[en] In this work, a wind tunnel model of a wing undergoing stall flutter oscillations is studied. It is a rectangular wing with pitch and plunge degrees of freedom and low pitch stiffness. The objective of this study is to promote the understanding of the stall flutter phenomenon by measuring the unsteady pressure distribution around the wing as well as the wing displacement, during unforced motion in two degrees of freedom. Both steady and unsteady pressures must be measured with sufficient accuracy during two types of tests. In the static tests the wing is to be clamped in position and not allowed to move and the steady pressures are to be measured around the centre-span section at different angles of attack. Thus the stall angle of attack can be identified and the stall mechanism characterized. In the dynamic tests the wing will be allowed to move and the unsteady pressures will be measured and recorded during a number of cycles of the oscillation, at a number of free stream airspeeds.
Disciplines :
Aerospace & aeronautics engineering
Author, co-author :
Li, Jing; University of Manchester > School of Mechanical Aerospace and Civil Engineering
Dimitriadis, Grigorios ; Université de Liège - ULiège > Département d'aérospatiale et mécanique > Interactions Fluide-Structure - Aérodynamique expérimentale
Gu, Fengshu; University of Manchester > School of Mechanical Aerospace and Civil Engineering
Chen, Q.; Sinocera Piezotronics Inc, China
Language :
English
Title :
Novel Instrumentation for the Measurement of the Unsteady Pressure Distribution around a Wing Undergoing Stall Flutter Oscillations
Publication date :
October 2007
Event name :
Autumn Conference of the Institute of Acoustics 2007: Advances in Noise and Vibration Engineering
Event organizer :
Institute of Acoustics, United Kingdom
Event place :
Oxford, United Kingdom
Event date :
du 17 octobre au 18 octobre 2007
Audience :
International
Main work title :
Autumn Conference of the Institute of Acoustics 2007: Advances in Noise and Vibration Engineering
Publisher :
Institute of Acoustics, St Albans, United Kingdom
ISBN/EAN :
1 901656 87 X
Collection name :
Proceedings of the Institute of Acoustics, Volume 29, Part 5
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