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Chun Li
Chun Li
Bestätigte E-Mail-Adresse bei nrc-cnrc.gc.ca
Titel
Zitiert von
Zitiert von
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Enhancement of mechanical performance of epoxy/carbon fiber laminate composites using single-walled carbon nanotubes
B Ashrafi, J Guan, V Mirjalili, Y Zhang, L Chun, P Hubert, B Simard, ...
Composites science and technology 71 (13), 1569-1578, 2011
2922011
In-situ measurement of chemical shrinkage of MY750 epoxy resin by a novel gravimetric method
C Li, K Potter, MR Wisnom, G Stringer
Composites Science and Technology 64 (1), 55-64, 2004
2512004
A Review of Corrosion in Aircraft Structures and Graphene-Based Sensors for Advanced Corrosion Monitoring
L Li, M Chakik, R Prakash
Sensors 21 (9), 2021
542021
Assessment of debond simulation and cohesive zone length in a bonded composite joint
G Li, C Li
Composites Part B: Engineering 69, 359-368, 2015
472015
Interconversion of linearly viscoelastic material functions expressed as Prony series: a closure
J Luk-Cyr, T Crochon, C Li, M Lévesque
Mechanics of Time-Dependent Materials 17, 53-82, 2013
432013
On finite-element implementation strategies of Schapery-type constitutive theories
T Crochon, T Schönherr, C Li, M Lévesque
Mechanics of Time-Dependent Materials 14, 359-387, 2010
332010
High-fidelity simulation of low-velocity impact damage in fiber-reinforced composite laminates using integrated discrete and continuum damage models
P Shabani, L Li, J Laliberte, G Qi, D Rapking, D Mollenhauer
Composite Structures 313, 116910, 2023
262023
Linking bilinear traction law parameters to cohesive zone length for laminated composites and bonded joints
G Li, C Li
Advances in aircraft and spacecraft science 1 (2), 177, 2014
252014
An analytical analysis of energy release rate in bonded composite joints in a mode I condition
G Li, C Li
Composites Part B: Engineering 44 (1), 704-713, 2013
242013
Investigation of an accelerated moisture removal approach of a composite aircraft control surface
C Li, R Ueno, V Lefebvre
Society for the Advancement of Material and Process Engineering, 2006
232006
Failure analysis of adhesively bonded GFRP/aluminum matrix single composite lap joint with cold worked penetrative reinforcements
A Fawcett, X Chen, X Huang, C Li
Composites Part B: Engineering 161, 96-106, 2019
162019
On the onset of the asymptotic stable fracture region in the mode II fatigue delamination growth behaviour of composites
CD Rans, J Atkinson, C Li
Journal of Composite Materials 49 (6), 685-697, 2015
162015
Investigation of moisture ingress and migration mechanisms of an aircraft rudder composites sandwich structure
C Li, J Teuwen, R Ueno, V Lefebvre
38th international society for the advancement of manufacturing and process …, 2006
11*2006
4-point bending fatigue testing of thin carbon-epoxy laminates
C Marsden, C Li, M Biernacki, SJ Carnegie
Proceedings of the 19th Internafional Conference on COmposite Materials, 2013
82013
On time–temperature-dependent viscoelastic behavior of an amorphous polyimide
T Crochon, C Li, M Lévesque
Mechanics of Time-Dependent Materials 19, 305-324, 2015
72015
Effect of process-induced residual stresses on mechanical properties and fatigue crack initiation in fibre metal laminates
J Laliberté, M Mahendran, D Djokic, C Li, J Kratz
24th International Committee on Aircraft Fatigue Symposium, 2007
72007
Compression after impact (CAI) failure mechanisms and damage evolution in large composite laminates: High-fidelity simulation and experimental study
P Shabani, L Li, J Laliberte, G Qi
Composite Structures, 118143, 2024
62024
Advances in riblets design
MR Pakatchian, J Rocha, L Li
Applied Sciences 13 (19), 10893, 2023
62023
Adhesive bonding of ceramic-based armor system
S Noormohammed, C Li, S Nikumb
NATO STO AVT-266 Specialists-Meeting-Use of Bonded Joints in Military …, 2018
62018
Simulation of process-induced residual stresses in thick filament wound tubes
C Li, MR Wisnom, LG Stringer
Fourth Canada-Japan Workshop on Composites, 271-282, 2002
6*2002
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