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Details of Grant 

EPSRC Reference: EP/W032236/1
Title: Nonlinear Ground Vibration Testing using Control-based Continuation
Principal Investigator: Renson, Dr L
Other Investigators:
Researcher Co-Investigators:
Project Partners:
Rolls-Royce Plc (UK) Vertical Aerospace Ltd
Department: Mechanical Engineering
Organisation: Imperial College London
Scheme: New Investigator Award
Starts: 03 January 2023 Ends: 02 January 2026 Value (£): 500,651
EPSRC Research Topic Classifications:
Eng. Dynamics & Tribology
EPSRC Industrial Sector Classifications:
Aerospace, Defence and Marine
Related Grants:
Panel History:
Panel DatePanel NameOutcome
06 Apr 2022 Engineering Prioritisation Panel Meeting 6 and 7 April 2022 Announced
Summary on Grant Application Form
The UK is a world leader in the design, manufacture, and support of high-value aeronautic structures such as wings and jet engines. The UK's technology strategy is to reduce aeronautic structure weight by 35% by 2035 compared to 2019. Lighter structures are prone to complex nonlinear phenomena which cannot be identified and characterised using current ground vibration tests (GVTs). Building on recent advances in control-based continuation and nonlinear modal analysis, this project will develop a general and systematic GVT method that can overcome this issue. The method will be demonstrated on two academic benchmark structures before being tested on a full-scale aircraft structure thanks to an international collaboration with ONERA. The project will not only unlock the rigorous characterization of modal properties of nonlinear structures but will also bridge the gap currently preventing the development and validation of nonlinear models.
Key Findings
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Summary
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Further Information:  
Organisation Website: http://www.imperial.ac.uk