Meso-crack evolution based constitutive model for concrete material under compression

被引:4
|
作者
Ren, Darui [1 ]
Liu, Xiaoli [1 ]
Cui, Baoqing [1 ,2 ]
Wang, Enzhi [1 ]
Ma, Qing [1 ]
Yan, Fayuan [1 ]
Xie, Weiqiang [1 ,3 ]
机构
[1] Tsinghua Univ, State Key Lab Hydrosci & Engn, Beijing 100084, Peoples R China
[2] Renmin Univ China, New Campus Construct Off, Beijing 100084, Peoples R China
[3] Yunlong Lake Lab Deep Underground Sci & Engn, Xuzhou 221116, Peoples R China
基金
中国国家自然科学基金;
关键词
Concrete; Wings-crack; Constitutive model; Mesoscale crack evolution; QUASI-BRITTLE MATERIALS; COARSE AGGREGATE SIZE; DAMAGE MODEL; ELASTIC PROPERTIES; BEHAVIOR; STRESS; SOLIDS; MICROMECHANICS; COMPOSITES; MECHANICS;
D O I
10.1016/j.compositesb.2023.110956
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
Concrete is a heterogeneous material at the mesoscale, with components that significantly influence its macroscale behavior. In this study, a wings-crack based model which could reflect the influence of coarse aggregate and cement mortar on stress-strain relationship of concrete under compression was proposed. The wings-crack was assumed to be the form of a sliding main crack with two asymmetrically distributed type I wing cracks. The size of the main crack was considered to follow a random distribution based on the coarse aggregate sieve curve, while the propagation of wing cracks was controlled by the type I fracture toughness of the cement mortar. By incorporating the wings-crack model into an evolution square, crack interaction as concrete approached failure was considered by the difference between the evolution square size and the wing crack length. The influence of coarse aggregate gradation, coarse aggregate content, and water-to-cement ratio on the stress-strain relationship was successfully reproduced through an appropriate parameter determination method, and good agreement with experimental results were achieved. Additionally, the crack evolution process was also studied by the active wings-crack number, the velocity of main crack slip, and the speed of wing crack propagation extracted from the model. Comparisons with acoustic emission (short for AE) data revealed similar trends between the model and experimental observations.
引用
收藏
页数:28
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