Research Article

Experimental Analysis and Finite Element Modeling of S-Core Sandwich Panel Composites Drop Impact Response

Volume: 15 Number: 1 March 29, 2024
TR EN

Experimental Analysis and Finite Element Modeling of S-Core Sandwich Panel Composites Drop Impact Response

Abstract

Sandwich panel composites have several applications in material technology. The sandwich panel composite material is constructed of stainless steel-316 for the top and bottom plates, aluminum 1050A-0 for the core, and DP-8405 acrylic adhesive for the binding element. The impact behavior of S-core composite sandwich panels was examined using low-velocity drop impact tests and finite element models. Finite element models have been created to characterize the influence of composite element bending behavior on variations. The specific flexural modulus and strength of composite S-core sandwich structures are equivalent to those found in the literature for core structures. As a result, the minimum weight design served as a guideline for producing weight and density-efficient hybrid composite sandwich panels. The energy absorbed in the test findings rose between 15.15% and 30% as the core thickness grew and between 3.571% and 41.34% as the core arrays changed. Impact load-bearing capability increases with varied core heights and array designs.

Keywords

Supporting Institution

Inonu University

Project Number

BAP Project Code: FDK-2020-2306

Thanks

The authors thank Inonu University for funding the project.

References

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Details

Primary Language

English

Subjects

Material Design and Behaviors

Journal Section

Research Article

Early Pub Date

March 29, 2024

Publication Date

March 29, 2024

Submission Date

September 25, 2023

Acceptance Date

January 15, 2024

Published in Issue

Year 2024 Volume: 15 Number: 1

IEEE
[1]H. M. Öztemiz and Ş. Temiz, “Experimental Analysis and Finite Element Modeling of S-Core Sandwich Panel Composites Drop Impact Response”, DUJE, vol. 15, no. 1, pp. 131–139, Mar. 2024, doi: 10.24012/dumf.1365978.