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N-24 (n24-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: N-24 (n24-il)
Reynolds number: 500,000
Max Cl/Cd: 91.55 at α=2.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-n24-il-500000.txt
Download as CSV file: xf-n24-il-500000.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 =     0.500 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -15.500  -0.7146   0.06364   0.06053  -0.0697   0.9129   0.0345
 -15.250  -0.7700   0.04838   0.04488  -0.0878   0.9041   0.0343
 -15.000  -0.7966   0.04282   0.03902  -0.0919   0.8967   0.0342
 -14.750  -0.8116   0.03975   0.03572  -0.0907   0.8887   0.0342
 -14.500  -0.8150   0.03719   0.03290  -0.0893   0.8829   0.0342
 -14.250  -0.8102   0.03500   0.03046  -0.0881   0.8775   0.0343
 -14.000  -0.8001   0.03308   0.02831  -0.0870   0.8714   0.0344
 -13.750  -0.7876   0.03146   0.02647  -0.0856   0.8663   0.0345
 -13.500  -0.7725   0.03008   0.02486  -0.0843   0.8616   0.0347
 -13.250  -0.7540   0.02866   0.02326  -0.0835   0.8556   0.0348
 -13.000  -0.7374   0.02675   0.02117  -0.0824   0.8500   0.0350
 -12.750  -0.7190   0.02527   0.01955  -0.0811   0.8451   0.0353
 -12.500  -0.6963   0.02408   0.01832  -0.0805   0.8395   0.0356
 -12.250  -0.6731   0.02313   0.01730  -0.0798   0.8338   0.0360
 -12.000  -0.6500   0.02229   0.01636  -0.0789   0.8287   0.0363
 -11.750  -0.6258   0.02146   0.01544  -0.0781   0.8234   0.0366
 -11.500  -0.6005   0.02067   0.01456  -0.0776   0.8171   0.0369
 -11.250  -0.5755   0.01994   0.01372  -0.0768   0.8113   0.0372
 -11.000  -0.5503   0.01927   0.01294  -0.0761   0.8057   0.0375
 -10.750  -0.5234   0.01861   0.01221  -0.0758   0.7994   0.0379
 -10.500  -0.4970   0.01800   0.01151  -0.0752   0.7934   0.0382
 -10.250  -0.4708   0.01747   0.01086  -0.0746   0.7878   0.0386
 -10.000  -0.4428   0.01694   0.01027  -0.0743   0.7813   0.0389
  -9.750  -0.4153   0.01644   0.00970  -0.0739   0.7749   0.0392
  -9.500  -0.3895   0.01577   0.00896  -0.0733   0.7689   0.0398
  -9.250  -0.3615   0.01521   0.00840  -0.0732   0.7617   0.0405
  -9.000  -0.3336   0.01477   0.00791  -0.0728   0.7547   0.0412
  -8.750  -0.3055   0.01441   0.00748  -0.0726   0.7483   0.0421
  -8.500  -0.2764   0.01405   0.00709  -0.0725   0.7409   0.0430
  -8.250  -0.2478   0.01374   0.00669  -0.0723   0.7339   0.0438
  -8.000  -0.2189   0.01336   0.00629  -0.0722   0.7268   0.0451
  -7.750  -0.1898   0.01305   0.00596  -0.0721   0.7189   0.0467
  -7.500  -0.1607   0.01281   0.00565  -0.0720   0.7117   0.0487
  -7.250  -0.1310   0.01255   0.00543  -0.0721   0.7032   0.0523
  -7.000  -0.1015   0.01240   0.00526  -0.0720   0.6954   0.0589
  -6.750  -0.0711   0.01232   0.00518  -0.0722   0.6867   0.0682
  -6.500  -0.0410   0.01229   0.00508  -0.0722   0.6778   0.0757
  -6.250  -0.0112   0.01213   0.00494  -0.0724   0.6686   0.0819
  -6.000   0.0185   0.01203   0.00476  -0.0725   0.6594   0.0868
