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N-24 (n24-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: N-24 (n24-il)
Reynolds number: 1,000,000
Max Cl/Cd: 108.68 at α=4°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-n24-il-1000000.txt
Download as CSV file: xf-n24-il-1000000.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 =     1.000 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -17.500  -0.8116   0.08480   0.08226  -0.0461   0.9139   0.0263
 -17.250  -0.8836   0.06865   0.06584  -0.0594   0.9104   0.0261
 -17.000  -0.9263   0.05716   0.05412  -0.0697   0.9046   0.0260
 -16.750  -0.9527   0.04779   0.04451  -0.0793   0.8984   0.0260
 -16.500  -0.9675   0.04067   0.03716  -0.0881   0.8906   0.0260
 -16.250  -0.9779   0.03709   0.03338  -0.0898   0.8829   0.0261
 -16.000  -0.9849   0.03496   0.03109  -0.0880   0.8759   0.0261
 -15.750  -0.9812   0.03322   0.02920  -0.0865   0.8693   0.0262
 -15.500  -0.9724   0.03170   0.02752  -0.0851   0.8634   0.0263
 -15.250  -0.9590   0.03034   0.02604  -0.0840   0.8578   0.0264
 -15.000  -0.9434   0.02914   0.02471  -0.0829   0.8520   0.0265
 -14.750  -0.9262   0.02809   0.02352  -0.0818   0.8465   0.0266
 -14.500  -0.9068   0.02715   0.02246  -0.0809   0.8412   0.0267
 -14.250  -0.8859   0.02631   0.02151  -0.0800   0.8355   0.0268
 -14.000  -0.8697   0.02463   0.01967  -0.0788   0.8297   0.0269
 -13.750  -0.8516   0.02313   0.01805  -0.0778   0.8244   0.0272
 -13.500  -0.8300   0.02202   0.01689  -0.0769   0.8194   0.0274
 -13.250  -0.8072   0.02114   0.01595  -0.0762   0.8139   0.0276
 -13.000  -0.7835   0.02039   0.01512  -0.0754   0.8085   0.0278
 -12.750  -0.7586   0.01970   0.01438  -0.0748   0.8035   0.0280
 -12.500  -0.7331   0.01906   0.01369  -0.0742   0.7978   0.0282
 -12.250  -0.7074   0.01849   0.01305  -0.0736   0.7920   0.0285
 -12.000  -0.6811   0.01796   0.01244  -0.0731   0.7866   0.0288
 -11.750  -0.6544   0.01740   0.01183  -0.0727   0.7813   0.0290
 -11.500  -0.6276   0.01687   0.01124  -0.0722   0.7756   0.0292
 -11.250  -0.6007   0.01639   0.01067  -0.0718   0.7698   0.0295
 -11.000  -0.5731   0.01590   0.01014  -0.0714   0.7646   0.0297
 -10.750  -0.5453   0.01545   0.00963  -0.0711   0.7586   0.0299
 -10.500  -0.5175   0.01504   0.00914  -0.0708   0.7522   0.0301
 -10.250  -0.4891   0.01465   0.00870  -0.0705   0.7463   0.0303
 -10.000  -0.4606   0.01429   0.00829  -0.0703   0.7395   0.0305
  -9.750  -0.4319   0.01399   0.00792  -0.0701   0.7329   0.0306
  -9.500  -0.4044   0.01336   0.00724  -0.0698   0.7268   0.0310
  -9.250  -0.3762   0.01289   0.00672  -0.0696   0.7199   0.0315
  -9.000  -0.3474   0.01254   0.00630  -0.0695   0.7127   0.0319
  -8.750  -0.3181   0.01221   0.00595  -0.0694   0.7060   0.0323
  -8.500  -0.2887   0.01194   0.00563  -0.0694   0.6983   0.0328
  -8.250  -0.2591   0.01170   0.00533  -0.0694   0.6908   0.0333
  -8.000  -0.2294   0.01146   0.00506  -0.0694   0.6824   0.0339
  -7.750  -0.1996   0.01128   0.00481  -0.0695   0.6737   0.0344
  -7.500  -0.1696   0.01108   0.00456  -0.0696   0.6642   0.0348
  -7.250  -0.1399   0.01083   0.00426  -0.0696   0.6547   0.0358
  -7.000  -0.1100   0.01062   0.00401  -0.0697   0.6451   0.0368
  -6.750  -0.0799   0.01046   0.00380  -0.0699   0.6354   0.0379
  -6.500  -0.0498   0.01032   0.00362  -0.0701   0.6254   0.0392
