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基于高精度2D-DIC的推进剂应力强度因子测量研究

王卓 俞立平 潘兵 崔辉如

固体火箭技术2026,Vol.49Issue(3):399-408,10.
固体火箭技术2026,Vol.49Issue(3):399-408,10.DOI:10.7673/j.issn.1006-2793.2026.03.009

基于高精度2D-DIC的推进剂应力强度因子测量研究

Propellant stress intensity factor measurement using high-accuracy 2D-DIC

王卓 1俞立平 1潘兵 1崔辉如2

作者信息

  • 1. 北京航空航天大学 航空科学与工程学院,北京 102200
  • 2. 陆军工程大学 国防工程学院,南京 210007||香港城市大学 机械工程系,香港 999077
  • 折叠

摘要

Abstract

The stress intensity factor(SIF)serves as a critical index to evaluate the structural integrity of cracked solid rocket motor propellant grain,particularly under ignition and pressurization loading.However,existing measurement methods for stress intensity factor of solid propellants primarily depend on indirect inference from macroscopic load data.Such methods are strongly affected by off-crack-tip interference and prone to systematic measurement errors.The high-precision two-dimensional digital image correlation(2D-DIC)method was adopted to capture the surface displacement field of the propellant specimens.Based on the analytical relationship between the crack-tip displacement field and the SIF,the crack-tip SIF of the propellant was calculated via the displacement extrapolation method.Furthermore,an effective calculation sector screening strategy was established,which takes the Mode Ⅱ stress intensity factor and the determination coefficient of linear fitting as dual criteria,based on which the fracture toughness of the HTPB propellant was evaluated.The results show that under loading,the propellant crack tip presents evident nonlinear deformation and localized micro-damage,resulting in a strong angular dependence of the extrapolated stress intensity factors.With the proposed screening strategy,an effective computational domain consistent with the crack-tip asymptotic theoretical solution was accurately determined.Within this optimized computational domain,the evaluated Mode Ⅰ stress intensity factors exhibit favorable repeatability and convergence stability.The critical fracture toughness of the tested HTPB propellant was experimentally measured to be 1.22 MPa·mm1/2.

关键词

HTPB推进剂/应力强度因子/2D-DIC/位移外推法/断裂韧性

Key words

HTPB propellant/stress intensity factor/2D-DIC/displacement extrapolation method/fracture toughness

分类

航空航天

引用本文复制引用

王卓,俞立平,潘兵,崔辉如..基于高精度2D-DIC的推进剂应力强度因子测量研究[J].固体火箭技术,2026,49(3):399-408,10.

基金项目

国家自然科学基金(12202496,12572204) (12202496,12572204)

香江学者计划(XJ2023015) (XJ2023015)

中国博士后科学基金资助项目(2022M723866). (2022M723866)

固体火箭技术

1006-2793

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