The paper is focused on the development of a validated procedure for modelling, by means
of Finite Element tools, the post-buckling behaviour of stiffened composite flat panels …

The structural behaviour of composite stiffened flat panels under axial compression is here
investigated up to collapse. The panel configuration is designed to buckle once the limit load …

This paper presents a detailed experimental and numerical investigation on absorption and
shear behaviors of stiffened composite panel subjected to hygrothermal environment. Due to …

The results of numerical studies carried out on high‐aspect‐ratio wings with different
planforms are discussed: the transonic regime is analysed for a swept wing and a curved …

Multi-walled carbon nanotube-reinforced epoxy matrix composites are processed with
varying reinforcement fractions and the fracture toughness and mechanical properties are …

Traditional aircraft composite stiffened panels are designed to avoid buckling of the skin at
service loads, to prevent initiation and growth of delamination damages. In stitched …

The high-strength-to-weight ratio and corrosion resistance properties of glass-fiber-
reinforced polymer (GFRP) composites makes them potentially well-suited for application in …

This research investigates the postbuckling behaviour of composite stiffened panels under
axial compression up to collapse. Two different panel configurations are designed to …

Aircraft producers have extensively adopted the use of T-shaped stiffened fibre reinforced
composite panels in the thin walled structures such as the fuselage and wings. The …

The high-strength-to-weight ratio and corrosion resistance properties of glass-fiber-
reinforced polymer (GFRP) composites makes them potentially well-suited for application in …