Results 11 to 20 of about 4,033 (212)
Aeroelasticity belongs to the larger family of fluid-structure interaction problems that are characterized by the interplay between a fluid and deforming body [...]
Andrea Da Ronch
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MATHEMATICAL MODELING IN NON-LINEAR AEROELASTICITY PROBLEMS
The modern aircraft aeroelasticity problems solving are considered. Mathematical models of aeroelasticity joined by non-linear vortex methods of numerical aerodynamics are described for different objects.
V. I. Morozov, V. V. Ovchinnikov
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Introduction to Aeroelasticity
The lecture gives an introduction into aeroelasticity and presents the mathematical background for the description of torsional divergence and flutter for a two-dimensional airfoil in pitch and plunge ...
Krüger, Wolf R.
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Aeroelastic tailoring for aerospace applications. [PDF]
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
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Aeroelastics Flight Dynamics Coupling Effects of the Semi-Aeroelastic Hinge Device [PDF]
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
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A beginners guide to literature in the field of aeroelasticity
This document is meant primarily for students (or readers) who may not be familiar with the field of aeroelasticity. The main objective of this paper is to point the reader to some important texts and papers that have been published in the areas which ...
Battoo, R. S.
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zuckberj/nastran-aeroelasticity: v0.2.1-alpha
Full Changelog: https://github.com/zuckberj/nastran-aeroelasticity/compare/v0.2.0-alpha...v0.2.1 ...
zuckberj, DeepSource Bot
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Aeroelastic Dynamic Response and Control of an Aeroelastic System with Hysteresis Nonlinearities [PDF]
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
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Viscoelastic damping design – Thermal impact on a constrained layer damping treatment
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
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This chapter deals with the basic principles of aeroelasticity theory (Theodorsen theory) and how these can be applied to bridge structures with sensitive deck shapes. The most common aerodynamical models with two or three forces as well as buffeting forces are briefly presented.
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