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

GOE 414 AIRFOIL (goe414-il)

GOE 414 AIRFOIL - Gottingen 414 airfoil


Airfoil goe414-il
Details Dat file Parser  
(goe414-il) GOE 414 AIRFOIL
Gottingen 414 airfoil
Max thickness 13.6% at 29.7% chord.
Max camber 5.3% at 39.7% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 414 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0119600 0.0190400
 0.0241500 0.0300800
 0.0486400 0.0480700
 0.0732500 0.0618700
 0.0979400 0.0729700
 0.1474100 0.0916600
 0.1970700 0.1037700
 0.2966700 0.1177800
 0.3966700 0.1179100
 0.4968400 0.1117400
 0.5972200 0.0984700
 0.6977100 0.0811100
 0.7983500 0.0583500
 0.8991200 0.0313000
 0.9495400 0.0162200
 1.0000000 0.0010500

 0.0000000 0.0000000
 0.0128500 -.0124400
 0.0254800 -.0168800
 0.0506400 -.0225700
 0.0757000 -.0246600
 0.1007200 -.0253500
 0.1507100 -.0250400
 0.2006700 -.0236300
 0.3005100 -.0181100
 0.4003600 -.0126900
 0.5002600 -.0092700
 0.6002000 -.0070400
 0.7001500 -.0052200
 0.8001100 -.0040000
 0.9000800 -.0028700
 0.9500700 -.0024600
 1.0000000 -.0010500
No parser warnings Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file

Similar airfoils

GOE 615 AIRFOILPreviewDetails
Dayton-Wright 6PreviewDetails
USA 27 mod. AIRFOILPreviewDetails
USA 29 AIRFOILPreviewDetails
GOE 398 AIRFOILPreviewDetails
GOE 412 AIRFOILPreviewDetails
GOE 553 AIRFOILPreviewDetails
GOE 533 AIRFOILPreviewDetails
GOE 549 AIRFOILPreviewDetails
GOE 758 AIRFOILPreviewDetails

Polars for GOE 414 AIRFOIL (goe414-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe414-il50,00098.6 at α=2.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe414-il50,000528.7 at α=4.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe414-il100,000952.1 at α=9.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe414-il100,000554.6 at α=6.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe414-il200,000974.5 at α=7°Mach=0 Ncrit=9Xfoil predictionDetails
   goe414-il200,000573 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe414-il500,0009100 at α=7.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe414-il500,000597 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   goe414-il1,000,0009124.9 at α=6.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe414-il1,000,0005119 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
Reynolds number calculator
Set Reynolds number and Ncrit rangeLowHigh
Reynolds Number
NCrit