René Alderliesten

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Rinze BenedictusProfessor Structural Integrity & Composites, Delft University, Faculty of Aerospace EngineeringVerified email at tudelft.nl
Calvin RansDelft University of TechnologyVerified email at tudelft.nl
Liaojun YaoDelft University of TechnologyVerified email at tudelft.nl
John-Alan PascoeDelft University of TechnologyVerified email at tudelft.nl
Mojtaba SadighiProfessor of Mechanical Engineering, Amirkabir University of TechnologyVerified email at aut.ac.ir
Sharif Ullah KhanPhD Researcher, Delft University of TechnologyVerified email at tudelft.nl
Dimitrios ZarouchasAssociate Professor, Aerospace Engineering Faculty, Delft University of TechnologyVerified email at tudelft.nl
S. van der ZwaagDelft University of TechnologyVerified email at tudelft.nl
Rafiullah KhanVerified email at iiu.edu.pk
Maria Odila Hilário CioffiProfessor associado, UNESPVerified email at unesp.br
Marcos Yutaka ShiinoInstituto de Ciência e Tecnologia, UNESP - Univ Estadual Paulista, Departamento de EngenhariaVerified email at ict.unesp.br
Nick EleftheroglouAssistant Professor at Technische Universiteit DelftVerified email at tudelft.nl
Theodoros LoutasAssociate Professor, University of PatrasVerified email at mech.upatras.gr
Mauricio DonadonInstituto Tecnológico de AeronáuticaVerified email at ita.br
Babak AbazadehAssistant Professor, dept. of Mechanical eng. University of BonabVerified email at ubonab.ac.ir
Michiel HagenbeekSenior project manager, TNOVerified email at tno.nl
Gianni CampoliVerified email at tudelft.nl
Simon BarterRMIT UniversityVerified email at RMIT.edu.au
Marcias MartinezClarkson UniversityVerified email at clarkson.edu
A J KinlochImperial College London, UKVerified email at imperial.ac.uk

René Alderliesten

Delft University of Technology

Verified email at tudelft.nl - Homepage

Fatigue Damage Tolerance Structural integrity Impact


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Impact resistance of fiber-metal laminates: A review M Sadighi, RC Alderliesten, R Benedictus International Journal of Impact Engineering 49, 77-90, 2012	368	2012
Methods for the prediction of fatigue delamination growth in composites and adhesive bonds–a critical review JA Pascoe, RC Alderliesten, R Benedictus Engineering Fracture Mechanics 112, 72-96, 2013	249	2013
Fatigue and damage tolerance issues of Glare in aircraft structures RC Alderliesten, JJ Homan International Journal of Fatigue 28 (10), 1116-1123, 2006	212	2006
A review of T-stress and its effects in fracture mechanics M Gupta, RC Alderliesten, R Benedictus Engineering Fracture Mechanics 134, 218-241, 2015	208	2015
Misinterpreting the results: How similitude can improve our understanding of fatigue delamination growth C Rans, R Alderliesten, R Benedictus Composites Science and Technology 71 (2), 230-238, 2011	181	2011
Fatigue crack propagation and delamination growth in Glare RC Alderliesten Delft University Press, 2005	170	2005
Experimental and numerical investigation of metal type and thickness effects on the impact resistance of fiber metal laminates M Sadighi, T Pärnänen, RC Alderliesten, M Sayeaftabi, R Benedictus Applied Composite Materials 19, 545-559, 2012	162	2012
Analytical prediction model for fatigue crack propagation and delamination growth in Glare RC Alderliesten International Journal of Fatigue 29 (4), 628-646, 2007	156	2007
Fiber/metal composite technology for future primary aircraft structures RC Alderliesten, R Benedictus Journal of Aircraft 45 (4), 1182-1189, 2008	147	2008
The applicability of magnesium based fibre metal laminates in aerospace structures R Alderliesten, C Rans, R Benedictus Composites Science and Technology 68 (14), 2983-2993, 2008	136	2008
An integrated study on the low-velocity impact response of the GLARE fibre-metal laminate FD Morinière, RC Alderliesten, M Sadighi, R Benedictus Composite Structures 100, 89-103, 2013	122	2013
Fatigue and damage tolerance of glare RC Alderliesten, M Hagenbeek, JJ Homan, PA Hooijmeijer, TJ De Vries, ... Applied Composite Materials 10, 223-242, 2003	110	2003
Application of the energy release rate approach for delamination growth in Glare RC Alderliesten, J Schijve, S Van der Zwaag Engineering Fracture Mechanics 73 (6), 697-709, 2006	109	2006
Modelling of impact damage and dynamics in fibre-metal laminates–A review FD Morinière, RC Alderliesten, R Benedictus International Journal of Impact Engineering 67, 27-38, 2014	104	2014
Fatigue crack growth prediction in GLARE hybrid laminates DJ Shim, RC Alderliesten, SM Spearing, DA Burianek Composites Science and Technology 63 (12), 1759-1767, 2003	101	2003
Bridging effect on mode I fatigue delamination behavior in composite laminates L Yao, R Alderliesten, M Zhao, R Benedictus Composites Part A: Applied Science and Manufacturing 63, 103-109, 2014	94	2014
Riveting process induced residual stresses around solid rivets in mechanical joints C Rans, PV Straznicky, R Alderliesten Journal of aircraft 44 (1), 323-329, 2007	89	2007
On the development of hybrid material concepts for aircraft structures R Alderliesten Recent Patents on Engineering 3 (1), 25-38, 2009	88	2009
Designing for damage tolerance in aerospace: A hybrid material technology RC Alderliesten Materials & Design 66, 421-428, 2015	85	2015
Discussion on the use of the strain energy release rate for fatigue delamination characterization L Yao, RC Alderliesten, M Zhao, R Benedictus Composites Part A: Applied Science and Manufacturing 66, 65-72, 2014	85	2014

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