MSc - Aerospace Engineering

University of Hertfordshire

This module introduces students to structural dynamics and static aeroelastic phenomenon such as divergence and control reversal, together with unsteady aerodynamics and dynamic aeroelastic phenomenon such as flutter. Typical aerospace vehicle aeroelastic problems are considered, while aeroelastic analysis is introduced through the consideration of the behaviour of a typical aerofoil and a high aspect ratio wing in bending and torsion. Student learning is supported by assignments making use of aeroelastic analysis software and finite element analysis software.

This module develops the student's knowledge of aerodynamics and experience of using CFD. Topics include potential flow theory, panel methods, lifting line and slender body theory, together with hypersonic aerodynamics. CFD applications cover a range of applications, making extensive use of commercial codes to simulate airflows.

The module content includes an introduction to materials engineering and manufacturing, as well as covering details on engineering alloys, materials science and materials selection. Materials pertinent to the aerospace industry are looked at including polymers and composites for high performance structures as well sustainable options and those suitable for aerospace manufacturing processes. The module also includes a look at supply chain management issues related to materials and manufacturing.

Module introduces various implementations of computational fluid dynamics (CFD) and its theoretical foundation. It covers how to tackle complex engineering challenges with CFD; to evaluate and to analyse efficiently the resulting data.

The module introduces development of simulation models replicating engineering problems. It will examine the effect of mesh density, domain size, boundary conditions, material properties on the optimisation of systems performance. Analytical approximation techniques and numerical schemes will be explored to validate and correlate the results against benchmark solutions.

This module develops student's knowledge and understanding of aircraft dynamics, stability, and control beyond undergraduate level. Topics covered include compressibility, thrust-offset, and static aeroelastic effects on aircraft static stability and control; dynamics stability analysis; quasi-steady asymmetric flight; sideslipping and turning; methods for estimating aerodynamic derivatives; and an introduction to parameter identification methods. Student learning is supported by assignments making use of simulation software and, when possible, flight simulators.

This module develops the student's knowledge and skills in the mathematical modelling of aircraft with an applied focus in the implementation of flight simulation methods, including modelling of navigation in the Earth's environment, dynamic behaviour of aircraft, and propulsion systems. Students will also look at the design and use of flight simulators for both pilot training and engineering design and the associated design requirements for each case. Students will also be introduced to techniques for programming and numerical computation of flight models.

The Masters Project serves as a pivotal integrating component of the programme, aimed at challenging and enhancing critical thinking skills. It offers students the opportunity to synthesise and apply the knowledge and skills gained throughout their postgraduate studies under the mentorship of an academic supervisor. The project typically requires 600 hours of self-driven scholarly work. This effort predominantly involves self-directed independent study, which may encompass a variety of activities such as scheduled sessions, supervisory meetings, literature review, software analysis, and preparation for assessments.

The module aims to enhance student's skills and knowledge in conventional aerospace propulsion systems (e.g., gas turbine cycles, turbofan design, propeller performance analysis) as well as introduce modern technologies covering electric propulsion. This includes the principles and concepts of electrification of aircraft towards the implementation of urban air mobility and addressing global sustainability concerns. Students will cover advanced analysis and design methods for components of gas turbines, design and performance characterisation of propellers, and in the design, specification, and analysis of the performance of electric motors and other components for electric aircraft propulsion.