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GOE 670 AIRFOIL (goe670-il)

GOE 670 AIRFOIL - Gottingen 670 airfoil


Airfoil goe670-il
Details Dat file Parser  
(goe670-il) GOE 670 AIRFOIL
Gottingen 670 airfoil
Max thickness 9% at 30% chord.
Max camber 3.4% at 40% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 670 AIRFOIL
       15.       15.

 0.0000000 0.0000000
 0.0125000 0.0167700
 0.0250000 0.0250400
 0.0500000 0.0380700
 0.0750000 0.0471100
 0.1000000 0.0546500
 0.2000000 0.0703000
 0.3000000 0.0769500
 0.4000000 0.0786000
 0.5000000 0.0757500
 0.6000000 0.0674000
 0.7000000 0.0570500
 0.8000000 0.0417000
 0.9000000 0.0223500
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0125000 -.0147300
 0.0250000 -.0189600
 0.0500000 -.0219300
 0.0750000 -.0223900
 0.1000000 -.0213500
 0.2000000 -.0172000
 0.3000000 -.0130500
 0.4000000 -.0109000
 0.5000000 -.0097500
 0.6000000 -.0091000
 0.7000000 -.0089500
 0.8000000 -.0063000
 0.9000000 -.0036500
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 670 AIRFOIL (goe670-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe670-il50,000935.7 at α=6.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe670-il50,000537.2 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   goe670-il100,000957.1 at α=5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe670-il100,000554.4 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe670-il200,000978.4 at α=4°Mach=0 Ncrit=9Xfoil predictionDetails
   goe670-il200,000570.5 at α=3.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe670-il500,0009101.9 at α=3.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe670-il500,000581.9 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe670-il1,000,0009114.1 at α=2.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe670-il1,000,000597.8 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
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