A Damage Model for Adhesively Bonded Single-Lap Thick Composite Joints
Source abstract
Abstract
A proposed damage model is used for investigating the deformation and interfacial failure behavior of an adhesively bonded single-lap thick joint made of S2 glass/SC-15 epoxy resin composite material. The bonding material is 3M Scotch-Weld Epoxy Adhesive DP405 Black. Continuum damage mechanics models are used to describe the damage initiation and final failure at or near the interface. The effect of adhesive overlap length, thickness, and plasticity on the interfacial shear and normal stresses is studied. Experimental and analytical data are used to validate the proposed damage models.
Source: crossref · Quality: baseline
Research context
OpenAlex topics: Mechanical Behavior of Composites · Structural Load-Bearing Analysis · Epoxy Resin Curing Processes
SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.
Affiliations
Fellow ASME
Department of Mechanical Engineering, Fastening and Joining Research Institute, Oakland University, Rochester, MI 48309
US Army TARDEC, Warren, MI 48397
References (31)
Show source-provided references
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