6H-SiC transistor integrated circuits demonstrating prolonged operation at 500 deg C
100 years of flight, Part 2: A century of progress in aircraft materials
Accession of titanium as an aircraft material - a current view
Accuracy of a simple hole damage analysis method in composite structures
A chromate-free post-anodising treatment for aluminium alloys using a double-immersion process
A comparative study of the pin-bearing responses of two glass-based fibre metal laminates
A comparison of shaped piezoelectric actuators for divergence control
A comparison of the fatigue behavior of high strength cast aluminum alloys 201 and A 357