Flapping Wing
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Recent papers in Flapping Wing
We describe the design of four ornithopters ranging in wing span from 10 cm to 40 cm, and in weight from 5 g to 45 g. The controllability and power supply are two major considerations, so we compare the efficiency and characteristics... more
We describe the design of four ornithopters ranging in wing span from 10 cm to 40 cm, and in weight from 5 g to 45 g. The controllability and power supply are two major considerations, so we compare the efficiency and characteristics between different types of subsystems such as gearbox and tail shape. Our current ornithopter is radio-controlled with inbuilt visual sensing and capable of takeoff and landing. We also concentrate on its wing efficiency based on design inspired by a real insect wing and consider that aspects of insect flight such as delayed stall and wake capture are essential at such small size. Most importantly, the advance ratio, controlled either by enlarging the wing beat amplitude or raising the wing beat frequency, is the most significant factor in an ornithopter which mimics an insect.
Insect- and bird-size drones—micro air vehicles (MAV) that can perform autonomous flight in natural and man-made environments are now an active and well-integrated research area. MAVs normally operate at a low speed in a Reynolds number... more
Insect- and bird-size drones—micro air vehicles (MAV) that can perform autonomous flight in natural and man-made environments are now an active and well-integrated research area. MAVs normally operate at a low speed in a Reynolds number regime of 104–105 or lower, in which most flying animals of insects, birds and bats fly, and encounter unconventional challenges in generating sufficient aerodynamic forces to stay airborne and in controlling flight autonomy to achieve complex manoeuvres. Flying insects that power and control flight by flapping wings are capable of sophisticated aerodynamic force production and precise, agile manoeuvring, through an integrated system consisting of wings to generate aerodynamic force, muscles to move the wings and a control system to modulate power output from the muscles. In this article, we give a selective review on the state of the art of biomechanics in bioinspired flight systems in terms of flapping and flexible wing aerodynamics, flight dynamics and stability, passive and active mechanisms in stabilization and control, as well as flapping flight in unsteady environments. We further highlight recent advances in biomimetics of flapping-wing MAVs with a specific focus on insect-inspired wing design and fabrication, as well as sensing systems.
This article is part of the themed issue ‘Moving in a moving medium: new perspectives on flight’.
This article is part of the themed issue ‘Moving in a moving medium: new perspectives on flight’.
Oscillating hydrofoils generate power from the motion of water by oscillating in pitch and heave. They exhibit number of advantages compared to traditional, rotary turbines, including opportunity for placement in arrays due to their... more
Oscillating hydrofoils generate power from the motion of water by oscillating in pitch and heave. They exhibit number of advantages compared to traditional, rotary turbines, including opportunity for placement in arrays due to their coherent, structured wake.
In this thesis, direct numerical simulations with a dynamic mesh approach are employed to study two-hydrofoil arrays with applications in energy harvesting. Twelve different configurations of linear, slightly-staggered and highly-staggered orientation between the hydrofoils are compared in terms of power coefficients and individual hydrofoil and system efficiencies. Vortex-foil interactions of both constructive and destructive nature are observed. It is shown that the trailing hydrofoil can have efficiency up to 19.1 % higher than the leading hydrofoil. The total system efficiency is reported to reach values of up to 0.431. It can be concluded that oscillating hydrofoil arrays may be used for increased energy density of hydrokinetic harvesters.
In this thesis, direct numerical simulations with a dynamic mesh approach are employed to study two-hydrofoil arrays with applications in energy harvesting. Twelve different configurations of linear, slightly-staggered and highly-staggered orientation between the hydrofoils are compared in terms of power coefficients and individual hydrofoil and system efficiencies. Vortex-foil interactions of both constructive and destructive nature are observed. It is shown that the trailing hydrofoil can have efficiency up to 19.1 % higher than the leading hydrofoil. The total system efficiency is reported to reach values of up to 0.431. It can be concluded that oscillating hydrofoil arrays may be used for increased energy density of hydrokinetic harvesters.
High-resolution numerical simulations of a tethered model bumblebee in forward flight are performed superimposing homogeneous isotropic turbulent fluctuations to the uniform inflow. Despite tremendous variation in turbulence intensity,... more
High-resolution numerical simulations of a tethered model bumblebee in forward flight are performed superimposing homogeneous isotropic turbulent fluctuations to the uniform inflow. Despite tremendous variation in turbulence intensity, between 17% and 99% with respect to the mean flow, we do not find significant changes in cycle-averaged aerodynamic forces, moments, or flight power when averaged over realizations, compared to laminar inflow conditions. The variance of aerodynamic measures, however, significantly increases with increasing turbulence intensity, which may explain flight instabilities observed in freely flying bees.
