An investigation of fracture behavior in layered NiAl/V composites

Journal Article · Fri Jan 22 00:00:00 EST 1999 · Scripta Materialia

DOI:https://doi.org/10.1016/S1359-6462(98)00480-1· OSTI ID:349867

Li, M; Soboyejo, W O ^[1]; Wang, R; Katsube, N ^[2]

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1. Ohio State Univ., Columbus, OH (United States). Dept. of Materials Science and Engineering
2. Dept. of Aerospace Engineering, Applied Mechanics, and Aviation, Columbus, OH (United States). Applied Mechanics Section

The possible use of vanadium microlaminates in the toughening of NiAl composites is examined in this paper. Ductile layer reinforcement has been shown to offer higher toughening of brittle intermetallics than ductile particles and fibers. Vanadium layers with thickness of 100, 200 and 400 {micro}m are shown to significantly improve the fracture toughness of NiAl. The extent of toughening, which increases with increasing layer thickness, is attributed to crack bridging and the interactions of propagating cracks with vanadium layers. Finite element models are used to explain the re-initiation of cracks in adjacent NiAl layers after retardation by the vanadium layers in the crack arrestor orientation.

• OSTI ID: 349867
• Journal Information: Scripta Materialia, Vol. 40, Issue 4; Other Information: PBD: 22 Jan 1999
• Country of Publication: United States
• Language: English

Related Subjects

36 MATERIALS SCIENCE
FRACTURE PROPERTIES
NICKEL ALLOYS
ALUMINIUM ALLOYS
VANADIUM
COMPOSITE MATERIALS
LAYERS
CRACK PROPAGATION
FINITE ELEMENT METHOD