The Application of New Technology to Military Aircraft Structure Rockwell International Corporation

Format:

Conference/Event

Author/Creator:

Haviland, George P., author.

Conference Name:

Aerospace Engineering and Manufacturing Meeting (1975-11-17 : Los Angeles, California, United States)

Language:

English

Physical Description:

1 online resource

Place of Publication:

Warrendale, PA SAE International 1975

Summary:

The paper presents some of the problems encountered when advanced technology hardware and/or software are made a part of an ongoing system such as the B-1 bomber. The introduction of diffusion bonded Titanium, superplastically formed parts and the use of boron reinforced longerons are three examples of new technological applications of hardware. The requirement to conduct a fracture mechanics control program, the new computer programto determine the combination of the fatigue effects and fracture behavior and a new flutter optimization methodology are three other examples of new applications of software to a military aircraft. The paper treats each example to show why it was adopted, the pressing need to make it work in the real world outside the laboratory and some of the problems of using the new technology which were not anticipated

Notes:

Vendor supplied data

Publisher Number:

751081

Access Restriction:

Restricted for use by site license