Skip to Main Content

Abstract

Alloy 6156 is an Al-Si-Mg-Cu-Mn weldable alloy, developed for the lower portion of the fuselage, which required a T6 temper strength level and high damage tolerance properties. This datasheet provides information on key alloy metallurgy of this 6xxx series alloy. Fatigue crack growth and material toughness for various thicknesses of alloy 6156 clad T62 are illustrated.

You do not currently have access to this chapter.
Don't already have an account? Register

2019. "6156: Fuselage Sheet", Properties and Selection of Aluminum Alloys, Kevin Anderson, John Weritz, J. Gilbert Kaufman

Download citation file:


Close
Close Modal
This Feature Is Available To Subscribers Only

Sign In or Create an Account

Close Modal
Close Modal