1989
DOI: 10.1299/jsmea1988.32.1_67
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The Peculiar Behavior of the Poisson's Ratio of Laminated Fibrous Composites

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Cited by 24 publications
(29 citation statements)
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“…The key requirement for this to be generated is that the individual ply material is highly anisotropic. So, carbon fibre has been the preferred reinforcement and prediction of suitable stacking sequences has been carried out along with basic experimental work to verify the Poisson's ratio [5,13,[15][16][17]. It should be noted that work has also been reported on producing negative Poisson's ratios in Kevlar laminates [18] and filament wound tubes [19] and one study has reported a negative in-plane Poisson's ratio in glass fibre laminates [20].…”
Section: Introductionmentioning
confidence: 99%
“…The key requirement for this to be generated is that the individual ply material is highly anisotropic. So, carbon fibre has been the preferred reinforcement and prediction of suitable stacking sequences has been carried out along with basic experimental work to verify the Poisson's ratio [5,13,[15][16][17]. It should be noted that work has also been reported on producing negative Poisson's ratios in Kevlar laminates [18] and filament wound tubes [19] and one study has reported a negative in-plane Poisson's ratio in glass fibre laminates [20].…”
Section: Introductionmentioning
confidence: 99%
“…Several groups have considered auxetic angle ply laminate composites [2,3,5,[9][10][11][12] either theoretically, practically or both. Most of the work on fibre reinforced composites has concentrated on using carbon fibre as the reinforcement.…”
Section: Introductionmentioning
confidence: 99%
“…around ν = -0.17 [2,3,5,8,11,12]. This is achieved in the through-thickness direction by a stacking sequence of [±θ] s with the laminate construction typically considered being [±30°] s .…”
Section: Introductionmentioning
confidence: 99%
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“…Investigations into laminates made of prepregs with carbon fibers and epoxy matrix have shown that ν xz of the composite obtained at small packing angles of the layers (10°-40°) is negative [10,11]. Another method of designing biphasic composite materials incorporating stiff inclusions and a compliant matrix shown in Fig.…”
Section: Non-auxetic Inclusions (Anisotropic Auxetics)mentioning
confidence: 99%