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N-24 (n24-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: N-24 (n24-il)
Reynolds number: 1,000,000
Max Cl/Cd: 104.14 at α=4.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-n24-il-1000000-n5.txt
Download as CSV file: xf-n24-il-1000000-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 =     1.000 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -18.500  -0.8981   0.08896   0.08597  -0.0422   0.8930   0.0221
 -18.250  -0.9321   0.08021   0.07710  -0.0483   0.8886   0.0221
 -18.000  -0.9758   0.07015   0.06688  -0.0555   0.8837   0.0221
 -17.750  -1.0266   0.05878   0.05532  -0.0641   0.8783   0.0220
 -17.500  -1.0738   0.04598   0.04226  -0.0758   0.8709   0.0220
 -17.250  -1.0995   0.03552   0.03144  -0.0890   0.8621   0.0220
 -17.000  -1.1061   0.03280   0.02857  -0.0886   0.8540   0.0220
 -16.750  -1.1061   0.03106   0.02670  -0.0867   0.8454   0.0221
 -16.500  -1.0964   0.02959   0.02512  -0.0855   0.8371   0.0222
 -16.250  -1.0832   0.02833   0.02374  -0.0844   0.8281   0.0223
 -16.000  -1.0673   0.02721   0.02252  -0.0833   0.8210   0.0223
 -15.750  -1.0494   0.02619   0.02142  -0.0823   0.8150   0.0224
 -15.500  -1.0301   0.02527   0.02040  -0.0813   0.8091   0.0225
 -15.250  -1.0097   0.02440   0.01944  -0.0804   0.8036   0.0226
 -15.000  -0.9882   0.02359   0.01855  -0.0796   0.7982   0.0227
 -14.750  -0.9658   0.02283   0.01771  -0.0788   0.7924   0.0228
 -14.500  -0.9429   0.02212   0.01691  -0.0780   0.7872   0.0230
 -14.250  -0.9192   0.02144   0.01616  -0.0773   0.7824   0.0231
 -14.000  -0.8949   0.02079   0.01544  -0.0766   0.7768   0.0232
 -13.750  -0.8702   0.02018   0.01475  -0.0760   0.7707   0.0233
 -13.500  -0.8449   0.01961   0.01410  -0.0753   0.7653   0.0235
 -13.250  -0.8191   0.01907   0.01350  -0.0748   0.7600   0.0236
 -13.000  -0.7930   0.01856   0.01292  -0.0743   0.7543   0.0238
 -12.750  -0.7665   0.01808   0.01236  -0.0738   0.7488   0.0240
 -12.500  -0.7398   0.01759   0.01181  -0.0733   0.7437   0.0241
 -12.250  -0.7129   0.01712   0.01128  -0.0729   0.7374   0.0243
 -12.000  -0.6856   0.01669   0.01077  -0.0725   0.7307   0.0244
 -11.750  -0.6581   0.01627   0.01028  -0.0721   0.7246   0.0245
 -11.500  -0.6303   0.01588   0.00983  -0.0718   0.7177   0.0246
 -11.250  -0.6023   0.01551   0.00939  -0.0715   0.7112   0.0247
 -11.000  -0.5740   0.01515   0.00898  -0.0712   0.7052   0.0248
 -10.750  -0.5456   0.01482   0.00859  -0.0710   0.6982   0.0249
 -10.500  -0.5169   0.01452   0.00822  -0.0708   0.6913   0.0250
 -10.250  -0.4890   0.01405   0.00770  -0.0706   0.6846   0.0253
 -10.000  -0.4605   0.01367   0.00726  -0.0704   0.6765   0.0255
  -9.750  -0.4316   0.01334   0.00687  -0.0703   0.6689   0.0257
  -9.500  -0.4025   0.01304   0.00653  -0.0702   0.6603   0.0259
  -9.250  -0.3732   0.01279   0.00621  -0.0701   0.6526   0.0262
  -9.000  -0.3438   0.01254   0.00592  -0.0701   0.6449   0.0264
  -8.750  -0.3143   0.01232   0.00565  -0.0701   0.6369   0.0267
  -8.500  -0.2846   0.01210   0.00539  -0.0701   0.6297   0.0269
  -8.250  -0.2549   0.01191   0.00515  -0.0701   0.6216   0.0272
