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GOE 512 AIRFOIL (goe512-il)

GOE 512 AIRFOIL - Gottingen 512 airfoil


Airfoil goe512-il
Details Dat file Parser  
(goe512-il) GOE 512 AIRFOIL
Gottingen 512 airfoil
Max thickness 13.9% at 19.9% chord.
Max camber 5.6% at 29.9% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 512 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0121500 0.0301400
 0.0244900 0.0447800
 0.0492400 0.0660700
 0.0740600 0.0813500
 0.0989300 0.0926400
 0.1487500 0.1087100
 0.1986500 0.1172800
 0.2985700 0.1244300
 0.3986100 0.1210800
 0.4987000 0.1127400
 0.5988600 0.0988900
 0.6990600 0.0820400
 0.7993000 0.0606900
 0.8996100 0.0343500
 0.9497899 0.0179200
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0126200 -.0103500
 0.0251700 -.0147100
 0.0502200 -.0189200
 0.0752400 -.0211300
 0.1002600 -.0228500
 0.1502700 -.0232700
 0.2002500 -.0217000
 0.3001400 -.0120500
 0.4001300 -.0109000
 0.5001400 -.0122500
 0.6001700 -.0151000
 0.7001899 -.0169500
 0.8001800 -.0153000
 0.9001200 -.0106500
 0.9500700 -.0060700
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 512 AIRFOIL (goe512-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe512-il50,000919.5 at α=4.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe512-il50,000531.6 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe512-il100,000948.8 at α=4°Mach=0 Ncrit=9Xfoil predictionDetails
   goe512-il100,000547.4 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe512-il200,000964.2 at α=3.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe512-il200,000560.9 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe512-il500,000983.6 at α=6°Mach=0 Ncrit=9Xfoil predictionDetails
   goe512-il500,000574.1 at α=7.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe512-il1,000,000995.9 at α=8.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe512-il1,000,000588.2 at α=9.25°Mach=0 Ncrit=5Xfoil predictionDetails
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