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

GOE 367 AIRFOIL (goe367-il)

GOE 367 AIRFOIL - Gottingen 367 airfoil


Airfoil goe367-il
Details Dat file Parser  
(goe367-il) GOE 367 AIRFOIL
Gottingen 367 airfoil
Max thickness 16.3% at 29.7% chord.
Max camber 4.6% at 39.7% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 367 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0118100 0.0268100
 0.0240000 0.0387200
 0.0485400 0.0562600
 0.0732100 0.0691000
 0.0978900 0.0813400
 0.1474400 0.0990200
 0.1970700 0.1130000
 0.2967300 0.1261900
 0.3967100 0.1271700
 0.4969000 0.1197700
 0.5972600 0.1059700
 0.6977900 0.0852700
 0.7984400 0.0601800
 0.8991800 0.0317900
 0.9495700 0.0165900
 1.0000000 0.0016000

 0.0000000 0.0000000
 0.0130500 -.0213600
 0.0257200 -.0279300
 0.0508700 -.0335800
 0.0759500 -.0366300
 0.1009700 -.0375800
 0.1509700 -.0373900
 0.2009700 -.0372900
 0.3009500 -.0366100
 0.4009100 -.0351200
 0.5008400 -.0325300
 0.6007800 -.0299400
 0.7006800 -.0262500
 0.8005500 -.0212700
 0.9003000 -.0115800
 0.9501600 -.0060900
 1.0000000 -.0016000
No parser warnings Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file

Similar airfoils

GOE 413 AIRFOILPreviewDetails
GOE 506 AIRFOILPreviewDetails
GOE 256 (JUNKERS E) AIRFOILPreviewDetails
GOE 425 AIRFOILPreviewDetails
GOE 797 AIRFOILPreviewDetails
GOE 692 AIRFOILPreviewDetails
GOE 681 AIRFOILPreviewDetails
GOE 513 AIRFOILPreviewDetails
GOE 624 AIRFOILPreviewDetails
Rhode St. Genese 36PreviewDetails

Polars for GOE 367 AIRFOIL (goe367-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe367-il50,00095.3 at α=3.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe367-il50,000520.8 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe367-il100,000941.2 at α=7.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe367-il100,000547.7 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe367-il200,000968 at α=6°Mach=0 Ncrit=9Xfoil predictionDetails
   goe367-il200,000564.8 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe367-il500,000993.2 at α=5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe367-il500,000583.7 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   goe367-il1,000,0009111.3 at α=6.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe367-il1,000,000598.4 at α=7°Mach=0 Ncrit=5Xfoil predictionDetails
Reynolds number calculator
Set Reynolds number and Ncrit rangeLowHigh
Reynolds Number
NCrit