Thermo-mechanical progressive analysis on multiple delaminations in composite laminates

被引:5
|
作者
Li, D. H. [1 ]
Yun, Z. X. [1 ]
机构
[1] Civil Aviat Univ China, Coll Aeronaut Engn, Tianjin 300300, Peoples R China
关键词
Composite laminated plates; Extended layerwise method; Thermo-mechanical cohesive zone model; Delamination; Traction-separation law; EXTENDED LAYERWISE METHOD; COHESIVE ZONE MODEL; THERMAL BUCKLING ANALYSIS; THERMOELASTIC ANALYSIS; FINITE-ELEMENTS; CRACK-GROWTH; PLATES; FRACTURE; SIMULATION; STRESSES;
D O I
10.1007/s00161-021-01073-5
中图分类号
O414.1 [热力学];
学科分类号
摘要
The multiple delaminations at different interfaces and their interactions should be described simultaneously in an accurate analysis approach of composite laminates under the multi-physics loading, but it is not studied thoroughly in the existing research works. A thermo-mechanical cohesive zone model is proposed to investigate the thermo-mechanical progressive growth of multiple delaminations in composite laminated plates. The multiple delaminations are simulated by the extended layerwise method (XLWM), and their thermo-mechanical progressive damage characterization is described by a discrete damage zone model (DDZM). A traction-separation law is employed to account for the heat flux transfer and mechanical load transfer across the delamination front. Several numerical examples of double cantilever beams and laminated plates are carried out to verify the proposed model for the contact and degradation problems. The thermo-mechanical progressive growth mechanism is also investigated for the multiple delaminations in composite laminated plates
引用
收藏
页码:341 / 366
页数:26
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