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

GOE 738 AIRFOIL (goe738-il)

GOE 738 AIRFOIL - Gottingen 738 airfoil


Airfoil goe738-il
Details Dat file Parser  
(goe738-il) GOE 738 AIRFOIL
Gottingen 738 airfoil
Max thickness 15.4% at 30% chord.
Max camber 2.1% at 30% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 738 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0125000 0.0266700
 0.0250000 0.0388400
 0.0500000 0.0539800
 0.0750000 0.0653100
 0.1000000 0.0738500
 0.1500000 0.0864200
 0.2000000 0.0932000
 0.3000000 0.0984500
 0.4000000 0.0934000
 0.5000000 0.0809500
 0.6000000 0.0636000
 0.7000000 0.0435500
 0.8000000 0.0243000
 0.9000000 0.0091500
 0.9500000 0.0038200
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0125000 -.0218300
 0.0250000 -.0298600
 0.0500000 -.0389200
 0.0750000 -.0444900
 0.1000000 -.0486500
 0.1500000 -.0531800
 0.2000000 -.0553000
 0.3000000 -.0559500
 0.4000000 -.0536000
 0.5000000 -.0488500
 0.6000000 -.0419000
 0.7000000 -.0333500
 0.8000000 -.0233000
 0.9000000 -.0128500
 0.9500000 -.0071700
 1.0000000 0.0000000
No parser warnings Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file

Similar airfoils

MH 104 15.28%PreviewDetails
DAVIS BASIC B-24 WING AIRFOILPreviewDetails
NASA/LANGLEY NLF(1)-0416 AIRFOILPreviewDetails
GEMINI (smoothed)PreviewDetails
NACA 2415PreviewDetails
NACA 2415PreviewDetails
Gottingen 765 airfoil (recovered).PreviewDetails
MB253515 15.0% smoothedPreviewDetails
S8037 (16%)PreviewDetails
RAF-48 AIRFOILPreviewDetails

Polars for GOE 738 AIRFOIL (goe738-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe738-il50,000910.1 at α=-1°Mach=0 Ncrit=9Xfoil predictionDetails
   goe738-il50,000523.4 at α=7.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe738-il100,000941.3 at α=10°Mach=0 Ncrit=9Xfoil predictionDetails
   goe738-il100,000544.5 at α=7.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe738-il200,000962.4 at α=7.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe738-il200,000561.4 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe738-il500,000987.3 at α=6°Mach=0 Ncrit=9Xfoil predictionDetails
   goe738-il500,000579.3 at α=7.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe738-il1,000,0009102.9 at α=7.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe738-il1,000,000593.6 at α=7.75°Mach=0 Ncrit=5Xfoil predictionDetails
Reynolds number calculator
Set Reynolds number and Ncrit rangeLowHigh
Reynolds Number
NCrit