TUO
Aeroelasticity and Dynamics of Deployable Space Structures
✓ Funded (Competition)
🎓 Aerospace Engineering
🎓 Dynamics
🎓 Fluid Mechanics
🎓 Machine Learning
🎓 Mathematical Modelling
🎓 Mechanical Engineering
🎓 Mechanics
🎓 Solid Mechanics
🎓 Structural Mechanics
mathematical modelling
computational modelling
aeroelasticity
Martian environments
deployable space structures
low-gravity
lunar environments
space engineering
structural dynamics
This PhD investigates the coupled aeroelastic and dynamic behaviour of deployable space structures, such as solar arrays and antennas, to understand and optimize deployment reliability, vibration modes, and operational performance in low-gravity and extraterrestrial environments.
Project Description
Deployable space structures rely on flexible materials for folding, stowing, and deployment. In low-gravity or planetary environments, inertial forces, thermal stresses, and environmental interactions (e.g., dust, micrometeoroid impacts) can cause vibrations, buckling, or oscillations that compromise functionality. Unlike rigid components, these structures require careful analysis of coupled structural and dynamic interactions.
This project will develop a comprehensive theoretical and computational framework to model these interactions. Key objectives include:
Developing mathematical and computational models capturing coupled dynamics of structural deformation, inertial loads, and environmental forces during deployment and operation.
Quantifying the influence of structural properties (membrane stiffness, hinge flexibility, mass distribution, damping) on deployment reliability, vibration modes, and functional stability.
Exploring strategies to optimize structure design for consistent deployment, long-term stability, and resistance to dynamic perturbations in lunar, Martian, or orbital conditions.
Simulating environmental interactions (dust, thermal gradients, micrometeoroid impacts) to predict operational performance and guide material and mechanism selection.
Providing insights for mission planning, including deployment sequences, robotic assistance, and structural health monitoring.
Entry Requirements
Applicants should have or expect a 2.1 honours degree or master’s (or equivalent) in a relevant science or engineering discipline.
How to Apply
Apply online via https://uom.link/pgr-apply-2425
. Specify the project title, supervisor name, funding status, previous study, and two referees. Upload final and interim transcripts, CV, supporting statement, and English language certificate (if applicable). Contact the supervisor for informal enquiries.
. Specify the project title, supervisor name, funding status, previous study, and two referees. Upload final and interim transcripts, CV, supporting statement, and English language certificate (if applicable). Contact the supervisor for informal enquiries.
Eligibility
UK/Home
EU
International
Supervisor Profile
DA
Dr Ajay Harish
The University of Manchester, Department of Mechanical and Aerospace Engineering
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