Compressive failure of woven fabric reinforced thermoplastic composites with an open-hole: An experimental and numerical study

被引:40
|
作者
Liu, Haibao [1 ]
Falzon, Brian G. [2 ]
Li, Shipeng [3 ]
Tan, Wei [4 ]
Liu, Jun [1 ]
Chai, Hui [5 ]
Blackman, Bamber R. K. [1 ]
Dear, John P. [1 ]
机构
[1] Imperial Coll London, Dept Mech Engn, South Kensington Campus, London SW7 2AZ, England
[2] Queens Univ Belfast, Adv Composites Res Grp, Sch Mech & Aerosp Engn, Ashby Bldg,Stranmillis Rd, Belfast BT9 5AH, Antrim, North Ireland
[3] Tianjin Univ, Key Lab Mech Theory & Equipment Design, Minist Educ, Tianjin 300350, Peoples R China
[4] Univ Cambridge, Dept Engn, Trumpington St, Cambridge CB2 1PZ, England
[5] First Aircraft Inst, 1 East Renmin Rd, Xian 710089, Shaanxi, Peoples R China
关键词
Woven composites; Combined Loading Compression (CLC); Damage mechanism; Finite Element Analysis (FEA); VELOCITY IMPACT DAMAGE; INTRALAMINAR FRACTURE-TOUGHNESS; MECHANICS APPROACH; MODELING IMPACT; PART II; BEHAVIOR; DELAMINATION; CURVE;
D O I
10.1016/j.compstruct.2019.01.070
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
This research presents a detailed experimental and numerical study on the compressive failure of woven fabric reinforced thermoplastic composites, with an open-hole and with a pinned open-hole. The experimental evaluations are performed on the composite specimens using the Combined Loading Compression (CLC) evaluation method. Experimental results, including load response and damage morphology, are obtained and analysed. A novel meso-scale damage model is developed, based on Continuum-Damage-Mechanics (CDM), for predicting damage in woven fabric reinforced composites. The developed model, which can capture fibre fracture and matrix cracking, as well as the nonlinear response within the woven composite materials, is employed to conduct virtual Combined Loading Compression (CLC) tests. Numerical simulation results are compared with the extracted experimental results for model validation. Good correlation is achieved between experimental and computational results for both the open-hole and the pinned open-hole, with a two-stage failure process being observed for the pinned open-hole.
引用
收藏
页码:108 / 117
页数:10
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