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Brian Egan
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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
1672012
Modelling bearing failure in countersunk composite joints under quasi-static loading using 3D explicit finite element analysis
B Egan, MA McCarthy, RM Frizzell, PJ Gray, CT McCarthy
Composite Structures 108, 963-977, 2014
992014
Static and high-rate loading of single and multi-bolt carbon–epoxy aircraft fuselage joints
B Egan, CT McCarthy, MA McCarthy, PJ Gray, RM O’Higgins
Composites Part A: Applied Science and Manufacturing 53, 97-108, 2013
842013
Modelling a single-bolt countersunk composite joint using implicit and explicit finite element analysis
B Egan, CT McCarthy, MA McCarthy, PJ Gray, RM Frizzell
Computational Materials Science 64, 203-208, 2012
802012
An analytical model for strength prediction in multi-bolt composite joints at various loading rates
PA Sharos, B Egan, CT McCarthy
Composite Structures 116, 300-310, 2014
462014
Finite element analysis of catastrophic failure of dynamically-loaded countersunk composite fuselage joints
B Egan, MA McCarthy, RM Frizzell, CT McCarthy
Composite Structures 133, 1198-1208, 2015
192015
Finite element modelling and high speed testing of countersunk composite aircraft joints
B Egan
Ph. D. Thesis, 2014
22014
An efficient analytical model of composite bolted lap joints subjected to high rates of loading
PA Sharos, B Egan, CT McCarthy
ICCM International conferences on composite materials 28, 0
1
FE modelling of countersunk composite joints for next-generation aircraft
B Egan, C MC CARTHY, M McCarthy
UL-NUIG Research Day 2013, 2013
2013
Static and High-Rate Loading of Single and Multi-Bolt Carbon-Epoxy Fuselage Joints
B Egan, CT McCarthy, MA McCarthy, PJ Gray, RM O’Higgins
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Articles 1–10