Impact of flexibility on the aerodynamics of an aspect ratio two membrane wing

Development of an aeroelastic solver with application to flexible membrane wings for micro air vehicles is presented. A high-order (up to sixth order) Navier–Stokes solver is coupled with a geometrically nonlinear p-version Reissner–Mindlin finite element plate model to simulate the highly flexible...

Ausführliche Beschreibung

Bibliographische Detailangaben

Veröffentlicht in:	Journal of fluids and structures 2014-02, Vol.45, p.138-152
Hauptverfasser:	Gordnier, Raymond E., Attar, Peter J.
Format:	Artikel
Sprache:	eng
Schlagworte:	Aerodynamics Aeroelasticity Angle of attack Computational fluid dynamics Flexibility Lift Membrane wing Membranes Micro air vehicle Navier-Stokes equations Unsteady aerodynamics Vortex dynamics Wings (aircraft)
Online-Zugang:	Volltext
Tags:	Tag hinzufügen Keine Tags, Fügen Sie den ersten Tag hinzu!