| Three-dimensional finite element analysis of single-bolt, single-lap composite bolted joints: part I—model development and validation MA McCarthy, CT McCarthy, VP Lawlor, WF Stanley Composite structures 71 (2), 140-158, 2005 | 365 | 2005 |
| Bolt-hole clearance effects and strength criteria in single-bolt, single-lap, composite bolted joints MA McCarthy, VP Lawlor, WF Stanley, CT McCarthy Composites science and technology 62 (10-11), 1415-1431, 2002 | 326 | 2002 |
| Progressive damage analysis of multi-bolt composite joints with variable bolt–hole clearances CT McCarthy, MA McCarthy, VP Lawlor Composites Part B: Engineering 36 (4), 290-305, 2005 | 307 | 2005 |
| Mechanical characterisation of carbon fibre–PEEK manufactured by laser-assisted automated-tape-placement and autoclave AJ Comer, D Ray, WO Obande, D Jones, J Lyons, I Rosca, RM O’higgins, ... Composites Part A: Applied Science and Manufacturing 69, 10-20, 2015 | 249 | 2015 |
| Modelling of bird strike on an aircraft wing leading edge made from fibre metal laminates–Part 2: modelling of impact with SPH bird model MA McCarthy, JR Xiao, CT McCarthy, A Kamoulakos, J Ramos, ... Applied Composite Materials 11, 317-340, 2004 | 248 | 2004 |
| Three-dimensional finite element analysis of single-bolt, single-lap composite bolted joints: Part II––effects of bolt-hole clearance CT McCarthy, MA McCarthy Composite structures 71 (2), 159-175, 2005 | 237 | 2005 |
| A simple method for determining the effects of bolt–hole clearance on load distribution in single-column multi-bolt composite joints MA McCarthy, CT McCarthy, GS Padhi Composite Structures 73 (1), 78-87, 2006 | 212 | 2006 |
| Comparison of open hole tension characteristics of high strength glass and carbon fibre-reinforced composite materials RM O’Higgins, MA McCarthy, CT McCarthy Composites Science and Technology 68 (13), 2770-2778, 2008 | 204 | 2008 |
| Vibration response of double-walled carbon nanotubes subjected to an externally applied longitudinal magnetic field: a nonlocal elasticity approach T Murmu, MA McCarthy, S Adhikari Journal of Sound and Vibration 331 (23), 5069-5086, 2012 | 188 | 2012 |
| Analysis of thick functionally graded plates by using higher-order shear and normal deformable plate theory and MLPG method with radial basis functions DF Gilhooley, RC Batra, JR Xiao, MA McCarthy, JW Gillespie Jr Composite Structures 80 (4), 539-552, 2007 | 180 | 2007 |
| Stress analysis of single-bolt, single-lap, countersunk composite joints with variable bolt-hole clearance B Egan, CT McCarthy, MA McCarthy, RM Frizzell Composite Structures 94 (3), 1038-1051, 2012 | 162 | 2012 |
| An experimental study of bolt–hole clearance effects in double-lap, multi-bolt composite joints VP Lawlor, MA McCarthy, WF Stanley Composite structures 71 (2), 176-190, 2005 | 157 | 2005 |
| In-plane magnetic field affected transverse vibration of embedded single-layer graphene sheets using equivalent nonlocal elasticity approach T Murmu, MA McCarthy, S Adhikari Composite Structures 96, 57-63, 2013 | 142 | 2013 |
| Experiences with modeling friction in composite bolted joints CT McCarthy, MA McCarthy, WF Stanley, VP Lawlor Journal of composite materials 39 (21), 1881-1908, 2005 | 130 | 2005 |
| Analysis of thick composite laminates using a higher-order shear and normal deformable plate theory (HOSNDPT) and a meshless method JR Xiao, DF Gilhooley, RC Batra, JW Gillespie Jr, MA McCarthy Composites Part B: Engineering 39 (2), 414-427, 2008 | 125 | 2008 |
| BOJCAS: bolted joints in composite aircraft structures MA McCartney University of Limerick, 2003 | 113 | 2003 |
| Numerical investigation of a crash test of a composite helicopter subfloor structure MA McCarthy, JFM Wiggenraad Composite structures 51 (4), 345-359, 2001 | 110 | 2001 |
| Finite element analysis of effects of clearance on single shear composite bolted joints MA McCarthy, CT McCarthy Plastics, rubber and composites 32 (2), 65-70, 2003 | 106 | 2003 |
| Multiwall Nanotubes Can Be Stronger than Single Wall Nanotubes and Implications<? format?> for Nanocomposite Design EM Byrne, MA McCarthy, Z Xia, WA Curtin Physical review letters 103 (4), 045502, 2009 | 103 | 2009 |
| Modelling of bird strike on an aircraft wing leading edge made from fibre metal laminates–Part 1: material modelling MA McCarthy, JR Xiao, N Petrinic, A Kamoulakos, V Melito Applied Composite Materials 11, 295-315, 2004 | 98 | 2004 |
Conor McCarthyAssociate Professor of Aeronautical Engineering, University of Limerick在 ul.ie 的电子邮件经过验证
