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NACA 0015 (naca0015-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: NACA 0015 (naca0015-il)
Reynolds number: 1,000,000
Max Cl/Cd: 75.1 at α=10.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-naca0015-il-1000000-n5.txt
Download as CSV file: xf-naca0015-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NACA 0015                                       
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -19.750  -1.3543   0.09065   0.08669  -0.0171   1.0000   0.0219
 -19.500  -1.3750   0.08409   0.08002  -0.0201   1.0000   0.0221
 -19.250  -1.3937   0.07786   0.07368  -0.0228   1.0000   0.0222
 -19.000  -1.4104   0.07207   0.06778  -0.0252   1.0000   0.0224
 -18.750  -1.4243   0.06680   0.06240  -0.0274   1.0000   0.0226
 -18.500  -1.4358   0.06191   0.05741  -0.0293   1.0000   0.0228
 -18.250  -1.4446   0.05753   0.05294  -0.0309   1.0000   0.0230
 -18.000  -1.4512   0.05351   0.04882  -0.0323   1.0000   0.0232
 -17.750  -1.4556   0.04987   0.04508  -0.0334   1.0000   0.0234
 -17.500  -1.4581   0.04656   0.04169  -0.0343   1.0000   0.0236
 -17.250  -1.4587   0.04357   0.03861  -0.0350   1.0000   0.0238
 -17.000  -1.4571   0.04090   0.03586  -0.0355   1.0000   0.0241
 -16.750  -1.4540   0.03847   0.03335  -0.0358   1.0000   0.0244
 -16.500  -1.4492   0.03632   0.03112  -0.0359   1.0000   0.0247
 -16.250  -1.4433   0.03433   0.02905  -0.0358   1.0000   0.0249
 -16.000  -1.4363   0.03253   0.02718  -0.0356   1.0000   0.0252
 -15.750  -1.4281   0.03091   0.02549  -0.0352   1.0000   0.0254
 -15.500  -1.4197   0.02938   0.02389  -0.0347   1.0000   0.0256
 -15.250  -1.4134   0.02775   0.02220  -0.0338   1.0000   0.0260
 -15.000  -1.4052   0.02637   0.02077  -0.0329   1.0000   0.0264
 -14.750  -1.3952   0.02518   0.01953  -0.0318   1.0000   0.0268
 -14.500  -1.3841   0.02413   0.01843  -0.0307   1.0000   0.0272
 -14.250  -1.3720   0.02319   0.01745  -0.0295   1.0000   0.0275
 -14.000  -1.3591   0.02235   0.01656  -0.0282   1.0000   0.0280
 -13.750  -1.3454   0.02160   0.01576  -0.0269   1.0000   0.0284
 -13.500  -1.3311   0.02091   0.01502  -0.0255   1.0000   0.0287
 -13.250  -1.3164   0.02027   0.01434  -0.0240   1.0000   0.0291
 -13.000  -1.3009   0.01970   0.01372  -0.0225   1.0000   0.0294
 -12.750  -1.2865   0.01911   0.01309  -0.0208   1.0000   0.0298
 -12.500  -1.2728   0.01852   0.01248  -0.0188   1.0000   0.0304
 -12.250  -1.2588   0.01802   0.01194  -0.0168   1.0000   0.0309
 -12.000  -1.2438   0.01756   0.01146  -0.0148   1.0000   0.0314
 -11.750  -1.2266   0.01713   0.01101  -0.0132   1.0000   0.0320
 -11.500  -1.2089   0.01673   0.01059  -0.0116   1.0000   0.0326
 -11.250  -1.1912   0.01636   0.01020  -0.0100   1.0000   0.0333
 -11.000  -1.1738   0.01603   0.00983  -0.0082   1.0000   0.0338
 -10.750  -1.1575   0.01567   0.00946  -0.0062   1.0000   0.0345
 -10.500  -1.1416   0.01532   0.00909  -0.0040   1.0000   0.0354
 -10.250  -1.1258   0.01499   0.00876  -0.0019   1.0000   0.0363
 -10.000  -1.0962   0.01460   0.00836  -0.0026   0.9983   0.0375
  -9.750  -1.0659   0.01424   0.00799  -0.0034   0.9963   0.0387
  -9.500  -1.0354   0.01385   0.00761  -0.0043   0.9945   0.0405
  -9.250  -1.0040   0.01348   0.00724  -0.0054   0.9930   0.0429
  -9.000  -0.9750   0.01314   0.00691  -0.0059   0.9900   0.0454
  -8.750  -0.9454   0.01277   0.00657  -0.0065   0.9868   0.0486
  -8.500  -0.9149   0.01245   0.00625  -0.0073   0.9836   0.0519
  -8.250  -0.8847   0.01211   0.00594  -0.0080   0.9802   0.0563
