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FX 84-W-127 (fx84w127-il) Xfoil prediction polar at RE=100,000 Ncrit=5


Details Polar file
Airfoil: FX 84-W-127 (fx84w127-il)
Reynolds number: 100,000
Max Cl/Cd: 54.8 at α=8°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx84w127-il-100000-n5.txt
Download as CSV file: xf-fx84w127-il-100000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: FX 84-W-127                                     
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -10.500  -0.3320   0.10074   0.09582  -0.0524   1.0000   0.0356
 -10.250  -0.3365   0.09672   0.09188  -0.0539   1.0000   0.0357
 -10.000  -0.3458   0.09329   0.08855  -0.0543   1.0000   0.0358
  -9.750  -0.3450   0.08832   0.08362  -0.0581   0.9893   0.0357
  -9.500  -0.3390   0.08219   0.07750  -0.0643   0.9785   0.0356
  -9.250  -0.3362   0.07483   0.07014  -0.0722   0.9676   0.0354
  -9.000  -0.3395   0.06506   0.06033  -0.0840   0.9542   0.0351
  -8.750  -0.3551   0.05654   0.05160  -0.0925   0.9370   0.0347
  -8.500  -0.3692   0.05010   0.04482  -0.0960   0.9227   0.0347
  -8.250  -0.3781   0.04462   0.03884  -0.0970   0.9108   0.0350
  -8.000  -0.3811   0.03981   0.03338  -0.0966   0.9003   0.0357
  -7.750  -0.3719   0.03725   0.03048  -0.0958   0.8913   0.0370
  -7.500  -0.3527   0.03595   0.02905  -0.0956   0.8849   0.0385
  -7.250  -0.3375   0.03398   0.02676  -0.0947   0.8768   0.0399
  -7.000  -0.3204   0.03160   0.02391  -0.0940   0.8704   0.0413
  -6.750  -0.3020   0.02950   0.02133  -0.0930   0.8634   0.0430
  -6.500  -0.2811   0.02797   0.01949  -0.0924   0.8569   0.0454
  -6.250  -0.2573   0.02704   0.01845  -0.0920   0.8521   0.0480
  -6.000  -0.2355   0.02589   0.01705  -0.0912   0.8446   0.0504
  -5.750  -0.2108   0.02474   0.01556  -0.0906   0.8394   0.0537
  -5.500  -0.1875   0.02388   0.01471  -0.0902   0.8336   0.0572
  -5.250  -0.1635   0.02310   0.01382  -0.0896   0.8273   0.0610
  -5.000  -0.1378   0.02227   0.01277  -0.0890   0.8227   0.0657
  -4.750  -0.1146   0.02167   0.01221  -0.0885   0.8163   0.0709
  -4.500  -0.0898   0.02106   0.01145  -0.0879   0.8106   0.0769
  -4.250  -0.0645   0.02043   0.01084  -0.0875   0.8064   0.0845
  -4.000  -0.0411   0.01998   0.01032  -0.0868   0.7995   0.0928
  -3.750  -0.0162   0.01952   0.00984  -0.0864   0.7942   0.1044
  -3.500   0.0095   0.01902   0.00933  -0.0859   0.7901   0.1184
  -3.250   0.0328   0.01869   0.00905  -0.0853   0.7829   0.1365
  -3.000   0.0580   0.01825   0.00869  -0.0849   0.7779   0.1620
  -2.750   0.0831   0.01782   0.00837  -0.0845   0.7730   0.1992
  -2.500   0.1063   0.01743   0.00820  -0.0839   0.7663   0.2550
  -2.250   0.1304   0.01682   0.00795  -0.0834   0.7617   0.3497
  -2.000   0.1513   0.01618   0.00791  -0.0822   0.7561   0.5011
  -1.750   0.1705   0.01582   0.00809  -0.0799   0.7500   0.6530
  -1.500   0.1928   0.01569   0.00812  -0.0777   0.7457   0.7456
  -1.250   0.2143   0.01575   0.00822  -0.0758   0.7398   0.8046
  -1.000   0.2376   0.01581   0.00825  -0.0741   0.7341   0.8487
  -0.750   0.2657   0.01578   0.00813  -0.0733   0.7300   0.8855
  -0.500   0.2969   0.01586   0.00815  -0.0735   0.7240   0.9172
  -0.250   0.3368   0.01588   0.00807  -0.0755   0.7187   0.9452
   0.000   0.3937   0.01578   0.00782  -0.0809   0.7149   0.9726
   0.250   0.4524   0.01573   0.00766  -0.0872   0.7094   0.9921
   0.500   0.4864   0.01575   0.00760  -0.0889   0.7034   1.0000
   0.750   0.5071   0.01574   0.00748  -0.0878   0.6988   1.0000
   1.000   0.5237   0.01595   0.00766  -0.0862   0.6914   1.0000
   1.250   0.5440   0.01601   0.00765  -0.0849   0.6859   1.0000
   1.500   0.5646   0.01612   0.00768  -0.0837   0.6803   1.0000
   1.750   0.5836   0.01631   0.00785  -0.0824   0.6734   1.0000
   2.000   0.6074   0.01635   0.00781  -0.0816   0.6686   1.0000
   2.250   0.6274   0.01659   0.00805  -0.0805   0.6616   1.0000
   2.500   0.6510   0.01672   0.00814  -0.0798   0.6559   1.0000
   2.750   0.6763   0.01682   0.00820  -0.0793   0.6509   1.0000
   3.000   0.6978   0.01710   0.00849  -0.0785   0.6436   1.0000
   3.250   0.7243   0.01718   0.00853  -0.0782   0.6387   1.0000
