A Comparative Study of Constitutive Modeling of an Aero-Engine Single Crystal Superalloy under Creep-Thermomechanical Fatigue-Reference-Cited by-同舟云学术

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A Comparative Study of Constitutive Modeling of an Aero-Engine Single Crystal Superalloy under Creep-Thermomechanical Fatigue

Published:2022-01-03 Issue: Volume: Page:
ISSN:
Container-title:AIAA SCITECH 2022 Forum
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Author:

Wijeyeratne Navindra P.¹,Irmak Firat¹,O'Nora Nathan¹,Gordon Ali¹

Affiliation:

1. University of Central Florida

Publisher

American Institute of Aeronautics and Astronautics

Link

https://arc.aiaa.org/doi/pdf/10.2514/6.2022-0629

Reference25 articles.

1. Zhang, L. F., Yan, P., Zhao, M. H., Li, J. T., Zhao, J. C., Zeng, Q., and Han, F. K. Tensile Anisotropy of a Single Crystal Superalloy. No. 1, 2013, pp.475-484.

2. Dynamic Strain Aging in a New Single Crystal Nickel-Based Superalloy (CMSX-4)

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1. Microstructure analysis and life prediction of DD6 superalloy under 760 °C combined high and low cycle fatigue conditions;Engineering Fracture Mechanics;2024-01

2. A Comparative Study of Crystal Viscoplastic Modeling of Directionally Solidified Nickel-Base Superalloys;Journal of Engineering for Gas Turbines and Power;2022-11-29

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