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NACA 0024 (naca0024-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: NACA 0024 (naca0024-il)
Reynolds number: 1,000,000
Max Cl/Cd: 68.81 at α=9°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-naca0024-il-1000000.txt
Download as CSV file: xf-naca0024-il-1000000.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 =     1.000 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -19.750  -1.3130   0.07618   0.07152  -0.0430   1.0000   0.0813
 -19.500  -1.3173   0.07279   0.06808  -0.0437   1.0000   0.0827
 -19.250  -1.3203   0.06954   0.06477  -0.0444   1.0000   0.0841
 -19.000  -1.3200   0.06667   0.06184  -0.0450   1.0000   0.0854
 -18.750  -1.3216   0.06364   0.05876  -0.0455   1.0000   0.0867
 -18.500  -1.3283   0.06010   0.05517  -0.0460   1.0000   0.0883
 -18.250  -1.3312   0.05700   0.05203  -0.0465   1.0000   0.0898
 -18.000  -1.3296   0.05442   0.04941  -0.0467   1.0000   0.0914
 -17.750  -1.3267   0.05198   0.04691  -0.0470   1.0000   0.0928
 -17.500  -1.3240   0.04957   0.04445  -0.0471   1.0000   0.0943
 -17.250  -1.3255   0.04681   0.04166  -0.0471   1.0000   0.0962
 -17.000  -1.3238   0.04437   0.03918  -0.0471   1.0000   0.0980
 -16.750  -1.3191   0.04225   0.03703  -0.0471   1.0000   0.0999
 -16.500  -1.3105   0.04055   0.03528  -0.0470   1.0000   0.1015
 -16.250  -1.3080   0.03832   0.03302  -0.0467   1.0000   0.1036
 -16.000  -1.3041   0.03627   0.03096  -0.0463   1.0000   0.1058
 -15.750  -1.2965   0.03459   0.02925  -0.0459   1.0000   0.1080
 -15.500  -1.2870   0.03310   0.02772  -0.0455   1.0000   0.1099
 -15.250  -1.2792   0.03153   0.02612  -0.0450   1.0000   0.1121
 -15.000  -1.2727   0.02992   0.02451  -0.0442   1.0000   0.1148
 -14.750  -1.2638   0.02854   0.02311  -0.0435   1.0000   0.1173
 -14.500  -1.2515   0.02747   0.02201  -0.0428   1.0000   0.1196
 -14.250  -1.2438   0.02615   0.02068  -0.0417   1.0000   0.1225
 -14.000  -1.2361   0.02495   0.01949  -0.0404   1.0000   0.1255
 -13.750  -1.2262   0.02402   0.01855  -0.0390   1.0000   0.1283
 -13.500  -1.2178   0.02317   0.01767  -0.0371   1.0000   0.1307
 -13.250  -1.2159   0.02222   0.01673  -0.0343   1.0000   0.1340
 -13.000  -1.2150   0.02148   0.01599  -0.0310   1.0000   0.1368
 -12.750  -1.2173   0.02090   0.01539  -0.0269   1.0000   0.1393
 -12.500  -1.1937   0.02010   0.01459  -0.0276   0.9985   0.1432
 -12.250  -1.1680   0.01923   0.01375  -0.0287   0.9964   0.1479
 -12.000  -1.1387   0.01861   0.01313  -0.0302   0.9945   0.1518
 -11.750  -1.1115   0.01782   0.01236  -0.0315   0.9927   0.1569
 -11.500  -1.0816   0.01717   0.01173  -0.0330   0.9913   0.1619
 -11.250  -1.0534   0.01658   0.01115  -0.0341   0.9884   0.1665
 -11.000  -1.0278   0.01593   0.01053  -0.0347   0.9838   0.1718
 -10.750  -0.9996   0.01545   0.01005  -0.0355   0.9792   0.1764
 -10.500  -0.9761   0.01489   0.00952  -0.0355   0.9731   0.1819
 -10.250  -0.9568   0.01442   0.00906  -0.0344   0.9638   0.1869
 -10.000  -0.9362   0.01407   0.00869  -0.0334   0.9549   0.1909
  -9.750  -0.9203   0.01360   0.00823  -0.0316   0.9439   0.1966
  -9.500  -0.9019   0.01325   0.00787  -0.0301   0.9333   0.2018
  -9.250  -0.8824   0.01295   0.00753  -0.0288   0.9225   0.2064
  -9.000  -0.8640   0.01257   0.00717  -0.0273   0.9108   0.2124
  -8.750  -0.8436   0.01230   0.00687  -0.0261   0.8998   0.2177
  -8.500  -0.8227   0.01202   0.00658  -0.0250   0.8879   0.2234
  -8.250  -0.8025   0.01173   0.00628  -0.0237   0.8764   0.2296
  -8.000  -0.7798   0.01153   0.00604  -0.0228   0.8640   0.2347
