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GOE 322 (HANSA-BRANDENBURG IV.1) AIRFOIL (goe322-il)

GOE 322 (HANSA-BRANDENBURG IV.1) AIRFOIL - Gottingen 322 (Hansa-Brandenburg IV.1) airfoil


Airfoil goe322-il
Details Dat file Parser  
(goe322-il) GOE 322 (HANSA-BRANDENBURG IV.1) AIRFOIL
Gottingen 322 (Hansa-Brandenburg IV.1) airfoil
Max thickness 13.1% at 29.8% chord.
Max camber 6% at 29.8% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 322 (HANSA-BRANDENBURG IV.1) AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0121400 0.0246800
 0.0244300 0.0395500
 0.0491100 0.0612100
 0.0738700 0.0778700
 0.0986800 0.0909300
 0.1484500 0.1071500
 0.1983000 0.1173800
 0.2981800 0.1255200
 0.3982100 0.1234700
 0.4983700 0.1122300
 0.5986300 0.0941800
 0.6989800 0.0706400
 0.7993100 0.0474900
 0.8996300 0.0257400
 0.9497899 0.0142700
 1.0000000 0.0030000

 0.0000000 0.0000000
 0.0127000 -.0138200
 0.0252300 -.0158300
 0.0502400 -.0167700
 0.0752200 -.0154100
 0.1002000 -.0140500
 0.1501500 -.0103200
 0.2001200 -.0081000
 0.3000700 -.0051500
 0.4000600 -.0042000
 0.5000600 -.0041500
 0.6000600 -.0038000
 0.7000600 -.0038500
 0.8000500 -.0034000
 0.9000500 -.0033500
 0.9500500 -.0036200
 1.0000000 -.0030000
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Lednicer format dat file
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Polars for GOE 322 (HANSA-BRANDENBURG IV.1) AIRFOIL (goe322-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe322-il50,00099.2 at α=2.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe322-il50,000528.9 at α=6.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe322-il100,000949.9 at α=8°Mach=0 Ncrit=9Xfoil predictionDetails
   goe322-il100,000553.7 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   goe322-il200,000975.2 at α=6.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe322-il200,000573.7 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe322-il500,0009104.8 at α=4.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe322-il500,000595.7 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe322-il1,000,0009123.2 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe322-il1,000,0005114.2 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
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