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GOE 321 (HANSA-BRANDENBURG III.1) AIRFOIL (goe321-il)

GOE 321 (HANSA-BRANDENBURG III.1) AIRFOIL - Gottingen 321 (Hansa-Brandenburg III.1) airfoil


Airfoil goe321-il
Details Dat file Parser  
(goe321-il) GOE 321 (HANSA-BRANDENBURG III.1) AIRFOIL
Gottingen 321 (Hansa-Brandenburg III.1) airfoil
Max thickness 11.2% at 29.9% chord.
Max camber 5.1% at 29.9% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 321 (HANSA-BRANDENBURG III.1) AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0121400 0.0256700
 0.0244800 0.0378400
 0.0492200 0.0559800
 0.0740400 0.0695300
 0.0988900 0.0800700
 0.1487200 0.0924600
 0.1986100 0.1004500
 0.2985100 0.1072300
 0.3985400 0.1055200
 0.4987000 0.0941100
 0.5989100 0.0784900
 0.6991900 0.0585800
 0.7994500 0.0397700
 0.8997100 0.0209600
 0.9498500 0.0109600
 1.0000000 0.0021500

 0.0000000 0.0000000
 0.0127000 -.0137200
 0.0252200 -.0156500
 0.0502100 -.0148000
 0.0751800 -.0128600
 0.1001500 -.0111100
 0.1501200 -.0086200
 0.2000900 -.0067300
 0.3000600 -.0043400
 0.4000500 -.0036600
 0.5000700 -.0047700
 0.6000700 -.0051900
 0.7000700 -.0047000
 0.8000500 -.0038200
 0.9000500 -.0035300
 0.9500400 -.0028400
 1.0000000 -.0021500
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Lednicer format dat file
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Polars for GOE 321 (HANSA-BRANDENBURG III.1) AIRFOIL (goe321-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe321-il50,000920.9 at α=7.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe321-il50,000534.1 at α=7.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe321-il100,000954.3 at α=7°Mach=0 Ncrit=9Xfoil predictionDetails
   goe321-il100,000555.7 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   goe321-il200,000977.7 at α=6°Mach=0 Ncrit=9Xfoil predictionDetails
   goe321-il200,000573.7 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe321-il500,0009105.3 at α=4.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe321-il500,000590.3 at α=3°Mach=0 Ncrit=5Xfoil predictionDetails
   goe321-il1,000,0009120.9 at α=3.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe321-il1,000,0005104.6 at α=8.25°Mach=0 Ncrit=5Xfoil predictionDetails
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