Impact Resistance Research of Composite Laminate Structure

Hong Peng Li; Shu Li; Fang Lue Huang

doi:10.4028/www.scientific.net/AMR.712-715.1045

Paper Titles

Numerical Simulation of Deflection Fracturing with Finite Element Method Considering Crack Initiation Angle
p.1027

Static Characteristics Research of Bed with Three-Point Support Using Bionics
p.1032

The Finite Element Analysis of Pile-Raft Foundation after Optimization of the Raft Thickness
p.1037

Stiffness Calculation of Boiler Horizontal Support
p.1041

Impact Resistance Research of Composite Laminate Structure
p.1045

Transmission Parameters Optimization Design and Load Factor Formula Fitting of WN Gears Drive
p.1050

Influence of Screw Spacing on the Strength of Self-Drilling Screw Connection for the High Strength Cold-Formed Steel
p.1054

Pressure Cooker with Composite Bottom Thermo-Mechanical Coupling Simulation
p.1058

Determination of Residual Fracture Toughness of Post-Fire Concrete
p.1062

HomeAdvanced Materials ResearchAdvanced Materials Research Vols. 712-715Impact Resistance Research of Composite Laminate...

Impact Resistance Research of Composite Laminate Structure

Abstract:

The composite material has been widely used in aircraft structures. But this kind of material has some shortage such as poor impact resistance, low residual compressive strength, which have a negative influence on the performance of aircraft structures. In this paper, simulations of low-velocity impact and compression process of composite laminates with AL ply and different core material has been done. The simulation results show that softer core materials and AL ply with certain thickness can improve the residual compressive strength

You might also be interested in these eBooks

Advances in Manufacturing Science and Engineering

View Preview

Info:

Periodical:

Advanced Materials Research (Volumes 712-715)

Pages:

1045-1049

DOI:

https://doi.org/10.4028/www.scientific.net/AMR.712-715.1045

Citation:

Cite this paper

Online since:

June 2013

Authors:

Hong Peng Li, Shu Li, Fang Lue Huang

Keywords:

Fiber-Metal Laminate (FML), Low Velocity Impact (LVI), Residual Compressive Strength, Sandwich Composite Laminate

Export:

RIS, BibTeX

Price:

Permissions CCC:

Request Permissions

Permissions PLS:

Request Permissions

Сopyright:

Citation:

References

[1] Zhen Shen. Xiaojing Zhang: Introduction to design and verification for composite aircraft structures (Shanghai Jiao Tong University Press, Shanghai 2011).

Google Scholar

[2] M.Meo, A.J. Morris, R.Vignjevic and G.Marengo: Composite structures. Forum Vol. 62 (2003), pp.353-360.

DOI: 10.1016/j.compstruct.2003.09.035

Google Scholar

[3] J.P. Hou, N.Petrinic, C.Ruiz and S.R. Hallett: Composites science and technology. Forum Vol. 60(2000), pp.273-281.

Google Scholar

[4] J.P. Hou, N.Petrinic, and C.Ruiz: Composites science and technology. Forum Vol. 61(2001), pp.2069-2074.

Google Scholar

[5] R. K. Luo: Composites science and technology. Forum Vol. 60(2000), pp.49-58.

Google Scholar