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  1. 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

  2. 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

  3. 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

  4. 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

  5. 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

  6. 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

  7. 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

  8. 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

  9. 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

  10. 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

  11. 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

  12. 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

  13. 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

  14. 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

  15. 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

  16. 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

  17. 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

  18. 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

  19. 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

  20. 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

  21. Thermotropic liquid crystalline polymers as protective coatings for aerospace

    Article • Progress in Organic Coatings, April 2011, Elsevier

    Theo Dingemans, Dr.ir. René C Alderliesten

  22. 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

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

    Article • Engineering Fracture Mechanics, April 2010, Elsevier

    Dr.ir. René C Alderliesten

  24. International conference on damage tolerance of aircraft structures

    Article • International Journal of Fatigue, June 2009, Elsevier

    Dr.ir. René C Alderliesten

  25. 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

  26. 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

  27. Practical Applications of Improvements in Fml Crack Bridging Theory

    Article • January 2009, Springer Science + Business Media

    Dr.ir. René C Alderliesten

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

    Article • January 2009, Springer Science + Business Media

    Dr.ir. René C Alderliesten

  29. 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

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

    Article • January 2009, Springer Science + Business Media

    Dr.ir. René C Alderliesten

  31. 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

  32. 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

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

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

    Dr.ir. René C Alderliesten

  34. 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

  35. 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

  36. Fatigue

    Article • January 2001, Springer Science + Business Media

    Dr.ir. René C Alderliesten