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

GOE 370 AIRFOIL (goe370-il)

GOE 370 AIRFOIL - Gottingen 370 airfoil


Airfoil goe370-il
Details Dat file Parser  
(goe370-il) GOE 370 AIRFOIL
Gottingen 370 airfoil
Max thickness 4.7% at 20% chord.
Max camber 5.7% at 40% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 370 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0124300 0.0120700
 0.0249000 0.0186400
 0.0498400 0.0297700
 0.0747900 0.0389100
 0.0997400 0.0465500
 0.1496800 0.0588200
 0.1996300 0.0671000
 0.2995800 0.0766500
 0.3995600 0.0797000
 0.4995800 0.0757500
 0.5996300 0.0678000
 0.6997000 0.0543500
 0.7997900 0.0384000
 0.8998800 0.0209500
 0.9499400 0.0112200
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0125300 -.0054300
 0.0250300 -.0053600
 0.0500200 -.0032200
 0.0750000 0.0004100
 0.0999700 0.0045500
 0.1499200 0.0138200
 0.1998900 0.0206000
 0.2998300 0.0306500
 0.3998100 0.0352000
 0.4998200 0.0332500
 0.5998500 0.0278000
 0.6998800 0.0213500
 0.7999300 0.0129000
 0.8999700 0.0049500
 0.9499900 0.0022200
 1.0000000 0.0000000
No parser warnings Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file

Similar airfoils

GOE 427 AIRFOILPreviewDetails
GOE 342 AIRFOILPreviewDetails
GOE 123 AIRFOILPreviewDetails
GOE 483 AIRFOILPreviewDetails
S1091PreviewDetails
GOE 494 AIRFOILPreviewDetails
E63 (4.25%)PreviewDetails
GOE 417 AIRFOILPreviewDetails
GOE 394 AIRFOILPreviewDetails
GOE 396 AIRFOILPreviewDetails

Polars for GOE 370 AIRFOIL (goe370-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe370-il50,000945.2 at α=6.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe370-il50,000544.8 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   goe370-il100,000967.2 at α=5.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe370-il100,000567.5 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe370-il200,000992 at α=4.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe370-il200,000592.3 at α=4.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe370-il500,0009128.1 at α=3.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe370-il500,0005121.6 at α=3.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe370-il1,000,0009154.2 at α=2.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe370-il1,000,0005119.5 at α=3.5°Mach=0 Ncrit=5Xfoil predictionDetails
Reynolds number calculator
Set Reynolds number and Ncrit rangeLowHigh
Reynolds Number
NCrit