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

GOE 8K AIRFOIL (goe08k-il)

GOE 8K AIRFOIL - Gottingen 8K airfoil


Airfoil goe08k-il
Details Dat file Parser  
(goe08k-il) GOE 8K AIRFOIL
Gottingen 8K airfoil
Max thickness 14.9% at 50% chord.
Max camber 6.1% at 50% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 8K AIRFOIL
       16.       16.

 0.0000000 0.0000000
 0.0250000 0.0311200
 0.0500000 0.0463500
 0.0750000 0.0583700
 0.1000000 0.0691900
 0.1500000 0.0865300
 0.2000000 0.1000800
 0.3000000 0.1202700
 0.4000000 0.1316600
 0.5000000 0.1355500
 0.6000000 0.1321400
 0.7000000 0.1175300
 0.8000000 0.0925200
 0.9000000 0.0553100
 0.9500000 0.0320500
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0250000 -.0140800
 0.0500000 -.0158600
 0.0750000 -.0164300
 0.1000000 -.0175100
 0.1500000 -.0184700
 0.2000000 -.0180200
 0.3000000 -.0163300
 0.4000000 -.0146400
 0.5000000 -.0129500
 0.6000000 -.0112600
 0.7000000 -.0095700
 0.8000000 -.0078800
 0.9000000 -.0061900
 0.9500000 -.0053500
 1.0000000 0.0000000
No parser warnings Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file

Similar airfoils

UAG 88-143/20PreviewDetails
GOE 13K AIRFOILPreviewDetails
NREL's S832 AirfoilPreviewDetails
AH 94-145PreviewDetails
EPPLER 678 AIRFOILPreviewDetails
NACA 1-H-15 AIRFOILPreviewDetails
NASA LRN 1015 (NASA TM 102840)PreviewDetails
FX 67-K-150/17 AIRFOILPreviewDetails
AH 95-160PreviewDetails
EPPLER 694 AIRFOILPreviewDetails

Polars for GOE 8K AIRFOIL (goe08k-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe08k-il50,000918 at α=14°Mach=0 Ncrit=9Xfoil predictionDetails
   goe08k-il50,000515.7 at α=12.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe08k-il100,000926.9 at α=11.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe08k-il100,000524.1 at α=11.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe08k-il200,000944.4 at α=9.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe08k-il200,000543.5 at α=9°Mach=0 Ncrit=5Xfoil predictionDetails
   goe08k-il500,0009103.5 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe08k-il500,000596.2 at α=4.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe08k-il1,000,0009143.1 at α=3°Mach=0 Ncrit=9Xfoil predictionDetails
   goe08k-il1,000,0005122 at α=3.25°Mach=0 Ncrit=5Xfoil predictionDetails
Reynolds number calculator
Set Reynolds number and Ncrit rangeLowHigh
Reynolds Number
NCrit