Chenyang Liu , Sheng Zhang , Xu Zhang , Chengqian Dong , Fang Wang , Xiguang Gao , Yingdong Song
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引用次数: 0
Abstract
Aerospace laminated composite structures often require thickness variations along one or more directions in order to satisfy weight and aerodynamic efficiency requirements. Thickness variation is achieved by introducing dropped plies at appropriate locations. However, the influence mechanism of the ply drop location has not been adequately elucidated. In this work, the effect of ply drop location on the mechanical properties of tapered laminates has been investigated by experiment and simulation. Three different ply-drop configurations of tapered laminates were subjected to quasi-static tensile tests. The main failure modes are delamination and ply damage. Delamination can significantly reduce the load-bearing capacity of the structure. The simulation results are in good agreement with the test results in terms of failure load, load–displacement response, and delamination regions. The results demonstrate that the ply drop location affects the order of occurrence of the main failure modes of tapered laminates and the propagation path of ply damage cracks, thereby influencing their mechanical properties.
期刊介绍:
The past few decades have seen outstanding advances in the use of composite materials in structural applications. There can be little doubt that, within engineering circles, composites have revolutionised traditional design concepts and made possible an unparalleled range of new and exciting possibilities as viable materials for construction. Composite Structures, an International Journal, disseminates knowledge between users, manufacturers, designers and researchers involved in structures or structural components manufactured using composite materials.
The journal publishes papers which contribute to knowledge in the use of composite materials in engineering structures. Papers deal with design, research and development studies, experimental investigations, theoretical analysis and fabrication techniques relevant to the application of composites in load-bearing components for assemblies, ranging from individual components such as plates and shells to complete composite structures.