• René Alderliesten
Part of the Solid Mechanics and Its Applications book series (SMIA, volume 236)


Historically, Fibre Metal Laminates were introduced as a laminated material concept to improve the fatigue and damage tolerance properties of metallic structures in aeronautics. However, the concept can be viewed from different perspectives. This chapter discusses that the FML concept can be seen either as reinforcement of metallic structures or as reinforcement of fibre-reinforced polymer composite structures. Cases are given to illustrate how the concept of damage tolerance can be exploited with FMLs, in particular if the concept is viewed as structural concept rather than a material concept.


Fatigue Crack Growth Damage Tolerance Crack Growth Resistance Fibre Reinforce Polymer Composite Fatigue Crack Growth Resistance 
These keywords were added by machine and not by the authors. This process is experimental and the keywords may be updated as the learning algorithm improves.


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Copyright information

© Springer International Publishing AG 2017

Authors and Affiliations

  • René Alderliesten
    • 1
  1. 1.Faculty of Aerospace EngineeringDelft University of TechnologyDelftThe Netherlands

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