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N-24 (n24-il) Xfoil prediction polar at RE=200,000 Ncrit=9


Details Polar file
Airfoil: N-24 (n24-il)
Reynolds number: 200,000
Max Cl/Cd: 65.65 at α=4°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-n24-il-200000.txt
Download as CSV file: xf-n24-il-200000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: N-24                                            
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -11.750  -0.3397   0.06194   0.05819  -0.0915   0.8925   0.0613
 -11.500  -0.3341   0.06083   0.05710  -0.0898   0.8847   0.0616
 -11.250  -0.3642   0.05247   0.04844  -0.0943   0.8764   0.0600
 -11.000  -0.3983   0.04301   0.03832  -0.0967   0.8677   0.0585
 -10.750  -0.4083   0.03732   0.03196  -0.0952   0.8623   0.0581
 -10.500  -0.3975   0.03382   0.02798  -0.0948   0.8537   0.0583
 -10.250  -0.3843   0.03147   0.02525  -0.0930   0.8478   0.0589
 -10.000  -0.3672   0.02957   0.02296  -0.0915   0.8418   0.0598
  -9.750  -0.3467   0.02784   0.02081  -0.0906   0.8339   0.0608
  -9.500  -0.3262   0.02645   0.01921  -0.0890   0.8285   0.0617
  -9.250  -0.3018   0.02557   0.01829  -0.0882   0.8219   0.0626
  -9.000  -0.2767   0.02473   0.01736  -0.0875   0.8145   0.0638
  -8.750  -0.2534   0.02383   0.01630  -0.0861   0.8091   0.0653
  -8.500  -0.2273   0.02297   0.01522  -0.0856   0.8016   0.0671
  -8.250  -0.2017   0.02206   0.01418  -0.0848   0.7942   0.0690
  -8.000  -0.1772   0.02142   0.01352  -0.0836   0.7889   0.0712
  -7.750  -0.1489   0.02090   0.01288  -0.0834   0.7800   0.0750
  -7.500  -0.1231   0.02016   0.01215  -0.0827   0.7734   0.0790
  -7.250  -0.0968   0.01953   0.01138  -0.0820   0.7675   0.0855
  -7.000  -0.0690   0.01894   0.01081  -0.0818   0.7589   0.0948
  -6.750  -0.0426   0.01850   0.01034  -0.0811   0.7527   0.1047
  -6.500  -0.0146   0.01824   0.01014  -0.0810   0.7449   0.1130
  -6.250   0.0136   0.01800   0.00984  -0.0808   0.7375   0.1199
  -6.000   0.0413   0.01789   0.00964  -0.0803   0.7320   0.1265
  -5.750   0.0705   0.01770   0.00944  -0.0805   0.7235   0.1324
  -5.500   0.0986   0.01754   0.00923  -0.0802   0.7163   0.1385
  -5.250   0.1274   0.01741   0.00898  -0.0800   0.7086   0.1438
  -5.000   0.1555   0.01699   0.00860  -0.0798   0.6998   0.1489
  -4.750   0.1836   0.01679   0.00831  -0.0795   0.6926   0.1554
  -4.500   0.2125   0.01653   0.00806  -0.0796   0.6836   0.1626
  -4.250   0.2408   0.01633   0.00783  -0.0794   0.6773   0.1716
  -4.000   0.2695   0.01609   0.00764  -0.0795   0.6702   0.1824
  -3.750   0.2981   0.01583   0.00741  -0.0795   0.6632   0.1977
  -3.500   0.3262   0.01554   0.00716  -0.0793   0.6576   0.2203
  -3.250   0.3548   0.01536   0.00710  -0.0795   0.6502   0.2492
  -3.000   0.3831   0.01513   0.00698  -0.0795   0.6434   0.2806
  -2.750   0.4111   0.01495   0.00686  -0.0794   0.6380   0.3195
  -2.500   0.4391   0.01476   0.00692  -0.0796   0.6307   0.3736
  -2.250   0.4659   0.01444   0.00688  -0.0794   0.6243   0.4546
  -2.000   0.4902   0.01398   0.00687  -0.0785   0.6188   0.5921
  -1.750   0.5715   0.01318   0.00701  -0.0888   0.6092   1.0002
  -1.500   0.5987   0.01327   0.00690  -0.0886   0.6031   1.0002
  -1.250   0.6260   0.01342   0.00696  -0.0886   0.5963   1.0002
  -1.000   0.6533   0.01354   0.00697  -0.0885   0.5891   1.0002
  -0.750   0.6806   0.01367   0.00690  -0.0883   0.5829   1.0002
  -0.500   0.7076   0.01381   0.00703  -0.0883   0.5747   1.0002
  -0.250   0.7348   0.01392   0.00701  -0.0882   0.5673   1.0002
   0.000   0.7619   0.01410   0.00710  -0.0882   0.5598   1.0002
   0.250   0.7889   0.01424   0.00718  -0.0881   0.5517   1.0002
   0.500   0.8162   0.01442   0.00720  -0.0881   0.5447   1.0002
   0.750   0.8426   0.01458   0.00737  -0.0880   0.5355   1.0002
   1.000   0.8698   0.01475   0.00737  -0.0880   0.5278   1.0002
   1.250   0.8957   0.01493   0.00757  -0.0879   0.5177   1.0002
   1.500   0.9226   0.01512   0.00760  -0.0878   0.5094   1.0002
   1.750   0.9481   0.01533   0.00783  -0.0877   0.4990   1.0002
   2.000   0.9748   0.01555   0.00789  -0.0876   0.4906   1.0002
   2.250   0.9995   0.01578   0.00815  -0.0874   0.4798   1.0002
   2.500   1.0255   0.01603   0.00828  -0.0873   0.4710   1.0002
