Vortex-induced vibrations (VIVs) of a fixed two-dimensional perimeter-reinforced (PR)
membrane wing at 0 ≤ α 0≤ α Re (Reynolds number) ≤≤ 1000 and 0^ ∘ ≤ α 0∘≤ α …

In this study, an experimental investigation of a low aspect ratio rectangular membrane wing
with excess length was presented at angles of attack ranging from 0° to 25° at Reynolds …

Fluid–structure interaction of a flexible membrane wing was investigated experimentally at a
fixed angle of attack (α= 14). The Reynolds numbers (Re) based on the chord length of the …

An experimental study of a low aspect ratio rectangular membrane wing in a wind tunnel
was conducted for a Reynolds number range of 2.4× 104–4.8× 104. Time-accurate …

Dynamic responses of a two-dimensional (2D) perimeter-reinforced (PR) membrane wing in
laminar viscous flows are investigated numerically. The 2D Navier–Stokes equations and a …

In this study, we present a global Fourier mode decomposition framework for unsteady fluid–
structure interaction. We apply the framework to isolate and extract the aeroelastic modes …

In this study, the effect of the aspect ratio on the aerodynamics characteristic of flexible
membrane wings with different aspect ratios (AR= 1 and AR= 3) is experimentally …

In this paper, we study the fluid–structure interaction of a three-dimensional (3-D) flexible
membrane immersed in an unsteady separated flow at moderate Reynolds numbers. We …

The kinematic characteristics of flexible membrane wing have vital influences on its
aerodynamic characteristics. To deeply explore the regularities between them, time-resolved …

In this paper, we investigate the aeroelasticity of bio-inspired flexible membrane wings using
our recently developed three-dimensional (3D) variational fluid-structure interaction solver …