Aims

The aims of the course are to:

• develop the basic ideas necessary to understand some advanced concepts in aerodynamics.
• cover the aerodynamic effects that constrain an aircraft design.
• appreciate the challenges of reducing the environmental impact of aviation.

Objectives

As specific objectives, by the end of the course students should be able to:

• have an appreciation of the aerodynamic factors likely to feature in the designs of new aircraft.
• have an understanding of the behaviour of boundary layers over swept wings in compressible flow.
• have sufficient knowledge to be able to predict the different supersonic zones on a wing.
• understand how the basic physics can be integrated into the design of an aircraft.
• understand how to make design trade-offs.
• have a basic appreciation of the impact of aviation on the environment and possible responses.

Content

This course aims to develop the basic ideas necessary to enable the student to understand some advanced concepts in aerodynamics. In particular the course will cover the aerodynamic effects that constrain an aircraft design. The course will highlight those factors determining the configuration of aircraft for different duties relating them to the effect of compressibility at transonic speeds. Coursework will illustrate undelying flow physics, via transonic airfoil design and the integration of these basics via a study of the trade-offs made in producing a transonic wing section design for a given specification. The course will end by reviewing the environmental impact of aviation and show how aircraft design might change to reduce this impact.

Introduction to Transonic Aerodynamics (3L, Dr J.P. Jarrett)

• Overview of transonic design concepts;
• Transonic flow about two-dimensional airfoils;
• Shock-boundary layer interaction;
• Supercritical airfoils with delayed shock-induced drag rise.

Transonic Airfoil Design (4h coursework, Dr J.P. Jarrett)

This coursework section will allow the interactive design of a transonic airfoil profile. The aim is to consolidate the lecture material and illustrate how the various design constraints compete in practice.

Aircraft Aerodynamic Design (3L, Dr J.P. Jarrett)

• Airframe / Intake integration
• Stability of swept wing aircraft
• Practical swept wing design
• Delta and slender ogival wings
• Vertical / short take-off and landing

Aviation and the Environment (6L, Prof W.N. Dawes)

The impact of air transport on the environment; the relationship between technology, operational practice, regulation and economics.

• Basic modelling
• The environment - overview of atmospheric chemistry, fluid dynamics & mixing; the greenhouse effect; radiative forcing.
• Airframe - aircraft range & endurance, the Breguet equation; ML/D payload, fuel and structure weight; choice of fuel. Why do airplanes fly at the altitude they do? Payload and fuel efficiency.
• Engine - simple modelling of a high-bypass ratio turbofan engine. Cycle efficiency and propulsive efficiency, trading production of NOx and CO2.
• What would an airplane look like if optimised to reduce environmental impact?

Reducing the Environmental Impact of Aircraft (Coursework, Prof W.N. Dawes)

The coursework consists of a choice of one from three case studies, based on the simple modelling above to study from the perspective of environmental impact the trade-offs associated with (A) design range;(B) cruise altitude;and (C) engine overall pressure ratio. It is intended that the case studies will be spreadsheet based.

This syllabus contributes to the following areas of the UK-SPEC standard:

Toggle display of UK-SPEC areas.

 
Last modified: 20/05/2021 07:41