Modeling and evaluation of dynamic degradation behaviours of carbon fibre-reinforced epoxy composite shells

被引:11
作者
Li, Hui [1 ,2 ]
Lv, Haiyu [1 ]
Zhang, Tinan [1 ]
Han, Qingkai [1 ]
Liu, Jinguo [2 ]
Xiong, Jian [3 ]
Guan, Zhongwei [4 ]
机构
[1] Northeastern Univ, Sch Mech Engn & Automat, Shenyang 110819, Peoples R China
[2] Chinese Acad Sci, Shenyang Inst Automat, State Key Lab Robot, Shenyang 110016, Peoples R China
[3] Harbin Inst Technol, Ctr Composite Mat & Struct, Harbin 150001, Peoples R China
[4] Univ Liverpool, Sch Engn, Brownlow St, Liverpool L69 3GQ, England
基金
中国国家自然科学基金;
关键词
Carbon fibres; Composite shell; Environmental degradation; Dynamic degradation; Degradation model; GRADED CYLINDRICAL-SHELLS; THERMAL-DEGRADATION; NONLINEAR VIBRATION; TEMPERATURE; PLATES;
D O I
10.1016/j.apm.2021.11.015
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
In this study, a segmented degradation model was established for the first time to pre-dict and evaluate the dynamic degradation characteristics of carbon fibre-reinforced epoxy composite (CFRC) shells accurately by considering temperature variations during heating, maintenance, and cooling. The model is based on the Reddy's high-order shear deforma-tion theory, complex modulus method, and coefficient fitting approach. First, explicit ex-pressions of material parameters and thermal expansion coefficients (TECs) in different thermal degradation stages were proposed, followed by the derivation of the differential equations to solve the structural dynamic degradation characteristics. Moreover, an iden-tification method for the fitting coefficients of the CFRC material was described, which is based on experimental tests and iterative calculations of elastic moduli, loss factors, and TECs at different degradation time points in different thermal degradation stages. Finally, the natural frequencies, damping ratios, and time-domain responses were measured using a novel testing system for the dynamic degradation of specimens subjected to a pulse exci-tation load to validate the developed model. Theoretical and experimental results indicate that the natural frequencies decreased as the degradation time increases at the heating-up and temperature maintenance stages, whereas they increased at the cooling stage. How-ever, an uptrend in the damping and response behaviours was observed in the first two stages, whereas a downtrend was recognized at the cooling stage. (c) 2021 Elsevier Inc. All rights reserved.
引用
收藏
页码:21 / 33
页数:13
相关论文
共 37 条
[1]   Evaluation of thermal ageing of a carbon fibre reinforced bismalemide [J].
Akay, M. ;
Spratt, G. R. .
COMPOSITES SCIENCE AND TECHNOLOGY, 2008, 68 (15-16) :3081-3086
[2]   Investigation of thermal degradation behavior of polymeric composites: prediction of thermal cycling effect from isothermal data [J].
Chung, K ;
Seferis, JC ;
Nam, JD .
COMPOSITES PART A-APPLIED SCIENCE AND MANUFACTURING, 2000, 31 (09) :945-957
[3]   Variational Mode Decomposition [J].
Dragomiretskiy, Konstantin ;
Zosso, Dominique .
IEEE TRANSACTIONS ON SIGNAL PROCESSING, 2014, 62 (03) :531-544
[4]   Nonlinear resonance behavior of functionally graded cylindrical shells in thermal environments [J].
Du, Changcheng ;
Li, Yinghui .
COMPOSITE STRUCTURES, 2013, 102 :164-174
[6]  
Guenab F, 2008, J ACOUST SOC AM, V123, P3396
[7]   DEGRADATION OF MECHANICAL-PROPERTIES OF ADVANCED COMPOSITES EXPOSED TO AIRCRAFT ENVIRONMENT [J].
HORN, WJ ;
SHAIKH, FM ;
SOEGANTO, A .
AIAA JOURNAL, 1989, 27 (10) :1399-1405
[8]   Criticality of degradation in composite materials subjected to cyclic loading [J].
Kahirdeh, Ali ;
Khonsari, M. M. .
COMPOSITES PART B-ENGINEERING, 2014, 61 :375-382
[9]   Buckling and post-buckling responses of smart doubly curved composite shallow shells embedded in SMA fiber under hygro-thermal loading [J].
Karimiasl, Mahsa ;
Ebrahimi, Farzad ;
Akgoz, Bekir .
COMPOSITE STRUCTURES, 2019, 223
[10]   Strength degradation and stress analysis of composite plates with circular, square and rectangular notches using digital image correlation [J].
Khechai, A. ;
Tati, A. ;
Guerira, B. ;
Guettala, A. ;
Mohite, P. M. .
COMPOSITE STRUCTURES, 2018, 185 :699-715