PhD in Bio-inspired Active Morphing Aircraft Wing: Design, Aeroelasticity Modelling, and Control University of Birmingham in United Kingdom

Are you passionate about developing next-generation adaptive aircraft that mimic nature? This fully funded PhD opportunity at the University of Birmingham invites you to join a cutting-edge research project focused on the design, experimental investigation, aeroelasticity modelling, and control of an aircraft wing with a bio-inspired active morphing wingtip. The project is led by Dr Jun Wu in the School of Metallurgy & Materials, within the College of Engineering and Physical Sciences.

The research aims to develop a small-scale wing prototype featuring a bio-inspired morphing wingtip, utilizing smart materials for both actuation and self-sensing. The long-term vision is to create aircraft with actively morphing wingtips that sense and respond to aerodynamic loads in real time, closely mimicking avian flight. The project will involve an integrated computational–experimental approach, including CAD for structural design, aeroelasticity modelling, experimental validation, and control system development for active morphing integration. Experimental work will include modal, fatigue, and wind tunnel testing.

This PhD offers a comprehensive research journey from structural design and dynamics to aeroelasticity and flight control. The project directly contributes to the UK’s net-zero aviation targets by improving aerodynamic efficiency and reducing emissions. You will join a vibrant, multidisciplinary aerospace team with access to dedicated experimental dynamics facilities and opportunities for collaboration with researchers at the University of Bristol and the University of Oxford.

Funding: Home students receive a tax-free annual stipend of £20,780 for up to 3.5 years, plus full tuition fee coverage. International students receive tuition fee coverage only. Additional funding is available for training events, workshops, and academic conferences.

Eligibility: Applicants must have a 1st class undergraduate or Master’s degree (or equivalent) in Aerospace Engineering, Mechanical Engineering, or a related discipline. Essential skills include knowledge of structural dynamics and experimental testing, and motivation for hands-on laboratory work and independent research. Experience with CAD/FEA (Abaqus/ANSYS), MATLAB/Simulink, wind tunnel testing, and flight dynamics and control is desirable.

Application: Applications are accepted year-round. Apply via the University of Birmingham’s online system. Please provide a cover letter summarizing your research interests and suitability, a CV, transcripts, and contact details of two referees. It is recommended to contact Dr Jun Wu ([email protected]) before applying.

For more information and to apply, visit the official project page or the university application portal.