Research on the constitutive equations of HTPB composite solid propellant with damage and aging

被引:0
|
作者
Yang, Jian-Hong [1 ]
Yu, Mao-Hong [1 ]
Hou, Gen-Liang [2 ]
Wang, You-Jun [2 ]
Lu, Qiu-Juan [2 ]
机构
[1] Dept. of Civil Eng., Xi'an Jiaotong Univ., Xi'an 710049, China
[2] Eng. Coll., Second Artillery, Xi'an 710025, China
来源
关键词
Aging of materials - Creep - Viscoelasticity;
D O I
暂无
中图分类号
学科分类号
摘要
Through heat aging experiment, AE experiment and creep experiment, the constitutive equations of HTPB composite propellant with damage and aging was presented. Compared with Schapery nonlinear constitutive equations, this equations are more simple and exact. The constitutive equations of HTPB composite propellant with damage and aging can be used to analyze the mechanical properties and explain the nonlinear characteristics of HTPB composite propellant.
引用
收藏
页码:509 / 512
相关论文
共 50 条
  • [31] Micro-CT Experimental Study on the Mesostructure of HTPB Composite Solid Propellant
    Li S.-Q.
    Wang G.
    Qiang H.-F.
    Wang X.-R.
    Wang Z.-J.
    Wang J.-X.
    Huozhayao Xuebao/Chinese Journal of Explosives and Propellants, 2021, 44 (03): : 387 - 393
  • [32] TG studies of a composite solid rocket propellant based on HTPB-binder
    Rocco, JAFF
    Lima, JES
    Frutuoso, AG
    Iha, K
    Ionashiro, M
    Matos, JR
    Suárez-Iha, MEV
    JOURNAL OF THERMAL ANALYSIS AND CALORIMETRY, 2004, 77 (03) : 803 - 813
  • [33] TG studies of a composite solid rocket propellant based on HTPB-binder
    J. A. F. F. Rocco
    J. E. S. Lima
    A. G. Frutuoso
    K. Iha
    M. Ionashiro
    J. R. Matos
    M. E. V Suárez-Iha
    Journal of Thermal Analysis and Calorimetry, 2004, 77 : 803 - 813
  • [34] A NONLINEAR VISCOELASTIC AND MICROMECHANICAL DAMAGE CONSTITUTIVE MODEL FOR SOLID PROPELLANT
    Gu, Zhixu
    Zheng, Jian
    Peng, Wei
    Tang, Xi'nan
    Yin, Junhui
    ADVANCED ENGINEERING MATERIALS III, PTS 1-3, 2013, 750-752 : 2196 - +
  • [35] Constitutive modeling of solid propellant materials with evolving microstructural damage
    Xu, F.
    Aravas, N.
    Sofronis, P.
    JOURNAL OF THE MECHANICS AND PHYSICS OF SOLIDS, 2008, 56 (05) : 2050 - 2073
  • [36] Mechanical properties and constitutive model of a composite solid propellant under the synergistic effects of accelerated aging time, pre-strain, and damage growth
    Wang, Jianjun
    Cheng, Jiming
    Lei, Ming
    Hu, Xueyao
    Wen, Lihua
    MECHANICS OF MATERIALS, 2020, 148
  • [37] Methods of Swanson constitutive model establishment for composite solid propellant
    Ning, Chao
    Qiang, Hongfu
    Wang, Guang
    FRONTIERS OF MANUFACTURING AND DESIGN SCIENCE IV, PTS 1-5, 2014, 496-500 : 476 - 480
  • [39] Aluminum agglomeration of AP/HTPB composite propellant
    Yuan, Jifei
    Liu, Jianzhong
    Zhou, Yunan
    Wang, Jianru
    Xv, Tuanwei
    ACTA ASTRONAUTICA, 2019, 156 : 14 - 22
  • [40] Investigation on A Viscoelastic Creep Damage Constitutive Model for HTPB Propellant and Its Application in Finite Element Analysis
    Zhang, Yanshen
    Qiang, Hongfu
    Wang, Xueren
    Wang, Zhejun
    Wang, Jiaxiang
    Cui, Huiru
    JOURNAL OF ELECTRICAL SYSTEMS, 2024, 20 (03) : 823 - 840