   1.0000   0.0127
 -12.250  -1.1538   0.02712   0.02278  -0.0282   1.0000   0.0131
 -12.000  -1.1503   0.02629   0.02186  -0.0244   1.0000   0.0133
 -11.750  -1.1389   0.02583   0.02131  -0.0219   1.0000   0.0137
 -11.500  -1.1274   0.02506   0.02044  -0.0195   1.0000   0.0140
 -11.250  -1.1138   0.02452   0.01980  -0.0173   1.0000   0.0142
 -11.000  -1.1079   0.02289   0.01802  -0.0142   1.0000   0.0148
 -10.750  -1.0929   0.02237   0.01747  -0.0122   1.0000   0.0150
 -10.500  -1.0760   0.02206   0.01713  -0.0105   1.0000   0.0153
 -10.250  -1.0584   0.02181   0.01684  -0.0088   1.0000   0.0156
 -10.000  -1.0414   0.02139   0.01636  -0.0070   1.0000   0.0160
  -9.750  -1.0237   0.02103   0.01596  -0.0054   1.0000   0.0165
  -9.500  -1.0062   0.02054   0.01539  -0.0036   1.0000   0.0170
  -9.250  -0.9878   0.02017   0.01496  -0.0020   1.0000   0.0176
  -9.000  -0.9685   0.02001   0.01473  -0.0004   1.0000   0.0180
  -8.750  -0.9494   0.01978   0.01441   0.0012   1.0000   0.0182
  -8.500  -0.9363   0.01787   0.01245   0.0034   1.0000   0.0191
  -8.250  -0.9173   0.01743   0.01200   0.0050   1.0000   0.0195
  -8.000  -0.8979   0.01711   0.01165   0.0065   1.0000   0.0200
  -7.750  -0.8784   0.01675   0.01126   0.0080   1.0000   0.0207
  -7.500  -0.8589   0.01637   0.01085   0.0095   1.0000   0.0213
  -7.250  -0.8391   0.01607   0.01050   0.0110   1.0000   0.0220
  -7.000  -0.8200   0.01567   0.01006   0.0127   1.0000   0.0225
  -6.750  -0.8002   0.01555   0.00989   0.0143   1.0000   0.0229
  -6.500  -0.7734   0.01441   0.00870   0.0141   0.9989   0.0236
  -6.250  -0.7422   0.01349   0.00780   0.0128   0.9970   0.0248
  -6.000  -0.7085   0.01303   0.00734   0.0113   0.9952   0.0256
  -5.750  -0.6754   0.01258   0.00688   0.0099   0.9935   0.0264
  -5.500  -0.6443   0.01212   0.00640   0.0091   0.9908   0.0271
  -5.250  -0.6117   0.01171   0.00598   0.0079   0.9883   0.0278
  -5.000  -0.5780   0.01138   0.00563   0.0065   0.9862   0.0286
  -4.750  -0.5434   0.01104   0.00528   0.0049   0.9845   0.0291
  -4.500  -0.5125   0.01074   0.00497   0.0042   0.9800   0.0294
  -4.250  -0.4832   0.00998   0.00414   0.0037   0.9752   0.0306
  -4.000  -0.4486   0.00953   0.00368   0.0022   0.9722   0.0318
  -3.750  -0.4229   0.00919   0.00333   0.0027   0.9623   0.0326
  -3.500  -0.3944   0.00889   0.00302   0.0026   0.9533   0.0335
  -3.250  -0.3601   0.00859   0.00270   0.0013   0.9456   0.0345
  -3.000  -0.3212   0.00832   0.00241  -0.0011   0.9366   0.0356
  -2.750  -0.2659   0.00806   0.00213  -0.0073   0.9270   0.0371
  -2.500  -0.2124   0.00782   0.00185  -0.0131   0.9117   0.0424
  -2.250  -0.1773   0.00742   0.00162  -0.0149   0.8915   0.1048
  -2.000  -0.1501   0.00722   0.00150  -0.0148   0.8708   0.1417
  -1.750  -0.1312   0.00670   0.00131  -0.0130   0.8528   0.2457
  -1.500  -0.1122   0.00627   0.00122  -0.0113   0.8352   0.3490
  -1.250  -0.0898   0.00612   0.00116  -0.0100   0.8151   0.3940
  -1.000  -0.0671   0.00601   0.00110  -0.0088   0.7947   0.4252
  -0.750  -0.0469   0.00579   0.00102  -0.0072   0.7720   0.4812
  -0.500  -0.0316   0.00540   0.00096  -0.0045   0.7476   0.5925
  -0.250  -0.0141   0.00521   0.00094  -0.0021   0.7192   0.6670
   0.000   0.0052   0.00519   0.00092  -0.0001   0.6842   0.7071
   0.250   0.0249   0.00519   0.00093   0.0019   0.6475   0.7431
   0.500   0.0444   0.00520   0.00097   0.0039   0.6135   0.7828
   0.750   0.0645   0.00526   0.00102   0.0058   0.5780   0.8202
   1.000   0.0861   0.00538   0.00107   0.0073   0.5364   0.8445
   1.250   0.1091   0.00553   0.00112   0.0084   0.4952   0.8600
   1.500   0.1316   0.00575   0.00117   0.0096   0.4388   0.8727
   1.750   0.1537   0.00604   0.00124   0.0108   0.3696   0.8860
   2.000   0.1782   0.00628   0.00133   0.0115   0.3222   0.8986
   2.250   0.2076   0.00645   0.00143   0.0111   0.2915   0.9100
   2.500   0.2433   0.00662   0.00156   0.0094   0.2692   0.9236
   2.750   0.2839   0.00682   0.00170   0.0065   0.2476   0.9342
