Overview
- Start dateFebruary
- DurationMSc: three years part-time; PgDip: two years part-time; PgCert: two years part-time
- DeliveryTaught modules 40%, group project 30%, individual research project 30%
- QualificationMSc, PgDip, PgCert
- Study typePart-time
- CampusCranfield campus
Who is it for?
We recognise the challenge of undertaking part-time study while you are working. This course is specifically designed for people working in engineering or technical management positions in the aerospace industry who wish to study for an accredited master's degree while they are in employment.
You are required to attend a total of nine weeks of lectures over three years on a modular basis. The first year attendance pattern is two weeks in February, followed by one week in June and one week in November. Following a series of compulsory modules, you may choose three specialist optional modules in order to tailor the course to your particular interests and requirements.
Why this course?
This course provides accelerated development of engineering staff whilst delivering the right mix of technical and business skills for careers in the aerospace industry. The course will broaden your understanding of aircraft engineering and design subjects, and provide a strong foundation for career development in technical, integration and leadership roles. This accredited master's course supports your career development by meeting the further learning requirements for Chartered Engineer status. The group project allows you to gain hands on experience of development and design lifecycle, and the individual project allows you to investigate a topic that is of interest to your employer, with supervision from experienced staff.
Cranfield has been at the forefront of postgraduate education in aircraft engineering since 1946. We have a global reputation for our advanced postgraduate education and extensive applied research. You can be sure that your qualification will be valued and respected by employers.
Informed by industry
The Industrial Advisory Panel, comprising senior industry professionals, provides input into the curriculum in order to improve the employment prospects of our graduates. Panel members include:
- Airbus UK - Filton,
- BAE Systems,
- Canadian High Commission,
- Department for Business, Enterprise and Regulatory Reform,
- Marshall Aerospace,
- Messier-Bugatti-Dowty,
- RAF,
- Military Aviation Authority.
Course details
The MSc in Aircraft Engineering consists of three elements: taught modules, a group design project and an individual research project.
Course delivery
Taught modules 40%, group project 30%, individual research project 30%
Group project
The group project is undertaken throughout year two of your studies and provides a wealth of learning opportunities. You will work together on a significant design project, progressing from concept to hardware. Each student takes on a technical design role related to a major structural, systems or avionics item as well as a management role such as Chief Engineer, Project Manager, Finance Manager etc.
Recent group projects have covered:
- Turbo-jet powered unmanned air vehicles,
- An advanced aircraft systems and avionics integration rig,
- An electric ultralight aircraft,
- The development of a hand controller for pilots with lower limb disability.
Individual project
The individual research project allows you to delve deeper into an area of specific interest of your choice, and you are encouraged to select a project that is of relevance to your sponsoring company. You will complete the individual project during year three of your studies.
Recent individual research projects have included:
- Study into the effect of environmental conditioning on the pull-through performance of countersunk bolted joints in thin composite structures;
- The effect of alternative fuels on military aircraft fuel systems;
- Conceptual design of a UAV with STOL capability for operation in remote, unpaved surfaces;
- Development of a MATLAB linear model of the NIMROD pitch flight control system;
- An industrial study of multi-disciplinary optimisation.
Modules
Keeping our courses up-to-date and current requires constant innovation and change. The modules we offer reflect the needs of business and industry and the research interests of our staff and, as a result, may change or be withdrawn due to research developments, legislation changes or for a variety of other reasons. Changes may also be designed to improve the student learning experience or to respond to feedback from students, external examiners, accreditation bodies and industrial advisory panels.
To give you a taster, we have listed the compulsory and elective (where applicable) modules which are currently affiliated with this course. All modules are indicative only, and may be subject to change for your year of entry.
Course modules
Compulsory modules
All the modules in the following list need to be taken as part of this course.
