Weight Efficiency of Anisogrid Circular Cylindrical Shells in Transverse Bending

The research results are obtained on the basis of a technique implementing the finite element method for solving the problems of strength and stability of reinforced cylindrical shells made of the composite material, taking into account the momentness and nonlinearity of their subcritical stress-strain state. The stability of an anisogrid circular cylindrical shell made of a composite material under transverse bending is investigated. The effect of deformation nonlinearity, reinforcing set stiffness, the angles of laying the reinforcement on critical loads of shell buckling and weight efficiency of applying the composite materials, is determined.

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Publication Details

Journal
Russian Aeronautics
Published
2024-12-01
DOI
https://doi.org/10.3103/s1068799824040044
Primary Topic
Structural Analysis and Optimization
Type
article
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article

Weight Efficiency of Anisogrid Circular Cylindrical Shells in Transverse Bending

L. P. Zheleznov
Russian Aeronautics
Structural Analysis and Optimization
article

Weight Efficiency of Anisogrid Circular Cylindrical Shells in Transverse Bending

L. P. Zheleznov
article en

Abstract

The research results are obtained on the basis of a technique implementing the finite element method for solving the problems of strength and stability of reinforced cylindrical shells made of the composite material, taking into account the momentness and nonlinearity of their subcritical stress-strain state. The stability of an anisogrid circular cylindrical shell made of a composite material under transverse bending is investigated. The effect of deformation nonlinearity, reinforcing set stiffness, the angles of laying the reinforcement on critical loads of shell buckling and weight efficiency of applying the composite materials, is determined.

Russian AeronauticsVol. 67(4)
Siberian Aeronautical Research Institute Named After S.A. Chaplygin (RU)
Openalex Percentile: Top 68%
Structural Analysis and Optimization
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