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GOE 155 (SSW D.1) AIRFOIL (goe155-il)

GOE 155 (SSW D.1) AIRFOIL - Gottingen 155 (SSW D.1) airfoil


Airfoil goe155-il
Details Dat file Parser  
(goe155-il) GOE 155 (SSW D.1) AIRFOIL
Gottingen 155 (SSW D.1) airfoil
Max thickness 7% at 29.9% chord.
Max camber 5.3% at 39.9% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 155 (SSW D.1) AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0123900 0.0171800
 0.0248400 0.0250600
 0.0497600 0.0384100
 0.0746900 0.0490700
 0.0996300 0.0586300
 0.1495400 0.0722400
 0.1995000 0.0796600
 0.2994500 0.0869900
 0.3994600 0.0865200
 0.4994900 0.0815500
 0.5995500 0.0714800
 0.6996500 0.0563100
 0.7997600 0.0387400
 0.8998800 0.0192700
 0.9499400 0.0095800
 1.0000000 0.0020000

 0.0000000 0.0000000
 0.0125500 -.0082200
 0.0250500 -.0075400
 0.0500400 -.0057800
 0.0750100 -.0023300
 0.1000000 0.0000300
 0.1499600 0.0064400
 0.1999300 0.0117600
 0.2998900 0.0167900
 0.3998800 0.0191200
 0.4998800 0.0191500
 0.5998900 0.0175800
 0.6999199 0.0127100
 0.7999500 0.0078400
 0.9000000 0.0001700
 0.9500100 -.0012100
 1.0000000 -.0020000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 155 (SSW D.1) AIRFOIL (goe155-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe155-il50,000940.1 at α=8.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe155-il50,000542.4 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   goe155-il100,000959.8 at α=5.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe155-il100,000561.6 at α=4.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe155-il200,000982.6 at α=4.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe155-il200,000578.6 at α=4.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe155-il500,0009107.7 at α=3°Mach=0 Ncrit=9Xfoil predictionDetails
   goe155-il500,000598.6 at α=4.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe155-il1,000,0009123.2 at α=4.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe155-il1,000,0005111 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
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