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BEng (Hons) Aerospace Design Engineering
Information Booklet
Level 2
2007/8
University of the West of England, Bristol
Page 1
Information Booklet
ContentsThis booklet contains selected information about the year of the programme on which you areregistered.
The academic Staff involvedThe full structure of the ProgrammeThe compulsory and optional (if any) modules in your year of the programme
Students OnlineThis booklet has been generated from the FOLD database which supports the CEMS StudentsOnline web site http://www.cems.uwe.ac.uk/studentsonline. On this site you will also findinformation on:
All programmes and modules in the faculty.All staff in the faculty and its organisational structure.A glossary of terminology and frequently asked questions.The academic calendar and key dates such as the assignment schedule.Availability of marked coursework for collection.Other information, information tools and links.
Other information sourcesIn addition to Students Online, you will find further information in the following places:
The UWE Student HandbookThe CEMS Student Handbook
Blackboard (UWEOnline) – UWE’s e-learning environment.MyUWE – links to email, Blackboard, your academic record and other links.
Links to all these sources can be found on the UWE web site and on Students Online.
Disclaimer“Nothing endures but change” Heraclitus (540 BC – 480 BC)
Staffing programme structures, module specifications and indeed the structure of the universityare all subject to change. You should check on Students Online for the latest information andwith your programme leader or a student advisor if you have specific queries about the contentof this booklet or academic regulations.
Production detailsGenerated from FOLD via Apache FOP on September 7, 2007
Page 2
Page 3
Academic Contact Information
Role Name Room Phone e-mail
Programme Director Tod Burton 2N34 ext. 82156 [email protected]
Programme Leader Laurent Dala 2N35 ext. 82019 [email protected]
Module Leader for:
UFMEBV-30-2 Laurent Dala 2N35 ext. 82019 [email protected]
UFQEFB-20-2 Robert Laister 2P34 ext. 83143 [email protected]
UFMEBS-15-2 TBA ext.
UFMEBT-15-2 Vince Coveney 1N17 ext. 82639 [email protected]
UFMEEN-20-2 John Kamalu 2N13 ext. 82489 [email protected]
UFPENX-20-2 Terry Winnington 2N34 ext. 82156 [email protected]
Page 4
BEng (Hons) Aerospace Design Engineering
Programme Structure Note: This structure is indicative and subject to change
Year 1UFMEDB-20-1
Materials & ManufacturingProcesses
UFMEQU-20-1
Thermodynamics and Fluids
UFMEQT-20-1
Stress & Dynamics
UFPEDA-30-1
Aerospace and Engineering Design
UFQEFH-20-1
Engineering Mathematics 1
UFEE6U-10-1
ElectricalInterface
Year 2UFMEBV-30-2
Fundamental Aeronautics
UFQEFB-20-2
Mathematics for MechanicalEngineering
UFMEBS-15-2
Stress Analysis
UFMEBT-15-2
Dynamics
UFMEEN-20-2
Design Embodiment &Materials Selection
UFPENX-20-2
Group Project andManagement
Year 2PIndustrial Placement Year
Year 3UFMEAY-30-3
Individual Project
UFMEBX-10-3
LightweightStructures
UFPEEL-20-3
Operations & QualityManagement
UFMEBC-10-3
Aero-Propulsion
UFMEBW-20-3
Applied Aeronautics
UFMECK-10-3
AerospaceMaterials
UFMESC-10-3
Aeroelasticity
UFMEAK-10-3
Finite ElementAnalysis
Page 5
COMPULSORY MODULE SPECIFICATION(Indicative and subject to change)
Code: UFMEBV-30-2 Title: Fundamental Aeronautics Version: 2006
Level: 2 UWE credit rating: 30 ECTS credit rating: 15
Module Type: Standard Field: Mechanical, Manufacturing andAerospace Engineering
Owning Faculty: CEMS
Valid from: 1st September 2006 Discontinued From:
Pre-requisites: UFMEBF-40-1 Mechanical Engineering Principles OR UFMEQU-20-1 Thermodynamics and Fluids
Co-requisites: None
Excluded combinations: UFMEAV-20-3 Aerofluid Systems
Learning Outcomes
On completion of this module a student will typically be able to:- Assessed incomponent(s):
A. Show a detailed knowledge and understanding of
i) use appropriate terminology to describe aircraft configurations and components, and visualrepresentations of fluid flows;
A, B
