This paper gives a simplified calculation method which solves equilibrium composition of the combustion products of compositepropellants.
本文介绍一种求解复合推进剂燃烧产物平衡成分的简化计算方法。
2
Based on an effective nonlinear viscoelastic model, the differential constitutive equation and strain-rate equation of solid compositepropellants are induced.
根据一个有效的非线性粘弹模型，导出复合固体推进剂微分形式本构方程和应变速率关系式。
3
The rheology is a useful tool to the study of the action mechanism of special functional agents for these complex systems such as composite solid propellants.