2019
DOI: 10.1080/09276440.2019.1707586
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Numerical evaluation on the influence of void defects and interphase on the thermal expansion coefficients of three-dimensional woven carbon/carbon composites

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Cited by 9 publications
(12 citation statements)
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“…The volume fraction of the orthotropic sphere is equal to the total volume fraction of the pores and fibers. The three-dimensional parametric FVDAM is used to establish the micro-scale model according to the micromechanical formula of composites [15]. The stress-strain relationship of the equivalent model and the equivalent stiffness 1 C can be calculated as follows:…”
Section: First Step-equivalence Of Pores and Random Micro-fibersmentioning
confidence: 99%
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“…The volume fraction of the orthotropic sphere is equal to the total volume fraction of the pores and fibers. The three-dimensional parametric FVDAM is used to establish the micro-scale model according to the micromechanical formula of composites [15]. The stress-strain relationship of the equivalent model and the equivalent stiffness 1 C can be calculated as follows:…”
Section: First Step-equivalence Of Pores and Random Micro-fibersmentioning
confidence: 99%
“…With respective to pore distributed in matrix and fiber bundle, Mekonnen et al [14] developed a finite element model, which demonstrated that elastic modulus gradually decreased Page2 when more pore defects were considered. Wei et al [15] investigated the influence of pore defects on thermal expansion coefficient of composites, and employed a finite element method to calculate their thermal expansion coefficients. In addition, Yang et al [16] established a Voronoi-structure model and evaluated equivalent shear modulus of composites with different pore shapes by finite element software.…”
Section: Introductionmentioning
confidence: 99%
“…The mismatch effect on the properties can also be estimated by adopting a micromechanics approach [ 21 , 22 ]. Many authors have used two-stage homogenization techniques to characterize the elastic and thermal behavior of composite materials in the presence of defects such as voids and debonding [ 23 , 24 ]. NFR composites’ mechanical properties are certainly influenced by non-cellulosic compounds such as hemicelluloses, lignin, waxes, pectin, etc.…”
Section: Introductionmentioning
confidence: 99%
“…The thermal protection structure in aircraft usually consists of several layers, such as the fiber, matrix and interphase layer of composites. 11,12…”
mentioning
confidence: 99%
“…The thermal protection structure in aircraft usually consists of several layers, such as the fiber, matrix and interphase layer of composites. 11,12 Normally, fiber rods pierce spread tow woven fabrics in the direction of thickness to construct a spread tow woven pierced fabric to improve interlayer performance. [13][14][15] Theoretical computation and finite element analysis (FEA) methods for predicting the thermal conductive behavior of textile reinforced composites have always been the focus of researchers.…”
mentioning
confidence: 99%