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N-24 (n24-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: N-24 (n24-il)
Reynolds number: 200,000
Max Cl/Cd: 64.59 at α=3°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-n24-il-200000-n5.txt
Download as CSV file: xf-n24-il-200000-n5.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 =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -14.250  -0.6802   0.04492   0.03981  -0.0948   0.8847   0.0356
 -14.000  -0.6961   0.04150   0.03609  -0.0945   0.8763   0.0357
 -13.750  -0.6977   0.03880   0.03310  -0.0939   0.8687   0.0359
 -13.500  -0.6944   0.03663   0.03065  -0.0925   0.8632   0.0361
 -13.250  -0.6829   0.03466   0.02844  -0.0919   0.8563   0.0363
 -13.000  -0.6698   0.03298   0.02652  -0.0908   0.8499   0.0365
 -12.750  -0.6556   0.03152   0.02482  -0.0894   0.8448   0.0367
 -12.500  -0.6371   0.03019   0.02328  -0.0886   0.8386   0.0369
 -12.250  -0.6176   0.02897   0.02197  -0.0877   0.8321   0.0372
 -12.000  -0.5983   0.02791   0.02082  -0.0865   0.8266   0.0375
 -11.750  -0.5771   0.02694   0.01976  -0.0856   0.8211   0.0378
 -11.500  -0.5541   0.02602   0.01875  -0.0850   0.8146   0.0381
 -11.250  -0.5319   0.02515   0.01777  -0.0841   0.8087   0.0385
 -11.000  -0.5093   0.02434   0.01683  -0.0831   0.8033   0.0389
 -10.750  -0.4843   0.02355   0.01596  -0.0827   0.7960   0.0394
 -10.500  -0.4602   0.02283   0.01511  -0.0819   0.7898   0.0399
 -10.250  -0.4358   0.02215   0.01429  -0.0811   0.7844   0.0406
 -10.000  -0.4093   0.02151   0.01355  -0.0808   0.7773   0.0413
  -9.750  -0.3840   0.02087   0.01285  -0.0802   0.7710   0.0420
  -9.500  -0.3584   0.02032   0.01222  -0.0796   0.7652   0.0428
  -9.250  -0.3311   0.01980   0.01165  -0.0794   0.7574   0.0436
  -9.000  -0.3047   0.01931   0.01106  -0.0789   0.7508   0.0445
  -8.750  -0.2774   0.01885   0.01052  -0.0785   0.7440   0.0456
  -8.500  -0.2496   0.01843   0.01006  -0.0783   0.7367   0.0468
  -8.250  -0.2224   0.01806   0.00963  -0.0779   0.7305   0.0484
  -8.000  -0.1939   0.01772   0.00927  -0.0778   0.7233   0.0507
  -7.750  -0.1656   0.01743   0.00896  -0.0776   0.7159   0.0538
  -7.500  -0.1375   0.01718   0.00865  -0.0773   0.7094   0.0586
  -7.250  -0.1082   0.01698   0.00840  -0.0773   0.7011   0.0652
  -7.000  -0.0796   0.01679   0.00810  -0.0771   0.6941   0.0718
  -6.750  -0.0506   0.01661   0.00783  -0.0771   0.6872   0.0776
  -6.500  -0.0218   0.01639   0.00757  -0.0771   0.6799   0.0825
  -6.250   0.0066   0.01618   0.00728  -0.0769   0.6736   0.0868
  -6.000   0.0357   0.01599   0.00707  -0.0770   0.6660   0.0913
  -5.750   0.0645   0.01582   0.00683  -0.0770   0.6585   0.0953
  -5.500   0.0932   0.01564   0.00663  -0.0770   0.6513   0.0992
  -5.250   0.1222   0.01551   0.00644  -0.0770   0.6426   0.1034
  -5.000   0.1508   0.01537   0.00625  -0.0770   0.6344   0.1082
  -4.750   0.1799   0.01525   0.00611  -0.0771   0.6244   0.1131
  -4.500   0.2085   0.01514   0.00594  -0.0771   0.6161   0.1187
  -4.250   0.2377   0.01504   0.00584  -0.0772   0.6073   0.1259
  -4.000   0.2664   0.01495   0.00573  -0.0773   0.6003   0.1351
  -3.750   0.2954   0.01486   0.00566  -0.0775   0.5935   0.1467
  -3.500   0.3243   0.01478   0.00559  -0.0776   0.5866   0.1609
  -3.250   0.3530   0.01472   0.00550  -0.0777   0.5808   0.1759
  -3.000   0.3820   0.01466   0.00547  -0.0779   0.5745   0.1913
  -2.750   0.4108   0.01459   0.00544  -0.0781   0.5678   0.2084
  -2.500   0.4392   0.01456   0.00539  -0.0782   0.5617   0.2278
  -2.250   0.4679   0.01450   0.00541  -0.0784   0.5551   0.2513
  -2.000   0.4963   0.01444   0.00543  -0.0786   0.5489   0.2808
  -1.750   0.5243   0.01438   0.00544  -0.0787   0.5433   0.3209
  -1.500   0.5523   0.01428   0.00551  -0.0789   0.5370   0.3691
  -1.250   0.5797   0.01417   0.00557  -0.0789   0.5302   0.4265
  -1.000   0.6058   0.01399   0.00562  -0.0787   0.5240   0.5159
  -0.750   0.6304   0.01365   0.00575  -0.0781   0.5173   0.6526
  -0.250   0.7296   0.01338   0.00601  -0.0870   0.5023   1.0002
