LIGHTWEIGHT MATERIALS FOR AIRCRAFT APPLICATIONS

Citation
Jp. Immarigeon et al., LIGHTWEIGHT MATERIALS FOR AIRCRAFT APPLICATIONS, Materials characterization, 35(1), 1995, pp. 41-67
Citations number
86
Categorie Soggetti
Materials Science, Characterization & Testing
Journal title
ISSN journal
10445803
Volume
35
Issue
1
Year of publication
1995
Pages
41 - 67
Database
ISI
SICI code
1044-5803(1995)35:1<41:LMFAA>2.0.ZU;2-Z
Abstract
Reducing structural weight is one of the major ways to improve aircraf t performance. Lighter and/or stronger materials allow greater range a nd speed and may also contribute to reducing operational costs. The ar ticle reviews some recent developments in lightweight materials for ai rframe components (aluminum alloys, composites, and hybrid materials) and engine components (titanium aluminides and titanium-based composit es). Emphasis is placed on microstructural characterization and the re lationship between the microstructure and mechanical properties of spe cific materials systems being investigated at the National Research Co uncil's Institute for Aerospace Research.