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  1. ICEFlight: Powering the Future of Aviation With Cryogenic Innovation in the Netherlands

    Article • January 2026, American Institute of Aeronautics and Astronautics (AIAA)

    Dr.ir. René C Alderliesten

  2. Tailoring the fatigue response of flax FRP composites by exploiting Micro-structural re-arrangements and auxiliary loading sequences

    Article • Composites Part A Applied Science and Manufacturing, December 2025, Elsevier

    Dr.ir. René C Alderliesten

  3. Adopting Principles from Physics to Fatigue Crack Growth

    Article • October 2025, Taylor & Francis

    Dr.ir. René C Alderliesten

  4. Failure modes and energy absorption in Glass Reinforced aluminum (GLARE) hybrid laminates subjected to three-point bending

    Article • Composites Part C Open Access, October 2025, Elsevier

    Dr.ir. René C Alderliesten

  5. Thermoset (epoxy) - thermoplastic (polyetherimide) carbon fiber reinforced laminates featuring improved crack resistance in double cantilever beam tests due to hybridization

    Article • Composites Part C Open Access, October 2025, Elsevier

    Dr.ir. René C Alderliesten

  6. Effect of carbon nanotube buckypapers on interlaminar fracture toughness of thermoplastic composites subjected to fatigue tests

    Article • International Journal of Fatigue, June 2025, Elsevier

    Dr.ir. René C Alderliesten

  7. Experimental investigation of the effect of interface angle on mode-I fracture toughness in DCB laminates using digital image correlation

    Article • Engineering Fracture Mechanics, May 2025, Elsevier

    Dr.ir. René C Alderliesten

  8. Developments and future prospects of welding technology for carbon fiber thermoplastic composites

    Article • Composites Part B Engineering, May 2025, Elsevier

    Dr.ir. René C Alderliesten

  9. Stiffened composite plates as equivalent structures for sandwich panels under low-velocity hail impact

    Article • Mechanics Based Design of Structures and Machines, February 2025, Taylor & Francis

    Dr.ir. René C Alderliesten

  10. Comparison of mode II delamination behaviours in multidirectional and unidirectional composite laminates

    Article • Composites Part B Engineering, February 2025, Elsevier

    Dr.ir. René C Alderliesten

  11. In-plane compressive properties of 3D braided jute/epoxy composite honeycombs: Structure-property relationships

    Article • Journal of Reinforced Plastics and Composites, January 2025, SAGE Publications

    Dr.ir. René C Alderliesten

  12. Advancing Hydrogen Storage in Aviation: Stress State of Discretely Loaded All-Composite Double-Walled Vacuum-Insulated Cryo-Compressed Vessels

    Article • January 2025, American Institute of Aeronautics and Astronautics (AIAA)

    Dr.ir. René C Alderliesten, Victor Poorte

  13. Corrigendum to “Crashworthiness in preliminary design: mean crushing force prediction for closed-section thin-walled metallic structures” [International Journal of Impact Engineering, Volume 188, June 2024, 104946]

    Article • International Journal of Impact Engineering, December 2024, Elsevier

    Dr.ir. René C Alderliesten

  14. Hygrothermal ageing effects on mode I fatigue delamination in multidirectional composite laminates

    Article • International Journal of Fatigue, November 2024, Elsevier

    Dr.ir. René C Alderliesten

  15. A new interpretation of mode I interlaminar fracture in layered materials

    Article • Engineering Fracture Mechanics, October 2024, Elsevier

    Dr.ir. René C Alderliesten

  16. FLAx‐REinforced Aluminum (FLARE): A Bio‐Based Fiber Metal Laminate Alternative Combining Impact Resistance and Vibration Damping

    Article • Advanced Engineering Materials, August 2024, Wiley

    Dr.ir. René C Alderliesten

  17. Does hygrothermal degradation of Mode I fatigue delamination resistance in carbon fibre reinforced polymer laminates depend on the ageing conditions?

    Article • Composite Structures, August 2024, Elsevier

    Dr.ir. René C Alderliesten

  18. Effect of pre-existing damage on delamination growth in repeatedly indented composites

    Article • Materials & Design, July 2024, Elsevier

    Dr.ir. René C Alderliesten

  19. Planar delamination behaviour of CFRP panels under quasi-static out-of-plane loading

    Article • Composite Structures, July 2024, Elsevier

    Dr.ir. René C Alderliesten

  20. Crashworthiness in preliminary design: Mean crushing force prediction for closed-section thin-walled metallic structures

    Article • International Journal of Impact Engineering, June 2024, Elsevier

    Dr.ir. René C Alderliesten

  21. Crashworthiness of the Flying-V Aircraft Concept with Vertical Drop Test Simulations

    Article • February 2024, Open Engineering Inc

    Dr.ir. René C Alderliesten

  22. Hygrothermal effects on fatigue delamination behavior in composite laminates

    Article • Composite Structures, February 2024, Elsevier

    Dr.ir. René C Alderliesten

  23. Low-fidelity crashworthiness assessment of unconventional aircraft: Modelling of plastic bending

    Article • January 2024, American Institute of Aeronautics and Astronautics (AIAA)

    Dr.ir. René C Alderliesten

  24. Structural integration of a full-composite, double-walled, vacuum-insulated, cryo-compressed tank

    Article • January 2024, American Institute of Aeronautics and Astronautics (AIAA)

    Dr.ir. René C Alderliesten, Victor Poorte

  25. On the post-impact fatigue behavior and theoretical life prediction of CF/PEEK-titanium hybrid laminates using an energy dissipation approach

    Article • Composites Science and Technology, January 2024, Elsevier

    Dr.ir. René C Alderliesten

  26. A proposal for similitude in characterizing fatigue delamination behavior with fibre bridging of carbon-fibre reinforced polymer composites

