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 | 292 | 2011 |
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 | 251 | 2004 |
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 | 54 | 2021 |
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 | 47 | 2015 |
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 | 43 | 2013 |
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 | 33 | 2010 |
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 | 26 | 2023 |
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 | 25 | 2014 |
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 | 24 | 2013 |
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 | 23 | 2006 |
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 | 16 | 2019 |
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 | 16 | 2015 |
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 | 8 | 2013 |
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 | 7 | 2015 |
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 | 7 | 2007 |
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 | 6 | 2024 |
Advances in riblets design MR Pakatchian, J Rocha, L Li Applied Sciences 13 (19), 10893, 2023 | 6 | 2023 |
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 | 6 | 2018 |
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 |