Fatigue property-performance relationship of additively manufactured Ti-6Al-4V bracket for aero-engine application: An experimental study (2022)

First Author: Gupta A

Abstract

No abstract provided

Bibliographic Information

Digital Object Identifier: http://dx.doi.org/10.1016/j.prostr.2022.03.005

Publication URI: http://dx.doi.org/10.1016/j.prostr.2022.03.005

Type: Journal Article/Review

Parent Publication: Procedia Structural Integrity