    Article • Engineering Fracture Mechanics, January 2024, Elsevier

    Dr.ir. René C Alderliesten

  27. Temperature effects on fatigue delamination behavior in thermoset composite laminates

    Article • Engineering Fracture Mechanics, January 2024, Elsevier

    Dr.ir. René C Alderliesten

  28. Investigating apparent plateau phases in fatigue after impact damage growth in CFRP with ultrasound scan and acoustic emissions

    Article • International Journal of Fatigue, December 2023, Elsevier

    Dr.ir. René C Alderliesten

  29. Synergistic Toughening of Epoxy through Layered Poly(ether imide) with Dual-Scale Morphologies

    Article • ACS Applied Materials & Interfaces, November 2023, American Chemical Society (ACS)

    Dr.ir. René C Alderliesten

  30. Delamination link-ups in composite laminates due to multiple hail impacts

    Article • Engineering Structures, November 2023, Elsevier

    Babak Soltannia, Dr.ir. René C Alderliesten

  31. Does carbon nanotube buckypaper affect mode-I and II interlaminar fracture toughness under quasi-static loading?

    Article • Composite Structures, November 2023, Elsevier

    Dr.ir. René C Alderliesten

  32. Fatigue delamination behavior in composite laminates at different stress ratios and temperatures

    Article • International Journal of Fatigue, October 2023, Elsevier

    Dr.ir. René C Alderliesten

  33. Assessment of two quasi-static approaches to mimic repeated impact response and damage behaviour of CFRP laminates

    Article • Chinese Journal of Aeronautics, August 2023, Tsinghua University Press

    Dr.ir. René C Alderliesten

  34. Special Issue: Advanced Modeling and Design for Composite Materials and Structures

    Article • Applied Composite Materials, July 2023, Springer Science + Business Media

    Dr.ir. René C Alderliesten

  35. Interlaminar and intralaminar fracture resistance of recycled carbon fibre/PPS composites with tailored fibre/matrix adhesion

    Article • Composites Science and Technology, July 2023, Elsevier

    Dr.ir. René C Alderliesten

  36. A Review of Analytical Models for Determining the Behavior of Metallic Tubular Structures Submitted to Axial Crushing

    Article • June 2023, ASME International

    Dr.ir. René C Alderliesten

  37. On the application of strong thermoplastic–thermoset interactions for developing advanced aerospace-composite joints

    Article • Thin-Walled Structures, May 2023, Elsevier

    Dr.ir. René C Alderliesten

  38. Explaining the multiple energy thresholds for damage mechanisms activation in laminate composites under cyclic loadings

    Article • Composites Part A Applied Science and Manufacturing, April 2023, Elsevier

    Dr.ir. René C Alderliesten

  39. Effects of different joint wall lengths on in-plane compression properties of 3D braided jute/epoxy composite honeycombs

    Article • Journal of Reinforced Plastics and Composites, March 2023, SAGE Publications

    Dr.ir. René C Alderliesten

  40. Investigation of compression after impact failure in carbon fiber reinforced polymers using acoustic emission

    Article • Journal of Composite Materials, March 2023, SAGE Publications

    Dr.ir. René C Alderliesten

  41. In-situ damage mechanism investigation and a prediction model for delamination with fibre bridging in composites

    Article • Engineering Fracture Mechanics, March 2023, Elsevier

    Dr.ir. René C Alderliesten

  42. Influence of neighbouring damage on delamination growth in multiple indented composites

    Article • Materials & Design, March 2023, Elsevier

    Dr.ir. René C Alderliesten

  43. Experimental and theoretical study on residual ultimate strength after impact of CF/PEEK-titanium hybrid laminates with nano-interfacial enhancement

    Article • Composites Science and Technology, February 2023, Elsevier

    Dr.ir. René C Alderliesten

  44. Delamination initiation in fully clamped rectangular CFRP laminates subjected to out-of-plane quasi-static indentation loading

    Article • Composite Structures, January 2023, Elsevier

    Dr.ir. René C Alderliesten

  45. On the interlayer toughening of carbon fibre/epoxy composites using surface-activated ultra-thin PEEK films

    Article • Composite Structures, January 2023, Elsevier

    Dr.ir. René C Alderliesten

  46. In-Service Delaminations in FRP Structures under Operational Loading Conditions: Are Current Fracture Testing and Analysis on Coupons Sufficient for Capturing the Essential Effects for Reliable Predictions?

    Article • Materials, December 2022, MDPI AG

    Dr.ir. René C Alderliesten

  47. Development and analysis of a three-dimensional braided honeycomb structure

    Article • Textile Research Journal, November 2022, SAGE Publications

    Dr.ir. René C Alderliesten

  48. A criterion for predicting delamination growth in composite laminates

    Article • Materials & Design, November 2022, Elsevier

    Dr.ir. René C Alderliesten

  49. Applying the new experimental midpoint concept on strain energy density for fracture assessment of composite materials

    Article • Theoretical and Applied Fracture Mechanics, October 2022, Elsevier

    Dr.ir. René C Alderliesten

  50. Co-cured carbon fibre/epoxy composite joints by advanced thermoplastic films with excellent structural integrity and thermal resistance

    Article • International Journal of Adhesion and Adhesives, October 2022, Elsevier

    Dr.ir. René C Alderliesten

  51. Impact fatigue, multiple and repeated low-velocity impacts on FRP composites: A review

    Article • Composite Structures, October 2022, Elsevier

    Dr.ir. René C Alderliesten

  52. On the mix-mode fracture of carbon fibre/epoxy composites interleaved with various thermoplastic veils

    Article • Composites Communications, August 2022, Elsevier

    Dr.ir. René C Alderliesten

  53. Co-curing bonding of carbon fibre/epoxy composite joints with excellent structure integrity using carbon fibre/PEEK tapes

