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NACA 0015 (naca0015-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: NACA 0015 (naca0015-il)
Reynolds number: 1,000,000
Max Cl/Cd: 77.88 at α=9°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-naca0015-il-1000000.txt
Download as CSV file: xf-naca0015-il-1000000.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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -19.750  -1.2970   0.09858   0.09490  -0.0142   1.0000   0.0253
 -19.500  -1.3072   0.09342   0.08964  -0.0166   1.0000   0.0255
 -19.250  -1.3172   0.08835   0.08447  -0.0189   1.0000   0.0257
 -19.000  -1.3264   0.08347   0.07949  -0.0210   1.0000   0.0259
 -18.750  -1.3346   0.07874   0.07466  -0.0231   1.0000   0.0260
 -18.500  -1.3416   0.07426   0.07008  -0.0250   1.0000   0.0261
 -18.250  -1.3528   0.06938   0.06509  -0.0269   1.0000   0.0263
 -18.000  -1.3680   0.06409   0.05971  -0.0288   1.0000   0.0266
 -17.750  -1.3805   0.05922   0.05476  -0.0306   1.0000   0.0268
 -17.500  -1.3899   0.05483   0.05028  -0.0321   1.0000   0.0271
 -17.250  -1.3961   0.05093   0.04629  -0.0333   1.0000   0.0273
 -17.000  -1.3996   0.04745   0.04273  -0.0343   1.0000   0.0276
 -16.750  -1.4005   0.04438   0.03958  -0.0351   1.0000   0.0278
 -16.500  -1.3991   0.04163   0.03675  -0.0356   1.0000   0.0281
 -16.250  -1.3963   0.03912   0.03418  -0.0360   1.0000   0.0285
 -16.000  -1.3920   0.03686   0.03184  -0.0362   1.0000   0.0288
 -15.750  -1.3864   0.03481   0.02971  -0.0362   1.0000   0.0292
 -15.500  -1.3796   0.03295   0.02777  -0.0360   1.0000   0.0295
 -15.250  -1.3718   0.03127   0.02602  -0.0356   1.0000   0.0298
 -15.000  -1.3622   0.02981   0.02448  -0.0351   1.0000   0.0300
 -14.750  -1.3558   0.02817   0.02276  -0.0344   1.0000   0.0304
 -14.500  -1.3544   0.02625   0.02078  -0.0330   1.0000   0.0309
 -14.250  -1.3476   0.02486   0.01934  -0.0317   1.0000   0.0314
 -14.000  -1.3376   0.02375   0.01819  -0.0304   1.0000   0.0319
 -13.750  -1.3257   0.02283   0.01722  -0.0291   1.0000   0.0324
 -13.500  -1.3132   0.02199   0.01633  -0.0277   1.0000   0.0329
 -13.250  -1.3000   0.02122   0.01551  -0.0262   1.0000   0.0334
 -13.000  -1.2858   0.02055   0.01479  -0.0247   1.0000   0.0339
 -12.750  -1.2704   0.01997   0.01416  -0.0232   1.0000   0.0344
 -12.500  -1.2573   0.01931   0.01345  -0.0213   1.0000   0.0349
 -12.250  -1.2479   0.01854   0.01265  -0.0187   1.0000   0.0357
 -12.000  -1.2357   0.01797   0.01206  -0.0163   1.0000   0.0364
 -11.750  -1.2206   0.01748   0.01154  -0.0143   1.0000   0.0372
 -11.500  -1.2037   0.01704   0.01107  -0.0126   1.0000   0.0379
 -11.250  -1.1862   0.01665   0.01065  -0.0110   1.0000   0.0387
 -11.000  -1.1686   0.01632   0.01028  -0.0092   1.0000   0.0394
 -10.750  -1.1553   0.01580   0.00974  -0.0067   1.0000   0.0407
 -10.500  -1.1406   0.01538   0.00932  -0.0044   1.0000   0.0419
 -10.250  -1.1251   0.01503   0.00896  -0.0022   1.0000   0.0431
 -10.000  -1.1092   0.01474   0.00865   0.0000   1.0000   0.0444
  -9.750  -1.0944   0.01439   0.00828   0.0024   1.0000   0.0459
  -9.500  -1.0800   0.01402   0.00793   0.0048   1.0000   0.0481
  -9.250  -1.0641   0.01374   0.00764   0.0070   1.0000   0.0503
  -9.000  -1.0379   0.01333   0.00726   0.0070   0.9991   0.0541
  -8.750  -1.0050   0.01295   0.00689   0.0057   0.9975   0.0588
  -8.500  -0.9719   0.01255   0.00654   0.0043   0.9959   0.0649
  -8.250  -0.9383   0.01216   0.00619   0.0028   0.9944   0.0722
  -8.000  -0.9039   0.01179   0.00588   0.0012   0.9931   0.0799
