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T.E. Tay (Tong-Earn Tay)
T.E. Tay (Tong-Earn Tay)
Verified email at nus.edu.sg
Title
Cited by
Cited by
Year
Characterization of a novel polymeric scaffold for potential application in tendon/ligament tissue engineering
S Sahoo, H Ouyang, JCH Goh, TE Tay, SL Toh
Tissue engineering 12 (1), 91-99, 2006
4452006
Strengthening fabric armour with silica colloidal suspensions
VBC Tan, TE Tay, WK Teo
International journal of solids and structures 42 (5-6), 1561-1576, 2005
3092005
Modelling deformation and damage characteristics of woven fabric under small projectile impact
VPW Shim, VBC Tan, TE Tay
International Journal of Impact Engineering 16 (4), 585-605, 1995
2981995
Progressive failure analysis of composites
TE Tay, G Liu, VBC Tan, XS Sun, DC Pham
Journal of Composite Materials 42 (18), 1921-1966, 2008
2832008
A floating node method for the modelling of discontinuities in composites
BY Chen, ST Pinho, NV De Carvalho, PM Baiz, TE Tay
Engineering Fracture Mechanics 127, 104-134, 2014
1922014
Numerical analysis of size effects on open-hole tensile composite laminates
BY Chen, TE Tay, PM Baiz, ST Pinho
Composites Part A: Applied Science and Manufacturing 47, 52-62, 2013
1762013
Modelling complex progressive failure in notched composite laminates with varying sizes and stacking sequences
M Ridha, CH Wang, BY Chen, TE Tay
Composites Part A: Applied Science and Manufacturing 58, 16-23, 2014
1692014
Traction–separation laws for progressive failure of bonded scarf repair of composite panel
M Ridha, VBC Tan, TE Tay
Composite structures 93 (4), 1239-1245, 2011
1662011
Effects of hybridization and hybrid fibre dispersion on the mechanical properties of woven flax-carbon epoxy at low carbon fibre volume fractions
U Kureemun, M Ravandi, LQN Tran, WS Teo, TE Tay, HP Lee
Composites Part B: Engineering 134, 28-38, 2018
1602018
Low velocity impact performance of stitched flax/epoxy composite laminates
M Ravandi, WS Teo, LQN Tran, MS Yong, TE Tay
Composites Part B: Engineering 117, 89-100, 2017
1582017
Modelling damage growth in composites subjected to impact and compression after impact
MR Abir, TE Tay, M Ridha, HP Lee
Composite Structures 168, 13-25, 2017
1402017
Damage progression by the element-failure method (EFM) and strain invariant failure theory (SIFT)
TE Tay, SHN Tan, VBC Tan, JH Gosse
Composites science and technology 65 (6), 935-944, 2005
1382005
Modeling delamination growth in laminated composites
F Shen, KH Lee, TE Tay
Composites Science and Technology 61 (9), 1239-1251, 2001
1172001
On cohesive element parameters and delamination modelling
X Lu, M Ridha, BY Chen, VBC Tan, TE Tay
Engineering Fracture Mechanics 206, 278-296, 2019
1152019
The effects of through-the-thickness stitching on the Mode I interlaminar fracture toughness of flax/epoxy composite laminates
M Ravandi, WS Teo, LQN Tran, MS Yong, TE Tay
Materials & Design 109, 659-669, 2016
1142016
An empirical strain rate-dependent constitutive relationship for glass-fibre reinforced epoxy and pure epoxy
TE Tay, HG Ang, VPW Shim
Composite Structures 33 (4), 201-210, 1995
1131995
Energy storing composite prosthetic foot
JCH Goh, SL Toh, TE Tay
US Patent 5,258,039, 1993
1131993
Shear thickening fluid impregnated ballistic fabric composites for shock wave mitigation
A Haris, HP Lee, TE Tay, VBC Tan
International Journal of Impact Engineering 80, 143-151, 2015
1102015
Modelling the tensile failure of composites with the floating node method
BY Chen, TE Tay, ST Pinho, VBC Tan
Computer Methods in Applied Mechanics and Engineering 308, 414-442, 2016
1012016
On the relationship between failure mechanism and compression after impact (CAI) strength in composites
MR Abir, TE Tay, M Ridha, HP Lee
Composite Structures 182, 242-250, 2017
982017
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