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

GOE 328 AIRFOIL (goe328-il)

GOE 328 AIRFOIL - Gottingen 328 airfoil


Airfoil goe328-il
Details Dat file Parser  
(goe328-il) GOE 328 AIRFOIL
Gottingen 328 airfoil
Max thickness 8.2% at 30% chord.
Max camber 4.3% at 30% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 328 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0125000 0.0171900
 0.0250000 0.0253700
 0.0500000 0.0377500
 0.0750000 0.0481300
 0.1000000 0.0565000
 0.1500000 0.0702500
 0.2000000 0.0780000
 0.3000000 0.0845000
 0.4000000 0.0830000
 0.5000000 0.0775000
 0.6000000 0.0670000
 0.7000000 0.0535000
 0.8000000 0.0380000
 0.9000000 0.0215000
 0.9500000 0.0132500
 1.0000000 0.0050000

 0.0000000 0.0000000
 0.0125000 -.0138100
 0.0250000 -.0146200
 0.0500000 -.0122500
 0.0750000 -.0098800
 0.1000000 -.0075000
 0.1500000 -.0037500
 0.2000000 -.0010000
 0.3000000 0.0025000
 0.4000000 0.0040000
 0.5000000 0.0045000
 0.6000000 0.0040000
 0.7000000 0.0030000
 0.8000000 0.0020000
 0.9000000 0.0010000
 0.9500000 0.0007500
 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 277 (DAIMLER VIII) AIRFOILPreviewDetails
GOE 315 (HANSA-BRANDENBURG III.5)PreviewDetails
GOE 133 (MVA H.11) AIRFOILPreviewDetails
GOE 178 AIRFOILPreviewDetails
GOE 280 (DAIMLER XI) AIRFOILPreviewDetails
NACA M14 AIRFOILPreviewDetails
GOE 309 (MVA H.41) AIRFOILPreviewDetails
GOE 408 AIRFOILPreviewDetails
GOE 314 (HANSA-BRANDENBURG) AIRFOILPreviewDetails
GOE 187 (SCHTTE-LANZ 2U10) AIRFOILPreviewDetails

Polars for GOE 328 AIRFOIL (goe328-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe328-il50,000936.1 at α=9.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe328-il50,000539.6 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe328-il100,000956.9 at α=8.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe328-il100,000557.1 at α=7.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe328-il200,000975.2 at α=7.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe328-il200,000574.8 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe328-il500,0009101.6 at α=5.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe328-il500,000596.9 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe328-il1,000,0009120.7 at α=4.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe328-il1,000,0005111.3 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
Reynolds number calculator
Set Reynolds number and Ncrit rangeLowHigh
Reynolds Number
NCrit