Failure Analysis of Composite Laminates Under Biaxial Tensile Load Due To Variations in Lamination Scheme / Mohamad Mali ... [et al.]

Mali, Mohamad and Samsudin, Azizul Hakim and Mahmud, Jamaluddin and Hussain, Ahmad Kamil (2017) Failure Analysis of Composite Laminates Under Biaxial Tensile Load Due To Variations in Lamination Scheme / Mohamad Mali ... [et al.]. Journal of Mechanical Engineering (JMechE), SI 4 (5). pp. 167-182. ISSN 18235514

Abstract

Due to its variability in mechanical properties and complex anisotropy behaviour, the work related to the design and analysis of composite laminates or composite structures is complicated yet crucial. At present, the analytical and finite element simulation techniques are the more preferred methods than the tedious and costly physical testing procedures. Unfortunately, even after many research works have been conducted, there is still a lack of understanding in relation to the failure behaviour of composite laminates under the effect of biaxial load. This paper investigates the failure behaviour of fibre-reinforced composite laminates under biaxial tensile load due to variations in lamination scheme by comparing results obtained from analytical approach and finite element simulation. Failures in the laminates follow Maximum stress and Tsai-Wu criteria based on FSDT. The analytical approach was developed based on the CLT in which the computed strains, global stresses, principal stresses and displacements were used to predict the failure. The results from the finite element models were validated by comparing with the accepted published results. Three variations of lamination scheme; symmetric unidirectional-ply, cross-ply and angle-ply ([0/0]s & [90/90]s, [0/90]s and [+45/-45]s) were investigated. Comparison of the results obtained from the analytical and FEM were found in good agreement for all three schemes. In addition, it was found that the lamination scheme affected the failure behaviour composite laminates under the biaxial load. In conclusion, it can be concluded that the present study is useful and significant in enhancing knowledge about failure behaviour of composite laminates under biaxial tensile load.

Metadata

Item Type: Article
Creators:
CreatorsEmail / ID. Num
Mali, Mohamadutahq10@yahoo.com
Samsudin, Azizul HakimUNSPECIFIED
Mahmud, JamaluddinUNSPECIFIED
Hussain, Ahmad KamilUNSPECIFIED
Subjects: T Technology > TJ Mechanical engineering and machinery
Divisions: Universiti Teknologi MARA, Shah Alam > Faculty of Mechanical Engineering
Journal or Publication Title: Journal of Mechanical Engineering (JMechE)
Journal: UiTM Journal > Journal of Mechanical Engineering (JMechE)
ISSN: 18235514
Volume: SI 4
Number: 5
Page Range: pp. 167-182
Item ID: 39344
Uncontrolled Keywords: Composite laminates, biaxial tensile load, analytical method, ANSYS
URI: http://ir.uitm.edu.my/id/eprint/39344

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