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NACA 23024 (naca23024-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: NACA 23024 (naca23024-il)
Reynolds number: 1,000,000
Max Cl/Cd: 56.88 at α=8.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-naca23024-il-1000000.txt
Download as CSV file: xf-naca23024-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NACA 23024                                      
  
 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  -1.1752   0.06826   0.06346  -0.0657   1.0000   0.0679
 -19.500  -1.1789   0.06535   0.06050  -0.0658   1.0000   0.0691
 -19.250  -1.1790   0.06291   0.05799  -0.0657   1.0000   0.0701
 -19.000  -1.1861   0.05973   0.05477  -0.0657   1.0000   0.0715
 -18.750  -1.1912   0.05684   0.05184  -0.0654   1.0000   0.0725
 -18.500  -1.1950   0.05416   0.04912  -0.0651   1.0000   0.0740
 -18.250  -1.1968   0.05170   0.04662  -0.0646   1.0000   0.0753
 -18.000  -1.1951   0.04964   0.04450  -0.0640   1.0000   0.0765
 -17.750  -1.1989   0.04712   0.04194  -0.0633   1.0000   0.0781
 -17.500  -1.2022   0.04470   0.03949  -0.0625   1.0000   0.0796
 -17.250  -1.2031   0.04259   0.03735  -0.0615   1.0000   0.0814
 -17.000  -1.2006   0.04085   0.03556  -0.0604   1.0000   0.0831
 -16.750  -1.2012   0.03889   0.03357  -0.0592   1.0000   0.0848
 -16.500  -1.2027   0.03697   0.03163  -0.0577   1.0000   0.0869
 -16.250  -1.2018   0.03533   0.02997  -0.0561   1.0000   0.0892
 -16.000  -1.1990   0.03388   0.02848  -0.0545   1.0000   0.0912
 -15.750  -1.2005   0.03225   0.02684  -0.0524   1.0000   0.0934
 -15.500  -1.2013   0.03079   0.02537  -0.0502   1.0000   0.0962
 -15.250  -1.2001   0.02957   0.02412  -0.0478   1.0000   0.0986
 -15.000  -1.1832   0.02814   0.02270  -0.0485   0.9989   0.1023
 -14.750  -1.1626   0.02689   0.02145  -0.0496   0.9973   0.1069
 -14.500  -1.1419   0.02566   0.02023  -0.0506   0.9953   0.1111
 -14.250  -1.1191   0.02461   0.01918  -0.0518   0.9935   0.1164
 -14.000  -1.0975   0.02348   0.01808  -0.0528   0.9921   0.1223
 -13.750  -1.0768   0.02247   0.01707  -0.0532   0.9898   0.1277
 -13.500  -1.0578   0.02140   0.01604  -0.0533   0.9869   0.1337
 -13.250  -1.0359   0.02044   0.01510  -0.0538   0.9843   0.1409
 -12.750  -0.9862   0.01875   0.01348  -0.0555   0.9805   0.1559
 -12.500  -0.9590   0.01802   0.01279  -0.0565   0.9792   0.1636
 -12.250  -0.9372   0.01732   0.01211  -0.0563   0.9758   0.1705
 -12.000  -0.9196   0.01654   0.01136  -0.0554   0.9702   0.1779
 -11.750  -0.8921   0.01598   0.01081  -0.0560   0.9673   0.1849
 -11.500  -0.8652   0.01529   0.01018  -0.0567   0.9650   0.1934
 -11.250  -0.8489   0.01476   0.00965  -0.0550   0.9570   0.1997
 -11.000  -0.8257   0.01416   0.00909  -0.0547   0.9517   0.2071
 -10.750  -0.7973   0.01364   0.00859  -0.0553   0.9477   0.2151
 -10.500  -0.7760   0.01314   0.00811  -0.0545   0.9385   0.2219
 -10.250  -0.7397   0.01267   0.00767  -0.0566   0.9342   0.2305
 -10.000  -0.7025   0.01221   0.00723  -0.0588   0.9275   0.2388
  -9.750  -0.6625   0.01187   0.00688  -0.0616   0.9190   0.2458
  -9.500  -0.6222   0.01148   0.00651  -0.0645   0.9092   0.2553
  -9.250  -0.5841   0.01126   0.00624  -0.0667   0.8960   0.2617
  -9.000  -0.5545   0.01096   0.00595  -0.0674   0.8817   0.2700
  -8.750  -0.5190   0.01081   0.00573  -0.0691   0.8674   0.2767
  -8.500  -0.4957   0.01059   0.00550  -0.0685   0.8529   0.2836
  -8.250  -0.4668   0.01041   0.00530  -0.0689   0.8381   0.2910