Tools for Integrated Product Development
Aim |
The aim of this module is to introduce students to the major issues faced in product development today, and show them how new technologies can be implemented to help overcome those problems. The module will focus primarily on Computer Aided Design but will also discuss Digital Mockup and Computer Aided Manufacture. |
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Syllabus |
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Intended learning outcomes |
On successful completion of this study the student should:
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Major Component Design and Manufacture
Aim |
The aim of this module is to explain the reasons behind the design choices to be made in the structural layout and manufacture of components such as wings and fuselages. |
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Syllabus |
Component Design Structural requirements |
Intended learning outcomes |
On successful completion of this module a student should be able to: 1. Define the constraints imposed on aircraft design by manufacturing and operational considerations. |
Introduction and Initial Aerospace Vehicle Design
Aim |
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Syllabus |
In addition to familiarising the students with the design process the module is designed to encourage them to work together effectively as a team and to develop communication skills that will be further utilised throughout the MSc course in the GDP. Introduction to Aircraft Design • The design and development process • Importance of requirements and mass • Reliability and Maintainability Aircraft Conceptual Design • Project design process and parametric techniques • Flight path performance • Drag and weight prediction: Drag sources, polar estimation, weight prediction methods • Layout aspects: wing; powerplant; landing gear; fuselage • Overview of stability and control: tailplane/elevator, fin/rudder, aileron layout • Overall project synthesis |
Intended learning outcomes |
On successful completion of this module a student should be able to: 1. Have a broad understanding of the multidisciplinary nature of aircraft design and manufacture. 2. Be able to apply conceptual design methods to simple aircraft design problems. 3. Have developed transferable skills in team building, networking (including intersite communication) and independent learning. |
Manufacturing
Module Leader |
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Aim |
The aim of the Manufacturing module is to provide students with a basic understanding of a broad range of issues associated with aircraft manufacture. The module will cover technical and management topics ranging from strategy and factory planning to composite manufacture. |
Syllabus |
• Lean and cellular manufacturing principles • Modelling and simulation of manufacturing systems and use of factory physics • Manufacturing planning and control systems • Supply chain strategy • Through-life capability • Manufacturing cost engineering • Quality management • Composite Manufacture |
Intended learning outcomes |
On successful completion of this module a student should be able to: 1. Have a critical awareness of manufacturing systems design, analysis and control that will enable them to contribute to the cost-effective manufacture of aircraft. 2. Have a comprehensive understanding of the interrelationships between design, manufacturing, supply chain and customer facing disciplines and how these can contribute to meeting the challenges of aircraft manufacture. 3. Be able to assess the implications for design and production of the use of composites. 4. Be able to apply their acquired knowledge to contribute effectively to Integrated Product Teams representing or taking into account the manufacturing issues related to aerospace product realisation. |
Methodologies for Integrated Product Development
Aim |
This module aims to introduce several major topics associated with Engineering Integration in the context of what has been known in recent years as Integrated Product Development (IPD) in the Extended/Virtual Enterprise. The objective is to follow the process from the early stages of the product development lifecycle when the Prime has to deal with vague or difficult to quantify customer needs and to convert those to sound (functional) requirements and subsequently to design embodiments. The emphasis is on the architectural design enabling methods, but tools and technologies are also discussed. |
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Syllabus |
Overview of the topics covered in the module. Included also are brief introductions to Quality Function Deployment (QFD) and Design Space Exploration, Optimisation and Trade-off Analysis. Object Oriented Approach to Systems Modelling This lecture covers the fundamental concepts, including also a very brief introduction to the Unified Modelling Language (UML) and the Systems Modelling Language (SysML). The lecture is essential since software and systems engineering play an increasing role in aerospace product development. Engineering Integration and Architectural Design Covered are the principles of the semi-formal Axiomatic Design approach. Useful for both engineering architecture and software design. Included also is an exercise. System Life Cycle Processes Covers established standards for the engineering of systems such as ANSI/EIA 632 and ISO/IEC 15288. Information and Knowledge Sharing Covers the principles of information sharing and standards such as STEP (Standard for the exchange of product model data) and its modelling language EXPRESS. Systems Modelling Covers the basics of the Systems Modeling Language (SysML) – a de facto standard, general-purpose modelling language for systems engineering applications. A hands on exercise is included. BAE Systems Case Studies Customer and Market Needs Definition- Mapping to Requirements, integrated design, modelling and simulation (Synthetic Environments), engineering integration, managing by maturity, integrated product teams and organisation. Product Lifecycle Management (PLM) This lecture covers state of the art in PLM including also the need for information management in integrated product development, key elements of Product Data Management (PDM), standards, integration and implementation issues. |
Intended learning outcomes |
On successful completion of this module a student should be able to: |
Elective modules
A selection of modules from the following list need to be taken as part of this course
Finite Element Analysis
Module Leader |
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Aim |
The course is aimed at giving potential Finite Element USERS basic understanding of the inner workings of the method. |
Syllabus |
