ALUMINUM 7079 is a high strength alloy especially applicable to highly stressed aircraft parts in thick sections. It responds to age-hardening heat treatment. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties. It also includes information on corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: Al-84. Producer or source: Aluminum Company of America.

aircraft components, Aluminum 7079, chemical composition, corrosion-resistant alloys, elasticity, hardness, heat treatability, joinability, machinability, physical properties, tensile properties, workability
This content is only available as a PDF.
Copyright © ASM International® 1996
1996
ASM International
Topics
Aircraft components Corrosion-resistant alloys Aluminum alloys Chemical composition Heat treatability Joinability Machinability Workability Elastic modulus Hardness Tensile properties Physical properties Thermal properties
You do not currently have access to this content.