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GOE 173 (ALBATROS 6020) AIRFOIL (goe173-il)

GOE 173 (ALBATROS 6020) AIRFOIL - Gottingen 173 (Albatros 6020) airfoil


Airfoil goe173-il
Details Dat file Parser  
(goe173-il) GOE 173 (ALBATROS 6020) AIRFOIL
Gottingen 173 (Albatros 6020) airfoil
Max thickness 7.8% at 20% chord.
Max camber 5.9% at 40% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 173 (ALBATROS 6020) AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0124100 0.0195600
 0.0248600 0.0311100
 0.0497800 0.0472300
 0.0747300 0.0593400
 0.0996800 0.0689600
 0.1496200 0.0836900
 0.1995800 0.0915200
 0.2995600 0.0964800
 0.3995600 0.0953400
 0.4996000 0.0878000
 0.5996500 0.0755600
 0.6997200 0.0599200
 0.7998000 0.0429800
 0.8998900 0.0248400
 0.9499400 0.0139700
 1.0000000 0.0009000

 0.0000000 0.0000000
 0.0125300 -.0054400
 0.0250200 -.0043800
 0.0500100 -.0019700
 0.0750000 0.0008400
 0.0999800 0.0036600
 0.1499600 0.0091900
 0.1999400 0.0139200
 0.2999100 0.0198800
 0.3998900 0.0228400
 0.4998900 0.0230000
 0.5999100 0.0205600
 0.6999199 0.0167200
 0.7999500 0.0115800
 0.8999700 0.0056400
 0.9499900 0.0028700
 1.0000000 -.0009000
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Lednicer format dat file
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Polars for GOE 173 (ALBATROS 6020) AIRFOIL (goe173-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe173-il50,000933.1 at α=10.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe173-il50,000542.2 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe173-il100,000956.9 at α=4°Mach=0 Ncrit=9Xfoil predictionDetails
   goe173-il100,000560.3 at α=4°Mach=0 Ncrit=5Xfoil predictionDetails
   goe173-il200,000977.7 at α=3°Mach=0 Ncrit=9Xfoil predictionDetails
   goe173-il200,000575.7 at α=2.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe173-il500,0009101.6 at α=7°Mach=0 Ncrit=9Xfoil predictionDetails
   goe173-il500,0005101.5 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   goe173-il1,000,0009124.6 at α=6.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe173-il1,000,0005122.3 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
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