    Article • Composites Science and Technology, August 2022, Elsevier

    Dr.ir. René C Alderliesten

  54. The energy dissipation during fatigue crack growth in adhesive joints under Mode-I loading

    Article • Theoretical and Applied Fracture Mechanics, August 2022, Elsevier

    Dr.ir. René C Alderliesten

  55. The development of high performance hybrid joints between epoxy composites and PEEK/PPS composites: The mode-II and mix mode-I/II fracture behaviour

    Article • Composite Structures, July 2022, Elsevier

    Dr.ir. René C Alderliesten

  56. Recycled carbon fibre mats for interlayer toughening of carbon fibre/epoxy composites

    Article • Materials & Design, June 2022, Elsevier

    Dr.ir. René C Alderliesten

  57. The energy dissipation during fatigue crack growth in metallic materials

    Article • Engineering Fracture Mechanics, June 2022, Elsevier

    Dr.ir. René C Alderliesten

  58. Fatigue delamination behaviour of carbon fibre/epoxy composites interleaved with thermoplastic veils

    Article • Composite Structures, February 2022, Elsevier

    Dr.ir. René C Alderliesten

  59. On the fracture behaviour of aerospace-grade Polyether-ether-ketone composite-to-aluminium adhesive joints

    Article • Composites Communications, February 2022, Elsevier

    Dr.ir. René C Alderliesten

  60. Experimental investigation of fatigue after impact damage growth in CFRP

    Article • Procedia Structural Integrity, January 2022, Elsevier

    Dr.ir. René C Alderliesten

  61. On the effect of plastic model on simulation of adhesive bonded joints with FM94

    Article • International Journal of Adhesion and Adhesives, October 2021, Elsevier

    Dr.ir. René C Alderliesten

  62. Measuring crack growth and related opening and closing stresses using continuous potential drop recording

    Article • Engineering Fracture Mechanics, July 2021, Elsevier

    Dr.ir. René C Alderliesten

  63. The relation between fatigue crack growth rate and plastic energy dissipation in 7075-T6

    Article • Engineering Fracture Mechanics, July 2021, Elsevier

    Dr.ir. René C Alderliesten

  64. The influence of carbon nanotube buckypaper/poly (ether imide) mats on the thermal properties of poly (ether imide) and poly (aryl ether ketone)/carbon fiber laminates

    Article • Diamond and Related Materials, June 2021, Elsevier

    Dr.ir. René C Alderliesten

  65. Loading rate dependency of strain energy release rate in mode I delamination of composite laminates

    Article • Theoretical and Applied Fracture Mechanics, April 2021, Elsevier

    Professor Mahmood Mehrdad Shokrieh, Dr.ir. René C Alderliesten

  66. Erratum to “Unraveling the myth of closure corrections: Sharpening the definition of opening and closure stresses with an energy approach” [Int. J. Fatigue 143 (2021) 106016]

    Article • International Journal of Fatigue, April 2021, Elsevier

    Dr.ir. René C Alderliesten

  67. Unraveling the myth of closure corrections: Sharpening the definition of opening and closure stresses with an energy approach

    Article • International Journal of Fatigue, February 2021, Elsevier

    Dr.ir. René C Alderliesten

  68. The residual stress characteristics and mechanical behavior of shot peened fiber metal laminates based on the aluminium-lithium alloy

    Article • Composite Structures, December 2020, Elsevier

    Dr.ir. René C Alderliesten

  69. Enhancing the fracture toughness of carbon fibre/epoxy composites by interleaving hybrid meltable/non-meltable thermoplastic veils

    Article • Composite Structures, November 2020, Elsevier

    Dr.ir. René C Alderliesten

  70. Co-cure joining of epoxy composites with rapidly UV-irradiated PEEK and PPS composites to achieve high structural integrity

    Article • Composite Structures, November 2020, Elsevier

    Dr.ir. René C Alderliesten

  71. Scrutinizing interlaminar fatigue loading cycle in composites using acoustic emission technique: Stress ratio influence on damage formation

    Article • Composites Part A Applied Science and Manufacturing, November 2020, Elsevier

    Dr.ir. René C Alderliesten

  72. Significantly enhanced structural integrity of adhesively bonded PPS and PEEK composite joints by rapidly UV-irradiating the substrates

    Article • Composites Science and Technology, October 2020, Elsevier

    Dr.ir. René C Alderliesten

  73. The influence of interlayer/epoxy adhesion on the mode-I and mode-II fracture response of carbon fibre/epoxy composites interleaved with thermoplastic veils

    Article • Materials & Design, July 2020, Elsevier

    Dr.ir. René C Alderliesten

  74. Loading rate effects on mode-I delamination in glass/epoxy and glass/CNF/epoxy laminated composites

    Article • Engineering Fracture Mechanics, April 2020, Elsevier

    Professor Mahmood Mehrdad Shokrieh, Dr.ir. René C Alderliesten

  75. The effect of bond-line thickness on fatigue crack growth rate in adhesively bonded joints

    Article • Engineering Fracture Mechanics, April 2020, Elsevier

    Dr.ir. René C Alderliesten

  76. The effect of temperature on fatigue strength of poly(ether‐imide)/multiwalled carbon nanotube/carbon fibers composites for aeronautical application

    Article • Journal of Applied Polymer Science, February 2020, Wiley

    Dr.ir. René C Alderliesten

  77. Teaching Aerospace Structures and Materials to the World – Analysis of the edX MOOC Introduction to Aerospace Structures and Materials

