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

GOE 627 AIRFOIL (goe627-il)

GOE 627 AIRFOIL - Gottingen 627 airfoil


Airfoil goe627-il
Details Dat file Parser  
(goe627-il) GOE 627 AIRFOIL
Gottingen 627 airfoil
Max thickness 15.8% at 30% chord.
Max camber 4.1% at 30% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 627 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0125000 0.0350000
 0.0250000 0.0500000
 0.0500000 0.0705000
 0.0750000 0.0840000
 0.1000000 0.0945000
 0.1500000 0.1085000
 0.2000000 0.1155000
 0.3000000 0.1195000
 0.4000000 0.1160000
 0.5000000 0.1075000
 0.6000000 0.0945000
 0.7000000 0.0780000
 0.8000000 0.0575000
 0.9000000 0.0315000
 0.9500000 0.0160000
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0125000 -.0125000
 0.0250000 -.0170000
 0.0500000 -.0230000
 0.0750000 -.0270000
 0.1000000 -.0305000
 0.1500000 -.0345000
 0.2000000 -.0370000
 0.3000000 -.0380000
 0.4000000 -.0370000
 0.5000000 -.0345000
 0.6000000 -.0305000
 0.7000000 -.0250000
 0.8000000 -.0180000
 0.9000000 -.0095000
 0.9500000 -.0050000
 1.0000000 0.0000000
No parser warnings Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file

Similar airfoils

STRAND AIRFOILPreviewDetails
WORTMANN FX 77-W-153 AIRFOILPreviewDetails
GOE 741 AIRFOILPreviewDetails
FX S 02/1-158 AIRFOILPreviewDetails
FX 63-158 AIRFOILPreviewDetails
GOE 425 AIRFOILPreviewDetails
FX 79-W-151 APreviewDetails
GOE 648 AIRFOILPreviewDetails
GOE 256 (JUNKERS E) AIRFOILPreviewDetails
DEFIANT CANARD BL110 AIRFOILPreviewDetails

Polars for GOE 627 AIRFOIL (goe627-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe627-il50,000925.4 at α=3.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe627-il50,000529.1 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe627-il100,000943.3 at α=3.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe627-il100,000541.5 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   goe627-il200,000955.2 at α=1.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe627-il200,000552.8 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   goe627-il500,000974.2 at α=4.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe627-il500,000571.9 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe627-il1,000,000993.4 at α=6°Mach=0 Ncrit=9Xfoil predictionDetails
   goe627-il1,000,000590.5 at α=7.5°Mach=0 Ncrit=5Xfoil predictionDetails
Reynolds number calculator
Set Reynolds number and Ncrit rangeLowHigh
Reynolds Number
NCrit