| Determination of activation energy for glass transition of an epoxy adhesive using dynamic mechanical analysis G Li, P Lee-Sullivan, RW Thring Journal of thermal analysis and calorimetry 60, 377-390, 2000 | 184 | 2000 |
| Nonlinear finite element analysis of stress and strain distributions across the adhesive thickness in composite single-lap joints G Li, P Lee-Sullivan, RW Thring Composite Structures 46 (4), 395-403, 1999 | 141 | 1999 |
| Finite element and experimental studies on single-lap balanced joints in tension G Li, P Lee-Sullivan International journal of adhesion and adhesives 21 (3), 211-220, 2001 | 108 | 2001 |
| Studies of residual stress in single-row countersunk riveted lap joints G Li, G Shi, NC Bellinger Journal of Aircraft 43 (3), 592-599, 2006 | 71 | 2006 |
| Effect of the riveting process on the residual stress in fuselage lap joints G Li, G Shi Canadian Aeronautics and Space Journal 50 (2), 91-105, 2004 | 57 | 2004 |
| Static strength of a composite butt joint configuration with different attachments G Li, JH Chen, M Yanishevsky, NC Bellinger Composite Structures 94 (5), 1736-1744, 2012 | 43 | 2012 |
| 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 | 42 | 2015 |
| Study of the residual strain in lap joints G Li, G Shi, NC Bellinger Journal of Aircraft 43 (4), 1145-1151, 2006 | 39 | 2006 |
| Fractographic examination of coupons representing aircraft structural joints with and without hole cold expansion M Yanishevsky, G Li, G Shi, D Backman Engineering Failure Analysis 30, 74-90, 2013 | 27 | 2013 |
| Stress in triple-row riveted lap joints under the influence of specific factors G Li, G Shi, NC Bellinger Journal of Aircraft 48 (2), 527-539, 2011 | 27 | 2011 |
| Residual stress/strain in three-row, countersunk, riveted lap joints G Li, G Shi, NC Bellinger Journal of aircraft 44 (4), 1275-1285, 2007 | 24 | 2007 |
| Liquid phase sintering of metal matrix composites G Li, L Lu, MO Lai Journal of materials processing technology 63 (1-3), 286-291, 1997 | 24 | 1997 |
| 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 | 22 | 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 | 22 | 2013 |
| Elastic analysis of closed-form solutions for adhesive stresses in bonded single-strap butt joints G Li Journal of Mechanics of Materials and Structures 5 (3), 409-426, 2010 | 19 | 2010 |
| Elastic deformation analysis of adhesively bonded composite butt joints in tension G Li, A Johnston, M Yanishevsky, NC Bellinger Journal of Aircraft 48 (2), 578-590, 2011 | 15 | 2011 |
| Crack detection on composite and metallic aerospace structures M Martinez, L Gang, D Backman, A Oudovikine, N Bellinger Structural Health Monitoring, 560-569, 2008 | 15 | 2008 |
| Re-visiting the beam models for adhesively bonded single lap joints, Part II: Comparison of adhesive stress predictions G Li, P Lee-Sullivan Canadian Aeronautics and Space Journal 52 (4), 173-180, 2006 | 15* | 2006 |
| Deformation of balanced and unbalanced adhesively bonded single-lap joints G Li National Library of Canada= Bibliothèque nationale du Canada, Ottawa, 2002 | 15 | 2002 |
| Assessing the riveting process and the quality of riveted lap joints in aerospace and other applications G Li, G Renaud, M Liao Welding and joining of aerospace materials, 383-426, 2021 | 12 | 2021 |
