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GOE 320 (HANSA-BRANDENBURG II.1) AIRFOIL (goe320-il)

GOE 320 (HANSA-BRANDENBURG II.1) AIRFOIL - Gottingen 320 (Hansa-Brandenburg II.1) airfoil


Airfoil goe320-il
Details Dat file Parser  
(goe320-il) GOE 320 (HANSA-BRANDENBURG II.1) AIRFOIL
Gottingen 320 (Hansa-Brandenburg II.1) airfoil
Max thickness 12.3% at 29.8% chord.
Max camber 6.2% at 29.8% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 320 (HANSA-BRANDENBURG II.1) AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0119100 0.0319200
 0.0241400 0.0462500
 0.0487200 0.0689000
 0.0734200 0.0849600
 0.0982000 0.0970200
 0.1479500 0.1106400
 0.1977900 0.1189700
 0.2977100 0.1235200
 0.3977400 0.1215800
 0.4978900 0.1139400
 0.5981900 0.0978000
 0.6985800 0.0764600
 0.7990400 0.0518200
 0.8995000 0.0271900
 0.9497300 0.0146200
 1.0000000 0.0026500

 0.0000000 0.0000000
 0.0128700 -.0188600
 0.0253800 -.0207300
 0.0503500 -.0187700
 0.0752900 -.0158000
 0.1002300 -.0126400
 0.1501300 -.0068200
 0.2000600 -.0034900
 0.3000000 0.0002600
 0.3999800 0.0012200
 0.4999800 0.0012700
 0.5999900 0.0005300
 0.7000100 -.0003100
 0.8000200 -.0010600
 0.9000400 -.0020000
 0.9500500 -.0025800
 1.0000000 -.0026500
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Lednicer format dat file
Selig format dat file

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Polars for GOE 320 (HANSA-BRANDENBURG II.1) AIRFOIL (goe320-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe320-il50,000929.3 at α=6.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe320-il50,000533.6 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe320-il100,000952.3 at α=4°Mach=0 Ncrit=9Xfoil predictionDetails
   goe320-il100,000548.4 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe320-il200,000966.1 at α=3.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe320-il200,000563.1 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe320-il500,000989.2 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe320-il500,000585 at α=4.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe320-il1,000,0009109.1 at α=5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe320-il1,000,000598.3 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
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