  -7.750  -0.8723   0.01144   0.00558   0.0002   0.9906   0.0878
  -7.500  -0.8394   0.01112   0.00529  -0.0011   0.9880   0.0960
  -7.250  -0.8054   0.01080   0.00503  -0.0025   0.9858   0.1046
  -7.000  -0.7707   0.01046   0.00475  -0.0042   0.9841   0.1153
  -6.750  -0.7355   0.01012   0.00448  -0.0059   0.9825   0.1270
  -6.500  -0.7028   0.00981   0.00424  -0.0071   0.9796   0.1395
  -6.250  -0.6737   0.00951   0.00401  -0.0074   0.9742   0.1529
  -6.000  -0.6430   0.00921   0.00378  -0.0080   0.9697   0.1677
  -5.750  -0.6153   0.00894   0.00358  -0.0080   0.9633   0.1821
  -5.500  -0.5885   0.00869   0.00338  -0.0077   0.9559   0.1968
  -5.250  -0.5623   0.00845   0.00320  -0.0073   0.9477   0.2124
  -5.000  -0.5364   0.00822   0.00303  -0.0067   0.9387   0.2292
  -4.750  -0.5108   0.00800   0.00287  -0.0062   0.9285   0.2475
  -4.500  -0.4850   0.00778   0.00271  -0.0057   0.9183   0.2690
  -4.250  -0.4591   0.00758   0.00257  -0.0051   0.9062   0.2895
  -4.000  -0.4328   0.00740   0.00244  -0.0047   0.8938   0.3080
  -3.750  -0.4063   0.00725   0.00231  -0.0043   0.8806   0.3258
  -3.500  -0.3798   0.00711   0.00219  -0.0039   0.8664   0.3441
  -3.250  -0.3530   0.00698   0.00209  -0.0035   0.8510   0.3619
  -3.000  -0.3261   0.00687   0.00200  -0.0032   0.8353   0.3805
  -2.750  -0.2990   0.00677   0.00191  -0.0029   0.8188   0.3986
  -2.500  -0.2720   0.00668   0.00183  -0.0026   0.8018   0.4171
  -2.250  -0.2450   0.00660   0.00176  -0.0023   0.7844   0.4366
  -2.000  -0.2179   0.00653   0.00169  -0.0020   0.7660   0.4562
  -1.750  -0.1908   0.00647   0.00164  -0.0017   0.7474   0.4763
  -1.500  -0.1636   0.00642   0.00159  -0.0015   0.7280   0.4961
  -1.250  -0.1364   0.00638   0.00155  -0.0012   0.7086   0.5153
  -1.000  -0.1091   0.00636   0.00152  -0.0009   0.6892   0.5343
  -0.750  -0.0819   0.00634   0.00150  -0.0007   0.6693   0.5530
  -0.500  -0.0546   0.00633   0.00148  -0.0005   0.6497   0.5721
  -0.250  -0.0273   0.00632   0.00147  -0.0002   0.6302   0.5913
   0.250   0.0273   0.00632   0.00147   0.0002   0.5912   0.6302
   0.500   0.0546   0.00633   0.00148   0.0005   0.5720   0.6498
   0.750   0.0819   0.00634   0.00150   0.0007   0.5531   0.6691
   1.000   0.1091   0.00635   0.00152   0.0009   0.5345   0.6891
   1.250   0.1364   0.00638   0.00155   0.0012   0.5153   0.7086
   1.500   0.1636   0.00642   0.00159   0.0015   0.4962   0.7282
   1.750   0.1908   0.00647   0.00164   0.0017   0.4761   0.7475
   2.000   0.2179   0.00653   0.00169   0.0020   0.4561   0.7660
   2.250   0.2450   0.00660   0.00176   0.0023   0.4366   0.7843
   2.500   0.2720   0.00668   0.00183   0.0026   0.4171   0.8019
   2.750   0.2990   0.00677   0.00191   0.0029   0.3986   0.8189
   3.000   0.3260   0.00687   0.00200   0.0032   0.3804   0.8353
   3.250   0.3530   0.00698   0.00209   0.0035   0.3619   0.8510
   3.500   0.3798   0.00711   0.00219   0.0039   0.3441   0.8663
   3.750   0.4063   0.00725   0.00231   0.0043   0.3259   0.8806
   4.000   0.4328   0.00740   0.00244   0.0047   0.3079   0.8938
   4.250   0.4591   0.00758   0.00257   0.0051   0.2896   0.9062
   4.500   0.4850   0.00778   0.00271   0.0056   0.2691   0.9183
   4.750   0.5108   0.00800   0.00287   0.0062   0.2474   0.9285
   5.000   0.5364   0.00822   0.00303   0.0067   0.2292   0.9387
   5.250   0.5623   0.00845   0.00320   0.0073   0.2123   0.9477
   5.500   0.5885   0.00869   0.00338   0.0077   0.1967   0.9558
   5.750   0.6153   0.00894   0.00358   0.0080   0.1820   0.9633
