Show simple item record

dc.contributor.advisorNomura, Seiichi
dc.creatorKarimi, Behrooz
dc.date.accessioned2018-02-15T21:12:28Z
dc.date.available2018-02-15T21:12:28Z
dc.date.created2017-12
dc.date.issued2018-01-05
dc.date.submittedDecember 2017
dc.identifier.urihttp://hdl.handle.net/10106/27206
dc.description.abstractComposite materials fail for various reasons and extensive research has been conducted both experimentally and theoretically. However, theoretical prediction of composite failure by yielding seems scarce. Adding reinforcing elements to matrix significantly affects the structural behavior of composite materials. The inserted particles on one hand obstruct the progress of cracks and on the other hand cause stress concentration on the interface of the particle-matrix and eventually influence the ultimate strength of the material. In this research, we study the interface stresses and strength in particulate reinforced composites under uniform mechanical and thermal loading. We theoretically obtain failure envelopes for particulate reinforced composites. This is achieved by estimating the stress field in the matrix phase around a spheroidal particle in an unbounded matrix phase along with the self-consistent approximation that determines the effective elastic modulus of the composite. The failure envelopes are calculated on the basis of the maximum von Mises stress as a function of the applied far-field stresses or heat flow. We also discuss the effect of the particle volume fractions and the particle to matrix stiffness ratios on the interface stresses and ultimate yielding strength. Parametric analysis enables us to predict these envelopes for various loading conditions, volume fractions and particle to matrix stiffness ratios.
dc.format.mimetypeapplication/pdf
dc.language.isoen_US
dc.subjectFailure envelopes
dc.subjectParticulate reinforced
dc.subjectComposites
dc.subjectMicromechanics
dc.subjectYielding onset
dc.titleA MICROMECHNICS APPROACH TO PREDICTING THE ONSET YIELDING ENVELOPE OF PARTICULATE COMPOSITE MATERIALS
dc.typeThesis
dc.degree.departmentMechanical and Aerospace Engineering
dc.degree.nameDoctor of Philosophy in Mechanical Engineering
dc.date.updated2018-02-15T21:14:36Z
thesis.degree.departmentMechanical and Aerospace Engineering
thesis.degree.grantorThe University of Texas at Arlington
thesis.degree.levelDoctoral
thesis.degree.nameDoctor of Philosophy in Mechanical Engineering
dc.type.materialtext
dc.creator.orcid0000-0002-0819-6998


Files in this item

Thumbnail


This item appears in the following Collection(s)

Show simple item record