Aerospace Engineering including an Industrial Year BEng

This module will give you with the knowledge, concepts and principles of fluid mechanics and aerodynamics. You will complete this module over the course of a year.

Topics covered are:

• atmospheric physics
• standard atmosphere
• static pressure
• hydrostatics
• inviscid flows – conservation of mass and momentum
• Euler and Bernoulli equations
• Introduction to compressible conservation of viscous flows
• Introduction to shock waves lifting surfaces – aerofoil and wings
• basic forces
• pressure distributions
• fluid structure interaction phenomena

This year long module introduces students on the Aerospace Engineering courses to the basic concepts and practices of design and manufacture in an aerospace context and includes the following topics:

• The process of concept generation through to detail design in an aerospace context
• The use of computer aided engineering tools in the design processes
• Part and assembly design using CATIA
• Basic machine elements and their function
• How materials, stress analysis and manufacturing disciplines fit within the framework of design
• Machining processes and metrology
• Lab-based demonstration of manufacturing processes
• Machine shop practical training
• An appreciation of modern working practices - interaction with technical staff and conveying design intent

This year-long module provides a basic introduction to electrical and electronic devices, power transmission and the distribution and utilisation of electrical energy in an Aerospace Engineering context.

Topics covered are:

• Electrical circuits: Resistors and Kirchhoff’s Laws, superposition, Gauss and Ampere Laws, Transient analysis of circuits, capacitance and inductance, phasors, AC circuits, 3-phase AC systems
• Communications: introduction to signals (analogue and digital), basic electronic components (diodes, transistors and operational-amplifiers)

• Electrical systems: electrical machines, electrical power sources in aircraft, transformers, power distribution to aircraft electrical systems, introduction to electrical loads in aircraft

This year-long module introduces students on the Aerospace Engineering courses to the fundamental concepts and principles of solid mechanics and dynamics. It covers their application to simple engineering scenarios in an aerospace context.

Topics include:

• Review of basic mechanics : vectors, units, forces and moments, Newton’s laws
• Static equilibrium: force and moment analysis in design; frictional forces
• Free body diagrams and Pin-jointed structures
• Stress, strain and elasticity
• Multi-axial stress-strain; thin walled vessels under pressure
• Shear stress and torsion of shafts
• Plane stress; Mohr's circle analysis
• Beam bending: shear force & bending moment diagrams
• 2nd moments of area of cross-sections
• Bending stresses in beams
• Linear and rotational motion: Displacement, velocity and acceleration
• Relationship between angular and linear motion• Newton's Laws for linear & rotational motion
• Linear and Angular Momentum, including conservation of momentum
• Work, Energy & Power, including kinetic & potential energy
• Geared systems
• Drive systems, including tangential drives and vehicles
• Load characteristics and steady-state characteristics
• Flywheel design
• Static and dynamic balancing

This year-long module introduces students on the Aerospace Engineering courses to the basic concepts and practices of aircraft design and flight mechanics. It covers the following topics:

• Aircraft classification and configurations
• Aircraft design procedures
• Aircraft characteristics and performance
• Preliminary aerodynamics analysis
• Flight envelopes
• Steady flight conditions
• Static stability

This year-long module comprises a number of elements and these are:

• Essential professional engineering elements:, report writing, information searching, data analysis
• Essential engineering study support elements: Maths, MATLAB, Using MS Excel, Word, Powerpoint
• Essential project skills: team working, project management, MS Project

These skills will be covered to a level appropriate to first year aerospace engineering students.

In addition the module includes a year-long integrating group project element that draws in technical elements from the other 5 modules running in the first year of the course. An output from the project is a model scale aircraft designed to meet the specification set.

This year long foundational module is a direct continuation of first year aerospace design, incorporating new information and methods as well as enabling practice of previously learned concepts. The module includes the following topics:

• Sustainability issues in design
• Design for manufacture considerations and cost
• Machine elements function and correct selection
• CNC processes
• Group design project with manufacture of the finished design in the January workshop slot
• Individual design and analysis project
• Machine shop practical training

You will learn fundamental thermodynamics including key underlying equation sets such as the first and second law of thermodynamics, perfect gas relationships and analysis of relevant cycles for Aerospace propulsion such as the Brayton cycle. The principles of aircraft propulsion are further developed with a focus on:

• jet engines including the principles of gas turbine engines
• layout and the application of compressible flow and turbomachinery principles
• Factors influencing design and choice of engine configuration are introduced

This year long module introduces key principles of aerospace systems control, focusing on examples relevant to aerospace applications. Topics covered are:

• Introduction to control systems design in aerospace context
• Digital and analogue control systems
• Fundamentals of aerospace electrical and electronic systems including
  • power generation and conversion
  • electric machines and drives
  • flight control actuation systems

This module extends and deepens your knowledge of materials, concentrating on the composites and alloys used in aerospace structures and engines. An overview of current aerospace research will be used to highlight likely future developments.

Topics include:

• Introduction to airframe
• shear stress beams
• deflection and conditions
• column buckling
• thin-walled structures
• semi-monocoque structures
• web-boom idealisation
• static indeterminate structures
• bending & torsion of single
• multi-celled thin-walled beams
• shear center
• static and fatigue failure

This module introduces concepts of rigid body dynamics and vibrations and develops your ability to analyse aspects in simplified engineering situations, as well as in analysing rigid aircraft dynamics.

This module covers the dynamics of point masses and rigid bodies. It considers both motion in an inertia frame, as well as in a moving reference frame. The principals of linearization of a nonlinear dynamical system are demonstrated and basic characteristics of linear systems are introduced.

