Finite Element and Experimental Study of the Fiber-Reinforced Composite Laminates under Low-Velocity Impact

Han Yang Liu; Xin Ming Qiu; Deng Yu Zhang; Yu Huai He; Jin Juan Fan

doi:10.4028/www.scientific.net/KEM.535-536.505

Paper Titles

Effect of Tensile Speed on the Failure Load of Laser Welding under Combined Loading Conditions
p.489

Elasticity Effect in Dynamic Response of Beams with Pre-Cracks Impinged by Striker
p.493

Experimental Research on Dynamic Mechanical Properties of 5083 Aluminum Alloy
p.497

Experimental Study of Sandwich Panels Subjected to Foam Projectile Impact
p.501

Finite Element and Experimental Study of the Fiber-Reinforced Composite Laminates under Low-Velocity Impact
p.505

Microstructure Evolution of Ti-46.5Al-2Nb-2Cr at Different Strain Rates and Temperatures
p.509

Numerical Studies on the Blast-Resistant Capacity of Stiffened Multiple-Arch Panel
p.514

Numerical Study of Round-Robin Tests on the Split Hopkinson Pressure Bar Technique
p.518

On the Strength Enhancement of Cellular Materials under Dynamic Loadings
p.522

HomeKey Engineering MaterialsKey Engineering Materials Vols. 535-536Finite Element and Experimental Study of the...

Finite Element and Experimental Study of the Fiber-Reinforced Composite Laminates under Low-Velocity Impact

Abstract:

Experimental and numerical studies of the 2D woven composite laminates under low-velocity impact with different energy are discussed in this paper. The traditional Hashin failure criteria are improved to cover the failure modes of fiber rupture and delamination. It is found that the damage level depend on the impact energy. The matrix deformation is the main reason of delamination. The simulating results are in good agreement with the experimental phenomenon observed by nondestructive examination (ultrasonic C scanning) and cross-section examination

You might also be interested in these eBooks

View Preview

Info:

Periodical:

Key Engineering Materials (Volumes 535-536)

Pages:

505-508

DOI:

https://doi.org/10.4028/www.scientific.net/KEM.535-536.505

Citation:

Cite this paper

Online since:

January 2013

Authors:

Han Yang Liu, Xin Ming Qiu, Deng Yu Zhang, Yu Huai He, Jin Juan Fan

Keywords:

2D Woven Composite Laminates, Delamination, Finite Element, Low Velocity Impact (LVI)

Export:

RIS, BibTeX

Price:

Permissions CCC:

Request Permissions

Permissions PLS:

Request Permissions

Сopyright:

Citation:

References

[1] Sun CT, Rechak S. Effect of adhesive layers on impact damage in composite laminates. Composite Materials Testing and Design (Eighth Conf) 1988;ASTM STP 972:97.

DOI: 10.1520/stp26130s

Google Scholar

[2] Liu D. Impact-induced delamination—a View of bending stiffness mismatching. J Compos Mater 1988;22:674.

DOI: 10.1177/002199838802200706

Google Scholar

[3] Hong S, Liu D. On the relationship between impact energy and delamination area. Exp Mech 1989;29:115.

Google Scholar

[4] Chang F, Chang K. A progressive damage model for laminated composites containing stress concentration. J Compos Mater 1987;21:834.

Google Scholar

[5] Tsai SW, Wu EM. A general theory of strength for anisotropic materials. J Compos Mater 1971;5:58.

Google Scholar

[6] Hou JP, Petrinic N, Ruiz C, Hallett SR. Prediction of impact damage in composite plates. Compos Sci Technol 2000;60:273.

DOI: 10.1016/s0266-3538(99)00126-8

Google Scholar

[7] Collombet F, Lalbin X, Lataillade JL. Impact behavior of laminated composites: Physical basis for finite element analysis. Compos Sci Technol 1998;58:463.

DOI: 10.1016/s0266-3538(97)00146-2

Google Scholar

[8] Zhen S. Experimental study on the compressive failure mechanisms of damaged composites laminates. Acta Aeronautica et Astronautica Sinica 1991;12:105.

Google Scholar