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WORTMANN FX 77-080 (fx77080-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: WORTMANN FX 77-080 (fx77080-il)
Reynolds number: 500,000
Max Cl/Cd: 58.42 at α=4.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-fx77080-il-500000.txt
Download as CSV file: xf-fx77080-il-500000.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 =     0.500 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -12.250  -0.6290   0.09078   0.08857  -0.0048   1.0000   0.0176
 -12.000  -0.9149   0.06235   0.05974  -0.0192   1.0000   0.0146
 -11.750  -0.9382   0.05360   0.05078  -0.0278   1.0000   0.0145
 -11.500  -0.9700   0.04669   0.04359  -0.0315   1.0000   0.0140
 -11.250  -0.9861   0.04320   0.03989  -0.0304   1.0000   0.0142
 -11.000  -1.0004   0.03988   0.03631  -0.0276   1.0000   0.0142
 -10.750  -1.0039   0.03692   0.03307  -0.0254   1.0000   0.0144
 -10.500  -1.0040   0.03392   0.02975  -0.0232   1.0000   0.0145
 -10.250  -0.9990   0.03129   0.02682  -0.0210   1.0000   0.0147
 -10.000  -0.9901   0.02899   0.02422  -0.0190   1.0000   0.0150
  -9.750  -0.9768   0.02723   0.02221  -0.0173   1.0000   0.0152
  -9.500  -0.9606   0.02591   0.02066  -0.0157   1.0000   0.0156
  -9.250  -0.9483   0.02357   0.01804  -0.0138   1.0000   0.0159
  -9.000  -0.9352   0.02136   0.01565  -0.0119   1.0000   0.0168
  -8.750  -0.9154   0.02056   0.01482  -0.0107   1.0000   0.0177
  -8.500  -0.8952   0.01972   0.01388  -0.0095   1.0000   0.0183
  -8.250  -0.8752   0.01877   0.01282  -0.0082   1.0000   0.0191
  -8.000  -0.8542   0.01801   0.01193  -0.0070   1.0000   0.0203
  -7.750  -0.8325   0.01737   0.01119  -0.0058   1.0000   0.0210
  -7.500  -0.8165   0.01576   0.00946  -0.0038   1.0000   0.0224
  -7.250  -0.7958   0.01507   0.00873  -0.0026   1.0000   0.0240
  -7.000  -0.7738   0.01458   0.00820  -0.0015   1.0000   0.0258
  -6.750  -0.7513   0.01415   0.00769  -0.0004   1.0000   0.0276
  -6.500  -0.7323   0.01326   0.00673   0.0013   1.0000   0.0301
  -6.250  -0.7112   0.01271   0.00617   0.0027   1.0000   0.0331
  -6.000  -0.6890   0.01232   0.00574   0.0038   1.0000   0.0360
  -5.750  -0.6686   0.01170   0.00510   0.0054   1.0000   0.0408
  -5.500  -0.6468   0.01132   0.00469   0.0066   1.0000   0.0461
  -5.250  -0.6258   0.01082   0.00422   0.0080   1.0000   0.0541
  -5.000  -0.6047   0.01040   0.00385   0.0094   1.0000   0.0679
  -4.750  -0.5836   0.01000   0.00357   0.0108   1.0000   0.0908
  -4.500  -0.5616   0.00974   0.00337   0.0119   1.0000   0.1112
  -4.250  -0.5396   0.00951   0.00319   0.0131   1.0000   0.1276
  -4.000  -0.5176   0.00931   0.00303   0.0143   1.0000   0.1421
  -3.750  -0.4957   0.00911   0.00288   0.0155   1.0000   0.1564
  -3.500  -0.4739   0.00892   0.00274   0.0168   1.0000   0.1714
  -3.250  -0.4522   0.00874   0.00260   0.0180   1.0000   0.1875
  -3.000  -0.4308   0.00854   0.00250   0.0193   1.0000   0.2101
  -2.750  -0.4099   0.00832   0.00241   0.0206   1.0000   0.2417
  -2.500  -0.3806   0.00800   0.00234   0.0200   0.9982   0.2968
  -2.250  -0.3447   0.00760   0.00225   0.0180   0.9942   0.3739
  -2.000  -0.3079   0.00718   0.00219   0.0159   0.9903   0.4608
  -1.750  -0.2730   0.00673   0.00211   0.0143   0.9848   0.5537
  -1.500  -0.2380   0.00635   0.00203   0.0128   0.9791   0.6338
  -1.250  -0.2011   0.00597   0.00196   0.0111   0.9734   0.7101
  -1.000  -0.1674   0.00564   0.00190   0.0103   0.9655   0.7806
