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of the Extended Finite Element Method (XFEM), the mechanisms of fracture and crack propagation in advanced composite structures such as fibre metal laminates (FML) used in the aerospace industries. Funding Notes
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the development of new numerical strategies, e.g. pioneering the use of the Extended Finite Element Method in the prediction of delamination in composite structures (Curiel Sosa et al., 2018). This will permit you
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Structural Integrity Finite Element Analyses of Formula I Composite Panels for Safer and Lighter Designs School of Mechanical, Aerospace and Civil Engineering PhD Research Project Self Funded Dr J L
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Advanced metal matrix composite machining for aerospace applications School of Mechanical, Aerospace and Civil Engineering PhD Research Project Self Funded Prof Hassan Ghadbeigi Application
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Advanced metal matrix composite machining for aerospace applications School of Mechanical, Aerospace and Civil Engineering PhD Research Project Self Funded Prof Hassan Ghadbeigi Application Deadline
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the prediction of chip formation and service life of the components. Previous experience / requirements: Experimental methods, Finite element modelling, computer programming, Manufacturing Please contact Dr
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, or other Relevant Discipline. Previous experience / requirements: Finite element modelling, experimental solid mechanics View DetailsEmail EnquiryApply Online
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degree in Engineering, Materials Science, Physics, Chemistry, Applied Mathematics, or other Relevant Discipline. Previous experience / requirements: Finite element modelling, Composites, Fracture mechanics
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/ requirements: Experimental methods, Finite element modelling, computer programming, Manufacturing Please contact Dr Hassan Ghadbeigi (h.ghadbeigi@sheffield.ac.uk) for more details. Funding Notes This project
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Discipline. Previous experience / requirements: Finite element modelling, Fracture mechanics View DetailsEmail EnquiryApply Online