Coupled fluid structure analysis for wing 445.6 flutter using a fast dynamic mesh technology

DOI10.1080/10618562.2016.1254201OpenAlexW2552074778MaRDI QIDQ5073702

Jize Zhong, Zi-Li Xu

Publication date: 3 May 2022

Published in: International Journal of Computational Fluid Dynamics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1080/10618562.2016.1254201

zbMATH Keywords

flow separationwing flutteroscillating shock wavetransonic dipfast dynamic mesh technologyfluid structure coupling

Mathematics Subject Classification ID

Fluid mechanics (76-XX) Partial differential equations (35-XX)

Related Items (1)

A fast mesh deformation method for marine propeller flow

Uses Software

• FEAPpv
• Flutter
• Spalart-Allmaras

Cites Work

• Unnamed Item
• Efficient mesh motion using radial basis functions with data reduction algorithms
• The ball-vertex method: a new simple spring analogy method for unstructured dynamic meshes
• Reduced-order fluid/structure modeling of a complete aircraft configuration
• Design and analysis of ALE schemes with provable second-order time-accuracy for inviscid and viscous flow simulations.
• Application of a three-field nonlinear fluid-structure formulation to the prediction of the aeroelastic parameters of an F-16 fighter
• Mesh Moving Techniques for Fluid-Structure Interactions With Large Displacements
• A survey of direct time-integration methods in computational structural dynamics—II. Implicit methods
• Geometric Conservation Law and Its Application to Flow Computations on Moving Grids
• A collocated finite volume method for predicting flows at all speeds
• A doublet-lattice method for calculating lift distributions on oscillating surfaces in subsonic flows.
• Numerical simulation of 3-D wing flutter with fully coupled fluid-structural interaction

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