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NACA 0024 (naca0024-il) Xfoil prediction polar at RE=100,000 Ncrit=9


Details Polar file
Airfoil: NACA 0024 (naca0024-il)
Reynolds number: 100,000
Max Cl/Cd: 34.7 at α=8.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-naca0024-il-100000.txt
Download as CSV file: xf-naca0024-il-100000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NACA 0024                                       
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.100 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -14.750  -0.3738   0.15984   0.15298  -0.0193   1.0000   0.2448
 -14.500  -0.4340   0.15746   0.15061  -0.0231   1.0000   0.2518
 -14.250  -1.0669   0.05481   0.04656  -0.0535   1.0000   0.2186
 -14.000  -1.0216   0.05559   0.04753  -0.0539   1.0000   0.2233
 -13.750  -0.9997   0.05532   0.04734  -0.0533   1.0000   0.2278
 -13.500  -1.0497   0.05057   0.04234  -0.0495   1.0000   0.2309
 -13.250  -1.0996   0.04692   0.03841  -0.0437   1.0000   0.2336
 -13.000  -1.1086   0.04520   0.03663  -0.0403   1.0000   0.2373
 -12.750  -1.0679   0.04553   0.03718  -0.0412   1.0000   0.2427
 -12.500  -1.0876   0.04391   0.03546  -0.0363   1.0000   0.2465
 -12.250  -1.1240   0.04219   0.03357  -0.0288   1.0000   0.2495
 -12.000  -1.1682   0.04097   0.03213  -0.0190   1.0000   0.2516
 -11.750  -1.1067   0.04093   0.03244  -0.0237   1.0000   0.2585
 -11.500  -1.1235   0.04020   0.03167  -0.0175   1.0000   0.2622
 -11.250  -1.1559   0.03941   0.03076  -0.0086   1.0000   0.2652
 -11.000  -1.1895   0.03842   0.02956   0.0004   1.0000   0.2683
 -10.750  -1.1572   0.03816   0.02956  -0.0004   1.0000   0.2741
 -10.500  -1.1584   0.03771   0.02913   0.0039   1.0000   0.2789
 -10.250  -1.1753   0.03691   0.02819   0.0104   1.0000   0.2833
 -10.000  -1.1826   0.03610   0.02728   0.0155   1.0000   0.2881
  -9.750  -1.1628   0.03596   0.02735   0.0166   1.0000   0.2937
  -9.500  -1.1651   0.03543   0.02677   0.0210   1.0000   0.2992
  -9.250  -1.1794   0.03460   0.02568   0.0270   1.0000   0.3045
  -9.000  -1.1569   0.03440   0.02573   0.0276   1.0000   0.3104
  -8.750  -1.1508   0.03406   0.02541   0.0306   1.0000   0.3165
  -8.500  -1.1572   0.03336   0.02448   0.0354   1.0000   0.3229
  -8.250  -1.1389   0.03314   0.02446   0.0365   1.0000   0.3289
  -8.000  -1.1023   0.03290   0.02420   0.0339   0.9933   0.3388
  -7.750  -1.0619   0.03259   0.02393   0.0307   0.9855   0.3480
  -7.500  -1.0208   0.03242   0.02374   0.0274   0.9774   0.3586
  -7.250  -0.9847   0.03209   0.02346   0.0252   0.9681   0.3677
  -7.000  -0.9421   0.03191   0.02328   0.0218   0.9604   0.3788
  -6.750  -0.9108   0.03157   0.02299   0.0207   0.9497   0.3878
  -6.500  -0.8664   0.03137   0.02279   0.0171   0.9424   0.3994
  -6.250  -0.8391   0.03105   0.02251   0.0168   0.9309   0.4083
  -6.000  -0.7940   0.03082   0.02230   0.0134   0.9237   0.4201
  -5.750  -0.7679   0.03053   0.02206   0.0134   0.9120   0.4292
  -5.500  -0.7245   0.03028   0.02183   0.0104   0.9045   0.4410
  -5.250  -0.6950   0.03001   0.02161   0.0100   0.8938   0.4506
  -5.000  -0.6561   0.02974   0.02137   0.0080   0.8851   0.4621
  -4.750  -0.6006   0.02933   0.02104   0.0031   0.8807   0.4741
  -4.500  -0.5864   0.02919   0.02089   0.0055   0.8662   0.4838
  -4.250  -0.5335   0.02873   0.02051   0.0013   0.8611   0.4958
  -4.000  -0.5082   0.02851   0.02028   0.0018   0.8500   0.5070
  -3.750  -0.4679   0.02812   0.01997   0.0000   0.8416   0.5178
  -3.500  -0.4239   0.02753   0.01934  -0.0024   0.8365   0.5312
  -3.250  -0.4013   0.02748   0.01940  -0.0011   0.8228   0.5401
  -3.000  -0.3626   0.02696   0.01885  -0.0024   0.8159   0.5531
  -2.750  -0.3270   0.02671   0.01869  -0.0032   0.8065   0.5633
  -2.500  -0.3014   0.02641   0.01838  -0.0024   0.7953   0.5753
  -2.250  -0.2529   0.02589   0.01792  -0.0050   0.7896   0.5865
  -2.000  -0.2404   0.02591   0.01795  -0.0021   0.7747   0.5977
  -1.750  -0.1964   0.02545   0.01751  -0.0040   0.7676   0.6089
  -1.500  -0.1793   0.02547   0.01755  -0.0018   0.7540   0.6204
  -1.250  -0.1402   0.02511   0.01721  -0.0029   0.7453   0.6316
  -1.000  -0.1188   0.02512   0.01724  -0.0013   0.7327   0.6432
