摘要
简述了体积松弛模量K(t)与体积蠕变柔量B(t)之问的精确与近似转换关系,提出一种根据实测B(t)诊断K(t)的数值积分算法。通过体积蠕变实验给出一种下羟固体推进剂的B(t)和K(t)的实测与转换计算结果。
he exact and approximate inversion relationships between volume relaxation modulus K (t) and volume creep compliance R (t) are summarized.A numerical integration algorithm for solving K (t) from expermetal B (t) is presented.The experimental and calculated results of D (t) and K (t) are gi on for a HTPBsolid propellant on the basis of the volume creep experiments.
出处
《固体火箭技术》
EI
CAS
CSCD
1995年第1期60-63,共4页
Journal of Solid Rocket Technology
关键词
粘弹性
复合推进剂
体积弹性模量
蠕变
Terms
Viscoelastieity
Composite propellant Bulk modulus
Creep