T. Wilson, A. Castrichini, A. Azabal, J.E. Cooper, R. Ajaj, M. Herring

DOI Number: N/A

Conference number: IFASD-2017-216

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.

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In Categories: 1.Events, Active Control and Adaptive Structures, IFASD 2017
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