Low velocity impact and compression after impact tests on thin carbon/epoxy laminates

By D. Ghelli, G. Minak. 2011

216 citations recorded by the source corpus.

Subfields: Civil and Structural Engineering, Mechanical Engineering, Mechanics of Materials

View Paper: https://www.semanticscholar.org/paper/e7d2f06606a434889868b7375c3a10a231029252

How researchers see this paper

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

In Civil and Structural Engineering

1. S. Rivallant
2. C. Bouvet
3. N. Hongkarnjanakul
4. Wei Tan
5. Brian G. Falzon

In Mechanical Engineering

1. Wei Tan
2. Brian G. Falzon
3. Louis N. S. Chiu
4. Mark Price
5. N. Hongkarnjanakul
6. C. Bouvet
7. S. Rivallant

In Mechanics of Materials

1. Wei Tan
2. N. Hongkarnjanakul
3. Brian G. Falzon
4. Louis N. S. Chiu
5. Mark Price
6. S. Rivallant
7. C. Bouvet

Citations in the corpus

• Failure analysis of CFRP laminates subjected to compression after impact: FE simulation using discrete interface elements (2013, background): “…the final rupture of the plate in CAI are the same whatever the ply thickness and orientation within a relatively wide range: the combination of bending stress due to buckling and compressive stress concentration leading to fiber failure, as mentioned in a number of recent experimental works [37–40].”
• Predicting low velocity impact damage and Compression-After-Impact (CAI) behaviour of composite laminates (2015, background): “Ghelli and Minak [14] conducted CAI tests on thin laminates where interactions between the extent of impact damage and buckling mode shape were shown to influence the overall strength of the specimens.”