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GOE 315 (HANSA-BRANDENBURG III.5) AIRFOIL (goe315-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: GOE 315 (HANSA-BRANDENBURG III.5) AIRFOIL (goe315-il)
Reynolds number: 200,000
Max Cl/Cd: 69.49 at α=4.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe315-il-200000-n5.txt
Download as CSV file: xf-goe315-il-200000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 315 (HANSA-BRANDENBURG III.5) AIRFOIL       
  
 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
  ------ -------- --------- --------- -------- -------- --------
  -8.000  -0.3457   0.08861   0.08511  -0.0212   1.0000   0.0267
  -7.750  -0.3443   0.08597   0.08252  -0.0217   1.0000   0.0272
  -7.500  -0.3453   0.08344   0.08005  -0.0220   1.0000   0.0279
  -7.250  -0.3433   0.08065   0.07731  -0.0238   1.0000   0.0292
  -7.000  -0.3378   0.07724   0.07391  -0.0317   1.0000   0.0306
  -6.750  -0.3284   0.07361   0.07023  -0.0359   1.0000   0.0309
  -6.500  -0.3044   0.06890   0.06542  -0.0418   0.9883   0.0309
  -6.250  -0.2813   0.06331   0.05978  -0.0463   0.9723   0.0312
  -6.000  -0.2605   0.05958   0.05607  -0.0481   0.9516   0.0319
  -5.750  -0.2306   0.05618   0.05260  -0.0521   0.9265   0.0332
  -5.500  -0.1930   0.05241   0.04865  -0.0583   0.8991   0.0364
  -5.250  -0.1460   0.04892   0.04454  -0.0654   0.8690   0.0390
  -5.000  -0.1190   0.04581   0.04111  -0.0671   0.8441   0.0391
  -4.750  -0.1037   0.04111   0.03636  -0.0681   0.8238   0.0401
  -4.500  -0.0847   0.03911   0.03428  -0.0681   0.8055   0.0415
  -4.250  -0.0631   0.03725   0.03225  -0.0682   0.7895   0.0436
  -4.000  -0.0311   0.03657   0.03097  -0.0681   0.7752   0.0492
  -3.750  -0.0068   0.03487   0.02894  -0.0677   0.7624   0.0494
  -3.500   0.0132   0.03106   0.02493  -0.0678   0.7512   0.0502
  -3.250   0.0346   0.02885   0.02263  -0.0676   0.7399   0.0513
  -2.750   0.0874   0.02430   0.01730  -0.0659   0.7184   0.0386
  -2.500   0.1118   0.02254   0.01530  -0.0654   0.7082   0.0379
  -2.250   0.1372   0.02111   0.01361  -0.0648   0.6973   0.0376
  -2.000   0.1632   0.01991   0.01217  -0.0643   0.6864   0.0377
  -1.750   0.1899   0.01925   0.01121  -0.0636   0.6757   0.0388
  -1.500   0.2160   0.01820   0.00996  -0.0630   0.6647   0.0387
  -1.250   0.2423   0.01724   0.00881  -0.0625   0.6532   0.0385
  -1.000   0.2687   0.01644   0.00785  -0.0620   0.6415   0.0385
  -0.750   0.2950   0.01579   0.00703  -0.0615   0.6284   0.0386
  -0.500   0.3211   0.01524   0.00633  -0.0609   0.6138   0.0388
  -0.250   0.3471   0.01479   0.00573  -0.0602   0.5976   0.0390
   0.000   0.3725   0.01416   0.00502  -0.0596   0.5823   0.0399
   0.250   0.3978   0.01376   0.00457  -0.0590   0.5695   0.0415
   0.500   0.4237   0.01348   0.00427  -0.0585   0.5591   0.0428
   0.750   0.4496   0.01321   0.00397  -0.0580   0.5505   0.0433
   1.000   0.4754   0.01300   0.00374  -0.0575   0.5422   0.0440
   1.250   0.5013   0.01284   0.00355  -0.0570   0.5340   0.0449
   1.500   0.5272   0.01274   0.00341  -0.0565   0.5254   0.0460
   1.750   0.5534   0.01267   0.00330  -0.0560   0.5169   0.0475
   2.000   0.5795   0.01267   0.00323  -0.0556   0.5084   0.0493
   2.250   0.6058   0.01262   0.00320  -0.0552   0.5002   0.0549
   2.500   0.6320   0.01266   0.00320  -0.0548   0.4921   0.0607
   2.750   0.6580   0.01256   0.00329  -0.0543   0.4833   0.1200
   3.250   0.7309   0.01101   0.00349  -0.0582   0.4526   1.0000
   3.500   0.7555   0.01117   0.00356  -0.0575   0.4329   1.0000
   3.750   0.7798   0.01136   0.00364  -0.0568   0.4093   1.0000
   4.000   0.8036   0.01161   0.00374  -0.0560   0.3811   1.0000
   4.250   0.8270   0.01191   0.00390  -0.0551   0.3531   1.0000
   4.500   0.8505   0.01224   0.00410  -0.0544   0.3289   1.0000