   0.250   0.7828   0.01372   0.00618  -0.0868   0.4877   1.0002
   0.500   0.8093   0.01389   0.00630  -0.0868   0.4797   1.0002
   0.750   0.8354   0.01408   0.00640  -0.0867   0.4714   1.0002
   1.000   0.8615   0.01428   0.00654  -0.0866   0.4635   1.0002
   1.250   0.8874   0.01448   0.00668  -0.0864   0.4549   1.0002
   1.500   0.9129   0.01470   0.00684  -0.0863   0.4466   1.0002
   1.750   0.9381   0.01493   0.00701  -0.0861   0.4371   1.0002
   2.000   0.9629   0.01518   0.00720  -0.0859   0.4278   1.0002
   2.250   0.9871   0.01545   0.00740  -0.0855   0.4176   1.0002
   2.500   1.0111   0.01573   0.00763  -0.0852   0.4078   1.0002
   2.750   1.0341   0.01606   0.00787  -0.0847   0.3987   1.0002
   3.000   1.0574   0.01637   0.00814  -0.0844   0.3900   1.0002
   3.250   1.0794   0.01673   0.00843  -0.0838   0.3821   1.0002
   3.500   1.1016   0.01709   0.00874  -0.0832   0.3745   1.0002
   3.750   1.1227   0.01748   0.00908  -0.0825   0.3671   1.0002
   4.000   1.1433   0.01789   0.00944  -0.0818   0.3608   1.0002
   4.250   1.1642   0.01828   0.00982  -0.0811   0.3547   1.0002
   4.500   1.1838   0.01873   0.01022  -0.0802   0.3495   1.0002
   4.750   1.2027   0.01919   0.01063  -0.0793   0.3447   1.0002
   5.000   1.2219   0.01962   0.01108  -0.0784   0.3393   1.0002
   5.250   1.2375   0.02012   0.01156  -0.0769   0.3338   1.0002
   5.500   1.2514   0.02071   0.01208  -0.0753   0.3289   1.0002
   5.750   1.2683   0.02121   0.01261  -0.0741   0.3241   1.0002
   6.000   1.2844   0.02176   0.01318  -0.0729   0.3192   1.0002
   6.250   1.2994   0.02239   0.01379  -0.0717   0.3145   1.0002
   6.500   1.3149   0.02306   0.01441  -0.0706   0.3102   1.0002
   6.750   1.3315   0.02365   0.01507  -0.0697   0.3056   1.0002
   7.000   1.3471   0.02431   0.01577  -0.0687   0.3011   1.0002
   7.250   1.3620   0.02504   0.01649  -0.0677   0.2970   1.0002
   7.500   1.3772   0.02580   0.01721  -0.0668   0.2935   1.0002
   7.750   1.3934   0.02649   0.01799  -0.0661   0.2900   1.0002
   8.000   1.4088   0.02725   0.01882  -0.0653   0.2861   1.0002
   8.250   1.4231   0.02808   0.01969  -0.0645   0.2823   1.0002
   8.500   1.4369   0.02895   0.02057  -0.0636   0.2789   1.0002
   8.750   1.4507   0.02986   0.02146  -0.0629   0.2758   1.0002
   9.000   1.4650   0.03076   0.02249  -0.0622   0.2723   1.0002
   9.250   1.4781   0.03173   0.02355  -0.0615   0.2686   1.0002
   9.500   1.4902   0.03279   0.02466  -0.0608   0.2649   1.0002
   9.750   1.5013   0.03393   0.02581  -0.0600   0.2615   1.0002
  10.000   1.5126   0.03507   0.02700  -0.0593   0.2582   1.0002
  10.250   1.5236   0.03630   0.02835  -0.0587   0.2543   1.0002
  10.500   1.5333   0.03762   0.02975  -0.0581   0.2502   1.0002
  10.750   1.5418   0.03905   0.03123  -0.0574   0.2463   1.0002
  11.000   1.5491   0.04056   0.03274  -0.0567   0.2427   1.0002
  11.250   1.5573   0.04214   0.03447  -0.0563   0.2382   1.0002
  11.500   1.5634   0.04392   0.03633  -0.0558   0.2335   1.0002
  11.750   1.5681   0.04583   0.03828  -0.0553   0.2290   1.0002
  12.000   1.5736   0.04776   0.04029  -0.0549   0.2247   1.0002
  12.250   1.5782   0.04986   0.04250  -0.0546   0.2197   1.0002
  12.500   1.5804   0.05219   0.04488  -0.0543   0.2149   1.0002
  12.750   1.5825   0.05460   0.04734  -0.0541   0.2101   1.0002
  13.000   1.5839   0.05720   0.05006  -0.0540   0.2043   1.0002
  13.250   1.5819   0.06016   0.05304  -0.0539   0.1987   1.0002
  13.500   1.5808   0.06314   0.05610  -0.0539   0.1928   1.0002
  13.750   1.5768   0.06649   0.05950  -0.0540   0.1866   1.0002
  14.000   1.5721   0.06998   0.06303  -0.0542   0.1807   1.0002
  14.250   1.5667   0.07364   0.06676  -0.0544   0.1743   1.0002
  14.500   1.5594   0.07753   0.07066  -0.0547   0.1687   1.0002
  14.750   1.5537   0.08134   0.07455  -0.0552   0.1630   1.0002
  15.000   1.5454   0.08550   0.07874  -0.0557   0.1580   1.0002
  15.250   1.5396   0.08938   0.08269  -0.0563   0.1535   1.0002
  15.500   1.5333   0.09336   0.08674  -0.0569   0.1490   1.0002
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