ii) demonstrate an understanding of the types of force acting on an aircraft in flight, theprocesses which produce them and how they will vary as flight conditions change;
A, B
iii) describe the nature of static and dynamic stability and the relationship between the level ofstatic stability exhibited by an aircraft and the magnitude and location of the aerodynamicforces acting on it in flight ;
A
iv) understand the balance of forces acting on an aircraft in steady flight and how to relate thisto flight conditions such as airspeed, angle of attack and engine thrust and power output;
A, B
v) understand the principles of numerical modelling and the physical phenomena described; A, B
vi) undertake a simple aerodynamics experiment in a wind tunnel and present the results in anappropriate format, both personally and in report form;
B
B. Demonstrate subject specific skills with respect to
i) define and calculate geometrical properties of lifting surfaces and airframe components; A, B
ii) calculate force and moment coefficients for a lifting surface and an aircraft, and use theseresults to locate the aerodynamic centre, centre of pressure and/or neutral point of either;
A, B
iii) estimate performance limits in straight and level, climbing and gliding flight, and interms of range and endurance, given a basic description of the aircraft's aerodynamiccharacteristics;
A, B
iv) use numerical models to produce simulations of aerodynamic flows for basic geometries --aerofoils, wings, engine chamber & nozzles;
B
v) convert experimental measurements into standard non-dimensional form and describe theirvariation with relevant variables;
A, B
C. Show cognitive skills with respect to
i) relate standard aeronautical concepts to existing and future designs, and to theoretical andobserved flow behaviour;
A, B
ii) apply theoretical predictions and experimental measurements of aerodynamic behaviour toexisting and possible designs of lifting surface, controls and aircraft;
A, B
Page 6
iii) discuss the contributions of the wing, fuselage and tail to the overall forces and moments,and static stability of an aircraft, in the longitudinal plane;
A, B
iv) apply good experimental techniques in investigating flow simulations around or throughsimple aerodynamic shapes;
B
v) relate experimental observations and measured data to theoretical models and assess thelevel of agreement;
B
D. Demonstrate key transferable skills in
i) communication skills A, B
ii) self-management skills B
iii) IT skills in context A, B
iv) problem formulation and decision making B
v) awareness of professional literature B
vi) working with others B
Syllabus Outline
1. Basic aerodynamics:
The atmosphere: variation of pressure, temperature and density with height; the ISA and its variants; non-standard,idealised atmosphere models; pressure and density altitudes.
Aeronautical terminology: axes systems and degrees of freedom; classification of aircraft components andconfigurations; visual representations of body shapes and flow behaviour.
Viscous flow: Reynolds' experiments; laminar and turbulent flows; the boundary layer concept; velocity profiles;transition and separation.
Low-speed aerodynamics: flow over an aerofoil; effects of angle of attack; vorticity. Forces on an aerofoil: forceand moment coefficients; variation of lift, drag and pitching moment with angle of attack; effects of lift on drag andpitching moment; aerodynamic centre and centre of pressure.
2. Mechanics of Flight:
Performance: straight and level flight; performance envelope estimation; climbing and descent performance; glidingflight; limiting cases; range and endurance estimation; flight profiles for maximum range.
Stability and control: static and dynamic stability; longitudinal static stability determination; stick-fixed and stick-freecases.
3. Computational Fluid Dynamics:
Introduction to CFD: relevant equations, principles of discretisation, turbulence models, mesh generation,boundary conditions, consistency, convergence, stability, obtaining flow solutions, post-processing, validation andassessment of results.
