This paper compares early and very recent approaches to the static analysis of reinforced-
shell wing structures. Early approaches were those based on the pure semimonocoque …

DEFORMATIONS of aircraft's structure during flight have a significant effect on the
aerodynamic performance of the aircraft. The process of aircraft wing design is …

In the framework of structural mechanics, the classical beam theories that are commonly
adopted in many applications may be affected by inconsistencies, because they are not able …

The need for better conceptual design methodologies of skin/stringer wing-box panels
becomes apparent when a large number of candidate material and geometric shapes must …

Equivalent beam finite element models, also known as stick models, are often used for static
or dynamic aeroelastic analysis and optimization. These stick models are usually generated …

The design of a large aircraft at high speeds is a challenge in the very active research on
aeroelasticity. The computational aeroelasticity analysis in 3D for such a large system of …

The need for better conceptual design methodologies of skin/stringer wing-box panels
becomes apparent when a large number of candidate material and geometric shapes must …

Equivalent beam finite element models, also known as stick models, are often used for static
or dynamic aeroelastic analysis and optimization. These stick models are usually generated …