Free vibration behaviors of carbon fiber reinforced lattice-core sandwich cylinder

被引：98

作者：

Zhang, He ^{[1
]}

Sun, Fangfang ^{[1
]}

Fan, Hualin ^{[1
,2
]}

Chen, Haosen ^{[3
]}

Chen, Liming ^{[4
]}

Fang, Daining ^{[3
]}

机构：

[1] Hohai Univ, Coll Mech & Mat, Lab Struct Anal Def Engn & Equipment, Nanjing 210098, Jiangsu, Peoples R China

[2] Nanjing Univ Aeronaut & Astronaut, State Key Lab Mech & Control Mech Struct, Nanjing 210016, Jiangsu, Peoples R China

[3] Peking Univ, Coll Engn, Beijing 100871, Peoples R China

[4] Chongqing Univ, Sch Aerosp Engn, Chongqing Key Lab Heterogeneous Mat Mech, Chongqing 400030, Peoples R China

来源：

COMPOSITES SCIENCE AND TECHNOLOGY | 2014年 / 100卷

基金：

中国国家自然科学基金;

关键词：

Structural composites; Vibration; Sandwich structures; Filament winding;

D O I：

10.1016/j.compscitech.2014.05.030

中图分类号：

TB33 [复合材料];

学科分类号：

摘要：

To study mechanical behaviors of advanced carbon fiber reinforced composite (CFRC) sandwich cylinder with lattice cores, uni-axial compression and free vibration experiments were carried out. Load carrying capacity and local failure modes of the lattice-core sandwich cylinder (LSC) were revealed. Natural frequencies and vibration modes of CFRC LSC were revealed by experiments for the first time. For usual LSC in astronautic engineering, the first order vibration is in the plane of the cross section, turning from a circle to an oval. An equivalent method was proposed to predict the primary frequency and mode shape of the LSC, which is in excellent accordance with the experiment. Compared with grid stiffened cylinder (GSC), LSC of the same weight and dimension always has higher primary frequency, indicating that LSC is much stiffer and could be designed even lighter in astronautic applications. (C) 2014 Elsevier Ltd. All rights reserved.

引用

页码：26 / 33

页数：8

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