A mid-fidelity aerodynamic solver based on the vortex particle method for wake modeling,
DUST, is coupled through the partitioned multi-physics coupling library preCICE to a …

The study of the complex aerodynamics that characterise tiltrotors represents a challenge for
computational fluid dynamics tools. URANS numerical solvers are typically used to explore …

This work presents the high-fidelity aerodynamic and acoustic modelling processes
supporting the preliminary design of a large eVTOL vehicle at the University of Glasgow in …

Tiltrotor aircraft are challenging machines to design considering the various operating
conditions and multipurpose missions that are expected to be performed by this complex …

Abstract Electric Vertical Take-off Landing (eVTOL) vehicles can transform aviation, but the
unconventional aircraft development currently requires an extensive knowledge base. This …

The present work proposes a new aeroelastic solution applicable to rotors and tiltrotors
configuration by joining the multibody software MBDyn and the mid-fidelity aerodynamic tool …

The present paper describes the results of a numerical investigation of a wing with an
integrated propeller using the midfidelity aerodynamic solver DUST. The wing/propeller …

The tilt-wing aircraft has attracted widespread attention due to its excellent performance.
However, its aerodynamic characteristics during the tilt transition section are characterized …

A nonlinear aeroelastic numerical tool was used in the present work for the evaluation of
loads and vibratory levels of a tiltrotor aircraft during critical transient manoeuvres. The …

Tiltrotors combine the speed and range of a conventional fixed-wing aircraft with the vertical
take off and landing capabilities of helicopter, by tilting their proprotors positioned at the end …