Marage Steel for Welded Airframe Structure

Format:

Conference/Event

Author/Creator:

Hofstatter, Alfred F., author.

Conference Name:

National Aeronautic and Space Engineering and Manufacturing Meeting (Los Angeles, Calif)

Language:

English

Physical Description:

1 online resource

Place of Publication:

Warrendale, PA SAE International 1963

Summary:

Eighteen percent nickel marage steel can be used to fabricate welded airframe structure. The weldability is excellent and the heat treatment is simple. The mechanical properties of marage steel sheet is presented at ambient and elevated temperatures. TIG welded properties are also determined. The adaptation of this alloy for use in a tubular truss weldment is discussed. The tensile, notch tensile, and compressive yield strengths are very good, but the fatigue strength is low compared to a weldable low alloy steel. Marage steel can be used to advantage for high strength, short life applications such as experimental aircraft structure

Notes:

Vendor supplied data

Publisher Number:

630389

Access Restriction:

Restricted for use by site license