← Airfoil Catalog

NACA-0009 (smoothed)

NACA-0009 (smoothed) outline

Filename: n0009sm.dat
t/c: 9.0%
Max Camber: 0.0%

Download Selig Coordinates Run in Airfoil Model

Quick Analysis

Reynolds Number

Include Mach Number

Errors & Warnings

Similar Airfoils