Assessment of digital image correlation as a method of obtaining deformations of a structure under fluid load

J Banks, LM Giovannetti, X Soubeyran… - Journal of Fluids and …, 2015 - Elsevier
Abstract Digital Image Correlation (DIC) is employed for the measurement of full-field
deformation during fluid–structure interaction experiments in a wind tunnel. The …

Novel method for measuring a dense 3d strain map of robotic flapping wings

B Li, S Zhang - Measurement Science and Technology, 2018 - iopscience.iop.org
Measuring dense 3D strain maps of the inextensible membranous flapping wings of robots
is of vital importance to the field of bio-inspired engineering. Conventional high-speed 3D …

Videogrammetry dynamics measurements of a lightweight flexible wing in a wind tunnel

JT Black, NA Pitcher, MF Reeder, RC Maple - Journal of aircraft, 2010 - arc.aiaa.org
Videogrammetry is a measurement technique well suited to characterizing lightweight,
flexible wings in windtunnel testing. It is noncontact, full field, and can capture the large …

Effects of wing flexibility on bumblebee propulsion

S Tobing, J Young, JCS Lai - Journal of Fluids and Structures, 2017 - Elsevier
This study provides a comprehensive analysis of the effects of flexibility on bumblebee
propulsion. The unusual stiffness distribution of bumblebee wings caused by the absence of …

[HTML][HTML] Optimization of aerodynamic efficiency for twist morphing MAV wing

NI Ismail, AH Zulkifli, MZ Abdullah, MH Basri… - Chinese Journal of …, 2014 - Elsevier
Twist morphing (TM) is a practical control technique in micro air vehicle (MAV) flight.
However, TM wing has a lower aerodynamic efficiency (CL/CD) compared to membrane and …

Numerical research on segmented flexible airfoils considering fluid-structure interaction

D Hefeng, W Chenxi, L Shaobin, SX Zhen - Procedia Engineering, 2015 - Elsevier
This paper investigated four kinds of segmented flexible airfoils with membrane material on
the upper surface and rigid structure on the lower surface. Fluid-structure interaction method …

Unsteady aerodynamics and flow-induced vibrations of a low aspect ratio rectangular membrane wing with excess length

MS Genç - Experimental Thermal and Fluid Science, 2013 - Elsevier
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 …

Full-field wing deformation measurement scheme for in-flight cantilever monoplane based on 3D digital image correlation

LG Li, J Liang, X Guo, C Guo, H Hu… - … Science and Technology, 2014 - iopscience.iop.org
In this paper, a new non-contact scheme, based on 3D digital image correlation technology,
is presented to measure the full-field wing deformation of in-flight cantilever monoplanes …

Eigenmode analysis of membrane stability in inviscid flow

C Mavroyiakoumou, S Alben - Physical Review Fluids, 2021 - APS
We study the instability of a thin membrane (of zero bending rigidity) to out-of-plane
deflections, when the membrane is immersed in an inviscid fluid flow and sheds a trailing …

Nonlinear dynamic responses of a perimeter-reinforced membrane wing in laminar flows

X Sun, XL Ren, JZ Zhang - Nonlinear Dynamics, 2017 - Springer
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 …