  -5.750   0.0484   0.01191   0.00462  -0.0727   0.6504   0.0915
  -5.500   0.0783   0.01185   0.00448  -0.0729   0.6414   0.0948
  -5.250   0.1079   0.01168   0.00431  -0.0731   0.6330   0.0986
  -5.000   0.1378   0.01159   0.00419  -0.0733   0.6246   0.1022
  -4.750   0.1676   0.01155   0.00408  -0.0735   0.6175   0.1048
  -4.500   0.1975   0.01142   0.00396  -0.0737   0.6100   0.1085
  -4.250   0.2272   0.01136   0.00387  -0.0740   0.6034   0.1128
  -4.000   0.2572   0.01130   0.00380  -0.0742   0.5973   0.1180
  -3.750   0.2871   0.01121   0.00375  -0.0745   0.5907   0.1258
  -3.500   0.3166   0.01116   0.00369  -0.0748   0.5843   0.1371
  -3.250   0.3465   0.01106   0.00366  -0.0751   0.5783   0.1552
  -3.000   0.3762   0.01098   0.00362  -0.0754   0.5721   0.1769
  -2.750   0.4055   0.01092   0.00360  -0.0757   0.5664   0.2009
  -2.500   0.4351   0.01084   0.00361  -0.0761   0.5610   0.2271
  -2.250   0.4647   0.01075   0.00362  -0.0765   0.5553   0.2573
  -2.000   0.4939   0.01070   0.00362  -0.0768   0.5493   0.2924
  -1.750   0.5229   0.01062   0.00365  -0.0771   0.5436   0.3363
  -1.500   0.5520   0.01046   0.00369  -0.0775   0.5377   0.3959
  -1.250   0.5801   0.01028   0.00374  -0.0777   0.5318   0.4787
  -1.000   0.6064   0.01000   0.00383  -0.0775   0.5263   0.6109
  -0.750   0.6632   0.00918   0.00400  -0.0834   0.5195   0.9802
  -0.500   0.7095   0.00938   0.00411  -0.0875   0.5124   1.0002
  -0.250   0.7374   0.00951   0.00416  -0.0876   0.5061   1.0002
   0.000   0.7654   0.00959   0.00420  -0.0878   0.4990   1.0002
   0.250   0.7928   0.00974   0.00426  -0.0878   0.4919   1.0002
   0.500   0.8208   0.00984   0.00433  -0.0880   0.4849   1.0002
   0.750   0.8483   0.00997   0.00440  -0.0881   0.4770   1.0002
   1.000   0.8757   0.01012   0.00449  -0.0882   0.4693   1.0002
   1.250   0.9030   0.01025   0.00458  -0.0883   0.4600   1.0002
   1.500   0.9299   0.01043   0.00469  -0.0884   0.4504   1.0002
   1.750   0.9565   0.01061   0.00481  -0.0884   0.4391   1.0002
   2.000   0.9830   0.01080   0.00494  -0.0885   0.4275   1.0002
   2.250   1.0087   0.01104   0.00511  -0.0884   0.4157   1.0002
   2.500   1.0339   0.01131   0.00529  -0.0883   0.4032   1.0002
   2.750   1.0592   0.01157   0.00549  -0.0882   0.3917   1.0002
   3.000   1.0835   0.01189   0.00573  -0.0880   0.3812   1.0002
   3.250   1.1074   0.01221   0.00597  -0.0877   0.3711   1.0002
   3.500   1.1313   0.01253   0.00624  -0.0874   0.3624   1.0002
   3.750   1.1544   0.01287   0.00652  -0.0870   0.3543   1.0002
   4.000   1.1772   0.01321   0.00681  -0.0866   0.3478   1.0002
   4.250   1.2007   0.01350   0.00709  -0.0863   0.3419   1.0002
   4.500   1.2221   0.01389   0.00742  -0.0857   0.3360   1.0002
   4.750   1.2436   0.01425   0.00776  -0.0851   0.3309   1.0002
   5.000   1.2661   0.01454   0.00806  -0.0847   0.3266   1.0002
   5.250   1.2866   0.01490   0.00841  -0.0839   0.3220   1.0002
