Elastic-Plastic Thermal and Residual Stress Analysis of Adhesively Bonded Single Lap Joint. Issue 1 (January 2016)
- Record Type:
- Journal Article
- Title:
- Elastic-Plastic Thermal and Residual Stress Analysis of Adhesively Bonded Single Lap Joint. Issue 1 (January 2016)
- Main Title:
- Elastic-Plastic Thermal and Residual Stress Analysis of Adhesively Bonded Single Lap Joint
- Authors:
- Sen, Faruk
- Abstract:
- In this work, an elastic-plastic thermal and residual stress analysis were performed for adhesively bonded single lap joint. For this purpose, thermoplastic composite adherents were bonded to each other with epoxy adhesive. Thermoplastic composite material was reinforced by steel-fibres, unidirectionally. Finite element method (FEM) was preferred to obtain thermal elastic and elastic-plastic stress distributions on single lap joint. Accordingly, modelling and solution processes were achieved using ANSYS software. So as to determine effects of uniform temperature loadings on thermal and residual stresses, different values of it were loaded on the joint, uniformly. Briefly, both thermal and residual thermal stresses were calculated under uniform temperature loading which was selected from 40 °C to 80 °C. According to obtained results different thermal expansion coefficients of composite adherents and adhesive layer caused thermal and residual stresses on adhesively bonded single lap joint due to applied uniform temperature loadings. Thermal stress values for x and y-directions are very different from each other owing to orthotropic material properties of thermoplastic composite. The magnitudes of elastic analyses results are higher than elastic-plastic analysis results. Contrary to elastic analysis results, elastic-plastic analysis results were nonlinear. Thermal and residual stresses are increased by increasing uniform temperature values, so the highest values were calculatedIn this work, an elastic-plastic thermal and residual stress analysis were performed for adhesively bonded single lap joint. For this purpose, thermoplastic composite adherents were bonded to each other with epoxy adhesive. Thermoplastic composite material was reinforced by steel-fibres, unidirectionally. Finite element method (FEM) was preferred to obtain thermal elastic and elastic-plastic stress distributions on single lap joint. Accordingly, modelling and solution processes were achieved using ANSYS software. So as to determine effects of uniform temperature loadings on thermal and residual stresses, different values of it were loaded on the joint, uniformly. Briefly, both thermal and residual thermal stresses were calculated under uniform temperature loading which was selected from 40 °C to 80 °C. According to obtained results different thermal expansion coefficients of composite adherents and adhesive layer caused thermal and residual stresses on adhesively bonded single lap joint due to applied uniform temperature loadings. Thermal stress values for x and y-directions are very different from each other owing to orthotropic material properties of thermoplastic composite. The magnitudes of elastic analyses results are higher than elastic-plastic analysis results. Contrary to elastic analysis results, elastic-plastic analysis results were nonlinear. Thermal and residual stresses are increased by increasing uniform temperature values, so the highest values were calculated when 80 °C. The plastic yielding was firstly come into being for 50 °C loading and it is expanded related to raising thermal loadings as nonlinear. … (more)
- Is Part Of:
- Advanced composites letters. Volume 25:Issue 1(2016)
- Journal:
- Advanced composites letters
- Issue:
- Volume 25:Issue 1(2016)
- Issue Display:
- Volume 25, Issue 1 (2016)
- Year:
- 2016
- Volume:
- 25
- Issue:
- 1
- Issue Sort Value:
- 2016-0025-0001-0000
- Page Start:
- Page End:
- Publication Date:
- 2016-01
- Subjects:
- Thermal analysis -- Elastic-plastic analysis -- Residual stress -- FEM -- Thermoplastic composites
Composite materials -- Periodicals
620.118 - Journal URLs:
- http://www.uk.sagepub.com/home.nav ↗
https://uk.sagepub.com/en-gb/eur/advanced-composites-letters/journal203579 ↗ - DOI:
- 10.1177/096369351602500104 ↗
- Languages:
- English
- ISSNs:
- 0963-6935
- Deposit Type:
- Legaldeposit
- View Content:
- Available online (eLD content is only available in our Reading Rooms) ↗
- Physical Locations:
- British Library DSC - BLDSS-3PM
British Library STI - ELD Digital store - Ingest File:
- 9671.xml