• Introduction to FE modelling: Idealisation, Discretisation, Meshing and Post Processing • Tracking and controlling errors in a finite element analysis. ‘Do’s and don’ts’ of modelling. • Illustration of basics of FEM using the Direct Stiffness method to define both terminology and theoretical approach. • Problems of large systems of equations for FE, and solution methods. • FE method for continua illustrated with membrane and shell elements. • Nonlinear analysis in FEM and examples • NASTRAN application sessions |
Intended learning outcomes |
On successful completion of this module a student should be able to: 1. Understand the underlying principles and key aspects of practical application of FEA to structural problems. 2. Understand the main mathematical and numerical aspects of the element formulations for 1D, 2D and 3D elements. 3. Build and analyse finite element models based on structural and continuum elements with proper understanding of limitations of the FEM. 4. Interpret results of the analyses and assess error levels. 5. Critically evaluate the constraints and implications imposed by the finite element method. 6. Extend their knowledge and skills to the FE analysis of more complex structures on their thesis work. |
Fatigue, Fracture Mechanics and Damage Tolerance
Aim |
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Syllabus |
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Intended learning outcomes |
On successful completion of this study the student should:
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Aircraft Loading Actions and Aeroelasticity
Module Leader |
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Aim |
This module is separated into two ten hour blocks. The aim of the first ten hours is to describe all the main loading cases, including those encountered on the ground, in the air and those induced by the environment. In addition, the student is introduced to the history and significance of the various airworthiness requirements. The aim of the second ten hour block is to introduce students to the concept of aeroelasticity, develop the importance of aeroelastic phenomena as applied to aircraft design and to provide students with methods of analysis and criteria. |
Syllabus |
Standard requirements, their application, interpretation and limitations Flight loading cases Structural design data Factors Aeroelasticity |
Intended learning outcomes |
On successful completion of this study the student should:
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Detail Stressing
Module Leader |
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Aim |
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Syllabus |
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Intended learning outcomes |
On successful completion of this module a student should be able to:
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Introduction to Aircraft Structural Crashworthiness
Module Leader |
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Aim |
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Syllabus |
o Objectives and Approach
o Regulations o Human Tolerance • Crash Energy Management • Structural Collapse o Collapse of metallic and composite structural components o Component collapse vs. structural collapse • Introduction to methods for crash analysis o Hand calculations o Hybrid analysis methods o Detailed analysis methods • Role and capability of testing and simulation in the crashworthiness field |
Intended learning outcomes |
On successful completion of this module a student should be able to:
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Design and Development of Airframe Systems
Aim |
To expand the students’ knowledge of airframe systems, their role, design and integration. In particular, to provide students with an appreciation of the considerations necessary and methods used when selecting aircraft systems and the effect of systems on the aircraft as a whole. |
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Syllabus |
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Intended learning outcomes |
On successful completion of this module a student should be able to:
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Design, Durability and Integrity of Composite Aircraft Structures
Aim |
The course seeks to provide engineers with knowledge of polymer composite properties and behaviour relevant to their in-service performance durability and maintenance in aircraft structures |
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Syllabus |
Basic principles |
Intended learning outcomes |
On successful completion of this module a student should be able to: |
Aircraft Performance for Aircraft Engineering
Aim |
Please note that this is a 2 week module. |
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Syllabus |
• Air data systems, Standard Atmosphere and pressure error measurement • Lift, drag and cruise performance Non-assessed elements: • Static equilibrium and trim • Longitudinal static stability, trim, pitching moment equation, static margins • Manoeuvrability: and manoeuvre margins • Lateral-directional trim and static stability • Introduction to dynamic stability |
Intended learning outcomes |
On successful completion of this module a student should be able to: 1. Critically evaluate the lift, drag and cruise performance characteristics of a conventional aircraft. |
Flight Dynamics Principles for Aircraft Engineering
Aim |
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Syllabus |
• Development of the linearised equations for longitudinal symmetric motion and lateral directional asymmetric motion. Solution of the equations of motion:- aircraft response transfer functions and state space models. Aerodynamic modelling:- Aerodynamic stability and control derivatives, derivative estimation, modelling limitations. Stability: interpretation on the s-plane • Flight Dynamics (10 lectures) • Aircraft dynamics:- Stability modes, longitudinal dynamics, lateral-directional dynamics, reduced order models, time response. Flying and handling qualities:- Assessment, requirements, aircraft role, pilot opinion rating, flying qualities requirements on the s-plane • Flight control:- Introduction to stability augmentation, closed loop system analysis, the root locus plot, longitudinal stability augmentation, lateral-directional stability augmentation |
Intended learning outcomes |
On successful completion of this module a student should be able to: 1. Derive and solve the small perturbation equations of motion for a conventional aircraft. 2. Assess the flying qualities of an aeroplane. 3. Recommend and design simple stability augmentation system strategies to rectify flying qualities deficiencies. |
Methodologies for Integrated Product Development
Aim |