  -7.750  -0.7589   0.01126   0.00576  -0.0217   0.8521   0.2414
  -7.500  -0.7368   0.01104   0.00553  -0.0207   0.8392   0.2478
  -7.250  -0.7134   0.01087   0.00532  -0.0199   0.8272   0.2533
  -7.000  -0.6924   0.01064   0.00508  -0.0187   0.8138   0.2607
  -6.750  -0.6688   0.01048   0.00490  -0.0179   0.8017   0.2670
  -6.500  -0.6471   0.01032   0.00471  -0.0167   0.7882   0.2737
  -6.250  -0.6259   0.01016   0.00455  -0.0154   0.7756   0.2810
  -6.000  -0.6032   0.01009   0.00443  -0.0144   0.7628   0.2865
  -5.750  -0.5825   0.00993   0.00428  -0.0130   0.7496   0.2948
  -5.500  -0.5586   0.00983   0.00415  -0.0122   0.7372   0.3019
  -5.250  -0.5346   0.00972   0.00402  -0.0114   0.7240   0.3090
  -5.000  -0.5109   0.00960   0.00390  -0.0106   0.7119   0.3170
  -4.750  -0.4855   0.00956   0.00381  -0.0100   0.6989   0.3233
  -4.500  -0.4618   0.00942   0.00369  -0.0092   0.6871   0.3323
  -4.250  -0.4370   0.00936   0.00360  -0.0085   0.6741   0.3400
  -4.000  -0.4119   0.00926   0.00351  -0.0080   0.6629   0.3482
  -3.750  -0.3875   0.00920   0.00342  -0.0072   0.6500   0.3566
  -3.500  -0.3610   0.00915   0.00336  -0.0069   0.6389   0.3638
  -3.250  -0.3370   0.00907   0.00327  -0.0061   0.6265   0.3730
  -3.000  -0.3105   0.00902   0.00322  -0.0057   0.6157   0.3809
  -2.750  -0.2858   0.00898   0.00315  -0.0050   0.6034   0.3896
  -2.500  -0.2596   0.00891   0.00310  -0.0046   0.5933   0.3983
  -2.250  -0.2339   0.00891   0.00306  -0.0041   0.5812   0.4060
  -2.000  -0.2083   0.00883   0.00301  -0.0036   0.5711   0.4156
  -1.750  -0.1820   0.00884   0.00298  -0.0032   0.5596   0.4234
  -1.500  -0.1564   0.00878   0.00294  -0.0027   0.5496   0.4330
  -1.250  -0.1304   0.00877   0.00292  -0.0022   0.5385   0.4420
  -1.000  -0.1043   0.00875   0.00289  -0.0018   0.5287   0.4510
  -0.750  -0.0784   0.00873   0.00288  -0.0013   0.5182   0.4608
  -0.500  -0.0519   0.00875   0.00287  -0.0009   0.5083   0.4691
  -0.250  -0.0262   0.00870   0.00286  -0.0004   0.4986   0.4796
   0.000   0.0000   0.00875   0.00286   0.0000   0.4882   0.4882
   0.250   0.0262   0.00870   0.00285   0.0004   0.4796   0.4985
   0.500   0.0520   0.00875   0.00287   0.0009   0.4692   0.5083
   0.750   0.0784   0.00873   0.00287   0.0013   0.4608   0.5182
   1.000   0.1043   0.00875   0.00289   0.0018   0.4509   0.5286
   1.250   0.1304   0.00877   0.00292   0.0022   0.4420   0.5385
   1.500   0.1564   0.00878   0.00294   0.0027   0.4331   0.5496
   1.750   0.1820   0.00884   0.00298   0.0032   0.4234   0.5596
   2.000   0.2083   0.00883   0.00301   0.0036   0.4156   0.5711
   2.250   0.2339   0.00891   0.00306   0.0041   0.4059   0.5812
   2.500   0.2597   0.00891   0.00310   0.0046   0.3983   0.5933
   2.750   0.2859   0.00898   0.00315   0.0050   0.3895   0.6034
   3.000   0.3106   0.00902   0.00322   0.0057   0.3809   0.6157
   3.250   0.3371   0.00907   0.00327   0.0061   0.3730   0.6265
   3.500   0.3611   0.00915   0.00336   0.0069   0.3638   0.6389
   3.750   0.3876   0.00920   0.00342   0.0072   0.3566   0.6500
   4.000   0.4120   0.00926   0.00351   0.0079   0.3481   0.6629
   4.250   0.4372   0.00936   0.00360   0.0085   0.3400   0.6741
   4.500   0.4620   0.00942   0.00369   0.0092   0.3323   0.6870
   4.750   0.4857   0.00955   0.00381   0.0100   0.3233   0.6989
   5.000   0.5111   0.00960   0.00390   0.0105   0.3170   0.7119
   5.250   0.5349   0.00972   0.00402   0.0113   0.3089   0.7240
   5.500   0.5589   0.00983   0.00415   0.0121   0.3019   0.7372
   5.750   0.5829   0.00993   0.00428   0.0129   0.2948   0.7497
