← Airfoil Catalog

NACA 63(2)-215 MOD B

NACA 63(2)-215 MOD B outline

Filename: n63215b.dat
t/c: 15.0%
Max Camber: 1.5%

Download Selig Coordinates Run in Airfoil Model

Quick Analysis

Reynolds Number

Include Mach Number

Errors & Warnings

Similar Airfoils