Results 11 to 20 of about 517 (182)

Aeroelastic tailoring for aerospace applications. [PDF]

open access: yesHeliyon, 2023
This study presents a brief account of the seminal works on aeroelastic tailoring for aerospace applications. Tailoring using advanced composites is a revolutionary process in the ever-evolving realm of aerospace design. The rapid growth in scientific knowledge and research necessitates the consolidation of the latest research and technological ...
Najmi J   +4 more
europepmc   +4 more sources

Aeroelastics Flight Dynamics Coupling Effects of the Semi-Aeroelastic Hinge Device [PDF]

open access: yesJournal of Aircraft, 2020
A recent consideration in aircraft design is the use of folding wingtips, with the aim of enabling higher-aspect-ratio aircraft with less induced drag but also meeting airport gate limitations.
Castrichini A.   +5 more
openaire   +5 more sources

Aeroelastic Dynamic Response and Control of an Aeroelastic System with Hysteresis Nonlinearities [PDF]

open access: yesJournal of Control Science and Engineering, 2015
A state feedback control law based on the sliding mode control method is derived for the aeroelastic response and flutter suppression of a two-dimensional airfoil section with hysteresis nonlinearity in pitch. An observer is constructed to estimate the unavailable state variables of the system.
Xingzhi Xu, Yakui Gao, Weiguo Zhang
openaire   +3 more sources

Viscoelastic damping design – Thermal impact on a constrained layer damping treatment

open access: yesMaterials & Design, 2021
Constrained layer damping treatments have been commonly used for vibration damping. The included viscoelastic material exhibits high damping potential that is retrieved under shear deformation.
Martin Gröhlich   +3 more
doaj   +1 more source

Design and Optimization of an Aeroservoelastic Wind Tunnel Model

open access: yesFluids, 2020
Through the combination of passive and active load alleviation techniques, this paper presents the design, optimization, manufacturing, and update of a flexible composite wind tunnel model.
Johannes K. S. Dillinger   +4 more
doaj   +1 more source

NUMERICAL SIMULATION OF OSCILLATIONS OF A PLATE IN RESTING FLUID

open access: yesInternational Journal for Computational Civil and Structural Engineering, 2023
This paper presents a numerical solution of the problem of oscillations of a flexible plate placed in a viscous incompressible fluid done with ANSYS. In constructing a finite element model of the plate, both volumetric and shell finite elements, which ...
Irina Negrozova, Oleg Goryachevsky
doaj   +1 more source

Modeling and Analysis of Aeroelasticity and Sloshing for Liquid Rocket

open access: yesIEEE Access, 2019
In this paper, based on the advantages of Newtonian mechanics method, mixed coordinate method, and analytical mechanics method, the dynamic model of rigid-aeroelasticity-sloshing coupling is established for longitudinal vibration and liquid fuel sloshing,
Dewei Zhang   +4 more
doaj   +1 more source

Aerodynamic Performance and Wake Flow of Crosswind Kite Power Systems

open access: yesEnergies, 2022
This paper presents some results from a computational fluid dynamics (CFD) model of a multi-megawatt crosswind kite spinning on a circular path in a straight downwind configuration. The unsteady Reynolds averaged Navier-Stokes equations closed by the k−ω
Mojtaba Kheiri   +4 more
doaj   +1 more source

Measurement of FRFs and Modal Identification in Case of Correlated Multi-Point Excitation

open access: yesShock and Vibration, 2008
The modal identification of large and dynamically complex structures often requires a multi-point excitation. Sine sweep excitation runs are applied when it is necessary to concentrate more energy on each line of the frequency spectrum.
U. Fuellekrug   +3 more
doaj   +1 more source

Geometrical Nonlinear Aeroelastic Stability Analysis of a Composite High-Aspect-Ratio Wing

open access: yesShock and Vibration, 2008
A composite high-aspect-ratio wing of a high-altitude long-endurance (HALE) aircraft was modeled with FEM by MSC/NASTRAN, and the nonlinear static equilibrium state is calculated under design load with follower force effect, but without load ...
Chang Chuan Xie   +2 more
doaj   +1 more source

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