Skip to Main Content
Umbrella Alt Text
header search
Search
Advanced Search
Search ASM
Skip Nav Destination
Properties and Selection of Aluminum Alloys
ASM Handbook
Properties and Selection of Aluminum Alloys
Edited by
Kevin Anderson
Kevin Anderson
Search for other works by this author on:
This Site
Google Scholar
John Weritz
John Weritz
Search for other works by this author on:
This Site
Google Scholar
J. Gilbert Kaufman
J. Gilbert Kaufman
Search for other works by this author on:
This Site
Google Scholar
ASM International
Volume
2B
DOI:
https://doi.org/10.31399/asm.hb.v02b.9781627082105
ISBN electronic:
978-1-62708-210-5
Publication date:
2019
Book Chapter

6156: Fuselage Sheet

Doi:
https://doi.org/10.31399/asm.hb.v02b.a0006722
  • Published:
    2019
Page range:
404
Search with book

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.

Topics
Creep-fatigue crack growth, Sheets and strips, Aluminum alloys, Weldability, Fracture toughness, Fuselage and wing structures
You do not currently have access to this chapter.
Don't already have an account? Register
Citation

6156: Fuselage Sheet, Properties and Selection of Aluminum Alloys, Vol 2B, ASM Handbook, Edited By Kevin Anderson, John Weritz, J. Gilbert Kaufman, ASM International, 2019, p 404, https://doi.org/10.31399/asm.hb.v02b.a0006722

Download citation file:

  • ASM International
  • 9639 Kinsman Road
  • Materials Park, OH 44073-0002
Close Modal
This Feature Is Available To Subscribers Only

or Create an Account

Close Modal
Close Modal
This site uses cookies. By continuing to use our website, you are agreeing to our privacy policy.
Accept