[HTML][HTML] Investigation on flow structure and aerodynamic characteristics over an airfoil at low Reynolds number—A review

T Xia, H Dong, L Yang, S Liu, Z Jin - AIP Advances, 2021 - pubs.aip.org
This Review summarizes the progress in research on the flow structure and aerodynamic
characteristics of an airfoil at a low Reynolds number encountered by near-space low-speed …

Identification of flow phenomena over NACA 4412 wind turbine airfoil at low Reynolds numbers and role of laminar separation bubble on flow evolution

K Koca, MS Genç, HH Açıkel, M Çağdaş, TM Bodur - Energy, 2018 - Elsevier
Objective of this study is to elucidate relationship with aerodynamic properties and vortex
shedding from suction surface and wake of wind turbine blade at low Reynolds numbers …

Effect of dielectric barrier discharge plasma actuator on the dynamic moment behavior of pitching airfoil at low Reynolds number

G Huang, Y Dai, C Yang, Y Wu, Y Xia - Physics of Fluids, 2021 - pubs.aip.org
The purpose of this paper is to investigate the feasibility of using dielectric barrier discharge
plasma actuation for the pitch stability control of a National Advisory Committee for …

Hydroelastic response and stability of a hydrofoil in viscous flow

A Ducoin, YL Young - Journal of fluids and structures, 2013 - Elsevier
The objective of this research is to investigate the hydroelastic response and stability of a
flexible hydrofoil in viscous flow. The focus is on viscous effects, such as laminar to turbulent …

[HTML][HTML] Numerical and experimental investigation of natural flow-induced vibrations of flexible hydrofoils

EJ Chae, DT Akcabay, A Lelong, JA Astolfi… - Physics of …, 2016 - pubs.aip.org
The objective of this work is to present combined numerical and experimental studies of
natural flow-induced vibrations of flexible hydrofoils. The focus is on identifying the …

Unsteady aerodynamic effects in small-amplitude pitch oscillations of an airfoil

PS Negi, R Vinuesa, A Hanifi, P Schlatter… - International Journal of …, 2018 - Elsevier
High-fidelity wall-resolved large-eddy simulations (LES) are utilized to investigate the flow-
physics of small-amplitude pitch oscillations of an airfoil at R ec= 100, 000. The investigation …

Active flow control of a wing section in stall flutter by dielectric barrier discharge plasma actuators

M Hajipour, A Ebrahimi, X Amandolese - Physics of Fluids, 2022 - pubs.aip.org
This paper investigates the potential of using an active flow control technique to modify stall
flutter oscillations of a NACA (National Advisory Committee for Aeronautics) 0015 wing …

An experimental study of boundary-layer transition induced vibrations on a hydrofoil

A Ducoin, JA Astolfi, ML Gobert - Journal of Fluids and Structures, 2012 - Elsevier
This paper aims at characterizing experimentally laminar to turbulent transition induced
vibrations. Here, the transition is known to be triggered by a Laminar Separation Bubble that …

Computational aeroelastic simulations of self-sustained pitch oscillations of a NACA0012 at transitional Reynolds numbers

D Poirel, V Métivier, G Dumas - Journal of Fluids and Structures, 2011 - Elsevier
The phenomenon of low amplitude self-sustained pitch oscillations in the transitional
Reynolds number regime is studied numerically through unsteady, two-dimensional …

Nonlinear flow-induced instability of an elastically mounted pitching wing

Y Zhu, Y Su, K Breuer - Journal of Fluid Mechanics, 2020 - cambridge.org
We experimentally study the nonlinear flow-induced instability of an elastically mounted
pitching wing in a circulating water tunnel. The structural parameters of the finite-span wing …