  -8.000  -0.8575   0.01180   0.00566  -0.0080   0.9743   0.0607
  -7.750  -0.8278   0.01152   0.00539  -0.0085   0.9694   0.0655
  -7.500  -0.8013   0.01121   0.00512  -0.0084   0.9625   0.0712
  -7.250  -0.7739   0.01094   0.00487  -0.0083   0.9553   0.0769
  -7.000  -0.7478   0.01069   0.00464  -0.0080   0.9468   0.0830
  -6.750  -0.7217   0.01043   0.00439  -0.0076   0.9378   0.0894
  -6.500  -0.6958   0.01022   0.00419  -0.0072   0.9271   0.0952
  -6.250  -0.6703   0.00998   0.00397  -0.0067   0.9162   0.1028
  -6.000  -0.6445   0.00978   0.00377  -0.0062   0.9038   0.1102
  -5.750  -0.6185   0.00959   0.00358  -0.0058   0.8904   0.1185
  -5.500  -0.5927   0.00938   0.00339  -0.0053   0.8765   0.1291
  -5.250  -0.5668   0.00918   0.00320  -0.0049   0.8619   0.1407
  -5.000  -0.5406   0.00902   0.00303  -0.0045   0.8466   0.1517
  -4.750  -0.5144   0.00886   0.00287  -0.0041   0.8304   0.1643
  -4.500  -0.4886   0.00865   0.00270  -0.0037   0.8134   0.1826
  -4.250  -0.4625   0.00847   0.00255  -0.0033   0.7959   0.2016
  -4.000  -0.4362   0.00832   0.00241  -0.0029   0.7778   0.2190
  -3.750  -0.4095   0.00820   0.00229  -0.0026   0.7592   0.2338
  -3.500  -0.3827   0.00809   0.00218  -0.0024   0.7405   0.2491
  -3.250  -0.3557   0.00800   0.00208  -0.0021   0.7220   0.2635
  -3.000  -0.3286   0.00791   0.00199  -0.0019   0.7035   0.2790
  -2.750  -0.3014   0.00784   0.00191  -0.0017   0.6851   0.2941
  -2.500  -0.2742   0.00776   0.00183  -0.0015   0.6668   0.3097
  -2.250  -0.2470   0.00769   0.00176  -0.0013   0.6485   0.3273
  -1.750  -0.1925   0.00756   0.00164  -0.0010   0.6116   0.3636
  -1.500  -0.1652   0.00750   0.00160  -0.0008   0.5935   0.3823
  -1.250  -0.1379   0.00746   0.00156  -0.0006   0.5748   0.4008
  -1.000  -0.1103   0.00743   0.00153  -0.0005   0.5565   0.4175
  -0.750  -0.0828   0.00741   0.00150  -0.0004   0.5385   0.4344
  -0.500  -0.0551   0.00740   0.00149  -0.0003   0.5210   0.4509
  -0.250  -0.0276   0.00739   0.00148  -0.0001   0.5036   0.4681
   0.000   0.0000   0.00739   0.00148   0.0000   0.4857   0.4859
   0.250   0.0276   0.00739   0.00148   0.0001   0.4681   0.5035
   0.500   0.0551   0.00740   0.00149   0.0003   0.4508   0.5211
   0.750   0.0828   0.00741   0.00150   0.0004   0.4344   0.5389
   1.000   0.1104   0.00743   0.00153   0.0005   0.4177   0.5565
   1.250   0.1379   0.00746   0.00156   0.0006   0.4007   0.5747
   1.500   0.1652   0.00750   0.00160   0.0008   0.3823   0.5935
   1.750   0.1925   0.00756   0.00164   0.0010   0.3637   0.6118
   2.250   0.2470   0.00769   0.00176   0.0013   0.3271   0.6483
   2.500   0.2742   0.00777   0.00183   0.0015   0.3096   0.6667
   2.750   0.3014   0.00783   0.00191   0.0017   0.2941   0.6853
   3.000   0.3287   0.00791   0.00199   0.0019   0.2790   0.7035
   3.250   0.3557   0.00800   0.00208   0.0021   0.2636   0.7221
   3.500   0.3827   0.00809   0.00218   0.0024   0.2489   0.7406
   3.750   0.4095   0.00820   0.00229   0.0026   0.2338   0.7592
   4.000   0.4362   0.00832   0.00241   0.0029   0.2189   0.7778
   4.250   0.4626   0.00847   0.00255   0.0033   0.2024   0.7959
   4.500   0.4886   0.00865   0.00270   0.0037   0.1827   0.8134
   4.750   0.5144   0.00886   0.00287   0.0041   0.1641   0.8304
   5.000   0.5407   0.00902   0.00303   0.0045   0.1517   0.8465
   5.250   0.5669   0.00918   0.00320   0.0049   0.1406   0.8619
   5.500   0.5928   0.00938   0.00339   0.0053   0.1291   0.8765
   5.750   0.6186   0.00959   0.00358   0.0058   0.1185   0.8904
