In-Situ Computed Tomography — Analysis of a Single-Lap Shear Test with Composite-Metal Pin Joints
نویسندگان
چکیده
Abstract Lightweight design in the form of intelligent multi-material structures that combine advantages high strength steel and continuous fibre reinforced thermoplastics (CFRTs) gain increasing relevance. In this context, joining operation is a major challenge as it has to be time cost efficient resulting joint exhibit mechanical durability. One possible approach use cold formed pin structures, which can inserted into CFRT create fitting under avoidance damage commonly case for bolted or riveted joints. The deformation phenomena joints are usually investigated by macrosectioning (ex-situ) computed tomography. However, due resetting elastic deformations cracks close after unloading an inaccurate state inner structure measured. Furthermore, investigation different stages with load progressing failure very consuming, because multiple samples have tested investigated. Alternatively, in-situ tomography (in-situ CT) used investigate testing paper, method CT analysis single-lap shear test composite-metal presented. pins plastically extruded height approx. 1.8 mm from metal sheet (1.5 thick) pressed locally heated glass thermoplastic (FRT) (approx. 2 creating fit. Specimens quasi-unidirectional reinforcement 0° 90° direction tested. With procedure, three-dimensional observed identified each respectively. Thus, also validating numerical simulations.
منابع مشابه
Semi Analytical Transient Dynamic Analysis of Composite Adhesive Single-lap Joints
A novel semi analytical method is developed for transient analysis of single-lap adhesive joints with laminated composite adherends subjected to dynamical loads. The presented approach has the capability of choosing arbitrary loadings and boundary conditions. In this model, adherends are assumed to be orthotropic plates that pursuant to the classical lamination theory. Stacking sequences can be...
متن کاملAnalytical Solution of Stress Field in Adhesively Bonded Composite Single-Lap Joints Under Mechanical Loadings
In this paper, considering an adhesively bonded composite single-lap joint, a novel approach is presented to predict the peel and shear stress distributions of the adhesive layer for an ASTM standard test sample. In current method, the equilibrium equations are derived using the energy method and based on the Timoshenko’s beam theory. Two solution procedures then are discussed, one of which rep...
متن کاملFatigue behaviour of composite adhesive lap joints
This paper is concerned with a fatigue study of composite adhesive lap joints produced from a bi-directional woven E-glass fibres and polypropylene. The adhesive used was a Bostik 7452 (Rubber & Plastics Grade) ethyl cyanoacrylate type. The effects of layer orientation, lap joint length and water immersion on the fatigue behaviour were studied. The specimens were immersed in water during period...
متن کاملEvaluation of Metal Artifact Reduction software in Computed Tomography
Introduction: The image quality of computed tomography (CT) can be seriously lowered by metal implants of patients. These implants are known to exert a significant impact on diagnostic accuracy due to artifacts. The current study aimed to assess the usefulness of Metal Artifact Reduction (MAR) software in the reduction of metal artifacts, in comparison to iterative rec...
متن کاملThe Effect of Fiber Breakage on Transient Stress Distribution in a Single-Lap Joint Composite Material
In the present study, the transient stress distribution caused by a break in the fibers of an adhesive bonding is investigated. Transient stress is a dynamic response of the system to any discontinuity in the fibers from detachment time till their equilibrium state (or steady state). To derive the governing dynamic equilibrium equations shear lag model is used. Here, it is assumed that the tens...
متن کاملذخیره در منابع من
با ذخیره ی این منبع در منابع من، دسترسی به آن را برای استفاده های بعدی آسان تر کنید
ژورنال
عنوان ژورنال: Journal of physics
سال: 2023
ISSN: ['0022-3700', '1747-3721', '0368-3508', '1747-3713']
DOI: https://doi.org/10.1088/1742-6596/2526/1/012067