Semi-Discrete Model for Progressive Damage and Failure of Fiber Reinforced Laminates | Anthony Waas

:collision: Expert Lecture Spotlight | Prof. Anthony Waas
Semi-Discrete Model for Progressive Damage and Failure of Fiber Reinforced Laminates

As carbon fiber-reinforced polymer (CFRP) composites become essential for primary load-bearing structures across aerospace, automotive, and energy sectors, engineers face increasing pressure to deliver robust, predictive models for their complex failure behavior.

In this lecture, Prof. Anthony Waas introduces a novel, semi-discrete modeling framework for capturing the progressive damage and failure of CFRP laminates—offering both computational efficiency and physical fidelity.

:magnifying_glass_tilted_left: Key damage mechanisms addressed include:

  • Intralaminar matrix cracking, which weakens individual plies
  • Interlaminar delamination, the out-of-plane separation between adjacent plies
  • Interaction effects, where matrix cracks trigger or accelerate delamination

The talk begins with experimental evidence that delineates these mechanisms, followed by the introduction of a semi-discrete progressive damage model that integrates:
:small_orange_diamond: ASTM-based Mode I, Mode II, and mixed-mode fracture data
:small_orange_diamond: Finite Element Analysis (FEA) for structural response prediction
:small_orange_diamond: An efficient framework for simulating damage evolution and failure interaction

The resulting model offers a powerful tool for evaluating the structural integrity and damage tolerance of CFRP components under realistic loading conditions—bridging the gap between material testing and structural design.

:television: Now streaming on the cdmHUB YouTube channel as part of the Global Composites Expert Webinar Series.