  -0.750  -0.0841   0.02488   0.01700  -0.0017   0.7228   0.6543
  -0.500  -0.0592   0.02491   0.01704  -0.0007   0.7109   0.6661
  -0.250  -0.0280   0.02476   0.01688  -0.0006   0.7000   0.6772
   0.000   0.0000   0.02484   0.01698   0.0000   0.6887   0.6887
   0.250   0.0280   0.02476   0.01688   0.0006   0.6772   0.7000
   0.500   0.0592   0.02491   0.01704   0.0007   0.6661   0.7109
   0.750   0.0841   0.02488   0.01700   0.0017   0.6543   0.7228
   1.000   0.1188   0.02512   0.01724   0.0013   0.6432   0.7327
   1.250   0.1402   0.02511   0.01721   0.0029   0.6316   0.7453
   1.500   0.1793   0.02547   0.01755   0.0018   0.6204   0.7540
   1.750   0.1964   0.02545   0.01751   0.0040   0.6089   0.7676
   2.000   0.2404   0.02591   0.01794   0.0021   0.5977   0.7747
   2.250   0.2529   0.02589   0.01792   0.0050   0.5865   0.7897
   2.500   0.3014   0.02641   0.01838   0.0024   0.5753   0.7953
   2.750   0.3269   0.02670   0.01869   0.0032   0.5633   0.8066
   3.000   0.3626   0.02696   0.01885   0.0025   0.5531   0.8159
   3.250   0.4012   0.02748   0.01940   0.0011   0.5401   0.8229
   3.500   0.4238   0.02753   0.01934   0.0024   0.5312   0.8365
   3.750   0.4679   0.02812   0.01997   0.0000   0.5178   0.8416
   4.000   0.5080   0.02850   0.02027  -0.0018   0.5070   0.8501
   4.250   0.5335   0.02873   0.02051  -0.0013   0.4959   0.8611
   4.500   0.5863   0.02919   0.02089  -0.0055   0.4838   0.8662
   4.750   0.6006   0.02933   0.02104  -0.0031   0.4741   0.8808
   5.000   0.6561   0.02974   0.02136  -0.0080   0.4621   0.8852
   5.250   0.6947   0.03000   0.02160  -0.0099   0.4506   0.8939
   5.500   0.7245   0.03027   0.02182  -0.0105   0.4410   0.9046
   5.750   0.7677   0.03052   0.02205  -0.0134   0.4292   0.9121
   6.000   0.7941   0.03081   0.02229  -0.0134   0.4201   0.9238
   6.250   0.8390   0.03104   0.02251  -0.0168   0.4083   0.9310
   6.500   0.8665   0.03136   0.02278  -0.0172   0.3994   0.9425
   6.750   0.9108   0.03156   0.02298  -0.0207   0.3878   0.9498
   7.000   0.9423   0.03190   0.02327  -0.0219   0.3788   0.9605
   7.250   0.9848   0.03207   0.02345  -0.0252   0.3677   0.9682
   7.500   1.0210   0.03241   0.02373  -0.0275   0.3586   0.9775
   7.750   1.0621   0.03257   0.02392  -0.0307   0.3480   0.9856
   8.000   1.1026   0.03289   0.02418  -0.0339   0.3388   0.9934
   8.250   1.1386   0.03312   0.02445  -0.0364   0.3289   1.0000
   8.500   1.1571   0.03335   0.02446  -0.0354   0.3229   1.0000
   8.750   1.1506   0.03405   0.02540  -0.0306   0.3166   1.0000
   9.000   1.1566   0.03438   0.02572  -0.0275   0.3104   1.0000
   9.250   1.1793   0.03458   0.02566  -0.0270   0.3045   1.0000
   9.500   1.1649   0.03542   0.02675  -0.0209   0.2992   1.0000
   9.750   1.1626   0.03595   0.02733  -0.0166   0.2937   1.0000
  10.000   1.1823   0.03609   0.02727  -0.0154   0.2881   1.0000
  10.250   1.1752   0.03689   0.02816  -0.0104   0.2834   1.0000
  10.500   1.1583   0.03769   0.02910  -0.0039   0.2789   1.0000
  10.750   1.1571   0.03815   0.02954   0.0004   0.2741   1.0000
  11.000   1.1895   0.03840   0.02954  -0.0004   0.2683   1.0000
  11.250   1.1560   0.03939   0.03074   0.0086   0.2652   1.0000
  11.500   1.1238   0.04018   0.03165   0.0174   0.2622   1.0000
  11.750   1.1071   0.04091   0.03241   0.0237   0.2585   1.0000
  12.000   1.1684   0.04095   0.03212   0.0189   0.2516   1.0000
  12.250   1.1244   0.04218   0.03354   0.0287   0.2494   1.0000
  12.500   1.0881   0.04388   0.03543   0.0363   0.2464   1.0000
  12.750   1.0690   0.04548   0.03713   0.0411   0.2426   1.0000
  13.000   1.1120   0.04510   0.03651   0.0399   0.2371   1.0000
  13.250   1.1001   0.04691   0.03840   0.0436   0.2336   1.0000
  13.500   1.0508   0.05053   0.04231   0.0494   0.2308   1.0000
  13.750   1.0028   0.05515   0.04717   0.0530   0.2276   1.0000
  14.000   1.0307   0.05503   0.04693   0.0534   0.2230   1.0000
  14.250   1.0674   0.05483   0.04659   0.0533   0.2186   1.0000
  14.500   0.4349   0.15759   0.15074   0.0228   0.2518   1.0000
  14.750   0.3756   0.15997   0.15311   0.0189   0.2446   1.0000
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