Governed by: Ministry of Industry and Information Technology of the People's Republic of China
Sponsored by: Northwestern Polytechnical University  Chinese Society Aeronautics and Astronautics
Address: Aviation Building,Youyi Campus, Northwestern Polytechnical University
Influence of Initial Defects on Thermal Residual Stress of Plain Weave C/SiC Composites
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Affiliation:

Northwestern Polytechnical University

Clc Number:

V257;TB332/V257

Fund Project:

the National Key Research&Development Project of China(2016YFB0700503);National Natural Science Foundation(51772244,11072195)

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    Abstract:

    The thermal residual stress of C/SiC affects the service performance of the material. In order to explore the influence of initial defects on the thermal residual stress, the steady change temperature method and the finite element computational mechanics (FECM) method are used to determine the relationship with thermal residual stress and initial defects of plain weave C/SiC composites. The distribution characteristics of various initial defects of the material were measured and statistically analyzed by scanning electron microscopy (SEM) of the sample. The representative volume unit (RVE) and the fiber bundle RVE finite element model of the macroscopic material with initial defects were established to predict effective performance parameters and thermal residual stress of fiber bundle RVE, and obtain the quantitative relationship between various initial defects and thermal residual stress of macroscopic materials.

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baiguodong, tongxiaoyan, yaoleijiang. Influence of Initial Defects on Thermal Residual Stress of Plain Weave C/SiC Composites[J]. Advances in Aeronautical Science and Engineering,2020,11(3):332-337

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History
  • Received:October 10,2019
  • Revised:October 28,2019
  • Adopted:November 07,2019
  • Online: June 21,2020
  • Published: