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contributor authorZhi-Min
contributor authorLi
contributor authorWei
contributor authorGu
contributor authorYi-Xi
contributor authorZhao
date accessioned2017-05-08T21:33:54Z
date available2017-05-08T21:33:54Z
date copyrightOctober 2012
date issued2012
identifier other%28asce%29as%2E1943-5525%2E0000164.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/56312
description abstractPostbuckling behavior of three-dimensional (3D) braided rectangular plates subjected to biaxial compression is presented. The 3D braided composite may be treated as a cell system, and the geometry of each cell is deeply dependent on its position in the cross section of the plate. Based on Reddy’s higher-order shear deformation plate theory and general von Kármán–type equations that include the initial geometric imperfection of the plate, a perturbation technique is employed to determine postbuckling equilibrium paths of 3D braided rectangular plates. The results reveal that the geometric and physical properties have a significant effect on the postbuckling behavior of braided composite plates.
publisherAmerican Society of Civil Engineers
titlePostbuckling Behavior of 3D Braided Rectangular Plates Subjected to Biaxial Compression
typeJournal Paper
journal volume25
journal issue4
journal titleJournal of Aerospace Engineering
identifier doi10.1061/(ASCE)AS.1943-5525.0000164
treeJournal of Aerospace Engineering:;2012:;Volume ( 025 ):;issue: 004
contenttypeFulltext


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