Flight mechanics is progressed through the development of equations of motion for rigid aircraft. Ideas of equilibrium and trim are captured by determining the steady control inputs needed to fly simple steady trajectories. Based on the nonlinear equations, linearization about a trimmed point are considered, as well as the linear dynamic response of an aircraft and basic flight control.

Within this module you will cover essential study skills, such as:

• Maths
• Report writing
• Data analysis
• Management

A year long group project will play a crucial role in your learning. The project will draw on learning from other modules within the year.

The project aims to give experience in the practice of engineering and scientific approaches at a professional level. It involves the planning, execution and reporting of a programme of work which will normally involve a mixture of experimental, and/or theoretical and and/or computational methods and analysis together with a detailed and critical review of relevant previous literature in the field. The detailed content and project balance relating to the extent of experimental/theoretical/computational/ design work is a matter for discussion between the student and his/her supervisor, factoring in the students course.

This module covers management and professional practice elements essential to professional engineers. Included here are range of management techniques and tools including:

• Life Cycle Costing
• Project selection and evaluation including PERT
• Financial evaluation
• Risk Management; Evaluating risk, Risk contingency, Fault trees,
• Failure Mode and Effect Analysis,
• Programme Monitoring; Milestones, Earned Value Analysis, Cost and schedule performance indices,
• Marketing; Marketing methods, Price and volume analysis, Customer evaluation, The power of brands,
• Quality Management; Six-Sigma quality, Six-Sigma tools, Statistical process control,
• An introduction to English Law; The origins or English law, The Legal Structure, Civil law, Criminal law, Contract law.Certification, safety and reliability in an aerospace context are covered. The underpinning legal framework is presented along with the relevant legal statutes such as rules of the air, airworthiness and pilot licensing. Case studies and guest lectures are used to support this element of the module.

This module aims to provide students with a basic knowledge and understanding of the main stream computer modelling techniques used in modern engineering practice, including Finite Element, Finite Difference and Finite Volume methods.

Topics covered will include:

• Introduction to numerical methods in engineering
• Finite Element Analysis (FEA) of structures
• Computational Fluid Dynamics (CFD) for thermo-fluids problems
• Coursework on running FEA and CFD software

This module extends and deepens knowledge of students on the Aerospace Engineering courses in aerodynamics in an aerospace context. It covers the following topics:

• Lifting wing theories
• Compressible flow in nozzles and diffusers
• Shock wave theory and aerothermodynamics
• Transonic flow – supercritical aerofoils, swept wing theory, wave drag, area rule
• Supersonic flow – double-wedge aerofoils, delta wings, slender wing theory
• Hypersonic flow – a brief introduction
• Low- and high-speed flow control and drag reduction

This module will build on the knowledge in H42AEP/MECH2028 and widen the context and application to include considerations of the propulsion requirements of light aircraft, military applications and supersonic flight.

Alternative propulsion units such as ramjets, scramjets and rockets will be evaluated.  Propeller design knowledge from H42AEP/MECH2028 will be extended and Helicopter propulsion introduced.  Future propulsion technologies, including electrification of propulsion, will be appraised. 

Throughout these topics factors influencing design and choice of engine configuration will be evaluated.At the end of the module student will have a wider and deeper knowledge relating to propulsion choices for aerospace applications and be in a position to design the key elements of these propulsion system.

This is a module which requires personal engagement in the classes and there is no examination. In this way the module is like the Individual Project.

The module has four cycles,  each comprising students individually preparing a talk, and report, on a topic within a theme and with a title that has been negotiated with the Teachers straight after the Teachers have delivered an introductory lecture on that theme.

The point of this module is to improve oral presentation and engineering report-writing skills using advanced materials as a vehicle.

The classes are seminars, where good practice is openly discussed and materials' advantages and disadvantages are openly debated.

This module is designed to deal with a wide range of materials (including advanced metallic, ceramic, glass, composite and polymeric-based materials) for a wide range of applications. Also it considers materials' themes, such as aerospace materials, medical materials, coatings, carbon-based materials, and so on.

The module deals with:

• the underlying principles behind the suitability of material properties for the targeted applications
• the processing of these materials
• the effects of processing on their subsequent structure and properties
• ultimate performance

This module provides a detailed introduction to the more-electric aircraft and key technologies enabling the technological direction of the aircraft.

Topics covered are:

• Overview of more-electric aircraft technologies and future hybrid electric aircraft technology
• Electrical machine and drives: introduction to different types of electrical machine including induction machines and permanent magnet machines and related control for more-electric aircraft applications
• Power electronics: introduction of power electronic converters for more-electric aircraft applications
• Electrical systems: power distribution to aircraft electrical systems including AC systems and DC systems
• Modelling techniques: introduction of modelling and simulation technologies for aerospace applications
• There is a course work that is a project on aircraft electrical system modelling and simulation

This module introduces avionics, providing a detailed introduction to all the major avionic systems on current civil and military aircraft and spacecraft. To help in understanding the concepts, a number of application examples will be included throughout the classes.

Topics covered are:

• History of avionics;
• Aircraft control including fly-by-wire and autopilot
• Displays and man-machine interaction
• Avionic systems in navigation;
• Sensors in avionics;
• Radar technology;
• Electronic warfare;
• Avionics applications in current aircraft

The aim of this module is to provide an introduction to Space Missions elements such that the students will have a preliminary idea of what knowledge is required to design a space system. The main topics covered are:

• A brief history of Space Conquest,
• The Space Environment and its effects
• Space Missions Elements and Design Phases
• Orbital Mechanics and Orbital Transfer Overview
• Spacecraft Elements ( Structure, EPS, OBDH, AODCS, TT&C, Thermal)
• Space Debris

As part of the module students will use a range of software to design and analyse the performance of a space mission. The outcome of the study will be presented and assessed via a 5,000 word report.