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

DOI10.1007/978-3-540-36183-1_31zbMath1391.76271OpenAlexW74876883MaRDI QIDQ4643545

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Publication date: 24 May 2018

Published in: High Performance Computing in Science and Engineering ’06 (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/978-3-540-36183-1_31

Mathematics Subject Classification ID

Fluid-solid interactions (including aero- and hydro-elasticity, porosity, etc.) (74F10) Finite volume methods applied to problems in fluid mechanics (76M12) General aerodynamics and subsonic flows (76G25)

Uses Software

• MEGAFLOW

Cites Work

• An adaptive multiscale finite volume solver for unsteady and steady state flow computations
• The MEGAFLOW project
• Algorithmic Developments in TAU

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