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WORTMANN FX 77-080 (fx77080-il) Xfoil prediction polar at RE=50,000 Ncrit=5


Details Polar file
Airfoil: WORTMANN FX 77-080 (fx77080-il)
Reynolds number: 50,000
Max Cl/Cd: 23.88 at α=5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx77080-il-50000-n5.txt
Download as CSV file: xf-fx77080-il-50000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: WORTMANN FX 77-080                              
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -10.250  -0.6948   0.09326   0.08590  -0.0059   1.0000   0.0553
 -10.000  -0.7080   0.08531   0.07801  -0.0112   1.0000   0.0548
  -9.750  -0.7283   0.07690   0.06962  -0.0176   1.0000   0.0540
  -9.500  -0.7536   0.07037   0.06304  -0.0208   1.0000   0.0534
  -9.250  -0.7744   0.06496   0.05749  -0.0215   1.0000   0.0532
  -9.000  -0.7885   0.05980   0.05208  -0.0216   1.0000   0.0531
  -8.750  -0.7962   0.05503   0.04698  -0.0210   1.0000   0.0536
  -8.500  -0.7980   0.05071   0.04223  -0.0199   1.0000   0.0550
  -8.250  -0.7962   0.04653   0.03749  -0.0185   1.0000   0.0571
  -8.000  -0.7887   0.04291   0.03333  -0.0170   1.0000   0.0596
  -7.750  -0.7736   0.04071   0.03103  -0.0159   1.0000   0.0625
  -7.500  -0.7582   0.03807   0.02804  -0.0146   1.0000   0.0653
  -7.250  -0.7413   0.03546   0.02487  -0.0132   1.0000   0.0701
  -7.000  -0.7227   0.03374   0.02308  -0.0121   1.0000   0.0754
  -6.750  -0.7024   0.03179   0.02082  -0.0109   1.0000   0.0817
  -6.500  -0.6820   0.03023   0.01916  -0.0097   1.0000   0.0892
  -6.250  -0.6607   0.02874   0.01747  -0.0086   1.0000   0.0997
  -6.000  -0.6385   0.02734   0.01585  -0.0074   1.0000   0.1116
  -5.750  -0.6177   0.02619   0.01472  -0.0063   1.0000   0.1275
  -5.500  -0.5963   0.02506   0.01358  -0.0052   1.0000   0.1460
  -5.250  -0.5745   0.02406   0.01252  -0.0041   1.0000   0.1698
  -5.000  -0.5531   0.02316   0.01166  -0.0031   1.0000   0.1949
  -4.750  -0.5312   0.02231   0.01083  -0.0021   1.0000   0.2219
  -4.500  -0.5088   0.02149   0.01006  -0.0011   1.0000   0.2510
  -4.250  -0.4863   0.02070   0.00934  -0.0002   1.0000   0.2831
  -4.000  -0.4641   0.01989   0.00869   0.0008   1.0000   0.3201
  -3.750  -0.4436   0.01912   0.00808   0.0022   1.0000   0.3649
  -3.500  -0.4243   0.01836   0.00760   0.0039   1.0000   0.4228
  -3.250  -0.4058   0.01762   0.00724   0.0061   1.0000   0.4962
  -3.000  -0.3869   0.01699   0.00700   0.0085   1.0000   0.5824
  -2.750  -0.3646   0.01654   0.00688   0.0107   1.0000   0.6769
  -2.500  -0.3331   0.01635   0.00688   0.0116   1.0000   0.7680
  -2.250  -0.2904   0.01637   0.00688   0.0101   1.0000   0.8456
  -2.000  -0.2390   0.01646   0.00679   0.0066   1.0000   0.9057
  -1.750  -0.1737   0.01655   0.00664  -0.0002   1.0000   0.9527
  -1.500  -0.1038   0.01644   0.00630  -0.0086   1.0000   0.9901
  -1.250  -0.0724   0.01623   0.00597  -0.0101   1.0000   1.0000
  -1.000  -0.0583   0.01606   0.00574  -0.0081   1.0000   1.0000
