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NACA 0024 (naca0024-il) Xfoil prediction polar at RE=200,000 Ncrit=9


Details Polar file
Airfoil: NACA 0024 (naca0024-il)
Reynolds number: 200,000
Max Cl/Cd: 42.99 at α=10°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-naca0024-il-200000.txt
Download as CSV file: xf-naca0024-il-200000.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 =     0.200 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -19.750  -1.2026   0.08451   0.07774  -0.0536   1.0000   0.1207
 -19.500  -1.1773   0.08485   0.07824  -0.0531   1.0000   0.1228
 -19.250  -1.1728   0.08250   0.07588  -0.0538   1.0000   0.1250
 -19.000  -1.1838   0.07823   0.07147  -0.0552   1.0000   0.1272
 -18.750  -1.2059   0.07277   0.06576  -0.0568   1.0000   0.1293
 -18.500  -1.1994   0.07079   0.06378  -0.0570   1.0000   0.1316
 -18.250  -1.1860   0.06961   0.06267  -0.0571   1.0000   0.1339
 -18.000  -1.1845   0.06706   0.06008  -0.0575   1.0000   0.1364
 -17.750  -1.1934   0.06344   0.05630  -0.0582   1.0000   0.1389
 -17.500  -1.2041   0.05978   0.05245  -0.0587   1.0000   0.1412
 -17.250  -1.1847   0.05922   0.05203  -0.0584   1.0000   0.1439
 -17.000  -1.1786   0.05734   0.05015  -0.0584   1.0000   0.1466
 -16.750  -1.1804   0.05473   0.04744  -0.0585   1.0000   0.1494
 -16.500  -1.1905   0.05150   0.04399  -0.0584   1.0000   0.1519
 -16.250  -1.1721   0.05078   0.04341  -0.0580   1.0000   0.1550
 -16.000  -1.1645   0.04922   0.04186  -0.0577   1.0000   0.1580
 -15.750  -1.1632   0.04716   0.03972  -0.0573   1.0000   0.1612
 -15.500  -1.1694   0.04464   0.03700  -0.0566   1.0000   0.1640
 -15.250  -1.1514   0.04388   0.03638  -0.0561   1.0000   0.1675
 -15.000  -1.1440   0.04250   0.03501  -0.0554   1.0000   0.1708
 -14.750  -1.1420   0.04078   0.03321  -0.0545   1.0000   0.1743
 -14.500  -1.1415   0.03904   0.03134  -0.0532   1.0000   0.1777
 -14.250  -1.1265   0.03820   0.03062  -0.0525   1.0000   0.1813
 -14.000  -1.1203   0.03698   0.02940  -0.0513   1.0000   0.1851
 -13.750  -1.1193   0.03556   0.02787  -0.0496   1.0000   0.1889
 -13.500  -1.1104   0.03451   0.02684  -0.0481   1.0000   0.1928
 -13.250  -1.1021   0.03361   0.02600  -0.0465   1.0000   0.1966
 -13.000  -1.0993   0.03261   0.02496  -0.0443   1.0000   0.2007
 -12.750  -1.1029   0.03154   0.02376  -0.0412   1.0000   0.2045
 -12.500  -1.0909   0.03087   0.02323  -0.0394   1.0000   0.2088
 -12.250  -1.0888   0.03016   0.02254  -0.0364   1.0000   0.2127
 -12.000  -1.0916   0.02945   0.02178  -0.0327   1.0000   0.2169
 -11.750  -1.0954   0.02879   0.02106  -0.0286   1.0000   0.2208
 -11.500  -1.0918   0.02829   0.02067  -0.0253   1.0000   0.2248
 -11.250  -1.0971   0.02784   0.02023  -0.0206   1.0000   0.2287
 -11.000  -1.1065   0.02742   0.01976  -0.0153   1.0000   0.2326
 -10.750  -1.1174   0.02704   0.01930  -0.0096   1.0000   0.2362
 -10.500  -1.1189   0.02666   0.01904  -0.0053   1.0000   0.2402
 -10.250  -1.1294   0.02640   0.01879   0.0004   1.0000   0.2438
 -10.000  -1.1149   0.02596   0.01827   0.0016   0.9966   0.2499
  -9.750  -1.0804   0.02541   0.01780  -0.0007   0.9922   0.2570
  -9.500  -1.0517   0.02496   0.01733  -0.0019   0.9861   0.2642
  -9.250  -1.0195   0.02444   0.01681  -0.0036   0.9802   0.2717
  -9.000  -0.9827   0.02402   0.01643  -0.0061   0.9762   0.2797
  -8.750  -0.9590   0.02358   0.01590  -0.0060   0.9670   0.2871
  -8.500  -0.9197   0.02305   0.01551  -0.0088   0.9625   0.2953
  -8.250  -0.8881   0.02263   0.01500  -0.0101   0.9561   0.3038
