Thin-walled Structures
IF
4.44
Papers
6,148
Papers 5,990
1 page of 599 pages (5,990 results)
Newest
#1Hossein Bakhshi Khaniki (University of Adelaide)H-Index: 13
#2Mergen H. Ghayesh (University of Adelaide)H-Index: 68
Last. Li-Qun Chen (SHU: Shanghai University)H-Index: 54
view all 4 authors...
Abstract null null Comprehensively investigated in this paper is the coupled nonlinear dynamics of hyperelastic beams. Experimental testing is performed to accurately model the hyperelasticity using different hyperelastic energy density models. Samples were fabricated using 3D printing technique for flexible thermoplastic polyurethane filaments following the ASTM D638 guidance and tested using a tensile testing machine. For a proper hyperelastic energy density model, coupled nonlinear equations ...
Source
#1Shaohua Li (CUP: China University of Petroleum, Beijing)
#2Wenchun Jiang (CUP: China University of Petroleum, Beijing)H-Index: 23
Last. Xuefang Xie (CUP: China University of Petroleum, Beijing)H-Index: 5
view all 4 authors...
Abstract null null The localized defects, including the ruptured truss and debonding joint, have been severely threatening the structural integrity of the pyramidal lattice truss panel structure (PLTPS). In this paper, a series of analytical models, i.e., equivalent elastic modulus, plastic and creep strain rate models, were developed to study the effects of localized defects on the mechanical properties and creep performance of the PLTPS, which have been verified by the experiments and finite e...
Source
#2Jiang Nan (CUG: China University of Geosciences)H-Index: 3
Last. Bin Zhu (CUG: China University of Geosciences)H-Index: 24
view all 6 authors...
Source
#1Zhi-jia Zhang (XJTU: Xi'an Jiaotong University)H-Index: 8
Last. Feng Jin (XJTU: Xi'an Jiaotong University)H-Index: 21
view all 7 authors...
Abstract null null In this work, the bending stiffness, initial failure load, initial failure modes and minimum mass design of square honeycomb-corrugation hybrid core sandwich structures (SHCH) subjected to bending were explored by a combined theoretical analysis, experimental testing, and numerical prediction method. Samples were fabricated by brazing process and measured under three-point bending. To theoretically obtain the initial failure mechanism map, six different initial failure modes w...
Source
Source
Source
#1Xin Xue (FZU: Fuzhou University)H-Index: 11
#2Wei Yuhan (FZU: Fuzhou University)
Last. Juan Liao (FZU: Fuzhou University)
view all 6 authors...
Abstract null null Elastic–porous sandwich structure with entangled metallic wire mesh (EMWM) is of particular interest, and is a complex and novel rigid–flexible heterogeneous material. This study introduced the fabrication technology and explored the shear failure behaviours of elastic–porous sandwich structures. The elastic–porous sandwich structure with different configurations such as the side structures, the core relative density and the thickness ratio of core/face-sheet on the failure be...
Source
#1Pedro M. A. Areias (Instituto Superior Técnico)H-Index: 37
#2F.J.M.Q. de Melo (University of Porto)H-Index: 8
Last. J.N. Sikta (University of Évora)
view all 3 authors...
Abstract null null Thin-walled structures impose zero-stress constraints at free faces. These are in general nonlinear functions of strain and, in the elasto-plastic case, non-smooth. Under these circumstances, the conjugate strain components become constitutive unknowns. By iterating for the elastic Cauchy–Green tensor in the null null null null 6 null − null null null dimensional space, we directly obtain a system that includes the zero-stress constraints. Coupling of the stress and strain con...
Source
#1Jie Zhou (NPU: Northwestern Polytechnical University)
#2Zhen Wu (NPU: Northwestern Polytechnical University)H-Index: 1
Last. Han HanH-Index: 1
view all 7 authors...
Abstract null null Composite curved shells are widely utilized as structural components in aerospace engineering. To inspire the potentiality of such structure, it is very necessary to well understand mechanical behaviors of composite curved shells. Compared to the composite plates, it is more difficult to predict accurately interlaminar stresses of composite curved shells. Therefore, this paper attempts to propose an alternative triangular composite shell element in terms of the Reddy-type glob...
Source
Source
12345678910
Top fields of study
This website uses cookies.
We use cookies to improve your online experience. By continuing to use our website we assume you agree to the placement of these cookies.
To learn more, you can find in our Privacy Policy.