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

GOE 360 AIRFOIL (goe360-il)

GOE 360 AIRFOIL - Gottingen 360 airfoil


Airfoil goe360-il
Details Dat file Parser  
(goe360-il) GOE 360 AIRFOIL
Gottingen 360 airfoil
Max thickness 9.7% at 29.9% chord.
Max camber 5.9% at 29.9% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 360 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0123000 0.0212200
 0.0247000 0.0319400
 0.0495300 0.0491700
 0.0744100 0.0621100
 0.0993000 0.0729500
 0.1491500 0.0895200
 0.1990500 0.0998000
 0.2989800 0.1070600
 0.3990000 0.1043100
 0.4990900 0.0952700
 0.5992300 0.0808200
 0.6993901 0.0643800
 0.7995800 0.0441400
 0.8997900 0.0217900
 0.9498900 0.0116700
 1.0000000 0.0010500

 0.0000000 0.0000000
 0.0126000 -.0104800
 0.0250900 -.0098600
 0.0500500 -.0053200
 0.0750200 -.0018800
 0.0999900 0.0008500
 0.1499500 0.0048300
 0.1999300 0.0076100
 0.2999000 0.0102600
 0.3998900 0.0117200
 0.4999000 0.0100700
 0.5999300 0.0081700
 0.6999400 0.0058000
 0.7999700 0.0033400
 0.8999800 0.0010800
 0.9500000 0.0000700
 1.0000000 -.0010500
No parser warnings Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file

Similar airfoils

GOE 238 (HANSA-BRANDENBURG) AIRFOILPreviewDetails
GOE 319 (HANSA-BRANDENBURG II)PreviewDetails
GOE 329 (PFALZ 58) AIRFOILPreviewDetails
GOE 336 (MVA H.44) AIRFOILPreviewDetails
GOE 746 AIRFOILPreviewDetails
GOE 92 AIRFOILPreviewDetails
GOE 303 (FRIEDRICHSHAFEN G03)PreviewDetails
GOE 529 AIRFOILPreviewDetails
GOE 14 AIRFOILPreviewDetails
GOE 801 (MVA 301) AIRFOILPreviewDetails

Polars for GOE 360 AIRFOIL (goe360-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe360-il50,000920.7 at α=3°Mach=0 Ncrit=9Xfoil predictionDetails
   goe360-il50,000536.2 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe360-il100,000951.4 at α=10.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe360-il100,000556.8 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe360-il200,000973.4 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe360-il200,000576.2 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe360-il500,0009105.3 at α=7.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe360-il500,0005104.6 at α=6.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe360-il1,000,0009131.2 at α=7°Mach=0 Ncrit=9Xfoil predictionDetails
   goe360-il1,000,0005127.3 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
Reynolds number calculator
Set Reynolds number and Ncrit rangeLowHigh
Reynolds Number
NCrit