Inscrição na biblioteca: Guest
Portal Digital Begell Biblioteca digital da Begell eBooks Diários Referências e Anais Coleções de pesquisa
TsAGI Science Journal

ISSN Imprimir: 1948-2590
ISSN On-line: 1948-2604

TsAGI Science Journal

DOI: 10.1615/TsAGISciJ.2018026632
pages 773-787

BEAM STIFFNESSES OF A COMPOSITE WING WITH ANISOTROPIC SKIN

E. I. Kryuchkov
Central Aerohydrodynamic Institute (TsAGI), 1, Zhukovsky Str., Zhukovsky, Moscow Region, 140180, Russian Federation

RESUMO

Equations for the definition of beam stiffnesses, positions of neutral axes, and rotation centers at bending and torsion, stresses, and deformations of a composite wing with an anisotropic skin are obtained based on the classical beam theory. A comparison of the results obtained from the analytical solutions and the results obtained from the finite-element computations is performed.


Articles with similar content:

ELASTIC PROPERTIES OF QUASIPERIODIC COMPOSITES WITH ACCOUNT FOR CORRELATION FUNCTIONS OF THE STRUCTURE
Nanoscience and Technology: An International Journal, Vol.2, 2011, issue 3
A. A. Pankov
THERMOELASTIC BENDING ANALYSIS OF ORTHOTROPIC PLATES USING HYPERBOLIC SHEAR DEFORMATION THEORY
Composites: Mechanics, Computations, Applications: An International Journal, Vol.4, 2013, issue 3
Atteshamuddin Shamshuddin Sayyad, Yuwaraj M. Ghugal, B. M. Shinde
MODELING OF THIN COMPOSITE LAMINATES WITH GENERAL ANISOTROPY UNDER HARMONIC VIBRATIONS BY THE ASYMPTOTIC HOMOGENIZATION METHOD
International Journal for Multiscale Computational Engineering, Vol.15, 2017, issue 3
I.D. Dimitrienko, Yu. I. Dimitrienko
LAMINATED COMPOSITE STIFFNESS AND STRENGTH ESTIMATION METHOD
TsAGI Science Journal, Vol.48, 2017, issue 7
Vladimir Dmitrievich Vermel, Leonid Leonidovich Chernyshev, Aleksander Ivanovich Oleinikov
Influence of the Follower Force Orientation on Stability Domains of the Upper Equilibrium State of Inverted Double Pendulum
Journal of Automation and Information Sciences, Vol.34, 2002, issue 11
Lada L. Lobas, Leonid G. Lobas