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TsAGI Science Journal

ISSN Imprimir: 1948-2590
ISSN En Línea: 1948-2604

TsAGI Science Journal

DOI: 10.1615/TsAGISciJ.2019031136
pages 325-339

TOPOLOGY OPTIMIZATION OF POLYMER COMPOSITE WING LOAD-BEARING ELEMENT GEOMETRY

Sergei Vladislavovich Baranovski
Moscow State Technical University Named after N.E. Bauman, ul. Baumanskaya 2-ya, 5/1, Moscow, 105005, Russian Federation
Konstantin Valerievich Mikhailovskiy
Moscow State Technical University Named after N.E. Bauman, ul. Baumanskaya 2-ya, 5/1, Moscow, 105005, Russian Federation

SINOPSIS

The topological optimization of a wing and wing box for isotropic and anisotropic materials under operational loads at several angles of attack is performed. The geometrical parameters of carbon fiber elements with a reinforcement pattern different from quasi-isotropic and having different orientation steps of the layers are obtained. The most loaded zones of the structure and the geometric shape of the reinforcement area of the elements are analyzed. The results are considered and used in developing methods of designing a polymer composite wing using parametrical modeling.

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