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

GOE 394 AIRFOIL (goe394-il)

GOE 394 AIRFOIL - Gottingen 394 airfoil


Airfoil goe394-il
Details Dat file Parser  
(goe394-il) GOE 394 AIRFOIL
Gottingen 394 airfoil
Max thickness 6.1% at 19.9% chord.
Max camber 5.9% at 39.9% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 394 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0123000 0.0181400
 0.0247000 0.0267800
 0.0495500 0.0395600
 0.0744500 0.0488400
 0.0993700 0.0561200
 0.1492300 0.0681800
 0.1991400 0.0767400
 0.2990500 0.0848600
 0.3990500 0.0846900
 0.4991000 0.0801100
 0.5992000 0.0709400
 0.6993901 0.0538700
 0.7995900 0.0368000
 0.8997900 0.0186200
 0.9499000 0.0091900
 1.0000000 0.0007500

 0.0000000 0.0000000
 0.0126100 -.0098600
 0.0251300 -.0112200
 0.0501200 -.0106400
 0.0750800 -.0069600
 0.1000100 -.0008700
 0.1499100 0.0081900
 0.1998200 0.0157500
 0.2997000 0.0268700
 0.3996300 0.0330000
 0.4996000 0.0356200
 0.5996100 0.0345500
 0.6997200 0.0245700
 0.7998300 0.0154000
 0.8999299 0.0066200
 0.9499800 0.0021900
 1.0000000 -.0007500
No parser warnings Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file

Similar airfoils

GOE 417 AIRFOILPreviewDetails
GOE 342 AIRFOILPreviewDetails
GOE 362 AIRFOILPreviewDetails
GOE 361 AIRFOILPreviewDetails
GOE 57 AIRFOILPreviewDetails
AH-6-40-7 AIRFOILPreviewDetails
GOE 483 AIRFOILPreviewDetails
GOE 400 AIRFOILPreviewDetails
GOE 803 (HACKLINGER) AIRFOILPreviewDetails
GOE 123 AIRFOILPreviewDetails

Polars for GOE 394 AIRFOIL (goe394-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe394-il50,000940.4 at α=8.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe394-il50,000544.5 at α=6.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe394-il100,000964.4 at α=6°Mach=0 Ncrit=9Xfoil predictionDetails
   goe394-il100,000566.6 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe394-il200,000990.5 at α=4.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe394-il200,000585.9 at α=4.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe394-il500,0009116.6 at α=4.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe394-il500,0005108 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe394-il1,000,0009139.2 at α=5.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe394-il1,000,0005112.6 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
Reynolds number calculator
Set Reynolds number and Ncrit rangeLowHigh
Reynolds Number
NCrit