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WORTMANN FX 76-100 (fx76100-il) Xfoil prediction polar at RE=50,000 Ncrit=5


Details Polar file
Airfoil: WORTMANN FX 76-100 (fx76100-il)
Reynolds number: 50,000
Max Cl/Cd: 26.13 at α=5.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx76100-il-50000-n5.txt
Download as CSV file: xf-fx76100-il-50000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: WORTMANN FX 76-100                              
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.050 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -11.750  -0.7250   0.09544   0.08780  -0.0172   1.0000   0.0609
 -11.500  -0.7482   0.08626   0.07862  -0.0232   1.0000   0.0606
 -11.250  -0.7725   0.07833   0.07064  -0.0286   1.0000   0.0601
 -11.000  -0.7983   0.07169   0.06390  -0.0323   1.0000   0.0596
 -10.750  -0.8259   0.06627   0.05831  -0.0337   1.0000   0.0596
 -10.500  -0.8482   0.06214   0.05399  -0.0327   1.0000   0.0596
 -10.250  -0.8674   0.05819   0.04973  -0.0308   1.0000   0.0601
 -10.000  -0.8805   0.05435   0.04546  -0.0287   1.0000   0.0610
  -9.750  -0.8739   0.05181   0.04291  -0.0274   1.0000   0.0629
  -9.500  -0.8681   0.04928   0.04022  -0.0258   1.0000   0.0649
  -9.250  -0.8627   0.04641   0.03704  -0.0240   1.0000   0.0669
  -9.000  -0.8550   0.04371   0.03397  -0.0222   1.0000   0.0696
  -8.750  -0.8466   0.04102   0.03067  -0.0202   1.0000   0.0731
  -8.500  -0.8306   0.03917   0.02890  -0.0190   1.0000   0.0769
  -8.250  -0.8146   0.03718   0.02670  -0.0176   1.0000   0.0808
  -8.000  -0.7981   0.03519   0.02432  -0.0160   1.0000   0.0864
  -7.750  -0.7810   0.03375   0.02295  -0.0147   1.0000   0.0925
  -7.500  -0.7616   0.03206   0.02095  -0.0133   1.0000   0.0996
  -7.250  -0.7441   0.03077   0.01970  -0.0119   1.0000   0.1079
  -7.000  -0.7258   0.02947   0.01835  -0.0105   1.0000   0.1184
  -6.750  -0.7071   0.02823   0.01707  -0.0090   1.0000   0.1311
  -6.500  -0.6891   0.02714   0.01600  -0.0075   1.0000   0.1477
  -6.250  -0.6706   0.02611   0.01492  -0.0060   1.0000   0.1691
  -6.000  -0.6528   0.02517   0.01408  -0.0044   1.0000   0.1925
  -5.750  -0.6346   0.02433   0.01328  -0.0028   1.0000   0.2200
  -5.500  -0.6161   0.02358   0.01256  -0.0013   1.0000   0.2485
  -5.250  -0.5974   0.02290   0.01192   0.0003   1.0000   0.2783
  -5.000  -0.5785   0.02226   0.01131   0.0018   1.0000   0.3090
  -4.750  -0.5592   0.02164   0.01077   0.0033   1.0000   0.3401
  -4.500  -0.5396   0.02104   0.01027   0.0049   1.0000   0.3721
  -4.250  -0.5197   0.02047   0.00980   0.0064   1.0000   0.4055
  -4.000  -0.4996   0.01991   0.00933   0.0079   1.0000   0.4412
  -3.750  -0.4803   0.01939   0.00895   0.0097   1.0000   0.4794
  -3.500  -0.4612   0.01891   0.00865   0.0117   1.0000   0.5206
  -3.250  -0.4419   0.01848   0.00840   0.0137   1.0000   0.5667
  -3.000  -0.4220   0.01813   0.00821   0.0158   1.0000   0.6170
  -2.750  -0.4002   0.01787   0.00814   0.0177   1.0000   0.6693
  -2.500  -0.3755   0.01773   0.00814   0.0193   1.0000   0.7232
  -2.250  -0.3466   0.01772   0.00819   0.0201   1.0000   0.7757
  -2.000  -0.3120   0.01782   0.00828   0.0197   1.0000   0.8234
  -1.750  -0.2730   0.01797   0.00837   0.0183   1.0000   0.8666
  -1.500  -0.2265   0.01814   0.00843   0.0152   1.0000   0.9023
  -1.250  -0.1741   0.01828   0.00845   0.0108   1.0000   0.9324
  -1.000  -0.1186   0.01834   0.00839   0.0053   1.0000   0.9587
