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Nonlinear Intrinsic Instability of Solid Propellant Combustion Including Gas-Phase Thermal Inertia

机译:固体推进剂燃烧的非线性固有不稳定性,包括气相热惯性

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摘要

The problem of homogeneous solid propellant combustion instability is studied with a one-dimen- sional flame model, including the effects of gas-phase thermal inertia and nonlinearity. Computa- tional results presented in this paper show nonlinear instabilities inherent in the equations, due to which periodic burning is found even under steady ambient conditions such as pressure. The stability boundary is obtained in terms of Denison-Baum parameters. It is found that inclusion of gas-phase thermal inertia stabilizes the combustion. Also, the effect of a distributed heat release in the gas phase, compared to the flame sheet model, is to destabilize the burning.
机译:用一维火焰模型研究了均匀固体推进剂燃烧不稳定性的问题,其中包括气相热惯性和非线性的影响。本文介绍的计算结果表明了方程固有的非线性不稳定性,因此即使在稳定的环境条件下(例如压力)也可以发现周期性燃烧。根据Denison-Baum参数获得稳定性边界。发现包含气相热惯性使燃烧稳定。而且,与火焰片模型相比,气相中分布的热量释放的效果是使燃烧不稳定。

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