海军航空工程学院学报2011，Vol.26Issue(3)：309-313,5.
定应力幅值往复拉伸过程中推进剂的损伤扩展
Damage Characteristic of Propellant in the Process of Cyclic Tension Under Certain Stress Amplitude
刘著卿 1李高春 1丁彪 1李建2
作者信息
- 1. 海军航空工程学院飞行器工程系
- 2. 91980部队,山东,烟台,264001
- 折叠
摘要
Abstract
By the cyclic tensile test of composite solid propellant under different stress, the change rules of cyclic tensile curve, characteristic strain and dissipated energy in the process of loading were found, and the damage characteristic of composite solid propellant was analyzed. The results showed that the change rules of dissipated energy in the process of cyclic tension reflected the different damage mode of the propellant at different tensile strain, the main portion of the dissipated energy was supplied by the matrix, and the amplitude of stress and the logarithm of the cyclic tensile life had good linear relation.关键词
复合固体推进剂/往复拉伸/损伤扩展/耗散能Key words
composite solid propellant/ cyclic tension/ damage characteristic/ dissipated energy分类
航空航天引用本文复制引用
刘著卿,李高春,丁彪,李建..定应力幅值往复拉伸过程中推进剂的损伤扩展[J].海军航空工程学院学报,2011,26(3):309-313,5.