  -8.000  -0.4361   0.01032   0.00513  -0.0695   0.8213   0.2964
  -7.750  -0.4127   0.01011   0.00491  -0.0688   0.8039   0.3047
  -7.500  -0.3887   0.01000   0.00474  -0.0681   0.7866   0.3108
  -7.250  -0.3667   0.00991   0.00459  -0.0669   0.7700   0.3174
  -7.000  -0.3483   0.00977   0.00442  -0.0651   0.7532   0.3250
  -6.750  -0.3281   0.00969   0.00430  -0.0635   0.7384   0.3313
  -6.500  -0.3102   0.00962   0.00417  -0.0615   0.7224   0.3378
  -6.250  -0.2933   0.00949   0.00404  -0.0592   0.7083   0.3453
  -6.000  -0.2744   0.00944   0.00394  -0.0573   0.6950   0.3517
  -5.750  -0.2571   0.00936   0.00383  -0.0551   0.6811   0.3588
  -5.500  -0.2409   0.00928   0.00373  -0.0527   0.6685   0.3655
  -5.250  -0.2234   0.00924   0.00365  -0.0504   0.6556   0.3724
  -5.000  -0.2070   0.00917   0.00357  -0.0480   0.6438   0.3793
  -4.750  -0.1920   0.00911   0.00349  -0.0452   0.6305   0.3867
  -4.500  -0.1739   0.00908   0.00343  -0.0431   0.6191   0.3933
  -4.250  -0.1589   0.00905   0.00336  -0.0403   0.6065   0.4003
  -4.000  -0.1446   0.00898   0.00330  -0.0374   0.5958   0.4084
  -3.750  -0.1288   0.00898   0.00325  -0.0347   0.5829   0.4152
  -3.500  -0.1143   0.00894   0.00320  -0.0318   0.5714   0.4227
  -3.250  -0.1005   0.00891   0.00316  -0.0287   0.5598   0.4308
  -3.000  -0.0844   0.00892   0.00313  -0.0261   0.5490   0.4375
  -2.750  -0.0720   0.00887   0.00309  -0.0227   0.5388   0.4456
  -2.500  -0.0630   0.00886   0.00307  -0.0186   0.5294   0.4539
  -2.250  -0.0486   0.00886   0.00305  -0.0156   0.5204   0.4603
  -2.000  -0.0416   0.00883   0.00302  -0.0110   0.5110   0.4691
  -1.750  -0.0297   0.00882   0.00301  -0.0075   0.5030   0.4778
  -1.500  -0.0164   0.00883   0.00300  -0.0043   0.4934   0.4852
  -1.250  -0.0087   0.00883   0.00300   0.0001   0.4847   0.4943
  -1.000   0.0060   0.00882   0.00300   0.0030   0.4767   0.5028
  -0.750   0.0165   0.00884   0.00301   0.0068   0.4673   0.5108
  -0.500   0.0257   0.00884   0.00302   0.0109   0.4594   0.5202
  -0.250   0.0396   0.00887   0.00304   0.0140   0.4516   0.5286
   0.000   0.0464   0.00888   0.00306   0.0186   0.4434   0.5381
   0.250   0.0600   0.00890   0.00309   0.0217   0.4360   0.5481
   0.500   0.0757   0.00892   0.00312   0.0244   0.4286   0.5571
   0.750   0.0873   0.00897   0.00316   0.0279   0.4192   0.5683
   1.250   0.1197   0.00900   0.00323   0.0330   0.4050   0.5894
   1.500   0.1341   0.00909   0.00330   0.0358   0.3961   0.5991
   1.750   0.1505   0.00909   0.00334   0.0383   0.3895   0.6107
   2.000   0.1668   0.00916   0.00341   0.0407   0.3816   0.6222
   2.250   0.1818   0.00920   0.00348   0.0434   0.3743   0.6344
   2.500   0.2004   0.00925   0.00355   0.0454   0.3673   0.6462
   2.750   0.2150   0.00932   0.00364   0.0481   0.3595   0.6585
   3.000   0.2322   0.00940   0.00373   0.0503   0.3525   0.6719
   3.250   0.2496   0.00944   0.00381   0.0525   0.3454   0.6849
   3.500   0.2662   0.00957   0.00393   0.0547   0.3371   0.6984
   3.750   0.2842   0.00962   0.00404   0.0567   0.3306   0.7133
   4.000   0.3024   0.00972   0.00416   0.0586   0.3237   0.7272
   4.250   0.3191   0.00985   0.00431   0.0607   0.3157   0.7436
   4.500   0.3401   0.00991   0.00444   0.0620   0.3094   0.7594
   4.750   0.3591   0.01006   0.00461   0.0636   0.3010   0.7759
   5.000   0.3801   0.01019   0.00478   0.0648   0.2944   0.7934
   5.250   0.4067   0.01032   0.00496   0.0648   0.2870   0.8104
   5.500   0.4327   0.01052   0.00518   0.0648   0.2789   0.8264
