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FX 61-184 AIRFOIL (fx61184-il) Xfoil prediction polar at RE=100,000 Ncrit=5


Details Polar file
Airfoil: FX 61-184 AIRFOIL (fx61184-il)
Reynolds number: 100,000
Max Cl/Cd: 43.42 at α=8.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx61184-il-100000-n5.txt
Download as CSV file: xf-fx61184-il-100000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: FX 61-184 AIRFOIL                               
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.100 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -13.500  -0.4496   0.09525   0.09013  -0.0732   1.0000   0.0277
 -13.250  -0.4828   0.08569   0.08048  -0.0787   1.0000   0.0271
 -13.000  -0.5122   0.07851   0.07319  -0.0823   1.0000   0.0266
 -12.750  -0.5406   0.07272   0.06729  -0.0845   1.0000   0.0265
 -12.500  -0.5666   0.06829   0.06277  -0.0851   1.0000   0.0264
 -12.250  -0.5776   0.06255   0.05677  -0.0897   0.9739   0.0269
 -12.000  -0.5841   0.05745   0.05133  -0.0942   0.9539   0.0272
 -11.750  -0.5845   0.05272   0.04616  -0.0989   0.9396   0.0279
 -11.500  -0.5783   0.04837   0.04129  -0.1032   0.9281   0.0285
 -11.250  -0.5643   0.04482   0.03730  -0.1063   0.9172   0.0291
 -11.000  -0.5394   0.04233   0.03463  -0.1087   0.9091   0.0298
 -10.750  -0.5146   0.04032   0.03245  -0.1109   0.9011   0.0309
 -10.500  -0.4920   0.03857   0.03049  -0.1124   0.8930   0.0324
 -10.250  -0.4686   0.03684   0.02843  -0.1134   0.8854   0.0344
 -10.000  -0.4400   0.03529   0.02660  -0.1141   0.8792   0.0356
  -9.750  -0.4109   0.03409   0.02541  -0.1143   0.8731   0.0370
  -9.500  -0.3843   0.03307   0.02432  -0.1149   0.8676   0.0390
  -9.250  -0.3610   0.03224   0.02335  -0.1147   0.8616   0.0414
  -9.000  -0.3363   0.03146   0.02248  -0.1143   0.8559   0.0439
  -8.750  -0.3129   0.03063   0.02167  -0.1143   0.8510   0.0463
  -8.500  -0.2954   0.02994   0.02095  -0.1134   0.8450   0.0488
  -8.250  -0.2772   0.02929   0.02019  -0.1127   0.8394   0.0529
  -8.000  -0.2621   0.02839   0.01930  -0.1121   0.8346   0.0572
  -7.750  -0.2516   0.02771   0.01858  -0.1105   0.8287   0.0622
  -7.500  -0.2426   0.02691   0.01779  -0.1088   0.8230   0.0677
  -7.250  -0.2317   0.02618   0.01701  -0.1074   0.8185   0.0771
  -7.000  -0.2289   0.02548   0.01638  -0.1049   0.8126   0.0881
  -6.750  -0.2238   0.02456   0.01561  -0.1031   0.8072   0.1092
  -6.500  -0.2195   0.02323   0.01457  -0.1019   0.8027   0.1597
  -6.250  -0.2232   0.02166   0.01359  -0.1000   0.7968   0.2584
  -6.000  -0.2154   0.02090   0.01369  -0.0980   0.7918   0.3973
  -5.750  -0.1880   0.02209   0.01515  -0.0957   0.7885   0.4742
  -5.250  -0.1395   0.02309   0.01587  -0.0945   0.7802   0.5371
  -5.000  -0.1133   0.02460   0.01730  -0.0924   0.7760   0.5597
  -4.750  -0.0857   0.02575   0.01833  -0.0908   0.7725   0.5748
  -4.500  -0.0569   0.02614   0.01856  -0.0902   0.7697   0.5812
  -4.250  -0.0392   0.02598   0.01829  -0.0895   0.7644   0.5896
  -4.000  -0.0158   0.02623   0.01845  -0.0883   0.7600   0.5934
  -3.750   0.0099   0.02576   0.01776  -0.0894   0.7563   0.6033
  -3.500   0.0381   0.02588   0.01777  -0.0890   0.7535   0.6060
  -3.250   0.0565   0.02609   0.01795  -0.0873   0.7483   0.6094
  -3.000   0.0792   0.02600   0.01776  -0.0870   0.7437   0.6148
  -2.750   0.1069   0.02565   0.01726  -0.0880   0.7401   0.6211
  -2.500   0.1351   0.02565   0.01716  -0.0879   0.7374   0.6237
  -2.250   0.1531   0.02578   0.01727  -0.0865   0.7319   0.6273
  -2.000   0.1773   0.02562   0.01702  -0.0867   0.7272   0.6326
  -1.750   0.2063   0.02536   0.01664  -0.0877   0.7237   0.6373
  -1.500   0.2352   0.02530   0.01650  -0.0878   0.7210   0.6397
  -1.250   0.2516   0.02548   0.01670  -0.0862   0.7149   0.6428
  -1.000   0.2766   0.02540   0.01657  -0.0863   0.7103   0.6466
  -0.750   0.3103   0.02504   0.01606  -0.0886   0.7069   0.6521
  -0.500   0.3401   0.02493   0.01590  -0.0889   0.7043   0.6540
  -0.250   0.3531   0.02523   0.01626  -0.0868   0.6971   0.6564
   0.000   0.3793   0.02518   0.01619  -0.0867   0.6929   0.6590
   0.250   0.4106   0.02501   0.01595  -0.0877   0.6899   0.6621
