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

GOE 137 (MVA H.15) AIRFOIL (goe137-il)

GOE 137 (MVA H.15) AIRFOIL - Gottingen 137 (MVA H.15) airfoil


Airfoil goe137-il
Details Dat file Parser  
(goe137-il) GOE 137 (MVA H.15) AIRFOIL
Gottingen 137 (MVA H.15) airfoil
Max thickness 8.6% at 29.9% chord.
Max camber 4.4% at 39.9% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 137 (MVA H.15) AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0123200 0.0175300
 0.0247100 0.0276600
 0.0495600 0.0420200
 0.0744500 0.0522900
 0.0993600 0.0610500
 0.1492400 0.0719700
 0.1991500 0.0801000
 0.2990800 0.0870600
 0.3991100 0.0856100
 0.4991700 0.0785700
 0.5993000 0.0668200
 0.6994400 0.0528800
 0.7996000 0.0376400
 0.8997900 0.0199900
 0.9498900 0.0105200
 1.0000000 0.0014500

 0.0000000 0.0000000
 0.0125900 -.0089700
 0.0251100 -.0105400
 0.0501200 -.0110700
 0.0751200 -.0112100
 0.1001000 -.0099400
 0.1500700 -.0063200
 0.2000400 -.0033900
 0.2999900 0.0011600
 0.3999700 0.0028200
 0.4999600 0.0038700
 0.5999500 0.0038300
 0.6999600 0.0033800
 0.7999800 0.0019400
 0.9000000 0.0003900
 0.9500100 -.0007800
 1.0000000 -.0014500
No parser warnings Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file

Similar airfoils

GOE 180 (MVA H.26) AIRFOILPreviewDetails
GOE 117 (MVA MK.4) AIRFOILPreviewDetails
Eiffel 428 (Bleriot)PreviewDetails
GOE 326 (PFALZ 55) AIRFOILPreviewDetails
GOE 287 AIRFOILPreviewDetails
GOE 281 (DAIMLER XII) AIRFOILPreviewDetails
GOE 310 (MVA H.42) AIRFOILPreviewDetails
GOE 450 AIRFOILPreviewDetails
I.S.A. 960PreviewDetails
S4320PreviewDetails

Polars for GOE 137 (MVA H.15) AIRFOIL (goe137-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe137-il50,000935.2 at α=9.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe137-il50,000539.8 at α=7°Mach=0 Ncrit=5Xfoil predictionDetails
   goe137-il100,000956.9 at α=7.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe137-il100,000559.5 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe137-il200,000978.4 at α=6.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe137-il200,000577.3 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe137-il500,0009104.3 at α=5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe137-il500,000597.3 at α=4.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe137-il1,000,0009120.7 at α=4.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe137-il1,000,0005109.2 at α=3.75°Mach=0 Ncrit=5Xfoil predictionDetails
Reynolds number calculator
Set Reynolds number and Ncrit rangeLowHigh
Reynolds Number
NCrit