Study on Delamination Propagation Behavior and Measurement Method for One Kind of New Fiber Metal Laminates

Xiao Huang; Jian Zhong Liu

doi:10.4028/www.scientific.net/AMR.538-541.1773

Paper Titles

Study on the Crack Extension Properties under Ultrasonic Vibration Uniaxial Tensile Load
p.1751

Mechanics Analysis of Reinforcing Rib Structure in Aluminum Heating-Plate Automatic Casting System
p.1755

Structural Behavior of a New GSZ Panel under Lateral Loads
p.1762

A Study of Hydraulic Jet Fracturing in Shallow Reservoir
p.1769

Study on Delamination Propagation Behavior and Measurement Method for One Kind of New Fiber Metal Laminates
p.1773

Investigation on Wall Thinning and Creep Damage in Boiler Tube due to Scale Formation
p.1781

Inspection and Evaluation of Load-Bearing Capacity of Single Tower Composite Girder Cable-Stayed Bridge
p.1785

Orthogonal Test Research on Compressive Strength Size Effect of ECC
p.1789

Mechanical Property Test Study on Composite Board Box
p.1796

HomeAdvanced Materials ResearchAdvanced Materials Research Vols. 538-541Study on Delamination Propagation Behavior and...

Study on Delamination Propagation Behavior and Measurement Method for One Kind of New Fiber Metal Laminates

Abstract:

The delamination at the interface between the aluminium and prepreg layers has greater influence on the fatigue crack growth in fiber metal laminates. To study delamination propagation property of one kind of new fiber metal laminates, by using 2/1 lay-up specimen, this article accomplished delamination propagation test under various stress levels at R=0.1 by optical method and compliance method respectively. The delamination propagation property of this laminate is obtained by analyzing and calculating. A modified compliance equation is created to calculate the delamination size of this laminate more accurately by adding a non-dimensional factor.

You might also be interested in these eBooks

View Preview

Info:

Periodical:

Advanced Materials Research (Volumes 538-541)

Pages:

1773-1780

DOI:

https://doi.org/10.4028/www.scientific.net/AMR.538-541.1773

Citation:

Cite this paper

Online since:

June 2012

Authors:

Xiao Huang, Jian Zhong Liu

Keywords:

Compliance Method, Delamination, Energy Release Rate, Fiber-Metal Laminate (FML)

Export:

RIS, BibTeX

Price:

Permissions CCC:

Request Permissions

Permissions PLS:

Request Permissions

Сopyright:

Citation:

References

[1] J. Schijve: Fatigue of Structures and Materials (Springer, Netherlands 2008).

Google Scholar

[2] A. Vlot, J.W. Gunnink. Fibre Metal Laminates, an introduction. (Kluwer Academic Publishers, Netherlands 2001).

Google Scholar

[3] R. Marissen. Fatigue Crack Growth in ARALL, A hybrid Aluminium-Aramid Composite Material, crack growth mechanisms and quantitative predictions of the crack growth rate. PhD Thesis, Delft University of Technology, 1988.

DOI: 10.2514/3.45553

Google Scholar

[4] A.S.J. Suiker, N.A. Fleck. International Journal of Fracture, 2004, 125: 1-32.

Google Scholar

[5] R.C. Alderliesten. Fatigue Crack Propagation and Delamination Growth in Glare. PhD Thesis, Delft University of Technology, 2005.

Google Scholar

[6] Y.J. Guo, X.R. Wu, Z.L. Zhang. Fatigue and Fracture of Engineering Materials and Structures, 1997, 20: 1699-1708.

Google Scholar

[7] R.C. Alderliesten. International Journal of Fatigue, 2007, 29: 628–646.

Google Scholar

[8] R.C. Alderliesten, J. Schijve, van der Zwaag. Engineering Fracture Mechanics, 2006, 73:697-709.

DOI: 10.1016/j.engfracmech.2005.10.006

Google Scholar

[9] S. Oken, R.R. June. Analytical and Experimental Investigation of Aircraft Metal Structures Reinforced with Filamentary Composites. NASA CR 1895, 1977.

Google Scholar