1981
DOI: 10.1177/002199838101500207
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Some Observations on the Cured Shape of Thin Unsymmetric Laminates

Abstract: This paper discusses the fact that the cured shape of thin unsymmetric laminates do not conform to the predictions of classical lamination theory. Rather than being saddle shaped, as predicted by the classical theory, the paper shows that thin unsymmetric laminates cure into a shape of a right circular cylinder. This anomalous behavior has been observed by many but the paper serves to quantify the effect and to inspire investigators to begin thinking about using the phenomenon to advantage. The paper indicates… Show more

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Cited by 462 publications
(175 citation statements)
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“…These composite structures are capable of attaining two statically stable states, 5 and can be manufactured to be attached to a more complex structure by adequate design of the lay-up. 6 In addition to the bi-stability, the usual high strength, lightweight, and, crucially, high fatigue resistance of composites, renders bi-stable laminates suitable for morphing solutions in wind turbine applications.…”
Section: Copyright 2012 Author(s) This Article Is Distributed Under mentioning
confidence: 99%
“…These composite structures are capable of attaining two statically stable states, 5 and can be manufactured to be attached to a more complex structure by adequate design of the lay-up. 6 In addition to the bi-stability, the usual high strength, lightweight, and, crucially, high fatigue resistance of composites, renders bi-stable laminates suitable for morphing solutions in wind turbine applications.…”
Section: Copyright 2012 Author(s) This Article Is Distributed Under mentioning
confidence: 99%
“…Hyer observed the large deformation of thin [0/90] cross-ply unsymmetric composite laminates in curing experiments (Hyer, 1981). They found that the shapes of cured unsymmetric composite laminates were a part of cylinder, which were stable at room temperature.…”
Section: Methodsmentioning
confidence: 99%
“…Hyper [40,41] was the pioneer to establish geometric formula and calculate the thermal deformations in anisotropic composite material, which is cross-ply composites. Nawab et al [42] calculated the thermal and chemical deformations together, by considering a non-linear geometrical approach to understanding the evolution of shape and hence residual stresses induced during carbon/epoxy laminates fabrication process.…”
Section: Calculation Of Composite Materials Deformationmentioning
confidence: 99%