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GOE 177 AIRFOIL (goe177-il)

GOE 177 AIRFOIL - Gottingen 177 airfoil


Airfoil goe177-il
Details Dat file Parser  
(goe177-il) GOE 177 AIRFOIL
Gottingen 177 airfoil
Max thickness 7.7% at 20% chord.
Max camber 5% at 40% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 177 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0125000 0.0151100
 0.0250000 0.0267200
 0.0500000 0.0394500
 0.0750000 0.0516800
 0.1000000 0.0599000
 0.1500000 0.0733500
 0.2000000 0.0818000
 0.3000000 0.0867000
 0.4000000 0.0836000
 0.5000000 0.0755000
 0.6000000 0.0644000
 0.7000000 0.0513000
 0.8000000 0.0372000
 0.9000000 0.0211000
 0.9500000 0.0115500
 1.0000000 0.0020000

 0.0000000 0.0000000
 0.0125000 -.0058900
 0.0250000 -.0077700
 0.0500000 -.0085500
 0.0750000 -.0063200
 0.1000000 -.0041000
 0.1500000 0.0003500
 0.2000000 0.0048000
 0.3000000 0.0127000
 0.4000000 0.0176000
 0.5000000 0.0175000
 0.6000000 0.0154000
 0.7000000 0.0123000
 0.8000000 0.0082000
 0.9000000 0.0041000
 0.9500000 0.0025500
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 177 AIRFOIL (goe177-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe177-il50,000939.1 at α=8.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe177-il50,000541.5 at α=6.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe177-il100,000958.3 at α=7.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe177-il100,000557.8 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe177-il200,000974.7 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe177-il200,000571.5 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe177-il500,000991.2 at α=3.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe177-il500,000579.8 at α=2.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe177-il1,000,000999.9 at α=2.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe177-il1,000,000589.6 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
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