units
MEC4446
Faculty of Engineering
This unit entry is for students who completed this unit in 2015 only. For students planning to study the unit, please refer to the unit indexes in the the current edition of the Handbook. If you have any queries contact the managing faculty for your course or area of study.
Refer to the specific census and withdrawal dates for the semester(s) in which this unit is offered.
Level | Undergraduate |
Faculty | Faculty of Engineering |
Organisational Unit | Department of Mechanical and Aerospace Engineering |
Offered | Clayton First semester 2015 (Day) |
Coordinator(s) | Dr W Yan |
Specific modulus and specific strength; 3D stress and 3D strain tensors; anisotropic elasticity; composite lamina and composite laminate; hygrothermal strain and hygrothermal stress analysis of composite structures; failure theories for a composite lamina; micromechanical analysis of a composite lamina; classical lamination theory for composite laminate, failure analysis of composite laminates, design of composite laminates, finite element analysis of composite materials and structures.
On completion of this unit, students should be able to:
Continuous assessment: 40%
Examination (3 hours): 60%
Students are required to achieve at least 45% in the total continuous assessment component and at least 45% in the final examination component and an overall mark of 50% to achieve a pass grade in the unit. Students failing to achieve this requirement will be given a maximum of 45% in the unit.
2 hours of lectures, 2 hours of laboratory/tutorial classes and 8 hours private study per week.
See also Unit timetable information
120 credit points completed