About this document
NACA 6415 Airfoil Characteristics by Paul Gernah is a document available to read on EtoBox.
The document provides airfoil characteristics data for the NACA 6415 airfoil profile. It includes tables with lift coefficient (CL), angle of attack (α), drag coefficient (CD), pitching moment coefficient (Cm), and other values across a range of angles of attack. The tables are accompanied by graphs of the lift, drag, and moment coefficients as functions of alpha. Equations are also provided for calculating corrections and adjustments to the coefficient values based on airfoil geometry.
- Author
- Paul Gernah
- Language
- EN