考虑围压效应的N15固体推进剂本构模型

Jiye Zhang, Jinsheng Xu*, Feng Han, Shixin Wang

*此作品的通讯作者

科研成果: 期刊稿件文章同行评审

1 引用 (Scopus)

摘要

Mechanical properties of N15 solid propellant under different confining pressures were obtained by using the confining pressure test system. Result showed that the initial modulus of the propellant did not change with the confining pressure, but the maximum tensile strength, rupture strength, the maximum elongation and elongation at break increased with the increase of confining pressure; combined with propellant's mesoscopic structure and cross section analysis, the mechanical mechanism of confining pressure effect on the propellant was revealed preliminarily; as a result of the existence of confining pressure, the particle dewetting inside the propellant was reduced, the holes' propagation delayed due to the pressure, and its crack extension and germination was inhibited, which proved that the confining pressure had strengthening effect for propellant; according to the elastic-viscoelastic correspondence principle, a constitutive model considering the confining pressure effect was established for N15 propellant. The results showed that accuracy of the constitutive model was good, and it can describe the influence of confining pressure on the mechanical properties of N15 propellant accurately.

投稿的翻译标题Constitutive model of N15 solid propellant considering confining pressure effect
源语言繁体中文
页(从-至)1335-1344
页数10
期刊Hangkong Dongli Xuebao/Journal of Aerospace Power
36
6
DOI
出版状态已出版 - 6月 2021

关键词

  • Confining pressure environment
  • Confining pressure test system
  • Constitutive model
  • Mechanical properties
  • N15 propellant

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