    Article • January 2020, American Institute of Aeronautics and Astronautics (AIAA)

    Dr.ir. René C Alderliesten

  78. Development of a physics-based theory for mixed mode I/II delamination onset in orthotropic laminates

    Article • Theoretical and Applied Fracture Mechanics, October 2019, Elsevier

    Professor Mahmood Mehrdad Shokrieh, Dr.ir. René C Alderliesten

  79. Determining finite-width-correction factors for fatigue crack growth prediction in GLARE using the equivalent compliance method

    Article • International Journal of Fatigue, October 2019, Elsevier

    Dr.ir. René C Alderliesten

  80. Physics of delamination onset in unidirectional composite laminates under mixed-mode I/II loading

    Article • Engineering Fracture Mechanics, April 2019, Elsevier

    Professor Mahmood Mehrdad Shokrieh, Dr.ir. René C Alderliesten

  81. New Materials and Processes for Transport Applications: Going Hybrid and Beyond

    Article • Advanced Engineering Materials, March 2019, Wiley

    Dr.ir. René C Alderliesten

  82. Fatigue in fibre metal laminates: The interplay between fatigue in metals and fatigue in composites

    Article • Fatigue & Fracture of Engineering Materials & Structures, February 2019, Wiley

    Dr.ir. René C Alderliesten

  83. Fibre-bridged fatigue delamination in multidirectional composite laminates

    Article • Composites Part A Applied Science and Manufacturing, December 2018, Elsevier

    Dr.ir. René C Alderliesten

  84. On the physics of applying finite width and geometry correction factors in fatigue crack growth predictions of GLARE

    Article • International Journal of Fatigue, December 2018, Elsevier

    Dr.ir. René C Alderliesten

  85. Cyclic fatigue fracture of composites: What has testing revealed about the physics of the processes so far?

    Article • Engineering Fracture Mechanics, November 2018, Elsevier

    Dr.ir. René C Alderliesten

  86. Structural health monitoring data fusion for in-situ life prognosis of composite structures

    Article • Reliability Engineering & System Safety, October 2018, Elsevier

    Dr.ir. René C Alderliesten

  87. A new mixed mode I/II failure criterion for laminated composites considering fracture process zone

    Article • Theoretical and Applied Fracture Mechanics, September 2018, Elsevier

    Professor Mahmood Mehrdad Shokrieh, Dr.ir. René C Alderliesten

  88. Fatigue delamination of composite materials – approach to exclude large scale fibre bridging

    Article • IOP Conference Series Materials Science and Engineering, July 2018, Institute of Physics Publishing

    Dr.ir. René C Alderliesten

  89. Delamination fatigue growth in polymer-matrix fibre composites: A methodology for determining the design and lifing allowables

    Article • Composite Structures, July 2018, Elsevier

    Professor Rhys Jones, Dr.ir. René C Alderliesten

  90. Thickness effects on fibre-bridged fatigue delamination growth in composites

    Article • Composites Part A Applied Science and Manufacturing, July 2018, Elsevier

    Dr.ir. René C Alderliesten

  91. Towards a physics-based relationship for crack growth under different loading modes

    Article • Engineering Fracture Mechanics, May 2018, Elsevier

    Dr.ir. René C Alderliesten

  92. Using acoustic emission to understand fatigue crack growth within a single load cycle

    Article • Engineering Fracture Mechanics, May 2018, Elsevier

    Dr.ir. René C Alderliesten

  93. The Challenge of Reversing Theories to Hybridize Structures with Fiber Metal Laminate Design Concepts

    Article • Advanced Engineering Materials, March 2018, Wiley

    Dr.ir. René C Alderliesten

  94. Mode I fatigue delamination growth with fibre bridging in multidirectional composite laminates

    Article • Engineering Fracture Mechanics, February 2018, Elsevier

    Dr.ir. René C Alderliesten

  95. The effect of temperature on fatigue crack growth in FM94 epoxy adhesive bonds investigated by means of energy dissipation

    Article • Engineering Fracture Mechanics, February 2018, Elsevier

    Dr.ir. René C Alderliesten

  96. Fatigue crack surface area and crack front length: new ways to look at fatigue crack growth

    Article • MATEC Web of Conferences, January 2018, EDP Sciences

    Dr.ir. René C Alderliesten

  97. The stress ratio effect on plastic dissipation during fatigue crack growth

    Article • MATEC Web of Conferences, January 2018, EDP Sciences

    Dr.ir. René C Alderliesten

  98. Introduction to Aerospace Structures and Materials

    Article • January 2018, Delft University of Technology

    Dr.ir. René C Alderliesten

  99. Fibre bridging effect on the Paris relation of mode I fatigue delamination in composite laminates with different thicknesses

    Article • International Journal of Fatigue, October 2017, Elsevier

    Dr.ir. René C Alderliesten

  100. A modified Paris relation for fatigue delamination with fibre bridging in composite laminates

    Article • Composite Structures, September 2017, Elsevier

    Dr.ir. René C Alderliesten

  101. An experimental study on the low velocity impact resistance of fibre metal laminates under successive impacts with reduced energies

    Article • Aerospace Science and Technology, August 2017, Elsevier

    Dr.ir. René C Alderliesten

  102. Understanding mixed-mode cyclic fatigue delamination growth in unidirectional composites: An experimental approach

    Article • Engineering Fracture Mechanics, July 2017, Elsevier

    Dr.ir. René C Alderliesten

  103. On the physical interpretation of the R-ratio effect and the LEFM parameters used for fatigue crack growth in adhesive bonds

