Aircraft Aerodynamics and Performance 2

Overview

The course reviews fundamentals of aircraft performance considering cruise, climb, take-off, landing and accelerating flight considerations. Basic principles of stability and control are introduced, with the distinction between static and dynamic stability discussed. Methods for calculation of forces on thin wing sections and finite-span wings in low-speed flow are developed from fundamental fluid principles, introducing concepts of stream functions, velocity potentials, vorticity and circulation for flow analysis. Laminar, turbulent and transitional boundary layer development are discussed with relation to aircraft performance, and methods for their preliminary analysis established.

Learning Objectives

Analyse complex problems to reach substantiated conclusions using first principles of mathematics, statistics, natural science and engineering principles

Select and apply appropriate computational and analytical techniques to model complex problems, recognising the limitations of the techniques employed

Select and apply appropriate materials, equipment, engineering technologies and processes, recognising their limitations

Apply a comprehensive knowledge of mathematics, statistics, natural science and engineering principles to the solution of complex problems. Much of the knowledge will be at the forefront of the particular subject of study and informed by a critical awareness of new developments and the wider context of engineering

Select and apply appropriate computational and analytical techniques to model complex problems, discussing the limitations of the techniques employed

Skills

Analyse data using appropriate techniques

Demonstrate analytical and problem-solving skills

Plan self-learning and improve performance, as the foundation for lifelong learning/CPD

Manage time effectively in order to achieve intended goals

Identify their own information needs in order to support complex problem requirements

Assessment

None.