Parametric fuselage design - integration of mechanics ads acoustic & thermal insulation

Multi-disciplinary design of aircraft fuselage structures

Post-buckled precompressed (PBP) piezoelectric actuators for UAV flight control

A generalized stress singularity approach for material failure prediction and its application to adhesive joint strength analysis

Integration of acoustics and mechanics in a stiffened shell fuselage, III

Application of a Visco-Elastic Layer. Part V

Integration of mechanics and acoustics in a sandwich fuselage Part IV

Design and technology in aerospace, flying high

Design and technology in aerospace; parametric modelling of complex systems including active components

A design & engineering engine to investigate acoustics in preliminary fuselage design

Active noise control in fuselage design

Design and Technology in aerospace, flying high

A Design Engine to Evaluate Sound Damping of Flat Panels in the Low Frequency Range

Development of an ICAD Generative Model for Blended Wing Body Aircraft Design

Development of an ICAD Generative Model for Aircraft Design, Analysis and Optimisation

Overview of numerical results for the Smart Panels Project

A numerical method to analyse and design adhesively bonded joints in structures

Numerical Tool to predict transfer functions of panels developed for the Smart Panel Project

Experimental verification of a numerical model to analyse and design adhesively bonded joints connections in structures