TY - JOUR
T1 - Effective property prediction and experiment test for fiber tow composites
AU - Zhang, Hongji
AU - Shi, Yaoyao
AU - Tang, Hong
AU - Chen, Liuding
AU - Zhao, Pan
AU - Kang, Chao
N1 - Publisher Copyright:
© 2016, BUAA Culture Media Group Ltd. All right reserved.
PY - 2016/8/1
Y1 - 2016/8/1
N2 - According to the value of geometrical structure parameters and determined geometrical structure size of representative volume element (RVE) model of the fiber tow composites, finite element software MSC. Patran/Nastran as a platform to establish RVE finite element models of fiber tow composite and corresponding manufacturing defects were also implemented into the models. Grid element deletion method was utilized to implement all types of manufacturing defects. When crack-like manufacturing defects implemented into the RVE models, the crack width was obtained by moving the two opposite surfaces of the elements at the both sides of offset crack. The real morphologies of void-like manufacturing defects should be simulated as much as possible. According to material property parameter definitions of mechanics of composites and basic theories of micro-mechanics, the finite element computational micro-mechanics (FECM) methods to predict effective elastic properties and effective thermal expansion properties of composites were derived. Based on FECM methods, elastic constants and effective thermal expansion coefficients without manufacturing defects, containing a single manufacturing defect and containing all types of manufacturing defects were respectively predicted. The results show that the presence of all manufacturing defects will reduce elastic modulus and shear modulus, while Poisson's ratios and coefficients of thermal expansions may increase or decrease. Through comparison with the experimental test results, numerical prediction results are generally a little larger than experiment test results, but the overall effect is ideal. Wherein, the maximum relative error is 6.04%.
AB - According to the value of geometrical structure parameters and determined geometrical structure size of representative volume element (RVE) model of the fiber tow composites, finite element software MSC. Patran/Nastran as a platform to establish RVE finite element models of fiber tow composite and corresponding manufacturing defects were also implemented into the models. Grid element deletion method was utilized to implement all types of manufacturing defects. When crack-like manufacturing defects implemented into the RVE models, the crack width was obtained by moving the two opposite surfaces of the elements at the both sides of offset crack. The real morphologies of void-like manufacturing defects should be simulated as much as possible. According to material property parameter definitions of mechanics of composites and basic theories of micro-mechanics, the finite element computational micro-mechanics (FECM) methods to predict effective elastic properties and effective thermal expansion properties of composites were derived. Based on FECM methods, elastic constants and effective thermal expansion coefficients without manufacturing defects, containing a single manufacturing defect and containing all types of manufacturing defects were respectively predicted. The results show that the presence of all manufacturing defects will reduce elastic modulus and shear modulus, while Poisson's ratios and coefficients of thermal expansions may increase or decrease. Through comparison with the experimental test results, numerical prediction results are generally a little larger than experiment test results, but the overall effect is ideal. Wherein, the maximum relative error is 6.04%.
KW - Composites
KW - Effective property prediction
KW - Finite element computational micro-mechanics method
KW - Homogenization theory
KW - Manufacturing defects
UR - http://www.scopus.com/inward/record.url?scp=84983249768&partnerID=8YFLogxK
U2 - 10.13801/j.cnki.fhclxb.20151106.001
DO - 10.13801/j.cnki.fhclxb.20151106.001
M3 - 文章
AN - SCOPUS:84983249768
SN - 1000-3851
VL - 33
SP - 1819
EP - 1829
JO - Fuhe Cailiao Xuebao/Acta Materiae Compositae Sinica
JF - Fuhe Cailiao Xuebao/Acta Materiae Compositae Sinica
IS - 8
ER -