Effect of Laminate Properties on the Failure of Cross Arm Structure under Multi-Axial Load

Daud Mohamad, Agusril Syamsir, Salmia Beddu, Nur Liyana Mohd Kamal, M. M. Zainoodin, M. F. Razali, A. Abas, S. A.H.A. Seman, F. C. Ng

Research output: Contribution to journalConference article

Abstract

This study investigated the influence of laminate properties toward the collapse of composite cross arm structure under multi-axial quasi-static loading. A three-dimensional finite-element model of a cross arm was developed and integrated with Hashin's failure subroutine to predict the inter-laminar damages of the composite upon its application. The mechanical deformation and failure of the composite structure were evaluated over three laminate properties. This investigation revealed that variation in laminates properties yielded different structural deflection and laminate damages. The cross arm with a greater young modulus and ultimate stresses (laminate B) experienced a single failure mode of fiber buckling in compression at deflection of 0.082 m. For the given multi-axial load, the laminate configuration and properties considered in this study failed to prevent the failure of the cross arm.

Original languageEnglish
Article number012029
JournalIOP Conference Series: Materials Science and Engineering
Volume530
Issue number1
DOIs
Publication statusPublished - 01 Jan 2019
EventInternational Conference on Recent Advances on Industrial Engineering and Manufacturing 2018, ICRAIEM 2018 - Penang, Malaysia
Duration: 12 Dec 201813 Dec 2018

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Axial loads
Laminates
Subroutines
Composite materials
Composite structures
Failure modes
Buckling
Compaction
Elastic moduli
Fibers

All Science Journal Classification (ASJC) codes

  • Materials Science(all)
  • Engineering(all)

Cite this

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title = "Effect of Laminate Properties on the Failure of Cross Arm Structure under Multi-Axial Load",
abstract = "This study investigated the influence of laminate properties toward the collapse of composite cross arm structure under multi-axial quasi-static loading. A three-dimensional finite-element model of a cross arm was developed and integrated with Hashin's failure subroutine to predict the inter-laminar damages of the composite upon its application. The mechanical deformation and failure of the composite structure were evaluated over three laminate properties. This investigation revealed that variation in laminates properties yielded different structural deflection and laminate damages. The cross arm with a greater young modulus and ultimate stresses (laminate B) experienced a single failure mode of fiber buckling in compression at deflection of 0.082 m. For the given multi-axial load, the laminate configuration and properties considered in this study failed to prevent the failure of the cross arm.",
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Effect of Laminate Properties on the Failure of Cross Arm Structure under Multi-Axial Load. / Mohamad, Daud; Syamsir, Agusril; Beddu, Salmia; Mohd Kamal, Nur Liyana; Zainoodin, M. M.; Razali, M. F.; Abas, A.; Seman, S. A.H.A.; Ng, F. C.

In: IOP Conference Series: Materials Science and Engineering, Vol. 530, No. 1, 012029, 01.01.2019.

Research output: Contribution to journalConference article

TY - JOUR

T1 - Effect of Laminate Properties on the Failure of Cross Arm Structure under Multi-Axial Load

AU - Mohamad, Daud

AU - Syamsir, Agusril

AU - Beddu, Salmia

AU - Mohd Kamal, Nur Liyana

AU - Zainoodin, M. M.

AU - Razali, M. F.

AU - Abas, A.

AU - Seman, S. A.H.A.

AU - Ng, F. C.

PY - 2019/1/1

Y1 - 2019/1/1

N2 - This study investigated the influence of laminate properties toward the collapse of composite cross arm structure under multi-axial quasi-static loading. A three-dimensional finite-element model of a cross arm was developed and integrated with Hashin's failure subroutine to predict the inter-laminar damages of the composite upon its application. The mechanical deformation and failure of the composite structure were evaluated over three laminate properties. This investigation revealed that variation in laminates properties yielded different structural deflection and laminate damages. The cross arm with a greater young modulus and ultimate stresses (laminate B) experienced a single failure mode of fiber buckling in compression at deflection of 0.082 m. For the given multi-axial load, the laminate configuration and properties considered in this study failed to prevent the failure of the cross arm.

AB - This study investigated the influence of laminate properties toward the collapse of composite cross arm structure under multi-axial quasi-static loading. A three-dimensional finite-element model of a cross arm was developed and integrated with Hashin's failure subroutine to predict the inter-laminar damages of the composite upon its application. The mechanical deformation and failure of the composite structure were evaluated over three laminate properties. This investigation revealed that variation in laminates properties yielded different structural deflection and laminate damages. The cross arm with a greater young modulus and ultimate stresses (laminate B) experienced a single failure mode of fiber buckling in compression at deflection of 0.082 m. For the given multi-axial load, the laminate configuration and properties considered in this study failed to prevent the failure of the cross arm.

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