Page 339 - Engineered Interfaces in Fiber Reinforced Composites
P. 339
320 Engineered interfaces in jiber reinforced composites
frictional shear stress (see Section 6.1). The inefficiency of the expanding monomers
in composites other than CFRP needs further work to explain the observed results
before this technique can be applied widely.
Because the shrinkage stress depends not only on the type of matrix materials
used but also on the state of matrix cure (Piggott et al., 1985), it is necessary to
specify the optimum cure cycle for a given expanding monomer. In addition to the
direct influence of the expanding monomers on fracture toughness, resins which can
cure without generating residual stresses are highly desirable for various practical
applications, such as high performance adhesives, coatings, precision castings,
dental fillings, binders for solid propellants, etc. There are now significant research
efforts toward the control of shrinkage stresses in polymers, particularly epoxies
(Shimbo et al., 1985; Ochi et al., 1989; He et al., 1989; Sikes and Brady, 1990) and
polyesters (Bucknall et al., 1991).
References
Aboudi, J. (1991). Microfailure criteria for coated fiber composites. J. Reinforced Plast. Composites 10,
146157.
Ahaim, R. and Heuer, A.H. (1987). The interface between (Nicalon) Sic fibers and a glass-ceramic
matrix. Adv. Ceram. Mater. 2, 154158.
Almond E.A., Embury J.D. and Wright E.S. (1969). Fracture in laminated materials. In Interfaces in
Composites, ASTM STP 452, ASTM, Philadelphia, PA, pp. 107-129.
Arnold, S.M., Arya, V.K. and Melis, M.E. (1990). Elastic/plastic analysis of advanced composite
investigating the use of the compliant layer concept in reducing residual stresses resulting from
processing, NASA TM-103204.
Arnold, S.M., Arya, V.K. and Melis, M.E. (1992). Reduction of thermal residual stresses in advanced
metallic composites based on a compensating/compliant layer concept. J. Composite Mater. 26, 1287-
1309.
Arnold, S.M. and Wilt, T.E. (1992). Influence of engineered interfaces on residual stresses and
mechanical response in metal matrix composites, NASA TM-105438. (Also in Composite Interfaces 1,
38 1402.)
Arridge, R.G.C. (1975). The effect of interlayers on the transverse stresses in fiber composites. Polym.
Eng. Sei. 15, 757-760.
Atkins A.G. (1974). Imparting strength and toughness to brittle composites. Nature 252, 116-1 18.
Atkins A.G. (1975). Intermittent bonding fro high toughness/high strength composites. J. Muter. Sci. 10,
8 19-832.
Atkins A.G. and Mai Y.W. (1976). Effect of water and ice on strength and fracture toughness of
intermittently bonded boron-epoxy composites J. Mater. Sci. 11, 2297-2306.
Bader M.G., Bailey J.E. and Bell I. (1973). The effect of fiber-matrix interface strength on the impact and
fracture properties of carbon fiber-reinforced epoxy resin composites. J. Phys. D: Appl. Phys. 6, 572-
586.
Bailey W.J., Sun R.L., Katsuki H., Endo T., Iwama I., Tsushima R., Saigo K. and Bitritto M.M. (1977).
Ring opening polymerization. In Proc. Am. Chem. SOC. Symp. (T. Saegusa and M. Goethals, eds.), p.
38.
Bannister, D.J., Andrews, M.C., Cervenka, A.J. and Young, R.J. (1995). Analysis of the single fiber pull-
out test by means of Raman spectroscopy, Part 11. Micromechanics of deformation for an aramid/
epoxy system. Composites Sci. Technol. 53, 41 1421.
Barnes, J.A., Simms, I.J., Farrow, G.J., Jackson, D., Wostenholm, G. and Yates, B. (1991). Thermal
expansion characteristics of PEEK composites. J. Mater. Sei. 26, 2259-2271.
Barnes, J.A. and Byerly, G.E. (1994). The formation of residual stresses in laminated thermoplastic
composites. Composites Sci. Technol. 51, 479494.