Novel method for measuring surface residual stress using flat-ended cylindrical indentation  

作　　者：Guangzhao HAN Lixun CAI Xiaokun LIU 

机构地区：[1]Applied Mechanics and Structure Safety Key Laboratory of Sichuan Province,School of Mechanics and Aerospace Engineering,Southwest Jiaotong University,Chengdu 610031,China [2]Zhengzhou Machinery Research Institute Transmission Technology Co.,Ltd,Zhengzhou 518115,China

出　　处：《Chinese Journal of Aeronautics》2024年第8期486-495,共10页中国航空学报（英文版）

基　　金：supported by the National Natural Science Foundation of China(Nos.11872320 and 12072294).

摘　　要：Instrumented indentation is a promising technique for estimating surface residual stresses and mechanical properties in engineering components.The relative difference between the indentation loads for unstressed and stressed specimens was selected as the key parameter for measuring surface residual stresses in flat-ended cylindrical indentations.Based on the equivalent material method and finite element simulations,a dimensionless mapping model with six constants was established between the relative load difference,constitutive model parameters,and normalized residual stress.A novel method for measuring the surface residual stress and constitutive model parameters of metallic material through flat-ended cylindrical indentations was proposed using this model and a mechanical properties determination method.Numerical simulations were conducted using numerous elastoplastic materials with different residual stresses to verify the proposed model;good agreements were observed between the predicted residual stresses and those previously applied in finite element analysis.Flat-ended cylindrical indentation tests were performed on four metallic materials using cruciform specimens subjected to various equibiaxial stresses.The results exhibited good conformance between the stress–strain curves obtained using the proposed method and those from traditional tensile tests,and the absolute differences between the predicted residual stresses and applied stresses were within 40 MPa in most cases.

关 键 词：Instrumented indentation Residual stress Finite element simulation Equivalent material method Mechanical property 

分 类 号：V261[航空宇航科学与技术—航空宇航制造工程]