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论文类型：期刊论文

发表时间：2021-01-13

发表刊物：CHINA OCEAN ENGINEERING

卷号：22

期号：2

页面范围：313-330

ISSN号：0890-5487

关键字：rectangular footing; upper bound limit analysis; failure mechanism; failure envelope; combined loading

摘要：This paper presents two kinematic failure mechanisms of three-dimensional rectangular footing resting on homogeneous undrained clay foundation under uniaxial vertical loading and uniaxial moment loading. The failure mechanism under vertical loading comprises a plane strain Prandil-type mechanism over the central part of the longer side, and the size of the mechanism gradually reduces at the ends of the longer side and over the shorter side as the corner of rectangular footing is being approached where the direction of soil motion remains normal to each corresponding side respectively. ne failure mechanism under moment loading comprises a plane strain scoop sliding mechanism over the central pail of the longer side, and the radius of scoop sliding mechanism increases linearly at the ends of the longer side. On the basis of the kinematic failure mechanisms mentioned above, the vertical ultimate beating capacity and the ultimate bearing capacity against moment or moment ultimate beating capacity are obtained by use of upper bound limit analysis theory. At the same time, numerical analysis results, Skempton's results and Salgado el al.'s results are compared with this upper bound solution. It shows that the presented failure mechanisms and plastic limit analysis predictions are validated. In order to investigate the behaviors of undrained clay foundation beneath the rectangular footing subjected to the combined loadings, numerical analysis is adopted by virtue of the general-purpose FEM software ABAQUS, where the clay is assumed to obey the Mohr-Coulomb yielding criterion. The failure envelope and the ultimate bearing capacity are achieved by the numerical analysis results with tire varying aspect ratios from length L to breadth B of the rectangular footing. The failure mechanisms of rectangular footing which are subjected to the combined vertical loading V and horizontal loading H (Vertical loading V and moment loading M, and horizontal loading H and moment loading M respectively are observed in the finite element analysis.) is explained by use of the upper bound plasticity limit analysis theory. Finally, the reason of eccentricity of failure envelope in H-M loading space is given in this study, which can not be explained by use of the traditional 'swipe test'.