Non-linear model reduction for flexible structures
Lead Research Organisation:
CRANFIELD UNIVERSITY
Department Name: Sch of Aerospace, Transport & Manufact
Abstract
This studentship will answer the following question: can we use a model reduction strategy when dealing with the non-linear dynamics of a high aspect ratio wing structure in experimental conditions? The research will resort to recently developed techniques in non-linear dynamics, based on spectral-submanifolds and non-linear normal modes to represent the non-linear dynamic behaviour of a structure with a reduced non-linear model with few degrees of freedom (less than ten) that could be easily numerically integrated in a simulation environment.
Organisations
Publications
DaĆ¢ssi D
(2023)
Degradation of endocrine-disrupting chemicals in wastewater by new thermophilic fungal isolates and their laccases.
in 3 Biotech
Dessena G
(2023)
The Accuracy and Computational Efficiency of the Loewner Framework for the System Identification of Mechanical Systems
in Aerospace
Dessena G
(2022)
Ground Vibration Testing of a Flexible Wing: A Benchmark and Case Study
in Aerospace
Dessena G
(2024)
A global-local meta-modelling technique for model updating
in Computer Methods in Applied Mechanics and Engineering
Dessena G
(2023)
A Loewner-Based System Identification and Structural Health Monitoring Approach for Mechanical Systems
in Structural Control and Health Monitoring
Studentship Projects
Project Reference | Relationship | Related To | Start | End | Student Name |
---|---|---|---|---|---|
EP/N509450/1 | 30/09/2016 | 29/09/2021 | |||
2277626 | Studentship | EP/N509450/1 | 30/09/2019 | 29/09/2022 | Gabriele Dessena |
EP/R513027/1 | 30/09/2018 | 29/09/2023 | |||
2277626 | Studentship | EP/R513027/1 | 30/09/2019 | 29/09/2022 | Gabriele Dessena |