Reduced order model for the lift coefficient of an airfoil equipped with extrados and/or trailing edge flexible flaps

DOI10.1016/J.COMPFLUID.2018.11.029zbMath1410.76041OpenAlexW2903555850WikidataQ128827411 ScholiaQ128827411MaRDI QIDQ667376

Talel Ben Mbarek, Chedhli Hafien

Publication date: 12 March 2019

Published in: Computers and Fluids (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/j.compfluid.2018.11.029

zbMATH Keywords

unsteady flowvan der Pol oscillatorcomputational fluid dynamics (CFD)reduced order modelflexible-flapstwo-way fluid-structure interaction (FSI)

Mathematics Subject Classification ID

Navier-Stokes equations for incompressible viscous fluids (76D05) General aerodynamics and subsonic flows (76G25) Software, source code, etc. for problems pertaining to fluid mechanics (76-04)

Uses Software

• Unnamed Item

Cites Work

• Modeling Steady-state and Transient Forces on a Cylinder

This page was built for publication: Reduced order model for the lift coefficient of an airfoil equipped with extrados and/or trailing edge flexible flaps