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WORTMANN FX 76-120 (fx76120-il) Xfoil prediction polar at RE=100,000 Ncrit=5


Details Polar file
Airfoil: WORTMANN FX 76-120 (fx76120-il)
Reynolds number: 100,000
Max Cl/Cd: 37.79 at α=6.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx76120-il-100000-n5.txt
Download as CSV file: xf-fx76120-il-100000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: WORTMANN FX 76-120                              
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -14.750  -0.8386   0.09882   0.09284  -0.0229   1.0000   0.0431
 -14.500  -0.8932   0.08426   0.07805  -0.0327   1.0000   0.0425
 -14.250  -0.9262   0.07505   0.06861  -0.0387   1.0000   0.0423
 -14.000  -0.9516   0.06793   0.06125  -0.0429   1.0000   0.0424
 -13.750  -0.9707   0.06234   0.05542  -0.0457   1.0000   0.0426
 -13.500  -0.9868   0.05762   0.05046  -0.0473   1.0000   0.0430
 -13.250  -1.0006   0.05359   0.04615  -0.0480   1.0000   0.0436
 -13.000  -1.0101   0.05026   0.04254  -0.0478   1.0000   0.0441
 -12.750  -1.0107   0.04782   0.04003  -0.0470   1.0000   0.0450
 -12.500  -1.0087   0.04586   0.03804  -0.0461   1.0000   0.0460
 -12.250  -1.0079   0.04399   0.03609  -0.0447   1.0000   0.0472
 -12.000  -1.0072   0.04214   0.03408  -0.0430   1.0000   0.0486
 -11.750  -1.0053   0.04033   0.03209  -0.0410   1.0000   0.0499
 -11.500  -1.0025   0.03859   0.03012  -0.0388   1.0000   0.0514
 -11.250  -0.9973   0.03699   0.02835  -0.0364   1.0000   0.0527
 -11.000  -0.9912   0.03570   0.02708  -0.0341   1.0000   0.0544
 -10.750  -0.9841   0.03451   0.02585  -0.0317   1.0000   0.0563
 -10.500  -0.9747   0.03329   0.02450  -0.0295   1.0000   0.0586
 -10.250  -0.9634   0.03205   0.02305  -0.0274   1.0000   0.0610
 -10.000  -0.9528   0.03081   0.02180  -0.0253   1.0000   0.0633
  -9.750  -0.9415   0.02978   0.02074  -0.0232   1.0000   0.0662
  -9.500  -0.9286   0.02878   0.01963  -0.0211   1.0000   0.0696
  -9.250  -0.9156   0.02773   0.01851  -0.0190   1.0000   0.0732
  -9.000  -0.9032   0.02677   0.01754  -0.0168   1.0000   0.0768
  -8.750  -0.8890   0.02590   0.01657  -0.0147   1.0000   0.0818
  -8.500  -0.8757   0.02499   0.01567  -0.0126   1.0000   0.0869
  -8.250  -0.8610   0.02419   0.01483  -0.0105   1.0000   0.0933
  -8.000  -0.8466   0.02338   0.01404  -0.0084   1.0000   0.1005
  -7.750  -0.8308   0.02267   0.01328  -0.0065   1.0000   0.1099
  -7.500  -0.8153   0.02198   0.01261  -0.0045   1.0000   0.1202
  -7.250  -0.7993   0.02134   0.01202  -0.0025   1.0000   0.1322
  -7.000  -0.7827   0.02078   0.01147  -0.0007   1.0000   0.1456
  -6.750  -0.7657   0.02026   0.01096   0.0012   1.0000   0.1597
  -6.500  -0.7483   0.01980   0.01051   0.0030   1.0000   0.1743
  -6.250  -0.7307   0.01937   0.01008   0.0048   1.0000   0.1889
  -6.000  -0.7130   0.01897   0.00968   0.0065   1.0000   0.2036
  -5.750  -0.6951   0.01859   0.00930   0.0083   1.0000   0.2183
  -5.500  -0.6770   0.01823   0.00896   0.0100   1.0000   0.2331
  -5.250  -0.6588   0.01789   0.00863   0.0117   1.0000   0.2481
  -5.000  -0.6405   0.01756   0.00831   0.0134   1.0000   0.2633
  -4.750  -0.6221   0.01725   0.00802   0.0151   1.0000   0.2789
  -4.500  -0.6037   0.01694   0.00775   0.0168   1.0000   0.2950
  -4.250  -0.5854   0.01664   0.00751   0.0184   1.0000   0.3119
  -4.000  -0.5669   0.01636   0.00729   0.0201   1.0000   0.3297
  -3.750  -0.5484   0.01610   0.00711   0.0217   1.0000   0.3485
  -3.500  -0.5299   0.01586   0.00695   0.0233   1.0000   0.3687
  -3.250  -0.5048   0.01564   0.00680   0.0236   0.9977   0.3937
  -3.000  -0.4681   0.01539   0.00670   0.0215   0.9904   0.4253
  -2.750  -0.4308   0.01515   0.00661   0.0195   0.9825   0.4603
  -2.500  -0.3939   0.01488   0.00653   0.0176   0.9739   0.4986
  -2.250  -0.3575   0.01464   0.00647   0.0159   0.9652   0.5410
  -2.000  -0.3193   0.01442   0.00644   0.0140   0.9573   0.5855
  -1.750  -0.2852   0.01422   0.00641   0.0130   0.9474   0.6287
  -1.500  -0.2470   0.01405   0.00643   0.0114   0.9388   0.6725
  -1.250  -0.2055   0.01392   0.00644   0.0092   0.9297   0.7151
  -1.000  -0.1657   0.01382   0.00648   0.0076   0.9181   0.7533
