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NACA 23024 (naca23024-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: NACA 23024 (naca23024-il)
Reynolds number: 500,000
Max Cl/Cd: 43.4 at α=8.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-naca23024-il-500000-n5.txt
Download as CSV file: xf-naca23024-il-500000-n5.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 =     0.500 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -19.750  -1.0452   0.08245   0.07690  -0.0641   1.0000   0.0685
 -19.500  -1.0470   0.07955   0.07394  -0.0645   1.0000   0.0697
 -19.250  -1.0496   0.07658   0.07092  -0.0648   1.0000   0.0706
 -19.000  -1.0552   0.07330   0.06760  -0.0652   1.0000   0.0720
 -18.750  -1.0597   0.07019   0.06446  -0.0654   1.0000   0.0735
 -18.500  -1.0621   0.06741   0.06162  -0.0655   1.0000   0.0747
 -18.250  -1.0635   0.06476   0.05892  -0.0654   1.0000   0.0762
 -18.000  -1.0660   0.06204   0.05615  -0.0653   1.0000   0.0774
 -17.750  -1.0699   0.05924   0.05331  -0.0651   1.0000   0.0789
 -17.500  -1.0726   0.05661   0.05064  -0.0648   1.0000   0.0805
 -17.250  -1.0735   0.05424   0.04823  -0.0643   1.0000   0.0824
 -17.000  -1.0739   0.05198   0.04592  -0.0637   1.0000   0.0841
 -16.750  -1.0769   0.04951   0.04342  -0.0630   1.0000   0.0858
 -16.500  -1.0780   0.04731   0.04119  -0.0622   1.0000   0.0880
 -16.250  -1.0774   0.04534   0.03917  -0.0612   1.0000   0.0901
 -16.000  -1.0780   0.04332   0.03712  -0.0601   1.0000   0.0920
 -15.750  -1.0788   0.04139   0.03517  -0.0588   1.0000   0.0939
 -15.500  -1.0790   0.03958   0.03334  -0.0573   1.0000   0.0966
 -15.250  -1.0777   0.03799   0.03170  -0.0558   1.0000   0.0988
 -15.000  -1.0761   0.03619   0.02990  -0.0546   0.9997   0.1019
 -14.750  -1.0587   0.03455   0.02823  -0.0558   0.9984   0.1054
 -14.500  -1.0415   0.03292   0.02659  -0.0570   0.9965   0.1093
 -14.250  -1.0238   0.03141   0.02508  -0.0580   0.9943   0.1140
 -14.000  -1.0050   0.02999   0.02365  -0.0591   0.9919   0.1185
 -13.750  -0.9891   0.02860   0.02226  -0.0594   0.9894   0.1239
 -13.500  -0.9721   0.02729   0.02096  -0.0597   0.9864   0.1286
 -13.250  -0.9532   0.02610   0.01977  -0.0602   0.9833   0.1342
 -13.000  -0.9331   0.02495   0.01863  -0.0609   0.9806   0.1402
 -12.750  -0.9097   0.02396   0.01764  -0.0619   0.9784   0.1465
 -12.500  -0.8983   0.02291   0.01661  -0.0604   0.9718   0.1515
 -12.250  -0.8784   0.02200   0.01571  -0.0605   0.9670   0.1584
 -12.000  -0.8621   0.02105   0.01479  -0.0598   0.9611   0.1657
 -11.750  -0.8463   0.02029   0.01403  -0.0587   0.9528   0.1721
 -11.500  -0.8271   0.01946   0.01322  -0.0584   0.9472   0.1798
 -11.250  -0.8095   0.01882   0.01258  -0.0573   0.9381   0.1853
 -11.000  -0.7852   0.01803   0.01183  -0.0577   0.9329   0.1941
 -10.750  -0.7591   0.01738   0.01118  -0.0582   0.9259   0.2017
 -10.500  -0.7266   0.01673   0.01056  -0.0599   0.9195   0.2105
 -10.250  -0.6886   0.01606   0.00990  -0.0628   0.9136   0.2196
  -9.750  -0.6099   0.01501   0.00886  -0.0687   0.8948   0.2370
  -9.500  -0.5708   0.01464   0.00845  -0.0714   0.8828   0.2449
  -9.250  -0.5317   0.01422   0.00802  -0.0743   0.8696   0.2536
  -9.000  -0.4970   0.01396   0.00771  -0.0761   0.8545   0.2609
  -8.750  -0.4614   0.01360   0.00733  -0.0782   0.8395   0.2696
  -8.500  -0.4315   0.01339   0.00705  -0.0789   0.8218   0.2768
