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

GOE 490 AIRFOIL (goe490-il)

GOE 490 AIRFOIL - Gottingen 490 airfoil


Airfoil goe490-il
Details Dat file Parser  
(goe490-il) GOE 490 AIRFOIL
Gottingen 490 airfoil
Max thickness 8.8% at 19.9% chord.
Max camber 3.8% at 39.9% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 490 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0122000 0.0162300
 0.0245100 0.0264500
 0.0492500 0.0404100
 0.0740500 0.0513700
 0.0989100 0.0588300
 0.1487200 0.0692500
 0.1986000 0.0756700
 0.2984900 0.0815200
 0.3985600 0.0798700
 0.4986200 0.0747200
 0.5987900 0.0655800
 0.6990100 0.0534300
 0.7992800 0.0387900
 0.8996000 0.0216400
 0.9497800 0.0120700
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0127100 -.0112600
 0.0252700 -.0145300
 0.0503300 -.0175700
 0.0753400 -.0186100
 0.1003400 -.0181400
 0.1502800 -.0152200
 0.2002300 -.0123000
 0.3000900 -.0049500
 0.4000900 -.0031600
 0.5000500 -.0027500
 0.6000500 -.0029000
 0.7000600 -.0030500
 0.8000700 -.0037000
 0.9000599 -.0033500
 0.9500400 -.0019200
 1.0000000 0.0000000
No parser warnings Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file

Similar airfoils

USA 22 AIRFOILPreviewDetails
GOE 585 AIRFOILPreviewDetails
HOBIESMO1.DATPreviewDetails
I.S.A. 961PreviewDetails
HOBIEPreviewDetails
GOE 415 AIRFOILPreviewDetails
S4083 (8%)PreviewDetails
GOE 457 AIRFOILPreviewDetails
USA 26 AIRFOILPreviewDetails
I.S.A. 962PreviewDetails

Polars for GOE 490 AIRFOIL (goe490-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe490-il50,000933.2 at α=6.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe490-il50,000538.3 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   goe490-il100,000954.3 at α=5.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe490-il100,000554.1 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   goe490-il200,000972.5 at α=4.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe490-il200,000570.1 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe490-il500,000996.2 at α=4.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe490-il500,000589.6 at α=4°Mach=0 Ncrit=5Xfoil predictionDetails
   goe490-il1,000,0009114.1 at α=3.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe490-il1,000,000598.5 at α=4°Mach=0 Ncrit=5Xfoil predictionDetails
Reynolds number calculator
Set Reynolds number and Ncrit rangeLowHigh
Reynolds Number
NCrit