An efficient finite differences method for the computation of compressible, subsonic, unsteady flows past airfoils and panels

DOI10.1016/J.JCP.2017.05.046zbMath1378.76072OpenAlexW2620663465MaRDI QIDQ1692049

Miguel Pérez-Saborid, Manuel Colera

Publication date: 26 January 2018

Published in: Journal of Computational Physics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/j.jcp.2017.05.046

zbMATH Keywords

unsteady aerodynamicsflutterconvected wave equationcompressible subsonic flowairfoil-fluid interactionlinearized potential flow

Mathematics Subject Classification ID

Experimental work for problems pertaining to fluid mechanics (76-05) Finite difference methods applied to problems in fluid mechanics (76M20) General aerodynamics and subsonic flows (76G25)

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Uses Software

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• ANSYS-CFX

Cites Work

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• An efficient boundary element method for two-dimensional transient wave propagation problems
• Time domain numerical calculations of unsteady vortical flows about a flat plate airfoil
• An explicit finite element method for the wave equation
• Low-Speed Aerodynamics
• On the aeroelastic instability of two-dimensional panels in uniform incompressible flow
• Fundamentals of Modern Unsteady Aerodynamics
• Aeroelastic instability of cantilevered flexible plates in uniform flow
• A modern course in aeroelasticity.

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