Skip to main content

Unit information: Dynamics of Rotors 3 in 2012/13

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 Dynamics of Rotors 3
Unit code AENG30005
Credit points 10
Level of study H/6
Teaching block(s) Teaching Block 2 (weeks 13 - 24)
Unit director Dr. Brano Titurus
Open unit status Not open
Pre-requisites

AENG 21301 Vibrations 2, AENG 21100 Aerodynamics 2

Co-requisites

None

School/department Department of Aerospace Engineering
Faculty Faculty of Engineering

Description including Unit Aims

The aim of this course is to develop an understanding of the dynamics of blades and rotors in the context of helicopter and wind turbine technologies. Students will be shown mixture of analytical, numerical and experimental methods for rotor and blade analyses. The theories developed for helicopters will be adapted to wind turbine rotors, highlighting the differences and similarities in their dynamics.

Intended Learning Outcomes

On successful completion of the unit the student will: - understand key terminology, parameters and operational principles used in helicopter and wind turbine rotors with particular focus on dynamics problems, - be able to formulate equations of motion of rigid and elastic rotating blades, extract essential dynamic properties and understand their significance during design, development and structural assessment, - be able to use selected analytical and experimental methods based on Modal Analysis to interpret and tackle dynamics and vibration problems, - be able to use the blade element theory to formulate rotor blade aeroelastic problems and appreciate corresponding changes in structural responses and stability, - understand the mechanical filtering effect in helicopter and wind turbine rotors and its influence on the structural loads and vibrations, - be able to approach and understand the importance of the current vibration and load control research efforts in helicopter and wind turbine technology sectors.

Teaching Information

Lectures

Assessment Information

80% for 2 hour exam paper, 20% for written report

Reading and References

Newman, S., The Foundations of Helicopter Flight, Butterworth-Heinemann, 1994; Bramwell, A.R.S., Done, G., Balmford, D., Bramwell's Helicopter Dynamics, 2nd ed., Butterworth-Heinemann, 2001; Spera, D.A., ed., Wind turbine technology: fundamental concepts of wind turbine engineering, ASME Press, 2009

Feedback