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Naji, M. |
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Motta, Antonella |
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Aletan, Dirar |
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Mohamed, Tarek |
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Ertürk, Emre |
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Taccardi, Nicola |
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Kononenko, Denys |
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Petrov, R. H. | Madrid |
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Alshaaer, Mazen | Brussels |
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Bih, L. |
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Casati, R. |
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Muller, Hermance |
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Kočí, Jan | Prague |
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Šuljagić, Marija |
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Kalteremidou, Kalliopi-Artemi | Brussels |
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Azam, Siraj |
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Ospanova, Alyiya |
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Blanpain, Bart |
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Ali, M. A. |
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Popa, V. |
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Rančić, M. |
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Ollier, Nadège |
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Azevedo, Nuno Monteiro |
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Landes, Michael |
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Rignanese, Gian-Marco |
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Khan, Muhammad Kashif
Coventry University
in Cooperation with on an Cooperation-Score of 37%
Topics
Publications (8/8 displayed)
- 2020Effect of Post Weld Heat Treatment on the Microstructure and Electrochemical Characteristics of Dissimilar Material Welded by Butter Methodcitations
- 2019Experimental investigation on the quasi-static mechanical behavior of autoclaved aerated concrete insulated sandwich panelscitations
- 2018Effect of ultrasonic nanocrystal surface modification on residual stress and fatigue cracking in engineering alloyscitations
- 2011Effect of residual stress on the nanoindentation response of aerospace aluminium alloyscitations
- 2011Application of synchrotron X-ray diffraction and nanoindentation for the determination of residual stress fields around scratchescitations
- 2011A combined experimental and finite element approach for determining mechanical properties of aluminium alloys by nanoindentationcitations
- 2010Determination of the residual stress field around scratches using synchrotron X-rays and nanoindentationcitations
- 2009Effect of tool profile and fatigue loading on the local hardness around scratches in clad and unclad aluminium alloy 2024citations
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article
Effect of residual stress on the nanoindentation response of aerospace aluminium alloys
Abstract
Experimental measurements and finite element simulations have been used to study the effect of residual stresses on the nanoindentation response of an aerospace-grade aluminium alloy. Tensile and compressive residual stresses lead to changes in the nanoindentation load–displacement curves. Loading and unloading curves were studied to observe the effect of residual stresses. The maximum load of indentation, curvature of the loading curve, elastically recovered depth, work of indentation, pile-up and contact area were measured and found to have a linear relationship with residual stress. To calculate residual stress from the load–displacement curve, it was concluded that pile-up should be measured carefully. The paper presents a methodology of calculation of area of contact based on the work of indentation which can be extracted from the nanoindentation load–displacement data. This allows extr