In this paper, a new flexible sandwich structure is introduced, which can be employed in
morphing aircrafts capable of intelligently changing their shape in different flight conditions …

Geometrically nonlinear aeroelastic behavior of pretwisted composite high aspect ratio
wings, structurally modeled as thin walled beams (TWB) is studied. The structural equations …

This study reports the formulation of a realistic aircraft wing model based on thin-walled
composite beam theory. In this model, NACA 4-digit-series airfoils were selected for the wing …

Calculation Method for the effective shear modulus of composite plates with sandwich cores
is presented. This elastic coefficient represents one very important material property …

This study investigates the flexural–torsional coupled vibration of thin-walled composite
beams. We first derived the thin-walled beam theory for an arbitrary cross-section and …

The coupled bending-torsion flutter is here investigated through Carrera Unified Formulation
(CUF). The hierarchical capabilities of CUF offer a procedure to obtain refined one …

Flutter is one of the most known instability phenomena. This condition occurs when a given
structure exhibits sustained, harmonic oscillations, sometimes leading to catastrophic …

W pracy przedstawiono koncepcję badań sztywności giętnej i skrętnej oraz sposób
wyznaczania środka sił poprzecznych cienkościennej, kompozytowej struktury skrzydła …