Anisogrid composite lattice structures – Development and aerospace applications

Vasiliev, Valery V.; Barynin, V.A.; Razin, A. F.

doi:10.1016/j.compstruct.2011.10.023

Cited by 352 publications

(114 citation statements)

References 12 publications

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“…These structures demonstrate enhanced properties of strength and stiffness and have significant potential in the field of construction of rockets and spacecrafts, aircrafts and deep-diving vehicles, buildings and high-duty structures [1].…”

Section: Introductionmentioning

confidence: 99%

Calculation and design of lattice cylindrical shells manufactured of unidirectional CFRPs

Golushko

Семисалов

2017

J. Phys.: Conf. Ser.

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Abstract. The work is devoted to numerical simulation of the stationary stress-strain state of lattice cylindrical shells made of unidirectional carbon fiber reinforced plastics and to their optimal design. After averaging stiffness characteristics of lattice structure, the displacement and stress formulations for continuum anisotropic equivalents of lattice shells are given on the basis of classical relations of 3D theory of elasticity. While using a special fast pseudo-spectral algorithm, the solutions to problems of axial compression of anisogrid shells are obtained and compared one to another. The algorithm provides exponential decrease of error of approximation and requires small computational resources. Using this algorithm we have found the optimal geometrical parameters of structure ensuring its bearing capacity under given non-uniform loads.

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Section: Introductionmentioning

confidence: 99%

Calculation and design of lattice cylindrical shells manufactured of unidirectional CFRPs

Golushko

Семисалов

2017

J. Phys.: Conf. Ser.

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“…They are characterized by high specific strength and stiffness, making them promising for lightweight applications. The history and development of this kind of structures can be found in literature, mostly published by Vasiliev et al [1][2][3][4][5].…”

Section: Introductionmentioning

confidence: 99%

“…Despite the aforementioned developments in designing composite lattice structures, their application is still limited in some spacecraft applications [3,21].…”

Section: Introductionmentioning

confidence: 99%

The Buckling Response of Lattice Fuselage Structures: Validation of Finite Element Models by Using Smeared Unit Cell Analytical Methodology

Kostopoulos¹,

Κοτζακόλιος²,

De³

2017

J Aeronaut Aerospace Eng

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Composite lattice structures are shells that are reinforced by unidirectional helical and hoop ribs. Their main advantage over contemporary composite structures is their superior stiffness to mass ratio. However, their application in industry is still limited. In this paper, the lattice structure concept was applied for the case of a small business aircraft. Emphasis here is given at the initial stages of the design. More specifically, the buckling modes for bending loads were calculated by utilizing a continum unit cell model which was correlated with finite element models for a cylindrical small fuselage structure and two scaled down versions.

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“…Carbon composite materials combined with lattice structures for the next generation fuselage design have the potential to fulfill these requirements. This novel design of a lattice composite fuselage has been investigated recently for a new weight-efficient composite fuselage section [1].…”

Section: Introductionmentioning

confidence: 99%

Metamodels for Composite Lattice Fuselage Design

Liu¹,

Zhou²,

Toropov³

2015

IJMMM

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Abstract-This paper presents a novel design of an anisogrid composite aircraft fuselage by a global metamodel-based optimization approach. A 101-point design of numerical experiments (DOE) has been developed to generate a set of individual fuselage barrel designs and these designs have further been analyzed by the finite element (FE) method. Using these training data, global metamodels of all structural responses of interest have been built as explicit expressions of the design variables using a Genetic Programming approach. Finally, the parametric optimization of the fuselage barrel by genetic algorithm (GA) has been performed to obtain the best design configuration in terms of weight savings subject to stability, global stiffness and strain requirements.Index Terms-Composite fuselage structure, anisogrid design, genetic programming, metamodel.

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Anisogrid composite lattice structures – Development and aerospace applications

Cited by 352 publications

References 12 publications

Calculation and design of lattice cylindrical shells manufactured of unidirectional CFRPs

Calculation and design of lattice cylindrical shells manufactured of unidirectional CFRPs

The Buckling Response of Lattice Fuselage Structures: Validation of Finite Element Models by Using Smeared Unit Cell Analytical Methodology

Metamodels for Composite Lattice Fuselage Design

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