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Wouter M. van den Brink

Observed names: W. M. Van Den Brink, W.M. Van den Brink, W.M. van den Brink, Wouter van den Brink
Observed institution: Netherlands Aerospace Centre
ORCID: 0000-0002-8007-1065
Observed ORCID: 0000-0002-8007-1065
OpenAlex ID: A5024402514
On the fracture toughness of metal-composite adhesive joints with bending-extension coupling and residual thermal stresses effect
2019 · Panayiotis Tsokanas, Theodoros Loutas, et al. · Composites Part B Engineering · 49
Numerical prediction of impact damage in thick fabric composite laminates
2024 · Niels van Hoorn, Sergio Turteltaub, et al. · Composite Structures · 15
Strain energy release rate and mode partitioning of moment-loaded elastically coupled laminated beams with hygrothermal stresses
2020 · Panayiotis Tsokanas, Theodoros Loutas, et al. · Composite Structures · 15
Buckling-optimized variable stiffness laminates for a composite fuselage window section
2012 · W.M. van den Brink, W.J. Vankan, et al. · 14
Design for manufacturing of fuselage panels with curved grid stiffening
2013 · W.M. van den Brink, W.J. Vankan · 9
Modelling and simulation of damage in woven fabric composites on meso-macro level using the independent mesh method
2013 · W.M. Van den Brink, G. Van de Vrie, et al. · International Journal of Materials Engineering Innovation · 7
Impact response prediction and sensitivity analysis of thick laminated composite plates
2019 · Niels van Hoorn, Christos Kassapoglou, et al. · 6
Multiple unmanned aerial systems collision impacts on wing leading edge
2022 · A.J. de Wit, W.M. van den Brink, et al. · The Aeronautical Journal · 3
Validation and correlation of aircraft composite fuselage structure models
2016 · W.J. Vankan, W.M. van den Brink, et al. · 3
Design and Optimization Method for 3d Printed Carbon Reinforced Aircraft Components
2017 · W.M. van den Brink, R. Bruins, et al. · Data Archiving and Networked Services (DANS) · 2
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Comparison of integrated rib stiffened and L-blade stiffened composite panels manufactured using simple tooling methods
2016 · J. Marcelo Müller, W.M. van den Brink · 2
Topology Optimization for Aircraft Applications Using Hybrid and Multi-Material Methods for Different Component Scales
2025 · Wouter van den Brink, Tim Koenis, et al. · 1
Moment loading testing and data reduction for characterizing the fracture toughness of hybrid joints
2019 · W.M. van den Brink, P. Nijhuis, et al. · 1
Fibre steered skin design of composite thermoplastic horizontal stabilizer torsion box
2016 · W.M. van den Brink, Rhj Rick Bruins, et al. · 1
Manufacturing process simulation and structural evaluation of grid stiffened composite structures
2014 · W.M. van den Brink, W.J. Vankan, et al. · 1
Generic Linking of Finite Element Models for non-linear static and global dynamic analyses of aircraft structures
2012 · A.J. de Wit, D. Akçay Perdahcıoğlu, et al. · 1
Aircraft composite fuselage optimization through barrel and panel level analyses
2011 · W.J. Vankan, W.M. van den Brink, et al. · 1
Additive Manufacturing Design in Aerospace: Topology Optimization and Virtual Manufacturing
2020 · L. Paletti, W.M. van den Brink, et al.
Composite manufacturing supported by simulation
2019 · L. Paletti, W.M. van den Brink
Dimensionally Stable CFRP Grid Stiffened Structures for Space Applications
2019 · S. Sterk, W.M. van den Brink
On the manufacturing and testing of dissimilar and adhesive Ti-CFRP joints
2018 · W.M. van den Brink, P. Nijhuis, et al.
Impact response of thick composite structures
2017 · Niels van Hoorn, Christos Kassapoglou, et al.
Multi-level structural analysis for sub-component validation in aircraft composite fuselage structures
2015 · W.J. Vankan, W.M. van den Brink, et al.
Generic linking of finite element models for non-linear static and global dynamic analyses for aircraft structures
2011 · A.J. de Wit, Didem Akcay-Perdahcioglu, et al. · University of Twente Research Information
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Works count: 25
Citation count: 131
H-index: 6
I10-index: 4
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