A dissertation submitted to the Faculty of Engineering and the Built Environment, University of the Witwatersrand, Johannesburg, in ful filment of the requirements for the degree of Master of Science in Engineering. Johannesburg, May 2018This work was aimed at the advancement of the Laser Shock Peening (LSP) process for aeronautical applications. This involved developing a robust strategy for residual stress measurements to various depths in LSP treated samples with different thicknesses and then to perform a parametric analysis of the LSP process. For the residual stress measurement part of the study, aluminium alloy 7075 samples with thicknesses of 10, 6, 3 and 1.6 mm were treated with LSP and the residual stresses were measured using...
none8siLaser Shock Peening (LSP) is a material enhancement process used to introduce compressive res...
This paper reports measurements of the distribution of residual stress with depth from the surface i...
none3In order to slow down the manifestation of fatigue related problems in an aircraft, or in any o...
Laser shock peening (LSP) is a surface treatment which improves the fatigue performance of metallic ...
Laser shock peening (LSP) is a surface treatment which improves the fatigue performance of metallic ...
Laser Shock Peening is a fatigue enhancement treatment using laser energy to induce compressive Resi...
Laser Shock Peening is a fatigue enhancement treatment using laser energy to induce compressive Resi...
This thesis work encloses activities carried out in the Laser Center of the Polytechnic University o...
This study compares the residual stresses formed on samples before Laser Shock Peening (LSP) and aft...
Fatigue is one of the main failure mechanisms in engineering. Mechanical surface treatments are bein...
This paper reports selected findings from a collaborative research study into the fundamental unders...
compressive stresses close to the surface of a metal component. The method is particularly useful in...
Laser Shock Peening is a fatigue enhancement treatment using laser energy to induce compressive Resi...
AbstractLaser shock processing is a recently developed surface treatment designed to improve the mec...
In order to slow down the manifestation of fatigue related problems in an aircraft, or in any other ...
none8siLaser Shock Peening (LSP) is a material enhancement process used to introduce compressive res...
This paper reports measurements of the distribution of residual stress with depth from the surface i...
none3In order to slow down the manifestation of fatigue related problems in an aircraft, or in any o...
Laser shock peening (LSP) is a surface treatment which improves the fatigue performance of metallic ...
Laser shock peening (LSP) is a surface treatment which improves the fatigue performance of metallic ...
Laser Shock Peening is a fatigue enhancement treatment using laser energy to induce compressive Resi...
Laser Shock Peening is a fatigue enhancement treatment using laser energy to induce compressive Resi...
This thesis work encloses activities carried out in the Laser Center of the Polytechnic University o...
This study compares the residual stresses formed on samples before Laser Shock Peening (LSP) and aft...
Fatigue is one of the main failure mechanisms in engineering. Mechanical surface treatments are bein...
This paper reports selected findings from a collaborative research study into the fundamental unders...
compressive stresses close to the surface of a metal component. The method is particularly useful in...
Laser Shock Peening is a fatigue enhancement treatment using laser energy to induce compressive Resi...
AbstractLaser shock processing is a recently developed surface treatment designed to improve the mec...
In order to slow down the manifestation of fatigue related problems in an aircraft, or in any other ...
none8siLaser Shock Peening (LSP) is a material enhancement process used to introduce compressive res...
This paper reports measurements of the distribution of residual stress with depth from the surface i...
none3In order to slow down the manifestation of fatigue related problems in an aircraft, or in any o...