Academic literature on the topic 'Honeycomb structures Mechanical properties'

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Journal articles on the topic "Honeycomb structures Mechanical properties"

1

Avramov, Kostiantyn V., Borys V. Uspenskyi, and Ihor I. Derevianko. "Analytical Calculation of the Mechanical Properties of Honeycombs Printed Using the FDM Additive Manufacturing Technology." Journal of Mechanical Engineering 24, no. 2 (2021): 16–23. http://dx.doi.org/10.15407/pmach2021.02.016.

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FDM 3D printed honeycombs are investigated. A honeycomb is composed of regular hexagonal cells. A honeycomb is 3D printed so that the fused filament runs along the walls of its cells. We emphasize that the thickness of these walls is one or two times the thickness of the fused filament. When calculating the mechanical properties of a honeycomb, its walls are considered as a Euler-Bernoulli beam bending in one plane. To describe honeycombs, a homogenization procedure is used, which reduces a honeycomb to a homogeneous orthotropic medium. An adequate analytical calculation of the mechanical prop
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2

Zhu, Xuefeng, Longkun Xu, Xiaochen Liu, Jinting Xu, Ping Hu, and Zheng-Dong Ma. "Theoretical prediction of mechanical properties of 3D printed Kagome honeycombs and its experimental evaluation." Proceedings of the Institution of Mechanical Engineers, Part C: Journal of Mechanical Engineering Science 233, no. 18 (2019): 6559–76. http://dx.doi.org/10.1177/0954406219860538.

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Kagome honeycomb structure is proved to incorporate excellent mechanical and actuation performances due to its special configuration. However, until now, the mechanical properties of 3D printed Kagome honeycomb have not been investigated. Hence, the objective of this work is to explore some mechanical properties of 3D-printed Kagome honeycomb structures such as elastic properties, buckling, and so on. In this paper, the analytical formulas of some mechanical properties of Kagome honeycombs made of 3D-printed materials are given. Effective elastic moduli such as Young's modulus, shear modulus,
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3

Wang, A. J., and D. L. McDowell. "In-Plane Stiffness and Yield Strength of Periodic Metal Honeycombs." Journal of Engineering Materials and Technology 126, no. 2 (2004): 137–56. http://dx.doi.org/10.1115/1.1646165.

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In-plane mechanical properties of periodic honeycomb structures with seven different cell types are investigated in this paper. Emphasis is placed on honeycombs with relative density between 0.1 and 0.3, such that initial yield is associated with short column compression or bending, occurring prior to elastic buckling. Effective elastic stiffness and initial yield strength of these metal honeycombs under in-plane compression, shear, and diagonal compression (for cell structures that manifest in-plane anisotropy) are reported as functions of relative density. Comparison among different honeycom
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4

Xie, Lu, Tianhua Wang, Chenwei He, Zhihui Sun, and Qing Peng. "Molecular Dynamics Simulation on Mechanical and Piezoelectric Properties of Boron Nitride Honeycomb Structures." Nanomaterials 9, no. 7 (2019): 1044. http://dx.doi.org/10.3390/nano9071044.

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Boron nitride honeycomb structure is a new three-dimensional material similar to carbon honeycomb, which has attracted a great deal of attention due to its special structure and properties. In this paper, the tensile mechanical properties of boron nitride honeycomb structures in the zigzag, armchair and axial directions are studied at room temperature by using molecular dynamics simulations. Effects of temperature and strain rate on mechanical properties are also discussed. According to the observed tensile mechanical properties, the piezoelectric effect in the zigzag direction was analyzed fo
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5

Miranda, A., M. Leite, L. Reis, E. Copin, MF Vaz, and AM Deus. "Evaluation of the influence of design in the mechanical properties of honeycomb cores used in composite panels." Proceedings of the Institution of Mechanical Engineers, Part L: Journal of Materials: Design and Applications 235, no. 6 (2021): 1325–40. http://dx.doi.org/10.1177/1464420720985191.

