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.