Potential Use of Work Hardening Aluminum Alloy X5090 Sheet in Civil Aircraft Conalco, Incorporated

Format:

Conference/Event

Author/Creator:

Graham, D. L., author.

Conference Name:

National Business Aircraft Meeting and Engineering Display (1974-04-02 : Wichita, Kansas, United States)

Language:

English

Physical Description:

1 online resource

Place of Publication:

Warrendale, PA SAE International 1974

Summary:

Aluminum alloy X5090, containing a nominal 7% magnesium, is a recent introduction to the moderately high-strength class of alloys, but it represents a change from a heat-treatable to a work-hardening type. Advantages of low density, corrosion resistance, fatigue, and fracture toughness are stressed. Mechanical, physical, and corrosion properties are presented, with emphasis on problems related to stress-corrosion and formability, and their solutions. Potential uses are discussed

Notes:

Vendor supplied data

Publisher Number:

740398

Access Restriction:

Restricted for use by site license