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GOE 610-B MOD. AIRFOIL (goe610bm-il)

GOE 610-B MOD. AIRFOIL - Gottingen 610-B MOD airfoil


Airfoil goe610bm-il
Details Dat file Parser  
(goe610bm-il) GOE 610-B MOD. AIRFOIL
Gottingen 610-B MOD airfoil
Max thickness 7.7% at 30% chord.
Max camber 5.5% at 40% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 610-B MOD. AIRFOIL
       15.       15.

 0.0000000 0.0000000
 0.0125000 0.0170900
 0.0250000 0.0281800
 0.0500000 0.0433500
 0.1000000 0.0617000
 0.1500000 0.0740500
 0.2000000 0.0834000
 0.3000000 0.0931000
 0.4000000 0.0928000
 0.5000000 0.0865000
 0.6000000 0.0772000
 0.7000000 0.0629000
 0.8000000 0.0466000
 0.9000000 0.0273000
 1.0000000 0.0080000

 0.0000000 0.0000000
 0.0125000 -.0069100
 0.0250000 -.0068300
 0.0500000 -.0046500
 0.1000000 -.0003000
 0.1500000 0.0040500
 0.2000000 0.0094000
 0.3000000 0.0161000
 0.4000000 0.0208000
 0.5000000 0.0225000
 0.6000000 0.0232000
 0.7000000 0.0209000
 0.8000000 0.0146000
 0.9000000 0.0073000
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 610-B MOD. AIRFOIL (goe610bm-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe610bm-il50,000940.4 at α=8.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe610bm-il50,000543.4 at α=7.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe610bm-il100,000962.8 at α=7.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe610bm-il100,000563.5 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe610bm-il200,000983.1 at α=6.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe610bm-il200,000582.3 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe610bm-il500,0009110.5 at α=5.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe610bm-il500,0005107.3 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe610bm-il1,000,0009130.3 at α=4.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe610bm-il1,000,0005125 at α=4°Mach=0 Ncrit=5Xfoil predictionDetails
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