This paper is a review of the most influential approaches to developing beam models that
have been proposed over the last few decades. Essentially, primary attention has been paid …

Advanced structural models, based on variable one-, two-, and three-dimensional
kinematics, are proposed in this paper and applied to the analysis of the free vibration of …

This paper is devoted to investigate the aerothermoelastic flutter and thermal buckling
characteristics of composite laminated cylindrical shells with elastic boundary conditions. In …

This paper proposes the use of an advanced one-dimensional (1D) variable kinematic
model to analyze typical civil engineering structures. The model is referred to as component …

This paper aims at investigating the influence of some typical manufacturing geometric
imperfections on the pre-buckling behavior of transversally loaded GFRP I-beam. One …

Low-velocity impact responses and impact-induced damages evaluation problems are
investigated for the stiffened composite laminated plates based on the progressive failure …

This paper presents advanced-kinematics beam models to compute the dispersion
characteristics of one-dimensional guides. High-order functions are used to interpolate the …

Aircraft and spacecraft skin can undergo potentially destructive aeroelastic motions in high-
speed flight. Reliable mathematical modelling is crucial for understanding such phenomena …

Panel flutter is an aeroelastic phenomenon that can critically affect aircraft skin in supersonic
flight. The majority of works published on this subject treat each skin panel as an isolated …

In this paper, a static and free vibration analysis of functionally graded porous shallow shells
with double curvature containing an even distribution of porosity is investigated using a …