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Curricular information is subject to change
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.
Student Effort Type | Hours |
---|---|
Lectures | 30 |
Tutorial | 6 |
Laboratories | 2 |
Autonomous Student Learning | 72 |
Total | 110 |
Not applicable to this module.
Description | Timing | Component Scale | % of Final Grade | ||
---|---|---|---|---|---|
Not yet recorded. |
Resit In | Terminal Exam |
---|---|
Spring | No |
• Feedback individually to students, post-assessment
• Group/class feedback, post-assessment
Assignments: Feedback for Brightspace Quizzes will be available immediately after the Quiz has been submitted. Laboratory Report: Will be submitted via Brightspace and a short individual feedback will be provided (also via Brightspace) by the teaching assistant in charge of the lab. Exam: Individual feedback will be provided on request after the final results have been released.