4. Laboratory work and design project(s):
Wind tunnel design and operation: types of tunnel; tunnel components and their functions; data acquisition andprocessing; standard representations; flow visualisation techniques; similarities and differences between low-speedand high-speed facilities.
Component and/or aircraft design: design to meet a specific requirement; the design loop and iteration; effects ofconstruction methods on the finished product; documentation; testing and evaluation of a prototype.
Page 7
Teaching and Learning Methods
Students will learn through a combination of formal lectures, tutorials, laboratory sessions, computer lab sessions,demonstrations and exercises -- individual and group. Formal tuition in the CFX software package will be given.Results of laboratory and design work are to be delivered in the form of verbal/audio-visual presentations to staffand fellow students as well as in report form.
Indicative Reading List
The following list is offered to provide validation panels/accrediting bodies with an indication of the type and level of information students may beexpected to consult. As such, its currency may wane during the life span of the module specification. However, CURRENT advice on readingswill be available via other more frequently updated mechanisms.
Anderson, J.D. Jr. (2001). Fundamentals of Aerodynamics, 3rd Edition, McGraw-Hill
Anderson, J.D. Jr. (2000). Introduction to Flight, 4th Edition, McGraw-Hill
Anderson, J.D. Jr. (1995). Computational Fluid Dynamics - the basics with Applications, McGraw-Hill
Barnard, R.H. & Philpott, D.R. (1989). Aircraft Flight, Longman
Bertin, J.L. & Smith, M.L. (1998). Aerodynamics for Engineers, 3rd Edition, Prentice-Hall
Carpenter, C. (1996). Flightwise Volume 1 - Principles of Aircraft Flight, Airlife
Carpenter, C. (1997). Flightwise Volume 2 - Aircraft Stability and Control, Airlife
Fletcher, C.A.J. (1991). Computational Techniques for Fluid Dynamics, Volumes I & II, 2nd Edition,Springer-Verlag
Houghton & Carruthers (1982). Aerodynamics for Engineering Students, 3rtd Edition,
Houghton & Carruthers (1993). Aerodynamics for Engineering Students, 4th Edition,
Kermode, A.C. (1996). Mechanics of Flight, 10th Edition, Pitman
McCormick, B.W. (1995). Aerodynamics, Aeronautics and Flight Mechanics, Wiley
Page 8
Assessment
Weighting between components A and B A: 35% B: 65%
ATTEMPT 1
First Assessment Opportunity
Element Description % of Component % of Assessment
Component A (Controlled Conditions)
Examination 100% 35%
Component B
Laboratory Experiment 15% 9.75%
Design Project 35% 22.75%
CFD Assignment 50% 32.5%
Second Assessment Opportunity (further attendance at taught classes is not required)
Element Description % of Component % of Assessment
Component A (Controlled Conditions)
Examination 100% 35%
Component B
Assignment 50% 32.5%
CFD Assignment 50% 32.5%
SECOND (OR SUBSEQUENT) ATTEMPT
Attendance at taught classes is required.