This module aims to introduce several major topics associated with Engineering Integration in the context of what has been known in recent years as Integrated Product Development (IPD) in the Extended/Virtual Enterprise. The objective is to follow the process from the early stages of the product development lifecycle when the Prime has to deal with vague or difficult to quantify customer needs and to convert those to sound (functional) requirements and subsequently to design embodiments. The emphasis is on the architectural design enabling methods, but tools and technologies are also discussed. |
---|---|
Syllabus |
Overview of the topics covered in the module. Included also are brief introductions to Quality Function Deployment (QFD) and Design Space Exploration, Optimisation and Trade-off Analysis. Object Oriented Approach to Systems Modelling This lecture covers the fundamental concepts, including also a very brief introduction to the Unified Modelling Language (UML) and the Systems Modelling Language (SysML). The lecture is essential since software and systems engineering play an increasing role in aerospace product development. Engineering Integration and Architectural Design Covered are the principles of the semi-formal Axiomatic Design approach. Useful for both engineering architecture and software design. Included also is an exercise. System Life Cycle Processes Covers established standards for the engineering of systems such as ANSI/EIA 632 and ISO/IEC 15288. Information and Knowledge Sharing Covers the principles of information sharing and standards such as STEP (Standard for the exchange of product model data) and its modelling language EXPRESS. Systems Modelling Covers the basics of the Systems Modeling Language (SysML) – a de facto standard, general-purpose modelling language for systems engineering applications. A hands on exercise is included. BAE Systems Case Studies Customer and Market Needs Definition- Mapping to Requirements, integrated design, modelling and simulation (Synthetic Environments), engineering integration, managing by maturity, integrated product teams and organisation. Product Lifecycle Management (PLM) This lecture covers state of the art in PLM including also the need for information management in integrated product development, key elements of Product Data Management (PDM), standards, integration and implementation issues. |
Intended learning outcomes |
On successful completion of this module a student should be able to: |
Introduction to Avionics
Module Leader |
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Aim |
To provide a comprehensive overview of avionics systems and infrastructures. |
Syllabus |
• Airborne sensor systems. • Navigation and communications systems – terrestrial and satellite-based systems, autonomous navigation systems, digital data links. • Radar – principle of operation, operational modes, radar cross section. • Displays – head down, head up and helmet mounted displays. • Avionics systems architectures and integration, databases. • Flight management and situational awareness systems, air traffic management. • Military applications – electronic warfare and countermeasures. • Product design considerations – design standards, fault tolerance and product life cycle. • Case study – a complete avionics installation. This module has an additional tutorial inside the cockpit of the large aircraft flight simulator. Students will be able to appreciate the cockpit layout design, understand information displayed to the pilot, and have the opportunity of flying the simulator. This tutorial is intended to enhance the learning process and the knowledge gained. |
Intended learning outcomes |
On successful completion of this module a student should be able to: |
SATM Introduction to Autonomous Systems
Aim |
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Syllabus |
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Intended learning outcomes |
On successful completion of this module a student should be able to: Explain the concept of autonomy, the main application domains and limitations of autonomous systems, as well as the potential problems and technical challenges. Evaluate and assess explain lifecycle development processes of autonomous systems, as well as describe the general frameworks and architectures for autonomous systems. Demonstrate a knowledge of some of the key technologies and principles for implementing autonomous systems and their implications for autonomous systems design.
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SATM Through life System Effectiveness
Aim |
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Syllabus |
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Intended learning outcomes |
On successful completion of this module a student should be able to: Appraise supportability concepts & logistics and how they contribute to system effectiveness and sustainment. Analyse the measures of AR&M, how they are manipulated and applied and how their delivery can be assured. Defend the AR&M and logistic techniques, including testing and trials, used throughout the lifecycle. Evaluate the management issues for AR&M and Supportability in providing operational availability at minimum Through Life Cost (including programme management, risk management and capability integration). Critically evaluate the strategies to plan system effectiveness through-life. |
Teaching team
You will be taught by experienced Cranfield academic staff, many of whom have industrial experience. The course also includes visiting lecturers from industry who will relate the theory to current best practice. Past speakers include: Head of Worldwide Suppliers, Airbus, Head of Engineering Capability, BAE Systems, Chief of Manufacturing Engineering Processes and Capability, BAE Systems. The Course Director for this programme is Dr Wenli Liu.
Accreditation
Re-accreditation for the MSc in Aircraft Engineering is currently being sought with the Institution of Mechanical Engineers (IMechE) and the Royal Aeronautical Society (RAeS) on behalf of the Engineering Council as meeting the requirements for Further Learning for registration as a Chartered Engineer. Candidates must hold a CEng accredited BEng/BSc (Hons) undergraduate first degree to comply with full CEng registration requirements.
Your career
This course will provide you with the tools and experience to help enhance your career opportunities in the aerospace industry, enabling you to progress further in your present discipline, or move into other specialist or integration roles. Networking with students from different backgrounds is valuable to gain an appreciation of how other companies work.
This course can be used for Chartered Engineer status, which can result in new career opportunities for the future.
How to apply
Online application form. UK students are normally expected to attend an interview and financial support is best discussed at this time. Overseas and EU students may be interviewed by telephone.