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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
4472006
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
3132005
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
3011995
Progressive failure analysis of composites
TE Tay, G Liu, VBC Tan, XS Sun, DC Pham
Journal of Composite Materials 42 (18), 1921-1966, 2008
2882008
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
2012014
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
1792013
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
1752011
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
1742018
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
1732014
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
1642017
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
1432017
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
On cohesive element parameters and delamination modelling
X Lu, M Ridha, BY Chen, VBC Tan, TE Tay
Engineering Fracture Mechanics 206, 278-296, 2019
1312019
Modeling delamination growth in laminated composites
F Shen, KH Lee, TE Tay
Composites Science and Technology 61 (9), 1239-1251, 2001
1192001
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
1161995
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
1152016
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
1152015
Energy storing composite prosthetic foot
JCH Goh, SL Toh, TE Tay
US Patent 5,258,039, 1993
1131993
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
1072016
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
1042017
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