Page 9
COMPULSORY MODULE SPECIFICATION(Indicative and subject to change)
Code: UFQEFB-20-2 Title: Mathematics for Mechanical Engineering Version: 2007
Level: 2 UWE credit rating: 20 ECTS credit rating: 10
Module Type: Standard Field: Mathematical Sciences Owning Faculty: CEMS
Valid from: 1st September 2007 Discontinued From:
Pre-requisites: UFQEFH-20-1 Engineering Mathematics 1
Co-requisites: None
Excluded combinations: None
Learning Outcomes
On completion of this module a student will typically be able to:- Assessed incomponent(s):
A. Show a detailed knowledge and understanding of
i) the mathematical language, concepts and techniques which will form the basis for theanalysis of engineering problems;
A, B
ii) the mathematical formulation of applied problems A, B
B. Demonstrate subject specific skills with respect to
i) the implementation of a numerical technique to solve a partial differential equation B
ii) the analytical solution of a partial differential equation using Fourier series and numericalsoftware
B
iii) the applications of vectors in geometric problem solving A
iv) the solution of differential equations using Laplace transforms A
v) the solution of systems of differential and difference equations using eigenvalues andeigenvectors
A
C. Show cognitive skills with respect to
i) application of mathematical techniques in the formulation and solution of problems A, B
ii) interpret solutions obtained using mathematical techniques A, B
iii) interpret solutions in a physical/engineering context B
D. Demonstrate key transferable skills in
i) communication skills A, B
ii) IT skills in context B
iii) problem formulation and decision making A, B
iv) progression to independent learning B
Page 10
Syllabus Outline
Further Vectors and Matrices: Vector geometry of lines and planes. Vector geometry of curves and differentiation ofvectors. Eigenvalues and eigenvectors. Soluton of discrete linear systems x(n+1)=Ax(n) and continuous systems x'= Ax
Laplace Transforms: Definition and manipulation of standard transforms. Inverse transform. Solution of lineardifferential equations.
Fourier Series: Periodic functions and fundamental period. Computation of Fourier Series. Convergence of FourierSeries.
Partial Differential Equations: Derive a PDE in context of either the Heat equation or Laplace's equation. UseFourier series and separation of variable techniques to solve the PDE. Use appropriate software to display resultsand aid interpretation. Use a numerical solution which uses a finite-difference scheme to solve the PDE, withappropriate software to implement and display the numerical solution.
Teaching and Learning Methods
Lectures in which students will acquire the theoretical knowledge and will see how this can be applied.
Tutorial/practical classes where students will develop their skills in the application of their mathematical knowledge,under supervision.
Students are introduced to the theory behind analytical and numerical solutions of partial differential equations.There will be computer lab sessions in which students will learn how to use supporting software packages. Thestudents will be encouraged to work in groups during and outside these sessions.
Reading StrategyEssential: Students will be supplied with a variety of printed notes (or accessable electronically from the library)taken from some of the texts below and lecture notes available via Blackboard. Students will also be expected totake further notes in lectures and read them on a weekly basis.
Indicative Reading List
The following list is offered to provide validation panels/accrediting bodies with an indication of the type and level of information students may beexpected to consult. As such, its currency may wane during the life span of the module specification. However, CURRENT advice on readingswill be available via other more frequently updated mechanisms.
James, G (2001). Modern Engineering Mathematics, 3rd Ed, Pearson Education
Croft, A., Davison, R., Hargreaves, M. (2001). Engineering Mathematics ( A Foundation for Electronic, Electrical,communications and Systems Engineers), 3rd Ed., Pearson Education
Berry, J., Wainwright, P. (1991). Foundation Mathematics for Engineers, Macmillan
Evans, C.W. (1992). Engineering Mathematics (a programmed approach), Chapman & Hall
Stroud, K.A. (2001). Engineering Mathematics, 5th ed., Palgreave MacMillan
Stroud, K.A. (2003). Advanced Engineering Mathematics, Palgreave MacMillan
Jeffrey, Alan (1996). Mathematics for Engineering and Scientists, Chapman and Hall
Page 11
Assessment
Weighting between components A and B A: 50% B: 50%
ATTEMPT 1
First Assessment Opportunity
Element Description % of Component % of Assessment
Component A (Controlled Conditions)
Examination 100% 50%
Component B
Case study 100% 50%
Second Assessment Opportunity (further attendance at taught classes is not required)
Element Description % of Component % of Assessment
Component A (Controlled Conditions)
Examination 100% 50%
Component B
Case study 100% 50%
SECOND (OR SUBSEQUENT) ATTEMPT
Attendance at taught classes is not required.