Aerodynamic ground effect in flapping-wing insect flight is of importance to comparative morphologies and of interest to the micro-air-vehicle (MAV) community. Recent studies, however, show apparently contradictory results of either some... more
Aerodynamic ground effect in flapping-wing insect flight is of importance to comparative morphologies and of interest to the micro-air-vehicle (MAV) community. Recent studies, however, show apparently contradictory results of either some significant extra lift or power savings, or zero ground effect. Here we present a numerical study of fruitfly sized insect takeoff with a specific focus on the significance of leg thrust and wing kinematics. Flapping-wing takeoff is studied using numerical modelling and high performance computing. The aerodynamic forces are calculated using a three-dimensional Navier–Stokes solver based on a pseudo-spectral method with volume penalization. It is coupled with a flight dynamics solver that accounts for the body weight, inertia and the leg thrust, while only having two degrees of freedom: the vertical and the longitudinal horizontal displacement. The natural voluntary takeoff of a fruitfly is considered as reference. The parameters of the model are then varied to explore possible effects of interaction between the flapping-wing model and the ground plane. These modified takeoffs include cases with decreased leg thrust parameter , and/or with periodic wing kinematics, constant body pitch angle. The results show that the ground effect during natural voluntary takeoff is negligible. In the modified takeoffs, when the rate of climb is slow, the difference in the aerodynamic forces due to the interaction with the ground is up to 6%. Surprisingly, depending on the kinematics, the difference is either positive or negative, in contrast to the intuition based on the helicopter theory, which suggests positive excess lift. This effect is attributed to unsteady wing-wake interactions. A similar effect is found during hovering.
Wing flexibility controls the aerodynamic-force generation of flapping-wing flyers. As the wing flaps through the air, it is subjected to both aerodynamic force acting on the surface of the wing and inertial force due to the acceleration... more
Wing flexibility controls the aerodynamic-force generation of flapping-wing flyers. As the wing flaps through the air, it is subjected to both aerodynamic force acting on the surface of the wing and inertial force due to the acceleration or deceleration of the wing’s mass. The interaction between these inertial–elastic and aerodynamic forces resulted in wing deformation. To study the effects of skin flexibility and wing deformation on the aerodynamic performance of a flapping wing, fluid flow and structural analyses (two-way fluid structure interaction) are implemented in real-time application through the Multi-Physics Code Coupling Interface, using FLUENT and ABAQUS solvers. The different bending stiffness ratios are highlighted at 2,489; 159 and 1, which correspond to rigid, flexible, and highly flexible cases, respectively. In the present research, wing flexibility is investigated at low Reynolds number (Re≈9,000) and reduced frequency (k=1.92). To validate the numerical model, an experimental study was conducted, and the result of the mean aerodynamic lift and drag coefficient showed good agreement. The time-averaged aerodynamic performances, such as mean lift coefficient, drag coefficient, and lift-to-drag ratio, revealed that the aerodynamic performance of flapping wings increases with the increase in flexibility.
Keywords: flapping wing, aero-elasticity, fluid structure interaction, unsteady aerodynamics, deformation
Keywords: flapping wing, aero-elasticity, fluid structure interaction, unsteady aerodynamics, deformation
The natural wind environment that volant insects encounter is unsteady and highly complex, posing significant flight-control and stability challenges. It is critical to understand the strategies insects employ to safely navigate in... more
The natural wind environment that volant insects encounter is unsteady and highly complex, posing significant flight-control and stability challenges. It is critical to understand the strategies insects employ to safely navigate in natural environments. We combined experiments on free flying bumblebees with high-fidelity numerical simulations and lower-order modeling to identify the mechanics that mediate insect flight in unsteady winds. We trained bumblebees to fly upwind towards an artificial flower in a wind tunnel under steady wind and in a von Kármán street formed in the wake of a cylinder. Analysis revealed that at lower frequencies in both steady and unsteady winds the bees mediated lateral movement with body roll - typical casting motion. Numerical simulations of a bumblebee in similar conditions permitted the separation of the passive and active components of the flight trajectories. Consequently, we derived simple mathematical models that describe these two motion components. Comparison between the free-flying live and modeled bees revealed a novel mechanism that enables bees to passively ride out high-frequency perturbations while performing active maneuvers at lower frequencies. The capacity of maintaining stability by combining passive and active modes at different timescales provides a viable means for animals and machines to tackle the challenges posed by complex airflows.
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