@inproceedings{d641d41811b64b1bb192376195e301e5,
title = "Aeroelastic behaviour of hinged wing tips",
abstract = "The primary purpose of a hinged wing tip on an airliner aircraft is to allow an aerodynamically efficient high aspect ratio wing to enter an airport gate of standard dimensions. There exists a potential opportunity to allow a wing tip to move in flight to alleviate the loads and achieve a lower wing weight – or enable the wing span to be maximised. This paper will provide a summary of the latest studies investigating the (semi) Aeroelastic behaviour (loads, flutter and rolling) of hinged wing tips.",
keywords = "Aeroelastic, Flutter, Gusts, Hinged / folding wing tips, Load alleviation, Manoeuvres",
author = "T. Wilson and A. Castrichini and A. Azabal and Cooper, {J. E.} and R. Ajaj and M. Herring",
note = "Publisher Copyright: {\textcopyright} 2017 International Forum on Aeroelasticity and Structural Dynamics (IFASD). All Rights Reserved.; 17th International Forum on Aeroelasticity and Structural Dynamics, IFASD 2017 ; Conference date: 25-06-2017 Through 28-06-2017",
year = "2017",
language = "British English",
series = "17th International Forum on Aeroelasticity and Structural Dynamics, IFASD 2017",
booktitle = "17th International Forum on Aeroelasticity and Structural Dynamics, IFASD 2017",
}