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Thesis

Development of data-driven constitutive models for aerospace materials

Abstract:

This study presents novel techniques to develop data-driven constitutive models. The adoption of data-based machine learning-driven models obtained from mechanical loading experiments allows for the accurate and computationally efficient prediction of the mechanical behaviour of materials eliminating the need for theoretical assumptions and potential constraints associated with traditional models.

The research is divided into four phases. In the first phase, uniaxial compression experimental data is used to develop surrogate models for the temperature and strain-rate dependent stress-strain response of a polymeric syntactic foam. In the second phase, the proposed techniques are applied to the history-dependent non-monotonic uniaxial response of commercially pure titanium. The third phase introduces a strategy to formulate data-driven constitutive models from random multiaxial experiments. The obtained surrogate constitutive models are capable of capturing the in-plane stress response of isotropic, elastic-plastic materials loaded by combined normal and shear stresses. The feasibility of this approach is evaluated by conducting virtual experiments by means of Finite Element (FE) simulations in which a hollow, cylindrical, thin-walled test specimen is subjected to random histories of axial displacement and rotation. Finally, in the fourth phase, the methodology developed in the third phase is applied to the real experimental combined normal and shear response of aluminium specimens.

To validate the surrogate models, their predictions are compared against experimental data not used in the training process. The results demonstrate a very good agreement between the measurements and the predictions of the data-driven surrogate models.

In conclusion, this research proposes an innovative approach to data analytics and materials constitutive modelling based on machine learning techniques, offering significant potential to enhance the accuracy and efficiency of predicting the mechanical behaviour of aerospace materials.

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Authors

More by this author
Institution:
University of Oxford
Division:
MPLS
Department:
Engineering Science
Sub department:
Engineering Science
Research group:
Solid Mechanics
Oxford college:
Linacre College
Role:
Author
ORCID:
https://orcid.org/0000-0002-1958-8559

Contributors

Institution:
University of Oxford
Division:
MPLS
Department:
Engineering Science
Sub department:
Engineering Science
Research group:
Solid Mechanics
Role:
Supervisor
ORCID:
https://orcid.org/0000-0002-3824-3679
Institution:
Imperial College London
Research group:
Department of Aeronautics
Role:
Supervisor
ORCID:
https://orcid.org/0000-0002-6696-676X


More from this funder
Funder identifier:
http://dx.doi.org/10.13039/501100013898
Funding agency for:
Tasdemir, B
Programme:
Republic of Turkey Ministry of National Education- YLSY Programme


DOI:
Type of award:
DPhil
Level of award:
Doctoral
Awarding institution:
University of Oxford

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