   5.500   1.3041   0.01539   0.00885  -0.0828   0.3171   1.0002
   5.750   1.3220   0.01576   0.00924  -0.0816   0.3133   1.0002
   6.000   1.3398   0.01612   0.00964  -0.0805   0.3097   1.0002
   6.250   1.3567   0.01657   0.01009  -0.0793   0.3060   1.0002
   6.500   1.3727   0.01710   0.01059  -0.0780   0.3023   1.0002
   6.750   1.3885   0.01771   0.01117  -0.0768   0.2983   1.0002
   7.000   1.4082   0.01810   0.01163  -0.0762   0.2956   1.0002
   7.250   1.4271   0.01855   0.01213  -0.0756   0.2925   1.0002
   7.500   1.4449   0.01909   0.01268  -0.0748   0.2892   1.0002
   7.750   1.4613   0.01971   0.01330  -0.0740   0.2858   1.0002
   8.000   1.4764   0.02045   0.01401  -0.0730   0.2821   1.0002
   8.250   1.4949   0.02098   0.01461  -0.0725   0.2795   1.0002
   8.500   1.5128   0.02156   0.01525  -0.0720   0.2765   1.0002
   8.750   1.5298   0.02221   0.01593  -0.0714   0.2731   1.0002
   9.000   1.5448   0.02298   0.01673  -0.0707   0.2697   1.0002
   9.250   1.5581   0.02389   0.01761  -0.0698   0.2660   1.0002
   9.500   1.5743   0.02463   0.01842  -0.0693   0.2631   1.0002
   9.750   1.5907   0.02538   0.01925  -0.0689   0.2596   1.0002
  10.000   1.6046   0.02629   0.02020  -0.0684   0.2555   1.0002
  10.250   1.6152   0.02745   0.02134  -0.0675   0.2511   1.0002
  10.500   1.6282   0.02848   0.02243  -0.0670   0.2467   1.0002
  10.750   1.6416   0.02952   0.02353  -0.0666   0.2416   1.0002
  11.000   1.6505   0.03089   0.02491  -0.0659   0.2363   1.0002
  11.250   1.6603   0.03224   0.02630  -0.0653   0.2312   1.0002
  11.500   1.6711   0.03356   0.02767  -0.0649   0.2253   1.0002
  11.750   1.6761   0.03537   0.02947  -0.0641   0.2195   1.0002
  12.000   1.6859   0.03686   0.03102  -0.0638   0.2137   1.0002
  12.250   1.6909   0.03880   0.03299  -0.0632   0.2070   1.0002
  12.500   1.6957   0.04080   0.03501  -0.0628   0.2006   1.0002
  12.750   1.6984   0.04304   0.03727  -0.0623   0.1932   1.0002
  13.000   1.6993   0.04552   0.03976  -0.0618   0.1861   1.0002
  13.250   1.6980   0.04828   0.04254  -0.0613   0.1785   1.0002
  13.500   1.6972   0.05103   0.04530  -0.0610   0.1718   1.0002
  13.750   1.6940   0.05407   0.04836  -0.0606   0.1654   1.0002
  14.000   1.6912   0.05712   0.05143  -0.0604   0.1600   1.0002
  14.250   1.6891   0.06015   0.05451  -0.0602   0.1548   1.0002
  14.500   1.6816   0.06383   0.05820  -0.0601   0.1502   1.0002
  14.750   1.6810   0.06675   0.06119  -0.0601   0.1465   1.0002
  15.000   1.6785   0.06992   0.06441  -0.0602   0.1427   1.0002
  15.250   1.6716   0.07368   0.06820  -0.0603   0.1393   1.0002
  15.500   1.6657   0.07734   0.07190  -0.0605   0.1363   1.0002
  15.750   1.6662   0.08023   0.07488  -0.0608   0.1336   1.0002
  16.000   1.6616   0.08381   0.07851  -0.0611   0.1307   1.0002
  16.250   1.6547   0.08770   0.08244  -0.0616   0.1279   1.0002
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