Numerical study of low-speed impact response of sandwich panel with tube filled honeycomb core

© 2019 Elsevier Ltd Sandwich panel with Honeycomb Filled with Circular Tubes (HFCT) as core is numerically investigated by using ABAQUS/Explicit in this study. To calibrate the numerical model, the panels equipped with conventional hexagon honeycomb cores are modeled. Good agreement between numerica...

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Main Authors: Liu, J., Chen, Wensu, Hao, Hong, Wang, Z.
Format: Journal Article
Language:English
Published: ELSEVIER SCI LTD 2019
Subjects:
Online Access:http://purl.org/au-research/grants/arc/DE160101116
http://hdl.handle.net/20.500.11937/91682
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author Liu, J.
Chen, Wensu
Hao, Hong
Wang, Z.
author_facet Liu, J.
Chen, Wensu
Hao, Hong
Wang, Z.
author_sort Liu, J.
building Curtin Institutional Repository
collection Online Access
description © 2019 Elsevier Ltd Sandwich panel with Honeycomb Filled with Circular Tubes (HFCT) as core is numerically investigated by using ABAQUS/Explicit in this study. To calibrate the numerical model, the panels equipped with conventional hexagon honeycomb cores are modeled. Good agreement between numerical and experimental results is achieved. The sandwich panels with HFCT are compared with the sandwich panels with Honeycomb and Multi-tube cores of identical mass subjected to vertical and oblique impacts. The maximum displacement of face-sheets, plastic energy absorption, boundary reaction forces and impact load time history are calculated to assess the impact resistant capacity. The panel with HFCT core has smaller rear face-sheet displacement and higher energy absorption capacity as compared to the panels with the Multi-tube and Honeycomb core. Under oblique impact, both HFCT and Multi-tube panels have superior impact resistant capacity than the Honeycomb panel. In addition, the impact resistances of four types of multi-arc tube filled Honeycomb (HFMT) are also analysed. Their performances under vertical and oblique impacts are compared with those of HFCT.
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institution Curtin University Malaysia
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publishDate 2019
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spelling curtin-20.500.11937-916822023-05-23T08:00:14Z Numerical study of low-speed impact response of sandwich panel with tube filled honeycomb core Liu, J. Chen, Wensu Hao, Hong Wang, Z. Science & Technology Technology Mechanics Materials Science, Composites Materials Science Sandwich panel Filled honeycomb Interaction Oblique impact Finite element analysis STRUCTURAL INSULATED PANEL MECHANICAL PERFORMANCE BENDING BEHAVIOR BLAST-RESISTANCE ALUMINUM TUBES PART 2 SIMULATION COMPRESSION LIGHTWEIGHT STRENGTH © 2019 Elsevier Ltd Sandwich panel with Honeycomb Filled with Circular Tubes (HFCT) as core is numerically investigated by using ABAQUS/Explicit in this study. To calibrate the numerical model, the panels equipped with conventional hexagon honeycomb cores are modeled. Good agreement between numerical and experimental results is achieved. The sandwich panels with HFCT are compared with the sandwich panels with Honeycomb and Multi-tube cores of identical mass subjected to vertical and oblique impacts. The maximum displacement of face-sheets, plastic energy absorption, boundary reaction forces and impact load time history are calculated to assess the impact resistant capacity. The panel with HFCT core has smaller rear face-sheet displacement and higher energy absorption capacity as compared to the panels with the Multi-tube and Honeycomb core. Under oblique impact, both HFCT and Multi-tube panels have superior impact resistant capacity than the Honeycomb panel. In addition, the impact resistances of four types of multi-arc tube filled Honeycomb (HFMT) are also analysed. Their performances under vertical and oblique impacts are compared with those of HFCT. 2019 Journal Article http://hdl.handle.net/20.500.11937/91682 10.1016/j.compstruct.2019.04.023 English http://purl.org/au-research/grants/arc/DE160101116 ELSEVIER SCI LTD restricted
spellingShingle Science & Technology
Technology
Mechanics
Materials Science, Composites
Materials Science
Sandwich panel
Filled honeycomb
Interaction
Oblique impact
Finite element analysis
STRUCTURAL INSULATED PANEL
MECHANICAL PERFORMANCE
BENDING BEHAVIOR
BLAST-RESISTANCE
ALUMINUM TUBES
PART 2
SIMULATION
COMPRESSION
LIGHTWEIGHT
STRENGTH
Liu, J.
Chen, Wensu
Hao, Hong
Wang, Z.
Numerical study of low-speed impact response of sandwich panel with tube filled honeycomb core
title Numerical study of low-speed impact response of sandwich panel with tube filled honeycomb core
title_full Numerical study of low-speed impact response of sandwich panel with tube filled honeycomb core
title_fullStr Numerical study of low-speed impact response of sandwich panel with tube filled honeycomb core
title_full_unstemmed Numerical study of low-speed impact response of sandwich panel with tube filled honeycomb core
title_short Numerical study of low-speed impact response of sandwich panel with tube filled honeycomb core
title_sort numerical study of low-speed impact response of sandwich panel with tube filled honeycomb core
topic Science & Technology
Technology
Mechanics
Materials Science, Composites
Materials Science
Sandwich panel
Filled honeycomb
Interaction
Oblique impact
Finite element analysis
STRUCTURAL INSULATED PANEL
MECHANICAL PERFORMANCE
BENDING BEHAVIOR
BLAST-RESISTANCE
ALUMINUM TUBES
PART 2
SIMULATION
COMPRESSION
LIGHTWEIGHT
STRENGTH
url http://purl.org/au-research/grants/arc/DE160101116
http://hdl.handle.net/20.500.11937/91682