The influence of the Mache effect on combustion stability in a solid rocket motor

被引：1
|
作者：
Assovskii, IG [1 ]
Rashkovskii, SA
机构：
[1] NN Semenov Chem Phys Inst, Moscow 117977, Russia
[2] Moscow Inst Heat Engn, Moscow, Russia
来源：
COMBUSTION EXPLOSION AND SHOCK WAVES | 1998年 / 34卷 / 05期
关键词：
Combustion; Combustion Chamber; Combustion Surface; Solid Propellant; Rocket Motor;
D O I：
10.1007/BF02672675
中图分类号：
O414.1 [热力学];
学科分类号：
摘要：
A model of intrachamber combustion that takes into account the change in the temperature distribution in the fuel-combustion products when the pressure in the combustion chamber changes (Mache effect) is proposed. The influence of the Mache effect on the combustion stability in a solid rocket motor is investigated. It is shown that the Mache effect facilitates the appearance of low-frequency combustion instability and substantially reduces the range of parameters for stable operation of the rocket motor. A numerical study of the Mache effect is performed for typical values of the solid-propellant parameters.
引用
收藏
页码：528 / 533
页数：6
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