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

GOE 7K AIRFOIL (goe07k-il)

GOE 7K AIRFOIL - Gottingen 7K airfoil


Airfoil goe07k-il
Details Dat file Parser  
(goe07k-il) GOE 7K AIRFOIL
Gottingen 7K airfoil
Max thickness 11% at 50% chord.
Max camber 4.5% at 50% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 7K AIRFOIL
       16.       16.

 0.0000000 0.0000000
 0.0250000 0.0231100
 0.0500000 0.0344300
 0.0750000 0.0433400
 0.1000000 0.0513500
 0.1500000 0.0641800
 0.2000000 0.0741000
 0.3000000 0.0891500
 0.4000000 0.0975000
 0.5000000 0.1004500
 0.6000000 0.0980000
 0.7000000 0.0871500
 0.8000000 0.0686000
 0.9000000 0.0409500
 0.9500000 0.0237800
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0250000 -.0102900
 0.0500000 -.0116800
 0.0750000 -.0124600
 0.1000000 -.0129500
 0.1500000 -.0136200
 0.2000000 -.0133000
 0.3000000 -.0120500
 0.4000000 -.0108000
 0.5000000 -.0095500
 0.6000000 -.0083000
 0.7000000 -.0070500
 0.8000000 -.0058000
 0.9000000 -.0045500
 0.9500000 -.0039300
 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 12K AIRFOILPreviewDetails
NREL's S802 AirfoilPreviewDetails
NREL's S806A Airfoil (modified linePreviewDetails
NACA 6-H-10 AIRFOILPreviewDetails
NREL's S803 AirfoilPreviewDetails
GOE 14K AIRFOILPreviewDetails
FX 74-130 WP1PreviewDetails
74-130 WP2 MODPreviewDetails
S4158PreviewDetails
AH 88-K-130/20PreviewDetails

Polars for GOE 7K AIRFOIL (goe07k-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe07k-il50,000924.4 at α=9.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe07k-il50,000525.2 at α=8.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe07k-il100,000938.7 at α=7.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe07k-il100,000540.7 at α=7.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe07k-il200,000969.7 at α=6.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe07k-il200,000570.2 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   goe07k-il500,0009122.3 at α=4.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe07k-il500,0005116.5 at α=3.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe07k-il1,000,0009159.9 at α=2.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe07k-il1,000,0005142.8 at α=2.75°Mach=0 Ncrit=5Xfoil predictionDetails
Reynolds number calculator
Set Reynolds number and Ncrit rangeLowHigh
Reynolds Number
NCrit