Incremental Hole Drilling Residual Stress Measurement in Thin Aluminum Alloy Plates Subjected to Laser Shock Peening

被引:0
作者
J. P. Nobre
C. Polese
S. N. van Staden
机构
[1] University of the Witwatersrand,School of Mechanical, Industrial and Aeronautical Engineering
[2] University of Coimbra,CFisUC
[3] hosted by the University of the Witwatersrand, The Centre for Physics of the University of Coimbra
来源
Experimental Mechanics | 2020年 / 60卷
关键词
Residual stress; Hole drilling method; Thin plates, laser shock peening; X-ray diffraction; Neutron diffraction; Energy dispersive synchrotron X-ray diffraction;
D O I
暂无
中图分类号
学科分类号
摘要
The American standard ASTM E837 presents a standard procedure to determine residual stresses in isotropic materials using the incremental hole drilling technique (IHD). The standard, however, presents limitations regarding its applicability, such as those related with the thin thickness of the samples. According to this standard, in depth non uniform residual stresses can only be determined, roughly, in plates where the thickness is greater than the mean diameter of the strain gage rosette used. This limitation excludes important experimental cases and, therefore, deserves to be investigated. In this work this limitation is numerically and experimentally investigated in detail, considering the case of residual stresses induced by laser shock peening (LSP) in aluminum alloy 7075-T651 plates. The obtained results using the incremental hole drilling technique (IHD), based on the integral method, are benchmarked against the results of several diffraction techniques, used as reference, and a procedure to correct the experimentally determined strain-depth relaxation curves, to accurately still apply the ASTM E837 standard procedure is discussed and validated.
引用
收藏
页码:553 / 564
页数:11
相关论文
共 73 条
  • [1] Schajer GS(2018)Hole-drilling method for measuring residual stresses Synthesis SEM Lectures on Experimental Mechanics 1 1-186
  • [2] Whitehead PS(2006)Finite element modelling of shot peening process: prediction of the compressive residual stresses, the plastic deformations and the surface integrity Mater Sci Eng A 426 173-180
  • [3] Frija M(1990)Crack propagation in the presence of shot peening residual stresses Eng Fract Mech 37 373-387
  • [4] Hassine T(2014)Laser shock peening to repair, design and manufacture current and future aircraft structures by residual stress engineering Adv Mater Res 891-892 992-1000
  • [5] Fathallah R(2017)Ball-burnishing effect on deep residual stress on AISI 1038 and AA2017-T4 Mater Manuf Process 32 1279-1289
  • [6] Bouraoui C(2014)Fatigue crack growth in laser shock peened thin metallic panels Adv Mater Res 996 775-781
  • [7] Dogui A(2015)Laser shock processing of thin Al2024-T351 plates for induction of through-thickness compressive residual stresses fields J Mater Process Technol 223 8-15
  • [8] Hammond DW(2016)Effects of laser shock peening on the surface integrity of 18% Ni Maraging steel Strojniški vestnik - Journal of Mechanical Engineering 62 291-298
  • [9] Meguid SA(2000)Cross-sectional mapping of residual stresses by measuring the surface contour after a cut J Eng Mater Technol 123 162-168
  • [10] Furfari D(2013)Analytical solutions for determining residual stresses in two-dimensional domains using the contour method Proceedings of the Royal Society a: mathematical, physical and engineering sciences 469 20130367-4428