   3.000   0.3228   0.00706   0.00186   0.0039   0.2250   0.9440
   3.250   0.3636   0.00734   0.00202   0.0009   0.1933   0.9483
   3.500   0.3922   0.00797   0.00231   0.0005   0.1123   0.9544
   3.750   0.4223   0.00825   0.00255  -0.0001   0.0968   0.9598
   4.000   0.4524   0.00875   0.00281  -0.0007   0.0482   0.9636
   4.250   0.4793   0.00907   0.00308  -0.0005   0.0410   0.9698
   4.500   0.5111   0.00934   0.00336  -0.0013   0.0383   0.9730
   4.750   0.5446   0.00960   0.00364  -0.0026   0.0365   0.9752
   5.000   0.5764   0.00989   0.00394  -0.0036   0.0348   0.9780
   5.250   0.6032   0.01025   0.00431  -0.0034   0.0332   0.9831
   5.500   0.6356   0.01077   0.00488  -0.0045   0.0310   0.9849
   5.750   0.6698   0.01104   0.00517  -0.0060   0.0304   0.9866
   6.000   0.7029   0.01135   0.00551  -0.0073   0.0295   0.9887
   6.250   0.7350   0.01167   0.00585  -0.0084   0.0283   0.9911
   6.500   0.7664   0.01204   0.00623  -0.0094   0.0271   0.9937
   6.750   0.7987   0.01256   0.00677  -0.0106   0.0257   0.9954
   7.000   0.8294   0.01336   0.00764  -0.0117   0.0244   0.9975
   7.250   0.8630   0.01355   0.00785  -0.0131   0.0237   0.9990
   7.500   0.8927   0.01387   0.00821  -0.0138   0.0228   1.0000
   7.750   0.9100   0.01414   0.00850  -0.0118   0.0220   1.0000
   8.000   0.9279   0.01444   0.00881  -0.0099   0.0213   1.0000
   8.250   0.9458   0.01477   0.00915  -0.0081   0.0206   1.0000
   8.500   0.9545   0.01594   0.01038  -0.0047   0.0194   1.0000
   8.750   0.9757   0.01605   0.01052  -0.0035   0.0191   1.0000
   9.000   0.9959   0.01626   0.01078  -0.0021   0.0185   1.0000
   9.250   1.0142   0.01664   0.01120  -0.0003   0.0179   1.0000
   9.500   1.0331   0.01695   0.01155   0.0013   0.0172   1.0000
   9.750   1.0521   0.01725   0.01187   0.0028   0.0167   1.0000
  10.000   1.0702   0.01761   0.01225   0.0045   0.0162   1.0000
  10.250   1.0801   0.01864   0.01333   0.0074   0.0154   1.0000
  10.500   1.0957   0.01920   0.01396   0.0095   0.0150   1.0000
  10.750   1.1135   0.01955   0.01437   0.0112   0.0147   1.0000
  11.000   1.1301   0.01997   0.01485   0.0131   0.0142   1.0000
  11.250   1.1476   0.02029   0.01521   0.0147   0.0136   1.0000
  11.500   1.1628   0.02077   0.01574   0.0168   0.0133   1.0000
  11.750   1.1770   0.02130   0.01631   0.0189   0.0130   1.0000
  12.000   1.1903   0.02186   0.01691   0.0211   0.0127   1.0000
  12.250   1.1952   0.02262   0.01772   0.0248   0.0123   1.0000
  12.500   1.1865   0.02417   0.01941   0.0302   0.0119   1.0000
  12.750   1.1939   0.02493   0.02026   0.0331   0.0118   1.0000
  13.000   1.2021   0.02572   0.02114   0.0356   0.0116   1.0000
  13.250   1.2083   0.02672   0.02224   0.0380   0.0114   1.0000
  13.500   1.2131   0.02787   0.02351   0.0403   0.0112   1.0000
  13.750   1.2165   0.02924   0.02499   0.0424   0.0110   1.0000
  14.000   1.2220   0.03051   0.02636   0.0439   0.0107   1.0000
  14.250   1.2273   0.03191   0.02784   0.0452   0.0105   1.0000
  14.500   1.2307   0.03358   0.02960   0.0461   0.0103   1.0000
  14.750   1.2375   0.03506   0.03113   0.0466   0.0101   1.0000
  15.000   1.2387   0.03722   0.03339   0.0469   0.0099   1.0000
  15.250   1.2342   0.04022   0.03650   0.0467   0.0098   1.0000
  15.500   1.2315   0.04330   0.03968   0.0459   0.0097   1.0000
  15.750   1.2244   0.04720   0.04370   0.0445   0.0095   1.0000
  16.000   1.2066   0.05289   0.04954   0.0418   0.0094   1.0000
  16.250   1.1901   0.05879   0.05559   0.0386   0.0093   1.0000
  16.500   1.1758   0.06465   0.06159   0.0354   0.0093   1.0000
  16.750   1.1498   0.07269   0.06980   0.0308   0.0093   1.0000
  17.000   1.1341   0.07926   0.07649   0.0272   0.0093   1.0000
  17.250   1.1048   0.08834   0.08572   0.0222   0.0093   1.0000
  17.500   1.0872   0.09545   0.09294   0.0183   0.0094   1.0000
  17.750   1.0562   0.10527   0.10288   0.0129   0.0093   1.0000
  18.000   1.0219   0.11620   0.11398   0.0071   0.0095   1.0000
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