  -0.750  -0.0441   0.01592   0.00557  -0.0061   1.0000   1.0000
  -0.500  -0.0296   0.01583   0.00545  -0.0040   1.0000   1.0000
  -0.250  -0.0148   0.01578   0.00538  -0.0020   1.0000   1.0000
   0.000   0.0000   0.01576   0.00536   0.0000   1.0000   1.0000
   0.250   0.0149   0.01578   0.00538   0.0020   1.0000   1.0000
   0.500   0.0296   0.01583   0.00545   0.0041   1.0000   1.0000
   0.750   0.0442   0.01592   0.00557   0.0061   1.0000   1.0000
   1.000   0.0584   0.01606   0.00574   0.0081   1.0000   1.0000
   1.250   0.0725   0.01623   0.00596   0.0101   1.0000   1.0000
   1.500   0.1033   0.01643   0.00628   0.0087   0.9903   1.0000
   1.750   0.1743   0.01654   0.00663   0.0001   0.9523   1.0000
   2.000   0.2397   0.01646   0.00680  -0.0066   0.9049   1.0000
   2.250   0.2902   0.01637   0.00687  -0.0101   0.8460   1.0000
   2.500   0.3331   0.01635   0.00688  -0.0116   0.7685   1.0000
   2.750   0.3646   0.01654   0.00687  -0.0107   0.6757   1.0000
   3.000   0.3869   0.01700   0.00700  -0.0085   0.5813   1.0000
   3.250   0.4058   0.01763   0.00723  -0.0060   0.4955   1.0000
   3.500   0.4242   0.01836   0.00760  -0.0039   0.4222   1.0000
   3.750   0.4437   0.01912   0.00812  -0.0022   0.3649   1.0000
   4.000   0.4640   0.01990   0.00868  -0.0008   0.3197   1.0000
   4.250   0.4863   0.02070   0.00934   0.0002   0.2827   1.0000
   4.500   0.5088   0.02150   0.01007   0.0011   0.2510   1.0000
   4.750   0.5312   0.02231   0.01083   0.0021   0.2217   1.0000
   5.000   0.5531   0.02316   0.01167   0.0031   0.1949   1.0000
   5.250   0.5745   0.02407   0.01253   0.0041   0.1698   1.0000
   5.500   0.5963   0.02507   0.01360   0.0052   0.1461   1.0000
   5.750   0.6177   0.02620   0.01472   0.0063   0.1275   1.0000
   6.000   0.6386   0.02734   0.01586   0.0074   0.1116   1.0000
   6.250   0.6606   0.02873   0.01746   0.0086   0.0996   1.0000
   6.500   0.6818   0.03018   0.01910   0.0097   0.0888   1.0000
   6.750   0.7024   0.03180   0.02083   0.0109   0.0816   1.0000
   7.000   0.7227   0.03375   0.02309   0.0121   0.0754   1.0000
   7.250   0.7412   0.03549   0.02491   0.0132   0.0699   1.0000
   7.500   0.7581   0.03808   0.02806   0.0146   0.0652   1.0000
   7.750   0.7736   0.04072   0.03103   0.0159   0.0624   1.0000
   8.000   0.7890   0.04278   0.03313   0.0170   0.0592   1.0000
   8.250   0.7958   0.04658   0.03755   0.0185   0.0568   1.0000
   8.500   0.7980   0.05071   0.04223   0.0199   0.0548   1.0000
   8.750   0.7961   0.05507   0.04701   0.0210   0.0535   1.0000
   9.000   0.7883   0.05986   0.05215   0.0216   0.0531   1.0000
   9.250   0.7737   0.06510   0.05763   0.0215   0.0530   1.0000
   9.500   0.7530   0.07050   0.06319   0.0207   0.0534   1.0000
   9.750   0.7286   0.07692   0.06964   0.0175   0.0540   1.0000
  10.000   0.7078   0.08551   0.07821   0.0109   0.0547   1.0000
  10.250   0.6954   0.09330   0.08594   0.0058   0.0553   1.0000
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