Published December 2015 | Version v1
Journal article

Syntactic foam core metal matrix sandwich composite under bending conditions

  • 1. Composite Materials and Mechanics Laboratory, Mechanical and Aerospace Engineering Department, New York University, Polytechnic School of Engineering, 6 MetroTech Center, Brooklyn, NY 11201 (United States)
  • 2. Deep Springs Technology Inc., Toledo, OH 43615 (United States)
  • 3. U.S. Army Research Laboratory, Weapons and Materials Research Directorate, Aberdeen Proving Ground, MD 21005 (United States)

Description

Highlights: • Flexural properties of A356 matrix syntactic foam core sandwich are studied. • Alumina hollow particle filled syntactic foam is combined with carbon fabric skins. • Flexural strength of 91.2 MPa and flexural stiffness of 20.6 GPA are measured. • Failure mode is included as tensile skin fracture and crack propagation in the core. • Cracks pass through the particles instead of crack tip blunting or bowing. - Abstract: The present work aims at characterizing a metal matrix syntactic foam core sandwich composite under three-point bending conditions. The sandwich comprises alumina hollow particle reinforced A356 alloy syntactic foam with carbon fabric skins. Crack initiation in the tensile side of the specimen causing failure of the skin, followed by rapid failure of the core in the direction applied load, is observed as the failure mechanism. Crack propagation through the alumina particles is observed in the failed specimens instead of interfacial failure. The average maximum strength, flexural strain and stiffness were measured as 91.2 ± 5.6 MPa, 0.49 ± 0.06% and 20.6 ± 0.7 GPa respectively. The collapse load is theoretically predicted using mechanics of sandwich beams. Experimental values show good agreement with theoretical predictions.

Availability note (English)

Available from http://dx.doi.org/10.1016/j.matdes.2015.07.127

Additional details

Identifiers

DOI
10.1016/j.matdes.2015.07.127;
PII
S0264127515301969;

Publishing Information

Journal Title
Materials and Design
Journal Volume
86
Journal Page Range
p. 536-544
ISSN
0264-1275

INIS

Country of Publication
United Kingdom
Country of Input or Organization
International Atomic Energy Agency (IAEA)
INIS RN
50033481
Subject category
S36: MATERIALS SCIENCE;
Descriptors DEI
ALUMINIUM ALLOYS; ALUMINIUM OXIDES; CARBON; CRACK PROPAGATION; FLEXIBILITY; FLEXURAL STRENGTH; FORECASTING; FRACTURES; STRAINS
Descriptors DEC
ALLOYS; ALUMINIUM COMPOUNDS; CHALCOGENIDES; ELEMENTS; FAILURES; MECHANICAL PROPERTIES; NONMETALS; OXIDES; OXYGEN COMPOUNDS; TENSILE PROPERTIES

Optional Information

Copyright
Copyright (c) 2017 Elsevier Science B.V., Amsterdam, The Netherlands, All rights reserved.