首页 | 本学科首页   官方微博 | 高级检索  
     

应变率和加载方式对HTPB推进剂力学性能及耗散特性的影响
引用本文:王玉峰,李高春,刘著卿,丁彪. 应变率和加载方式对HTPB推进剂力学性能及耗散特性的影响[J]. 含能材料, 2010, 18(4): 377-382. DOI: 10.3969/j.issn.1006-9941.2010.04.005
作者姓名:王玉峰  李高春  刘著卿  丁彪
作者单位:海军航空工程学院飞行器工程系,山东,烟台,264001
摘    要:为揭示机械载荷作用下HTPB推进剂的力学性能变化规律和破坏机理,利用单向拉伸法研究了应变率和加载方式对HTPB推进剂力学性能的影响,并基于耗散能方法分析了其在机械载荷作用下的耗散特性。结果表明,推进剂力学性能有明显的应变率相关性,抗拉强度、伸长率等与应变率的对数成线性增加关系;不同的应变控制也影响推进剂的力学性能;应变率和应变控制对推进剂试件的耗散能有较大的影响,耗散能与应变率的对数也成线性关系。

关 键 词:固体力学   HTPB推进剂; 力学性能; 应力-应变; 耗散能
收稿时间:2009-10-21
修稿时间:2009-12-14

Effect of Strain Rate and Loading on Mechanical Properties and Dissipated Energy for HTPB Propellant
WANG Yu-feng,DING Biao,LIU Zhu-qing and LI Gao-chun. Effect of Strain Rate and Loading on Mechanical Properties and Dissipated Energy for HTPB Propellant[J]. Chinese Journal of Energetic Materials, 2010, 18(4): 377-382. DOI: 10.3969/j.issn.1006-9941.2010.04.005
Authors:WANG Yu-feng  DING Biao  LIU Zhu-qing  LI Gao-chun
Affiliation:(Department of Airborne Vehicle Engineering, Naval Aeronautical and Astronautical University, Yantai 264001, China);(Department of Airborne Vehicle Engineering, Naval Aeronautical and Astronautical University, Yantai 264001, China);(Department of Airborne Vehicle Engineering, Naval Aeronautical and Astronautical University, Yantai 264001, China);(Department of Airborne Vehicle Engineering, Naval Aeronautical and Astronautical University, Yantai 264001, China)
Abstract:In order to understand the change of mechanical properties and damage mechanism of HTPB propellant, the influence of strain rate and loading on tensile properties of HTPB propellant was studied by means of uniaxial tension. The dissipated characteristics under mechanical loading was analyzed based on dissipated energy model. Results show that the mechanical properties and the dissipated energy of HTPB propellant were distinctly influenced by strain rate and by different control of strain. Tensile strength, elongation and dissipated energy increased linearly with the logarithm of strain rate. The results can be used as reference to research on properties of HTPB propellant in storage and use.
Keywords:solid mechanics   HTPB propellant   mechanical property   stress-strain   dissipated energy
本文献已被 CNKI 维普 万方数据 等数据库收录!
点击此处可从《含能材料》浏览原始摘要信息
点击此处可从《含能材料》下载全文
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号