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GOE 314 (HANSA-BRANDENBURG) AIRFOIL (goe314-il) Xfoil prediction polar at RE=100,000 Ncrit=9


Details Polar file
Airfoil: GOE 314 (HANSA-BRANDENBURG) AIRFOIL (goe314-il)
Reynolds number: 100,000
Max Cl/Cd: 48.7 at α=6.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe314-il-100000.txt
Download as CSV file: xf-goe314-il-100000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 314 (HANSA-BRANDENBURG) AIRFOIL             
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.100 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
  -7.750  -0.3048   0.09454   0.08966  -0.0231   1.0000   0.0656
  -7.500  -0.3080   0.09266   0.08787  -0.0231   1.0000   0.0669
  -7.250  -0.3141   0.09123   0.08654  -0.0240   1.0000   0.0682
  -7.000  -0.3183   0.09057   0.08595  -0.0285   1.0000   0.0692
  -6.750  -0.3184   0.09010   0.08545  -0.0334   1.0000   0.0696
  -6.500  -0.3163   0.08530   0.08076  -0.0310   1.0000   0.0702
  -6.250  -0.3137   0.08113   0.07670  -0.0261   1.0000   0.0714
  -6.000  -0.3133   0.07858   0.07421  -0.0234   1.0000   0.0727
  -5.750  -0.3146   0.07653   0.07222  -0.0216   1.0000   0.0744
  -5.500  -0.3161   0.07463   0.07035  -0.0204   1.0000   0.0762
  -5.250  -0.3158   0.07270   0.06844  -0.0200   1.0000   0.0782
  -5.000  -0.3095   0.07106   0.06674  -0.0219   1.0000   0.0811
  -4.750  -0.2916   0.07054   0.06589  -0.0279   1.0000   0.0832
  -4.500  -0.2917   0.06636   0.06187  -0.0251   1.0000   0.0839
  -4.250  -0.2663   0.06211   0.05768  -0.0272   0.9944   0.0864
  -4.000  -0.2237   0.05842   0.05388  -0.0337   0.9856   0.0920
  -3.750  -0.1739   0.05462   0.04980  -0.0423   0.9757   0.0989
  -3.500  -0.1358   0.05120   0.04634  -0.0466   0.9666   0.1051
  -3.250  -0.0855   0.04776   0.04261  -0.0538   0.9575   0.1135
  -3.000  -0.0383   0.04591   0.04038  -0.0592   0.9455   0.1260
  -2.750  -0.0064   0.04190   0.03652  -0.0617   0.9351   0.1318
  -2.500   0.0428   0.03899   0.03344  -0.0670   0.9274   0.1483
  -2.250   0.0837   0.03680   0.03103  -0.0706   0.9148   0.1740
  -2.000   0.1242   0.03447   0.02860  -0.0738   0.9033   0.2045
  -1.750   0.1625   0.03153   0.02570  -0.0764   0.8926   0.2392
  -1.250   0.2288   0.02693   0.02109  -0.0785   0.8644   0.3473
  -1.000   0.2564   0.02486   0.01904  -0.0779   0.8452   0.3847
  -0.750   0.2860   0.02323   0.01730  -0.0775   0.8241   0.4137
  -0.500   0.3235   0.02210   0.01581  -0.0785   0.8028   0.4068
  -0.250   0.3926   0.02277   0.01482  -0.0811   0.7806   0.1698
   0.000   0.4236   0.02168   0.01329  -0.0797   0.7568   0.1367
   0.250   0.4534   0.02097   0.01215  -0.0785   0.7349   0.1235
   0.500   0.4791   0.02029   0.01127  -0.0773   0.7106   0.1232
   0.750   0.5062   0.01960   0.01037  -0.0763   0.6897   0.1220
   1.000   0.5327   0.01903   0.00963  -0.0752   0.6692   0.1203
   1.250   0.5588   0.01862   0.00908  -0.0742   0.6494   0.1202
   1.500   0.5849   0.01831   0.00863  -0.0733   0.6314   0.1228
   1.750   0.6101   0.01791   0.00821  -0.0723   0.6145   0.1293
   2.000   0.6362   0.01772   0.00792  -0.0714   0.5982   0.1355
   2.250   0.6617   0.01760   0.00766  -0.0705   0.5822   0.1434
   2.500   0.6870   0.01755   0.00755  -0.0697   0.5669   0.1638
   2.750   0.7377   0.01584   0.00739  -0.0739   0.5494   1.0000
   3.000   0.7619   0.01620   0.00745  -0.0728   0.5357   1.0000
   3.250   0.7859   0.01659   0.00766  -0.0719   0.5227   1.0000
   3.500   0.8104   0.01700   0.00788  -0.0710   0.5107   1.0000
   3.750   0.8350   0.01741   0.00814  -0.0702   0.4989   1.0000