   6.000   0.6431   0.00921   0.00378   0.0080   0.1677   0.9697
   6.250   0.6738   0.00951   0.00400   0.0074   0.1530   0.9743
   6.500   0.7028   0.00980   0.00424   0.0071   0.1395   0.9797
   6.750   0.7355   0.01012   0.00448   0.0059   0.1269   0.9825
   7.000   0.7708   0.01046   0.00475   0.0041   0.1152   0.9841
   7.250   0.8055   0.01080   0.00502   0.0025   0.1045   0.9859
   7.500   0.8395   0.01112   0.00529   0.0010   0.0959   0.9880
   7.750   0.8723   0.01144   0.00558  -0.0002   0.0877   0.9906
   8.000   0.9040   0.01179   0.00588  -0.0012   0.0799   0.9931
   8.250   0.9384   0.01216   0.00619  -0.0028   0.0722   0.9944
   8.500   0.9720   0.01255   0.00654  -0.0043   0.0649   0.9959
   8.750   1.0051   0.01295   0.00689  -0.0057   0.0588   0.9976
   9.000   1.0381   0.01333   0.00725  -0.0071   0.0541   0.9992
   9.250   1.0639   0.01374   0.00764  -0.0070   0.0503   1.0000
   9.500   1.0799   0.01402   0.00793  -0.0048   0.0481   1.0000
   9.750   1.0943   0.01439   0.00828  -0.0024   0.0459   1.0000
  10.000   1.1091   0.01473   0.00864   0.0000   0.0444   1.0000
  10.250   1.1251   0.01503   0.00896   0.0022   0.0431   1.0000
  10.500   1.1405   0.01538   0.00932   0.0044   0.0419   1.0000
  10.750   1.1554   0.01579   0.00974   0.0067   0.0407   1.0000
  11.000   1.1687   0.01631   0.01028   0.0092   0.0394   1.0000
  11.250   1.1864   0.01665   0.01065   0.0109   0.0387   1.0000
  11.500   1.2039   0.01704   0.01107   0.0126   0.0379   1.0000
  11.750   1.2210   0.01748   0.01154   0.0143   0.0372   1.0000
  12.000   1.2362   0.01797   0.01206   0.0162   0.0364   1.0000
  12.250   1.2485   0.01854   0.01265   0.0185   0.0357   1.0000
  12.500   1.2579   0.01932   0.01346   0.0212   0.0349   1.0000
  12.750   1.2712   0.01997   0.01416   0.0230   0.0344   1.0000
  13.000   1.2867   0.02054   0.01478   0.0245   0.0339   1.0000
  13.250   1.3008   0.02122   0.01551   0.0260   0.0334   1.0000
  13.500   1.3142   0.02198   0.01632   0.0275   0.0329   1.0000
  13.750   1.3268   0.02282   0.01721   0.0289   0.0324   1.0000
  14.000   1.3387   0.02375   0.01819   0.0302   0.0319   1.0000
  14.250   1.3488   0.02485   0.01932   0.0315   0.0314   1.0000
  14.500   1.3558   0.02624   0.02076   0.0328   0.0309   1.0000
  14.750   1.3567   0.02819   0.02278   0.0342   0.0303   1.0000
  15.000   1.3640   0.02976   0.02443   0.0349   0.0300   1.0000
  15.250   1.3736   0.03123   0.02597   0.0354   0.0298   1.0000
  15.500   1.3816   0.03289   0.02772   0.0357   0.0295   1.0000
  15.750   1.3883   0.03476   0.02966   0.0359   0.0292   1.0000
  16.000   1.3941   0.03680   0.03178   0.0359   0.0288   1.0000
  16.250   1.3985   0.03906   0.03411   0.0357   0.0285   1.0000
  16.500   1.4016   0.04153   0.03665   0.0354   0.0281   1.0000
  16.750   1.4029   0.04430   0.03950   0.0348   0.0278   1.0000
  17.000   1.4022   0.04736   0.04263   0.0340   0.0275   1.0000
  17.250   1.3986   0.05084   0.04620   0.0330   0.0273   1.0000
  17.500   1.3925   0.05475   0.05019   0.0318   0.0270   1.0000
  17.750   1.3830   0.05916   0.05469   0.0302   0.0268   1.0000
  18.000   1.3704   0.06405   0.05967   0.0285   0.0265   1.0000
  18.250   1.3550   0.06937   0.06509   0.0265   0.0263   1.0000
  18.500   1.3453   0.07406   0.06988   0.0246   0.0261   1.0000
  18.750   1.3383   0.07856   0.07448   0.0227   0.0260   1.0000
  19.000   1.3300   0.08330   0.07932   0.0207   0.0258   1.0000
  19.250   1.3208   0.08819   0.08431   0.0185   0.0257   1.0000
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