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WORTMANN FX 80-080 (fx80080-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: WORTMANN FX 80-080 (fx80080-il)
Reynolds number: 200,000
Max Cl/Cd: 74.73 at α=3.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx80080-il-200000-n5.txt
Download as CSV file: xf-fx80080-il-200000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: WORTMANN FX 80-080                              
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.200 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
  -9.000  -0.4468   0.09484   0.09123  -0.0311   1.0000   0.0159
  -8.750  -0.4477   0.09076   0.08720  -0.0325   1.0000   0.0151
  -8.500  -0.4492   0.08688   0.08337  -0.0340   1.0000   0.0149
  -8.250  -0.4529   0.08294   0.07949  -0.0354   1.0000   0.0142
  -8.000  -0.4598   0.07915   0.07577  -0.0365   1.0000   0.0136
  -7.750  -0.4705   0.07581   0.07253  -0.0372   1.0000   0.0139
  -7.500  -0.4803   0.07112   0.06790  -0.0401   1.0000   0.0133
  -7.250  -0.4843   0.06250   0.05922  -0.0469   0.9961   0.0119
  -7.000  -0.4630   0.05880   0.05542  -0.0519   0.9898   0.0129
  -6.750  -0.4412   0.05426   0.05072  -0.0569   0.9821   0.0143
  -6.500  -0.4182   0.04826   0.04445  -0.0619   0.9745   0.0157
  -6.250  -0.3946   0.04208   0.03791  -0.0659   0.9679   0.0149
  -6.000  -0.3704   0.03609   0.03147  -0.0685   0.9616   0.0144
  -5.750  -0.3441   0.03053   0.02534  -0.0703   0.9561   0.0140
  -5.500  -0.3139   0.02589   0.02006  -0.0720   0.9529   0.0138
  -5.250  -0.2859   0.02270   0.01632  -0.0725   0.9476   0.0141
  -5.000  -0.2552   0.02029   0.01345  -0.0734   0.9437   0.0149
  -4.750  -0.2227   0.01840   0.01119  -0.0744   0.9409   0.0158
  -4.500  -0.1889   0.01731   0.00981  -0.0758   0.9386   0.0179
  -4.250  -0.1611   0.01606   0.00836  -0.0759   0.9334   0.0195
  -4.000  -0.1312   0.01475   0.00695  -0.0765   0.9295   0.0209
  -3.750  -0.0989   0.01390   0.00603  -0.0777   0.9264   0.0233
  -3.500  -0.0686   0.01324   0.00527  -0.0784   0.9222   0.0265
  -3.250  -0.0397   0.01269   0.00468  -0.0788   0.9174   0.0347
  -3.000  -0.0086   0.01216   0.00408  -0.0797   0.9138   0.0483
  -2.750   0.0232   0.01169   0.00369  -0.0808   0.9106   0.0808
  -2.500   0.0487   0.01114   0.00344  -0.0808   0.9049   0.1566
  -2.250   0.0754   0.01024   0.00320  -0.0813   0.9004   0.3433
  -2.000   0.0967   0.00923   0.00325  -0.0803   0.8963   0.6301
  -1.750   0.1191   0.00916   0.00336  -0.0787   0.8906   0.7323
  -1.500   0.1458   0.00918   0.00338  -0.0781   0.8865   0.7758
  -1.250   0.1728   0.00920   0.00339  -0.0776   0.8830   0.8060
  -1.000   0.1934   0.00926   0.00349  -0.0755   0.8775   0.8415
  -0.750   0.2153   0.00926   0.00351  -0.0736   0.8732   0.8720
  -0.500   0.2423   0.00925   0.00346  -0.0732   0.8699   0.8870
  -0.250   0.2663   0.00926   0.00346  -0.0723   0.8645   0.8965
   0.000   0.2942   0.00925   0.00342  -0.0723   0.8601   0.9036
   0.250   0.3240   0.00925   0.00339  -0.0727   0.8565   0.9111
