Mesoscale damage behavior and meso-macroscale correlation of low-cycle fatigue in Z2CND18.12N austenitic stainless steel

Feng, Chao; Zhang, Ping; Meng, Yiyuan; Luo, Zhongbing; Li, Lin; Silberschmidt, Vadim V.

doi:10.1016/j.msea.2022.143894

Cited by 3 publications

(1 citation statement)

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“…Atapek et al (2016) investigated the fatigue behavior of Cu-2.55Ni-055Si alloy specimens tested under various stress levels to obtain the stress-life curve. On the other hand, numerous stress-, strain-and energy-based fatigue models have been developed in the past few decades to predict the LCF life of metallic materials (Zhang et al, 2020;Che et al, 2022;Smith, 1970), such as the Manson-Coffin formula and Smith-Watson-Topper (SWT) model (Smith, 1970;Mozafari et al, 2020;Xu et al, 2022), which has been widely adopted in engineering application and proved to be feasible and efficient. In summary, the design of rocket engines' thrust chamber walls requires an accurate analysis of the material's deformation behavior at high temperatures and an evaluation of its fatigue life.…”

Section: Introductionmentioning

confidence: 99%

An investigation on the cyclic deformation and service life of a reusable liquid rocket engine thrust chamber wall

Gao¹,

Zhang²,

Huo³

2023

MMMS

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PurposeRegeneratively cooled thrust chamber is a key component of reusable liquid rocket engines. Subjected to cyclic thermal-mechanical loadings, its failure can seriously affect the service life of engines. QCr0.8 copper alloy is widely used in thrust chamber walls due to its excellent thermal conductivity, and its mechanical and fatigue properties are essential for the evaluation of thrust chamber life. This paper contributes to the understanding of the damage mechanism and material selection of regeneratively cooled thrust chambers for reusable liquid rocket engines.Design/methodology/approachIn this paper, tensile and low-cycle fatigue (LCF) tests were conducted for QCr0.8 alloy, and a Chaboche combined hardening model was established to describe the elastic-plastic behavior of QCr0.8 at different temperatures and strain levels. In addition, an LCF life prediction model was established based on the Manson–Coffin formula. The reliability and accuracy of models were then verified by simulations in ABAQUS. Finally, the service life was evaluated for a regenerative cooling thrust chamber, under the condition of cyclic startup and shutdown.FindingsIn this paper, a Chaboche combined hardening model was established to describe the elastoplastic behavior of QCr0.8 alloy at different temperatures and strain levels through LCF experiments. The parameters of the fitted Chaboche model were simulated in ABAQUS, and the simulation results were compared with the experimental results. The results show that the model has high reliability and accuracy in characterizing the viscoplastic behavior of QCr0.8 alloy.Originality/value(1)The parameters of a Chaboche combined hardening constitutive model and LCF life equation were optimized by tensile and strain-controlled fatigue tests of QCr0.8 copper alloy. (2) Based on the Manson–Coffin formula, the reliability and accuracy of constitutive model were then verified by simulations in ABAQUS. (3)Thermal-mechanical analysis was carried out for regeneratively cooled thrust chamber wall of a reusable liquid rocket engine, and the service life considering LCF, creep and ratcheting damage was analyzed.

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