    Article • International Journal of Fatigue, April 2017, Elsevier

    Dr.ir. René C Alderliesten

  104. Stress ratio dependence of fibre bridging significance in mode I fatigue delamination growth of composite laminates

    Article • Composites Part A Applied Science and Manufacturing, April 2017, Elsevier

    Dr.ir. René C Alderliesten

  105. Energy dissipation in mode II fatigue crack growth

    Article • Engineering Fracture Mechanics, March 2017, Elsevier

    Dr.ir. René C Alderliesten

  106. Development of a finite element model for comparing metal and composite fuselage section drop testing

    Article • International Journal of Crashworthiness, January 2017, Taylor & Francis

    Dr.ir. René C Alderliesten

  107. Fatigue and Fracture of Fibre Metal Laminates

    Article • January 2017, Springer Science + Business Media

    Dr.ir. René C Alderliesten

  108. Fibre bridging effect on the Paris relation for mode I fatigue delamination growth in composites with consideration of interface configuration

    Article • Composite Structures, January 2017, Elsevier

    Dr.ir. René C Alderliesten

  109. A Bayesian tolerance interval estimation method for fatigue strength substantiation of rotorcraft dynamic components

    Article • International Journal of Fatigue, November 2016, Elsevier

    Dr.ir. René C Alderliesten

  110. EXPERIMENTAL INVESTIGATION OF THE MICROSCOPIC DAMAGE DEVELOPMENT AT MODE I FATIGUE DELAMINATION TIPS IN CARBON/EPOXY LAMINATES

    Article • Jurnal Teknologi (Sciences & Engineering), October 2016, Penerbit UTM Press

    Dr.ir. René C Alderliesten

  111. Online Remaining Fatigue Life Prognosis for Composite Materials Based on Strain Data and Stochastic Modeling

    Article • Key Engineering Materials, September 2016, Trans Tech Publications

    Dr.ir. René C Alderliesten

  112. Reliability modelling for rotorcraft component fatigue life prediction with assumed usage

    Article • The Aeronautical Journal, July 2016, Cambridge University Press

    Dr.ir. René C Alderliesten

  113. Fatigue crack growth in residual stress fields

    Article • International Journal of Fatigue, June 2016, Elsevier

    Dr.ir. René C Alderliesten

  114. The effect of fibre bridging on the Paris relation for mode I fatigue delamination growth in composites

    Article • Composite Structures, April 2016, Elsevier

    Dr.ir. René C Alderliesten

  115. A brief discussion on (pure mode I) fatigue crack growth rate data in 5HS weave fabric composites: Evaluation of empirical relations

    Article • International Journal of Fatigue, March 2016, Elsevier

    Dr.ir. René C Alderliesten

  116. Predicting the paths of fatigue cracks in alloys with anisotropic crack resistance

    Article • January 2016, American Institute of Aeronautics and Astronautics (AIAA)

    ir Sjoerd O van der Veen, Dr.ir. René C Alderliesten

  117. Characterising resistance to fatigue crack growth in adhesive bonds by measuring release of strain energy

    Article • Procedia Structural Integrity, January 2016, Elsevier

    Dr.ir. René C Alderliesten

  118. How proper similitude can improve our understanding of crack closure and plasticity in fatigue

    Article • International Journal of Fatigue, January 2016, Elsevier

    Dr.ir. René C Alderliesten

  119. Interpreting the stress ratio effect on delamination growth in composite laminates using the concept of fatigue fracture toughness

    Article • Composites Part A Applied Science and Manufacturing, November 2015, Elsevier

    Dr.ir. René C Alderliesten

  120. The effect of disbonds on stability aspects of adhesively bonded aluminum panels during compression loading

    Article • Thin-Walled Structures, November 2015, Elsevier

    Dr.ir. René C Alderliesten

  121. The relationship between pure delamination modes I and II on the crack growth rate process in cracked lap shear specimen (CLS) of 5 harness satin composites

    Article • Composites Part A Applied Science and Manufacturing, November 2015, Elsevier

    Dr.ir. René C Alderliesten

  122. Finite Element Modeling of Fatigue in Fiber–Metal Laminates

    Article • AIAA Journal, August 2015, American Institute of Aeronautics and Astronautics (AIAA)

    Dr.ir. René C Alderliesten

  123. The relation between the strain energy release in fatigue and quasi-static crack growth

    Article • Engineering Fracture Mechanics, August 2015, Elsevier

    Dr.ir. René C Alderliesten

  124. Predicting the influence of discretely notched layers on fatigue crack growth in fibre metal laminates

    Article • Engineering Fracture Mechanics, August 2015, Elsevier

    Dr.ir. René C Alderliesten

  125. Effect of stress ratio or mean stress on fatigue delamination growth in composites: Critical review

    Article • Composite Structures, June 2015, Elsevier

    Dr.ir. René C Alderliesten

  126. Lay-up optimisation of fibre metal laminates based on fatigue crack propagation and residual strength

    Article • Composite Structures, June 2015, Elsevier

    Dr.ir. René C Alderliesten

  127. Design optimisation procedure for fibre metal laminates based on fatigue crack initiation

    Article • Composite Structures, February 2015, Elsevier

    Dr.ir. René C Alderliesten

  128. Designing for damage tolerance in aerospace: A hybrid material technology

    Article • Materials & Design (1980-2015), February 2015, Elsevier

    Dr.ir. René C Alderliesten

  129. A review of T-stress and its effects in fracture mechanics

    Article • Engineering Fracture Mechanics, January 2015, Elsevier

    Dr.ir. René C Alderliesten

  130. Exploring the option of fatigue life improvement of aluminium AA2024 via dynamic precipitation in the under-aged state

