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This study investigates the dynamics of passively morphing foils under accelerated plunging, establishing mechanistic links between transient kinematics, structural compliance, and aerodynamic performance. Two-way coupled simulations are…

流体动力学 · 物理学 2026-03-31 Hibah Saddal , Lucky Babu Jayswal , Chandan Bose

Submerged flapping foils can convert wave energy directly into thrust, which could be potentially utilised for green marine propulsion. This study analyses the wave-induced flapping hydrofoil propulsion using an in-house developed, new…

流体动力学 · 物理学 2022-09-14 Jingru Xing , Dimitris Stagonas , Phil Hart , Chengchun Zhang , Jianhui Yang , Liang Yang

We study experimentally a four-winged flapping flyer with chord-wise flexible wings in a self-propelled setup. For a given physical configuration of the flyer (i.e. fixed distance between the forewing and hindwing pairs and fixed wing…

流体动力学 · 物理学 2017-10-03 Ramiro Godoy-Diana , Prasann Jain , Mariana Centeno , Alexis Weinreb , Benjamin Thiria

The unsteady aerodynamic thrust and aeroelastic response of a two-dimensional membrane airfoil under prescribed harmonic motion are investigated computationally with a high-order Navier-Stokes solver coupled to a nonlinear membrane…

流体动力学 · 物理学 2018-10-18 Justin W. Jaworski , Raymond E. Gordnier

We perform direct numerical simulations of laminar separated flows over finite-aspect-ratio swept wings at a chord-base Reynolds number of $Re = 400$ to reveal a variety of wake structures generated for a range of aspect ratios…

流体动力学 · 物理学 2020-10-28 Kai Zhang , Shelby Hayostek , Michael Amitay , Anton Burtsev , Vassilios Theofilis , Kunihiko Taira

Sub-gram flapping-wing flying insect robots (FIRs) are challenging to model because of mechanical complexity in their wings, unsteady aerodynamic flow, and the difficulty of making precise measurements at a small scale. Coupling effects…

系统与控制 · 电气工程与系统科学 2026-04-27 Aaron Weber , Daksh Dhingra , Sawyer B. Fuller

We study experimentally a a three-dimensional reduced model of a sail shape performing pitching oscillations around a mean incidence angle ($\alpha_{m}$) with respect to an incoming flow in a hydrodynamic channel at a constant velocity…

流体动力学 · 物理学 2026-03-24 Gauthier Bertrand , Ramiro Godoy-Diana , Benjamin Thiria , Marc Fermigier

Flow over a seal whisker-inspired undulated cylinder at swept back angles is computationally investigated, comparing the vortex shedding, forces, and wake characteristics to those of an equivalent smooth geometry. Numerous prior studies…

Compared with fixed-wing flight, flapping flight can generate a higher lift and is also more maneuverable, largely resulting from the benefits of wing rotation. By analyzing the real wing kinematics of fruit flies, we found that the wing…

流体动力学 · 物理学 2019-06-19 Yang Xiang , Haotian Hang , Hong Liu

The flow-induced flutter has a significant role in aircraft stability, renewable energy extraction, animal locomotion, among many other applications. While being a ubiquitous phenomenon, the control of the flutter response has been…

流体动力学 · 物理学 2022-01-26 Tso-Kang Wang , Kourosh Shoele

Flapping wing propulsion offers unrivalled manoeuvrability and efficiency at low flight speeds and in hover. These advantages are attributed to the leading edge vortex developing on an unsteady wing, which induces additional lift. We…

流体动力学 · 物理学 2021-02-10 Johannes Kissing , Bastian Stumpf , Jochen Kriegseis , Jeanette Hussong , Cameron Tropea

Passive flow control research is commonly utilized to provide desirable drag and oscillating lift reduction across a range of engineering applications. This research explores the spanwise undulated cylinder inspired by seal whiskers, shown…

流体动力学 · 物理学 2023-09-13 Kathleen Lyons , Raúl Bayoán Cal , Jennifer A. Franck

We investigate the dynamics and the stability of the incompressible flow past a corrugated dragonfly-inspired airfoil in the two-dimensional (2D) $\alpha-Re$ parameter space, where $\alpha$ is the angle of attack and $Re$ is the Reynolds…

流体动力学 · 物理学 2025-04-16 Alessandro Chiarini , Gabriele Nastro

Through triglobal resolvent analysis, we reveal the effects of wing tip and sweep angle on laminar separated wakes over swept wings. For the present study, we consider wings with semi-aspect ratios from $1$ to $4$, sweep angles from…

流体动力学 · 物理学 2022-12-06 Jean Hélder Marques Ribeiro , Chi-An Yeh , Kunihiko Taira

The propulsion of a flapping wing or foil is emblematic of bird flight and fish swimming. Previous studies have identified hallmarks of the propulsive dynamics that have been attributed to unsteady effects such as the formation and shedding…

流体动力学 · 物理学 2026-04-07 Olivia Pomerenk , Leif Ristroph

Accurate prediction of wake dynamics behind hydrofoils is critical for mitigating vortex-induced vibrations and improving the performance of hydraulic machinery. Conventional turbulence modeling approaches often struggle to capture the…

流体动力学 · 物理学 2026-01-30 Gabriele Gaiti , Chirag Trivedi , Kristian F. Sagmo

Experimental results of towing a cylinder through a dense suspension of cornstarch and sucrose-water are presented. Focus is placed on the jamming fronts that exist in such systems. The literature has concentrated on the propagation of the…

软凝聚态物质 · 物理学 2021-06-14 Olav Rømcke , Ivo R. Peters , R. Jason Hearst

The aim of this work is to study the dynamics and stability of soft shape-morphing configurations and specifically the modes of interaction between the front and rear airfoil segments. Initially we present several steady-state solutions,…

流体动力学 · 物理学 2018-05-08 Netanel Hassan , Shai B. Elbaz , Amir D. Gat

Wing flexibility plays an essential role in the aerodynamic performance of insects due to the considerable deformation of their wings during flight under the impact of inertial and aerodynamic forces. These forces come from the complex wing…

流体动力学 · 物理学 2020-07-20 Hung Truong , Thomas Engels , Dmitry Kolomenskiy , Kai Schneider

The unsteady characteristics of the flow over thick flatback airfoils have been investigated by means of CFD calculations. Sandia airfoils which have 35% maximum thickness with three different trailing edge thicknesses were selected. The…

流体动力学 · 物理学 2017-05-12 Galih Bangga , Thorsten Lutz , Ewald Krämer