宽温域宽应变率下丁羟四组元 HTPB 推进剂单轴压缩力学行为

Ran Wang, Yi Wu*, Long Bai, Yi Ming Zhang, Ning Fei Wang

*此作品的通讯作者

科研成果: 期刊稿件文章同行评审

摘要

In order to investigate the uniaxial compression mechanical behavior of four‐component HTPB propellant under wide temperature and wide strain rate ranges,uniaxial compressive mechanical performance tests of propellant were conducted under wide temperature and strain rate ranges based on universal material testing machine,high‐speed hydraulic servo testing machine,split Hopkinson pressure bar,and programmatic constant temperature and humidity testing machine. Stress‐strain curves of HTPB propellant under 10-4-103 s-1 at -40,-25,-10,20 ℃ and 50 ℃ were obtained,and the segmented uniaxial compression rate‐temperature constitutive relationship of HTPB propellant was established. The results indicate that the mechanical response of HTPB propellant exhibits a significant rate‐temperature correlation. At any strain rate,its mechanical response undergoes staged changes,i.e.,linear elastic stage‐nonlinear yield stage‐strain softening or strain hardening stage. Moreover,at high strain rates,the strain softening phenomenon after the nonlinear yield behavior is significantly weaker than that at low and medium strain rates. In addition,at high strain rates,as the temperature decreases,the changing rate of the stress‐strain curve gradually slows down;while at low and medium strain rates,the changing rate of the stress‐strain curve gradually increases as the temperature decreases. The mechanical strength of HTPB propellant increases significantly with decreasing temperature. When the temperature drops from 50 ℃ to -40 ℃ ,the maximum stress under wide strain rate increases from about 2.2-8.8 MPa to 11-22 MPa. The segmented rate‐temperature constitutive relationship constructed based on the experimental data has a better fitting effect at higher temperatures,which can better predict the mechanical behavior of HTPB propellant.

投稿的翻译标题Uniaxial Compressive Mechanical Behavior of Four⁃component HTPB Propellant under Wide Temperature and Strain Rate Range
源语言繁体中文
页(从-至)183-192
页数10
期刊Hanneng Cailiao/Chinese Journal of Energetic Materials
32
2
DOI
出版状态已出版 - 25 2月 2024

关键词

  • four‐component HTPB propellant
  • mechanical properties
  • uniaxial compression constitutive relationship
  • wide strain rate range
  • wide temperature range

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