High-velocity impact behaviour of aluminium honeycomb sandwich panels with different structural configurations

2018 ◽  
Vol 122 ◽  
pp. 119-136 ◽  
Author(s):  
Guangyong Sun ◽  
Dongdong Chen ◽  
Hongxu Wang ◽  
Paul J. Hazell ◽  
Qing Li
2020 ◽  
Vol 29 (8) ◽  
pp. 707-721
Author(s):  
Fatemeh Hassanpour Roudbeneh ◽  
Gholamhossein Liaghat ◽  
Hadi Sabouri ◽  
Homayoun Hadavinia

2018 ◽  
Vol 138 ◽  
pp. 1-11 ◽  
Author(s):  
W.H. Xie ◽  
S.H. Meng ◽  
L. Ding ◽  
H. Jin ◽  
S.Y. Du ◽  
...  

2020 ◽  
Vol 248 ◽  
pp. 112520 ◽  
Author(s):  
I. Ivañez ◽  
S. Sánchez-Saez ◽  
S.K. Garcia-Castillo ◽  
E. Barbero ◽  
A. Amaro ◽  
...  

2012 ◽  
Vol 450-451 ◽  
pp. 563-567 ◽  
Author(s):  
Joel Bell ◽  
Yi Xia Zhang ◽  
Khin Soe ◽  
Phillip Hermes

High-velocity impact behaviour of hybrid-fibre engineered cementitious composite (ECC) panels subjected to an impact from a hardened steel, ogive-nosed projectile at velocities between 300-700 m/s is investigated and reported in this paper. The new ECC mix contains a proportion of 0.75% volume high-modulus steel fibres and 1.25% volume low modulus polyvinyl-alcohol (PVA) fibres. The mix is designed to achieve a desired balance between the strain hardening behaviour and impact resistance of material required for impact and blast resistant structures. The new hybrid-fibre ECC demonstrates its excellent capability for impact resistance and strong potential as a protective material with reduced impact damage and distributed micro cracking.


2021 ◽  
pp. 107348
Author(s):  
Hongxu Wang ◽  
Caizheng Wang ◽  
Paul J. Hazell ◽  
Ashleigh Wright ◽  
Zhifang Zhang ◽  
...  

2016 ◽  
Vol 852 ◽  
pp. 66-71 ◽  
Author(s):  
M. Nalla Mohamed ◽  
D. Ananthapadmanaban ◽  
M. Selvaraj

Sandwich structures based on Fibre Reinforced Polymer (FRP) facesheet skins bonded with low density aluminium foam core are increasing in use in aerospace and marine industries. These structures are very sensitive to high velocity impact during the service. Therefore, it is necessary to study the energy absorption of the structures to ensure the reliability and safety in use. Experimental investigation of these transient events is expensive and time-consuming, and nowadays the use of numerical approaches is on the increase. Hence, the purpose of this paper is to develop a numerical model of sandwich panels with aluminium foam as a core and Glass, Carbon and Kevlar Fibre Reinforced polymer composite as faceplate, subjected to high velocity impact using ABAQUS/Explicit. The influence of individual elements of the sandwich panel on the energy absorption of the structures subjected to high velocity impact loading was analysed. Selection of suitable constitutive models and erosion criterion for the damage were discussed. The numerical models were validated with experimental data obtained from the scientific literature. Good agreement was obtained between the simulations and the experimental results. The contribution of the face sheet, foam core on the impact behaviour was evaluated by the analysis of the residual velocity, ballistic limit, and damaged area.


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