  -8.000  -0.2250   0.01173   0.00492  -0.0702   0.6137   0.0275
  -7.750  -0.1951   0.01157   0.00471  -0.0703   0.6033   0.0278
  -7.500  -0.1651   0.01143   0.00451  -0.0704   0.5931   0.0282
  -7.250  -0.1351   0.01131   0.00433  -0.0706   0.5828   0.0285
  -7.000  -0.1050   0.01118   0.00416  -0.0707   0.5749   0.0288
  -6.750  -0.0751   0.01101   0.00395  -0.0709   0.5663   0.0294
  -6.500  -0.0450   0.01088   0.00378  -0.0711   0.5585   0.0299
  -6.250  -0.0149   0.01076   0.00363  -0.0712   0.5504   0.0305
  -6.000   0.0152   0.01068   0.00349  -0.0715   0.5422   0.0312
  -5.750   0.0454   0.01057   0.00337  -0.0717   0.5360   0.0319
  -5.500   0.0756   0.01050   0.00326  -0.0719   0.5288   0.0327
  -5.250   0.1057   0.01041   0.00314  -0.0722   0.5228   0.0345
  -5.000   0.1358   0.01028   0.00302  -0.0724   0.5181   0.0381
  -4.750   0.1656   0.01009   0.00294  -0.0727   0.5133   0.0623
  -4.500   0.1958   0.01006   0.00291  -0.0730   0.5085   0.0670
  -4.250   0.2262   0.01006   0.00288  -0.0734   0.5040   0.0698
  -4.000   0.2565   0.01000   0.00284  -0.0737   0.4997   0.0723
  -3.750   0.2867   0.00997   0.00280  -0.0740   0.4941   0.0746
  -3.500   0.3170   0.00999   0.00278  -0.0744   0.4884   0.0762
  -3.250   0.3472   0.00997   0.00275  -0.0748   0.4842   0.0774
  -3.000   0.3774   0.00992   0.00271  -0.0752   0.4797   0.0796
  -2.750   0.4076   0.00990   0.00269  -0.0756   0.4744   0.0813
  -2.500   0.4376   0.00992   0.00268  -0.0760   0.4687   0.0829
  -2.250   0.4678   0.00991   0.00267  -0.0764   0.4635   0.0846
  -2.000   0.4978   0.00991   0.00266  -0.0768   0.4562   0.0877
  -1.750   0.5276   0.00993   0.00267  -0.0773   0.4489   0.0923
  -1.500   0.5573   0.00988   0.00268  -0.0777   0.4420   0.1100
  -1.250   0.5867   0.00986   0.00272  -0.0781   0.4335   0.1419
  -1.000   0.6164   0.00986   0.00275  -0.0786   0.4253   0.1586
  -0.750   0.6457   0.00993   0.00281  -0.0790   0.4146   0.1734
  -0.500   0.6750   0.00998   0.00287  -0.0795   0.4025   0.1918
  -0.250   0.7039   0.01007   0.00296  -0.0799   0.3884   0.2127
   0.000   0.7324   0.01018   0.00307  -0.0803   0.3736   0.2396
   0.250   0.7607   0.01029   0.00319  -0.0807   0.3606   0.2705
   0.500   0.7891   0.01037   0.00332  -0.0811   0.3501   0.3054
   0.750   0.8173   0.01044   0.00345  -0.0815   0.3419   0.3449
   1.000   0.8454   0.01047   0.00358  -0.0818   0.3344   0.3968
   1.250   0.8728   0.01048   0.00374  -0.0821   0.3275   0.4704
   1.500   0.8995   0.01033   0.00391  -0.0823   0.3213   0.5983
   1.750   0.9255   0.01032   0.00410  -0.0823   0.3139   0.6935
   2.250   1.0097   0.01014   0.00456  -0.0892   0.3030   0.9994
   2.500   1.0384   0.01034   0.00472  -0.0898   0.2991   1.0002
   2.750   1.0644   0.01055   0.00489  -0.0897   0.2946   1.0002
   3.000   1.0906   0.01072   0.00504  -0.0898   0.2908   1.0002
   3.250   1.1166   0.01090   0.00520  -0.0898   0.2863   1.0002
   3.500   1.1420   0.01111   0.00538  -0.0897   0.2821   1.0002
   3.750   1.1670   0.01134   0.00557  -0.0896   0.2784   1.0002
   4.000   1.1922   0.01154   0.00577  -0.0896   0.2754   1.0002
