摘要
本文从粘弹性力学和复合材料力学理论说明,高填充(固体填充比φ>0.6)复合固体推进剂的初始粘弹性泊松比(0.01~10s)可能小子0.4,并讨论了粘弹性泊松比的测试方法,利用一种新方法得出了相应的实验数据。
Based on the viscoelastic mechanics and composite material mechanics, it is shown that the mittal viscoelastic Poisson' s ratio of high -filled composite propellant at 0. 01 ~10s may be less than 0. 4. The methods for measuring viscoelastic poisson' s ratio are discussed, and tested data are given by means of a new method suggested by the paper.
出处
《固体火箭技术》
EI
CAS
CSCD
1996年第4期46-50,共5页
Journal of Solid Rocket Technology
关键词
固体推进剂
泊松比
粘弹性理论
Solid propellant
Poisson ratio
Viscoelastic theory