Page 12
Page 13
COMPULSORY MODULE SPECIFICATION(Indicative and subject to change)
Code: UFMEBS-15-2 Title: Stress Analysis Version: 2005
Level: 2 UWE credit rating: 15 ECTS credit rating: 7.5
Module Type: Standard Field: Mechanical, Manufacturing andAerospace Engineering
Owning Faculty: CEMS
Valid from: 1st September 2003 Discontinued From:
Pre-requisites: UFMEBF-40-1 Mechanical Engineering Principles OR (UFMEQT-20-1 Stress & Dynamics AND UFMEQU-20-1 Thermodynamics and Fluids)
Co-requisites: None
Excluded combinations: None
Learning Outcomes
On completion of this module a student will typically be able to:- Assessed incomponent(s):
A. Show a detailed knowledge and understanding of
i) stress analysis and structural behaviour with regard to the design of modern industrialcomponents and engineering artefacts
A
B. Demonstrate subject specific skills with respect to
i) solve complex problems in the general stress analysis of realistic engineering componentsand understand the design principles involved.
A
C. Show cognitive skills with respect to
i) select, apply and evaluate advanced stress analysis techniques for a wide range ofengineering problems.
A
ii) demonstrate a comprehensive understanding of analytical methods for the solution ofstrength and stiffness
A
iii) analyse structures subjected to a variety of load types and be able to predict modes offailure.
A
D. Demonstrate key transferable skills in
i) communication skills A
ii) self-management skills A
iii) problem formulation and decision making A
iv) awareness of professional literature A
Syllabus Outline
Stress analysis, Strain analysis, Mohr's Circle for stress, strain and section propert, Rosette analysis, Sectionproperties, Un-symmetric bending, Buckling of struts, Pressure vessels (thin & thick), Failure criteria and FOS,Elastic plastic analysis.
Page 14
Teaching and Learning Methods
Lectures will introduce the general theoretical concepts and present examples in the use of these techniques.Laboratory sessions will be used to underpin some of the key theoretical concepts.
Indicative Reading List
The following list is offered to provide validation panels/accrediting bodies with an indication of the type and level of information students may beexpected to consult. As such, its currency may wane during the life span of the module specification. However, CURRENT advice on readingswill be available via other more frequently updated mechanisms.
Case, Chilvers & Ross (1993). Strength of Materials & Structure, Arnold
Benham (1996). Mechanics of Engineering Materials, Crawford & Armstrong
Assessment
Weighting between components A and B A: 100% B: 0%
ATTEMPT 1
First Assessment Opportunity
Element Description % of Component % of Assessment
Component A (Controlled Conditions)
Examination 100% 100%
Second Assessment Opportunity (further attendance at taught classes is not required)
Element Description % of Component % of Assessment
Component A (Controlled Conditions)
Examination 100% 100%
SECOND (OR SUBSEQUENT) ATTEMPT
Attendance at taught classes is required.
Page 15
COMPULSORY MODULE SPECIFICATION(Indicative and subject to change)
Code: UFMEBT-15-2 Title: Dynamics Version: 2007
Level: 2 UWE credit rating: 15 ECTS credit rating: 7.5
Module Type: Standard Field: Mechanical, Manufacturing andAerospace Engineering
Owning Faculty: CEMS
Valid from: 1st September 2007 Discontinued From:
Pre-requisites: UFMEBF-40-1 Mechanical Engineering Principles OR (UFMEQT-20-1 Stress & Dynamics AND UFMEQU-20-1 Thermodynamics and Fluids)
Co-requisites: None
Excluded combinations: None
Learning Outcomes
On completion of this module a student will typically be able to:- Assessed incomponent(s):
A. Show a detailed knowledge and understanding of
i) Dynamics analysis techniques applied to a range of engineering problems; A, B
B. Demonstrate subject specific skills with respect to
i) measurement and modelling, obtaining solutions and critically assessing solutions andmeasurements;
A, B
C. Show cognitive skills with respect to
i) Application of fundamental principles of dynamics to modelling and simplification/analysis ofengineering problems;
A, B
ii) making practical recommendations on the basis of the analysis and practicalmeasurements;
A, B
D. Demonstrate key transferable skills in
i) communication A, B
ii) self-management B
iii) problem formulation and decision making A
iv) awareness of the literature B
Syllabus Outline
Rigid body motion: Vector methods for velocity, acceleration and displacement assessment; Introduction tonumerical methods; Application of closed and open mechanisms in 2-D and 3-D.
