Within the transonic regime, the aeroelastic problems exhibit many unique characteristics
compared with subsonic and supersonic cases. Although a lot of research has been carried …

In recent years, there has been a considerable growth in the demand for low-orbit satellites,
leading to a need for more flexible and cost-effective launch systems. This study presents a …

In this paper, aeroelastic modeling of aircraft wings with variations in sweep angle, taper
ratio, and variable pre-twist angle along the span is considered. The wing structure is …

In this research, a set of computational algorithms have been developed to obtain a solution
for steady and unsteady aeroelastic effects with specific applications to rectangular and …

This research aims to investigate the static aeroelastic characteristics of a slender straight
2D wing using aerodynamic strip theory. The finite element method is employed to …

The dynamic aeroelastic responses in the transonic regime for a conventional swept wing
and a curved-planform wing, both having a high aspect ratio, are analysed in detail. Using 2 …

This paper focuses on the derivation of the aerodynamic force for the cantilever plate in
subsonic flow. For the first time, a new analytical expression of the quasi‐steady …

The goal of the paper is to investigate the static aeroelastic characteristics of the slender
straight (2D) wing using aerodynamic strip theory. The finite element method is employed to …

The results of studies on a curved planform wing are discussed: these studies consist of
three-dimensional unsteady Computational Fluid Dynamics analyses. To test the calculation …