  -8.000  -0.8549   0.02210   0.01461  -0.0115   0.9488   0.3117
  -7.750  -0.8158   0.02163   0.01409  -0.0141   0.9443   0.3212
  -7.500  -0.7698   0.02103   0.01360  -0.0180   0.9420   0.3305
  -7.250  -0.7497   0.02073   0.01327  -0.0167   0.9305   0.3385
  -7.000  -0.7109   0.02018   0.01277  -0.0190   0.9258   0.3476
  -6.750  -0.6721   0.01970   0.01230  -0.0212   0.9220   0.3573
  -6.500  -0.6547   0.01940   0.01199  -0.0192   0.9091   0.3651
  -6.250  -0.6199   0.01893   0.01160  -0.0204   0.9036   0.3743
  -5.750  -0.5699   0.01823   0.01094  -0.0190   0.8842   0.3916
  -5.500  -0.5468   0.01797   0.01062  -0.0179   0.8745   0.4008
  -5.250  -0.5211   0.01761   0.01033  -0.0172   0.8639   0.4093
  -5.000  -0.4948   0.01732   0.01002  -0.0167   0.8552   0.4187
  -4.750  -0.4731   0.01708   0.00977  -0.0153   0.8425   0.4274
  -4.500  -0.4451   0.01679   0.00950  -0.0150   0.8336   0.4366
  -4.250  -0.4258   0.01665   0.00928  -0.0131   0.8200   0.4459
  -4.000  -0.3965   0.01635   0.00906  -0.0131   0.8105   0.4550
  -3.750  -0.3759   0.01624   0.00890  -0.0115   0.7969   0.4647
  -3.500  -0.3481   0.01600   0.00868  -0.0112   0.7864   0.4739
  -3.250  -0.3258   0.01589   0.00856  -0.0099   0.7731   0.4838
  -3.000  -0.2996   0.01572   0.00836  -0.0094   0.7621   0.4935
  -2.750  -0.2757   0.01561   0.00828  -0.0084   0.7490   0.5032
  -2.500  -0.2509   0.01551   0.00810  -0.0076   0.7376   0.5135
  -2.250  -0.2256   0.01539   0.00804  -0.0068   0.7249   0.5232
  -2.000  -0.2020   0.01535   0.00789  -0.0058   0.7133   0.5340
  -1.750  -0.1754   0.01523   0.00785  -0.0053   0.7009   0.5436
  -1.500  -0.1516   0.01521   0.00775  -0.0043   0.6893   0.5548
  -1.250  -0.1253   0.01510   0.00771  -0.0038   0.6771   0.5646
  -1.000  -0.1010   0.01510   0.00765  -0.0029   0.6657   0.5760
  -0.750  -0.0751   0.01503   0.00761  -0.0023   0.6538   0.5861
  -0.500  -0.0505   0.01504   0.00759  -0.0014   0.6425   0.5977
  -0.250  -0.0250   0.01499   0.00757  -0.0008   0.6308   0.6082
   0.000   0.0000   0.01502   0.00757   0.0000   0.6198   0.6198
   0.250   0.0251   0.01499   0.00757   0.0008   0.6082   0.6308
   0.500   0.0505   0.01504   0.00759   0.0014   0.5977   0.6425
   0.750   0.0751   0.01503   0.00761   0.0023   0.5861   0.6538
   1.000   0.1011   0.01510   0.00765   0.0029   0.5760   0.6657
   1.250   0.1253   0.01510   0.00771   0.0038   0.5646   0.6771
   1.500   0.1517   0.01521   0.00775   0.0043   0.5548   0.6893
   1.750   0.1755   0.01523   0.00785   0.0053   0.5436   0.7009
   2.000   0.2020   0.01535   0.00789   0.0058   0.5340   0.7133
   2.250   0.2257   0.01539   0.00804   0.0068   0.5231   0.7249
   2.500   0.2509   0.01551   0.00810   0.0075   0.5135   0.7376
   2.750   0.2758   0.01561   0.00827   0.0083   0.5032   0.7490
   3.000   0.2996   0.01572   0.00836   0.0093   0.4935   0.7621
   3.250   0.3259   0.01589   0.00856   0.0099   0.4838   0.7731
   3.500   0.3481   0.01600   0.00868   0.0112   0.4739   0.7864
   3.750   0.3760   0.01624   0.00890   0.0115   0.4647   0.7969
   4.000   0.3966   0.01635   0.00906   0.0131   0.4549   0.8105
   4.250   0.4259   0.01665   0.00928   0.0131   0.4459   0.8200
   4.500   0.4452   0.01679   0.00950   0.0149   0.4366   0.8337
   4.750   0.4732   0.01708   0.00977   0.0152   0.4274   0.8425
   5.000   0.4949   0.01732   0.01002   0.0166   0.4187   0.8552
   5.250   0.5212   0.01761   0.01033   0.0172   0.4093   0.8639
   5.500   0.5469   0.01797   0.01062   0.0179   0.4008   0.8745
