The interaction between a flexible structure and the surrounding fluid gives rise to a variety
of phenomena with applications in many areas, such as, stability analysis of airplane wings …

Shell-like structures are used in various engineering applications including civil, aerospace,
mechanical, marine, and automotive engineering. This article reviews most of the recent …

HYPERSONIC flight began in February 1949 when a WAC Corporal rocket was ignited from
a US-captured V-2 rocket [1]. In the six decades since this milestone, there have been …

Domain decomposition is nowadays a common way to speed up complex computations.
However, the discrete meshes used in the different domains do not have to match at their …

The aerodynamic performance of a wing deteriorates considerably as the Reynolds number
decreases from 106 to 104. In particular, flow separation can result in substantial change in …

Aeroelasticity is still dynamic, challenging, and a key part of cutting-edge airplane
technology. Emerging trends, as well as challenges and needs in the eld of airplane …

In multiphysics simulations using a partitioned approach, each physics component solves on
its own mesh, and the interfaces between these meshes are in general non‐matching …

In this paper, an integrated geometrically nonlinear aeroelastic framework to analyze the
static nonlinear aeroelastic response of morphing composite wing with orthotropic materials …

Preliminary aircraft design studies use structural weight models that are calibrated with data
from existing aircraft. Computing weights with these models is a fast procedure that provides …

In fluid–structure interaction (FSI) simulations the meshes at the fluid–structure interface
usually do not match due to the different mesh requirements for the flow and structure. The …