Mathematical model for determination of effective physical and mechanical characteristics of cross-reinforced composite layer

Marchuk, M. V.; Харченко, В. М.; Khomyak, M.

doi:10.15407/apmm2018.16.64-73

Prykl. Probl. Mekh. Mat.

2018

DOI: 10.15407/apmm2018.16.64-73

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Mathematical model for determination of effective physical and mechanical characteristics of cross-reinforced composite layer

M. V. Marchuk¹,

В. М. Харченко²,

M. Khomyak³

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Loading of rocket joins with account for features of constructions of adjacent compartments

Харченко

Klymenko²

2019

Prykl. Probl. Mekh. Mat.

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Розроблено методику розрахунку зусиль на кріпильні елементи стику відсіків ракети, які мають конструктивні особливості (нерівномірність товщини стінок у коловому або поздовжньому напрямках, наявність отворів) за дії осьових сил та згинальних моментів. Методика враховує умови закріплення ракети в контейнері чи на транспортному засобі та дає можливість визначити основні випадки та максимальні навантаження на кріпильні елементи для подальшого розрахунку стиків ракети на міцність. Ключові слова: відсік ракети, стик, кріпильний елемент, осьове зусилля, згинальний момент, міцність, коефіцієнт розподілу навантаження. LOADING OF ROCKET JOINS WITH ACCOUNT FOR FEATURES OF CONSTRUCTIONS OF ADJACENT COMPARTMENTSThe method of calculation of efforts on the fasteners of the junction of missile compartments, which have structural features (uneven wall thickness in a circular or longitudinal direction, the presence of openings) under the action of axial forces and bending moments. The technique takes into account the conditions of rocket fastening in the container or vehicle and allows to determine the basic cases and maximum loads on the fasteners for further calculation of the joints for strength.

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Loading of rocket joins with account for features of constructions of adjacent compartments

Харченко

Klymenko²

2019

Prykl. Probl. Mekh. Mat.

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Effective thermoelastic moduli of discrete composite layers within the framework of the orthotropic material model

Marchuk,

Pakosh,

Kharchenko

et al. 2022

Mat. Met. Fiz. Mekh. Polya

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Mathematical model for determination of effective physical and mechanical characteristics of cross-reinforced composite layer

Cited by 2 publications

References 4 publications

Loading of rocket joins with account for features of constructions of adjacent compartments

Loading of rocket joins with account for features of constructions of adjacent compartments

Effective thermoelastic moduli of discrete composite layers within the framework of the orthotropic material model

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