    Article • January 2015, IOS Press

    Dr.ir. René C Alderliesten

  131. On the relationship between disbond growth and the release of strain energy

    Article • Engineering Fracture Mechanics, January 2015, Elsevier

    Dr.ir. René C Alderliesten

  132. Predicting fatigue crack initiation in fibre metal laminates based on metal fatigue test data

    Article • International Journal of Fatigue, January 2015, Elsevier

    Dr.ir. René C Alderliesten

  133. Crack closure and fibre bridging during delamination growth in carbon fibre/epoxy laminates under mode I fatigue loading

    Article • Composites Part A Applied Science and Manufacturing, December 2014, Elsevier

    Dr.ir. René C Alderliesten

  134. Discussion on the use of the strain energy release rate for fatigue delamination characterization

    Article • Composites Part A Applied Science and Manufacturing, November 2014, Elsevier

    Dr.ir. René C Alderliesten

  135. Two-parameter model for delamination growth under mode I fatigue loading (Part A: Experimental study)

    Article • Composites Part A Applied Science and Manufacturing, October 2014, Elsevier

    Dr.ir. René C Alderliesten

  136. Two-parameter model for delamination growth under mode I fatigue loading (Part B: Model development)

    Article • Composites Part A Applied Science and Manufacturing, October 2014, Elsevier

    Dr.ir. René C Alderliesten

  137. Investigation of the response of an aluminium plate subjected to repeated low velocity impact using a continuum damage mechanics approach

    Article • Fatigue & Fracture of Engineering Materials & Structures, September 2014, Wiley

    Rahmatollah Ghajar, Dr.ir. René C Alderliesten

  138. Applicability of standard delamination tests (double cantilever beam and end notch flexure) for 5HS fabric-reinforced composites in weft-dominated surface

    Article • Journal of Composite Materials, September 2014, SAGE Publications

    Dr.ir. René C Alderliesten

  139. Bridging effect on mode I fatigue delamination behavior in composite laminates

    Article • Composites Part A Applied Science and Manufacturing, August 2014, Elsevier

    Dr.ir. René C Alderliesten

  140. Modelling of impact damage and dynamics in fibre-metal laminates – A review

    Article • International Journal of Impact Engineering, May 2014, Elsevier

    Dr.ir. René C Alderliesten

  141. Fatigue Crack Growth Rate in Mode I of a Carbon Fiber 5HS Weave Composite Laminate Processed via RTM

    Article • Advanced Materials Research, March 2014, Trans Tech Publications

    Dr.ir. René C Alderliesten

  142. The Explanation of Stress Ratio Effect and Crack Opening Corrections for Fatigue Crack Growth in Metallic Materials

    Article • Advanced Materials Research, March 2014, Trans Tech Publications

    Dr.ir. René C Alderliesten

  143. Postponing Crack Nucleation in 2024 Aluminium Alloy by Dynamic Precipitation from the Supersaturated State

    Article • Advanced Materials Research, March 2014, Trans Tech Publications

    Dr.ir. René C Alderliesten

  144. On the Development of a Prediction Methodology for Crack Growth in Fibre Metal Laminates with MSD Scenario

    Article • Advanced Materials Research, March 2014, Trans Tech Publications

    Dr.ir. René C Alderliesten

  145. The effect of impact energy division over repeated low-velocity impact on fiber metal laminates

    Article • Journal of Composite Materials, February 2014, SAGE Publications

    Dr.ir. René C Alderliesten

  146. Towards Understanding Fatigue Disbond Growth via Cyclic Strain Energy

    Article • Procedia Materials Science, January 2014, Elsevier

    Dr.ir. René C Alderliesten

  147. Critical review on the assessment of fatigue and fracture in composite materials and structures

    Article • Engineering Failure Analysis, December 2013, Elsevier

    Dr.ir. René C Alderliesten

  148. Low-velocity impact energy partition in GLARE

    Article • Mechanics of Materials, November 2013, Elsevier

    Dr.ir. René C Alderliesten

  149. Methods for the prediction of fatigue delamination growth in composites and adhesive bonds – A critical review

    Article • Engineering Fracture Mechanics, November 2013, Elsevier

    Dr.ir. René C Alderliesten

  150. Crack paths in fibre metal laminates: Role of fibre bridging

    Article • Engineering Fracture Mechanics, August 2013, Elsevier

    Dr.ir. René C Alderliesten

  151. Effect of interference fitting and/or bolt clamping on the fatigue behavior of Al alloy 2024-T3 double shear lap joints in different cyclic load ranges

    Article • International Journal of Mechanical Sciences, July 2013, Elsevier

    Dr.ir. René C Alderliesten

  152. A generalized solution to the crack bridging problem of fiber metal laminates

    Article • Engineering Fracture Mechanics, June 2013, Elsevier

    Dr.ir. René C Alderliesten

  153. An integrated study on the low-velocity impact response of the GLARE fibre-metal laminate

    Article • Composite Structures, June 2013, Elsevier

    Dr.ir. René C Alderliesten

  154. Experimental investigation on distance effects in repeated low velocity impact on fiber–metal laminates

    Article • Composite Structures, May 2013, Elsevier

    Dr.ir. René C Alderliesten

  155. Analytical prediction of Mode I stress intensity factors for cracked panels containing bonded stiffeners

    Article • Engineering Fracture Mechanics, January 2013, Elsevier

    Dr.ir. René C Alderliesten

  156. Fatigue life estimation of bolt clamped and interference fitted-bolt clamped double shear lap joints using multiaxial fatigue criteria