  -8.250  -0.4088   0.01313   0.00676  -0.0783   0.8034   0.2838
  -8.000  -0.3864   0.01295   0.00651  -0.0775   0.7851   0.2907
  -7.750  -0.3650   0.01281   0.00629  -0.0763   0.7681   0.2970
  -7.500  -0.3486   0.01260   0.00605  -0.0743   0.7515   0.3036
  -7.250  -0.3308   0.01246   0.00586  -0.0724   0.7353   0.3106
  -7.000  -0.3133   0.01236   0.00567  -0.0704   0.7187   0.3165
  -6.750  -0.2991   0.01221   0.00549  -0.0678   0.7031   0.3228
  -6.500  -0.2822   0.01209   0.00534  -0.0657   0.6897   0.3293
  -6.250  -0.2658   0.01203   0.00520  -0.0634   0.6757   0.3352
  -6.000  -0.2517   0.01188   0.00505  -0.0607   0.6626   0.3418
  -5.750  -0.2367   0.01181   0.00492  -0.0581   0.6500   0.3480
  -5.000  -0.1906   0.01156   0.00460  -0.0503   0.6150   0.3676
  -4.750  -0.1751   0.01154   0.00452  -0.0477   0.6028   0.3739
  -4.500  -0.1605   0.01144   0.00443  -0.0450   0.5925   0.3803
  -4.250  -0.1467   0.01139   0.00435  -0.0420   0.5815   0.3873
  -4.000  -0.1309   0.01136   0.00429  -0.0394   0.5707   0.3940
  -3.750  -0.1184   0.01131   0.00422  -0.0362   0.5596   0.4006
  -3.500  -0.1049   0.01127   0.00416  -0.0332   0.5502   0.4077
  -3.250  -0.0897   0.01125   0.00412  -0.0304   0.5390   0.4148
  -3.000  -0.0787   0.01123   0.00407  -0.0268   0.5286   0.4220
  -2.750  -0.0661   0.01119   0.00403  -0.0236   0.5182   0.4296
  -2.250  -0.0426   0.01118   0.00398  -0.0166   0.4985   0.4441
  -2.000  -0.0339   0.01118   0.00397  -0.0125   0.4880   0.4517
  -1.750  -0.0237   0.01119   0.00396  -0.0087   0.4798   0.4587
  -1.500  -0.0155   0.01117   0.00395  -0.0044   0.4721   0.4658
  -1.250  -0.0121   0.01119   0.00394   0.0008   0.4625   0.4742
  -1.000  -0.0008   0.01119   0.00395   0.0044   0.4558   0.4821
  -0.750   0.0067   0.01118   0.00395   0.0088   0.4480   0.4896
  -0.500   0.0148   0.01121   0.00396   0.0130   0.4404   0.4982
   0.000   0.0394   0.01123   0.00400   0.0197   0.4241   0.5156
   0.250   0.0512   0.01127   0.00403   0.0231   0.4170   0.5247
   0.500   0.0662   0.01128   0.00406   0.0259   0.4097   0.5332
   0.750   0.0783   0.01132   0.00411   0.0292   0.4015   0.5431
   1.250   0.1066   0.01139   0.00421   0.0350   0.3872   0.5628
   1.500   0.1203   0.01146   0.00427   0.0379   0.3798   0.5734
   1.750   0.1341   0.01151   0.00434   0.0408   0.3731   0.5837
   2.000   0.1493   0.01156   0.00441   0.0434   0.3650   0.5954
   2.250   0.1628   0.01165   0.00451   0.0463   0.3576   0.6059
   2.500   0.1776   0.01171   0.00460   0.0490   0.3515   0.6184
   2.750   0.1931   0.01179   0.00469   0.0515   0.3434   0.6291
   3.000   0.2063   0.01190   0.00482   0.0544   0.3363   0.6417
   3.250   0.2231   0.01197   0.00493   0.0566   0.3301   0.6535
   3.500   0.2379   0.01207   0.00506   0.0591   0.3232   0.6675
   3.750   0.2520   0.01221   0.00522   0.0617   0.3166   0.6802
   4.000   0.2687   0.01230   0.00535   0.0638   0.3096   0.6954
   4.250   0.2841   0.01243   0.00553   0.0661   0.3025   0.7092
   4.750   0.3180   0.01271   0.00590   0.0701   0.2907   0.7400
   5.000   0.3350   0.01288   0.00612   0.0719   0.2834   0.7567
   5.250   0.3530   0.01308   0.00635   0.0735   0.2779   0.7735
   5.500   0.3745   0.01324   0.00658   0.0744   0.2714   0.7919
   5.750   0.3974   0.01347   0.00687   0.0749   0.2648   0.8103
   6.000   0.4238   0.01371   0.00716   0.0747   0.2585   0.8270
