Evaluation of crush and energy absorption characteristics of corrugated origami tube by additive manufacturing DOI

Xudong Sun,

Zhiyu Jiang, Jian Zhao

et al.

Polymer Composites, Journal Year: 2024, Volume and Issue: unknown

Published: Nov. 23, 2024

Abstract Origami tube (OT) has attracted significant attention in the realm of thin‐walled structures owing to their remarkable energy‐absorption capabilities. Nevertheless, deformation modes, particularly buckling, present considerable stability challenges. In this research, we introduce a novel corrugated structure enhance energy absorption and stabilize mode OT. The origami (COT) was manufactured using high‐specific modulus, high‐strength, lightweight short carbon fiber‐reinforced nylon via 3D printing, followed by axial quasi‐static compression tests. findings demonstrate that incorporation corrugations COT greatly stabilizes deformation, boosting 21.3% compared OT reducing peak crashworthiness force up 21.37%. Finite element analysis accurately replicates experimental performance COT, affirming feasibility simulation. Optimization Non‐dominated Sorting Genetic Algorithm II (NSGA‐II) produced Pareto front, revealing trade‐offs among various indicators offering flexible design approach meet diverse requirements. This study provides valuable insights guidance for lightweight, structures. Highlights effectively significantly improves reduces initial multi‐objective optimization variety solutions different needs.

Language: Английский

Out-of-plane energy absorption of 3D printed basalt-fiber-reinforced hierarchical honeycomb composite DOI
Luqing Hua,

Lining Ding,

Xin Wang

et al.

International Journal of Mechanical Sciences, Journal Year: 2024, Volume and Issue: unknown, P. 109784 - 109784

Published: Oct. 1, 2024

Language: Английский

Citations

6

Compressive properties of aperiodic but ordered cellular materials inspired by Penrose tilings DOI
Qi Ge,

Tian JiJing,

Chenxi Liu

et al.

Thin-Walled Structures, Journal Year: 2024, Volume and Issue: 204, P. 112287 - 112287

Published: July 31, 2024

Language: Английский

Citations

4

Programmable mechanical responses of a hybrid star-rhombus honeycomb based on digital design method DOI
Shun Wang, Hai‐Tao Liu,

Guangbin Cai

et al.

Thin-Walled Structures, Journal Year: 2024, Volume and Issue: 205, P. 112399 - 112399

Published: Sept. 3, 2024

Language: Английский

Citations

4

Monotonic and cyclic compressive performance of self-monitoring MWCNT/PA12 cellular composites manufactured by selective laser sintering DOI Creative Commons
Muhammad Umar Azam, S. Kumar, Andreas Schiffer

et al.

Composites Part C Open Access, Journal Year: 2025, Volume and Issue: 16, P. 100566 - 100566

Published: Jan. 29, 2025

Language: Английский

Citations

0

Quasi-static and dynamic response of open lattice structures for enhanced plateau stresses: simulation and experiment validation DOI
Dara Ashok,

A. Johnney Mertens,

Gunji Bala Murali

et al.

Materials Today Communications, Journal Year: 2025, Volume and Issue: unknown, P. 111953 - 111953

Published: Feb. 1, 2025

Language: Английский

Citations

0

Energy absorption of auxetic honeycomb with graded beam thickness based on Bezier curve DOI

Jianzhong Zhou,

Yifan Wang,

Huichen Luo

et al.

Aerospace Science and Technology, Journal Year: 2024, Volume and Issue: unknown, P. 109619 - 109619

Published: Sept. 1, 2024

Language: Английский

Citations

1

Experimental analysis of quasi‐static indentation in composite sandwich multilayers with corrugated core DOI

Benyamin Vahidimanesh,

Mohammad Sajjad Gazor, Amin Farrokhabadi

et al.

Polymer Composites, Journal Year: 2024, Volume and Issue: unknown

Published: Oct. 1, 2024

Abstract This study examines the effects of multilayering in sandwich panel composite structures with different corrugated core configurations under quasi‐static indentation loading. The panels were fabricated using woven glass fibers and epoxy resin via Vacuum Infusion Process. Experiments conducted two hemispherical cylindrical indenters a diameter 20 mm (ID = mm) 10 behavior structure terms contact force fracture mechanisms for corrugations (square butterfly) investigated ways foam without foam. experimental results demonstrate that, among geometries foam, butterfly cores outperform square structural strength, maximum force, moment energy absorption, specific displacement until full indentation. Moreover, shows higher peak load failure compared to core. Under loading indenter, only experienced perforation area, completely. Also, adding did not change mechanical geometry. However, geometry, filled gaps between core, preventing completely leading unlike specimen visual analysis during process revealed several significant damage mechanisms, including matrix cracking, fiber breakage, delamination, buckling crushing cell walls, top sheets, separation, complete samples. Highlights Delamination seen on Skin rib Butterfly best performance without/with shape was more effective strength than addition.

Language: Английский

Citations

1

A Review of Structural Health Monitoring for Flexible Composite Materials DOI

Xiangli Hu,

Jiangxing Wu, Yantao Gao

et al.

Applied Composite Materials, Journal Year: 2024, Volume and Issue: unknown

Published: Nov. 16, 2024

Language: Английский

Citations

1

Compressive and flexural properties and damage modes of aluminum foam/epoxy resin interpenetrating phase composites reinforced by silica powder DOI
Mingming Su, Zhiming Zhou, Han Wang

et al.

Polymer Composites, Journal Year: 2024, Volume and Issue: unknown

Published: Sept. 17, 2024

Abstract Interpenetrating phase composites (IPCs) can combine the advantages of each component and have a good application prospect. IPCs were prepared by combining open‐cell aluminum foam (AF) epoxy resin (EP) in three‐dimensional space this study. Different contents silica powder (SP, 80, 100, 120, 140 wt%) added to EP improve compressive three‐point bending properties IPCs. In test, acoustic emission (AE) was applied track deformation samples, k ‐means clustering algorithm identify damage modes. The increased first then decreased with increase SP content, reached maximum when content 100 wt%, yield strength 74.6 MPa peak load 1.96 kN. performance degradation mainly attributed AF/EP debonding due distribution at interface. X‐type shear band EP/AF appeared compression failures AF IPCs, respectively. AE results showed that under load, plastic matrix (60–200 kHz) fracture failure (230–340 modes AF, while (60–120 kHz), (120–230 (230–250 Highlights Silica Acoustic used monitor firstly. classify patterns.

Language: Английский

Citations

0

Mechanical properties of phenolic foam composite meta-aramid honeycomb under various directional loads and thermal environments DOI
Hao Wang, Suchao Xie, Kunkun Jing

et al.

Mechanics of Advanced Materials and Structures, Journal Year: 2024, Volume and Issue: unknown, P. 1 - 18

Published: Nov. 13, 2024

To enhance the mechanical properties of honeycomb structures, a phenolic foam composite meta-aramid core (PFAH) was developed. Experimental, simulation, and theoretical analyses revealed that PFAH increased out-of-plane energy absorption by 89.47% without altering specific aramid honeycomb, maintaining smooth plastic deformation. At 150 °C, it retained 90.7% properties. In in-plane direction, PF raised plateau stress 798.73%. The study identified critical spinodal for off-axis angle deformation modes established relationship between strength angle, demonstrating superior resistance to shallow-angle oblique loading compared unfilled honeycomb.

Language: Английский

Citations

0