Modelling damage evolution in composite laminates subjected to low velocity impact

By Yu Shi, T. Swait, Constantinos Soutis. 2012

664 citations recorded by the source corpus.

Subfields: Mechanical Engineering, Mechanics of Materials

View Paper: https://www.semanticscholar.org/paper/7ac6b8d7370b1912a13a634e020ae8f825da2e07

How researchers see this paper

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

In Mechanical Engineering

1. Guangyong Sun
2. Qing Li
3. Wei Tan
4. Dongdong Chen
5. N. Hongkarnjanakul
6. M. Saeedifar
7. Mehdi Ahmadi Najafabadi
8. C. Bouvet

In Mechanics of Materials

1. Guangyong Sun
2. Wei Tan
3. Qing Li
4. N. Hongkarnjanakul
5. Dongdong Chen
6. S. Rivallant
7. C. Bouvet
8. M. Saeedifar

Citations in the corpus

• Assessment of failure criteria and damage evolution methods for composite laminates under low-velocity impact (2019, background): “on fracture energy, which are typical of semi-empirical methods, are now widely employed by researchers for predicting the progressive damage behavior of composite materials [4-7,17-22].”
• Validation of low velocity impact modelling on different stacking sequences of CFRP laminates and influence of fibre failure (2013, background): “Then, V and S can be reduced in terms of an internal element length l, which is comparable to the FE characteristic length [7] [8] [10] to make FE model mesh-size independent.”
• Barely visible impact damage assessment in laminated composites using acoustic emission (2018, background): “Fiber Reinforced Polymer (FRP) composites have key advantages such as high specific strength and stiffness, high corrosion resistance, and high fatigue life [1,2].”
• Experimental and numerical studies on the impact response of damage-tolerant hybrid unidirectional/woven carbon-fibre reinforced composite laminates (2018, neutral): “Y. Shi et al. [16,17] used stress-based criteria and fracture mechanics techniques to capture composite laminate damage initiation and evolution of damage during an impact event.”
• Failure analysis of CFRP laminates subjected to compression after impact: FE simulation using discrete interface elements (2013, methodology): “Then, V and S can be reduced in terms of an internal element length l, which is comparable to the FE characteristic length used in [27,28] to make FE model mesh size independent.”
• Low velocity impact behavior of interlayer hybrid composite laminates with carbon/glass/basalt fibres (2019, background): “cracking and delamination as cohesive elements [20] and spring elements [8].”
• Low velocity impact modeling in composite laminates capturing permanent indentation (2012, neutral): “[15]: impacted side (a) and through the thickness (b).”