简介概要

Mechanical Behavior and Failure Mechanisms of Carbon Fiber Composite Pyramidal Core Sandwich Panel after Thermal Exposure

来源期刊:JOURNAL OF MATERIALS SCIENCE TECHNOLOG2013年第9期

论文作者:Jiayi Liu Zhengong Zhou Linzhi Wu Li Ma

文章页码:846 - 854

摘    要:An attempt has been made here to evaluate the effect of thermal exposure on the mechanical behavior and failure mechanisms of carbon fiber composite sandwich panel with pyramidal truss core under axial compression.Analytical formulae for the collapse strength of composite sandwich panel after thermal exposure were derived.Axial compression tests of composite laminates and sandwich panels after thermal exposure were conducted at room temperature to assess the degradation caused by the thermal exposure.Experimental results showed that the failure of sandwich panel are not only temperature dependent,but are time dependent as well.The decrease in residual compressive strength is mainly attributed to the degradation of the matrix and the degradation of fibere-matrix interface,as well as the formation of cracks and pores when specimens are exposed to high temperature.The measured failure loads obtained in the experiments showed reasonable agreement with the analytical predictions.

详情信息展示

Mechanical Behavior and Failure Mechanisms of Carbon Fiber Composite Pyramidal Core Sandwich Panel after Thermal Exposure

Jiayi Liu,Zhengong Zhou,Linzhi Wu,Li Ma

Center for Composite Materials and Structures,Harbin Institute of Technology

摘 要:An attempt has been made here to evaluate the effect of thermal exposure on the mechanical behavior and failure mechanisms of carbon fiber composite sandwich panel with pyramidal truss core under axial compression.Analytical formulae for the collapse strength of composite sandwich panel after thermal exposure were derived.Axial compression tests of composite laminates and sandwich panels after thermal exposure were conducted at room temperature to assess the degradation caused by the thermal exposure.Experimental results showed that the failure of sandwich panel are not only temperature dependent,but are time dependent as well.The decrease in residual compressive strength is mainly attributed to the degradation of the matrix and the degradation of fibere-matrix interface,as well as the formation of cracks and pores when specimens are exposed to high temperature.The measured failure loads obtained in the experiments showed reasonable agreement with the analytical predictions.

关键词:

<上一页 1 下一页 >

有色金属在线官网  |   会议  |   在线投稿  |   购买纸书  |   科技图书馆

中南大学出版社 技术支持 版权声明   电话:0731-88830515 88830516   传真:0731-88710482   Email:administrator@cnnmol.com

互联网出版许可证:(署)网出证(京)字第342号   京ICP备17050991号-6      京公网安备11010802042557号