G
Gin Boay Chai
Researcher at Nanyang Technological University
Publications - 67
Citations - 2022
Gin Boay Chai is an academic researcher from Nanyang Technological University. The author has contributed to research in topics: Buckling & Finite element method. The author has an hindex of 20, co-authored 64 publications receiving 1636 citations.
Papers
More filters
Journal ArticleDOI
Low velocity impact response of fibre-metal laminates – A review
TL;DR: A comprehensive review of past and current research work published on the dynamic response of fiber-metal laminates subjected to low velocity impact is given in this paper, which concludes with detailed discussions on the future works needed for fibre-metal Laminates.
Journal ArticleDOI
Mechanical properties of Nomex material and Nomex honeycomb structure
TL;DR: In this paper, extensive test results of linear elastic mechanical properties of Nomex paper and nomex honeycomb structures are presented, which are then used in the finite element modeling and analysis of NOMEX honeycomb structure.
Journal ArticleDOI
A model to predict low-velocity impact response and damage in sandwich composites
TL;DR: In this paper, a modified energy-balance model coupled with the law of conservation of momentum is proposed to extend the validity of elastic impact models beyond the elastic regime, and three parameters were derived from the static load-deformation response: the elastic stiffness, the critical load at the onset of damage, and the damaged stiffness.
Journal ArticleDOI
A review of low-velocity impact on sandwich structures
Gin Boay Chai,Shengqing Zhu +1 more
TL;DR: In this paper, a review of past and current research progress on dynamic response of composites sandwich structures subjected to low-velocity impact is provided and described in some details, including a summary of some commonly used theoretical solutions.
Journal ArticleDOI
Low-velocity impact failure of aluminium honeycomb sandwich panels
TL;DR: In this article, the failure response of aluminium sandwich panels subjected to low-velocity impact is discussed and a three-dimensional geometrically correct finite element model of the honeycomb sandwich plate and a rigid impactor is developed using the commercial software, ABAQUS.