    Article • Materials & Design (1980-2015), January 2013, Elsevier

    Dr.ir. René C Alderliesten

  157. Fractographic Observations on the Mechanism of Fatigue Crack Growth in Aluminium Alloys

    Article • January 2013, Springer Science + Business Media

    Dr.ir. René C Alderliesten

  158. Impact resistance of fiber-metal laminates: A review

    Article • International Journal of Impact Engineering, November 2012, Elsevier

    Dr.ir. René C Alderliesten

  159. Fractographic Observations on the Mechanism of Fatigue Crack Growth in Aluminium Alloys

    Article • October 2012, Wiley

    Dr.ir. René C Alderliesten

  160. Mechanistic Approach towards Fatigue Initiation and Damage Propagation in Fibre Metal Laminates & Hybrid Materials

    Article • October 2012, Wiley

    Dr.ir. René C Alderliesten

  161. Applicability of AZ31B-H24 magnesium in Fibre Metal Laminates – An experimental impact research

    Article • Composites Part A Applied Science and Manufacturing, September 2012, Elsevier

    Dr.ir. René C Alderliesten

  162. Effect of residual stresses on crack behaviour in single edge bending specimens

    Article • Fatigue & Fracture of Engineering Materials & Structures, June 2012, Wiley

    Dr.ir. René C Alderliesten

  163. Development of fibre-metal laminates for improved impact performance

    Article • The European Physical Journal Special Topics, May 2012, Springer Science + Business Media

    Dr.ir. René C Alderliesten

  164. Numerical and experimental investigations of effects of residual stresses on crack behavior in Aluminum 6082-T6

    Article • Proceedings of the Institution of Mechanical Engineers Part C Journal of Mechanical Engineering Science, January 2012, SAGE Publications

    Dr.ir. René C Alderliesten

  165. Damage evolution in GLARE fibre-metal laminate under repeated low-velocity impact tests

    Article • Open Engineering, January 2012, De Gruyter

    Dr.ir. René C Alderliesten

  166. Fatigue Behavior of Fiber/Metal Laminate Panels Containing Internal Carbon Tear Straps

    Article • Journal of Aircraft, November 2011, American Institute of Aeronautics and Astronautics (AIAA)

    Dr.ir. René C Alderliesten

  167. Experimental and Numerical Investigation of Metal Type and Thickness Effects on the Impact Resistance of Fiber Metal Laminates

    Article • Applied Composite Materials, October 2011, Springer Science + Business Media

    Dr.ir. René C Alderliesten

  168. Delamination in Fiber Metal Laminates (GLARE) during fatigue crack growth under variable amplitude loading

    Article • International Journal of Fatigue, September 2011, Elsevier

    Dr.ir. René C Alderliesten

  169. Predicting the influence of temperature on fatigue crack propagation in Fibre Metal Laminates

    Article • Engineering Fracture Mechanics, July 2011, Elsevier

    Dr.ir. René C Alderliesten

  170. Thermotropic liquid crystalline polymers as protective coatings for aerospace

    Article • Progress in Organic Coatings, April 2011, Elsevier

    Theo Dingemans, Dr.ir. René C Alderliesten

  171. Macro and microscopic observations of fatigue crack growth in friction stir welded aluminum joints

    Article • Engineering Fracture Mechanics, April 2011, Elsevier

    Dr.ir. René C Alderliesten

  172. Evaluating the fatigue initiation location in friction stir welded AA2024-T3 joints

    Article • International Journal of Fatigue, March 2011, Elsevier

    Dr.ir. René C Alderliesten

  173. Misinterpreting the results: How similitude can improve our understanding of fatigue delamination growth

    Article • Composites Science and Technology, January 2011, Elsevier

    Dr.ir. René C Alderliesten

  174. The generation of deformation damage during fatigue loading in Al-Cu alloy studied by the Doppler Broadening technique

    Article • Journal of Physics Conference Series, January 2011, Institute of Physics Publishing

    Dr.ir. René C Alderliesten

  175. Fatigue initiation behaviour throughout friction stir welded joints in AA2024-T3

    Article • International Journal of Fatigue, December 2010, Elsevier

    Dr.ir. René C Alderliesten

  176. Crack-Tip Behavior in Fiber/Metal Laminates by Means of Digital-Image Correlation

    Article • Journal of Aircraft, September 2010, American Institute of Aeronautics and Astronautics (AIAA)

    Dr.ir. René C Alderliesten

  177. Yield Strength and Residual Stress Measurements on Friction-Stir-Welded Aluminum Alloys

    Article • Journal of Aircraft, September 2010, American Institute of Aeronautics and Astronautics (AIAA)

    Dr.ir. René C Alderliesten

  178. Discussion on “Modeling of fatigue crack growth in notched fibre metal laminates” by Po-Yu Chang and Jenn-Ming Yang [Int. J. Fatigue 30 (2008) 2165–2174]

    Article • International Journal of Fatigue, August 2010, Elsevier

    Dr.ir. René C Alderliesten

  179. Fatigue crack paths in AA2024-T3 when loaded with constant amplitude and simple underload spectra

    Article • Engineering Fracture Mechanics, July 2010, Elsevier

    Dr.ir. René C Alderliesten

  180. Application of a modified Wheeler model to predict fatigue crack growth in Fibre Metal Laminates under variable amplitude loading

    Article • Engineering Fracture Mechanics, June 2010, Elsevier

    Dr.ir. René C Alderliesten

  181. Experimental characterization of the crack-tip-opening angle in fibre metal laminates

    Article • Engineering Fracture Mechanics, April 2010, Elsevier

    Dr.ir. René C Alderliesten

  182. Delamination growth in Fibre Metal Laminates under variable amplitude loading

    Article • Composites Science and Technology, December 2009, Elsevier

    Dr.ir. René C Alderliesten

  183. Linear Damage Accumulation for Predicting Fatigue in Fiber Metal Laminates

    Article • Journal of Aircraft, September 2009, American Institute of Aeronautics and Astronautics (AIAA)

