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  针对海绵橡胶的物理特性展开了准静态单轴压缩实验和分离式Hopkinson压杆动态压缩实验,得到海绵橡胶材料的应力-应变曲线,并对材料的应变率效应及材料的变形和破坏特性进行深入分析,在此基础上给出材料的动静态本构关系。结果表明:海绵橡胶材料在准静态加载下,应变大于0.3时,应力-应变曲线才开始偏离坐标轴,表现出非线性特征;在冲击载荷下,海绵橡胶的应变率效应并不明显。

Quasi?static uniaxial compression test and SHPB dynamic compression experiments were carried out on the physical properties of sponge rubber. Basic mechanical parameters and stress ? strain curve of the rubber were obtained through experiments. The static and dynamic constitutive model was presented based on necessary analysis of deformation behavior of materials,strain rate effects and destruction properties. The results show that under quasi?static loading with strain more than 0.3,stress?strain curve begins to be off the coordinate axis and appears the nonlinear property;strain rate effect is not obvious under shock loading with the increase of strain rate.

参考文献

[1] Mary C. Boyce;Ellen M. Arruda .Constitutive models of rubber elasticity: a review[J].Rubber Chemistry and Technology,2000(3):504-523.
[2] 郑明军,王文静,陈政南,吴利军.橡胶Mooney-Rivlin模型力学性能常数的确定[J].橡胶工业,2003(08):462-465.
[3] 王宝珍,胡时胜,周相荣.不同温度下橡胶的动态力学性能及本构模型研究[J].实验力学,2007(01):1-6.
[4] 刘锋,朱艳峰,李丽娟,黄小清.橡胶类材料大应变硬化的本构关系[J].华南理工大学学报(自然科学版),2006(04):9-12.
[5] 王锐,李世其,宋少云.隔振橡胶本构建模研究[J].振动与冲击,2007(01):77-79,83.
[6] 李宇明,郑坚,白鸿柏.金属橡胶材料的动态力学模型[J].材料研究学报,2003(05):499-504.
[7] Shim VPW.;Yang LM.;Lim CT.;Law PH. .A visco-hyperelastic constitutive model to characterize both tensile and compressive behavior of rubber[J].Journal of Applied Polymer Science,2004(1):523-531.
[8] Song B;Chen W N;Ming Cheng .Novel model of unixial strain-rate-dependent stress-strain behavior of ethylene-propylene-di-ene monomer rubber in compression or tension[J].Journal of Applied Polymer Science,2002,92:1553-1558.
[9] 高光发,李永池,李建阳,王道荣,蒋东.真空橡胶的动静态力学性能及本构关系的研究[J].功能材料,2010(09):1647-1649,1654.
[10] 王晓燕,卢芳云,林玉亮.SHPB实验中端面摩擦效应研究[J].爆炸与冲击,2006(02):134-139.
[11] 卢芳云,D.J.Frew,W.Chen.软材料的SHPB实验设计[J].爆炸与冲击,2002(01):15-19.
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