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A.V. Azarov, "The Problem of Designing Aerospace Mesh Composite Structures," Mech. Solids. 53 (4), 427-434 (2018)
Year 2018 Volume 53 Number 4 Pages 427-434
DOI 10.3103/S0025654418040088
Title The Problem of Designing Aerospace Mesh Composite Structures
Author(s) A.V. Azarov (Central Research Institute for Special Machinery, ul. Zavodskaya 1, Khotkovo, Moscow Region, 141371 Russia; Bauman Moscow State Technical University, ul. 2-ya Baumanskaya 5, str. 1, Moscow, 105005 Russia, avazar@bk.ru)
Abstract The review paper is devoted to the problem of designing mesh composite structures that are widely used in Russian rocket and space technology. Mesh structures developed in our country and made of composites by the method of automatic continuous winding significantly exceed the traditional stringer and three-layer structures, both metal and composite, in terms of their weight efficiency. The features of the structural-technological concept of aerospace mesh structures, their design methods and basic applications are considered. The results obtained in this area by the scientific school of academician V.V. Vasiliev are discussed.
Keywords composite materials, shells, mesh structures, design
References
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Received 28 February 2018
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