1989
DOI: 10.1243/pime_proc_1989_203_051_01
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Fatigue of Composite Materials

Abstract: This paper reviews the area of fatigue of composite materials, particularly fibre-reinforced plastics, used in aerospace and other industries. The review concentrates on carbon, glass and aramid reinforcing fibres and epoxy resin as a matrix material. Mention is also made of newer matrices such as those based on thermoplastics.

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Cited by 9 publications
(5 citation statements)
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“…In fact, the presence of the damage in composites has a great influence on dynamic properties, such as stiffness, damping and natural frequency [10]. Stiffness, and hence natural frequency, is reduced as damage develops, and the latter parameter can be used as a criterion to define fatigue failure.…”
Section: Endurance Testing Of the Coupons Subject To Simulated Randommentioning
confidence: 99%
See 1 more Smart Citation
“…In fact, the presence of the damage in composites has a great influence on dynamic properties, such as stiffness, damping and natural frequency [10]. Stiffness, and hence natural frequency, is reduced as damage develops, and the latter parameter can be used as a criterion to define fatigue failure.…”
Section: Endurance Testing Of the Coupons Subject To Simulated Randommentioning
confidence: 99%
“…degradation of the material can occur with repeated stresses cycles with magnitude below those needed for static failure) but the failure mechanisms are different from those in metals [9,10]. In composites, one or more of damage mode (e.g.…”
Section: Introductionmentioning
confidence: 99%
“…Several studies showed that adhesively bonded joints are prone to mode-I cyclic delamination [9][10][11]. As a consequence, several approaches have been proposed that incorporate delamination properties into structural designs, and that predict cyclic failure mechanisms in CFRP structures [12][13][14][15][16][17]. Ashcroft et al [18] suggested that the maximum load that composite specimens under cyclic loading could withstand before failure was approximately 26% to 62% of the quasi-static strength.…”
Section: Introductionmentioning
confidence: 99%
“…where, F ij and F i are functions of the number of cycles N, the stress ratio R and the frequency of loading. The tensor components, F ij and F i are calculated from the fatigue failure stresses (X t , X c , Y t , Y c and S) in the longitudinal, transverse and shear (1,2,6) directions, which are obtained by the S-N curve values of the laminate in the same directions and under the same conditions.…”
Section: Fatigue Life Diagram Of Unidirectional Compositesmentioning
confidence: 99%
“…However, FRP composites are highly propose a fatigue design criteria for FRP bridge decks. [22][23][24][25][26][27] AASHTO Standard Specification and LRFD specifications require that the number of cycles to check for fatigue to be two million cycles, and the level of fatigue load be 75% of the actual axle load of a HS20-44 design truck to evaluate fatigue and fracture in steel structures [1,2]. In order to develop a practical qualification test and, in agreement with AASHTO Standard Specifications, two million cycles is being adopted by most researchers to evaluate the fatigue response of the FRP deck [23].…”
Section: Design Approachmentioning
confidence: 99%