Open AccessNumerical stress analysis for single-lap adhesive joint under thermo-mechanical load using non-linear material
Author(s) -
Nawres Al-Ramahi,
Roberts Joffe,
Jānis Vārna
Publication year - 2020
Publication title -
iop conference series. materials science and engineering
Language(s) - English
Resource type - Journals
eISSN - 1757-899X
pISSN - 1757-8981
DOI - 10.1088/1757-899x/881/1/012070
Subject(s) - materials science , finite element method , residual stress , joint (building) , composite material , adhesive , stress (linguistics) , shear stress , structural engineering , superposition principle , thermal , nonlinear system , linear elasticity , shear (geology) , layer (electronics) , engineering , mathematics , mathematical analysis , linguistics , philosophy , physics , quantum mechanics , meteorology
A comprehensive stress analysis by means of Finite Element Method (FEM) for single-lap joint subjected to thermal and mechanical loads is presented in this paper. Simulation is used to predict the effect of residual thermal stresses (caused by difference of temperature of use and elevated temperature during the assembly of the joint) on stress distribution within adhesive layer. The residual thermal stresses are assigned to joint members as initial condition before the mechanical load is applied. The FEM model employs linear and nonlinear material model and accounts for geometrical nonlinearity. It is confirmed that the difference between the manufacturing and the ambient temperature results in high residual thermal stresses, especially in axial and lateral directions of the joint. The calculation of total stress as superposition of thermal and mechanical stresses works only for linear materials. Moreover, simultaneous application of temperature and mechanical load (applied strain in case of displacement controlled test) in FEM produces inaccurate results, since in real situation the strain is applied to already thermally loaded structure. It is also found that the residual thermal stresses may reduce the peel and shear stress concentration in the adhesive at the ends of overlap and the shear stress within the overlap.