A physically-based representative stress methodology for predicting stress rupture life of Ni-based DS superalloy-Reference-Cited by-同舟云学术

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A physically-based representative stress methodology for predicting stress rupture life of Ni-based DS superalloy

Published:2022-07 Issue: Volume: Page:
ISSN:1000-9361
Container-title:Chinese Journal of Aeronautics
language:en
Short-container-title:Chinese Journal of Aeronautics

Author:

HUANG Jia,HE Zhenzhuo,LYU Shuangqi,YANG Xiaoguang,SHI Duoqi,SUN Yantao,LYU Yongzhao,FU Zhizhong,MIAO Guolei,SONG Jianan

Publisher

Elsevier BV

Subject

Mechanical Engineering,Aerospace Engineering

Reference45 articles.

1. Stress-controlled LCF experiments and ratcheting behaviour simulation of a nickel-based single crystal superalloy with[001]orientation;Zhang;Chin J Aeronaut,2021

2. A physically-based model considering dislocation-solute atom dynamic interactions for a nickel-based superalloy at intermediate temperatures;Lin;Mater Des,2019

3. Analysis of the material damage influence on the stress-strain state of gas-turbine engine blades;Zadvorniy;Strength Mater,2015

4. A numerical study of parameters controlling stress redistribution in circular notched specimens during creep;Eggeler;J Strain Anal Eng Des,1993

5. Effect of constraint on creep behavior of 9Cr-1Mo steel;Goyal;Metall Mater Trans A,2014

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1. Investigation of the Influence of Multi-Source Load Uncertainty on Turbine Disk Damage;2024

2. Creep life prediction of Ni‐based single‐crystal superalloy plate with film‐cooling holes using a modified critical distance method based on the improved weight function;Fatigue & Fracture of Engineering Materials & Structures;2023-10-14

3. Dependence of microstructural evolution on the geometric structure for serviced DZ125 turbine blades;Frontiers in Materials;2023-04-10

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