Trevor M. Young
TítuloCitado porAño
Surface treatment of titanium for adhesive bonding to polymer composites: a review
P Molitor, V Barron, T Young
International Journal of Adhesion and Adhesives 21 (2), 129-136, 2001
2542001
Bonded repair of composite aircraft structures: A review of scientific challenges and opportunities
KB Katnam, LFM Da Silva, TM Young
Progress in Aerospace Sciences 61, 26-42, 2013
2082013
Inclusion of a thermoplastic phase to improve impact and post-impact performances of carbon fibre reinforced thermosetting composites—A review
NH Nash, TM Young, PT McGrail, WF Stanley
Materials & Design 85, 582-597, 2015
902015
Adhesives bonding of a titanium alloy to a glass fibre reinforced composite material
P Molitor, T Young
International Journal of Adhesion and Adhesives 22 (2), 101-107, 2002
642002
Characterising the behaviour of composite single lap bonded joints using digital image correlation
AJ Comer, KB Katnam, WF Stanley, TM Young
International Journal of Adhesion and Adhesives 40, 215-223, 2013
502013
Plasma surface treatment of aerospace materials for enhanced adhesive bonding
W Leahy, V Barron, M Buggy, T Young, A Mas, F Schue, T McCabe, ...
The Journal of Adhesion 77 (3), 215-249, 2001
472001
Investigations into the use of excimer laser irradiation as a titanium alloy surface treatment in a metal to composite adhesive bond
P Molitor, T Young
International journal of adhesion and adhesives 24 (2), 127-134, 2004
332004
Taguchi analysis of bonded composite single-lap joints using a combined interface–adhesive damage model
DC O'Mahoney, KB Katnam, NP O'Dowd, CT McCarthy, TM Young
International Journal of Adhesion and Adhesives 40, 168-178, 2013
282013
Comparison of liquid impingement results from whirling arm and water-jet rain erosion test facilities
EF Tobin, TM Young, D Raps, O Rohr
Wear 271 (9-10), 2625-2631, 2011
282011
Thermo-mechanical fatigue analysis of liquid shim in mechanically fastened hybrid joints for aerospace applications
AJ Comer, JX Dhôte, WF Stanley, TM Young
Composite Structures 94 (7), 2181-2187, 2012
252012
Impact of Nd-YAG laser drilled holes on the strength and stiffness of laminar flow carbon fibre reinforced composite panels
T Young, D O'Driscoll
Composites Part A: Applied Science and Manufacturing 33 (1), 1-9, 2002
252002
Tensile strength of two-part epoxy paste adhesives: Influence of mixing technique and micro-void formation
KB Katnam, JPJ Stevenson, WF Stanley, M Buggy, TM Young
International journal of adhesion and adhesives 31 (7), 666-673, 2011
242011
Simplified thrust and fuel consumption models for modern two-shaft turbofan engines
M Bartel, TM Young
Journal of Aircraft 45 (4), 1450-1456, 2008
232008
Aircraft design innovation: creating an environment for creativity
TM Young
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of …, 2007
232007
The influence of hydrothermal conditioning on the Mode-I, thermal and flexural properties of Carbon/Benzoxazine composites with a thermoplastic toughening interlayer
NH Nash, D Ray, TM Young, WF Stanley
Composites Part A: Applied Science and Manufacturing 76, 135-144, 2015
212015
Composite repair in wind turbine blades: an overview
KB Katnam, AJ Comer, D Roy, LFM Da Silva, TM Young
The Journal of Adhesion 91 (1-2), 113-139, 2015
212015
Study of the effect of liquid shim on single-lap joint using 3D Digital Image Correlation
JX Dhôte, AJ Comer, WF Stanley, TM Young
Composite Structures 96, 216-225, 2013
202013
The effect of moisture ingress on through-thickness residual stresses in unsymmetric composite laminates: a combined experimental–numerical analysis
R Telford, KB Katnam, TM Young
Composite Structures 107, 502-511, 2014
192014
Liquid anti-contamination systems for hybrid laminar flow control aircraft—a review of the critical issues and important experimental results
TM Young, B Humphreys
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of …, 2004
192004
Investigation of hybrid laminar flow control (HLFC) surfaces
TM Young, B Humphreys, JP Fielding
Aircraft Design 4 (2-3), 127-146, 2001
192001
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