Ballistic damage in hybrid composite laminates

被引:2
|
作者
Phadnis, Vaibhav A. [1 ]
Pandya, Kedar S. [2 ]
Naik, Niranjan K. [3 ]
Roy, Anish [4 ]
Silberschmidt, Vadim V. [4 ]
机构
[1] Univ Sheffield, AMRC Boeing, Composite Ctr, Sheffield S60 5TZ, S Yorkshire, England
[2] Univ Cambridge, Dept Engn, Cambridge CB2 1TN, England
[3] Indian Inst Technol, Dept Aerosp Engn, Bombay 400076, Maharashtra, India
[4] Univ Loughborough, Wolfson Sch Mech & Mfg Engn, Loughborough LE11 3TU, Leics, England
关键词
THICK COMPOSITES; IMPACT BEHAVIOR;
D O I
10.1088/1742-6596/628/1/012092
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
Ballistic damage of hybrid woven-fabric composites made of plain-weave E-glass-fabric/epoxy and 8H satin-weave T300 carbon-fabric/epoxy is studied using a combination of experimental tests, microstructural studies and finite-element (FE) analysis Ballistic tests were conducted with a single-stage gas gun. Fibre damage and delamination were observed to be dominating failure modes. A ply-level FE model was developed, with a fabric-reinforced ply modelled as a homogeneous orthotropic material with capacity to sustain progressive stiffness degradation due to fibre/matrix cracking, fibre breaking and plastic deformation under shear loading. Simulated damage patterns on the front and back faces of fabric-reinforced composite plates provided an insight into their damage mechanisms under ballistic loading.
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页数:8
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