Trchalik, Josef (2009) Aeroelastic modelling of gyroplane rotors. PhD thesis. http://theses.gla.ac.uk/1232/ Copyright and moral rights for this thesis are retained by the author A copy can be downloaded for personal non-commercial research or study, without prior permission or charge This thesis cannot be reproduced or quoted extensively from without first obtaining permission in writing from the Author The content must not be changed in any way or sold commercially in any format or medium without the formal permission of the Author When referring to this work, full bibliographic details including the author, title, awarding institution and date of the thesis must be given Glasgow Theses Service http://theses.gla.ac.uk/
[email protected] Aeroelastic Modelling of Gyroplane Rotors Josef Trchalík, Dipl.Ing. Ph. D. Thesis Department of Aerospace Engineering University of Glasgow July 2009 Thesis submitted to the Faculty of Engineering in fulfillment of the requirements for the degree of Doctor of Philosophy c J. Trchalík, 2009 Abstract The gyroplane represents the first successful rotorcraft design and it paved the way for the development of the helicopter during the 1940s. Gyroplane rotors are not powered in flight and work in autorotative regime and hence the characteristics of a helicopter rotor during powered flight and a rotor in autorotation differ sig- nificantly. Gyroplanes in the UK have been involved in number of fatal accidents during the last two decades. Despite several research projects focused on gyroplane flight dynamics, the cause of some of gyroplane accidents still remains unclear. The aeroelastic behaviour of autorotating rotors is a relatively unexplored problem and it has not yet been investigated as possible cause of the accidents.