   3.500   0.7470   0.01745   0.00883  -0.0775   0.6318   1.0000
   3.750   0.7720   0.01761   0.00901  -0.0771   0.6257   1.0000
   4.000   0.7982   0.01774   0.00913  -0.0768   0.6200   1.0000
   4.250   0.8209   0.01802   0.00946  -0.0761   0.6124   1.0000
   4.500   0.8492   0.01806   0.00950  -0.0760   0.6072   1.0000
   4.750   0.8702   0.01843   0.00996  -0.0752   0.5987   1.0000
   5.000   0.8977   0.01851   0.01005  -0.0750   0.5929   1.0000
   5.250   0.9196   0.01885   0.01048  -0.0743   0.5848   1.0000
   5.500   0.9462   0.01897   0.01065  -0.0740   0.5783   1.0000
   5.750   0.9684   0.01929   0.01106  -0.0732   0.5699   1.0000
   6.000   0.9952   0.01938   0.01118  -0.0730   0.5626   1.0000
   6.250   1.0162   0.01971   0.01163  -0.0720   0.5528   1.0000
   6.500   1.0424   0.01981   0.01177  -0.0716   0.5447   1.0000
   6.750   1.0639   0.02011   0.01218  -0.0707   0.5347   1.0000
   7.000   1.0860   0.02039   0.01258  -0.0698   0.5250   1.0000
   7.250   1.1113   0.02051   0.01275  -0.0693   0.5154   1.0000
   7.500   1.1315   0.02071   0.01302  -0.0680   0.5013   1.0000
   7.750   1.1469   0.02096   0.01335  -0.0660   0.4818   1.0000
   8.000   1.1618   0.02120   0.01362  -0.0639   0.4594   1.0000
   8.250   1.1753   0.02157   0.01398  -0.0617   0.4371   1.0000
   8.500   1.1870   0.02205   0.01447  -0.0593   0.4142   1.0000
   8.750   1.1951   0.02264   0.01504  -0.0565   0.3904   1.0000
   9.000   1.2006   0.02340   0.01573  -0.0534   0.3642   1.0000
   9.250   1.2042   0.02437   0.01662  -0.0504   0.3353   1.0000
   9.500   1.2055   0.02561   0.01776  -0.0475   0.3022   1.0000
   9.750   1.2036   0.02717   0.01914  -0.0446   0.2668   1.0000
  10.000   1.1996   0.02905   0.02083  -0.0419   0.2310   1.0000
  10.250   1.1943   0.03123   0.02281  -0.0395   0.1958   1.0000
  10.500   1.1886   0.03362   0.02501  -0.0374   0.1635   1.0000
  10.750   1.1832   0.03617   0.02739  -0.0355   0.1345   1.0000
  11.000   1.1794   0.03873   0.02982  -0.0340   0.1117   1.0000
  11.250   1.1762   0.04134   0.03235  -0.0327   0.0959   1.0000
  11.500   1.1746   0.04392   0.03491  -0.0316   0.0842   1.0000
  11.750   1.1745   0.04644   0.03746  -0.0307   0.0755   1.0000
  12.000   1.1725   0.04921   0.04021  -0.0299   0.0694   1.0000
  12.250   1.1744   0.05168   0.04279  -0.0293   0.0635   1.0000
  12.500   1.1727   0.05460   0.04571  -0.0288   0.0592   1.0000
  12.750   1.1755   0.05711   0.04833  -0.0283   0.0554   1.0000
  13.000   1.1778   0.05973   0.05104  -0.0280   0.0520   1.0000
  13.250   1.1781   0.06261   0.05395  -0.0278   0.0493   1.0000
  13.500   1.1823   0.06511   0.05656  -0.0275   0.0466   1.0000
  13.750   1.1872   0.06759   0.05916  -0.0273   0.0440   1.0000
  14.000   1.1915   0.07013   0.06177  -0.0272   0.0419   1.0000
  14.250   1.1953   0.07275   0.06441  -0.0270   0.0401   1.0000
  14.500   1.2022   0.07507   0.06685  -0.0268   0.0382   1.0000
  14.750   1.2088   0.07753   0.06947  -0.0267   0.0364   1.0000
  15.000   1.2140   0.08016   0.07222  -0.0268   0.0347   1.0000
  15.250   1.2196   0.08274   0.07487  -0.0268   0.0334   1.0000
  15.500   1.2267   0.08511   0.07726  -0.0267   0.0323   1.0000
  15.750   1.2327   0.08785   0.08017  -0.0268   0.0313   1.0000
  16.000   1.2339   0.09137   0.08395  -0.0274   0.0301   1.0000
  16.250   1.2346   0.09498   0.08777  -0.0282   0.0291   1.0000
  16.500   1.2338   0.09881   0.09178  -0.0293   0.0282   1.0000
  16.750   1.2325   0.10276   0.09589  -0.0306   0.0274   1.0000
  17.000   1.2316   0.10670   0.09997  -0.0319   0.0268   1.0000
  17.250   1.2305   0.11073   0.10414  -0.0333   0.0264   1.0000
  17.500   1.2291   0.11483   0.10836  -0.0348   0.0259   1.0000
  17.750   1.2245   0.11962   0.11329  -0.0368   0.0255   1.0000
  18.000   1.2117   0.12619   0.12013  -0.0402   0.0254   1.0000
  18.250   1.1965   0.13351   0.12772  -0.0444   0.0252   1.0000
  18.500   1.1800   0.14139   0.13585  -0.0492   0.0252   1.0000
  18.750   1.1608   0.15032   0.14502  -0.0549   0.0252   1.0000
  19.000   1.1388   0.16057   0.15548  -0.0617   0.0252   1.0000
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