   0.500   0.4352   0.02503   0.01595  -0.0881   0.6847   0.6661
   0.750   0.4593   0.02506   0.01597  -0.0883   0.6791   0.6691
   1.000   0.4870   0.02498   0.01589  -0.0884   0.6755   0.6710
   1.250   0.5186   0.02483   0.01570  -0.0890   0.6728   0.6733
   1.500   0.5321   0.02520   0.01615  -0.0873   0.6651   0.6760
   1.750   0.5608   0.02512   0.01607  -0.0879   0.6609   0.6787
   2.000   0.5959   0.02488   0.01579  -0.0896   0.6579   0.6817
   2.250   0.6151   0.02516   0.01611  -0.0891   0.6509   0.6848
   2.500   0.6390   0.02520   0.01620  -0.0886   0.6459   0.6867
   2.750   0.6705   0.02502   0.01603  -0.0893   0.6427   0.6887
   3.000   0.6886   0.02532   0.01640  -0.0883   0.6362   0.6909
   3.250   0.7132   0.02540   0.01652  -0.0882   0.6307   0.6934
   3.500   0.7473   0.02519   0.01632  -0.0895   0.6273   0.6964
   3.750   0.7685   0.02549   0.01667  -0.0893   0.6207   0.6995
   4.000   0.7925   0.02555   0.01681  -0.0890   0.6150   0.7015
   4.250   0.8255   0.02529   0.01658  -0.0898   0.6115   0.7032
   4.500   0.8388   0.02574   0.01714  -0.0880   0.6035   0.7053
   4.750   0.8669   0.02566   0.01713  -0.0882   0.5983   0.7078
   5.000   0.9039   0.02531   0.01680  -0.0897   0.5949   0.7106
   5.250   0.9134   0.02596   0.01756  -0.0877   0.5857   0.7136
   5.500   0.9499   0.02562   0.01726  -0.0892   0.5808   0.7163
   5.750   0.9621   0.02601   0.01778  -0.0871   0.5722   0.7182
   6.000   0.9923   0.02578   0.01761  -0.0874   0.5661   0.7202
   6.250   1.0083   0.02606   0.01799  -0.0859   0.5577   0.7226
   6.500   1.0385   0.02583   0.01783  -0.0863   0.5504   0.7254
   6.750   1.0518   0.02617   0.01826  -0.0844   0.5408   0.7286
   7.000   1.0884   0.02586   0.01797  -0.0859   0.5335   0.7318
   7.250   1.0937   0.02646   0.01873  -0.0829   0.5237   0.7341
   7.500   1.1270   0.02618   0.01850  -0.0836   0.5167   0.7364
   7.750   1.1335   0.02689   0.01935  -0.0809   0.5060   0.7391
   8.000   1.1525   0.02719   0.01974  -0.0800   0.4962   0.7421
   8.250   1.1796   0.02717   0.01977  -0.0801   0.4862   0.7454
   8.500   1.1877   0.02797   0.02069  -0.0780   0.4739   0.7487
   8.750   1.1990   0.02858   0.02140  -0.0761   0.4619   0.7516
   9.000   1.2134   0.02911   0.02199  -0.0747   0.4494   0.7549
   9.250   1.2279   0.02969   0.02264  -0.0735   0.4362   0.7583
   9.500   1.2415   0.03039   0.02338  -0.0723   0.4223   0.7618
   9.750   1.2519   0.03127   0.02432  -0.0709   0.4078   0.7649
  10.000   1.2586   0.03234   0.02545  -0.0691   0.3922   0.7681
  10.250   1.2635   0.03363   0.02677  -0.0673   0.3752   0.7718
  10.500   1.2680   0.03507   0.02824  -0.0658   0.3573   0.7760
  10.750   1.2723   0.03660   0.02979  -0.0643   0.3387   0.7802
  11.000   1.2746   0.03822   0.03142  -0.0626   0.3199   0.7840
  11.250   1.2767   0.03997   0.03314  -0.0612   0.3012   0.7882
  11.500   1.2782   0.04193   0.03506  -0.0599   0.2823   0.7926
  11.750   1.2780   0.04409   0.03721  -0.0587   0.2635   0.7968
  12.000   1.2773   0.04631   0.03943  -0.0575   0.2460   0.8010
  12.250   1.2771   0.04864   0.04176  -0.0565   0.2297   0.8060
  12.500   1.2771   0.05110   0.04424  -0.0558   0.2143   0.8114
  12.750   1.2762   0.05360   0.04678  -0.0550   0.2000   0.8169
  13.000   1.2753   0.05629   0.04950  -0.0544   0.1860   0.8235
  13.250   1.2740   0.05905   0.05230  -0.0539   0.1731   0.8304
  13.500   1.2721   0.06197   0.05526  -0.0535   0.1605   0.8386
  13.750   1.2693   0.06501   0.05836  -0.0531   0.1482   0.8479
  14.000   1.2665   0.06811   0.06152  -0.0529   0.1362   0.8597
  14.250   1.2628   0.07112   0.06464  -0.0524   0.1255   0.8765
  14.750   1.2499   0.07770   0.07132  -0.0519   0.1074   1.0000
  15.000   1.2495   0.08147   0.07516  -0.0529   0.0979   1.0000
  15.250   1.2483   0.08537   0.07910  -0.0540   0.0901   1.0000
  15.500   1.2454   0.08955   0.08328  -0.0553   0.0834   1.0000
  15.750   1.2455   0.09338   0.08719  -0.0565   0.0772   1.0000
  16.000   1.2431   0.09758   0.09142  -0.0579   0.0722   1.0000
  16.250   1.2427   0.10147   0.09536  -0.0592   0.0679   1.0000
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