Skip to main content

Unit information: Aeroelasticity in 2014/15

Please note: you are viewing unit and programme information for a past academic year. Please see the current academic year for up to date information.

Unit name Aeroelasticity
Unit code AENG30007
Credit points 10
Level of study H/6
Teaching block(s) Teaching Block 2 (weeks 13 - 24)
Unit director Professor. Cooper
Open unit status Not open
Pre-requisites

AENG21301 Vibrations 2

Co-requisites

None

School/department School of Engineering Mathematics and Technology
Faculty Faculty of Engineering

Description including Unit Aims

To develop an understanding of aeroelastic behaviour of aerospace, civil and mechanical structures, covering static and dynamic aspects of attached and separated flows. Content Instabilities of non-aerodynamic self-excited systems Static aeroelasticity 3D wings – divergence/control reversal Unsteady aerodynamics – Wagner & Theodorsen functions Flutter 3D Wings: binary flutter, solution of flutter equations, frequency matching, control surface flutter, flight flutter testing. Prediction of flutter speed from flight test results. Non-linear aeroelasticity – stall flutter, buffet, buzz, Limit Cycle Oscillations, affect of structural non-linearities, aeroservoelasticity, transonic effects, vortex shedding Gusts – simple gusts analysis. Kussner and Sears functions. Discrete tuned gusts Aeroservoelasticity – loads alleviation and flutter suppression.

Intended Learning Outcomes

On successful completion the student should be able to:- 1.1 Determine criterion for stability of systems subject to follower forces 1.2 Perform divergence and control reversal calculations 1.3 Predict onset of flutter for binary systems 1.4 Predict flutter onset based upon sub-critical measurements 1.5 Understand the effect of unsteady aerodynamics on aeroelastic calculations 1.6 Understand the effect of non-linearities on aeroelastic behaviour 1.7 Perform experimental aeroelastic measurements and perform relevant analysis

Teaching Information

Lectures, example classes and laboratories

Assessment Information

20% Assessed Laboratory Class on Aeroelastic Wind Tunnel Test (LOs 1.3, 1.4) 80% 2 hour exam, 3 questions out of 5 (LOs 1.1, 1.2, 1.3, 1.4, 1.5, 1.6)

Reading and References

Introduction to Aircraft Aeroelasticity and Loads. J.R. Wright and J.E. Cooper. Wiley 2007 Introduction to the Theory of Aeroelasticity. Y C Fung. Dover 2003.

Feedback