The effort to reduce costs and environmental impact of modern commercial aircraft requires
an ever better understanding of aircraft physics, including the characterisation of the …

A thorough understanding of the effects of sloshing on aircraft dynamic loads is of great
relevance for the future design of flexible aircraft to be able to reduce their structural mass …

The aim of this work is to provide a reduced-order model to describe the dissipative behavior
of nonlinear vertical sloshing involving Rayleigh–Taylor instability by means of a feed …

The main goal of this paper is to provide a Reduced Order Model (ROM) able to predict the
liquid induced dissipation of the violent and vertical sloshing problem for a wide range of …

Characterizing the movement of space propellant in the tank subjected to maneuvers and
predicting its damping is a fundamental requirement for the success of space missions. In …

This paper explores methods to reduce aircraft design loads through an optimal fuel usage
strategy, which maximises the beneficial effects of wing-tank sloshing-induced damping. A …

Reduced-order models (ROMs) can effectively balance the accuracy and efficiency of
computational fluid dynamics (CFD). The nonlinear flow field characteristics cannot be …

A physics-based reduced order model is presented as a viable approach to accurately
predict unsteady flowfield solutions at a fraction of the computational time that is required by …

The present paper introduces the sloshing effects on aeroelastic stability and response of
flying wing configurations. Using reduced order model based on data provided by …

The fuel tank, as a significant component for the propellant system in satellites, plays an
important role in managing propellant and maintaining stability through its propellant …