Evaluation of different techniques in estimating orientation of crack initiation planes and fatigue lifetime under complex multiaxial loading paths

被引:11
|
作者
Wang, Yingyu [1 ]
Faruq, N. Zuhair [2 ]
Susmel, Luca [2 ]
机构
[1] Nanjing Univ Aeronaut & Astronaut, Key Lab Fundamental Sci Natl Def Adv Design Techn, Nanjing 210016, Jiangsu, Peoples R China
[2] Univ Sheffield, Dept Civil & Struct Engn, Sheffield S1 3JD, S Yorkshire, England
关键词
Multiaxial fatigue; Variable amplitude; Critical plane; Crack initiation plane; Nonproportional loading; PRINCIPAL STRESS DIRECTIONS; DAMAGE; SIMULATION;
D O I
10.1016/j.ijfatigue.2016.12.026
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
In the present investigation, the accuracy of two methods, i.e., the Shear Strain-Maximum Variance Method (gamma-MVM) and the Maximum Damage Method (MDM), in predicting the orientation of the crack initiation planes was checked by considering several results taken from the literature and generated by testing five different metallic materials under complex multiaxial loading. The gamma-MVM postulates that the critical plane is that material plane containing the direction experiencing the maximum variance of the resolved shear strain. In contrast, the MDM defines the critical plane as that material plane on which the accumulated damage reaches its maximum value. In the present investigation, the MDM was applied in conjunction with Fatemi-Socie's (FS) multiaxial fatigue criterion, Bannantine-Socie's (BS) cycle counting method, and Miner's linear rule. The validation exercise being performed demonstrated that both the gamma-MVM and the MDM were capable of accurately predicting the orientation of the crack initiation planes in the selected metals. Subsequently, the reliability of three different design methodologies suitable for estimating fatigue lifetime of metals subjected to variable amplitude multiaxial loading was assessed quantitatively by using a number of experimental results taken from the literature. In more detail, Methodology A was based on the MDM applied along with the FS criterion, the BS cycle counting method, and Miner's rule. Methodology B made use of the gamma-MVM, the FS criterion, the BS cycle counting method, and Miner's linear rule. Finally, Methodology C involved the gamma-MVM, the Modified Manson Coffin Curve Method (MMCCM), the classical Rain-Flow cycle counting method, and Miner's linear rule. According to this systematic validation exercise, the usage of these three design procedures was seen to result in satisfactory predictions, with the estimates falling within an error band of three. (C) 2016 Elsevier Ltd. All rights reserved.
引用
收藏
页码:521 / 529
页数:9
相关论文
共 26 条
  • [21] Deformation response and microstructure evolution in 304LN stainless steel subjected to multiaxial fatigue loading under different strain paths
    Bharti, Adarsh
    Dey, Rima
    Sivaprasad, S.
    Tarafder, S.
    Bhattacharyya, Abir
    INTERNATIONAL JOURNAL OF PRESSURE VESSELS AND PIPING, 2025, 214
  • [22] NUMERICAL EVALUATION OF 2 CREEP-FATIGUE DAMAGE MODELS UNDER COMPLEX LOADING HISTORIES AND MULTIAXIAL STATES OF STRESS
    BERTINI, L
    VITALE, E
    JOURNAL OF PRESSURE VESSEL TECHNOLOGY-TRANSACTIONS OF THE ASME, 1988, 110 (01): : 97 - 100
  • [23] Evaluation of fatigue crack network growth in cast iron for different biaxial loading paths via full-field measurements
    Tomicevic, Zvonimir
    Roux, Stephane
    Hild, Francois
    INTERNATIONAL JOURNAL OF FATIGUE, 2016, 92 : 281 - 303
  • [24] Influence of different loading paths on the multiaxial fatigue behavior of 2024 aluminum alloy under the same amplitude values of the second invariant of the stress deviator tensor
    Yankin, A. S.
    Mugatarov, A., I
    Wildemann, V. E.
    FRATTURA ED INTEGRITA STRUTTURALE, 2021, 15 (55): : 327 - 335
  • [25] Fatigue life evaluation of welded joints under multiaxial loading for different stress concepts using an extended Gough-Pollard criterion
    Bauer, N. M.
    Baumgartner, J.
    Fass, M.
    WELDING IN THE WORLD, 2024, 68 (08) : 2141 - 2155
  • [26] Crack initiation and early propagation plane orientation of 2A12-T4 aluminum alloy under tension-torsion fatigue loading including mean tensile stress
    Shi Xinhong
    Zhang Jianyu
    Xiao Qingshan
    Liu Tianqi
    FRATTURA ED INTEGRITA STRUTTURALE, 2016, Gruppo Italiano Frattura (35): : 441 - 448