Vibration/Oscillation/Sound: Single degree of freedom: free and forced, undamped and damped; Two degree offreedom: free, undamped; Introduction to numerical methods; Principles of vibration measurements; Wave equation(1-D): derivation, standing waves; introduction to 3-D waves;
Page 16
Teaching and Learning Methods
Lectures will introduce the general theoretical concepts and present examples in the use of these techniques.Laboratory sessions will be used to underpin some of the key theoretical concepts.
Reading Strategy
Essential study material will be provided as printed notes and in other media as appropriate. Further reading is notrequired but students may wish to further their knowledge of the subjects by consulting books such as those givenin the Indicative Reading List.
Indicative Reading List
The following list is offered to provide validation panels/accrediting bodies with an indication of the type and level of information students may beexpected to consult. As such, its currency may wane during the life span of the module specification. However, CURRENT advice on readingswill be available via other more frequently updated mechanisms.
Beer, F.P., Johnston, E.R. (1990). Vector Mechanics for Engineers, Dynamics, 6th Edition, McGraw-Hill
Harrison, H.R., Nettleton, T. (1994). Principles of Engineering Mechanics, 2nd Edition, Edward Arnold
Rao, S.S. (1995). Mechanical Vibrations, Addison Wesley
Assessment
Weighting between components A and B A: 75% B: 25%
ATTEMPT 1
First Assessment Opportunity
Element Description % of Component % of Assessment
Component A (Controlled Conditions)
Examination 100% 75%
Component B
Laboratory Based Assignment 100% 25%
Second Assessment Opportunity (further attendance at taught classes is not required)
Element Description % of Component % of Assessment
Component A (Controlled Conditions)
Examination 100% 75%
Component B
Laboratory Based Assignment 100% 25%
SECOND (OR SUBSEQUENT) ATTEMPT
Attendance at taught classes is required.
Page 17
COMPULSORY MODULE SPECIFICATION(Indicative and subject to change)
Code: UFMEEN-20-2 Title: Design Embodiment & Materials SelectionVersion: 2007
Level: 2 UWE credit rating: 20 ECTS credit rating: 10
Module Type: Standard Field: Mechanical, Manufacturing andAerospace Engineering
Owning Faculty: CEMS
Valid from: 1st September 2007 Discontinued From:
Pre-requisites: UFMEDB-20-1 Materials & Manufacturing Processes
Co-requisites: None
Excluded combinations: None
Learning Outcomes
On completion of this module a student will typically be able to:- Assessed incomponent(s):
A. Show a detailed knowledge and understanding of
i) Design of machine components throughout the entire engineering process from thecustomer design brief and the design specification including structural integrity assessmentand practical applications;
B
ii) Communication of design details using standard engineering rules; B
iii) The principles and procedures for materials selection and its integration with design; A
B. Demonstrate subject specific skills with respect to
i) Design using standard components and manufacturers catalogue data and the use ofmaterials for specific applications;
B
ii) Use of solid modelling computer aided design (CAD) and drawing board skill in the designand embodiment of machine components.
B
iii) Explain materials manipulation processes and their implications for different aspects ofmaterials properties.
A
iv) Explain failure mechanisms, their origin and the presentation of data and hence avoidanceof failure by materials selection and use.
A
C. Show cognitive skills with respect to
i) Evaluate and implement solutions to design embodiment of mechanical components usingengineering principles;
B
ii) Appreciate the integrative role of design generated geometry for computer aided analysisand manufacture;
B
iii) Choose materials in a logical manner, either singly or as a composite; A
iv) Understand test data and recognise potential failure situations; A
v) Analyse a proposed artefact and propose an appropriate design and relevant NDTtechnique to give a safe working component;
A
D. Demonstrate key transferable skills in
i) Working with minimum guidance. A, B
ii) Identifying and selecting relevant information from available resources. A, B
iii) Using written and computerised formats to communicate ideas and information clearly,effectively and in a reasoned way.