   5.750   0.5700   0.01823   0.01094   0.0190   0.3916   0.8842
   6.250   0.6201   0.01892   0.01160   0.0204   0.3743   0.9036
   6.500   0.6548   0.01940   0.01199   0.0191   0.3651   0.9092
   6.750   0.6723   0.01969   0.01230   0.0211   0.3573   0.9220
   7.000   0.7111   0.02017   0.01276   0.0190   0.3476   0.9258
   7.250   0.7499   0.02072   0.01327   0.0167   0.3384   0.9305
   7.500   0.7701   0.02103   0.01359   0.0180   0.3304   0.9420
   7.750   0.8161   0.02162   0.01408   0.0141   0.3212   0.9444
   8.000   0.8552   0.02210   0.01460   0.0115   0.3117   0.9489
   8.250   0.8881   0.02262   0.01499   0.0101   0.3038   0.9563
   8.500   0.9202   0.02304   0.01550   0.0087   0.2952   0.9626
   8.750   0.9595   0.02357   0.01589   0.0059   0.2870   0.9670
   9.000   0.9833   0.02401   0.01642   0.0060   0.2797   0.9762
   9.250   1.0202   0.02444   0.01680   0.0035   0.2717   0.9802
   9.500   1.0524   0.02495   0.01732   0.0018   0.2642   0.9862
   9.750   1.0813   0.02539   0.01778   0.0006   0.2569   0.9923
  10.000   1.1157   0.02595   0.01826  -0.0017   0.2498   0.9967
  10.250   1.1295   0.02638   0.01876  -0.0004   0.2438   1.0000
  10.500   1.1190   0.02664   0.01902   0.0053   0.2402   1.0000
  10.750   1.1174   0.02701   0.01928   0.0096   0.2362   1.0000
  11.000   1.1066   0.02740   0.01973   0.0153   0.2326   1.0000
  11.250   1.0972   0.02781   0.02020   0.0206   0.2287   1.0000
  11.500   1.0919   0.02826   0.02064   0.0253   0.2248   1.0000
  11.750   1.0956   0.02876   0.02102   0.0285   0.2208   1.0000
  12.000   1.0919   0.02942   0.02174   0.0327   0.2169   1.0000
  12.250   1.0892   0.03013   0.02250   0.0364   0.2127   1.0000
  12.500   1.0914   0.03084   0.02319   0.0393   0.2087   1.0000
  12.750   1.1034   0.03151   0.02372   0.0411   0.2045   1.0000
  13.000   1.1001   0.03257   0.02492   0.0442   0.2007   1.0000
  13.250   1.1030   0.03358   0.02596   0.0464   0.1965   1.0000
  13.500   1.1117   0.03447   0.02679   0.0480   0.1927   1.0000
  13.750   1.1204   0.03554   0.02784   0.0494   0.1888   1.0000
  14.000   1.1216   0.03695   0.02936   0.0511   0.1850   1.0000
  14.250   1.1281   0.03816   0.03058   0.0523   0.1812   1.0000
  14.500   1.1437   0.03898   0.03127   0.0530   0.1775   1.0000
  14.750   1.1436   0.04076   0.03318   0.0542   0.1742   1.0000
  15.000   1.1458   0.04246   0.03497   0.0551   0.1707   1.0000
  15.250   1.1536   0.04382   0.03632   0.0558   0.1674   1.0000
  15.500   1.1710   0.04464   0.03700   0.0563   0.1640   1.0000
  15.750   1.1652   0.04713   0.03969   0.0570   0.1611   1.0000
  16.000   1.1668   0.04917   0.04181   0.0574   0.1579   1.0000
  16.250   1.1747   0.05071   0.04333   0.0577   0.1549   1.0000
  16.500   1.1924   0.05151   0.04400   0.0580   0.1519   1.0000
  16.750   1.1827   0.05471   0.04741   0.0581   0.1493   1.0000
  17.000   1.1814   0.05728   0.05008   0.0580   0.1465   1.0000
  17.250   1.1878   0.05912   0.05192   0.0580   0.1438   1.0000
  17.500   1.2089   0.05954   0.05218   0.0584   0.1410   1.0000
  17.750   1.1958   0.06344   0.05630   0.0578   0.1388   1.0000
  18.000   1.1876   0.06700   0.06001   0.0571   0.1363   1.0000
  18.250   1.1896   0.06949   0.06254   0.0567   0.1338   1.0000
  18.500   1.2036   0.07060   0.06358   0.0566   0.1315   1.0000
  18.750   1.2081   0.07283   0.06583   0.0564   0.1292   1.0000
  19.000   1.1868   0.07821   0.07145   0.0547   0.1271   1.0000
  19.250   1.1767   0.08238   0.07575   0.0534   0.1249   1.0000
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