  -6.250  -0.0198   0.01014   0.00342  -0.0702   0.6166   0.0429
  -6.000   0.0100   0.00994   0.00333  -0.0704   0.6071   0.0622
  -5.750   0.0405   0.00992   0.00329  -0.0707   0.5979   0.0702
  -5.500   0.0711   0.00991   0.00326  -0.0710   0.5893   0.0749
  -5.250   0.1014   0.00988   0.00319  -0.0713   0.5820   0.0780
  -5.000   0.1318   0.00980   0.00312  -0.0716   0.5759   0.0815
  -4.750   0.1622   0.00979   0.00307  -0.0719   0.5690   0.0837
  -4.500   0.1925   0.00977   0.00301  -0.0722   0.5624   0.0854
  -4.250   0.2227   0.00967   0.00291  -0.0725   0.5565   0.0882
  -4.000   0.2530   0.00962   0.00284  -0.0729   0.5505   0.0906
  -3.750   0.2832   0.00961   0.00280  -0.0732   0.5448   0.0929
  -3.500   0.3136   0.00956   0.00275  -0.0736   0.5402   0.0947
  -3.250   0.3438   0.00950   0.00269  -0.0740   0.5349   0.0988
  -3.000   0.3739   0.00948   0.00267  -0.0744   0.5290   0.1040
  -2.750   0.4039   0.00939   0.00265  -0.0747   0.5242   0.1191
  -2.500   0.4339   0.00929   0.00264  -0.0752   0.5191   0.1481
  -2.250   0.4638   0.00924   0.00264  -0.0756   0.5138   0.1683
  -2.000   0.4937   0.00924   0.00266  -0.0760   0.5084   0.1865
  -1.750   0.5237   0.00916   0.00267  -0.0765   0.5042   0.2105
  -1.500   0.5535   0.00908   0.00269  -0.0769   0.4990   0.2438
  -1.250   0.5831   0.00905   0.00272  -0.0774   0.4930   0.2784
  -1.000   0.6127   0.00897   0.00276  -0.0778   0.4877   0.3220
  -0.500   0.6711   0.00876   0.00286  -0.0787   0.4752   0.4483
  -0.250   0.6996   0.00858   0.00293  -0.0790   0.4693   0.5425
   0.000   0.7269   0.00831   0.00302  -0.0791   0.4626   0.6749
   0.250   0.7766   0.00778   0.00322  -0.0839   0.4535   0.9865
   0.500   0.8261   0.00796   0.00335  -0.0888   0.4433   1.0002
   0.750   0.8540   0.00811   0.00342  -0.0890   0.4331   1.0002
   1.000   0.8817   0.00828   0.00350  -0.0892   0.4208   1.0002
   1.250   0.9094   0.00844   0.00360  -0.0894   0.4083   1.0002
   1.500   0.9366   0.00865   0.00372  -0.0896   0.3946   1.0002
   1.750   0.9634   0.00889   0.00387  -0.0897   0.3807   1.0002
   2.000   0.9897   0.00917   0.00404  -0.0897   0.3667   1.0002
   2.250   1.0161   0.00941   0.00421  -0.0898   0.3545   1.0002
   2.500   1.0423   0.00966   0.00439  -0.0899   0.3443   1.0002
   2.750   1.0680   0.00993   0.00458  -0.0899   0.3354   1.0002
   3.000   1.0943   0.01013   0.00476  -0.0899   0.3295   1.0002
   3.250   1.1203   0.01034   0.00493  -0.0900   0.3243   1.0002
   3.500   1.1454   0.01061   0.00515  -0.0899   0.3183   1.0002
   3.750   1.1710   0.01082   0.00534  -0.0898   0.3135   1.0002
   4.000   1.1966   0.01101   0.00552  -0.0899   0.3093   1.0002
   4.250   1.2214   0.01125   0.00573  -0.0898   0.3052   1.0002
   4.500   1.2451   0.01155   0.00599  -0.0895   0.3002   1.0002
   4.750   1.2700   0.01175   0.00620  -0.0894   0.2966   1.0002
   5.000   1.2948   0.01195   0.00639  -0.0894   0.2928   1.0002
   5.250   1.3185   0.01220   0.00664  -0.0891   0.2890   1.0002
   5.500   1.3408   0.01251   0.00692  -0.0887   0.2852   1.0002
   5.750   1.3620   0.01285   0.00724  -0.0881   0.2814   1.0002
   6.000   1.3858   0.01304   0.00747  -0.0879   0.2795   1.0002
   6.250   1.4082   0.01329   0.00774  -0.0876   0.2769   1.0002
   6.500   1.4281   0.01361   0.00806  -0.0868   0.2740   1.0002
