AustralieFrV1, PascalFrancis, Checkpoint, bibRecord, 002F11

Simulation and Parameter Variation of Flapping-Wing Motion Based on Dragonfly Hovering

Identifieur interne : 002F11 ( PascalFrancis/Checkpoint ); précédent : 002F10; suivant : 002F12

Simulation and Parameter Variation of Flapping-Wing Motion Based on Dragonfly Hovering

Auteurs : John Young [Australie] ; Joseph C. S. Lai [Australie] ; Charly Germain [France]

Source :

AIAA journal [ 0001-1452 ] ; 2008.

RBID : Pascal:08-0247403

Descripteurs français

Pascal (Inist)
- Ecoulement instationnaire, Fluide incompressible, Robotique, Robot mobile, Génération maille, Modélisation, Simulation numérique, Véhicule aérien inhabité, Battement alaire, Vol stationnaire, Biomimétique, Libellulidae, Equation Navier Stokes, Aérodynamique.
Wicri :
- topic : Robotique, Aérodynamique.

English descriptors

KwdEn :
- Aerodynamics, Biomimetics, Hovering, Incompressible fluid, Libellulidae, Mesh generation, Modeling, Moving robot, Navier Stokes equation, Numerical simulation, Robotics, Unmanned aerial vehicle, Unsteady flow, Wing beat.

Abstract

The flapping motion of a wing based on the hind wing of the Aeschna juncea dragonfly is simulated using a three-dimensional incompressible Navier-Stokes solver. The performance of the wing is investigated by variation of a number of kinematic parameters. Flapping amplitudes of between 10 and 60 deg (half-angle) and frequencies of 1 to 300 Hz are considered, resulting in a Reynolds number range of 100 to 50,000. The flapping amplitude observed for Aeschna juncea is shown to maximize the ratio of mean vertical force produced to power required.

Affiliations:

Australie, France

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Pascal:08-0247403

Le document en format XML

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<front><div type="abstract" xml:lang="en">The flapping motion of a wing based on the hind wing of the Aeschna juncea dragonfly is simulated using a three-dimensional incompressible Navier-Stokes solver. The performance of the wing is investigated by variation of a number of kinematic parameters. Flapping amplitudes of between 10 and 60 deg (half-angle) and frequencies of 1 to 300 Hz are considered, resulting in a Reynolds number range of 100 to 50,000. The flapping amplitude observed for Aeschna juncea is shown to maximize the ratio of mean vertical force produced to power required.</div>
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Simulation and Parameter Variation of Flapping-Wing Motion Based on Dragonfly Hovering

Simulation and Parameter Variation of Flapping-Wing Motion Based on Dragonfly Hovering

Source :

Descripteurs français

English descriptors

Abstract

Links toward previous steps (curation, corpus...)

Links to Exploration step

Le document en format XML

Pour manipuler ce document sous Unix (Dilib)

Pour mettre un lien sur cette page dans le réseau Wicri