Module overview
Aerothemodynamics is essential to the design of high speed flight vehicles (in this context high speed refers to anything above about Mach 0.3). The subject integrates thermodynamics and fluid mechanics concepts to cover the fundamentals of compressible flow, along with applications to external and internal aerodynamics.
Linked modules
Pre-requisites: SESA2022 OR FEEG2003
Aims and Objectives
Learning Outcomes
Transferable and Generic Skills
Having successfully completed this module you will be able to:
- Study and learn independently, solving engineering problems
- Apply basic finite difference techniques to solve partial differential equations
- Communicate work in written reports
Subject Specific Practical Skills
Having successfully completed this module you will be able to:
- Apply simple correlations for estimation of convective heat transfer
- Apply the inverse-design MoC technique for nozzle design
- Apply shock/expansion theory to external and internal aerodynamic application
- Apply Prandtl-Glauert correction for subsonic flows
- Apply Ackerets’ theory to supersonic flow, including design optimisation
Knowledge and Understanding
Having successfully completed this module, you will be able to demonstrate knowledge and understanding of:
- Understanding of how the full governing equations can be simplified for sub- and supersonic flow regimes and awareness of established/emerging numerical technique to solve them
- Knowledge and understanding of inviscid compressible high-speed flows
- Knowledge and understanding of the basic principles of thermodynamics and heat transfer and how this integrates into high speed aerodynamics
Partial CEng Programme Level Learning Outcomes
Having successfully completed this module you will be able to:
- The assessed coursework exercise requires an individual written report that includes a non-technical summary, with the main body of the report aimed at a technical audience.
- Students learn and are assessed (in examination and coursework) on the use of aerothermodynamics tools and concepts, to perform (i) linear and nonlinear analysis of wing sections under supersonic flow conditions (ii) nozzle design and analysis for the complete range of ratios of back pressure to stagnation pressure (iii) thermal analysis and assessment of heat exchanger performance.
Full CEng Programme Level Learning Outcomes
Having successfully completed this module you will be able to:
- The final examination and coursework exercises assess the application of engineering principles to the solution of complex aerothermodynamics problems, involving shock waves, expansion fans and heat transfer, including state-of-the-art method of characteristics for analysis and design of internal flows.
- The assessed coursework exercise involves the design of a supersonic nozzle, including the selection of an appropriate computational tool and including discussion specifically of the limitations of the technique.
Syllabus
Introduction
- Review of 1D gasdynamics and basic concept from thermodynamics
Two-dimensional gas dynamics
- Oblique shock waves; shock reflections (regular and Mach); shock/shock interactions; Prandtl-Meyer expansion waves; shock/expansion method for airfoils; under/over-expanded flow; supersonic wind tunnel.
Conservation laws and simplifications
- Conservation of mass, momentum and energy leading to the compressible Navier-Stokes equations, Crocco equation. Rotational and potential flows. Euler and potential flow equations.
Method of characteristics
- Derivation of method of charactersitsics (MoC). 2-D supersonic nozzle design using MoC.
External aerodynamics
- Flow patterns in transonic and supersonic airfoil flow; critical Mach number; thin airfoils in compressible flow; velocity potential and pressure coefficient; Prandtl-Glauert transformation; Ackeret
theory for supersonic airfoil flow; minimum wave drag; effect of sweepback; sub- and supersonic leading edges.
Heat transfer
- Elements of conduction, convection and radiation heat transfer. Laminar and turbulent boundary layers. Finite difference solution of heat equation. Heat exchangers. Application to heat transfer on high speed vehicles.
Revision
Coursework (e.g. MoC exercise) and examples sheets
Learning and Teaching
Teaching and learning methods
Teaching and learning methods
- Lectures.
- Tutorials/examples classes.
- Supporting material on Blackboard.
Type | Hours |
---|---|
Lecture | 36 |
Follow-up work | 18 |
Preparation for scheduled sessions | 18 |
Completion of assessment task | 18 |
Wider reading or practice | 36 |
Revision | 24 |
Total study time | 150 |
Assessment
Assessment strategy
Can be repeated externally (100% exam) or internally.
Summative
This is how we’ll formally assess what you have learned in this module.
Method | Percentage contribution |
---|---|
Final Assessment | 80% |
Continuous Assessment | 20% |
Referral
This is how we’ll assess you if you don’t meet the criteria to pass this module.
Method | Percentage contribution |
---|---|
Set Task | 100% |
Repeat
An internal repeat is where you take all of your modules again, including any you passed. An external repeat is where you only re-take the modules you failed.
Method | Percentage contribution |
---|---|
Set Task | 100% |
Repeat Information
Repeat type: Internal & External