Overview
Finite element analysis (FEA) in computer-aided design; finite element formulation; first-order and second-order elements; stiffness matrix; integration points and stress recovery; convergence and mesh refinement; FEA of plane stress and plane strain problems; FEA of axisymmetric problems; FEA of nonlinear materials; FEA of contact problems; FEA of large deformation problems; … For more content click the Read More button below.
Offerings
S2-01-CLAYTON-FLEXIBLE
Requisites
Prerequisite
Prohibition
Contacts
Chief Examiner(s)
Dr Katherine Grigoriou
Unit Coordinator(s)
Dr Katherine Grigoriou
Learning outcomes
On successful completion of this unit, you should be able to:
1.
Assess mesh requirements sufficient to obtain accurate results from finite element analysis.
2.
Construct finite element models for truss structures, plan stress, plane strain, axisymmetric and general 3D structural problems.
3.
Execute finite element analyses on aerospace structural problems using industry-standard software packages.
4.
Determine the strength and stiffness of composite laminate structures.
5.
Design composite laminates to meet strength, stiffness and cost requirements for aerospace applications.
Teaching approach
Problem-based learning
Online learning
Assessment summary
Continuous assessment: 100%
Assessment
1 - In-semester test 1
2 - In-semester test 2
3 - Weekly prac assessment
4 - Individual report
Scheduled and non-scheduled teaching activities
Laboratories
Workshops
Workload requirements
Workload
Availability in areas of study
E3001 Bachelor of Engineering (Honours) - Specialisation: Aerospace engineering