  -0.750  -0.1243   0.00538   0.00184   0.0075   0.9598   0.8379
  -0.500  -0.0848   0.00523   0.00181   0.0055   0.9486   0.8783
  -0.250  -0.0439   0.00517   0.00181   0.0031   0.9381   0.9061
   0.000  -0.0002   0.00515   0.00180   0.0000   0.9245   0.9239
   0.250   0.0443   0.00517   0.00180  -0.0032   0.9042   0.9376
   0.500   0.0847   0.00524   0.00180  -0.0054   0.8747   0.9484
   0.750   0.1243   0.00538   0.00184  -0.0075   0.8374   0.9598
   1.000   0.1691   0.00565   0.00192  -0.0106   0.7831   0.9661
   1.250   0.2024   0.00598   0.00198  -0.0114   0.7110   0.9736
   1.500   0.2380   0.00634   0.00203  -0.0128   0.6343   0.9791
   1.750   0.2725   0.00674   0.00211  -0.0142   0.5513   0.9847
   2.000   0.3083   0.00718   0.00219  -0.0160   0.4608   0.9903
   2.250   0.3452   0.00760   0.00225  -0.0181   0.3738   0.9943
   2.500   0.3813   0.00800   0.00234  -0.0201   0.2967   0.9984
   2.750   0.4099   0.00832   0.00242  -0.0206   0.2413   1.0000
   3.000   0.4308   0.00854   0.00250  -0.0193   0.2094   1.0000
   3.250   0.4522   0.00874   0.00261  -0.0180   0.1874   1.0000
   3.500   0.4738   0.00893   0.00274  -0.0167   0.1706   1.0000
   3.750   0.4955   0.00913   0.00288  -0.0155   0.1553   1.0000
   4.000   0.5175   0.00931   0.00303  -0.0143   0.1419   1.0000
   4.250   0.5396   0.00951   0.00319  -0.0131   0.1278   1.0000
   4.500   0.5616   0.00974   0.00337  -0.0119   0.1112   1.0000
   4.750   0.5836   0.00999   0.00358  -0.0107   0.0917   1.0000
   5.000   0.6047   0.01039   0.00385  -0.0094   0.0686   1.0000
   5.250   0.6259   0.01082   0.00422  -0.0080   0.0544   1.0000
   5.500   0.6467   0.01132   0.00469  -0.0066   0.0460   1.0000
   5.750   0.6686   0.01170   0.00510  -0.0054   0.0408   1.0000
   6.000   0.6890   0.01232   0.00574  -0.0038   0.0360   1.0000
   6.250   0.7113   0.01269   0.00615  -0.0027   0.0329   1.0000
   6.500   0.7322   0.01327   0.00674  -0.0013   0.0299   1.0000
   6.750   0.7516   0.01410   0.00765   0.0003   0.0274   1.0000
   7.000   0.7741   0.01453   0.00815   0.0014   0.0255   1.0000
   7.250   0.7958   0.01507   0.00873   0.0026   0.0239   1.0000
   7.500   0.8163   0.01579   0.00948   0.0039   0.0223   1.0000
   7.750   0.8324   0.01740   0.01121   0.0059   0.0209   1.0000
   8.000   0.8542   0.01802   0.01195   0.0070   0.0201   1.0000
   8.250   0.8746   0.01893   0.01299   0.0083   0.0194   1.0000
   8.500   0.8952   0.01974   0.01391   0.0096   0.0184   1.0000
   8.750   0.9156   0.02050   0.01474   0.0107   0.0175   1.0000
   9.000   0.9352   0.02134   0.01562   0.0119   0.0167   1.0000
   9.250   0.9478   0.02369   0.01817   0.0138   0.0159   1.0000
   9.500   0.9616   0.02568   0.02043   0.0156   0.0155   1.0000
   9.750   0.9772   0.02716   0.02213   0.0172   0.0153   1.0000
  10.000   0.9895   0.02911   0.02436   0.0190   0.0150   1.0000
  10.250   0.9999   0.03115   0.02666   0.0209   0.0147   1.0000
  10.500   1.0051   0.03377   0.02959   0.0231   0.0144   1.0000
  10.750   1.0054   0.03675   0.03287   0.0253   0.0144   1.0000
  11.000   1.0023   0.03968   0.03609   0.0275   0.0140   1.0000
  11.250   0.9868   0.04315   0.03984   0.0303   0.0139   1.0000
  11.500   0.9624   0.04771   0.04466   0.0311   0.0143   1.0000
  11.750   0.9463   0.05246   0.04961   0.0284   0.0140   1.0000
  12.000   0.9131   0.06319   0.06060   0.0180   0.0144   1.0000
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