NACA 5 Series Airfoil Generator
The NACA 5-series tool can be used to plot and extract coordinates of any NACA 5-series airfoil.
Andrew Wood | 28 September 2022
The calculator below can be used to display and extract coordinates of any NACA 5-series airfoil. The chord can be varied and either a blunt or sharp leading selected. The most common NACA 5-series airfoils are available from the drop-down menu; or alternatively you can design your own.
Select from dropdown
Create your own
Select Airfoil
Design Lift Coefficient
Chordwise Max Camber (%)
Thickness (%)
0 to 25%
Reflex Airfoil
Airfoil Designation
NACA: 23012
Chord
Number of Points
Closed Trailing Edge
Alternatively try our NACA 4 Series airfoil plotter.
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