Rong Jiang

ORCID: 0000-0002-5126-3922
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About
Contact & Profiles
Research Areas
  • High Temperature Alloys and Creep
  • Fatigue and fracture mechanics
  • Metal Alloys Wear and Properties
  • High-Velocity Impact and Material Behavior
  • High-Temperature Coating Behaviors
  • Metallurgy and Material Forming
  • Surface Treatment and Residual Stress
  • Nuclear Materials and Properties
  • Microstructure and Mechanical Properties of Steels
  • Hydrogen embrittlement and corrosion behaviors in metals
  • Additive Manufacturing Materials and Processes
  • Intermetallics and Advanced Alloy Properties
  • Mechanical Failure Analysis and Simulation
  • Electromagnetic Effects on Materials
  • Microstructure and mechanical properties
  • Metal and Thin Film Mechanics
  • Concrete and Cement Materials Research
  • Advanced ceramic materials synthesis
  • Inhalation and Respiratory Drug Delivery
  • Synthesis and properties of polymers
  • Data Stream Mining Techniques
  • Smart Materials for Construction
  • High Entropy Alloys Studies
  • Innovative concrete reinforcement materials
  • Material Properties and Failure Mechanisms

Nanjing University of Aeronautics and Astronautics
2018-2025

Applied Mathematics (United States)
2025

University of Chicago
2025

Ningbo Institute of Industrial Technology
2023-2024

Chinese Academy of Sciences
2012-2024

Ministry of Industry and Information Technology
2018-2024

Ningbo University
2023-2024

Northern University of Malaysia
2023

University of Southampton
2013-2022

Zhejiang University
2022

Using crystal plasticity, finite element analyses were carried out to model cyclic deformation for a low solvus high refractory (LSHR) nickel superalloy at elevated temperature. The implemented using representative volume (RVE), consisting of realistic microstructure obtained from SEM images the material. Monotonic, stress-relaxation and test data 725 °C used determine parameters fitting process their sensitivity RVE size random grain orientation. In combination with extended method (XFEM),...

10.1016/j.commatsci.2015.09.054 article EN cc-by Computational Materials Science 2015-10-18

10.1109/tit.2025.3555071 article EN IEEE Transactions on Information Theory 2025-01-01

ABSTRACT The complex geometrical configuration of shaped film cooling holes (FCHs) enhances the efficiency turbine blades, while stress concentration at FCH edge and manufacturing defects usually leads to high‐cycle fatigue (HCF) failure under service conditions. In this study, HCF tests 900°C were conducted on DD6 single‐crystal superalloy containing dustpan dovetail FCHs. effect FCHs strength was investigated, related mechanism analyzed using SEM, EDS, EBSD. results show that including...

10.1111/ffe.14641 article EN Fatigue & Fracture of Engineering Materials & Structures 2025-04-06

Ni-based superalloys in turbine disc applications face increasing susceptibility to oxygen-assisted fatigue crack propagation due increased entry temperatures. The continued lack of understanding the interplay between factors operating during limits: (1) development lifing methodologies accurately predict performance alloys/components and (2) associated alloy developments. An underpinning requirement better understand role oxygen is characterise process diffusion localised stress/strain...

10.1080/02670836.2016.1148227 article EN Materials Science and Technology 2016-02-18

Abstract The strain localization and crack initiation behavior of a powder metallurgy (PM) nickel‐based superalloy FGH4098 under low cycle fatigue (LCF) loads at room temperature is investigated by combining scanning electron microscope (SEM)‐digital image correlation (DIC) characterization with crystal plasticity simulation. elastic anisotropy near annealing twin boundaries contributes to results in high propensity LCF failure. effect local microstructure on the {111} slip bands tortuous...

10.1111/ffe.13685 article EN Fatigue & Fracture of Engineering Materials & Structures 2022-03-09
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