   6.000   0.6036   0.01009   0.00443   0.0143   0.2865   0.7627
   6.250   0.6264   0.01016   0.00455   0.0153   0.2809   0.7756
   6.500   0.6476   0.01032   0.00471   0.0166   0.2737   0.7882
   6.750   0.6693   0.01048   0.00490   0.0178   0.2670   0.8016
   7.000   0.6929   0.01064   0.00508   0.0186   0.2607   0.8137
   7.250   0.7140   0.01087   0.00532   0.0198   0.2532   0.8271
   7.500   0.7374   0.01104   0.00553   0.0206   0.2478   0.8392
   7.750   0.7595   0.01126   0.00576   0.0215   0.2414   0.8520
   8.000   0.7805   0.01152   0.00604   0.0227   0.2347   0.8640
   8.250   0.8032   0.01173   0.00627   0.0236   0.2295   0.8762
   8.500   0.8235   0.01202   0.00657   0.0248   0.2233   0.8878
   8.750   0.8444   0.01230   0.00686   0.0259   0.2177   0.8997
   9.000   0.8649   0.01257   0.00717   0.0271   0.2124   0.9107
   9.250   0.8833   0.01295   0.00753   0.0286   0.2063   0.9224
   9.500   0.9030   0.01324   0.00786   0.0299   0.2017   0.9331
   9.750   0.9214   0.01360   0.00822   0.0314   0.1966   0.9438
  10.000   0.9373   0.01407   0.00868   0.0332   0.1909   0.9548
  10.250   0.9579   0.01442   0.00905   0.0342   0.1868   0.9637
  10.500   0.9772   0.01488   0.00951   0.0353   0.1818   0.9731
  10.750   1.0007   0.01544   0.01004   0.0353   0.1764   0.9792
  11.000   1.0289   0.01592   0.01051   0.0345   0.1717   0.9838
  11.250   1.0544   0.01656   0.01113   0.0339   0.1664   0.9885
  11.500   1.0828   0.01715   0.01171   0.0328   0.1618   0.9913
  11.750   1.1128   0.01780   0.01234   0.0312   0.1569   0.9928
  12.000   1.1401   0.01859   0.01310   0.0299   0.1517   0.9946
  12.250   1.1695   0.01920   0.01372   0.0285   0.1478   0.9965
  12.500   1.1952   0.02007   0.01456   0.0273   0.1431   0.9986
  12.750   1.2171   0.02085   0.01535   0.0270   0.1393   1.0000
  13.000   1.2151   0.02144   0.01594   0.0310   0.1368   1.0000
  13.250   1.2165   0.02217   0.01668   0.0343   0.1340   1.0000
  13.500   1.2187   0.02313   0.01762   0.0370   0.1307   1.0000
  13.750   1.2275   0.02397   0.01849   0.0388   0.1282   1.0000
  14.000   1.2377   0.02490   0.01943   0.0401   0.1254   1.0000
  14.250   1.2456   0.02610   0.02063   0.0414   0.1224   1.0000
  14.500   1.2538   0.02740   0.02194   0.0425   0.1195   1.0000
  14.750   1.2660   0.02848   0.02305   0.0432   0.1172   1.0000
  15.000   1.2751   0.02986   0.02445   0.0439   0.1146   1.0000
  15.250   1.2817   0.03146   0.02605   0.0446   0.1120   1.0000
  15.500   1.2899   0.03301   0.02763   0.0452   0.1098   1.0000
  15.750   1.2995   0.03451   0.02916   0.0455   0.1079   1.0000
  16.000   1.3071   0.03619   0.03087   0.0459   0.1057   1.0000
  16.250   1.3110   0.03825   0.03294   0.0463   0.1035   1.0000
  16.500   1.3141   0.04042   0.03515   0.0465   0.1015   1.0000
  16.750   1.3227   0.04213   0.03690   0.0466   0.0998   1.0000
  17.000   1.3273   0.04427   0.03908   0.0467   0.0979   1.0000
  17.250   1.3291   0.04670   0.04155   0.0467   0.0961   1.0000
  17.500   1.3275   0.04948   0.04436   0.0466   0.0941   1.0000
  17.750   1.3309   0.05184   0.04676   0.0465   0.0927   1.0000
  18.000   1.3339   0.05428   0.04926   0.0462   0.0913   1.0000
  18.250   1.3354   0.05687   0.05189   0.0459   0.0897   1.0000
  18.500   1.3324   0.05999   0.05506   0.0455   0.0882   1.0000
  18.750   1.3255   0.06356   0.05866   0.0450   0.0866   1.0000
  19.000   1.3252   0.06644   0.06161   0.0445   0.0853   1.0000
  19.250   1.3250   0.06938   0.06461   0.0439   0.0840   1.0000
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