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

GOE 549 AIRFOIL (goe549-il)

GOE 549 AIRFOIL - Gottingen 549 airfoil


Airfoil goe549-il
Details Dat file Parser  
(goe549-il) GOE 549 AIRFOIL
Gottingen 549 airfoil
Max thickness 13.9% at 30% chord.
Max camber 4.7% at 40% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 549 AIRFOIL
       21.       21.

 0.0000000 0.0000000
 0.0020000 0.0085700
 0.0040000 0.0124400
 0.0060000 0.0151100
 0.0080000 0.0179800
 0.0125000 0.0229300
 0.0250000 0.0343600
 0.0500000 0.0517300
 0.0750000 0.0645900
 0.1000000 0.0759500
 0.1500000 0.0931800
 0.2000000 0.1044000
 0.3000000 0.1143500
 0.4000000 0.1133000
 0.5000000 0.1032500
 0.6000000 0.0867000
 0.7000000 0.0686500
 0.8000000 0.0466000
 0.9000000 0.0235500
 0.9500000 0.0122700
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0020000 -.0058300
 0.0040000 -.0087600
 0.0060000 -.0105900
 0.0080000 -.0120200
 0.0125000 -.0145200
 0.0250000 -.0176400
 0.0500000 -.0217800
 0.0750000 -.0244100
 0.1000000 -.0255500
 0.1500000 -.0268200
 0.2000000 -.0271000
 0.3000000 -.0241500
 0.4000000 -.0197000
 0.5000000 -.0142500
 0.6000000 -.0083000
 0.7000000 -.0038500
 0.8000000 -.0014000
 0.9000000 -.0004500
 0.9500000 -.0002300
 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 758 AIRFOILPreviewDetails
GOE 398 AIRFOILPreviewDetails
GOE 533 AIRFOILPreviewDetails
GOE 553 AIRFOILPreviewDetails
Rhode St. Genese 34PreviewDetails
GOE 655 AIRFOILPreviewDetails
GOE 426 AIRFOILPreviewDetails
Dayton-Wright 6PreviewDetails
Dayton-Wright T-1PreviewDetails
GOE 478 AIRFOILPreviewDetails

Polars for GOE 549 AIRFOIL (goe549-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe549-il50,00097.6 at α=3.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe549-il50,000526.4 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe549-il100,000943 at α=11.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe549-il100,000552.8 at α=7.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe549-il200,000974.4 at α=7.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe549-il200,000575.7 at α=6.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe549-il500,0009107.9 at α=6°Mach=0 Ncrit=9Xfoil predictionDetails
   goe549-il500,0005100.8 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe549-il1,000,0009128.7 at α=4.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe549-il1,000,0005115.8 at α=3.75°Mach=0 Ncrit=5Xfoil predictionDetails
Reynolds number calculator
Set Reynolds number and Ncrit rangeLowHigh
Reynolds Number
NCrit