DEVELOPMENT AND VALIDATION OF NUMERICAL METHOD FOR STRENGTH ANALYSIS OF LATTICE COMPOSITE FUSELAGE STRUCTURES

DEVELOPMENT AND VALIDATION OF NUMERICAL METHOD FOR STRENGTH ANALYSIS OF LATTICE COMPOSITE FUSELAGE STRUCTURES

Lattice composite fuselage structures are developed as an alternative to conventional composite structures based on laminated skin and stiffeners. Structure layout of lattice structures allows to realize advantages of current composite materials to a maximal extent, at the same time minimizing their...

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Bibliographic Details
Main Author: I. O. Kondakov
Format: Article
Language:Russian
Published: Moscow State Technical University of Civil Aviation 2017-01-01
Series:Научный вестник МГТУ ГА
Subjects:
composite fuselage
lattice structures
numerical strength analysis
finite-element modeling
Online Access:https://avia.mstuca.ru/jour/article/view/995
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