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FX 61-163 AIRFOIL (fx61163-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: FX 61-163 AIRFOIL (fx61163-il)
Reynolds number: 500,000
Max Cl/Cd: 98.78 at α=5.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx61163-il-500000-n5.txt
Download as CSV file: xf-fx61163-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: FX 61-163 AIRFOIL                               
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.500 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -12.250  -0.6236   0.05884   0.05593  -0.0661   1.0001   0.0052
 -12.000  -0.6492   0.05279   0.04966  -0.0681   1.0001   0.0052
 -11.750  -0.6689   0.04815   0.04483  -0.0688   1.0001   0.0052
 -11.500  -0.6846   0.04439   0.04089  -0.0685   1.0001   0.0052
 -11.250  -0.6923   0.04076   0.03705  -0.0690   0.9969   0.0052
 -11.000  -0.6919   0.03746   0.03354  -0.0701   0.9764   0.0053
 -10.750  -0.6496   0.03302   0.02870  -0.0806   0.9289   0.0054
 -10.500  -0.6120   0.03007   0.02521  -0.0874   0.8522   0.0055
 -10.250  -0.6019   0.02856   0.02333  -0.0867   0.8057   0.0056
 -10.000  -0.5903   0.02717   0.02164  -0.0860   0.7766   0.0058
  -9.750  -0.5769   0.02590   0.02012  -0.0852   0.7546   0.0059
  -9.500  -0.5599   0.02469   0.01867  -0.0849   0.7374   0.0060
  -9.250  -0.5413   0.02355   0.01732  -0.0845   0.7234   0.0062
  -9.000  -0.5216   0.02249   0.01608  -0.0842   0.7115   0.0064
  -8.750  -0.5011   0.02154   0.01496  -0.0838   0.7012   0.0065
  -8.250  -0.4583   0.01984   0.01298  -0.0832   0.6829   0.0068
  -8.000  -0.4363   0.01910   0.01210  -0.0830   0.6753   0.0070
  -7.750  -0.4126   0.01851   0.01142  -0.0830   0.6683   0.0072
  -7.500  -0.3907   0.01770   0.01051  -0.0829   0.6623   0.0075
  -7.250  -0.3678   0.01695   0.00970  -0.0830   0.6571   0.0078
  -7.000  -0.3436   0.01633   0.00902  -0.0832   0.6517   0.0081
  -6.750  -0.3189   0.01574   0.00836  -0.0834   0.6468   0.0083
  -6.500  -0.2932   0.01518   0.00773  -0.0838   0.6422   0.0085
  -6.250  -0.2670   0.01466   0.00715  -0.0842   0.6375   0.0088
  -6.000  -0.2401   0.01420   0.00662  -0.0847   0.6334   0.0092
  -5.750  -0.2128   0.01379   0.00613  -0.0852   0.6299   0.0097
  -5.500  -0.1847   0.01342   0.00571  -0.0858   0.6263   0.0102
  -5.250  -0.1565   0.01301   0.00524  -0.0864   0.6226   0.0111
  -5.000  -0.1279   0.01271   0.00489  -0.0870   0.6189   0.0124
  -4.500  -0.0698   0.01211   0.00424  -0.0884   0.6125   0.0224
  -4.250  -0.0401   0.01166   0.00392  -0.0894   0.6092   0.0533
  -3.750   0.0268   0.00959   0.00288  -0.0949   0.6023   0.3375
  -3.500   0.0650   0.00860   0.00261  -0.0986   0.5993   0.5323
  -3.250   0.0959   0.00858   0.00270  -0.0993   0.5962   0.5760
  -3.000   0.1260   0.00865   0.00275  -0.0997   0.5930   0.5960
  -2.750   0.1557   0.00872   0.00277  -0.1001   0.5900   0.6055
  -2.500   0.1858   0.00876   0.00272  -0.1007   0.5873   0.6117
  -2.250   0.2153   0.00881   0.00272  -0.1011   0.5846   0.6153
  -2.000   0.2451   0.00884   0.00273  -0.1015   0.5813   0.6198
  -1.750   0.2751   0.00888   0.00271  -0.1020   0.5776   0.6246
  -1.500   0.3048   0.00892   0.00269  -0.1025   0.5739   0.6284
  -1.250   0.3339   0.00899   0.00271  -0.1028   0.5708   0.6315
  -1.000   0.3636   0.00903   0.00274  -0.1032   0.5680   0.6349
  -0.750   0.3935   0.00906   0.00275  -0.1037   0.5651   0.6382
  -0.500   0.4234   0.00910   0.00274  -0.1043   0.5619   0.6412
  -0.250   0.4527   0.00914   0.00276  -0.1047   0.5587   0.6434
   0.000   0.4818   0.00921   0.00280  -0.1050   0.5559   0.6456
   0.250   0.5112   0.00925   0.00284  -0.1054   0.5528   0.6479
   0.500   0.5407   0.00929   0.00288  -0.1058   0.5487   0.6503
   0.750   0.5700   0.00934   0.00291  -0.1062   0.5444   0.6529
   1.000   0.5993   0.00941   0.00293  -0.1067   0.5408   0.6555
   1.250   0.6289   0.00945   0.00298  -0.1072   0.5374   0.6576
   1.500   0.6579   0.00949   0.00306  -0.1075   0.5338   0.6595
   1.750   0.6868   0.00955   0.00313  -0.1078   0.5299   0.6614
   2.000   0.7155   0.00963   0.00319  -0.1081   0.5262   0.6634
