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出 处:《Applied Mathematics and Mechanics(English Edition)》1994年第2期101-108,共8页应用数学和力学(英文版)
摘 要:This paper presents the stress and strain distrihution obtained numerically in thethickness direction in the central region of symmetric composite laminates underuniaxial exlension and in-plane pure shear loading. It is shown that in the symmetricangle-ply laminates,near the interlaminar surface,thereis an interlaminarboundary-layer effect.The abrupt change of the fiber orientation at the interlaminarsurface causes a high concentration of stresses and a local three dimensional stress state.This paper presents the stress and strain distrihution obtained numerically in thethickness direction in the central region of symmetric composite laminates underuniaxial exlension and in-plane pure shear loading. It is shown that in the symmetricangle-ply laminates,near the interlaminar surface,thereis an interlaminarboundary-layer effect.The abrupt change of the fiber orientation at the interlaminarsurface causes a high concentration of stresses and a local three dimensional stress state.
关 键 词:compotsite matenals.laminates. three dimensional stressanalvsis
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