Problems of Transition from Aluminum to Exotic Materials in Aerospace Structures Norair Div., Northrop Corporation

Format:

Conference/Event

Author/Creator:

Emmerich, E. W., author.

Conference Name:

Aeronautic and Space Engineering and Manufacturing Meeting (1965-10-04 : Los Angeles, California, United States)

Language:

English

Physical Description:

1 online resource

Place of Publication:

Warrendale, PA SAE International 1965

Summary:

It is now necessary to implement a systems engineering approach to structural design of aerospace vehicles in order to solve interdisciplinary problems encountered between concept and product. Higher temperatures and loads beyond the structural limits of aluminum alloys dictate exotic materials ranging from titanium through the refractory materials to ceramics. This paper presents an approach to transitional problems in application of these materials, from basic material selection considerations across all the design, processing, and manufacturing technologies. Methodologies are summarized in the brazing of molybdenum, the hot forming of titanium alloys, welding and machining of titanium, and adhesive bonding techniques

Notes:

Vendor supplied data

Publisher Number:

650790

Access Restriction:

Restricted for use by site license