Abstract

This study details and demonstrates a strain-based criterion for the prediction of polymer matrix composite material damage and failure under shock loading conditions. Shock loading conditions are characterized by high-speed impacts or explosive events that result in very high pressures in the materials involved. These material pressures can reach hundreds of kbar and often exceed the material strengths by several orders of magnitude. Researchers have shown that under these high pressures, composites exhibit significant increases in stiffness and strength. In this work we summarize modifications to a previous stress based interactive failure criterion based on the model initially proposed by Hashin, to include strain dependence. The failure criterion is combined with the multi-constituent composite constitutive model (MCM) within a shock physics hydrocode. The constitutive model allows for decomposition of the composite stress and strain fields into the individual phase averaged constituent level stress and strain fields, which are then applied to the failure criterion. Numerical simulations of a metallic sphere impacting carbon/epoxy composite plates at velocities up to 1000 m/s are performed using both the stress and strain based criterion. These simulation results are compared to experimental tests to illustrate the advantages of a strain-based criterion in the shock environment.

Highlights

  • Composite materials are often used in shock loading applications caused by high-velocity impacts, where the strain rates can reach on the order of 107 and the pressures are often in the hundreds of kbar

  • The deviatoric or distortional response of the material is modeled with a constitutive model, while the volumetric (P) response is modeled using an equation of state (EOS)

  • The work presented in this paper utilizes the shock physics hydrocode CTH [1] to model unidirectional composite materials under high velocity impacts where the pressures can reach very high levels

Read more

Summary

Introduction

Composite materials are often used in shock loading applications caused by high-velocity impacts, where the strain rates can reach on the order of 107 and the pressures are often in the hundreds of kbar. This data shows a nearly 2 times increase in the matrix dominated failure modes of the material as a result of the applied pressure being increased from standard atmospheric conditions to 6 kbar. These observations lead to the suggestion that a deformation or strain-based criterion may be more suitable for shock loading problems. We briefly outline the composite material constitutive model and the equation of state model used for these initial studies We detail both the stress and strain-based failure criterion used along with the experimental test details used to support that analytical work. We compare the results of the two failure criterion against the experimental test results of a carbonepoxy panel subjected to spherical projectile impacts

Constitutive model
Equation of state coupling
Failure criteria
Stress-based failure criterion
Strain-based failure criterion
Experimental testing details
Numerical model details
Results
Conclusions
Full Text
Published version (Free)

Talk to us

Join us for a 30 min session where you can share your feedback and ask us any queries you have

Schedule a call