ติดตาม
Stephen Hallett
Stephen Hallett
ยืนยันอีเมลแล้วที่ bristol.ac.uk
ชื่อ
อ้างโดย
อ้างโดย
ปี
Cohesive zone length in numerical simulations of composite delamination
PW Harper, SR Hallett
Engineering Fracture Mechanics 75 (16), 4774-4792, 2008
6792008
Prediction of impact damage in composite plates
JP Hou, N Petrinic, C Ruiz, SR Hallett
Composites Science and Technology 60 (2), 273-281, 2000
6392000
An experimental and numerical investigation into the damage mechanisms in notched composites
SR Hallett, BG Green, WG Jiang, MR Wisnom
Composites Part A: Applied Science and Manufacturing 40 (5), 613-624, 2009
4712009
An experimental investigation into the tensile strength scaling of notched composites
BG Green, MR Wisnom, SR Hallett
Composites Part A: Applied Science and Manufacturing 38 (3), 867-878, 2007
4632007
A concise interface constitutive law for analysis of delamination and splitting in composite materials and its application to scaled notched tensile specimens
WG Jiang, SR Hallett, BG Green, MR Wisnom
International journal for numerical methods in engineering 69 (9), 1982-1995, 2007
3592007
Size effects in unnotched tensile strength of unidirectional and quasi-isotropic carbon/epoxy composites
MR Wisnom, B Khan, SR Hallett
Composite Structures 84 (1), 21-28, 2008
3342008
A fatigue degradation law for cohesive interface elements–development and application to composite materials
PW Harper, SR Hallett
International Journal of Fatigue 32 (11), 1774-1787, 2010
3202010
Mechanical modelling of 3D woven composites considering realistic unit cell geometry
SD Green, MY Matveev, AC Long, D Ivanov, SR Hallett
Composite Structures 118, 284-293, 2014
2992014
Modelling the interaction between matrix cracks and delamination damage in scaled quasi-isotropic specimens
SR Hallett, WG Jiang, B Khan, MR Wisnom
Composites Science and Technology 68 (1), 80-89, 2008
2422008
Failure mechanisms and damage evolution of laminated composites under compression after impact (CAI): Experimental and numerical study
XC Sun, SR Hallett
Composites Part A: Applied Science and Manufacturing 104, 41-59, 2018
2292018
The role of delamination in strength, failure mechanism and hole size effect in open hole tensile tests on quasi-isotropic laminates
MR Wisnom, SR Hallett
Composites Part A: Applied Science and Manufacturing 40 (4), 335-342, 2009
2192009
Scaling effects in notched composites
MR Wisnom, SR Hallett, C Soutis
Journal of composite materials 44 (2), 195-210, 2010
2152010
Numerical modelling of 3D woven preform deformations
SD Green, AC Long, BSF El Said, SR Hallett
Composite Structures 108, 747-756, 2014
1992014
Compressive failure of laminates containing an embedded wrinkle; experimental and numerical study
S Mukhopadhyay, MI Jones, SR Hallett
Composites Part A: Applied Science and Manufacturing 73, 132-142, 2015
1912015
Barely visible impact damage in scaled composite laminates: Experiments and numerical simulations
XC Sun, SR Hallett
International Journal of Impact Engineering 109, 178-195, 2017
1772017
A crack tip tracking algorithm for cohesive interface element analysis of fatigue delamination propagation in composite materials
LF Kawashita, SR Hallett
International Journal of Solids and Structures 49 (21), 2898-2913, 2012
1752012
Computational modeling of complex failure mechanisms in laminates
FP Van der Meer, LJ Sluys, SR Hallett, MR Wisnom
Journal of Composite Materials 46 (5), 603-623, 2012
1722012
Modelling the effect of gaps and overlaps in automated fibre placement (AFP)-manufactured laminates
X Li, SR Hallett, MR Wisnom
Science and Engineering of Composite Materials 22 (2), 115-129, 2015
1592015
Understanding and predicting defect formation in automated fibre placement pre-preg laminates
JPH Belnoue, T Mesogitis, OJ Nixon-Pearson, J Kratz, DS Ivanov, ...
Composites Part A: Applied Science and Manufacturing 102, 196-206, 2017
1472017
Damage development in open-hole composite specimens in fatigue. Part 1: Experimental investigation
OJ Nixon-Pearson, SR Hallett, PJ Withers, J Rouse
Composite Structures 106, 882-889, 2013
1412013
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บทความ 1–20