Calculation of the characteristics of agglomerates during combustion of high-energy composite solid propellants

被引：1

作者：

Babuk, V. A. ^{[1
]}

Ivonenko, A. N. ^{[1
]}

Nnizyaev, A. A. ^{[1
]}

机构：

[1] Ustinov Baltika State Tech Univ Voenmekh, St Petersburg 190005, Russia

来源：

COMBUSTION EXPLOSION AND SHOCK WAVES | 2015年 / 51卷 / 05期

关键词：

agglomeration; combustion; propellant; condensation products; modeling; ALUMINUM AGGLOMERATION; BURNING SURFACE; ROCKET PROPELLANT; PRODUCTS; MODEL;

D O I：

10.1134/S0010508215050056

中图分类号：

O414.1 [热力学];

学科分类号：

摘要：

The problem of calculating the characteristics of the agglomerates formed during combustion of high-energy composite solid propellants is considered. It is shown that the mathematical models developed by the authors can be used for different propellant formulations to evaluate not only the dispersion of agglomerates, but also their quantity, chemical composition, and structure. The rules (algorithm) of using the developed models for a wide range of propellant formulations are determined. Modeling results for a number of propellant formulations based on various components are analyzed.

引用

页码：549 / 559

页数：11

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