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GOE 63 AIRFOIL (goe63-il)

GOE 63 AIRFOIL - Gottingen 63 airfoil


Airfoil goe63-il
Details Dat file Parser  
(goe63-il) GOE 63 AIRFOIL
Gottingen 63 airfoil
Max thickness 8.3% at 19.9% chord.
Max camber 6.7% at 39.9% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 63 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0122000 0.0266400
 0.0245500 0.0394800
 0.0493400 0.0576600
 0.0742000 0.0699500
 0.0991000 0.0790300
 0.1489500 0.0918000
 0.1988600 0.0998700
 0.2987900 0.1062100
 0.3988000 0.1056500
 0.4988800 0.0979900
 0.5990500 0.0834300
 0.6992500 0.0654700
 0.7994800 0.0456100
 0.8997100 0.0257600
 0.9498300 0.0150300
 1.0000000 0.0035000

 0.0000000 0.0000000
 0.0126600 -.0142600
 0.0251500 -.0135100
 0.0500900 -.0077300
 0.0750200 -.0017400
 0.0999600 0.0037400
 0.1498700 0.0113100
 0.1998000 0.0173800
 0.2997200 0.0244200
 0.3996800 0.0282600
 0.4996900 0.0273000
 0.5997200 0.0241400
 0.6998000 0.0178800
 0.7998800 0.0107200
 0.8999600 0.0035600
 0.9499900 0.0008300
 1.0000000 -.0035000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 63 AIRFOIL (goe63-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe63-il50,000930.4 at α=8.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe63-il50,000541.3 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   goe63-il100,000961 at α=6°Mach=0 Ncrit=9Xfoil predictionDetails
   goe63-il100,000563.3 at α=4.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe63-il200,000986.5 at α=4.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe63-il200,000580.7 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe63-il500,0009110.3 at α=4.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe63-il500,0005102.6 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe63-il1,000,0009128.4 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe63-il1,000,0005121.5 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
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