Computational Study of the Aeroelastic Equilibrium Configuration of a Swept Wind Tunnel Wing Model in Subsonic Flow

L. Reimer (), C. Braun () and J. Ballmann
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L. Reimer: RWTH Aachen, Lehrstuhl für Computergestützte Analyse Technischer Systeme (CATS)
C. Braun: RWTH Aachen, Lehr- und Forschungsgebiet für Mechanik (LFM)
J. Ballmann: RWTH Aachen, Lehr- und Forschungsgebiet für Mechanik (LFM)

A chapter in High Performance Computing in Science and Engineering ’06, 2007, pp 421-434 from Springer

Abstract: Abstract In the Collaborative Research Center SFB 401 at RWTH Aachen University, the numerical aeroelastic method SOFIA for direct numerical aeroelastic simulation is being progressively developed. Numerical results obtained by applying SOFIA were compared with measured data of static and dynamic aeroelastic wind tunnel tests for an elastic swept wing in subsonic flow.

Keywords: Wind Tunnel; Wing Model; Root Angle; Wing Structure; Wind Tunnel Model (search for similar items in EconPapers)
Date: 2007
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Persistent link: https://EconPapers.repec.org/RePEc:spr:sprchp:978-3-540-36183-1_31

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DOI: 10.1007/978-3-540-36183-1_31

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