A, B
Page 18
iv) Understanding the criteria to be applied when choosing materials, technologies ormechanical principles and produce a reasonable engineering design specification in details.
A, B
Syllabus Outline
The key aim of the course is to establish design practices through lectures, coursework and self-learning. Itemphasises practical hands-on design approach with 'real' components. The course include:
* Using standard mechanical components (fasteners, seals, bearings, etc.) and features (location, limits and fits,welds, stress raisers, etc.)
* Selection or specification of bought-out equipment (making use of catalogue library and Technical Index).* Use of I-DEAS solid modelling software.* Integration of analytical areas, especially stress analysis, into the design process.* Selection of materials. For example, heat treatment of metals, structure behaviour and manufacturing process
of ceramics.* Composite structures, anisotropic conditions, high performance composites, metal matrix and ceramic matrix
composites.* Failure mechanisms in components and materials: fatigue, creep, corrosion and fracture toughness.
Mechanisms involved in these failures.* Design and material selection to overcome likely failure modes. NDT and non-destructive evaluation,
techniques. Case studies of failure.
Teaching and Learning Methods
Lectures introduce theoretical concepts and present practical examples used in mechanical design and studentsconduct several individual assignments, using both drawing board and CAD, covering various aspects of thelearning material.
Reading Strategy
Students will not be expected to purchase a set text for this module. Essential lecture notes will be providedelectronically. A printed study pack will be provided for the design component of the module.
Indicative Reading List
The following list is offered to provide validation panels/accrediting bodies with an indication of the type and level of information students may beexpected to consult. As such, its currency may wane during the life span of the module specification. However, CURRENT advice on readingswill be available via other more frequently updated mechanisms.
The following list is indicative of the type and level of reading expected in this module. This list will be updatedannually and made available to students through the students’ handbook.
Mott, R.L. (1992). Machine Element Design, Maxwell
Polak, P. (1991). Engineering Design Elements, McGraw Hill
Mucci, P. (1990). Handbook for Engineering Design Using Standard Materials & Components, PER Mucci Ltd
Ashby, M. (1999). Materials Selection in Mechanical Design, 2nd Edition, Butterworth Heneman
Crane & Charles (1991). Selection and Use of Engineering Materials, 2nd Edition, Butterworths
Stanley (1989). Non Destructive Evaluation, McGraw Hill
Page 19
Assessment
Weighting between components A and B A: 50% B: 50%
ATTEMPT 1
First Assessment Opportunity
Element Description % of Component % of Assessment
Component A (Controlled Conditions)
Examination 100% 50%
Component B
Coursework 1 20% 10%
Coursework 2 20% 10%
Coursework 3 30% 15%
Coursework 4 30% 15%
Second Assessment Opportunity (further attendance at taught classes is not required)
Element Description % of Component % of Assessment
Component A (Controlled Conditions)
Examination 100% 50%
Component B
Coursework 100% 50%
SECOND (OR SUBSEQUENT) ATTEMPT
Attendance at taught classes is required.
Page 20
Page 21
COMPULSORY MODULE SPECIFICATION(Indicative and subject to change)
Code: UFPENX-20-2 Title: Group Project and Management Version: 2005
Level: 2 UWE credit rating: 20 ECTS credit rating: 10
Module Type: Project Field: Professional Studies Owning Faculty: CEMS
Valid from: 1st September 2005 Discontinued From:
Pre-requisites: None
Co-requisites: None
Excluded combinations: UFPE6D-10-3 Project Management
Learning Outcomes
On completion of this module a student will typically be able to:- Assessed incomponent(s):
A. Show a detailed knowledge and understanding of
i) Suitable planning and accounting structures for the application of resources to theexecution of engineering projects
A
ii) Working knowledge of the processes available for team building and the balances requiredbetween people orientated and task orientated approaches to project management.
