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Wind tunnel testing of a high aspect ratio wing model

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hdl:2117/177833

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Cooper, Jonathan E.
Cook, Robbie G
Francois, G.
Torre Rodríguez, Óscar de laMés informació
Neild, Simon A.
Lowenberg, Mark H.
Alexander, S. S.
Coetzee, E. B.
Evans, M.
Document typeConference report
Defense date2019
PublisherCurran
Rights accessOpen Access
All rights reserved. This work is protected by the corresponding intellectual and industrial property rights. Without prejudice to any existing legal exemptions, reproduction, distribution, public communication or transformation of this work are prohibited without permission of the copyright holder
Abstract
There is much current interest in the development of High Aspect Ratio Wing (HARW) designs for improved aircraft performance. However, there are a lack of relevant data sets available to validate aeroelastic modelling approaches for highly flexible wings. The design and manufacture of a highly flexible 2.4m semi-span wing is described. A series of low speed wind tunnel tests were performed to generate displacement, acceleration, strain gauge, aerodynamic pressure and six component balance measurements for a range of airspeeds and wing root angles of attack. Numerous static and dynamic measurements were made. Preliminary results are shown for the static and dynamic, structural and aerodynamic behaviour over a range of different airspeeds and wing root angles of attack.
CitationCooper, J. [et al.]. Wind tunnel testing of a high aspect ratio wing model. A: International Forum on Aeroelasticity and Structural Dynamics. "Proceedings of Forum of Aeroelasticity and Structural Dynamics IFASD 2019, 9-13 June 2019, Savannah, Georgia, USA". Red Hook, NY: Curran, 2019, p. 094:1-094:26. 
URIhttp://hdl.handle.net/2117/177833
ISBN1974-5117
Publisher versionhttps://www.asdjournal.org/public/Proceedings/IFASD_2019/IFASD-2019-094.pdf
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  • Departament de Mecànica de Fluids - Ponències/Comunicacions de congressos [178]
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