Low cycle fatigue performance of SLM Ti-6Al-4V aero-engine bracket at 200°C: An experimental study (2023)

First Author: Gupta A
Attributed to:  Cornerstone: Mechanical Engineering Science to Enable Aero Propulsion Futures funded by UUI

Abstract

No abstract provided

Bibliographic Information

Digital Object Identifier: http://dx.doi.org/10.1016/j.prostr.2023.06.007

Publication URI: http://dx.doi.org/10.1016/j.prostr.2023.06.007

Type: Journal Article/Review

Parent Publication: Procedia Structural Integrity