Engineering topics
Ding, Rengen
Publications and source records attributed to Ding, Rengen.
Fatigue crack growth resistance of the austenitic stainless steel Alloy 709 at elevated temperatures
Not provided.
Deformation microstructure and tensile properties of Alloy 709 at different temperatures
Not Available
Creep and Creep-Fatigue Crack Growth Mechanisms in Alloy709 — NEUPRC-3.2 (Final Report)
This report is a summary of the work carried out by an interdisciplinary team from USA (Department of Mechanical and Aerospace Engineering, North Carolina State University) and UK (School of Metallurgy and Materials, University of Birmingham) to study creep and creep-fatigue crack growth mechanisms of alloy 709 under plane stress and more constrained ‘plane strain’ conditions. While the US team was funded through the DOE-NEUP program, NEUP RC 3.2, 15-8432 the UK team was funded through Research Council UK Energy Program (RCUKEP) award number EP/N016351/1. The UK team’s program ends in September 2019, while the US program ends in December 2018. As such some of the activities of the program will continue till late 2019. The USA team utilized a novel technique including in-situ heating - loading and Scanning Electron Microscope (SEM) imaging to study the “real-time” crack growth of alloy 709 under plane stress conditions, while the UK team focused on ex-situ fatigue, creep and creep fatigue on larger samples under constrained conditions. Transmission Electron Microscope (TEM) characterization of samples before, during and after creep and creep-fatigue testing was used to address local deformation behavior, dislocation analysis and damage evaluation. Attention was directed towards establishing micro-mechanisms of fatigue crack growth, crack growth under dwell fatigue loading, creep and creep-fatigue crack growth at temperatures ranging from 500 to 750°C in air and in vacuum.