Learning Outcomes:
On successful completion of this subject the student will be able to:
1. Formulate an analytical solution for the stress fields in classic elasticity problems using the method of Airy stress functions.
2. Calculate the state of stress in thick-walled composite cylinders formed by a specified interference fit between an outer jacket and an inner sleeve.
3. Calculate the deflections and bending stresses of commonly-encountered rectangular & circular plates subjected to a variety of boundary conditions.
4. Analyze dynamic stress waves in bars subjected to impact loading.
5. Determine the collapse load for simple beam structures.