   6.250   0.4524   0.01396   0.00745   0.0740   0.2524   0.8437
   6.500   0.4907   0.01432   0.00783   0.0711   0.2458   0.8596
   6.750   0.5283   0.01459   0.00815   0.0685   0.2405   0.8730
   7.000   0.5659   0.01495   0.00854   0.0658   0.2347   0.8869
   7.250   0.6074   0.01544   0.00903   0.0622   0.2286   0.8978
   7.500   0.6482   0.01586   0.00948   0.0588   0.2231   0.9071
   7.750   0.6871   0.01640   0.01002   0.0558   0.2183   0.9150
   8.000   0.7244   0.01702   0.01063   0.0529   0.2131   0.9207
   8.250   0.7577   0.01753   0.01116   0.0510   0.2092   0.9270
   8.500   0.7860   0.01811   0.01174   0.0500   0.2050   0.9335
   8.750   0.8115   0.01878   0.01241   0.0493   0.2014   0.9389
   9.250   0.8540   0.01995   0.01360   0.0498   0.1945   0.9532
   9.500   0.8700   0.02062   0.01428   0.0509   0.1913   0.9617
   9.750   0.8902   0.02139   0.01504   0.0508   0.1877   0.9668
  10.000   0.9129   0.02212   0.01577   0.0504   0.1850   0.9714
  10.500   0.9549   0.02360   0.01729   0.0502   0.1787   0.9801
  10.750   0.9782   0.02452   0.01820   0.0491   0.1751   0.9827
  11.000   1.0007   0.02542   0.01911   0.0482   0.1724   0.9855
  11.250   1.0238   0.02625   0.01998   0.0474   0.1696   0.9884
  11.500   1.0436   0.02727   0.02101   0.0469   0.1664   0.9912
  11.750   1.0650   0.02836   0.02210   0.0458   0.1631   0.9934
  12.000   1.0864   0.02947   0.02322   0.0445   0.1604   0.9956
  12.250   1.1105   0.03042   0.02421   0.0431   0.1581   0.9976
  12.500   1.1323   0.03162   0.02543   0.0417   0.1545   0.9992
  12.750   1.1467   0.03290   0.02673   0.0414   0.1519   1.0000
  13.000   1.1480   0.03429   0.02812   0.0433   0.1496   1.0000
  13.250   1.1545   0.03538   0.02926   0.0447   0.1478   1.0000
  13.500   1.1593   0.03667   0.03059   0.0461   0.1457   1.0000
  13.750   1.1637   0.03806   0.03200   0.0474   0.1435   1.0000
  14.000   1.1654   0.03972   0.03368   0.0487   0.1411   1.0000
  14.250   1.1665   0.04149   0.03546   0.0498   0.1390   1.0000
  14.500   1.1723   0.04293   0.03696   0.0507   0.1370   1.0000
  14.750   1.1760   0.04459   0.03866   0.0515   0.1349   1.0000
  15.000   1.1781   0.04644   0.04054   0.0523   0.1324   1.0000
  15.250   1.1785   0.04850   0.04263   0.0530   0.1307   1.0000
  15.500   1.1793   0.05057   0.04472   0.0536   0.1286   1.0000
  15.750   1.1826   0.05247   0.04668   0.0540   0.1267   1.0000
  16.000   1.1848   0.05450   0.04875   0.0544   0.1245   1.0000
  16.250   1.1836   0.05693   0.05121   0.0547   0.1222   1.0000
  16.500   1.1810   0.05953   0.05384   0.0548   0.1204   1.0000
  16.750   1.1821   0.06182   0.05618   0.0550   0.1184   1.0000
  17.000   1.1825   0.06421   0.05863   0.0550   0.1163   1.0000
  17.250   1.1815   0.06677   0.06123   0.0549   0.1146   1.0000
  17.500   1.1774   0.06973   0.06423   0.0547   0.1125   1.0000
  17.750   1.1738   0.07266   0.06719   0.0544   0.1109   1.0000
  18.000   1.1734   0.07531   0.06991   0.0541   0.1090   1.0000
  18.250   1.1726   0.07800   0.07265   0.0538   0.1072   1.0000
  18.500   1.1669   0.08131   0.07600   0.0532   0.1051   1.0000
  18.750   1.1626   0.08448   0.07920   0.0526   0.1035   1.0000
  19.000   1.1580   0.08774   0.08252   0.0519   0.1019   1.0000
  19.250   1.1571   0.09055   0.08539   0.0513   0.1002   1.0000
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