   4.000   0.8582   0.01783   0.00854  -0.0693   0.4866   1.0000
   4.250   0.8820   0.01828   0.00893  -0.0684   0.4749   1.0000
   4.500   0.9065   0.01873   0.00927  -0.0676   0.4639   1.0000
   4.750   0.9301   0.01917   0.00966  -0.0667   0.4523   1.0000
   5.000   0.9529   0.01966   0.01018  -0.0658   0.4406   1.0000
   5.250   0.9768   0.02018   0.01065  -0.0650   0.4301   1.0000
   5.500   1.0011   0.02064   0.01102  -0.0642   0.4193   1.0000
   5.750   1.0229   0.02112   0.01158  -0.0631   0.4072   1.0000
   6.000   1.0455   0.02161   0.01209  -0.0622   0.3958   1.0000
   6.250   1.0695   0.02202   0.01241  -0.0614   0.3852   1.0000
   6.500   1.0914   0.02241   0.01284  -0.0603   0.3735   1.0000
   6.750   1.1128   0.02292   0.01345  -0.0592   0.3628   1.0000
   7.000   1.1375   0.02340   0.01384  -0.0586   0.3546   1.0000
   7.250   1.1581   0.02398   0.01460  -0.0574   0.3452   1.0000
   7.500   1.1820   0.02453   0.01513  -0.0568   0.3379   1.0000
   7.750   1.2027   0.02510   0.01589  -0.0556   0.3295   1.0000
   8.000   1.2268   0.02565   0.01642  -0.0550   0.3230   1.0000
   8.250   1.2464   0.02629   0.01729  -0.0538   0.3153   1.0000
   8.500   1.2720   0.02671   0.01762  -0.0534   0.3092   1.0000
   8.750   1.2893   0.02748   0.01874  -0.0519   0.3021   1.0000
   9.000   1.3124   0.02795   0.01926  -0.0512   0.2962   1.0000
   9.250   1.3319   0.02861   0.02012  -0.0500   0.2897   1.0000
   9.500   1.3521   0.02900   0.02065  -0.0488   0.2823   1.0000
   9.750   1.3698   0.02928   0.02110  -0.0473   0.2732   1.0000
  10.000   1.3893   0.02917   0.02099  -0.0458   0.2627   1.0000
  10.250   1.4026   0.02911   0.02105  -0.0435   0.2499   1.0000
  10.500   1.4113   0.02904   0.02108  -0.0407   0.2344   1.0000
  10.750   1.4172   0.02930   0.02152  -0.0375   0.2184   1.0000
  11.000   1.4207   0.02982   0.02227  -0.0342   0.1998   1.0000
  11.250   1.4183   0.03063   0.02312  -0.0302   0.1787   1.0000
  11.500   1.4115   0.03199   0.02449  -0.0261   0.1529   1.0000
  11.750   1.4011   0.03404   0.02645  -0.0225   0.1249   1.0000
  12.000   1.3880   0.03671   0.02899  -0.0196   0.1060   1.0000
  12.250   1.3724   0.03999   0.03217  -0.0176   0.0957   1.0000
  12.500   1.3565   0.04373   0.03588  -0.0164   0.0892   1.0000
  12.750   1.3408   0.04784   0.04002  -0.0158   0.0839   1.0000
  13.000   1.3268   0.05210   0.04433  -0.0158   0.0796   1.0000
  13.250   1.3127   0.05646   0.04861  -0.0157   0.0754   1.0000
  13.500   1.3066   0.06015   0.05241  -0.0157   0.0712   1.0000
  13.750   1.3085   0.06261   0.05469  -0.0142   0.0664   1.0000
  14.000   1.3202   0.06444   0.05658  -0.0122   0.0623   1.0000
  14.250   1.3261   0.06709   0.05933  -0.0114   0.0589   1.0000
  14.500   1.3639   0.06805   0.06006  -0.0080   0.0537   1.0000
  14.750   1.3574   0.07183   0.06413  -0.0084   0.0528   1.0000
  15.000   1.3537   0.07571   0.06827  -0.0088   0.0520   1.0000
  15.250   1.3468   0.08005   0.07287  -0.0097   0.0513   1.0000
  15.500   1.3380   0.08475   0.07782  -0.0109   0.0509   1.0000
  15.750   1.3258   0.08999   0.08331  -0.0127   0.0506   1.0000
  16.000   1.3106   0.09581   0.08938  -0.0152   0.0505   1.0000
  16.250   1.2919   0.10238   0.09620  -0.0185   0.0505   1.0000
  16.500   1.2705   0.10972   0.10377  -0.0226   0.0508   1.0000
  16.750   1.2462   0.11802   0.11230  -0.0277   0.0511   1.0000
  17.000   1.2197   0.12731   0.12180  -0.0336   0.0518   1.0000
  17.250   1.1908   0.13776   0.13243  -0.0405   0.0525   1.0000
  17.500   1.1617   0.14917   0.14397  -0.0479   0.0534   1.0000
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