   6.750   1.4437   0.01401   0.00846  -0.0853   0.2710   1.0002
   7.000   1.4591   0.01448   0.00893  -0.0839   0.2675   1.0002
   7.250   1.4765   0.01493   0.00939  -0.0829   0.2646   1.0002
   7.500   1.4975   0.01525   0.00974  -0.0824   0.2625   1.0002
   7.750   1.5173   0.01564   0.01016  -0.0819   0.2597   1.0002
   8.000   1.5361   0.01610   0.01063  -0.0813   0.2566   1.0002
   8.250   1.5531   0.01666   0.01119  -0.0805   0.2532   1.0002
   8.500   1.5684   0.01735   0.01187  -0.0795   0.2490   1.0002
   8.750   1.5893   0.01774   0.01230  -0.0793   0.2461   1.0002
   9.000   1.6080   0.01827   0.01285  -0.0789   0.2420   1.0002
   9.250   1.6234   0.01900   0.01358  -0.0781   0.2373   1.0002
   9.500   1.6389   0.01975   0.01432  -0.0775   0.2321   1.0002
   9.750   1.6560   0.02041   0.01500  -0.0770   0.2266   1.0002
  10.000   1.6688   0.02137   0.01594  -0.0762   0.2205   1.0002
  10.250   1.6838   0.02221   0.01680  -0.0756   0.2158   1.0002
  10.500   1.6979   0.02311   0.01772  -0.0750   0.2102   1.0002
  10.750   1.7074   0.02436   0.01894  -0.0740   0.2034   1.0002
  11.000   1.7195   0.02545   0.02004  -0.0734   0.1964   1.0002
  11.250   1.7262   0.02696   0.02153  -0.0723   0.1881   1.0002
  11.500   1.7331   0.02849   0.02303  -0.0713   0.1792   1.0002
  11.750   1.7379   0.03021   0.02474  -0.0703   0.1710   1.0002
  12.000   1.7392   0.03229   0.02679  -0.0691   0.1623   1.0002
  12.250   1.7433   0.03420   0.02870  -0.0683   0.1545   1.0002
  12.500   1.7440   0.03645   0.03094  -0.0673   0.1472   1.0002
  12.750   1.7462   0.03865   0.03315  -0.0666   0.1411   1.0002
  13.000   1.7467   0.04107   0.03557  -0.0659   0.1358   1.0002
  13.250   1.7500   0.04327   0.03781  -0.0654   0.1319   1.0002
  13.500   1.7502   0.04581   0.04036  -0.0649   0.1280   1.0002
  13.750   1.7508   0.04836   0.04295  -0.0645   0.1244   1.0002
  14.000   1.7546   0.05066   0.04530  -0.0643   0.1221   1.0002
  14.250   1.7557   0.05323   0.04793  -0.0641   0.1196   1.0002
  14.500   1.7547   0.05607   0.05080  -0.0639   0.1170   1.0002
  14.750   1.7515   0.05919   0.05396  -0.0637   0.1141   1.0002
  15.000   1.7529   0.06186   0.05670  -0.0637   0.1123   1.0002
  15.250   1.7542   0.06454   0.05944  -0.0638   0.1103   1.0002
  15.500   1.7525   0.06758   0.06253  -0.0638   0.1081   1.0002
  15.750   1.7473   0.07107   0.06607  -0.0639   0.1060   1.0002
  16.000   1.7401   0.07485   0.06990  -0.0640   0.1034   1.0002
  16.250   1.7404   0.07776   0.07287  -0.0643   0.1017   1.0002
  16.500   1.7385   0.08093   0.07612  -0.0647   0.0998   1.0002
  16.750   1.7351   0.08430   0.07954  -0.0650   0.0975   1.0002
  17.000   1.7261   0.08844   0.08373  -0.0655   0.0951   1.0002
  17.250   1.7158   0.09282   0.08817  -0.0660   0.0926   1.0002
  17.500   1.7155   0.09586   0.09128  -0.0666   0.0904   1.0002
  17.750   1.7074   0.09999   0.09547  -0.0673   0.0873   1.0002
  18.000   1.6943   0.10483   0.10035  -0.0681   0.0841   1.0002
  18.250   1.6881   0.10878   0.10435  -0.0690   0.0805   1.0002
  18.500   1.6718   0.11420   0.10979  -0.0702   0.0754   1.0002
  18.750   1.6562   0.11955   0.11518  -0.0715   0.0702   1.0002
  19.000   1.6371   0.12551   0.12117  -0.0730   0.0650   1.0002
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