   6.000   0.6446   0.00979   0.00377   0.0062   0.1101   0.9038
   6.250   0.6703   0.00999   0.00397   0.0067   0.1028   0.9161
   6.500   0.6959   0.01022   0.00419   0.0072   0.0952   0.9271
   6.750   0.7218   0.01043   0.00439   0.0076   0.0894   0.9378
   7.000   0.7479   0.01069   0.00464   0.0080   0.0829   0.9468
   7.250   0.7739   0.01094   0.00487   0.0083   0.0768   0.9553
   7.500   0.8014   0.01121   0.00512   0.0083   0.0711   0.9625
   7.750   0.8279   0.01152   0.00539   0.0085   0.0654   0.9694
   8.000   0.8576   0.01180   0.00566   0.0080   0.0606   0.9743
   8.250   0.8848   0.01211   0.00594   0.0080   0.0562   0.9803
   8.500   0.9150   0.01245   0.00625   0.0073   0.0519   0.9837
   8.750   0.9455   0.01277   0.00657   0.0065   0.0485   0.9868
   9.000   0.9751   0.01314   0.00691   0.0059   0.0454   0.9901
   9.250   1.0042   0.01347   0.00724   0.0054   0.0430   0.9930
   9.500   1.0356   0.01385   0.00761   0.0043   0.0405   0.9945
   9.750   1.0661   0.01424   0.00799   0.0034   0.0387   0.9963
  10.000   1.0963   0.01460   0.00836   0.0026   0.0375   0.9983
  10.250   1.1258   0.01499   0.00876   0.0019   0.0363   1.0000
  10.500   1.1416   0.01531   0.00909   0.0041   0.0354   1.0000
  10.750   1.1575   0.01567   0.00946   0.0062   0.0345   1.0000
  11.000   1.1738   0.01603   0.00983   0.0082   0.0338   1.0000
  11.250   1.1913   0.01636   0.01019   0.0099   0.0333   1.0000
  11.500   1.2091   0.01673   0.01058   0.0116   0.0326   1.0000
  11.750   1.2269   0.01713   0.01101   0.0131   0.0320   1.0000
  12.000   1.2442   0.01756   0.01146   0.0147   0.0314   1.0000
  12.250   1.2593   0.01802   0.01194   0.0167   0.0309   1.0000
  12.500   1.2735   0.01852   0.01248   0.0187   0.0304   1.0000
  12.750   1.2871   0.01911   0.01309   0.0207   0.0298   1.0000
  13.000   1.3017   0.01970   0.01372   0.0224   0.0294   1.0000
  13.250   1.3172   0.02027   0.01433   0.0239   0.0291   1.0000
  13.500   1.3320   0.02090   0.01501   0.0253   0.0287   1.0000
  13.750   1.3463   0.02159   0.01575   0.0267   0.0284   1.0000
  14.000   1.3601   0.02234   0.01655   0.0280   0.0279   1.0000
  14.250   1.3732   0.02318   0.01743   0.0293   0.0275   1.0000
  14.500   1.3853   0.02412   0.01842   0.0305   0.0271   1.0000
  14.750   1.3965   0.02517   0.01951   0.0316   0.0268   1.0000
  15.000   1.4066   0.02635   0.02075   0.0327   0.0264   1.0000
  15.250   1.4150   0.02773   0.02217   0.0336   0.0260   1.0000
  15.500   1.4212   0.02937   0.02387   0.0344   0.0256   1.0000
  15.750   1.4301   0.03086   0.02544   0.0349   0.0254   1.0000
  16.000   1.4382   0.03248   0.02713   0.0353   0.0252   1.0000
  16.250   1.4453   0.03428   0.02900   0.0355   0.0249   1.0000
  16.500   1.4516   0.03623   0.03103   0.0356   0.0247   1.0000
  16.750   1.4562   0.03842   0.03330   0.0355   0.0244   1.0000
  17.000   1.4596   0.04081   0.03577   0.0352   0.0241   1.0000
  17.250   1.4613   0.04348   0.03852   0.0347   0.0238   1.0000
  17.500   1.4609   0.04646   0.04158   0.0340   0.0236   1.0000
  17.750   1.4585   0.04975   0.04496   0.0331   0.0234   1.0000
  18.000   1.4542   0.05339   0.04870   0.0319   0.0231   1.0000
  18.250   1.4479   0.05738   0.05278   0.0306   0.0229   1.0000
  18.500   1.4391   0.06177   0.05726   0.0289   0.0228   1.0000
  18.750   1.4277   0.06664   0.06224   0.0270   0.0226   1.0000
  19.000   1.4138   0.07193   0.06764   0.0249   0.0224   1.0000
  19.250   1.3972   0.07771   0.07353   0.0224   0.0222   1.0000
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