   5.750   0.4586   0.01066   0.00535   0.0649   0.2730   0.8421
   6.000   0.4883   0.01087   0.00559   0.0641   0.2652   0.8574
   6.250   0.5156   0.01107   0.00582   0.0638   0.2588   0.8721
   6.500   0.5456   0.01129   0.00606   0.0629   0.2524   0.8871
   6.750   0.5795   0.01160   0.00638   0.0611   0.2448   0.8999
   7.000   0.6150   0.01184   0.00665   0.0591   0.2398   0.9126
   7.250   0.6589   0.01224   0.00704   0.0552   0.2329   0.9214
   7.500   0.6959   0.01263   0.00743   0.0528   0.2278   0.9308
   7.750   0.7366   0.01303   0.00783   0.0496   0.2230   0.9353
   8.000   0.7701   0.01354   0.00832   0.0478   0.2181   0.9403
   8.250   0.7917   0.01403   0.00880   0.0483   0.2134   0.9492
   8.500   0.8214   0.01444   0.00923   0.0474   0.2101   0.9528
   8.750   0.8451   0.01493   0.00970   0.0476   0.2063   0.9586
   9.000   0.8627   0.01554   0.01029   0.0486   0.2021   0.9654
   9.250   0.8927   0.01604   0.01079   0.0474   0.1985   0.9678
   9.500   0.9219   0.01649   0.01125   0.0463   0.1954   0.9706
   9.750   0.9357   0.01714   0.01190   0.0482   0.1925   0.9781
  10.000   0.9649   0.01779   0.01252   0.0466   0.1881   0.9792
  10.250   0.9953   0.01834   0.01307   0.0450   0.1850   0.9805
  10.500   1.0263   0.01881   0.01356   0.0433   0.1821   0.9820
  10.750   1.0542   0.01943   0.01417   0.0420   0.1787   0.9838
  11.000   1.0787   0.02023   0.01495   0.0411   0.1749   0.9863
  11.250   1.1041   0.02089   0.01562   0.0402   0.1721   0.9888
  11.500   1.1270   0.02162   0.01637   0.0398   0.1692   0.9916
  11.750   1.1551   0.02228   0.01704   0.0381   0.1663   0.9928
  12.000   1.1795   0.02316   0.01789   0.0368   0.1627   0.9944
  12.250   1.2059   0.02391   0.01867   0.0353   0.1598   0.9962
  12.500   1.2325   0.02464   0.01941   0.0338   0.1575   0.9979
  12.750   1.2576   0.02554   0.02032   0.0322   0.1540   0.9994
  13.000   1.2682   0.02668   0.02145   0.0329   0.1510   1.0000
  13.250   1.2718   0.02767   0.02246   0.0351   0.1492   1.0000
  13.500   1.2793   0.02852   0.02335   0.0369   0.1473   1.0000
  13.750   1.2846   0.02959   0.02445   0.0387   0.1452   1.0000
  14.000   1.2888   0.03079   0.02566   0.0404   0.1429   1.0000
  14.250   1.2891   0.03233   0.02720   0.0422   0.1404   1.0000
  14.500   1.2946   0.03357   0.02848   0.0436   0.1383   1.0000
  14.750   1.3008   0.03483   0.02978   0.0448   0.1365   1.0000
  15.000   1.3062   0.03619   0.03116   0.0459   0.1342   1.0000
  15.250   1.3077   0.03793   0.03292   0.0470   0.1320   1.0000
  15.500   1.3057   0.03999   0.03500   0.0482   0.1296   1.0000
  15.750   1.3126   0.04138   0.03643   0.0490   0.1279   1.0000
  16.000   1.3165   0.04307   0.03817   0.0497   0.1260   1.0000
  16.250   1.3191   0.04488   0.04001   0.0504   0.1238   1.0000
  16.500   1.3170   0.04719   0.04233   0.0511   0.1218   1.0000
  16.750   1.3130   0.04970   0.04488   0.0517   0.1198   1.0000
  17.000   1.3182   0.05142   0.04666   0.0520   0.1182   1.0000
  17.250   1.3187   0.05361   0.04888   0.0524   0.1162   1.0000
  17.500   1.3180   0.05596   0.05127   0.0526   0.1144   1.0000
  17.750   1.3092   0.05918   0.05451   0.0527   0.1117   1.0000
  18.000   1.3090   0.06156   0.05693   0.0528   0.1105   1.0000
  18.250   1.3094   0.06396   0.05939   0.0527   0.1088   1.0000
  18.500   1.3080   0.06652   0.06200   0.0526   0.1066   1.0000
  18.750   1.3002   0.06985   0.06536   0.0523   0.1045   1.0000
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