Mechanical characterization of 3D angle-interlock Kevlar/basalt reinforced polypropylene composites

• Published in: Polymer testing Vol. 55; pp. 238 - 246
• Main Authors: Bandaru, Aswani Kumar, Patel, Shivdayal, Sachan, Yogesh, Ahmad, Suhail, Alagirusamy, R., Bhatnagar, Naresh
• Format: Journal Article
• Language: English
• Published: Barking Elsevier Ltd 01.10.2016; Elsevier BV
• Subjects: 3-D technology; 3D fabrics; Aramid fiber reinforced plastics; Basalt; Compression tests; Computer simulation; Cracking (fracturing); Damage assessment; Damage patterns; Deformation; Fabrics; Finite element method; Fracture mechanics; Hybrid; Kevlar; Kevlar (trademark); Mechanical behavior; Mechanical properties; Modulus of elasticity; Polymer matrix composites; Polypropylene; Pressure molding; Strain; Textile composites; Three dimensional composites; Yarns; Hybrid; Basalt; Mechanical behavior; Kevlar; Polypropylene; 3D fabrics
• ISSN: 0142-9418; 1873-2348
• DOI: 10.1016/j.polymertesting.2016.08.024

The present work reported the mechanical characterization of novel polypropylene (PP) composites reinforced with three-dimensional angle-interlock (3D-A) Kevlar/basalt fabrics. Two homogeneous fabrics with Kevlar (K3D) and basalt yarns (B3D), and a hybrid fabric (H3D) with a combination of both Kevlar and basalt yarns were produced. Three types of two layer 3D-A composites were manufactured using vacuum-assisted compression molding method. Static tensile and in-plane compression tests were carried out on the manufactured composites. The mechanical behavior of the three 3D-A composites was compared in terms of stress-strain response, elastic modulus, strength and failure strain. Influence of hybridization on the mechanical behavior of the 3D-A composites was also studied. Significant improvement in the tensile behavior of 3D-A homogeneous composites was observed due to hybridization. Meanwhile, there was no considerable improvement in in-plane compression behavior. The damage patterns for in-plane compression loading were examined through scanning electron microscopy (SEM) to explore the possible damage patterns such as matrix cracking, fiber failure, delamination and deformation. Numerical simulations were carried out using ABAQUS/Standard, by implementing a user-defined material subroutine (VUMAT) based on the Chang-Chang linear orthotropic damage model. Good agreement between experimental and numerical simulations was achieved in terms of damage patterns.