Numerical investigation of crack initiation in high-pressure gas turbine blade subjected to thermal-fluid-mechanical low-cycle fatigue-Reference-Cited by-同舟云学术

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Numerical investigation of crack initiation in high-pressure gas turbine blade subjected to thermal-fluid-mechanical low-cycle fatigue

Published:2023-03 Issue: Volume:202 Page:123748
ISSN:0017-9310
Container-title:International Journal of Heat and Mass Transfer
language:en
Short-container-title:International Journal of Heat and Mass Transfer

Author:

Vo Duy-Tan^ORCID,Mai Thanh-Dam^ORCID,Kim Byungwook^ORCID,Jung Jine-Sung,Ryu Jaiyoung

Funder

Korea Electric Power Corporation

Chung-Ang University

Ministry of Trade, Industry and Energy

Korea Institute of Energy Technology Evaluation and Planning

Publisher

Elsevier BV

Subject

Fluid Flow and Transfer Processes,Mechanical Engineering,Condensed Matter Physics

Reference35 articles.

1. Failure analysis of a first stage IN738 gas turbine blade tip cracking in a thermal power plant;Rani;Case Stud. Eng. Fail Anal.,2017

2. Thermomechanical fatigue experiment and failure analysis on a nickel-based superalloy turbine blade;Wang;Eng. Fail. Anal.,2019

3. High temperature fatigue testing of gas turbine blades;Beghini,2017

4. Turbine blade temperature calculation and life estimation-a sensitivity analysis;Reyhani;Propuls. Power Res.,2013

5. Thermal-fluid-solid coupling analysis on the temperature and thermal stress field of a nickel-base superalloy turbine blade;Cai;Materials,2021

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