The published literature on corrosion of aluminium metal matrix composites based on silicon carbide, graphite, alumina, and boron reinforcements is reviewed. In general, the composites are more susceptible to corrosion attack than the matrix alloy. Corrosion tends to be localised with galvanic couples, ‘active’ reaction products, increased density of intermetallic particles, microcrevices, and voids cited as possible factors for specific composites.
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MansfeldF. and JeanjaquetS. L.: Corros. Sci., 1986, 26, (9), 727–734.
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ManspeldF., LinS., KIMS., and SHIHH.: Corrosion, 1989, 45, (8), 615–630.
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11.
HintonB. R. W., ArnottD. R., and RYANN. E.: Mater. Forum., 1986, 9, 162.
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PaciejR. C. and AgarwalaV. S.: ‘Metallurgical variables influencing the corrosion susceptibility of a P/M aluminum/ Sic, composite’, Report NADC-86071-60, Naval AW Development Center, Warminster, PA, 1985.
13.
PaciejR. C. and V. S. AGARWALA: Corrosion, 1988, 44, (10), 680–684.
14.
FtsHmANS. G.: ‘Weapons support materials’, Report NSWC MP82–190, Naval Surface Weapons Center, White Oak, MD, April1982.
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StrangwoodM.: ‘Corrosion fatigue behaviour of powder processed2014 and 2014–20volume % SiCp material’, Report AEA—TRs-4009, AERE R-13665, AEA Technology, Harwell, 1990.
16.
DullD. L., HarriganW. C.Jr, and AmateauM. F.: ‘The effect of matrix and fiber composition on mechanical strengths and corrosion behavior of graphite—aluminum composites’, Report ATR-76 (7564) -1, The Aerospace Corp., El Segundo, CA, 1977.
17.
KendallE. G.: in ‘Metallic matrix composites’, Vol. 4, (ed. KreiderK. G.), 399; 1974, New York, Academic Press.
18.
DavisL. W. and SullivanP. G.: ‘Evaluation of graphite/ aluminum composite materials’, Contract 0017-73—C-4313, First, Second, Third, and Fourth Quarterly Reports, Naval Ordnance Systems Command, Washington, DC, 1973.
19.
PayerJ. H. and PfeiferW. H.: Proc. Workshop on ‘Launch vehicle materials corrosion’, Daytana Beach, FL, February1975, Battelle Columbus Laboratories.
20.
PfeiferW. H.: in ‘Hybrid and select metal matrix composites’, (ed. RentonW.), 159; 1977, New York, American Institute of Aeronautics and Astronautics.
21.
PfeiferW. H.: ‘Applications analysis for the utilisation of graphite aluminum composites for navy applications’, Report N0004-75—C-5311, Nevada Engineering and Technology Corp., Reno, NV, 1975.
DavisD. A., VassilarosM. G., and GUDASJ. P.: Mater. Perform., 1982, 21, (3), 38–42.
25.
HiharaL. H.: ‘Corrosion of aluminum metal-matrix compo-sites’, PhD thesis, Massachusetts Institute of Technology, Cambridge, MA, 1989.
26.
BhagatR. B., AmateauM. F., CONWAYJ. C.Jr, PAULICKJ. M., CHISHOLMJ. M., PARNELLJ. M., and SEIDENSTICKERD. G.: J. Composite Mater., 1989, 23, 961–975.
27.
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28.
DardiL. E. and KreiderK. G.: in ‘Composite materials: testing and design’, STP546, 269; 1974, Philadelphia, PA, ASTM.
29.
SedriksA. I., GreenJ. A. S., and NOVAKD. L.: Metall. Trans., 1971, 2, 871–875.
30.
PohlmanS. L.: Corrosion, 1978, 34, 156.
31.
ChampionA. R., KruegerW. H., HARTMANNH. S., and DHINGRAA. K.: Proc. 2nd Int. Conf. on Composite Materials, (ed.NortonB. et al), 883; 1978, Warrendale, PA, The Metallurgical Society of AIME.
32.
AgarwalaV. S.: Naval Air Development Center, Warminster, PA; cited as personal communication in R f. 1.
33.
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