液体推进剂燃烧中流体动力不稳定性的脉动和细胞形式

Stephen B. Margolis
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引用次数: 9

摘要

一种扩展的液体推进剂燃烧朗道-列维奇模型,允许燃烧速率局部依赖于液气界面处的(气体)压力,不仅表现出归因于朗道的分类流体动力细胞不稳定性,而且还表现出与足够负压敏感性相关的脉动流体动力不稳定性。利用气液密度比p的小值的现实极限,可以通过在三种不同的波数状态中展开p的适当幂的所有质量来获得两个中性稳定边界的解析公式。特别推导了中性稳定边界Ap(k)的复合解析表达式,其中Ap为燃速的压力灵敏度,k为扰动的波数。对于细胞边界,研究结果明确地证明了重力对长波扰动的稳定作用,粘度(液体和气体)和表面张力对短波扰动的稳定作用,以及与Ap负值的中间波数相关的不稳定性,这是许多硝酸羟胺基液体推进剂在一定压力范围内的特征。相比之下,脉动流体动力稳定性边界对重力和表面张力效应不敏感,但对液体粘度的影响更敏感,因为对于后者的典型非零值,随着k的增加,脉动边界通过O(1)值减小到较大的负值。因此,预测液体推进剂燃烧是稳定的(即,隐蔽的和平面的),只有在负压灵敏度范围内,该范围位于细胞边界以下,存在足够小的负Ap值,并高于脉动边界,存在较大的负Ap值。
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On pulsating and cellular forms of hydrodynamic instability in liquid-propellant combustion

An extended Landau-Levich model of liquid-propellant combustion, one that allows for a local dependence of the burning rate on the (gas) pressure at the liquid-gas interface, exhibits not only the classival hydrodynamic cellular instability attributed to Landau but also a pulsating hydrodynamic instability associated with sufficiently negative pressure sensitivities. Exploiting the realistic limit of small values of the gas-to-liquid density ratio p, analytical formulas for both neutral sability boundaries may be obtained by expanding all quatities in appropriate powers of p in each of three distinguished wave-number regimes. In particular, composite analytical expressions are derived for the neutral stability boundaries Ap(k), where Ap is the pressure sensitivity of the burning rate and k is the wave number of the disturbance. For the cellular boundary, the results demonstrate explicitly the stabilizing effect of gravity on long-wave disturbances, the stabilizing effect of viscosity (both liquid and gas) and surface tension on short-wave perturbations, and the instability associated with intermediate wave numbers for negative values of Ap, which is characteristic of many hydroxylammoninum nitrate-based liquid propellants over certain pressure ranges. In contrast, the pulsating hydrodynamic stability boundary is insensitive to gravitational and surface-tension effects but is more sensitive to the effects of liquid viscosity because, for typical nonzero values of the latter, the pulsating boundary decreases to larger negative values of Ap as k increases through O(1) values. Thus, liquid-propellant combustion is predicted to be stable (that is, stealy and planar) only for a range of negative pressure sensitivities that lie below the cellular boundary that exists for sufficiently small negative values of Ap and above the pulsating boundary that exists for larger negative values of this parameter.

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