   0.500   0.3506   0.00927   0.00341  -0.0725   0.8510   0.9180
   0.750   0.3797   0.00928   0.00341  -0.0729   0.8462   0.9256
   1.000   0.4116   0.00927   0.00340  -0.0737   0.8415   0.9324
   1.250   0.4405   0.00928   0.00344  -0.0740   0.8342   0.9412
   1.500   0.4745   0.00927   0.00345  -0.0752   0.8283   0.9490
   1.750   0.5067   0.00926   0.00349  -0.0762   0.8190   0.9586
   2.000   0.5405   0.00923   0.00349  -0.0774   0.8078   0.9693
   2.250   0.5743   0.00916   0.00343  -0.0786   0.7925   0.9832
   2.500   0.6040   0.00912   0.00342  -0.0788   0.7743   1.0000
   2.750   0.6260   0.00913   0.00344  -0.0775   0.7532   1.0000
   3.000   0.6500   0.00915   0.00344  -0.0765   0.7302   1.0000
   3.250   0.6735   0.00921   0.00348  -0.0755   0.7008   1.0000
   3.500   0.6965   0.00932   0.00351  -0.0743   0.6568   1.0000
   3.750   0.7136   0.00975   0.00353  -0.0717   0.5550   1.0000
   4.000   0.7233   0.01074   0.00384  -0.0682   0.4258   1.0000
   4.250   0.7347   0.01182   0.00434  -0.0654   0.3077   1.0000
   4.500   0.7509   0.01271   0.00484  -0.0636   0.2238   1.0000
   4.750   0.7686   0.01357   0.00537  -0.0621   0.1546   1.0000
   5.000   0.7870   0.01442   0.00592  -0.0608   0.1010   1.0000
   5.250   0.8075   0.01510   0.00646  -0.0597   0.0717   1.0000
   5.500   0.8290   0.01569   0.00709  -0.0588   0.0560   1.0000
   5.750   0.8502   0.01633   0.00775  -0.0577   0.0448   1.0000
   6.000   0.8703   0.01712   0.00855  -0.0565   0.0366   1.0000
   6.250   0.8911   0.01782   0.00932  -0.0554   0.0303   1.0000
   6.500   0.9096   0.01881   0.01036  -0.0539   0.0261   1.0000
   6.750   0.9294   0.01971   0.01141  -0.0525   0.0237   1.0000
   7.000   0.9497   0.02055   0.01235  -0.0514   0.0204   1.0000
   7.250   0.9669   0.02194   0.01383  -0.0499   0.0171   1.0000
   7.500   0.9887   0.02263   0.01469  -0.0490   0.0142   1.0000
   7.750   1.0091   0.02343   0.01557  -0.0480   0.0115   1.0000
   8.000   1.0242   0.02582   0.01812  -0.0462   0.0099   1.0000
   8.250   1.0439   0.02756   0.02013  -0.0450   0.0092   1.0000
   8.500   1.0623   0.02977   0.02266  -0.0436   0.0086   1.0000
   8.750   1.0782   0.03238   0.02565  -0.0419   0.0080   1.0000
   9.000   1.0903   0.03533   0.02901  -0.0398   0.0077   1.0000
   9.250   1.0975   0.03862   0.03274  -0.0371   0.0075   1.0000
   9.500   1.0992   0.04218   0.03673  -0.0340   0.0074   1.0000
   9.750   1.0947   0.04596   0.04093  -0.0305   0.0073   1.0000
  10.000   1.0831   0.04959   0.04491  -0.0263   0.0073   1.0000
  10.250   1.0677   0.05321   0.04883  -0.0224   0.0072   1.0000
  10.500   1.0487   0.05726   0.05316  -0.0193   0.0073   1.0000
  10.750   1.0277   0.06174   0.05788  -0.0175   0.0074   1.0000
  11.000   1.0064   0.06666   0.06300  -0.0170   0.0074   1.0000
  11.250   0.9825   0.07262   0.06915  -0.0182   0.0075   1.0000
  11.500   0.9594   0.07949   0.07618  -0.0214   0.0076   1.0000
  11.750   0.9357   0.08846   0.08529  -0.0272   0.0078   1.0000
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