   2.250   0.7447   0.00968   0.00327  -0.1085   0.5221   0.6656
   2.500   0.7739   0.00974   0.00336  -0.1089   0.5179   0.6679
   2.750   0.8027   0.00982   0.00342  -0.1093   0.5129   0.6700
   3.000   0.8317   0.00988   0.00349  -0.1097   0.5072   0.6719
   3.250   0.8601   0.00994   0.00359  -0.1099   0.5009   0.6734
   3.500   0.8882   0.01003   0.00369  -0.1101   0.4961   0.6750
   3.750   0.9167   0.01010   0.00381  -0.1104   0.4897   0.6768
   4.000   0.9444   0.01021   0.00392  -0.1105   0.4816   0.6786
   4.250   0.9726   0.01030   0.00404  -0.1107   0.4725   0.6804
   4.500   1.0004   0.01042   0.00417  -0.1109   0.4646   0.6823
   4.750   1.0276   0.01058   0.00430  -0.1110   0.4525   0.6843
   5.000   1.0544   0.01076   0.00445  -0.1110   0.4367   0.6862
   5.250   1.0805   0.01097   0.00464  -0.1109   0.4212   0.6878
   5.500   1.1063   0.01120   0.00486  -0.1107   0.4061   0.6894
   5.750   1.1317   0.01147   0.00511  -0.1105   0.3903   0.6910
   6.000   1.1573   0.01173   0.00536  -0.1103   0.3770   0.6928
   6.250   1.1827   0.01200   0.00563  -0.1101   0.3649   0.6947
   6.750   1.2318   0.01267   0.00626  -0.1095   0.3335   0.6984
   7.000   1.2536   0.01319   0.00667  -0.1088   0.3063   0.7002
   7.250   1.2730   0.01386   0.00719  -0.1077   0.2716   0.7019
   7.500   1.2900   0.01466   0.00780  -0.1063   0.2345   0.7034
   7.750   1.3056   0.01553   0.00849  -0.1047   0.1964   0.7048
   8.000   1.3199   0.01643   0.00924  -0.1029   0.1652   0.7063
   8.250   1.3329   0.01737   0.01002  -0.1010   0.1353   0.7079
   8.500   1.3447   0.01830   0.01083  -0.0988   0.1098   0.7098
   8.750   1.3546   0.01914   0.01159  -0.0963   0.0908   0.7117
   9.000   1.3637   0.02003   0.01242  -0.0937   0.0742   0.7136
   9.500   1.3811   0.02205   0.01437  -0.0891   0.0513   0.7167
   9.750   1.3901   0.02309   0.01545  -0.0871   0.0420   0.7182
  10.250   1.3976   0.02618   0.01851  -0.0828   0.0232   0.7217
  10.500   1.4057   0.02762   0.02002  -0.0816   0.0199   0.7237
  10.750   1.4126   0.02929   0.02173  -0.0805   0.0172   0.7256
  11.000   1.4209   0.03092   0.02344  -0.0797   0.0153   0.7274
  11.250   1.4269   0.03284   0.02542  -0.0789   0.0128   0.7291
  11.500   1.4321   0.03490   0.02753  -0.0782   0.0100   0.7308
  11.750   1.4357   0.03714   0.02983  -0.0776   0.0070   0.7323
  12.000   1.4372   0.03964   0.03240  -0.0769   0.0047   0.7339
  12.250   1.4393   0.04209   0.03493  -0.0764   0.0040   0.7358
  12.500   1.4413   0.04458   0.03752  -0.0758   0.0036   0.7378
  12.750   1.4426   0.04717   0.04019  -0.0753   0.0033   0.7398
  13.000   1.4433   0.04982   0.04294  -0.0749   0.0031   0.7418
  13.250   1.4431   0.05258   0.04580  -0.0744   0.0029   0.7436
  13.500   1.4428   0.05544   0.04875  -0.0741   0.0028   0.7454
  13.750   1.4431   0.05825   0.05167  -0.0738   0.0027   0.7471
  14.000   1.4432   0.06117   0.05470  -0.0737   0.0027   0.7488
  14.250   1.4425   0.06426   0.05791  -0.0736   0.0026   0.7508
  14.500   1.4410   0.06750   0.06126  -0.0737   0.0025   0.7528
  14.750   1.4399   0.07075   0.06462  -0.0738   0.0025   0.7549
  15.000   1.4379   0.07414   0.06813  -0.0740   0.0025   0.7570
  15.250   1.4352   0.07773   0.07185  -0.0743   0.0024   0.7593
  15.500   1.4318   0.08148   0.07571  -0.0748   0.0024   0.7615
  15.750   1.4280   0.08533   0.07968  -0.0753   0.0023   0.7639
  16.000   1.4239   0.08926   0.08374  -0.0759   0.0023   0.7665
  16.250   1.4192   0.09336   0.08797  -0.0767   0.0022   0.7692
  16.500   1.4144   0.09754   0.09226  -0.0776   0.0022   0.7720
  16.750   1.4090   0.10187   0.09671  -0.0787   0.0022   0.7747
  17.000   1.4031   0.10629   0.10126  -0.0798   0.0022   0.7774
  17.250   1.3959   0.11101   0.10610  -0.0812   0.0021   0.7804
  17.500   1.3890   0.11576   0.11098  -0.0827   0.0021   0.7836
  17.750   1.3817   0.12063   0.11597  -0.0844   0.0021   0.7871
  18.250   1.3673   0.13057   0.12616  -0.0883   0.0020   0.7947
  18.500   1.3587   0.13587   0.13159  -0.0906   0.0020   0.7992
  18.750   1.3516   0.14100   0.13684  -0.0930   0.0019   0.8041
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