Creep life prediction for a nickel-based single crystal turbine blade
Author:
Affiliation:
1. School of Mechanics, Civil Engineering and Architecture, Northwestern Polytechnical University, Xi’an, PR China
2. School of Civil Engineering and Transportation, South China University of Technology, Guangzhou, Guangdong, PR China
Publisher
Informa UK Limited
Subject
Mechanical Engineering,Mechanics of Materials,General Materials Science,General Mathematics,Civil and Structural Engineering
Link
https://www.tandfonline.com/doi/pdf/10.1080/15376494.2021.1972187
Reference43 articles.
1. Evolution of Ni-based superalloys for single crystal gas turbine blade applications
2. Forming property and broaching error prediction of a forged nickel-based superalloy turbine disc
3. Reliability-based design optimization approach for compressor disc with multiple correlated failure modes
4. Dynamic surrogate modeling approach for probabilistic creep-fatigue life evaluation of turbine disks
5. Probabilistic-based combined high and low cycle fatigue assessment for turbine blades using a substructure-based kriging surrogate model
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2. The low-cycle fatigue behavior and an entropy-based life prediction model for Nickel-based single crystal superalloy across an extensive temperature range;Engineering Fracture Mechanics;2024-05
3. Creep behavior of different elliptical film cooling holes in complex temperature fields;International Journal of Pressure Vessels and Piping;2024-02
4. Influence of Enhanced Laves Phase Shape and Distribution on Atomic-Scale Frictional Wear Mechanisms in Nickel-Based Single Crystal Alloys;2024
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