    Dr.ir. René C Alderliesten

  184. International conference on damage tolerance of aircraft structures

    Article • International Journal of Fatigue, June 2009, Elsevier

    Dr.ir. René C Alderliesten

  185. Damage tolerance of bonded aircraft structures

    Article • International Journal of Fatigue, June 2009, Elsevier

    Dr.ir. René C Alderliesten

  186. Characterization of the Crack Tip Behavior in Fibre Metal Laminates by Means of Digital Image Correlation

    Article • May 2009, American Institute of Aeronautics and Astronautics (AIAA)

    Dr.ir. René C Alderliesten

  187. Steady State Crack Growth Prediction Method for Glare and Advanced FMLs

    Article • May 2009, American Institute of Aeronautics and Astronautics (AIAA)

    Dr.ir. René C Alderliesten

  188. Damage tolerance assessment by bend and shear tests of two multilayer composites: Glass fibre reinforced metal laminate and aluminium roll-bonded laminate

    Article • Composites Science and Technology, March 2009, Elsevier

    Dr.ir. René C Alderliesten

  189. Fatigue crack growth in fibre metal laminates under selective variable‐amplitude loading

    Article • Fatigue & Fracture of Engineering Materials & Structures, March 2009, Wiley

    Dr.ir. René C Alderliesten

  190. Post-stretching induced stress redistribution in Fibre Metal Laminates for increased fatigue crack growth resistance

    Article • Composites Science and Technology, March 2009, Elsevier

    Dr.ir. René C Alderliesten

  191. Assessing the effects of riveting induced residual stresses on fatigue crack behaviour in lap joints by means of fractography

    Article • International Journal of Fatigue, February 2009, Elsevier

    Dr.ir. René C Alderliesten

  192. The meaning of threshold fatigue in fibre metal laminates

    Article • International Journal of Fatigue, February 2009, Elsevier

    Dr.ir. René C Alderliesten

  193. Practical Applications of Improvements in Fml Crack Bridging Theory

    Article • January 2009, Springer Science + Business Media

    Dr.ir. René C Alderliesten

  194. An Experimental Approach to Investigate Detailed Failure Mechanisms in Fibre Metal Laminates

    Article • January 2009, Springer Science + Business Media

    Dr.ir. René C Alderliesten

  195. On the Development of Hybrid Material Concepts for Aircraft Structures

    Article • Recent Patents on Engineering, January 2009, Bentham Science Publishers

    Dr.ir. René C Alderliesten

  196. Hybrid Structures for Concentrated Load Transmission in Fibre Composites: Initial Experiments

    Article • January 2009, Springer Science + Business Media

    Dr.ir. René C Alderliesten

  197. The applicability of magnesium based Fibre Metal Laminates in aerospace structures

    Article • Composites Science and Technology, November 2008, Elsevier

    Dr.ir. René C Alderliesten

  198. Fiber/Metal Composite Technology for Future Primary Aircraft Structures

    Article • Journal of Aircraft, July 2008, American Institute of Aeronautics and Astronautics (AIAA)

    Dr.ir. René C Alderliesten

  199. On crack tunneling and plane-strain delamination in laminates

    Article • International Journal of Fracture, December 2007, Springer Science + Business Media

    Dr.ir. René C Alderliesten

  200. Modelling cyclic shear deformation of fibre/epoxy layers in fibre metal laminates

    Article • Composites Science and Technology, September 2007, Elsevier

    Dr.ir. René C Alderliesten

  201. Crack closure in fibre metal laminates

    Article • Fatigue & Fracture of Engineering Materials & Structures, June 2007, Wiley

    Dr.ir. René C Alderliesten

  202. Fiber/Metal composite technology for future primary aircraft structures

    Article • April 2007, American Institute of Aeronautics and Astronautics (AIAA)

    Dr.ir. René C Alderliesten

  203. Effects of Rivet Installation on Residual Stresses and Secondary Bending Stresses in a Riveted Lap Joint

    Article • April 2007, American Institute of Aeronautics and Astronautics (AIAA)

    Dr.ir. René C Alderliesten

  204. Analytical prediction model for fatigue crack propagation and delamination growth in Glare

    Article • International Journal of Fatigue, April 2007, Elsevier

    Dr.ir. René C Alderliesten

  205. On the available relevant approaches for fatigue crack propagation prediction in Glare

    Article • International Journal of Fatigue, February 2007, Elsevier

    Dr.ir. René C Alderliesten

  206. Riveting Process Induced Residual Stresses Around Solid Rivets in Mechanical Joints

    Article • Journal of Aircraft, January 2007, American Institute of Aeronautics and Astronautics (AIAA)

    Dr.ir. René C Alderliesten

  207. Fatigue and damage tolerance issues of Glare in aircraft structures

    Article • International Journal of Fatigue, October 2006, Elsevier

    Dr.ir. René C Alderliesten

  208. Application of the energy release rate approach for delamination growth in Glare

    Article • Engineering Fracture Mechanics, April 2006, Elsevier

    Dr.ir. René C Alderliesten

  209. Fatigue crack growth prediction in GLARE hybrid laminates

    Article • Composites Science and Technology, September 2003, Elsevier

    Dr.ir. René C Alderliesten

  210. Fatigue and Damage Tolerance of Glare

    Article • Applied Composite Materials, July 2003, Springer Science + Business Media

    Dr.ir. René C Alderliesten

  211. Fibre metal laminates: a state of the art

    Article • International Journal of Materials and Product Technology, January 2002, Inderscience Publishers

    Dr.ir. René C Alderliesten

  212. Fatigue

    Article • January 2001, Springer Science + Business Media

    Dr.ir. René C Alderliesten