   4.750   0.8735   0.01262   0.00435  -0.0536   0.3061   1.0000
   5.000   0.8966   0.01300   0.00464  -0.0528   0.2844   1.0000
   5.250   0.9200   0.01337   0.00493  -0.0521   0.2684   1.0000
   5.500   0.9434   0.01374   0.00525  -0.0514   0.2547   1.0000
   5.750   0.9666   0.01412   0.00559  -0.0507   0.2415   1.0000
   6.000   0.9897   0.01451   0.00595  -0.0499   0.2288   1.0000
   6.250   1.0128   0.01489   0.00631  -0.0492   0.2167   1.0000
   6.500   1.0359   0.01528   0.00669  -0.0485   0.2032   1.0000
   6.750   1.0589   0.01566   0.00709  -0.0478   0.1898   1.0000
   7.000   1.0814   0.01610   0.00751  -0.0470   0.1732   1.0000
   7.250   1.1018   0.01672   0.00800  -0.0460   0.1385   1.0000
   7.500   1.1137   0.01820   0.00903  -0.0441   0.0778   1.0000
   7.750   1.1316   0.01908   0.00984  -0.0428   0.0531   1.0000
   8.000   1.1497   0.01989   0.01060  -0.0415   0.0459   1.0000
   8.250   1.1682   0.02063   0.01137  -0.0403   0.0429   1.0000
   8.500   1.1864   0.02135   0.01215  -0.0390   0.0412   1.0000
   8.750   1.2043   0.02206   0.01300  -0.0377   0.0401   1.0000
   9.000   1.2207   0.02284   0.01390  -0.0363   0.0389   1.0000
   9.250   1.2349   0.02373   0.01490  -0.0346   0.0375   1.0000
   9.500   1.2467   0.02473   0.01600  -0.0327   0.0364   1.0000
   9.750   1.2546   0.02585   0.01721  -0.0302   0.0356   1.0000
  10.000   1.2567   0.02715   0.01861  -0.0271   0.0347   1.0000
  10.250   1.2586   0.02855   0.02008  -0.0244   0.0340   1.0000
  10.500   1.2644   0.02981   0.02147  -0.0223   0.0333   1.0000
  10.750   1.2690   0.03128   0.02306  -0.0205   0.0325   1.0000
  11.000   1.2725   0.03296   0.02485  -0.0190   0.0318   1.0000
  11.250   1.2756   0.03483   0.02681  -0.0178   0.0311   1.0000
  11.500   1.2782   0.03687   0.02896  -0.0168   0.0303   1.0000
  11.750   1.2803   0.03907   0.03123  -0.0161   0.0295   1.0000
  12.000   1.2819   0.04141   0.03361  -0.0154   0.0288   1.0000
  12.250   1.2826   0.04393   0.03613  -0.0145   0.0279   1.0000
  12.500   1.2875   0.04608   0.03839  -0.0139   0.0273   1.0000
  12.750   1.2923   0.04827   0.04074  -0.0137   0.0267   1.0000
  13.000   1.2963   0.05060   0.04321  -0.0135   0.0258   1.0000
  13.250   1.2993   0.05308   0.04583  -0.0135   0.0249   1.0000
  13.500   1.3024   0.05560   0.04846  -0.0134   0.0242   1.0000
  13.750   1.3051   0.05820   0.05114  -0.0135   0.0235   1.0000
  14.000   1.3088   0.06072   0.05372  -0.0134   0.0229   1.0000
  14.250   1.3158   0.06289   0.05585  -0.0128   0.0221   1.0000
  14.500   1.3137   0.06625   0.05945  -0.0136   0.0217   1.0000
  14.750   1.3114   0.06976   0.06318  -0.0145   0.0211   1.0000
  15.000   1.3080   0.07351   0.06713  -0.0156   0.0204   1.0000
  15.250   1.3049   0.07731   0.07110  -0.0168   0.0198   1.0000
  15.500   1.3016   0.08126   0.07521  -0.0182   0.0193   1.0000
  15.750   1.2981   0.08532   0.07942  -0.0198   0.0188   1.0000
  16.000   1.2944   0.08951   0.08373  -0.0214   0.0185   1.0000
  16.250   1.2905   0.09379   0.08814  -0.0232   0.0182   1.0000
  16.500   1.2874   0.09801   0.09245  -0.0251   0.0179   1.0000
  16.750   1.2850   0.10214   0.09666  -0.0268   0.0176   1.0000
  17.000   1.2738   0.10823   0.10297  -0.0299   0.0174   1.0000
  17.250   1.2597   0.11515   0.11014  -0.0337   0.0171   1.0000
  17.500   1.2461   0.12221   0.11743  -0.0377   0.0169   1.0000
  17.750   1.2304   0.13003   0.12547  -0.0425   0.0166   1.0000
  18.000   1.2150   0.13797   0.13361  -0.0473   0.0166   1.0000
  18.250   1.1972   0.14691   0.14276  -0.0529   0.0164   1.0000
  18.500   1.1770   0.15686   0.15289  -0.0593   0.0164   1.0000
  18.750   1.1524   0.16864   0.16485  -0.0669   0.0165   1.0000
  19.000   1.1157   0.18531   0.18167  -0.0774   0.0169   1.0000
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