Modelling complex progressive failure in notched composite laminates with varying sizes and stacking sequences

By M. Ridha, Chun Hui Wang, B. Chen, Tong Earn Tay. 2014

159 citations recorded by the source corpus.

Subfields: Mechanics of Materials

View Paper: https://www.semanticscholar.org/paper/48ab2b8942767bfea7f404fb334a856a897a2807

How researchers see this paper

The researchers whose trusted networks rank it highest, strongest advocate first. Every researcher gets a different order.

In Mechanics of Materials

1. M. Ridha
2. B. Chen
3. Tong Earn Tay
4. Z. Su

Citations in the corpus

• Progressive damage modeling of open-hole composite laminates under compression (2015, methodology): “[18] developed a progressive damage model with in-plane damage and delamination between plies to predict the OHT strengths and failure progression for notched composite laminates with varying sizes and stacking sequences.”
• On cohesive element parameters and delamination modelling (2019, unknown): “Unlike the other previous cases, failure of OHT specimens consists of multiple delamination propagations at different interfaces and the interaction between matrix cracking and interface delamination may not be ignored.”