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 …

This paper presents the study on vibration characteristics of an aircraft wing. A300 aircraft
wing with NACA 64215 aerofoil is used for this investigation. A computer-aided design …

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 …

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 …

The content of this paper is all about the analysis of natural frequency for avoiding
resonance on the material to prevent failure and to simulate according to the boundary …

In this study, a closely coupled fluid-structure interaction analysis is carried out in order to
investigate the effect of mass distribution on wing flutter. A commercial software is used 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 …

This paper presents an analytical feature for limit cycle oscillation (LCO) in the nonlinear
aeroelastic system of an airfoil, with major emphasis on its applications in LCO …

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 …

Erratum Erratum to (Aeroelastic Analysis of Wings in the Transonic Regime: Planform’s
Influence on the Dynamic Instability) Page 1 Erratum Erratum to (Aeroelastic Analysis of …