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GOE 316 (HANSA-BRANDENBURG IV.5) AIRFOIL (goe316-il)

GOE 316 (HANSA-BRANDENBURG IV.5) AIRFOIL - Gottingen 316 (Hansa-Brandenburg IV.5) airfoil


Airfoil goe316-il
Details Dat file Parser  
(goe316-il) GOE 316 (HANSA-BRANDENBURG IV.5) AIRFOIL
Gottingen 316 (Hansa-Brandenburg IV.5) airfoil
Max thickness 9.1% at 29.9% chord.
Max camber 4.2% at 29.9% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 316 (HANSA-BRANDENBURG IV.5) AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0123000 0.0210200
 0.0247100 0.0308300
 0.0495800 0.0443700
 0.0744700 0.0556100
 0.0993900 0.0642400
 0.1492700 0.0769200
 0.1991900 0.0852900
 0.2991700 0.0878400
 0.3992000 0.0839900
 0.4992900 0.0749400
 0.5994000 0.0626900
 0.6995500 0.0472500
 0.7997000 0.0319000
 0.8998400 0.0170500
 0.9499100 0.0092200
 1.0000000 0.0021000

 0.0000000 0.0000000
 0.0126100 -.0104800
 0.0251000 -.0114500
 0.0500900 -.0090200
 0.0750600 -.0072800
 0.1000500 -.0056500
 0.1500300 -.0036700
 0.2000300 -.0032000
 0.3000300 -.0029500
 0.4000200 -.0025000
 0.5000300 -.0026500
 0.6000300 -.0027000
 0.7000300 -.0028500
 0.8000300 -.0029000
 0.9000200 -.0025500
 0.9500200 -.0025700
 1.0000000 -.0021000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 316 (HANSA-BRANDENBURG IV.5) AIRFOIL (goe316-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe316-il50,000923.4 at α=2.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe316-il50,000534.4 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe316-il100,000950.9 at α=10.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe316-il100,000552 at α=9.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe316-il200,000971.2 at α=9.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe316-il200,000572 at α=9°Mach=0 Ncrit=5Xfoil predictionDetails
   goe316-il500,0009100.5 at α=8.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe316-il500,000598.8 at α=7.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe316-il1,000,0009123.4 at α=7.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe316-il1,000,0005118.6 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
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