首页|针刺复合材料层次化建模及弹性性能预测

针刺复合材料层次化建模及弹性性能预测

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针对针刺复合材料中网胎层等结构复杂导致难以划分周期性网格的问题,基于局部径向基点插值模型(LRPIM)发展了非周期性网格的周期性边界条件施加方法.开展X射线断层扫描试验并分析材料微观组织,提取出非针刺区域、针刺绕过区域和针刺穿过区域三种典型特征结构.考虑到针刺复合材料组成成分复杂的特点,提出了基于多特征结构的层次化建模方法,将复杂微观特征结构分解至单一材料相进行精细化建模,并按层次逐级均匀化以获取材料弹性性能.开展针刺复合材料力学性能试验,结果表明x方向拉伸模量和面内切变模量的预测误差分别为1.5%和6.4%,验证了所提建模方法的准确性.
Hierarchical modeling and elastic property prediction of the needled composite
In order to address the problem of complex structures such as random fiber layers in needled composites that make it difficult to assign periodic meshes,a periodic boundary condition imposition method for non-periodic meshes was developed based on the local radial point interpolation model(LRPIM).First,X-ray tomography tests were carried out to analyze the material microstructure,from which three typical characteristic structures of un-needling region,needling bypass region and needling through region were extracted.Subsequently,considering the complex composition of needled composites,a hierarchical modeling method based on multiple feature structures was proposed to decompose the complex microscopic feature structures into single material phases for refinement modeling,and homogenization by level was achieved to obtain the material's elastic properties.Finally,the mechanical properties tests of the needled composites were carried out.The results showed that the prediction errors of the x-direction tensile modulus and in-plane shear modulus were 1.5%and 6.4%,respectively,which verified the accuracy of the proposed modeling approach.

C/C-SiC compositeneedled compositemicrostructurehierarchical modelingperiodic boundary conditionselastic properties

刘昱、王荣桥、胡殿印、刘茜、庞生洋

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北京航空航天大学能源与动力工程学院,北京 102206

北京航空航天大学航空发动机研究院,北京 102206

北京航空航天大学航空发动机结构强度北京市重点实验室,北京 102206

北京航空航天大学中小型航空发动机联合研究中心,北京 102206

中国科学院金属研究所,沈阳 110016

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C/C-SiC复合材料 针刺复合材料 微观组织 层次化建模 周期性边界条件 弹性性能

国家自然科学基金国家自然科学基金国家自然科学基金

520220075210513852275142

2024

航空动力学报
中国航空学会

航空动力学报

CSTPCD北大核心
影响因子:0.59
ISSN:1000-8055
年,卷(期):2024.39(2)
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