  -0.750  -0.1236   0.01376   0.00650   0.0055   0.9064   0.7866
  -0.500  -0.0802   0.01371   0.00650   0.0032   0.8940   0.8147
  -0.250  -0.0388   0.01370   0.00653   0.0014   0.8789   0.8390
   0.000  -0.0001   0.01369   0.00652   0.0000   0.8608   0.8610
   0.250   0.0387   0.01370   0.00653  -0.0014   0.8390   0.8788
   0.500   0.0801   0.01371   0.00650  -0.0032   0.8150   0.8939
   0.750   0.1236   0.01376   0.00649  -0.0055   0.7862   0.9064
   1.000   0.1658   0.01382   0.00648  -0.0076   0.7531   0.9182
   1.250   0.2054   0.01391   0.00644  -0.0092   0.7155   0.9297
   1.500   0.2470   0.01405   0.00643  -0.0114   0.6733   0.9388
   1.750   0.2853   0.01422   0.00641  -0.0130   0.6291   0.9475
   2.000   0.3195   0.01442   0.00644  -0.0140   0.5855   0.9573
   2.250   0.3575   0.01464   0.00647  -0.0159   0.5408   0.9652
   2.500   0.3940   0.01488   0.00653  -0.0176   0.4985   0.9740
   2.750   0.4309   0.01515   0.00660  -0.0195   0.4600   0.9826
   3.000   0.4682   0.01539   0.00670  -0.0215   0.4251   0.9905
   3.250   0.5049   0.01563   0.00681  -0.0236   0.3938   0.9977
   3.500   0.5298   0.01586   0.00695  -0.0233   0.3692   1.0000
   3.750   0.5484   0.01610   0.00711  -0.0217   0.3485   1.0000
   4.000   0.5669   0.01636   0.00729  -0.0201   0.3297   1.0000
   4.250   0.5853   0.01664   0.00751  -0.0184   0.3119   1.0000
   4.500   0.6037   0.01694   0.00775  -0.0168   0.2952   1.0000
   4.750   0.6221   0.01725   0.00802  -0.0151   0.2789   1.0000
   5.000   0.6405   0.01756   0.00831  -0.0134   0.2634   1.0000
   5.250   0.6588   0.01789   0.00863  -0.0117   0.2483   1.0000
   5.500   0.6770   0.01823   0.00895  -0.0100   0.2333   1.0000
   5.750   0.6950   0.01859   0.00930  -0.0083   0.2183   1.0000
   6.000   0.7129   0.01897   0.00968  -0.0065   0.2036   1.0000
   6.250   0.7307   0.01937   0.01008  -0.0048   0.1891   1.0000
   6.500   0.7483   0.01980   0.01051  -0.0030   0.1747   1.0000
   6.750   0.7656   0.02027   0.01096  -0.0012   0.1600   1.0000
   7.000   0.7827   0.02078   0.01147   0.0007   0.1456   1.0000
   7.250   0.7993   0.02134   0.01202   0.0025   0.1322   1.0000
   7.500   0.8153   0.02198   0.01261   0.0045   0.1204   1.0000
   7.750   0.8308   0.02266   0.01327   0.0065   0.1098   1.0000
   8.000   0.8467   0.02337   0.01402   0.0084   0.1006   1.0000
   8.250   0.8610   0.02419   0.01482   0.0105   0.0934   1.0000
   8.500   0.8758   0.02499   0.01568   0.0126   0.0870   1.0000
   8.750   0.8890   0.02590   0.01658   0.0148   0.0818   1.0000
   9.000   0.9033   0.02677   0.01754   0.0168   0.0768   1.0000
   9.250   0.9155   0.02774   0.01850   0.0190   0.0730   1.0000
   9.500   0.9287   0.02877   0.01963   0.0211   0.0696   1.0000
   9.750   0.9416   0.02978   0.02074   0.0231   0.0661   1.0000
  10.000   0.9528   0.03080   0.02178   0.0253   0.0632   1.0000
  10.250   0.9636   0.03205   0.02305   0.0274   0.0610   1.0000
  10.500   0.9748   0.03328   0.02449   0.0295   0.0585   1.0000
  10.750   0.9845   0.03453   0.02587   0.0316   0.0563   1.0000
  11.000   0.9915   0.03570   0.02709   0.0341   0.0543   1.0000
  11.250   0.9981   0.03700   0.02837   0.0364   0.0528   1.0000
  11.500   1.0027   0.03860   0.03014   0.0387   0.0513   1.0000
  11.750   1.0060   0.04032   0.03209   0.0409   0.0499   1.0000
  12.000   1.0073   0.04211   0.03407   0.0430   0.0484   1.0000
  12.250   1.0083   0.04391   0.03600   0.0446   0.0470   1.0000
  12.500   1.0094   0.04581   0.03798   0.0460   0.0459   1.0000
  12.750   1.0116   0.04777   0.03998   0.0469   0.0450   1.0000
  13.000   1.0108   0.05025   0.04253   0.0477   0.0441   1.0000
  13.250   1.0006   0.05366   0.04623   0.0479   0.0435   1.0000
  13.500   0.9877   0.05763   0.05046   0.0472   0.0430   1.0000
  13.750   0.9718   0.06232   0.05540   0.0456   0.0426   1.0000
  14.000   0.9525   0.06795   0.06127   0.0428   0.0423   1.0000
  14.250   0.9275   0.07502   0.06857   0.0386   0.0422   1.0000
  14.500   0.8929   0.08455   0.07835   0.0322   0.0424   1.0000
  14.750   0.8369   0.09950   0.09353   0.0223   0.0431   1.0000
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