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Tensile-Compressive Asymmetric Mechanical Properties and Constitutive Model of HTPB Propellant

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成果类型:
期刊论文
作者:
Peng, Pai;Fan, Zijian;Yu, Peng;Shen, Zhibin
通讯作者:
Fan, ZJ
作者机构:
[Peng, Pai] Changsha Univ Sci & Technol, Sch Civil Engn, Changsha 410073, Peoples R China.
[Yu, Peng; Shen, Zhibin; Peng, Pai; Fan, Zijian] Natl Univ Def Technol, Coll Aerosp Sci & Engn, Changsha 410073, Peoples R China.
[Yu, Peng; Shen, Zhibin; Peng, Pai; Fan, Zijian] Hunan Key Lab Intelligent Planning & Simulat Aeros, Changsha 410073, Peoples R China.
通讯机构:
[Fan, ZJ ] N
Natl Univ Def Technol, Coll Aerosp Sci & Engn, Changsha 410073, Peoples R China.
Hunan Key Lab Intelligent Planning & Simulat Aeros, Changsha 410073, Peoples R China.
语种:
英文
关键词:
Particle-reinforced material;Solid propellant;Tension-compression asymmetry;Nonlinear viscoelasticity;Numerical simulation calculation
期刊:
Applied Composite Materials
ISSN:
0929-189X
年:
2025
页码:
1-14
基金类别:
National Natural Science Foundation of China [12372203]; National Natural Science Foundation of China
机构署名:
本校为第一机构
院系归属:
土木工程学院
摘要:
The solid propellant is a particle-reinforced material with significant tension-compression asymmetry. Based on the constant-speed tensile test, constant-speed compression test, and cross-sectional SEM scanning test, this study investigated the differences in the mechanical properties of the HTPB propellant under tensile and compressive loading and the underlying mechanisms. The results show that the tensile strength of HTPB propellant is much smaller than compressive strength. According to the SEM test results of the failure surface, the tensile mechanical properties of the propellant are mai...

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