Finite element analysis of sandwich panels with stepwise graded aluminum honeycomb cores under blast loading. (January 2016)

• Record Type: Journal Article
• Authors: Li, Shiqiang; Li, Xin; Wang, Zhihua; Wu, Guiying; Lu, Guoxing; Zhao, Longmao
• Is Part Of: Composites. Volume 80(2016)
• Page Start: 1
• Page End: 12
• Publication Date: 2016-01
• Subjects: A. Honeycomb -- Sandwich structures -- B. Plastic deformation -- C. Finite element analysis (FEA); Composite materials -- Periodicals; Manufacturing processes -- Periodicals; Composite materials; Manufacturing processes; Periodicals; 620.11805
• DOI: 10.1016/j.compositesa.2015.09.025
• Languages: English
• ISSNs: 1359-835X

Abstract

Abstract: This paper presents details and brief results of an experimental investigation on the response of metallic sandwich panels with stepwise graded aluminum honeycomb cores under blast loading. Based on the experiments, corresponding finite element simulations have been undertaken using the LS-DYNA software. It is observed that the core compression stage was coupled with the fluid–structure interaction stage, and the compression of the core layer decreased from the central to the peripheral zone. The blast resistance capability of sandwich panels was moderately sensitive to the core relative density and graded distribution. For the graded panels with relative density descending core arrangement, the core plastic energy dissipation and the transmitted force attenuation were larger than that of the ungraded ones under the same loading condition. The graded sandwich panels, especially for relative density descending core arrangement, would display a better blast resistance than the ungraded ones at a specific loading region.