The aviation sector is experiencing an increasing pressure to reduce emissions via long-
term strategies for a ceaselessly growing number of flight passengers. Aircraft currently in …

A high-fidelity simulation of the shock/transitional boundary layer interaction caused by a
axisymmetrical compression ramp is performed at a free stream Mach number of 5 and a …

We perform the large-eddy simulation of the flow past a helicopter rotor to support the
investigation of rotorcraft wake characteristics and decay mechanisms. A hybrid Lagrangian …

In this paper, we present recent improvements of an Immersed Boundary Method (IBM) for
the simulation of turbulent compressible flows on Cartesian grids. The proposed approach …

A high-fidelity simulation of the massively separated shock/transitional boundary layer
interaction caused by a 15-degrees axisymmetrical compression ramp is performed at a free …

We aim at computing time-and span-periodic flow fields in span-invariant configurations.
The streamwise and cross-stream derivatives are discretised with finite volumes while time …

For many years, aircraft noise reduction has been the subject of research studies and
continuous improvements were achieved through an enhanced understanding of the noise …

In the past decades, a wide range of immersed boundary approaches have been developed
to deal with incompressible flows for elastic and moving obstacles Due to the increase of the …

Abstract The Council of European Aerospace Societies (CEAS) Aeroacoustics Specialists
Committee (ASC) supports and promotes the interests of the scientific and industrial …

T role of supersonic air inlets is to decelerate the incoming supersonic air to a low subsonic
flow. This operation must induce the minimum possible total pressure losses while ensuring …