Residual Stress Evolution of Graphene-Reinforced AA2195 (Aluminum–Lithium) Composite for Aerospace Structural Hydrogen Fuel Tank Application

Manokaran, V ORCID: 0000-0002-1154-4164, Michael, AX ORCID: 0000-0002-6921-1178, Pazhani, A and Batako, A ORCID: 0000-0002-4613-7067 (2025) Residual Stress Evolution of Graphene-Reinforced AA2195 (Aluminum–Lithium) Composite for Aerospace Structural Hydrogen Fuel Tank Application. Journal of Composites Science, 9 (7). ISSN 2504-477X

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Abstract

This study investigates the fabrication and residual stress behavior of a 0.5 wt.% graphene-reinforced AA2195 aluminum matrix composite, developed for advanced aerospace structural applications. The composite was synthesized via squeeze casting, followed by a multi-pass hot rolling process and subsequent T8 heat treatment. The evolution of residual stress was systematically examined after each rolling pass and during thermal treatments. The successful incorporation of graphene into the matrix was confirmed through Energy-Dispersive Spectroscopy (EDS) analysis. Residual stress measurements after each pass revealed a progressive increase in compressive stress, reaching a maximum of −68 MPa after the fourth hot rolling pass. Prior to the fifth pass, a solution treatment at 530 °C was performed to dissolve coarse precipitates and relieve internal stresses. Cold rolling during the fifth pass reduced the compressive residual stress to −40 MPa, and subsequent artificial aging at 180 °C for 48 h further decreased it to −23 MPa due to recovery and stress relaxation mechanisms. Compared to the unreinforced AA2195 alloy in the T8 condition, which exhibited a tensile residual stress of +29 MPa, the graphene-reinforced composite in the same condition retained a compressive residual stress of −23 MPa. This represents a net improvement of 52 MPa, highlighting the composite’s superior capability to retain compressive residual stress. The presence of graphene significantly influenced the stress distribution by introducing thermal expansion mismatch and acting as a barrier to dislocation motion. Overall, the composite demonstrated enhanced residual stress characteristics, making it a promising candidate for lightweight, fatigue-resistant aerospace components.

Item Type:	Article
Uncontrolled Keywords:	40 Engineering; 4016 Materials Engineering; 4016 Materials engineering
Subjects:	T Technology > TL Motor vehicles. Aeronautics. Astronautics
Divisions:	Engineering
Publisher:	MDPI AG
Date of acceptance:	15 July 2025
Date of first compliant Open Access:	18 September 2025
Date Deposited:	18 Sep 2025 09:56
Last Modified:	18 Sep 2025 10:15
DOI or ID number:	10.3390/jcs9070369
URI:	https://researchonline.ljmu.ac.uk/id/eprint/27176

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