| | Mechanics of Solids A Journal of Russian Academy of Sciences | | Founded
in January 1966
Issued 6 times a year
Print ISSN 0025-6544 Online ISSN 1934-7936 |
Archive of Issues
Total articles in the database: | | 12804 |
In Russian (Èçâ. ÐÀÍ. ÌÒÒ): | | 8044
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In English (Mech. Solids): | | 4760 |
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<< Previous article | Volume 53, Issue 4 / 2018 | Next article >> |
A.V. Lopatin and A.A. Khakhlenkova, "Finite Element Modeling of a Mesh Composite Coupling Section of a Spacecraft," Mech. Solids. 53 (4), 435-439 (2018) |
Year |
2018 |
Volume |
53 |
Number |
4 |
Pages |
435-439 |
DOI |
10.3103/S002565441804009X |
Title |
Finite Element Modeling of a Mesh Composite Coupling Section of a Spacecraft |
Author(s) |
A.V. Lopatin (Reshetnev Siberian State University of Science and Technology, Krasnoyarsky Rabochy pr. 31, Krasnoyarsk, 660037 Russia, lopatin@krasmail.ru)
A.A. Khakhlenkova (Reshetnev Siberian State University of Science and Technology, Krasnoyarsky Rabochy pr. 31, Krasnoyarsk, 660037 Russia) |
Abstract |
A design for a coupling section (adapter) of a spacecraft, consisting of two mesh composite conical shells and a three-layer carrier panel, designed to accommodate three spacecraft, is proposed. A finite element model of the adapter was developed and a generating program was created. An analysis of influence of parameters of a three-layer panel and parameters of the mesh structure of the shells on the main frequency of transverse vibrations is carried out. A set of parameters providing the specified oscillation frequency is computed. |
Keywords |
spacecraft, adapter, finite element method, mesh conical shell, three-layer panel, modal analysis |
References |
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"Buckling Analysis and Design of Anisogrid Composite Lattice Conical Shells,"
93, 3150-3162 (2011). |
5. | V.V. Vasiliev,
Mechanics of Composite Structures
(Taylor and Francis, Washington, 1993). |
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Comp. Struct.
153, 738-745 (2016). |
8. | MSC Nastran. Quick reference guide's: MSC. Software Co. |
|
Received |
08 April 2018 |
Link to Fulltext |
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