ADVANCED STRESS ANALYSIS - 2020/1
Module code: ENG3171
Module Overview
As engineers it is important to avoid structure or component failure due to overloading or excessive deflection, and stress analysis is the way of assessing such conditions. This module extends the stress analysis delivered in earlier years to cover advanced topics to provide the student with a comprehensive range of skills. This includes increased complexity due to component shape (non-symmetric sections, plates) and stresses caused by loading conditions not previously considered in detail (pressure, torsion and shear forces). Many structures, components and forms of loading are too complex to obtain exact solutions for. In such cases Energy methods can often be used to provide approximate solutions, enabling the engineer to carry out structural assessment. The module shows how energy methods can be used to find the response of structural systems to static loads.
Module provider
Mechanical Engineering Sciences
Module Leader
VIQUERAT Andrew (Mech Eng Sci)
Number of Credits: 15
ECTS Credits: 7.5
Framework: FHEQ Level 6
Module cap (Maximum number of students): N/A
Overall student workload
Independent Learning Hours: 106
Lecture Hours: 33
Tutorial Hours: 11
Module Availability
Semester 2
Prerequisites / Co-requisites
None
Module content
Indicative content includes:
Asymmetric bending of beams:
Product 2nd moment of area
Symmetric sections, asymmetric loading
Asymmetric sections
Axes of maximum and minimum bending stiffness
Torsion of non-circular sections:
Thin closed tubes - stress and twist
Open straight thin walled sections - stress and twist
Thin walled cellular structures - stress and twist
Shearing of thin walled sections:
Open sections - shear distribution and shear centre
Closed sections - shear distribution and shear centre
Pressurised thick walled cylinder
Lames equations
Internal and external pressure
Compound cylinders
Circular plates:
Moment-deflection stress relationships
General deflection equation
Displacement and stresses for various boundary conditions
Annular plates
Energy theorems:
Method of virtual forces and displacements
Theorem of stationary total potential energy
Deflection of beams:
Strain and potential energy in terms of deflection
Choice of suitable deflected shapes for various end conditions
Solutions for constant and stepped section beams
Deflection of plates:
Moment and torque-deflection-stress relationships
Strain energy expression for plate in terms of deflections
Solution of different types of planar edge boundary conditions
Buckling of beams and plates:
Beams
In-plane energy terms
Plates
Assessment pattern
Assessment type | Unit of assessment | Weighting |
---|---|---|
Examination | EXAMINATION (2 HRS) | 70 |
School-timetabled exam/test | IN-SEMESTER TEST 1 (1 HOUR) | 10 |
School-timetabled exam/test | IN-SEMESTER TEST 2 (1 HOUR) | 10 |
School-timetabled exam/test | IN-SEMESTER TEST 3 (1 HOUR) | 10 |
Alternative Assessment
All tests replaced by coursework.
Assessment Strategy
The assessment strategy is designed to provide students with the opportunity to demonstrate their proficiency in applying some of the core concepts of stress analysis to real problems.
The summative assessment for this module consists of:
- 3 class tests [ Learning outcome 1, 2 ] (3 hours) {30%}
- Examination [ Learning outcomes 1, 2 ] (2 hours) {70%}
Formative assessment and feedback
- Formative verbal feedback is given in tutorials and following class tests 1 and 2
Module aims
- complete the strength and stiffness analyses of previous courses by considering other forms of commonly encountered structures and structural loading
- provide an awareness of the role of energy principles generally in determining approximate solutions for complex structural problems
Learning outcomes
Attributes Developed | ||
1 | Calculate the strength and stiffness of a representative range of structures subject to static loading | KC |
2 | Demonstrate a comprehensive understanding of the concept of stationery potential energy and use this to obtain estimates of the response of rectangular plates to both lateral and in-plane loading. | KC |
Attributes Developed
C - Cognitive/analytical
K - Subject knowledge
T - Transferable skills
P - Professional/Practical skills
Methods of Teaching / Learning
The learning and teaching strategy is designed to:
The material is delivered in a series of lectures for which there are supporting tutorial questions. Problems in solving the tutorial questions are covered in the tutorial sessions. The module is supported through SurreyLearn with extensive online module information, notes, tutorial solutions and past papers with numerical solutions.
The learning and teaching methods include:
- 3 hours lectures per week x 11 weeks
- 1 hour tutorial per week x 11 weeks
Indicated Lecture Hours (which may also include seminars, tutorials, workshops and other contact time) are approximate and may include in-class tests where one or more of these are an assessment on the module. In-class tests are scheduled/organised separately to taught content and will be published on to student personal timetables, where they apply to taken modules, as soon as they are finalised by central administration. This will usually be after the initial publication of the teaching timetable for the relevant semester.
Reading list
https://readinglists.surrey.ac.uk
Upon accessing the reading list, please search for the module using the module code: ENG3171
Programmes this module appears in
Programme | Semester | Classification | Qualifying conditions |
---|---|---|---|
Biomedical Engineering MEng | 2 | Optional | A weighted aggregate mark of 40% is required to pass the module |
Aerospace Engineering BEng (Hons) | 2 | Optional | A weighted aggregate mark of 40% is required to pass the module |
Automotive Engineering MEng | 2 | Optional | A weighted aggregate mark of 40% is required to pass the module |
Mechanical Engineering BEng (Hons) | 2 | Optional | A weighted aggregate mark of 40% is required to pass the module |
Mechanical Engineering MEng | 2 | Optional | A weighted aggregate mark of 40% is required to pass the module |
Aerospace Engineering MEng | 2 | Optional | A weighted aggregate mark of 40% is required to pass the module |
Please note that the information detailed within this record is accurate at the time of publishing and may be subject to change. This record contains information for the most up to date version of the programme / module for the 2020/1 academic year.