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

GOE 235 (SCHTTE-LANZ) AIRFOIL (goe235-il)

GOE 235 (SCHTTE-LANZ) AIRFOIL - Gottingen 235 (SCHATTE-LANZ) airfoil


Airfoil goe235-il
Details Dat file Parser  
(goe235-il) GOE 235 (SCHTTE-LANZ) AIRFOIL
Gottingen 235 (SCHATTE-LANZ) airfoil
Max thickness 6.5% at 19.9% chord.
Max camber 3.5% at 39.9% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 235 (SCHTTE-LANZ) AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0121900 0.0203900
 0.0245900 0.0264800
 0.0494300 0.0369600
 0.0743000 0.0453400
 0.0991900 0.0526300
 0.1490800 0.0598000
 0.1990300 0.0631700
 0.2989600 0.0674000
 0.3989800 0.0662400
 0.4990500 0.0619900
 0.5991900 0.0523300
 0.6993600 0.0416700
 0.7995700 0.0277100
 0.8997700 0.0149600
 0.9498800 0.0077300
 1.0000000 0.0016000

 0.0000000 0.0000000
 0.0127400 -.0157000
 0.0252600 -.0166100
 0.0502000 -.0130300
 0.0751600 -.0105400
 0.1001300 -.0085600
 0.1500800 -.0050900
 0.2000300 -.0022200
 0.2999600 0.0025200
 0.3999300 0.0045600
 0.4999400 0.0040000
 0.5999600 0.0028400
 0.6999700 0.0017800
 0.7999800 0.0012200
 0.9000000 0.0000600
 0.9500200 -.0010700
 1.0000000 -.0016000
No parser warnings Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file

Similar airfoils

GOE 100 (SOPWITH) AIRFOILPreviewDetails
GOE 488 AIRFOILPreviewDetails
GOE 142 (MVA H.19) AIRFOILPreviewDetails
SA7024PreviewDetails
GOE 344 (PFALZ 71) AIRFOILPreviewDetails
AG27 Bubble Dancer DLG by Mark DrelaPreviewDetails
GOE 121 (MVA H.1) AIRFOILPreviewDetails
MA409 (smoothed)PreviewDetails
BE50 (smoothed)PreviewDetails
HAM-STD HS1-606 AIRFOILPreviewDetails

Polars for GOE 235 (SCHTTE-LANZ) AIRFOIL (goe235-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe235-il50,000936.9 at α=6.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe235-il50,000537.5 at α=4°Mach=0 Ncrit=5Xfoil predictionDetails
   goe235-il100,000952.2 at α=3.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe235-il100,000548 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe235-il200,000960.8 at α=5.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe235-il200,000557.6 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe235-il500,000973.9 at α=4°Mach=0 Ncrit=9Xfoil predictionDetails
   goe235-il500,000568.8 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe235-il1,000,000980.8 at α=5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe235-il1,000,000581.6 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
Reynolds number calculator
Set Reynolds number and Ncrit rangeLowHigh
Reynolds Number
NCrit