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The aerospace, automotive, and marine industries are heavily reliant on sandwich panels with cellular material cores. Although honeycombs with hexagonal cells are the most commonly used geometries as cores, recently there have been new alternatives in the design of lightweight structures. The present work aims to evaluate the mechanical properties of metallic and polymeric honeycomb structures, with configurations recently proposed and different in-plane orientations, produced by additive and subtractive manufacturing processes. Structures with configurations such as regular hexagonal honeycom
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Spratt, Myranda, Sudharshan Anandan, Rafid Hussein, et al. "Build accuracy and compression properties of additively manufactured 304L honeycombs." Rapid Prototyping Journal 26, no. 6 (2020): 1049–57. http://dx.doi.org/10.1108/rpj-08-2018-0201.

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Purpose The purpose of this study is to analyze the build quality and compression properties of thin-walled 304L honeycomb structures manufactured by selective laser melting. Four honeycomb wall thicknesses, from 0.2 to 0.5 mm, were built and analyzed. Design/methodology/approach The density of the honeycombs was changed by increasing the wall thickness of each sample. The honeycombs were tested under compression. Differences between the computer-assisted design model and the as-built structure were quantified by measuring physical dimensions. The microstructure was evaluated by optical micros
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7

Fojtl, Ladislav, Soňa Rusnáková, and Milan Žaludek. "Influence of Honeycomb Core Compression on the Mechanical Properties of the Sandwich Structure." Applied Mechanics and Materials 486 (December 2013): 283–88. http://dx.doi.org/10.4028/www.scientific.net/amm.486.283.

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This research paper deals with an investigation of the influence of honeycomb core compression on the mechanical properties of sandwich structures. These structures consist of prepreg facing layers and two different material types of honeycomb and are produced by modified compression molding called Crush-Core technology. Produced structures are mechanically tested in three-point bending test and subjected to low-velocity impact and Charpy impact test.
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8

Xie, Zong Hong, Xiao Yu Liu, Xi Shan Yue, Qun Yan, Jun Feng Sun, and Yong Juan Jing. "Out-of-Plane Mechanical Property Test on Titanium Honeycomb Cores." Advanced Materials Research 718-720 (July 2013): 1018–23. http://dx.doi.org/10.4028/www.scientific.net/amr.718-720.1018.

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As a typical cellular solid, the honeycomb core shows an orthotropic behavior in its mechanical properties. Engineering analysis often adopts a homogeneity assumption that honeycomb core is equivalent to an anisotropic continuum. Currently available cellular solid model cannot predict the physical properties of titanium honeycomb core with acceptable accuracy. Therefore, mechanical test must be carried out to obtain the mechanical properties of metallic honeycomb structures. This paper introduces the work on flatwise compression test and out-of-plane shear test on titanium honeycomb core struc
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9

Vesenjak, Matej, Andreas Öchsner, and Zoran Ren. "Evaluation of Thermal and Mechanical Filler Gas Influence on Honeycomb Structures Behavior." Materials Science Forum 553 (August 2007): 190–95. http://dx.doi.org/10.4028/www.scientific.net/msf.553.190.

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In this paper the behavior of hexagonal honeycombs under dynamic in-plane loading is described. Additionally, the presence and influence of the filler gas inside the honeycomb cells is considered. Such structures are subjected to very large deformation during an impact, where the filler gas might strongly affect their behavior and the capability of deformational energy absorption, especially at very low relative densities. The purpose of this research was therefore to evaluate the influence of filler gas on the macroscopic cellular structure behavior under dynamic uniaxial loading conditions b
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10

Zhou, Hui, Ping Xu, and Suchao Xie. "Composite energy-absorbing structures combining thin-walled metal and honeycomb structures." Proceedings of the Institution of Mechanical Engineers, Part F: Journal of Rail and Rapid Transit 231, no. 4 (2016): 394–405. http://dx.doi.org/10.1177/0954409716631579.

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The energy-absorbing structure of a crashworthy railway vehicle was designed by combining the characteristics of thin-walled metal structures and aluminum honeycomb structures: finite element models of collisions involving energy-absorbing structures were built in ANSYS/LS-DYNA. In these models, the thin-walled metal structure was modeled as a plastic kinematic hardening material, and the honeycomb structure was modeled as an equivalent solid model with orthotropic–anisotropic mechanical properties. The analysis showed that the safe velocity standard for rail vehicle collisions was improved fr
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