Numerical Simulation of Compressive Residual Strength for Damaged Composite Laminates

Tian Jiao Qu; Xi Tao Zheng; Di Zhang

doi:10.4028/www.scientific.net/KEM.525-526.385

Paper Titles

Experimental Study on Residual Strength of Panels with Multiple Site Damage
p.369

Damage Analysis of 2D Woven Composite Laminates Containing an Open-Hole under Tensile Loadings
p.373

A New Approach to Determine Dynamic Strength Model Parameters under Taylor Impact Test
p.377

A Novel Testing Method for Measuring Through-Thickness Properties of Thick Composite Laminates
p.381

Numerical Simulation of Compressive Residual Strength for Damaged Composite Laminates
p.385

A Research on Characterization for Damage Tolerance of Composite Laminates
p.389

The Simulation of Low-Velocity Impact on Composite Laminates with the Damage Model Based on Strain
p.393

Investigation into Damage of Stainless Steel Mesh/ALPlate Multi-Shock Shield under Hypervelocity AL-Spheres Impact
p.397

Numerical Simulation of Hypervelocity Impact on Mesh Bumper Causing Fragmentation and Ejection
p.401

HomeKey Engineering MaterialsKey Engineering Materials Vols. 525-526Numerical Simulation of Compressive Residual...

Numerical Simulation of Compressive Residual Strength for Damaged Composite Laminates

Abstract:

After the low-velocity impact test of composite laminates of T800/BA9916, CAI test and compression test of laminates with a hole have been carried out. Two types of models were set up by the finite element software ABAQUS respectively. The FEA results were good agreement with the testing results. The investigation of models with a hole indicates that the appearance time of ultimate compressive load is earlier than that of fiber breakage expanding to boundary. Moreover, the diameter and the depth of blind hole significantly influence the ultimate compressive load.

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Periodical:

Key Engineering Materials (Volumes 525-526)

Pages:

385-388

DOI:

https://doi.org/10.4028/www.scientific.net/KEM.525-526.385

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Online since:

November 2012

Authors:

Tian Jiao Qu, Xi Tao Zheng, Di Zhang

Keywords:

Compressive Test, Finite Element Analysis (FEA), Impact, Ultimate Compressive Load

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References

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