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

GOE 703 AIRFOIL (goe703-il)

GOE 703 AIRFOIL - Gottingen 703 airfoil


Airfoil goe703-il
Details Dat file Parser  
(goe703-il) GOE 703 AIRFOIL
Gottingen 703 airfoil
Max thickness 19.4% at 30% chord.
Max camber 2.3% at 30% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 703 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0125000 0.0305000
 0.0250000 0.0435000
 0.0500000 0.0610000
 0.0750000 0.0750000
 0.1000000 0.0850000
 0.1500000 0.1000000
 0.2000000 0.1105000
 0.3000000 0.1200000
 0.4000000 0.1185000
 0.5000000 0.1080000
 0.6000000 0.0915000
 0.7000000 0.0720000
 0.8000000 0.0490000
 0.9000000 0.0255000
 0.9500000 0.0135000
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0125000 -.0275000
 0.0250000 -.0360000
 0.0500000 -.0465000
 0.0750000 -.0540000
 0.1000000 -.0595000
 0.1500000 -.0665000
 0.2000000 -.0705000
 0.3000000 -.0740000
 0.4000000 -.0750000
 0.5000000 -.0730000
 0.6000000 -.0680000
 0.7000000 -.0595000
 0.8000000 -.0460000
 0.9000000 -.0260000
 0.9500000 -.0135000
 1.0000000 0.0000000
No parser warnings Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file

Similar airfoils

EPPLER 1214 AIRFOILPreviewDetails
GOE 683 AIRFOILPreviewDetails
EPPLER 550 AIRFOILPreviewDetails
NASA/LANGLEY LS(1)-0421MOD AIRFOILPreviewDetails
NACA 2418PreviewDetails
ARA-D 20% AIRFOILPreviewDetails
EPPLER 549 AIRFOILPreviewDetails
NACA 2421PreviewDetails
WORTMANN FX 66-17AII-182 AIRFOIL (ASPreviewDetails
NACA 63(3)-218PreviewDetails

Polars for GOE 703 AIRFOIL (goe703-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe703-il50,00095.5 at α=0.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe703-il50,000522.3 at α=3.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe703-il100,000940 at α=9.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe703-il100,000543 at α=7.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe703-il200,000963.3 at α=7.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe703-il200,000549.1 at α=8.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe703-il500,000967 at α=9°Mach=0 Ncrit=9Xfoil predictionDetails
   goe703-il500,000557.4 at α=7.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe703-il1,000,000975.5 at α=8°Mach=0 Ncrit=9Xfoil predictionDetails
   goe703-il1,000,000565.6 at α=8°Mach=0 Ncrit=5Xfoil predictionDetails
Reynolds number calculator
Set Reynolds number and Ncrit rangeLowHigh
Reynolds Number
NCrit