   2.750   1.0498   0.01628   0.00853  -0.0871   0.4603   1.0002
   3.000   1.0749   0.01657   0.00872  -0.0869   0.4516   1.0002
   3.250   1.0990   0.01685   0.00899  -0.0867   0.4420   1.0002
   3.500   1.1239   0.01718   0.00922  -0.0865   0.4343   1.0002
   3.750   1.1474   0.01750   0.00955  -0.0862   0.4257   1.0002
   4.000   1.1725   0.01786   0.00976  -0.0861   0.4189   1.0002
   4.250   1.1948   0.01822   0.01018  -0.0856   0.4109   1.0002
   4.500   1.2186   0.01857   0.01046  -0.0854   0.4044   1.0002
   4.750   1.2423   0.01900   0.01086  -0.0852   0.3984   1.0002
   5.000   1.2642   0.01938   0.01126  -0.0847   0.3917   1.0002
   5.250   1.2882   0.01979   0.01155  -0.0846   0.3857   1.0002
   5.500   1.3088   0.02023   0.01204  -0.0839   0.3793   1.0002
   5.750   1.3293   0.02064   0.01245  -0.0833   0.3730   1.0002
   6.000   1.3541   0.02112   0.01277  -0.0833   0.3671   1.0002
   6.250   1.3704   0.02158   0.01336  -0.0821   0.3610   1.0002
   6.500   1.3896   0.02204   0.01382  -0.0813   0.3554   1.0002
   6.750   1.4152   0.02256   0.01420  -0.0816   0.3505   1.0002
   7.000   1.4320   0.02311   0.01487  -0.0805   0.3462   1.0002
   7.250   1.4492   0.02365   0.01547  -0.0795   0.3417   1.0002
   7.500   1.4685   0.02417   0.01599  -0.0788   0.3374   1.0002
   7.750   1.4974   0.02473   0.01642  -0.0797   0.3330   1.0002
   8.000   1.5061   0.02538   0.01723  -0.0774   0.3291   1.0002
   8.250   1.5172   0.02603   0.01796  -0.0756   0.3248   1.0002
   8.500   1.5329   0.02663   0.01857  -0.0745   0.3204   1.0002
   8.750   1.5633   0.02716   0.01898  -0.0757   0.3157   1.0002
   9.000   1.5653   0.02803   0.02003  -0.0727   0.3120   1.0002
   9.250   1.5742   0.02886   0.02096  -0.0710   0.3076   1.0002
   9.500   1.5886   0.02956   0.02169  -0.0700   0.3034   1.0002
   9.750   1.6161   0.03008   0.02210  -0.0707   0.2989   1.0002
  10.000   1.6170   0.03123   0.02343  -0.0682   0.2951   1.0002
  10.250   1.6222   0.03231   0.02464  -0.0663   0.2906   1.0002
  10.500   1.6338   0.03318   0.02554  -0.0653   0.2862   1.0002
  10.750   1.6593   0.03368   0.02593  -0.0658   0.2816   1.0002
  11.000   1.6525   0.03536   0.02785  -0.0630   0.2774   1.0002
  11.250   1.6552   0.03675   0.02935  -0.0614   0.2726   1.0002
  11.500   1.6656   0.03775   0.03034  -0.0606   0.2680   1.0002
  11.750   1.6738   0.03902   0.03166  -0.0596   0.2631   1.0002
  12.000   1.6679   0.04110   0.03392  -0.0578   0.2579   1.0002
  12.250   1.6720   0.04259   0.03544  -0.0568   0.2528   1.0002
  12.500   1.6810   0.04388   0.03670  -0.0561   0.2477   1.0002
  12.750   1.6706   0.04663   0.03965  -0.0547   0.2421   1.0002
  13.000   1.6719   0.04853   0.04158  -0.0539   0.2367   1.0002
  13.250   1.6729   0.05062   0.04370  -0.0532   0.2310   1.0002
  13.500   1.6638   0.05380   0.04703  -0.0526   0.2249   1.0002
  13.750   1.6694   0.05554   0.04868  -0.0523   0.2192   1.0002
  14.000   1.6579   0.05931   0.05263  -0.0519   0.2133   1.0002
  14.250   1.6538   0.06235   0.05573  -0.0519   0.2076   1.0002
  14.500   1.6567   0.06462   0.05796  -0.0518   0.2024   1.0002
  14.750   1.6466   0.06863   0.06214  -0.0519   0.1971   1.0002
  15.000   1.6462   0.07141   0.06493  -0.0521   0.1923   1.0002
  15.250   1.6481   0.07393   0.06745  -0.0522   0.1879   1.0002
  15.500   1.6385   0.07811   0.07178  -0.0527   0.1834   1.0002
  15.750   1.6367   0.08124   0.07495  -0.0531   0.1794   1.0002
  16.000   1.6480   0.08245   0.07606  -0.0531   0.1755   1.0002
  16.250   1.6344   0.08732   0.08115  -0.0538   0.1721   1.0002
  16.500   1.6277   0.09125   0.08519  -0.0545   0.1685   1.0002
  16.750   1.6296   0.09393   0.08789  -0.0551   0.1652   1.0002
  17.000   1.6397   0.09533   0.08922  -0.0553   0.1618   1.0002
  17.250   1.6232   0.10082   0.09494  -0.0566   0.1588   1.0002
  17.500   1.6139   0.10527   0.09950  -0.0577   0.1555   1.0002
  17.750   1.6153   0.10809   0.10235  -0.0586   0.1522   1.0002
  18.000   1.6280   0.10906   0.10323  -0.0589   0.1489   1.0002
  18.250   1.6074   0.11541   0.10982  -0.0609   0.1463   1.0002
  18.500   1.5955   0.12048   0.11504  -0.0626   0.1434   1.0002
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