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

GOE 528 AIRFOIL (goe528-il)

GOE 528 AIRFOIL - Gottingen 528 airfoil


Airfoil goe528-il
Details Dat file Parser  
(goe528-il) GOE 528 AIRFOIL
Gottingen 528 airfoil
Max thickness 12.5% at 29.8% chord.
Max camber 6.2% at 39.8% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 528 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0120500 0.0301800
 0.0243600 0.0423700
 0.0491000 0.0597400
 0.0739000 0.0731100
 0.0987300 0.0849800
 0.1484700 0.1017300
 0.1983100 0.1124700
 0.2981600 0.1224700
 0.3981900 0.1209700
 0.4983400 0.1109800
 0.5985600 0.0959800
 0.6988600 0.0759800
 0.7992100 0.0524900
 0.8995900 0.0274900
 0.9497800 0.0147500
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0126600 -.0108100
 0.0252000 -.0131200
 0.0502100 -.0142500
 0.0752100 -.0138700
 0.1002000 -.0130000
 0.1501600 -.0107500
 0.2001200 -.0080000
 0.3000300 -.0020000
 0.3999600 0.0030000
 0.4999000 0.0065000
 0.5998900 0.0075000
 0.6998900 0.0075000
 0.7999099 0.0060000
 0.8999600 0.0030000
 0.9499700 0.0017500
 1.0000000 0.0000000
No parser warnings Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file

Similar airfoils

St. CYR 24 (Bartel 35-IIIC)PreviewDetails
GOE 446 AIRFOILPreviewDetails
NACA 6412PreviewDetails
GOE 611 AIRFOILPreviewDetails
GOE 332 (PFALZ 61) AIRFOILPreviewDetails
DAE-11 AIRFOILPreviewDetails
DAE-21 AIRFOILPreviewDetails
USA 29 AIRFOILPreviewDetails
GOE 480 AIRFOILPreviewDetails
GOE 320 (HANSA-BRANDENBURG II.1)PreviewDetails

Polars for GOE 528 AIRFOIL (goe528-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe528-il50,00099 at α=2.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe528-il50,000529.8 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe528-il100,000946.6 at α=7.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe528-il100,000555.7 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe528-il200,000975.5 at α=7.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe528-il200,000577.6 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe528-il500,0009110.5 at α=6°Mach=0 Ncrit=9Xfoil predictionDetails
   goe528-il500,0005106.7 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe528-il1,000,0009137.7 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe528-il1,000,0005128.9 at α=4.75°Mach=0 Ncrit=5Xfoil predictionDetails
Reynolds number calculator
Set Reynolds number and Ncrit rangeLowHigh
Reynolds Number
NCrit