composite solid propellants 复合固体推进剂
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This paper gives a simplified calculation method which solves equilibrium composition of the combustion products of composite propellants.
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。
The BDP steady burning model is revised in this paper and the revised BDP model is used in the prediction of steady burning rates of composite propellants.
本文对BDP稳态燃烧模型进行了必要修正，并用于预估推进剂稳态燃速。
Based on an effective nonlinear viscoelastic model, the differential constitutive equation and strain-rate equation of solid composite propellants 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。
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