   4.250   1.2176   0.01172   0.00594  -0.0895   0.2728   1.0002
   4.500   1.2424   0.01193   0.00614  -0.0894   0.2689   1.0002
   4.750   1.2664   0.01217   0.00636  -0.0892   0.2651   1.0002
   5.000   1.2895   0.01245   0.00662  -0.0889   0.2612   1.0002
   5.250   1.3128   0.01270   0.00686  -0.0886   0.2578   1.0002
   5.500   1.3361   0.01292   0.00709  -0.0883   0.2550   1.0002
   5.750   1.3587   0.01318   0.00735  -0.0880   0.2522   1.0002
   6.000   1.3799   0.01348   0.00765  -0.0874   0.2491   1.0002
   6.250   1.3976   0.01386   0.00802  -0.0863   0.2459   1.0002
   6.500   1.4131   0.01427   0.00843  -0.0847   0.2427   1.0002
   6.750   1.4321   0.01461   0.00880  -0.0839   0.2407   1.0002
   7.000   1.4512   0.01499   0.00919  -0.0831   0.2380   1.0002
   7.250   1.4698   0.01541   0.00962  -0.0823   0.2347   1.0002
   7.500   1.4875   0.01591   0.01012  -0.0815   0.2309   1.0002
   7.750   1.5044   0.01648   0.01068  -0.0806   0.2268   1.0002
   8.000   1.5235   0.01695   0.01117  -0.0801   0.2237   1.0002
   8.250   1.5413   0.01750   0.01173  -0.0794   0.2194   1.0002
   8.500   1.5564   0.01824   0.01244  -0.0785   0.2137   1.0002
   8.750   1.5724   0.01894   0.01314  -0.0778   0.2080   1.0002
   9.000   1.5852   0.01985   0.01402  -0.0768   0.1994   1.0002
   9.250   1.5975   0.02083   0.01497  -0.0758   0.1907   1.0002
   9.500   1.6072   0.02201   0.01611  -0.0746   0.1813   1.0002
   9.750   1.6154   0.02333   0.01738  -0.0734   0.1708   1.0002
  10.000   1.6230   0.02472   0.01874  -0.0722   0.1608   1.0002
  10.250   1.6294   0.02625   0.02024  -0.0710   0.1519   1.0002
  10.750   1.6420   0.02943   0.02339  -0.0689   0.1372   1.0002
  11.000   1.6466   0.03121   0.02516  -0.0678   0.1309   1.0002
  11.250   1.6536   0.03288   0.02684  -0.0671   0.1261   1.0002
  11.500   1.6586   0.03474   0.02871  -0.0663   0.1216   1.0002
  11.750   1.6655   0.03648   0.03048  -0.0658   0.1182   1.0002
  12.000   1.6723   0.03831   0.03234  -0.0653   0.1151   1.0002
  12.250   1.6767   0.04038   0.03443  -0.0648   0.1117   1.0002
  12.500   1.6800   0.04259   0.03666  -0.0643   0.1083   1.0002
  12.750   1.6862   0.04456   0.03868  -0.0640   0.1062   1.0002
  13.000   1.6911   0.04670   0.04086  -0.0637   0.1039   1.0002
  13.250   1.6946   0.04901   0.04321  -0.0635   0.1014   1.0002
  13.500   1.6960   0.05159   0.04582  -0.0632   0.0989   1.0002
  13.750   1.6974   0.05419   0.04847  -0.0631   0.0967   1.0002
  14.000   1.7024   0.05642   0.05076  -0.0631   0.0952   1.0002
  14.250   1.7047   0.05898   0.05338  -0.0631   0.0932   1.0002
  14.500   1.7043   0.06189   0.05633  -0.0630   0.0906   1.0002
  14.750   1.7013   0.06510   0.05957  -0.0630   0.0878   1.0002
  15.000   1.7006   0.06807   0.06260  -0.0631   0.0853   1.0002
  15.250   1.6961   0.07153   0.06610  -0.0632   0.0811   1.0002
  15.500   1.6869   0.07560   0.07019  -0.0633   0.0760   1.0002
  15.750   1.6734   0.08024   0.07484  -0.0635   0.0693   1.0002
  16.000   1.6576   0.08523   0.07985  -0.0637   0.0631   1.0002
  16.250   1.6421   0.09031   0.08497  -0.0642   0.0581   1.0002
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