Validation of low velocity impact modelling on different stacking sequences of CFRP laminates and influence of fibre failure

By N. Hongkarnjanakul, C. Bouvet, S. Rivallant. 2013

270 citations recorded by the source corpus.

Subfields: Building and Construction, Mechanical Engineering, Mechanics of Materials

View Paper: https://www.semanticscholar.org/paper/c346ddd9e7acad1817f2a34e3eb464e6c08b5ec2

How researchers see this paper

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

In Building and Construction

1. Brian G. Falzon
2. Qing Li
3. Tong Earn Tay
4. Wei Tan
5. M. Ridha
6. B. Chen

In Mechanical Engineering

1. Guangyong Sun
2. Qing Li
3. Dongdong Chen
4. Brian G. Falzon
5. Tong Earn Tay
6. Louis N. S. Chiu
7. Mark Price
8. Wei Tan

In Mechanics of Materials

1. Guangyong Sun
2. Qing Li
3. M. Ridha
4. Dongdong Chen
5. Wei Tan
6. Vincent B. C. Tan
7. B. Chen
8. Chao Zhang

Citations in the corpus

• Predicting low velocity impact damage and Compression-After-Impact (CAI) behaviour of composite laminates (2015, methodology): “Material properties for T700/M21 [20,12] 3.”
• 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].”
• Experimental and numerical studies on the impact response of damage-tolerant hybrid unidirectional/woven carbon-fibre reinforced composite laminates (2018, unknown): “Based on the non-destructive inspection and microscopic examination results, no delamination was found at the interface between blocked plies with the same fibre orientation [8].”
• Low velocity impact behavior of interlayer hybrid composite laminates with carbon/glass/basalt fibres (2019, background): “As reported in [46], every two adjacent plies were considered as a single layer and SC8R element was chosen in order to reduce the computation cost.”
• On cohesive element parameters and delamination modelling (2019, background): “5 × 10(4) Sun [65] IM7/8552 Impact 60/90 60/90 McElroy [87] IM7/8552 Impact 129/93 129/93 Bouvet [88] T700/M21 Impact 50/90 50/90 10(6) Hongkarnjanakul [41] T700/M21 Impact 60/110 60/110 Abir [42] T700/M21 Impact 75/150 75/150 10(6) Zhi [73] Hexcel 913C Impact 60/105/105 10(6) Su [39] IM7/8552 OHC 6”