  -0.750  -0.0598   0.01827   0.00824  -0.0011   1.0000   0.9820
  -0.500  -0.0088   0.01813   0.00805  -0.0064   1.0000   1.0000
  -0.250  -0.0042   0.01803   0.00795  -0.0033   1.0000   1.0000
   0.000   0.0000   0.01800   0.00791   0.0000   1.0000   1.0000
   0.250   0.0043   0.01803   0.00795   0.0033   1.0000   1.0000
   0.500   0.0089   0.01813   0.00804   0.0065   1.0000   1.0000
   0.750   0.0602   0.01827   0.00824   0.0010   0.9818   1.0000
   1.000   0.1183   0.01834   0.00839  -0.0053   0.9588   1.0000
   1.250   0.1741   0.01828   0.00844  -0.0107   0.9324   1.0000
   1.500   0.2267   0.01814   0.00843  -0.0153   0.9021   1.0000
   1.750   0.2730   0.01797   0.00837  -0.0183   0.8665   1.0000
   2.000   0.3120   0.01781   0.00828  -0.0197   0.8234   1.0000
   2.250   0.3467   0.01772   0.00818  -0.0201   0.7754   1.0000
   2.500   0.3754   0.01773   0.00814  -0.0192   0.7231   1.0000
   2.750   0.4002   0.01787   0.00813  -0.0177   0.6691   1.0000
   3.000   0.4219   0.01813   0.00821  -0.0158   0.6164   1.0000
   3.250   0.4419   0.01848   0.00840  -0.0137   0.5665   1.0000
   3.500   0.4612   0.01891   0.00865  -0.0117   0.5205   1.0000
   3.750   0.4802   0.01939   0.00895  -0.0097   0.4791   1.0000
   4.000   0.4996   0.01991   0.00933  -0.0079   0.4410   1.0000
   4.250   0.5197   0.02046   0.00980  -0.0064   0.4056   1.0000
   4.500   0.5396   0.02105   0.01027  -0.0049   0.3720   1.0000
   4.750   0.5592   0.02164   0.01078  -0.0033   0.3402   1.0000
   5.000   0.5785   0.02226   0.01131  -0.0018   0.3089   1.0000
   5.250   0.5974   0.02290   0.01192  -0.0003   0.2784   1.0000
   5.500   0.6161   0.02358   0.01256   0.0013   0.2487   1.0000
   5.750   0.6346   0.02433   0.01328   0.0029   0.2199   1.0000
   6.000   0.6528   0.02516   0.01407   0.0044   0.1923   1.0000
   6.250   0.6706   0.02610   0.01494   0.0060   0.1685   1.0000
   6.500   0.6891   0.02714   0.01600   0.0075   0.1475   1.0000
   6.750   0.7070   0.02823   0.01706   0.0090   0.1309   1.0000
   7.000   0.7257   0.02946   0.01834   0.0105   0.1182   1.0000
   7.250   0.7441   0.03077   0.01970   0.0119   0.1076   1.0000
   7.500   0.7616   0.03207   0.02095   0.0133   0.0995   1.0000
   7.750   0.7810   0.03376   0.02295   0.0147   0.0924   1.0000
   8.000   0.7981   0.03519   0.02432   0.0160   0.0864   1.0000
   8.250   0.8147   0.03719   0.02671   0.0176   0.0808   1.0000
   8.500   0.8307   0.03919   0.02892   0.0190   0.0769   1.0000
   8.750   0.8467   0.04103   0.03068   0.0202   0.0732   1.0000
   9.000   0.8552   0.04370   0.03396   0.0222   0.0696   1.0000
   9.250   0.8627   0.04642   0.03704   0.0240   0.0668   1.0000
   9.500   0.8683   0.04928   0.04021   0.0257   0.0649   1.0000
   9.750   0.8735   0.05190   0.04302   0.0273   0.0631   1.0000
  10.000   0.8811   0.05435   0.04544   0.0286   0.0610   1.0000
  10.250   0.8675   0.05824   0.04978   0.0307   0.0601   1.0000
  10.500   0.8486   0.06216   0.05402   0.0326   0.0596   1.0000
  10.750   0.8261   0.06637   0.05842   0.0337   0.0596   1.0000
  11.000   0.8014   0.07150   0.06369   0.0325   0.0598   1.0000
  11.250   0.7777   0.07774   0.07004   0.0291   0.0603   1.0000
  11.500   0.7491   0.08627   0.07862   0.0231   0.0606   1.0000
  11.750   0.7270   0.09520   0.08756   0.0174   0.0610   1.0000
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