Airfoil Tools
Search 1636 airfoils Google+
You have 0 airfoils loaded.
Your Reynold number range is 50,000 to 1,000,000. (set)

GOE 513 AIRFOIL (goe513-il)

GOE 513 AIRFOIL - Gottingen 513 airfoil


Airfoil goe513-il
Details Dat file Parser  
(goe513-il) GOE 513 AIRFOIL
Gottingen 513 airfoil
Max thickness 16.6% at 29.8% chord.
Max camber 5.2% at 39.8% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 513 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0119400 0.0322100
 0.0241500 0.0484200
 0.0487500 0.0713500
 0.0734600 0.0882900
 0.0982300 0.1012200
 0.1479200 0.1185900
 0.1977600 0.1279600
 0.2976300 0.1352100
 0.3977000 0.1314600
 0.4978900 0.1207100
 0.5981200 0.1074700
 0.6984600 0.0877200
 0.7988600 0.0649800
 0.8993700 0.0357400
 0.9496900 0.0176200
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0128000 -.0172800
 0.0253900 -.0225600
 0.0505000 -.0286200
 0.0755800 -.0331800
 0.1006300 -.0362400
 0.1506900 -.0393600
 0.2006600 -.0379900
 0.3005400 -.0307400
 0.4004700 -.0269900
 0.5004900 -.0282400
 0.6005300 -.0304900
 0.7005200 -.0297400
 0.8004300 -.0244900
 0.9002900 -.0167400
 0.9501800 -.0103700
 1.0000000 0.0000000
No parser warnings Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file

Similar airfoils

GOE 508 AIRFOILPreviewDetails
Rhode St. Genese 36PreviewDetails
GOE 449 AIRFOILPreviewDetails
N-24PreviewDetails
GOE 506 AIRFOILPreviewDetails
GOE 692 AIRFOILPreviewDetails
GOE 624 AIRFOILPreviewDetails
GOE 527 AIRFOILPreviewDetails
GOE 413 AIRFOILPreviewDetails
GOE 367 AIRFOILPreviewDetails

Polars for GOE 513 AIRFOIL (goe513-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe513-il50,000910.3 at α=3.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe513-il50,000528.6 at α=4°Mach=0 Ncrit=5Xfoil predictionDetails
   goe513-il100,000944.5 at α=3°Mach=0 Ncrit=9Xfoil predictionDetails
   goe513-il100,000543 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe513-il200,000958.9 at α=4.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe513-il200,000554.6 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe513-il500,000975.4 at α=5.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe513-il500,000566.1 at α=7.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe513-il1,000,000986.6 at α=7.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe513-il1,000,000576.8 at α=8.5°Mach=0 Ncrit=5Xfoil predictionDetails
Reynolds number calculator
Set Reynolds number and Ncrit rangeLowHigh
Reynolds Number
NCrit