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

GOE 319 (HANSA-BRANDENBURG II) AIRFOIL (goe319-il)

GOE 319 (HANSA-BRANDENBURG II) AIRFOIL - Gottingen 319 (Hansa-Brandenburg II) airfoil


Airfoil goe319-il
Details Dat file Parser  
(goe319-il) GOE 319 (HANSA-BRANDENBURG II) AIRFOIL
Gottingen 319 (Hansa-Brandenburg II) airfoil
Max thickness 10.3% at 29.8% chord.
Max camber 5.8% at 29.8% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 319 (HANSA-BRANDENBURG II) AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0120600 0.0306700
 0.0243700 0.0438500
 0.0491100 0.0617100
 0.0739200 0.0745700
 0.0987900 0.0839300
 0.1486000 0.0967500
 0.1985100 0.1033700
 0.2984300 0.1088100
 0.3984600 0.1065600
 0.4986000 0.0968000
 0.5988100 0.0823500
 0.6990800 0.0637000
 0.7993600 0.0439500
 0.8996800 0.0220000
 0.9498400 0.0113300
 1.0000000 0.0005500

 0.0000000 0.0000000
 0.0127000 -.0139200
 0.0252100 -.0146400
 0.0501800 -.0127700
 0.0751400 -.0099100
 0.1001000 -.0069500
 0.1500300 -.0023300
 0.1999700 0.0022900
 0.2999100 0.0063300
 0.3999100 0.0062800
 0.4999300 0.0047200
 0.5999400 0.0041700
 0.6999600 0.0026100
 0.7999800 0.0014600
 0.9000100 -.0008900
 0.9500200 -.0012700
 1.0000000 -.0005500
No parser warnings Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file

Similar airfoils

GOE 329 (PFALZ 58) AIRFOILPreviewDetails
GOE 238 (HANSA-BRANDENBURG) AIRFOILPreviewDetails
GOE 360 AIRFOILPreviewDetails
GOE 364 AIRFOILPreviewDetails
GOE 746 AIRFOILPreviewDetails
GOE 323 (HANSA-BRANDENBURG V.1)PreviewDetails
GOE 330 (PFALZ 59) AIRFOILPreviewDetails
GOE 388 AIRFOILPreviewDetails
GOE 303 (FRIEDRICHSHAFEN G03)PreviewDetails
GOE 321 (HANSA-BRANDENBURG III.1)PreviewDetails

Polars for GOE 319 (HANSA-BRANDENBURG II) AIRFOIL (goe319-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe319-il50,000926.1 at α=5.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe319-il50,000536.7 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe319-il100,000953.3 at α=5.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe319-il100,000555.2 at α=4.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe319-il200,000975.2 at α=4.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe319-il200,000571.6 at α=3.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe319-il500,0009101.6 at α=3.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe319-il500,000591.1 at α=7°Mach=0 Ncrit=5Xfoil predictionDetails
   goe319-il1,000,0009114 at α=8°Mach=0 Ncrit=9Xfoil predictionDetails
   goe319-il1,000,0005112.8 at α=8.25°Mach=0 Ncrit=5Xfoil predictionDetails
Reynolds number calculator
Set Reynolds number and Ncrit rangeLowHigh
Reynolds Number
NCrit