A
iii) Project planning and control methodologies including work-breakdown structures, taskestimation, precedence relationships, critical path analysis, progress reporting and the useof computers in progress monitoring
A
iv) formal project management techniques to a group project related to their award A
v) The need to undertake independent research to supplement the knowledge of a team. A
vi) The relationship between good management practices and group project success A
B. Demonstrate subject specific skills with respect to
i) Eliciting stakeholder requirements and developing a working brief for meeting thoserequirements.
A
ii) Effectively distributing a programme of work to resolve technical problems and deliver arealistic outcome
A
iii) Working effectively in teams and maintaining a high quality record of activity, decisions anddeliverables
A
C. Show cognitive skills with respect to
i) Synthesising and evaluating data from multiple sources A
ii) Understanding the issues involved with planning and executing complex projects. A
iii) Understanding and responding to demands and events which push a project off theplanned track.
A
D. Demonstrate key transferable skills in
i) self-management skills A
ii) IT skills in context A
iii) problem formulation and decision making A
iv) progression to independent learning A
Page 22
Syllabus Outline
Illustrative examples of topics to be presented in the module include:
Projects and stakeholders. Project life-cycle models. Customers\' requirements analysis and capture. Systemmodelling and validation. Feasibility studies. Goal setting. Work breakdown structures and schedule controlsystems. Project team structures. Team-building and management. Project control techniques and managementstrategies.
Groups may also receive presentations of domain specific material appropriate to the project that they areundertaking.
Teaching and Learning Methods
The module is structured to encourage students to put into practice and develop their domain competences in aframework that will also develop their professional management skills.
Students will form into groups of typically 6 to 8 having received initial guidance on team dynamics. The projectswill proceed in parallel with keynote lectures to introduce topics and guide student-centred learning with supportmaterial mounted on the internet. Students will be required to operate within a set of guidelines which will mandatea professional standard of record keeping both by individuals and the team. Teams will receive guidance andsupport during their team meetings which we be held in the tutorials. Much of the project work will be undertakenoutside the taught sessions.
Students will be assessed on the basis of group presentations, group reports and evidence of individual effort. Theassessment will take into account both the professional practice demonstrated in the management of the projectsand outcomes of the projects themselves. The projects will proceed in phases and the overall assessment will bebuilt up from the performance in each of these. Students will receive feedback at each phase review.
The referral coursework will require the student to build on the work they started in the group project, report on thatand also to reflect on the issues arising from the group work.
Indicative Reading List
The following list is offered to provide validation panels/accrediting bodies with an indication of the type and level of information students may beexpected to consult. As such, its currency may wane during the life span of the module specification. However, CURRENT advice on readingswill be available via other more frequently updated mechanisms.
Kerzner, H (2003). Project Management - A systems approach to planning scheduling and controlling projects(8th edition), Wiley
Meredith, JR & Matel, SJ (2003). Project Management - A Managerial Approach, Wiley
Slack, Chambers, Harland, Harrison & Johnston (1998). Operations Management, Pitman
Stevens, Brooks, Jackson & Arnolds (1998). Systems Engineering: Coping with Complexity, Prentice Hall
Page 23
Assessment
Weighting between components A and B A: 100% B: 0%
ATTEMPT 1
First Assessment Opportunity
Element Description % of Component % of Assessment
Component A (Controlled Conditions)
Group Project Reports and Files, Presentations& Oral Examination plus personal log books
100% 100%
Second Assessment Opportunity (further attendance at taught classes is not required)
Element Description % of Component % of Assessment
Component A (Controlled Conditions)
Individual Assignment - Report, presentation &oral examination
100% 100%
SECOND (OR SUBSEQUENT) ATTEMPT
Attendance at taught classes is required.
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